WorldWideScience

Sample records for large civil aircraft

  1. Aeroservoelastic model based active control for large civil aircraft

    Institute of Scientific and Technical Information of China (English)

    2010-01-01

    A modeling and control approach for an advanced configured large civil aircraft with aeroservoelasticity via the LQG method and control allocation is presented.Mathematical models and implementation issues for the multi-input/multi-output(MIMO) aeroservoelastic system simulation developed for a flexible wing with multi control surfaces are described.A fuzzy logic based optimization approach is employed to solve the constrained control allocation problem via intelligently adjusting the components of output vector and find a proper vector in the attainable moment set(AMS) autonomously.The basic idea is to minimize the L2 norm of error between the desired moment and achievable moment using the designing freedom provided by redundantly allocated actuators and control surfaces.Considering the constraints of control surfaces,in order to obtain acceptable performance of aircraft such as stability and maneuverability,the fuzzy weights are updated by the learning algorithm,which makes the closed-loop system self-adaptation.Finally,an application example of flight control designing for the advanced civil aircraft is discussed as a demonstration.The studies we have performed showed that the advanced configured large civil aircraft has good performance with the proper designed control law designed via the proposed approach.The gust alleviation and flutter suppression are applied with the synergetic effects of elevator,ailerons,equivalent rudders and flaps.The results show good closed loop performance and meet the requirement of constraint of control surfaces.

  2. Information fusion based optimal control for large civil aircraft system.

    Science.gov (United States)

    Zhen, Ziyang; Jiang, Ju; Wang, Xinhua; Gao, Chen

    2015-03-01

    Wind disturbance has a great influence on landing security of Large Civil Aircraft. Through simulation research and engineering experience, it can be found that PID control is not good enough to solve the problem of restraining the wind disturbance. This paper focuses on anti-wind attitude control for Large Civil Aircraft in landing phase. In order to improve the riding comfort and the flight security, an information fusion based optimal control strategy is presented to restrain the wind in landing phase for maintaining attitudes and airspeed. Data of Boeing707 is used to establish a nonlinear mode with total variables of Large Civil Aircraft, and then two linear models are obtained which are divided into longitudinal and lateral equations. Based on engineering experience, the longitudinal channel adopts PID control and C inner control to keep longitudinal attitude constant, and applies autothrottle system for keeping airspeed constant, while an information fusion based optimal regulator in the lateral control channel is designed to achieve lateral attitude holding. According to information fusion estimation, by fusing hard constraint information of system dynamic equations and the soft constraint information of performance index function, optimal estimation of the control sequence is derived. Based on this, an information fusion state regulator is deduced for discrete time linear system with disturbance. The simulation results of nonlinear model of aircraft indicate that the information fusion optimal control is better than traditional PID control, LQR control and LQR control with integral action, in anti-wind disturbance performance in the landing phase. Copyright © 2014 ISA. Published by Elsevier Ltd. All rights reserved.

  3. Active fault-tolerant control strategy of large civil aircraft under elevator failures

    Directory of Open Access Journals (Sweden)

    Wang Xingjian

    2015-12-01

    Full Text Available Aircraft longitudinal control is the most important actuation system and its failures would lead to catastrophic accident of aircraft. This paper proposes an active fault-tolerant control (AFTC strategy for civil aircraft with different numbers of faulty elevators. In order to improve the fault-tolerant flight control system performance and effective utilization of the control surface, trimmable horizontal stabilizer (THS is considered to generate the extra pitch moment. A suitable switching mechanism with performance improvement coefficient is proposed to determine when it is worthwhile to utilize THS. Furthermore, AFTC strategy is detailed by using model following technique and the proposed THS switching mechanism. The basic fault-tolerant controller is designed to guarantee longitudinal control system stability and acceptable performance degradation under partial elevators failure. The proposed AFTC is applied to Boeing 747-200 numerical model and simulation results validate the effectiveness of the proposed AFTC approach.

  4. Active fault-tolerant control strategy of large civil aircraft under elevator failures

    Institute of Scientific and Technical Information of China (English)

    Wang Xingjian; Wang Shaoping; Yang Zhongwei; Zhang Chao

    2015-01-01

    Aircraft longitudinal control is the most important actuation system and its failures would lead to catastrophic accident of aircraft. This paper proposes an active fault-tolerant control (AFTC) strategy for civil aircraft with different numbers of faulty elevators. In order to improve the fault-tolerant flight control system performance and effective utilization of the control surface, trim-mable horizontal stabilizer (THS) is considered to generate the extra pitch moment. A suitable switching mechanism with performance improvement coefficient is proposed to determine when it is worthwhile to utilize THS. Furthermore, AFTC strategy is detailed by using model following technique and the proposed THS switching mechanism. The basic fault-tolerant controller is designed to guarantee longitudinal control system stability and acceptable performance degradation under partial elevators failure. The proposed AFTC is applied to Boeing 747-200 numerical model and simulation results validate the effectiveness of the proposed AFTC approach.

  5. 14 CFR 375.11 - Other foreign civil aircraft.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 4 2010-01-01 2010-01-01 false Other foreign civil aircraft. 375.11... PROCEEDINGS) SPECIAL REGULATIONS NAVIGATION OF FOREIGN CIVIL AIRCRAFT WITHIN THE UNITED STATES Authorization § 375.11 Other foreign civil aircraft. A foreign civil aircraft other than those referred to in § 375.10...

  6. Perspectives of civil aircraft avionics development

    Directory of Open Access Journals (Sweden)

    А. В. Наумов

    1999-05-01

    Full Text Available Considered are main directions for civil avionics development. General requirements for airborne equipment functions. Analysis of airborne avionics selection per architecture and economical effectiveness in made. Proposed is the necessity of new approach to integrated avionics complex design, first of all, on basis of mathematical method for aircraft equipment and technical characteristics definition

  7. Analyses on Large Civil Aircraft Flight Control Actuator System%大型民用飞机新型飞控作动系统浅析

    Institute of Scientific and Technical Information of China (English)

    沈磊

    2012-01-01

    通过分析对比当代大型民用飞机典型作动系统的组成、工作原理和相关技术的优缺点,结合实际工作经验和相关工程参数,探讨了目前可用于新一代单通道民用运输机飞控作动系统的功率电传技术和分布式控制技术的应用前景.在此基础上,提出了一种有发展前景的基于电传技术的新型作动系统架构,通过对该新型作动系统在提升安全性、系统减重和提高通用扩展性方面的分析,认为在单通道民用运输机上采用该新型作动系统具有一定的技术优势.该新型作动系统的架构设计具有实际的工程应用价值.%Based on analysis of contemporary large civil aircraft typical actuator system composition, working principle and related technologies, it proposes the application prospect of the power telex technology and distributed control technology in a new generation of single channel civil transport aircraft flight control actuator system. It establishes the new actuator system architecture based on the telex technology, describes the characteristics of the actuator system in improved security, optimization weight and the general scalability aspects. This new type of actuator system architecture has the actual engineering application value.

  8. The Study of Large Civil Aircraft Flight Control System Design Philosophy%大型民用飞机飞控系统设计理念研究

    Institute of Scientific and Technical Information of China (English)

    谢殿煌

    2015-01-01

    Design philosophy shall be an idea which will be built before project starts to launch. As the flight control system’s top level input, it will directly affect the design of control handling device, system architecture, control law architecture and so on. Civil aircraft flight control system’s design philosophy was studied from the view of methodology. Lifecycle, philosophy characteristics and strategic essence were erected, the influence factors were analyzed importantly, architecture and evaluation method were set up, and the relative database between aircraft accidents and design philosophy were developed, provided aircraft manufacturers to define the flight control system’s design philosophy for the theoretical method direction and technical basis.%飞控系统设计理念是大型民用飞机飞控系统设计的顶层输入,直接影响着飞控操纵器件、系统架构、控制律架构等设计。该文从方法论角度探索和研究了民用飞机飞控系统设计理念,重点分析了设计理念影响因素,建立了设计理念体系结构,提出了设计理念评估方法,建立了民机事故与设计理念的关系数据库,为民机制造商确立自己的民用飞机飞控系统设计理念提供了理论方法指导和技术基础。

  9. Direct carbon dioxide emissions from civil aircraft

    Science.gov (United States)

    Grote, Matt; Williams, Ian; Preston, John

    2014-10-01

    Global airlines consume over 5 million barrels of oil per day, and the resulting carbon dioxide (CO2) emitted by aircraft engines is of concern. This article provides a contemporary review of the literature associated with the measures available to the civil aviation industry for mitigating CO2 emissions from aircraft. The measures are addressed under two categories - policy and legal-related measures, and technological and operational measures. Results of the review are used to develop several insights into the challenges faced. The analysis shows that forecasts for strong growth in air-traffic will result in civil aviation becoming an increasingly significant contributor to anthropogenic CO2 emissions. Some mitigation-measures can be left to market-forces as the key-driver for implementation because they directly reduce airlines' fuel consumption, and their impact on reducing fuel-costs will be welcomed by the industry. Other mitigation-measures cannot be left to market-forces. Speed of implementation and stringency of these measures will not be satisfactorily resolved unattended, and the current global regulatory-framework does not provide the necessary strength of stewardship. A global regulator with ‘teeth' needs to be established, but investing such a body with the appropriate level of authority requires securing an international agreement which history would suggest is going to be very difficult. If all mitigation-measures are successfully implemented, it is still likely that traffic growth-rates will continue to out-pace emissions reduction-rates. Therefore, to achieve an overall reduction in CO2 emissions, behaviour change will be necessary to reduce demand for air-travel. However, reducing demand will be strongly resisted by all stakeholders in the industry; and the ticket price-increases necessary to induce the required reduction in traffic growth-rates place a monetary-value on CO2 emissions of approximately 7-100 times greater than other common

  10. Perspectives on Unmanned Aircraft Classification for Civil Airworthiness Standards

    Science.gov (United States)

    Maddalon, Jeffrey M.; Hayhurst, Kelly J.; Koppen, Daniel M.; Upchurch, Jason M.; Morris, A. Terry; Verstynen, Harry A.

    2013-01-01

    The use of unmanned aircraft in the National Airspace System (NAS) has been characterized as the next great step forward in the evolution of civil aviation. Although use of unmanned aircraft systems (UAS) in military and public service operations is proliferating, civil use of UAS remains limited in the United States today. This report focuses on one particular regulatory challenge: classifying UAS to assign airworthiness standards. This paper provides observations related to how the current regulations for classifying manned aircraft could apply to UAS.

  11. Using Synthetic Kerosene in Civil Jet Aircraft

    NARCIS (Netherlands)

    Snijders, T.A.; Melkert, J.A.

    2008-01-01

    TU Delft in the Netherlands is performing research into the effects of the use of synthetic kerosene in aircraft. The research program consists of both desk research and tests. In the desk research gas turbine simulations will be combined with payload range performance calculations to show engine ef

  12. Using Synthetic Kerosene in Civil Jet Aircraft

    NARCIS (Netherlands)

    Snijders, T.A.; Melkert, J.A.

    2008-01-01

    TU Delft in the Netherlands is performing research into the effects of the use of synthetic kerosene in aircraft. The research program consists of both desk research and tests. In the desk research gas turbine simulations will be combined with payload range performance calculations to show engine

  13. Electromagnetic launch systems for civil aircraft assisted take-off

    Directory of Open Access Journals (Sweden)

    Bertola Luca

    2015-12-01

    Full Text Available This paper considers the feasibility of different technologies for an electromagnetic launcher to assist civil aircraft take-off. This method is investigated to reduce the power required from the engines during initial acceleration. Assisted launch has the potential of reducing the required runway length, reducing noise near airports and improving overall aircraft efficiency through reducing engine thrust requirements. The research compares two possible linear motor topologies which may be efficaciously used for this application. The comparison is made on results from both analytical and finite element analysis (FEA.

  14. MANPADS protection for civil aircraft using an expendable decoy

    Science.gov (United States)

    Walmsley, Roy H.; Friede, Johan; Millwood, Nicolas; Butters, Brian

    2009-09-01

    With the ever present threat of MANPADS throughout the world the protection of civil aircraft is a desirable capability that has special requirements in terms of certification, safety, logistics, affordability, environmental impact and exportability. The Civil Aircraft Missile Protection System (CAMPS), which includes the CIV-IR (infrared) leaf-based pyrophoric (not pyrotechnic) expendable countermeasure, is a system designed to meet these requirements. This paper presents the operating aspects of the decoy, including discussion of design features necessary to ensure safety both on the ground and in flight and assure successful deployment. The characteristics of the CIV-IR have been measured, both on static single leaves in the laboratory and on deployed packs in field tests and aircraft trials. These measured properties have been used in engagement modelling and simulation to assess the level of protection that can be afforded to commercial airliners against generation 1 and 2 MANPADS threats. Aircraft flight trials with ground based seekers have also been carried out to validate the modelling work. These combine to define the deployment patterns necessary for a successful seduction of the MANPAD.

  15. Hierarchical Colored Timed Petri Nets for Maintenance Process Modeling of Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    FU Cheng-cheng; SUN You-chao; LU Zhong

    2008-01-01

    Civil aircraft maintenance process simulation model is an effective method for analyzing the maintainability of a civil aircraft. First, we present the Hierarchical Colored Timed Petri Nets for maintenance process modeling of civil aircraft. Then, we expound a general method of civil aircraft maintenance activities, determine the maintenance level for decomposition, and propose the methods of describing logic of relations between the maintenance activities based on Petri Net. Finally, a time Colored Petri multi-level network modeling and simulation procedures and steps are given with the maintenance example of the landing gear burst tire of a certain type of aircraft. The feasibility of the method is proved by the example.

  16. METHOD IMPROVEMENT FOR DETERMINING THE TECHNICAL LEVEL OF CIVIL AIRCRAFT

    Directory of Open Access Journals (Sweden)

    2016-01-01

    Full Text Available Aircraft are high-tech engineering products which are characterized by a wide range of properties including the two most important groups that respectively characterize the efficiency and technical level.Improving the aircraft efficiency is an essential factor for air transport development, but the efficiency can not be fully describe the technical system, especially in forecasting and new technology requirements development. Aircraft de- signer must evaluate the prospects of a technical solution, but it’s not always possible to calculate the efficiency accuratelyat the design stage. The operator should be able to choose the most technically-advanced aircraft available in the market inorder not to let it grow obsolete quickly. This determines the need for non-economic evaluation of technical systems that can be done by assessment of their technical level.The technical level is a general index that includes a set of technical perfection indicators. Technical perfection is reflected in terms of material and energy intensity, in terms of ergonomics, safety, etc. and is achieved as a result of origi- nal design solutions, the use of new high-strength low-density materials, the introduction of advanced technological pro-cesses, calculation methods, verification, testing, etc.There is a tight connection between the product properties and its weight, because weight is the material reflection of these properties. Therefore, improvement of the product properties usually leads to an intense increase of its weight. To deal with this phenomenon is only possible with widely using scientific and technical progress results. In accordance with this, the technical perfection can be interpreted as a major component of quality that is created without the weight increase. This approach requires investment in research and testing new technical solutions.The method was developed to determine the technical level of civil long-haul aircraft which has been modified to

  17. The Research on Hidden Failures of Civil Aircraft

    Directory of Open Access Journals (Sweden)

    Lin Lie Shu

    2016-01-01

    Full Text Available The hidden failure is often appear on civil aircraft, and it is a big risk for normal safe operation. The reason for this failure is the instability of the resistance of the electrical contact. The study on electrical contact is applied science of the reliability, the contact resistance is an important parameter of the reliability of the electrical contact system. In this paper, It also Produces the latest research results from factors that affect contact resistance and contact resistance microscopic model, and then it produces the method of the calculating and measuring engineering about the contact resistance. Lastly, it is point out the future direction of the electrical contacts.

  18. Census of U.S. Civil Aircraft. Calendar Year 1981.

    Science.gov (United States)

    1981-12-31

    41 t 0 1 1 EL CAMINO 70-1 1 41 1 0 1 1 EL GRINGO 1 41 1 0 1 1 ELG O 1 41 1 0 1 1 EMERAUOE 3 41 1 0 5 5 A-101 US REGISTERED CIVIL AIRCRAFT BY...479 90 41 30 1 20 3 27 7 24 Blanco 18 7 6 2 3 Borden 1 1 Bosque 35 13 22 Bowie 122 49 48 9 14 1 Brazoria 318 133 106 20 5 1 5 5 41 Brazes 118 43 51

  19. Scaling Trajectories in Civil Aircraft (1913-1997)

    CERN Document Server

    Frenken, Koen

    2010-01-01

    Using entropy statistics we analyse scaling patterns in terms of changes in the ratios among product characteristics of 143 designs in civil aircraft. Two allegedly dominant designs, the piston propeller DC3 and the turbofan Boeing 707, are shown to have triggered a scaling trajectory at the level of the respective firms. Along these trajectories different variables have been scaled at different moments in time: this points to the versatility of a dominant design which allows a firm to react to a variety of user needs. Scaling at the level of the industry took off only after subsequently reengineered models were introduced, like the piston propeller Douglas DC4 and the turbofan Boeing 767. The two scaling trajectories in civil aircraft corresponding to the piston propeller and the turbofan paradigm can be compared with a single, less pronounced scaling trajectory in helicopter technology for which we have data during the period 1940-1996. Management and policy implications can be specified in terms of the pha...

  20. European activities in civil applications of drones: an overview of remotely piloted aircraft systems (RPAS)

    Science.gov (United States)

    Creutzburg, Reiner

    2015-05-01

    The aim of this paper is to give an overview of recent research, development and civil application of remotely piloted aircraft systems (RPAS) in Europe. It describes a European strategy for the development of civil applications of Remotely Piloted Aircraft Systems (RPAS) and reflects most of the contents of the European staff working document SWD(2012) 259 final.

  1. 14 CFR 375.10 - Certain foreign civil aircraft registered in ICAO member states.

    Science.gov (United States)

    2010-01-01

    ... in ICAO member states. 375.10 Section 375.10 Aeronautics and Space OFFICE OF THE SECRETARY... WITHIN THE UNITED STATES Authorization § 375.10 Certain foreign civil aircraft registered in ICAO member... of the International Civil Aviation Organization (ICAO), and registered in a State that at the...

  2. 14 CFR 91.711 - Special rules for foreign civil aircraft.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 2 2010-01-01 2010-01-01 false Special rules for foreign civil aircraft. 91.711 Section 91.711 Aeronautics and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) AIR TRAFFIC AND GENERAL OPERATING RULES GENERAL OPERATING AND FLIGHT RULES Foreign Aircraft Operations and Operations of...

  3. 基于 Logistics 模型的我国大飞机产业演化分析%Research on evolution of large civil aircraft industry based on logistics model

    Institute of Scientific and Technical Information of China (English)

    蔡敏

    2015-01-01

    This paper used industry evolution theory and Logistics model to simulate and ana-lyze of industrial growth trend to help to give some guide to the future development of China's large aircraft industry .%综合运用产业演化理论和Logistics模型仿真分析我国大飞机产业包括产业增长率,产值等行业指标的中长期演化过程,对于指导我国大飞机未来的发展有一定的前瞻性和指导意义。

  4. 大型民用飞机风挡鸟撞的适航分析与数值仿真%Airworthiness Analysis and Numerical Simulation of Bird Impact on Large Civil Aircraft Windshield

    Institute of Scientific and Technical Information of China (English)

    陈佳慧; 胡宇群; 陈川

    2016-01-01

    鸟撞一直都是航空安全的隐患,对此需要有相应的适航条款来表明民用飞机相关部件的抗鸟撞性能符合要求。针对风挡鸟撞问题现状,分析了目前民用飞机鸟撞适航验证的方法和手段,对比研究了不同鸟撞数值模型,通过计算机辅助设计软件建立了某型民用飞机风挡三维几何模型,采用显式非线性数值分析软件ANSYS/LS-DYNA进行风挡鸟撞过程的数值仿真分析,以期为大型民机风挡鸟撞适航验证提供更有效的方法和手段,提高适航验证工作效率,降低工作成本。%Bird strike is a major threat to aircraft windshields and need a certification requirement for a proven level of impact resistance. Apart from costly bird strike experiments, explicit numerical modeling techniques have been employed. This paper summarized the current airworthiness verification methods of bird strike,compared the different bird strike analysis models. With the help of Computer Aided Design software,established a three-dimensional geometric model of a certain type of civil aircraft windshield,and the simulation of the dynamic process of bird impacting windshield is run using the nonlinear explicit finite element code ANSYS/LS-DYNA. The solution of analysis presents the theoretical basis for the airworthi-ness certification methods of bird strike windshield,in hope of improving the efficiency of airworthiness ver-ification work and reducing the cost.

  5. 19 CFR 10.183 - Duty-free entry of civil aircraft, aircraft engines, ground flight simulators, parts, components...

    Science.gov (United States)

    2010-04-01

    ... ARTICLES CONDITIONALLY FREE, SUBJECT TO A REDUCED RATE, ETC. General Provisions Civil Aircraft § 10.183... merchandise under a provision for which the rate of duty “Free (C)” appears in the “Special” subcolumn of the... paragraph will be without interest, notwithstanding the provision of 19 U.S.C. 1505(c). (g) Verification...

  6. Economic Shocks and Civil Conflict: The Case of Large Floods

    OpenAIRE

    Ghimire, Ramesh; Ferreira, Susana

    2013-01-01

    We investigate the impact of large floods on the risk of civil conflict in a sample of 125 countries between 1985 and 2009. We control for endogeneity of floods and the potential spatial and temporal dependency of civil conflict. We find that floods increase the probability of conflict incidence through a negative impact on short-run GDP growth.

  7. Large Civil Tiltrotor Wake Hazard Assessment Tool Project

    Data.gov (United States)

    National Aeronautics and Space Administration — Both NASA and the FAA have identified large civil tiltrotors (LCTRs) as the most promising method for meeting FAA goals for extending future airport capacity,...

  8. A United Allocation Method of Spare Parts and Ground Maintenance Equipment for Civil Aircraft

    Directory of Open Access Journals (Sweden)

    Li Yongkai

    2017-01-01

    Full Text Available Aimed at multi-echelon inventory allocation problem with finite repair capacity for civil aircraft,a united planning method based on queuing theory and Vari-Metric model is presented to deploy the aircraft spare parts and ground maintenance equipment. Through the analysis of actual engineering, the effect of repair time is quantified by the number of maintenance equipment. On this basis, the available of fleet and the cost expense are selected as the objective and constraint respectively, marginal analysis method is set as the optimization, a new allocation scheme which was suit to civil aircraft’s maintenance resources is put forward. By applied examples analysis, it is shows that this method is reasonable and feasible.

  9. Research on Estimation of Take-off Weight of Large and Medium Civil Aircraft%大中型民用飞机起飞总重估算方法研究

    Institute of Scientific and Technical Information of China (English)

    班凯

    2012-01-01

    推导了基于发动机推力估算起飞总重和基于旅客座位数估算起飞总重的公式.通过多种大中型喷气式民用客机相关参数的统计值,建立起飞总重对相关参数的多元回归分析模型,通过显著性检验,说明模型是有效的,并据此建立了新的起飞总重估算公式.通过算例结果分析表明,新的起飞总重估算公式具有很高精度.在新机的方案设计阶段若能给定此公式所需的相关参数,可以计算得到相对合理的设计起飞总重值.%Formulas for estimating civil airplane take- off weight based on engine thrust and seating capacity are presented respectively. Through a variety of jet civil airplanes' statistical data of related parameters, the multiple regression analysis model of take- off weight with respect to the related parameters is built. The significance test shows that the model is effective, and a novel formula for estimating civil airplane take- off weight is established. The analysis of examples shows that the new formula is accurate. If the parameters required is given in the scheme design stage,then the relatively reasonable design take-off weight value can be obtained by the method of this paper.

  10. Variable-Speed Power-Turbine for the Large Civil Tilt Rotor

    Science.gov (United States)

    Suchezky, Mark; Cruzen, G. Scott

    2012-01-01

    Turbine design concepts were studied for application to a large civil tiltrotor transport aircraft. The concepts addressed the need for high turbine efficiency across the broad 2:1 turbine operating speed range representative of the notional mission for the aircraft. The study focused on tailoring basic turbine aerodynamic design design parameters to avoid the need for complex, heavy, and expensive variable geometry features. The results of the study showed that good turbine performance can be achieved across the design speed range if the design focuses on tailoring the aerodynamics for good tolerance to large swings in incidence, as opposed to optimizing for best performance at the long range cruise design point. A rig design configuration and program plan are suggested for a dedicated experiment to validate the proposed approach.

  11. Concept to Reality: Contributions of the Langley Research Center to US Civil Aircraft of the 1990s

    Science.gov (United States)

    Chambers, Joseph R.

    2003-01-01

    This document is intended to be a companion to NASA SP-2000-4519, 'Partners in Freedom: Contributions of the Langley Research Center to U.S. Military Aircraft of the 1990s'. Material included in the combined set of volumes provides informative and significant examples of the impact of Langley's research on U.S. civil and military aircraft of the 1990s. This volume, 'Concept to Reality: Contributions of the NASA Langley Research Center to U.S. Civil Aircraft of the 1990s', highlights significant Langley contributions to safety, cruise performance, takeoff and landing capabilities, structural integrity, crashworthiness, flight deck technologies, pilot-vehicle interfaces, flight characteristics, stall and spin behavior, computational design methods, and other challenging technical areas for civil aviation. The contents of this volume include descriptions of some of the more important applications of Langley research to current civil fixed-wing aircraft (rotary-wing aircraft are not included), including commercial airliners, business aircraft, and small personal-owner aircraft. In addition to discussions of specific aircraft applications, the document also covers contributions of Langley research to the operation of civil aircraft, which includes operating problems. This document is organized according to disciplinary technologies, for example, aerodynamics, structures, materials, and flight systems. Within each discussion, examples are cited where industry applied Langley technologies to specific aircraft that were in operational service during the 1990s and the early years of the new millennium. This document is intended to serve as a key reference for national policy makers, internal NASA policy makers, Congressional committees, the media, and the general public. Therefore, it has been written for a broad general audience and does not presume any significant technical expertise. An extensive bibliography is provided for technical specialists and others who desire a

  12. Flight dynamics simulation modeling and control of a large flexible tiltrotor aircraft

    Science.gov (United States)

    Juhasz, Ondrej

    A high order rotorcraft mathematical model is developed and validated against the XV-15 and a Large Civil Tiltrotor (LCTR) concept. The mathematical model is generic and allows for any rotorcraft configuration, from single main rotor helicopters to coaxial and tiltrotor aircraft. Rigid-body and inflow states, as well as flexible wing and blade states are used in the analysis. The separate modeling of each rotorcraft component allows for structural flexibility to be included, which is important when modeling large aircraft where structural modes affect the flight dynamics frequency ranges of interest, generally 1 to 20 rad/sec. Details of the formulation of the mathematical model are given, including derivations of structural, aerodynamic, and inertial loads. The linking of the components of the aircraft is developed using an approach similar to multibody analyses by exploiting a tree topology, but without equations of constraints. Assessments of the effects of wing flexibility are given. Flexibility effects are evaluated by looking at the nature of the couplings between rigid-body modes and wing structural modes and vice versa. The effects of various different forms of structural feedback on aircraft dynamics are analyzed. A proportional-integral feedback on the structural acceleration is deemed to be most effective at both improving the damping and reducing the overall excitation of a structural mode. A model following control architecture is then implemented on full order flexible LCTR models. For this aircraft, the four lowest frequency structural modes are below 20 rad/sec, and are thus needed for control law development and analysis. The impact of structural feedback on both Attitude-Command, Attitude-Hold (ACAH) and Translational Rate Command (TRC) response types are investigated. A rigid aircraft model has optimistic performance characteristics, and a control system designed for a rigid aircraft could potentially destabilize a flexible one. The various

  13. A Psychoacoustic Evaluation of Noise Signatures from Advanced Civil Transport Aircraft

    Science.gov (United States)

    Rizzi, Stephen A.; Christian, Andrew

    2016-01-01

    The NASA Environmentally Responsible Aviation project has been successful in developing and demonstrating technologies for integrated aircraft systems that can simultaneously meet aggressive goals for fuel burn, noise and emissions. Some of the resulting systems substantially differ from the familiar tube and wing designs constituting the current civil transport fleet. This study attempts to explore whether or not the effective perceived noise level metric used in the NASA noise goal accurately reflects human subject response across the range of vehicles considered. Further, it seeks to determine, in a quantitative manner, if the sounds associated with the advanced aircraft are more or less preferable to the reference vehicles beyond any differences revealed by the metric. These explorations are made through psychoacoustic tests in a controlled laboratory environment using simulated stimuli developed from auralizations of selected vehicles based on systems noise assessments.

  14. Self-defense of Large Aircraft

    Science.gov (United States)

    2008-03-01

    121 Figure 69. DHL aircraft was hit by MANPADs. .................................................. 122 Figure 70. A C-5 was...impact. Then the highest priority missile is jammed with a custom jam code in a sequence that would cause the 103 missile to break lock and move...European Air Transport and operated on behalf of DHL , was hit by an SA-14 SAM while climbing through 8000 feet shortly after departure from Baghdad

  15. Federal Aviation Administration (FAA airworthiness certification for ceramic matrix composite components in civil aircraft systems

    Directory of Open Access Journals (Sweden)

    Gonczy Stephen T.

    2015-01-01

    Full Text Available Ceramic matrix composites (CMCs are being designed and developed for engine and exhaust components in commercial aviation, because they offer higher temperature capabilities, weight savings, and improved durability compared to metals. The United States Federal Aviation Administration (FAA issues and enforces regulations and minimum standards covering the safe manufacture, operation, and maintenance of civil aircraft. As new materials, these ceramic composite components will have to meet the certification regulations of the FAA for “airworthiness”. The FAA certification process is defined in the Federal Aviation Regulations (Title 14 of the Code of Federal Regulations, FAA policy statements, orders, advisory circulars, technical standard orders, and FAA airworthiness directives. These regulations and documents provide the fundamental requirements and guidelines for design, testing, manufacture, quality assurance, registration, operation, inspection, maintenance, and repair of aircraft systems and parts. For metallic parts in aircraft, the FAA certification and compliance process is well-established for type and airworthiness certification, using ASTM and SAE standards, the MMPDS data handbook, and FAA advisory circulars. In a similar manner for polymer matrix composites (PMC, the PMC industry and the FAA have jointly developed and are refining parallel guidelines for polymer matrix composites (PMCs, using guidance in FAA circulars and the CMH-17 PMC handbook. These documents discuss design methods and codes, material testing, property data development, life/durability assessment, production processes, QA procedures, inspection methods, operational limits, and repairs for PMCs. For ceramic composites, the FAA and the CMC and aerospace community are working together (primarily through the CMH-17 CMC handbook to define and codify key design, production, and regulatory issues that have to be addressed in the certification of CMC components in

  16. Application of MBSE Method During Landing Gear System Design for Civil Aircraft%MBSE在民机起落架系统设计中的应用

    Institute of Scientific and Technical Information of China (English)

    汤超; 方俊伟; 谢陵; 张磊; 夏语冰

    2015-01-01

    This paper clearly introduces function analysis process and method of large-scale civil aircraft based on Raphsody, and its implementation in landing gear system design. Usecase, function flow, sequence and executable state machine of syetem are set up by model. toguide the requirement analysis, function analysis and architecture design of highly complex system in large-scale civil aircraft, and to explore practice of MBSE in highly complex system of civil aircraft.%详细介绍基于Raphsody的大型民机系统功能开发流程与方法,及其在民用飞机起落架系统设计中的应用。通过模型的方式对系统建立用例、功能流、时序关系和可用于执行验证的状态机来描述系统,指导大型民机复杂系统设计过程中的需求分析、功能分析和设计综合工作,探索MBSE方法在民机复杂系统设计中的指导作用。

  17. A fault diagnosis based reconfigurable longitudinal control system for managing loss of air data sensors for a civil aircraft

    OpenAIRE

    Varga, Andreas; Ossmann, Daniel; Joos, Hans-Dieter

    2014-01-01

    An integrated fault diagnosis based fault tolerant longitudinal control system architecture is proposed for civil aircraft which can accommodate partial or total losses of angle of attack and/or calibrated airspeed sensors. A triplex sensor redundancy is assumed for the normal operation of the aircraft using a gain scheduled longitudinal normal control law. The fault isolation functionality is provided by a bank of 6 fault detection filters, which individually monitor each of the 6 sensors us...

  18. 民用飞机选型样机需求分析%Requirement Analysis of Civil Aircraft Selection Prototype

    Institute of Scientific and Technical Information of China (English)

    侯盼盼

    2014-01-01

    随着我国大型客机市场营销工作的深入以及工程设计进程的不断推进,越来越多的客户希望能够有途径深入了解大型客机,越来越多的设计评估工作需要有合适的平台。本文从市场营销产品价值理论出发分析了选型样机的市场需求,从工程角度对选型样机的工程试验功能进行了阐述,并对选型样机的实现形式—实物选型样机和虚拟选型样机的实用方式进行了分析,为我国大型客机的市场营销工作和工程评估工作提供新思路和新方向。%China's large commercial aircraft wil directly face the market. With the deepening of marketing and engineering design progresses, more and more customers expect to have access to in-depth understanding of large aircraft. In addition, a growing number of design evaluation work needs to have the right platform. This article analyzed the requirement of selection prototype by the product-value theory in marketing, described the function of engineering test and evaluation. Also this paper analyzed practical purpose of physical and virtual prototype. It provided new ideas and a new way to the work of civil aircraft marketing and designing.

  19. Advanced energy systems (APU) for large commercial aircraft

    Energy Technology Data Exchange (ETDEWEB)

    Westenberger, A.; Bleil, J.; Arendt, M. [Airbus Deutschland GmbH, Hamburg (Germany)

    2013-06-01

    The intention of using a highly integrated component using on fuel cell technology installed on board of large commercial passenger aircraft for the generation of onboard power for the systems demand during an entire aircraft mission was subject of several studies. The results of these studies have been based on the simulation of the whole system in the context of an aircraft system environment. In front of the work stood the analyses of different fuel cell technologies and the analyses of the aircraft system environment. Today onboard power is provided on ground by an APU and in flight by the main engines. In order to compare fuel cell technology with the today's usual gas turbine operational characteristics have been analysed. A second analysis was devoted to the system demand for typical aircraft categories. The MEA system concept was supposed in all cases. The favourable concept represented an aircraft propelled by conventional engines with starter generator units, providing AC electrical power, covering in total proximately half of the power demand and a component based on fuel cell technology. This component provided electrical DC power, clean potable water, thermal energy at 180 degrees Celsius and nitrogen enriched air for fire suppression and fire extinguishing agent. In opposite of a usual gas turbine based APU, this new unit was operated as the primary power system. (orig.)

  20. Crashworthiness uncertainty analysis of typical civil aircraft based on Box-Behnken method

    Institute of Scientific and Technical Information of China (English)

    Ren Yiru; Xiang Jinwu

    2014-01-01

    The crashworthiness is an important design factor of civil aircraft related with the safety of occupant during impact accident. It is a highly nonlinear transient dynamic problem and may be greatly influenced by the uncertainty factors. Crashworthiness uncertainty analysis is conducted to investigate the effects of initial conditions, structural dimensions and material properties. Simplified finite element model is built based on the geometrical model and basic physics phenomenon. Box-Behnken sampling and response surface methods are adopted to obtain gradient information. Results show that the proposed methods are effective for crashworthiness uncertainty analysis. Yield stress, frame thickness, impact velocity and angle have great influence on the failure behavior, and yield stress and frame thickness dominate the uncertainty of internal energy. Failure strain and tangent modulus have the smallest influence on the initial peak acceleration, and gradients of mean acceleration increase because the appearance of material plastic deformation and element failure.

  1. Behavioral Traits and Airport Type Affect Mammal Incidents with U.S. Civil Aircraft

    Science.gov (United States)

    Schwarz, Kristin B.; Belant, Jerrold L.; Martin, James A.; DeVault, Travis L.; Wang, Guiming

    2014-10-01

    Wildlife incidents with aircraft cost the United States (U.S.) civil aviation industry >US1.4 billion in estimated damages and loss of revenue from 1990 to 2009. Although terrestrial mammals represented only 2.3 % of wildlife incidents, damage to aircraft occurred in 59 % of mammal incidents. We examined mammal incidents (excluding bats) at all airports in the Federal Aviation Administration (FAA) National Wildlife Strike Database from 1990 to 2010 to characterize these incidents by airport type: Part-139 certified (certificated) and general aviation (GA). We also calculated relative hazard scores for species most frequently involved in incidents. We found certificated airports had more than twice as many incidents as GA airports. Incidents were most frequent in October ( n = 215 of 1,764 total) at certificated airports and November ( n = 111 of 741 total) at GA airports. Most (63.2 %) incidents at all airports ( n = 1,523) occurred at night but the greatest incident rate occurred at dusk (177.3 incidents/hr). More incidents with damage ( n = 1,594) occurred at GA airports (38.6 %) than certificated airports (19.0 %). Artiodactyla (even-toed ungulates) incidents incurred greatest (92.4 %) damage costs ( n = 326; US51.8 million) overall and mule deer ( Odocoileus hemionus) was the most hazardous species. Overall, relative hazard score increased with increasing log body mass. Frequency of incidents was influenced by species relative seasonal abundance and behavior. We recommend airport wildlife officials evaluate the risks mammal species pose to aircraft based on the hazard information we provide and consider prioritizing management strategies that emphasize reducing their occurrence on airport property.

  2. Aerodynamic Limits on Large Civil Tiltrotor Sizing and Efficiency

    Science.gov (United States)

    Acree, C W., Jr.

    2014-01-01

    The NASA Large Civil Tiltrotor (2nd generation, or LCTR2) has been the reference design for avariety of NASA studies of design optimization, engine and gearbox technology, handling qualities, andother areas, with contributions from NASA Ames, Glenn and Langley Centers, plus academic and industrystudies. Ongoing work includes airfoil design, 3D blade optimization, engine technology studies, andwingrotor aerodynamic interference. The proposed paper will bring the design up to date with the latestresults of such studies, then explore the limits of what aerodynamic improvements might hope toaccomplish. The purpose is two-fold: 1) determine where future technology studies might have the greatestpayoff, and 2) establish a stronger basis of comparison for studies of other vehicle configurations andmissions.

  3. Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM

    Directory of Open Access Journals (Sweden)

    Fan Liu

    2015-02-01

    Full Text Available In order to incorporate airworthiness requirements for flight characteristics into the entire development cycle of electronic flight control system (EFCS equipped civil aircraft, digital virtual flight testing and evaluation method based on handling qualities rating method (HQRM is proposed. First, according to HQRM, flight characteristics airworthiness requirements of civil aircraft in EFCS failure states are determined. On this basis, digital virtual flight testing model, comprising flight task digitized model, pilot controlling model, aircraft motion and atmospheric turbulence model, is used to simulate the realistic process of a pilot controlling an airplane to perform assigned flight tasks. According to the simulation results, flight characteristics airworthiness compliance of the airplane can be evaluated relying on the relevant regulations for handling qualities (HQ rating. Finally, this method is applied to a type of passenger airplane in a typical EFCS failure state, and preliminary conclusions concerning airworthiness compliance are derived quickly. The research results of this manuscript can provide important theoretical reference for EFCS design and actual airworthiness compliance verification of civil aircraft.

  4. Digital virtual flight testing and evaluation method for flight characteristics airworthiness compliance of civil aircraft based on HQRM

    Institute of Scientific and Technical Information of China (English)

    Liu Fan; Wang Lixin; Tan Xiangsheng

    2015-01-01

    In order to incorporate airworthiness requirements for flight characteristics into the entire development cycle of electronic flight control system (EFCS) equipped civil aircraft, digital virtual flight testing and evaluation method based on handling qualities rating method (HQRM) is proposed. First, according to HQRM, flight characteristics airworthiness requirements of civil aircraft in EFCS failure states are determined. On this basis, digital virtual flight testing model, comprising flight task digitized model, pilot controlling model, aircraft motion and atmospheric tur-bulence model, is used to simulate the realistic process of a pilot controlling an airplane to perform assigned flight tasks. According to the simulation results, flight characteristics airworthiness com-pliance of the airplane can be evaluated relying on the relevant regulations for handling qualities (HQ) rating. Finally, this method is applied to a type of passenger airplane in a typical EFCS failure state, and preliminary conclusions concerning airworthiness compliance are derived quickly. The research results of this manuscript can provide important theoretical reference for EFCS design and actual airworthiness compliance verification of civil aircraft.

  5. CORRELATION OF THE CHICAGO CONVENTION OF 1944 AND THE PEKING CONVENTION OF 2010 IN THE FIELD OF THE MISUSE OF CIVIL AIRCRAFT

    Directory of Open Access Journals (Sweden)

    R. . Luli

    2015-01-01

    Full Text Available The article considers the issue concerning the international legal problem of using armed forces to counter the threats posed by the misuse of civil aircraft, in particular, the use of civil aircraft as a weapon to kill people and destroy objects on the territory of States (the events of 11th September 2001 in the USA. It proves the need for universal international legal norms regulating the actions of States to prevent and suppress acts of the misuse of civil aircraft.

  6. Additional Development and Systems Analyses of Pneumatic Technology for High Speed Civil Transport Aircraft

    Science.gov (United States)

    Englar, Robert J.; Willie, F. Scott; Lee, Warren J.

    1999-01-01

    In the Task I portion of this NASA research grant, configuration development and experimental investigations have been conducted on a series of pneumatic high-lift and control surface devices applied to a generic High Speed Civil Transport (HSCT) model configuration to determine their potential for improved aerodynamic performance, plus stability and control of higher performance aircraft. These investigations were intended to optimize pneumatic lift and drag performance; provide adequate control and longitudinal stability; reduce separation flowfields at high angle of attack; increase takeoff/climbout lift-to-drag ratios; and reduce system complexity and weight. Experimental aerodynamic evaluations were performed on a semi-span HSCT generic model with improved fuselage fineness ratio and with interchangeable plain flaps, blown flaps, pneumatic Circulation Control Wing (CCW) high-lift configurations, plain and blown canards, a novel Circulation Control (CC) cylinder blown canard, and a clean cruise wing for reference. Conventional tail power was also investigated for longitudinal trim capability. Also evaluated was unsteady pulsed blowing of the wing high-lift system to determine if reduced pulsed mass flow rates and blowing requirements could be made to yield the same lift as that resulting from steady-state blowing. Depending on the pulsing frequency applied, reduced mass flow rates were indeed found able to provide lift augmentation at lesser blowing values than for the steady conditions. Significant improvements in the aerodynamic characteristics leading to improved performance and stability/control were identified, and the various components were compared to evaluate the pneumatic potential of each. Aerodynamic results were provided to the Georgia Tech Aerospace System Design Lab. to conduct the companion system analyses and feasibility study (Task 2) of theses concepts applied to an operational advanced HSCT aircraft. Results and conclusions from these

  7. Civil aircraft for the regular investigation of the atmosphere based on an instrumented container: the new CARIBIC system

    Directory of Open Access Journals (Sweden)

    C. A. M. Brenninkmeijer

    2007-04-01

    Full Text Available A large airfreight container with automated instruments for measurement of atmospheric gases and trace compounds was operated on a monthly basis onboard a Boeing 767-300 ER of LTU International Airways during long-distance flights from 1997 to 2002 (CARIBIC, Civil Aircraft for Regular Investigation of the Atmosphere Based on an Instrument Container, http://www.caribic-atmospheric.com. Subsequently a more advanced system has been developed, using a larger capacity container with additional equipment and an improved inlet system. CARIBIC phase #2 was implemented on a new long-range aircraft type Airbus A340-600 of the Lufthansa German Airlines (Star Alliance in December 2004, creating a powerful flying observatory. The instrument package comprises detectors for the measurement of O3, total and gaseous H2O, NO and NOy, CO, CO2, O2, Hg, and number concentrations of sub-micrometer particles (>4 nm, >12 nm, and >18 nm diameter. Furthermore, an optical particle counter and a proton transfer mass spectrometer (PTR-MS are installed. Aerosol samples are collected for analyses of elemental composition and particle morphology after flight. Air samples are taken in glass containers for laboratory analyses of hydrocarbons, halocarbons and greenhouse gases in several laboratories. Absorption tubes collect oxygenated volatile organic compounds. Three differential optical absorption spectrometers (DOAS with their telescopes mounted in the inlet system measure atmospheric trace gases such as BrO, HONO, and NO2. A video camera mounted in the inlet provides information about clouds along the flight track. Here we describe the flying observatory and report examples of measurement results.

  8. Civil aircraft for the regular investigation of the atmosphere based on an instrumented container: the new CARIBIC system

    OpenAIRE

    Brenninkmeijer, C. A. M.; Crutzen, P.; Boumard, F.; Dauer, T.; B. Dix; Ebinghaus, R.; Filippi, D.; Fischer, H.; Franke, H.; U. Frieβ; Heintzenberg, J; F. Helleis; Hermann, M; H. H. Kock; Koeppel, C.

    2007-01-01

    An airfreight container with automated instruments for measurement of atmospheric gases and trace compounds was operated on a monthly basis onboard a Boeing 767-300 ER of LTU International Airways during long-distance flights from 1997 to 2002 (CARIBIC, Civil Aircraft for Regular Investigation of the Atmosphere Based on an Instrument Container, http://www.caribic-atmospheric.com). Subsequently a more advanced system has be...

  9. Drag prediction method of powered-on civil aircraft based on thrust drag bookkeeping

    Directory of Open Access Journals (Sweden)

    Zhang Yufei

    2015-08-01

    Full Text Available A drag prediction method based on thrust drag bookkeeping (TDB is introduced for civil jet propulsion/airframe integration performance analysis. The method is derived from the control volume theory of a powered-on nacelle. Key problem of the TDB is identified to be accurate prediction of velocity coefficient of the powered-on nacelle. Accuracy of CFD solver is validated by test cases of the first AIAA Propulsion Aerodynamics Workshop. Then the TDB method is applied to thrust and drag decomposing of a realistic aircraft. A linear relation between the computations assumed free stream Mach number and the velocity coefficient result is revealed. The thrust losses caused by nozzle internal drag and pylon scrubbing are obtained by the isolated nacelle and mapped on to the in-flight whole configuration analysis. Effects of the powered-on condition are investigated by comparing through-flow configuration with powered-on configuration. The variance on aerodynamic coefficients and pressure distribution is numerically studied.

  10. 民用飞机风挡排雨液选择设计初探%The Study of windshield rain repellent fluid choosing for civil aircraft

    Institute of Scientific and Technical Information of China (English)

    白穆; 霍西恒

    2016-01-01

    This paper analyzed and studied the rain repellent fluid choosing for civil aircraft; summarized the design improvement of rain repellent fluid choosing for civil aircraft.%本文对民用飞机风挡排雨液选择进行了初步分析与研究,给出风挡排雨液选择优化设计概述。

  11. Research on Civil Aircraft Fuel Saving Strategy%民机节油策略研究

    Institute of Scientific and Technical Information of China (English)

    张伟

    2016-01-01

    Fuel saving is a very important and long-term action for airlines. Based on aircraft performance analy-sis, this paper presents fuel saving suggestions on weight, center of gravity and APU usage and taxiing before flight, and also presents economy flight fuel saving strategy suggestions on take-off, climb, cruise, descent, ap-proach and landing phase. By the research of fuel saving measures in each detailed aspect of a flight circle, the pa-per suggests the method of well using flight planning tool to improve fuel consuming efficiency, with a case study and the comparison of different flight planning methods, and educes the conclusion that the integration IT solutions including flight planning and QAR ( Quick Access Recorder ) analysis systems from civil aircraft manufacture is a high performance-price ratio choice for airlines’ fuel saving.%节油是航空公司的长效措施,各航空公司均很重视。从飞行具体环节出发,基于性能研究民机节油策略,给出飞行前重量、重心、APU使用和滑行等措施分析和建议,并给出起飞、爬升、巡航、下降和进近着陆的经济飞行节油策略分析和建议。通过对飞行具体环节节油策略的研究,提出重视飞行计划优化和执行的思路,案例分析优化效果,对比分析现有飞行计划方法,得出飞机制造商提供包含飞行计划和QAR ( Quick Access Recorder)分析系统等的整体IT解决方案,是提升节油效果的一个性价比很高的选择的结论。

  12. Large capacity oblique all-wing transport aircraft

    Science.gov (United States)

    Galloway, Thomas L.; Phillips, James A.; Kennelly, Robert A., Jr.; Waters, Mark H.

    1996-01-01

    Dr. R. T. Jones first developed the theory for oblique wing aircraft in 1952, and in subsequent years numerous analytical and experimental projects conducted at NASA Ames and elsewhere have established that the Jones' oblique wing theory is correct. Until the late 1980's all proposed oblique wing configurations were wing/body aircraft with the wing mounted on a pivot. With the emerging requirement for commercial transports with very large payloads, 450-800 passengers, Jones proposed a supersonic oblique flying wing in 1988. For such an aircraft all payload, fuel, and systems are carried within the wing, and the wing is designed with a variable sweep to maintain a fixed subsonic normal Mach number. Engines and vertical tails are mounted on pivots supported from the primary structure of the wing. The oblique flying wing transport has come to be known as the Oblique All-Wing (OAW) transport. This presentation gives the highlights of the OAW project that was to study the total concept of the OAW as a commercial transport.

  13. Laser Welding of Large Scale Stainless Steel Aircraft Structures

    Science.gov (United States)

    Reitemeyer, D.; Schultz, V.; Syassen, F.; Seefeld, T.; Vollertsen, F.

    In this paper a welding process for large scale stainless steel structures is presented. The process was developed according to the requirements of an aircraft application. Therefore, stringers are welded on a skin sheet in a t-joint configuration. The 0.6 mm thickness parts are welded with a thin disc laser, seam length up to 1920 mm are demonstrated. The welding process causes angular distortions of the skin sheet which are compensated by a subsequent laser straightening process. Based on a model straightening process parameters matching the induced welding distortion are predicted. The process combination is successfully applied to stringer stiffened specimens.

  14. 民用飞机FPGA设计研究%Preliminary Research of FPGA Design in Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    郭林

    2011-01-01

    This paper studies the FPGA design in the civil aircraft,including the FPGA development life cycle,design and verification process,as well as the consideration of single-event upset preventing and the consideration of fully testable in critical system.%研究了民用飞机中FPGA的设计,主要包括FPGA设计的研制生命周期、设计与验证过程,以及在关键系统中FPGA设计的单粒子翻转效应及可测试性考虑。

  15. System Analyses of Pneumatic Technology for High Speed Civil Transport Aircraft

    Science.gov (United States)

    Mavris, Dimitri N.; Tai, Jimmy C.; Kirby, Michelle M.; Roth, Bryce A.

    1999-01-01

    The primary aspiration of this study was to objectively assess the feasibility of the application of a low speed pneumatic technology, in particular Circulation Control (CC) to an HSCT concept. Circulation Control has been chosen as an enabling technology to be applied on a generic High Speed Civil Transport (HSCT). This technology has been proven for various subsonic vehicles including flight tests on a Navy A-6 and computational application on a Boeing 737. Yet, CC has not been widely accepted for general commercial fixed-wing use but its potential has been extensively investigated for decades in wind tunnels across the globe for application to rotorcraft. More recently, an experimental investigation was performed at Georgia Tech Research Institute (GTRI) with application to an HSCT-type configuration. The data from those experiments was to be applied to a full-scale vehicle to assess the impact from a system level point of view. Hence, this study attempted to quantitatively assess the impact of this technology to an HSCT. The study objective was achieved in three primary steps: 1) Defining the need for CC technology; 2) Wind tunnel data reduction; 3) Detailed takeoff/landing performance assessment. Defining the need for the CC technology application to an HSCT encompassed a preliminary system level analysis. This was accomplished through the utilization of recent developments in modern aircraft design theory at Aerospace Systems Design Laboratory (ASDL). These developments include the creation of techniques and methods needed for the identification of technical feasibility show stoppers. These techniques and methods allow the designer to rapidly assess a design space and disciplinary metric enhancements to enlarge or improve the design space. The takeoff and landing field lengths were identified as the concept "show-stoppers". Once the need for CC was established, the actual application of data and trends was assessed. This assessment entailed a reduction of the

  16. Reduction environmental effects of civil aircraft through multi-objective flight plan optimisation

    Science.gov (United States)

    Lee, D. S.; Gonzalez, L. F.; Walker, R.; Periaux, J.; Onate, E.

    2010-06-01

    With rising environmental alarm, the reduction of critical aircraft emissions including carbon dioxides (CO2) and nitrogen oxides (NOx) is one of most important aeronautical problems. There can be many possible attempts to solve such problem by designing new wing/aircraft shape, new efficient engine, etc. The paper rather provides a set of acceptable flight plans as a first step besides replacing current aircrafts. The paper investigates a green aircraft design optimisation in terms of aircraft range, mission fuel weight (CO2) and NOx using advanced Evolutionary Algorithms coupled to flight optimisation system software. Two multi-objective design optimisations are conducted to find the best set of flight plans for current aircrafts considering discretised altitude and Mach numbers without designing aircraft shape and engine types. The objectives of first optimisation are to maximise range of aircraft while minimising NOx with constant mission fuel weight. The second optimisation considers minimisation of mission fuel weight and NOx with fixed aircraft range. Numerical results show that the method is able to capture a set of useful trade-offs that reduce NOx and CO2 (minimum mission fuel weight).

  17. Legislation of China Civil Aircraft Industry and WTO Rules%WTO规则与我国民用飞机产业发展立法

    Institute of Scientific and Technical Information of China (English)

    庄浩刚; 李乾贵

    2012-01-01

    WTO Rules have huge impact and positive significance for the development of China' s civil aircraft industry. Facing the opportunities and challenges of joining the WTO, the civil aircraft industry must take appropriate , while avoiding disadvantages. China' s legal system is not perfect and the current civil aviation roles and regulations do not meet the requirements of the WTO rules. The concept of the law has not been fully established. China' s civil aircraft industry should reduce the risks of entering WTO. The key point is the relationship between government administrative behavior and the legal system of civil aircraft industry. In order to protect and promote the development of civil aircraft industry, China' s civil aircraft industry needs to establish a sound system of rules and regulations to make China act in accordance with WTO rules and international convention. At the same time, the legislation experience of the typical national civil aircraft industry development can provide useful inspiration and help China to accelerate its sustainable development of civil aircraft industry.%WTO规则对中国民用航空产业特别是我国民用飞机产业的发展有着巨大的影响和积极意义。从目前来看,中国的法律体系尚不完善,现行的民航法规和规章,要么在一些方面规定阙如。要么不符合WTO规则的要求,法治观念还没有完全树立起来。在这种法制环境下,中国民机产业必须规避入世风险。其核心问题是处理好政府的行政管理行为与民机产业法制之间的关系。对此,中国民机产业要建立健全法律法规制度,才能使我国作为WTO成员按照WTO规则和国际惯例保障和促进民机产业的发展。同时,通过典型国家民机产业发展立法的经验借鉴,也能为我国民机产业发展立法提供有益的启示,从而加速我国民机产业的可持续发展。

  18. Remotely Piloted Aircraft Systems (RPAS) for high resolution topography and monitoring: civil protection purposes on hydrogeological contexts

    Science.gov (United States)

    Bertacchini, Eleonora; Castagnetti, Cristina; Corsini, Alessandro; De Cono, Stefano

    2014-10-01

    The proposed work concerns the analysis of Remotely Piloted Aircraft Systems (RPAS), also known as drones, UAV (Unmanned Aerial Vehicle) or UAS (Unmanned Aerial System), on hydrogeological contexts for civil protection purposes, underlying the advantages of using a flexible and relatively low cost system. The capabilities of photogrammetric RPAS multi-sensors platform were examined in term of mapping, creation of orthophotos, 3D models generation, data integration into a 3D GIS (Geographic Information System) and validation through independent techniques such as GNSS (Global Navigation Satellite System). The RPAS used (multirotor OktoXL, of the Mikrokopter) was equipped with a GPS (Global Positioning System) receiver, digital cameras for photos and videos, an inertial navigation system, a radio device for communication and telemetry, etc. This innovative way of viewing and understanding the environment showed huge potentialities for the study of the territory, and due to its characteristics could be well integrated with aircraft surveys. However, such characteristics seem to give priority to local applications for rigorous and accurate analysis, while it remains a means of expeditious investigation for more extended areas. According to civil protection purposes, the experimentation was carried out by simulating operational protocols, for example for inspection, surveillance, monitoring, land mapping, georeferencing methods (with or without Ground Control Points - GCP) based on high resolution topography (2D and 3D information).

  19. Fuel-rich, catalytic reaction experimental results. [fuel development for high-speed civil transport aircraft

    Science.gov (United States)

    Rollbuhler, Jim

    1991-01-01

    Future aeropropulsion gas turbine combustion requirements call for operating at very high inlet temperatures, pressures, and large temperature rises. At the same time, the combustion process is to have minimum pollution effects on the environment. Aircraft gas turbine engines utilize liquid hydrocarbon fuels which are difficult to uniformly atomize and mix with combustion air. An approach for minimizing fuel related problems is to transform the liquid fuel into gaseous form prior to the completion of the combustion process. Experimentally obtained results are presented for vaporizing and partially oxidizing a liquid hydrocarbon fuel into burnable gaseous components. The presented experimental data show that 1200 to 1300 K reaction product gas, rich in hydrogen, carbon monoxide, and light-end hydrocarbons, is formed when flowing 0.3 to 0.6 fuel to air mixes through a catalyst reactor. The reaction temperatures are kept low enough that nitrogen oxides and carbon particles (soot) do not form. Results are reported for tests using different catalyst types and configurations, mass flowrates, input temperatures, and fuel to air ratios.

  20. 14 CFR 91.9 - Civil aircraft flight manual, marking, and placard requirements.

    Science.gov (United States)

    2010-01-01

    ... available in the aircraft a current approved Airplane or Rotorcraft Flight Manual, approved manual material... prohibited range takes place over water on which a safe ditching can be accomplished and if the helicopter is... emergency ditching on open water....

  1. Large Field Photogrammetry Techniques in Aircraft and Spacecraft Impact Testing

    Science.gov (United States)

    Littell, Justin D.

    2010-01-01

    The Landing and Impact Research Facility (LandIR) at NASA Langley Research Center is a 240 ft. high A-frame structure which is used for full-scale crash testing of aircraft and rotorcraft vehicles. Because the LandIR provides a unique capability to introduce impact velocities in the forward and vertical directions, it is also serving as the facility for landing tests on full-scale and sub-scale Orion spacecraft mass simulators. Recently, a three-dimensional photogrammetry system was acquired to assist with the gathering of vehicle flight data before, throughout and after the impact. This data provides the basis for the post-test analysis and data reduction. Experimental setups for pendulum swing tests on vehicles having both forward and vertical velocities can extend to 50 x 50 x 50 foot cubes, while weather, vehicle geometry, and other constraints make each experimental setup unique to each test. This paper will discuss the specific calibration techniques for large fields of views, camera and lens selection, data processing, as well as best practice techniques learned from using the large field of view photogrammetry on a multitude of crash and landing test scenarios unique to the LandIR.

  2. Preliminary Assessment of the Interior Noise Environment in the Large Civil Tiltrotor (LCTR2)

    Science.gov (United States)

    Grosveld, Ferdinand W.; Cabell, Randolph H.

    2011-01-01

    The second-generation Large Civil Tiltrotor (LCTR2) serves as a representative vehicle under the NASA Fundamental Aeronautics Program (FAP) Subsonic Rotary Wing (SRW) project with a design goal to transport 90 passengers over a distance of 1800 km at a speed of 550 km/hr. The tiltrotor combines the vertical lift capability of a helicopter with the speed, altitude, and range of a turboprop airplane. The blade-passage frequency of the four-bladed rotor is as low as 6.9 Hz during cruise conditions. The resulting low-frequency acoustic excitation and its harmonics, combined with the anticipated use of lightweight composite and sandwich materials for the fuselage sidewall, may pose a challenge to achieving acceptable interior noise levels. The objective of the present study is to perform a preliminary assessment of the expected interior noise environment in the LCTR2 cabin. The approach includes a combination of semi-empirical, analytical, and statistical energy analysis methods. Because the LCTR2 is a notional vehicle, the prediction approach was also applied to the XV-15 tiltrotor and Bombardier Q400 turobprop aircraft to compare predictions with publicly available experimental data. Guidance for the expected interior noise levels in the LCTR2 was obtained by considering both the predicted exterior noise levels and the transmission loss of a basic fuselage sidewall consisting of a skin, porous layer and a trim panel. Structural and acoustic resonances are expected to coincide with low order harmonics of the blade passage frequency. The estimated sound pressure levels in the LCTR2 may not be acceptable when evaluated against known characteristics of human response to low frequency sound.

  3. Research on Zonal Inspection Intervals of Civil Aircraft Based on Improved FAHP

    Directory of Open Access Journals (Sweden)

    Lu Xiang

    2013-07-01

    Full Text Available One of the most important things in formulating aircraft maintenance program is to determine the zonal inspection intervals. In accordance with the current situation that there has no perfect rating systems of zonal inspection under MSG-3 (Maintenance Steering Group-3 analysis system, a method to calculate the integrate level of zonal rating is to analyze the impact of aircraft zonal rating factors, establish a hierarchical index evaluation system and then utilize the improved fuzzy analytic hierarchy process (FAHP to determine the indexes’ weight. Moreover, the zonal inspection intervals can be established according to the correspondence between rates and intervals. Finally, take a typical zone of an aircraft as an example to verify the method.  

  4. The dynamics of the HSCT environment. [air pollution from High Speed Civil Transport Aircraft

    Science.gov (United States)

    Douglass, Anne R.; Rood, Richard B.

    1991-01-01

    Assessments of the impact of aircraft engine exhausts on stratospheric ozone levels are currently limited to 2D zonally-averaged models which, while completely representing chemistry, involve high parameterization of transport processes. Prospective 3D models under development by NASA-Goddard will use winds from a data-assimilation procedure; the upper troposphere/lower stratosphere behavior of one such model has been verified by direct comparison of model simulations with satellite, balloon, and sonde measurements. Attention is presently given to the stratosphere/troposphere exchange and nonzonal distribution of aircraft engine exhaust.

  5. Domesticating the Drone: The Demilitarisation of Unmanned Aircraft for Civil Markets.

    Science.gov (United States)

    Boucher, Philip

    2015-12-01

    Remotely piloted aviation systems (RPAS) or 'drones' are well known for their military applications, but could also be used for a range of non-military applications for state, industrial, commercial and recreational purposes. The technology is advanced and regulatory changes are underway which will allow their use in domestic airspace. As well as the functional and economic benefits of a strong civil RPAS sector, the potential benefits for the military RPAS sector are also widely recognised. Several actors have nurtured this dual-use aspect of civil RPAS development. However, concerns have been raised about the public rejecting the technology because of their association with military applications and potentially controversial applications, for example in policing and border control. In contrast with the enthusiasm for dual-use exhibited throughout the EC consultation process, the strategy for avoiding public rejection devised in its roadmap would downplay the connection between military and non-military RPAS and focus upon less controversial applications such as search and rescue. We reflect upon this contrast in the context of the European agenda of responsible research and innovation. In doing so, we do not rely upon critique of drones per se, in their neither their civil nor military guise, but explore the extent to which current strategies for managing their public acceptability are compatible with a responsible and socially beneficial development of RPAS for civil purposes.

  6. Research and Application on Civil Aircraft Ground Flotation%民用飞机地面漂浮性分析研究及应用

    Institute of Scientific and Technical Information of China (English)

    房务官; 魏小辉; 宋晓晨; 吴卜圣

    2012-01-01

    民用飞机地面漂浮性是评估飞机-机场相容性的一个重要指标,其直接影响到飞机设计参数选择以及地面适应性的优劣.在总体概念设计阶段就必须对飞机的漂浮性能进行分析评估,从而选择恰当的飞机参数.对民用飞机在刚性道面和柔性道面上漂浮性分析方法做了简要说明,并针对国际民用航空组织所推广使用的ACN/PCN(飞机分类号/机场分类号)方法进行了详细分析研究,在此基础上,开发出了飞机地面漂浮性分析软件.通过直接输入飞机相关参数可以快速准确地计算出飞机分类号ACN值.可以有效地对飞机地面漂浮性进行评估和优化,从而解决了用手工方式评估飞机地面漂浮性时的繁琐及不准确,并降低了对从事飞机地面漂浮性计算的人员要求.%Civil aircraft ground flotation is an important evaluation indicator of aircraft- airport compatibility , which affects the aircraft design parameters selection and the pros and cons of the ground adaptability directly. In the general conceptual design stage, the analysis and evaluation of the aircraft flotation must be done to select the appropriate parameters of the aircraft. This paper briefly describes the analysis methods of civil aircraft floating in the rigid pavement and flexible pavement, and carried out a detailed analysis and research for the ACN / PCN,the aircraft and airport's class number method,that is promoted by International Civil Aviation Organization and developed a aircraft ground flotation analysis software on that base. Inputting the relevant aircraft parameters directly, it can calculate the value the class number of aircraft, ACN, quickly and accurately. The software can effectively evaluate and optimize aircraft ground flotation , thus solve the problem of the complication and inaccuracy caused by evaluating the aircraft ground flotation by hand. In addition,it also reduces the demand for the personnel engaged in it.

  7. Requirements to micro-unmanned aircraft systems in civil protection and environmental monitoring

    Energy Technology Data Exchange (ETDEWEB)

    Fischer-Stabel, Peter; Hardt, Christopher [Univ. of Applied Sciences Trier, Birkenfeld (Germany). Dept. of Environmental Planning

    2013-07-01

    Especially in application fields such as environmental monitoring or in the field of information and operations management with technical or natural disasters, increased demands on communication and sensor technology to micro unmanned aircraft systems (UAS) are given. These are currently covered by the system manufacturers, however inadequately. The use case of wildlife monitoring with micro UAS comes with some special requirements and problems, addressed in this paper. (orig.)

  8. Flight Dynamics Simulation Modeling and Control of a Large Flexible Tiltrotor Aircraft

    Science.gov (United States)

    2014-09-01

    TECHNICAL REPORT CR-RDMR-AF-14-01 FLIGHT DYNAMICS SIMULATION MODELING AND CONTROL OF A LARGE FLEXIBLE TILTROTOR AIRCRAFT...September 2014 3. REPORT TYPE AND DATES COVERED Final 4. TITLE AND SUBTITLE Flight Dynamics Simulation Modeling and Control of a Large Flexible...18 298-102 i/ii (Blank) FLIGHT DYNAMICS SIMULATION MODELING AND CONTROL OF A LARGE FLEXIBLE TILTROTOR AIRCRAFT by Ondrej Juhasz Dissertation

  9. Large eddy simulation of soot evolution in an aircraft combustor

    Science.gov (United States)

    Mueller, Michael E.; Pitsch, Heinz

    2013-11-01

    An integrated kinetics-based Large Eddy Simulation (LES) approach for soot evolution in turbulent reacting flows is applied to the simulation of a Pratt & Whitney aircraft gas turbine combustor, and the results are analyzed to provide insights into the complex interactions of the hydrodynamics, mixing, chemistry, and soot. The integrated approach includes detailed models for soot, combustion, and the unresolved interactions between soot, chemistry, and turbulence. The soot model is based on the Hybrid Method of Moments and detailed descriptions of soot aggregates and the various physical and chemical processes governing their evolution. The detailed kinetics of jet fuel oxidation and soot precursor formation is described with the Radiation Flamelet/Progress Variable model, which has been modified to account for the removal of soot precursors from the gas-phase. The unclosed filtered quantities in the soot and combustion models, such as source terms, are closed with a novel presumed subfilter PDF approach that accounts for the high subfilter spatial intermittency of soot. For the combustor simulation, the integrated approach is combined with a Lagrangian parcel method for the liquid spray and state-of-the-art unstructured LES technology for complex geometries. Two overall fuel-to-air ratios are simulated to evaluate the ability of the model to make not only absolute predictions but also quantitative predictions of trends. The Pratt & Whitney combustor is a Rich-Quench-Lean combustor in which combustion first occurs in a fuel-rich primary zone characterized by a large recirculation zone. Dilution air is then added downstream of the recirculation zone, and combustion continues in a fuel-lean secondary zone. The simulations show that large quantities of soot are formed in the fuel-rich recirculation zone, and, furthermore, the overall fuel-to-air ratio dictates both the dominant soot growth process and the location of maximum soot volume fraction. At the higher fuel

  10. Architecture and Key Techniques of Augmented Reality Maintenance Guiding System for Civil Aircrafts

    Science.gov (United States)

    hong, Zhou; Wenhua, Lu

    2017-01-01

    Augmented reality technology is introduced into the maintenance related field for strengthened information in real-world scenarios through integration of virtual assistant maintenance information with real-world scenarios. This can lower the difficulty of maintenance, reduce maintenance errors, and improve the maintenance efficiency and quality of civil aviation crews. Architecture of augmented reality virtual maintenance guiding system is proposed on the basis of introducing the definition of augmented reality and analyzing the characteristics of augmented reality virtual maintenance. Key techniques involved, such as standardization and organization of maintenance data, 3D registration, modeling of maintenance guidance information and virtual maintenance man-machine interaction, are elaborated emphatically, and solutions are given.

  11. Significance of Operating Environment in Condition Monitoring of Large Civil Structures

    Directory of Open Access Journals (Sweden)

    Sreenivas Alampalli

    1999-01-01

    Full Text Available Success of remote long-term condition monitoring of large civil structures and developing calibrated analytical models for damage detection, depend significantly on establishing accurate baseline signatures and their sensitivity. Most studies reported in the literature concentrated on the effect of structural damage on modal parameters without emphasis on reliability of modal parameters. Thus, a field bridge structure was studied for the significance of operating conditions in relation to baseline signatures. Results indicate that in practice, civil structures should be monitored for at least one full cycle of in-service environmental changes before establishing baselines for condition monitoring or calibrating finite-element models. Boundary conditions deserve special attention.

  12. The Ĝ Infrared Search for Extraterrestrial Civilizations with Large Energy Supplies. I. Background and Justification

    Science.gov (United States)

    Wright, J. T.; Mullan, B.; Sigurdsson, S.; Povich, M. S.

    2014-09-01

    We motivate the Ĝ infrared search for extraterrestrial civilizations with large energy supplies. We discuss some philosophical difficulties of the search for extraterrestrial intelligence (SETI), and how communication SETI circumvents them. We review "Dysonian SETI," the search for artifacts of alien civilizations, and find that it is highly complementary to traditional communication SETI; the two together might succeed where either one alone has not. We discuss the argument of Hart that spacefaring life in the Milky Way should be either galaxy-spanning or non-existent, and examine a portion of his argument that we call the "monocultural fallacy." We discuss some rebuttals to Hart that invoke sustainability and predict long Galaxy colonization timescales. We find that the maximum Galaxy colonization timescale is actually much shorter than previous work has found (counter-arguments to Hart's thesis suffer from the monocultural fallacy. We extend Hart's argument to alien energy supplies and argue that detectably large energy supplies can plausibly be expected to exist because life has the potential for exponential growth until checked by resources or other limitations, and intelligence implies the ability to overcome such limitations. As such, if Hart's thesis is correct, then searches for large alien civilizations in other galaxies may be fruitful; if it is incorrect, then searches for civilizations within the Milky Way are more likely to succeed than Hart argued. We review some past Dysonian SETI efforts and discuss the promise of new mid-infrared surveys, such as that of WISE.

  13. Magnesium Diboride Superconducting Coils for Electric Propulsion Systems for Large Aircraft Project

    Data.gov (United States)

    National Aeronautics and Space Administration — For electric propulsion systems for large aircraft it is desirable to have very light weight electric motors. Cryogenic motors offer much lighter weight than...

  14. No Winglets: What a Drag...Argument for Adding Winglets to Large Air Force Aircraft

    Science.gov (United States)

    2008-01-01

    22134-5068 MASTER OF MILITARY STUDIES NO WINGLETS : WHAT A DRAG... ARGUMENT FOR ADDING WINGLETS TO LARGE AIR FORCE AIRCRAFT ,SUBMITTED IN PARTIAL...currently valid OMB control number. 1. REPORT DATE 2008 2. REPORT TYPE 3. DATES COVERED 00-00-2008 to 00-00-2008 4. TITLE AND SUBTITLE No Winglets ...What a Drag...Argument for Adding Winglets to Large Air Force Aircraft 5a. CONTRACT NUMBER 5b. GRANT NUMBER 5c. PROGRAM ELEMENT NUMBER 6. AUTHOR

  15. Civil Aircraft for the regular investigation of the atmosphere based on an instrumented container: The new CARIBIC system

    Directory of Open Access Journals (Sweden)

    C. A. M. Brenninkmeijer

    2007-09-01

    Full Text Available An airfreight container with automated instruments for measurement of atmospheric gases and trace compounds was operated on a monthly basis onboard a Boeing 767-300 ER of LTU International Airways during long-distance flights from 1997 to 2002 (CARIBIC, Civil Aircraft for Regular Investigation of the Atmosphere Based on an Instrument Container, http://www.caribic-atmospheric.com. Subsequently a more advanced system has been developed, using a larger capacity container with additional equipment and an improved inlet system. CARIBIC phase #2 was implemented on a new long-range aircraft type Airbus A340-600 of the Lufthansa German Airlines (Star Alliance in December 2004, creating a powerful flying observatory. The instrument package comprises detectors for the measurement of O3, total and gaseous H2O, NO and NOy, CO, CO2, O2, Hg, and number concentrations of sub-micrometer particles (>4 nm, >12 nm, and >18 nm diameter. Furthermore, an optical particle counter (OPC and a proton transfer mass spectrometer (PTR-MS are incorporated. Aerosol samples are collected for analysis of elemental composition and particle morphology after flight. Air samples are taken in glass containers for laboratory analyses of hydrocarbons, halocarbons and greenhouse gases (including isotopic composition of CO2 in several laboratories. Absorption tubes collect oxygenated volatile organic compounds. Three differential optical absorption spectrometers (DOAS with their telescopes mounted in the inlet system measure atmospheric trace gases such as BrO, HONO, and NO2. A video camera mounted in the inlet provides information about clouds along the flight track. The flying observatory, its equipment and examples of measurement results are reported.

  16. Civil Aircraft for the regular investigation of the atmosphere based on an instrumented container: The new CARIBIC system

    Science.gov (United States)

    Brenninkmeijer, C. A. M.; Crutzen, P.; Boumard, F.; Dauer, T.; Dix, B.; Ebinghaus, R.; Filippi, D.; Fischer, H.; Franke, H.; Frieß, U.; Heintzenberg, J.; Helleis, F.; Hermann, M.; Kock, H. H.; Koeppel, C.; Lelieveld, J.; Leuenberger, M.; Martinsson, B. G.; Miemczyk, S.; Moret, H. P.; Nguyen, H. N.; Nyfeler, P.; Oram, D.; O'Sullivan, D.; Penkett, S.; Platt, U.; Pupek, M.; Ramonet, M.; Randa, B.; Reichelt, M.; Rhee, T. S.; Rohwer, J.; Rosenfeld, K.; Scharffe, D.; Schlager, H.; Schumann, U.; Slemr, F.; Sprung, D.; Stock, P.; Thaler, R.; Valentino, F.; van Velthoven, P.; Waibel, A.; Wandel, A.; Waschitschek, K.; Wiedensohler, A.; Xueref-Remy, I.; Zahn, A.; Zech, U.; Ziereis, H.

    2007-09-01

    An airfreight container with automated instruments for measurement of atmospheric gases and trace compounds was operated on a monthly basis onboard a Boeing 767-300 ER of LTU International Airways during long-distance flights from 1997 to 2002 (CARIBIC, Civil Aircraft for Regular Investigation of the Atmosphere Based on an Instrument Container, http://www.caribic-atmospheric.com). Subsequently a more advanced system has been developed, using a larger capacity container with additional equipment and an improved inlet system. CARIBIC phase #2 was implemented on a new long-range aircraft type Airbus A340-600 of the Lufthansa German Airlines (Star Alliance) in December 2004, creating a powerful flying observatory. The instrument package comprises detectors for the measurement of O3, total and gaseous H2O, NO and NOy, CO, CO2, O2, Hg, and number concentrations of sub-micrometer particles (>4 nm, >12 nm, and >18 nm diameter). Furthermore, an optical particle counter (OPC) and a proton transfer mass spectrometer (PTR-MS) are incorporated. Aerosol samples are collected for analysis of elemental composition and particle morphology after flight. Air samples are taken in glass containers for laboratory analyses of hydrocarbons, halocarbons and greenhouse gases (including isotopic composition of CO2) in several laboratories. Absorption tubes collect oxygenated volatile organic compounds. Three differential optical absorption spectrometers (DOAS) with their telescopes mounted in the inlet system measure atmospheric trace gases such as BrO, HONO, and NO2. A video camera mounted in the inlet provides information about clouds along the flight track. The flying observatory, its equipment and examples of measurement results are reported.

  17. Aircraft

    Science.gov (United States)

    Hibbs, Bart D.; Lissaman, Peter B. S.; Morgan, Walter R.; Radkey, Robert L.

    1998-01-01

    This disclosure provides a solar rechargeable aircraft that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Travelling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing's top surface, the aircraft uses only differential thrust of its eight propellers to turn. Each of five sections of the wing has one or more engines and photovoltaic arrays, and produces its own lift independent of the other sections, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft is capable of a top speed of about ninety miles per hour, which enables the aircraft to attain and can continuously maintain altitudes of up to sixty-five thousand feet. Regenerative fuel cells in the wing store excess electricity for use at night, such that the aircraft can sustain its elevation indefinitely. A main spar of the wing doubles as a pressure vessel that houses hydrogen and oxygen gasses for use in the regenerative fuel cell. The aircraft has a wide variety of applications, which include weather monitoring and atmospheric testing, communications, surveillance, and other applications as well.

  18. Aircraft

    Science.gov (United States)

    Hibbs, B.D.; Lissaman, P.B.S.; Morgan, W.R.; Radkey, R.L.

    1998-09-22

    This disclosure provides a solar rechargeable aircraft that is inexpensive to produce, is steerable, and can remain airborne almost indefinitely. The preferred aircraft is a span-loaded flying wing, having no fuselage or rudder. Travelling at relatively slow speeds, and having a two-hundred foot wingspan that mounts photovoltaic cells on most all of the wing`s top surface, the aircraft uses only differential thrust of its eight propellers to turn. Each of five sections of the wing has one or more engines and photovoltaic arrays, and produces its own lift independent of the other sections, to avoid loading them. Five two-sided photovoltaic arrays, in all, are mounted on the wing, and receive photovoltaic energy both incident on top of the wing, and which is incident also from below, through a bottom, transparent surface. The aircraft is capable of a top speed of about ninety miles per hour, which enables the aircraft to attain and can continuously maintain altitudes of up to sixty-five thousand feet. Regenerative fuel cells in the wing store excess electricity for use at night, such that the aircraft can sustain its elevation indefinitely. A main spar of the wing doubles as a pressure vessel that houses hydrogen and oxygen gases for use in the regenerative fuel cell. The aircraft has a wide variety of applications, which include weather monitoring and atmospheric testing, communications, surveillance, and other applications as well. 31 figs.

  19. Optimization Based Clearance of Flight Control Laws A Civil Aircraft Application

    CERN Document Server

    Hansson, Anders; Puyou, Guilhem

    2012-01-01

    This book summarizes the main achievements of the EC funded 6th Framework Program project COFCLUO – Clearance of Flight Control Laws Using Optimization. This project successfully contributed to the achievement of a top-level objective to meet society’s needs for a more efficient, safer and environmentally friendly air transport by providing new techniques and tools for the clearance of flight control laws. This is an important part of the certification and qualification process of an aircraft – a costly and time-consuming process for the aeronautical industry.   The overall objective of the COFCLUO project was to develop and apply optimization techniques to the clearance of flight control laws in order to improve efficiency and reliability. In the book, the new techniques are explained and benchmarked against traditional techniques currently used by the industry. The new techniques build on mathematical criteria derived from the certification and qualification requirements together with suitable models...

  20. 民机典型前缘结构抗鸟撞分析研究%Study of Bird Impact Resistance for Typical Civil Aircraft Leading Edge Structure

    Institute of Scientific and Technical Information of China (English)

    何瑞

    2013-01-01

    为保障飞行安全,CCAR25部对民机结构抗鸟撞性能提出了严格的指令性要求,须对机翼前缘、平尾前缘和垂尾前缘等典型前缘结构进行鸟撞分析。鸟撞分析涉及到结构的动力学分析、鸟体的本构关系模拟、材料的高速非线性效应以及结构大变形等多方面因素的影响,相关的计算复杂,会耗费结构设计人员大量的精力和时间。通过采用经验公式和仿真分析方法对前缘结构抗鸟撞性能进行快速的分析,可达到对结构的抗鸟撞能力进行快速预估并从而指导设计的目的。%For flying safety, leading edge structures include wing leading edge horizontal leading edge and vertical leading edge, which are very typical structures in civil aircraft. Bird impact analysis has relations with the structure dynamic analysis the physical model of bird the high speed non-linear influences of material and the structure large displacements. It will cost many energies and much time to accurately analyze bird impact resistance's properties of the structure, and will reduce the work efficiency. In the paper, experienced formula and simulation to quickly an-alyze the bird impact resistance of the aircraft leading edge is employed, then according to the analysis estimates the structure's bird impact resistance, finally depending on the estimation we can quickly revise the design to achieve the aim at the analysis guiding design.

  1. Overview of NASA Electrified Aircraft Propulsion Research for Large Subsonic Transports

    Science.gov (United States)

    Jansen, Ralph H.; Bowman, Cheryl; Jankovsky, Amy; Dyson, Rodger; Felder, James

    2017-01-01

    NASA is investing in Electrified Aircraft Propulsion (EAP) research as part of the portfolio to improve the fuel efficiency, emissions, and noise levels in commercial transport aircraft. Turboelectric, partially turboelectric, and hybrid electric propulsion systems are the primary EAP configurations being evaluated for regional jet and larger aircraft. The goal is to show that one or more viable EAP concepts exist for narrow body aircraft and mature tall-pole technologies related to those concepts. A summary of the aircraft system studies, technology development, and facility development is provided. The leading concept for mid-term (2035) introduction of EAP for a single aisle aircraft is a tube and wing, partially turbo electric configuration (STARC-ABL), however other viable configurations exist. Investments are being made to raise the TRL level of light weight, high efficiency motors, generators, and electrical power distribution systems as well as to define the optimal turbine and boundary layer ingestion systems for a mid-term tube and wing configuration. An electric aircraft power system test facility (NEAT) is under construction at NASA Glenn and an electric aircraft control system test facility (HEIST) is under construction at NASA Armstrong. The correct building blocks are in place to have a viable, large plane EAP configuration tested by 2025 leading to entry into service in 2035 if the community chooses to pursue that goal.

  2. 民用飞机预研项目存在问题及对策%Problems and Countermeasures in Advanced Research Projects for Civil Aircraft Technology

    Institute of Scientific and Technical Information of China (English)

    舒秀丽

    2015-01-01

    In this paper, three common problems are pointed out and dissected in advanced research projects for civil aircraft technology in China and three corresponding countermeasures being successfully implemented are pro-posed. These countermeasures are:establishment and application of innovation information repository supporting the setting-up of advanced research projects to reflect correct demand traction, effective formation and operation of the Integrated Project Team for effective project implementation and enhanced Technology Readiness Assessment promo-ting the application of research achievements. Good results of the application of the above-mentioned countermeas-ures are being achieved in the setting-up and implementation of three "serialized" advanced civil aircraft cockpit technology research projects, which break through the bottleneck of the advanced researches' leading and support-ing role to civil aircraft product development and provide a reference to advanced research projects in other indus-tries as well as in different civil aircraft technical fields.%指出我国民用飞机预研项目常见的三类问题并加以剖析,相应提出三项对策付诸实践:建创新信息库助正确需求牵引,组综合项目团队( IPT)助预研高效实施,抓技术成熟度评估( TRA)促研究成果应用. 上述对策在民用飞机驾驶舱技术领域三个系列化预研项目的立项和实施中显现成效,突破制约民用飞机预研引领和支撑民用飞机产品研发的瓶颈,可供民用飞机各技术领域和其他产业的预研项目借鉴.

  3. Civil Aircraft Operate in Cold Weather%民航飞机在寒冷天气下的运行

    Institute of Scientific and Technical Information of China (English)

    韩军

    2014-01-01

    寒冷天气对民航运行的威胁与危害是不容忽视的。该文就如何在寒冷天气下运行,进行了详细的分析与论述。首先提出了机场的保障能力和法规有待完善。然后阐述了飞机在寒冷天气下除冰,防冰的原因及原理。最后列出了机组在寒冷天气下运行需要注意的重要事项。%Threats and hazards of cold weather for civil aviation operation can not be ignored. This article on how to run in cold weather, carry out a detailed analysis and discussion. First proposed the airport security capabilities and regulations need to be im-proved. And then expounds the reason and principle of the aircraft deicing and anti-icing in cold weather. Finally, lists the impor-tant matters for the flight crew ,which need to be attention during operation in cold weather.

  4. 民用飞机蓄电池选型浅析%Analysis for Battery Category Selection of Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    魏娟

    2015-01-01

    The function and category of batteries on civil aircraft are introduced in this article. The differences between Nickel-cadmium Battery and Lithium-Ion Battery on power density, charge/discharge characteristics, maintainability, service life, safety, economical efficiency and airworthiness are also analyzed. The result shows that the Lithium-Ion Battery has superior power density and charge/discharge characteristics, while Nickel-cadmium Battery is predominant in maintainability, service life, safety, economical efficiency and airworthiness based on its mature usage.%介绍了当前民用飞机蓄电池的主要功能和类型,对比分析了镍镉蓄电池和锂离子蓄电池在功率密度、充放电特性、维护性、使用寿命、安全性、经济性以及适航性方面的差异,结果表明锂离子蓄电池在功率密度和充/放电特性方面明显占优势,而镍镉蓄电池电池由于其目前应用时间长,在维护性、寿命、安全性、经济性和适航性等方面具有优势。

  5. The Scientific Research Achievement Transformation in Civil Aircraft Devleopment%民机制造科研项目成果转化问题研究

    Institute of Scientific and Technical Information of China (English)

    王长法; 周竹维; 赵雄

    2013-01-01

    It is necessary for civil aircraft companies to transform the scientific achievement into production pow -er.Based on the concept description of scientific research achievement transformation , it defines the content of scientific research achievement transformation , proposes the status quo and characteristics of the scientific re-search achievement transformation in civil aircraft development , builds the model of scientific research achieve-ment transformation .This provides the technology innovation reference for the civil aircraft companies .%后发的民机制造企业只有将技术成果转化为现实生产力,才能不断提高其技术水平。首先对技术成果转化的概念进行了讨论,在此基础上界定了成果转化涉及的内容;其次对民机制造技术成果转化的现状及特点进行了介绍;然后对成果转化(或转移)进行了系统分析,在此基础上提出了成果转化的模型,为实现成果转化,最终为实现民机创新性技术进步提供一种有益的思考。

  6. Analysing the effects of rigid and flexible aircraft dynamics on the ejection of a large store

    CSIR Research Space (South Africa)

    Jamison, Kevin

    2011-09-01

    Full Text Available Aeronautical Systems Competency Defence, Peace, Safety and Security (DPSS) ANALYSING THE EFFECTS OF RIGID AND FLEXIBLE AIRCRAFT DYNAMICS ON THE EJECTION OF A LARGE STORE International Aerospace Symposium of South Africa 26 ? 28... & rigid aircraft dynamics on store release ? Closing the loop ? comparison with flight tests ? Conclusions ? CSIR 2011 Slide 3 Background to Hawk / Katleho project ? CSIR 2011 Slide 4 ? Katleho is a PGM under development by Denel Dynamics...

  7. The Gˆ Mid-Infrared Search for Extraterrestrial Civilizations with Large Power Supplies: First Results

    Science.gov (United States)

    Povich, M. S.; Wright, J. T.; Griffith, R.; Sigurdsson, S.; Maldonado, J. T.; Mullan, B.

    2014-03-01

    We present initial results from the Glimpsing Heat from Alien Technologies ("G-HAT" or Gˆ), in which we use the WISE all-sky mid-infrared (MIR) Source Catalog to search for and place constraints on the abundance of extraterrestrial civilizations with large power supplies. A civilization consuming a significant fraction of the luminous power of their host star (Kardashev type II civilization or K2; Kardashev 1964) or galaxy (K3) and operating at a temperature similar to the equilibrium temperatures in or near stellar habitable zones will produce MIR excess emission in the form of waste heat. Searches for such MIR excesses from K2s have been performed in the past, notably by Carrigan (2009) using the IRAS source catalog. Taking advantage of the 103 improvement in sensitivity over IRAS provided by WISE, Gˆ has enabled the first systematic search for waste heat from galaxy-spanning K3 civilizations and will search for K2s throughout a significant fraction of the Milky Way's volume. We find that a galaxy-spanning (K III) civilization with an power supply of more than about one percent of its stellar luminosity will have detectable mid-infrared excess. We have produced a catalog of 32,000 WISE extended sources and visually reviewed the data and literature on the reddest 4000 of them, identifying several hundred candidates worthy of detailed observational follow-up. Mid-infrared spectra, far-infrared photometry, and radio emission from CO could be used to distinguish extraterrestrial mid-infrared radiation from dust. We will extend this analysis to WISE point sources to search for K2s.

  8. Matching design for payload and range of civil aircraft family%民用飞机系列商载航程匹配设计

    Institute of Scientific and Technical Information of China (English)

    蒙文巩; 马东立; 崔飞

    2013-01-01

    There has been a pattern transform from single model to family with multiple models for the civil aircraft-developing concept. According to the strategies of modularization and generality, the aircraft family design method was developed. The design principle of the main parameters and the economic description method for the aircraft family were presented. Then the matching design model for payload and range of the aircraft family was established. The impact of the matching relationship of the payload and the range acting on the economy of the aircraft family was analyzed, too. With application of Pareto multi-objective genetic algorithm, the matching design for payload and range of a civil aircraft family was accomplished. The parameter comparison of different design schemes was carried out,and the results are satisfactory.%民用飞机产品开发的模式已从“单型飞机”的概念向“飞机系列”概念转化.根据模块化和通用性的策略,发展了飞机系列化设计方法,给出了飞机系列主要参数的设计原则和飞机系列经济性的描述方法,建立了飞机系列商载航程匹配设计模型.分析了商载和航程的匹配关系对飞机系列经济性的影响,利用Pareto多目标遗传算法,完成了某一民用飞机系列商载和航程的匹配设计,对不同设计方案的参数进行了比较分析,取得了较好的设计结果.

  9. The Application of Requirements Management in Civil Aircraft Development%大型客机设计中的需求管理

    Institute of Scientific and Technical Information of China (English)

    郭博智; 李浩敏

    2013-01-01

    The requirements development and requirements management, including the requirement capture, re-quirement analysis, requirement definition, requirement validation and requirement management, are introduced. According the civil aircraft development needs, the effect and importance of the implementation of requirements management in civil aircraft development are depicted. The requirements management process definition, require-ments management strategy, requirement validation and verification etc in civil aircraft development are introduced. It shows that it's effective to improve the correctness, completeness and coordination of requirements by conducting requirements management in civil aircraft development, and it's helpful to ensure all the development activities con-sistent with the original requirements. Resultant, the civil aircraft development, market, and commercial success can be achieved.%介绍了需求开发和需求管理的基本概念,说明了需求捕获、需求分析、需求定义、需求确认以及需求管理的具体内容。结合大型客机的设计研制特点,阐述了在大型客机设计中开展需求管理工作的重要作用与意义,重点介绍大型客机需求管理流程定义、需求管理策略、需求确认与验证等内容。实践证明,在大型客机设计中实施需求管理工作、实现需求的规范化与精细化管理,可有效提高需求的正确性、完整性和协调性,并确保设计结果与需求之间的一致性,促进大型客机的研制、市场和商业成功。

  10. The Ĝ infrared search for extraterrestrial civilizations with large energy supplies. I. Background and justification

    Energy Technology Data Exchange (ETDEWEB)

    Wright, J. T.; Mullan, B.; Sigurdsson, S. [Department of Astronomy and Astrophysics, 525 Davey Lab, The Pennsylvania State University, University Park, PA 16802 (United States); Povich, M. S. [Department of Physics and Astronomy, California State Polytechnic University, Pomona, 3801 West Temple Avenue, Pomona, CA 91768 (United States)

    2014-09-01

    We motivate the Ĝ infrared search for extraterrestrial civilizations with large energy supplies. We discuss some philosophical difficulties of the search for extraterrestrial intelligence (SETI), and how communication SETI circumvents them. We review 'Dysonian SETI', the search for artifacts of alien civilizations, and find that it is highly complementary to traditional communication SETI; the two together might succeed where either one alone has not. We discuss the argument of Hart that spacefaring life in the Milky Way should be either galaxy-spanning or non-existent, and examine a portion of his argument that we call the 'monocultural fallacy'. We discuss some rebuttals to Hart that invoke sustainability and predict long Galaxy colonization timescales. We find that the maximum Galaxy colonization timescale is actually much shorter than previous work has found (<10{sup 9} yr), and that many 'sustainability' counter-arguments to Hart's thesis suffer from the monocultural fallacy. We extend Hart's argument to alien energy supplies and argue that detectably large energy supplies can plausibly be expected to exist because life has the potential for exponential growth until checked by resources or other limitations, and intelligence implies the ability to overcome such limitations. As such, if Hart's thesis is correct, then searches for large alien civilizations in other galaxies may be fruitful; if it is incorrect, then searches for civilizations within the Milky Way are more likely to succeed than Hart argued. We review some past Dysonian SETI efforts and discuss the promise of new mid-infrared surveys, such as that of WISE.

  11. The \\^G Infrared Search for Extraterrestrial Civilizations with Large Energy Supplies. I. Background and Justification

    CERN Document Server

    Wright, J T; Sigurðsson, S; Povich, M S

    2014-01-01

    We motivate the \\^G infrared search for extraterrestrial civilizations with large energy supplies. We discuss some philosophical difficulties of SETI, and how communication SETI circumvents them. We review "Dysonian SETI", the search for artifacts of alien civilizations, and find that it is highly complementary to traditional communication SETI; the two together might succeed where either one, alone, has not. We discuss the argument of Hart (1975) that spacefaring life in the Milky Way should be either galaxy-spanning or non-existent, and examine a portion of his argument that we dub the "monocultural fallacy". We discuss some rebuttals to Hart that invoke sustainability and predict long Galaxy colonization timescales. We find that the maximum Galaxy colonization timescale is actually much shorter than previous work has found ($< 10^9$ yr), and that many "sustainability" counter-arguments to Hart's thesis suffer from the monocultural fallacy. We extend Hart's argument to alien energy supplies, and argue th...

  12. Analysis of impact of large commercial aircraft on a prestressed containment building

    Energy Technology Data Exchange (ETDEWEB)

    Lee, Kyoungsoo, E-mail: kylee@pvamu.edu [Center for Energy and Environmental Sustainability, Prairie View A and M University, Prairie view, TX, 77446 (United States); Han, Sang Eul, E-mail: hsang@inha.ac.kr [Department of Architectural Engineering, School of Architecture, Inha University, 253 Yonghyundong Nam-gu, Incheon, 402-751 (Korea, Republic of); Hong, Jung-Wuk, E-mail: j.hong@kaist.ac.kr [Department of Civil and Environmental Engineering, KAIST, 373-1 Guseon-dong, Yuseong-gu, Daejeon, 305-701 (Korea, Republic of)

    2013-12-15

    Highlights: • Aircraft impact analyses are performed using the missile–target interaction method. • A large commercial B747 aircraft is considered with erosion effect. • The rigid wall impact test shows the validity of the developed aircraft model. • The parametric studies on the fictitious containment building are performed. • The plastic failure of the target is governed by the impulse of aircraft at the first momentum peak. - Abstract: In this paper, the results of nonlinear dynamic analyses of a concrete containment building under extreme loads are presented. The impact of a large commercial B747 airliner is investigated as the extreme load, and a rigid wall impact test is performed using commercial nonlinear finite element codes. The impact forces exerted by the aircraft are verified compared with the time-dependent impact force provided by OECD/NEA (2002), which was calculated based on the so-called Riera method. The rigid wall impact analysis shows that the finite element model of a B747 is appropriate for the purpose of the aircraft crash analysis exposed to the external hazard of “Beyond Design-Basis Events” defined by U.S. Nuclear Regulatory Commission. Finally, the applicability of this methodology is further studied and verified by conducting parametric studies on the critical infrastructures of nuclear power plant containment structures.

  13. Development of pressure containment and damage tolerance technology for composite fuselage structures in large transport aircraft

    Science.gov (United States)

    Smith, P. J.; Thomson, L. W.; Wilson, R. D.

    1986-01-01

    NASA sponsored composites research and development programs were set in place to develop the critical engineering technologies in large transport aircraft structures. This NASA-Boeing program focused on the critical issues of damage tolerance and pressure containment generic to the fuselage structure of large pressurized aircraft. Skin-stringer and honeycomb sandwich composite fuselage shell designs were evaluated to resolve these issues. Analyses were developed to model the structural response of the fuselage shell designs, and a development test program evaluated the selected design configurations to appropriate load conditions.

  14. 民用飞机设计驾驶舱操纵设备的评估%Evaluation on Flight Cockpit Control Equipments of Civil Aircraft Design

    Institute of Scientific and Technical Information of China (English)

    丰立东; 赵京洲; 田金强

    2013-01-01

    人机工效影响着飞行员操纵飞机的感受,因此在民用飞机设计过程中,对人机工效进行及早考虑是非常重要的。在民用飞机设计的各个阶段,都需要适时邀请具有一定资质的飞行员对驾驶舱的人机工效进行评估。对民用飞机设计中飞控驾驶舱飞行员评估方法进行介绍,对评估的要点进行总结分析,供相关工程设计人员参考。%Human factors affect the feeling of pilots operating airplanes. It is necessary to take human factors into account at the beginning of designing civil aircraft. During each phase of designing civil aircraft, it is necessary to invite qualified pilots to evaluate human factors in cockpit when needed. A method of pilot evaluation related with flight cockpit control system in designing civil airplane is introduced and some important issues are summarized and analyzed so as to refer to other relevant engineers and designers when necessary.

  15. Aircraft noise monitoring hardware platform design based on software radio technology at civil airport%基于软件无线电的民用机场航空器噪声监测硬件平台设计

    Institute of Scientific and Technical Information of China (English)

    魏麟; 李忠良; 王冲; 刘晔璐

    2016-01-01

    Civil aircraft noise is a major factor in the civil airport noise. For the civil aviation airport noise characteristics, a concrete realization of airport noise signal monitoring and processing center hardware platform architecture is proposed. By using high-speed large-capacity FPGA programmable logic devices, PowerPC embedded processors, PCI-e, and SRIO (RapidIO) high-speed IO technology, constructed based on software radio technology hardware platform to achieve a higher real-time processing and monitoring platform highly reconfigurable.%民用航空器噪声是民用机场噪声的主要因素。针对民用机场航空器噪声的特点,提出了一种具体实现民用机场航空器噪声信号监测及处理中心的硬件平台架构。通过使用高速大容量FPGA可编程逻辑器件、PowerPC嵌入式处理器、PCI-e和SRIO(RapidIO)高速IO技术,构建了基于软件无线电技术的硬件平台,实现了监测平台的较高实时处理能力和高度可重构性。

  16. The \\^G Infrared Search for Extraterrestrial Civilizations with Large Energy Supplies. II. Framework, Strategy, and First Result

    CERN Document Server

    Wright, J T; Sigurðsson, S; Povich, M S; Mullan, B

    2014-01-01

    We describe the framework and strategy of the \\^G infrared search for extraterrestrial civilizations with large energy supplies, which will use the wide-field infrared surveys of WISE and Spitzer to search for these civilizations' waste heat. We develop a formalism for translating mid-infrared photometry into quantitative upper limits on extraterrestrial energy supplies. We discuss the likely sources of false positives, how dust can and will contaminate our search, and prospects for distinguishing dust from alien waste heat. We argue that galaxy-spanning civilizations may be easier to distinguish from natural sources than circumstellar civilizations (i.e., Dyson spheres), although Gaia will significantly improve our capability to identify the latter. We present a "zeroth order" null result of our search based on the WISE all-sky catalog: we show, for the first time, that Kardashev Type III civilizations (as Kardashev originally defined them) are very rare in the local universe. More sophisticated searches can...

  17. Application of Reliability Design in Civil Aircraft Environment Control System%可靠性设计在民用飞机环控系统中的应用

    Institute of Scientific and Technical Information of China (English)

    闫旭东

    2016-01-01

    民用飞机环控系统可靠性设计的目标是保证飞机达到规定的可靠性定量指标和定性要求,以提高飞机的可靠度,降低运营费用,使飞机具有良好的经济性和市场竞争能力。民用飞机环控系统在设计中大量采用了冗余设计、成熟技术及标准化设计等设计手段,以保证飞机的可靠性和安全性。通过可靠性分析验证飞机平均故障间隔时间和签派可靠度是否满足环控系统设计要求。%The purpose of the reliability design on civil aircraft environment control system is to ensure the aircraft meet the qualitative and quantitative reliability requirements, reduce the cost in working, and to make better eco-nomical and compete ability. In order to ensure the reliability and safety, a fairly large number of technology are used in aircraft environment control system design, redundancy design, mature technology and standardization de-sign . Reliability analysis is used to validate whether mean time between failures and dispatch reliability meet the re-quirement.

  18. 民用飞机阵风载荷及减缓技术的研究%esearch on Gust Load and its Load Alleviation Technology of Civil Aircrafts

    Institute of Scientific and Technical Information of China (English)

    赵继伟; 胡赞远

    2012-01-01

    Due to the characteristic of large ratio wing of civil aircrafts, gust load often composes of the severe conditions of civil aircrafts. And it must be emphasized by all countries' airworthiness regulations. Moreover, owing to the elasticity of the aircraft structure, gust disturbance induces the elastic vibrations, reduces the structure stress, produces the fatigue damage, and even promote flutter. Thus it is of very importance and significance to investigate and research in gust load and gust load alleviation technologies in flight load design. This paper gives a brief introduction of gust load theories and the relevant technologies and also puts forward a type of gust load alleviation of method direct lift control to carry out gust load alleviation of the wing.%由于民用飞机机翼具有大展弦比的特点,因此阵风载荷经常成为民用飞机飞行载荷的严重情况,是各国适航标准重点考察的飞行情况。而且,阵风干扰还会因飞机机体的自身弹性引起结构弹性振动,使飞机结构刚度降低,造成机体疲劳损伤,甚至引起颤振。因此,在民用飞机载荷设计过程中对阵风载荷及其减缓技术进行研究具有非常重要的意义。介绍了民用飞机阵风载荷的原理及相关技术,以及阵风载荷减缓技术中用直接升力控制方法来实现机翼的阵风载荷减缓。

  19. ShakeNet: a portable wireless sensor network for instrumenting large civil structures

    Science.gov (United States)

    Kohler, Monica D.; Hao, Shuai; Mishra, Nilesh; Govindan, Ramesh; Nigbor, Robert

    2015-08-03

    We report our findings from a U.S. Geological Survey (USGS) National Earthquake Hazards Reduction Program-funded project to develop and test a wireless, portable, strong-motion network of up to 40 triaxial accelerometers for structural health monitoring. The overall goal of the project was to record ambient vibrations for several days from USGS-instrumented structures. Structural health monitoring has important applications in fields like civil engineering and the study of earthquakes. The emergence of wireless sensor networks provides a promising means to such applications. However, while most wireless sensor networks are still in the experimentation stage, very few take into consideration the realistic earthquake engineering application requirements. To collect comprehensive data for structural health monitoring for civil engineers, high-resolution vibration sensors and sufficient sampling rates should be adopted, which makes it challenging for current wireless sensor network technology in the following ways: processing capabilities, storage limit, and communication bandwidth. The wireless sensor network has to meet expectations set by wired sensor devices prevalent in the structural health monitoring community. For this project, we built and tested an application-realistic, commercially based, portable, wireless sensor network called ShakeNet for instrumentation of large civil structures, especially for buildings, bridges, or dams after earthquakes. Two to three people can deploy ShakeNet sensors within hours after an earthquake to measure the structural response of the building or bridge during aftershocks. ShakeNet involved the development of a new sensing platform (ShakeBox) running a software suite for networking, data collection, and monitoring. Deployments reported here on a tall building and a large dam were real-world tests of ShakeNet operation, and helped to refine both hardware and software. 

  20. Study on the Forecast Method of Market Demand for Civil Aircraft%民用飞机市场需求预测方法研究

    Institute of Scientific and Technical Information of China (English)

    王晶

    2013-01-01

    民用飞机市场预测包含需求(航空运量)预测和供应(飞机机队)预测两个部分,其中需求预测为自上而下的预测,是对航空市场宏观运量进行分析和预测,这部分预测在预测模型中起着非常重要的作用。针对民用飞机市场需求预测方法和流程进行了详细的论述,该方法是大型客机市场预测和市场研究工作的基础。%The civil aircraft market forecast includes two parts:demand( aviation traffic) forecast and supply( air-craft fleet) forecast. The demand forecast is top-down forecast, which is the analysis and forecast of aviation market macroscopic traffic, and this part of forecast is very important role in the forecast model. The forecast method and process of market demand for civil aviation are discussed in detail in this paper. The method is the basic of market forecast and market research for commercial airliner.

  1. Exploring Advanced Technology Gas Turbine Engine Design and Performance for the Large Civil Tiltrotor (LCTR)

    Science.gov (United States)

    Snyder, Christopher A.

    2014-01-01

    A Large Civil Tiltrotor (LCTR) conceptual design was developed as part of the NASA Heavy Lift Rotorcraft Systems Investigation in order to establish a consistent basis for evaluating the benefits of advanced technology for large tiltrotors. The concept has since evolved into the second-generation LCTR2, designed to carry 90 passengers for 1,000 nautical miles at 300 knots, with vertical takeoff and landing capability. This paper explores gas turbine component performance and cycle parameters to quantify performance gains possible for additional improvements in component and material performance beyond those identified in previous LCTR2 propulsion studies and to identify additional research areas. The vehicle-level characteristics from this advanced technology generation 2 propulsion architecture will help set performance levels as additional propulsion and power systems are conceived to meet ever-increasing requirements for mobility and comfort, while reducing energy use, cost, noise and emissions. The Large Civil Tiltrotor vehicle and mission will be discussed as a starting point for this effort. A few, relevant engine and component technology studies, including previous LCTR2 engine study results will be summarized to help orient the reader on gas turbine engine architecture, performance and limitations. Study assumptions and methodology used to explore engine design and performance, as well as assess vehicle sizing and mission performance will then be discussed. Individual performance for present and advanced engines, as well as engine performance effects on overall vehicle size and mission fuel usage, will be given. All results will be summarized to facilitate understanding the importance and interaction of various component and system performance on overall vehicle characteristics.

  2. A Vision-Based Dynamic Rotational Angle Measurement System for Large Civil Structures

    Directory of Open Access Journals (Sweden)

    Jong-Jae Lee

    2012-05-01

    Full Text Available In this paper, we propose a vision-based rotational angle measurement system for large-scale civil structures. Despite the fact that during the last decade several rotation angle measurement systems were introduced, they however often required complex and expensive equipment. Therefore, alternative effective solutions with high resolution are in great demand. The proposed system consists of commercial PCs, commercial camcorders, low-cost frame grabbers, and a wireless LAN router. The calculation of rotation angle is obtained by using image processing techniques with pre-measured calibration parameters. Several laboratory tests were conducted to verify the performance of the proposed system. Compared with the commercial rotation angle measurement, the results of the system showed very good agreement with an error of less than 1.0% in all test cases. Furthermore, several tests were conducted on the five-story modal testing tower with a hybrid mass damper to experimentally verify the feasibility of the proposed system.

  3. A vision-based dynamic rotational angle measurement system for large civil structures.

    Science.gov (United States)

    Lee, Jong-Jae; Ho, Hoai-Nam; Lee, Jong-Han

    2012-01-01

    In this paper, we propose a vision-based rotational angle measurement system for large-scale civil structures. Despite the fact that during the last decade several rotation angle measurement systems were introduced, they however often required complex and expensive equipment. Therefore, alternative effective solutions with high resolution are in great demand. The proposed system consists of commercial PCs, commercial camcorders, low-cost frame grabbers, and a wireless LAN router. The calculation of rotation angle is obtained by using image processing techniques with pre-measured calibration parameters. Several laboratory tests were conducted to verify the performance of the proposed system. Compared with the commercial rotation angle measurement, the results of the system showed very good agreement with an error of less than 1.0% in all test cases. Furthermore, several tests were conducted on the five-story modal testing tower with a hybrid mass damper to experimentally verify the feasibility of the proposed system.

  4. the Ĝ infrared search for extraterrestrial civilizations with large energy supplies. II. Framework, strategy, and first result

    Energy Technology Data Exchange (ETDEWEB)

    Wright, J. T.; Griffith, R. L.; Sigurdsson, S. [Department of Astronomy and Astrophysics, 525 Davey Lab, The Pennsylvania State University, University Park, PA, 16802 (United States); Povich, M. S. [Department of Physics and Astronomy, California State Polytechnic University, Pomona, 3801 West Temple Avenue, Pomona, CA 91768 (United States); Mullan, B. [Blue Marble Space Institution of Science, P.O. Box 85561, Seattle, WA 98145-1561 (United States)

    2014-09-01

    We describe the framework and strategy of the Ĝ infrared search for extraterrestrial civilizations with large energy supplies, which will use the wide-field infrared surveys of WISE and Spitzer to search for these civilizations' waste heat. We develop a formalism for translating mid-infrared photometry into quantitative upper limits on extraterrestrial energy supplies. We discuss the likely sources of false positives, how dust can and will contaminate our search, and prospects for distinguishing dust from alien waste heat. We argue that galaxy-spanning civilizations may be easier to distinguish from natural sources than circumstellar civilizations (i.e., Dyson spheres), although GAIA will significantly improve our capability to identify the latter. We present a zeroth order null result of our search based on the WISE all-sky catalog: we show, for the first time, that Kardashev Type III civilizations (as Kardashev originally defined them) are very rare in the local universe. More sophisticated searches can extend our methodology to smaller waste heat luminosities, and potentially entirely rule out (or detect) both Kardashev Type III civilizations and new physics that allows for unlimited 'free' energy generation.

  5. Epidemiological investigation on invasion situation of cockroaches in civil aircraft%民航客机蜚蠊侵害状况的流行病学调查

    Institute of Scientific and Technical Information of China (English)

    梁朝晖; 王锦平; 冯显炘; 彭伟年; 卢江民; 王晓雨; 林国川

    2016-01-01

    Objective To provide scientific evidence for studying biological characteristic of cockroaches and control countermeasures by investigating the species distribution and inroads situation of cockroaches in civil aircraft.Methods In August 2015,the onsite investigations were done for 19 A320 and A321 aircrafts harbored at Sanya airport and Haikou airport for getting the cockroach density.The difference of cockroache density was compared by aircraft type,aircraft age and the 4 areas of the aircraft.Results The total invasion rate was 84.21% on 19 aircrafts.Blauella germanica is the dominant specie.The invasion rates of cockroaches was not statistically significant neither by the comparison of aircraft type (x2 =1.362,P>0.05) nor by the comparison of aircraft age (x2=0.281,P > 0.05).But statistical significance on cockroaches density was found in the comparison of 4 areas of aircrafts (x2=14.629,P<0.01).Conclusions The comprehensive countermeasures,including environmental,physical and chemical controls,should be adopted according to the aircraft structure,operation and safety requirements.%目的 通过对民航客机蜚蠊种群分布及侵害情况的调查,为研究客机蜚蠊的生态特性及防治对策提供依据. 方法 2015年8月,采用现况调查的方法对三亚及海口机场的19架A320及A321客机进行蜚蠊密度监测;比较两种不同机型、不同机龄以及客机4个不同部位蜚蠊侵害情况. 结果 共调查19架客机,蜚蠊总侵害率为84.21%;客机蜚蠊以德国小蠊为优势种群.不同机型客机的蜚蠊侵害率差异无统计学意义(x2=1.362,P>0.05);不同机龄客机蜚蠊侵害率差异无统计学意义(x2 =0.281,P>0.05);客机不同部位蜚蠊密度差异有统计学意义(x2=14.629,P<0.01). 结论 应根据客机特殊的结构、运行特点、安全要求,并结合德国小蠊在客机上的分布特点,采取环境治理、物理防治、化学防治等综合防治措施.

  6. A new principle and device for large aircraft components gaining accurate support by ball joint

    Institute of Scientific and Technical Information of China (English)

    Bao-gui QIU; Jun-xia JIANG; Ying-lin KE

    2011-01-01

    How to obtain an accurate support for large components by ball joint is a key process in aircraft digital assembly. A novel principle and device is developed to solve the problem. Firstly, the working principle of the device is introduced. When three or four displacement sensors installed in the localizer are touched by the ball-head, the spatial relation is calculated between the large aircraft component's ball-head and the localizer's ball-socket. The localizer is driven to achieve a new position by compensation. Relatively, a support revising algorithm is proposed. The localizer's ball-socket approaches the ball-head based on the displacement sensors. According to the points selected from its spherical surface, the coordinates of ball-head spherical center are computed by geometry. Finally, as a typical application, the device is used to conduct a test-fuselage's ball-head into a localizer's ball-socket. Positional deviations of the spherical centers between the ball-head and the ball-socket in the x, y, and z directions are all controlled within ±0.05 mm under various working conditions. The results of the experiments show that the device has the characteristics of high precision, excellent stability, strong operability, and great potential to be applied widely in the modern aircraft industry.

  7. Dihedral influence on lateral-directional dynamic stability on large aspect ratio tailless flying wing aircraft

    Institute of Scientific and Technical Information of China (English)

    Song Lei; Yang Hua; Zhang Yang; Zhang Haoyu; Huang Jun

    2014-01-01

    The influence of dihedral layout on lateral-directional dynamic stability of the tailless flying wing aircraft is discussed in this paper. A tailless flying wing aircraft with a large aspect ratio is selected as the object of study, and the dihedral angle along the spanwise sections is divided into three segments. The influence of dihedral layouts is studied. Based on the stability derivatives cal-culated by the vortex lattice method code, the linearized small-disturbance equations of the lateral modes are used to determine the mode dynamic characteristics. By comparing 7056 configurations with different dihedral angle layouts, two groups of stability optimized dihedral layout concepts are created. Flight quality close to Level 2 requirements is achieved in these optimized concepts without any electric stability augmentation system.

  8. Conceptual Design of a Two Spool Compressor for the NASA Large Civil Tilt Rotor Engine

    Science.gov (United States)

    Veres, Joseph P.; Thurman, Douglas R.

    2010-01-01

    This paper focuses on the conceptual design of a two spool compressor for the NASA Large Civil Tilt Rotor engine, which has a design-point pressure ratio goal of 30:1 and an inlet weight flow of 30.0 lbm/sec. The compressor notional design requirements of pressure ratio and low-pressure compressor (LPC) and high pressure ratio compressor (HPC) work split were based on a previous engine system study to meet the mission requirements of the NASA Subsonic Rotary Wing Projects Large Civil Tilt Rotor vehicle concept. Three mean line compressor design and flow analysis codes were utilized for the conceptual design of a two-spool compressor configuration. This study assesses the technical challenges of design for various compressor configuration options to meet the given engine cycle results. In the process of sizing, the technical challenges of the compressor became apparent as the aerodynamics were taken into consideration. Mechanical constraints were considered in the study such as maximum rotor tip speeds and conceptual sizing of rotor disks and shafts. The rotor clearance-to-span ratio in the last stage of the LPC is 1.5% and in the last stage of the HPC is 2.8%. Four different configurations to meet the HPC requirements were studied, ranging from a single stage centrifugal, two axi-centrifugals, and all axial stages. Challenges of the HPC design include the high temperature (1,560deg R) at the exit which could limit the maximum allowable peripheral tip speed for centrifugals, and is dependent on material selection. The mean line design also resulted in the definition of the flow path geometry of the axial and centrifugal compressor stages, rotor and stator vane angles, velocity components, and flow conditions at the leading and trailing edges of each blade row at the hub, mean and tip. A mean line compressor analysis code was used to estimate the compressor performance maps at off-design speeds and to determine the required variable geometry reset schedules of the

  9. Introduction to civil aircraft optical fiber cable installation design requirements%浅谈民用飞机光缆安装设计要求

    Institute of Scientific and Technical Information of China (English)

    魏培坤

    2015-01-01

    Optical fiber communication compared with the traditional electrical communication has many advantages in terms of signal transmission; Optical fiber communication technology also has been widely used in civil aircraft, in this paper, the optical fiber cable installation design requirements are introduced to ensure the optical fiber communication function work normally during installation without damage.%光纤通信和传统电气通信相比在信号传输方面有许多优势,光纤通信技术在民用飞机上也得到了越来越多的应用,对光缆的安装设计要求进行了介绍,确保光缆在安装敷设过程中不会受到破坏以及保证光纤通信正常。

  10. 32 CFR 855.13 - Civil fly-ins.

    Science.gov (United States)

    2010-07-01

    ... 32 National Defense 6 2010-07-01 2010-07-01 false Civil fly-ins. 855.13 Section 855.13 National Defense Department of Defense (Continued) DEPARTMENT OF THE AIR FORCE AIRCRAFT CIVIL AIRCRAFT USE OF UNITED STATES AIR FORCE AIRFIELDS Civil Aircraft Landing Permits § 855.13 Civil fly-ins. (a)...

  11. Handling Qualities of a Large Civil Tiltrotor in Hover using Translational Rate Command

    Science.gov (United States)

    Malpica, Carlos A.; Theodore, Colin R.; Lawrence, Ben; Lindsey, James; Blanken, Chris

    2012-01-01

    A Translational Rate Command (TRC) control law has been developed to enable low speed maneuvering of a large civil tiltrotor with minimal pitch changes by means of automatic nacelle angle deflections for longitudinal velocity control. The nacelle actuator bandwidth required to achieve Level 1 handling qualities in hover and the feasibility of additional longitudinal cyclic control to augment low bandwidth nacelle actuation were investigated. A frequency-domain handling qualities criterion characterizing TRC response in terms of bandwidth and phase delay was proposed and validated against a piloted simulation conducted on the NASA-Ames Vertical Motion Simulator. Seven experimental test pilots completed evaluations in the ADS-33E-PRF Hover Mission Task Element (MTE) for a matrix of nacelle actuator bandwidths, equivalent rise times and control response sensitivities, and longitudinal cyclic control allocations. Evaluated against this task, longitudinal phase delay shows the Level 1 boundary is around 0.4 0.5 s. Accordingly, Level 1 handling qualities were achieved either with a nacelle actuator bandwidth greater than 4 rad/s, or by employing longitudinal cyclic control to augment low bandwidth nacelle actuation.

  12. Interior Noise Predictions in the Preliminary Design of the Large Civil Tiltrotor (LCTR2)

    Science.gov (United States)

    Grosveld, Ferdinand W.; Cabell, Randolph H.; Boyd, David D.

    2013-01-01

    A prediction scheme was established to compute sound pressure levels in the interior of a simplified cabin model of the second generation Large Civil Tiltrotor (LCTR2) during cruise conditions, while being excited by turbulent boundary layer flow over the fuselage, or by tiltrotor blade loading and thickness noise. Finite element models of the cabin structure, interior acoustic space, and acoustically absorbent (poro-elastic) materials in the fuselage were generated and combined into a coupled structural-acoustic model. Fluctuating power spectral densities were computed according to the Efimtsov turbulent boundary layer excitation model. Noise associated with the tiltrotor blades was predicted in the time domain as fluctuating surface pressures and converted to power spectral densities at the fuselage skin finite element nodes. A hybrid finite element (FE) approach was used to compute the low frequency acoustic cabin response over the frequency range 6-141 Hz with a 1 Hz bandwidth, and the Statistical Energy Analysis (SEA) approach was used to predict the interior noise for the 125-8000 Hz one-third octave bands.

  13. Defining Gas Turbine Engine Performance Requirements for the Large Civil TiltRotor (LCTR2)

    Science.gov (United States)

    Snyder, Christopher A.

    2013-01-01

    Defining specific engine requirements is a critical part of identifying technologies and operational models for potential future rotary wing vehicles. NASA's Fundamental Aeronautics Program, Subsonic Rotary Wing Project has identified the Large Civil TiltRotor (LCTR) as the configuration to best meet technology goals. This notional vehicle concept has evolved with more clearly defined mission and operational requirements to the LCTR-iteration 2 (LCTR2). This paper reports on efforts to further review and refine the LCTR2 analyses to ascertain specific engine requirements and propulsion sizing criteria. The baseline mission and other design or operational requirements are reviewed. Analysis tools are described to help understand their interactions and underlying assumptions. Various design and operational conditions are presented and explained for their contribution to defining operational and engine requirements. These identified engine requirements are discussed to suggest which are most critical to the engine sizing and operation. The most-critical engine requirements are compared to in-house NASA engine simulations to try to ascertain which operational requirements define engine requirements versus points within the available engine operational capability. Finally, results are summarized with suggestions for future efforts to improve analysis capabilities, and better define and refine mission and operational requirements.

  14. Large >60 gallon/day ‘pulse-tube’ oxygen liquefier for aircraft carriers

    Science.gov (United States)

    Spoor, P. S.

    2015-12-01

    An oxygen liquefier using a large ‘pulse-tube’ or acoustic-Stirling cryocooler is described, which has a liquefaction rate in excess of 60 gallons per day (227 liters per day) as measured by the increase in weight of a storage dewar, from <20 kWe input. Several of these systems will be deployed on U.S. Navy aircraft carriers to provide shipboard liquid oxygen. Paths to improvement in future systems are identified, although it is noted that since the present system exceeds the required specifications, these improvements may not be implemented in the near term.

  15. Safety assessment of A92 reactor building for large commercial aircraft crash

    Energy Technology Data Exchange (ETDEWEB)

    Kostov, M., E-mail: marin.kostov@riskeng.bg [Risk Engineering Ltd., Sofia (Bulgaria); Henkel, F.O. [Woelfel Beratende Ingenieure, Hoechberg (Germany); Andonov, A. [Risk Engineering Ltd., Sofia (Bulgaria)

    2014-04-01

    The current paper presents key elements of the comprehensive analyses of the effects due to a large aircraft collision with the reactor building of Belene NPP in Bulgaria. The reactor building is a VVER A92; it belongs to the third+ generation and includes structural measures for protection against an aircraft impact as standard design. The A92 reactor building implements a double shell concept and is composed of thick RC external walls and an external shell which surrounds an internal pre-stressed containment and the internal walls of the auxiliary building. The malevolent large aircraft impact is considered as a beyond design base accident (Design Extended Conditions, DEC). The main issues under consideration are the structural integrity, the equipment safety due to the induced vibrations, and the fire safety of the entire installation. Many impact scenarios are analyzed varying both impact locations and loading intensity. A large number of non-linear dynamic analyses are used for assessment of the structural response and capacity, including different type of structural models, different finite element codes, and different material laws. The corresponding impact loadings are represented by load time functions calculated according to three different approaches, i.e. loading determined by Riera's method (Riera, 1968), load time function calculated by finite element analysis (Henkel and Klein, 2007), and coupled dynamic analysis with dynamic interaction between target and projectile. Based on the numerical results and engineering assessments the capacity of the A92 reactor building to resist a malevolent impact of a large aircraft is evaluated. Significant efforts are spent on safety assessment of equipment by using an evaluation procedure based on damage indicating parameters. As a result of these analyses several design modifications of structure elements are performed. There are changes of the layout of reinforcement, special arrangements and spatial

  16. Analysis on the Wing Jacking Equipment of Civil Aircraft%民机机翼千斤顶顶升装置分析

    Institute of Scientific and Technical Information of China (English)

    薄晓莉

    2011-01-01

    Jacking condition must be considered when maintaining and replacing parts of a civil aircraft. In this paper, relevant airworthiness standards is be analyzed, and the advantages and disadvantages of the 13737 and A320 aircraft wing lifting devices is compared, through the force transmission analysis. Vertical component of the 13737 wing jacking load is home by the reinforcing rib and pass to the front spar, horizontal component is borne by the lower skin through the hearing. Vertical component of the A320 wing jacking load is home by the reinforcing rib and pass to the rear spar, horizontal component is borne by the lower skin and the reinforcing rib through the bearing. The aircraft wing jacking connection joints of 13737 is simple, but the force transmission of A320 aircraft wing lifting connection is clearer.%千斤顶顶升情况是民用飞机在进行维修、更换零部件时必须考虑的一个状态。对民机顶升的相关适航条款进行了理解;对B737及A320的机翼顶升装置进行了总结对比,通过传力分析,比较了其优缺点。两种机型的传力方式稍有不同:B737机翼顶升载荷的垂直分量由加强肋承担主要传递到前梁,水平分量通过挤压由下壁板承担;A320机翼顶升载荷的垂直分量由加强肋承担,主要传递到后梁,水平分量通过挤压由下壁板和加强肋承担。B737机翼顶升接头的连接方式操作简单,但A320机翼顶升接头传力路径更清晰。

  17. Effects of engine emissions from high-speed civil transport aircraft: A two-dimensional modeling study, part 2

    Science.gov (United States)

    Ko, Malcolm K. W.; Weisenstein, Debra K.; Sze, Nein Dak; Shia, Run-Lie; Rodriguez, Jose M.; Heisey, Curtis

    1991-01-01

    The AER two-dimensional chemistry-transport model is used to study the effect of supersonic and subsonic aircraft operation in the 2010 atmosphere on stratospheric ozone (O3). The results show that: (1) the calculated O3 response is smaller in the 2010 atmosphere compared to previous calculations performed in the 1980 atmosphere; (2) with the emissions provided, the calculated decrease in O3 column is less than 1 percent; and (3) the effect of model grid resolution on O3 response is small provided that the physics is not modified.

  18. Design and Development of Civil Aircraft Flight Performance Auxiliary Calculation System%民用飞机的飞机性能辅助计算系统设计与开发

    Institute of Scientific and Technical Information of China (English)

    褚双磊; 董奇; 刘子昂; 温瑞英

    2016-01-01

    The performance engineer's daily work in the airline is that making the low-speed performance analysis and route operation evaluation by the software performance corresponding to aircraft model,it has a large amount of daily performance calculation. The research is oriented by pre-flight performance assis-tant calculation of performance engineer, the aircraft performance auxiliary calculation software was de-signed and developed. First it established basic performance database of civil aircraft,including aerody-namic data and engine thrust data,the programming language was used in order to complete the primary basic performance calculation, senior professional performance calculation performance curves output of the three main module design,the daily work of the performance engineers achieved quick and simple cal-culation,it laid the data foundation for the follow-up aircraft professional performance calculation,at the same time,it can offer help for the daily performance training of flight dispatcher.%航空公司性能工程师的日常工作就是使用机型对应的飞机性能软件进行低速性能分析和航线评估,日常计算量很大.面向性能工程师的前期飞行性能辅助计算工作,设计并开发了一款飞机性能辅助计算软件,建立机型基础性能数据库,包含气动数据和发动机推力数据,采用编程语言依次完成初级基础性能计算、高级专业性能计算、性能曲线绘制3个主要模块设计、实现性能工程师日常工作的快捷和简便性计算,为后续专业飞机性能计算打下数据基础,同时也可以为飞行签派员的日常性能训练工作提供帮助.

  19. Evaluation of a large capacity heat pump concept for active cooling of hypersonic aircraft structure

    Science.gov (United States)

    Pagel, L. L.; Herring, R. L.

    1978-01-01

    Results of engineering analyses assessing the conceptual feasibility of a large capacity heat pump for enhancing active cooling of hypersonic aircraft structure are presented. A unique heat pump arrangement which permits cooling the structure of a Mach 6 transport to aluminum temperatures without the aid of thermal shielding is described. The selected concept is compatible with the use of conventional refrigerants, with Freon R-11 selected as the preferred refrigerant. Condenser temperatures were limited to levels compatible with the use of conventional refrigerants by incorporating a unique multipass condenser design, which extracts mechanical energy from the hydrogen fuel, prior to each subsequent pass through the condenser. Results show that it is technically feasible to use a large capacity heat pump in lieu of external shielding. Additional analyses are required to optimally apply this concept.

  20. 基于事故/事件的民机人因防错设计关键因素研究%Research on key factors of human error proofing design for civil aircraft based on accidents/incidents

    Institute of Scientific and Technical Information of China (English)

    高扬; 王向章; 李晓旭

    2015-01-01

    Aiming at the influence of human error proofing design for civil aircraft on flight safety, 92 typical acci-dents cases by human factors were selected from the world civil aviation safety accidents/incidents database.The element incident analysis method was applied to conduct deep analysis, then the important design factors which need to be considered in the human error proofing design for civil aircraft was summarized, and the important design factor set was established.Based on the man-machine-environment model in systems engineering, and combined with the relevant standards for aircrafts design at home and abroad, an index system of important factors about hu-man error proofing design for civil aircraft was built.The FAHP method was used to calculate the weight of inde-xes, and 14 key factors of human error proofing design that influence the flight safety were determined.Finally, the general requirements of human error proofing design for civil aircraft were proposed against the key factors.It can provide reference for the human error proofing design for civil aircraft to better meet the requirements of initial air-worthiness.%针对民机人因防错设计对飞行安全的影响,从世界民航安全事故/事件数据库中筛选出92起典型的人为因素事故案例,采用基元事件分析法进行深度分析,提炼出民机人因防错设计需要考虑的重要设计因素,并建立重要设计因素集。基于系统工程学的“人机环”模型,结合国内外飞机设计相关标准,建立民机人因防错设计重要因素指标体系。运用模糊层次分析法对因素指标进行权重计算,确立影响飞行安全的14项人因防错设计关键因素,并针对这些关键因素提出民机人因防错设计通用要求,以期为民机人因防错设计满足初始适航要求提供参考。

  1. Air Traffic Management: Civil/Military Systems and Technologies.

    Science.gov (United States)

    1980-02-01

    develops the- following functions: - data generation, row by row, of the ILP tableau ; - memorization of the coefficient matrix in a compact form...many people on bord or on the ground can be killed if a wide-bodied civil aircraft or an equivalent small military aircraft with large fuel capacity...ver a helicopter at nap-of-the-earth (NOE) altitudes to a distant destination. The source of this perceptual information (i.e., a pilotage system

  2. Approach of Improving the Inertial Navigation System Error for Large Transport Aircraft

    Institute of Scientific and Technical Information of China (English)

    WU Huzi; GENG Jianzhong; TANG Changhong; LI Wei

    2013-01-01

    The corresponding corrected method is proposed for the INS (INS-Inertial Navigation System) accumulated error of large transport aircraft.System errors contain aircraft position error,altitude error and speed error,one is increasing the accuracy of hardware; the other is development of low cost software algorithms.Because of improving hardware is more difficult in my country at present,developing software algorithms is essential way,which have been validated in my types of airplane.The combined heuristic algorithms (ABPNN,Advanced Back-propagation neural networks algorithm and LSM-least square method) are presented,which incorporates the effects of flight region and measured terrain height data by radar and barometer.Based on this algorithm,the appropriate match region was gotten by recognition of fiducial digital map in real time online.In process of work,the minimum of position error as a cost function and the constraint conditions are gave,the flight positions are recognized in real time and continuously,least sum of square is calculated based on LSM,in other words,the optimized result is obtained.The simulation case demonstrate that the method is very successful,the correct rate of recognition is more 90 percent.In words,the algorithm presented is economical,validation and effective.

  3. 民用飞机研制项目风险管理研究与应用%Research and Application of Risk Management in Civil Aircraft Development Project

    Institute of Scientific and Technical Information of China (English)

    卢新来; 丁常宏; 任长伟; 于晓伟

    2015-01-01

    民用飞机研制项目具有技术含量高、难度大、复杂度高、高投入、高风险、不确定性大等特点,在项目管理中引入风险管理对项目的顺利推进具有重要意义。在研究风险管理理论和流程的基础上,提出了民用飞机研制项目的风险识别方法和量化评估方法,建立了风险管理的组织结构和运行流程,给出了风险管理平台的系统架构和技术实现,开发的系统可用于民用飞机研制项目风险管理。%There are high technical content, dififcult and highly complex, high input, high risks, uncertainties and other great features in civil aircraft development project. Bringing risk management in civil aircraft development project has important signiifcance for project development. Based on researching the theory and procedure of risk management, the methods of risk identification and quantitative assessment in civil aircraft development project was presented, organizational structure and operation process of risk management was established. An architecture framework of risk management system, together with its implementation was proposed, and the developed system was applied in risk management of civil aircraft development project.

  4. Civil Aircraft Thrust Management Function Research%大型飞机推力管理功能研究

    Institute of Scientific and Technical Information of China (English)

    孙鹏; 刘超; 柯劫

    2012-01-01

    推力管理是现代民用客机的重要功能,能改善飞机的燃油经济性。对推力管理功能的提出及其功能与系统组成做了全面介绍与分析,同时介绍了当前先进机型在推力管理功能框架设计上的一些先进理念,总结了推力管理功能涉及的两项关键技术。%Power Thrust management is the critical function of modern civil airplane, which can improve the air- plane's fuel efficiency. This paper gave the full introduction and analysis for thrust management and system archi- tecture, and introduced the advance concepts on the structure of design for power thrust management, and summa- rized the two key technologies relevant to power thrust management.

  5. 民用飞机构型标识方法%Configuration Identification Method for Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    贺璐; 张乐

    2015-01-01

    构型标识是构型管理的四要素之一,从EIA649《national consensus standard for configuration management》中对标识的定义开始,通过解析定义,结合民用飞机全生命周期中构型标识遇到的实际问题及发展瓶颈,给出了全新的构型标识方法,并深入分析了该方法在实际工程应用中的优势。%Configuration identification is one of the four principle elements of configuration management. Begin-ning with the definition and analysis of configuration identification, this paper presents the brand-new configuration identification method, combined with problems and critical issues which happened in civil airplane whole-life-cy-cle configuration identification. The method is analyzed deeply in the advantages of the project application.

  6. 基于模糊综合的民机可达性设计评价方法研究%Study on the Accessibility of Civil Aircraft Based on the Fuzzy Comprehensive Evaluation

    Institute of Scientific and Technical Information of China (English)

    吴昊; 孙玛丽

    2016-01-01

    In order to analyze the maintenance accessibility of civil aircraft better, this paper explains the defini-tion of accessibility firstly. An accessibility evaluation system for civil aircraft is established secondly, and the meth-od of accessibility evaluation is researched finally, an example is analyzed in detail for the method mentioned above and the result shows that the paper can provide an effective idea for the maintenance accessibility analysis of civil aircraft.%为更好地对民用飞机的维修可达性进行评价,首先解释了维修可达性的定义及内涵,其次构建了民用飞机维修可达性的评价体系,研究了模糊综合的维修可达性评价方法。最后通过实例分析,为民用飞机维修可达性设计分析提供了一种有效的思路。

  7. Transient effects of harsh luminous conditions on the visual performance of aviators in a civil aircraft cockpit.

    Science.gov (United States)

    Yang, Biao; Lin, Yandan; Sun, Yaojie

    2013-03-01

    The aim of this work was to examine how harsh luminous conditions in a cockpit, such as lightning in a thunderstorm or direct sunlight immediately after an aircraft passes through clouds, may affect the visual performance of pilots, and how to improve it. Such lighting conditions can result in the temporary visual impairment of aviators, which may greatly increase the risk of accidents. Tests were carried out in a full-scale simulator cockpit in which two kinds of dynamic lighting scenes, namely pulse changed and step changed lighting, were used to represent harsh luminous conditions. Visual acuity (VA), reaction time (RT) and identification accuracy (IA) were recorded as dependent variables. Data analysis results indicate that standardized VA values decreased significantly in both pulsing and step conditions in comparison with the dark condition. Standardized RT values increased significantly in the step condition; on the contrary, less reaction time was observed in the pulsing condition. Such effects could be reduced by an ambient illumination provided by a fluorescent lamp in both conditions. The results are to be used as a principle for optimizing lighting design with a thunderstorm light.

  8. Integrated Aerodynamic/Structural/Dynamic Analyses of Aircraft with Large Shape Changes

    Science.gov (United States)

    Samareh, Jamshid A.; Chwalowski, Pawel; Horta, Lucas G.; Piatak, David J.; McGowan, Anna-Maria R.

    2007-01-01

    The conceptual and preliminary design processes for aircraft with large shape changes are generally difficult and time-consuming, and the processes are often customized for a specific shape change concept to streamline the vehicle design effort. Accordingly, several existing reports show excellent results of assessing a particular shape change concept or perturbations of a concept. The goal of the current effort was to develop a multidisciplinary analysis tool and process that would enable an aircraft designer to assess several very different morphing concepts early in the design phase and yet obtain second-order performance results so that design decisions can be made with better confidence. The approach uses an efficient parametric model formulation that allows automatic model generation for systems undergoing radical shape changes as a function of aerodynamic parameters, geometry parameters, and shape change parameters. In contrast to other more self-contained approaches, the approach utilizes off-the-shelf analysis modules to reduce development time and to make it accessible to many users. Because the analysis is loosely coupled, discipline modules like a multibody code can be easily swapped for other modules with similar capabilities. One of the advantages of this loosely coupled system is the ability to use the medium-to high-fidelity tools early in the design stages when the information can significantly influence and improve overall vehicle design. Data transfer among the analysis modules are based on an accurate and automated general purpose data transfer tool. In general, setup time for the integrated system presented in this paper is 2-4 days for simple shape change concepts and 1-2 weeks for more mechanically complicated concepts. Some of the key elements briefly described in the paper include parametric model development, aerodynamic database generation, multibody analysis, and the required software modules as well as examples for a telescoping wing, a

  9. Magnesium Diboride Superconducting Coils for Electric Propulsion Systems for Large Aircraft Project

    Data.gov (United States)

    National Aeronautics and Space Administration — The recent development of magnesium diboride superconducting wires makes possible the potential to have much lighter weight superconducting coils for heavy aircraft...

  10. 32 CFR 855.15 - Detaining an aircraft.

    Science.gov (United States)

    2010-07-01

    ... 32 National Defense 6 2010-07-01 2010-07-01 false Detaining an aircraft. 855.15 Section 855.15 National Defense Department of Defense (Continued) DEPARTMENT OF THE AIR FORCE AIRCRAFT CIVIL AIRCRAFT USE OF UNITED STATES AIR FORCE AIRFIELDS Civil Aircraft Landing Permits § 855.15 Detaining an aircraft...

  11. The Design of the The Electrical Structure Network(ESN)of the Civil Aircraft%民用飞机电通路结构网络的设计

    Institute of Scientific and Technical Information of China (English)

    孙健宇

    2016-01-01

    An stable electrical network which has low resistances must be constituted of high conductive structures for any electrical and electronic equipments on civil aircraft, which provides electrical functions such as grounding、bonding、voltage reference、protection from electromagnetic interference and protection against lightning strike. A conventional metallic aircraft inherently provides electrical a high conductive network; at present the advanced composite aircraft requires additional electrical structure network (ESN) to provide electrical functions, due to poor electrical conductivity of composite structures compared to metal. the text introduces the electrical structure network designing for main models of the civil aircraft at present, and summarizes and concludes a general design method for the electrical structure network of civil aircraft, guiding the development of the civil aircraft in our country.%民用飞机上的任何电子电气系统都需要通过导电性较好的结构连接建立一条稳定的低阻抗电通路网络,以满足接地、导电、基准电压、防电磁干扰和闪电防护等电气性能。传统金属材料飞机自身形成了较好的结构电通路;目前较先进的碳纤维复合材料飞机由于其自身结构导电性较差,便需要设计额外的电通路结构网络(ESN)来实现上述的电气性能。通过介绍目前主流飞机的电通路结构网络方案,总结归纳出一种典型的民用飞机电通路结构网络的设计方法,对国内民用飞机的研制具有重要的意义。

  12. Compton imaging tomography for nondestructive evaluation of large multilayer aircraft components and structures

    Science.gov (United States)

    Romanov, Volodymyr; Grubsky, Victor; Zahiri, Feraidoon

    2017-02-01

    We present a novel NDT/NDE tool for non-contact, single-sided 3D inspection of aerospace components, based on Compton Imaging Tomography (CIT) technique, which is applicable to large, non-uniform, and/or multilayer structures made of composites or lightweight metals. CIT is based on the registration of Compton-scattered X-rays, and permits the reconstruction of the full 3D (tomographic) image of the inspected objects. Unlike conventional computerized tomography (CT), CIT requires only single-sided access to objects, and therefore can be applied to large structures without their disassembly. The developed tool provides accurate detection, identification, and precise 3D localizations and measurements of any possible internal and surface defects (corrosions, cracks, voids, delaminations, porosity, and inclusions), and also disbonds, core and skin defects, and intrusion of foreign fluids (e.g., fresh and salt water, oil) inside of honeycomb sandwich structures. The NDE capabilities of the system were successfully demonstrated on various aerospace structure samples provided by several major aerospace companies. Such a CIT-based tool can detect and localize individual internal defects with dimensions about 1-2 mm3, and honeycomb disbond defects less than 6 mm by 6 mm area with the variations in the thickness of the adhesive by 100 m. Current maximum scanning speed of aircraft/spacecraft structures is about 5-8 min/ft2 (50-80 min/m2).

  13. Eulerian method for super-cooled large-droplet ice-accretion on aircraft wings

    NARCIS (Netherlands)

    Hospers, J.M.

    2013-01-01

    Many research has been done to provide scientists and aviation engineers with tools to predict ice accretions on in ight aircraft. The ice accretion problem is often sudden, its eects can be dramatic, leading to aircraft accidents with possible loss of lives. Until now this eld has been relatively s

  14. Robots for Aircraft Maintenance

    Science.gov (United States)

    1993-01-01

    Marshall Space Flight Center charged USBI (now Pratt & Whitney) with the task of developing an advanced stripping system based on hydroblasting to strip paint and thermal protection material from Space Shuttle solid rocket boosters. A robot, mounted on a transportable platform, controls the waterjet angle, water pressure and flow rate. This technology, now known as ARMS, has found commercial applications in the removal of coatings from jet engine components. The system is significantly faster than manual procedures and uses only minimal labor. Because the amount of "substrate" lost is minimal, the life of the component is extended. The need for toxic chemicals is reduced, as is waste disposal and human protection equipment. Users of the ARMS work cell include Delta Air Lines and the Air Force, which later contracted with USBI for development of a Large Aircraft Paint Stripping system (LARPS). LARPS' advantages are similar to ARMS, and it has enormous potential in military and civil aircraft maintenance. The technology may also be adapted to aircraft painting, aircraft inspection techniques and paint stripping of large objects like ships and railcars.

  15. Vibration Test Requirements and Application Analysis of Civil Aircraft Equipment (Ⅱ) Vibration Test Requirements of Civil Fixed-wing Aircraft Equipment in DO 160F/G%民用飞机机载设备振动试验要求和应用分析(二)DO 160F/G民用固定翼飞机机载设备振动试验要求

    Institute of Scientific and Technical Information of China (English)

    祝耀昌; 李韻; 徐俊; 王星皓

    2016-01-01

    阐述了民用飞机机载设备振动环境的特点和振动试验分类,归纳和汇总了DO 160 F/G中的各类民用飞机机载设备的振动试验要求,包括振动谱、振动量值和试验持续时间等,并进行了分析和说明,以便于查阅和使用。最后对民用飞机机载设备振动试验方法的应用进行了概括,介绍了民用固定翼飞机的机载设备振动试验要求,按设备在机上的区域不同进行分类,详细地对比说明各个位置上设备的振动试验要求;介绍了民用直升机的机载设备振动试验要求。%ABSTRACT:The paper set forth the characteristics of the vibration environment of civil aircraft equipment and the classifica-tion of vibration tests. The vibration test requirements of various civil aircraft equipment in DO 160 F/G were concluded and summarized, including vibration spectrum, magnitude and duration, and then were analyzed and explained accordingly, so as to facilitate the reference and application thereof. At last, the application of vibration test method for civil aircraft equipment was generalized. Vibration test requirements of civil fixed-wing aircraft equipment was described and classified according to the different sections of the equipment in the aircraft. The vibration test requirements of the equipment at each position were de-scribed in details by contrast; and the vibration test requirements of the airborne equipment of civil helicopters was presented.

  16. Research on New Airworthiness Requirements of Lightning Protection for Civil Aircraft Fuel Tank Explosion Prevention%民机燃油箱防爆闪电防护新适航要求研究

    Institute of Scientific and Technical Information of China (English)

    张斌; 岳鹏; 薛勇; 周宇穗

    2015-01-01

    民用飞机燃油箱系统防爆设计是飞机设计的一个重要方面,其中适航对燃油箱系统闪电防护设计要求作为燃油箱防爆设计及验证的一个重要组成部分,历来受到航空工业界及美国联邦航空局( FAA )的普遍关注.通过研究FAA关于民用飞机燃油箱系统防爆方面闪电防护的最新适航要求,总结了相关条款的变化内容及相应的符合性验证方法,并预判了未来航空工业界由此产生的影响,对民用飞机适航验证有一定借鉴意义.%Fuel tank system explosion prevention of civil aircraft is an important part of aircraft design, and air-worthiness requirements lightning protection regulatory for fuel tank system as an important part of fuel tank explo-sion proof design and validation, has attracted widespread attention in the aviation industry and Federal Aviation Administration( FAA) . This paper studies the latest FAA lightning protection airworthiness requirements of civil aircraft fuel tank system, summarized the evolution of the corresponding provisions and compliance validation meth-od, and also predicted the future effect on aviation industry. The results show the method can provide useful refer-ence for the civil aircraft airworthiness certification.

  17. Crashworthiness Optimization of Civil Aircraft Subfloor Structure%民机机身下部结构耐撞性优化设计

    Institute of Scientific and Technical Information of China (English)

    郑建强; 向锦武; 罗漳平; 任毅如

    2012-01-01

    针对含多设计参数的典型民机机身下部结构耐撞性设计,提出了一种设计方法,该方法以最小化客舱地板的初始加速度峰值与最大化参考压溃状态的结构内能为优化双目标,通过Kriging模型对结构的冲击响应进行预测,采用非支配排序遗传算法Ⅱ(NSGA-Ⅱ)对双目标进行优化,进而由Nash-Pareto策略获得最优方案.为了得到最优设计方案,同时研究设计参数对机身结构耐撞性的影响,提出最大化期望提高与最大化预测方差同步加点准则建立代理模型.采用该设计方法,以典型民机机身下部结构设计问题为算例,对客舱地板支撑结构、货舱地板和泡沫构件形状参数进行优化.结果表明,相对原始设计客舱地板的加速度峰值降低约18.3%,次高加速度峰值也得到有效降低,改善了机身结构的耐撞性;Kriging模型预测响应与有限元分析结果误差小于1%,说明了设计方法的有效性.%For a typical civil aircraft fuselage structural crashworthiness design with several design parameters, a design approach is proposed to minimize the peak acceleration of the cabin floor and maximize the internal energy of the structure at a certain crushing state. A Kriging surrogate model is adopted for impact response approximation, a nondominated sorting genetic algorithm II (NSGA-II) for dual objective optimization, and Nash-Pareto strategy for the optimum design selection. In order to obtain the effect of design parameters on crashworthiness as well as the optimum design, a synchronous sampling criterion of the maximum expected improvement and the maximum predicted variance Is suggested to construct a surrogate model. Using this design approach, a typical civil aircraft fuselage structural design with the shape parameters of the cabin floor struts, cargo floor and foam components is studied as a design case. The results indicate that the peak acceleration of the cabin floor is reduced by

  18. 民机货舱压差载荷的分析与解决方案%Analysis and Solution of Civil Aircraft Cargo Differential Pressure Load

    Institute of Scientific and Technical Information of China (English)

    王旭阳; 林石泉; 李革萍

    2014-01-01

    One-dimension model is built up for cargo differential pressure calculation in this article, and then the effect of cargo volume and cargo leakage areas on cargo differential pressure load is analyzed. Secondly, this article brief introduces the internal design guide of cargo pressure equalization equipment. And the configurations of pressure equalization valves equipped on China self-developed civil aircraft are presented then. At last, a novel solution of cargo differential pressure load is proposed. The outlet of cargo ventilation shut-off valve is considered to keep open in normal condition to achieve differential pressure relief for cargo. This novel solution will bring some decrease of A/C weight and cost.%本文建立了一维的货舱压差载荷计算方法,并对货舱容积和货舱等效泄漏面积等因素对货舱压差载荷的影响进行了分析。介绍了我国民机货舱压差平衡装置的设计准则,简介了我国自主研制的货舱压差平衡装置结构。最后提出了一种新颖的货舱压差载荷解决方案,即把货舱压差平衡功能集成至货舱出口关断活门中。该方案可减少一定的飞机重量,并节省原货舱压力平衡装置的研制成本。

  19. The Optimization Design of Door Connecting Rod Bracket Structure of Civil Aircraft%民用飞机舱门连杆支架优化研究

    Institute of Scientific and Technical Information of China (English)

    袁修起

    2014-01-01

    The cabin latch mechanism of civil aircraft is to prevent the door accidentally open parts. When a jam occurs forced operation, it will produce a greater internal force. The equipment door latch mechanism is all stem shape and load is small except the connecting rod bracket. Connecting rod bracket structure is complex and load is bigger. Based on analyzingresistance load ,using the finite element analysis software HyperMesh and Opti-Struct , three kinds of structure forms of connecting rod bracket are simulated. With comparison and analysis, connecting rod bracket structure satisfied equipment doors functional requirements and prototype test purpose, which provides reference for the follow-up of the real product design.%民用飞机舱门闩机构是防止舱门意外开启的机构部件。当机构发生卡阻且强制操作时,将产生较大的内力。在设备舱门闩机构中除连杆支架外都是杆形件且载荷较小,连杆支架结构形式复杂且载荷较大。在分析机构卡阻载荷的基础上使用有限元分析软件HyperMesh和Opti-Struct对三种结构形式的连杆支架进行了数值模拟。通过对比分析,得到了满足样机设备舱门功能要求和试验目的的连杆支架形式,为后续真实产品的设计提供参考。

  20. Geophylosophy of circumpolar civilization

    Directory of Open Access Journals (Sweden)

    I. A. Zhuvaka

    2014-09-01

    Under the influence of colonization occurred the interpenetration of civilizations, indigenous peoples have largely lose its image, the traditional way of life and culture. Arctic civilization has appeared in a crisis and facing the threat of extinction.

  1. Computational Assessment of the Aerodynamic Performance of a Variable-Speed Power Turbine for Large Civil Tilt-Rotor Application

    Science.gov (United States)

    Welch, Gerard E.

    2011-01-01

    The main rotors of the NASA Large Civil Tilt-Rotor notional vehicle operate over a wide speed-range, from 100% at take-off to 54% at cruise. The variable-speed power turbine offers one approach by which to effect this speed variation. Key aero-challenges include high work factors at cruise and wide (40 to 60 deg.) incidence variations in blade and vane rows over the speed range. The turbine design approach must optimize cruise efficiency and minimize off-design penalties at take-off. The accuracy of the off-design incidence loss model is therefore critical to the turbine design. In this effort, 3-D computational analyses are used to assess the variation of turbine efficiency with speed change. The conceptual design of a 4-stage variable-speed power turbine for the Large Civil Tilt-Rotor application is first established at the meanline level. The design of 2-D airfoil sections and resulting 3-D blade and vane rows is documented. Three-dimensional Reynolds Averaged Navier-Stokes computations are used to assess the design and off-design performance of an embedded 1.5-stage portion-Rotor 1, Stator 2, and Rotor 2-of the turbine. The 3-D computational results yield the same efficiency versus speed trends predicted by meanline analyses, supporting the design choice to execute the turbine design at the cruise operating speed.

  2. Real-time Simulation of Large Aircraft Flying Through Microburst Wind Field

    Institute of Scientific and Technical Information of China (English)

    Gao Zhenxing; Gu Hongbin; Liu Hui

    2009-01-01

    This article deals with real-time hi-fi simulation of large aircraft flying in turbulent wind in a simulator to study its takeoff and landing behavior in microburst wind shear. A parameterized three-dimensional (3D) microburst model is built up on the basis of vortex ring and Rankine vortex principle. Complicated microburst wind fields are simulated by means of vortex ring declination and multi-vortex superposition. Based on the modeling data of Boeing 747-100, a dynamic model with wind shear effects considered is established and a general method to modify the aerodynamic model is proposed. A controller for longitudinal and lateral escapes is designed and verified in simulated microburst wind field. Results indicate that, with high extensibility, reasonability and effectiveness, the 3D microburst model with wind shear effects considered is fit to simulate real wind fields. Different escape schemes can be adopted to fly through a wind field from different locations. The model can be used for real-time flight simulation in a flight simulator.

  3. Designs and Technology Requirements for Civil Heavy Lift Rotorcraft

    Science.gov (United States)

    Johnson, Wayne; Yamauchi, Gloria K.; Watts, Michael E.

    2006-01-01

    The NASA Heavy Lift Rotorcraft Systems Investigation examined in depth several rotorcraft configurations for large civil transport, designed to meet the technology goals of the NASA Vehicle Systems Program. The investigation identified the Large Civil Tiltrotor as the configuration with the best potential to meet the technology goals. The design presented was economically competitive, with the potential for substantial impact on the air transportation system. The keys to achieving a competitive aircraft were low drag airframe and low disk loading rotors; structural weight reduction, for both airframe and rotors; drive system weight reduction; improved engine efficiency; low maintenance design; and manufacturing cost comparable to fixed-wing aircraft. Risk reduction plans were developed to provide the strategic direction to support a heavy-lift rotorcraft development. The following high risk areas were identified for heavy lift rotorcraft: high torque, light weight drive system; high performance, structurally efficient rotor/wing system; low noise aircraft; and super-integrated vehicle management system.

  4. Efficient Multidisciplinary Analysis Approach for Conceptual Design of Aircraft with Large Shape Change

    Science.gov (United States)

    Chwalowski, Pawel; Samareh, Jamshid A.; Horta, Lucas G.; Piatak, David J.; McGowan, Anna-Maria R.

    2009-01-01

    The conceptual and preliminary design processes for aircraft with large shape changes are generally difficult and time-consuming, and the processes are often customized for a specific shape change concept to streamline the vehicle design effort. Accordingly, several existing reports show excellent results of assessing a particular shape change concept or perturbations of a concept. The goal of the current effort was to develop a multidisciplinary analysis tool and process that would enable an aircraft designer to assess several very different morphing concepts early in the design phase and yet obtain second-order performance results so that design decisions can be made with better confidence. The approach uses an efficient parametric model formulation that allows automatic model generation for systems undergoing radical shape changes as a function of aerodynamic parameters, geometry parameters, and shape change parameters. In contrast to other more self-contained approaches, the approach utilizes off-the-shelf analysis modules to reduce development time and to make it accessible to many users. Because the analysis is loosely coupled, discipline modules like a multibody code can be easily swapped for other modules with similar capabilities. One of the advantages of this loosely coupled system is the ability to use the medium- to high-fidelity tools early in the design stages when the information can significantly influence and improve overall vehicle design. Data transfer among the analysis modules are based on an accurate and automated general purpose data transfer tool. In general, setup time for the integrated system presented in this paper is 2-4 days for simple shape change concepts and 1-2 weeks for more mechanically complicated concepts. Some of the key elements briefly described in the paper include parametric model development, aerodynamic database generation, multibody analysis, and the required software modules as well as examples for a telescoping wing

  5. MRO oriented civil aircraft engine removal date prediction system%面向MRO的民航发动机拆发日期预测系统

    Institute of Scientific and Technical Information of China (English)

    雷达; 钟诗胜

    2013-01-01

    Aiming at the business requirements of Maintenance,Repair and Operations (MRO) for civil aircraft engine,a software system for engine removal date prediction was developed.The system predicted the removal date of the on-wing engines according to three types of factors affecting the service of the aircraft engine,which were performance,fault and time limit.The concept of damage baseline was proposed by considering the factors that the major fault of the aircraft core engine was always limited,and a damage propagation model based on linear degradation path was established to realize the removal date prediction based on hardware damage fault.This system was currently in service in Air China Limited,and was seamlessly integrated with the existing engine health management and maintenance decision support system via interfaces as a subsystem.The developed system obtained support data from its parent system and provided the prediction results for its parent system as support data.Thus an integrated process was formed including the engine condition monitoring process,the removal date prediction process and the maintenance decision-making process,which satisfied the MRO requirements of Air China Limited.%针对民航发动机维护、维修和大修的业务需求,开发了民航发动机拆发日期预测系统.系统可以根据影响民航发动机使用的性能、故障和时限三类因素,对在翼民航发动机进行拆发日期预测.考虑到故障因素中的硬件损伤数据样本偏少,提出损伤基线的概念,并建立了基于线性退化轨道的硬件损伤发展模型,实现了基于硬件损伤故障的发动机拆发日期预测.该系统应用于中国国际航空股份有限公司(国航),并且通过接口与其现有的发动机健康管理和维修决策支持系统实现无缝集成,成为其子系统.系统从母系统中获得支撑数据并将预测结果提供给母系统,作为维修计划制定模块的支撑数据,从而使发动机状

  6. Large strain variable stiffness composites for shear deformations with applications to morphing aircraft skins

    Science.gov (United States)

    McKnight, G. P.; Henry, C. P.

    2008-03-01

    Morphing or reconfigurable structures potentially allow for previously unattainable vehicle performance by permitting several optimized structures to be achieved using a single platform. The key to enabling this technology in applications such as aircraft wings, nozzles, and control surfaces, are new engineered materials which can achieve the necessary deformations but limit losses in parasitic actuation mass and structural efficiency (stiffness/weight). These materials should exhibit precise control of deformation properties and provide high stiffness when exercised through large deformations. In this work, we build upon previous efforts in segmented reinforcement variable stiffness composites employing shape memory polymers to create prototype hybrid composite materials that combine the benefits of cellular materials with those of discontinuous reinforcement composites. These composites help overcome two key challenges for shearing wing skins: the resistance to out of plane buckling from actuation induced shear deformation, and resistance to membrane deflections resulting from distributed aerodynamic pressure loading. We designed, fabricated, and tested composite materials intended for shear deformation and address out of plane deflections in variable area wing skins. Our designs are based on the kinematic engineering of reinforcement platelets such that desired microstructural kinematics is achieved through prescribed boundary conditions. We achieve this kinematic control by etching sheets of metallic reinforcement into regular patterns of platelets and connecting ligaments. This kinematic engineering allows optimization of materials properties for a known deformation pathway. We use mechanical analysis and full field photogrammetry to relate local scale kinematics and strains to global deformations for both axial tension loading and shear loading with a pinned-diamond type fixture. The Poisson ratio of the kinematically engineered composite is ~3x higher than

  7. Large Eddy Simulation of Aircraft Wake Vortices in a Homogeneous Atmospheric Turbulence: Vortex Decay and Descent

    Science.gov (United States)

    Han, Jongil; Lin, Yuh-Lang; Arya, S. Pal; Proctor, Fred H.

    1999-01-01

    The effects of ambient turbulence on decay and descent of aircraft wake vortices are studied using a validated, three-dimensional: large-eddy simulation model. Numerical simulations are performed in order to isolate the effect of ambient turbulence on the wake vortex decay rate within a neutrally-stratified atmosphere. Simulations are conducted for a range of turbulence intensities, by injecting wake vortex pairs into an approximately homogeneous and isotropic turbulence field. The decay rate of the vortex circulation increases clearly with increasing ambient turbulence level, which is consistent with field observations. Based on the results from the numerical simulations, simple decay models are proposed as functions of dimensionless ambient turbulence intensity (eta) and dimensionless time (T) for the circulation averaged over a range of radial distances. With good agreement with the numerical results, a Gaussian type of vortex decay model is proposed for weak turbulence: while an exponential type of Tortex decay model can be applied for strong turbulence. A relationship for the vortex descent based on above vortex decay model is also proposed. Although the proposed models are based on simulations assuming neutral stratification, the model predictions are compared to Lidar vortex measurements observed during stable, neutral, and unstable atmospheric conditions. In the neutral and unstable atmosphere, the model predictions appear to be in reasonable agreement with the observational data, while in the stably-stratified atmosphere, they largely underestimate the observed circulation decay with consistent overestimation of the observed vortex descent. The underestimation of vortex decay during stably-stratified conditions suggests that stratification has an important influence on vortex decay when ambient levels of turbulence are weak.

  8. Rotordynamic Feasibility of a Conceptual Variable-Speed Power Turbine Propulsion System for Large Civil Tilt-Rotor Applications

    Science.gov (United States)

    Howard, Samuel

    2012-01-01

    A variable-speed power turbine concept is analyzed for rotordynamic feasibility in a Large Civil Tilt-Rotor (LCTR) class engine. Implementation of a variable-speed power turbine in a rotorcraft engine would enable high efficiency propulsion at the high forward velocities anticipated of large tilt-rotor vehicles. Therefore, rotordynamics is a critical issue for this engine concept. A preliminary feasibility study is presented herein to address this concern and identify if variable-speed is possible in a conceptual engine sized for the LCTR. The analysis considers critical speed placement in the operating speed envelope, stability analysis up to the maximum anticipated operating speed, and potential unbalance response amplitudes to determine that a variable-speed power turbine is likely to be challenging, but not impossible to achieve in a tilt-rotor propulsion engine.

  9. Wind Tunnel Testing of a 120th Scale Large Civil Tilt-Rotor Model in Airplane and Helicopter Modes

    Science.gov (United States)

    Theodore, Colin R.; Willink, Gina C.; Russell, Carl R.; Amy, Alexander R.; Pete, Ashley E.

    2014-01-01

    In April 2012 and October 2013, NASA and the U.S. Army jointly conducted a wind tunnel test program examining two notional large tilt rotor designs: NASA's Large Civil Tilt Rotor and the Army's High Efficiency Tilt Rotor. The approximately 6%-scale airframe models (unpowered) were tested without rotors in the U.S. Army 7- by 10-foot wind tunnel at NASA Ames Research Center. Measurements of all six forces and moments acting on the airframe were taken using the wind tunnel scale system. In addition to force and moment measurements, flow visualization using tufts, infrared thermography and oil flow were used to identify flow trajectories, boundary layer transition and areas of flow separation. The purpose of this test was to collect data for the validation of computational fluid dynamics tools, for the development of flight dynamics simulation models, and to validate performance predictions made during conceptual design. This paper focuses on the results for the Large Civil Tilt Rotor model in an airplane mode configuration up to 200 knots of wind tunnel speed. Results are presented with the full airframe model with various wing tip and nacelle configurations, and for a wing-only case also with various wing tip and nacelle configurations. Key results show that the addition of a wing extension outboard of the nacelles produces a significant increase in the lift-to-drag ratio, and interestingly decreases the drag compared to the case where the wing extension is not present. The drag decrease is likely due to complex aerodynamic interactions between the nacelle and wing extension that results in a significant drag benefit.

  10. Multi-Sensing system for outdoor thermal monitoring: Application to large scale civil engineering components

    Science.gov (United States)

    Crinière, Antoine; Dumoulin, Jean; Manceau, Jean-Luc; Perez, Laetitia; Bourquin, Frederic

    2014-05-01

    Aging of transport infrastructures combined with traffic and climatic solicitations contribute to the reduction of their performances. To address and quantify the resilience of civil engineering structure, investigations on robust, fast and efficient methods are required. Among research works carried out at IFSTTAR, methods for long term monitoring face an increasing demand. Such works take benefits of this last decade technological progresses in ICT domain. The present study follows the ISTIMES European project [1], which aimed at demonstrate the ability of different electromagnetic sensing techniques, processing methods and ICT architecture, to be used for long term monitoring of critical transport infrastructures. Thanks to this project a multi-sensing techniques system, able to date and synchronize measurements carried out by infrared thermography coupled with various measurements data (i.e. weather parameters), have been designed, developed and implemented on real site [2]. Among experiments carried out on real transport infrastructure, it has been shown, for the "Musmesci" bridge deck (Italy), that by using infrared thermal image sequence with weather measurements during sevral days it was possible to develop analysis methods able to produce qualitative and quantitative data [3]. In the present study, added functionalities were designed and added to the "IrLAW" system in order to reach full autonomy in term of power supply, very long term measurement capability (at least 1 year) and automated data base feeding. The surveyed civil engineering structures consist in two concrete beams of 16 m long and 21 T weight each. One of the two beams was damage by high energy mechanical impact at the IFSTTAR falling rocks test station facilities located in the French Alpes [4]. The system is composed of one IR uncooled microbolometric camera (FLIR SC325) with a 320X240 Focal Plane Array detector in band III, a weather station VAISALA WXT520, a GPS, a failover power supply

  11. Population census of a large common tern colony with a small unmanned aircraft.

    Directory of Open Access Journals (Sweden)

    Dominique Chabot

    Full Text Available Small unmanned aircraft systems (UAS may be useful for conducting high-precision, low-disturbance waterbird surveys, but limited data exist on their effectiveness. We evaluated the capacity of a small UAS to census a large (>6,000 nests coastal Common tern (Sterna hirundo colony of which ground surveys are particularly disruptive and time-consuming. We compared aerial photographic tern counts to ground nest counts in 45 plots (5-m radius throughout the colony at three intervals over a nine-day period in order to identify sources of variation and establish a coefficient to estimate nest numbers from UAS surveys. We also compared a full colony ground count to full counts from two UAS surveys conducted the following day. Finally, we compared colony disturbance levels over the course of UAS flights to matched control periods. Linear regressions between aerial and ground counts in plots had very strong correlations in all three comparison periods (R2 = 0.972-0.989, P < 0.001 and regression coefficients ranged from 0.928-0.977 terns/nest. Full colony aerial counts were 93.6% and 94.0%, respectively, of the ground count. Varying visibility of terns with ground cover, weather conditions and image quality, and changing nest attendance rates throughout incubation were likely sources of variation in aerial detection rates. Optimally timed UAS surveys of Common tern colonies following our method should yield population estimates in the 93-96% range of ground counts. Although the terns were initially disturbed by the UAS flying overhead, they rapidly habituated to it. Overall, we found no evidence of sustained disturbance to the colony by the UAS. We encourage colonial waterbird researchers and managers to consider taking advantage of this burgeoning technology.

  12. Analysis of Advanced Integration Procedure for Systems Onboard Civil Aircrafts%先进的民用飞机机载系统集成流程分析

    Institute of Scientific and Technical Information of China (English)

    徐科华; 陈谋; 吴庆宪

    2012-01-01

    为解决现有民用飞机机载系统设计流程难以在设计前期发现顶层设计偏差的问题,对现有的瀑布式设计流程、V形设计流程及螺旋形设计流程进行了详细分析及对比,总结了各自在系统设计中的优势和局限性,提出采用螺旋形流程对V形流程进行改造的设计方法.该方法强调在设计前期采用模型对设计结果进行充分仿真验证,发现前期设计偏差,进行反复迭代,完善设计;在后期系统综合各阶段进行充分的综合测试验证,并根据结果对系统设计进行修正,确保系统满足前期各项需求.经详细分析表明,该流程集中了传统设计方法的优点,能在设计初期发现各种问题,具有很好的可行性.%It is difficult to discover the top-level design deviation for the complicated system of civil aircraft ahead of schedule based on traditional design procedure. To solve the problem, we analyzed the cascade design procedure, V-shaped procedure and spiral procedure in detail,summarized their advantages and limits, and proposed a method using the spiral procedure to optimize the V-shaped procedure. During early design stage, this method focuses on simulation and verification to the system scheme based on model, thus can discover the early designing error. Iterations are made to make the scheme complete. In latter system integration, test and validation are carried out, and the design is modified based on the test result,thus to make the system satisfy all the requirements. Detailed analysis shows that this is a method which has all the advantages of the traditional procedure, it is a feasible method that can discover the design error ahead of schedule.

  13. Large eddy simulation of air pollution produced by aircraft engine emissions inside the airport

    Energy Technology Data Exchange (ETDEWEB)

    Synylo, Kateryna [National Aviation University (Ukraine)], email: synylo@nau.edu.ua

    2011-07-01

    With the increase of air traffic movement, air pollution from airport emissions has become an important concern. In the past, various research has been undertaken on the impact of aircraft engines on the upper troposphere and lower stratosphere, however the impact that emissions have on airports themselves is not taken into account by the most frequently used monitoring software programs. The aim of this paper is to present the use of a CFD simulation to determine the dynamic and fluid mechanics characteristics of aircraft emissions near the ground. The CFD simulation was carried out using Fluent 6.3 software and the effects of counter-rotating vortices and wind conditions on fulfilled gases jet. It was found that numerical simulation is able to resolve difficult equations and provide realistic results. This study demonstrated that the use of CFD computation could be used to improve local air quality modeling and assessment of the impact of aircraft emissions at airports.

  14. Dynamics modeling and control of large transport aircraft in heavy cargo extraction

    Institute of Scientific and Technical Information of China (English)

    2011-01-01

    In this paper,a novel version of six-degree-of-freedom nonlinear model for transport aircraft motion in cargo extraction is developed and validated by the theoretical mechanics and flight mechanics.In this model constraint force and moment reflecting the flight dynamic effects of inner moving cargo are formulated.A methodology for a control law design in this phase is presented,which linearizes the aircraft dynamics making use of piecewise linearization and utilizes robust control technique for interval sys...

  15. Emission analysis of large number of various passenger electronic devices in aircraft

    Science.gov (United States)

    Schüür, Jens; Oppermann, Lukas; Enders, Achim; Nunes, Rafael R.; Oertel, Carl-Henrik

    2016-09-01

    The ever increasing use of PEDs (passenger or portable electronic devices) has put pressure on the aircraft industry as well as operators and administrations to reevaluate established restrictions in PED-use on airplanes in the last years. Any electronic device could cause electromagnetic interference to the electronics of the airplane, especially interference at receiving antennas of sensitive wireless navigation and communication (NAV/COM) systems. This paper presents a measurement campaign in an Airbus A320. 69 test passengers were asked to actively use a combination of about 150 electronic devices including many attached cables, preferentially with a high data load on their buses, to provoke maximal emissions. These emissions were analysed within the cabin as well as at the inputs of aircraft receiving antennas outside of the fuselage. The emissions of the electronic devices as well as the background noise are time-variant, so just comparing only one reference and one transmission measurement is not sufficient. Repeated measurements of both cases lead to a more reliable first analysis. Additional measurements of the absolute received power at the antennas of the airplane allow a good estimation of the real interference potential to aircraft NAV/COM systems. Although there were many measured emissions within the cabin, there were no disturbance signals detectable at the aircraft antennas.

  16. Ageing aircraft research in the Netherlands

    Science.gov (United States)

    Dejonge, J. B.; Bartelds, G.

    1992-01-01

    The problems of aging aircraft are worldwide. Hence, international cooperative actions to overcome or prevent problems should be taken. The Federal Aviation Administration (FAA) and the Netherlands Civil Aviation Department (RLD) signed a Memorandum of Cooperation in the area of structural integrity, with specific reference to research on problems in the area of aging aircraft. Here, an overview is given of aging research that is going on in the Netherlands. The work described is done largely at the National Aerospace Laboratory; much of the research is part of the forementioned cooperative agreement.

  17. Flight assessment of a large supersonic drone aircraft for research use

    Science.gov (United States)

    Eckstrom, C. V.; Peele, E. L.

    1974-01-01

    An assessment is made of the capabilities of the BQM-34E supersonic drone aircraft as a test bed research vehicle. This assessment is made based on a flight conducted for the purpose of obtaining flight test measurements of wing loads at various maneuver flight conditions. Flight plan preparation, flight simulation, and conduct of the flight test are discussed along with a presentation of the test data obtained and an evaluation of how closely the flight test followed the test plan.

  18. Efficiency and economics of large scale hydrogen liquefaction. [for future generation aircraft requirements

    Science.gov (United States)

    Baker, C. R.

    1975-01-01

    Liquid hydrogen is being considered as a substitute for conventional hydrocarbon-based fuels for future generations of commercial jet aircraft. Its acceptance will depend, in part, upon the technology and cost of liquefaction. The process and economic requirements for providing a sufficient quantity of liquid hydrogen to service a major airport are described. The design is supported by thermodynamic studies which determine the effect of process arrangement and operating parameters on the process efficiency and work of liquefaction.

  19. Aircraft avoidance for laser propagation at the Large Binocular Telescope Observatory: life under a busy airspace

    Science.gov (United States)

    Rahmer, Gustavo; Lefebvre, Michael; Christou, Julian C.

    2016-07-01

    A key aspect of LGS operations is the implementation of measures to prevent the illumination of airplanes flying overhead. The most basic one is the use of "aircraft spotters" in permanent communication with the laser operator. Although this is the default method accepted by the FAA to authorize laser propagation, it relies on the inherent subjectivity of human perception, and requires keeping a small army of spotters to cover all the nights scheduled for propagation. Following the successful experience of other observatories (Keck and APO), we have installed an automatic aircraft detection system developed at UCSD known as TBAD (Transponder-Based Aircraft Detection). The system has been in continuous operation since April 2015, collecting detection data every night the telescope is open. We present a description of our system implementation and operational procedures. We also describe and discuss the analysis of the TBAD detection data, that shows how busy our airspace is, and the expected impact on the operation efficiency of the observatory.

  20. Assessment of Aerodynamic Challenges of a Variable-Speed Power Turbine for Large Civil Tilt-Rotor Application

    Science.gov (United States)

    Welch, Gerand E.

    2010-01-01

    The main rotors of the NASA Large Civil Tilt-Rotor notional vehicle operate over a wide speed-range (100% at take-off to 54% at cruise). The variable-speed power turbine, when coupled to a fixed-gear-ratio transmission, offers one approach to accomplish this speed variation. The key aero-challenges of the variable-speed power turbine are related to high work factors at cruise, where the power turbine operates at 54% of take-off speed, wide incidence variations into the vane, blade, and exit-guide-vane rows associated with the power-turbine speed change, and the impact of low aft-stage Reynolds number (transitional flow) at 28 kft cruise. Meanline and 2-D Reynolds-Averaged Navier- Stokes analyses are used to characterize the variable-speed power-turbine aerodynamic challenges and to outline a conceptual design approach that accounts for multi-point operation. Identified technical challenges associated with the aerodynamics of high work factor, incidence-tolerant blading, and low Reynolds numbers pose research needs outlined in the paper

  1. The \\^G Infrared Search for Extraterrestrial Civilizations with Large Energy Supplies. III. The Reddest Extended Sources in WISE

    CERN Document Server

    Griffith, Roger L; Maldonado, Jessica; Povich, Matthew S; Sigurdsson, Steinn; Mullan, Brendan

    2015-01-01

    Nearby Type II (galaxy-spanning) Kardashev supercivilizations would have high mid-infrared (MIR) luminosities. We have used the Wide-field Infrared Survey Explorer (WISE) to survey ~$1 \\times 10^5$ galaxies for extreme MIR emission, $10^3$ times more galaxies than the only previous such search. We have calibrated the WISE All-sky Catalog pipeline products to improve its photometry for extended sources. We present 563 extended sources with $|b| \\ge 10$ and red MIR colors, having visually vetted them to remove artifacts. No galaxies in our sample host an alien civilization reprocessing more than 85% of its starlight into the MIR, and only 50 galaxies, including Arp 220, have MIR luminosities consistent with >50% reprocessing. Ninety of these (likely) extragalactic sources have little literature presence; in most cases they are likely barely resolved galaxies or pairs of galaxies undergoing large amounts of star formation. Five are new to science and deserve further study. The Be star 48 Librae sits within a MIR...

  2. Academic Training Lecture Regular Programme: How Large-Scale Civil Engineering Projects Realise the Potential of a City

    CERN Multimedia

    2012-01-01

    How Large-Scale Civil Engineering Projects Realise the Potential of a City (1/3), by Bill Hanway (Excecutive Director of Operations, AECOM Europe).   Wednesday, June 6, 2012 from 11:00 to 12:00 (Europe/Zurich) at CERN ( 80-1-001 - Globe 1st Floor ) In this series of three special lectures, leading experts from AECOM would explore the impact of a trio of major projects on a single city. In common with every metropolis, London has run-down districts and infrastructure in need of upgrading. The lectures propose to cover three of the biggest challenges: regenerating run-down areas; reducing congestion and transporting people more efficiently; and improving water and wastewater systems. Each project contributes to a collective public aim - to realise the potential of a growing city, and ensure its healthy, sustainable and competitive future. Lecture 1: Into the lecture series and The London 2012 Olympic Games Most cities share a group of common complex challenges – growing populations, agei...

  3. 民用飞机典型腐蚀环境区域的聚类及差异性研究%Cluster Analysis for Typical Ground Environment Areas of Civil Airports and Regional Difference Analysis for Corrosion of Civil Aircrafts

    Institute of Scientific and Technical Information of China (English)

    苏景新; 张春晓; 徐天杰

    2012-01-01

    收集百余架某系列民航飞机近十年的腐蚀损伤数据,及其过夜停放的16个基地机场的气象环境指标数据,利用动态聚类分析方法,对基地机场的腐蚀环境区域进行了划分,得到对该系列飞机的腐蚀行为影响规律具有相似性的4类腐蚀环境区域。其次应用方差分析方法,对在不同类型机场环境区域的腐蚀频率进行了差异性研究。结果表明,不同机场环境区域的飞机结构腐蚀频率有显著的差异。研究成果对编制民用机场环境谱和进行腐蚀加速试验选取参数有重要的参考价值。%Based on the corrosion data of a series of aircraft for recent 10 years, meteorological and environmental indicators of aircraft base airports, using dynamic clustering method, the environmental areas of aircraft base airports were divided firstly, and then four types of corrosion environment area for corrosion behavior of this series aircraft were got out with similar affecting laws. Secondly, the corrosion frequency of different types of airport environment was investigated by analysis of variance. The results show that the aircraft corrosion frequency in different airport environments varied as region varied. This research provides an important reference for working out a civil airport environment spectrum and selecting the parameters for the acceleraed corrosion testing.

  4. Large Aircraft Robotic Paint Stripping (LARPS) system and the high pressure water process

    Science.gov (United States)

    See, David W.; Hofacker, Scott A.; Stone, M. Anthony; Harbaugh, Darcy

    1993-03-01

    The aircraft maintenance industry is beset by new Environmental Protection Agency (EPA) guidelines on air emissions, Occupational Safety and Health Administration (OSHA) standards, dwindling labor markets, Federal Aviation Administration (FAA) safety guidelines, and increased operating costs. In light of these factors, the USAF's Wright Laboratory Manufacturing Technology Directorate and the Aircraft Division of the Oklahoma City Air Logistics Center initiated a MANTECH/REPTECH effort to automate an alternate paint removal method and eliminate the current manual methylene chloride chemical stripping methods. This paper presents some of the background and history of the LARPS program, describes the LARPS system, documents the projected operational flow, quantifies some of the projected system benefits and describes the High Pressure Water Stripping Process. Certification of an alternative paint removal method to replace the current chemical process is being performed in two phases: Process Optimization and Process Validation. This paper also presents the results of the Process Optimization for metal substrates. Data on the coating removal rate, residual stresses, surface roughness, preliminary process envelopes, and technical plans for process Validation Testing will be discussed.

  5. 基于突破式创新局限性的民用飞机制造产业创新窘境分析%Analysis of the Dilemma of Civil Aircraft Manufacturing Industry Innovation Based on Radical Innovation Limitations

    Institute of Scientific and Technical Information of China (English)

    刘花清; 黄莹灿; 杨蕾; 冯亚秋

    2015-01-01

    From the research of the radical innovation mode and its development and application situation, this article finds out the limitations of radical innovation through the comparison of different innovation modes in various aspects, combined with the analysis of the status quo of civil aircraft manufacturing industry innovation, and discusses the six innovation dilemmas of radical innovation in civil aircraft manufacturing industry. In view of this background, the authors hope that analysis of the dilemmas of radical innovation in civil aircraft manufacturing industry can promote the development of China's civil aircraft manufacturing industry.%本文从突破式创新模式的探究及其发展和应用情况出发,通过不同创新模式在各方面的比较,发现突破式创新存在的局限性,结合民用飞机制造业的创新现状分析,重点探讨了突破式创新在民用飞机制造产业的六大创新窘境。鉴于此背景之下,希望通过分析当前民用飞机制造产业突破式创新中存在的窘境,促进中国民用飞机制造产业的发展。

  6. Civil Aircraft ACS Venturi flow Simulation and Error Analysis using Matlab/Simulink%基于Matlab/Simulink的民机空调系统文氏管流量精度仿真分析

    Institute of Scientific and Technical Information of China (English)

    戴铮

    2014-01-01

    Venturi is an important equipment used to estimate the ACS inlet airflow on the civil aircraft. This paper compares the estimated airflow sensing errors resulted from using different sensing positions to obtain temperature and pressure sensor signals based on Matlab/Simulink.%文氏管是测量民用飞机空调系统组件进口流量的重要部件,其精度指标直接影响到组件进口流量的控制。本文通过Matlab/Simulink仿真的方式分析温度压力测量位置的不同对于文氏管流量计算精度的影响。

  7. Analysis of Influencing Factor of Risk Communication in Civil Aircraft Supply Chain Based on TPB%基于TPB的民机供应链风险沟通影响因素分析

    Institute of Scientific and Technical Information of China (English)

    徐祎飞; 张亚莉; 姜香美

    2013-01-01

    With theory of planned behavior, a few factors are proposed to analyze between members of civil aircraft supply chain enterprises in risk communication, type of partnership, power structure, risk type, expected results, trust and commitment, the degree of resource and so on. Finally, three measures to improve risk communication are put forward.%本文以计划行为理论(TPB)为基础,分析了民机供应链成员企业之间在风险沟通方面的影响因素,主要有合作伙伴关系类型、力量格局、风险类型、期望结果、信任与承诺、资源配合度,并给出3点建议.

  8. 民用飞机两跨裂纹结构的剩余强度分析%Residual Strength Analysis about the Two-span Crack Structure of Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    许海生

    2012-01-01

    According the universal method, the residual strength of civil aircraft fuselage skin and wing skin can meet two-span crack. The designer need evaluates the residual strength of the skin in the condition of two-span crack in the primary-phrase design.%根据通用做法,民用飞机机身和机翼壁板在“两跨”长度裂纹存在情况下剩余强度能够满足要求,设计人员在飞机设计的初级阶段就要对两跨裂纹情况下壁板剩余强度进行评估.

  9. Fault mechanism analysis and simulation for continuity resistance test of electrical components in aircraft engine

    Science.gov (United States)

    Shi, Xudong; Yin, Yaping; Wang, Jialin; Sun, Zhaorong

    2017-01-01

    A large number of electrical components are used in civil aircraft engines, whose electrical circuits are usually intricate and complicated. Continuity resistance is an important parameter for the operating state of electrical components. Electrical continuity fault has serious impact on the reliability of the aircraft engine. In this paper, mathematical models of electrical components are established, and simulation is made by Simulink to analyze the electrical continuity fault.

  10. Design Study of Propulsion and Drive Systems for the Large Civil TiltRotor (LCTR2) Rotorcraft

    Science.gov (United States)

    Robuck, Mark; Wilkerson, Joseph; Zhang, Yiyi; Snyder, Christopher A.; Vonderwell, Daniel

    2013-01-01

    Boeing, Rolls Royce, and NASA have worked together to complete a parametric sizing study for NASA's Large Civil Tilt Rotor (LCTR2) concept 2nd iteration. Vehicle gross weight and fuel usage were evaluated as propulsion and drive system characteristics were varied to maximize the benefit of reduced rotor tip speed during cruise conditions. The study examined different combinations of engine and gearbox variability to achieve rotor cruise tip speed reductions down to 54% of the hover tip speed. Previous NASA studies identified that a 54% rotor speed reduction in cruise minimizes vehicle gross weight and fuel burn. The LCTR2 was the study baseline for initial sizing. This study included rotor tip speed ratios (cruise to hover) of 100%, 77% and 54% at different combinations of engine RPM and gearbox speed reductions, which were analyzed to achieve the lightest overall vehicle gross weight (GW) at the chosen rotor tip speed ratio. Different engine and gearbox technology levels are applied ranging from commercial off-the-shelf (COTS) engines and gearbox technology to entry-in-service (EIS) dates of 2025 and 2035 to assess the benefits of advanced technology on vehicle gross weight and fuel burn. Interim results were previously reported1. This technical paper extends that work and summarizes the final study results including additional engine and drive system study accomplishments. New vehicle sizing data is presented for engine performance at a single operating speed with a multispeed drive system. Modeling details for LCTR2 vehicle sizing and subject engine and drive sub-systems are presented as well. This study was conducted in support of NASA's Fundamental Aeronautics Program, Subsonic Rotary Wing Project.

  11. The Ĝ Infrared Search for Extraterrestrial Civilizations with Large Energy Supplies. III. The Reddest Extended Sources in WISE

    Science.gov (United States)

    Griffith, Roger L.; Wright, Jason T.; Maldonado, Jessica; Povich, Matthew S.; Sigurđsson, Steinn; Mullan, Brendan

    2015-04-01

    Nearby Type iii (galaxy-spanning) Kardashev supercivilizations would have high mid-infrared (MIR) luminosities. We have used the Wide-field Infrared Survey Explorer (WISE) to survey ∼ 1× {{10}5} galaxies for extreme MIR emission, 1 × 103 times more galaxies than the only previous such search. We have calibrated the WISE All-sky Catalog pipeline products to improve their photometry for extended sources. We present 563 extended sources with |b|≥slant 10 and red MIR colors, having visually vetted them to remove artifacts. No galaxies in our sample host an alien civilization reprocessing more than 85% of its starlight into the MIR, and only 50 galaxies, including Arp 220, have MIR luminosities consistent with \\gt 50% reprocessing. Ninety of these (likely) extragalactic sources have little literature presence; in most cases, they are likely barely resolved galaxies or pairs of galaxies undergoing large amounts of star formation. Five are new to science and deserve further study. The Be star 48 Librae sits within a MIR nebula, and we suggest that it may be creating dust. WISE, 2MASS, and Spitzer imagery shows that IRAS 04287+6444 is consistent with a previously unnoticed, heavily extinguished cluster of young stellar objects. We identify five “passive” (i.e., red) spiral galaxies with unusually high MIR and low NUV luminosity. We search a set of H i dark galaxies for MIR emission and find none. These 90 poorly understood sources and 5 anomalous passive spirals deserve follow-up via both SETI and conventional astrophysics.

  12. 中国大型运输机的发展%Discussion about Developing China Large Transport

    Institute of Scientific and Technical Information of China (English)

    谢钧

    2005-01-01

    Aircraft manufacturers always try to do new aircraft on an old basis. A300 is the basis of A380. It is very important for China to own a basis-one type of Chinese own commercial large transport. Trying to find some enlightenment from A380,for Chinese regional aircraft such as ARJ21, ERJ145 and other commercial large transports. Simultaneously,the opportunities and challenges to China Civil Aviation Industry are also discussed in this paper.

  13. Technical and economic assessment of swept-wing span-distributed load concepts for civil and military air cargo transports

    Science.gov (United States)

    1977-01-01

    The feasibility of large freighter aircraft was assessed, including the impact of military requirements on the performance, economics, and fuel consumption characteristics. Only configurations having net payloads of 272,155 to 544,311 kilograms contained within swept wings of constant chord were studied. These configurations were of advanced composite construction with controllable winglets and full-span digitally-controlled trailing-edge surfaces. Civil, military, and joint civil/military production programs were considered.

  14. Adjoint based on high precise aerodynamic shape optimization for transonic civil aircraft%基于伴随算子的大飞机气动布局精细优化设计

    Institute of Scientific and Technical Information of China (English)

    吴文华; 范召林; 陈德华; 覃宁; 孟德虹

    2012-01-01

    After decades of studies, the potentialities of traditional wing-body configuration are almost exhausted. So, it is difficult to improve the performance of the traditional aerodynamic shape of transonic civil aircraft by conventional design method. In this paper we develop ADJOINT method based on aerodynamics optimization software-ADJOPT, and the software is used to optimize the wing of a transonic civil aircraft with fuselage and nacelle, which is already optimized by traditional way. The optimization is multi-parameter, high precise and taking the influence of the fuselage and nacelle into account. The software performs well and gets obvious performance improvement. The research shows that multi-parameter optimization has the ability to exploit potentialities of a high-performance shape and increases the aerodynamic performance of it.%发展了基于伴随算子的气动布局优化设计软件-ADJOPT,并将该软件用于经过传统设计方法优化的大飞机布局上,开展全机状态下的机翼多参数、高精度优化设计,计入了短舱和机身对机翼气动特性的影响,取得了明显的优化效果.研究结果表明,多参数优化设计能够充分挖掘一个优良布局的设计潜力,进一步提高布局性能.

  15. 基于相异性表示的民机液压系统健康评估%Health Assessment of Civil Aircraft Hydraulic System Based on Dissimilarity Representation

    Institute of Scientific and Technical Information of China (English)

    侯晓云; 张天刚

    2012-01-01

    This paper carries out the health assessment of the civil aircraft hydraulic system. Based on the dissimilarity representation, one-class LP classifier is taken for the health assessment, to determine the parameters affecting the accuracy of the model assessment, to define the health index, to make the assessment of the overall test samples and non-normal samples, and to compare the results with the support vector machine hyper-sphere model. The evaluation results show that in the case of the selected appropriate parameters, one-class LP classifier based on the dissimilarity classifier model can assess the health of the civil aircraft hydraulic system, and performs better than the support vector machine hyper-sphere model.%为了实现对民航飞机液压系统的健康评估,基于相异性表示的方法,利用单类线性规划分类器模型进行健康评估,确定了影响模型评估准确率的参数,定义了健康指数,得到总体测试样本以及非正常样本的评估结果,且与支持向量机超球模型的评估结果进行比较.结果表明,在已选择相应参数的情况下,采用基于相异性表示的单类线性规划分类器模型可以对民机液压系统进行健康评估.

  16. Research on the Limitations of Cooling Mechanism Based on FRM for Civil Aircraft%民用飞机冷却降燃方案的局限性研究

    Institute of Scientific and Technical Information of China (English)

    张斌

    2016-01-01

    The fuel tank flammability reduction means design for civil aircraft is an important part of fuel tank ex-plosion proof design, it is necessary to carry out the related research. By studying the 25. 981 airworthiness require-ments for civil aircraft, this paper summarizes the fuel tank flammability requirements and the corresponding FRM ( flammability reduction means) , and also studies the applicability of cooling mechanism based on FRM. The re-sults show that this concept has some limitations in actual application, especially it can’ t meet flammability airwor-thiness requirement for the fuel tank within the fuselage configuration.%民用飞机降低燃油箱可燃性设计是燃油箱防爆设计的一个重要方面,有必要对其开展相关研究。通过对民用飞机燃油箱25.981适航条款要求的解读,总结了适航对燃油箱可燃性要求以及对应的降低燃油箱可燃性措施( FRM),并对基于冷却降燃方案的适用性进行分析研究,研究结果表明该方案在实际应用中具有一定局限性,尤其是无法满足位于机身内非主燃油箱的可燃性适航要求。

  17. Resin Film Infusion (RFI) Process Modeling for Large Transport Aircraft Wing Structures

    Science.gov (United States)

    Knott, Tamara W.; Loos, Alfred C.

    2000-01-01

    Resin film infusion (RFI) is a cost-effective method for fabricating stiffened aircraft wing structures. The RFI process lends itself to the use of near net shape textile preforms manufactured through a variety of automated textile processes such as knitting and braiding. Often, these advanced fiber architecture preforms have through-the-thickness stitching for improved damage tolerance and delamination resistance. The challenge presently facing RFI is to refine the process to ensure complete infiltration and cure of a geometrically complex shape preform with the high fiber volume fraction needed for structural applications. An accurate measurement of preform permeability is critical for successful modeling of the RFI resin infiltration process. Small changes in the permeability can result in very different infiltration behavior and times. Therefore, it is important to accurately measure the permeabilities of the textile preforms used in the RFI process. The objective of this investigation was to develop test methods that can be used to measure the compaction behavior and permeabilities of high fiber volume fraction, advanced fiber architecture textile preforms. These preforms are often highly compacted due to through-the-thickness stitching used to improve damage tolerance. Test fixtures were designed and fabricated and used to measure both transverse and in-plane permeabilities. The fixtures were used to measure the permeabilities of multiaxial warp knit and triaxial braided preforms at fiber volume fractions from 55% to 65%. In addition, the effects of stitching characteristics, thickness, and batch variability on permeability and compaction behavior were investigated.

  18. RISK DEFINITION IN CIVIL UNMANNED AVIATION

    Directory of Open Access Journals (Sweden)

    Volodymyr Kharchenko

    2016-12-01

    Full Text Available Objective: The risks in unmanned civil aviation are considered as one of the most important. In the article is proved applicability of ensuring the flight safety of aircraft and considered the basic risks of manned civil aviation. Methods: Analyzed statistical data on aviation accidents, organized probabilities distribution of aviation accidents for manned and unmanned civil aviation to identify factors that influence the occurrence of emergency situations in manned and unmanned aviation. Results: We proposed typology of risk components in civil aviation and systematized methods and techniques to reduce risks. Over the analogies defined possible risks, their causes and remedies in civil unmanned aircraft. Weight coefficients distribution was justified between risk types for development of recommendations on risk management in unmanned civil aviation. Discussion: We found that the most probable risk in manned civil aviation is the human factor, organization of air traffic control, design flaws of unmanned aviation system as a whole, as well as maintenance of unmanned aviation system.

  19. Description of Re-manufacture Project of Civil Aircraft Structure%民用飞机结构再制造工程概论

    Institute of Scientific and Technical Information of China (English)

    范耀宇

    2015-01-01

    This article states the status of re-manufacture, typical re-manufacture process. It is also planning the method, outline and critical issues of civil airplane structure re-manufacture program from the top level.%阐述再制造工程现状、典型工艺,并从顶层规划了民机结构再制造工程研究思路、总体框架和关键技术。

  20. Detection of triazole deicing additives in soil samples from airports with low, mid, and large volume aircraft deicing activities.

    Science.gov (United States)

    McNeill, K S; Cancilla, D A

    2009-03-01

    Soil samples from three USA airports representing low, mid, and large volume users of aircraft deicing fluids (ADAFs) were analyzed by LC/MS/MS for the presence of triazoles, a class of corrosion inhibitors historically used in ADAFs. Triazoles, specifically the 4-methyl-1H-benzotriazole and the 5-methyl-1H-benzotriazole, were detected in a majority of samples and ranged from 2.35 to 424.19 microg/kg. Previous studies have focused primarily on ground and surface water impacts of larger volume ADAF users. The detection of triazoles in soils at low volume ADAF use airports suggests that deicing activities may have a broader environmental impact than previously considered.

  1. On Civility and Civilizations

    Institute of Scientific and Technical Information of China (English)

    DAVID GOSSET

    2010-01-01

    @@ At a time when misunderstand-ings between cultures run rampant, when walls of fear, prejudice and hatred divide the members of the human family, it is urgent to intensify the dialogue between civilizations. Under the new leadership of its Director General lrina Bokova, the United Nations Educational, Scientific and Cultural Organization (UNESCO) declared 2010 as the "Year for the Rapprochement of Cultures." In this context, the concerted reflections and actions of Europe and China can be highly meaningful.

  2. Aircraft Disinsection: A Guide for Military and Civilian Air Carriers (Desinsectisation des aeronefs: Un guide a l’intention des responsables des transports aeriens civils et militaires)

    Science.gov (United States)

    1996-04-01

    and other pests (e.g., viruses, bac- within the fuselage. The exterior surfaces teria, fungi, amphibians , snakes, birds, and and wheel housings are of...Sudan to the subject of aircraft disinsection. The - Sri Lanka - Surinam resurgence has been caused by the disin- - Swaziland - Tanzania tegration of...is being re- birds, amphibians ), seeds, and meat pro- turned from abroad, every effort should be ducts. made to ensure that it is free of pests

  3. Validation of a New Developed Aerodynamics Analysis Toolkit for Civil Aircraft Configurations%运输类飞机气动力分析软件ATTF的开发与验证

    Institute of Scientific and Technical Information of China (English)

    李广宁; 李凤蔚; 周志宏

    2011-01-01

    针对我国运输类飞机设计与发展的实际需要,开发设计了一种高效的复杂外形气动力计算与分析软件ATTF(Analysis Toolkit for Transonic Flows).软件采用结构化多块计算网格,通过求解Navier-Stokes方程,实现三维复杂外形粘性绕流流场的数值模拟.控制方程的求解采用Jameson中心有限体积+人工粘性格式,并采用显式五步Runge-Kutta格式进行时间推进求解.方程求解采用了当地时间步长、变系数隐式残值光顺以及多重网格等多种加速收敛措施.程序采用动态内存管理技术以提高计算机有限内存的利用率.在确保控制信息和边界信息准确无误、内存容量允许的条件下,同一个可执行文件可以用于不同几何外形、不同网格规模和拓扑结构的流场数值求解.为检验ATTF程序的计算效率和稳定性,验证其对于复杂外形气动力特性的预测和评估能力,文章针对DLR-F6带短舱挂架的跨声速宽体运输类飞机外形进行了数值模拟与计算,并与风洞试验结果、CFL3D和TRIP2.0的计算结果进行了分析对比,结果显示AM软件的计算结果是可靠的,其计算精度与国内外同类软件相当.%An efficient computational fluid dynamics (CFD) software named ATTF ( Analysis Toolkit for Transonic Flows) for the aerodynamics prediction of complex configurations is developed to meet the engineering requirement for the large aircraft project in China. The compressible thin-layer Reynolds-averaged Navier-Stokes equations are solved to simulate the three-dimensional complex viscous flows, and the computational grids are structured multi-block grids with one-to-one mapping style to exchange the flow field information. The control equations are solved using Jameson's central differenced finite volume method and an explicit five-stage Runge-Kutta scheme is used to advance the solutions to steady state. To improve the efficiency of the solver, several techniques such as

  4. Test and Evaluation of Ultrasonic Additive Manufacturing (UAM) for a Large Aircraft Maintenance Shelter (LAMS) Baseplate

    Science.gov (United States)

    2015-03-26

    to machine . A new manufacturing process is emerging called additive manufacturing (AM) and its beginnings can be traced to the 1980s. AM, as...opposed to subtractive manufacturing , builds a design up layer by layer into a component saving time and machining cost in addition to granting a wide...TEST AND EVALUATION OF ULTRASONIC ADDITIVE MANUFACTURING (UAM) FOR A LARGE AREA MAINTENANCE

  5. Aircraft Emissions Characterization

    Science.gov (United States)

    1988-03-01

    sample from each trap through a heated (1500C) six-port valve ’ Carle Instruments Model 5621) and onto the analytical column. The coLoponents in each...Environmental Protection, Vol. II. Aircraft Engine Emissions, Int. Civil Aviation Organ., 1981. 7. Nebel , G. J., "Benzene in Auto Exhaust," J. Air Poll

  6. Computational Flame Characterization of New Large Aircraft Immersed in Hydrocarbon Pool Fires

    Science.gov (United States)

    2013-08-01

    Composite Profile Map of the A380 1 2 The NLA Mockup Engulfed in a JP-8 Pool Fire and After the JP-8 Pool Fire Using Infrared Imagery 2 3 The...Government’s approval or disapproval of its ideas or findings. 2 (a) (b) Figure 2. The NLA Mockup (a) Engulfed in a JP-8 Pool...CFD software suite, and simulation development. The literature survey briefly introduces the physical principles associated with large-scale

  7. Effect of drop size on the impact thermodynamics for supercooled large droplet in aircraft icing

    Science.gov (United States)

    Zhang, Chen; Liu, Hong

    2016-06-01

    Supercooled large droplet (SLD), which can cause abnormal icing, is a well-known issue in aerospace engineering. Although efforts have been exerted to understand large droplet impact dynamics and the supercooled feature in the film/substrate interface, respectively, the thermodynamic effect during the SLD impact process has not received sufficient attention. This work conducts experimental studies to determine the effects of drop size on the thermodynamics for supercooled large droplet impingement. Through phenomenological reproduction, the rapid-freezing characteristics are observed in diameters of 400, 800, and 1300 μm. The experimental analysis provides information on the maximum spreading rate and the shrinkage rate of the drop, the supercooled diffusive rate, and the freezing time. A physical explanation of this unsteady heat transfer process is proposed theoretically, which indicates that the drop size is a critical factor influencing the supercooled heat exchange and effective heat transfer duration between the film/substrate interface. On the basis of the present experimental data and theoretical analysis, an impinging heating model is developed and applied to typical SLD cases. The model behaves as anticipated, which underlines the wide applicability to SLD icing problems in related fields.

  8. The Supplier Quality Management System Evaluation of Civil Aircraft Development%民机研制供应商质量管理体系评价

    Institute of Scientific and Technical Information of China (English)

    张培发; 张发玉

    2012-01-01

    对主制造商-供应商研制模式下的供应商质量对飞机研制的影响做了探讨,叙述了不同类型供应商的质量体系评价原则,主要包括体系标准、审核要素、审核周期、不符合项更改等指标.对于供应商绩效考核则主要依据其在飞机研制中的重要度等级采取不同周期和内容的考核方式,通过上述供应商质量体系的评价与考核,可以首先选择通过AS/EN/JAN9100标准的公司,最大限度地降低供应商选择的风险.%Based on the aircraft development, it analyzes the mode of main manufacturer -supplier development such as the evaluation principles for different types of suppliers, the quality system standards, audit and audit cycle , non - conformance and so on. Aiming at the main basis of the aircraft development, it researches the supplier performance evaluation, choices the AS/EN/JAN9100 standard of the company, reduces the risk in choosing suppliers.

  9. 民用航空器侵权责任主体的相对性及其突破%The Relativity of Civil Aircraft Tort Liability Subject and Its Breakthrough

    Institute of Scientific and Technical Information of China (English)

    王锡柱

    2015-01-01

    The tort liability of civil aircraft in Tort Liability Law belongs to the category of high risk liability. Whether or not the operator of a civil aircraft is at fault or not,he has to assume responsibility. However,besides the operator,whether or not the third party is at fault could be taken as the responsibility subject,and whether the victim can claim directly to such third party,are not specified in Tort Liability Law,which results in the relativity of subject of tort liability in civil aircraft. The relativity to some extent is beneficial to victims as balance between risks and benefits as well as an embodiment of the economic responsibility,but the relativity is not conducive to intactness of tort liability law system and could not protect the benefits of victims and operators perfectly. Given the balance of interests as well as the standard of making a clear distinction between right and wrong,it is necessary to break the relativity,taking the third party at fault as responsibility subject and to give the victim the right to claim directly to the third party.%我国《侵权责任法》中民用航空器侵权责任属于高度危险责任范畴,民用航空器经营人有无过错,均应承担责任。然而,对于经营人之外有过失的第三人能否作为责任主体,以及受害人能否向此类第三人直接求偿并未在该法中得到明确,进而造成了民用航空器侵权责任主体的相对性。这种相对性在一定程度上保护了受害者,是风险与收益平衡的选择以及经济责任的体现,但是这种相对性不利于侵权责任法体系的完整,对于受害人以及航空器经营人的保护并不周延。基于利益平衡以及明辨是非的标准有必要突破这种责任主体的相对性,将具有过失的第三人作为责任主体,并赋予受害人向第三人的直接请求权。

  10. Developing Large-Scale Bayesian Networks by Composition: Fault Diagnosis of Electrical Power Systems in Aircraft and Spacecraft

    Science.gov (United States)

    Mengshoel, Ole Jakob; Poll, Scott; Kurtoglu, Tolga

    2009-01-01

    In this paper, we investigate the use of Bayesian networks to construct large-scale diagnostic systems. In particular, we consider the development of large-scale Bayesian networks by composition. This compositional approach reflects how (often redundant) subsystems are architected to form systems such as electrical power systems. We develop high-level specifications, Bayesian networks, clique trees, and arithmetic circuits representing 24 different electrical power systems. The largest among these 24 Bayesian networks contains over 1,000 random variables. Another BN represents the real-world electrical power system ADAPT, which is representative of electrical power systems deployed in aerospace vehicles. In addition to demonstrating the scalability of the compositional approach, we briefly report on experimental results from the diagnostic competition DXC, where the ProADAPT team, using techniques discussed here, obtained the highest scores in both Tier 1 (among 9 international competitors) and Tier 2 (among 6 international competitors) of the industrial track. While we consider diagnosis of power systems specifically, we believe this work is relevant to other system health management problems, in particular in dependable systems such as aircraft and spacecraft. (See CASI ID 20100021910 for supplemental data disk.)

  11. 大型民机企业人力资源能力建设评价研究*%Research on Human Resource Construction Evaluation of Large Aircraft Corporation

    Institute of Scientific and Technical Information of China (English)

    杨生斌; 孙振杰; 孔莹

    2013-01-01

    Large aircraft corporations need strong human resources to support,in view of "I am the Lord", "the Lord manufacturers and suppliers" develop-ment model in China's large aircraft corporations, the importance of corporations internal human resources con-struction is indicated. Through using the benchmarking corporations Boeing and Airbus company human resource practices, from investment, performance and output three aspects, the large aircraft corporations human resources construction evaluation index system and evaluation model are constructed so as to improve human resources con-struction standard of large aircraft corporations in China.%大型民机企业需要强有力的人力资源做支撑,针对我国大型民机企业“以我为主”、“主制造商+供应商”的发展模式,明确企业内部人力资源能力建设的重要性。通过借鉴标杆企业波音和空客的人力资源实践,从投入、表现和产出3方面入手构建了大型民机企业人力资源能力建设评价指标体系和评价模型,以期促进我国大型民机企业人力资源能力不断提升。

  12. Aerodynamic Analysis of Civil Aircraft Equipped with Winglet on Numerical Simulation%民机翼梢小翼气动特性数值模拟分析研究

    Institute of Scientific and Technical Information of China (English)

    蒋彪; 李杰

    2011-01-01

    A certain type of civil aircraft wing and body are equipped with two different forms of winglets - Fusion Winglet and tip- fence. The point- to- point patched multi- block technology was used to generate high quality grid by ICEM software. Three- dimensional time- dependent compressible Reynolds- averaged Navier- Stokes equations were solved with third- order upwind- biased flux- difference splitting method and approximate factorization method. The numerical simulation was adopted to obtain reasonable geometry parameters of two different winglets at cruise point. The result data indicates that both winglet has increased lift coefficient and decreased drag coefficient, compared with the original wing- body model. The fusion wing, let increased the lift to drag ratio by 9%, and the tip fence increased the lift to drag ratio by 6%. However, the advantage of wing-body equipped with tip-fence in moment characteristic is obvious.The conclusions have great engineering application value in the design of civil aircraft winglet.%针对某民机翼身组合体加装不同翼梢小翼--融合式翼梢小翼和翼尖涡扩散器进行对比分析.用软件ICEM生成原始翼身组合体及加装不同小翼的翼身组合体的点对点对接多块网格技术生成高质量的数值计算网格,运用Roe三阶迎风偏置通量差分裂方法和隐式近似因子分解方法求解雷诺平均N-S方程.对两种不同翼梢小翼在巡航点进行数值模拟,得到合理的翼稍小翼几何参数;对比升阻特性数据,两种翼梢小翼都可以提高升力系数,减少阻力系数.相对原始翼身组合体,融合式翼梢小翼升阻比增加9%,翼尖涡扩散器升阻比增加6%;但翼尖涡扩散器在力矩特性上有较大优势.所得结论对民用飞机翼稍小翼设计工作具有较大的工程应用价值.

  13. 民用飞机外翼与中央翼上壁板连接形式的研究%Research on the Upper Panel Joint of Outer Wing and Center Wing for Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    方采文; 张树军; 贾大炜; 李同

    2015-01-01

    The design and assembly of joint between outer wing and center wing is essential for the developing commercial aircraft. Five kinds of joints for upper panel between outer wing and center wing were researched in this article. CATIA models were established. Using the finite element calculation, the stress and strain condition of the same load was obtained. Comparation and analysis were given from loading, manufacturing and weight, in order to get the advantages and disadvantages of the different joints. The research could provide a technology support for civ-il aircraft structure design.%在现代民用飞机的设计研发中,外翼与中央翼连接处的设计和装配是重中之重。通过对5种外翼与中央翼上壁板连接形式进行研究,建立CATIA模型,通过有限元计算,得出相同载荷形式下的应力应变情况。并从受力、工艺和重量等方面进行分析、比较,初步给出几种外翼与中央翼连接形式的优劣。旨在为类似机型外翼与中央翼上壁板连接形式的确定提供有效思路和技术支持。

  14. 14 CFR 183.27 - Designated aircraft maintenance inspectors.

    Science.gov (United States)

    2010-01-01

    ... 14 Aeronautics and Space 3 2010-01-01 2010-01-01 false Designated aircraft maintenance inspectors...: Privileges § 183.27 Designated aircraft maintenance inspectors. A designated aircraft maintenance inspector (DAMI) may approve maintenance on civil aircraft used by United States military flying clubs in foreign...

  15. Estimation of the Aircraft CO2 Emission of China's Civil Aviation During 1960-2009%1960-2009年中国民航飞机的CO2逐年排放变化

    Institute of Scientific and Technical Information of China (English)

    何吉成

    2011-01-01

    基于中国民航部门逐年统计数据,计算了1960- 2009年中国民航飞机的CO2逐年排放量,分析了中国民肮飞机CO2排放强度及其变化特点.结果表明:中国民航飞机CO2总排放量由1960年的12.0万t增至2009年的4144万t;CO2排放强度呈明显的降低趋势,由1960年的2.9 kg/换算吨公里降至2009年的0.96 kg/换算吨公里,年均降低0.04 kg/换算吨公里.中国民肮飞机的CO2排放量占整个交通运输仓储和邮政行业CO2排放量的比例较低,仅占6.6%,占全国化石燃料燃烧CO2排放量的比例也很小,平均只有0.25%.%Based on the annual production data collected by Chinese Civil Aviation Statistic Center, the yearly CO2 emission of aircrafts during 1960-2009 was calculated, and the emission intensity and its dynamic characteristics were analyzed. The results show that the total CO2 emission of aircrafts in China increased from 120 kt in 1960 to 41.44 Mt in 2009. The emission intensity of CO2 decreased from 2.9 kg/(converted t · Km) in 1960 to 0.96 kg/(converted t · km) in 2009 at an average rate of 0.04 kg/(converted t · km) per year. The average proportion of the CO2 emission of aircrafts to the total CO2 emission from the sector of transportation, storage and post was 6.6% in the period of 1980-2005, and to the total emission from fossil fuel combustion was 0.25% in the period of 1971-2008.

  16. Wind tunnel test for turbo-fan engine re-ingestion characteristic of civil aircraft%民机涡扇发动机重吸入特性风洞试验

    Institute of Scientific and Technical Information of China (English)

    李达新; 赵克良; 王奇志; 盛鸣剑; 黄勇; 张美红

    2012-01-01

    民机在滑跑减速阶段一般会使用发动机的反向推力来提高其减速性能和滑跑安全性,当滑跑速度较低时使用该装置,从发动机排出的向前方喷射的气流存在被发动机重新吸入的可能,该喷流受发动机风扇的压缩做功,喷流的温度比环境温度高,如果此气流被发动机重新吸入,将会导致发动机进气气流的温度畸变,而该畸变将会引起发动机风扇叶片的颤振,影响发动机的寿命和安全性.故对于一个使用涡扇发动机的新型飞机,有必要通过风洞试验来得到其在各工况下的重吸入特性,并且根据其重吸入特性,设定截止使用反推力的滑跑速度.本文主要论述通过风洞试验获得发动机重吸入特性,并且确定反推力使用截止滑跑速度的方法.%For civil aircraft it is common method to use thrust reverser to improve the deceleration and the safety during landing run. However, if the ground running speed of the aircraft is too low, the forward moving plume flow can be re-ingested by the engine. The temperature of the plume flow is much higher than ambient temperature since it gains energy from fan compressor. As a result the re-ingestion may lead to the temperature distortion for inlet flow causing the flutter of the fan blade, thus harming the engine life and safety. Therefore, for a new turbo-fan aircraft it is necessary to obtain the re-ingestion characteristic of the engine through wind tunnel test in order to determine the turn-off speed limit for thrust reverser. This paper mainly states the method to get the A/C's re-ingestion characteristics from the wind tunnel test and acquire the thrust reverser cut-off taxiing speeds.

  17. Research of Data Management in the Development Phase of Civil Aircraft Based on System Engineering%基于系统工程的民用飞机研制阶段数据管理研究

    Institute of Scientific and Technical Information of China (English)

    刘冰

    2016-01-01

    Through analysis of major work content at the various stages of airplane development process,combined of system engineering methods to analyze the producing process,relevance and use of data,defined the main goal of civil aircraft data management,presented the ideal of data inventory planning and the key elements of data management programs,and gave recommendations of data management software evaluation.%通过对飞机研制各阶段主要工作内容的分析,结合系统工程方法对数据的产生、数据的关联性以及数据用途进行研究,进而确定民用飞机数据管理的主要目标,提出数据清单规划的工作思路,定义数据管理计划的关键要素,并对数据管理软件的评估给出建议。

  18. Study on Electrically Conductive Elastomer Shielding Efficiency for HIRF Condition of Civil Aircraft Electronics Equipment Bay%民用飞机设备舱舱门导电橡胶屏蔽效能研究

    Institute of Scientific and Technical Information of China (English)

    王永根; 代继刚; 王乐意

    2014-01-01

    通过理论计算和软件仿真相结合的方法,给出了民用飞机电子电气设备舱高强度辐射场( HIRF)条件下的腔体谐振特性,并对腔体内部电磁场进行仿真。通过对比舱门缝隙导电橡胶屏蔽效能的仿真结果,给出了电子电气设备舱不同状态下的电磁场分布结果,为电子电气舱舱门屏蔽设计提供技术支持。%Resonance Characteristic of the civil aircraft electronics equipment bay ( E/E Bay ) on HIRF condition is obtained through combining the theory calculation with software simulation method .Compa-ring the simulation results of the electrically conductive elastomer shield efficiency , the electromagnetic field inside the E/E bay are supplied ,and this simulation results can support the E/E bay door design .

  19. Successfully Managing the Experimental Area of a Large Physics Experiment from Civil Engineering to the First Beams

    CERN Document Server

    Butin, F

    2010-01-01

    The role of "Experimental Area Manager" supported by a well organized, charismatic and motivated team is absolutely essential for managing the huge effort needed for a multi-cultural, multi-disciplinary installation of cathedral-size underground caverns housing a billion dollar physics experiment. Between the years 2002 and 2008, we supervised and coordinated the ATLAS work site at LHC, from the end of the civil engineering to the first circulating beams, culminating with 240 workers on the site, 24 hours a day, 7 days a week, with activities taking place simultaneously on the surface, in the 60 m shafts and in the 100 m underground experimental cavern. We depict the activities preparation scheme (including tasks ranging from the installation of 280 ton cranes to super-delicate silicon detectors), the work-site organization method, the safety management that was a top priority throughout the whole project, and the opencommunication strategy that required maintaining permanent public visits. The accumulation o...

  20. 襟缝翼对民用飞机失速特性的影响%Effect of Slat and Flap on Stall Characteristic of Civil Aircraft

    Institute of Scientific and Technical Information of China (English)

    周涛; 李亚林; 梁益华; 陈迎春

    2012-01-01

    To detect factors of affecting stall characteristic and stability of aircraft, slot parameter of out board slat, separation face of inboard slat and fuselage, slot between slat and pylon, and slot parameter of flap were investigated. The results indicate that, root and tip of slat may affect pitching moment character- istic, slot between slat and pylon may improve lift coefficient, but no contribution for pitching moment characteristic, and, adjusting deploy angle of flap may not improve separation characteristic on main wing, because effective camber of wing is not changed.%从外侧缝翼缝道参数、内侧缝翼分离面、缝翼与挂架间隙以及后缘襟翼缝道参数等方面考虑,分析了民用飞机失速特性和失稳特性的影响因素.结果表明,前缘缝翼根部和梢部细节对力矩特性有较大影响,缝翼挂架堵缝可提高升力,不影响力矩特性,调整襟翼偏角,可改变机翼有效弯度,不改变主翼分离特性.

  1. Design, analysis, and control of large transport aircraft utilizing engine thrust as a backup system for the primary flight controls

    Science.gov (United States)

    Gerren, Donna S.

    1993-01-01

    A review of accidents that involved the loss of hydraulic flight control systems serves as an introduction to this project. In each of the accidents--involving transport aircraft such as the DC-10, the C-5A, the L-1011, and the Boeing 747--the flight crew attempted to control the aircraft by means of thrust control. Although these incidents had tragic endings, in the absence of control power due to primary control system failure, control power generated by selective application of engine thrust has proven to be a viable alternative. NASA Dryden has demonstrated the feasibility of controlling an aircraft during level flight, approach, and landing conditions using an augmented throttles-only control system. This system has been successfully flown in the flight test simulator for the B-720 passenger transport and the F-15 air superiority fighter and in actual flight tests for the F-15 aircraft. The Douglas Aircraft Company is developing a similar system for the MD-11 aircraft. The project's ultimate goal is to provide data for the development of thrust control systems for mega-transports (600+ passengers).

  2. China's Civil Regional Transport Aircraft Sales Model: Research on Xinzhou 60 Aircraft Market Sales Model%中国民用支线运输飞机销售模式——新舟60飞机市场销售模式研究

    Institute of Scientific and Technical Information of China (English)

    蔡长宏

    2011-01-01

    目前对飞机市场销售模式的研究还处在探讨阶段,大量的文献都是对一些普通产品做一些市场分析,在对飞机销售市场研究方面并没有过多的分析.因此,本文主要以新舟60飞机销售体系为列,运用市场细分、产品定位和渠道管理、宣传推广等理论,制定出新舟60飞机市场销售体系模式.%At present, the research on the market sales model of aircraft is still in discussion stage. A large number of literatures only do some market analysis on common products, the research on the aircraft sales market is less. Therefore, taking Xinzhou 60 aircraft sales system as an example, this article formulates Xinzhou 60 aircraft market sales system using market segment, product positioning and channel management, promotion.

  3. ABMS of Civil Aircraft Partnership Risk Management:Taking Civil Aircraft Supply Chain as an Example%跨组织项目的合作伙伴关系风险仿真研究--以民机供应链为例

    Institute of Scientific and Technical Information of China (English)

    张亚莉; 姜香美; 鲁梦华

    2014-01-01

    作为典型的跨组织项目,大飞机项目涉及多个供应商,并面临诸多风险。为了准确描绘复杂系统的风险管理过程,与目前普遍采用的单纯数学解析风险模型的技术视角不同,本文利用智能体仿真建模来研究民机供应链风险沟通过程及风险沟通影响因素对风险管理绩效的影响,仿真结果表明:1)民机制造商在力量格局中处于劣势状态的情况下,在供应链合作伙伴间增加沟通次数能够降低整个项目周期的风险影响;2)在民机制造商的风险控制能力一定的条件下,适当规模的供应链合作伙伴关系能够降低项目风险。最后,文章提出了管理建议。%As a typical cross-organizational project involving multiple vendors,large aircraft project is faced with numerous risks.Suitable risk management strategies are required to be established based on the past experience and existing risk man-agement methods.Different from mathematical analyzing model,Agent-based Modeling is applied to simulate performance of risk management effected by risk communication processes as well as the risk communication effectors.The simulation re-sults show that:1)At a disadvantage in the power equation,the risk of the entire project cycle can be lowered by increasing the communication between supply chain partners;2)Under certain ability of risk control,project risks can be reduced by appropriate size of supply chain partnership.At last,management recommendations are put forward.

  4. Pressure Reliefs of Cockpit Doors of Civil Aircraft%民机驾驶舱门卸压方式选择探讨

    Institute of Scientific and Technical Information of China (English)

    安琳琳; 汪洋

    2014-01-01

    If the cockpit windshields of civilian aircraft have holes in the process of high speed ,the pressure fall sharply and the differential pressure of cockpit and cabin increases quickly ,w hich must relieve pressure to balance the cockpit and cabin pressure . Such as pressure relief in a untimely manner will cause serious harm to the crew body as well as cockpit floor and structure and cause serious damage ,even to pilots’ lives to cause plane crash .So the cockpit has quick pressure relief device .The discharge pressure plate often designed on the cockpit doors .There are mechanical pressure relief and electronic pressure ,and this paper analyzes the two kinds of pressure reliefs .%民用飞机在高空高速飞行过程中,若驾驶舱风挡玻璃出现孔洞,则驾驶舱门内压力急剧下降,此时驾驶舱和客舱压差迅速增大,必须通过快速卸压以平衡驾驶舱和客舱压力。如卸压不及时将会对机组人员身体造成严重伤害,同时对驾驶舱地板和结构等造成严重破坏。严重时将危及飞行员生命,使整个飞机失去控制,且有坠机发生。因此驾驶舱内必须设计有快速卸压装置。民机通常将卸压板设计在驾驶舱门上,目前有机械式卸压和电子卸压两种卸压方式,对这两种卸压方式进行了介绍分析。

  5. Flutter of a civil aircraft with wing ice accumulation%民用飞机翼面结冰颤振特性研究

    Institute of Scientific and Technical Information of China (English)

    范石磊; 章俊杰; 李效法

    2011-01-01

    翼面结冰是运输类飞机适航标准气动弹性稳定性要求条款(CCAR25.629)规定的必须考虑的失效、故障与不利条件之一,必须通过风洞试验和理论分析相结合的方法来表明飞机对该适航条款的符合性.针对某型民用飞机,进行了模拟翼面不同结冰状态的颤振模型风洞试验,采用希利普法外推得到颤振速度;同时对不同结冰状态进行了理论分析.试验与分析结果表明,该型飞机翼面结冰状态下颤振形式为机翼弯扭耦合;翼面结冰对该型飞机颤振速度无不利影响;该型飞机翼面结冰状态满足颤振包线要求.%The aeroelastic stability requirements of airworthiness standard for transport category airplanes ( CCAR25.629) prescribe that icing on wing surfaces is one of failures, malfunctions, and adverse conditions which must be considered.The compliance with the airworthiness standard must be shown with wind tunnel test and theoretical analysis.For a civil airplane, wind tunnel test was carried out to simulate different ice accumulation expected on wing surfaces.Schlipp's Method was used to extrapolate the flutter speed.And study was done to analyze different icing conditions.The results of test and analysis showed that the flutter form under icing condition is coupled with wing's bending and torsion; ice accumulation on wing surfaces has no adverse influence on aeroplane's flutter speed; and this type of aeroplane can satisfy the requests of a flutter envelope.

  6. Large-eddy simulation of a turbulent jet and a vortex sheet interaction: particle formation and evolution in the near field of an aircraft wake

    Directory of Open Access Journals (Sweden)

    Roberto Paoli

    2008-04-01

    Full Text Available Aircraft are prolific sources of particles (soot, liquid aerosols and contrails that can impact cloudiness and affect the Earth's radiative budget balance. In order to study the formation and evolution of these particles, a numerical approach has been developed combining large-eddy simulation (LES and a detailed microphysical model. Generally very detailed microphysical models are run along a single average trajectory, without any temperature fluctuation. However, this approach may lead to significant differences in particle properties and particle size distribution as it oversimplifies dynamical and mixing processes compared to multidimensional descriptions of aircraft wakes. This may affect the initialisation of meso-scale models, such as, for example, the formation of cloud condensation nuclei from persistent contrails, and heterogeneous chemical reactions. In this paper, we present the results of detailed microphysical processes calculations applied to a large number of fluid parcels trajectories, generated by a LES two-phase flow solver.

  7. Research of Wing Anti-ice System Performance Validation for Civil Aircraft%某型飞机机翼防冰系统性能验证研究

    Institute of Scientific and Technical Information of China (English)

    霍西恒; 王大伟; 李革萍; 李志茂

    2013-01-01

    A certain type of civil aircraft wing anti-ice system performance validation was introduced briefly first:the 2. 5D test model to verify the performance of three dimensional wing anti-ice system. A typical test condition selected to carry out the calculation of 2. 5D model and 3D model performance, meantime the icing wind tunnel test result of 2. 5D model for same condition was analyzed. At last, the 2. 5D model calculation results with the experi-mental results were compared and analyzed, and fixed the calculation results of 3D model,so as to achieve the pur-pose to verify the ice protection system performance.%介绍了某型支线客机机翼防冰系统的性能验证思路,即通过采用2.5D试验模型验证三维防冰系统的性能。选取一个典型状态点分别进行了2.5D及三维模型的性能计算分析,同时进行了相同状态点时2.5D模型的冰风洞试验结果分析,最后将2.5D模型计算结果与试验结果进行对比分析,修正3D模型的计算结果,从而达到验证整个防冰系统性能的目的。

  8. 民用飞机高升力控制系统安全性评估方法浅析%The review on the safety assessment method for high lift control system of civil aircraft

    Institute of Scientific and Technical Information of China (English)

    杨志丹

    2015-01-01

    It introduces the processes and methods for the safety assessment, proposes the analysis items in the stage such as the Functional Hazard Analysis( FHA) , Preliminary System Safety Assessment( PSSA) and System Safety Assessment( SSA) , discusses the assessment method at various stages.Based on the above safety assess-ment methods, it takes a type of civil aviation aircraft as an example, carries out functional hazard analysis, de-fines all function failure in the system process.Based on the extent of failure damage, it classifies these failure, establishes the failure trees according to 1 class function, carries PSSA and SSA, verifies that the system design satisfies the requirement of safety index.%对系统安全性评估的流程和方法进行了研究,分析了功能危害性评估( FHA)、初步安全性评估( PSSA)、系统安全性评估( SSA)3个阶段内容,并探讨了各阶段运用的评估方法。基于以上安全性评估方法,对某民机高升力控制系统进行FHA,确定了系统可能发生的所有功能失效故障,然后按失效故障危害影响程度对这些失效故障进行了分类。以其中一项Ⅰ类功能故障为例建立故障树,对其开展了PSSA和SSA,验证了系统设计满足安全性指标要求。

  9. Toward the bi-modal camber morphing of large aircraft wing flaps: the CleanSky experience

    Science.gov (United States)

    Pecora, R.; Amoroso, F.; Magnifico, M.

    2016-04-01

    The Green Regional Aircraft (GRA), one of the six CleanSky platforms, represents the largest European effort toward the greening of next generation air transportation through the implementation of advanced aircraft technologies. In this framework researches were carried out to develop an innovative wing flap enabling airfoil morphing according to two different modes depending on aircraft flight condition and flap setting: - Camber morphing mode. Morphing of the flap camber to enhance high-lift performances during take-off and landing (flap deployed); - Tab-like morphing mode. Upwards and downwards deflection of the flap tip during cruise (flap stowed) for load control at high speed and consequent optimization of aerodynamic efficiency. A true-scale flap segment of a reference aircraft (EASA CS25 category) was selected as investigation domain for the new architecture in order to duly face the challenges posed by real wing installation issues especially with reference to the tapered geometrical layout and 3D aerodynamic loads distributions. The investigation domain covered the flap region spanning 3.6 m from the wing kink and resulted characterized by a taper ratio equal to 0.75 with a root chord of 1.2 m. High TRL solutions for the adaptive structure, actuation and control system were duly analyzed and integrated while assuring overall device compliance with industrial standards and applicable airworthiness requirements.

  10. Civil Identity

    DEFF Research Database (Denmark)

    Petersen, Lars Axel

    scanning, etc., to discussions of Shari'a law versus common civil law in India; from the study of religious cult in ancient city states to the processes of constitutional reconstruction in former Communist countries; and from attempts at conflict resolution and prevention between Jewish and Arab citizens...... of Israel to Luce Irigaray's Feminist agenda of elaborating gender specific civil identities. My intention is to investigate whether these different employments of 'civil identity' point towards a common, and fairly well defined object field asking questions of contemporary relevance to the philosophy...... of technology and of law. If such a field can be established, the answers to those questions might be relevant to such contemporary issues as inter-ethnic, religious, and -cultural conflict or reconciliation, migration and nationality, civil rights and surveillance, security and privacy, bureaucracy and inter...

  11. The longitudinal static stability of tailless aircraft

    OpenAIRE

    de Castro, Helena V.

    2001-01-01

    This paper describes the development of a simple theory of the longitudinal controls fixed static stability of tailless aeroplanes. The classical theory, as developed for the conventional aircraft, is modified to accommodate the particular features of the tailless aeroplanes. The theory was then applied to a particular blended-wing-body tailless civil transport aircraft, BWB-98. Cranfield University

  12. Maintenance of air worthiness of aircrafts

    Directory of Open Access Journals (Sweden)

    В. А. Горячев

    2000-09-01

    Full Text Available Described are modem conditions of operation of Russian civil aviation, state of aircraft stock, the main principles of maintaining air worthiness of airplanes and helicopters. Considered is a stage by stage prolongation of the service life of each specimen of aircraft with certification being obligatory

  13. Study on Failure Seriousness Quantitative Analysis Method of Civil Aircraft Flight Test Based on Extenic Theory%基于可拓学的民用飞机外场失效后果定量分析方法研究

    Institute of Scientific and Technical Information of China (English)

    李飞敏; 顾仁碗

    2015-01-01

    Based on failure data of civil aircraft in lfight test, under consideration of lfight test characteristics and failure seriousness grade at present, failure seriousness evaluation index system of civil aircraft in flight test and failure seriousness quantitative analysis method of civil aircraft lfight test based on extenics theory were established. Finally, the methods were validated by lfight test data. The validation results show that the methods were reasonable and viable. The method can solve the problem of failure seriousness quantitative analysis based on lfight test data and offer ways for safety evaluation and validation based on lfight test failure data.%本文立足民用飞机外场失效数据,综合试飞特点以及目前失效后果等级划分特点,建立了民用飞机外场失效后果评价指标体系,引入可拓学方法,建立了民用飞机外场失效后果定量分析方法,并采用外场实例数据进行了方法验证,充分说明了方法的合理性和可行性,解决了目前试飞阶段基于失效数据的失效后果定量分析的难题。本方法的提出为民用飞机外场基于失效数据的安全性评估验证工作提供了方法和思路。

  14. Integrated biodosimetry in large scale radiological events. Opportunities for civil military co-operation; Integrierte Biodosimetrie bei radiologischen Grossschadensereignissen. Moeglichkeiten fuer zivil-militaerische Zusammenarbeit

    Energy Technology Data Exchange (ETDEWEB)

    Port, M.; Eder, S.F.; Lamkowski, A.; Majewski, M.; Abend, M. [Institut fuer Radiobiologie der Bundeswehr, Muenchen (Germany)

    2016-07-01

    Radiological events like large scale radiological or nuclear accidents, terroristic attacks with radionuclide dispersal devices require rapid and precise medical classification (''triage'') and medical management of a large number of patients. Estimates on the absorbed dose and in particular predictions of the radiation induced health effects are mandatory for optimized allocation of limited medical resources and initiation of patient centred treatment. Among the German Armed Forces Medical Services the Bundeswehr Institute of Radiobiology offers a wide range of tools for the purpose of medical management to cope with different scenarios. The forward deployable mobile Medical Task Force has access to state of the art methodologies summarized into approaches such as physical dosimetry (including mobile gammaspectroscopy), clinical ''dosimetry'' (prodromi, H-Modul) and different means of biological dosimetry (e.g. dicentrics, high throughput gene expression techniques, gamma-H2AX). The integration of these different approaches enables trained physicians of the Medical Task Force to assess individual health injuries as well as prognostic evaluation, considering modern treatment options. To enhance the capacity of single institutions, networking has been recognized as an important emergency response strategy. The capabilities of physical, biological and clinical ''dosimetry'' approaches spanning from low up to high radiation exposures will be discussed. Furthermore civil military opportunities for combined efforts will be demonstrated.

  15. Civil Identity

    DEFF Research Database (Denmark)

    Petersen, Lars Axel

    scanning, etc., to discussions of Shari'a law versus common civil law in India; from the study of religious cult in ancient city states to the processes of constitutional reconstruction in former Communist countries; and from attempts at conflict resolution and prevention between Jewish and Arab citizens......In this paper I will go through a catalogue of examples of contexts in which the term civil identity is currently used, ranging from the formal and technical process of linking a set of administrative and other events to an individual biological person by means of identity cards, fingerprints, iris...... of technology and of law. If such a field can be established, the answers to those questions might be relevant to such contemporary issues as inter-ethnic, religious, and -cultural conflict or reconciliation, migration and nationality, civil rights and surveillance, security and privacy, bureaucracy and inter...

  16. Design of Through-flow Nacelle for Low-speed Wind Tunnel Testing of Civil Aircraft%民机低速风洞试验通气发房设计

    Institute of Scientific and Technical Information of China (English)

    胡仞与; 张东云; 施永毅

    2014-01-01

    通气发房是民机风洞试验中模拟发动机效应的一种有效手段。通过调整通气发房出口面积,可以对通过发房的流量进行控制,实现所需模拟的流量系数,保证进气流场的几何相似性。失速特性是民机的一个重要的性能指标,大量的低速风洞试验工作都着眼于着落构型下失速特性的研究;而在失速特性的适航审定试飞时的发动机将处于慢车功率状态,因此以模拟慢车流量系数作为低速风洞试验通气发房的设计目标,有助于在风洞试验中对失速特性进行预测。慢车功率时,由于发动机风扇压比很小,如保留外涵喷口形状,通气发房还能近似模拟风扇的喷流效应。发动机在慢车功率下的流量系数在0.5附近,为实现这一流量系数,在设计通气发房时,需调整内涵出口面积,使发房的总出口面积接近唇口面积的一半。 CFD计算证明这种设计方法得到的通气发房基本能够实现预期的流量系数。%Through-flow nacelle ( TFN) is an effective method of simulating engine effect in wind tunnel Testing. By adjusting the nozzle exit areas of a TFN, the flow passing the TFN could be controlled and the flow ratio ( MFR) could be achieved to make sure the similarity around the inlet flow field. As stall characteristics is one of the impor-tant factor in defining civil aircraft performance, a great portion of the low speed wind tunnel tests is devoted to the study of the stall characteristics of aircraft in landing configuration;and due to the fact that engines tend to be set at an idle condition during airworthy flight tests for stall speed determination, designing a TFN with a MFR corre-sponding to an idle power setting is desirable for the prediction of stall characteristics in wind tunnel testing. When running at idle conditions, an engine will have a very low fan pressure ratio, which means if the fan nozzle geometry is maintained, TFN can

  17. Blade containment evaluation of civil aircraft engines

    Institute of Scientific and Technical Information of China (English)

    Yang Bin

    2013-01-01

    The potential hazard resulting from uncontained turbine engine rotor blade failure has always been the long-term concern of each aero engine manufacturer,and to fully contain the failed blades under critical operating conditions is also one of the most important considerations to meet the rotor integrity requirements.Usually,there are many factors involving the engine containment capability which need to be reviewed during the engine design phases,such as case thickness,rotor support structure,blade weight and shape,etc.However,the premier method to demonstrate the engine containment capability is the fan blade-off test and margin of safety (MS) analysis.Based on a concrete engine model,this paper aims to explain the key points of aero engine containment requirements in FAR Part 33,and introduces the implementation of MS analysis and fan blade-off test in the engine airworthiness certification.Through the introduction,it would be greatly helpful to the industrial community to evaluate the engine containment capability and prepare the final test demonstration in engine certification procedure.

  18. Association between aircraft, road and railway traffic noise and depression in a large case-control study based on secondary data.

    Science.gov (United States)

    Seidler, Andreas; Hegewald, Janice; Seidler, Anna Lene; Schubert, Melanie; Wagner, Mandy; Dröge, Patrik; Haufe, Eva; Schmitt, Jochen; Swart, Enno; Zeeb, Hajo

    2017-01-01

    Few studies have examined the relationship between traffic noise and depression providing inconclusive results. This large case-control study is the first to assess and directly compare depression risks by aircraft, road traffic and railway noise. The study population included individuals aged ≥40 years that were insured by three large statutory health insurance funds and were living in the region of Frankfurt international airport. Address-specific exposure to aircraft, road and railway traffic noise in 2005 was estimated. Based on insurance claims and prescription data, 77,295 cases with a new clinical depression diagnosis between 2006 and 2010 were compared with 578,246 control subjects. For road traffic noise, a linear exposure-risk relationship was found with an odds ratio (OR) of 1.17 (95% CI=1.10-1.25) for 24-h continuous sound levels ≥70dB. For aircraft noise, the risk estimates reached a maximum OR of 1.23 (95% CI=1.19-1.28) at 50-55dB and decreased at higher exposure categories. For railway noise, risk estimates peaked at 60-65dB (OR=1.15, 95% CI=1.08-1.22). The highest OR of 1.42 (95% CI=1.33-1.52) was found for a combined exposure to noise above 50dB from all three sources. This study indicates that traffic noise exposure might lead to depression. As a potential explanation for the decreasing risks at high traffic noise levels, vulnerable people might actively cope with noise (e.g. insulate or move away). Copyright © 2016 Elsevier Inc. All rights reserved.

  19. Civil Disobedience.

    Science.gov (United States)

    Martz, Carlton

    2000-01-01

    This theme issue looks at three historical and recent instances of civil disobedience. The first article examines the Free Speech Movement, which arose on the Berkeley campus of the University of California in the 1960s. The second article recounts the struggle of Mahatma Gandhi to free India from the British Empire. The final article explores the…

  20. History of Civil Engineering Modal Analysis

    DEFF Research Database (Denmark)

    Brincker, Rune

    2008-01-01

    techniques are available for civil engineering modal analysis. The testing of civil structures defers from the traditional modal testing in the sense, that very often it is difficult, or sometimes impossible, to artificially excite a large civil engineering structure. Also, many times, even though...

  1. History of Civil Engineering Modal Analysis

    DEFF Research Database (Denmark)

    Brincker, Rune

    2008-01-01

    techniques are available for civil engineering modal analysis. The testing of civil structures defers from the traditional modal testing in the sense, that very often it is difficult, or sometimes impossible, to artificially excite a large civil engineering structure. Also, many times, even though...

  2. Research on automatic braking control system for large civil aircraft%基于CRM的酒店管理信息系统的分析与设计

    Institute of Scientific and Technical Information of China (English)

    吴晶

    2016-01-01

    In order to improve the efficiency of the hotel industry, to ensure that the hotel in the fierce market competition to be able to profit, and put forward the hotel management information system based on CRM design. This paper expounds the basic principle and characteristics of CRM, analyzes the needs of the hotel management information system, based on the CRM based hotel management information system for the modular design. At last, the flow chart of the system design is given, and the design of the two important modules of the website module and the background management module is given. Theoretical and practical application shows that the hotel management information system based on CRM can improve the efficiency of the hotel more than 20%, and can promote the hotel’s profitability, and achieve the expected research objectives.%为了提高酒店行业的效率,保证酒店在激烈的市场竞争中能够盈利,提出了基于CRM的酒店管理信息系统的设计方案。本文阐述了CRM的基本原理和特点,对酒店管理信息系统的需求进行了分析,在此基础上对基于CRM的酒店管理信息系统进行了模块化的设计。最后给出了系统设计的流程图,并给出了网站模块、后台管理模块两个重要模块的设计。理论和实际应用表明,基于CRM的酒店管理信息系统能提高酒店效率20%以上,并能对酒店的盈利有很大的促进,达到了预期的研究目标。

  3. Adapting existing training standards for unmanned aircraft: finding ways to train staff for unmanned aircraft operations

    CSIR Research Space (South Africa)

    Burger, CR

    2011-09-01

    Full Text Available are governed by the Civil Aviation Authority (CAA) under the terms of an interim policy1. This policy?s paragraph 4.3 describes the process for obtaining a Certificate of Waiver or Authorisation. There is also provision for the issuance of an airworthiness... experience as Designated Flight Examiner for the South African Civil Aviation Authority, and on his three- year project to analyse the strategic development of required technologies to facilitate unmanned aircraft operations in civil airspace. II...

  4. Discussion on the Necessity and Basic Ideas of Strengthening Metrology Administration Laws and Regulations for Civil Aircraft Industry%浅析加强民用飞机工业计量监管法规建设的必要性与基本思路

    Institute of Scientific and Technical Information of China (English)

    张学涛; 周世锋; 邢向楠; 李少壮

    2014-01-01

    Combined with the current development of civil aircraft industry and metrology work features of relevant departments, the paper analyzes the necessity to strengthen metrology administration laws and regulations for civil aircraft industry, and initially proposes principles, bas-ic ideas and main contents of metrology administration laws and regulations. It will provide a reference to prefect the metrology&measurement as-surance system and strengthen the metrology administration of product development for relevant departments.%结合当前我国民用飞机工业发展现状和相关部门计量工作特点,分析了加强民用飞机工业计量监管法规建设的必要性,初步提出了民用飞机工业计量监管法规的制定原则、基本思路和主要内容,为行业主管部门完善民用飞机产品计量测试保证体系和加强产品研制过程的计量监督管理提供了参考。

  5. Study and Sub-System Optimization of Propulsion and Drive Systems for the Large Civil TiltRotor (LCTR2) Rotorcraft

    Science.gov (United States)

    Robuck, Mark; Wilkerson, Joseph; Snyder, Christopher A.; Zhang, Yiyi; Maciolek, Bob

    2013-01-01

    In a series of study tasks conducted as a part of NASA's Fundamental Aeronautics Program, Rotary Wing Project, Boeing and Rolls-Royce explored propulsion, drive, and rotor system options for the NASA Large Civil Tilt Rotor (LCTR2) concept vehicle. The original objective of this study was to identify engine and drive system configurations to reduce rotor tip speed during cruise conditions and quantify the associated benefits. Previous NASA studies concluded that reducing rotor speed (from 650 fps hover tip speed) during cruise would reduce vehicle gross weight and fuel burn. Initially, rotor cruise speed ratios of 54% of the hover tip speed were of most interest during operation at cruise air speed of 310 ktas. Interim results were previously reported1 for cruise tip speed ratios of 100%, 77%, and 54% of the hover tip speed using engine and/or gearbox features to achieve the reduction. Technology levels from commercial off-the-shelf (COTS), through entry-in-service (EIS) dates of 2025 and 2035 were considered to assess the benefits of advanced technology on vehicle gross weight and fuel burn. This technical paper presents the final study results in terms of vehicle sizing and fuel burn as well as Operational and Support (O&S) costs. New vehicle sizing at rotor tip speed reduced to 65% of hover is presented for engine performance with an EIS 2035 fixed geometry variable speed power turbine. LCTR2 is also evaluated for missions range cases of 400, 600, 800, 1000, and 1200 nautical miles and cruise air speeds of 310, 350 and 375 ktas.

  6. Aircraft recognition and tracking device

    Science.gov (United States)

    Filis, Dimitrios P.; Renios, Christos I.

    2011-11-01

    The technology of aircraft recognition and tracking has various applications in all areas of air navigation, be they civil or military, spanning from air traffic control and regulation at civilian airports to anti-aircraft weapon handling and guidance for military purposes.1, 18 The system presented in this thesis is an alternative implementation of identifying and tracking flying objects, which benefits from the optical spectrum by using an optical camera built into a servo motor (pan-tilt unit). More specifically, through the purpose-developed software, when a target (aircraft) enters the field of view of the camera18, it is both detected and identified.5, 22 Then the servo motor, being provided with data on target position and velocity, tracks the aircraft while it is in constant communication with the camera (Fig. 1). All the features are so designed as to operate under real time conditions.

  7. Responsabilidade civil

    OpenAIRE

    Dalanhol, André

    2002-01-01

    Dissertação (mestrado) - Universidade Federal de Santa Catarina, Centro Tecnológico. Programa de Pós-Graduação em Engenharia de Produção. 1. INTRODUÇÃO - aborda o tema Responsabilidade Civil - Reparação do Dano Moral Ambiental, de forma sucinta, justificando sua aplicabilidade no direito brasileiro, discorrendo acerca de cada etapa do trabalho; 2. MEIO AMBIENTE - CONCEITO - proposta de um conceito mais amplo de meio ambiente, que melhor se coadune com a realidade atual, uma vez que os con...

  8. Commercial Aircraft Protection

    Energy Technology Data Exchange (ETDEWEB)

    Ehst, David A. [Argonne National Lab. (ANL), Argonne, IL (United States)

    2016-10-26

    This report summarizes the results of theoretical research performed during 3 years of P371 Project implementation. In results of such research a new scientific conceptual technology of quasi-passive individual infrared protection of heat-generating objects – Spatial Displacement of Thermal Image (SDTI technology) was developed. Theoretical substantiation and description of working processes of civil aircraft individual IR-protection system were conducted. The mathematical models and methodology were presented, there were obtained the analytical dependencies which allow performing theoretical research of the affect of intentionally arranged dynamic field of the artificial thermal interferences with variable contrast onto main parameters of optic-electronic tracking and homing systems.

  9. Analysis and Optimization of Logistics Management Mode of Large-scale Civil Engineering Projects%大型土木工程的物流管理模式优化分析

    Institute of Scientific and Technical Information of China (English)

    秦小玉; 杨乔

    2013-01-01

    In this paper,in accordance with the general characteristics of the logistics operation of large-scale civil engineering projects,we analyzed the material purchasing,warehousing management and distribution of large-scale civil engineering projects and then proposed the optimizing measures to segment the material purchasing management mechanism,improve warehousing operation level,and enhance the material distribution system.%根据大型土木工程的一般物流运作特点,对大型土木工程的物资采购、仓储管理与配送进行了分析研究,提出了细化物资采购管理控制、提升仓储作业水平、优化物资配送体系等优化措施.

  10. How Much Is Enough? Examining Computer Science and Civil Engineering Citation Data to Inform Collection Development and Retention Decisions in Three Large Canadian University Libraries

    Science.gov (United States)

    Spence, Michelle; Mawhinney, Tara; Barsky, Eugene

    2012-01-01

    Science and engineering libraries have an important role to play in preserving the intellectual content in research areas of the departments they serve. This study employs bibliographic data from the Web of Science database to examine how much research material is required to cover 90% of faculty citations in civil engineering and computer…

  11. Aircraft Carriers

    DEFF Research Database (Denmark)

    Nødskov, Kim; Kværnø, Ole

    There are many indications that China is actively researching the design of an aircraft carrier. It is unknown whether China will initiate the actual acquisition of a carrier, but the indications that are available of their research into aircraft carriers and carrier-capable aircraft, as well...... as their purchases of aircraft carrier systems, makes it more than likely that the country is preparing such an acquisition. China has territorial disputes in the South China Sea over the Spratly Islands and is also worried about the security of its sea lines of communications, by which China transports the majority...... of its foreign trade, as well as its oil imports, upon which the country is totally dependent. China therefore has good reasons for acquiring an aircraft carrier to enable it to protect its national interests. An aircraft carrier would also be a prominent symbol of China’s future status as a great power...

  12. Validation of fluxes of an extra large aperture scintillometer at Cabauw using Sky Arrow aircraft flux measurements

    NARCIS (Netherlands)

    Moene, A.F.; Meijninger, W.M.L.; Kohsiek, W.; Gioli, B.; Miglietta, F.; Bosveld, F.C.

    2006-01-01

    An extra-large aperture scintillometer (XLAS) has been operated at the Cabauw tower for several years over a path of 9.8 kilometers, at an average height of 43 meters (Kohsiek et al., 2002). This yields a long term record of the area-averaged sensible heat flux. During the RECAB summer campaign on J

  13. The effect of aircraft emissions on atmospheric ozone in the northern hemisphere

    NARCIS (Netherlands)

    Beck JP; Reeves CE; de Leeuw FAAM; Penkett SA

    1990-01-01

    The effect of aircraft emissions on tropospheric ozone was studied using a 2-D zonal model, of longitude versus altitude. An emission inventory for the 1987 civil aircraft fleet was constructed based on fuel usage and civil aviation statistics. For the area covered by the model (30 - 60 degrees N)

  14. Developing Large-Scale Bayesian Networks by Composition: Fault Diagnosis of Electrical Power Systems in Aircraft and Spacecraft

    Science.gov (United States)

    Mengshoel, Ole Jakob; Poll, Scott; Kurtoglu, Tolga

    2009-01-01

    This CD contains files that support the talk (see CASI ID 20100021404). There are 24 models that relate to the ADAPT system and 1 Excel worksheet. In the paper an investigation into the use of Bayesian networks to construct large-scale diagnostic systems is described. The high-level specifications, Bayesian networks, clique trees, and arithmetic circuits representing 24 different electrical power systems are described in the talk. The data in the CD are the models of the 24 different power systems.

  15. Analysis and Simulation of a Large Amphibian Aircraft Taxiing%大型水陆两栖飞机地面滑跑稳定性分析与仿真

    Institute of Scientific and Technical Information of China (English)

    韩纪军; 许锋; 聂宏

    2012-01-01

    The landing gear system works in concert with the safety of the aircraft's take off and landing directly, therefore it is one of the most important parts and systems of an aircraft. The landing gear design of an amphibian aircraft need to coordinate aerodynamics and liquid dynamics. It is a complicated dynamical problem, and it is the problem which is faced during the process of the large amphibian aircraft design nowadays. Depending on multi - body dynamical theories and the simulating plate of LMS Virtual. Lab, the dynamical model of a large amphibian aircraft taxiing process is proposed. By simulating the model, the a-nalysis of the heading stability during taxiing is conducted. The dynamical analysis and simulation of a large amphibian aircraft's heading taxiing is achieved.%起落装置直接关系到飞行器的起飞与着陆安全,是其重要部件和系统之一.大型水陆两栖飞机的起落架设计需在空气动力学与水动力学领域得到协调,是一个更为复杂的动力学问题,同时也是当前大型飞机研制中亟待解决的问题之一.基于多体动力学理论与LMS Virtual.Lab仿真环境,建立某大型水陆两栖飞机地面滑跑过程的动力学模型,通过对其地面对称滑跑等情况的仿真计算,着重对滑跑过程中的航向稳定性进行分析,实现水陆两栖飞机对称滑跑动力学分析与仿真.

  16. Aircraft Design

    Science.gov (United States)

    Bowers, Albion H. (Inventor); Uden, Edward (Inventor)

    2016-01-01

    The present invention is an aircraft wing design that creates a bell shaped span load, which results in a negative induced drag (induced thrust) on the outer portion of the wing; such a design obviates the need for rudder control of an aircraft.

  17. 盒式机翼布局大型飞机横航向飞行品质研究%Lateral-directional flying qualities research of large aircraft with box-wing configuration

    Institute of Scientific and Technical Information of China (English)

    吕新波; 刘振钦

    2011-01-01

    Compared with a large aircraft with conventional configuration, the aerodynamic characteristics of large aircraft with box-wing configuration were calculated and showed in this paper. The lateral-directional airframe flying qualities of the large aircraft with box-wing configuration were researched. The lateral-directional airframe flying qualities of the large aircraft with box-wing configuration will be deteriorated, so the effective measures which can improve flying qualities of large aircraft with box-wing configuration would be researched. The results show that the large aircraft with box-wing configuration has a larger ratio of lift to drag and special lateral-directional aerodynamic characteristics. Modifying configuration parameters are limited to improve the lateral-directional flying qualities of large aircraft with box-wing configuration and the design of control laws can assure satisfied flying qualities.%经计算并和常规布局大型飞机对比分析,给出了盒式机翼布局大型飞机的气动特点;然后研究了盒式机翼布局大型飞机本体横航向飞行品质;针对盒式机翼布局本体飞机横航向飞行品质较差的问题,研究了提高盒式机翼布局飞机横航向飞行品质的有效方法.研究结果表明:盒式机翼布局大型飞机具有良好的升阻特性和特殊的横航向气动特性;修改布局参数对提高盒式机翼布局飞机横航向飞行品质是有限的,控制律的设计可以保证其具有满意的横航向飞行品质.

  18. Analysis of the latitudinal variability of tropospheric ozone in the Arctic using the large number of aircraft and ozonesonde observations in early summer 2008

    Science.gov (United States)

    Ancellet, Gerard; Daskalakis, Nikos; Raut, Jean Christophe; Tarasick, David; Hair, Jonathan; Quennehen, Boris; Ravetta, François; Schlager, Hans; Weinheimer, Andrew J.; Thompson, Anne M.; Johnson, Bryan; Thomas, Jennie L.; Law, Katharine S.

    2016-10-01

    During the 2008 International Polar Year, the POLARCAT (Polar Study using Aircraft, Remote Sensing, Surface Measurements, and Models of Climate Chemistry, Aerosols, and Transport) campaign, conducted in summer over Greenland and Canada, produced a large number of measurements from three aircraft and seven ozonesonde stations. Here we present an observation-integrated analysis based on three different types of O3 measurements: airborne lidar, airborne UV absorption or chemiluminescence measurement, and intensified electrochemical concentration cell (ECC) ozonesonde profiles. Discussion of the latitudinal and vertical variability of tropospheric ozone north of 55° N during this period is performed with the aid of a regional model (WFR-Chem). The model is able to reproduce the O3 latitudinal and vertical variability but with a negative O3 bias of 6-15 ppbv in the free troposphere above 4 km, especially over Canada. For Canada, large average CO concentrations in the free troposphere above 4 km ( > 130 ppbv) and the weak correlation (ozone at latitudes less than 70° N, due to the fact that local biomass burning (BB) emissions were significant during the 2008 summer period. Conversely, significant STE is found over Greenland according to the better O3 vs. PV correlation ( > 40 %) and the higher values of the 75th PV percentile. It is related to the persistence of cyclonic activity during the summer over Baffin Bay. Using differences between average concentration above Northern and Southern Canada, a weak negative latitudinal summer ozone gradient of -6 to -8 ppbv is found in the mid-troposphere between 4 and 8 km. This is attributed to an efficient O3 photochemical production from BB emissions at latitudes less than 65° N, while the STE contribution is more homogeneous in the latitude range 55-70° N. A positive ozone latitudinal gradient of 12 ppbv is observed in the same altitude range over Greenland not because of an increasing latitudinal influence of STE, but

  19. 75 FR 9327 - Aircraft Noise Certification Documents for International Operations

    Science.gov (United States)

    2010-03-02

    ... as required by the International Civil Aviation Organization (ICAO), and to ensure compliance between domestic U.S. regulations and ICAO Annex 16, Amendment 8. DATES: This amendment becomes effective May 3... United States using aircraft subject to the International Civil Aviation Organization (ICAO) Annex 16...

  20. Posture Alignment and Joining Test System for Large Aircraft Fuselages%大型飞机机身调姿与对接试验系统

    Institute of Scientific and Technical Information of China (English)

    邱宝贵; 蒋君侠; 毕运波; 方强; 王青; 詹建潮; 李江雄; 柯映林

    2011-01-01

    To realize numeralization, automation end flexibility during large aircraft components assembly, a novel posture alignment and joining test system for large aircraft fuselages is developed.Firstly, the working principle of the test system is introduced.Based on test-fuselages' measurement data from the laser tracker, test-fuselages' postures are calculated by integrated management system, and several three coordinate numerical control Iocalizers are driven to move harmoniously by control system, to achieve test-fuselages' posture alignment end joining.Secondly, the kinematics model for the posture alignment system is established.The relevant software, including integrated menagement system, measure system and control system, are developed end integrated on the basis of the hardware platform.Finally, the test system is applied to simulate test-fuselages' posture alignment and joining.Experimental results show that test-fuselages' position alignment precision is better than 0.09 mm, and test-fuselages' posture alignment precision is better than 0.000 5*.Some technologies of the test system have been successfully applied in several national key projects, which cen greatly improve the quality and efficiency of the aircraft assembly.%为实现飞机大部件装配过程的数字化、自动化和柔性化,研制了大型飞机机身调姿与对接试验系统.阐述了该系统的工作原理,通过激光跟踪仪测量试验机身上的检测点,集成管理系统计算试验机身的位姿,控制系统驱动多个三坐标数控定位器协同运动,实现试验机身的调姿与对接.建立了位姿调整机构的运动学模型,针对构建的硬件平台完成了包括集成管理系统、测量系统和控制系统在内的软件开发与集成,并对系统的性能进行了测试.试验结果表明,试验机身的位置调整精度优于0.09 mm,姿态调整精度优于0.000 5°.试验系统涉及的若干关键技术已成功应用于多项国家重点型号工

  1. The longitudinal controls fixed static stability of tailless aircraft

    OpenAIRE

    de Castro, Helena V.

    2000-01-01

    This paper describes the development of a simple theory of the longitudinal controls fixed static stability of tailless aeroplanes. The classical theory, as developed for the conventional aircraft, is modified to accommodate the particular features of the tailless aeroplanes. The theory was then applied to a particular blended-wing-body tailless civil transport aircraft, BWB-98. Cranfield University

  2. 77 FR 14319 - Unmanned Aircraft System Test Sites

    Science.gov (United States)

    2012-03-09

    ... infrastructure and research needs; and (C) Consult with the National Aeronautics and Space Administration and the... Aeronautics and Space Administration (NASA); (4) Address both civil and public unmanned aircraft systems; (5... be flown using a data link to transmit commands to the aircraft. They may perform a variety of...

  3. On the Mechanical and Electrical Design and Installation of Large-scale Civil Air Defense Project%论大型人防工程中的机电设计与安装

    Institute of Scientific and Technical Information of China (English)

    王赞辉

    2016-01-01

    在人防工程机电项目的设计与安装过程当中,所包含的施工项目种类十分繁多。同时伴随着我国整体经济水平的快速发展,城市化进程的不断推进,对于人防工程的建设要求与标准也越来越高。因而就人防工程的机电设计与安装工作也提出了更为严苛的要求标准,本文将基于大型人防工程的施工特点,紧紧围绕着实际工程施工情况来展开相关的机电设计与安装工作。%In the mechanical and electrical design and installation of civil air defense engineering, there are many kings of construction project. With the rapid development of China's overall economic level and the constant advance of the urbanization process, the construction requirements and standards for civil air defense projects are also getting higher and higher. Therefore, the more stringent requirements of the standard of mechanical and electrical design and installation work of civil air defense projects are put forward. Based on the construction characteristics of large civil air defense project, this paper will focus on the actual engineering construction to expand the relevant mechanical and electrical design and installation work.

  4. Aerodynamic Design and Research for Wing-mounted-engine Integration of Civil Aircraft%民用飞机发动机一体化气动设计相关技术初探

    Institute of Scientific and Technical Information of China (English)

    于哲慧

    2015-01-01

    Aerodynamic design of aircraft-engine integration is an important part for wing-mounted-engine air-craft design. In order to solve the design problems between aircraft and engine, many solutions were made attempts from different perspectives during the design process, and classic technology patents and valuable experience were formed. Some of the technology solutions are to be discussed as follows to reveal the map and tendency of related integrated design technology.%飞机发动机一体化气动设计是翼吊布局飞机设计的重要组成部分. 为解决飞机与发动机之间的一体化设计问题,人们在设计过程中从不同角度尝试众多解决方案,形成很多典型技术专利,积累了宝贵经验. 通过分析较为典型的方案,以展现一体化气动设计技术发展的脉络和趋势.

  5. A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft

    NARCIS (Netherlands)

    Damveld, H.J.

    2009-01-01

    The future demand for larger and lighter civil transport aircraft leads to more flexible aircraft, which bring their own controlling and handling problems. A review of established handling qualities methods showed that they were either unsuitable for aeroelastic aircraft, or had significant

  6. Cyber threats within civil aviation

    Science.gov (United States)

    Heitner, Kerri A.

    Existing security policies in civil aviation do not adequately protect against evolving cyber threats. Cybersecurity has been recognized as a top priority among some aviation industry leaders. Heightened concerns regarding cyber threats and vulnerabilities surround components utilized in compliance with the Federal Aviation Administration's (FAA) Next Generation Air Transportation (NextGen) implementation. Automated Dependent Surveillance-B (ADS-B) and Electronic Flight Bags (EFB) have both been exploited through the research of experienced computer security professionals. Civil aviation is essential to international infrastructure and if its critical assets were compromised, it could pose a great risk to public safety and financial infrastructure. The purpose of this research was to raise awareness of aircraft system vulnerabilities in order to provoke change among current national and international cybersecurity policies, procedures and standards. Although the education of cyber threats is increasing in the aviation industry, there is not enough urgency when creating cybersecurity policies. This project intended to answer the following questions: What are the cyber threats to ADS-B of an aircraft in-flight? What are the cyber threats to EFB? What is the aviation industry's response to the issue of cybersecurity and in-flight safety? ADS-B remains unencrypted while the FAA's mandate to implement this system is rapidly approaching. The cyber threat of both portable and non-portable EFB's have received increased publicity, however, airlines are not responding quick enough (if at all) to create policies for the use of these devices. Collectively, the aviation industry is not being proactive enough to protect its aircraft or airport network systems. That is not to say there are not leaders in cybersecurity advancement. These proactive organizations must set the standard for the future to better protect society and it's most reliable form of transportation.

  7. Amphibious Aircraft

    Data.gov (United States)

    National Aeronautics and Space Administration — A brief self composed research article on Amphibious Aircrafts discussing their use, origin and modern day applications along with their advantages and disadvantages...

  8. Aircraft Disinsection

    Science.gov (United States)

    Some countries may require aircraft coming from countries where certain insects or insect-borne diseases are present, such as malaria and Zika virus, to be treated with insecticide. Find out about regulation of pesticides for this treatment.

  9. Some Considerations about the RIERA Approach and Missile-Structure Interaction Analysis Method in Aircraft Impact Assessment on Nuclear Power Plants

    Energy Technology Data Exchange (ETDEWEB)

    Jin, Byeong Moo; Kim, Young Jin [Daewoo E and C Co. Ltd., Suwon (Korea, Republic of); Jeon, Se Jin [Ajou Univ., Suwon (Korea, Republic of)

    2014-05-15

    In this paper, the classically preferred RIERA approach and the so-called missile-structure interaction (MSI) analysis methods which are indebted by the latest computing power are discussed about their inherent discrepancies. Studies on the safety assessments on the nuclear power plants against large civil aircraft crashes are ongoing actively. In this paper, the classically preferred RIERA approach and the so-called missile-structure interaction (MSI) analysis methods are discussed about their inherent discrepancies especially from the point of view energy balances. More advanced and simplified ways in the safety assessment of nuclear power plants against large civil aircrafts may be possible by understanding the inherent discrepancies of the RIERA approach method and the missile-structure interaction method and reducing the differences of structural responses.

  10. Interaction of Aircraft Wakes From Laterally Spaced Aircraft

    Science.gov (United States)

    Proctor, Fred H.

    2009-01-01

    Large Eddy Simulations are used to examine wake interactions from aircraft on closely spaced parallel paths. Two sets of experiments are conducted, with the first set examining wake interactions out of ground effect (OGE) and the second set for in ground effect (IGE). The initial wake field for each aircraft represents a rolled-up wake vortex pair generated by a B-747. Parametric sets include wake interactions from aircraft pairs with lateral separations of 400, 500, 600, and 750 ft. The simulation of a wake from a single aircraft is used as baseline. The study shows that wake vortices from either a pair or a formation of B-747 s that fly with very close lateral spacing, last longer than those from an isolated B-747. For OGE, the inner vortices between the pair of aircraft, ascend, link and quickly dissipate, leaving the outer vortices to decay and descend slowly. For the IGE scenario, the inner vortices ascend and last longer, while the outer vortices decay from ground interaction at a rate similar to that expected from an isolated aircraft. Both OGE and IGE scenarios produce longer-lasting wakes for aircraft with separations less than 600 ft. The results are significant because concepts to increase airport capacity have been proposed that assume either aircraft formations and/or aircraft pairs landing on very closely spaced runways.

  11. NASA technology program for future civil air transports

    Science.gov (United States)

    Wright, H. T.

    1983-01-01

    An assessment is undertaken of the development status of technology, applicable to future civil air transport design, which is currently undergoing conceptual study or testing at NASA facilities. The NASA civil air transport effort emphasizes advanced aerodynamic computational capabilities, fuel-efficient engines, advanced turboprops, composite primary structure materials, advanced aerodynamic concepts in boundary layer laminarization and aircraft configuration, refined control, guidance and flight management systems, and the integration of all these design elements into optimal systems. Attention is given to such novel transport aircraft design concepts as forward swept wings, twin fuselages, sandwich composite structures, and swept blade propfans.

  12. THE AIRPORT DE-ICING OF AIRCRAFTS

    Directory of Open Access Journals (Sweden)

    Robert KONIECZKA

    2015-03-01

    Full Text Available This article provides a summary of the issues involved in de-icing several kinds of aircrafts before flight. The basic risks of an iced aircraft and the factors that can influence its intensity are stated. It discusses the methods for de-icing and protecting against ice formation on small aircrafts, helicopters, and large aircrafts. It also classifies the fluids and other methods used for these de-icing operations, and explains the characteristics and limitations of their use.

  13. Review of High-lift Device Technology Development on Large Aircrafts%大型飞机增升装置技术发展综述

    Institute of Scientific and Technical Information of China (English)

    李丽雅

    2015-01-01

    高效的增升装置是现代大型飞机研制中的关键技术之一。详细介绍了增升装置的原理和现代大型飞机常用的增升装置类型及其支撑与驱动机构。增升装置设计是一个多学科多目标的问题,从气动性能要求、噪声要求和结构重量要求几个方面介绍了增升装置的设计目标。研究了增升装置的发展历程和气动计算与实验方法,最后提出了增升装置的发展趋势和新技术。%Efifcient high-lift device is one of the most important technologies in modern large aircraft research. High-lift theory was introduced in detail, including several types of common high-lift devices as well as their supporting and driving mechanisms. Since high-lift system design involves multidisciplinary and multi-objective issues, this paper introduced several design objectives of high-lift system in terms of aerodynamic performance, noise requirement and structural weight. Also, the development history of high-lift devices was studied, as well as the CFD technology and experiment approach. At last, this paper presented the development tendency of high-lift device and some promising technologies.

  14. Characteristics of civil aviation atmospheric hazards

    Science.gov (United States)

    Marshall, Robert E.; Montoya, J.; Richards, Mark A.; Galliano, J.

    1994-01-01

    Clear air turbulence, wake vortices, dry hail, and volcanic ash are hazards to civil aviation that have not been brought to the forefront of public attention by a catastrophic accident. However, these four hazards are responsible for major and minor injuries, emotional trauma, significant aircraft damage, and in route and terminal area inefficiency. Most injuries occur during clear air turbulence. There is significant aircraft damage for any volcanic ash encounter. Rolls induced by wake vortices occur near the ground. Dry hail often appears as an area of weak echo on the weather radar. This paper will present the meteorological, electromagnetic, and spatiotemporal characteristics of each hazard. A description of a typical aircraft encounter with each hazard will be given. Analyzed microwave and millimeter wave sensor systems to detect each hazard will be presented.

  15. 大型土建工程管理中成本控制增益均衡模型%The Cost Control Gain Equilibrium Model of The Large Civil Engineering Management

    Institute of Scientific and Technical Information of China (English)

    胡晓娟

    2015-01-01

    The increased cost of construction. For this, put forward a large civil engineering management cost control gain equilibrium model, using the data from the civil engineering construction of construction cost estimates, cost control gain balance model is established, through the forecast data and actual cost error gain balance calculation, the process of the project cost control for minimum error value. The simulation experiment indicates that the gain equalization algorithm can effectively improve the efficiency of soil construction cost management, reduce the error of cost management at the same time, with the most effective the most reasonable method, to budget, cost effective for the management of civil engineering to provide better protection.%提出大型土建工程管理中成本控制增益均衡模型,利用土建工程相关施工数据,对施工建设做成本预估,建立成本控制增益均衡模型,通过预估数据与实际成本误差进行增益均衡计算,使工程成本控制得到最小误差值的过程.仿真试验表明,这种增益均衡算法更能有效的提高土建工成本管理的效率,同时降低成本管理的误差,以最有效最合理的方法,对成本进行预算,有效的为土建工程的管理提供更好的保障.

  16. Design of a Parallel Robot with a Large Workspace for the Functional Evaluation of Aircraft Dynamics beyond the Nominal Flight Envelope

    Directory of Open Access Journals (Sweden)

    Umar Asif

    2012-08-01

    Full Text Available This paper summarizes the development of a robotic system for the analysis of aircraft dynamics within and beyond the nominal flight envelope. The paper proposes the development of a parallel robot and its motion cueing algorithm to attain a reasonable workspace with adequate motion capabilities to facilitate the testing of aircraft stall and fault manoeuvrability scenarios. The proposed design combines two parallel mechanisms and aims to provide six degrees of freedom motion with a much larger motion envelope than the conventional hexapods in order to realize the manoeuvrability matching of aircraft dynamics near and beyond the upset flight envelopes. Finally the paper draws a comparative evaluation of motion capabilities between the proposed motion platform and a conventional hexapod based on Stewart configuration in order to emphasize the significance of the design proposed herein.

  17. Det civile samfund

    DEFF Research Database (Denmark)

    Henriksen, Lars Skov

    2014-01-01

    Kapitlet giver en oversigt over de vigtigste teoretiske forståelser af begrebet om det civile samfund. Desuden giver kapitlet en empirisk oversigt over foreninger og organisationer i det danske civilsamfund samt befolkningens civile engagement.......Kapitlet giver en oversigt over de vigtigste teoretiske forståelser af begrebet om det civile samfund. Desuden giver kapitlet en empirisk oversigt over foreninger og organisationer i det danske civilsamfund samt befolkningens civile engagement....

  18. A Knowledge-based and Extensible Aircraft Conceptual Design Environment

    Institute of Scientific and Technical Information of China (English)

    FENG Haocheng; LUO Mingqiang; LIU Hu; WU Zhe

    2011-01-01

    Design knowledge and experience are the bases to carry out aircraft conceptual design tasks due to the high complexity and integration of the tasks during this phase.When carrying out the same task,different designers may need individual strategies to fulfill their own demands.A knowledge-based and extensible method in building aircraft conceptual design systems is studied considering the above requirements.Based on the theory,a knowledge-based aircraft conceptual design environment,called knowledge-based and extensible aircraft conceptual design environment (KEACDE) with open architecture,is built as to enable designers to wrap add-on extensions and make their own aircraft conceptual design systems.The architecture,characteristics and other design and development aspects of KEACDE are discussed.A civil airplane conceptual design system (CACDS) is achieved using KEACDE.Finally,a civil airplane design case is presented to demonstrate the usability and effectiveness of this environment.

  19. Citizenship in civil society?

    NARCIS (Netherlands)

    Ossewaarde, Marinus R.R.

    2007-01-01

    This article seeks to provide a conceptual framework to complement and guide the empirical analysis of civil society. The core argument is that civil society must be understood, not as a category of (post)industrialized society, but as one of individualized society. Civil society is characterized by

  20. Application Prospect Analysis of Environmental Protection Composites on Large Passenger Aircraft%环保复合材料在大型客机上的应用前景分析

    Institute of Scientific and Technical Information of China (English)

    张婷

    2013-01-01

    At present, composites widely used in large aircraft are mainly thermosetting resin matrix composites, while the problems of high cost of manufac-ture and dififculty of material recycle restrict its extensive application in aircraft. Today, people pay more and more attention on low cost manufacturing and environmental protection. “Green material” thermoplastic composites could be used as promising alternative materials in large aircraft structure parts owing to its excellent comprehen-sive properties and low cost advantage. In this paper, the possible application of thermoplastic composites in large aircraft are be analyzed from the manufacturing cost, mate-rials performance, materials processing, material recycling and reuse.%目前,在大型客机上广泛应用的复合材料主要是热固性树脂基复合材料,但由于高制造成本及材料难回收等问题,一定程度上制约其在飞机上的应用扩展。在强调低成本制造和环保的今天,“绿色材料”热塑性树脂基复合材料由于其优良的综合性能和低成本优势,可以作为一种有前途的替代材料使用在大型客机结构件上。本文将从热塑性复合材料制件的综合制造成本、性能、工艺以及材料的回收和再利用等方面分析热塑性复合材料在大型客机上的应用前景。

  1. Aircraft cybernetics

    Science.gov (United States)

    1977-01-01

    The use of computers for aircraft control, flight simulation, and inertial navigation is explored. The man-machine relation problem in aviation is addressed. Simple and self-adapting autopilots are described and the assets and liabilities of digital navigation techniques are assessed.

  2. Application of Digital Master Tooling in Large Aircraft Front Fuselage Structure Section Prototype%数字标工在大客前机身结构部段样件试制中的应用

    Institute of Scientific and Technical Information of China (English)

    刘春锋; 郑堂介; 廖建华; 汪建东

    2013-01-01

    The idea of digital master tooling, with character and usage of physical master tooling, in air-craft manufacture for assembly coordination is presented. By means of applying it in the fabrication of large aircraft front fuselage structure section prototype, selection and application of digital master tooling are described at length based on MBD environment.%提出了在飞机制造中采用具有实物标工特征及用法的数字标工进行装配协调的方法,并在大客前机身结构部段样件的制造中进行了应用研究,阐述了在三维MBD数模环境下,进行数字标工项目选取及应用的具体工艺方法。

  3. GRAPHICAL MODELS OF THE AIRCRAFT MAINTENANCE PROCESS

    Directory of Open Access Journals (Sweden)

    Stanislav Vladimirovich Daletskiy

    2017-01-01

    Full Text Available The aircraft maintenance is realized by a rapid sequence of maintenance organizational and technical states, its re- search and analysis are carried out by statistical methods. The maintenance process concludes aircraft technical states con- nected with the objective patterns of technical qualities changes of the aircraft as a maintenance object and organizational states which determine the subjective organization and planning process of aircraft using. The objective maintenance pro- cess is realized in Maintenance and Repair System which does not include maintenance organization and planning and is a set of related elements: aircraft, Maintenance and Repair measures, executors and documentation that sets rules of their interaction for maintaining of the aircraft reliability and readiness for flight. The aircraft organizational and technical states are considered, their characteristics and heuristic estimates of connection in knots and arcs of graphs and of aircraft organi- zational states during regular maintenance and at technical state failure are given. It is shown that in real conditions of air- craft maintenance, planned aircraft technical state control and maintenance control through it, is only defined by Mainte- nance and Repair conditions at a given Maintenance and Repair type and form structures, and correspondingly by setting principles of Maintenance and Repair work types to the execution, due to maintenance, by aircraft and all its units mainte- nance and reconstruction strategies. The realization of planned Maintenance and Repair process determines the one of the constant maintenance component. The proposed graphical models allow to reveal quantitative correlations between graph knots to improve maintenance processes by statistical research methods, what reduces manning, timetable and expenses for providing safe civil aviation aircraft maintenance.

  4. Analysis of Flight Test Technique on Ground Minimum Control Speed for Civil Aircraft%民机地面最小操纵速度试飞分析及技术

    Institute of Scientific and Technical Information of China (English)

    范祝斌

    2013-01-01

    According to the CCAR-25-R4 “Airworthiness Standards of Transport Category Airplanes” and FAA advisory AC25-7C“Flight Test Guide”, drawing on the flight test experiences of other planes, this paper analyses the flight test principle and impact factors of ground minimum control speed ( VMCG ) in theory, and discusses the flight test technique and the risk alleviated method of VMCG . It can provide guidance for the VMCG flight test of the civil airplane.%按照CCAR-25-R4《运输类飞机适航标准》要求,结合FAA咨询通告AC25-7 C《运输类飞机试飞指南》,总结其它机型的试飞经验,通过理论分析民机地面最小操纵速度( VMCG )试飞原理及影响因素,探讨了民机VMCG试飞的试飞方法及风险规避方法,可为民机的VMCG试飞提供参考。

  5. Global civil aviation black carbon emissions.

    Science.gov (United States)

    Stettler, Marc E J; Boies, Adam M; Petzold, Andreas; Barrett, Steven R H

    2013-09-17

    Aircraft black carbon (BC) emissions contribute to climate forcing, but few estimates of BC emitted by aircraft at cruise exist. For the majority of aircraft engines the only BC-related measurement available is smoke number (SN)-a filter based optical method designed to measure near-ground plume visibility, not mass. While the first order approximation (FOA3) technique has been developed to estimate BC mass emissions normalized by fuel burn [EI(BC)] from SN, it is shown that it underestimates EI(BC) by >90% in 35% of directly measured cases (R(2) = -0.10). As there are no plans to measure BC emissions from all existing certified engines-which will be in service for several decades-it is necessary to estimate EI(BC) for existing aircraft on the ground and at cruise. An alternative method, called FOX, that is independent of the SN is developed to estimate BC emissions. Estimates of EI(BC) at ground level are significantly improved (R(2) = 0.68), whereas estimates at cruise are within 30% of measurements. Implementing this approach for global civil aviation estimated aircraft BC emissions are revised upward by a factor of ~3. Direct radiative forcing (RF) due to aviation BC emissions is estimated to be ~9.5 mW/m(2), equivalent to ~1/3 of the current RF due to aviation CO2 emissions.

  6. Analysis of Joint Plane Between Outer Wing Box and Center Wing Box for Civil Aircraft%民用飞机外翼中央翼对接面位置的研究

    Institute of Scientific and Technical Information of China (English)

    汤平

    2014-01-01

    机翼对接设计是飞机结构设计的一个重要环节,而机翼对接面位置的选择对对接结构的设计有重要影响。基于客机外翼与中央翼的对接面,分析各种对接面位置对对接结构设计的影响,比较其中的优缺点;分析了修形面和其相对于机身等直段的变形量;并提出一种新型对接面位置,为民用飞机外翼中央翼对接的对接面设计提供一种选择。%Wing root joint is essential in aircraft structure design, and the joint rib design is greatly influenced by joint plane position. Based on the joint plane between wing and center wing, the joint rib design affected by differ-ent joint plane positions is analyzed and compared their advantages and disadvantages. The fuselage deformation from modified contour is analyzed. One new joint plane position is raised and the option of joint plane design be-tween wing and center wing is obtained.

  7. Chemistry in plumes of high-flying aircraft with H2 combustion engines: a modelling study

    Directory of Open Access Journals (Sweden)

    G. Weibring

    Full Text Available Recent discussions on high-speed civil transport (HSCT systems have renewed the interest in the chemistry of supersonic-aircraft plumes. The engines of these aircraft emit large concentrations of radicals like O, H, OH, and NO. In order to study the effect of these species on the composition of the atmosphere, the detailed chemistry of an expanding and cooling plume is examined for different expansion models.

    For a representative flight at 26 km the computed trace gas concentrations do not differ significantly for different models of the expansion behaviour. However, it is shown that the distributions predicted by all these models differ significantly from those adopted in conventional meso-scale and global models in which the plume chemistry is not treated in detail. This applies in particular to the reservoir species HONO and H2O2.

  8. Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft. [conducted in a Langley 8 foot transonic pressure tunnel

    Science.gov (United States)

    Larson, T. J.; Flechner, S. G.; Siemers, P. M., III

    1980-01-01

    The results of a wind tunnel investigation on an all flush orifice air data system for use on a KC-135A aircraft are presented. The investigation was performed to determine the applicability of fixed all flush orifice air data systems that use only aircraft surfaces for orifices on the nose of the model (in a configuration similar to that of the shuttle entry air data system) provided the measurements required for the determination of stagnation pressure, angle of attack, and angle of sideslip. For the measurement of static pressure, additional flush orifices in positions on the sides of the fuselage corresponding to those in a standard pitot-static system were required. An acceptable but less accurate system, consisting of orifices only on the nose of the model, is defined and discussed.

  9. Photochemical transformation of aircraft exhausts at their transition from the plume to the large scale dispersion in the Northern temperature belt

    Energy Technology Data Exchange (ETDEWEB)

    Karol, I.L.; Kiselev, A.A. [Main Geophysical Observatory, St.Petersburg (Russian Federation)

    1997-12-31

    The 2-D diurnally varying photochemical model of the Northern temperate zonal tropospheric belt with fixed (off line) temperature and air transport is used for the description of the formation of aircraft exhaust concentration distribution in the North Atlantic commercial flight corridor, based on actual flights in summer and winter. A strong diurnal and seasonal variation of emitted NO{sub x} oxidation rate is revealed and evaluated. (author) 11 refs.

  10. Which Air Force Civil Engineer Capabilities Can Complement USNORTHCOM’s Role in Defense Support to Civil Authorities (DSCA)?

    Science.gov (United States)

    2014-05-21

    fixed wing or rotary wing aircraft, airfield/landing zone under Visual Flight Rules (VFR) and Instrument Flight Rules ( IFR ) conditions for multiple...wing aircraft, airfield/landing zone under Visual Flight Rules (VFR) and Instrument Flight Rules ( IFR ) conditions for multiple aircraft types on small...under Visual Flight Rules (VFR) and Instrument Flight Rules ( IFR ) conditions for multiple aircraft types on small to large temporary/ permanent

  11. Civil Society and Governance

    DEFF Research Database (Denmark)

    Hulgård, Lars

    An illustration of how important the relationship is between civil society anbd governance. A short historic journey with four snapshots of times and situations that have provided interesting evidence about the connection between civil society and governance. My goal for the short historic journey...... is to make clear and hopefully even verify that providing knowledge about the impact of civil society and citizens’ participation on governance is one of the most urgent research tasks in the current period of time....

  12. Civil Society and Governance

    DEFF Research Database (Denmark)

    Hulgård, Lars

    An illustration of how important the relationship is between civil society anbd governance. A short historic journey with four snapshots of times and situations that have provided interesting evidence about the connection between civil society and governance. My goal for the short historic journey...... is to make clear and hopefully even verify that providing knowledge about the impact of civil society and citizens’ participation on governance is one of the most urgent research tasks in the current period of time....

  13. Legalisation of Civil Wars

    DEFF Research Database (Denmark)

    Buhl, Kenneth Øhlenschlæger

    2009-01-01

    -international armed conflict' is used here. Civil wars are usually limited to the territory of a state. Considering that international law is generally concerned with the legal relations between states – being a legal system based on the system of states with states as its subjects – the main question is how civil......This article is concerned with the legal challenges of regulating civil wars in international humanitarian law. Civil war is not a term used in international law; it falls however, withing the context of the legal term 'armed conflicts not of an international character', although the shorter 'non...... wars as internal conflicts have become subject to international humanitarian law....

  14. Reconceptualizing Civil Regulation

    DEFF Research Database (Denmark)

    Galang, Roberto Martin; Castello, Itziar

    2011-01-01

    This article re-conceptualizes the notion of civil regulation, through an analysis of 775 projects by firms located in 21 Asian countries, wherein we map the state of civil regulation initiatives in the region. We challenge two established assumptions in the Corporate Social Responsibility...... literature. First, contrary to what is commonly argued, we claim that strong states in Asia promote civil regulation in what we call the “paradox of the weak state”. Second, we not only argue that civil regulation is mainly enforced by multinational enterprises willing to promote international social...

  15. Climate Change and International Civil Aviation Negotiations

    Directory of Open Access Journals (Sweden)

    Veronica Korber Gonçalves

    Full Text Available Abstract The International Civil Aviation Organization (ICAO has discussed ways of regulating greenhouse gas (GHG emissions by civil aircraft for almost 20 years. Over the past four years, a consensus has developed about a market-based mechanism in the form of a carbon offset system. This article describes the route to the agreement reached by ICAO’s 39th Assembly, in order to contextualise the results and point out some of its limitations. It points to two main factors that contributed to the consensus: the role of the European Union, which sought to lead the negotiations, and the choice of a flexible and ultimately weak mechanism that received support from the international airlines.

  16. AASPT Carbon/Carbon Aircraft Brake Disk Granted MPA

    Institute of Scientific and Technical Information of China (English)

    2009-01-01

    @@ Xi'an Chaoma Technology Co. Ltd. was issued Parts Manufacturer Approval (PMA) for Carbon/Carbon aircraft brake disk for Airbus 320 series by Civil Aviation Administration of China (CAAC). The company is held by Academy of Aerospace Solid Propulsion Technology (AASPT), a subsidiary of China Aerospace Science and Technology Corporation (CASC). It is the first approval given to a Chinese company to design and produce brakes for main civilian aircraft.

  17. Modern trends of aircraft fly-by-wire systems

    Directory of Open Access Journals (Sweden)

    С. С. Юцкевич

    2013-07-01

    Full Text Available Specifics of civil aviation modern transport aircraft fly-by-wire control systems are described. A comparison of the systems-level hardware and software, expressed through modes of guidance, provision of aircraft Airbus A-320, Boeing B-777, Tupolev Tu-214, Sukhoi Superjet SSJ-100 are carried out. The possibility of transition from mechanical control wiring to control through fly-by-wire system in the backup channel is shown.

  18. Civil Procedure In Denmark

    DEFF Research Database (Denmark)

    Werlauff, Erik

    The book contains an up-to-date survey of Danish civil procedure after the profound Danish procedural reforms in 2007. It deals with questions concerning competence and function of Danish courts, commencement and preparation of civil cases, questions of evidence and burden of proof, international...

  19. Apps for Ancient Civilizations

    Science.gov (United States)

    Thompson, Stephanie

    2011-01-01

    This project incorporates technology and a historical emphasis on science drawn from ancient civilizations to promote a greater understanding of conceptual science. In the Apps for Ancient Civilizations project, students investigate an ancient culture to discover how people might have used science and math smartphone apps to make their lives…

  20. Refractions of Civil Society

    DEFF Research Database (Denmark)

    Kuzmanovic, Daniella

    The thesis investigates various perceptions of civil society among civic activists in Turkey, and how these perceptions are produced and shaped. The thesis is an anthropological contribution to studies of civil society in general, as well as to studies on political culture in Turkey....

  1. Large Aircraft Component Transport Based on Omni-Directional Mobile and Multi-Point Supporting%基于全向移动与多点柔性支撑的飞机大部件运输技术

    Institute of Scientific and Technical Information of China (English)

    姚定; 佘晶; 黄翔; 徐燕

    2012-01-01

    为实现飞机大部件车间叛运输机动灵活,基于全向移动技术,提出了一种飞机大部件全向移动运输平台,以满足大尺寸空间、重载条件的运输作业要求;为改变当首企业一车一用、专车专用现象,基于秉性的思想,提出了一种多点柔性支撑系统.结合某型飞机机翼大部件特点,实际研制了一辆全向移动柔性运输架车样车,在此基础上开发了相应控制与离线鳊程系统.研究结果表明:架丰可以实现较高精度的全向移动,具有较大的灵活性,能够满足飞机部件柔性运输要求.%To flexibly transport the large aircraft components in workshops, one type of omni-directional transporting platform of large aircraft component based on omni-directional technology is presented to meet the transportation requirements of large size and heavy load. To change the present condition that one car for a single use, as well as one car for a special use, a novel type of multi-point flexible supporting tool system based on the flexible supporting tool is proposed. Considering the characteristics of one certain type of aircraft wing components, an omni-directional transporting platform prototype is manufactured. And then the corresponding control and programming system is developed. Research result shows that higher accuracy and greater flexibility of transporting can be achieved by using omni-directional technology, and the requirements of aircraft component flexible transporting can be perfectly met.

  2. EUROPEIZAREA DREPTULUI PROCESUAL CIVIL

    Directory of Open Access Journals (Sweden)

    Alexandrina Zaharia

    2006-05-01

    Full Text Available The European Union increases the judiciary cooperation in civil and comercial cases with trans-border incidence, based on the principle of mutual recognition of judiciary rulings. The aim of adopting frame-legislation is to ensure the developement of civil procedures. The Council Regulations no. 44/2001 on the competence, the recognition and the enforcement of judiciary rulings in civil and commercial cases is a “real” Code of civil procedure in this matter, to be applied in the member states, thus ensuring the free circulation of the judiciary rulings according to the principles of mutual recognition, mutual trust and reinforcement of juridical security in the union. The community civil procedural code prevails over the national procedural code. The Regulations ensure the administration of the community justice and through their rules avoid the pronunciation, in the member states, of rulings that are irreconcilable with each other, the direct beneficiaries being legal and natural persons.

  3. 大飞机项目风险管理规划决策系统设计与实现%Design and Development of Large Aircraft Project Risk Management Planning Decision-making System

    Institute of Scientific and Technical Information of China (English)

    李炜宇

    2012-01-01

    风险管理是各个工程项目必须的环节之一.本文首先对现有的风险管理体系进行介绍和分析,进而完成适用于大飞机项目的风险管理规划中三大核心要素——甘特图、概率影响矩阵和角色权限控制的设计,最后完成了大飞机项目风险管理规划决策系统的实现,为项目风险识别和分析提供了良好的数据接口.%Risk management is an essential part of each project. In this paper, the existing risk management systems are introduced and analyzed, and then the three core elements-gantt chart, probability-impact matrix and role access control-of risk management plan for large aircraft project are designed. Finally the large aircraft project risk management planning decision-making system is successfully developed, providing good interfaces for risk management identification and analysis.

  4. Environmental Impact Evaluation of Aircraft at System-of-Systems Level

    NARCIS (Netherlands)

    Schroijen, M.J.T.; Van Tooren, M.J.L.; Voskuijl, M.; Curran, R.

    2011-01-01

    Next generations of civil transport aircraft will need to be evaluated not only against their behaviour as an aircraft system but also as a part of the larger air transport system. In addition to this are the sustainability issues related to for instance noise and emissions, represented by environme

  5. New principles of periodic aircraft maintenance conditions definition in accordance with aviation safety criteria

    Directory of Open Access Journals (Sweden)

    S. V. Daletskiy

    2015-01-01

    Full Text Available Based on the reliability theory schemes of justifying the volume and structural principles of periodic maintenance (repair of civil aircraft depending on operational conditions meeting the requirements on the failure-free operation, aircraft durability and flight safety are considered.

  6. Climates, Landscapes, and Civilizations

    Science.gov (United States)

    Schultz, Colin

    2013-10-01

    Humans are now the dominant driver of global climate change. From ocean acidification to sea level rise, changes in precipitation patterns, and rising temperatures, global warming is presenting us with an uncertain future. However, this is not the first time human civilizations have faced a changing world. In the AGU monograph Climates, Landscapes, and Civilizations, editors Liviu Giosan, Dorian Q. Fuller, Kathleen Nicoll, Rowan K. Flad, and Peter C. Clift explore how some ancient peoples weathered the shifting storms while some faded away. In this interview, Eos speaks with Liviu Giosan about the decay of civilizations, ancient adaptation, and the surprisingly long history of humanity's effect on the Earth.

  7. Civil War and Inoperativity

    DEFF Research Database (Denmark)

    Flohr, Mikkel

    2017-01-01

    This article analyses the penultimate publication in Giorgio Agambens Homo Sacer-series Stasis: Civil War as a Political Paradigm. It compares and contrasts the paradigm of civil war with the preceding paradigm of the exception, and identifies a significant displacement in the relationship between...... of inoperativity towards a concept of destituent power drawing on his other writings. It makes the argument for thinking civil war and inoperativity – stasis and stasis – together to derive a concept of destituent power as a form of revolution against the sovereign state, which does not constitute a new sovereign...

  8. Producing Civil Society

    DEFF Research Database (Denmark)

    Feldt, Liv Egholm; Hein Jessen, Mathias

    Since the beginning of the 1990’s, civil society has attracted both scholarly and political interest as the ‘third sphere’ outside the state and the market not only a normatively privileged site of communication and ‘the public sphere’, but also as a resource for democratization processes...... of the century. 2, the laws and strategies of implementing regarding the regulation of civil societal institutions (folkeoplysningsloven) since the 1970’s this paper shows how civil society in 20th century Denmark was produced both conceptually and practically and how this entailed a specific vision and version...

  9. Engine jet entrainment in the near field of an aircraft

    Energy Technology Data Exchange (ETDEWEB)

    Garnier, F.; Jacquin, L.; Laverdant, A. [Office National d`Etudes et de Recherches Aerospatiales (ONERA), 92 - Chatillon (France)

    1997-12-31

    A simplified approach has been applied to analyse the mixing and entrainment processes of the engine exhaust through their interaction with the vortex wake of an aircraft. These investigations are focused on the near filed, extending from exit nozzle to the beginning of the vortex phase (i.e. to about twenty seconds after the wake is generated). This study is performed using an integral model and a numerical simulation for a two-engine large civil aircraft. The properties of the wing-tip vortices on the calculation of the dilution ratio (defined as a tracer concentration) have been shown. The mixing process is also affected by the buoyancy effect, but only after the jet regime, when the trapping in the vortex core has occurred. Qualitative comparison with contrail photography shows similar features. Finally the distortion and stretching of the plume streamlines inside the vortices can be observed, and the role of the descent of the vortices on the maximum tracer concentration has been discussed. (author) 19 refs.

  10. Aircraft Electric Secondary Power

    Science.gov (United States)

    1983-01-01

    Technologies resulted to aircraft power systems and aircraft in which all secondary power is supplied electrically are discussed. A high-voltage dc power generating system for fighter aircraft, permanent magnet motors and generators for aircraft, lightweight transformers, and the installation of electric generators on turbine engines are among the topics discussed.

  11. Evaluation of the doses to aircrew members by considering the aircraft structures

    Science.gov (United States)

    Battistoni, G.; Ferrari, A.; Pelliccioni, M.; Villari, R.

    A mathematical model of an aircraft has been developed with the aim to investigate the influence of the aircraft structures and contents on the exposure of aircrew and passengers to the galactic component of cosmic rays. The irradiation of the mathematical model in the cosmic ray environment has been simulated using the Monte Carlo transport code FLUKA. Effective dose and ambient dose equivalent rates have been determined inside the aircraft at several locations along the fuselage at typical civil aviation altitudes.

  12. The Celestial Basis of Civilization

    Science.gov (United States)

    Masse, W. B.

    Scholars have long puzzled over the reasons for the ubiquity of celestial images in the residue of the world's earliest civilizations: in art, myth, religious cosmology, iconography, cosmogony, eschatological beliefs, and as portents for the conduct of royal and chiefly power. The general consensus is that these images represented a need by early societies to use the fixed celestial heavens in order to regulate ritual and agricultural cycles, and to satisfy a psychological need by people to relate themselves to their surrounding Universe. Such explanations are facile and miss an important aspect of the celestial heavens. The fixed celestial heavens served as the back-drop for a large number of often spectacular temporary naked-eye visible celestial events which animated the night and sometimes the daytime sky, and which created an 'otherworld' for virtually all cultural groups. In this paper I present a model derived from the detailed analysis of Hawaiian oral traditions and culture history in relation to historic astronomical records of temporary celestial events, and then apply this model to cultural traditions from Mesoamerica and other geographic regions in order to demonstrate that novae, supernovae, variable stars, comets, great meteor showers, aurorae, solar and lunar eclipses, and impacting Solar System debris, together played a critical role in the artistic, intellectual, and political development of early civilizations. These data not only provide important insights into the development of civilization, but also provide important details and longitudinal records of astronomical events and phenomena which are otherwise not readily available for scientific scrutiny.

  13. Civil Surgeon Info

    Data.gov (United States)

    Department of Homeland Security — USCIS designates certain doctors (also known as civil surgeons) to perform the medical exam required for most Green Card applicants. This data set represents the...

  14. Civil & Criminal Penalties

    Data.gov (United States)

    US Consumer Product Safety Commission — When CPSC is involved in a civil or criminal investigations into violations of the Consumer Products Safety Act the Commission publishes final determinations and...

  15. Transnationalising Civil Society?

    DEFF Research Database (Denmark)

    Jørgensen, Martin Bak

    The paper takes a transnational perspective on developing an analytical framework for understanding how transnationalism interacts with civil society and how immigrant organisations use transnational strategies to challenge the pre-given positions of immigrants within given integration- and citiz......The paper takes a transnational perspective on developing an analytical framework for understanding how transnationalism interacts with civil society and how immigrant organisations use transnational strategies to challenge the pre-given positions of immigrants within given integration...

  16. Development of a validated aircraft child restraint model

    NARCIS (Netherlands)

    Pipino, M.; Mugnai, A.; DeWeese, R.L.

    1999-01-01

    Studies conducted at the FAA Civil Aeromedical Institute have shown that when used in aircraft, automotive Child Restraint Devices (CRDs) do not always provide the level of safety desired. Various factors that contribute to poor performance, such as seat belt anchor location, cushion stiffness, and

  17. Aircraft maintenance. Citations from the International Aerospace Abstracts data base

    Science.gov (United States)

    Zollars, G. F.

    1980-01-01

    These citations from the international literature concern various aspects of aircraft maintenance. Both military and civil aviation experience are included. Articles cited concern airline operations, engine and avionics reliability, the use of automatic test equipment, maintenance scheduling, and reliability engineering. This updated bibliography contains 347 citations, 85 of which are new additions to the previous edition.

  18. Aircraft Natural/Artificial Icing

    Science.gov (United States)

    2009-02-12

    axial vibration is caused by an oscillator driving a coil in the probe to create a magnetostrictive force. A sensing coil within the probe senses the...Consequence TOP 7-3-537 12 February 2009 C-1 APPENDIX C. ICING TEST SITE SELECTION 1. INTRODUCTION Unlike large fixed-wing aircraft, helicopters

  19. Human Response to Aircraft Noise

    NARCIS (Netherlands)

    Kroesen, M.

    2011-01-01

    How can it be that one person is extremely annoyed by the sounds of aircrafts, while his neighbour claims not to be bothered at all? The present thesis attempts to explain this observation by applying a range of quantitative methods to field data gathered among residents living near large airports.

  20. Civil helicopter flight research. [for CH-53 helicopter

    Science.gov (United States)

    Snyder, W. J.; Schoultz, M. B.

    1976-01-01

    The paper presents a description of the NASA CH-53 Civil Helicopter Research Aircraft and discusses preliminary results of the aircraft flight research performed to evaluate factors and requirements for future helicopter transport operations. The CH-53 equipped with a 16-seat airline-type cabin and instrumented for flight research studies in noise, vibration, handling qualities, passenger acceptance, fuel utilization, terminal area maneuvers, and gust response. Predicted fuel usage for typical short-haul missions is compared with actual fuel use. Pilot ratings for an IFR handling quality task for three levels of stability augmentation are presented, and the effects of internal noise, vibration, and motion on passenger acceptance are discussed. Future planned CH-53 flight research within the Civil Helicopter Technology Program is discussed.

  1. Research on Emerging and Descending Aircraft Noise

    Directory of Open Access Journals (Sweden)

    Monika Bartkevičiūtė

    2013-12-01

    Full Text Available Along with an increase in the aircraft engine power and growth in air traffic, noise level at airports and their surrounding environs significantly increases. Aircraft noise is high level noise spreading within large radius and intensively irritating the human body. Air transport is one of the main sources of noise having a particularly strong negative impact on the environment. The article deals with activities and noises taking place in the largest nationwide Vilnius International Airport.The level of noise and its dispersion was evaluated conducting research on the noise generated by emerging and descending aircrafts in National Vilnius Airport. Investigation was carried out at 2 measuring points located in a residential area. There are different types of aircrafts causing different sound levels. It has been estimated the largest exceedances that occur when an aircraft is approaching. In this case, the noisiest types of aircrafts are B733, B738 and AT72. The sound level varies from 70 to 85 dBA. The quietest aircrafts are RJ1H and F70. When taking off, the equivalent of the maximum sound level value of these aircrafts does not exceed the authorized limits. The paper describes the causes of noise in aircrafts, the sources of origin and the impact of noise on humans and the environment.Article in Lithuanian

  2. INTEGRATING UNMANNED AIRCRAFT VEHICLES IN THE ROMANIAN NATIONAL AIRSPACE

    Directory of Open Access Journals (Sweden)

    Sorana Alina Catinca POP

    2015-07-01

    Full Text Available The use of unmanned aerial vehicles in the Romanian civil airspace brings us back to the 1920's, when the first aircraft started to fly over the Romanian sky. Little did the legislators at that time know how to create the proper legal framework for the use of such machines so that all aspects related to their use be covered, as well as identify all potential risks and effects. Nowadays, UAVs are the new aircraft and it is a challenge for the legislators to properly identify the legal framework so that the safety and security of civil aviation are not affected. The paper will address the challenges the regulator faces in the integration of the UAVs in the Romanian civil airspace, developments and issues raised by the current regulation, as well as aspects related to the national regulations expected to enter into force at the end of 2015, beginning of 2016.

  3. NASA/DOD Aerospace Knowledge Diffusion Research Project. Paper 62: The Influence of Knowledge Diffusion on Aeronautics Innovation: The Research, Development, and Production of Large Commercial Aircraft in France, Germany, and the United Kingdom

    Science.gov (United States)

    Golich, Vicki L.; Pinelli, Thomas E.

    1997-01-01

    This paper focuses on how European public policies-individually and collectively - influence the diffusion of knowledge and technology. It begins with an overview of the roles played historically and currently by European governments in the Research, Development and Production (RD&P) of Large Commercial Aircraft (LCA). The analytical framework brings together literature from global political economy, comparative politics, business management, and science and technology policy studies. It distinguishes between the production of knowledge, on the one hand, and the dissemination of knowledge, on the other. France, Germany, and the United Kingdom serve as the analytical cases. The paper concludes with a call for additional research in this area, some tentative lessons learned, and a discussion of the consequences of national strategies and policies for the diffusion of knowledge and technology in an era of globalizaton.

  4. The Analysis of Bailing Hydraulic Control System for a Large Extinguishing Aircraft%某灭火型飞机汲水液压控制系统分析

    Institute of Scientific and Technical Information of China (English)

    胡刚; 裴沛

    2015-01-01

    该文是对某大型灭火飞机汲水液压控制系统的设计进行分析,通过对汲水斗收放时间、收放同步性及外载荷等的计算分析,验证了汲水液压控制系统设计的可行性。%This article is designed to analyze bailing hydraulic control system for a large fire-fighting aircraft, by the time of the bailing buck-et retractable, retractable synchronization and external load calculation and analysis to verify bailing hydraulic control system Feasibility of design.

  5. Census of U.S. Civil Aircraft: Calendar Year 1989

    Science.gov (United States)

    1989-01-01

    0 1 1 FLUG & FAHRZEUGWERKE DIAMANT 16.5 ............................................ 1 10 0 0 5 5 FFA HBV -DIAMANT 16.5...1 10 0 0 17 17 HBV DIAMANT 18 ...................................... 1 10 0 0 5 5 HBV DIAMANT...NETHER ND... 81 - - - 1 NORWAY 21 - - -I PAIIAMA . - - PHILIPPINE ..... - 2 SAIDAN. .... , I - - I SAUDIARAB-. 4 - SINGAPO-... 7 - 5-- -- STCHIlSH

  6. Census of U.S. Civil Aircraft. Calendar Year 1982.

    Science.gov (United States)

    1982-12-31

    41 1 0 1 1 EOS/O01 1 41 1 0 2 2 ESP WILD GOOSE 2 41 1 0 1 1 ESPERANZA 4 2 41 1 0 3 3 EVANS 2 41 1 0 1 1 EVANS V.P 1 41 1 0 1 1 EVANS VOLKSPLANE 1 41 1...Gilpin 2 2 Grand 19 2 14 3 Gunnison 54 7 31 6 3 2 1 1 1 1 Hinsdale 2 2 Huerfano 6 4 2 Jackson 3 1 2 Jefferson 304 61 166 18 12 1 1 9 9 27 Kiowa 12 6 6...3 1 2 * h~ll oS 35 11 299 11 59 6 1 1 Prowers 6e 15 41 1 5 1 2 1 Pueolo 69 17 38 2 1 1 3 1 5 Rio Blanco 48 13 31 1 1 Rio Grande 59 20 20 5 2 12

  7. Census U.S. Civil Aircraft Calendar Year 1991

    Science.gov (United States)

    1991-12-31

    190 190 15 175 - - Flamenco Airways ............................ 3 -3 - Flight Trails dba Air Resorts Airlines...1 - Flamenco Airways ...................... 10 - - - 10 1 91 - Flying Boat Inc, dba Chalks Int’l. Airlines .. ............ ..... 4 .- 4 - 4

  8. Census of U.S. Civil Aircraft: Calendar Year 1987

    Science.gov (United States)

    1987-12-31

    34 --- 34 --- - - -- -- --- Fairways 2 2 --- 2 --- . . . . ...- Fischer Aviation 9 --- --- 9 --- 9 ... ... ... ... ... Flamenco Air .ys...Fischer Brothers Aviation dba Midway Commuter 9 --- ..- --- 9 --- 9 ... ... ... ... ... Flamenco Airways 5 --- 5 --- 1 4 Flight Lines dba

  9. 76 FR 30231 - Civil Supersonic Aircraft Panel Discussion

    Science.gov (United States)

    2011-05-24

    ... for attendees. The purpose of the meeting is to raise public awareness of the continuing technological... joint meeting of the 159th Acoustical Society of America and NOISE-CON 2010 in Baltimore, Maryland 21202. The purpose of these meetings is to raise public awareness on advances in supersonic technology,...

  10. Census of U.S. Civil Aircraft, Calendar Year 1986.

    Science.gov (United States)

    1986-12-31

    AUSTIN BARBARA JEAN 2 41 10 1 1 F/W S-ENG REC. ENG 41 0 1 1 TOTAL 0 1 1 AVIONS FAIREY TIPSY NIPPER T-66 I 41 0 2 2 F/W S-ENG REC. ENG 41 0 2 2...34 - "SP-" , K(OLB LLTRA-5-A; 4. KOL.E u_7P-’S4 KIORNS CAPER 2 " .4. KOSAN 039 1 4’ 0 , KOSTOOM-3 2 4 1 0 1 - KR I 2 4’ 0 O 1 1 KR P-51i 1 4’ 1 O 1 1 KR I

  11. 75 FR 8427 - Civil Supersonic Aircraft Panel Discussion

    Science.gov (United States)

    2010-02-24

    ... America and NOISE-CON 2010 and it will be held at the Baltimore Marriott Waterfront Hotel, Grand Ballroom... Society of America and ] NOISE-CON 2010. It will be held at the Baltimore Marriott Waterfront Hotel, Grand... Space Administration (NASA), and industry to get feedback from interested persons. Public involvement...

  12. FLIGHTS BY FOREIGN CIVIL AIRCRAFT TO SOUTH AFRICA

    Directory of Open Access Journals (Sweden)

    Jan Ploeger

    2012-02-01

    Full Text Available Legislation enabling effect to be given to the International Convention for regulating air navigation, and to make provision for the control, guidance and encouragement of flying within the Union of South Africa and for other purposes incidental thereto, for all purposes known as the Union Aviation Act [No. 16 of 1923], was passed on the 23rd of May 1923 to allow effect to be given to the International Air Navigation Convention of 1919, and to make the provisions referred to above.

  13. Census U.S. Civil Aircraft: Calendar Year 1990

    Science.gov (United States)

    1990-12-31

    1 1 EL BUTEO .......................................................... 2 41 1 0 1 1 EL CAMINO 70-1 ............................................... 1...1 BosQue 26 11 10 3 - - - - - - - - - - - - 2 Bowie.... 134 51 43 14 13 - - 9 - - - - - - 4 - - Brazona 260 114 90 22 6 - 2 3 - - - 3 - - 10

  14. Census of U.S. Civil Aircraft: Calendar Year 1988

    Science.gov (United States)

    1988-01-01

    1 0 1 1 EIPPER-COREY MX II 1 41 1 0 1 1 EIPPER/CURTISS MXL-2 2 41 1 0 1 1 EIPPERMX2QUICKSILVER 2 41 1 0 1 1 EL BUTED 2 41 1 0 1 1 EL CAMINO 70-1 1 41...Bee 43 21 16 2 1 1 1 1 Bell 143 58 58 6 7 2 3 1 4 2 2 Bexar 870 285 384 69 35 1 16 1 1 15 4 1 24 7 27 Blanco 24 16 5 2 1 Borden 1 1 Bosque 31 13 I5 3

  15. Census of U.S. Civil Aircraft, Calendar Year 1985.

    Science.gov (United States)

    1985-12-31

    2 4110 EL BUTEC 2 41 1 0 1 1 EL CAMINO 70-1 1 41 1 0 1 1 EL GRINGO 1 41 1 0 1 1 ELG 0 1 41 1 0 1 1 ELLIS PITTS 1 41 1 0 1 1 EM-60 2 41 I 0 1 I...62 7 15 9 4 3 2 2 3 3 Bexar 1065 299 46 92 59 38 9 2 s 8 5 27 12 36Blanco 22 11 10 1 ’I orden 2 1 ,1 • Bosque 40 15 21 2 1 1 . Bowie 126 40 50 13 15 4

  16. Census of U.S. Civil Aircraft, Calendar Year 1980.

    Science.gov (United States)

    1980-12-31

    FRANKLIN I 150 I 1 BREEZY RLU 1 1 41 CONT MOTOR 1 100 1 1 TURNER T-40 1 41 FRANKLIN 1 90 1 1 FW-180 4 41 UNKNOWN 1 0 1 1 EL CAMINO 70-1 1 41 VOLKSWAGEN 1...50 21 1 1 16 3 24 4 21 Blanco 11 6 2 3 Borden I 1 Bosque 31 12 19 Bowie 11 46 48 9 12 2 1 Brazoria 307 123 101 21 6 1 4 5 44 2 Brazos 104 41 46 7 3 4 3

  17. Census U.S. Civil Aircraft Calendar Year 1993

    Science.gov (United States)

    1993-12-31

    EIPPERMX20UICKSILVEFR 2 41 0EL CAMINO 70 1 0 1 1 EL GRINGO 1 41 1 0 1 1 ELG D 1 41 1 0 1 1 ELLIS PiTIS 41 1 0 1 1EMERALD 1 41 1 0 1 1 EMERAUDE 2 41 1 0...2 - - - - - - - - - - - - 2 Borden 1 - - - - - - - - - - - - - - - Bosque 28 11 13 2 - - - 1 - - - - - - - - I B5oa. 114 42 39 10 - - - 4 - - - - 1

  18. Civil Aircraft Side-Facing Seat Research Summary

    Science.gov (United States)

    2012-11-01

    9). Lumbar: The lumbar spine is at risk for a compression fracture during impacts with a significant vertical compo- nent. Providing protection to...was arranged through the FAA Center of Excellence for Airworthiness Assurance, with the prime contractor being TNO Science & Industry of the...Crashworthiness Program RPD Manager, served as the Contracting Officer’s Technical Representative for the project. He also arranged the follow-on study

  19. 大型民用航空制造企业技术管理体系构建方法研究%Research on the Building Method of Technical Management System for Large Civil Aviation Manufacturing Enterprises

    Institute of Scientific and Technical Information of China (English)

    王长法; 赵雄; 陈冰; 吴恒

    2013-01-01

    In order to build technical management system for large civil aviation manufacturing enterprises,it proposes the construction process and method based on normal basic element of technical management system.This model includes the resource,organization,process and system view model.It analyzes the interaction relationship among the decision-making coordination layer,the executive management layer and assessment monitoring layer,designs the indexes and weights for the technical management system,illustrates the radar map,shows the roles of sustainable development for enterprise technology management innovation mechanism.%为摸索出适合大型航空制造业的技术管理体系,基于一般的技术管理体系基本要素,首先构建了面向大型民用航空制造企业的技术管理体系模型,该模型包含资源、组织、流程和制度视图模型;然后按决策协调层、执行层和评估监督层分析了技术管理体系模型中各个层次的相互作用关系,并为该技术管理体系模型设计了指标和权重,进行了雷达图分析,指出企业技术管理的持续性发展为企业技术管理提供了创新机制与体制.

  20. [Fernand Braudel and the geo-history of civilizations].

    Science.gov (United States)

    Ribeiro, Guilherme

    2011-03-01

    The article discusses the valuable role of geography in the study of civilizations entitled Grammaire des civilisations (A history of civilizations), by French historian Fernand Braudel. It also focuses on the epistemological role of the concept of geo-history in Braudel's thought. The article's underlying assumption is that geography has been crucial to comprehending history over large spans of time.

  1. The socialization potential of the Eastern Partnership Civil Society Forum

    Directory of Open Access Journals (Sweden)

    Hrant KOSTANYAN

    2013-12-01

    Full Text Available This article assesses socialization in the Eastern Partnership Civil Society Forum, an institutionalized civil society cooperation consisting of nongovernmental organizations from the European Union and the Eastern Partnership countries: Belarus, Ukraine, Moldova, Georgia, Armenia, and Azerbaijan. The article argues that uniting the literature on socialization and on Eastern Partnership Civil Society Forum adds considerably to scholarly knowledge about the role of the institutionalized civil society in the world. The analysis of the activities of the Civil Society Forum shows that the conditions for socialization are largely fulfilled. We conclude that the organisation and functioning of the Eastern Partnership Civil Society Forum not only provides a passive framework for transmitting European values and norms, but also results in a middle degree of socialization between civil society organizations of the European Union and the Eastern Partnership countries. There is a large degree of internalization of European Union-sponsored norms and values among the participants of the Civil Society Forum: they fervently promote and defend such norms and values. The little-politicized environment in which discussions take place also allows civil society organisations to make ambitious statements, often more straightforward than political representatives (can make.

  2. Propulsion controlled aircraft computer

    Science.gov (United States)

    Cogan, Bruce R. (Inventor)

    2010-01-01

    A low-cost, easily retrofit Propulsion Controlled Aircraft (PCA) system for use on a wide range of commercial and military aircraft consists of an propulsion controlled aircraft computer that reads in aircraft data including aircraft state, pilot commands and other related data, calculates aircraft throttle position for a given maneuver commanded by the pilot, and then displays both current and calculated throttle position on a cockpit display to show the pilot where to move throttles to achieve the commanded maneuver, or is automatically sent digitally to command the engines directly.

  3. Aircraft Wake Vortex Deformation in Turbulent Atmosphere

    OpenAIRE

    Hennemann, Ingo; Holzaepfel, Frank

    2007-01-01

    Large-scale distortion of aircraft wake vortices appears to play a crucial role for aircraft safety during approach and landing. Vortex distortion is investigated based on large eddy simulations of wake vortex evolution in a turbulent atmosphere. A vortex identification method is developed that can be adapted to the vortex scales of interest. Based on the identified vortex center tracks, a statistics of vortex curvature radii is established. This statistics constitutes the basis for understan...

  4. Future aircraft networks and schedules

    Science.gov (United States)

    Shu, Yan

    2011-07-01

    Because of the importance of air transportation scheduling, the emergence of small aircraft and the vision of future fuel-efficient aircraft, this thesis has focused on the study of aircraft scheduling and network design involving multiple types of aircraft and flight services. It develops models and solution algorithms for the schedule design problem and analyzes the computational results. First, based on the current development of small aircraft and on-demand flight services, this thesis expands a business model for integrating on-demand flight services with the traditional scheduled flight services. This thesis proposes a three-step approach to the design of aircraft schedules and networks from scratch under the model. In the first step, both a frequency assignment model for scheduled flights that incorporates a passenger path choice model and a frequency assignment model for on-demand flights that incorporates a passenger mode choice model are created. In the second step, a rough fleet assignment model that determines a set of flight legs, each of which is assigned an aircraft type and a rough departure time is constructed. In the third step, a timetable model that determines an exact departure time for each flight leg is developed. Based on the models proposed in the three steps, this thesis creates schedule design instances that involve almost all the major airports and markets in the United States. The instances of the frequency assignment model created in this thesis are large-scale non-convex mixed-integer programming problems, and this dissertation develops an overall network structure and proposes iterative algorithms for solving these instances. The instances of both the rough fleet assignment model and the timetable model created in this thesis are large-scale mixed-integer programming problems, and this dissertation develops subproblem schemes for solving these instances. Based on these solution algorithms, this dissertation also presents

  5. The 1995 scientific assessment of the atmospheric effects of stratospheric aircraft

    Science.gov (United States)

    Stolarski, Richard S.; Baughcum, Steven L.; Brune, William H.; Douglass, Anne R.; Fahey, David W.; Friedl, Randall R.; Liu, Shaw C.; Plumb, R. Alan; Poole, Lamont R.; Wesoky, Howard L.

    1995-01-01

    This report provides a scientific assessment of our knowledge concerning the impact of proposed high-speed civil transport (HSCT) aircraft on the atmosphere. It comes at the end of Phase 1 of the Atmospheric Effects of Stratospheric Aircraft element of the NASA High-Speed Research Program. The fundamental problem with stratospheric flight is that pollutant residence times are long because the stratosphere is a region of permanent temperature inversion with stable stratification. Using improved two-dimensional assessment models and detailed fleet emissions scenarios, the assessment examines the possible impact of the range of effluents from aircraft. Emphasis is placed on the effects of NO(x) and H2O on the atmospheric ozone content. Measurements in the plume of an in-flight Concorde supersonic transport indicated a large number of small particles. These measurements, coupled with model sensitivity studies, point out the importance of obtaining a more detailed understanding of the fate of sulfur in the HSCT exhaust. Uncertainties in the current understanding of the processes important for determining the overall effects of HSCT's on the atmosphere are discussed and partially quantified. Research directions are identified to improve the quantification of uncertainties and to reduce their magnitude.

  6. AIRCRAFT MAINTENANCE HANGAR

    National Research Council Canada - National Science Library

    GEAMBASU Gabriel George

    2017-01-01

    .... The first part of research describes the aircraft maintenance process that has to be done after an updated maintenance manual according with aircraft type, followed by a short introduction about maintenance hangar...

  7. Flux Sampling Errors for Aircraft and Towers

    Science.gov (United States)

    Mahrt, Larry

    1998-01-01

    Various errors and influences leading to differences between tower- and aircraft-measured fluxes are surveyed. This survey is motivated by reports in the literature that aircraft fluxes are sometimes smaller than tower-measured fluxes. Both tower and aircraft flux errors are larger with surface heterogeneity due to several independent effects. Surface heterogeneity may cause tower flux errors to increase with decreasing wind speed. Techniques to assess flux sampling error are reviewed. Such error estimates suffer various degrees of inapplicability in real geophysical time series due to nonstationarity of tower time series (or inhomogeneity of aircraft data). A new measure for nonstationarity is developed that eliminates assumptions on the form of the nonstationarity inherent in previous methods. When this nonstationarity measure becomes large, the surface energy imbalance increases sharply. Finally, strategies for obtaining adequate flux sampling using repeated aircraft passes and grid patterns are outlined.

  8. Optimal Vibration Control of Civil Engineering Structures

    DEFF Research Database (Denmark)

    Thesbjerg, Leo

    In designing large civil engineering structures, an important consideration is prospective dynamic loadings which may include earthquake ground motion, wind gusts, severe sea states and moving vehicles, rotating and reciprocating machinery and others. successful design of such structures requires...... providing for the safety and integrity of the structure, and in some cases also providing for a measure of comfort for the occupants during such loading which the structure and its occupants must endure. Due to these uncertainties, the civil engineering community has traditionally adopted a very...

  9. Aircraft type influence on contrail properties

    Directory of Open Access Journals (Sweden)

    P. Jeßberger

    2013-05-01

    Full Text Available The investigation of the impact of aircraft parameters on contrail properties helps to better understand the climate impact from aviation. Yet, in observations, it is a challenge to separate aircraft and meteorological influences on contrail formation. During the CONCERT campaign in November 2008, contrails from 3 Airbus passenger aircraft of type A319-111, A340-311 and A380-841 were probed at cruise under similar meteorological conditions with in-situ instruments on board the DLR research aircraft Falcon. Within the 2 min old contrails detected near ice saturation, we find similar effective diameters Deff (5.2–5.9 μm, but differences in particle number densities nice (162–235 cm−3 and in vertical contrail extensions (120–290 m, resulting in large differences in contrail optical depths τ (0.25–0.94. Hence larger aircraft produce optically thicker contrails. Based on the observations, we apply the EULAG-LCM model with explicit ice microphysics and in addition the Contrail and Cirrus Prediction model CoCiP to calculate the aircraft type impact on young contrails under identical meteorological conditions. The observed increase in τ for heavier aircraft is confirmed by the models, yet for generally smaller τ. An aircraft dependence of climate relevant contrail properties persists during contrail lifetime, adding importance to aircraft dependent model initialization. We finally derive an analytical relationship between contrail, aircraft and meteorological parameters. Near ice saturation, contrail width × τ scales linearly with fuel flow rate as confirmed by observations. For higher saturation ratios approximations from theory suggest a non-linear increase in the form (RHI–12/3. Summarized our combined results could help to more accurately assess the climate impact from aviation using an aircraft dependent contrail parameterization.

  10. Unmanned aircraft systems

    Science.gov (United States)

    Unmanned platforms have become increasingly more common in recent years for acquiring remotely sensed data. These aircraft are referred to as Unmanned Airborne Vehicles (UAV), Remotely Piloted Aircraft (RPA), Remotely Piloted Vehicles (RPV), or Unmanned Aircraft Systems (UAS), the official term used...

  11. Creative Ventures: Ancient Civilizations.

    Science.gov (United States)

    Stark, Rebecca

    The open-ended activities in this book are designed to extend the imagination and creativity of students and encourage students to examine their feelings and values about historic eras. Civilizations addressed include ancient Egypt, Greece, Rome, Mayan, Stonehenge, and Mesopotamia. The activities focus upon the cognitive and affective pupil…

  12. History and Undergraduate Civilization.

    Science.gov (United States)

    Conroy, Peter

    1995-01-01

    It is argued that a traditional, historically-oriented course in 17th- and 18th-century French civilization continues to be an appropriate and effective approach for undergraduate French study, in preparation for later, more sophisticated cultural analysis. Four course components are discussed: class lectures; literary text selection; textbook…

  13. Re-thinking civil disobedience

    Directory of Open Access Journals (Sweden)

    Theresa Züger

    2013-11-01

    Full Text Available This article points out a struggle of today’s societies with the traditional concepts of civil disobedience and stresses the need for reevaluation of the concept of civil disobedience for policy making and public discourse. Starting with a minimal definition of civil disobedience, the article introduces Hannah Arendt’s approach for a legitimisation of civil disobedience and discusses her ideas for digital actions, which are increasingly framed as digital forms of civil disobedience. Addressing WikiLeaks as an example of digital civil disobedience, the author problematises the internal secrecy of WikiLeaks and the focus on Julian Assange as a single decision-maker. Both aspects challenge Arendt’s understanding of legitimate civil disobedience. Even though traditional criteria of civil disobedience need to be revisited in the digital age, organisations or disobedience actors might themselves in their actions be well-advised to comply with the principles they fight for.

  14. Civil partnerships five years on.

    Science.gov (United States)

    Ross, Helen; Gask, Karen; Berrington, Ann

    2011-01-01

    The Civil Partnership Act 2004, which came into force in December 2005 allowing same-sex couples in the UK to register their relationship for the first time, celebrated its fifth anniversary in December 2010. This article examines civil partnership in England and Wales, five years on from its introduction. The characteristics of those forming civil partnerships between 2005 and 2010 including age, sex and previous marital/civil partnership status are examined. These are then compared with the characteristics of those marrying over the same period. Further comparisons are also made between civil partnership dissolutions and divorce. The article presents estimates of the number of people currently in civil partnerships and children of civil partners. Finally the article examines attitudes towards same-sex and civil partner couples both in the UK and in other countries across Europe.

  15. The Limitation of Western Civilization And the Revival of Oriental Civilization

    Institute of Scientific and Technical Information of China (English)

    Su; Hao

    2014-01-01

    <正>In the distribution of modem world civilizations,the Oriental civilization and Western civilization are the two major civilization systems.Western civilization is often represented by the Christian civilization in Europe and North America on both sides across the North Atlantic.Oriental civilization appears more diversified,among which the Chinese civilization,India civilization and Islamic civilization are the most influential

  16. Exploring Civilizations with 'Seven Wolves'

    Institute of Scientific and Technical Information of China (English)

    Yang Jie

    2007-01-01

    @@ Beijing - A farewell party for the CCTV (China Central Television) crew 'Road to Civilizations-Global Exploration Tour of World Major Civilizations' - the world's first TV series documenting the journey of exploring the 12 civilizations in the human world, was sponsored by Fujian Septwolves Industry Co., Ltd and held at the Beijing Landmark hotel on 16 January.

  17. Civility in Classes and Sports

    Science.gov (United States)

    Lumpkin, Angela

    2010-01-01

    Civility is a polite or courteous act, expression, or standard of conduct, including the display of respect and tolerance to everyone. Teaching and modeling civility in classes and with sport teams is essential so students and athletes can learn the importance of and demonstrate civility in their interactions with others. Teachers and coaches…

  18. Research on Ecological Civilization Evaluation Index System

    Institute of Scientific and Technical Information of China (English)

    2009-01-01

    Ecological civilization, which refers to the harmonious development of man and the nature, has the connotation of the ecological material civilization, ecological consciousness civilization, ecological institutional civilization and ecological behavior civilization. The research on ecological civilization evaluation index system is important in that it can provide the guidance for the construction of ecological civilization, and besides it can improve public recognition of the importance of ecological civil...

  19. Aircraft Attitude Control by Fuzzy Control

    Science.gov (United States)

    Kato, Akio; Matsuba, Takashi

    The fuzzy control law to improve dutch roll characteristics of aircraft was designed and its control performance was evaluated. First, the control law was designed for a small-high speed aircraft at low altitude and low-speed flight conditions. The control law was then applied to flight conditions from minimum speed to supersonic speed and from sea level to high altitude. The control performance for these conditions was evaluated. Furthermore, this control law was adapted to a large transport aircraft with no parameter changes. The evaluation showed good control performance to improve the dutch roll characteristics under all flight conditions for both small high-speed aircraft and large transport aircraft without the parameter changes. This means that the fuzzy control proved to provide effective flexible application to aircraft stability augmentation. If an aircraft in actual flight is in strong air turbulence, inputs to the fuzzy controller may exceed the limit of its effective range. To cope with this problem, the countermeasures were introduced, their methods tested, and their effectiveness proved.

  20. Civil Society and Democratic Governance in Ghana: Emerging ...

    African Journals Online (AJOL)

    Contemporary Journal of African Studies ... Open Access DOWNLOAD FULL TEXT Subscription or Fee Access ... The use of the term civil society among Ghanaian scholars has been aligned largely with Tocqueville's ... OTHER RESOURCES.

  1. Intercomparison of aerosol single-scattering albedo derived from AERONET surface radiometers and LARGE in situ aircraft profiles during the 2011 DRAGON-MD and DISCOVER-AQ experiments

    Science.gov (United States)

    Schafer, J. S.; Eck, T. F.; Holben, B. N.; Thornhill, K. L.; Anderson, B. E.; Sinyuk, A.; Giles, D. M.; Winstead, E. L.; Ziemba, L. D.; Beyersdorf, A. J.; Kenny, P. R.; Smirnov, A.; Slutsker, I.

    2014-06-01

    Single-scattering albedo (SSA) retrievals obtained with CIMEL Sun-sky radiometers from the Aerosol Robotic Network (AERONET) aerosol monitoring network were used to make comparisons with simultaneous in situ sampling from aircraft profiles carried out by the NASA Langley Aerosol Group Experiment (LARGE) team in the summer of 2011 during the coincident DRAGON-MD (Distributed Regional Aerosol Gridded Observational Network-Maryland) and DISCOVER-AQ (Deriving Information on Surface conditions from Column and Vertically Resolved Observations Relevant to Air Quality) experiments. The single-scattering albedos (interpolated to 550 nm) derived from AERONET measurements for aerosol optical depth (AOD) at 440 nm ≥ 0.4 (mean SSA: 0.979) were on average 0.011 lower than the values derived from the LARGE profile measurements (mean SSA: 0.99). The maximum difference observed was 0.023 with all the observed differences within the combined uncertainty for the stated SSA accuracy (0.03 for AERONET; 0.02 for LARGE). Single-scattering albedo averages were also analyzed for lower aerosol loading conditions (AOD ≥ 0.2) and a dependence on aerosol optical depth was noted with significantly lower single-scattering albedos observed for lower AOD in both AERONET and LARGE data sets. Various explanations for the SSA trend were explored based on other retrieval products including volume median radius and imaginary refractive index as well as column water vapor measurements. Additionally, these SSA trends with AOD were evaluated for one of the DRAGON-MD study sites, Goddard Space Flight Center, and two other Mid-Atlantic AERONET sites over the long-term record dating to 1999.

  2. Intercomparison of aerosol optical and micro-physical properties derived from AERONET surface radiometers and LARGE in-situ aircraft profiles during the 2011 DRAGON-MD and DISCOVER-AQ experiments

    Science.gov (United States)

    Schafer, J.; Eck, T. F.; Thornhill, K. L.; Holben, B. N.; Anderson, B. E.; Sinyuk, A.; Ziemba, L. D.; Giles, D. M.; Winstead, E.; Beyersdorf, A. J.; Kenny, P.; Smirnov, A.; Slutsker, I.

    2013-12-01

    Measurements of aerosol single scattering albedo (SSA) obtained with CIMEL sun-sky radiometers from the AERONET aerosol monitoring network were used to make comparisons with simultaneous in-situ sampling from aircraft profiles carried out by the NASA Langley Aerosol Group Experiment (LARGE) team in the summer of 2011 during the coincident DRAGON-MD (Distributed Regional Aerosol Gridded Observational Network-Maryland) and DISCOVER-AQ air quality experiments. The single scattering albedos (interpolated to 550nm) derived from AERONET measurements for aerosol optical depth (AOD) at 440nm greater than 0.4 (mean SSA: 0.979) were on average 0.011 lower than the values derived from the LARGE profile measurements (mean SSA: 0.99) with a maximum difference observed of 0.023 with all the observed differences within the expected uncertainty for the stated accuracy of the SSA measurements (0.03 for AERONET; 0.02 for LARGE). Single scattering albedo averages were also analyzed for lower aerosol loading conditions (AOD > 0.2) and a trend of decreasing SSA as AOD decreased was found in both AERONET and LARGE datasets. Various explanations for the decreasing SSA trend were explored based on other retrieval products including volume median radius and imaginary refractive index as well as column water vapor measurements. Additionally, these SSA trends with AOD were evaluated for one of the DRAGON-MD study sites, Goddard Space Flight Center, and two other Mid-Atlantic AERONET sites over the long-term record dating to 1999.

  3. Design, analysis, and control of a large transport aircraft utilizing selective engine thrust as a backup system for the primary flight control. Ph.D. Thesis

    Science.gov (United States)

    Gerren, Donna S.

    1995-01-01

    A study has been conducted to determine the capability to control a very large transport airplane with engine thrust. This study consisted of the design of an 800-passenger airplane with a range of 5000 nautical miles design and evaluation of a flight control system, and design and piloted simulation evaluation of a thrust-only backup flight control system. Location of the four wing-mounted engines was varied to optimize the propulsive control capability, and the time constant of the engine response was studied. The goal was to provide level 1 flying qualities. The engine location and engine time constant did not have a large effect on the control capability. The airplane design did meet level 1 flying qualities based on frequencies, damping ratios, and time constants in the longitudinal and lateral-directional modes. Project pilots consistently rated the flying qualities as either level 1 or level 2 based on Cooper-Harper ratings. However, because of the limited control forces and moments, the airplane design fell short of meeting the time required to achieve a 30 deg bank and the time required to respond a control input.

  4. RISK ASSESSMENT PROCEDURE FOR CIVIL AIRPORT

    Directory of Open Access Journals (Sweden)

    Natalia Distefano

    2014-03-01

    Full Text Available A practical problem in air transport is how to manage risk and safety. In recent years have been developed special technical and managerial skills to the systematic, forward looking identification and control of hazards throughout the life cycle of a project, program, or activity. Safety Management System (SMS involves identifying, evaluating, and addressing of hazards or risk. Its sole purpose is to prevent accidents. Safety risk assessment is defined as the systematic identification and evaluation of the risk posed by the complete spectrum of possible accident scenarios. Risk assessment is a tool that supports decision making and as such supports risk management. Risk management comprises the safety optimization of the system, the verification process and risk acceptance, which support airport operations. This paper proposed a quantitative methodology for the risk assessment for a civil airport, which is based on historical data of aircraft accidents, contained in the Aviation Safety Network database, from 1 January 1980 to 31 December 2010.

  5. Optimum Climb to Cruise Noise Trajectories for the High Speed Civil Transport

    Science.gov (United States)

    Berton, Jeffrey J.

    2003-01-01

    By entraining large quantities of ambient air into advanced ejector nozzles, the jet noise of the proposed High Speed Civil Transport (HSCT) is expected to be reduced to levels acceptable for airport-vicinity noise certification. Away from the airport, however, this entrained air is shut off and the engines are powered up from their cutback levels to provide better thrust for the climb to cruise altitude. Unsuppressed jet noise levels propagating to the ground far from the airport are expected to be high. Complicating this problem is the HSCT's relative noise level with respect to the subsonic commercial fleet of 2010, which is expected to be much quieter than it is today after the retirement of older, louder, domestic stage II aircraft by the year 2000. In this study, the classic energy state approximation theory is extended to calculate trajectories that minimize the climb to cruise noise of the HSCT. The optimizer dynamically chooses the optimal altitude velocity trajectory, the engine power setting, and whether the ejector should be stowed or deployed with respect to practical aircraft climb constraints and noise limits.

  6. Escorting commercial aircraft to reduce the MANPAD threat

    Science.gov (United States)

    Hock, Nicholas; Richardson, M. A.; Butters, B.; Walmsley, R.; Ayling, R.; Taylor, B.

    2005-11-01

    This paper studies the Man-Portable Air Defence System (MANPADS) threat against large commercial aircraft using flight profile analysis, engagement modelling and simulation. Non-countermeasure equipped commercial aircraft are at risk during approach and departure due to the large areas around airports that would need to be secured to prevent the use of highly portable and concealable MANPADs. A software model (CounterSim) has been developed and was used to simulate an SA-7b and large commercial aircraft engagement. The results of this simulation have found that the threat was lessened when a escort fighter aircraft is flown in the 'Centreline Low' position, or 25 m rearward from the large aircraft and 15 m lower, similar to the Air-to-Air refuelling position. In the model a large aircraft on approach had a 50% chance of being hit or having a near miss (within 20m) whereas escorted by a countermeasure equipped F-16 in the 'Centerline Low' position, this was reduced to only 14%. Departure is a particularly vulnerable time for large aircraft due to slow climb rates and the inability to fly evasive manoeuvres. The 'Centreline Low' escorted departure greatly reduced the threat to 16% hit or near miss from 62% for an unescorted heavy aircraft. Overall the CounterSim modelling has showed that escorting a civilian aircraft on approach and departure can reduce the MANPAD threat by 3 to 4 times.

  7. Insolvencias. Civil y societaria

    Directory of Open Access Journals (Sweden)

    Gustavo Bordes Leone

    2014-01-01

    Full Text Available El deudor civil que, para substraerse al pago de sus obligaciones, ocultara sus bienes, simulara enajenaciones o créditos, se trasladara al extranjero o se ocultare sin dejar persona que lo represente, o bienes a la vista en cantidad suficiente para responder al pago de sus deudas, será castigado con pena de tres meses de prisión a tres años de penitenciaría. La acción penal no podrá ser ejercitada sino a denuncia de parte, y sólo en el caso de que la insolvencia del deudor resulte comprobada por actos infructuosos de ejecución en la vía civil.Antecedentes históricas. La insolvencia fraudulenta. Insolvencia societaria fraudulenta: Análisis crítico.

  8. Civil Procedure In Denmark

    DEFF Research Database (Denmark)

    Werlauff, Erik

    , enforcement in Denmark of judgments pronounced by Danish or foreign courts, as well as arbitration in Danish and international arbitral cases, based on the extensive Danish arbitral reform 2005, taking the Uncitral pattern arbitration law as its model. The book is written parly based on traditional legal...... on the author's extensive personal experience as arbitrator in numerous Danish and international arbitral proceedings.......The book contains an up-to-date survey of Danish civil procedure after the profound Danish procedural reforms in 2007. It deals with questions concerning competence and function of Danish courts, commencement and preparation of civil cases, questions of evidence and burden of proof, international...

  9. Civil Engineering Dispute Resolution

    CERN Document Server

    Osborne, J

    2001-01-01

    Construction work on the civil engineering contract started at Point 5 in August 1998. The new surface buildings and underground structures are necessary to accommodate the CMS detector for the LHC Project. The principal underground works consist of two new shafts, two parallel caverns separated by a supporting pillar, and a number of small connection tunnels and service galleries. A dispute resolution procedure has been included in the contract, whereby a Panel of Adjudicators may be called upon to make a decision in the case of a difference or dispute between the parties. The aim of this paper is to present CERN's first experience of civil engineering Adjudication arising from problems encountered with the ground freezing technique employed to allow construction of two new shafts.

  10. Manifestations of advanced civilizations

    Science.gov (United States)

    Bracewell, R. N.

    A list of possible modes of detecting advanced civilizations elsewhere in the universe is provided, including EM Alfven, and gravity waves, matter transfer, and exotica such as tachyons, black hole tunneling, and telepathy. Further study is indicated for low frequency radio wave propagation, which may travel along magnetic fields to reach the earth while laser beams are not favored because of the power needed for transmitting quanta instead of waves. IR, X ray, and UV astronomy are noted to be suitable for detecting signals in those ranges, while Alfven wave communication will be best observed by probes outside the orbit of Jupiter, where local anomalies have less effect. Particle propagation communication is viewed as unlikely, except as a trace of an extinct civilization, but panspermia, which involves interstellar spreading of seeds and/or spores, receives serious attention, as does laser probe or pellet propulsion.

  11. Civil society sphericules

    DEFF Research Database (Denmark)

    Tufte, Thomas

    2014-01-01

    This article explores the communicative practice of a Tanzanian NGO, Femina. Based on a tripartite model of engagement (Madianou, 2012) integrating speech, action and understanding, and drawing on fieldwork on the communication practices of Femina, I critically assess the forms of civic engagement...... movement and a media initiative. In the context of the growing literature on social networking sites and their affordances, dynamics and structures, the case of Femina illustrates how a civil society sphericule emerges within the dynamic co-evolution of new and old media platforms. The study is furthermore...... an example of the difficult shift in civil society practice, from service provision to an agenda of public service monitoring, social accountability and community engagement....

  12. [Civil status and suicide].

    Science.gov (United States)

    Gaxiola-Robles, Ramón; Bitzer-Quintero, Oscar Kurt; García-González, Adolfo; Celis-de la Rosa, Alfredo

    2009-01-01

    To determine if civil status acts as a risk factor in suicide and how it modifies according to gender, age and population size. A retrospective study which analyzes information from the mortality data from the National Institute of Statistics, Geography and Information, from 1998 to 2002. Variables like suicides age, sex, cause of death, federal entity, population size and civil status were registered. Single men showed twofold risk for committing suicide. Women did not show any associated risk for suicide according to civil status. The risk of married men for committing suicide increased gradually with age. Medium-sized communities with less than 19,999 habitants presented the highest risk for habitants to commit suicide. Suicide is associated to gender especially to men who are not married and living in small and medium-sized communities. One explanation could be the lack of integrated behavior as defined by Emile Durkheim, where the physical density of society will determine behavior and ideas. This social structure phenomenon is called the "moral cocoon." This works around the individual being less individualistic and granting him/her the feeling of belonging to a group.

  13. Civil Reserve Air Fleet: Looking from Desert Storm to The Future

    Science.gov (United States)

    1992-04-15

    disrupting other aircraft. RE IMBURSEMENT The subject of reimbursement centers on two areas. The first concerns payment for a one-way mission when in reality ...34Land Force in Transition: Challenges and Opportunities," Canadian Defence Quarterly (Winter 1991): 8. 67. MAC, Sources of Civil Airfleet Aumentation

  14. A second-generation high speed civil transport: Stingray

    Science.gov (United States)

    Engdahl, Sean; Lopes, Kevin; Ngan, Angelen; Perrin, Joseph; Phipps, Marcus; Westman, Blake; Yeo, Urn

    1992-01-01

    The Stingray is the second-generation High Speed Civil Transport (HSCT) designed for the 21st Century. This aircraft is designed to be economically viable and environmentally sound transportation competitive in markets currently dominated by subsonic aircraft such as the Boeing 747 and upcoming McDonnell Douglas MD-12. With the Stringray coming into service in 2005, a ticket price of 21 percent over current subsonic airlines will cover operational costs with a 10 percent return on investment. The cost per aircraft will be $202 million with the Direct Operating Cost equal to $0.072 per mile per seat. This aircraft has been designed to be a realistic aircraft that can be built within the next ten to fifteen years. There was only one main technological improvement factor used in the design, that being for the engine specific fuel consumption. The Stingray, therefore, does not rely on technology that does not exist. The Stingray will be powered by four mixed flow turbofans that meet both nitrous oxide emissions and FAR 36 Stage 3 noise regulations. It will carry 250 passengers a distance of 5200 nautical miles at a speed of Mach 2.4. The shape of the Stingray, while optimized for supersonic flight, is compatible with all current airline facilities in airports around the world. As the demand for economical, high-speed flight increases, the Stingray will be ready and able to meet those demands.

  15. Application of Critical Path Method in Risk Management System for Large Aircraft Project%关键路径法在大飞机项目风险管理中的应用

    Institute of Scientific and Technical Information of China (English)

    陶云霜

    2012-01-01

    By identifying the critical path, people can effectively identify the key activities that impact the project progress. Taking appropriate human and material resources and allocate them to key activities can shorten the project duration. This paper first analyzes the importance of using risk management in large aircraft project. Then it introduces how to find out the critical path in a Gantt graph generated by Microsoft Project from the perspective of data structures and algorithms, verifies the method by two examples. Finally, the paper analyzes the insufficient of CPM and proposes some suggestions about how to improve it.%通过识别关键路径可以有效识别出影响工程进度的关键活动,从非关键路径上的活动中适当抽取人力物力资源分配给关键活动可以缩短整个工程工期.本文首先分析大飞机制造项目中风险管理的重要性,进而从数据结构和算法的角度介绍如何在基于Microsoft Project生成的Gantt图上寻找出关键路径,最后结合实例加以分析并提出不足及待改进之处.

  16. Sociedad civil y movimientos sociales en El Salvador de postguerra

    Directory of Open Access Journals (Sweden)

    Alberto Martín Álvarez

    2013-10-01

    Full Text Available Este trabajo ofrece un acercamiento de carácter descriptivo y preliminar a algunas de las principales transformaciones experimentadas por la sociedad civil salvadoreña en el periodo de postguerra.  Dos rasgos fundamentales sobresalen al analizar la dinámica de la sociedad civil de este país en las últimas dos décadas. De una parte, la emergencia de nuevas identidades políticas que habían sido opacadas por la preminencia del discurso de clase del movimiento revolucionario. De otra, la emergencia de amplias movilizaciones estructuradas en base a coaliciones multisectoriales de organizaciones de la sociedad civil, como respuesta a la implementación de políticas neoliberales.Palabras Clave: Sociedad civil, movimientos sociales, El Salvador, postguerra._____________________Abstract:This paper offers a descriptive and preliminary approach to some of the major changes experienced by Salvadoran civil society in the postwar period. Two main features stand out when analyzing the dynamics of civil society in this country in the last two decades. On one hand, the emergence of new political identities that had been overshadowed by the prominence of the classist discourse of the revolutionary movement. On the other, the emergence of large mobilizations structured around multisectoral coalitions of civil society organizations, in response to the implementation of neoliberal policies.Keywords: Civil society, social movements, El Salvador, postwar

  17. The barbarism of civilization: cultural genocide and the 'stolen generations'.

    Science.gov (United States)

    van Krieken, R

    1999-06-01

    Norbert Elias suggested that 'civilization' involves the transformation of human habitus so that violence of all sorts is gradually subjected to greater and more sophisticated forms of management and control, whereas 'decivilization' encompasses processes which produce an increase in violence and a breakdown in the stability and consistency of on-going social relations. What remains unexplored is the extent to which 'civilizing offensives', the self-conscious attempts to bring about 'civilization', have revolved around essentially violent policies and practices. This paper examines the systematic removal of indigenous Australian children from their families, largely for the social engineering purpose of the gradual and systematic annihilation of Aboriginal cultural identity. At the time, these policies and practices were constructed by most observers as contributing to the 'welfare' of Australian Aborigines, and this intersection of welfare and violence raises the possibility that civilization and decivilization, rather than being different processes which may or may not run alongside each other, interpenetrate each other so that, under certain circumstances, societies are 'barbaric' precisely in their movement towards increasing civilization. It may also be possible to describe the move away from the systematic removal of Aboriginal children since the 1970s as itself part of a civilizing process, an increasing recognition of the human rights of Australian Aborigines and of the inhumanity of those policies and practices. The paper concludes by addressing the implications for theories of civilization and decivilization, as well as more generally for our contemporary understanding of what it means to be a 'civilized' modern citizen.

  18. 舰载机大失准角的快速二次传递对准方法%Rapid second time transfer alignment of large misalignment for carrier aircrafts

    Institute of Scientific and Technical Information of China (English)

    孙枫; 吴旭; 王根

    2012-01-01

    针对舰载机传递对准特点,直接利用主惯导的导航信息进行一次装订,引入了大失准角对准问题.为了解决舰载机传递对准问题,提出利用子惯导自主对准进行一次装订减小子惯导中间坐标系与主惯导间的失准角.分析Wahba问题提出统计意义的Quaternion(四元数)对准方法替换传统的Triad(双矢定姿)对准方法,提高了多信息冗余度和对准精度.基于分级修正思想,提出二次传递对准方法,第一次传递基于非线性模型和自适应渐消扩展卡尔曼滤波,并给出简化的渐消因子计算方法;第二次传递对准基于线性误差模型,采用速度+航向匹配,在补偿失准角的基础上,估计陀螺漂移.仿真结果表明二次传递方法能够满足舰载机传递对准需求.%Using the master inertial navigation system(MINS) navigation information,the slave inertial navigation system(SINS) was introduce to solve the large misalignment problem of the carrier aircraft transfer.The self-alignment was adopted before the transfer alignment to reduce the misalignment between the MINS and SINS.Then the Triad alignment method was replaced by statistical Quaternion method based on the solution of Wahba problem,which improved the alignment accuracy and redundancy.Then based on the cascaded calibration method,a second time transfer alignment was presented.The first alignment was based on the nonlinear error model and adaptive fading extended Kalman filter(AFEKF),and a new method of calculating fading factor was presented.The second alignment based on the linear error model,adopting velocity-yaw matching method not only estimate and compensate the misalignment angles,but also estimated the gyrocompass drift.The simulation results show that this method can satisfy the requirement for the carrier aircraft transfer alignment.

  19. Speech systems for autonomous unmanned aircraft: enabling autonomous unmanned aircraft to communicate in civil airspace

    CSIR Research Space (South Africa)

    Burger, CR

    2011-09-01

    Full Text Available (VFR) and Instrument Flight Rules (IFR). Typical local surveillance missions are done under VFR, but almost all passenger- carrying operations are done under IFR. Because many urban surveillance missions take place in close proximity to airline... hubs, IFR capability is required. Rural and peri-urban operations require VFR capability. The levels of control are: o Controlled airspace: In controlled airspace, a controller provides binding instructions to ensure that traffic separation...

  20. Aircraft Noise Prediction

    OpenAIRE

    2014-01-01

    This contribution addresses the state-of-the-art in the field of aircraft noise prediction, simulation and minimisation. The point of view taken in this context is that of comprehensive models that couple the various aircraft systems with the acoustic sources, the propagation and the flight trajectories. After an exhaustive review of the present predictive technologies in the relevant fields (airframe, propulsion, propagation, aircraft operations, trajectory optimisation), the paper add...

  1. Structural analysis at aircraft conceptual design stage

    Science.gov (United States)

    Mansouri, Reza

    In the past 50 years, computers have helped by augmenting human efforts with tremendous pace. The aircraft industry is not an exception. Aircraft industry is more than ever dependent on computing because of a high level of complexity and the increasing need for excellence to survive a highly competitive marketplace. Designers choose computers to perform almost every analysis task. But while doing so, existing effective, accurate and easy to use classical analytical methods are often forgotten, which can be very useful especially in the early phases of the aircraft design where concept generation and evaluation demands physical visibility of design parameters to make decisions [39, 2004]. Structural analysis methods have been used by human beings since the very early civilization. Centuries before computers were invented; the pyramids were designed and constructed by Egyptians around 2000 B.C, the Parthenon was built by the Greeks, around 240 B.C, Dujiangyan was built by the Chinese. Persepolis, Hagia Sophia, Taj Mahal, Eiffel tower are only few more examples of historical buildings, bridges and monuments that were constructed before we had any advancement made in computer aided engineering. Aircraft industry is no exception either. In the first half of the 20th century, engineers used classical method and designed civil transport aircraft such as Ford Tri Motor (1926), Lockheed Vega (1927), Lockheed 9 Orion (1931), Douglas DC-3 (1935), Douglas DC-4/C-54 Skymaster (1938), Boeing 307 (1938) and Boeing 314 Clipper (1939) and managed to become airborne without difficulty. Evidencing, while advanced numerical methods such as the finite element analysis is one of the most effective structural analysis methods; classical structural analysis methods can also be as useful especially during the early phase of a fixed wing aircraft design where major decisions are made and concept generation and evaluation demands physical visibility of design parameters to make decisions

  2. Differences in Characteristics of Aviation Accidents During 1993-2012 Based on Aircraft Type

    Science.gov (United States)

    Evans, Joni K.

    2015-01-01

    Civilian aircraft are available in a variety of sizes, engine types, construction materials and instrumentation complexity. For the analysis reported here, eleven aircraft categories were developed based mostly on aircraft size and engine type, and these categories were applied to twenty consecutive years of civil aviation accidents. Differences in various factors were examined among these aircraft types, including accident severity, pilot characteristics and accident occurrence categories. In general, regional jets and very light sport aircraft had the lowest rates of adverse outcomes (injuries, fatal accidents, aircraft destruction, major accidents), while aircraft with twin (piston) engines or with a single (piston) engine and retractable landing gear carried the highest incidence of adverse outcomes. The accident categories of abnormal runway contact, runway excursions and non-powerplant system/component failures occur frequently within all but two or three aircraft types. In contrast, ground collisions, loss of control - on ground/water and powerplant system/component failure occur frequently within only one or two aircraft types. Although accidents in larger aircraft tend to have less severe outcomes, adverse outcome rates also differ among accident categories. It may be that the type of accident has as much or more influence on the outcome as the type of aircraft.

  3. Research on precise forming process of aircraft aluminum large sheet metal part%飞机铝合金大型钣金件精确成形研究

    Institute of Scientific and Technical Information of China (English)

    白颖; 张引引; 赵刚; 陈磊

    2011-01-01

    Owing to the large size and low roughness, the forming process of large sheet metal parts of aircraft is difficult The shape and structure were optimized after increasing the corners and decreasing the length of adding straps based on the analysis of the part structure and assemble requirement The reasonable fabrication technology and a set of deformation-proof measures were defined using deep drawing method that improved the forming approach and the accuracy. By finite numerical simulation, theoretical computation and experiment, profile dimensions of the semi finished products were optimized, the reasonable tooling structure and the best BHP value were determined. Thus the precise forming requirement is satisfied.%飞机铝合金大型钣金件成形尺寸大,刚性差,制造难度大.通过对零件结构及装配要求的分析,提出了增大四周拐角角度,减少补加条带长度的改进意见,优化了零件的外形结构.借助双动拉深的优越性,采用了双动拉深的成形方法,确定出合理的制造流程和一套防止零件热处理产生变形的措施,提高了零件的成形准确度.利用有限元数值模拟、理论计算并结合实际试验,优化了展开毛坯的外形尺寸,确定出合理的工装结构以及压边力的最佳数值,达到零件精确成形的要求.

  4. 3D-CFD Investigation of Contrails and Volatile Aerosols Produced in the Near-Field of an Aircraft Wake

    Science.gov (United States)

    Garnier, F.; Ghedhaifi, W.; Vancassel, X.; Khou, J. C.; Montreuil, E.

    2015-12-01

    Civil aviation contributes to degradation of air quality around airport (SOx, NOx, speciated hydrocarbons,…) and climate change through its emissions of greenhouse gases (CO2, water vapor), as well as particulate matters. These particles include soot particles formed in the combustor, volatile aerosols and contrails generated in the aircraft wake. Although the aircraft emissions represent today only about 3% of all those produced on the surface of the earth by other anthropogenic sources, they are mostly released in the very sensitive region of the upper troposphere/lower stratosphere. These emissions have a radiative effect reinforced by specific physical and chemical processes at high altitudes, such as cloud formation and ozone production. In this context, most of the work to-date assessed that the actual effect of aviation on the climate are affected by very large uncertainties, partly due to lack of knowledge on the mechanisms of new particles formation and growth processes in the exhaust plume of the aircraft. The engine exhaust gases are mixed in the ambient air under the influence of the interaction between the jet engine and the wing tip vortices. The characteristics of vortices as well as their interaction with the jet depend on the aircraft airframe especially on the wing geometry and the engine position (distance from the wing tip). The aim of this study is to examine the influence of aircraft parameters on contrail formation using a 3D CFD calculation based on a RANS (Reynolds Average Navier-Stokes) approach. Numerical simulations have been performed using CEDRE, the multiphysics ONERA code for energetics. CEDRE is a CFD code using finite volume methods and unstructured meshes. These meshes are especially appropriate when complex geometries are used. A transport model has been used for condensation of water vapor onto ice particles. Growth is evaluated using a modified Fick's law to mass transfer on particles. In this study, different aircraft

  5. B 150 civil engineering futures

    DEFF Research Database (Denmark)

    Foreword B150 –Civil Engineering Futures consists of interviews made, articles written, and projects presented in connection with the 150th anniversary celebrations of the study of civil engineering in Denmark. Instead of a historical retrospect, it was decided to look into the future. What...... challenges will the next 150 years bring civil engineers? Researchers and lecturers at DTU’s Department of Civil Engineering (known as DTU Byg) suggested possible events, and we also consulted civil engineers and their business partners in the building industry. In this way, a programme was put together...... theme in twentieth century architecture. Together, civil engineer Peter Rice and architect Ian Ritchie created a paradigm shift with their revolutionary ideas for glass facades supported by cables. Glued and bolted constructions made entirely of glass are now a reality in small-scale projects, yet...

  6. Maintenance cost study of rotary wing aircraft, phase 2

    Science.gov (United States)

    1979-01-01

    The Navy's maintenance and materials management data base was used in a study to determine the feasibility of predicting unscheduled maintenance costs for the dynamic systems of military rotary wing aircraft. The major operational and design variables were identified and the direct maintenance man hours per flight hour were obtained by step-wise multiple regression analysis. Five nonmilitary helicopter users were contacted to supply data on which variables were important factors in civil applications. These uses included offshore oil exploration and support, police and fire department rescue and enforcement, logging and heavy equipment movement, and U.S. Army military operations. The equations developed were highly effective in predicting unscheduled direct maintenance man hours per flying hours for military aircraft, but less effective for commercial or public service helicopters, probably because of the longer mission durations and the much higher utilization of civil users.

  7. How persistent is civilization growth?

    OpenAIRE

    Garrett, Timothy J.

    2011-01-01

    In a recent study (Garrett, 2011), I described theoretical arguments and empirical evidence showing how civilization evolution might be considered from a purely physical basis. One implication is that civilization exhibits the property of persistence in its growth. Here, this argument is elaborated further, and specific near-term forecasts are provided for key economic variables and anthropogenic CO2 emission rates at global scales. Absent some external shock, civilization wealth, energy cons...

  8. Legal Officer Civil Law Study Guide

    Science.gov (United States)

    1991-06-01

    it may be more pr&udent to utilize black-and-white film . Pnlaroid prints offer instant review to ensure that the desired picture is obtain-ed, hut...dimensions. The investigative report should include the negatives plus complete tichnical rdetails relating to the camera tused (e.g., type, settings, film ...Act or the Act] which is- largely a reenactment of the Soldiers’ and Sailors’ Civil Relief Act of -1918. Except for specific relief provisions deemed

  9. Jet aircraft engine exhaust emissions database development: Year 1990 and 2015 scenarios

    Science.gov (United States)

    Landau, Z. Harry; Metwally, Munir; Vanalstyne, Richard; Ward, Clay A.

    1994-01-01

    Studies relating to environmental emissions associated with the High Speed Civil Transport (HSCT) military jet and charter jet aircraft were conducted by McDonnell Douglas Aerospace Transport Aircraft. The report includes engine emission results for baseline 1990 charter and military scenario and the projected jet engine emissions results for a 2015 scenario for a Mach 1.6 HSCT charter and military fleet. Discussions of the methodology used in formulating these databases are provided.

  10. Electrochromic windows - Applications for aircraft

    Science.gov (United States)

    Harris, Caroline S.; Greenberg, Charles B.

    1989-04-01

    A transparent, solid-state, electrochromic device is described. It demonstrates deep switching in the near infrared and visible spectral regions and good room temperature cycling stability. The response appears reasonably uniform over a 14 cm x 28 cm area, which gives hope for achieving large parts for cockpit and cabin windows. The reversible darkening of the transparency, controlled by an applied voltage or current, has potential application in aircraft to reduce glare and solar heat load to pilots and passengers. The active material in the device is a thin tungsten oxide film which is incorporated into a complex, multilayered structure, essentially that of a transparent battery. The performance of the window is discussed in terms of its configuration, its similarities with commercial batteries and issues critical to aircraft.

  11. Adaptive output feedback control of aircraft flexible modes

    OpenAIRE

    Ponnusamy, Sangeeth Saagar; Bordeneuve-Guibé, Joël

    2012-01-01

    The application of adaptive output feedback augmentative control to the flexible aircraft problem is presented. Experimental validation of control scheme was carried out using a three disk torsional pendulum. In the reference model adaptive control scheme, the rigid aircraft reference model and neural network adaptation is used to control structural flexible modes and compensate for the effects unmodeled dynamics and parametric variations of a classical high order large passenger aircraft. Th...

  12. Structural Weight Optimization of Aircraft Wing Component Using FEM Approach.

    OpenAIRE

    Arockia Ruban M,; Kaveti Aruna

    2015-01-01

    One of the main challenges for the civil aviation industry is the reduction of its environmental impact by better fuel efficiency by virtue of Structural optimization. Over the past years, improvements in performance and fuel efficiency have been achieved by simplifying the design of the structural components and usage of composite materials to reduce the overall weight of the structure. This paper deals with the weight optimization of transport aircraft with low wing configuratio...

  13. Influence of the aircraft crash induced local nonlinearities on the overall dynamic response of a RC structure through a parametric study

    Energy Technology Data Exchange (ETDEWEB)

    Rouzaud, C., E-mail: crouzaud@adm.estp.fr [LMT (ENS Cachan, CNRS, Université Paris Saclay) 61 avenue du Président Wilson, 94235 Cachan (France); Université Paris-Est, Institut de Recherche en Constructibilité, ESTP 28 avenue du Président Wilson, 94230 Cachan (France); AREVA, 10 rue Juliette Récamier, 69006 Lyon (France); Gatuingt, F. [LMT (ENS Cachan, CNRS, Université Paris Saclay) 61 avenue du Président Wilson, 94235 Cachan (France); Hervé, G. [Université Paris-Est, Institut de Recherche en Constructibilité, ESTP 28 avenue du Président Wilson, 94230 Cachan (France); Moussallam, N. [AREVA, 10 rue Juliette Récamier, 69006 Lyon (France); Dorival, O. [Icam, Site de Toulouse, 75 avenue de Grande-Bretagne, 31076 Toulouse Cedex 3 (France); Université de Toulouse, Institut Clément Ader (ICA), INSA, UPS, Mines Albi, ISAE 135 avenue de Rangueil, 31077 Toulouse Cedex (France)

    2016-03-15

    Highlights: • Structures could resist to the induced accelerations which they might undergo. • The characterization of non-linearities in the signal of an aircraft impact. • The non linear impact area are studied through a sensitivity analysis. • This analysis should allow to achieve a link between aircraft impact parameters. - Abstract: In the process of nuclear power plant design, the safety of structures is an important aspect. Civil engineering structures have to resist the accelerations induced by, for example, seismic loads or shaking loads resulting from the aircraft impact. This is even more important for the in-structures equipments that have also to be qualified against the vibrations generated by this kind of hazards. In the case of aircraft crash, as a large variety of scenarios has to be envisaged, it is necessary to use methods that are less CPU-time consuming and that consider appropriately the nonlinearities. The analysis presented in this paper deals with the problem of the characterization of nonlinearities (damaged area, transmitted force) in the response of a structure subjected to an aircraft impact. The purpose of our study is part of the development of a new decoupled nonlinear and elastic way for calculating the shaking of structures following an aircraft impact which could be very numerically costly if studied with classical finite element methods. The aim is to identify which parameters control the dimensions of the nonlinear zone and so will have a direct impact on the induced vibrations. In a design context, several load cases (and simulations) are analyzed in order to consider a wide range of impact (different loading surfaces, momentum) and data sets of the target (thickness, reinforcements). In this work, the nonlinear area generated by the impact is localized and studied through a parametric analysis associated with a sensitivity analysis to identify the boundaries between the elastic domain and this nonlinear area.

  14. Cable Tensiometer for Aircraft

    Science.gov (United States)

    Nunnelee, Mark (Inventor)

    2008-01-01

    The invention is a cable tensiometer that can be used on aircraft for real-time, in-flight cable tension measurements. The invention can be used on any aircraft cables with high precision. The invention is extremely light-weight, hangs on the cable being tested and uses a dual bending beam design with a high mill-volt output to determine tension.

  15. 22 CFR 1006.920 - Civil judgment.

    Science.gov (United States)

    2010-04-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 22 Foreign Relations 2 2010-04-01 2010-04-01 true Civil judgment. 1006.920 Section 1006.920...) Definitions § 1006.920 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  16. 34 CFR 85.920 - Civil judgment.

    Science.gov (United States)

    2010-07-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 34 Education 1 2010-07-01 2010-07-01 false Civil judgment. 85.920 Section 85.920 Education Office...) Definitions § 85.920 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  17. 21 CFR 1404.920 - Civil judgment.

    Science.gov (United States)

    2010-04-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 21 Food and Drugs 9 2010-04-01 2010-04-01 false Civil judgment. 1404.920 Section 1404.920 Food and...) Definitions § 1404.920 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  18. 22 CFR 1508.920 - Civil judgment.

    Science.gov (United States)

    2010-04-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 22 Foreign Relations 2 2010-04-01 2010-04-01 true Civil judgment. 1508.920 Section 1508.920...) Definitions § 1508.920 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  19. 22 CFR 208.920 - Civil judgment.

    Science.gov (United States)

    2010-04-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 22 Foreign Relations 1 2010-04-01 2010-04-01 false Civil judgment. 208.920 Section 208.920 Foreign...) Definitions § 208.920 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  20. 2 CFR 180.915 - Civil judgment.

    Science.gov (United States)

    2010-01-01

    ... creates a civil liability for the complained of wrongful acts, or a final determination of liability under... 2 Grants and Agreements 1 2010-01-01 2010-01-01 false Civil judgment. 180.915 Section 180.915... § 180.915 Civil judgment. Civil judgment means the disposition of a civil action by any court...

  1. How Effective Was Civil Affairs in Bosnia?

    Science.gov (United States)

    2013-12-13

    50 Planning the Deployment of the Implementation Force...Allied Rapid Reaction Corps BiH Bosnia and Herzegovina CA Civil Affairs CAO Civil Affairs Operations CIM Civil Information Management CIMIC Civil...and replaced a 2003 version. This publication serves as a guideline for planning and conducting civil military operations in the joint (multi

  2. Civil engineering studies for major projects after LHC

    CERN Document Server

    Osborne, John; Perez-Duenas, Eliseo

    2011-01-01

    CERN civil engineers are heavily involved in studying several major potential collider projects to succeed/complement the LHC. Infrastructure works typically represent one third of the cost of major physics projects, so it's critical that the construction costs are well understood from the conceptual stage. For example, CERN are studying infrastructure requirements for the Linear Collider (CLIC & ILC) and the LHeC projects. This paper presents some of the key civil engineering challenges faced in such large scale projects.

  3. Sensitivity of model assessments of high-speed civil transport effects on stratospheric ozone resulting from uncertainties in the NO x production from lightning

    Science.gov (United States)

    Smyshlyaev, Sergei P.; Geller, Marvin A.; Yudin, Valery A.

    1999-11-01

    Lightning NOx production is one of the most important and most uncertain sources of reactive nitrogen in the atmosphere. To examine the role of NOx lightning production uncertainties in supersonic aircraft assessment studies, we have done a number of numerical calculations with the State University of New York at Stony Brook-Russian State Hydrometeorological Institute of Saint-Petersburg two-dimensional model. The amount of nitrogen oxides produced by lightning discharges was varied within its quoted uncertainty from 2 to 12 Tg N/yr. Different latitudinal, altitudinal, and seasonal distributions of lightning NOx production were considered. Results of these model calculations show that the assessment of supersonic aircraft impacts on the ozone layer is very sensitive to the strength of NOx production from lightning. The high-speed civil transport produced NOx leads to positive column ozone changes for lightning NOx production less than 4 Tg N/yr, and to total ozone decrease for lightning NOx production more than 5 Tg N/yr for the same NOx emission scenario. For large lightning production the ozone response is mostly decreasing with increasing emission index, while for low lightning production the ozone response is mostly increasing with increasing emission index. Uncertainties in the global lightning NOx production strength may lead to uncertainties in column ozone up to 4%. The uncertainties due to neglecting the seasonal variations of the lightning NOx production and its simplified latitude distribution are about 2 times less (1.5-2%). The type of altitude distribution for the lightning NOx production does not significally impact the column ozone, but is very important for the assessment studies of aircraft perturbations of atmospheric ozone. Increased global lightning NOx production causes increased total ozone, but for assessment of the column ozone response to supersonic aircraft emissions, the increase of lightning NOx production leads to column ozone

  4. Propulsion controlled aircraft research

    Science.gov (United States)

    Fullerton, C. Gordon

    1993-01-01

    The NASA Dryden Flight Research Facility has been conducting flight, ground simulator, and analytical studies to investigate the use of thrust modulation on multi-engine aircraft for emergency flight control. Two general methods of engine only control have been studied; manual manipulation of the throttles by the pilot, and augmented control where a computer commands thrust levels in response to pilot attitude inputs and aircraft motion feedbacks. This latter method is referred to as the Propulsion Controlled Aircraft (PCA) System. A wide variety of aircraft have been investigated. Simulation studies have included the B720, F-15, B727, B747 and MD-11. A look at manual control has been done in actual flight on the F15, T-38, B747, Lear 25, T-39, MD-11 and PA-30 Aircraft. The only inflight trial of the augmented (PCA) concept has been on an F15, the results of which will be presented below.

  5. Aircraft operations management manual

    Science.gov (United States)

    1992-01-01

    The NASA aircraft operations program is a multifaceted, highly diverse entity that directly supports the agency mission in aeronautical research and development, space science and applications, space flight, astronaut readiness training, and related activities through research and development, program support, and mission management aircraft operations flights. Users of the program are interagency, inter-government, international, and the business community. This manual provides guidelines to establish policy for the management of NASA aircraft resources, aircraft operations, and related matters. This policy is an integral part of and must be followed when establishing field installation policy and procedures covering the management of NASA aircraft operations. Each operating location will develop appropriate local procedures that conform with the requirements of this handbook. This manual should be used in conjunction with other governing instructions, handbooks, and manuals.

  6. The fatigue life analysis and optimization of landing gear for a large amphibian aircraft%大型水陆两栖飞机起落架疲劳寿命分析与优化

    Institute of Scientific and Technical Information of China (English)

    姜成杰; 许锋

    2015-01-01

    以疲劳寿命分析理论成果为指导,对大型水陆两栖飞机主起落架进行疲劳寿命计算分析与结构优化研究。通过Hypermesh进行模型有限元前处理,在NASTRAN中计算应力分布结果,利用NcodeDesignlife研究起落架整体结构件疲劳寿命;通过LMS Virtual.Lab建立前起落架刚柔耦合模型,得到各个零部件连接部位节点力,从而完成对各个零部件的独立建模分析计算;基于疲劳寿命的结构优化技术,以Optistruct为工具对起落架疲劳寿命薄弱部位进行形状优化,使得疲劳寿命进一步提高。%Based on the theory of fatigue life analysis , it describes the fatigue life analysis and optimization of the main landing gear for a large amphibian aircraft .It builds the landing gear element model in Hypermesh , calcu-lates the distribution in NASTRAN , analyzes the landing gear overall structure fatigue life in NcodeDesignlife .It establishes the rigid flexible coupling model of the main landing gear and obtains the node forces of all connected parts through LMS Virtual .Lab, sets up the models one by one for each parts to obtain the more accurate fatigue life of each parts.At last, based on the fatigue life structure optimization technology , it realizes the shape optimi-zation for the positions of the main landing gear with little fatigue life to make further improvement in Optistruct .

  7. 大型客机机舱内饰板隔声性能计算与试验%Calculation and Testing of Sound Transmission Loss for Interior Panels of Large Aircraft Fuselages

    Institute of Scientific and Technical Information of China (English)

    韩峰

    2014-01-01

    结合单层板与夹层板隔声理论,推导了应用于计算典型飞机机舱内饰板隔声量的分析方法。根据所推导的计算公式,将真实环境条件与内饰板材料参数代入其中,获得地面与飞行状态下的隔声量计算结果。与实测数据对比之后,发现在特定频率区域内饰板计算量值与趋势都与试验吻合较好,但在共振频率、吻合频率和压缩频率上,计算值与试验测量值有较大起伏。对比飞行与地面两种条件,飞机状态下的隔声量普遍大于地面状态。%Combining the acoustic theories of plain panel and sandwich panel, an analysis method to calculate sound transmission loss of interior panel of typical aircraft fuselages is provided. According to the sound transmission loss equations, the real parameters of interior panel are defined and put into calculation process. Then, the results of sound insulation in flight and ground conditions are obtained. It is found that the value and tendency of the sound insulation agree well with the measurement data from the testing in a special frequency range. However, there are somewhat large differences between them in resonance frequencies, coincidence frequencies and dilatation frequencies of the sandwich panel. The sound insulation effect in flight condition is better than that in ground condition.

  8. 人类大文明略论%On the Great Civilizations of Mankind

    Institute of Scientific and Technical Information of China (English)

    吴灿新

    2012-01-01

    当今人类文明建设的实践,推动着我们对人类文明的认识必须走上一个新的台阶——人类大文明。人类大文明是一个极其复杂、十分庞大的系统,它由三大文明——生态文明、社态文明和个态文明构成。而生态文明又由天态文明、人态文明、地态文明(境态文明)、物态文明组成;社态文明则由物质文明、精神文明、制度文明(政治文明)、社会文明构成;个态文明也由身态文明、心态文明、思态文明、行态文明组成。它们之间对立统一,矛盾运动,推动着人类整个文明系统不断发展进步。%The practice of modern human civilization pushes our understanding of human civilization forward to a new stage-Great Human Civilization.Great human civilization is an extremely complicated and large system,which consists of three major civilizations-ecological state of civilization,social state of civilization,and personal state of civilization.The ecological state of civilization is comprised of day state of civilization,people state of civilization,ground state of civilization(environment state of civilization) and physical state of civilization.Social state of civilization is composed of material civilization,spiritual civilization,institutional civilization(political civilization) and social civilization.Personal state of civilization is made up of body state of civilization,mental state of civilization,thinking state of civilization and behavior state of civilization.They are unity of opposites and develop paradoxically to promote the progress of the whole civilized system.

  9. Reconstructing Sub-Saharan, Mayan, and Other Prehistoric Civilizations in Mathematical Macro-Theory of Civilizations

    CERN Document Server

    Blaha, S

    2003-01-01

    A study of the Great Zimbabwe Sub-Saharan civilization, Mayan civilization and other prehistoric civilizations within the framework of a mathematical macro theory of civilizations. We show these isolated and early civilizations conform to the general mathematical theory of civilizations in detail.

  10. Código civil colombiano

    OpenAIRE

    Secretaria del Senado Colombia

    2005-01-01

    El Código Civil como lo indica su articulo primero,comprende las disposiciones legales sustantivas que determinan especialmente los derechos de los particulares, por razón del estado de las personas, de sus bienes, obligaciones, contratos y acciones civiles.

  11. Environmental Ethics and Civil Engineering.

    Science.gov (United States)

    Vesilind, P. Aarne

    1987-01-01

    Traces the development of the civil engineering code of ethics. Points out that the code does have an enforceable provision that addresses the engineer's responsibility toward the environment. Suggests revisions to the code to accommodate the environmental impacts of civil engineering. (TW)

  12. Civil Engineering Technology Needs Assessment.

    Science.gov (United States)

    Oakland Community Coll., Farmington, MI. Office of Institutional Planning and Analysis.

    In 1991, a study was conducted by Oakland Community College (OCC) to evaluate the need for a proposed Civil Engineering Technology program. An initial examination of the literature focused on industry needs and the job market for civil engineering technicians. In order to gather information on local area employers' hiring practices and needs, a…

  13. Código civil colombiano

    OpenAIRE

    Secretaria del Senado Colombia

    2005-01-01

    El Código Civil como lo indica su articulo primero,comprende las disposiciones legales sustantivas que determinan especialmente los derechos de los particulares, por razón del estado de las personas, de sus bienes, obligaciones, contratos y acciones civiles.

  14. Codificación civil

    OpenAIRE

    Verdera Server, Rafael

    2012-01-01

    Conferencias sobre la codificación civil: aspectos históricos (R. Aznar) y jurídicos (J.M. Badenas)Actividad complementaria de los Departamentos de Historia del Derecho y Derecho Civil.Grado en Derecho

  15. Social Science and Civil Society

    OpenAIRE

    Hogg, Eddy

    2015-01-01

    This article gives an overview of key social science approaches to civil society. It addresses in turn civil society organizations, volunteering, and philanthropy. For each, it looks at how they are defined, their scope, how social science approaches the study of them, and how social policy has sought to encourage or coordinate them.

  16. Codificación civil

    OpenAIRE

    Verdera Server, Rafael

    2012-01-01

    Conferencias sobre la codificación civil: aspectos históricos (R. Aznar) y jurídicos (J.M. Badenas)Actividad complementaria de los Departamentos de Historia del Derecho y Derecho Civil.Grado en Derecho

  17. The Reconfiguration of Civil Society through Ethnic Communal Development

    Directory of Open Access Journals (Sweden)

    Walter Frank Lalich

    2009-11-01

    Full Text Available Migrant communities participate in the reconfiguration of civil society in places of settlement. Among the consequences of the large-scale culturally diverse postwar migration was in the regeneration, broadening and diversification of Australian civil society. This contribution outlines with unique data generated from ethnic communal organisations in Sydney the process of confluence of migration and civil society out of settlement constraints. Consecutive waves of migrants experienced settlement constraints that impaired the quality of their lives in a welfare state. Migrants, mostly left to themselves, acted collectively to improve the quality of their existence, to enable co-ethnic communication, and to mediate with the rest of society. They established thousands of grassroots organisations through collective mobilization of scarce resources. Many ethnic collectives through collective action appropriated their own communal places to satisfy spiritual, educational, welfare and other secular needs alongside the other forms of institutional development. Ethnic communal places, representatives of the re-territorialized cultures, heritages and elements of civil society, signify migrant inclusion in Australian social structures, including in civil society. Through development of community capital, ethnic collectives impacted on civil society in an environment experiencing limited cross-cultural social exchange. This development is representative of the unique structure of Australian civil society.

  18. Direct effects of lightning on an aircraft during intentional penetrations of thunderstorms. [T-28 aircraft

    Science.gov (United States)

    Musil, D. J.; Prodan, J.

    1980-01-01

    An armored T-28 aircraft was struck by lightning on two different days while participating in the 1979 severe environmental storm and mesoscale experiment in Oklahoma. The T-28, which is specially armored and instrumented, was making intentional penetrations of thunderstorms and was struck twice on 30 May and once on 5 June. Various degrees of damage, mainly in the form of large burn spots and holes, resulted to the aircraft.

  19. Aircraft noise and its nearfield propagation computations

    Institute of Scientific and Technical Information of China (English)

    Xin Zhang

    2012-01-01

    Noise generated by civil transport aircraft during take-off and approach-to-land phases of operation is an environmental problem.The aircraft noise problem is firstly reviewed in this article.The review is followed by a description and assessment of a number of sound propagation methods suitable for applications with a background mean flow field pertinent to aircraft noise.Of the three main areas of the noise problem,i.e.generation,propagation,and radiation,propagation provides a vital link between near-field noise generation and far-field radiation.Its accurate assessment ensures the overall validity of a prediction model.Of the various classes of propagation equations,linearised Euler equations are often casted in either time domain or frequency domain.The equations are often solved numerically by computational aeroacoustics techniques,bur are subject to the onset of Kelvin-Helmholtz (K-H) instability modes which may ruin the solutions. Other forms of linearised equations,e.g.acoustic perturbation equations have been proposed,with differing degrees of success.

  20. The Ambivalences of Civil Society

    Directory of Open Access Journals (Sweden)

    Henrik Kaare Nielsen

    2008-07-01

    Full Text Available This article discusses the conceptual heterogeneity in the field of ‘civil society’ in the light of a distinction between positions that reflect civil society as a democratic-emancipatory category and positions that consider civil society from the perspective of the state: as an instrumental resource for the technocratic planning of the competitive nation state.The article discusses the implications and perspectives in these two different strategic scenarios for conceptualizing civil society. The argument is made that civil society in relation to democratic citizenship should basically rather be understood as a concept for specific, communicative principles for institutionalizing societal relations and organizing public experience than as an overall concept for third sector organizations.

  1. Sustainability issues in civil engineering

    CERN Document Server

    Saride, Sireesh; Basha, B

    2017-01-01

    This compilation on sustainability issues in civil engineering comprises contributions from international experts who have been working in the area of sustainability in civil engineering. Many of the contributions have been presented as keynote lectures at the International Conference on Sustainable Civil Infrastructure (ICSCI) held in Hyderabad, India. The book has been divided into core themes of Sustainable Transportation Systems, Sustainable Geosystems, Sustainable Environmental and Water Resources and Sustainable Structural Systems. Use of sustainability principles in engineering has become an important component of the process of design and in this context, design and analysis approaches in civil engineering are being reexamined to incorporate the principles of sustainable designs and construction in practice. Developing economies are on the threshold of rapid infrastructure growth and there is a need to compile the developments in various branches of civil engineering and highlight the issues. It is th...

  2. 76 FR 71431 - Civil Penalty Calculation Methodology

    Science.gov (United States)

    2011-11-17

    ... TRANSPORTATION Federal Motor Carrier Safety Administration Civil Penalty Calculation Methodology AGENCY: Federal... its civil penalty methodology. Part of this evaluation includes a forthcoming explanation of the... methodology for calculation of certain civil penalties. To induce compliance with federal regulations,...

  3. Information note about the protection of nuclear facilities against aircraft crashes; Note d'information sur la protection des installations nucleaires contre les chutes d'avions

    Energy Technology Data Exchange (ETDEWEB)

    NONE

    2001-07-01

    The protection of nuclear facilities against external risks (earthquakes, floods, fires etc..) is an aspect of safety taken into consideration by the French authority of nuclear safety (ASN). Concerning the aircraft crashes, the fundamental safety rules make three categories of aircraft: the small civil aircraft (weight < 5.7 t), the military aircraft, and the commercial aircraft (w > 5.7 t). Nuclear facilities are designed to resist against crashes of aircraft from the first category only, because the probability of the accidental crash of a big aircraft are extremely low. This document comprises an information note about the protection of nuclear facilities against aircraft crashes, a dossier about the safety of nuclear facilities with respect to external risks in general (natural disasters and aircraft crashes), and an article about the protection of nuclear power plants against aircraft crashes (design, safety measures, regulation, surveillance, experience feedback). (J.S.)

  4. Predicting Visibility of Aircraft

    Science.gov (United States)

    Watson, Andrew; Ramirez, Cesar V.; Salud, Ellen

    2009-01-01

    Visual detection of aircraft by human observers is an important element of aviation safety. To assess and ensure safety, it would be useful to be able to be able to predict the visibility, to a human observer, of an aircraft of specified size, shape, distance, and coloration. Examples include assuring safe separation among aircraft and between aircraft and unmanned vehicles, design of airport control towers, and efforts to enhance or suppress the visibility of military and rescue vehicles. We have recently developed a simple metric of pattern visibility, the Spatial Standard Observer (SSO). In this report we examine whether the SSO can predict visibility of simulated aircraft images. We constructed a set of aircraft images from three-dimensional computer graphic models, and measured the luminance contrast threshold for each image from three human observers. The data were well predicted by the SSO. Finally, we show how to use the SSO to predict visibility range for aircraft of arbitrary size, shape, distance, and coloration. PMID:19462007

  5. 飞机大部件调姿平台力位混合控制系统设计%Design on hybrid force position control of large aircraft components posture alignment platform

    Institute of Scientific and Technical Information of China (English)

    罗中海; 孟祥磊; 巴晓甫; 费少华; 方强

    2015-01-01

    In order to solve the problem that perpendicularity and parallelism error of three‐axis localizers cause posture alignment error and internal force of aircraft components ,the paper introduces a hybrid force position control system for posture alignment platform of large aircraft components . Error model of posture alignment was established to explain the problem .Then the strategy to select axes under position control and axes under force control was proposed based on condition number of mechanism’s Jacobian matrix .Static error calculation indicates that hybrid control strategy may improve posture accuracy and reduce internal force significantly under the given posture alignment condition w hen 0 .05 mm/m perpendicularity error exists on each localizer and the maximum parallelism error was 0 .1 mm/m and the averaged parallelism error was 0 .07 mm/m between localizers .The experiment indicates that the torque controller follows the desire torque signal properly with disturbing position signal and the dynamic torque error is below 0 .03 N · m ,w hich is applicable on real posture alignment platform .%为了解决调姿平台中,由于三坐标定位器自身各轴垂直度和相互各轴平行度误差引起的调姿误差以及对飞机大部件造成内力的问题,提出一种飞机大部件调姿平台的力/位置混合控制方法.通过建立调姿误差模型,分析三坐标定位器自身垂直度和相互平行度误差对姿态控制以及部件内力的影响;根据机构雅可比矩阵条件数,提出调姿平台力控制轴和位置控制轴分配策略;通过静态误差计算得到,在三坐标定位器垂直度误差为0.05 m m/m ,同向轴两两之间最大平行度误差为0.1 mm/m且平均平行度误差为0.07 mm/m时,在给定的部件尺寸和调姿轨迹下,力/位置混合控制方法的调姿精度优于全位置控制方法,并且显著降低了调姿部件内力.实验结果表明,力控

  6. Energy Conversion and Storage Requirements for Hybrid Electric Aircraft

    Science.gov (United States)

    Misra, Ajay

    2016-01-01

    Among various options for reducing greenhouse gases in future large commercial aircraft, hybrid electric option holds significant promise. In the hybrid electric aircraft concept, gas turbine engine is used in combination with an energy storage system to drive the fan that propels the aircraft, with gas turbine engine being used for certain segments of the flight cycle and energy storage system being used for other segments. The paper will provide an overview of various energy conversion and storage options for hybrid electric aircraft. Such options may include fuel cells, batteries, super capacitors, multifunctional structures with energy storage capability, thermoelectric, thermionic or a combination of any of these options. The energy conversion and storage requirements for hybrid electric aircraft will be presented. The role of materials in energy conversion and storage systems for hybrid electric aircraft will be discussed.

  7. Information systems for civil engineering; Sistemas de informacion para ingenieria civil

    Energy Technology Data Exchange (ETDEWEB)

    De Buen R, Pablo R; Alvarado G, Alonso; Alaniz Q, Felipe de J; Guerrero F, Vicente A. [Instituto de Investigaciones Electricas, Cuernavaca, Morelos (Mexico)

    2004-07-01

    Since its beginnings, in the Gerencia de Ingenieria Civil (GIC) of the Instituto de Investigaciones Electricas (IIE) the interest has existed to take advantage of and to promote the advantages that the appropriate use of the computerizing systems in the different tasks of civil engineering in the power sector represent. Either as a part of its infrastructure or at the request of their clients, at the GIC have been developed calculation systems for the analysis and design of special structures such as turbo-generators foundations, poles for transmission and distribution and transmission towers, in addition the information systems for the consultation and the analysis of diverse information, such as the related to the Manuals of Civil Works of the Comision Federal de Electricidad (CFE) or the relative to the existing instruments in the large dams of our country. In this article are briefly described some of the computer systems developed by the GIC in recent years. [Spanish] Desde sus inicios, en la Gerencia de Ingenieria Civil (GIC) del Instituto de Investigaciones Electricas (IIE) ha existido el interes por aprovechar y promover las ventajas que representa el uso adecuado de los sistemas de computo en las diferentes tareas de ingenieria civil en el sector energetico. Ya sea como parte de su infraestructura o a solicitud de sus clientes, en la GIC se han desarrollado sistemas de calculo para el analisis y diseno de estructuras especiales como lo son las cimentaciones de turbogeneradores, los postes para transmision y distribucion y las torres de transmision, ademas de sistemas de informacion para la consulta y el analisis de informacion diversa, como es la relacionada con los manuales de obras civiles de la Comision Federal de Electricidad (CFE) o a la relativa a los instrumentos existentes en las grandes presas de nuestro pais. En este articulo se describen brevemente algunos de los sistemas de computo desarrollos por la GIC en anos recientes.

  8. Inertial Force Coupling to Nonlinear Aeroelasticity of Flexible Wing Aircraft

    Science.gov (United States)

    Nguyen, Nhan T.; Ting, Eric

    2016-01-01

    This paper investigates the inertial force effect on nonlinear aeroelasticity of flexible wing aircraft. The geometric are nonlinearity due to rotational and tension stiffening. The effect of large bending deflection will also be investigated. Flutter analysis will be conducted for a truss-braced wing aircraft concept with tension stiffening and inertial force coupling.

  9. Tropospheric sampling with aircraft

    Energy Technology Data Exchange (ETDEWEB)

    Daum, P.H.; Springston, S.R.

    1991-03-01

    Aircraft constitute a unique environment which places stringent requirements on the instruments used to measure the concentrations of atmospheric trace gases and aerosols. Some of these requirements such as minimization of size, weight, and power consumption are general; others are specific to individual techniques. This review presents the basic principles and considerations governing the deployment of trace gas and aerosol instrumentation on an aircraft. An overview of common instruments illustrates these points and provides guidelines for designing and using instruments on aircraft-based measurement programs.

  10. SOLAR AIRCRAFT DESIGN

    OpenAIRE

    RAHMATI, Sadegh; GHASED, Amir

    2015-01-01

    Abstract. Generally domain Aircraft uses conventional fuel. These fuel having limited life, high cost and pollutant. Also nowadays price of petrol and other fuels are going to be higher, because of scarcity of those fuels. So there is great demand of use of non-exhaustible unlimited source of energy like solar energy. Solar aircraft is one of the ways to utilize solar energy. Solar aircraft uses solar panel to collect the solar radiation for immediate use but it also store the remaining part ...

  11. Lightning hazards to aircraft

    Science.gov (United States)

    Corn, P. B.

    1978-01-01

    Lightning hazards and, more generally, aircraft static electricity are discussed by a representative for the Air Force Flight Dynamics Laboratory. An overview of these atmospheric electricity hazards to aircraft and their systems is presented with emphasis on electrical and electronic subsystems. The discussion includes reviewing some of the characteristics of lightning and static electrification, trends in weather and lightning-related mishaps, some specific threat mechanisms and susceptible aircraft subsystems and some of the present technology gaps. A roadmap (flow chart) is presented to show the direction needed to address these problems.

  12. Quiet propulsive-lift technology ready for civil and military applications

    Science.gov (United States)

    Cochrane, J. A.; Queen, S. J.

    1981-01-01

    The Quiet Short-Haul Research Aircraft (QSRA) was designed as research aircraft for investigating terminal-area operations with an advanced propulsive-lift aircraft. The QSRA is a modified De Havilland C-8 Buffalo. The modification to the C-8 consisted of adding a new swept wing with four top-mounted Lycoming YF-102 turbofan engines to provide high levels of propulsive-lift through upper-surface blowing. The state of the art has reached the point where consideration can be given to various applications, including military transport aircraft, civil transports, and business jets. Attention is also given to a ground attack plane with QSRA, the payload advantage resulting from applying propulsive-life technology, and aspects of takeoff performance

  13. Modelling exhaust plume mixing in the near field of an aircraft

    Directory of Open Access Journals (Sweden)

    F. Garnier

    Full Text Available A simplified approach has been applied to analyse the mixing and entrainment processes of the engine exhaust through their interaction with the vortex wake of an aircraft. Our investigation is focused on the near field, extending from the exit nozzle until about 30 s after the wake is generated, in the vortex phase. This study was performed by using an integral model and a numerical simulation for two large civil aircraft: a two-engine Airbus 330 and a four-engine Boeing 747. The influence of the wing-tip vortices on the dilution ratio (defined as a tracer concentration shown. The mixing process is also affected by the buoyancy effect, but only after the jet regime, when the trapping in the vortex core has occurred. In the early wake, the engine jet location (i.e. inboard or outboard engine jet has an important influence on the mixing rate. The plume streamlines inside the vortices are subject to distortion and stretching, and the role of the descent of the vortices on the maximum tracer concentration is discussed. Qualitative comparison with contrail photograph shows similar features. Finally, tracer concentration of inboard engine centreline of B-747 are compared with other theoretical analyses and measured data.

  14. Civil Code, 11 December 1987.

    Science.gov (United States)

    1988-01-01

    Article 162 of this Mexican Code provides, among other things, that "Every person has the right freely, responsibly, and in an informed fashion to determine the number and spacing of his or her children." When a marriage is involved, this right is to be observed by the spouses "in agreement with each other." The civil codes of the following states contain the same provisions: 1) Baja California (Art. 159 of the Civil Code of 28 April 1972 as revised in Decree No. 167 of 31 January 1974); 2) Morelos (Art. 255 of the Civil Code of 26 September 1949 as revised in Decree No. 135 of 29 December 1981); 3) Queretaro (Art. 162 of the Civil Code of 29 December 1950 as revised in the Act of 9 January 1981); 4) San Luis Potosi (Art. 147 of the Civil Code of 24 March 1946 as revised in 13 June 1978); Sinaloa (Art. 162 of the Civil Code of 18 June 1940 as revised in Decree No. 28 of 14 October 1975); 5) Tamaulipas (Art. 146 of the Civil Code of 21 November 1960 as revised in Decree No. 20 of 30 April 1975); 6) Veracruz-Llave (Art. 98 of the Civil Code of 1 September 1932 as revised in the Act of 30 December 1975); and 7) Zacatecas (Art. 253 of the Civil Code of 9 February 1965 as revised in Decree No. 104 of 13 August 1975). The Civil Codes of Puebla and Tlaxcala provide for this right only in the context of marriage with the spouses in agreement. See Art. 317 of the Civil Code of Puebla of 15 April 1985 and Article 52 of the Civil Code of Tlaxcala of 31 August 1976 as revised in Decree No. 23 of 2 April 1984. The Family Code of Hidalgo requires as a formality of marriage a certification that the spouses are aware of methods of controlling fertility, responsible parenthood, and family planning. In addition, Article 22 the Civil Code of the Federal District provides that the legal capacity of natural persons is acquired at birth and lost at death; however, from the moment of conception the individual comes under the protection of the law, which is valid with respect to the

  15. Characterization of emissions from commercial aircraft engines during the Aircraft Particle Emissions eXperiment (APEX) 1 to 3

    Science.gov (United States)

    The fine particulate matter emissions from aircraft operations at large airports located in areas of the U. S. designated as non-attainment for the National Ambient Air Quality Standard for PM-2.5 are of major environmental concern. PM emissions data for commercial aircraft engin...

  16. Institutions of Civil Society Participating in Public Relations

    Directory of Open Access Journals (Sweden)

    Olga S. Belokrylova

    2016-12-01

    Full Text Available The degree of maturity of the civil society of a country is now seen as an important indicator of the development of a socially oriented market economy. The authors explore two forms of state and civil society relations - qualitative, characterized by the diffusion of a relationship of trust in society, and quantitative, in the system of public procurement corruption identifiable pace of localization. Institutional capacity development of civil society in public relations is the simultaneous modernization of the qualitative and quantitative scope of its relationship with the state. The paper presents the mechanism of transition to a partnership model relations between the state and civil society, the most important form of which is the realization of public control, rapid formal institutionalization which has provided detection and elimination of large-scale irregularities in public procurement. Its swift formal institutionalization provided by representatives of civil society to identify and eliminate large-scale irregularities in public procurement. The experience of NGO Fund "Sodeistvie - XXI vek" to identify "blind" purchases, is offered as a tool to improve the efficiency of public control conduct free training of potential public controlles by institutions engaged in training of civil officials for the course "Management of state and municipal procurement".

  17. Essentials of aircraft armaments

    CERN Document Server

    Kaushik, Mrinal

    2017-01-01

    This book aims to provide a complete exposure about armaments from their design to launch from the combat aircraft. The book details modern ammunition and their tactical roles in warfare. The proposed book discusses aerodynamics, propulsion, structural as well as navigation, control, and guidance of aircraft armament. It also introduces the various types of ammunition developed by different countries and their changing trends. The book imparts knowledge in the field of design, and development of aircraft armaments to aerospace engineers and covers the role of the United Nations in peacekeeping and disarmament. The book will be very useful to researchers, students, and professionals working in design and manufacturing of aircraft armaments. The book will also serve air force and naval aspirants, and those interested in working on defence research and developments organizations. .

  18. Aircraft Fire Protection Laboratory

    Data.gov (United States)

    Federal Laboratory Consortium — The Navy Aircraft Protection Laboratory provides complete test support for all Navy air vehicle fire protection systems. The facility allows for the simulation of a...

  19. Aircraft Fire Protection Laboratory

    Data.gov (United States)

    Federal Laboratory Consortium — The Navy Aircraft Protection Laboratory provides complete test support for all Navy air vehicle fire protection systems.The facility allows for the simulation of a...

  20. Solar thermal aircraft

    Science.gov (United States)

    Bennett, Charles L.

    2007-09-18

    A solar thermal powered aircraft powered by heat energy from the sun. A heat engine, such as a Stirling engine, is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller. The heat engine has a thermal battery in thermal contact with it so that heat is supplied from the thermal battery. A solar concentrator, such as reflective parabolic trough, is movably connected to an optically transparent section of the aircraft body for receiving and concentrating solar energy from within the aircraft. Concentrated solar energy is collected by a heat collection and transport conduit, and heat transported to the thermal battery. A solar tracker includes a heliostat for determining optimal alignment with the sun, and a drive motor actuating the solar concentrator into optimal alignment with the sun based on a determination by the heliostat.

  1. Aircraft electromagnetic compatibility

    Science.gov (United States)

    Clarke, Clifton A.; Larsen, William E.

    1987-06-01

    Illustrated are aircraft architecture, electromagnetic interference environments, electromagnetic compatibility protection techniques, program specifications, tasks, and verification and validation procedures. The environment of 400 Hz power, electrical transients, and radio frequency fields are portrayed and related to thresholds of avionics electronics. Five layers of protection for avionics are defined. Recognition is given to some present day electromagnetic compatibility weaknesses and issues which serve to reemphasize the importance of EMC verification of equipment and parts, and their ultimate EMC validation on the aircraft. Proven standards of grounding, bonding, shielding, wiring, and packaging are laid out to help provide a foundation for a comprehensive approach to successful future aircraft design and an understanding of cost effective EMC in an aircraft setting.

  2. Depreciation of aircraft

    Science.gov (United States)

    Warner, Edward P

    1922-01-01

    There is a widespread, and quite erroneous, impression to the effect that aircraft are essentially fragile and deteriorate with great rapidity when in service, so that the depreciation charges to be allowed on commercial or private operation are necessarily high.

  3. CID Aircraft slap-down

    Science.gov (United States)

    1984-01-01

    , 1984, more than four years of effort passed trying to set-up final impact conditions considered survivable by the FAA. During those years while 14 flights with crews were flown the following major efforts were underway: NASA Dryden developed the remote piloting techniques necessary for the B-720 to fly as a drone aircraft; General Electric installed and tested four degraders (one on each engine); and the FAA refined AMK (blending, testing, and fueling a full-size aircraft). The 15 flights had 15 takeoffs, 14 landings and a larger number of approaches to about 150 feet above the prepared crash site under remote control. These flight were used to introduce AMK one step at a time into some of the fuel tanks and engines while monitoring the performance of the engines. On the final flight (No. 15) with no crew, all fuel tanks were filled with a total of 76,000 pounds of AMK and the remotely-piloted aircraft landed on Rogers Dry Lakebed in an area prepared with posts to test the effectiveness of the AMK in a controlled impact. The CID, which some wags called the Crash in the Desert, was spectacular with a large fireball enveloping and burning the B-720 aircraft. From the standpoint of AMK the test was a major set-back, but for NASA Langley, the data collected on crashworthiness was deemed successful and just as important.

  4. CID Aircraft slap-down

    Science.gov (United States)

    1984-01-01

    , 1984, more than four years of effort passed trying to set-up final impact conditions considered survivable by the FAA. During those years while 14 flights with crews were flown the following major efforts were underway: NASA Dryden developed the remote piloting techniques necessary for the B-720 to fly as a drone aircraft; General Electric installed and tested four degraders (one on each engine); and the FAA refined AMK (blending, testing, and fueling a full-size aircraft). The 15 flights had 15 takeoffs, 14 landings and a larger number of approaches to about 150 feet above the prepared crash site under remote control. These flight were used to introduce AMK one step at a time into some of the fuel tanks and engines while monitoring the performance of the engines. On the final flight (No. 15) with no crew, all fuel tanks were filled with a total of 76,000 pounds of AMK and the remotely-piloted aircraft landed on Rogers Dry Lakebed in an area prepared with posts to test the effectiveness of the AMK in a controlled impact. The CID, which some wags called the Crash in the Desert, was spectacular with a large fireball enveloping and burning the B-720 aircraft. From the standpoint of AMK the test was a major set-back, but for NASA Langley, the data collected on crashworthiness was deemed successful and just as important.

  5. Operation of the aircraft as a discipline of knowledge after 100 years of experience

    Directory of Open Access Journals (Sweden)

    Stanisław Danilecki

    2015-12-01

    Full Text Available The paper presents the course of the most important stages of development of the discipline related to the maintenance of aircrafts, as a synthesis of the 100-year experience. It is presented linking of technical maintenance of the aircraft with other disciplines of knowledge. The scope of technical maintenance was defined. The division and analysis of the methods for the maintenance was made. There were defined and discussed definitions used in the theory of maintenance, in conjunction with the construction of the aircraft and the tasks arising for constructor-manufacturer. MSG subsequent versions of the document constituting the logistical procedures for determining the programmable handling of civil airplanes were discussed.[b]Keywords[/b]: aviation, aircraft, maintenance aircrafts

  6. How persistent is civilization growth?

    CERN Document Server

    Garrett, Timothy J

    2011-01-01

    In a recent study (Garrett, 2011), I described theoretical arguments and empirical evidence showing how civilization evolution might be considered from a purely physical basis. One implication is that civilization exhibits the property of persistence in its growth. Here, this argument is elaborated further, and specific near-term forecasts are provided for key economic variables and anthropogenic CO2 emission rates at global scales. Absent some external shock, civilization wealth, energy consumption and carbon dioxide emissions will continue to grow exponentially at an average rate of about 2.3% per year.

  7. Global Standards of Market Civilization

    DEFF Research Database (Denmark)

    Fund's capacity to formulate a global standard of civilization in its reform programs; and problems in the development of the global trade, including the issue of intellectual property rights. This book will be of strong interest to students and scholars in wide range of fields relating to the study......Global Standards of Market Civilization brings together leading scholars, representing a range of political views, to investigate how global 'standards of market civilization' have emerged, their justification, and their political, economic and social impact. Key chapters show how as the modern...

  8. Precautionay Seizure of Civil Ship

    Directory of Open Access Journals (Sweden)

    Ciprian Alexandrescu

    2011-05-01

    Full Text Available Noting that many pending cases in the maritime and river sections of the courts concern the seizureof commercial ships, we intend to study in detail this institution of maritime law. This approach is due to thefact that the few Romanian law-writers, and especially the practitioners, who have approached the subject,have referred in particular to comment and interpretation of existing rules in the Commercial Code and theCivil Procedure Code, not considering the relationship between other institutions of maritime law and seizingthe ship. In our opinion the mentioned institution of law can not be examined thoroughly without priorinvestigation of what is the ship which is subject to seizure. Moreover, the ship is at the heart of all legalresearch on shipping. The concept of ship has been controversial since the seventeenth century, with the firstregulations that led to the development and adoption of commercial codes, and it is still controversial today.We can say that the diversity of opinions, expressed both in the legal literature and legal practice, on theconcept of ship, is largely due to the technical progress of shipping in modern times, this transport meanbenefiting from exceptional facilities to ensure a safely water transport of goods and people.

  9. Automatic aircraft recognition

    Science.gov (United States)

    Hmam, Hatem; Kim, Jijoong

    2002-08-01

    Automatic aircraft recognition is very complex because of clutter, shadows, clouds, self-occlusion and degraded imaging conditions. This paper presents an aircraft recognition system, which assumes from the start that the image is possibly degraded, and implements a number of strategies to overcome edge fragmentation and distortion. The current vision system employs a bottom up approach, where recognition begins by locating image primitives (e.g., lines and corners), which are then combined in an incremental fashion into larger sets of line groupings using knowledge about aircraft, as viewed from a generic viewpoint. Knowledge about aircraft is represented in the form of whole/part shape description and the connectedness property, and is embedded in production rules, which primarily aim at finding instances of the aircraft parts in the image and checking the connectedness property between the parts. Once a match is found, a confidence score is assigned and as evidence in support of an aircraft interpretation is accumulated, the score is increased proportionally. Finally a selection of the resulting image interpretations with the highest scores, is subjected to competition tests, and only non-ambiguous interpretations are allowed to survive. Experimental results demonstrating the effectiveness of the current recognition system are given.

  10. Civil Defense, U. S. A.: A Programmed Orientation to Civil Defense. Unit 5. Governmental Responsibilities for Civil Defense.

    Science.gov (United States)

    Defense Civil Preparedness Agency (DOD), Battle Creek, MI.

    A description of the laws and orders that provide necessary legal authorization for civil defense activities is provided. In addition, an outline of the responsibilities of all governments and the role of the private sector in civil defense is presented. Topics discussed include: (1) Legal authority for civil defense, (2) Civil defense…

  11. Credit and civilization.

    Science.gov (United States)

    Newton, Tim

    2003-09-01

    This paper analyses financial credit in order to re-examine the work of Norbert Elias, particularly his association of interdependency complexity with social discipline, and his approach to contradiction. Following a discussion of these issues, the paper examines Elias's writing on money and explores the emergence of financial credit networks in early modern England. Attention is paid to credit networks and social discipline, to credit and the state, and to the contradictory images associated with the transition to modern cash economies. From one perspective, early modern credit networks might be read as a confirmation of Elias, particularly his argument that interdependency complexity, changing power balances and self-restraint are interwoven. Yet the development of modern cash money raises questions, not just in relation to Elias's treatment of money, but also with regard to his assumptions about social discipline and his approach to ambivalence and contradiction. Drawing on the foregoing discussion, the paper argues that the relation between interdependency complexity and social discipline is contingent and variable, and that interdependency complexity may simultaneously encourage contradictory processes, such as those of civilizing and barbarity.

  12. Sensitivity of two-dimensional model predictions of ozone response to stratospheric aircraft: An update

    Energy Technology Data Exchange (ETDEWEB)

    Considine, D.B.; Douglass, A.R.; Jackman, C.H. [Applied Research Corp., Landover, MD (United States)]|[NASA, Goddard Space Flight Center, Greenbelt, MD (United States)

    1995-02-01

    The Goddard Space Flight Center (GSFC) two-dimensional model of stratospheric photochemistry and dynamics has been used to calculate the O3 response to stratospheric aircraft (high-speed civil transport (HSCT)) emissions. The sensitivity of the model O3 response was examined for systematic variations of five parameters and two reaction rates over a wide range, expanding on calculations by various modeling groups for the NASA High Speed Research Program and the World Meteorological Organization. In all, 448 model runs were required to test the effects of variations in the latitude, altitude, and magnetitude of the aircraft emissions perturbation, the background chlorine levels, the background sulfate aerosol surface area densities, and the rates of two key reactions. No deviation from previous conclusions concerning the response of O3 to HSCTs was found in this more exhaustive exploration of parameter space. Maximum O3 depletions occur for high-altitude, low altitude HSCT perturbations. Small increases in global total O3 can occur for low-altitude, high-altitude injections. Decreasing aerosol surface area densities and background chlorine levels increases the sensitivity of model O3 to the HSCT perturbations. The location of the aircraft emissions is the most important determinant of the model response. Response to the location of the HSCT emissions is not changed qualitatively by changes in background chlorine and aerosol loading. The response is also not very sensitive to changes in the rates of the reactions NO + HO2 yields NO2 + OH and HO2 + O3 yields OH + 2O2 over the limits of their respective uncertainties. Finally, levels of lower stratospheric HO(sub x) generally decrease when the HSCT perturbation is included, even though there are large increases in H2O due to the perturbation.

  13. Aircraft noise in the region of the Bucharest-Otopeni Airport. [noise pollution in airport environment

    Science.gov (United States)

    Costescu, M.; Gherghel, C.; Curtoglu, A.

    1974-01-01

    Aircraft noise, especially in the region adjoining airports, constitutes a problem that will be aggravated in the near future because of increasing aircraft traffic and the appearance of new types of large tonnage aircraft with continuously increasing powers and speeds. Criteria for the evaluation of aircraft noise are reported and some results of studies carried out in the region of Bucharest-Otopeni Airport are detailed.

  14. Teaching Mathematics to Civil Engineers

    Science.gov (United States)

    Sharp, J. J.; Moore, E.

    1977-01-01

    This paper outlines a technique for teaching a rigorous course in calculus and differential equations which stresses applicability of the mathematics to problems in civil engineering. The method involves integration of subject matter and team teaching. (SD)

  15. Preliminary design of a high speed civil transport: The Opus 0-001

    Science.gov (United States)

    1992-01-01

    Based on research into the technology and issues surrounding the design, development, and operation of a second generation High Speed Civil Transport, HSCT, the Opus 0-001 team completed the preliminary design of a sixty passenger, three engine aircraft. The design of this aircraft was performed using a computer program which the team wrote. This program automatically computed the geometric, aerodynamic, and performance characteristic of an aircraft whose preliminary geometry was specified. The Opus 0-001 aircraft was designed for a cruise Mach number of 2.2, a range of 4,700 nautical miles and its design was based in current or very near term technology. Its small size was a consequence of an emphasis on a profitable, low cost program, capable of delivering tomorrow's passengers in style and comfort at prices that make it an attractive competitor to both current and future subsonic transport aircraft. Several hundred thousand cases of Cruise Mach number, aircraft size and cost breakdown were investigated to obtain costs and revenues for which profit was calculated. The projected unit flyaway cost was $92.0 million per aircraft.

  16. Proposed Rule and Related Materials for Proposed Finding That Greenhouse Gas Emissions From Aircraft Cause or Contribute to Air Pollution That May Reasonably Be Anticipated To Endanger Public Health and Welfare and Advance Notice of Proposed Rulemaking

    Science.gov (United States)

    FR notice and fact sheet concerning Advance Notice of Proposed Rulemaking that provides information on the process for setting an international CO2 emissions standard for aircraft at the International Civil Aviation Organization (ICAO)

  17. 5 CFR 919.920 - Civil judgment.

    Science.gov (United States)

    2010-01-01

    ... 5 Administrative Personnel 2 2010-01-01 2010-01-01 false Civil judgment. 919.920 Section 919.920 Administrative Personnel OFFICE OF PERSONNEL MANAGEMENT (CONTINUED) CIVIL SERVICE REGULATIONS (CONTINUED) GOVERNMENTWIDE DEBARMENT AND SUSPENSION (NONPROCUREMENT) Definitions § 919.920 Civil judgment. Civil judgment...

  18. Communication Needs of Thai Civil Engineering Students

    Science.gov (United States)

    Kaewpet, Chamnong

    2009-01-01

    This article reports on an examination of the communication needs of a group of Thai civil engineering students. Twenty-five stakeholders helped identify the communication needs of the students by participating in individual interviews. These included employers, civil engineers, civil engineering lecturers, ex-civil engineering students of the…

  19. High-Speed Propeller for Aircraft

    Science.gov (United States)

    Sagerser, D. A.; Gatzen, B. S.

    1986-01-01

    Engine efficiency increased. Propeller blades required to be quite thin and highly swept to minimize compressibility losses and propeller noise during high-speed cruise. Use of 8 or 10 blades with highpropeller-power loading allows overall propeller diameter to be kept relatively small. Area-ruled spinner and integrated nacelle shape reduce compressibility losses in propeller hub region. Finally, large modern turboshaft engine and gearbox provide power to advanced propeller. Fuel savings of 30 to 50 percent over present systems anticipated. Propfan system adaptable to number of applications, such as highspeed (subsonic) business and general-aviation aircraft, and military aircraft including V/STOL.

  20. Frequency-domain identification of aircraft structural modes from short-duration flight tests

    Science.gov (United States)

    Vayssettes, J.; Mercère, G.; Vacher, P.; De Callafon, R. A.

    2014-07-01

    This article presents identification algorithms dedicated to the modal analysis of civil aircraft structures during in-flight flutter tests. This particular operational framework implies several specifications for the identification procedure. To comply with these requirements, the identification problem is formulated in the frequency domain as an output-error problem. Iterative identification methods based on structured matrix fraction descriptions are used to solve this problem and to identify a continuous-time model. These iterative methods are specifically designed to deal with experiments where short-duration tests with multiple-input excitations are used. These algorithms are first discussed and then evaluated through a simulation example illustrative of the in-flight modal analysis of a civil aircraft. Based on these evaluation results, an efficient iterative algorithm is suggested and applied to real flight-test data measured on board a military aircraft.

  1. Space civil engineering - A new discipline

    Science.gov (United States)

    Sadeh, Willy Z.; Criswell, Marvin E.

    1991-01-01

    Space Civil Engineering is an emerging engineering discipline that focuses on extending and expanding the Civil Engineering know-how and practice to the development and maintenance of infrastructure on celestial bodies. Space Civil Engineering is presently being developed as a new discipline within the Department of Civil Engineering at Colorado State University under a recently established NASA Space Grant College Program. Academic programs geared toward creating Space Civil Engineering Options at both undergraduate and graduate levels are being formulated. Basic ideas and concepts of the curriculum in the Space Civil Engineering Option at both undergraduate and graduate levels are presented. The role of Space Civil Engineering in the Space Program is discussed.

  2. Ciencia y sociedad civil

    Directory of Open Access Journals (Sweden)

    Ziman, John

    2003-06-01

    Full Text Available This paper analyses the relationship between scientific knowledge and the societies in which it is produced. After considering the diverse societal roles science has performed in different types of society, the discussion focuses on science’s role in democratic and pluralistic societies. Opposite to the increasing instrumental role knowledge production plays nowadays, for which it has been named «post-academic science» or «technoscience», non instrumental roles of traditional academic research are defended. It is argued that only if academic science keeps its autonomy and integrity from political and corporate interests, it may serve civil society by offering impartial and trustworthy knowledge to balance biases produced by the features of post-academic science.

    En este artículo se analizan las relaciones del conocimiento científico con las sociedades en las que se produce. Tras repasar sus diversas funciones en tipos distintos de sociedades, la discusión se centra en los fines de la ciencia en las sociedades democráticas pluralistas. Frente al cada vez mayor rol instrumental de la ciencia, por el que ha recibido los nombres de «ciencia postacadémica» o «tecnociencia», se defienden los roles no instrumentales tradicionales de la investigación académica clásica. Se argumenta que sólo si la ciencia académica mantiene su autonomía y su integridad frente a intereses políticos o empresariales podrá ser de utilidad al público al ofrecerle conocimiento imparcial y fidedigno frente a los sesgos producidos por la naturaleza propia de la ciencia postacadémica.

  3. Temperature Distribution in a Long-Span Aircraft Hangar

    Institute of Scientific and Technical Information of China (English)

    PEI Yongzhong; BAI Yin; SHI Yongjiu; ZHU Dan; WANG Yuanqing

    2008-01-01

    Long-span aircraft hangars have features which differ from other large structural systems. The temperature stresses due to temperature variations often greatly impact the mechanical performance of the structure. The paper presents an analysis of the heat transfer processes and factors which influence the temperature distribution. The AMECO-A380 aircraft hangar at the Beijing Capital International Airport was selected as a practical example to illustrate the use of finite volume analysis to calculate the temperature field taking into account meteorological conditions, solar radiation, heat convection, etc. The temperature distribution and the variation of the length of the upper and lower chords of the grid structure roof were ana-lyzed to develop guidelines for the temperature distributions in very large aircraft hangars. The results show that the temperature effect will be large for long-span hangars, and the temperature stresses due to non-uniform temperatures should be analyzed to guarantee the structural safety of large aircraft hangars.

  4. Globular Clusters as Cradles of Life and Advanced Civilizations

    Science.gov (United States)

    Di Stefano, R.; Ray, A.

    2016-08-01

    Globular clusters are ancient stellar populations in compact dense ellipsoids. There is no star formation and there are no core-collapse supernovae, but several lines of evidence suggest that globular clusters are rich in planets. If so, and if advanced civilizations can develop there, then the distances between these civilizations and other stars would be far smaller than typical distances between stars in the Galactic disk, facilitating interstellar communication and travel. The potent combination of long-term stability and high stellar densities provides a globular cluster opportunity. Yet the very proximity that promotes interstellar travel also brings danger, as stellar interactions can destroy planetary systems. We find, however, that large portions of many globular clusters are “sweet spots,” where habitable-zone planetary orbits are stable for long times. Globular clusters in our own and other galaxies are, therefore, among the best targets for searches for extraterrestrial intelligence (SETI). We use the Drake equation to compare the likelihood of advanced civilizations in globular clusters to that in the Galactic disk. We also consider free-floating planets, since wide-orbit planets can be ejected to travel through the cluster. Civilizations spawned in globular clusters may be able to establish self-sustaining outposts, reducing the probability that a single catastrophic event will destroy the civilization. Although individual civilizations may follow different evolutionary paths, or even be destroyed, the cluster may continue to host advanced civilizations once a small number have jumped across interstellar space. Civilizations residing in globular clusters could therefore, in a sense, be immortal.

  5. Dynamics and control of morphing aircraft

    Science.gov (United States)

    Seigler, Thomas Michael

    The following work is directed towards an evaluation of aircraft that undergo structural shape change for the purpose of optimized flight and maneuvering control authority. Dynamical equations are derived for a morphing aircraft based on two primary representations; a general non-rigid model and a multi-rigid-body. A simplified model is then proposed by considering the altering structural portions to be composed of a small number of mass particles. The equations are then extended to consider atmospheric flight representations where the longitudinal and lateral equations are derived. Two aspects of morphing control are considered. The first is a regulation problem in which it is desired to maintain stability in the presence of large changes in both aerodynamic and inertial properties. From a baseline aircraft model various wing planform designs were constructed using Datcom to determine the required aerodynamic contributions. Based on nonlinear numerical evaluations adequate stabilization control was demonstrated using a robust linear control design. In maneuvering, divergent characteristics were observed at high structural transition rates. The second aspect considered is the use of structural changes for improved flight performance. A variable span aircraft is then considered in which asymmetric wing extension is used to effect the rolling moment. An evaluation of the variable span aircraft is performed in the context of bank-to-turn guidance in which an input-output control law is implemented.

  6. Longitudinal dynamics of a perching aircraft concept

    Science.gov (United States)

    Wickenheiser, Adam; Garcia, Ephrahim; Waszak, Martin

    2005-05-01

    This paper introduces a morphing aircraft concept whose purpose is to demonstrate a new bio-inspired flight capability: perching. Perching is a maneuver that utilizes primarily aerodynamics -- as opposed to thrust generation -- to achieve a vertical or short landing. The flight vehicle that will accomplish this is described herein with particular emphasis on its addition levels of actuation beyond the traditional aircraft control surfaces. A computer model of the aircraft is developed in order to predict the changes in applied aerodynamic loads as it morphs and transitions through different flight regimes. The analysis of this model is outlined, including a lifting-line-based analytical technique and a trim and stability analysis. These analytical methods -- compared to panel or computational fluid dynamics (CFD) methods -- are considered desirable for the analysis of a large number of vehicle configurations and flight conditions. The longitudinal dynamics of this aircraft are studied, and several interesting results are presented. Of special interest are the changes in vehicle dynamics as the aircraft morphs from a cruise configuration to initiate the perching maneuver. Changes in trim conditions and stability are examined as functions of vehicle geometry. The time response to changes in vehicle configuration is also presented.

  7. Aircraft Operations Classification System

    Science.gov (United States)

    Harlow, Charles; Zhu, Weihong

    2001-01-01

    Accurate data is important in the aviation planning process. In this project we consider systems for measuring aircraft activity at airports. This would include determining the type of aircraft such as jet, helicopter, single engine, and multiengine propeller. Some of the issues involved in deploying technologies for monitoring aircraft operations are cost, reliability, and accuracy. In addition, the system must be field portable and acceptable at airports. A comparison of technologies was conducted and it was decided that an aircraft monitoring system should be based upon acoustic technology. A multimedia relational database was established for the study. The information contained in the database consists of airport information, runway information, acoustic records, photographic records, a description of the event (takeoff, landing), aircraft type, and environmental information. We extracted features from the time signal and the frequency content of the signal. A multi-layer feed-forward neural network was chosen as the classifier. Training and testing results were obtained. We were able to obtain classification results of over 90 percent for training and testing for takeoff events.

  8. Identification of Aircraft Hazards

    Energy Technology Data Exchange (ETDEWEB)

    K. Ashley

    2006-12-08

    Aircraft hazards were determined to be potentially applicable to a repository at Yucca Mountain in ''Monitored Geological Repository External Events Hazards Screening Analysis'' (BSC 2005 [DIRS 174235], Section 6.4.1). That determination was conservatively based upon limited knowledge of flight data in the area of concern and upon crash data for aircraft of the type flying near Yucca Mountain. The purpose of this report is to identify specific aircraft hazards that may be applicable to a monitored geologic repository (MGR) at Yucca Mountain, using NUREG-0800, ''Standard Review Plan for the Review of Safety Analysis Reports for Nuclear Power Plants'' (NRC 1987 [DIRS 103124], Section 3.5.1.6), as guidance for the inclusion or exclusion of identified aircraft hazards. The intended use of this report is to provide inputs for further screening and analysis of identified aircraft hazards based upon the criteria that apply to Category 1 and Category 2 event sequence analyses as defined in 10 CFR 63.2 [DIRS 176544] (Section 4). The scope of this report includes the evaluation of military, private, and commercial use of airspace in the 100-mile regional setting of the repository at Yucca Mountain with the potential for reducing the regional setting to a more manageable size after consideration of applicable screening criteria (Section 7).

  9. IDENTIFICATION OF AIRCRAFT HAZARDS

    Energy Technology Data Exchange (ETDEWEB)

    K.L. Ashley

    2005-03-23

    Aircraft hazards were determined to be potentially applicable to a repository at Yucca Mountain in the ''Monitored Geological Repository External Events Hazards Screening Analysis'' (BSC 2004, Section 6.4.1). That determination was conservatively based on limited knowledge of flight data in the area of concern and on crash data for aircraft of the type flying near Yucca Mountain. The purpose of this report is to identify specific aircraft hazards that may be applicable to a Monitored Geologic Repository (MGR) at Yucca Mountain using NUREG-0800, ''Standard Review Plan for the Review of Safety Analysis Reports for Nuclear Power Plants'' (NRC 1987, Section 3.5.1.6), as guidance for the inclusion or exclusion of identified aircraft hazards. NUREG-0800 is being used here as a reference because some of the same considerations apply. The intended use of this report is to provide inputs for further screening and analysis of the identified aircraft hazards based on the criteria that apply to Category 1 and 2 event sequence analyses as defined in 10 CFR 63.2 (see Section 4). The scope of this technical report includes the evaluation of military, private, and commercial use of airspace in the 100-mile regional setting of the MGR at Yucca Mountain with the potential for reducing the regional setting to a more manageable size after consideration of applicable screening criteria (see Section 7).

  10. B-52 Launch Aircraft in Flight

    Science.gov (United States)

    2001-01-01

    the development of parachute recovery systems used to recover the space shuttle solid rocket booster casings. It also supported eight orbiter (space shuttle) drag chute tests in 1990. In addition, the B-52 served as the air launch platform for the first six Pegasus space boosters. During its many years of service, the B-52 has undergone several modifications. The first major modification was made by North American Aviation (now part of Boeing) in support of the X-15 program. This involved creating a launch-panel-operator station for monitoring the status of the test vehicle being carried, cutting a large notch in the right inboard wing flap to accommodate the vertical tail of the X-15 aircraft, and installing a wing pylon that enables the B-52 to carry research vehicles and test articles to be air-launched/dropped. Located on the right wing, between the inboard engine pylon and the fuselage, this wing pylon was subjected to extensive testing prior to its use. For each test vehicle the B-52 carried, minor changes were made to the launch-panel operator's station. Built originally by the Boeing Company, the NASA B-52 is powered by eight Pratt & Whitney J57-19 turbojet engines, each of which produce 12,000 pounds of thrust. The aircraft's normal launch speed has been Mach 0.8 (about 530 miles per hour) and its normal drop altitude has been 40,000 to 45,000 feet. It is 156 feet long and has a wing span of 185 feet.

  11. Near-field commercial aircraft contribution to nitrogen oxides by engine, aircraft type, and airline by individual plume sampling.

    Science.gov (United States)

    Carslaw, David C; Ropkins, Karl; Laxen, Duncan; Moorcroft, Stephen; Marner, Ben; Williams, Martin L

    2008-03-15

    Nitrogen oxides (NOx) concentrations were measured in individual plumes from aircraft departing on the northern runway at Heathrow Airport in west London. Over a period of four weeks 5618 individual plumes were sampled by a chemiluminescence monitor located 180 m from the runway. Results were processed and matched with detailed aircraft movement and aircraft engine data using chromatographic techniques. Peak concentrations associated with 29 commonly used engines were calculated and found to have a good relationship with N0x emissions taken from the International Civil Aviation Organization (ICAO) databank. However, it is found that engines with higher reported NOx emissions result in proportionately lower NOx concentrations than engines with lower emissions. We show that it is likely that aircraft operational factors such as takeoff weight and aircraftthrust setting have a measurable and important effect on concentrations of N0x. For example, NOx concentrations can differ by up to 41% for aircraft using the same airframe and engine type, while those due to the same engine type in different airframes can differ by 28%. These differences are as great as, if not greater than, the reported differences in NOx emissions between different engine manufacturers for engines used on the same airframe.

  12. CERTIFICATION - The final and critical stage of every civil or military aviation program

    Directory of Open Access Journals (Sweden)

    Vasile STEFAN

    2012-06-01

    Full Text Available As a general rule the final step in every aviation program is the certification of the airplane, an important step in which the airplane, the engins and the equipments are checked by an authority or commission according to the airworthiness rules. The main scope of the certification is to promote a safe aviation product and to protect the general public from unnecessary risk. In all the contries the national authorieties require a civil certificability for all the parts or equipments and a full aircraft certification for a new or wholly modified airplane. The military aircrafts must pased and respond to a specific way of certification and many actual efforts are done in order to unify the diffrent national rules in this field. This paper presents the existing situation in the certification of civil and military airplans and the actual measures done for the unification of certification procedures in the world.

  13. Civil Airlines/Air Services in Bangladesh, India and Pakistan. Volumes 1 thru 4.

    Science.gov (United States)

    1985-03-01

    Calcutta-Dacca-Chittagong. The Indian subcontinent was partitioned into India and Pakistan in 1947; Bangladesh formed the eastern wing of Pakistan. Because...aircraft on following occasions: - Evacuation of refugees immediately after the partition of India and Pakistan during which period Indian civil aviation...year earlier to October 1946, when Mohammad Ali Jinnah , the founder of Pakistan, formed the Muslim-owned Orient Airways Limited in Calcutta. The

  14. Advanced Aircraft Material

    Directory of Open Access Journals (Sweden)

    Vivek Kumar Prince

    2013-06-01

    Full Text Available There has been long debate on “advanced aircraft material” from past decades & researchers too came out with lots of new advanced material like composites and different aluminum alloys. Now days a new advancement that is in great talk is third generation Aluminum-lithium alloy. Newest Aluminum-lithium alloys are found out to have low density, higher elastic modulus, greater stiffness, greater cryogenic toughness, high resistance to fatigue cracking and improved corrosion resistance properties over the earlier used aircraft material as mentioned in Table 3 [1-5]. Comparison had been made with nowadays used composite material and is found out to be more superior then that

  15. AIRCRAFT MAINTENANCE HANGAR

    Directory of Open Access Journals (Sweden)

    GEAMBASU Gabriel George

    2017-05-01

    Full Text Available The paper presents the maintenance process that is done on an airplane, at a certain period of time, or after a number of flight hours or cycles and describes the checks performed behind each inspection. The first part of research describes the aircraft maintenance process that has to be done after an updated maintenance manual according with aircraft type, followed by a short introduction about maintenance hangar. The second part of the paper presents a hangar design with a foldable roof and walls, which can be folded or extended, over an airplane when a maintenance process is done, or depending on weather condition.

  16. Aerodynamic Optimization Design for Large Upswept Afterbody of Transport Aircraft Based on FFD Technology%基于FFD技术的大型运输机上翘后体气动优化设计

    Institute of Scientific and Technical Information of China (English)

    王元元; 张彬乾; 郭兆电; 董强

    2013-01-01

    利用非均匀有理B样条(NURBS)基函数属性建立了任意空间的自由变形(FFD)参数化方法,进一步结合无限插值(TFI)变形网格技术、二阶振荡粒子群优化(PSO)算法以及计算流体力学(CFD)数值模拟技术,构建了通用的气动外形优化设计系统.采用该系统对C17运输机上翘后体进行气动优化设计,在满足后体最大宽度、高度以及上翘角不减小的情况下,巡航状态减阻2.6%,压差阻力减小19.8%.流态分析显示,优化后体阻力减小的主要原因是后体截面近圆度的增加以及近圆度沿机身轴线的变化量的减小使得后体周向逆压梯度减小所致.研究结果表明本文建立的基于FFD技术的气动优化设计系统对于大型运输机上翘后体的气动优化设计具有较好的实用性.%A free-form deformation parameterization (FFD) method is established based on non-uniform rational B-spline (NURBS) basis function.Furthermore,by coupling the transfinite interpolation (TFI) grid deformation technology and computational fluid dynamics (CFD) method with improved particle swarm optimization (PSO) arithmetic,a general aerodynamic optimization design system is constructed.Then,the aerodynamic optimization design system is applied to designing a large upswept afterbody of transport aircraft C17 on the restrictions of nondecreasing maximum structure height,width and upswept angle.The optimized afterbody decreases the total drag by 2.6% and pressure drag by 19.8% respectively.A comparison analysis of the aerodynamic shape and flow pattern reveals that the key factors for the optimized afterbody to decrease the pressure drag greatly are the increased near-roundness of the afterbody cross-section and decreased near-roundness change ratio along the fuselage axis.The two factors enable the adverse pressure gradient along the circumferential direction to become smaller,which can suspend aferbody separation and weaken afterbody vortex strength

  17. Minimum Climb to Cruise Noise Trajectories Modeled for the High Speed Civil Transport

    Science.gov (United States)

    Berton, Jeffrey J.

    1998-01-01

    The proposed U.S. High Speed Civil Transport (HSCT) will revolutionize commercial air travel by providing economical supersonic passenger service to destinations worldwide. Unlike the high-bypass turbofan engines that propel today's subsonic airliners, HSCT engines will have much higher jet exhaust speeds. Jet noise, caused by the turbulent mixing of high-speed exhaust with the surrounding air, poses a significant challenge for HSCT engine designers. To resolve this challenge, engineers have designed advanced mixer rejector nozzles that reduce HSCT jet noise to airport noise certification levels by entraining and mixing large quantities of ambient air with the engines' jet streams. Although this works well during the first several minutes of flight, far away from the airport, as the HSCT gains speed and climbs, poor ejector inlet recovery and ejector ram drag contribute to poor thrust, making it advantageous to turn off the ejector. Doing so prematurely, however, can cause unacceptable noise levels to propagate to the ground, even when the aircraft is many miles from the airport. This situation lends itself ideally to optimization, where the aircraft trajectory, throttle setting, and ejector setting can be varied (subject to practical aircraft constraints) to minimize the noise propagated to the ground. A method was developed at the NASA Lewis Research Center that employs a variation of the classic energy state approximation: a trajectory analysis technique historically used to minimize climb time or fuel burned in many aircraft problems. To minimize the noise on the ground at any given throttle setting, high aircraft altitudes are desirable; but the HSCT may either climb quickly to high altitudes using a high, noisy throttle setting or climb more slowly at a lower, quieter throttle setting. An optimizer has been programmed into NASA's existing aircraft and noise analysis codes to balance these options by dynamically choosing the best altitude-velocity path and

  18. Nonlinear Gust Response Analysis of Free Flexible Aircraft

    Directory of Open Access Journals (Sweden)

    Chen Shilu

    2013-01-01

    Full Text Available Gust response analysis plays a very important role in large aircraft design. This paper presents a methodology for calculating the flight dynamic characteristics and gust response of free flexible aircraft. A multidisciplinary coupled numerical tool is developed to simulate detailed aircraft models undergoing arbitrary free flight motion in the time domain, by Computational Fluid Dynamics (CFD, Computational Structure Dynamics (CSD and Computational Flight Mechanics (CFM coupling. To achieve this objective, a structured, time-accurate flow-solver is coupled with a computational module solving the flight mechanics equations of motion and a structural mechanics code determining the structural deformations. A novel method to determine the trim state of flexible aircraft is also stated. First, the field velocity approach is validated, after the trim state is attained, gust responses for the one-minus-cosine gust profile are analyzed for the longitudinal motion of a slender-wing aircraft configuration with and without the consideration of structural deformation.

  19. Propeller aircraft interior noise model utilization study and validation

    Science.gov (United States)

    Pope, L. D.

    1984-01-01

    Utilization and validation of a computer program designed for aircraft interior noise prediction is considered. The program, entitled PAIN (an acronym for Propeller Aircraft Interior Noise), permits (in theory) predictions of sound levels inside propeller driven aircraft arising from sidewall transmission. The objective of the work reported was to determine the practicality of making predictions for various airplanes and the extent of the program's capabilities. The ultimate purpose was to discern the quality of predictions for tonal levels inside an aircraft occurring at the propeller blade passage frequency and its harmonics. The effort involved three tasks: (1) program validation through comparisons of predictions with scale-model test results; (2) development of utilization schemes for large (full scale) fuselages; and (3) validation through comparisons of predictions with measurements taken in flight tests on a turboprop aircraft. Findings should enable future users of the program to efficiently undertake and correctly interpret predictions.

  20. Aircraft Fuel Systems Career Ladder.

    Science.gov (United States)

    1985-09-01

    type fittings remove and install fuel cells clean work areas inspect aircraft for safety pin installation purge tanks or cells using blow purge method...INSPECT AIRCRAFT FOR SAFETY PIN INSTALLATION 84 H254 PURGE TANKS OR CELLS USING BLOW PURGE METHOD 83 H227 CHECK AIRCRAFT FOR LIQUID OXYGEN (LOX...H243 INSPECT AIRCRAFT FOR SAFETY PIN INSTALLATION 52 M483 MIX SEALANTS BY HAND 48 K372 CONNECT OR DISCONNECT WIGGINS TYPE FITTINGS 48 H236 DISCONNECT

  1. The effects of aircraft certification rules on general aviation accidents

    Science.gov (United States)

    Anderson, Carolina Lenz

    The purpose of this study was to analyze the frequency of general aviation airplane accidents and accident rates on the basis of aircraft certification to determine whether or not differences in aircraft certification rules had an influence on accidents. In addition, the narrative cause descriptions contained within the accident reports were analyzed to determine whether there were differences in the qualitative data for the different certification categories. The certification categories examined were: Federal Aviation Regulations Part 23, Civil Air Regulations 3, Light Sport Aircraft, and Experimental-Amateur Built. The accident causes examined were those classified as: Loss of Control, Controlled Flight into Terrain, Engine Failure, and Structural Failure. Airworthiness certification categories represent a wide diversity of government oversight. Part 23 rules have evolved from the initial set of simpler design standards and have progressed into a comprehensive and strict set of rules to address the safety issues of the more complex airplanes within the category. Experimental-Amateur Built airplanes have the least amount of government oversight and are the fastest growing segment. The Light Sport Aircraft category is a more recent certification category that utilizes consensus standards in the approval process. Civil Air Regulations 3 airplanes were designed and manufactured under simpler rules but modifying these airplanes has become lengthy and expensive. The study was conducted using a mixed methods methodology which involves both quantitative and qualitative elements. A Chi-Square test was used for a quantitative analysis of the accident frequency among aircraft certification categories. Accident rate analysis of the accidents among aircraft certification categories involved an ANCOVA test. The qualitative component involved the use of text mining techniques for the analysis of the narrative cause descriptions contained within the accident reports. The Chi

  2. B 150 civil engineering futures

    DEFF Research Database (Denmark)

    theme in twentieth century architecture. Together, civil engineer Peter Rice and architect Ian Ritchie created a paradigm shift with their revolutionary ideas for glass facades supported by cables. Glued and bolted constructions made entirely of glass are now a reality in small-scale projects, yet...... related to sustainability – a Workshop on Traffic. The workshop discussed traffic prognoses and the way they are used in the preparation of urban transport and traffic strategies. Civil engineer Jonas Eliasson spoke about the experience in Sweden of developing a database for traffic prognoses. The main...... to develop a technically advanced form of aesthetics. The Master Class in low energy buildings was led by civil engineer, Svend Svendsen, a Professor at DTU Byg. Together with colleagues and students, he has achieved an extensive knowledge of Integrated Design. In fact, the situation is that our knowledge...

  3. Global Standards of Market Civilization

    DEFF Research Database (Denmark)

    Global Standards of Market Civilization brings together leading scholars, representing a range of political views, to investigate how global 'standards of market civilization' have emerged, their justification, and their political, economic and social impact. Key chapters show how as the modern...... thought, as well as its historical application part II presents original case studies that demonstrate the emergence of such standards and explore the diffusion of liberal capitalist ideas through the global political economy and the consequences for development and governance; the International Monetary...... Fund's capacity to formulate a global standard of civilization in its reform programs; and problems in the development of the global trade, including the issue of intellectual property rights. This book will be of strong interest to students and scholars in wide range of fields relating to the study...

  4. Artificial Intelligence in Civil Engineering

    Directory of Open Access Journals (Sweden)

    Pengzhen Lu

    2012-01-01

    Full Text Available Artificial intelligence is a branch of computer science, involved in the research, design, and application of intelligent computer. Traditional methods for modeling and optimizing complex structure systems require huge amounts of computing resources, and artificial-intelligence-based solutions can often provide valuable alternatives for efficiently solving problems in the civil engineering. This paper summarizes recently developed methods and theories in the developing direction for applications of artificial intelligence in civil engineering, including evolutionary computation, neural networks, fuzzy systems, expert system, reasoning, classification, and learning, as well as others like chaos theory, cuckoo search, firefly algorithm, knowledge-based engineering, and simulated annealing. The main research trends are also pointed out in the end. The paper provides an overview of the advances of artificial intelligence applied in civil engineering.

  5. Aircraft noise prediction

    Science.gov (United States)

    Filippone, Antonio

    2014-07-01

    This contribution addresses the state-of-the-art in the field of aircraft noise prediction, simulation and minimisation. The point of view taken in this context is that of comprehensive models that couple the various aircraft systems with the acoustic sources, the propagation and the flight trajectories. After an exhaustive review of the present predictive technologies in the relevant fields (airframe, propulsion, propagation, aircraft operations, trajectory optimisation), the paper addresses items for further research and development. Examples are shown for several airplanes, including the Airbus A319-100 (CFM engines), the Bombardier Dash8-Q400 (PW150 engines, Dowty R408 propellers) and the Boeing B737-800 (CFM engines). Predictions are done with the flight mechanics code FLIGHT. The transfer function between flight mechanics and the noise prediction is discussed in some details, along with the numerical procedures for validation and verification. Some code-to-code comparisons are shown. It is contended that the field of aircraft noise prediction has not yet reached a sufficient level of maturity. In particular, some parametric effects cannot be investigated, issues of accuracy are not currently addressed, and validation standards are still lacking.

  6. Aircraft Oxygen Generation

    Science.gov (United States)

    2012-02-01

    aircraft use some form of on-board oxygen generation provided by one of two corporations that dominate this market . A review of safety incident data...manufacture of synthetic resins (e.g., Bakelite), and for 161 making dyestuffs, flavorings, perfumes , and other chemicals. Some are used as

  7. Space Civil Engineering option - A progress report

    Science.gov (United States)

    Criswell, Marvin E.; Sadeh, Willy Z.

    1992-01-01

    Space Civil Engineering is an emerging engineering discipline that focuses on extending and expanding Civil Engineering to the development, operation, and maintenance of infrastructures on celestial bodies. Space Civil Engineering is presently being developed as a new discipline within the Department of Civil Engineering at Colorado State University and with support of the NASA Space Grant College Program. Academic programs geared toward creating Space Civil Engineering Options at both undergraduate and graduate levels are being formulated. Basic ideas and concepts and the current status of the curriculum in the Space Civil Engineering Option primarily at the undergraduate level are presented.

  8. Sociedad civil y capital social

    OpenAIRE

    José Fernández Santillán

    2009-01-01

    Este documento aborda el tema de la democracia desde una perspectiva opuesta al llamado neoinstitucionalismo; es decir, se orienta a analizar los procesos de democratización desde la base de la sociedad civil y, en es pe cial, desde lo que se conoce como el cap i tal so cial. Desde mediados de la década de 1980, el tema de la democracia desde la perspectiva de la sociedad civil fue cobrando cada vez mayor relevancia. Esta tendencia se vio reforzada por la caída del Muro de Berlín el 9 de nov...

  9. Tendencias del Derecho civil (2002)

    OpenAIRE

    Arellano Gómez, Francisco Javier

    2002-01-01

    Durante el año 2.002 han dado a luz, en el campo del Derecho Civil, un conjunto de leyes que suponen una importante actualización normativa ante determinadas necesidades presentadas por la dinámica realidad socio-económica de España, en un contexto de acelerada tecnificación, creciente vitalidad y fluidez de tejido social, y de progresiva armonización legislativa con los países de nuestro entorno. Para este informe de Derecho Civil hemos preferido seguir, por razón de mejor carácter sistemáti...

  10. The potential of biobased materials in the civil engineering sector

    NARCIS (Netherlands)

    Venema, Anne

    2012-01-01

    SUMMARY Large quantities of materials are used in the Dutch civil engineering sector every year. Many of these materials have a significant impact on the environment because these materials are based on non-renewable resources and the production is often

  11. Construction Site Environmental Impact in Civil Engineering Education

    Science.gov (United States)

    Teixeira, Jose M. Cardoso

    2005-01-01

    The environmental impact of construction activity has gained increasing importance in the last few years and become a key subject for civil engineering education. A survey of Portuguese higher education institutions shows that concern with this topic is mostly directed at the impact of large construction projects and especially focused on their…

  12. The potential of biobased materials in the civil engineering sector

    NARCIS (Netherlands)

    Venema, Anne

    2012-01-01

    SUMMARY Large quantities of materials are used in the Dutch civil engineering sector every year. Many of these materials have a significant impact on the environment because these materials are based on non-renewable resources and the production is often

  13. Aircraft Detection from VHR Images Based on Circle-Frequency Filter and Multilevel Features

    Science.gov (United States)

    Gao, Feng; Li, Bo

    2013-01-01

    Aircraft automatic detection from very high-resolution (VHR) images plays an important role in a wide variety of applications. This paper proposes a novel detector for aircraft detection from very high-resolution (VHR) remote sensing images. To accurately distinguish aircrafts from background, a circle-frequency filter (CF-filter) is used to extract the candidate locations of aircrafts from a large size image. A multi-level feature model is then employed to represent both local appearance and spatial layout of aircrafts by means of Robust Hue Descriptor and Histogram of Oriented Gradients. The experimental results demonstrate the superior performance of the proposed method. PMID:24163637

  14. Aircraft Detection from VHR Images Based on Circle-Frequency Filter and Multilevel Features

    Directory of Open Access Journals (Sweden)

    Feng Gao

    2013-01-01

    Full Text Available Aircraft automatic detection from very high-resolution (VHR images plays an important role in a wide variety of applications. This paper proposes a novel detector for aircraft detection from very high-resolution (VHR remote sensing images. To accurately distinguish aircrafts from background, a circle-frequency filter (CF-filter is used to extract the candidate locations of aircrafts from a large size image. A multi-level feature model is then employed to represent both local appearance and spatial layout of aircrafts by means of Robust Hue Descriptor and Histogram of Oriented Gradients. The experimental results demonstrate the superior performance of the proposed method.

  15. Braking performance of aircraft tires

    Science.gov (United States)

    Agrawal, Satish K.

    This paper brings under one cover the subject of aircraft braking performance and a variety of related phenomena that lead to aircraft hydroplaning, overruns, and loss of directional control. Complex processes involving tire deformation, tire slipping, and fluid pressures in the tire-runway contact area develop the friction forces for retarding the aircraft; this paper describes the physics of these processes. The paper reviews the past and present research efforts and concludes that the most effective way to combat the hazards associated with aircraft landings and takeoffs on contaminated runways is by measuring and displaying in realtime the braking performance parameters in the aircraft cockpit.

  16. A Symphony of Civilizations

    Institute of Scientific and Technical Information of China (English)

    DAVID; GOSSET

    2006-01-01

    Both China and the European Union have a major role to play in achieving global equilibrium and peace Escalation in the Middle East, chaos in Iraq, uncertainty in Afghanistan, tensions over Iran's and North Korea's nuclear programs, the spread of terrorism, large-scale economic exclusion, a deadlock in the Doha trade development agenda, rhetorical disputes between Washington and Moscow, the evaporation of U.S. soft power and the discrediting of the very values it is supposed to project.

  17. Optimal PID Controller Tuning for Multivariable Aircraft Longitudinal Autopilot Based on Particle Swarm Optimization Algorithm

    Directory of Open Access Journals (Sweden)

    Mostafa Lotfi Forushani

    2012-04-01

    Full Text Available This paper presents an optimized controller around the longitudinal axis of multivariable system in one of the aircraft flight conditions. The controller is introduced in order to control the angle of attack from the pitch attitude angle independently (that is required for designing a set of direct force-modes for the longitudinal axis based on particle swarm optimization (PSO algorithm. The autopilot system for military or civil aircraft is an essential component and in this paper, the autopilot system via 6 degree of freedom model for the control and guidance of aircraft in which the autopilot design will perform based on defining the longitudinal and the lateral-directional axes are supposed. The effectiveness of the proposed controller is illustrated by considering HIMAT aircraft. The simulation results verify merits of the proposed controller.

  18. Wake Vortices of Landing Aircraft, in High Performance Computing in Science and Engineering

    OpenAIRE

    Holzäpfel, Frank; Stephan, Anton; Heel, Tobias

    2014-01-01

    As an unavoidable consequence of lift aircraft generate a pair of counter-rotating and long-lived wake vortices that pose a potential risk to following aircraft. The prescribed aircraft separations during landing to avoid wake vortex hazards contribute significantly to capacity restrictions of large airports. Severe encounters of wake vortices have also been reported during cruise. Wake vortex behavior is largely controlled by the prevailing meteorological conditions a...

  19. Job Prospects for Civil Engineers.

    Science.gov (United States)

    Basta, Nicholas

    1985-01-01

    Government programs and renewed industrial activity have combined with stable enrollments to create bright job prospects for civil engineers. Areas with good opportunities include highway reconstruction and rehabilitation, water-resource management, and new factory construction. The subspecialty of structural engineering has a growing need in…

  20. Primary Sources Enliven Civil War

    Science.gov (United States)

    Robelen, Erik W.

    2011-01-01

    Today, a growing number of teachers are moving beyond the textbook in teaching about the war, and U.S. history more broadly. Teachers are digging directly into primary sources and harnessing technology, all in an attempt to help students better understand the past and bring it to life. Doing so may be especially important with the Civil War,…

  1. Aging of civil explosives (Poster)

    NARCIS (Netherlands)

    Krabbendam-La Haye, E.L.M.; Klerk, W.P.C. de; Hoen, C. 't; Krämer, R.E.

    2014-01-01

    For the Dutch MoD and police, TNO composed sets with different kinds of civil explosives to train their detection dogs. The manufacturer of these explosives guarantees several years of stability of these explosives. These sets of explosives are used under different conditions, like temperature and

  2. Getting the Civil War Right

    Science.gov (United States)

    Loewen, James W.

    2011-01-01

    William Faulkner famously wrote, "The past is never dead. It's not even past." He would not be surprised to learn that Americans, 150 years after the Civil War began, are still getting it wrong. Did America's most divisive war start over slavery or states' rights? The author says that too many people--including educators--get it wrong. The author…

  3. 1975 Textbooks for French Civilization.

    Science.gov (United States)

    Brown, Jack Davis

    Four 1975 textbooks for French civilization courses are cited including price, suggested level, format and a listing of contents. A review of one text follows: Rey and Santoni, "Quand les Francais parlent: Langue en contexte, culture en contraste," Newbury House Publishers. The reviewer states that this book is basically a sociological study of…

  4. Etica civile e beatitudini evangeliche

    Directory of Open Access Journals (Sweden)

    Nicola Colaianni

    2014-02-01

    Full Text Available Il contributo, sottoposto a valutazione, riproduce il testo dell’intervento nel dibattito a due voci (con il presidente della Corte costituzionale, Gaetano Silvestri a conclusione del convegno “La Bibbia sulle strade dell’uomo” (Messina, 23 novembre 2013, ed è destinato alla pubblicazione negli Atti.SOMMARIO: 1. L’etica civile come etica costituzionale – 2. L’etica evangelica – 3. Irriducibilità? – 4. La promessa e il terzo – 5. La libertà – 6. Il tratto di cammino insieme.  Civil Ethic and Evangelical Beatitudes ABSTRACT The differences between civil ethic and religious ethic, that the Author defines as constitutional principles and evangelic Beatitudes, are well known: it’s common knowledge that the ones are effective in the earthly life while the others are oriented to the eternal life. Nevertheless the Author argues that they both have a common feature before that last analysis: they cross as principles of continuing opposition to unjust society, to “unlawful law”, to spreading apart between the constitutional and evangelic must be and the legislative being of positive law.KEY-WORDS: Civil Ethic – Constitution – Evangelical Beatitudes – Differences - Common Feature.

  5. 17 CIVIL DISOBEDIENCE AND DEMOCRATIC SUSTAINABILITY IN ...

    African Journals Online (AJOL)

    HP

    government businesses were halted for about a week and the government of. President ... Unlike the understanding of civil disobedience in the postmodern world, ... 7 David Lefkowit, “On a Moral Right to Civil Disobedience,” Ethics Vol. 117,.

  6. Eternal inflation, black holes, and the future of civilizations

    CERN Document Server

    Garriga, J; Olum, K D; Vilenkin, A

    2000-01-01

    We discuss the large-scale structure of the universe in inflationary cosmology and the implications that it may have for the long-term future of civilizations. Although each civilization is doomed to perish, it may be possible to transmit its accumulated knowledge to future civilizations. We consider several scenarios of this sort. If the cosmological constant is positive, it eventually dominates the universe and bubbles of inflationary phase begin to nucleate at a constant rate. Thermalized regions inside these inflating bubbles will give rise to new galaxies and civilizations. It is possible in principle to send a message to one of them. It might even be possible to send a device whose purpose is to recreate an approximation of the original civilization in the new region. However, the message or device will almost certainly be intercepted by black holes, which nucleate at a much higher rate than inflating bubbles. Formation of new inflating regions can also be triggered by gravitational collapse, but again ...

  7. The Independence of Notary in The Civil Partnership of Notary

    Directory of Open Access Journals (Sweden)

    Adha Dia Agustin

    2014-06-01

    Full Text Available The continued development of business in Indonesia, would make the greater role of the notary. The number of notaries and needed in each region in Indonesia gets greater. This rapid development, then coupled with the new policy. Previously, Peraturan Jabatan Notaris(PJN prohibited Perserikatan, but since the establishment of Undang-Undang Jabatan Notaris (UUJN has changed otherwise. Notary possible to make associations in a Civil Partnership. Even Peraturan Menteri Hukum dan HAM RI Nomor: M.HH.01.AH.02.12 Tahun 2010 tentang Persyaratan Menjalankan Jabatan Notaris Dalam Bentuk Perserikatan Perdata described the formation of the implementing regulations of the Civil Partnership. Is it true that Civil Partnership would make science benefit for junior notary and will facilitate the work of a Notary Or it would make large colonies notary who compete each other, so that the function of a notary public is no longer as state officials, but it called the company deed. This journal examines the Civil Partnership in Kitab Undang-Undang Hukum Perdata and would review the principle of the independence of the notary as set forth in Undang-Undang Jabatan Notaris. How To Cite: Agustin, A. (2014. The Independence of Notary in The Civil Partnership of Notary. Rechtsidee, 1(2, 131-146. doi:http://dx.doi.org/10.21070/jihr.v1i2.102

  8. Climate Change and Civil Violence

    Science.gov (United States)

    van der Vink, G.; Plancherel, Y.; Hennet, C.; Jones, K. D.; Abdullah, A.; Bradshaw, J.; Dee, S.; Deprez, A.; Pasenello, M.; Plaza-Jennings, E.; Roseman, D.; Sopher, P.; Sung, E.

    2009-05-01

    The manifestations of climate change can result in humanitarian impacts that reverse progress in poverty- reduction, create shortages of food and resources, lead to migration, and ultimately result in civil violence and conflict. Within the continent of Africa, we have found that environmentally-related variables are either the cause or the confounding factor for over 80% of the civil violence events during the last 10 years. Using predictive climate models and land-use data, we are able to identify populations in Africa that are likely to experience the most severe climate-related shocks. Through geospatial analysis, we are able to overlay these areas of high risk with assessments of both the local population's resiliency and the region's capacity to respond to climate shocks should they occur. The net result of the analysis is the identification of locations that are becoming particularly vulnerable to future civil violence events (vulnerability hotspots) as a result of the manifestations of climate change. For each population group, over 600 social, economic, political, and environmental indicators are integrated statistically to measures the vulnerability of African populations to environmental change. The indicator time-series are filtered for data availability and redundancy, broadly ordered into four categories (social, political, economic and environmental), standardized and normalized. Within each category, the dominant modes of variability are isolated by principal component analysis and the loadings of each component for each variable are used to devise composite index scores. Comparisons of past vulnerability with known environmentally-related conflicts demonstrates the role that such vulnerability hotspot maps can play in evaluating both the potential for, and the significance of, environmentally-related civil violence events. Furthermore, the analysis reveals the major variables that are responsible for the population's vulnerability and therefore

  9. 7 CFR 3017.920 - Civil judgment.

    Science.gov (United States)

    2010-01-01

    ... by verdict, decision, settlement, stipulation, other disposition which creates a civil liability for the complained of wrongful acts, or a final determination of liability under the Program Fraud Civil... 7 Agriculture 15 2010-01-01 2010-01-01 false Civil judgment. 3017.920 Section 3017.920...

  10. 29 CFR 1471.920 - Civil judgment.

    Science.gov (United States)

    2010-07-01

    ..., stipulation, other disposition which creates a civil liability for the complained of wrongful acts, or a final determination of liability under the Program Fraud Civil Remedies Act of 1988 (31 U.S.C. 3801-3812). ... 29 Labor 4 2010-07-01 2010-07-01 false Civil judgment. 1471.920 Section 1471.920 Labor...

  11. 31 CFR 19.920 - Civil judgment.

    Science.gov (United States)

    2010-07-01

    ..., stipulation, other disposition which creates a civil liability for the complained of wrongful acts, or a final determination of liability under the Program Fraud Civil Remedies Act of 1988 (31 U.S.C. 3801-3812). ... 31 Money and Finance: Treasury 1 2010-07-01 2010-07-01 false Civil judgment. 19.920 Section...

  12. CIVILIZATION SCENARIOS OF DEVELOPMENT OF RUSSIA

    Directory of Open Access Journals (Sweden)

    A. N. Kharin

    2013-01-01

    Full Text Available In the modern world plays an important role civilization factor. In this connection beforeRussiaa task stands forming of civilization identity. A problem consists in that, that exists a few scenarios of civilization development. To their consideration and this article is devoted.

  13. 14 CFR 1274.924 - Civil rights.

    Science.gov (United States)

    2010-01-01

    ... Discrimination Act of 1975 (42 U.S.C. 6101 et seq.), and the NASA implementing regulations (14 CFR parts 1250... 14 Aeronautics and Space 5 2010-01-01 2010-01-01 false Civil rights. 1274.924 Section 1274.924... FIRMS Other Provisions and Special Conditions § 1274.924 Civil rights. Civil Rights July 2002 Work...

  14. 7 CFR 3560.2 - Civil rights.

    Science.gov (United States)

    2010-01-01

    ... 7 Agriculture 15 2010-01-01 2010-01-01 false Civil rights. 3560.2 Section 3560.2 Agriculture... DIRECT MULTI-FAMILY HOUSING LOANS AND GRANTS General Provisions and Definitions § 3560.2 Civil rights. (a... prohibition under Title VI of the Civil Rights Act of 1964, 42 U.S.C. 2000d and Title VI regulations...

  15. 7 CFR 761.3 - Civil rights.

    Science.gov (United States)

    2010-01-01

    ... 7 Agriculture 7 2010-01-01 2010-01-01 false Civil rights. 761.3 Section 761.3 Agriculture... SPECIAL PROGRAMS GENERAL PROGRAM ADMINISTRATION General Provisions § 761.3 Civil rights. Part 15d of this title contains applicable regulations pertaining to civil rights and filing of discrimination...

  16. 50 CFR 401.22 - Civil rights.

    Science.gov (United States)

    2010-10-01

    ... 50 Wildlife and Fisheries 7 2010-10-01 2010-10-01 false Civil rights. 401.22 Section 401.22..., DEVELOPMENT AND ENHANCEMENT § 401.22 Civil rights. Each application for Federal assistance, grant-in-aid award... Assisted Programs of the Civil Rights Act of 1964 and with the Secretary's regulations...

  17. 30 CFR 881.12 - Civil rights.

    Science.gov (United States)

    2010-07-01

    ... Civil Rights Act of 1964” (43 CFR part 17) and shall give assurances of compliance in such forms as may... 30 Mineral Resources 3 2010-07-01 2010-07-01 false Civil rights. 881.12 Section 881.12 Mineral... LAND RECLAMATION SUBSIDENCE AND STRIP MINE REHABILITATION, APPALACHIA § 881.12 Civil rights. State...

  18. The Transformed Civil Rights Data Collection (CRDC)

    Science.gov (United States)

    Office for Civil Rights, US Department of Education, 2012

    2012-01-01

    Since 1968, the Civil Rights Data Collection (CRDC) has collected data on key education and civil rights issues in our nation's public schools for use by the Department of Education's Office for Civil Rights (OCR), other Department offices, other federal agencies, and by policymakers and researchers outside of the Department. The CRDC has…

  19. Department of Health and Human Services, Office for Civil Rights

    Science.gov (United States)

    ... Z Index About Us Filing with OCR Civil Rights Health Information Privacy Newsroom HHS Home > Office for Civil ... Civil Rights Filing with OCR File a civil rights or health information privacy complaint. Newsroom Read the latest OCR ...

  20. Stratospheric aircraft: Impact on the stratosphere

    Energy Technology Data Exchange (ETDEWEB)

    Johnston, H.

    1992-02-01

    The steady-state distribution of natural stratospheric ozone is primarily maintained through production by ultraviolet photolysis of molecular oxygen, destruction by a catalytic cycle involving nitrogen oxides (NO{sub x}), and relocation by air motions within the stratosphere. Nitrogen oxides from the exhausts of a commercially viable fleet of supersonic transports would exceed the natural source of stratospheric nitrogen oxides if the t should be equipped with 1990 technology jet engines. This model-free comparison between a vital natural global ingredient and a proposed new industrial product shows that building a large fleet of passenger stratospheric aircraft poses a significant global problem. NASA and aircraft industries have recognized this problem and are studying the redesign of jet aircraft engines in order to reduce the nitrogen oxides emissions. In 1989 atmospheric models identified two other paths by which the ozone destroying effects of stratospheric aircraft might be reduced or eliminated: (1) Use relatively low supersonic Mach numbers and flight altitudes. For a given rate of nitrogen oxides injection into the stratosphere, the calculated reduction of total ozone is a strong function of altitude, and flight altitudes well below 20 kilometers give relatively low calculated ozone reductions. (2) Include heterogeneous chemistry in the two-dimensional model calculations. Necessary conditions for answering the question on the title above are to improve the quality of our understanding of the lower stratosphere and to broaden our knowledge of hetergeneous stratospheric chemistry. This article reviews recently proposed new mechanisms for heterogeneous reactions on the global stratospheric sulfate aerosols.