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Volume 39 Issue 5
May  2013
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Journal of Beijing University of Aeronautics and Astronautics  > 2013  >  39(5): 595-599.
Li Xing, Guan Zhidong, Liu Lu, et al. Damage simulation of composite materials based on strain invariant failure theory[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(2): 190-195. (in Chinese)
Citation: Tu Yi, Xiao Xiang, Li Nanet al. Computer analysis of large-scale aircraft landing gear retraction and extension control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 595-599. (in Chinese)
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Computer analysis of large-scale aircraft landing gear retraction and extension control system

  • Shanghai Aircraft Design And Research Institute, Commercial Aircraft Corporation of China, Shanghai 201203, China

  • Received Date: 11 May 2012
  • Rev Recd Date: 26 Nov 2012
  • Publish Date: 31 May 2013
    Abstract
  • A variety of constraints and influence factors need to be considered in landing gear retraction and extension (R/E) control system design. System simulation platform is an important auxiliary method for the system design. The hydraulic accessories simulation models of large-scale aircraft landing gear control system were established based on the fluid system simulation software Flowmaster, and the system simulation model was constructed using the established component models. Analysis of the landing gear retraction process for normal flight state was conducted based on the present system simulation model, and impacts of the actuator size on system entry pressure requirement, hydraulic fluid flowrate and the gear retraction time were also provided. The simulation method can be used for the preliminary design of the landing gear R/E control system and the verification of system design for different flight conditions.

     

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    • References(9)
  • [1]
    唐毅,魏鑫,曹克强.基于AMESim的某型飞机液压系统仿真研究[J].机床与液压,2007,35(6):198-200
    Tang Yi,Wei Xin,Cao Keqiang.The simulation of aero hydraulic system based on AMESim[J].Machine Tool & Hydraulics,2007,35(6):198-200(in Chinese)
    [2]
    王红玲,逯九利,田广来.基于AMESim的飞机防滑刹车系统数字仿真研究[J].机床与液压,2011,39(7):117-120
    Wang Hongling,Lu Jiuli,Tian Guanglai.Simulation research of aircraft braking system based on AMESim[J].Machine Tool & Hydraulics,2011,39(7):117-120(in Chinese)
    [3]
    Kong W,Sim C,Kim J.Modeling of a hydraulic power steering system and Its application to steering damper development[R].SAE 2005-01-1263,2005
    [4]
    张强,于辉,童明波.某型飞机起落架收放过程仿真[J].流体传动与控制,2009(2):29-31
    Zhang Qiang,Yu Hui,Tong Mingbo.Simulation of extending and retracting process for aircraft landing gear[J].Fluid Power Transmission and Control,2009(2):29-31(in Chinese)
    [5]
    Tu Y,Lin G P.Dynamic simulation of aircraft environmental control system based on Flowmaster[J].Journal of Aircraft,2011,48(6):2031-2041
    [6]
    Rowland P,Longvill M,Austin k,et al.Developing of the modeling environment for the simulation of an aircraft hydraulic system[R].AIAA 2000-5600,2000
    [7]
    陈博,杨国平,高军浩,等.基于Flowmaster的液压冲击器动态特性仿真研究[J].机床与液压,2011,39(11):95-97
    Chen Bo,Yang Guoping,Gao Junhao,et al.Dynamic characteristics simulation research of hydraulic impactor based on Flowmaster[J].Machine Tool & Hydraulics,2011,39(11):95-97(in Chinese)
    [8]
    屠毅,林贵平,李国栋.基于Flowmaster的运输机供氧系统仿真[J].北京航空航天大学学报,2009,35(11):1306-1310
    Tu Yi,Lin Guiping,Li Guodong.Computer analysis of transport aircraft oxygen system based on Flowmaster[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(11):1306-1310(in Chinese)
    [9]
    李彦江,刘永寿,姜志峰,等.飞机燃油系统功能仿真分析[J].航空计算技术,2009,39(4):113-116
    Li Yanjiang,Liu Yongshou,Jiang Zhifeng,et al.Analysis of functional simulation of aircraft fuel system[J].Aeronautical Computing Technique,2009,39(4):113-116(in Chinese)
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