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大型飞机起落架收放控制系统仿真

屠毅 肖翔 李楠

屠毅, 肖翔, 李楠等 . 大型飞机起落架收放控制系统仿真[J]. 北京航空航天大学学报, 2013, 39(5): 595-599.
引用本文: 屠毅, 肖翔, 李楠等 . 大型飞机起落架收放控制系统仿真[J]. 北京航空航天大学学报, 2013, 39(5): 595-599.
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)
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)

大型飞机起落架收放控制系统仿真

详细信息
  • 中图分类号: V226+.1

Computer analysis of large-scale aircraft landing gear retraction and extension control system

  • 摘要: 起落架收放控制系统设计需考虑多种约束条件和影响因素,系统仿真平台的使用是辅助系统设计的重要手段.基于流体系统仿真软件Flowmaster,建立了大型飞机起落架收放控制系统液压附件仿真模型,在此基础上构建了完整收放控制系统仿真模型.基于建立的系统仿真模型,进行了正常飞行状态下起落架收上过程仿真分析,仿真结果给出了液压作动器尺寸设计对收放过程中系统入口压力需求、系统液压流量及起落架收放时间的影响.该仿真方法可用于起落架收放控制系统初步设计及多种飞行状态下设计方案的校核.

     

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出版历程
  • 收稿日期:  2012-05-11
  • 修回日期:  2012-11-26
  • 网络出版日期:  2013-05-31

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