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新的被动自适应起落架缓冲器设计与着陆性能研究(英文)
引用本文:朱书华,童明波,许杰.新的被动自适应起落架缓冲器设计与着陆性能研究(英文)[J].南京航空航天大学学报(英文版),2009,26(1).
作者姓名:朱书华  童明波  许杰
作者单位:1. 南京航空航天大学航空宇航学院,南京,210016,中国
2. 成都飞机工业集团有限责任公司结构室,成都,610041,中国
摘    要:研究了一种双腔双阻尼的被动式自适应缓冲器;给出了此缓冲器的数学模型,并基于动力学仿真软件ADAMS建立了该缓冲器的虚拟样机;分析了该缓冲器的着陆动态性能及其主要参数对全机着陆动态性能的影响.分析表明:在使用功条件下,自适应缓冲器的着陆性能比单腔变油孔缓冲器性能略好;而在粗暴着陆条件下,自适应缓冲器的过载远小于单腔变油孔缓冲器,起到主要减载作用.增大高压腔、低压腔体积或增加低压腔压力或减小高压腔压力均可使自适应缓冲器的过载减少.

关 键 词:起落架(飞机)  自适应缓冲器  着陆  虚拟样机

DESIGN OF NEW PASSIVE ADAPTIVE SHOCK ABSORBER OF LANDING GEAR AND STUDY OF ITS LANDING PERFORMANCE
Zhu Shuhua,Tong Mingbo,Xu Jie.DESIGN OF NEW PASSIVE ADAPTIVE SHOCK ABSORBER OF LANDING GEAR AND STUDY OF ITS LANDING PERFORMANCE[J].Transactions of Nanjing University of Aeronautics & Astronautics,2009,26(1).
Authors:Zhu Shuhua  Tong Mingbo  Xu Jie
Institution:1.College of Aerospace Engineering;NUAA;29 Yudao Street;Nanjing;210016;P.R.China;2.Department of Structure;Chengdu Aircraft Design & Research Institute;Chengdu;610041;P.R.China
Abstract:A new passive adaptive shock absorber of the landing gear with double-cavity and dual-damping is studied.Its mathematical model and the virtual prototype are established based on the dynamics simulation software ADAMS.The landing dynamic characteristics and the effect of the parameters on the proposed adaptive shock absorber are analyzed.The results show that the proposed adaptive shock absorber has the slightly better landing performance at the normal load case and much less overload at the crudely landing...
Keywords:landing gear(aircraft)  shock absorbers  landing  virtual prototype
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