航空学报 > 2003, Vol. 24 Issue (6): 517-520

某歼击机前起落架着陆瞬间有关参数的试验研究

史海文1, 杨树勋2, 张大千3, 傅永宏4   

  1. 1. 北京航空航天大学固体力学所, 北京?? 100083;2. 沈阳飞机设计研究所, 辽宁沈阳?? 110035;3. 沈阳航空工业学院, 辽宁沈阳?? 110031;4. 沈阳飞机工业 集团 有限公司, 辽宁沈阳?? 110034
  • 收稿日期:2002-09-11 修回日期:2002-11-05 出版日期:2003-12-25 发布日期:2003-12-25

Parameters Study at Touchdown Instant of the Nose Undercarriage of Fighter Airplane

SHI Hai-wen1, YANG Shu-xun2, ZHANG Da-qian3, FU Yong-hong4   

  1. 1. Institute of Solid Mechanics; Beijing University of Aeronautics and Astronuntics; Beijing 100083; China;2. Shenyang Aircraft Design & Research Institute; Shenyang 110035; China;3. Shenyang Institute of Aeronautics Engineering; Shenyang 110031; China;4. Shenyang Aircraft Corporation; Shenyang 110034; China
  • Received:2002-09-11 Revised:2002-11-05 Online:2003-12-25 Published:2003-12-25

摘要: 以某歼击飞机前起落架为例, 用落震试验的方法, 通过分析起落架有关参数随机轮转速变化的情况,来研究飞机着陆瞬间起落架的状况。研究结果表明, 在飞机着陆过程中, 当起转水平载荷达到最大值时, 起落架逆航向的弹性变形还未结束; 当起落架逆航向的弹性变形达到最大值时, 机轮从滑动转为滚动。

关键词: 起落架, 落震试验, 机轮, 转速, 水平载荷

Abstract: The status of an under carr iag e at t he touchdow n instant is studied by analyzing the undercar riage par ameters w hich chang e w ith the w heel rotational speed in the drop test. The result indicates that when the spin-up horizo ntal load is the max imum dur ing t he landing , the opposite course residual elasticity of the under carriag e is not finished, and when the opposite course residual elasticity of t he under carr iag e is the max imum, the w heel mov ement ischanged from slide to roll.

Key words: undercarriage, drop test, wheel, rotational speed, horizontal load

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