吉林大学学报(工学版)

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飞机起落架疲劳损伤估算及其特点

刘克格, 阎楚良, 张书明   

  1. 北京机械结构强度研究中心,北京 100083
  • 收稿日期:2005-04-22 修回日期:2005-07-08 出版日期:2005-11-01 发布日期:2005-11-01
  • 通讯作者: 阎楚良

Estimation for Fatigue Damage of Airplane Landing Gear

LIU Kege, YAN Chuliang, ZHANG Shuming   

  1. Beijing Center of Mechanical Structural Strength Research and Development,Beijing 100083, China
  • Received:2005-04-22 Revised:2005-07-08 Online:2005-11-01 Published:2005-11-01
  • Contact: YAN Chuliang

摘要: 以战斗类飞机和运输类飞机主起落架为例,通过飞行实测获得起落架在实际工作过程中的载荷-时间历程(即实测载荷谱),并利用Miner准则对其疲劳寿命进行了估算。计算结果表明:战斗类飞机和运输类飞机起落架在着陆滑行段所造成的损伤分别占各自总损伤的75%以上和60%以上,运输类飞机在着陆瞬间撞击对起落架所造成的损伤约占总损伤的40%。通过分析战斗类飞机和运输类飞机的起落架疲劳损伤特点,为其可靠性设计和结构优化设计等提供了重要依据。

关键词: 航空器结构力学, 起落架, 疲劳损伤, 实测载荷谱, Miner准则

Abstract: Taking the main landing gears of fighter and transport airplane as example, the fatigue life was estimated by means of the Miner’s rule and the spectrum of the real measurement. The computed results show that the landing damage of the fighter and transport airplane is of 75% and 60% of the total damage, and the landing damge of the landing load of the transport airplane is of 40% of the landing gears damage. The fatigue damage properties can provide important information for the reliability design and the structural optimization.

Key words: aircraft structural mechanics, landing gear, fatigue damage, load spectrums of real measurement, Miner’s rule

中图分类号: 

  • O346.2
[1] 曹珊珊, 雷俊卿. 考虑区间不确定性的钢结构疲劳寿命分析[J]. 吉林大学学报(工学版), 2016, 46(3): 804-810.
[2] 刘克格,阎楚良,张书明. 飞机主起落架载荷谱实测的台架标定[J]. 吉林大学学报(工学版), 2006, 36(06): 1025-1028.
[3] 白瑞祥,张志峰,陈浩然. 含面\芯开裂损伤复合材料夹层板的自由振动[J]. 吉林大学学报(工学版), 2005, 35(02): 199-0204.
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