航空学报 > 2007, Vol. 28 Issue (1): 135-137

飞机结构关键件设计改进后的疲劳寿命评定技术

隋福成,刘文珽,王磊   

  1. 北京航空航天大学 航空科学与工程学院
  • 收稿日期:2005-09-02 修回日期:2005-11-18 出版日期:2007-01-10 发布日期:2007-01-10
  • 通讯作者: 刘文珽

Technique about Evaluating the Fatigue Life of the Improved Main Components in Aircraft

SUI Fucheng,LIU Wenting,WANG Lei   

  1. School of Aeronautical Science and Technology, Beijing University of Aeronautics and Astronautics
  • Received:2005-09-02 Revised:2005-11-18 Online:2007-01-10 Published:2007-01-10
  • Contact: LIU Wenting

摘要:

结合某型飞机重要疲劳关键件起落架梁设计改进后的寿命评定,建立了在不进行全尺寸试验的情况下,对设计改进结构进行寿命评定的方法。即在结构改进前后关键疲劳薄弱部位细节应力分析的基础上,通过该疲劳关键部位的模拟试件在改进前后应力谱下的寿命分析和疲劳对比试验,综合评定结构改进后的寿命增加系数,参照改进前该结构的全尺寸疲劳试验结果,确定设计改进后该关键件的疲劳寿命。用上述方法完成了对某型飞机重要疲劳关键件起落架梁改进后的寿命评定,其结果也应用到了该型飞机结构的定延寿。

关键词: 对比试验, 寿命评定, 模拟件, 裂纹扩展, 起落架梁

Abstract:

This paper takes example for evaluating the life of the improved undercarriage beam which is a main fatigue component in a kind of plane, and describes the method about evaluating the fatigue life of the improved components in the case of lack of whole size testing. This method bases on the detail stress analysis of the main fatigue parts between the improved component and the unimproved component, and evaluates synthetically the coefficient of life increase of the improved component by analyzing the life of the simulator specimen of this component by analyzing the life of the simulator specimen of this component in the case of each load spectrum and the fatigue compare testing, and ascertains the fatigue life of this improved main component by consulting the result of the whole size testing about this unimproved component.  The life evaluating of the undercarriage beam which is a main fatigue component in a kind of plane is completed by this method.  The result was applied to this kind of plane.

Key words: ompare , testing,  , life , evaluating,  , simulator , specimen,  , crack , propagation,  , undercarriage , beam

中图分类号: