航空学报 > 1992, Vol. 13 Issue (3): 182-186

耐久性分析的裂纹萌生方法研究

刘文珽, 熊峻江   

  1. 北京航空航天大学508教研室 北京 100083
  • 收稿日期:1991-07-04 修回日期:1991-10-10 出版日期:1992-03-25 发布日期:1992-03-25

A STUDY ON CRACK INITIATION METHOD FOR DURABILITY ANALYSIS

Liu Wen-ting, Xiong Jun-jiang   

  1. Faculty 508 of Beijing University of Aeronautics and Astronautics,Beijing, 100083
  • Received:1991-07-04 Revised:1991-10-10 Online:1992-03-25 Published:1992-03-25

摘要:

本文以裂纹尺寸达到经济修理极限对应的结构细节条件裂纹萌生P-S-N曲线为基础,将谱载下安全寿命的存活率与裂纹超越数概率联系在一起,建立各应力区的P(i,τ)随时间变化曲线,进而评估指定时间的结构损伤度,并预测经济寿命,构成完整的耐久性裂纹萌生方法,最后给出一个简单实例。

关键词: 耐久性分析, 裂纹萌生, 经济寿命

Abstract:

In this paper, a crack initiation metho . for durability analysis is developed. The method connected the reliability of safe life under load spectrum with the crack exceedance probability on the basis of P-S-N curves for structure members crack initiation, the condition is that the crack length reaches economic repairment limit. And the P(i,τ)-τ curves of every stress region are established. Then the structure damage degree is evaluated and the structure economic life is predicted. Finally, a simple example is given.

Key words: durability analysis, crack initiation, economic life