航空学报 > 1991, Vol. 12 Issue (2): 123-126

无限寿命可靠性分析方法

傅惠民, 高镇同, 何志敏   

  1. 北京航空航天大学
  • 收稿日期:1990-07-20 修回日期:1990-09-10 出版日期:1991-02-25 发布日期:1991-02-25

A METHOD OF INFINITE-LIFE RELIABILITY ANALYSIS

Fu Huimin, Gao Zhengtong, He Zhimin   

  1. Beijing University of Aeronautics and Astronautics
  • Received:1990-07-20 Revised:1990-09-10 Online:1991-02-25 Published:1991-02-25

关键词: 疲劳, 疲劳门槛值, 无限寿命设计, 可靠性分析

Abstract: A model of ΔK-ΔKth interference is presented, which is applicable to the reliability analysis and design of infinite life for structural members with cracks. By means of the model the reliability of no crack growth may be obtained, and the maximum permissible crack size or load can be determined at a given reliability level.

Key words: fatigue, fatigue threshold, infinite-life design, reliability analysis