航空学报 > 1991, Vol. 12 Issue (7): 365-372

P-S_a-S_m-N曲面的求法

凌静1, 高镇同2   

  1. 1. 北京理工大学 ;2. 北京航空航天大学
  • 收稿日期:1989-11-17 修回日期:1990-04-23 出版日期:1991-07-25 发布日期:1991-07-25

THE METHODS FOR GETTING THE P-S_a-S_m-N CURVED SURFACE

Ling Jing1, Gao Zhentong2   

  1. 1. Beijing Institute of Technology;2. Beij ing University of Aeronautics
  • Received:1989-11-17 Revised:1990-04-23 Online:1991-07-25 Published:1991-07-25

摘要: 本文论述了在疲劳可靠性分析和设计中求P-S_a-S_m-N曲面的必要性,探讨了P-S_a-S_m-N曲面一般形式的选择原则,提出了矩法和最大似然法两种疲劳试验方案,分别给出了根据试验所得的疲劳性能数据求P-S_a-S_m-N曲面的方法,并用实例加以说明。

关键词: 疲劳, 可靠性, 矩法, 最大似然法

Abstract: : The necessity of getting P-Sa-Sm-N curved surface in the fatigue reliability analysis and design is discussed, and the principles for choosing the P-Sa-Sm-N curved surface are given. Two different approaches (moment method and maximum likelihood method) for fatigue tests are presented, and the methods are respectively suggested by which the P=Sa-Sm-N curved surface could be obtained from the data of the above two kinds of fatigue tests.

Key words: fatigue, reliability, moment method, maximum likelihood method