航空学报 > 1988, Vol. 9 Issue (3): 113-118

给定寿命下的疲劳裂纹尺寸分布

傅惠民, 高镇同   

  1. 北京航空学院
  • 收稿日期:1987-05-11 修回日期:1900-01-01 出版日期:1988-03-25 发布日期:1988-03-25

DISTRIBUTION OF CRACK SIZES AT A GIVEN LIFE

Fu Hultnin, Gao Zhentong   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1987-05-11 Revised:1900-01-01 Online:1988-03-25 Published:1988-03-25

摘要: 本文论证了疲劳裂纹超值概率和疲劳寿命破坏率之间的等同性。由给定裂纹尺寸下疲劳寿命的分布推导出给定寿命下疲劳裂纹超值概率和疲劳裂纹尺寸分布,建立了三维空间的P-a-t曲面方程。

Abstract: The identity between the probability of occurrence of a crack which is larger than a given crack size a0 at t=t* and the probability of fatigue life which is less than t*at a=a0 is proved in this paper. The functional relation between the distribution of fatigue, life and the. distribution of crack sizes is established by probabilistic approach. In virtue of this relation the probability of crack exceedence and the probability density function of crack sizes at a given life, can be derived from those of fatigue life at a prescribed crack size. A P-a-t surface is also presented in this paper.