航空学报 > 1987, Vol. 8 Issue (10): 467-475

规范疲劳寿命及其标准差

施泽康   

  1. 空军航空修理研究所
  • 收稿日期:1986-07-01 修回日期:1900-01-01 出版日期:1987-10-25 发布日期:1987-10-25

SPECIFICATION FATIGUE LIFE AND ITS STANDARD ERROR

Shi Zekang   

  1. Air Force Aeronautical Overhaul Research Institute
  • Received:1986-07-01 Revised:1900-01-01 Online:1987-10-25 Published:1987-10-25

摘要: 从理论上严格证明了服从对数正态分布的试验寿命的样本标准差服从S分布,给出了母体标准差的无偏估计公式及纠偏系数表。给出了一定置信度下试验寿命安全标准差的计算公式及计算所必须的表格。提出了规范疲劳寿命的概念,它的标准差是试验寿命标准差的加权平均值。

Abstract: In this paper it is strictly proved in theory that the standard error of the sample of, testing life which obeys logarithm-normal distribution obeys S distribution and the latter is related to the capacity of the sample. In addition,the formulas. and relevant tables are given for making the unbiased estimation of the standard error of parents population and' for calculating the safe standard error of testing life.with these formulas and tables it is able to make fatigue life and reliability analysis.This paper also deals with the concept about specification fatigue life whose standard error is the weighted average of the standard error of testing life.Using the method offered in the paper,the standard error of specification fatigue and fatigue scatter coefficient are calculated on the basis 9f testing data of the materials made in China,and the obtained standard error are in good agreement with the overage of the standard errors used in United States,Britain and Japan.