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考虑相关性的同级叶片系统强度可靠度分析方法
引用本文:陆山,高雅娟,吕文林.考虑相关性的同级叶片系统强度可靠度分析方法[J].航空动力学报,2008,23(1):17-20.
作者姓名:陆山  高雅娟  吕文林
作者单位:西北工业大学,动力与能源学院,西安,710072
摘    要:提出了考虑相关性的同级叶片系统强度可靠度分析方法.该方法包括同级叶片强度随机变量相关系数的数值模拟方法、同级叶片强度临界状态函数之间相关系数的确定方法.并给出考虑材料相关性的同级叶片系统可靠度计算二阶窄界限公式.讨论了考虑失效相关的同级叶片系统强度可靠度不同计算方法.最后通过算例表明所提出方法的有效性.

关 键 词:航空、航天推进系统  相关系数  系统可靠度  叶片  数值仿真
文章编号:1000-8255(2008)01-0017-04
收稿时间:2006/12/29 0:00:00
修稿时间:2006年12月29

Analysis method for same-stage-blade system strength reliability concerning the correlation
LU Shan,GAO Ya-juan and L&#; Wen-lin.Analysis method for same-stage-blade system strength reliability concerning the correlation[J].Journal of Aerospace Power,2008,23(1):17-20.
Authors:LU Shan  GAO Ya-juan and L&#; Wen-lin
Institution:LU Shan,GAO Ya-juan,L(U) Wen-lin
Abstract:An analytical method for the strength reliability of the same-stage-blade system was proposed.The method covers numerical simulation and determination of the correlation coefficients of the same-stage-blade material strength and the strength limit state function.Moreover,the narrow limit formula for the same-stage-blade system strength reliability was presented.Then,the reliability calculation methods of the same-stage-blade system strength were discussed by taking into account failure-related factors.Finally,a numerical example of same-stageblade system was given to demonstrate the efficiency of the method.
Keywords:aerospace propulsion system  correlation coefficient  system reliability  blades  simulation
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