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程序载荷下疲劳可靠性分析的损伤等效递推方法
引用本文:谢里阳,胡俏,林文强.程序载荷下疲劳可靠性分析的损伤等效递推方法[J].航空学报,1995,16(2):113-115.
作者姓名:谢里阳  胡俏  林文强
作者单位:东北大学机械设计系, 沈阳, 110006
基金项目:霍英东教育基金,国家教委科学基金
摘    要:以载荷循环数-疲劳寿命干涉模型为基础,分析了程序载荷(包括随机载荷历程)作用下的疲劳可靠性问题的特点及计算方法。通过对疲劳失效过程的分析,针对复杂载荷下疲劳问题的物理本质,提出了一个以损伤等效原则转换不同载荷水平的当量循环数的可靠性递推方法,并进行了试验验证。

关 键 词:疲劳  可靠性  损伤  
收稿时间:1993-02-15
修稿时间:1994-04-01

DAMAGE EQUIVALENT RECURRENCE METHOD OF FATIGUE RELIABILITY ANALYSIS UNDER PROGRAM LOADING
Xie Liyang,Hu Qiao,Lin Wenqiang.DAMAGE EQUIVALENT RECURRENCE METHOD OF FATIGUE RELIABILITY ANALYSIS UNDER PROGRAM LOADING[J].Acta Aeronautica et Astronautica Sinica,1995,16(2):113-115.
Authors:Xie Liyang  Hu Qiao  Lin Wenqiang
Institution:Department of Mechanism Design,Northeastern University, Shenyag,110006
Abstract:ased on load cycle fatigue life interference model,the character as well as the calculating method of fatigue reliability under program loading is analyzed。Contrary to the traditional method using a recurrence formula according to “equivalent failure probability” to transform fatigue damage under different load levels and calculate reliability, according to the analysis on fatigue process and its physical nature,a “damage equivalent” recurrence method is proposed. Experiment under multi level load condition shows that the error of the “damage equivalent” recurrence formula is equal to 32.8%,while that of the “equivalent failure probability” recurrence formula is as high as 96.8%.
Keywords:fatgue  (forces)  reliability  damage  
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