航空学报 > 1995, Vol. 16 Issue (2): 99-103

耐久性分析的特征应力法

王志智, 聂学州, 郑仲   

  1. 飞机结构强度研究所, 西安, 710061
  • 收稿日期:1994-06-14 修回日期:1944-09-27 出版日期:1995-04-25 发布日期:1995-04-25

CHARACTERISTIC STRESS APPROACH FOR DURABILITY ANALYSIS

Wang Zhizhi, Nie Xuezhou, Zheng Minzhong   

  1. Aircraft Structure Strength Research Institute,Xi'an, 710061
  • Received:1994-06-14 Revised:1944-09-27 Online:1995-04-25 Published:1995-04-25

摘要: 给出了以特征应力为参量表示的结构细节的a-s-N曲线。利用此曲线、等寿命曲线和线性累积损伤理论将恒幅载荷下的(aK,NK)数据转换为谱载下的(aK,tK)数据,再由(aK,tK)数据确定当量初始缺陷(EIFS)分布。进而分析裂纹超越数概率和结构损伤度,完成结构耐久性分析。

关键词: 耐久性, 分布参数系统, 裂纹

Abstract: The a-s-N curve expressed by characteristic stress of structural details is presented. Then the ( a K ,N K ) data under constant loading are transformed into the ( a K ,t K ) data under spectrum loading by using Goodman diagram and Miner's rule,and equivalent initial flaw size (EIFS) distribution parameters are obtained by the ( a K ,t K ) data.Finally,the probability of crack exceedance and structural damage degree are calculated and the durability analysis is completed.

Key words: durability, distribution parameters systems, crack

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