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随机振动载荷下发射装置尾罩疲劳寿命分析

刘万远 张红波

航空兵器Issue(4):78-80,3.
航空兵器Issue(4):78-80,3.DOI:10.19297/j.cnki.41-1228/tj.2016.04.014

随机振动载荷下发射装置尾罩疲劳寿命分析

Fatigue Life Prediction on Launcher Trail Cover under Random Vibration Loadings

刘万远 1张红波2

作者信息

  • 1. 中国空空导弹研究院,河南洛阳 471009
  • 2. 驻中国空空导弹研究院军事代表室,河南洛阳 471009
  • 折叠

摘要

Abstract

For the problem of fatigue failure on launcher trail cover in random vibration test , the ran-dom vibration fatigue life is estimated by finite element method .The stress transfer function is obtained by frequency response simulation .Combined with S-N curve of 5 A06 aluminium alloy and acceleration power spectral density loads , random vibration fatigue life of trail cover is analyzed by Dirlik method .The results meet the requirements of random vibration test .

关键词

疲劳寿命/随机振动/尾罩/发射装置/有限元分析

Key words

fatigue life/random vibration/trail cover/launcher/finite element analysis

分类

航空航天

引用本文复制引用

刘万远,张红波..随机振动载荷下发射装置尾罩疲劳寿命分析[J].航空兵器,2016,(4):78-80,3.

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