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有限元分析在大推力火箭动力系统试验台承力架结构优化中的应用

孔凡超 沈冰妹 胡旭坤

火箭推进2011,Vol.37Issue(5):41-46,6.
火箭推进2011,Vol.37Issue(5):41-46,6.

有限元分析在大推力火箭动力系统试验台承力架结构优化中的应用

Application of FEA in structure optimization of load-bearing frame of propulsion system test-bed for large-thrust rockets

孔凡超 1沈冰妹 1胡旭坤1

作者信息

  • 1. 北京航天试验技术研究所,北京100074
  • 折叠

摘要

Abstract

The FEA software ANSYS is used in this study to construct the finite element model of the load-bearing frame of a certain propulsion system test-bed,and analyze the stess distribution of the load-bearing frame under the test and ready-tested status.The structure and layout of the loadbearing beam are optimized according to the results of stress analysis to make the strength of the model meet the working requirements.The stress analysis and optimization are also made on the legs of the load-bearing ring,part of the frame.The mode of the frame is studied at last.Its axial first-order mode is within the range of the axial first-order mode of UUT,so further measures should be taken to avoid resonance.

关键词

有限元分析/承力架/动力系统试验

Key words

FEA/load-bearing frame/propulsion system testing

分类

航空航天

引用本文复制引用

孔凡超,沈冰妹,胡旭坤..有限元分析在大推力火箭动力系统试验台承力架结构优化中的应用[J].火箭推进,2011,37(5):41-46,6.

基金项目

中国航天科技集团公司支撑项目 ()

火箭推进

OACSTPCD

1672-9374

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