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金属壳体支座角焊缝应力场数值模拟

秦占领 熊然 张黎旭

宇航材料工艺2018,Vol.48Issue(3):23-26,4.
宇航材料工艺2018,Vol.48Issue(3):23-26,4.DOI:10.12044/j.issn.1007-2330.2018.03.005

金属壳体支座角焊缝应力场数值模拟

Simulation of Welding Residual Stress in Metal Shell Fillet Welds Fabricated by Super-Strength Steel

秦占领 1熊然 1张黎旭1

作者信息

  • 1. 西安航天动力机械有限公司,西安710025
  • 折叠

摘要

Abstract

In this paper,the welding residual stress of metal shell fillet welds which are fabricated by super strength steel is simulated during welding and heat treatment process.Finite element simulation is performed by ANSYS code.The results show that the residual stress is concentrated in heat affected zone of support fillet welds.The peak stress increases with the number of spport fillet welds increaseing.In order to improve the performance of these metal shells,heat treatments (annealing and tempering) are used.It is revealed that the welding residual stress in the fillet welds decreases and redistribs after heat treatments.

关键词

固体发动机/角焊缝/应力场

Key words

Solid motor/Fillet weld/Welding residual stress

分类

矿业与冶金

引用本文复制引用

秦占领,熊然,张黎旭..金属壳体支座角焊缝应力场数值模拟[J].宇航材料工艺,2018,48(3):23-26,4.

宇航材料工艺

OA北大核心CSCDCSTPCD

1007-2330

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