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材料导报  2025, Vol. 39 Issue (13): 23110187-5    https://doi.org/10.11896/cldb.23110187
  金属与金属基复合材料 |
单筒排气管焊接有限元模拟及工序优化研究
戴浩1,2,†, 韩海波1,†, 刘湘波1,*, 高远洋1, 孙燕琼1, 池金虎1, 魏艳红1,3
1 南京航空航天大学材料科学与技术学院,南京 211106
2 昌河飞机工业(集团)有限责任公司,江西 景德镇 333002
3 南京航空航天大学无锡研究院,江苏 无锡 214187
Simulation of Single Cylinder Exhaust Pipe Welding and Process Optimization
DAI Hao1,2,†, HAN Haibo1,†, LIU Xiangbo1,*, GAO Yuanyang1, SUN Yanqiong1, CHI Jinhu1, WEI Yanhong1,3
1 College of Materials Science and Technology,Nanjing University of Aeronautics and Astronautics,Nanjing 211106, China
2 Changhe Aircraft Industry(Group) Co.,Ltd., Jingdezhen 333002, Jiangxi, China
3 Wuxi Research Institute, Nanjing University of Aeronautics and Astronautics, Wuxi 214187, Jiangsu, China
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摘要 直升机薄壁排气管焊接结构正面临由焊接残余应力和变形引起的装配难、服役寿命短的问题。通过热弹-塑性有限元法对GH3030单筒排气管TIG焊接过程进行模拟、验证,并对排气管的两道焊缝设计六种焊接工序进行优化研究,以控制焊接残余应力及焊后变形。结果表明:单筒排气管采用先长后短的焊接顺序和焊接方向相反的工艺方案,其焊接应力更小,焊后变形改善效果显著。
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戴浩
韩海波
刘湘波
高远洋
孙燕琼
池金虎
魏艳红
关键词:  热弹-塑性有限元法  氩弧焊  GH3030镍基高温合金  残余应力  残余变形    
Abstract: The welded structure of helicopter thin-walled exhaust pipes is facing problems such as difficulty in assembly and short service life caused by welding residual stress and deformation. The thermal elastic-plastic finite element method was used to simulate and verify the tungsten inert gas (TIG) welding process of the GH3030 single-cylinder exhaust pipe, and optimization research was conducted by designing six welding processes for the two-pass weld of the exhaust pipe, to control the welding residual stress and post-weld deformation. The results show that the welding stress of the single-cylinder exhaust pipe welded by the welding sequence of first long and then short, and the process plan with the opposite welding direction is the smallest, and the post-weld deformation improvement effect is significant.
Key words:  thermal elastic-plastic finite element method    TIG welding    GH3030 nickel-based high temperature alloy    residual stress    residual deformation
出版日期:  2025-07-10      发布日期:  2025-07-21
ZTFLH:  TG404  
通讯作者:  *刘湘波,南京航空航天大学材料科学与技术学院全职科研博士后。目前从事大型复杂焊件冷加工-装配矫形-焊接-热处理过程的多工序有限元模拟研究、金属材料焊接和电弧增材过程凝固显微组织演变的多物理场多尺度相场模拟研究、大型构件电弧增材变形预测和控制技术研究。xiangboliu56@foxmail.com   
作者简介:  戴浩,南京航空航天大学材料科学与技术学院硕士研究生,在魏艳红教授指导下进行研究。目前主要研究领域为航空构件焊接工艺与数值模拟。
韩海波,南京航空航天大学材料科学与技术学院硕士研究生,在魏艳红教授指导下进行研究。目前主要研究领域为航空构件焊接工艺与数值模拟。
†共同第一作者
引用本文:    
戴浩, 韩海波, 刘湘波, 高远洋, 孙燕琼, 池金虎, 魏艳红. 单筒排气管焊接有限元模拟及工序优化研究[J]. 材料导报, 2025, 39(13): 23110187-5.
DAI Hao, HAN Haibo, LIU Xiangbo, GAO Yuanyang, SUN Yanqiong, CHI Jinhu, WEI Yanhong. Simulation of Single Cylinder Exhaust Pipe Welding and Process Optimization. Materials Reports, 2025, 39(13): 23110187-5.
链接本文:  
https://www.mater-rep.com/CN/10.11896/cldb.23110187  或          https://www.mater-rep.com/CN/Y2025/V39/I13/23110187
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