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Low stress no distortion welding for aerospace shell structures 被引量:3

Low stress no distortion welding for aerospace shell structures
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摘要 To fit in with the strict geometrical integrity and ensure dimensionally consistent fabrication of the welded aerospace structures. the low stress no distortion(LSND)welding, a technique for thin materials, was poineered and developed to provide an ininprocess active control of welding distortion. Satisfactory distortion free results were achieved in both welding of jet engine cases of heat-resistance alloys and rocket fuel tanks of aluminuim alloys, and there need no. reworking operations for post-weld distortion correction. Based on the 'static' method a newly developed method for dvnamic in-process control is also discussed in this paper. Both methods provide quanutiative in-process control of incompatible strains in weld zone and low stress no distortion welding results. To fit in with the strict geometrical integrity and ensure dimensionally consistent fabrication of the welded aerospace structures. the low stress no distortion(LSND)welding, a technique for thin materials, was poineered and developed to provide an ininprocess active control of welding distortion. Satisfactory distortion free results were achieved in both welding of jet engine cases of heat-resistance alloys and rocket fuel tanks of aluminuim alloys, and there need no. reworking operations for post-weld distortion correction. Based on the 'static' method a newly developed method for dvnamic in-process control is also discussed in this paper. Both methods provide quanutiative in-process control of incompatible strains in weld zone and low stress no distortion welding results.
出处 《China Welding》 EI CAS 1996年第1期1-9,共9页 中国焊接(英文版)
关键词 aerospace shell structure residual stress DISTORTION low stress no distortion Welding aerospace shell structure, residual stress, distortion, low stress no distortion Welding
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  • 1M Kumagai.Recent technological developments in welding of aluminium and its alloys[J]. Welding International . 2003 (3)
  • 2LIU Hui-jie.Welding metallurgy and weldability. . 2007
  • 3GUAN Qiao.Several problems in popularizing weld-rolling technology. Aeronautical Manufacturing Technology . 1980
  • 4FANG Hong-yuan.Welded structure. . 2008
  • 5LIU Jing-an,XIE Shui-sheng.Application and development of aluminium alloys. . 2004
  • 6GEAN A,WESTGATE S A,KUCZA J C,EHRSTROM J C.Static and fatigue behavior of spot-welded 5182-0 aluminum alloy sheet. Welding Research Supplement . 1999
  • 7ISHCHENKO A Y.High-strength aluminum alloys for welded structures in the aircraft industry. Welding Research Abroad . 2005
  • 8SASABE S J.Welding properties of aluminum alloys for automotive structures. Welding Research Abroad . 2005
  • 9HAN M S.Fundamental studies on welding-induced distortion in thin plates. . 2002
  • 10Merklein M,Geiger M.New materials and production technologies for innovative lightweight constructions. Journal of Materials . 2002

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