首页|Strengthening mechanism and forming control of linear friction welded GH4169 alloy joints

Strengthening mechanism and forming control of linear friction welded GH4169 alloy joints

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Numerical simulation and experimental research on Linear Friction Welding(LFW)for GH4169 superalloy were carried out.Based on the joint microstructure and mechanical properties,a suitable welding process was determined,which provided an important theoretical basis for the manufacture and repair of aeroengine components such as the superalloy blisk.The results show that the joint strain rate gradually increases with the increase of welding frequency,and the defor-mation resistance of the thermoplastic metal increases in the welding process,resulting in the inter-face thermoplastic metal not being extruded in time to form a flash,so the joint shortening amount gradually decreases.The thermoplastic metal in the center of the welding surface is kept at high welding temperature for a long time,resulting in the decrease of the joint strength.The microhard-ness of the joint shows a"W"distribution perpendicular to the weld,and most of the joints break in the Thermo-Mechanically Affected Zone(TMAZ)with high tensile strength and low elongation.When the welding area is increased without changing the aspect ratio of the welding surface,the interface peak temperature increases gradually,and the joint shortening amount decreases with the increase of the welding interface size.

Linear Friction Welding(LFW)MicrostructureMechanical propertiesNumerical simulationJoint shortening amount

Yu SU、Xiawei YANG、Tingxi MENG、Xinyuan HE、Dong WU、Wenya LI、Shuo YIN

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State Key Laboratory of Solidification Processing,School of Materials Science and Engineering,Northwestern Polytechnical University,Xi'an 710072,China

Shaanxi Key Laboratory of Friction Welding Technologies,School of Materials Science and Engineering,Northwestern Polytechnical University,Xi'an 710072,China

Department of Mechanical,Manufacturing and Biomedical Engineering,Parsons Building,Trinity College Dublin,The University of Dublin,Dublin 2,Ireland

国家自然科学基金国家自然科学基金国家自然科学基金中国博士后科学基金Xi'an Beilin District Science and Technology Planning Project,China

5230542052074228518754702023M742830GX2349

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(4)
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