Fatigue Property and Small Crack Propagation Mechanism of MIG Welding Joint of 6005A-T6 Aluminum Alloy

被引:11
作者
Peng, Zeng [1 ]
Yang, Shanglei [1 ,2 ]
Wang, Zhentao [1 ]
Gao, Zihao [1 ]
机构
[1] Shanghai Univ Engn Sci, Sch Mat Engn, Shanghai 201620, Peoples R China
[2] Shanghai Laser Intelligent Mfg & Qual Inspect Pro, Shanghai 201620, Peoples R China
基金
中国国家自然科学基金;
关键词
6005A-T6 aluminum alloy; MIG; fatigue; crack propagation; FRICTION STIR WELDS; BEHAVIOR; MICROSTRUCTURE; INITIATION; GROWTH;
D O I
10.3390/ma15134698
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
In this study, metal inert gas welding (MIG) was applied to 4 mm thick 6005A-T6 aluminum alloy welding. Compared with other parts, the hardness of the weld zone (WZ) was the lowest, about 67 HV. There was the Softening in WZ, which might make WZ the weakest zone. Then, fatigue tests were carried out on MIG welded joints. All the fatigue specimens fractured at the weld toe of the lap joint, and the fracture was characterized by a cleavage fracture. Crack closure induced by oxide was observed during the steady propagation of the fatigue crack. Impurities hindered crack propagation, changed the direction of crack propagation, and appeared in stepped fatigue strip distribution morphology; in the process of the main crack propagation, the initiation and propagation of small cracks were easily restricted and hindered by the main crack, which slowed down the propagation rate and even stopped the propagation directly.
引用
收藏
页数:13
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