Microstructure, mechanical properties and stress corrosion behavior of friction stir welded joint of Al-Mg-Si alloy extrusion

被引:5
|
作者
Lin, Sen [1 ]
Deng, Yun-Lai [1 ,2 ,3 ]
Lin, Hua-Qiang [1 ,4 ]
Ye, Ling-Ying [1 ,3 ]
Zhang, Zhen [2 ]
Ji, Hua [2 ]
Zhang, Xin-Ming [1 ,2 ]
机构
[1] Cent South Univ, Sch Mat Sci & Engn, Changsha 410083, Peoples R China
[2] Cent South Univ, Light Alloy Res Inst, Changsha 410083, Peoples R China
[3] Guangxi Liuzhou Yinhai Aluminum Co Ltd, Liuzhou 545006, Peoples R China
[4] CRRC Qingdao Sifang Co Ltd, Natl Engn Res Ctr High Speed EMU, Qingdao 266000, Peoples R China
基金
中国国家自然科学基金;
关键词
EBSD; Slow strain rate test; Stress corrosion cracking; Al-Mg-Si alloy; Friction stir welding; ALUMINUM-ALLOY; FATIGUE LIFE; 6061-T6; EVOLUTION; DEFECTS; GAS; ZR;
D O I
10.1007/s12598-018-1126-7
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Microstructure, mechanical properties and stress corrosion behavior of friction stir welded (FSWed) Al-Mg-Si alloy were investigated. The average grain sizes of shoulder-affected zone (SAZ), nugget zone (NZ), heat-affected zone (HAZ) and base material (BM) are 6.03, 4.80, 168.30 and 127.24 mu m, respectively. The thermo-mechanically affected zone (TMAZ), which is generated on the edge position between HAZ and weld nugget zone, has a narrow width of 400 mu m. The ultimate tensile strength (UTS) of FSWed joint is 232.20 MPa, about 91.04% with respect to that of base material of 255.06 MPa, and the joint fracture occurs at HAZ on advancing side (AS). The FSWed joint is more susceptive to stress corrosion cracking (SCC) than base material, and the SCC susceptibility increases with the rise in temperature. The residual UTS of FSWed joints in constant loaded tests at the load levels of 90, 105 and 120 MPa is 89.97%, 67.50% and 54.75% of the UST of FSWed joint in air, respectively. The increase of the load in constant loaded tests and four-point beam-bent tests accelerates the SCC of FSWed joints.
引用
收藏
页码:2057 / 2067
页数:11
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