Cyclic deformation behavior of linear friction welded Ti6A14V joints

被引:21
作者
Wen, G. D. [1 ,2 ]
Ma, T. J. [1 ]
Li, W. Y. [1 ]
Li, J. L. [1 ]
Guo, H. Z. [1 ]
Chen, D. L. [2 ]
机构
[1] Northwestern Polytech Univ, Shaanxi Key Lab Frict Welding Technol, State Key Lab Solidificat Proc, Xian 710072, Shaanxi, Peoples R China
[2] Ryerson Univ, Dept Mech & Ind Engn, Toronto, ON M5B 2K3, Canada
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2014年 / 597卷
基金
加拿大创新基金会; 中国国家自然科学基金; 加拿大自然科学与工程研究理事会;
关键词
Titanium alloys; Linear friction welding; Low cycle fatigue; Microstructure; FATIGUE BEHAVIOR; MECHANICAL-PROPERTIES; TITANIUM-ALLOY; ELECTRON-BEAM; TI-6AL-4V ALLOY; YOUNGS MODULUS; MICROSTRUCTURE; TENSILE;
D O I
10.1016/j.msea.2014.01.006
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
This study was aimed at characterizing microstructural change and fatigue properties of linear friction welded (LFWed) Ti6AI4V joints with special attention to the relationship between the microstructure and cyclic deformation behavior. The welding process resulted in a remarkable microstructure change across the LFWed joint. The microstructure of the joint consisted of fine subgrains in the weld zone (WZ) and elongated grains in the thermomechanically affected zone (TMAZ), leading to a significantly higher hardness in the WZ. Both the base metal (BM) and joint exhibited essentially symmetrical hysteresis loops and equivalent fatigue life, while the cyclic strain hardening exponent of the welded joint was lower. Cyclic stabilization appeared at lower strain amplitudes up to 0.6% in both the BM and joint, however, cyclic softening occurred at higher strain amplitudes. Fatigue failure was observed to occur in the BM, and fatigue crack initiated from the specimen surface or near-surface defect. Fatigue crack propagation was basically characterized by fatigue striations, together with some secondary cracks. (C) 2014 Elsevier B.V. All rights reserved.
引用
收藏
页码:408 / 414
页数:7
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