Residual Stress Measurement and Calibration for A7N01 Aluminum Alloy Welded Joints by Using Longitudinal Critically Refracted (LCR) Wave Transmission Method

被引:14
|
作者
Zhu, Qimeng [1 ]
Chen, Jia [1 ,2 ]
Gou, Guoqing [1 ]
Chen, Hui [1 ]
Li, Peng [3 ]
Gao, W. [4 ]
机构
[1] Southwest Jiaotong Univ, Sch Mat Sci & Engn, Chengdu, Peoples R China
[2] Chengdu Ind & Trade Coll, Chengdu, Peoples R China
[3] CSR Qingdao Sifang Co Ltd, Qingdao, Peoples R China
[4] Univ Auckland, Dept Chem & Mat Engn, PB 92019, Auckland 1142, New Zealand
关键词
A7N01 aluminum alloy welded joints; flight time at free-stress condition (t(0)); initial stress (sigma(0)); longitudinal critically refracted wave (LCR); residual stress measurement; stress coefficient (K); MICROSTRUCTURE CHARACTERIZATION; STEEL; TEMPERATURE;
D O I
10.1007/s11665-016-2271-5
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Residual stress measurement and control are highly important for the safety of structures of high-speed trains, which is critical for the structure design. The longitudinal critically refracted wave technology is the most widely used method in measuring residual stress with ultrasonic method, but its accuracy is strongly related to the test parameters, namely the flight time at the free-stress condition (t (0)), stress coefficient (K), and initial stress (sigma(0)) of the measured materials. The difference of microstructure in the weld zone, heat affected zone, and base metal (BM) results in the divergence of experimental parameters. However, the majority of researchers use the BM parameters to determine the residual stress in other zones and ignore the initial stress (sigma(0)) in calibration samples. Therefore, the measured residual stress in different zones is often high in errors and may result in the miscalculation of the safe design of important structures. A serious problem in the ultrasonic estimation of residual stresses requires separation between the microstructure and the acoustoelastic effects. In this paper, the effects of initial stress and microstructure on stress coefficient K and flight time t (0) at free-stress conditions have been studied. The residual stress with or without different corrections was investigated. The results indicated that the residual stresses obtained with correction are more accurate for structure design.
引用
收藏
页码:4181 / 4189
页数:9
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