Effect of laser shock processing on fatigue life of fastener hole

被引:32
作者
Zhang, Xing-quan [1 ]
Chen, Liu-san [1 ]
Yu, Xiao-liu [1 ]
Zuo, Li-sheng [1 ]
Zhou, Yu [1 ]
机构
[1] Anhui Univ Technol, Sch Mech Engn, Maanshan 243002, Peoples R China
基金
中国国家自然科学基金;
关键词
laser shock processing; fastener hole; fatigue life; LY12CZ; ALUMINUM-ALLOY; RESIDUAL-STRESSES; BEHAVIOR;
D O I
10.1016/S1003-6326(14)63150-2
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
The fatigue properties of laser shock processing (LSP) on both side surfaces of fastener hole with diameter of 3 mm in the LY12CZ aluminum alloy specimens were investigated. The superficial residual stress was measured by X-ray diffraction method. Fatigue experiments of specimens with and without LSP were performed, and the microstructural features of fracture of specimens were characterized by scanning electron microscopy (SEM). The results indicate that the compressive residual stress can be induced into the surface of specimen, and the fatigue life of the specimen with LSP is 3.5 times as long as that of specimen without LSP. The location of fatigue crack initiation is transferred from the top surface to the sub-surface after LSP, and the fatigue striation spacing of the treated specimen during the expanding fatigue crack is narrower than that of the untreated specimen. Furthermore, the diameters of the dimples on the fatigue crack rupture zone of the specimen with LSP are relatively bigger, which is related to the serious plastic deformation in the material with LSP.
引用
收藏
页码:969 / 974
页数:6
相关论文
共 23 条
[1]   The effect of cold expansion on improving the fatigue life of fastener holes [J].
Chakherlou, TN ;
Vogwell, J .
ENGINEERING FAILURE ANALYSIS, 2003, 10 (01) :13-24
[2]  
DING Chuan-fu, 1994, ACTA AERONAUTICA AST, V15, P960
[3]  
Forget P., 1990, Materials and Manufacturing Processes, V5, P501, DOI 10.1080/10426919008953275
[4]  
FROST N E, 1987, WANG REN ZHI WU PEI, P125
[5]   Experimental investigation and fatigue life prediction for 7475-T7351 aluminum alloy with and without shot peening-induced residual stresses [J].
Gao, Y. K. ;
Wu, X. R. .
ACTA MATERIALIA, 2011, 59 (09) :3737-3747
[6]   Fatigue in laser shock peened open-hole thin aluminium specimens [J].
Ivetic, Goran ;
Meneghin, Ivan ;
Troiani, Enrico ;
Molinari, Gianluca ;
Ocana, Jose ;
Morales, Miguel ;
Porro, Juan ;
Lanciotti, Agostino ;
Ristori, Vjola ;
Polese, Claudia ;
Plaisier, Jasper ;
Lausi, Andrea .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2012, 534 :573-579
[7]  
Li Yuan, 2011, Journal of Mechanical Engineering, V47, P43, DOI 10.3901/JME.2011.22.043
[8]  
LING Chao, 1991, ACTA AERONAUTICA AST, V12, P83
[9]   Grain refinement mechanism of multiple laser shock processing impacts on ANSI 304 stainless steel [J].
Lu, J. Z. ;
Luo, K. Y. ;
Zhang, Y. K. ;
Sun, G. F. ;
Gu, Y. Y. ;
Zhou, J. Z. ;
Ren, X. D. ;
Zhang, X. C. ;
Zhang, L. F. ;
Chen, K. M. ;
Cui, C. Y. ;
Jiang, Y. F. ;
Feng, A. X. ;
Zhang, L. .
ACTA MATERIALIA, 2010, 58 (16) :5354-5362
[10]   Grain refinement of LY2 aluminum alloy induced by ultra-high plastic strain during multiple laser shock processing impacts [J].
Lu, J. Z. ;
Luo, K. Y. ;
Zhang, Y. K. ;
Cui, C. Y. ;
Sun, G. F. ;
Zhou, J. Z. ;
Zhang, L. ;
You, J. ;
Chen, K. M. ;
Zhong, J. W. .
ACTA MATERIALIA, 2010, 58 (11) :3984-3994