Improvement of fatigue life of Ti-6Al-4V alloy by laser shock peening

被引:249
作者
Zhang, X. C. [1 ]
Zhang, Y. K. [2 ]
Lu, J. Z. [2 ]
Xuan, F. Z. [1 ]
Wang, Z. D. [1 ]
Tu, S. T. [1 ]
机构
[1] E China Univ Sci & Technol, Key Lab Safety Sci Pressurized Syst, MOE, Shanghai 200237, Peoples R China
[2] Jiangsu Univ, Sch Mech Engn, Zhenjiang 212013, Peoples R China
来源
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING | 2010年 / 527卷 / 15期
关键词
Laser shock peening; Multiple laser peening; Residual stress; Fatigue life; Fatigue strength; SURFACE TREATMENTS; FRETTING FATIGUE; RESIDUAL-STRESS; ALUMINUM-ALLOY; BEHAVIOR; STEEL;
D O I
10.1016/j.msea.2010.01.076
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
The aim of this paper was to address the effects of multiple laser peening and laser peening intensity used in laser shock peening (LSP) on the residual stress, micro-hardness and three-point bending fatigue performance of Ti-6Al-4V alloy. The multiple laser peening was accomplished by using the successive laser shocks at the same spot and the laser peening intensity was changed through changing the number of overlapped laser spots. The microstructure, which was characterized by highly tangled and dense dislocation arrangements due to high strain rate, can be found near the surface of the laser-peened specimen. By comparing with the as-received specimen, high micro-hardness and compressive residual stress were introduced at the surface of the laser-peened specimen. With increasing the number of overlapped laser spots, the fatigue life of the laser-peened specimen increased, reached a local maximum and then decreased. The specimen treated by using three overlapped laser spots exhibited the highest fatigue life. When the number of overlapped laser spots was kept to be three, the LSP treatments with one single laser shock and two successive laser shocks respectively provided a 22.2% and 41.7% increase in the fatigue strength as compared with the as-received specimens. (C) 2010 Elsevier B.V. All rights reserved.
引用
收藏
页码:3411 / 3415
页数:5
相关论文
共 21 条
[1]  
BALLARD P, 1991, THESIS ECOLE POLY TE
[2]  
Clauer AH, 1996, SURFACE PERFORMANCE OF TITANIUM, P217
[3]  
CLAUER AH, 1983, LASERS MAT PROCESSIN, P7
[4]   Effect of surface treatments on fretting fatigue of Ti-6Al-4V [J].
Golden, Patrick J. ;
Hutson, Alisha ;
Sundaram, Vasan ;
Arps, James H. .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (07) :1302-1310
[5]   Surface prestressing to improve fatigue strength of components by laser shot peening [J].
Hammersley, G ;
Hackel, LA ;
Harris, F .
OPTICS AND LASERS IN ENGINEERING, 2000, 34 (4-6) :327-337
[6]   Overlapping rate effect on laser shock processing of 1045 steel by small spots with Nd:YAG pulsed laser [J].
Hu, Yongxiang ;
Yao, Zhenqiang .
SURFACE & COATINGS TECHNOLOGY, 2008, 202 (08) :1517-1525
[7]   Effects of fatigue and fretting on residual stresses introduced by laser shock peening [J].
King, A. ;
Steuwer, A. ;
Woodward, C. ;
Withers, P. J. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2006, 435 (12-18) :12-18
[8]   Mechanism of creation of compressive residual stress by shot peening [J].
Kobayashi, M ;
Matsui, T ;
Murakami, Y .
INTERNATIONAL JOURNAL OF FATIGUE, 1998, 20 (05) :351-357
[9]   The effects of laser peening and shot peening on fretting fatigue in Ti-6Al-4V coupons [J].
Liu, Kevin K. ;
Hill, Michael R. .
TRIBOLOGY INTERNATIONAL, 2009, 42 (09) :1250-1262
[10]   Laser shock processing and its effects on microstructure and properties of metal alloys: a review [J].
Montross, CS ;
Wei, T ;
Ye, L ;
Clark, G ;
Mai, YW .
INTERNATIONAL JOURNAL OF FATIGUE, 2002, 24 (10) :1021-1036