Microstructure Evolution of Ti834 Alloy Subjected to Laser Shock Processing in Strengthening Layer

被引:0
|
作者
Zan Yaoxu [1 ,2 ]
Jia Weiju [2 ]
Zhao Hengzhang [2 ]
Fan Jianfeng [1 ]
Mao Xiaonan [2 ]
Zhou Lian [2 ]
机构
[1] Taiyuan Univ Technol, Taiyuan 030024, Peoples R China
[2] Northwest Inst Nonferrous Met Res, Xian 710016, Peoples R China
关键词
laser shock processing; near alpha-titanium alloy; microstructure evolution; plastic deformation; strain rate; MECHANICAL-PROPERTIES; RESIDUAL-STRESSES; FATIGUE BEHAVIOR; GRAIN-REFINEMENT; TITANIUM-ALLOY;
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Laser shock processing (LSP), also known as laser peening, is a novel surface strengthening treatment technology, which is capable of introducing residual compressive stress, improving performance of fatigue strength and micro-hardness. With its preferable reinforcement effect, strong controllability and outstanding adaptability, LSP plays an irreplaceable role in improving the service life of key components. The evolution of microstructure in the plastic deformation layer of Ti834 alloy subjected to LSP impacts was investigated by transmission electron microscopy (TEM), and the microstructure evolution model in the surface layer and along depth direction was established. The results indicate that numerous dislocations are generated in the plastic deformation layer of Ti834 alloy subjected to LSP, and the plastic deformation becomes more intense and the dislocation density further increases as the number of impacts increases. Typical microstructure features due to decreasing strain rates can be observed along the depth direction, including mechanical twins (MTs), dense density dislocation walls (DDWs), dislocation tangles (DTs), dislocation arrays (DAs) and dislocation lines (DLs).
引用
收藏
页码:343 / 348
页数:6
相关论文
共 22 条
  • [1] Prediction and characterization of residual stresses from laser shock peening
    Brockman, Robert A.
    Braisted, William R.
    Olson, Steven E.
    Tenaglia, Richard D.
    Clauer, Allan H.
    Langer, Kristina
    Shepard, Michael J.
    [J]. INTERNATIONAL JOURNAL OF FATIGUE, 2012, 36 (01) : 96 - 108
  • [2] Laser shock peening of Ti-17 titanium alloy: Influence of process parameters
    Cellard, C.
    Retraint, D.
    Francois, M.
    Rouhaud, E.
    Le Saunier, D.
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2012, 532 : 362 - 372
  • [3] Laser-shock processing effects on surface microstructure and mechanical properties of low carbon steel
    Chu, JP
    Rigsbee, JM
    Banas, G
    Elsayed-Ali, HE
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1999, 260 (1-2): : 260 - 268
  • [4] Grain size dependence of the fatigue behaviour of a ultrafine-grained AISI 304 stainless steel
    Di Schino, A
    Kenny, JM
    [J]. MATERIALS LETTERS, 2003, 57 (21) : 3182 - 3185
  • [5] Surface prestressing to improve fatigue strength of components by laser shot peening
    Hammersley, G
    Hackel, LA
    Harris, F
    [J]. OPTICS AND LASERS IN ENGINEERING, 2000, 34 (4-6) : 327 - 337
  • [6] Hill MR, 2003, ADV MATER PROCESS, V161, P65
  • [7] Research on the thermal stability of a near α titanium alloy before and after laser shock peening
    Jia, Weiju
    Zhao, Hengzhang
    Hong, Quan
    Li, Lei
    Mao, Xiaonan
    [J]. MATERIALS CHARACTERIZATION, 2016, 117 : 30 - 34
  • [8] Jia Weiju, 2013, CHINESE J NONFERROUS, V23, P29
  • [9] Effects of fatigue and fretting on residual stresses introduced by laser shock peening
    King, A.
    Steuwer, A.
    Woodward, C.
    Withers, P. J.
    [J]. MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2006, 435 (12-18): : 12 - 18
  • [10] Microstructural response and grain refinement mechanism of commercially pure titanium subjected to multiple laser shock peening impacts
    Lu, J. Z.
    Wu, L. J.
    Sun, G. F.
    Luo, K. Y.
    Zhang, Y. K.
    Cai, J.
    Cui, C. Y.
    Luo, X. M.
    [J]. ACTA MATERIALIA, 2017, 127 : 252 - 266