Experimental investigation on surface integrity and fatigue performance of Ti60 alloy under ultrasonic impact treatment

被引:2
|
作者
Yao, Changfeng
Chen, Junlin
Tan, Liang [1 ]
机构
[1] Northwestern Polytech Univ, Key Lab High Performance Mfg Aero Engine, Minist Ind & Informat Technol, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Ultrasonic impact; Ti60; alloy; Surface integrity; Fatigue life; Fatigue fracture; COMPRESSIVE RESIDUAL-STRESS; CRACK-PROPAGATION; TI-6AL-4V ALLOY; ROLLING PROCESS; MACHINED SURFACE; LIFE PREDICTION; ALUMINUM-ALLOY; CARBON-STEEL; GRAIN-SIZE; BEHAVIOR;
D O I
10.1016/j.engfailanal.2024.108639
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The surface integrity and fatigue properties of Ti60 alloy under different ultrasonic impact processes were investigated. Ultrasonic impact treatment (UIT) with various parameters enhanced the surface integrity of the turned specimen. The R a values of the UIT specimens were all less than 0.380 mu m, with the surface stress concentration factor ( K st ) values ranging from 1.075 to 1.120. The compressive residual stress values of the UIT specimens were enhanced, leading to the localization of the maximum residual stress ( sigma rsm ) in the subsurface. Increases in surface residual stress ( sigma s ) values exceeded 21.9 % and sigma rsm values were improved by more than 74.4 % compared to the turned specimen. The microhardness values showed improvement after UIT, with surface microhardness ( HV s ) values ranging from 408.5 HV 0.025 to 461.6 HV 0.025 . The orientation of the grains was deflected in UIT specimens, and the depths of the plastic deformation layer ( h p ) values experienced increases of more than 17 times. The fatigue life ( N f ) value of the Comb. U2 with the best surface integrity was approximately 9328.4 % higher than that of turned and about 4362.1 % higher than that of Comb. U1 with the worst surface integrity among the UIT specimens. Observing the fatigue fractures, the crack initiation locations of the UIT specimens were relocated to the subsurface at a distance of more than 150 mu m from the surface. A higher fatigue life of the specimen was achieved when there was better surface integrity and when the fatigue crack source was located further away from the surface. The crack source in the UIT specimen exhibited a large and irregular shape, and there were numerous small, evenly distributed dimples and a limited number of cleavage planes in fatigue instantaneous fracture region. Additionally, it was found that the subsurface fatigue life prediction model demonstrates superior accuracy for shorter fatigue life.
引用
收藏
页数:20
相关论文
共 50 条
  • [1] Dwell and Normal Cyclic Fatigue Behaviours of Ti60 Alloy
    Lina Yang
    Jianrong Liu
    Jun Tan
    Zhiyong Chen
    Qingjiang Wang
    Rui Yang
    JournalofMaterialsScience&Technology, 2014, 30 (07) : 706 - 709
  • [2] Dwell and Normal Cyclic Fatigue Behaviours of Ti60 Alloy
    Yang, Lina
    Liu, Jianrong
    Tan, Jun
    Chen, Zhiyong
    Wang, Qingjiang
    Yang, Rui
    JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY, 2014, 30 (07) : 706 - 709
  • [3] Microstructure and properties of Ti60 alloy by laser solid forming and ultrasonic impact hybrid manufacturing
    Chen, Wen-jing
    Huang, Chun-ping
    Liu, Feng-gang
    Liang, Ren-yu
    Liu, Fen-cheng
    Yang, Hai-ou
    TRANSACTIONS OF NONFERROUS METALS SOCIETY OF CHINA, 2023, 33 (11) : 3319 - 3331
  • [4] Effects of heat treatment on microstructure and properties of Ti60 alloy
    Jia, Wei-Ju
    Zeng, Wei-Dong
    Zhang, Yao-Wu
    Zhou, Yi-Gang
    Zhongguo Youse Jinshu Xuebao/Chinese Journal of Nonferrous Metals, 2010, 20 (11): : 2136 - 2141
  • [5] On the influence of ultrasonic surface rolling process on surface integrity and fatigue performance of Ti-6Al-4V alloy
    Liu, Chengsong
    Liu, Daoxin
    Zhang, Xiaohua
    He, Guangyu
    Xu, Xingchen
    Ao, Ni
    Ma, Amin
    Liu, Dan
    SURFACE & COATINGS TECHNOLOGY, 2019, 370 : 24 - 34
  • [6] Experimental research on electrochemical machining of titanium alloy Ti60 for a blisk
    Chen Xuezhen
    Xu Zhengyang
    Zhu Dong
    Fang Zhongdong
    Zhu Di
    CHINESE JOURNAL OF AERONAUTICS, 2016, 29 (01) : 274 - 282
  • [7] Experimental research on electrochemical machining of titanium alloy Ti60 for a blisk
    Chen Xuezhen
    Xu Zhengyang
    Zhu Dong
    Fang Zhongdong
    Zhu Di
    Chinese Journal of Aeronautics, 2016, (01) : 274 - 282
  • [8] Experimental research on electrochemical machining of titanium alloy Ti60 for a blisk
    Chen Xuezhen
    Xu Zhengyang
    Zhu Dong
    Fang Zhongdong
    Zhu Di
    Chinese Journal of Aeronautics, 2016, 29 (01) : 274 - 282
  • [9] Effect of ultrasonic impact treatment on the surface integrity of nickel alloy 718
    Zhou, Zheng
    Yao, Chang-Feng
    Zhao, Yu
    Wang, Yang
    Tan, Liang
    ADVANCES IN MANUFACTURING, 2021, 9 (01) : 160 - 171
  • [10] Effect of ultrasonic impact treatment on the surface integrity of nickel alloy 718
    Zheng Zhou
    Chang-Feng Yao
    Yu Zhao
    Yang Wang
    Liang Tan
    Advances in Manufacturing, 2021, 9 : 160 - 171