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激光冲击强化前处理对TiN/Ti涂层/基体疲劳性能的影响

  • Xin Cao
  • , Weifeng He
  • , Shiguang Wang
  • , Lin Tang
  • , Jingyuan Liu
  • , Jiaxing Hu
  • China Aerodynamics Research and Development Center
  • Air Force Engineering University Xian
  • Aviation University of Air Force

科研成果: 期刊稿件文章同行评审

4 引用 (Scopus)

摘要

The anti-erosion TiN/Ti coating with multilayer gradient structure was prepared on the surface of TC4 titanium alloy by filtered cathodic vacuum arc (FCVA) deposition method. The substrate is subjected to laser shock strengthening pretreatment before deposition. The surface morphologies and mechanical properties of the specimens were characterized by atomic force microscope, nanoindentation, and scratch tester. The fatigue properties of the specimens were evaluated and the fatigue fracture morphologies were analyzed. The results showed that the LSP pretreatment formed a hardened layer with a thickness of about 300 μm, high hardness, and residual compressive stress on the surface of TC4. The average fatigue strength of the TC4 alloy is 373.8 MPa, and the fatigue strength of the sample after preparing the TiN/Ti coating is 363.7 MPa, which is slightly lower than that of the original substrate. The fatigue strength of the sample after LSP-pretreatment is 411.9 MPa, which is 13.3% higher than that of the TiN/Ti coated sample and 10.2% higher than that of the uncoated sample. TiN/Ti coating can inhibit the initiation of cracks on the surface and slow down its growth rate. However, the crack suppression effect is limited when the TiN/Ti coating is broken and peels off from the substrate during the tensile process, and the break of the coating promotes the crack propagation. After LSP pretreatment, the hardened layer formed on the surface of TC4 furtherincreases the difficulty of crack initiation, and the increased bonding strength can reduce the crack growth rate.

投稿的翻译标题Effect of Laser Shock Peening Pretreatment on Thefatigue Properties of TiN/Ticoating/Substrate
源语言繁体中文
页(从-至)120-129
页数10
期刊Zhongguo Biaomian Gongcheng/China Surface Engineering
34
3
DOI
出版状态已出版 - 23 6月 2021
已对外发布

关键词

  • Fatigue property
  • Laser shock peening
  • Ti-6Al-4V alloy
  • TiN/Ti coating

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