2级钛合金激光冲击强化后的散热及疲劳裂纹动力学特征

IF 1.2 Q4 MATERIALS SCIENCE, MULTIDISCIPLINARY
A. Iziumova, A. Vshivkov, A. Prokhorov, E. Gachegova, D. Davydov
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引用次数: 0

摘要

本文研究了激光冲击强化对带应力集中器的2级钛合金疲劳裂纹扩展速率和裂纹尖端散热的影响。结果表明,LSP对疲劳寿命既有正向影响,也有负向影响。提出了包括应力集中区在内的有效处理方案。这种处理形成了一个最佳的残余应力场,减缓了裂纹的萌生和扩展过程。有效的LSP处理方案降低了应力强度因子的值,从而影响了裂纹尖端的塑性变形强度。这种效应可以通过测量裂纹尖端区域的热流来可视化。在LSP处理的试样中,裂纹尖端的热流密度和裂纹速率都较小。在疲劳裂纹路径附近对LSP处理材料进行的结构研究表明,LSP导致的材料表面出现的结构缺陷(孪晶)对疲劳裂纹扩展没有显著影响,LSP产生的残余应力场的形态起决定性作用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Heat dissipation and fatigue crack kinetic features of titanium alloy Grade 2 after laser shock peening
The work is devoted to experimental investigation of the laser shock peening (LSP) effect on fatigue crack propagation rate and heat dissipation at the crack tip in specimens made of titanium alloy Grade 2 with a stress concentrator. It is shown that the LSP can leads both to positive and negative effect on fatigue lifetime. The effective processing scheme, which includes stress concentrator zone, was proposed. This type of treatment forms an optimal residual stress field, which slows down the crack initiation and propagation processes. The effective LSP processing scheme reduces the value of the stress intensity factor and, as a consequence, effects on an intensity of plastic deformation at the crack tip. This effect can be visualised by measurement of heat flux from the crack tip area. Both heat flux from the crack tip and crack rate are less in the LSP processed specimens. Structural investigations of LSP treated material near fatigue crack path have shown that structural defects (twins) that appear on the surface of the material as a result of LSP do not have a significant effect on the fatigue crack propagation, and the configuration of the residual stresses field created by LSP plays a decisive role.
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来源期刊
Frattura ed Integrita Strutturale
Frattura ed Integrita Strutturale Engineering-Mechanical Engineering
CiteScore
3.40
自引率
0.00%
发文量
114
审稿时长
6 weeks
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