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TC17钛合金激光喷丸应力场及支持向量机应力热松弛模型

李启鹏 李应红 何卫锋 汪诚 仝崇楼

李启鹏, 李应红, 何卫锋, 汪诚, 仝崇楼. TC17钛合金激光喷丸应力场及支持向量机应力热松弛模型[J]. 航空动力学报, 2012, 27(2): 307-311.
引用本文: 李启鹏, 李应红, 何卫锋, 汪诚, 仝崇楼. TC17钛合金激光喷丸应力场及支持向量机应力热松弛模型[J]. 航空动力学报, 2012, 27(2): 307-311.
LI Qi-peng, LI Ying-hong, HE Wei-feng, WANG Cheng, TONG Chong-lou. Residual stress of laser peening processed TC17 and stress relax prediction model based on support vector machines theory[J]. Journal of Aerospace Power, 2012, 27(2): 307-311.
Citation: LI Qi-peng, LI Ying-hong, HE Wei-feng, WANG Cheng, TONG Chong-lou. Residual stress of laser peening processed TC17 and stress relax prediction model based on support vector machines theory[J]. Journal of Aerospace Power, 2012, 27(2): 307-311.

TC17钛合金激光喷丸应力场及支持向量机应力热松弛模型

Residual stress of laser peening processed TC17 and stress relax prediction model based on support vector machines theory

  • 摘要: 对TC17钛合金进行了不同功率密度下激光喷丸强化,使用X射线衍射仪测试了激光喷丸冲击波诱导的残余压应力场的分布,测试了不同温度真空保温下残余压应力的热松弛规律,最后基于支持向量机理论建立了残余压应力热松弛预测模型,并用试验结果对模型进行验证.研究表明:TC17钛合金在功率密度为4GW/cm2时表层残余压应力场最佳;残余压应力在280℃和450℃真空保温150min后分别有11.24%和27.11%的松弛;在280℃和450℃交替保温160min后应力松弛33.9%;残余压应力在试验温度保温160min后有大部分剩余,可以有效提高TC17钛合金抗疲劳性能、基于支持向量机的预测模型能够较精确的表征TC17钛合金的应力松弛规律,满足工程使用要求,对其他材料表层残余压应力热松弛分析具有借鉴意义.

     

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出版历程
  • 收稿日期:  2011-05-29
  • 修回日期:  2011-09-02
  • 刊出日期:  2012-02-28

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