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Ni3Al基单晶高温合金蠕变本构模型

王荣桥 张斌 胡殿印

王荣桥, 张斌, 胡殿印. Ni3Al基单晶高温合金蠕变本构模型[J]. 航空动力学报, 2018, 33(3): 657-662. doi: 10.13224/j.cnki.jasp.2018.03.019
引用本文: 王荣桥, 张斌, 胡殿印. Ni3Al基单晶高温合金蠕变本构模型[J]. 航空动力学报, 2018, 33(3): 657-662. doi: 10.13224/j.cnki.jasp.2018.03.019
Creep constitutive model of Ni3Al-based single crystal superalloy[J]. Journal of Aerospace Power, 2018, 33(3): 657-662. doi: 10.13224/j.cnki.jasp.2018.03.019
Citation: Creep constitutive model of Ni3Al-based single crystal superalloy[J]. Journal of Aerospace Power, 2018, 33(3): 657-662. doi: 10.13224/j.cnki.jasp.2018.03.019

Ni3Al基单晶高温合金蠕变本构模型

doi: 10.13224/j.cnki.jasp.2018.03.019
基金项目: 国家自然科学基金(51375031,51305012,51675024)

Creep constitutive model of Ni3Al-based single crystal superalloy

  • 摘要: 结合Ni3Al基单晶高温合金蠕变行为的细观机理,在晶体滑移理论的基础上,建立了描述Ni3Al基单晶高温合金蠕变行为的本构模型,并通过ANSYS提供的UPFs二次开发平台对所建立的本构模型进行了有限元实现。利用蠕变试验数据,结合遗传算法获取了两种Ni3Al基材料的蠕变本构模型参数。利用所建立的蠕变本构模型对两种Ni3Al基材料的高温拉伸试件进行了有限元模拟,与试验结果吻合良好。这表明在晶体滑移理论基础上建立的本构模型是合理的,并且能够较好地描述Ni3Al基单晶高温合金三个阶段的蠕变行为,具有一定的应用价值。

     

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出版历程
  • 收稿日期:  2016-09-11
  • 刊出日期:  2018-03-28

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