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一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型

岳珠峰 陶仙德 尹泽勇 李海燕

岳珠峰, 陶仙德, 尹泽勇, 李海燕. 一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型[J]. 应用数学和力学, 2000, 21(4): 373-381.
引用本文: 岳珠峰, 陶仙德, 尹泽勇, 李海燕. 一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型[J]. 应用数学和力学, 2000, 21(4): 373-381.
Yue Zhufeng, Tao Xiande, Ying Zeyong, Li Haiyan. A Crystallographic Model for the Orientation Dependence of Low Cyclic Fatigue Property of a Nickel-Base Single Crystal Superalloy[J]. Applied Mathematics and Mechanics, 2000, 21(4): 373-381.
Citation: Yue Zhufeng, Tao Xiande, Ying Zeyong, Li Haiyan. A Crystallographic Model for the Orientation Dependence of Low Cyclic Fatigue Property of a Nickel-Base Single Crystal Superalloy[J]. Applied Mathematics and Mechanics, 2000, 21(4): 373-381.

一种镍基单晶超合金高温低周疲劳的晶体取向相关性模型

基金项目: 国家自然科学基金;(59501009);航空科学基础研究基金;西安交通大学力学开放实验室开放基金
详细信息
    作者简介:

    岳珠峰(1965~ ),男,江苏丹阳人,教授,博士.

  • 中图分类号: TG113

A Crystallographic Model for the Orientation Dependence of Low Cyclic Fatigue Property of a Nickel-Base Single Crystal Superalloy

  • 摘要: 在950℃t对[001]、[012]、[112]、[011]和[114]晶体取向的镍基单晶超合金DD3试样进行了对称循环低周疲劳(ICF)试验。应变率取1.0×10-2,1.33×10-3,0.33×10-3s-1.试验结果表明,LCF特性显着地取决于晶体取向和应变率。试样断口细观分析表明,除了[001]取向试样外,其余所有试样断口上均有明显的等间距疲劳纹。这些疲劳纹由微裂纹组成,其间距取决于试样的晶体取向和总应变范围。基于晶体滑移理论,建立了疲劳纹间距和总分切应变范围及取向和应变率函数的一个简单关系。对Lall-Chin-Pope(LCP)模型进行修正并推广应用于循环塑性和疲劳寿命研究,提出了一个晶体取向和应变率参数,该参数可以很好地描述镍基单晶超合金高温低周疲劳循环塑性和疲劳寿命的晶体取向和应变率相关性。
  • [1] Jiao F,Bettge D,Osterle W,Ziebs J.Tension-Compression asymmetry of the(001) single crystal nickel-base superalloy SC16 under cyclic loading at elevated temperature[J].Acta Mater,1996,44(10):3933~3942.
    [2] Lall C,Chin S,Pope D P.The orientation and temperature dependence of yield stress of Ni3(Al,Nb)single crystals[J].Metall Trans A,1979,10A(6):1323~1332.
    [3] Takeuchi S,Kuramoto E.Temperature and orientation dependence of yield stress in Ni3Ga single crystals[J].Acta Metall,1973,21(3):415~425.
    [4] Li S X,Smith D J.Temperature and orientation dependence of elastic and yield properties of single crystal nickel-base superalloys[J].Mat Sci Tech,1995,11(7):1253~1260.
    [5] Yue Z F,Zheng C Q.The study of the tension/compression yield behavior of single crystal blade superalloys [J].Acta Aeronautica et Astronautica Sinica,1993,14(12):A556~A559.
    [6] Milligan W W,Antolovich S D.Yielding and deformation behavior of the single crystal superalloy PWA1480[J].Metall Trans A,1987,18A(1):85~95.
    [7] Li S X,Smith D J.High temperature fatigue-creep behaviour of single crystal SRR99 nickel-base superalloy Part I-cyclic mechanical response[J].Fatigue and Fracture of Engineering Materials and Structure,1995,18(5):617~629.
    [8] Li S X,Smith D J.High temperature fatigue-creep behaviour of single crystal SRR99 nickel-base superalloy Part Ⅱ-fatigue-creep life behavior[J].Fatigue and Fracture of Engineering Materials and Structure,1995,18(5):630~643.
    [9] Henderson M B,Martin J W.The influence of crystal orientation on the high temperature fatigue crack growth of a nickel-based signal crystal superalloy[J].Acta Mater,1996,44(1):111~128.
    [10] Yue Z F,Lu Z Z,Zheng C Q.Fracture behavior of a nickel-base single crystal superalloy as predicted by the strain energy density criterion[J].Theoretical and Applied Mechanics,1997,26(1):89~104.
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出版历程
  • 收稿日期:  1997-10-20
  • 修回日期:  1999-03-20
  • 刊出日期:  2000-04-15

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