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Ni基单晶叶片粘塑性分析
岳珠峰1, 吕震宙1, 郑长卿1, 尹泽勇2
1.西北工业大学工程力学系;2.南华动力机械研究所
摘要:
从位错滑移机理出发,建立了一种适用于Ni基高温单晶结构分析用的晶体滑移粘塑性本构模型。该模型将八面体、十二面体及六面体滑移系作为潜在的开动滑移系,考虑阻应力和背应力两种内应力状态参量。利用某Ni基单晶叶片材料在700℃和950℃的试验结果对模型进行了考核并标定了模型参数。进而将所建模型编入有限元结构分析软件中,对某型发动机单晶叶片进行了计算分析。
关键词:  叶片  镍基合金  粘塑性  应变率  有限元法  本构方程
DOI:
分类号:V232.4
基金项目:航空基金,西安交大力学开放基金
A VISCOPLASTIC CRYSTALLOGRAPHIC ANALYSIS OF A NICKEL-BASE SINGLE CRYSTAL BLADE
Yue Zhufeng1, Lu Zhenzhou1, Zheng Changqing1, Yin Zeyong2
1.Dept.of Engineering Mechanics,Northwestern Polytechnical Unly.,Xi’an,710072;2.Nanhua Powerplant Research lust’, Zhuzhou,412002
Abstract:
Based on dislocation theory,an unified anisotrOPic crystallographic constitute has been developed for nickel-base single crystal superalloys.Detahedral{111} <110>,{111}<112> and cubic{100}<110> slip systems are consdered in the model.The constitute utilizes drag stress and back stress state variables to model the local inelastic flow.The model was tested with the experiments of nickel-base crystal superalloy DD3 at 700 ℃ and 950℃ The model parameters have been also simultaneously obtained at the two temperatures.The constitute has been implemented into a structure finite element program. The strength and life of a nickel-base single crystal turbine blade have been calculated.
Key words:  Blade  Nickel base superalloy  Viscoplasticity  Strain rate  Finite element method  Constitutive equation