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Crystal Orientation Optimization of Nickel-based Single Crystal Turbine Blade

机译:基于镍的单晶涡轮叶片晶体取向优化

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This paper presents a method to optimize crystal orientation of Nickel-based single crystal turbine blade. Total strain range, crystal orientation and temperature range have effect on the low cyclic fatigue life of Nickel-based single crystal superalloy, on other invariable thermo-mechanical cycle conditions. The experiment data of many concerned literatures were analysed and how crystal orientation effect single crystal blade damage and fatigue life was derived. The evaluating method for fatigue life of single crystal superalloy was proposed The 3 dimensional Nickel-based single crystal turbine blade was modeled in MARC program and this finite element model was capable of accounting for primary and secondary crystal orientation variation. Effects of variation in crystal orientation on blade fatigue life were studied based on finite element model with 68 material coordinate systems, by constitutive equation based on crystal slip systems. Result presented demonstrates that control of primary and secondary crystal orientation has the potential to significantly increase turbine blade resistance to fatigue without adding additional weight or cost.
机译:本文介绍了优化镍基单晶涡轮叶片晶体取向的方法。总应变范围,晶体取向和温度范围对镍基单晶超合金的低循环疲劳寿命有影响,在其他不变的热机械循环条件下。分析了许多有关文献的实验数据以及如何衍生出晶体叶片损伤和疲劳寿命。提出了单晶超合金疲劳寿命的评价方法,在MARC程序中建模了3维镍基单晶涡轮机叶片,并且该有限元模型能够考虑初级和次级晶体取向变化。基于晶体滑水系统的组成方程,研究了基于有限元模型的有限元模型研究了晶体取向对叶片疲劳寿命的影响。所提出的结果表明,初级和二级晶体取向的控制具有显着增加涡轮机叶片的抵抗力而不增加额外的重量或成本。

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