首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >STRESS-STRAIN STATE PREDICTION OF HIGH-TEMPERATURE TURBINE SINGLE CRYSTAL BLADES USING DEVELOPED PLASTICITY AND CREEP MODELS
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STRESS-STRAIN STATE PREDICTION OF HIGH-TEMPERATURE TURBINE SINGLE CRYSTAL BLADES USING DEVELOPED PLASTICITY AND CREEP MODELS

机译:利用改进的塑性和蠕变模型预测高温涡轮单晶叶片的应力-应变状态

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This paper discusses a novel approach to calculating inelastic strain that incorporates elastic anisotropy in combination with ANSYS finite element analysis (FEA) software to predict the stress-strain state kinetics of a single crystal (SX) nickel-based turbine blade. The approach is based on using "equivalent direction" and allows us to correctly define the critical load value and plastic strain field in SX details for different load types. The suggested approach is simple and generic and requires only a few standard experimental material properties. This should allow for an easy transition to actual blade design application. Predictions of plastic field distribution obtained using the suggested approach with anisotropic specimens are compared with experimental data as well as with the results obtained using a crystallographic approach. Good correlation was achieved. The second goal of this study is to develop a physically based, readily implementable creep model SX superalloy that accurately represents the creep phenomena of these materials under complex, thermomechanical loading conditions.
机译:本文讨论了一种新的计算非弹性应变的方法,该方法结合了弹性各向异性和ANSYS有限元分析(FEA)软件来预测单晶(SX)镍基涡轮叶片的应力-应变状态动力学。该方法基于使用“等效方向”,并允许我们针对不同的载荷类型在SX详细信息中正确定义临界载荷值和塑性应变场。所建议的方法既简单又通用,只需要一些标准的实验材料特性即可。这应该允许轻松过渡到实际的叶片设计应用程序。将使用建议的方法与各向异性样品获得的塑性场分布预测与实验数据以及使用晶体学方法获得的结果进行比较。实现了良好的相关性。这项研究的第二个目标是开发一种基于物理的,易于实现的蠕变模型SX超级合金,该模型可以准确表示这些材料在复杂的热机械载荷条件下的蠕变现象。

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