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Simulation and verification of near-net shaping a complex-shaped turbine disc by hot isostatic pressing process

机译:热等静压过程对复杂形状涡轮盘近净成形的仿真与验证

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摘要

A new constitutive relation for powder materials used in finite element analysis (FEA) of hot isostatic pressing (HIP) complex-shaped parts was derived from Perzyna's elastic-viscoplasticity equations, and the stick-slip boundary modelling and thermomechanical coupling solution were achieved. The temperature-dependent mechanical and thermal parameters were determined through experiments. A complex-shaped turbine disc from Inconel 625 alloy has been simulated and produced. The predicted dimensions and relative densities have been compared with those measured from the experiments, which shows a good agreement for most regions of the turbine disc. The reasons for local predicted discrepancies and physical defects were discussed, and future improvements for FEA simulation and HIP process were outlined.
机译:根据Perzyna的弹黏塑性方程,推导了用于热等静压(HIP)复杂形状零件有限元分析(FEA)中的粉末材料的一种新的本构关系,并获得了粘滑边界模型和热机械耦合解决方案。通过实验确定了温度相关的机械和热参数。模拟并生产了由Inconel 625合金制成的复杂形状的涡轮盘。预测的尺寸和相对密度已经与从实验中测得的尺寸和相对密度进行了比较,这表明涡轮盘的大多数区域都具有良好的一致性。讨论了局部预测的差异和物理缺陷的原因,并概述了FEA模拟和HIP工艺的未来改进。

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