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Three-dimensioanl, finite deformation, rate-dependent plasticity in single-crystal nickel alloys at elevated temperatures

机译:高温下单晶镍合金中的三维有限变形率依赖的塑性

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摘要

Future increases in gas turbine performance will require numerical algorithms capable of predicting the deformation and rupture of blade materials at elevated temperatures. The current generation of Ni-based superalloys requires constitutive models for rate-deponent plastic deformation of single-crystal turbine blades. Ni-based superalloys show a complicated relationship between temperature adn slip on octahedral or cubic slip systems. Ni-based superalloys show a complicated relationship between temperature and slip on octahedral or cubic slip systems, including softening. A three demsional (3-D) finite deformation algorithm is presented for finite element analysis (FEA) of stress and strain histories in anisotropic elastic materials with rate-dependent slip on specific, multiples slip systems. The FEA includes multiplicative decomposition of the deformation gradients, Hencky strain tensor, and Green-Naghdi stress rate with temperature-dependent crystal slip relations to compute finite deformation, slip induced rotations and material softening. Deformation predictions of Ni-based superalloys are compared with experimental measurements and analytical solutions. Good agreement is found, especially when the specimen-to-specimen variations are considered.
机译:燃气轮机性能的未来提高将需要能够预测高温下叶片材料的变形和破裂的数值算法。当前一代的镍基高温合金要求本构模型用于单晶涡轮叶片的速率响应塑性变形。镍基高温合金显示八面体或立方滑移系统的温度和滑移之间存在复杂的关系。镍基高温合金在八面体或立方滑动系统上显示出温度与滑动之间的复杂关系,包括软化。提出了一种针对各向异性弹性材料的应力和应变历史的有限元分析(FEA)的三元(3-D)有限变形算法,在特定的多次滑动系统上具有与速率相关的滑动。有限元分析包括变形梯度,Hencky应变张量和Green-Naghdi应力率的乘法分解,以及与温度相关的晶体滑动关系,以计算有限的变形,滑动引起的旋转和材料软化。将镍基高温合金的变形预测与实验测量和分析解决方案进行比较。发现良好的一致性,尤其是考虑到样本之间的差异时。

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