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Nonlinear thermo-mechanical coupled modeling for the analysis of stress distribution in air-plasma-sprayed thermal barrier coatings

机译:非线性热力耦合建模,用于分析等离子喷涂热障涂层中的应力分布

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Thermo-mechanical coupled modeling of air-plasma-sprayed (APS) thermal barrier coatings (TBCs) on Ni-based alloy was investigated. In the computational models, the stress distribution in the depth direction of the TBCs and also the influence of mechanical properties in heating, dwelling and cooling thermal cycles, were investigated. Nonlinear relationship (e.g., convective heat transfer between surrounding environment and coatings, and thermal transfer between the different layers etc.) was considered in the modeling. The results showed that the stress significantly reduced in the dwelling stage because of stress relaxation. The maximum stress occurred in the peak at the BC/TGO interface and it was amplified at the cooling stage. Moreover, the internal stress in the BC and TGO layer had a slight increase when TGO's thickness increased whilst the stress in the TBC and Sub were essentially unchanged. In the present work, the cracks in BC coating and the BC/TGO interface cracks were simulated as well. The failure mechanism Ⅰ/Ⅱ of TBCs had been investigated and the results showed that there was no stress concentration in the vicinity of cracks near the peak at the top coating layer, however, due to crack propagation, factures happened near the peak at the BC/TGO interface.
机译:研究了镍基合金上空气等离子喷涂(APS)热障涂层(TBC)的热力耦合建模。在计算模型中,研究了TBC深度方向上的应力分布,以及在加热,驻留和冷却热循环中力学性能的影响。在建模中考虑了非线性关系(例如,周围环境与涂层之间的对流传热,以及不同层之间的热传递等)。结果表明,由于应力松弛,在居住阶段应力显着降低。最大应力出现在BC / TGO界面的峰值处,并在冷却阶段被放大。此外,当TGO的厚度增加时,BC和TGO层的内部应力略有增加,而TBC和Sub的应力则基本不变。在目前的工作中,还对BC涂层的裂纹和BC / TGO界面裂纹进行了模拟。研究了TBCs的破坏机理Ⅰ/Ⅱ,结果表明在顶涂层顶峰附近的裂纹附近没有应力集中,但是由于裂纹扩展,在BC峰附近发生了断裂。 / TGO界面。

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