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

机译:空质喷涂热阻挡涂层应力分布分析非线性热机械耦合建模

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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:研究了空气等离子体喷涂(APS)热阻挡涂层(TBC)对Ni基合金的热机械耦合建模。在计算模型中,研究了TBCS的深度方向的应力分布以及机械性能在加热,居住和冷却热循环中的影响。在建模中考虑了非线性关系(例如,周围环境和涂层之间的对流热传递以及不同层等之间的热传递。结果表明,由于压力松弛,居住阶段的压力显着降低。在BC / TGO界面处的峰值中发生的最大应力,并且在冷却阶段被扩增。此外,当TGO的厚度增加时,BC和TGO层中的内部应力在TBC和Sub的应力基本不变时略有增加。在本作工作中,也模拟了BC涂层的裂缝和BC / TGO界面裂缝。已经研究了TBCS的失效机制I / II,结果表明,由于裂纹繁殖,因此,由于裂纹繁殖,由于裂纹繁殖,因此,BC在峰值附近发生的峰值附近的裂缝附近/ tgo接口。

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