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Variation of Thermal Barrier Coating Lifetime Characteristics with Thermal Durability Evaluation Methods

机译:具有热耐久性评估方法的热障涂层寿命特性的变化

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摘要

The thermal durability of thermal barrier coating systems (TBCs) obtained using feedstock powders with different purity and phase content was investigated by thermal shock testing with different cycle times, including the effects on the sintering and phase transformation behaviors. Four 8 wt.% yttria-stabilized zirconia powders, with regular purity (TC1), high purity (TC2 and TC3), and without monoclinic phase (TC4), were employed to prepare the topcoat of TBC by atmospheric plasma spray on a NiCoCrAlY bondcoat deposited by high velocity oxy-fuel. The microstructure and phase stability of the topcoats affected the TBCs' lifetime in the short-term (1h) and long-term (24h) furnace cyclic test (FCT) at 1100 degrees C and jet engine thermal shock (JETS) test. In the short-term FCT and JETS tests, in which coatings are severely subjected to thermal stress, the TBCs' lifetime is most affected by the microstructure of the topcoat. The coating layer with the lowest monoclinic phase in the as-sprayed state showed the lowest phase-transformation characteristics in the isothermal oxidation test (1400 degrees C). These properties resulted in the best lifetime in the long-term FCT. Therefore, the coating material and evaluating methods of TBCs' life should be selected depending on the usage environment.
机译:通过具有不同循环时间的热冲击试验研究了使用具有不同纯度和相含量的原料粉末获得的热阻挡涂层系统(TBC)的热耐久性,包括不同的循环时间,包括对烧结和相变行为的影响。用规则纯度(TC1),高纯度(TC2和TC3),没有单斜相(TC4),用常规纯度(TC2),通过大气等离子体喷雾在NicoScraly粘膜上制备TBC的底涂层,用常规纯度(TC1),高纯度(TC2和TC3),在NicoScly等离子粘膜上制备TBC的底涂层由高速氧燃料沉积。顶涂层的微观结构和相位稳定性在1100℃和喷射发动机热冲击(喷气机)测试中,在短期(1H)和长期(24h)炉循环试验(FCT)中影响TBC的寿命。在短期FCT和喷射试验中,其中涂层严重受到热应力,TBC的寿命受到面涂层的微观结构的影响。涂层具有最低单斜相的涂层在喷雾状态下显示出等温氧化试验(1400℃)中的最低相变特性。这些属性导致长期FCT中最好的寿命。因此,应根据使用环境选择涂层材料和评估TBC生命方法。

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