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首页> 外文期刊>Journal of Thermal Spray Technology >Behavior of plasma-sprayed thermal barrier coatings during thermal cycling and the effect of a preoxidized NiCrAlY bond coat
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Behavior of plasma-sprayed thermal barrier coatings during thermal cycling and the effect of a preoxidized NiCrAlY bond coat

机译:热循环期间等离子体喷涂的热阻挡涂层的行为及预氧化幼亮粘结粘附的作用

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摘要

The failure mechanisms of thermal barrier coatings (TBCs) subjected to a thermal load are still not entirely understood. Thermal stresses and/or oxidation cause the coating to fail and hence must be minimized. During the present investigation, TBCs up to 1.0 mm were sprayed and withstood high thermal stresses during thermal testing. Owing to the substantial thickness, the temperature at the top coat/bond coat interface was relatively low, resulting in a low oxidation rate. Furthermore, bond coats were preoxidized before applying a top coat. The bond strength and the behavior during three different thermal loads of the preoxidized TBCs were compared with a standard duplex TBC. Finite-element model (FEM) calculations that took account of bond coat preoxidation and interface roughness were made to calculate the stresses occurring during thermal shock. It is concluded that the thick TBCs applied during this research exhibit excellent thermal shock resistance and that a preoxidizing treatment of the bond coat increases the lifetime during thermal loading, where oxidation is the main cause of failure. The FEM analysis gives a first impression of the stress conditions on the interface undulations during thermal loading, but further development is required.
机译:经受热负荷的热阻挡涂层(TBC)的故障机制仍未完全理解。热应力和/或氧化导致涂层失效,因此必须最小化。在本研究期间,在热试验期间喷涂高达1.0 mm的TBC,并在热测试期间受到高热应力。由于厚度大,顶涂层/粘合涂层界面处的温度相对较低,导致氧化率低。此外,在施加顶层之前预氧化粘合涂层。将粘合强度和三种不同热负荷的行为与标准双相TBC进行比较。考虑了粘合涂层预氧化和界面粗糙度的有限元模型(FEM)计算,以计算热冲击期间发生的应力。结论是,在该研究期间施加的厚TBC表现出优异的热抗冲击性,并且粘合涂层的预氧化处理增加了热负荷期间的寿命,其中氧化是失效的主要原因。有限元分析给出了热负荷期间界面起伏的应力条件的第一印象,但需要进一步发展。

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