首页> 外文会议>Gas Turbines Materials Technology Conference >Failure mechanisms during thermal cycling of plasma sprayed Zr{sub}O{sub}2-Y{sub}2O{sub}3 TBC's and the effect of a pre-oxidized NiCrAlY bond coat
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Failure mechanisms during thermal cycling of plasma sprayed Zr{sub}O{sub}2-Y{sub}2O{sub}3 TBC's and the effect of a pre-oxidized NiCrAlY bond coat

机译:等离子体热循环期间的失效机制喷涂Zr {sub} 2-y {sub} 2o {sub} 3 TBC的效果及其对预氧化的幼亮粘合涂层的影响

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The failure mechanism of thermal barrier coatings (TBCs) subjected to a thermal load is still not entirely understood. Thermal stresses and/or oxidation cause the coating to fail and hence must be minimized. We sprayed TBCs up to 1.0 mm with a high intrinsic strength, withstanding the high thermal stresses during thermal cycling and lowering the interface temperature. Further more, we gave the bondcoat a pre-oxidizing treatment before applying a topcoat. The bond strength and the behavior during three different thermal loads of the pre-oxidized TBCs are compared with a standard duplex TBC. With FEM-calculations the occurring stresses during thermal shock are calculated. Bondcoat oxidation and interface roughness are implemented. It is concluded that the TBCs, applied during this research, exhibit excellent thermal shock resistance and that a pre-oxidizing treatment of the bondcoat increases the lifetime during thermal loading. The FE-model gives a first impression of the failure mechanisms during thermal loading, but further development is required.
机译:对热负荷进行热载体(TBC)的热阻挡涂层(TBC)的故障机理仍未完全理解。热应力和/或氧化导致涂层失效,因此必须最小化。我们将TBC喷涂高达1.0毫米,具有高质量强度,热循环期间高热应力并降低界面温度。此外,在施加面涂层之前,我们进一步提高了粘合剂进行预氧化处理。将预氧化TBC的三种不同热负载期间的粘合强度和行为与标准双相TBC进行比较。用FEM计算计算热冲击期间的发生应力。实施粘合剂氧化和界面粗糙度。结论是,在该研究期间应用的TBC表现出优异的热抗震性,并且对粘合剂的预氧化处理在热负荷期间增加了寿命。 Fe-Mobile在热负荷期间给出了失效机制的第一印象,但需要进一步发展。

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