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Thermal fatigue failure of thermal barrier coatings with a high-Cr MCrAlY bond coat

机译:高Cr MCrAlY粘结涂层的热障涂层的热疲劳失效

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摘要

Thermal barrier coatings (TBCs) were air-plasma sprayed onto Hastelloy X substrates. The TBCs consisted of a high-Cr MCrAlY (M for Ni and Co) bond coat and a yttria-stabilized zirconia (YSZ) top coat. The TBC samples were thermally cycled between 100℃ and 1100℃ with 1 hour dwell time at 1100℃. The thermal fatigue failure of the TBCs was investigated via microstructure analyses. The final fatigue failure of the TBCs was caused by the formation of interface-parallel cracks in the YSZ top coat. The formation of the cracks was found to be strongly related to the oxidation behaviour of the MCrAlY bond coat. The development of the oxide layers was therefore studied in detail. A thermo-kinetic model was also used to deepen the understanding on the elemental diffusion behavior in the materials.
机译:将热障涂层(TBC)空气等离子喷涂到Hastelloy X基片上。 TBC由高铬MCrAlY(对于Ni和Co表示M)键合涂层和氧化钇稳定的氧化锆(YSZ)面涂层组成。将TBC样品在100℃至1100℃之间进行热循环,在1100℃下停留1小时。通过微观结构分析研究了TBC的热疲劳破坏。 TBC的最终疲劳破坏是由YSZ面漆中界面平行裂纹的形成引起的。发现裂纹的形成与MCrAlY键合涂层的氧化行为密切相关。因此,详细研究了氧化物层的发展。还使用热动力学模型来加深对材料中元素扩散行为的了解。

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