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Thermal shock resistance of gadolinium zirconate coating with addition of nanostructured yttria partially-stabilized zirconia

机译:添加纳米结构的氧化钇部分稳定的氧化锆后,锆酸g涂层的抗热震性

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摘要

Gadolinium zirconate (Gd_2Zr_2O_7, GZ) as one of the promising thermal barrier coating materials for hightemperature application in gas turbine was toughened by nanostructured 3mol% yttria partially-stabilized zirconia (3YSZ) incorporation. The fracture toughness of the composite of 90mol%GZ-10mol% 3YSZ (GZ-YSZ) was increased by about 60% relative to the monolithic GZ. Both the GZ and GZ-YSZ composite coatings were deposited by atmospheric plasma spraying on Ni-base superalloys and then thermal-shock tested under the same conditions. The thermal-shock resistance of GZ-YSZ composite coating was improved significantly, which is believed to be mainly attributed to the enhancement of fracture toughness by the addition of nanostructured 3YSZ. In addition, the failure mechanisms of the thermal-shock tested GZ and GZ-YSZ composite coatings were also discussed.
机译:通过掺入纳米结构的3mol%氧化钇部分稳定的氧化锆(3YSZ),增韧了锆d(Gd_2Zr_2O_7,GZ)作为一种有前景的燃气轮机高温应用热障涂层材料。相对于整体式GZ,90mol%GZ-10mol%3YSZ(GZ-YSZ)的复合材料的断裂韧性提高了约60%。 GZ和GZ-YSZ复合涂层均通过大气等离子喷涂沉积在镍基高温合金上,然后在相同条件下进行热冲击测试。 GZ-YSZ复合涂层的耐热冲击性得到了显着改善,这主要归因于纳米结构3YSZ的加入,提高了断裂韧性。此外,还讨论了经热冲击测试的GZ和GZ-YSZ复合涂层的失效机理。

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