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Thermal cycling behavior of suspension plasma sprayed yttria partially-stabilized zirconia thick thermal barrier coating

机译:悬浮等离子喷涂氧化钇部分稳定氧化锆厚热障涂层的热循环行为

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摘要

The present paper focused on evaluating the cyclic thermal shock performance of the suspension plasma sprayed (SPS) 7.5wt% Y_2O_3 partially stabilized ZrO_2 (7.5YSZ) thick thermal barrier coatings (TBCs). The SPS 7.5YSZ coating in thickness of approximately 720 microns was deposited on a 150 micron-thick CoNiCrAlY bond coat. The vertically segmented cracks were observed in the SPS 7.5YSZ coatings. The phase analysis shows that the coating crystallized in non-transformable tetragonal phase of zirconia. The thermal cycling test of the SPS 7.5YSZ coatings was carried out on a burner rig with propane-oxygen flame which heated the coating surface at temperature of 1523 K, followed by quenching to temperature of 423 K by compressed air. The results obtained shows that the SPS 7.5YSZ coatings performs longer thermal shock life relative to the atmospheric plasma sprayed (APS) counterparts under the same test conditions, which is probably attributed to the improvement in strain tolerance through the vertically segmented cracks therein. The failure behaviour of the SPS coatings is distinctly different from that of the APS coatings, which is supposed to be related to the special microstructure.
机译:本文着重于评估悬浮等离子喷涂(SPS)7.5wt%Y_2O_3部分稳定的ZrO_2(7.5YSZ)厚热障涂层(TBC)的循环热冲击性能。将厚度约为720微米的SPS 7.5YSZ涂层沉积在150微米厚的CoNiCrAlY粘结涂层上。在SPS 7.5YSZ涂层中观察到垂直分段的裂纹。相分析表明,该涂层在氧化锆的不可变形四方相中结晶。 SPS 7.5YSZ涂层的热循环测试是在带有丙烷-氧气火焰的燃烧器装置上进行的,该装置将涂层表面加热到1523 K,然后用压缩空气淬火至423K。获得的结果表明,在相同的测试条件下,SPS 7.5YSZ涂层相对于大气等离子喷涂(APS)涂层具有更长的热冲击寿命,这很可能归因于其中的垂直分段裂纹改善了应变耐受性。 SPS涂层的失效行为与APS涂层的失效行为明显不同,这被认为与特殊的微观结构有关。

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