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Thermal cycling behavior of nanostructured 8YSZ, SZ/8YSZ and 8CSZ/8YSZ thermal barrier coatings fabricated by atmospheric plasma spraying

机译:由大气等离子喷涂制造的纳米结构80SZ,Sz / 8苏斯和8CSZ / 8苏斯热屏蔽涂层的热循环行为

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摘要

The nanostructured single-ceramic-layer (SCL) 8YSZ thermal barrier coatings (TBCs), double-ceramic-layer (DCL) Sm2Zr2O7 (SZ)/8YSZ and SZ doped with 8 wt% CeO2 nanoscale particles (8CSZ)/8YSZ TBCs were fabricated by atmospheric plasma spraying (APS) on nickel-based superalloy substrates with NiCoCrAlY as the bond coating. The thermal cycling behavior of the three as-sprayed TBCs was investigated systematically at 1000 degrees C and 1200 degrees C. The results reveal that the thermal cycling lifetime of the nanostructured DCL 8CSZ/8YSZ TBCs is the longest among them, which is largely due to the fact that the intermediate layer buffer effect of the DCL structure, more porosity and improvement of thermal expansion coefficient from doping CeO2 nanoparticles can relieve thermal stress to a great extent at elevated temperature. The failure mechanism of the nanostructured TBCs has been discussed in detail.
机译:用8wt%CeO2纳米粒子(8CSZ)/ 8YSZ TBCS掺杂掺杂8wt%CeO2纳米粒子(8CSZ)/ 8000SZ TBC的纳米结构的单陶瓷层(SCL)8毫秒的热阻挡涂层(TBCS),双陶瓷层(DCL)SM2ZR2O7(SZ)/ 8000SZ和SZ 通过大气压等离子体喷涂(APS)在基于镍的超合金基材上,具有NicoCraly作为键合涂层。 系统地在1000℃和1200摄氏度下系统地研究了三种喷雾的TBC的热循环行为。结果表明,纳米结构DCL 8CSZ / 8YSZ TBCS的热循环寿命是它们中最长的,这主要是由于 DCL结构的中间层缓冲效应,从掺杂CeO2纳米颗粒的热膨胀系数的中间层缓冲效应可以在很大程度上在很大程度上升高热应力。 已经详细讨论了纳米结构TBC的破坏机理。

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