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Thermal Shock Behavior of Nano-Structured Functionally Graded Thermal Barrier Coatings Deposited by Supersonic Plasma Spray

机译:由超声等离子体喷雾沉积的纳米结构功能渐变热阻挡涂层的热冲击行为

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The nano-structured functionally graded 8YSZ/NiCoCrAlY thermal barrier coatings (FG-TBCs) were prepared using a recently developed Supersonic Plasma Spraying (S-PS) system with dual powder feed ports. The alloy powders were fed into the lower temperature regions of the plasma plume through one of them to prevent it over molten and oxidation. The ceramic powders were fed into high temperature regions through another for fully melted. The thermal shock behavior of the FG-TBCs were investigated. It was found the totally 1mm thick FG-TBCs layer still maintained nano-structure form by TEM, and also exhibited a finely lamellate microstructure mixed by alloy and ceramic with gradient along the thickness direction by SEM. The FG-TBCs exhibit excellent thermal shock resistance due to it was still perfect without any spallation after thermal shock test over 200 cycles under heating by oxygen-acetylene flam to 1250°C in 30s and then quenching into ambient water.
机译:使用具有双粉末进料端口的最近开发的超声型等离子体喷涂(S-PS)系统,制备纳米结构功能梯度的8倍/幼级热阻挡涂层(FG-TBCS)。将合金粉末通过其中一个填充到等离子体羽流的较低温度区域中,以防止其熔融和氧化。将陶瓷粉末通过另一个陶瓷粉末进料到高温区域中以完全熔化。研究了FG-TBC的热冲击行为。发现完全1mm厚的FG-TBCS层仍然保持纳米结构形式的TEM,并且还通过SEM沿厚度方向沿厚度方向与梯度混合的细层状微观结构。由于氧 - 乙炔火焰在30℃加热至1250℃下,在热冲击测试之后,FG-TBCS仍然具有优异的热抗震性而没有任何脱模,而不会在200℃加热至1250℃。然后将其淬火到环境水中。

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