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Substructure formation mechanism and high temperature performance in CoNiCrA1Y seal coating by laser melting deposition with inside-laser coaxial powder feeding

机译:用内激光同轴粉末激光熔化沉积蛋白拉1Y密封涂层的亚结构形成机理和高温性能

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摘要

CoNiCrAlY coating with good bonding strength to the substrate, moderate hardness and fine integrity was produced by laser melting deposition inside-laser coaxial powder feeding, which is a promising seal coating for aircraft engine. Solidification mechanism of CoNiCrAlY coating was investigated to clarify the evolution of grains and substructures by SEM, XRD and TEM. Effect of cellular and dendritic substructure morphology with Y2O3 on the high temperature friction and oxidation behavior in CoNiCrAlY seal coating was also evaluated. The oxidation results of different temperature indicated that oxidation resistance of CoNiCrAlY coating is excellent. A continuous and protective Cr2O3 external oxide layer formed on coating surface at 873 K, while a more protective Al2O3 oxide layer formed on the coating surface at 1423 K. In-situ Y2O3 particles formed in CoNiCrAlY coating were thought to be beneficial for anchoring the oxide layer. The friction behavior at high temperature depends on substructure morphology. Wear resistance of CoNiCrAlY coating is significantly improved by cellular substructure with Y2O3. It is the main reason that the substructure morphology will change wear mechanism at high temperature.
机译:通过激光熔化沉积内激光同轴粉末进料,产生具有良好的粘合强度的对比粘接强度,适度的硬度和精细完整性,这是飞机发动机的有望密封涂层。 Conicraly涂层的凝固机制被研究以阐明SEM,XRD和TEM的晶粒和亚结构的演变。还评价了与Y2O3对同胞密封涂层高温摩擦和氧化行为的细胞和树突状亚结构形态的影响。不同温度的氧化结果表明,同色性涂层的抗氧化性是优异的。在873k的涂层表面上形成的连续和保护性CR2O3外氧化物层,而在1423k的涂层表面上形成的更具保护性Al2O3氧化物层。认为在同色性涂层中形成的原位Y2O3颗粒被认为是有益的锚定氧化物层。高温下的摩擦行为取决于亚结构形态。通过Y2O3通过细胞亚结构显着改善了同色涂层的耐磨性。亚结构形态将在高温下改变磨损机制的主要原因。

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