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Thermal Corrosion Behavior of NiCoCrAlY Coatings Prepared by Different Thermal Spraying Methods

机译:不同热喷涂方法制备的NiCoCrAlY涂层的热腐蚀行为

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The protection of thermal parts has become one of the most important techniques with the development of high capability and high thrust-weight ratio for advanced aeroengine. In this paper, using the nickel base superalloy as the substrate, the thermal corrosion performances of NiCoCrAlY coatings using different thermal spraying methods, which consisted of high velocity oxy-fuel (HV0F), detonation spraying (DS), atmospheric plasma praying (APS) and low pressure plasma spraying (LPPS), were studied. The thermal oxidation experiments, which consisted of isothermal oxidation and cycling oxidation experiments were performed to character the thermal performances. From the results, it was shown that the NiCoCrAlY coatings prepared by high velocity oxy-fuel method were slight for 100 hours at 1100°C. The surface of the NiCoCrAlY coatings prepared by HVOF had a dense, continued Al_2O_3 oxide layer. Among all the methods to prepare NiCoCrAlY coatings, the method of high velocity oxy-fuel showed excellent performance.
机译:随着先进航空发动机的高性能和高推重比的发展,热部件的保护已成为最重要的技术之一。本文以镍基高温合金为基体,采用高速含氧燃料(HV0F),爆轰喷涂(DS),大气等离子体祈祷(APS)等不同的热喷涂方法对NiCoCrAlY涂层的热腐蚀性能进行了研究。和低压等离子喷涂(LPPS)进行了研究。进行了由等温氧化和循环氧化实验组成的热氧化实验,以表征其热性能。从结果表明,通过高速氧-燃料法制备的NiCoCrAlY涂层在1100℃下保持100小时的时间很短。通过HVOF制备的NiCoCrAlY涂层的表面具有致密的连续Al_2O_3氧化物层。在制备NiCoCrAlY涂层的所有方法中,高速含氧燃料的方法表现出优异的性能。

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