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Effect of the microstructure of EB-PVD thermal barrier coatings on the thermal conductivity and the methods to reduce the thermal conductivity

机译:EB-PVD隔热涂层微观结构对导热系数的影响及降低导热系数的方法

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Purpose: The goal of the paper is to evaluate the effect of the microstructure of EB-PVD thermal barrier coatings on the thermal conductivity and the methods to reduce the thermal conductivity. Design/methodology/approach: In this study, the effect of microstructure of the coating to the thermal conductivity of EB-PVD TBCs and the methods to reduce the thermal conductivity of these coatings have been investigated. Findings: Microstructure of the EB-PVD coating - it is found that they are formed in two different structure and microstructural characteristics and they are different from each other. Practical implications: Nowadays, selection of materials for usage purpose is getting important because of new high technologic developments. Especially for the parts operating at high temperatures, materials which have low thermal conductivity and high mechanical resistance are preferred. Thermal Barrier Coatings (TBCs) are used in aerospace, diesel engine and power plant technologies due to porous structures and low thermal conductivity. Generally these coatings are applied by two methods, Electron Beam-Plasma Vapour Deposition (EB-PVD) and Atmospheric Plasma Spray (APS). Originality/value: This paper reviews the current status of EB-PVD thermal barrier coatings technology and investigation to reduce the thermal conductivity in future generations of EB-PVD thermal barrier coatings.
机译:目的:本文的目的是评估EB-PVD隔热涂层的微观结构对导热系数的影响以及降低导热系数的方法。设计/方法/方法:在这项研究中,研究了涂层的微观结构对EB-PVD TBCs导热系数的影响以及降低这些涂层导热系数的方法。发现:EB-PVD涂层的微观结构-发现它们以两种不同的结构和微观结构特征形成,并且彼此不同。实际意义:如今,由于新的高科技发展,用于用途的材料选择变得越来越重要。特别是对于在高温下工作的部件,具有低导热率和高机械阻力的材料是优选的。由于多孔结构和低导热性,热障涂层(TBC)用于航空航天,柴油发动机和发电厂技术。通常,这些涂层是通过两种方法施加的,电子束等离子气相沉积(EB-PVD)和大气等离子喷涂(APS)。原创性/价值:本文回顾了EB-PVD隔热涂层技术的现状,并进行了研究以降低下一代EB-PVD隔热涂层的导热性。

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