Effect of the Structure and Thickness of a Ceramic TBC Layer on the Thermal Conductivity

被引:0
|
作者
Budinovskii S.A. [1 ]
Chubarov D.A. [1 ]
Smirnov A.A. [1 ]
Matveev P.V. [1 ]
机构
[1] FGUP VNII VIAM, GNTs RF, Moscow
关键词
gas turbine engine; magnetron; thermal barrier coating; YSZ;
D O I
10.1134/S003602951806006X
中图分类号
学科分类号
摘要
The microstructure and the thermal conductivity of the ceramic layers of thermal barrier coatings of various compositions, which are deposited by medium-frequency magnetron sputtering of zirconium alloy targets, are studied. The change in the thermal conductivity as a function of the microstructure and thickness of the ceramic layer is investigated. © 2018, Pleiades Publishing, Ltd.
引用
收藏
页码:576 / 582
页数:6
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