Fracture mechanism of a thermal barrier coating

被引：0
作者：
Samoilenko V.M. [1 ]
Ravilov R.G. [2 ]
Drevnyak V.V. [1 ]
Petrova M.A. [1 ]
机构：
[1] Moscow State Technical University of Civil Aviation, Moscow
[2] Lytkarino Machine-Building Plant, Lytkarino, Moscow obl.
来源：
Samoilenko, V.M. (v-sam61@mail.ru) | 1600年 / Izdatel'stvo Nauka卷 / 2016期
关键词：
Thermal barrier coatings;
D O I：
10.1134/S0036029516060124
中图分类号：
学科分类号：
摘要：
The fracture mechanism of the thermal barrier coating of gas turbine blades is studied. The causes of the fracture of the ceramic layer are discussed and the possible ways to increase the fatigue life of the thermal barrier coating are considered. © 2016, Pleiades Publishing, Ltd.
引用
收藏
页码：555 / 558
页数：3
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