电邮这篇文章 Fracture mechanism of a thermal barrier coating
- 作者: Samoilenko V.1, Ravilov R.2, Drevnyak V.1, Petrova M.1
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隶属关系:
- Moscow State Technical University of Civil Aviation
- Lytkarino Machine-Building Plant
- 期: 卷 2016, 编号 6 (2016)
- 页面: 555-558
- 栏目: Hardening and Coating Technologies
- URL: https://journals.rcsi.science/0036-0295/article/view/170624
- DOI: https://doi.org/10.1134/S0036029516060124
- ID: 170624
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详细
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.
作者简介
V. Samoilenko
Moscow State Technical University of Civil Aviation
编辑信件的主要联系方式.
Email: v-sam61@mail.ru
俄罗斯联邦, Moscow, 125993
R. Ravilov
Lytkarino Machine-Building Plant
Email: v-sam61@mail.ru
俄罗斯联邦, Lytkarino, Moscow obl., 140080
V. Drevnyak
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
俄罗斯联邦, Moscow, 125993
M. Petrova
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
俄罗斯联邦, Moscow, 125993
