Enviar artigo por via de e-mail Fracture mechanism of a thermal barrier coating
- Autores: Samoilenko V.M.1, Ravilov R.G.2, Drevnyak V.V.1, Petrova M.A.1
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Afiliações:
- Moscow State Technical University of Civil Aviation
- Lytkarino Machine-Building Plant
- Edição: Volume 2016, Nº 6 (2016)
- Páginas: 555-558
- Seção: 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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Resumo
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.
Sobre autores
V. Samoilenko
Moscow State Technical University of Civil Aviation
Autor responsável pela correspondência
Email: v-sam61@mail.ru
Rússia, Moscow, 125993
R. Ravilov
Lytkarino Machine-Building Plant
Email: v-sam61@mail.ru
Rússia, Lytkarino, Moscow obl., 140080
V. Drevnyak
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
Rússia, Moscow, 125993
M. Petrova
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
Rússia, Moscow, 125993
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