Email this article Fracture mechanism of a thermal barrier coating
- Authors: Samoilenko V.M.1, Ravilov R.G.2, Drevnyak V.V.1, Petrova M.A.1
-
Affiliations:
- Moscow State Technical University of Civil Aviation
- Lytkarino Machine-Building Plant
- Issue: Vol 2016, No 6 (2016)
- Pages: 555-558
- Section: Hardening and Coating Technologies
- URL: https://journal-vniispk.ru/0036-0295/article/view/170624
- DOI: https://doi.org/10.1134/S0036029516060124
- ID: 170624
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
V. M. Samoilenko
Moscow State Technical University of Civil Aviation
Author for correspondence.
Email: v-sam61@mail.ru
Russian Federation, Moscow, 125993
R. G. Ravilov
Lytkarino Machine-Building Plant
Email: v-sam61@mail.ru
Russian Federation, Lytkarino, Moscow obl., 140080
V. V. Drevnyak
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
Russian Federation, Moscow, 125993
M. A. Petrova
Moscow State Technical University of Civil Aviation
Email: v-sam61@mail.ru
Russian Federation, Moscow, 125993
Supplementary files
