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- Article name
- ANALYSIS OF THERMAL BARRIER COATINGS FOR TURBINE BLADES OF MODERN GAS TURBINE ENGINES
- Authors
- Opokin V. G., , vladimir.opokin@mail.ru, Lytkarino mashinostrostoitelny factory branch of "Saturn", Moscow. reg., Lytkarino, Industrial Area Turaevo, p. 9
Ravilov R. G., , rinat.ravilov@lmz.npo-saturn, Lytkarino mashinostrostoitelny factory branch of "Saturn", Moscow. reg., Lytkarino, Industrial Area Turaevo, p. 9
Samoilenko V. M., , lisok-7@mail.ru, Professor Nicolay Zhukovsky and Yuri Gagarin Air Force Academy, Moscow, Russia
Nastas G. N., , nastas69@mail.ru, Professor Nicolay Zhukovsky and Yuri Gagarin Air Force Academy, Moscow, Russia
- Keywords
- turbine / rotor blades / thermal coating / durability
- Year
- 2012 Issue 1 Pages 3 - 5
- Code EDN
- Code DOI
- Abstract
- This article discusses the current state of application of thermal barrier coatings on various types of engines. Suggests ways to increase the stability of thermal barrier coatings for turbine blades GTE to increase their durability.
- Text
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