Email this article 
Estimation of a tension of a columnar thermal barrier coatings on nozzle turbine blades and segments of flame pipes of combustion chambers subject to frictional force between a ceramic layer and gas-dynamic flow
- Authors: Bychkov N.G.1, Khamidullin A.S.1, Pershin A.V.1
-
Affiliations:
- Central Institute of Aviation Motors
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 253-258
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6822
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-253-258
- ID: 6822
Cite item
Full Text
Abstract
In the present work the destruction model of columnar ceramic thermal barrier coatings deposited by electron beam technology is proposed. Estimation of a tension of a columnar thermal barrier coatings on nozzle turbine blades and segments of flame pipes of combustion chambers subject to conditions of their work is made.
About the authors
N. G. Bychkov
Central Institute of Aviation Motors
Author for correspondence.
Email: bychkov@rtc.ciam.ru
сandidate of technical science
Chief of sector
A. S. Khamidullin
Central Institute of Aviation Motors
Email: dizertir@list.ru
test engineer
Russian FederationA. V. Pershin
Central Institute of Aviation Motors
Email: bychkov@rtc.ciam.ru
research engineer
Russian FederationReferences
Supplementary files
