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Wearability, wearproof and heat-shielding coverings for details of the gas path of the turbine, the compressor and the chamber of combustion of gas turbine engine
- Authors: Barvinok V.A.1, Shitarev I.L.1, Bogdanovich V.I.1, Dokukina I.A.1, Karasev V.M.2
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Affiliations:
- Samara State Aerospace University
- “Metallist-Samara”
- Issue: Vol 8, No 3-1 (2009): Special Issue
- Pages: 11-28
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/671
- DOI: https://doi.org/10.18287/2541-7533-2009-0-3-1(19)-11-28
- ID: 671
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Abstract
The basic laws and features of plotting of wearability, wearproof and heat-resisting coverings on a detail of a gas path of the turbine, the compressor and the combustion chamber of gas turbine engine by gas-thermal plasma and ionicplasma vacuum methods are considered. The basic updates and elements of modernisation of the equipment for gasthermal and an ionic-plasma vacuum method are shown. For calculation of the temperatures, flowing and residual pressure real cases and receptions at spraying are considered.
About the authors
V. A. Barvinok
Samara State Aerospace University
Author for correspondence.
Email: bogdanovich@ssau.ru
Russian Federation
I. L. Shitarev
Samara State Aerospace University
Email: bogdanovich@ssau.ru
Russian Federation
V. I. Bogdanovich
Samara State Aerospace University
Email: bogdanovich@ssau.ru
Russian Federation
I. A. Dokukina
Samara State Aerospace University
Email: bogdanovich@ssau.ru
Russian Federation
V. M. Karasev
“Metallist-Samara”
Email: bogdanovich@ssau.ru
Russian Federation
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