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

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

References

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