Engineering design and experimental research of non-metallic parts and components of the hot section of the advanced gas turbine engine


Cite item

Full Text

Abstract

Technological and experimental research in support of creation of a high-temperature turbine nozzle unit made of diamond dust dispersion-hardened silicon carbide and the flame tube of a high-temperature combustion chamber made of carbon-fiber-reinforced-ray of ceramic composite material based on a ceramic polymer has been conducted. The studies demonstrated:

• technological capability of creating a composite structure of the nozzle made of super-hard diamond dust dispersion-hardened silicon carbide compatible with the mating metal turbine units;

• the results of testing the non-cooled flame tube made of carbon-fiber reinforced ceramic composite material based on a ceramic polymer.

The results will be used in the design, manufacture and tests of non-metallic components of combustion chambers and turbines of auxiliary power units, small-sized gas turbine engines and helicopter engines.

About the authors

T. D. Karimbayev

Central Institute of Aviation Motors named after P.I. Baranov, Moscow

Author for correspondence.
Email: karimbayev@ciam.ru

Doctor of Science (Engineering), Professor

Head of Department

Russian Federation

M. A. Mezentsev

Central Institute of Aviation Motors named after P.I. Baranov, Moscow

Email: mma@ciam.ru

Engineer

Russian Federation

A. J. Ezhov

Central Institute of Aviation Motors named after P.I. Baranov, Moscow

Email: mma@ciam.ru

Senior Engineer

Russian Federation

References

  1. Kameda T., Itoh Y. Fabrication and Mechanical Properties of Reaction Sintered Silicon Carbide Matrix Composite. Key Engineering Materials. 1999. V. 164-165. Р. 95-98. doi.org/10.4028/www.scientific.net/kem.164-165.95
  2. Karimbayev T.D., Gordeev S.K., Mezentsev M.A. Technology of manufacture nozzle block from disperse-strengthened composite material. All-Russian Scientific and Technical Conference Young Scientists and Specialists «New Decision and Technology in Gas-Turbine Structure». Moscow: CIAM Publ., 2010. (In Russ.)

Supplementary files

Supplementary Files
Action
1. JATS XML

Copyright (c) 2015 VESTNIK of the Samara State Aerospace University

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies