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The Comparison of Different Simplified Mathematical Models of the Gas Turbine Combustion Chamber as an Object of Temperature and Pressure Control FREE

[+] Author Affiliations
Marek Dzida

Technical University of Gdansk, Poland

Paper No. 92-GT-347, pp. V003T06A036; 8 pages
doi:10.1115/92-GT-347
From:
  • ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Cologne, Germany, June 1–4, 1992
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7895-8
  • Copyright © 1992 by ASME

abstract

The paper presents the mathematical model of the combustion chamber as an object of temperature and pressure control. Using the step function characteristics and the frequency method (in the range of low frequency f<20Hz), the theoretical models with different degrees of simplifications were compared with the results of the experimental investigations.

The proposed theoretical model may turn out very useful in the research of the gas turbine dynamics.

Copyright © 1992 by ASME
This article is only available in the PDF format.

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