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Gas Turbine Model With Intensive Cooling FREE

[+] Author Affiliations
Evgeni A. Khodak, Gallna A. Romakhova

St.-Petersburg State University, St.-Petersburg, Russia

Paper No. 94-GT-464, pp. V004T10A024; 11 pages
doi:10.1115/94-GT-464
From:
  • ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration
  • The Hague, Netherlands, June 13–16, 1994
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7886-6
  • Copyright © 1994 by ASME

abstract

A method of calculation of cooled gas turbine parameters is proposed. The method is based on the solution of the expansion process equation, heat transfer equations for cooled elements and on the results of the statistic processing of the parameters.

The method is valid for the turbine with any cooling system and gaseous heat carrier. Turbine output determination error does not exceed 0,5–1,0%.

The method allows to obtain the characteristics of gas turbines and gas turbine units (GTU) with open and closed air and steam cooling systems and to carry out an efficiency analysis of their performance in power generating units of various structure.

Copyright © 1994 by ASME
Topics: Cooling , Gas turbines
This article is only available in the PDF format.

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