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Prototype Testing Methods Variable Geometry Industrial Gas Turbines PUBLIC ACCESS

[+] Author Affiliations
G. McQuiggan

Westinghouse Canada Inc., Hamilton, ON, Canada

Paper No. 82-GT-75, pp. V001T01A032; 12 pages
doi:10.1115/82-GT-75
From:
  • ASME 1982 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • London, England, April 18–22, 1982
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7956-6
  • Copyright © 1982 by ASME

abstract

This paper describes the prototype engine testing methods used to determine the performance and integrity of a new industrial gas turbine in the 20-MW to 30-MW range (CW352). This gas turbine is very flexible in that it is designed with the following features: (i) Variable compressor inlet guide vanes; (ii) 15-, 16- or 17-stage compressor alternatives; (iii) Variable power turbine vanes; (iv) Regenerative or simple cycle mode of operation.

Copyright © 1982 by ASME
This article is only available in the PDF format.

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