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Observations on the Life and Overhaul Requirements of Aero Derivative Engines on Base Load Industrial Applications PUBLIC ACCESS

[+] Author Affiliations
P. Lowden, J. Liburdi

Liburdi Engineering Limited, Hamilton, ON, Canada

Paper No. 87-GT-105, pp. V003T07A003; 6 pages
doi:10.1115/87-GT-105
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7925-2
  • Copyright © 1987 by ASME

abstract

Experience in examining the overhauls on industrial aero-derivative engines has shown that the usual flight standards and procedures are not always applicable to ensure prolonged service under base load applications. Not only are changes often required in recommended overhaul intervals, but the methods used to analyze remaining life, and the repair procedures employed to refurbish turbine blades must be re-examined to allow for long term creep and aging phenomena. To illustrate the potential problems encountered, examples from various engines are presented and the changes in overhaul philosophy required to cope with the base load applications are outlined.

Copyright © 1987 by ASME
Topics: Engines , Stress
This article is only available in the PDF format.

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