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Simulation of an Advanced Twin-Spool Industrial Gas Turbine FREE

[+] Author Affiliations
Ping Zhu, H. I. H. Saravanamuttoo

Carleton University, Ottawa, Canada

Paper No. 91-GT-034, pp. V003T07A001; 8 pages
doi:10.1115/91-GT-034
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7900-9
  • Copyright © 1991 by ASME

abstract

A full range mathematical model of the LM-1600 gas turbine has been developed, for future use in EHM studies. No data was available from the manufacturer other than sales brochures giving some design and off-design performance. The model was developed using generalized component characteristics and shows excellent agreement with field data from a pipeline operator.

A new method has been developed for doing the matching calculations, starting from the turbine (hot) end rather than from the compressor operating point. This method permits solution on a PC, and can be used for studying the full range of operating conditions and the development of fault matrices.

Copyright © 1991 by ASME
This article is only available in the PDF format.

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