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Analysis of a Gas Turbine Cycle With Partial Oxidation FREE

[+] Author Affiliations
M. A. Korobitsyn

Netherlands Energy Research Foundation ECN, Petten, The Netherlands

P. W. Kers, G. G. Hirs

University of Twente, Enschede, The Netherlands

Paper No. 98-GT-033, pp. V003T08A001; 7 pages
doi:10.1115/98-GT-033
From:
  • ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Stockholm, Sweden, June 2–5, 1998
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7864-4
  • Copyright © 1998 by ASME

abstract

This paper addresses the use of the partial oxidation process within a gas turbine cycle. In a partial oxidation reaction fuel is oxidized in a sub-stoichiometric atmosphere at a pressure and a temperature similar to those in the combustion chamber of a conventional turbine. Following the sub-stoichiometric stage, oxidation of the fuel is completed in the final stage. The absence of excess air in the first stages makes it possible to reduce the work required by the compressor and to decrease NOx formation. To assess the partial oxidation concept, several gas turbine systems were simulated and optimized. The results of the comparison study and exergy analysis of the cycles considered are presented.

Copyright © 1998 by ASME
This article is only available in the PDF format.

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