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The Feasibility, From an Installational Viewpoint, of Gas-Turbine Pressure-Gain Combustors FREE

[+] Author Affiliations
J. A. C. Kentfield

The University of Calgary, Calgary, AB, Canada

Paper No. 88-GT-181, pp. V003T06A022; 7 pages
doi:10.1115/88-GT-181
From:
  • ASME 1988 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Amsterdam, The Netherlands, June 6–9, 1988
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7920-7
  • Copyright © 1988 by ASME

abstract

The principles of pressure-gain combustors based on the wave rotor and pulse-combustor concepts were reviewed briefly. A study, based on experimental data, in which current-technology pressure-gain combustors were applied to three aircraft-engine derivative industrial gas-turbines, covering a power range from 275 kW (370 hp) to 29 MW (39,000 hp), showed that engine power increased by 6.5% to 9.6% with corresponding reductions of equal magnitude in specific fuel consumption. It was concluded that pressure-gain combustors appear to offer sufficient improvements in performance without incurring crippling installational penalties, although decreases in engine power/weight ratios were noted, to warrant further research and development.

Copyright © 1988 by ASME
This article is only available in the PDF format.

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