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Development of a Catalytic Combustor for Small Gas Turbines PUBLIC ACCESS

[+] Author Affiliations
K. Mori, J. Kitajima, S. Kajita

Kawasaki Heavy Industries, Ltd., Akashi, Japan

S. Ichihara

Nippon Shokubai Kagaku Kogyo Co. Ltd., Himeji, Japan

Paper No. 87-GT-62, pp. V003T06A007; 8 pages
doi:10.1115/87-GT-62
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

To reduce NOx emissions significantly, a catalytic combustor was developed. Full scale tests of catalytic combustors designed for application in Kawasaki S1A-O2 type gas trubines were conducted. The combustor consisted of a pre-combustion zone, a premixing zone, a catalytic combustion zone, and a variable geometry dilution zone. Liquefied Natural Gas (LNG) was burned in combustor rig tests and results indicated low NOx emissions and high combustion efficiencies over a wide range of air/fuel ratios and that the catalytic combustor can be applied to the engine tests.

Copyright © 1987 by ASME
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