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TECHNICAL PAPERS: Gas Turbines: Combustion and Fuels

Performance of a Dry Low-NOx Gas Turbine Combustor Designed With a New Fuel Supply Concept

[+] Author and Article Information
T. Wakabayashi, S. Ito, S. Koga, M. Ippommatsu, K. Moriya

Osaka Gas Co., Ltd., 6-19-9, Torishima, Konohana-ku, Osaka 554-0051, Japan

K. Shimodaira, Y. Kurosawa, K. Suzuki

National Aerospace Laboratory, 7-44-1 Jindaiji-higashi, Chofu, Tokyo 182-8522, Japan

J. Eng. Gas Turbines Power 124(4), 771-775 (Sep 24, 2002) (5 pages) doi:10.1115/1.1473154 History: Received December 01, 2000; Revised March 01, 2001; Online September 24, 2002
Copyright © 2002 by ASME
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References

Figures

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New Fuel supply concept
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Cross section of the prototype combustor and the test rig
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Details of the fuel supply unit
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Equivalence ratio pattern in the fuel supply unit by numerical simulation
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Average equivalence ratio of the main region by numerical simulation
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Pressurized combustion test facility
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Cross section (Z-Z) of fuel supply unit (see Fig. 3)
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Average equivalence ratio of the main region
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NOx emissions (at 0% O2)
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Dependence of NOx emissions on CDP
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Average temperature of exhaust gas at the exit of the combustor

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