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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

Solt, J. C., and Tuzson, J., 1993, “Status of Low NOx Combustor Development,” ASME Paper No. 93-GT-270.
Aigner,  M., and Muller,  G., 1993, “Second-Generation Low-Emission Combustors for ABB Gas Turbines: Field Measurements with GT11N-EV,” ASME J. Eng. Gas Turbines Power, 115, pp. 533–536.
Kitajima, J., Kimura, T., Sasaki, T., Okuto, A., Kajita, S., Ohga, S., and Ogata, M., “Development of a Second Generation Dry Low NOx Combustor for 1.5MW Gas Turbine,” ASME Paper No. 95-GT-255.
Ishii,  J., 1999, “The Next Generation High-Efficiency Combined-Cycle Power Plants which used 1500C-class Steam Cooled Gas Turbine,” Journal of the Gas Turbine Society of Japan, 27(3), pp. 161–165.
Akita,  E., and Nishida,  M., 1999, “Development and Verificational Operation of 1500C Class Next Generation High Efficient G series Gas Turbine,” Journal of the Gas Turbine Society of Japan, 27(3), pp. 138–145.
Sato, H., Amano, T., Iiyama, Y., Mori, M., and Nakamura, T., 1999, “Development of a Three-Staged Low Emissions Combustor for Industrial Small-Size Gas Turbines,” ASME Paper No. 99-GT-236.
Smith, K. O., 1992, “Engine Testing of a Prototype Low NOx Gas Turbine Combustor,” ASME Paper No. 92-GT-116.
Etherdge, C. J., 1994, “Mars SoLoNOx-Lean Premix Combustion Technology in Production,” ASME Paper No. 94-GT-255.
Smith, K. O., Holsapple, A. C., Mak, H. K., and Watkins, L., 1991, “Development of a Natural Gas Fired, Ultra-Low NOx Can Combustor for 800 kW Gas Turbine Engines,” ASME Paper No. 91-GT-303.

Figures

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Average temperature of exhaust gas at the exit of the combustor
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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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