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Gas turbine combustor
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Patent number 5,758,503
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Issue date Jun 2, 1998
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United Technologies Corporation
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Thomas L. DuBell
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F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
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Combustor with first and second zones
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Patent number 5,749,219
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Issue date May 12, 1998
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United Technologies Corporation
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Thomas L. DuBell
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F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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Combustor
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Patent number 5,481,867
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Issue date Jan 9, 1996
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United Technologies Corporation
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Thomas L. Dubell
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F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
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Combustor
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Patent number 5,297,385
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Issue date Mar 29, 1994
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United Technologies Corporation
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Thomas L. Dubell
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F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
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Pressurized stem air blast fuel nozzle
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Patent number 5,078,324
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Issue date Jan 7, 1992
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United Technologies Corporation
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Thomas L. DuBell
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F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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Combustor fuel nozzle arrangement
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Patent number 4,991,398
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Issue date Feb 12, 1991
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United Technologies Corporation
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Jim A. Clark
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F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
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Fuel injection system
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Patent number 4,817,389
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Issue date Apr 4, 1989
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United Technologies Corporation
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Thomas E. Holladay
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F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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Method for distributing augmentor fuel
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Patent number 4,720,971
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Issue date Jan 26, 1988
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United Technologies Corporation
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Thomas L. DuBell
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F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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Mixed flow swirl augmentor for turbofan engine
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Patent number 4,461,146
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Issue date Jul 24, 1984
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The United States of America as represented by the Secretary of the Navy
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Thomas L. DuBell
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F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
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