F23R 3/08

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9939154 Combustor liners with U-shaped cooling channelsNov 06, 13Apr 10, 18United Technologies Corporation
9840924 Gas turbine system with a transition duct having axially extending cooling channelsAug 15, 14Dec 12, 17SIEMENS AKTIENGESELLSCHAFT
9494321 Wake reducing structure for a turbine systemDec 10, 13Nov 15, 16GENERAL ELECTRIC COMPANY
9322554 Temperature mixing enhancement with locally co-swirling quench jet pattern for gas turbine engine combustorJul 29, 11Apr 26, 16UNITED TECHNOLOGIES CORPORATION
9222672 Combustor liner cooling assemblyAug 14, 12Dec 29, 15GENERAL ELECTRIC COMPANY
9181813 Air regulation for film cooling and emission control of combustion gas structureJul 05, 12Nov 10, 15SIEMENS AKTIENGESELLSCHAFT
9182122 Combustor and method for supplying flow to a combustorOct 05, 11Nov 10, 15GENERAL ELECTRIC COMPANY
8991192 Fuel nozzle assembly for use as structural support for a duct structure in a combustor of a gas turbine engineSep 24, 09Mar 31, 15SIEMENS ENERGY, INC.
7802431 Combustor liner with reverse flow for gas turbine engineJul 27, 06Sep 28, 10SIEMENS ENERGY, INC.
5479772 Film cooling starter geometry for combustor linersDec 16, 93Jan 02, 96GENERAL ELECTRIC COMPANY
5253478 Flame holding diverging centerbody cup construction for a dry low NOx combustorDec 30, 91Oct 19, 93GENERAL ELECTRIC COMPANY
5220795 Method and apparatus for injecting dilution airApr 16, 91Jun 22, 93GENERAL ELECTRIC COMPANY
5209067 Gas turbine combustion chamber wall structure for minimizing cooling film disturbancesOct 17, 91May 11, 93SNECMA
5144793 Integrated connector/airtube for a turbomachine's combustion chamber wallsDec 24, 90Sep 08, 92UNITED TECHNOLOGIES CORPORATION
4949545 Turbine wheel and nozzle coolingDec 12, 88Aug 21, 90Sundstrand Corporation
4887432 Gas turbine combustion chamber with air scoopsOct 07, 88Dec 19, 89Westinghouse Electric Corp.
4887663 Hot gas duct linerMay 31, 88Dec 19, 89UNITED TECHNOLOGIES CORPORATION
4864828 Aircraft engine combustion liner cooling apparatusApr 29, 88Sep 12, 89UNITED TECHNOLOGIES CORPORATION, The United States of America as represented by the Secretary of the Air Force,
4723413 Reverse flow combustion chamber, especially reverse flow ring combustion chamber, for gas turbine propulsion units, with at least one flame tube wall film-cooling arrangementNov 19, 86Feb 09, 88MTU MOTOREN- UND TURBINEN-UNION MUNCHEN GMBH
4329848 Cooling of combustion chamber walls using a film of airFeb 29, 80May 18, 82SNECMA