F02C 1/00

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9988910 Staggered core printoutJan 30, 15Jun 05, 18United Technologies Corporation
9982629 cycle with independent shafts for combustion cycle elements and propulsion elementsJun 17, 16May 29, 18Rolls-Royce Corporation; Rolls-Royce North American Technologies Inc.;
9976480 Fluid intake systemDec 11, 14May 22, 18SNECMA
9976448 Regenerative thermodynamic power generation cycle systems, and methods for operating thereofMay 29, 15May 22, 18General Electric Company
9970360 Gas turbine engine configured to shape power outputJan 31, 13May 15, 18SIEMENS AKTIENGESELLSCHAFT
9964034 Methods for producing a fuel gas streamMar 27, 15May 08, 18ExxonMobil Upstream Research Company
9964038 Supersonic caret inlet system leading edge slat for improved inlet performance at off-design flight conditionsMar 16, 15May 08, 18The Boeing Company
9963241 Airplane with a fuel cell deviceOct 29, 14May 08, 18Airbus Defence and Space GmbH
9964307 Interface heat shield for a combustor of a gas turbine engineSep 30, 13May 08, 18United Technologies Corporation
9964309 Gas turbine engine combustor with CMC heat shield and methods thereforDec 22, 14May 08, 18General Electric Company
9957897 Gimbal tube systems for tangential onboard injectorsMar 19, 15May 01, 18United Technologies Corporation
9957918 Gas turbine engine front architectureAug 28, 07May 01, 18United Technologies Corporation
9957893 Combustor and gas turbine provided with sameMar 14, 12May 01, 18MITSUBISHI HITACHI POWER SYSTEMS, LTD.
9951721 Three-stream gas turbine engine architectureOct 21, 14Apr 24, 18United Technologies Corporation
9945249 Ventilation of a piece of electronic equipment of a turbomachineJul 31, 14Apr 17, 18SNECMA
9938895 Dual reheat topping cycle for improved energy efficiency for compressed air energy storage plants with high air storage pressureNov 13, 13Apr 10, 18Dresser-Rand Company
9938898 Geared turbofan bearing arrangementJul 29, 11Apr 10, 18United Technologies Corporation
9927125 Two-circuit injector for a turbine engine combustion chamberSep 23, 13Mar 27, 18Turbomeca
9927124 Fuel nozzle for axially staged fuel injectionMar 26, 15Mar 27, 18ANSALDO ENERGIA SWITZERLAND AG
9915200 System and method for controlling the combustion process in a gas turbine operating with exhaust gas recirculationJan 19, 15Mar 13, 18ExxonMobil Upstream Research Company, GENERAL ELECTRIC COMPANY,

Showing 1 to 20 of 1448 results