Patents
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
06/2007
06/27/2007EP1799989A1 Gas turbine intermediate structure and a gas turbine engine comprising the intermediate structure
06/27/2007CN1987065A Axial flow progressive cavity type gas generator
06/26/2007US7234914 Apparatus and method for enhancing lift produced by an airfoil
06/21/2007CA2571952A1 Compact booster bleed turbofan
06/20/2007EP1798383A1 Bleed system for axial rotary machine
06/19/2007US7231767 Forced air cooling system
06/19/2007CA2562588A1 Axial flow positive displacement worm gas generator
06/14/2007WO2007066053A2 Brazed joint between a metal part and a ceramic part
06/14/2007US20070130913 Coaxial propulsion systems with flow modification element
06/14/2007US20070130912 Shrouded turbofan bleed duct
06/14/2007CA2632716A1 Brazed joint between a metal part and a ceramic part
06/13/2007EP1795708A2 Shrouded turbofan bleed duct
06/12/2007US7228683 Methods and apparatus for generating gas turbine engine thrust using a pulse detonator
06/08/2007CA2570604A1 Shrouded turbofan bleed duct
06/07/2007US20070125086 Device for attaching a flame-arrestor arm to an afterburner casing and afterburner comprising such a device
06/07/2007US20070125066 Turbofan engine assembly and method of assembling same
06/07/2007US20070125065 Methods and apparatus for assembling gas turbine engines
06/06/2007CN1975144A Augmentor pilot nozzle
06/06/2007CN1975130A Turbofan gas turbine engine with variable fan outlet guide vanes
06/05/2007US7225623 Trapped vortex cavity afterburner
05/2007
05/31/2007US20070119150 Turbofan gas turbine engine with variable fan outlet guide vanes
05/30/2007EP1790831A2 Turbofan gas turbine engine with variable fan outlet guide vanes
05/30/2007EP1789728A1 Method and apparatus for providing an afterburner fuel-feed arrangement
05/29/2007CA2560448A1 Turbofan gas turbine engine with variable fan outlet guide vanes
05/22/2007US7219499 Methods and apparatus for operating gas turbine engines
05/22/2007US7219490 Nested core gas turbine engine
05/17/2007US20070107414 Jet engine noise suppressor
05/16/2007EP1785617A1 Gas turbine engine with power transfer and method
05/16/2007EP1579112B1 Thrust reverser comprising optimised deflector gratings
05/15/2007US7216475 Aft FLADE engine
05/09/2007EP1783346A2 Duct for reducing shock related noise
05/09/2007EP1783330A2 Turbofan case and method of making
05/09/2007CN1314894C Maintenance and inhibition plate for a thrust reverser
05/08/2007US7213391 Cooling systems
05/08/2007CA2355428C Blisk
05/03/2007WO2007049032A1 Turbofan engine for stol aircraft
05/02/2007EP1780387A2 Nested core gas turbine engine
05/02/2007EP1780382A2 Turbofan case and method of making
05/01/2007CA2184232C Arrangement of gas turbine engine comprising cascade vanes and an intermediate casing
04/2007
04/25/2007EP1777406A2 Turbofan engine with counterrotating fans
04/25/2007EP1777405A2 Gas turbine engine assembly and methods of assembling the same
04/25/2007EP1777404A2 Gas turbine engine assembly and methods of assembling same
04/25/2007EP1777391A2 Gas turbine engine assembly and methods of assembling same
04/25/2007EP1777390A2 Gas turbine engine assembly and methods of assembling same
04/25/2007EP1777379A2 Turbofan case and method of making
04/25/2007EP1777378A2 Turbofan case and method of making
04/25/2007EP1777370A2 Gas turbine engine assembly and methods of assembling same
04/25/2007EP1777369A2 Gas turbine engine assembly and methods of assembling same
04/21/2007CA2564677A1 Bleed valve for a gas turbine engine
04/19/2007WO2005099999A3 Compositions and methods for sealing
04/19/2007US20070084190 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084189 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084188 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084187 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084186 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084185 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084184 Gas turbine engine assembly and methods of assembling same
04/19/2007US20070084183 Gas turbine engine assembly and methods of assembling same
04/18/2007CN1950255A Boundary layer suction arrangement
04/11/2007CN1309944C Aero-gas turbine having control blades used for backward rotary low-pressure turbine
04/10/2007US7200999 Arrangement for bleeding the boundary layer from an aircraft engine
04/05/2007WO2007015916A3 Reinforcement rings for a diffuser section of a tip turbine engine fan rotor assembly
04/05/2007WO2006110122A3 Inflatable bleed valve for a turbine engine and a method of operating therefore
04/04/2007EP1451461B1 Jet nozzle mixer
04/04/2007CN1942665A Jet nozzle mixer
04/03/2007US7200538 Methods and apparatus for modeling gas turbine engines
03/2007
03/29/2007DE102005046208A1 Jet propulsion unit, especially for aircraft, has integrated motor/generator unit in rotation plane of at least first compressor stage, stator around compressor housing, rotor formed by blade elements at least of first compressor stage
03/29/2007CA2584641A1 Fan case reinforcement in a gas turbine jet engine
03/28/2007EP1470328B1 Turbofan exhaust nozzle and method of reducing noise in such a nozzle
03/22/2007WO2007031618A1 Method for attenuating the noise of a turbofan
03/22/2007CA2619292A1 Method for attenuating the noise of a turbofan
03/16/2007CA2551711A1 Augmentor radial fuel spray bar with counterswirling heat shield
03/13/2007US7188467 Methods and apparatus for assembling a gas turbine engine
03/13/2007US7188464 Methods for operating gas turbine engines
03/08/2007US20070051091 Turbofan arrangement
03/06/2007US7185485 Method and system for failure accommodation of gas generator fuel metering system
03/06/2007US7185484 Methods and apparatus for assembling a gas turbine engine
03/01/2007US20070044451 Cooling systems
02/2007
02/28/2007EP1757796A2 Compressor having a plurality of segments reconstructing an annular volume and thus separating the flow in a turbomachine
02/28/2007EP1756406A1 Gas turbine compression system and compressor structure
02/22/2007WO2006110125A3 Stacked annular components for turbine engines
02/22/2007US20070039327 Monobloc flameholder arm for an afterburner device of a bypass turbojet
02/22/2007US20070039310 Compressor comprising a plurality of cells reconstituting an annular volume of separation of flows in a turbine engine
02/22/2007CA2556485A1 Compressor with multiple dividers creating an annular volume separating the flow in a turbine engine
02/21/2007CN1916386A Multi-spool by-pass turbofan engine
02/14/2007EP1752709A2 Reheat combustion in gas turbine systems
02/08/2007WO2007015916A2 Reinforcement rings for a diffuser section of a tip turbine engine fan rotor assembly
02/08/2007US20070028621 Augmentor spray bar mounting
02/08/2007US20070028595 High pressure gas turbine engine having reduced emissions
02/01/2007US20070022739 Methods and apparatus for operating gas turbine engines
02/01/2007DE19617916B4 Verdampfer zum Verdampfen eines tiefkalten flüssigen Mediums Evaporator for evaporating a cryogenic liquid medium
01/2007
01/31/2007EP1748170A2 PTO assembly for a gas turbine engine, gas turbine engine and method of operation of a gas turbine engine
01/30/2007US7168253 Monobloc flameholder arm for an afterburner device of a bypass turbojet
01/24/2007EP1746252A2 Structural strut and shroud element
01/24/2007EP1744953A1 Boundary layer suction arrangement
01/24/2007CN1900508A Integrated counterrotating turbofan
01/18/2007US20070012026 Nested core gas turbine engine
01/17/2007EP1744045A1 Methods and apparatus for assembling gas turbine engines
01/16/2007US7162859 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation
01/11/2007US20070006590 Augmentor spray bars
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