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