| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 06/25/2009 | US20090158705 Hypermixing Fluid Ejector |
| 06/25/2009 | US20090158704 Gas Turbine Engine |
| 06/24/2009 | EP2072397A2 Intermediate casing extension for an aircraft jet engine, comprising a sectorised annular groove for receiving nacelle covers |
| 06/24/2009 | EP2072396A2 Intermediate casing for an aircraft jet engine with improved design |
| 06/24/2009 | EP2071930A2 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area |
| 06/23/2009 | US7549291 Methods and apparatus for operating gas turbine engines |
| 06/17/2009 | EP2071153A2 Gas turbine engine with a counter-rotating fan |
| 06/17/2009 | EP2069630A1 Gas turbine engine with axial movable fan variable area nozzle |
| 06/17/2009 | EP2069625A2 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 06/11/2009 | US20090148292 Axial compressor for tip turbine engine |
| 06/11/2009 | US20090148272 Tip turbine engine and operating method with reverse core airflow |
| 06/11/2009 | US20090145106 Turbofan engine utilizing an aerodynamically coupled pre-combustion power turbine |
| 06/10/2009 | EP2066896A2 Gas turbine engine with intermediate speed booster |
| 06/10/2009 | EP2066872A1 Method and device to avoid turbofan instability in a gas turbine engine |
| 06/09/2009 | US7543442 Turbojet engine comprising a connector arm for ancillary systems, and the connector arm for ancillary systems |
| 06/09/2009 | CA2494736C Fan case design with metal foam between kevlar |
| 06/04/2009 | US20090142184 Vectoring transition duct for turbine engine |
| 06/04/2009 | US20090139202 Convertible gas turbine propulsion system |
| 06/03/2009 | EP2065585A2 Gas turbine engine with pylon mounted accessory drive |
| 06/03/2009 | EP2064435A2 Open cycle internal combustion engine |
| 06/03/2009 | EP2064434A1 Operational line management of low pressure compressor in a turbofan engine |
| 06/02/2009 | US7540144 Bleed valve for a gas turbine engine |
| 05/27/2009 | EP2063095A2 Fan nozzle with adjustable cross-section |
| 05/27/2009 | EP2061964A1 Turbofan engine having inner fixed structure including ducted passages |
| 05/21/2009 | US20090126339 Thrust Reverser Door |
| 05/20/2009 | EP2060746A1 Discharge valve in a turbomachine |
| 05/20/2009 | CN100489398C Frame runner liner rest for gas turbine engine |
| 05/19/2009 | US7533760 Noise reduction tubes |
| 05/19/2009 | US7533526 Drive arrangement |
| 05/19/2009 | CA2420709C Mixed flow and centrifugal compressor for gas turbine engine |
| 05/14/2009 | WO2009061586A2 In situ optical probe and methods |
| 05/14/2009 | US20090121046 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws |
| 05/14/2009 | US20090120058 Tip Turbine Engine Integral Fan, Combustor, and Turbine Case |
| 05/13/2009 | CN100487712C Method and apparatus for modeling gas turbine engine |
| 05/07/2009 | US20090113894 Purged flameholder fuel shield |
| 05/07/2009 | DE202008010119U1 Einrichtung zur Reinigung von Abgasen der Turbostrahltriebwerke Means for purification of exhaust gases of the turbo-jet engines |
| 05/07/2009 | CA2643618A1 Turbine engine equipped with a means to heat the air entering the freepower turbine |
| 05/06/2009 | CN101426681A Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 05/06/2009 | CN101424228A Method for restraining flow separation in transition section by utilizing guide vane |
| 05/05/2009 | US7527220 Aircraft engine mount |
| 05/05/2009 | US7526913 Gas turbine engine assembly and methods of assembling same |
| 04/30/2009 | WO2009007564A3 Turbojet engine for aircraft |
| 04/30/2009 | WO2008145954A3 Method and apparatus for suppressing aeroengine contrails |
| 04/30/2009 | US20090107110 Fan control apparatus |
| 04/30/2009 | US20090107109 Variable bypass turbine fan |
| 04/30/2009 | US20090107108 Nacell for bypass engine with high bypass ratio |
| 04/30/2009 | US20090107106 Gas Turbine Engine Systems Involving Hydrostatic Face Seals |
| 04/29/2009 | EP2053231A2 Gas turbine engine reheat fuel system |
| 04/23/2009 | WO2007106059A3 Tip turbine engine with aspirated compressor |
| 04/23/2009 | WO2007001372A3 Ducted spinner for engine cooling |
| 04/23/2009 | US20090104019 Offset drive for gas turbine engine |
| 04/22/2009 | EP2050948A2 A gas turbine engine assembly with a variable area nozzle and a method of controlling this nozzle |
| 04/16/2009 | US20090094961 Thrust reversing variable area nozzle |
| 04/15/2009 | EP2048329A1 Turbine engine with electric generator arranged in the fan |
| 04/09/2009 | US20090090096 Epicyclic gear train for variable cycle engine |
| 04/09/2009 | US20090090095 Aircraft turbofan engine |
| 04/09/2009 | DE102007036930A1 Gas-turbine engine e.g. civilian aircraft engine or military aircraft engine, has thermoelectric generator generating electrical energy from temperature difference between hot current via core engine and cold current via bypass channel |
| 04/08/2009 | EP2045460A2 Double-fan turbomachine |
| 04/07/2009 | US7513103 Gas turbine engine assembly and methods of assembling same |
| 04/07/2009 | US7513102 Integrated counterrotating turbofan |
| 04/02/2009 | WO2008145953A3 Method and apparatus for suppressing aeroengine contrails |
| 04/01/2009 | EP2042721A1 Turbomachine nozzle cowl having jet noise suppression pattern, corresponding nozzle and turbomachine |
| 04/01/2009 | EP2041399A2 Aircraft engine inlet having zone of deformation |
| 04/01/2009 | EP1934456B1 Turbofan engine with a device for attenuating the jet noise |
| 03/26/2009 | US20090077978 Self-aligning liner support hanger |
| 03/26/2009 | US20090077946 Fan control apparatus |
| 03/25/2009 | EP2038534A1 Turbine engine for aircraft |
| 03/25/2009 | CN100472055C Methods and apparatus for assembling gas turbine engines |
| 03/24/2009 | US7506514 Augmentor fuel conduit bushing |
| 03/24/2009 | US7506513 Device for feeding air and fuel to a burner ring in an after-burner chamber |
| 03/24/2009 | US7506499 Turbofan jet engine with ancillaries distribution support |
| 03/19/2009 | US20090074568 Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method |
| 03/19/2009 | US20090071162 Peripheral combustor for tip turbine engine |
| 03/19/2009 | US20090071122 Thrust reverser mounting structure |
| 03/19/2009 | US20090071121 Counter-rotating gearbox for tip turbine engine |
| 03/18/2009 | EP2037126A1 Tubofan engine |
| 03/18/2009 | EP2035680A2 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 03/18/2009 | CN100470041C Turbojet engine structure with two fans at the front |
| 03/17/2009 | US7503164 Ducted fan with containment structure |
| 03/12/2009 | US20090067983 Centerline compression turbine engine |
| 03/12/2009 | US20090064659 Gas turbine engine with fan variable area nozzle having a rotational valve system |
| 03/12/2009 | US20090064658 Bypass turbomachine with reduction of jet noise |
| 03/11/2009 | EP2032822A1 Turboreactor for aircraft |
| 03/10/2009 | US7500352 Gas turbine engine |
| 03/10/2009 | US7500351 Gas turbine powerplant |
| 03/05/2009 | US20090056309 Gas Turbine Engine Systems and Related Methods Involving Multiple Gas Turbine Cores |
| 03/05/2009 | US20090056307 Actuating device, bypass air bleed system equipped therewith, and turbojet engine comprising these |
| 03/05/2009 | US20090056306 Gas turbine engine front architecture |
| 03/05/2009 | CA2639330A1 Activation device, discharge system so equipped and jet turbine engine containing them |
| 03/04/2009 | EP2031213A2 Apparatus and method for suppressing dynamic pressure instability in bleed duct |
| 03/03/2009 | US7497300 Noise reduction tubes |
| 02/26/2009 | WO2009024594A1 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise, and turbojet and motor assembly associated therewith |
| 02/26/2009 | US20090053043 Attachment interface for a gas turbine engine composite duct structure |
| 02/26/2009 | DE2809484A1 Nachbrenner für Gasturbinenstrahltriebwerke Afterburner for gas turbine jet engines |
| 02/26/2009 | DE19748214A1 Zündeinrichtung für Nachbrenner von Gasturbinentriebwerken Igniter for afterburner of gas turbine engines |
| 02/26/2009 | CA2696178A1 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise |
| 02/25/2009 | EP2028360A1 Dual-flow turbomachine with jet noise reduction |
| 02/25/2009 | EP1831530B1 Compressor variable stage remote actuation for turbine engine |
| 02/25/2009 | EP1831520B1 Tip turbine engine and corresponding operating method |
| 02/25/2009 | CN101374723A Dual flow turbine engine equipped with a precooler |