| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 02/28/2012 | CA2466756C Differential geared turbine engine with torque modulation capability |
| 02/22/2012 | EP2420665A1 Variable area fan nozzle |
| 02/22/2012 | EP2419621A1 System and method for managing thermal issues in gas turbine engines |
| 02/22/2012 | EP2419616A1 Double-body gas turbine engine provided with an inter-shaft bearing |
| 02/21/2012 | US8117827 Apparatus for operating gas turbine engines |
| 02/21/2012 | CA2517563C Rotary adjustable exhaust nozzle |
| 02/16/2012 | WO2012019419A1 Wind-driven turbine ramjet engine |
| 02/16/2012 | US20120036830 Thrust reversal device |
| 02/08/2012 | EP2415992A2 Ventilation Inlet |
| 02/08/2012 | EP2415965A2 Gas turbine engine |
| 02/08/2012 | EP2414655A1 Rotating inlet cowl for a turbine engine, including an eccentric front end |
| 02/07/2012 | US8109468 Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle |
| 02/02/2012 | US20120023901 Variable area fan nozzle for gas turbine engine |
| 02/02/2012 | US20120023900 Aircraft nacelle |
| 02/02/2012 | US20120023899 Turbofan engine |
| 02/02/2012 | DE102010032324A1 Heat exchanger for use in arrangement, particularly for gas turbine engine, has cross-flow matrix, distributor tube for guiding heat carrier medium into cross-flow matrix and collecting tube for discharging heat transfer medium |
| 02/01/2012 | EP2412939A1 Fan embedded power generator |
| 02/01/2012 | CN102341588A Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 01/31/2012 | US8104265 Gas turbines with multiple gas flow paths |
| 01/31/2012 | US8104262 Dual function cascade integrated variable area fan nozzle and thrust reverser |
| 01/31/2012 | US8104261 Tri-body variable area fan nozzle and thrust reverser |
| 01/26/2012 | WO2012010782A1 Turbine engine having two unducted propellers |
| 01/26/2012 | DE102010032097A1 Verdichterschaufel eines Gasturbinentriebwerks mit selbstschärfender Vorderkantenstruktur Compressor blade of a gas turbine engine with self-sharpening leading edge structure |
| 01/26/2012 | CA2805757A1 Turbine engine having two unducted propellers |
| 01/25/2012 | EP2410185A2 Bleed air output in the bypass flow channel of a turbofan engine |
| 01/25/2012 | EP2410165A2 Gas turbine with noise attenuating variable area fan nozzle |
| 01/25/2012 | EP2410152A2 Fan case assembly and method |
| 01/25/2012 | EP1825177B1 Inflatable bleed valve for turbine engine and method of controlling bleed air |
| 01/24/2012 | US8099944 Hybrid propulsive engine including at least one independently rotatable propeller/fan |
| 01/19/2012 | US20120011827 Bleed air outlet in the bypass duct of a turbofan engine |
| 01/19/2012 | US20120011826 Turbojet engine with an element of the nacelle attached to the intermediate casing |
| 01/19/2012 | US20120011825 Gas turbine engine with noise attenuating variable area fan nozzle |
| 01/19/2012 | DE102010027587A1 Zapfluftauslass im Nebenstromkanal eines Turbofantriebwerks Zapfluftauslass in the bypass duct of a turbofan engine |
| 01/18/2012 | EP2407660A2 Auxiliary hydraulic power generation system |
| 01/18/2012 | EP2407644A2 Geared turbofan emergency power |
| 01/18/2012 | EP2406484A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 01/18/2012 | EP2406012A2 Device for spraying a fluid using the air blast effect |
| 01/17/2012 | US8097972 Gas turbine with magnetic shaft forming part of a generator/motor assembly |
| 01/17/2012 | US8096106 Drive mechanism |
| 01/12/2012 | WO2011121355A3 Gas turbines |
| 01/12/2012 | US20120005999 Variable area fan nozzle and thrust reverser |
| 01/11/2012 | CN102317608A Air vehicle propulsion system with counter rotating fan design and method for noise reduction |
| 01/11/2012 | CN102317598A System of compact contra-rotating propellers |
| 01/10/2012 | CA2495594C Turbofan architecture having two front fans |
| 01/04/2012 | EP2401509A2 Fan blades with cyclic setting |
| 01/04/2012 | CN102305152A Hybrid exhaust aircraft engine |
| 01/03/2012 | CA2515852C Ventilated confluent exhaust nozzle |
| 12/29/2011 | WO2011162845A1 Adaptive fan system for a variable cycle turbofan engine |
| 12/29/2011 | WO2011160441A1 Thermal ramjet |
| 12/28/2011 | EP2399018A1 Air vehicle propulsion system with counter rotating fan design and method for noise reduction |
| 12/28/2011 | CN202091057U 高效涡轮喷气发动机 Efficient turbojet |
| 12/27/2011 | US8082727 Rear propulsor for a variable cycle gas turbine engine |
| 12/27/2011 | US8082726 Tangential anti-swirl air supply |
| 12/24/2011 | CA2742548A1 Ejector purge of cavity adjacent exhaust flowpath |
| 12/22/2011 | WO2011157965A1 Aircraft turbo jet engine fan casing |
| 12/22/2011 | WO2011157962A1 Airflow-straightening structure for the nacelle of an aircraft engine |
| 12/22/2011 | WO2011157926A1 Turbojet engine nacelle |
| 12/22/2011 | US20110309187 Nested core gas turbine engine |
| 12/22/2011 | CA2802590A1 Airflow-straightening structure for the nacelle of an aircraft engine |
| 12/22/2011 | CA2802398A1 Aircraft turbo jet engine fan casing |
| 12/22/2011 | CA2802008A1 Turbojet engine nacelle |
| 12/21/2011 | EP2396525A1 System of compact contra-rotating propellers |
| 12/15/2011 | US20110302907 Variable area fan nozzle |
| 12/13/2011 | US8075246 Relief device for a turbojet and a turbojet comprising same |
| 12/13/2011 | US8074440 Gas turbine engine with axial movable fan variable area nozzle |
| 12/08/2011 | DE102010022933A1 Bypass flow jet engine for use as counter flow engine in airplane, has central tubular fresh air intake channel in rotary axis of compressor and working turbine disks, by which fresh air is sucked in front area of engine |
| 12/08/2011 | DE102010022932A1 Bypass jet engine i.e. counterflow engine, for use in aircraft, has front blower deflecting fresh air around specified degrees in collecting cavity of core engine, where fresh air is sucked in front of outer housing of core engine |
| 12/07/2011 | EP2391536A2 Engine, in particular cror drive, for an aircraft |
| 12/06/2011 | US8069657 Diesel particulate filter regeneration system |
| 12/06/2011 | US8069647 Jet nozzle mixer |
| 12/01/2011 | US20110289900 Thrust reversing variable area nozzle |
| 11/30/2011 | EP2390472A2 Geared turbofan engine with integral gear and bearing supports |
| 11/30/2011 | CN202055935U Jet engine with parallel combustion chambers |
| 11/29/2011 | US8065867 Radial ball bearing |
| 11/23/2011 | CN102257260A System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 11/22/2011 | US8061144 Gas turbine engines |
| 11/22/2011 | US8061143 Gas turbine engine reheat systems |
| 11/22/2011 | CA2495992C Aerodynamic adaptation of the rear fan of a double fan turbofan |
| 11/17/2011 | US20110277448 Guide system for nacelle assembly |
| 11/17/2011 | US20110277446 Rockets, methods of rocket control and methods of rocket evaluation utilizing pressure compensation |
| 11/16/2011 | EP2315928B1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 11/10/2011 | DE102010016832A1 Fuel mixture, useful for noise reduction in a jet engine, preferably in an aircraft engine, comprises tert-butyl peroxybenzoate and kerosene |
| 11/09/2011 | CN102239323A Method and apparatus for using compressed air to increase the efficiency of a fuel driven turbine generator |
| 11/09/2011 | CN102235267A Gas turbine engine modified by using exservice turbofan engine through low-pressure crest truncation |
| 11/08/2011 | US8051639 Thrust reverser |
| 11/03/2011 | WO2011134031A1 Airfoil combination for aircraft turbofan |
| 11/03/2011 | US20110265448 Jet nozzle mixer |
| 11/03/2011 | US20110265447 Gas turbine engine exhaust mixer |
| 11/03/2011 | US20110265446 System for controlling at least one actuator of the cowlings of a turbojet engine thrust reverser |
| 11/03/2011 | DE102010018928A1 Passenger aircraft i.e. airplane, has intense internal thruster arranged at rear of fuselage, and intake ports integrated into sides of body, where air intake ports are arranged to obtain favorable aerodynamic form |
| 11/02/2011 | EP2383453A2 Flow mixing vent system |
| 11/02/2011 | EP2383442A2 Gas turbine engine |
| 11/02/2011 | EP2383441A2 A Gas Turbine Engine |
| 11/02/2011 | EP2383437A2 Gas turbine engine airfoil integrated heat exchanger |
| 11/02/2011 | EP2382026A1 Inlet particle separator system for a gas turbine engine |
| 11/01/2011 | US8047001 Media mixing insert for turbine blade in turbine engine |
| 10/25/2011 | US8042342 Engine assembly for aircraft comprising an engine as well as a device for locking said engine |
| 10/20/2011 | WO2011128551A2 Flow straightener device for turbomachine |
| 10/20/2011 | WO2011127901A1 Multi-shaft engine having a tandem generator |
| 10/20/2011 | DE102010014900A1 Nebenstromkanal eines Turbofantriebwerkes Bypass duct of a Turbofantriebwerkes |