| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 10/20/2011 | DE102010014826A1 Drive device for airplane, has low-pressure turbine commonly driving fan such that rotational torque is transferred to fan gear by mitre gear and shaft, where mitre gear and fan gear reduce rotation speed of fan |
| 10/20/2011 | CA2796170A1 Flow straightener device for turbomachine |
| 10/19/2011 | EP2378103A2 Aircraft gas turbine drive |
| 10/19/2011 | EP2378072A2 Bypass flow channel of a turbofan engine |
| 10/18/2011 | US8037687 Bypass turbomachine with reduction of jet noise |
| 10/11/2011 | US8033094 Cantilevered tip turbine engine |
| 10/11/2011 | US8033092 Tip turbine engine integral fan, combustor, and turbine case |
| 10/05/2011 | CN101105150B An engine core stand arrangement and method of removal and transportation of an engine core |
| 10/04/2011 | US8028513 Variable bypass turbine fan |
| 10/04/2011 | CA2564242C Turbofan engine |
| 09/28/2011 | EP2368030A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 09/28/2011 | CN102203401A Test device for the fan of an aircraft engine |
| 09/28/2011 | CN101825115B Blade with built-in bed frame-type pneumatic damping device |
| 09/21/2011 | EP2366871A1 Method and apparatus for a structural outlet guide vane |
| 09/18/2011 | CA2697292A1 Method and apparatus for a structural outlet guide vane |
| 09/15/2011 | DE102010002719A1 Aerodynamisch geformtes Stütz- und/oder Verkleidungselement im Nebenstromkanal eines Gasturbinentriebwerks Aerodynamically shaped support and / or cladding element in the bypass duct of a gas turbine engine |
| 09/14/2011 | EP2365199A2 Aerodynamically shaped support and/or cladding element in the bypass of a gas turbine engine |
| 09/13/2011 | US8015798 Geared counter-rotating gas turbofan engine |
| 09/13/2011 | US8015797 Thrust reverser nozzle for a turbofan gas turbine engine |
| 09/13/2011 | US8015796 Gas turbine engine with dual fans driven about a central core axis |
| 09/13/2011 | US8015795 Aircraft combination engines plural airflow conveyances system |
| 09/13/2011 | US8015794 Variable area flow duct employing secondary flows, and method therefor |
| 09/09/2011 | WO2011107691A1 Counterweight-based device for controlling the orientation of fan blades of a turboprop engine |
| 09/09/2011 | WO2011107320A1 Flow mixer and corresponding gas turbine engine |
| 09/09/2011 | CA2791640A1 Counterweight-based device for controlling the orientation of fan blades of a turboprop engine |
| 09/08/2011 | DE102010002541A1 Aerodynamic lining for turbofan, has transverse channel flowpath that is arranged extending transit channel due to difference in pressure existing in long sides |
| 09/06/2011 | US8011188 Augmentor with trapped vortex cavity pilot |
| 09/01/2011 | WO2011016945A3 Coannular ducted fan |
| 09/01/2011 | US20110209458 Aircraft gas turbine engine |
| 09/01/2011 | DE102010009477A1 Fluggasturbinenantrieb Aircraft gas turbine engine |
| 09/01/2011 | DE102010002395A1 Turbofan engine comprises support strut which is provided as aerodynamically formed structural guide vanes opposite to aerodynamic guide vanes of larger blade thickness |
| 09/01/2011 | DE102010002394A1 Nebenstromkanal eines Turbofantriebwerks Bypass duct of a turbofan engine |
| 08/31/2011 | EP2362069A2 Panelled liner assembly of a casing liner in a gas turbine |
| 08/31/2011 | EP2362066A2 Hollow fan blade |
| 08/31/2011 | EP2362065A2 Bypass duct with guide vane ring in a turbofan engine |
| 08/31/2011 | EP1825111B1 Counter-rotating compressor case for a tip turbine engine |
| 08/31/2011 | CN101426681B Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 08/30/2011 | US8006479 Thrust reversing variable area nozzle |
| 08/30/2011 | CA2485242C Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 08/26/2011 | CA2732464A1 Aircraft gas turbine engine |
| 08/25/2011 | WO2011101711A1 Engine for thrust or shaft output and corresponding operating method |
| 08/25/2011 | US20110203254 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise |
| 08/24/2011 | EP2360391A1 Epicyclic Gearbox |
| 08/24/2011 | EP2358989A2 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 08/24/2011 | CN1854486B Double reverse turbine engine, and method for assembling the same |
| 08/23/2011 | US8001764 Vibration isolation engine mount system and method for ducted fans |
| 08/23/2011 | CA2731914A1 Epicyclic gearbox |
| 08/23/2011 | CA2495624C Turbojet having a large bypass ratio |
| 08/16/2011 | US7997081 Gas delivery system |
| 08/16/2011 | US7997061 Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit |
| 08/11/2011 | US20110192134 Air intake structure for a turbine engine nacelle |
| 08/10/2011 | EP2354516A2 Translatable cascade thrust reverser |
| 08/03/2011 | EP2351925A2 Back-up featherer |
| 08/03/2011 | EP2350444A1 Gas turbine engine accessory system |
| 08/03/2011 | CN201916074U 喷气轮发动机 Jet turbine engine |
| 08/02/2011 | US7988087 VTOL aircraft nozzle |
| 07/27/2011 | EP2348211A1 Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/27/2011 | EP2348210A1 Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/27/2011 | CN102135035A Aircraft propulsion unit with a cooler installed at engine nacelle |
| 07/26/2011 | US7984607 Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity |
| 07/26/2011 | CA2444979C Explosive decoupling system for a turbojet nozzle |
| 07/26/2011 | CA2381029C Tip sealing configuration for a fan |
| 07/20/2011 | CN102128101A Jet engine with parallel combustion chambers |
| 07/20/2011 | CN101479455B Turboreactor for aircraft |
| 07/19/2011 | US7980058 Air compression type engine for aviation |
| 07/19/2011 | US7980054 Ejector cooling of outer case for tip turbine engine |
| 07/14/2011 | WO2011083137A1 Contra-rotating propeller system for an aircraft turbine engine |
| 07/14/2011 | US20110167792 Adaptive engine |
| 07/14/2011 | US20110167791 Convertible fan engine |
| 07/14/2011 | US20110167790 Translatable cascade thrust reverser |
| 07/14/2011 | US20110167786 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 07/14/2011 | US20110167785 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 07/14/2011 | US20110167784 Method of operating a convertible fan engine |
| 07/14/2011 | CA2786130A1 Contra-rotating propeller system for an aircraft turbine engine |
| 07/13/2011 | EP2343442A2 Turbine engine bypass fan-bleed noise reduction |
| 07/13/2011 | EP2342443A1 Method and apparatus for using compressed air to increase the efficiency of a fuel driven turbine generator |
| 07/13/2011 | CN1975130B Turbofan gas turbine engine with variable fan outlet guide vanes |
| 07/13/2011 | CN102124197A Inner wall for the nacelle of a turbine engine |
| 07/12/2011 | US7976273 Tip turbine engine support structure |
| 07/06/2011 | CN101374722B Dual flow turbine engine equipped with a precooler |
| 06/30/2011 | US20110154805 Power augmentation system for an engine powered air vehicle |
| 06/30/2011 | US20110154804 Exhaust for a gas turbine engine |
| 06/29/2011 | EP2339159A2 Method of mounting a heat exchanger in a gas turbine engine assembly |
| 06/29/2011 | EP2339144A2 Heat exchanger mounting assembly in a gas turbine |
| 06/29/2011 | EP2339143A2 Bleed assembly for a gas turbine engine, corresponding diffuser screen and gas turbine engine |
| 06/29/2011 | EP2339123A1 Inner side of the annular bypass duct of a turbojet engine and method for assembling such an annular duct |
| 06/29/2011 | EP2337940A1 Thermal management system |
| 06/29/2011 | CN102108915A Turbofan engine for stol aircraft |
| 06/28/2011 | US7967219 Thrust nozzle for a gas turbine engine |
| 06/28/2011 | US7966828 Variable area nozzle with woven sleeve extension |
| 06/28/2011 | US7966823 Exhaust dust flow splitter system |
| 06/28/2011 | US7966808 Baffle seal for gas turbine engine thrust reverser |
| 06/28/2011 | US7966807 Vapor cooled static turbine hardware |
| 06/28/2011 | US7966806 Turbofan engine assembly and method of assembling same |
| 06/23/2011 | US20110146230 Integrated Nacelle Assembly |
| 06/23/2011 | US20110146229 Integration of a Surface Heat Exchanger to the Wall of an Aerodynamic Flowpath by a Structure of Reinforcement Rods |
| 06/22/2011 | EP2336525A1 Integration of an air-liquid heat exchanger on an engine |
| 06/22/2011 | EP2336522A2 Intermediate fan stage |
| 06/22/2011 | EP2336504A2 Oil cooler |
| 06/22/2011 | EP2336491A2 Turbofan engine with power extraction system |