| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 10/21/2009 | CN101560890A Intermediate casing of turbojet |
| 10/20/2009 | US7603862 Combustion device |
| 10/20/2009 | US7603844 Gas turbine engine assembly and methods of assembling same |
| 10/15/2009 | WO2009092893A3 Method for improving the performance of a bypass turbojet engine and turbojet engine using said method |
| 10/15/2009 | WO2009061586A3 In situ optical probe and methods |
| 10/15/2009 | US20090259379 Reduced take-off field length using variable nozzle |
| 10/15/2009 | DE102008017844A1 Strömungsmaschine mit Fluid-Injektorbaugruppe Flow machine with fluid injector assembly |
| 10/14/2009 | EP2108806A1 Gas turbine engine systems involving variable nozzles with sliding doors |
| 10/14/2009 | EP2038534B1 Turbine engine for aircraft |
| 10/14/2009 | CN101558224A Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 10/14/2009 | CN100549398C Thrust vectoring aft FLADE engine |
| 10/13/2009 | US7603207 Surrogate air processor |
| 10/13/2009 | US7600383 Turbojet with protection means for a fuel injection device, an injection device and a protective plate for the turbojet |
| 10/13/2009 | US7600371 Thrust reversers including support members for inhibiting deflection |
| 10/07/2009 | EP2107216A2 Method for determining the total pressure distribution across a fan entry plane |
| 10/06/2009 | US7596950 Augmentor radial fuel spray bar with counterswirling heat shield |
| 10/01/2009 | US20090245997 Method and device to avoid turbo instability in a gas turbine engine |
| 09/29/2009 | US7594388 Counterrotating turbofan engine |
| 09/24/2009 | WO2009115593A1 Contra-rotating propeller system with device for feathering propeller blades |
| 09/24/2009 | US20090235642 Valve system for a gas turbine engine |
| 09/24/2009 | DE102008015207A1 Fluid-Injektor-Düse Fluid injector nozzle |
| 09/24/2009 | CA2718619A1 Contra-rotating propeller system with device for feathering propeller blades |
| 09/23/2009 | EP2103784A2 Valve system for a gas turbine engine |
| 09/22/2009 | US7593803 Method for controlling fuel splits to gas turbine combustor |
| 09/22/2009 | CA2511432C Thrust reverser comprising optimised deflector gratings |
| 09/22/2009 | CA2436664C Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines |
| 09/17/2009 | US20090229244 Device for pivoting at least one pivotable element in a gas turbine engine |
| 09/17/2009 | US20090229243 Aircraft propulsion unit in multi-fan design |
| 09/17/2009 | US20090229242 Nozzle extension assembly for ground and flight testing |
| 09/16/2009 | EP2101040A2 Turbomachine with multi-flow rotor assembly |
| 09/16/2009 | CN101535622A Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 09/15/2009 | CA2494433C One-piece flame-retention nozzle arm for a turbofan after-burner |
| 09/15/2009 | CA2333843C Fluted compressor flowpath |
| 09/09/2009 | EP2098714A2 High bypass-ratio turbofan jet engine |
| 09/09/2009 | EP2098704A2 Variable area fan nozzle fan flutter management system |
| 09/09/2009 | CN100537354C Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 09/08/2009 | US7584615 Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance |
| 09/08/2009 | US7584602 Augmentor flow control with thermal recirculation function using augmentor valves |
| 09/03/2009 | WO2009107646A1 Noise reducing device, and jet propulsion system |
| 09/03/2009 | US20090217643 Gas discharge device for a vehicle engine |
| 09/03/2009 | DE102008011643A1 Flugzeugantriebseinheit mit Multi-Fan-Ausgestaltung Aircraft propulsion unit with multi-fan design |
| 09/02/2009 | EP2096293A2 Aircraft engine with multiple fans |
| 09/02/2009 | EP2096269A2 Fan track liner assembly for a gas turbine engine |
| 09/02/2009 | EP2096029A2 Nose cone assembly and gas turbine engine comprising such an assemby |
| 09/01/2009 | US7581398 Purged flameholder fuel shield |
| 09/01/2009 | US7581381 Ducted air power plant |
| 08/27/2009 | US20090211222 Rear propulsor for a variable cycle gas turbine engine |
| 08/27/2009 | US20090211221 Auxiliary propulsor for a variable cycle gas turbine engine |
| 08/27/2009 | US20090211090 Turbine engine valve assembly and method of assembling the same |
| 08/25/2009 | US7578132 Gas turbine engine exhaust nozzle |
| 08/25/2009 | US7578131 Augmentor spray bar mounting |
| 08/20/2009 | WO2009029401A3 Variable area fan nozzle with bypass flow |
| 08/20/2009 | DE102008005163A1 Aircraft engine for use turbofan engine for civilian application, has propane fan stage with encased propane rotors, whose rotor blades are surrounded by co-rotating shell, where rotors are made from fiber-reinforced plastic |
| 08/19/2009 | EP2090765A2 Cooled pusher propeller system and method of directing an exhaust flow from a propulsion system |
| 08/19/2009 | CN101512136A Open cycle internal combustion engine |
| 08/19/2009 | CN100529359C Gas turbine engine and method of assembling same |
| 08/18/2009 | US7574866 Turbo-jet engine with a protective screen of the fuel manifold of a burner ring, the burner ring and the protective screen |
| 08/13/2009 | US20090199536 Process for reversing the thrust produced by a propulsion unit of an aircraft, device for its implementation, nacelle equipped with said device |
| 08/12/2009 | EP2088285A2 Compound propulsion engine |
| 08/12/2009 | EP1554524B1 A fuel injector |
| 08/11/2009 | CA2407702C Reduced noise fan stationary blade |
| 08/06/2009 | US20090193789 Variable area fan nozzle thrust reverser |
| 08/05/2009 | EP2085620A1 Jet engine compressor |
| 08/05/2009 | EP2085600A2 Thermal management system integrated pylon |
| 08/05/2009 | EP2085599A2 Shared flow thermal management system |
| 08/05/2009 | CN100523438C Method and device for supporting variable bypass valve system |
| 08/04/2009 | US7568346 Method and apparatus for assembling a flameholder for an augmenter |
| 08/04/2009 | US7568336 Aeroengine fitted with heat exchanger means |
| 07/30/2009 | WO2009092893A2 Method for improving the performance of a bypass turbojet engine and turbojet engine using said method |
| 07/30/2009 | US20090188234 Shared flow thermal management system |
| 07/30/2009 | US20090188233 Thrust reverser forming an adaptive nozzle |
| 07/30/2009 | CA2702684A1 Method for improving the performance of a bypass turbojet engine and turbojet engine using said method |
| 07/29/2009 | EP2083164A2 Aeroengine bleed valve |
| 07/29/2009 | CN100520011C Method and apparatus for operating gas turbine engine |
| 07/28/2009 | US7565804 Flameholder fuel shield |
| 07/28/2009 | US7565796 Turbofan case and method of making |
| 07/16/2009 | US20090178416 Bifurcation and aft vent used to vary fan nozzle exit area |
| 07/16/2009 | US20090178414 Flame holder for minimizing combustor screech |
| 07/16/2009 | US20090178386 Aircraft Propulsion System |
| 07/14/2009 | US7559191 Ducted spinner for engine cooling |
| 07/09/2009 | US20090173056 Methods and apparatus for operating gas turbine engines |
| 07/08/2009 | CN100510369C Methods and apparatus for operating gas turbine engines |
| 07/01/2009 | EP2075439A2 Modular architecture of gas turbine front end |
| 07/01/2009 | EP2075436A2 Ferry flight engine fairing kit |
| 07/01/2009 | EP2075420A2 Method of preparing an engine for transportation |
| 07/01/2009 | EP2075194A1 Air-oil exchanger arranged at the air separator nozzle of a jet engine and jet engine including such an air-oil exchanger |
| 07/01/2009 | EP2074323A1 Turbofan engine with variable bypass nozzle exit area and method of operation |
| 07/01/2009 | EP2074322A2 Turbofan engine |
| 07/01/2009 | EP2074321A2 Fan variable area nozzle with adaptive structure |
| 07/01/2009 | EP2074318A1 Bifurcation and aft vent used to vary fan nozzle exit area |
| 07/01/2009 | EP2074316A2 Managing low pressure turbine maximum speed in a turbofan engine |
| 07/01/2009 | EP2074314A1 Turbofan engine operation control |
| 07/01/2009 | EP2074313A1 Fan variable area nozzle with electromechanical actuator |
| 07/01/2009 | EP2074312A1 Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system |
| 07/01/2009 | EP2074309A1 Fan variable area nozzle with cable actuator system |
| 07/01/2009 | EP2074305A1 Translating core cowl for a gas turbine engine |
| 07/01/2009 | EP2074303A1 Core cowl airfoil for a gas turbine engine |
| 07/01/2009 | EP2074301A1 Reduced take-off field length using variable nozzle |
| 07/01/2009 | CN101469647A Turbojet engine suspended from a support strut of an aircraft |
| 06/25/2009 | WO2009004143A3 Dual flow turboshaft engine and improved hot flow nozzle |