Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
10/2010
10/26/2010US7818958 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle
10/21/2010WO2010121255A1 System and method for managing thermal issues in gas turbine engines
10/21/2010WO2010119115A1 Double-body gas turbine engine provided with an inter-shaft bearing
10/21/2010US20100264261 Aircraft drag management structure
10/21/2010US20100263351 Drive mechanism
10/21/2010CA2758175A1 Double-body gas turbine engine provided with an inter-shaft bearing
10/20/2010EP2241432A2 Intermediate-manufactured composite airfoil and method for manufacturing
10/19/2010CA2472605C Turbofan variable fan nozzle
10/19/2010CA2389525C Variable cycle propulsion device employing exhaust bypass for supersonic aircraft, and operating process
10/14/2010US20100257841 Variable area fan nozzle and thrust reverser
10/13/2010EP2239436A2 Reverse flow ceramic matrix composite combustor
10/13/2010EP2239420A2 Outlet guide vane assembly for a turbofan engine with combined acoustically absorbing and heat exchanging device, corresponding manufacturing method and turbofan engine
10/13/2010CN101858277A Nacelle assembly for turbofan aircraft engines
10/12/2010CA2389780C Emergency device for restarting a turbojet in autorotation
10/07/2010WO2010112453A1 Rotating inlet cowl for a turbine engine, including an eccentric front end
10/07/2010US20100251696 Plasma enhanced rapidly expanded gas turbine engine transition duct
10/07/2010US20100251693 Cascade-type thrust reverser
10/07/2010US20100251692 Methods of combining a series of more efficient aircraft engines into a unit, or modular units
10/07/2010CA2756845A1 Rotating inlet cowl for a turbine engine, including an eccentric front end
10/06/2010EP2236772A2 Gas turbine engine with active tip clearance control device and corresponding operating method
10/06/2010EP2235345A1 A gas turbine engine
10/06/2010CN101850845A Vertical landing lifting system of vertical landing plane
10/05/2010US7805949 Device for supporting and housing auxiliaries in a bypass turbojet
10/05/2010US7805947 Aircraft with disengageable engine and auxiliary power unit components
10/05/2010US7805925 Gas turbine engine exhaust duct ventilation
10/05/2010US7805924 Thermally decoupled mixer
10/02/2010CA2697741A1 Combined acoustic absorber and heat exchanging outlet guide vanes
09/2010
09/30/2010US20100242434 Method of monitoring a thrust reverser
09/30/2010US20100242433 Method for improving the performance of a bypass turbojet engine
09/29/2010EP2233726A2 Bypass duct of a turbofan engine
09/29/2010EP2233703A2 Gas turbine engine with 2.5 bleed duct core case section
09/29/2010EP2233394A2 Propeller with thermally protected blades
09/26/2010CA2696623A1 Active tip clearance control arrangement for gas turbine engine
09/23/2010US20100236216 Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power
09/22/2010EP1744953B1 Boundary layer suction arrangement
09/21/2010US7797922 Gas turbine engine case and method of making
09/19/2010CA2696289A1 Rotary air valve firing patterns for resonance detuning
09/16/2010WO2010102995A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train
09/16/2010US20100229528 Actuation system for a translating variable area fan nozzle
09/16/2010US20100229527 Translating variable area fan nozzle providing an upstream bypass flow exit
09/16/2010DE102009011924A1 Nebenstromkanal eines Turbofantriebwerks Bypass duct of a turbofan engine
09/16/2010CA2754175A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train
09/16/2010CA2658412A1 Hybrid compressor
09/14/2010US7793488 Turbofan case and method of making
09/14/2010CA2389531C Variable cycle propulsion device employing mechanical transmission for supersonic aircraft
09/09/2010US20100223905 Scoop of a running-gap control system of an aircraft gas turbine
09/09/2010US20100223903 Variable pressure ratio compressor
09/08/2010EP2226487A2 Variable drive gas turbine engine
09/08/2010EP2226473A2 Air guiding element of a system for tip clearance adjustment of an aero gas turbine
09/08/2010CN101825115A Blade with built-in bed frame-type pneumatic damping device
09/07/2010US7788899 Fixed nozzle thrust augmentation system
09/07/2010CA2475208C Control system for vertical take off and land (vtol) aircraft
09/02/2010WO2010097438A2 Fan blades with cyclic setting
09/02/2010US20100218505 Afterburner chamber for a turbomachine
09/02/2010US20100218479 Linear telescopic actuator for moving a first and a second element relative to a stationary element
09/02/2010US20100218478 Turbine engine compressor
09/02/2010CA2751805A1 Fan blades with cyclic setting
09/02/2010CA2692068A1 Variable drive gas turbine engine
09/01/2010EP2224120A2 Auxiliary lubricating pump for turbofan drive gear system
09/01/2010EP2224100A2 Controlled fan stream flow bypass
09/01/2010EP2223856A2 Turboprop engine with pusher propeller
09/01/2010EP2010773B1 Blade for a turbine
09/01/2010CN101818703A Turbine fan generator with variable front low pressure fan output vector for aircraft vertical takeoff and landing
08/2010
08/31/2010US7784267 Detonation engine and flying object provided therewith
08/26/2010US20100215479 Gas turbine engine inlet with noise reduction features
08/26/2010US20100212286 Thrust reverser configuration for a short fan duct
08/26/2010US20100212285 Turboprop propulsion unit with pusher propeller
08/25/2010EP2221247A2 Mounting arrangement for a nose cone of a gas turbine engine
08/19/2010WO2010093531A1 Air vehicle propulsion system with counter rotating fan design and method for noise reduction
08/19/2010WO2010092094A1 System of compact contra-rotating propellers
08/19/2010US20100205934 Bypass engine with contrarotating turbine wheels
08/19/2010CA2752214A1 System of compact contra-rotating propellers
08/18/2010CN101806259A Inner culvert turbofan and ram-type double-mode engine
08/17/2010US7775032 Method of operating an exhaust nozzle assembly
08/12/2010WO2010089880A1 Turbofan engine
08/12/2010US20100199633 Bleed structure for a bleed passage in a gas turbine engine
08/10/2010US7770381 Duct burning mixed flow turbofan and method of operation
08/10/2010US7770378 Turbofan case and method of making
08/10/2010US7770377 Turbofan arrangement
08/10/2010CA2455222C Methods and apparatus for operating gas turbine engines
08/05/2010US20100192540 Closing system for an aircraft fan shroud
08/04/2010EP2213866A2 Gas turbine engine assembly with gear and method of assembling same
08/04/2010EP2212538A2 Method for improving the performance of a bypass turbojet engine
08/03/2010US7765790 Stationary mechanical engines and subsonic jet engines using supersonic gas turbines
08/03/2010US7765789 Apparatus and method for assembling gas turbine engines
08/03/2010US7765787 Turbofan case and method of making
08/03/2010US7765786 Aircraft engine with separate auxiliary rotor and fan rotor
07/2010
07/30/2010CA2690665A1 Gas turbine engine assembly and methods of assembling same
07/29/2010US20100186369 Dual flow turboshaft engine and improved hot flow nozzle
07/27/2010US7762057 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines
07/27/2010US7762056 Aircraft combination engines exhaust thrust recovery
07/27/2010CA2389529C Variable cycle propulsion device employing compressed air bleed for supersonic aircraft
07/23/2010CA2690575A1 Blade preloading system and method
07/22/2010US20100180574 Gas turbine engine
07/22/2010US20100180573 A gas turbine engine
07/22/2010US20100180572 Flade fan with different inner and outer airfoil stagger angles at a shroud therebetween
07/13/2010US7752836 Gas turbine assembly and methods of assembling same
07/13/2010US7752835 Pulsed combustion engine
07/13/2010US7752834 Aircraft propulsion systems
07/08/2010US20100170224 Plasma enhanced booster and method of operation
1 ... 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 ... 46