| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
|---|
| 06/21/2011 | US7963098 Composite duct assembly |
| 06/21/2011 | CA2726503A1 Integrated nacelle assembly |
| 06/21/2011 | CA2724610A1 Intermediate fan stage |
| 06/16/2011 | US20110138773 Device for mounting a flame-holder arm on an afterburner casing |
| 06/16/2011 | US20110138772 Turbine detuner for recovering kinetic energy from gas turbine engine exhaust gases |
| 06/15/2011 | EP2333287A1 Vectoring transition duct for turbine engine |
| 06/15/2011 | EP2333286A1 Vectoring transition duct for turbine engine |
| 06/15/2011 | EP2333282A2 Variable area fan nozzle stiffeners and placement |
| 06/15/2011 | EP2333278A2 Gas turbine engine |
| 06/15/2011 | EP2333238A2 Gas turbine engine with outer fans |
| 06/15/2011 | EP2333237A2 Multistage bladed tip fan |
| 06/07/2011 | US7954328 Flame holder for minimizing combustor screech |
| 06/02/2011 | US20110126512 Turbofan gas turbine engine aerodynamic mixer |
| 06/01/2011 | EP2326822A2 Test device for the fan of an aircraft engine |
| 06/01/2011 | CN1654804B Three-axis bypass turbojet engine having bypass ratio |
| 06/01/2011 | CN101374723B Dual flow turbine engine equipped with a precooler |
| 05/31/2011 | US7950220 Turbine engine compressor |
| 05/26/2011 | US20110120083 Gas turbine engine with outer fans |
| 05/26/2011 | US20110120082 Multistage tip fan |
| 05/26/2011 | US20110120081 Variable area fan nozzle bearing track |
| 05/26/2011 | US20110120080 Variable area fan nozzle cowl airfoil |
| 05/26/2011 | US20110120079 Variable area fan nozzle stiffeners and placement |
| 05/26/2011 | US20110120078 Variable area fan nozzle track |
| 05/25/2011 | EP2325458A2 Bellows preload and centering spring for a fan drive gear system |
| 05/24/2011 | US7946106 Device for actuating mobile cowls equipping a thrust reverser |
| 05/24/2011 | US7946105 Bi-directional locking ring assembly for aircraft thrust reverser manual drive unit |
| 05/24/2011 | CA2515849C Confluent exhaust nozzle |
| 05/24/2011 | CA2488544C Flame detection method and apparatus for gas turbine exhaust path |
| 05/24/2011 | CA2476503C Duplex mixer exhaust nozzle |
| 05/20/2011 | CA2720158A1 Multistage tip fan |
| 05/20/2011 | CA2720157A1 Gas turbine engine with outer fans |
| 05/18/2011 | EP2322766A2 Oil capture and bypass system |
| 05/18/2011 | CN1950255B Boundary layer suction arrangement |
| 05/18/2011 | CN101598036B Flow control method in large expansion angle channel |
| 05/17/2011 | US7945353 Adaptive control in the presence of input constraints |
| 05/12/2011 | WO2011054806A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing |
| 05/12/2011 | US20110108663 Propulsion device with a plurality of energy converters for an aircraft |
| 05/12/2011 | CA2779253A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing |
| 05/11/2011 | EP2318679A1 Inner wall for the nacelle of a turbine engine |
| 05/05/2011 | WO2011053355A1 Hybrid propulsive engine including at least one independently rotatable compressor rotor |
| 05/04/2011 | EP2317108A2 A boundary layer energiser |
| 05/04/2011 | EP2317107A2 A boundary layer energiser |
| 05/04/2011 | EP2315928A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 05/04/2011 | CN201818391U Duct-suited turbojet engine |
| 05/04/2011 | CN201818390U Efficient turbojet engine |
| 05/04/2011 | CN1657757B Turbofan engine including connecting strut for service conduits and connecting strut for service conduits |
| 05/04/2011 | CN102046983A Air collector in a turbomachine |
| 04/28/2011 | US20110094204 Coupling system connecting an internal structure and an external stucture of a jet engine nacelle |
| 04/27/2011 | CN102032072A Exhaust system for gaseous film cooling central cone of turbofan aircraft engine |
| 04/21/2011 | WO2011045373A1 Gas turbine engine air intake in a nacelle |
| 04/21/2011 | DE102010038132A1 Temperaturmodulierter Kühlstrom von Gasturbinentriebwerken Temperature modulated cooling flow of gas turbine engines |
| 04/21/2011 | CA2776841A1 Gas turbine engine air intake in a nacelle |
| 04/20/2011 | CN201802505U Gas turbine with external ducted blanking cap |
| 04/19/2011 | US7926261 Turbofan provided with a pre-cooler |
| 04/19/2011 | US7926260 Flexible shaft for gas turbine engine |
| 04/19/2011 | US7926259 Turbofan engine assembly and method of assembling same |
| 04/19/2011 | CA2441518C Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans |
| 04/14/2011 | WO2010136710A3 Fluid-cooling device for a turbine engine propulsive unit |
| 04/14/2011 | WO2010059321A3 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 04/14/2011 | US20110083419 Systems and methods for bypassing an inlet air treatment filter |
| 04/14/2011 | US20110083417 Cooling system |
| 04/14/2011 | US20110083416 Propulsion engine |
| 04/14/2011 | DE102009042242A1 Turbofan driving gear has core duct and bypass duct and guide vane collar that is arranged in bypass duct, where selective positioning of supporting struts or bifurcations is determined in certain relation to guide vanes |
| 04/12/2011 | US7921637 High bypass-ratio turbofan jet engine |
| 04/12/2011 | US7921636 Tip turbine engine and corresponding operating method |
| 04/12/2011 | US7921635 Peripheral combustor for tip turbine engine |
| 04/12/2011 | US7921634 Turbofan engine assembly and method of assembling same |
| 04/06/2011 | EP1834076B1 Turbine blade cluster for a fan-turbine rotor assembly and method of mounting such a cluster |
| 04/06/2011 | CN101624945B Jet pressing burning splitting ring curled turbine engine |
| 03/31/2011 | WO2011038216A1 A convertible fan engine comprising a two block compressor |
| 03/31/2011 | WO2011038213A1 Convertible fan engine |
| 03/31/2011 | WO2011038196A1 Method of operating adaptive core engines |
| 03/31/2011 | WO2011038188A1 Adaptive core engine |
| 03/31/2011 | US20110072781 Systems and methods for passively directing aircraft engine nozzle flows |
| 03/31/2011 | US20110072780 Thrust Reverser Actuation |
| 03/31/2011 | CA2775142A1 Method of operating adaptive core engines |
| 03/31/2011 | CA2775139A1 Adaptive core engine |
| 03/31/2011 | CA2775116A1 A convertible fan engine comprising a two block compressor |
| 03/31/2011 | CA2775114A1 Convertible fan engine |
| 03/30/2011 | EP2302189A1 Module arranged at the downstream end of a bypass turbofan engine |
| 03/29/2011 | CA2559963C Gas turbine engine provided with a foreign matter removal passage |
| 03/24/2011 | WO2011033204A1 Turbine engine with contra-rotating non-ducted propellers |
| 03/24/2011 | US20110067407 Flame-holder device comprising an arm support and a heat-protection screen that are in one piece |
| 03/23/2011 | EP2299067A2 Turbomachine core coupling assembly |
| 03/23/2011 | EP1882096B1 Method of reducing noise emissions at the rear of a turbofan engine and turbofan engine thus improved |
| 03/23/2011 | EP1828568B1 Fan-turbine rotor assembly for a tip turbine engine |
| 03/22/2011 | US7908869 Thermal and external load isolating impeller shroud |
| 03/22/2011 | US7908868 Device for mounting an air-flow dividing wall in a turbojet engine afterburner |
| 03/17/2011 | US20110061362 Arrangement for controlling fluid jets injected into a fluid stream |
| 03/16/2011 | EP2295778A2 Energy absorbing fan blade spacer |
| 03/16/2011 | EP2295763A2 Reversed-flow core for a turbofan with a fan drive gear system |
| 03/16/2011 | EP2294320A2 Air collector in a turbomachine |
| 03/16/2011 | CN201763463U Ducted double-fan jet engine |
| 03/15/2011 | US7905083 Turbofan engine assembly and method of assembling same |
| 03/10/2011 | US20110056183 Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan |
| 03/08/2011 | US7900460 Outlet device for a jet engine and a jet engine comprising such an outlet device |
| 03/03/2011 | US20110047960 Dual-flow turbine engine for aircraft with low noise emission |
| 03/02/2011 | EP2290196A2 Adjustable fan case liner and mounting method |
| 03/02/2011 | EP2288797A1 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/02/2011 | EP1825128B1 Regenerative turbine blade and vane cooling for a tip turbine engine |