| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 02/24/2011 | DE102008024463B4 Flugzeugantriebssystem Aircraft propulsion system |
| 02/23/2011 | EP2286078A2 Fan blade retention and variable pitch system |
| 02/23/2011 | EP1941148B1 Turbofan engine for stol aircraft |
| 02/22/2011 | US7891167 Gas turbine engine flow reverser |
| 02/17/2011 | US20110036067 Airflow modulation for dual mode combined cycle propulsion systems |
| 02/16/2011 | EP1825126B1 Vectoring transition duct for turbine engine |
| 02/16/2011 | CN101978150A System of counter-rotating propellers with a feathering device for propeller blades |
| 02/16/2011 | CN101975121A Culvert sleeved turbojet engine |
| 02/15/2011 | US7887296 Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine |
| 02/15/2011 | US7887287 Turbofan jet engine |
| 02/15/2011 | US7886542 Device for attaching a flame-arrestor arm to an afterburner casing and afterburner comprising such a device |
| 02/15/2011 | US7886520 Gas turbine engine |
| 02/10/2011 | WO2011016945A2 Coannular ducted fan |
| 02/10/2011 | US20110030338 Bypass turbojet engine nacelle |
| 02/10/2011 | US20110030337 Wall cooling device |
| 02/10/2011 | US20110030336 Coannular ducted fan |
| 02/10/2011 | DE102009036011A1 Aircraft engine, has flow channel provided with inflow opening and extending within tip area of propeller blade in outflow opening, and gas turbine introducing gas flow e.g. exhaust gas flow, into outflow opening |
| 02/09/2011 | EP2282016A2 Turbofan temperature control with variable area nozzle |
| 02/09/2011 | CN201739027U Turbofan rear-mounted engine |
| 02/09/2011 | CN201739026U Turbofan post-type engine waste gas exhaust structure |
| 02/09/2011 | CN101970844A Method for improving the performance of a bypass turbojet engine and turbojet engine using said method |
| 02/09/2011 | CN101968013A Single-tube rotary valve type double-bypass pulse detonation engine |
| 02/09/2011 | CN101968012A High-efficiency turbojet engine |
| 02/08/2011 | US7882695 Turbine blow down starter for turbine engine |
| 02/08/2011 | US7882694 Variable fan inlet guide vane assembly for gas turbine engine |
| 02/08/2011 | US7882693 Turbofan engine assembly and method of assembling same |
| 02/03/2011 | WO2011014346A2 Integrated thrust reverser assembly |
| 02/03/2011 | WO2010018314A8 Inner wall for the nacelle of a turbine engine |
| 02/03/2011 | US20110023451 Propulsion System With Movable Thermal Choke |
| 02/03/2011 | US20110023450 Integrated Thrust Reverser Assembly |
| 02/03/2011 | CA2769313A1 Integrated thrust reverser assembly |
| 02/02/2011 | EP2074303B1 Core cowl airfoil for a gas turbine engine |
| 02/02/2011 | CN101963073A Counterrotating turbine with overhung rotor blade structure |
| 02/01/2011 | US7878003 Fuel control system for gas turbine engine reheat apparatus |
| 02/01/2011 | US7877980 Convertible gas turbine engine |
| 01/27/2011 | US20110016846 Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter |
| 01/26/2011 | EP2278147A2 Translating variable area fan nozzle providing an upstream bypass flow exit |
| 01/26/2011 | EP2278146A2 Actuation system for a translating variable area fan nozzle |
| 01/26/2011 | EP2278124A1 Swept turbomachinery blade |
| 01/26/2011 | CN101956629A Method for improving speed reducer of turboprop engine |
| 01/25/2011 | US7874142 Aeroengine thrust reverser |
| 01/20/2011 | WO2011008333A1 Heated guide vane |
| 01/20/2011 | US20110011058 Turbofan engine |
| 01/20/2011 | DE102009033755A1 Turbofantriebwerk Turbofan |
| 01/20/2011 | CA2766446A1 Heated guide vane |
| 01/19/2011 | EP2275663A2 Turbofan engine |
| 01/18/2011 | US7870740 Turbojet engine comprising an afterburner duct cooled by a variable-throughput ventilation stream |
| 01/18/2011 | US7870722 Systems and methods for passively directing aircraft engine nozzle flows |
| 01/18/2011 | US7870721 Gas turbine engine providing simulated boundary layer thickness increase |
| 01/13/2011 | US20110005196 Method and apparatus for increasing thrust or other useful energy output of a device with a rotating element |
| 01/13/2011 | US20110005194 Flashback shut-off |
| 01/13/2011 | DE10217399B4 Flugzeugturbine mit einer Vorrichtung zum sicheren Abschalten trotz Einwirken einer großen Unwucht des Laufrades Aircraft turbine with a device for safe disconnection, despite the action of a large unbalance of the impeller |
| 01/11/2011 | US7866142 Aeroengine thrust reverser |
| 01/11/2011 | US7866141 Cooling device for the primary nozzle of a dual-flow turbojet engine |
| 01/11/2011 | CA2478198C Methods and apparatus for flade engine nozzle |
| 01/06/2011 | US20110004388 Turbofan temperature control with variable area nozzle |
| 01/05/2011 | EP2270326A2 Turbofan engine |
| 01/05/2011 | CN101939528A Variable area fan nozzle with bypass flow |
| 01/04/2011 | US7861513 Aeroengine ventilation system |
| 01/04/2011 | US7861512 Turbofan bypass duct air cooled fluid cooler installation |
| 01/04/2011 | CA2646629C Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 12/30/2010 | US20100326050 Aircraft gas turbine engine counter-rotatable generator |
| 12/30/2010 | US20100326048 Gas turbine engine duct having a coupled fluid volume |
| 12/30/2010 | US20100326047 System and method for assembling a thrust reverser for a gas turbine propulsion system |
| 12/30/2010 | US20100326046 Valve system for a gas turbine engine |
| 12/29/2010 | CN101929406A Vortex cold vacuum aircraft engine |
| 12/28/2010 | US7856828 Flameholder arm for an afterburner |
| 12/28/2010 | US7856827 Structural track support of spraybars/tubing |
| 12/22/2010 | CN101922379A Translating variable area fan nozzle providing an upstream bypass flow exit |
| 12/21/2010 | US7854112 Vectoring transition duct for turbine engine |
| 12/16/2010 | US20100313546 Control system for turbojet engine nacelle |
| 12/15/2010 | EP2260197A1 Contra-rotating propeller system with device for feathering propeller blades |
| 12/09/2010 | US20100307130 Non-handed thrust reverser for installation on handed aircraft gas turbine propulsion engines |
| 12/08/2010 | CN201666197U Fan wheel disc |
| 12/07/2010 | US7845158 Turbine engine mounting arrangement |
| 12/07/2010 | US7845157 Axial compressor for tip turbine engine |
| 12/02/2010 | WO2010136686A2 Device for controlling the orientation of the blades of a turboprop fan |
| 12/02/2010 | WO2010136685A2 Movable actuator device for controlling the orientation of the blades of a turboprop fan |
| 12/02/2010 | CA2762830A1 Movable actuator device for controlling the orientation of the blades of a turboprop fan |
| 12/02/2010 | CA2762229A1 Device for controlling the orientation of the blades of a turboprop fan |
| 12/01/2010 | EP2256327A1 Noise reducing device, and jet propulsion system |
| 11/30/2010 | US7841165 Gas turbine engine assembly and methods of assembling same |
| 11/25/2010 | US20100293920 Propfan engine |
| 11/24/2010 | EP2253805A2 Zero gravity lubrication system |
| 11/23/2010 | US7837155 Boundary layer suction arrangement |
| 11/23/2010 | US7836700 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws |
| 11/23/2010 | US7836680 Aircraft combination engines thermal management system |
| 11/18/2010 | US20100287910 Nacelle with simplified cowling arrangement |
| 11/17/2010 | EP2251540A2 Turbofan mounting system |
| 11/17/2010 | CN201635864U Turbojet engine |
| 11/16/2010 | US7832193 Gas turbine engine assembly and methods of assembling same |
| 11/11/2010 | US20100281849 Door-type thrust reverser for a jet engine |
| 11/10/2010 | CN101881237A Turbofan postpose type engine |
| 11/09/2010 | CA2435360C Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 11/04/2010 | US20100275575 Method and systems for controlling engine thrust using variable trim |
| 11/03/2010 | EP2246529A2 Combined oil filter and debris monitor |
| 11/03/2010 | EP1828574B1 Close coupled gearbox assembly for a tip turbine engine |
| 11/03/2010 | CN201620968U Multielement inlet turbine rear augmentation fan engine |
| 11/02/2010 | US7823836 Optimal sun safe attitude for satellite ground tracking |
| 11/02/2010 | US7823374 Heat transfer system and method for turbine engine using heat pipes |