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)
10/2012
10/02/2012USRE43710 Swept turbomachinery blade
10/02/2012US8278774 Gas turbine with wired shaft forming part of a generator/motor assembly
10/02/2012US8276364 Bladder type variable area fan nozzle
10/02/2012US8276362 Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
09/2012
09/27/2012US20120240550 Vehicle Propulsion System
09/26/2012CN102695862A Fluid-cooling device for a turbine engine propulsive unit
09/25/2012US8272204 Core cowl airfoil for a gas turbine engine
09/25/2012US8272203 External fan duct casing in a turbomachine
09/25/2012CA2533425C Turbofan case and method of making
09/20/2012WO2012125895A1 System and method for operating a precooler in an aircraft
09/20/2012WO2012123684A1 Method for optimizing the speed of a twin-spool turbojet engine fan, and architecture for implementing same
09/20/2012WO2012123681A1 Turbomachine with fan(s) for aircraft, with mobile jet nozzle
09/20/2012US20120233982 Gas turbine engine compressor arrangement
09/20/2012US20120233981 Gas turbine engine with low fan pressure ratio
09/20/2012US20120233980 Variable cycle gas turbine engine
09/20/2012CA2829074A1 Turbomachine with fan(s) for aircraft, with mobile jet nozzle
09/19/2012CN102686864A Contra-rotating propeller system for an aircraft turbine engine
09/19/2012CN102678387A Rotary-cone blade jet engine and rotary-cone blade combustion engine
09/18/2012US8266886 Systems and methods involving multiple torque paths for gas turbine engines
09/13/2012WO2012121334A1 Guide vane attachment structure and fan
09/13/2012WO2012098321A3 Nacelle for an aircraft bypass turbojet engine
09/13/2012US20120227375 Gas turbine engine
09/13/2012CA2824281A1 Guide vane attachment structure and fan
09/12/2012EP2496795A1 Dual flow turbine engine for an aircraft including structural means for stiffening the central casing
09/12/2012CN102667072A Dual flow turbine engine for an aircraft including structural means for stiffening the central casing
09/11/2012US8261530 Cambered aero-engine inlet
09/07/2012WO2012117365A1 Fluid machine
09/06/2012US20120222398 Gas turbine engine with geared architecture
09/06/2012US20120222397 Gas turbine engine with low fan pressure ratio
09/06/2012US20120222396 Jet engine device with a bypass duct
09/06/2012DE102011013076A1 Strahltriebwerksvorrichtung mit einem Nebenstromkanal Jet engine device having a bypass duct
09/05/2012EP2495425A2 Jet engine device with a bypass flow channel
09/05/2012EP2495402A2 Fan casing for a turbofan engine
09/05/2012EP2495401A2 A turbomachine casing assembly
09/05/2012EP2495400A2 A turbomachine casing assembly
09/05/2012EP2494178A1 Hybrid propulsive engine including at least one independently rotatable compressor rotor
09/04/2012US8256204 Aircraft engine thrust reverser
09/04/2012US8256203 Rocket based combined cycle propulsion unit having external rocket thrusters
08/2012
08/30/2012WO2012114029A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine
08/30/2012WO2012113541A1 Cooling air inlet and method for operating a cooling air inlet
08/30/2012CA2827014A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine
08/29/2012EP2492484A2 Propfan engine
08/28/2012US8251306 Turbofan engine for stol aircraft
08/28/2012US8250854 Self-starting turbineless jet engine
08/28/2012US8250852 Dual flow turbine engine equipped with a precooler
08/28/2012CA2473819C Guide system for the outer pivot of a variable stator vane, for a turbojet stator
08/22/2012EP2488739A1 Gas turbine engine air intake in a nacelle
08/14/2012US8240124 Method of taking off auxiliary power from an airplane turbojet, and a turbojet fitted to implement such a method
08/09/2012US20120198817 Gas turbine engine with low stage count low pressure turbine
08/09/2012US20120198816 Gas turbine engine compressor arrangement
08/09/2012US20120198815 Gas turbine engine with low stage count low pressure turbine
08/09/2012US20120198814 Use of hot gases and devices
08/08/2012EP2484881A1 Turbine engine tailcone resonator
08/08/2012CN202370694U Gas turbine transformed from retired aircraft
08/08/2012CN101249725B Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained thereby
08/07/2012CA2550458C Valve assembly for a gas turbine engine
08/07/2012CA2432841C Methods and apparatus for operating gas turbine engines
08/02/2012US20120192544 Heated booster splitter plenum
08/02/2012US20120192543 Exhaust nozzle for a bypass airplane turbojet having a deployable secondary cover and a retractable central body
08/01/2012EP2481893A2 Heated booster splitter plenum
08/01/2012EP2480779A1 Convertible fan engine
08/01/2012EP2480778A1 A convertible fan engine comprising a two block compressor
08/01/2012EP2480770A1 Adaptive core engine
08/01/2012EP2480769A1 Method of operating adaptive core engines
08/01/2012EP2074305B1 Gas turbine engine system comprising a translating core cowl and operational method thereof
08/01/2012CN102619642A Efficient turbojet engine
07/2012
07/26/2012WO2012098322A2 Nacelle for an aircraft bypass turbojet engine
07/26/2012WO2012098321A2 Nacelle for an aircraft bypass turbojet engine
07/26/2012CA2824369A1 Nacelle for an aircraft bypass turbojet engine
07/26/2012CA2824367A1 Nacelle for an aircraft bypass turbojet engine
07/25/2012EP2479414A2 Variable area fan nozzle with bypass flow
07/25/2012CN202348475U Micro-turbofan engine
07/25/2012CN102606341A Method for refitting retired aircraft into engine, and engine refitted by such method
07/24/2012US8225593 Twin fan turbomachine
07/19/2012WO2012095592A1 Turbofan engine
07/19/2012DE102011008773A1 Wärmetauscher und Strahltriebwerk mit solchem Heat exchangers and jet engine with such
07/19/2012DE102011008768A1 Counter flow jet engine, has core engine whose counter flow region is divided into inner and outer counter flows by intermediate wall, where passage is provided outside housing of core engine and positioned in inner counter flow
07/19/2012CA2819384A1 Turbofan engine
07/18/2012CN102588143A Minitype turbofan engine
07/18/2012CN102588112A Jet-flow efficient thermal power system
07/12/2012US20120174559 System and method for controlling a gas turbine engine afterburner
07/11/2012CN102575582A Gas turbine engine air intake in a nacelle
07/11/2012CN102562361A Turbojet engine
07/10/2012US8215095 Model-based coordinated air-fuel control for a gas turbine
07/10/2012CA2536759C Induction coupled variable nozzle
07/05/2012WO2012092215A1 Gas turbine engine with bypass mixer
07/05/2012US20120171019 Attachment interface for a gas turbine engine composite duct structure
07/05/2012US20120167551 Electric turbine bypass fan and compressor for hybrid propulsion
07/05/2012US20120167550 Thrust augmented gas turbine engine
07/05/2012US20120167549 Flade discharge in 2-d exhaust nozzle
07/04/2012EP2472090A2 A gas engine turbine comprising a thrust augmentation system
07/04/2012EP2472089A2 Flade discharge in 2-d exhaust nozzle
07/04/2012EP2472067A1 Integration of a surface heat exchanger with controlled air flow in an airplane engine
07/04/2012EP2472060A1 Vane with spar mounted composite airfoil
07/04/2012EP2472059A1 Vane with spar mounted composite airfoil
07/04/2012CN102536511A High thrust aircraft engine
07/03/2012US8209987 Augmentor pilot
07/03/2012US8209953 Gas turbine engine system providing simulated boundary layer thickness increase
07/03/2012US8209952 Gas turbine engine with intermediate speed booster
06/2012
06/28/2012WO2012088543A1 Gas turbine engine heat exchanger
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