| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 02/27/2014 | WO2013172893A3 Composite airfoil with local tailoring of material properties |
| 02/27/2014 | US20140053533 Reverse flow gas turbine engine with thrust reverser |
| 02/26/2014 | CN103608547A Dual-flow turbine engine having decoupling device |
| 02/26/2014 | CN103608260A Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine |
| 02/26/2014 | CN102203401B Test device for the fan of an aircraft engine |
| 02/26/2014 | CN101970844B Method for improving the performance of a bypass turbojet engine and turbojet engine using said method |
| 02/25/2014 | CA2585893C Jet turbine engine having a post-combustion channel cooled by a variable-flow rate ventilation flow |
| 02/19/2014 | CN103597195A Tail cone for a microjet rotary turbine engine |
| 02/19/2014 | CN103590907A Temperature-changing internal combustion turbine |
| 02/18/2014 | US8650853 Noise reduction assembly for aircraft turbojet |
| 02/13/2014 | WO2014023891A1 Turbomachine comprising a plurality of fixed radial blades mounted upstream of the fan |
| 02/13/2014 | WO2013187944A3 Counter rotating low pressure compressor and turbine each having a gear system |
| 02/13/2014 | US20140041360 Flow conducting assembly for cooling the low-pressure turbine housing of a gas turbine jet engine |
| 02/12/2014 | EP2696040A1 Flow guidance device for cooling the low pressure turbine casing of a gas turbine radiation engine |
| 02/12/2014 | EP2694791A1 Quiet bleed valve for gas turbine engine |
| 02/12/2014 | CN103573469A Fan pneumatic layout structure and method of turbofan engine |
| 02/06/2014 | WO2014022344A1 Cmc core cowl and method of fabricating |
| 02/06/2014 | WO2014022119A1 Retrofitable auxiliary inlet scoop |
| 02/06/2014 | WO2013172905A3 Counter-rotating low pressure turbine with gear system mounted to mid turbine frame |
| 02/05/2014 | CN103562518A Gas turbine engine comprising three rotary bodies |
| 01/30/2014 | WO2014018198A1 Air-cooled engine surface cooler |
| 01/30/2014 | WO2014018141A2 Geared turbofan with three turbines all counter-rotating |
| 01/30/2014 | WO2014017585A1 Engine duct, and aircraft engine |
| 01/30/2014 | US20140030060 Geared fan with inner counter rotating compressor |
| 01/30/2014 | US20140027581 Aircraft having a rotating turbine engine |
| 01/28/2014 | CA2569762C Axial flow positive displacement worm compressor |
| 01/23/2014 | WO2014014596A1 Gearbox for gas turbine engine |
| 01/23/2014 | WO2013180797A3 Shark-bite tip shelf cooling configuration |
| 01/23/2014 | WO2013172892A3 Debris detection in turbomachinery and gas turbine engines |
| 01/22/2014 | EP2686539A1 Turbomachine with fan(s) for aircraft, with mobile jet nozzle |
| 01/22/2014 | EP2686522A1 System and method for operating a precooler in an aircraft |
| 01/21/2014 | CA2658412C Hybrid compressor |
| 01/16/2014 | WO2013176717A3 Pressure balanced area control of high aspect ratio nozzle |
| 01/16/2014 | WO2013172899A3 Gas turbine engine systems involving tip fans |
| 01/16/2014 | WO2013169316A3 Geared turbofan gas turbine engine architecture |
| 01/16/2014 | WO2013165524A3 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case |
| 01/16/2014 | WO2013165507A3 Cooling hole with asymmetric diffuser |
| 01/15/2014 | CN103511124A Air flow guide device |
| 01/09/2014 | WO2014008015A1 Gas turbine engine component having platform cooling channel |
| 01/09/2014 | WO2014007908A1 Turbine exhaust case duct |
| 01/09/2014 | WO2013172906A3 Counter rotating low pressure turbine with splitter gear system |
| 01/09/2014 | WO2013172903A3 Tapered thermal coating for airfoil |
| 01/09/2014 | WO2013165510A3 Multi-lobed cooling hole and method of manufacture |
| 01/09/2014 | WO2013165504A3 Manufacturing methods for multi-lobed cooling holes |
| 01/08/2014 | EP2681438A2 Fault tolerant control system for distributed micro-thrusters |
| 01/08/2014 | CN103502580A Integrated variable geometry flow restrictor and heat exchanger |
| 01/07/2014 | US8622687 Method of operating adaptive core engines |
| 01/07/2014 | US8621871 Systems and methods involving multiple torque paths for gas turbine engines |
| 01/07/2014 | CA2516752C Counter-rotating turbine engine and method of assembling same |
| 01/03/2014 | WO2014004266A1 Thrust reverser maintenance actuation system |
| 01/03/2014 | WO2014004122A1 Pre-turbine exhaust case variable area mixing plane |
| 01/03/2014 | WO2014003958A1 Turbine blade platform with u-channel cooling holes |
| 01/03/2014 | WO2013181389A3 Ladder seal system for gas turbine engines |
| 01/03/2014 | WO2013165527A3 High order shaped curve region for an airfoil |
| 01/03/2014 | WO2013165513A3 Counter-rotating low pressure turbine without turbine exhaust case |
| 01/03/2014 | WO2013165511A3 Edm method for multi-lobed cooling hole |
| 01/03/2014 | WO2013165506A3 Cooling hole with crenellation features |
| 01/03/2014 | WO2013165503A3 Cooling hole with enhanced flow attachment |
| 01/03/2014 | WO2013165502A3 Cooling hole with thermo-mechanical fatigue resistance |
| 01/03/2014 | WO2013154639A3 Gas turbine engine with improved fuel efficiency |
| 01/03/2014 | WO2013147944A3 Compressor guide vane and pilot control for gas turbine engine |
| 01/02/2014 | US20140000268 Igniter for a turbomachine and mounting assembly therefore |
| 01/02/2014 | DE102009053000B4 Fanrückhaltescheibe für ein Strahltriebwerk Fanrückhaltescheibe for a jet engine |
| 01/01/2014 | EP2678543A1 Driveshaft for the gearbox of auxiliary machines of a turbojet engine |
| 01/01/2014 | EP2678532A1 Cooling air inlet and method for operating a cooling air inlet |
| 01/01/2014 | CN103492158A Moulded article |
| 01/01/2014 | CN102235267B Gas turbine engine modified by using retired turbofan engine through low-pressure crest truncation |
| 12/31/2013 | US8615982 Integrated electric variable area fan nozzle thrust reversal actuation system |
| 12/27/2013 | WO2013192525A1 Liquid fuel turbine engine for reduced oscillations |
| 12/27/2013 | WO2013191889A1 Turbomachine flow stability enhancement device control |
| 12/27/2013 | WO2013191877A1 Airfoil including adhesively bonded shroud |
| 12/27/2013 | WO2013191195A1 Vane linking portion structure, and jet engine using same |
| 12/27/2013 | WO2013191070A1 Fan case for aircraft engine |
| 12/27/2013 | WO2013188956A1 Cryogenic fuel combustion engines |
| 12/27/2013 | WO2013165509A3 Multi-lobed cooling hole |
| 12/27/2013 | WO2013165508A3 Multi-lobed cooling hole array |
| 12/27/2013 | WO2013165505A3 Composite fan containment case assembly |
| 12/27/2013 | WO2013162665A3 Engine hot section vane with tapered flame holder surface |
| 12/27/2013 | CA2875928A1 Fan case for aircraft engine |
| 12/26/2013 | US20130343867 Gas turbine engine with reverse-flow core having a bypass flow splitter |
| 12/26/2013 | US20130340406 Fan stagger angle for geared gas turbine engine |
| 12/25/2013 | CN102108915B Turbofan engine for stol aircraft |
| 12/19/2013 | WO2013188722A1 High durability turbine exhaust case |
| 12/19/2013 | WO2013187944A2 Counter rotating low pressure compressor and turbine each having a gear system |
| 12/19/2013 | WO2013187938A1 Gas turbine engine shaft bearing arrangement |
| 12/19/2013 | WO2013165518A3 Gas turbine engine component with cusped, lobed cooling hole |
| 12/19/2013 | WO2013165517A3 Gas turbine engine component with diffusive cooling hole |
| 12/14/2013 | CA2780754A1 Turbine having cooperating and counter-rotating rotors in a same plane |
| 12/12/2013 | WO2013184568A1 Compressor power and torque transmitting hub |
| 12/12/2013 | WO2013184495A2 Combustor liner with decreased liner cooling |
| 12/12/2013 | WO2013184429A1 Front bearing support for a fan drive gear system |
| 12/12/2013 | WO2013184426A1 Nacelle bifurcation for gas turbine engine |
| 12/12/2013 | WO2013184330A1 Nacelle inner flow structure leading edge latching system |
| 12/12/2013 | WO2013184264A1 Integrated fuel pump and control |
| 12/12/2013 | US20130327014 Devices and Methods to Optimize Aircraft Power Plant and Aircraft Operations |
| 12/10/2013 | US8601789 Hydraulic control system for a thrust reversal device |
| 12/10/2013 | US8601788 Dual flow turboshaft engine and improved hot flow nozzle |
| 12/10/2013 | US8601786 Operational line management of low pressure compressor in a turbofan engine |
| 12/05/2013 | WO2013181389A2 Ladder seal system for gas turbine engines |
| 12/05/2013 | WO2013181051A1 Lubrication arrangement for a gas turbine engine gear assembly |