| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 05/08/2013 | EP2589781A2 Hollow fan blade tuning using distinct filler materials |
| 05/08/2013 | EP2589756A2 Transition Piece Aft Frame |
| 05/08/2013 | EP2589752A2 Non Axis-Symmetric Stator Vane Endwall Contour |
| 05/08/2013 | CN1900508B Integrated counterrotating turbofan |
| 05/08/2013 | CN101772635B Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise, and turbojet and motor assembly associated therewith |
| 05/07/2013 | US8434293 High stiffness shape memory alloy actuated aerostructure |
| 05/04/2013 | CA2756914A1 Turbofan mounting arrangement |
| 05/02/2013 | US20130104524 Turbofan with gear-driven compressor and fan-driven core |
| 05/02/2013 | US20130104523 Gas turbine engine with auxiliary fan |
| 05/02/2013 | US20130104522 Gas turbine engine with variable pitch first stage fan section |
| 05/02/2013 | US20130104521 Gas turbine engine with two-spool fan and variable vane turbine |
| 05/01/2013 | EP2587039A2 Gas turbine engine with auxiliary fan |
| 05/01/2013 | EP2587037A2 Turbofan engine mixer assembly |
| 04/30/2013 | CA2619292C Method for attenuating the noise of a turbofan |
| 04/25/2013 | WO2013059456A1 Gas turbine engine component axis configurations |
| 04/25/2013 | US20130101402 Fan housing with cooling slots |
| 04/25/2013 | US20130097997 Ram air fan diffuser |
| 04/25/2013 | US20130097996 Ram air fan inlet housing |
| 04/25/2013 | CA2792750A1 A support ring for a rotary assembly |
| 04/24/2013 | EP2582959A1 Aircraft turbo jet engine fan casing |
| 04/24/2013 | EP2582580A1 Airflow-straightening structure for the nacelle of an aircraft engine |
| 04/24/2013 | CN202900416U Jet-flow high-efficiency thermal power system |
| 04/24/2013 | CN103061918A Gas turbine engine assembly and method of assembling same |
| 04/24/2013 | CN101968013B Single-tube rotary valve type double-bypass pulse detonation engine |
| 04/23/2013 | CA2564677C Bleed valve for a gas turbine engine |
| 04/18/2013 | US20130092756 Variable area nozzle for gas turbine engine |
| 04/18/2013 | US20130091849 Augmentor spray bar with tip support bushing |
| 04/18/2013 | DE102011084360A1 Flow working machine for use in aircraft engine, has main rotor disk or drum driven by main shaft, and auxiliary rotor disk or drum driven by auxiliary shaft, where shafts comprise different rotational speed and/or rotational direction |
| 04/17/2013 | EP2580121A1 Turbojet engine nacelle |
| 04/17/2013 | CN103047049A Turbojet engine |
| 04/16/2013 | US8418437 Jet flow discharge nozzle and jet engine |
| 04/16/2013 | US8418436 Variable area fan nozzle and thrust reverser |
| 04/16/2013 | CA2565011C Boundary layer suction arrangement |
| 04/10/2013 | EP2578864A1 Variable area fan nozzle with bypass flow |
| 04/10/2013 | EP2578813A1 Strut rods for structural guide vanes |
| 04/09/2013 | CA2776318C Turbofan case and method of making |
| 04/09/2013 | CA2776254C Turbofan case and method of making |
| 04/04/2013 | US20130081375 Conformal inlet apparatus for a gas turbine engine |
| 04/03/2013 | EP2574758A2 Conformal inlet apparatus for a gas turbine engine |
| 04/03/2013 | CN101535622B Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with the device |
| 04/03/2013 | CN101117926B Flade fan with different inner and outer airfoil stagger angles at a shroud therebetween |
| 04/02/2013 | CA2776661C Turbofan case and method of making |
| 04/02/2013 | CA2776404C Turbofan case and method of making |
| 04/02/2013 | CA2776341C Turbofan case and method of making |
| 04/02/2013 | CA2776317C Turbofan case and method of making |
| 04/02/2013 | CA2776316C Turbofan case and method of making |
| 03/30/2013 | CA2790448A1 Conformal inlet apparatus for a gas turbine engine |
| 03/28/2013 | US20130075492 Thrust reverser translating sleeve assembly |
| 03/27/2013 | CN103003573A Turbine engine having two unducted propellers |
| 03/26/2013 | US8402765 Translating variable area fan nozzle providing an upstream bypass flow exit |
| 03/26/2013 | US8402743 Actuating of a thrust reverser in a turbomachine |
| 03/26/2013 | US8402742 Gas turbine engine systems involving tip fans |
| 03/26/2013 | US8402741 Gas turbine engine shaft bearing configuration |
| 03/26/2013 | US8402740 Aircraft propulsion unit in multi-fan design |
| 03/26/2013 | US8402739 Variable shape inlet section for a nacelle assembly of a gas turbine engine |
| 03/20/2013 | CN102985677A Aircraft turbo jet engine fan casing |
| 03/13/2013 | CN102971217A Airflow-straightening structure for the nacelle of an aircraft engine |
| 03/12/2013 | US8393139 Device with secondary jets reducing the noise generated by an aircraft jet engine |
| 03/12/2013 | CA2502793C High efficiency rotor for the second phase of a gas turbine |
| 03/06/2013 | EP2565424A2 Torque frame and asymmetric journal bearing for fan drive gear system |
| 03/06/2013 | EP2565423A2 Accessory gearbox buffer cooling air pump system and method of providing cooling air |
| 03/06/2013 | EP2564051A1 Airfoil combination for aircraft turbofan |
| 03/06/2013 | CN102953759A Pitch change mechanism for open rotor framework |
| 03/05/2013 | US8387362 Method and apparatus for operating gas turbine engine heat exchangers |
| 03/05/2013 | US8387357 Recuperated bypass turbine engine |
| 02/28/2013 | US20130047580 Turbine engine |
| 02/28/2013 | US20130047579 Gas turbine engine fan variable area nozzle with swivable insert system |
| 02/26/2013 | US8381510 Method and systems for controlling engine thrust using variable trim |
| 02/26/2013 | CA2786182A1 Pitch change mechanism for open rotor architecture |
| 02/21/2013 | WO2013025385A1 Panels and processes therefor |
| 02/21/2013 | WO2013024231A1 Method of determining the performance of at least one propeller of a turbomachine in an air stream under gyration |
| 02/21/2013 | CA2844624A1 Panels and processes therefor |
| 02/19/2013 | US8375699 Variable area fan nozzle with wall thickness distribution |
| 02/19/2013 | US8375698 Method for reducing the vibration levels of a propfan of contrarotating bladed disks of a turbine engine |
| 02/19/2013 | CA2608373C Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 02/19/2013 | CA2492418C Methods and apparatus for operating gas turbine engines |
| 02/14/2013 | WO2013021127A1 Hydraulic control system for controlling the orientation of fan blades |
| 02/13/2013 | CN102933462A Turbojet engine nacelle |
| 02/13/2013 | CN101614164B Thrust reverser cascade assembly and rear cascade ring with flow deflector portion |
| 02/12/2013 | US8371105 Hydraulic system for fan pitch change actuation of counter-rotating propellers |
| 02/12/2013 | CA2524141C Counter-rotating turbine engine and method of assembling same |
| 02/07/2013 | WO2013017771A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle |
| 02/07/2013 | CA2841167A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle |
| 02/06/2013 | EP2553251A1 Adaptive fan system for a variable cycle turbofan engine |
| 02/06/2013 | CN202719358U Core board and vane and hollow fan used in aero-engine |
| 02/05/2013 | US8365515 Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle |
| 02/05/2013 | US8365514 Hybrid turbofan engine |
| 02/05/2013 | US8365511 Tip turbine engine integral case, vane, mount and mixer |
| 01/31/2013 | US20130026301 Nacelle for variable section nozzle propulsion unit |
| 01/31/2013 | US20130025258 Geared turbofan bearing arrangement |
| 01/31/2013 | US20130025257 Three spool engine bearing configuration |
| 01/31/2013 | DE102011108887A1 Gasturbinenzentripetalringbrennkammer sowie Verfahren zur Strömungsführung Gasturbinenzentripetalringbrennkammer and methods for guiding the flow |
| 01/30/2013 | EP2551485A2 Gas turbine engine with aft core driven fan section |
| 01/29/2013 | CA2729685C Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 01/24/2013 | WO2013012316A1 Turbofan engine with convergent - divergent exhaust nozzle |
| 01/24/2013 | WO2013011225A2 Device for supplying fluid to a hydraulic jack for controlling the orientatin of the fan blades of a twin fan turboprop |
| 01/24/2013 | WO2012175863A3 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine |
| 01/24/2013 | US20130019585 Variable fan inlet guide vane for turbine engine |
| 01/24/2013 | CA2875090A1 Turbofan engine with convergent - divergent exhaust nozzle |
| 01/24/2013 | CA2842157A1 Device for supplying fluid to a hydraulic jack for controlling the orientatin of the fan blades of a twin fan turboprop |