| Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580) |
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| 07/08/2010 | US20100170222 Mechanical signal processing accumulator attenuation device and method |
| 07/08/2010 | US20100170221 Turbo fan engine |
| 07/08/2010 | US20100170220 Turbofan engine having inner fixed structure including ducted passages |
| 07/07/2010 | EP2204568A2 Gas turbine engine with ejector and corresponding operating method |
| 07/07/2010 | EP2204567A2 Gas turbine engine with ejector and corresponding operating method |
| 07/07/2010 | CN101772635A 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 |
| 07/01/2010 | WO2010072911A1 Aircraft propulsion equipment with an improved reduction gear transmission device |
| 07/01/2010 | WO2010028881A3 Test device for the fan of an aircraft engine |
| 07/01/2010 | US20100168982 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine |
| 07/01/2010 | US20100162684 Aircraft nozzle |
| 07/01/2010 | US20100162683 Turbofan engine |
| 07/01/2010 | US20100162682 Inlet particle separator system for a gas turbine engine |
| 07/01/2010 | US20100162680 Gas turbine engine with ejector |
| 07/01/2010 | DE202010004335U1 Luft- Multiplikator- Düsen- Antrieb für Flugzeuge Air multiplier jet propulsion for aircraft |
| 06/24/2010 | WO2010070066A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 06/24/2010 | US20100155525 Monolithic structure for mounting aircraft engine |
| 06/24/2010 | US20100154384 Geared differential speed counter-rotatable low pressure turbine |
| 06/24/2010 | US20100154383 Gas turbine engine |
| 06/24/2010 | CA2746569A1 System including counter-rotating propellers driven by an epicyclic train ensuring a balanced couple distribution between the two propellers |
| 06/23/2010 | EP2199568A2 Geared differential speed counter-rotatable low pressure turbine |
| 06/22/2010 | US7739866 Turbofan case and method of making |
| 06/22/2010 | US7739865 Gas turbine engine inlet with noise reduction features |
| 06/17/2010 | US20100146933 Nacelle rear assembly for turbojet engine |
| 06/16/2010 | EP2196634A2 Cavity ventilation |
| 06/16/2010 | CN1877100B Counterrotating turbofan engine |
| 06/16/2010 | CA2688727A1 Bypass air scoop for gas turbine engine |
| 06/10/2010 | US20100139243 Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle |
| 06/10/2010 | US20100139242 Thrust reverser with grids for jet engine |
| 06/10/2010 | US20100139241 Flow divider for a fan engine |
| 06/10/2010 | DE102008060489A1 Strömungsteiler für ein Fantriebwerk Flow divider for a fan engine |
| 06/10/2010 | DE102008060488A1 Verfahren und Vorrichtung zum Betrieb eines mit Schubpropellern versehenen Turboprop-Flugtriebwerkes Method and apparatus for operating a provided with thrust propellers turboprop aircraft engine |
| 06/09/2010 | EP2194255A2 Method and device for operating a turboprop aircraft engine with thrust propellers |
| 06/09/2010 | EP2194233A2 Flow splitter for a fan engine |
| 06/09/2010 | CN101730791A Turbojet engine for aircraft |
| 06/08/2010 | US7730715 Fan frame |
| 06/08/2010 | US7730714 Turbofan gas turbine engine with variable fan outlet guide vanes |
| 06/03/2010 | US20100133832 Aeroengine starter/generator arrangement |
| 06/03/2010 | US20100132332 Cascade-type thrust reverser for jet engine |
| 06/03/2010 | US20100132331 Baffle seal for gas turbine engine thrust reverser |
| 06/02/2010 | EP2191124A1 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 |
| 06/02/2010 | CN101716995A Waved wing and waved surface of object |
| 06/01/2010 | US7726116 Turbofan engine nozzle assembly and method of operating same |
| 05/27/2010 | WO2010059321A2 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 05/27/2010 | US20100126141 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 05/27/2010 | US20100126139 Pivoting fan nozzle nacelle |
| 05/27/2010 | CA2742837A1 Gas turbine engine booster having rotatable radially inwardly extending blades and non-rotatable vanes |
| 05/26/2010 | EP2189646A2 Variable pitch rotor arrangement in a gas turbine engine |
| 05/25/2010 | US7721555 Gas turbine with free-running generator driven by by-pass gas flow |
| 05/25/2010 | US7721525 Aircraft engine inlet having zone of deformation |
| 05/25/2010 | US7721524 Integrated airbreathing and non-airbreathing engine system |
| 05/24/2010 | CA2684521A1 Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades |
| 05/18/2010 | US7716914 Turbofan engine assembly and method of assembling same |
| 05/13/2010 | US20100115916 Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 05/13/2010 | US20100115915 Method for controlling electric motors of a thrust reverser |
| 05/13/2010 | US20100115914 Translating core cowl having aerodynamic flap sections |
| 05/12/2010 | EP2184448A2 An air bleeding assembly |
| 05/12/2010 | EP2184447A2 A noise reduction device |
| 05/12/2010 | CN201460989U Counter-rotating turbine with overhanging rotor vane structure |
| 05/12/2010 | CN1755080B Nose cone for a turbomachine |
| 05/11/2010 | US7712315 Augmentor variable vane flame stabilization |
| 05/11/2010 | CA2460662C Methods and apparatus for assembling gas turbine engines |
| 05/06/2010 | US20100107599 Thrust reverser for a jet engine |
| 05/06/2010 | US20100107598 Self-calibration method for the electric jacks of a turbojet nacelle |
| 05/06/2010 | US20100107597 Method for Reducing Sound Output at the Back of a Turbo Engine and Turbo Engine Improved By This Method |
| 05/06/2010 | DE102008037513A1 Baffle seal for deflector flap arrangement of thrust-reverser for gas turbine, has sealing edge including outer peripheral area that extends-out over outer peripheral area of central section, in order to define exposed sealing surface |
| 05/05/2010 | EP2181262A2 Variable area fan nozzle with bypass flow |
| 04/29/2010 | US20100101209 System and method for changing the efficiency of a combustion turbine |
| 04/22/2010 | US20100095650 Translating core cowl for a gas turbine engine |
| 04/21/2010 | EP2177735A2 Turbofan |
| 04/20/2010 | US7698885 Closure and locking detection system for turbojet thrust reverser |
| 04/15/2010 | WO2010042174A1 Method and apparatus for using compressed air to increase the efficiency of a fuel driven turbine generator |
| 04/15/2010 | WO2009144415A3 Air collector in a turbomachine |
| 04/15/2010 | US20100089030 Controlling the aerodynamic drag of a gas turbine engine during a shutdown state |
| 04/15/2010 | US20100089029 Actuator |
| 04/15/2010 | US20100089028 Corrugated core cowl for a gas turbine engine |
| 04/15/2010 | CA2739966A1 Method and apparatus for using compressed air to increase the efficiency of a fuel driven turbine generator |
| 04/13/2010 | US7694505 Gas turbine engine assembly and method of assembling same |
| 04/13/2010 | CA2482324C Gas turbine engine with variable pressure ratio fan system |
| 04/13/2010 | CA2470699C Gas turbine engine with offset drive |
| 04/13/2010 | CA2364124C Reduction gearing to counteract axial force generated by the fan of a turbojet engine |
| 04/08/2010 | US20100083632 Hybrid propulsive engine including at least one independently rotatable compressor rotor |
| 04/08/2010 | US20100083631 Hybrid propulsive engine including at least one independently rotatable turbine stator |
| 04/07/2010 | EP2171218A2 Dual flow turboshaft engine with advanced hot flow nozzle |
| 04/06/2010 | US7690190 Aircraft systems including cascade thrust reversers |
| 04/06/2010 | US7690189 Aircraft combination engines inlet airflow control system |
| 04/06/2010 | US7690188 Combination engines for aircraft |
| 04/06/2010 | CA2460854C Converging nozzle thrust reverser |
| 04/01/2010 | US20100077724 Core cowl airfoil for a gas turbine engine |
| 03/31/2010 | EP2167798A2 Turbojet engine for aircraft |
| 03/30/2010 | US7685808 Gas turbine engine assembly and methods of assembling same |
| 03/30/2010 | US7685805 Turbofan gas turbine engine and nacelle arrangement |
| 03/25/2010 | WO2010033706A1 Thermal management system |
| 03/25/2010 | US20100072324 Nacelle for double flow engine |
| 03/25/2010 | US20100071345 Thrust Engine |
| 03/25/2010 | CA2738593A1 Thermal management system |
| 03/18/2010 | US20100064660 Jet engine nacelle member |
| 03/18/2010 | US20100064659 Translating variable area fan nozzle with split beavertail fairings |
| 03/17/2010 | EP2163754A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine |
| 03/11/2010 | US20100058736 Device for opening and closing a thrust reverser door of a jet engine |
| 03/11/2010 | US20100058735 Operational line management of low pressure compressor in a turbofan engine |