| Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699) |
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| 05/16/2009 | CA2638840A1 Thrust reverser for a turbofan gas turbine engine |
| 05/16/2009 | CA2638720A1 Thrust reverser door |
| 05/14/2009 | WO2009060295A1 A device and method for controlling vortex structures in a turbulent air jet |
| 05/14/2009 | WO2009060133A2 Dual action telescopic linear actuator |
| 05/14/2009 | WO2009030837A3 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine |
| 05/14/2009 | US20090121078 Aircraft pod and aircraft equipped with at least one such pod |
| 05/14/2009 | US20090121046 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flaws |
| 05/14/2009 | CA2703226A1 A device and method for controlling vortex structures in a turbulent air jet |
| 05/07/2009 | WO2009056713A2 Double-acting telescopic linear actuator with single-motor drive system |
| 05/07/2009 | WO2009034246A3 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 05/07/2009 | WO2007005520A3 Jet nozzle mixer |
| 05/07/2009 | US20090114740 Nozzle assembly with flow conduits |
| 05/07/2009 | CA2700085A1 Actionneur lineaire telescopique double action a systeme d'entrainement a moteur unique |
| 05/06/2009 | EP2054608A1 Aircraft engine thrust reverser |
| 05/06/2009 | CN101426681A Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 04/30/2009 | WO2009053560A2 Structure for thrust inverter |
| 04/30/2009 | WO2009053554A1 Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron |
| 04/30/2009 | WO2009025895A3 Modular chevron exhaust nozzle |
| 04/30/2009 | DE19855708B4 Rohrkammerdämpfer Pipe chamber damper |
| 04/30/2009 | CA2696425A1 Structure for thrust inverter |
| 04/30/2009 | CA2695626A1 Turboshaft engine with reduced noise emission for aircraft |
| 04/30/2009 | CA2694996A1 Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron |
| 04/29/2009 | EP2053231A2 Gas turbine engine reheat fuel system |
| 04/28/2009 | US7523604 Thrust reverser mounting structure |
| 04/23/2009 | WO2009024688A3 System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system |
| 04/23/2009 | US20090100823 Gas turbine engine reheat fuel system |
| 04/23/2009 | US20090100678 Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing |
| 04/22/2009 | EP2050948A2 A gas turbine engine assembly with a variable area nozzle and a method of controlling this nozzle |
| 04/22/2009 | CN100480500C Axial-symmetric vector spray-tube A9/A8 area ratio dislocation protection hydraulic system |
| 04/21/2009 | US7520369 Soundproofing panel with beads, and a method of manufacture |
| 04/21/2009 | US7520135 Variable-section turbomachine nozzle |
| 04/21/2009 | US7520124 Asymmetric serrated nozzle for exhaust noise reduction |
| 04/16/2009 | WO2008139095A3 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained |
| 04/16/2009 | CA2638661A1 Exhaust duct with bypass channel |
| 04/15/2009 | EP2048344A2 Jet or rocket engine with heat insulated exhaust nozzle |
| 04/15/2009 | CN101410300A Air inlet shroud structure |
| 04/09/2009 | WO2008054436A3 Damped coil pin for attachment hanger hinge |
| 04/09/2009 | US20090090095 Aircraft turbofan engine |
| 04/08/2009 | CN101403349A Jet engine exhausting pipe of high-speed locomotive and its near-net-shape casting method |
| 04/07/2009 | US7513101 Synchronized motor thrust reverser actuation system |
| 04/02/2009 | US20090084111 Turbomachine nozzle cowl having jet noise reduction patterns |
| 04/01/2009 | EP2042721A1 Turbomachine nozzle cowl having jet noise suppression pattern, corresponding nozzle and turbomachine |
| 04/01/2009 | EP1934456B1 Turbofan engine with a device for attenuating the jet noise |
| 03/31/2009 | US7509797 Thrust vectoring missile turbojet |
| 03/31/2009 | US7509796 Pintle-controlled propulsion system with external dynamic seal |
| 03/28/2009 | CA2640236A1 Cowling for turbine engine nozzle with jet noise reduction patterns |
| 03/26/2009 | WO2008148999A3 Exhaust system for gas turbine |
| 03/24/2009 | US7506501 Compact mixer with trimmable open centerbody |
| 03/19/2009 | WO2009034247A1 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/19/2009 | WO2009034246A2 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/19/2009 | WO2009034245A1 Method and system for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/19/2009 | WO2009034240A1 Mobile thrust reverser cowl and thrust reverser provided with such a cowl |
| 03/19/2009 | US20090072047 Aircraft defense system and method |
| 03/19/2009 | US20090071164 Fluted chevron exhaust nozzle |
| 03/19/2009 | US20090071122 Thrust reverser mounting structure |
| 03/19/2009 | CA2707517A1 Mobile thrust reverser cowl and thrust reverser provided with such a cowl |
| 03/19/2009 | CA2694924A1 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/19/2009 | CA2694923A1 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/19/2009 | CA2693355A1 Method and system for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 03/18/2009 | EP2035680A2 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 03/17/2009 | US7503425 Integrated inlet attachment |
| 03/17/2009 | US7503164 Ducted fan with containment structure |
| 03/17/2009 | CA2565713C Method for opening a mobile cowl equipping a thrust reverser |
| 03/12/2009 | WO2009030837A2 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine |
| 03/12/2009 | WO2008111992A4 Monolithic thrust reverser components |
| 03/12/2009 | US20090067993 Coated variable area fan nozzle |
| 03/12/2009 | US20090064681 Scalloped Flexure Ring |
| 03/12/2009 | US20090064660 Nozzle with yaw vectoring vane |
| 03/12/2009 | US20090064659 Gas turbine engine with fan variable area nozzle having a rotational valve system |
| 03/12/2009 | US20090064658 Bypass turbomachine with reduction of jet noise |
| 03/12/2009 | CA2694992A1 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine |
| 03/11/2009 | EP2034136A2 Scalloped flexure ring |
| 03/11/2009 | EP2034135A2 Bipod flexure ring |
| 03/11/2009 | EP2032830A1 Guiding carrier for jet engine linings |
| 03/11/2009 | EP2032829A1 Engine exhaust system with directional nozzle |
| 03/11/2009 | EP2032828A2 Engine exhaust system |
| 03/10/2009 | US7500353 Eductor swirl buster |
| 03/05/2009 | WO2009029401A2 Variable area fan nozzle with bypass flow |
| 03/05/2009 | WO2009027591A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 03/05/2009 | CA2696393A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 03/04/2009 | EP2029880A1 Thrust reverser forming an adaptive nozzle |
| 03/04/2009 | EP2029879A1 Aircraft propulsion assembly comprising a jet pipe with a notched trailing edge |
| 03/03/2009 | US7497300 Noise reduction tubes |
| 02/26/2009 | WO2009025895A2 Modular chevron exhaust nozzle |
| 02/26/2009 | WO2009024688A2 System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system |
| 02/26/2009 | WO2009024659A1 Thrust reverser with a system for braking the actuators |
| 02/26/2009 | WO2009024658A1 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine |
| 02/26/2009 | WO2009024656A1 Device and method for controlling the power supply of at least one aircraft maintenance actuator |
| 02/26/2009 | WO2009024594A1 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 |
| 02/26/2009 | WO2008132009A3 Sound absorption device for a jet engine or a turbine |
| 02/26/2009 | DE4004919A1 Strahldüse für ein Flugzeug-Gasturbinentriebwerk Jet nozzle for an aircraft gas turbine engine |
| 02/26/2009 | CA2696231A1 Thrust reverser with a system for braking the actuators |
| 02/26/2009 | CA2696223A1 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine |
| 02/26/2009 | CA2696178A1 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise |
| 02/26/2009 | CA2693844A1 Modular chevron exhaust nozzle |
| 02/26/2009 | CA2693356A1 System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system |
| 02/26/2009 | CA2693352A1 Device and method for controlling the power supply of at least onr aircraft maintenance actuator |
| 02/25/2009 | EP2028360A1 Dual-flow turbomachine with jet noise reduction |
| 02/25/2009 | EP2028359A2 Gas turbine engine with axial movable fan variable area nozzle |
| 02/25/2009 | CN101372926A Dual-flow turbomachine with jet noise reduction |