| 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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| 04/12/2012 | WO2012045970A1 Thrust reverser |
| 04/12/2012 | WO2012045965A1 Aircraft propulsion assembly |
| 04/12/2012 | CA2811481A1 Aircraft propulsion assembly |
| 04/12/2012 | CA2810204A1 Thrust reverser |
| 04/11/2012 | EP2438286A1 Thrust reverser for a dual-flow turbine engine nacelle |
| 04/11/2012 | CN102414478A 特别用于飞行器涡轮喷气发动机机舱的致动器的扭矩限制器 Actuator torque limiter especially for turbojet aircraft cabin |
| 04/10/2012 | US8151550 Control method for actuating a thrust reverser |
| 04/10/2012 | CA2703115C Passive cooling system for auxiliary power unit installation |
| 04/05/2012 | WO2012044882A1 Thrust reverser assembly |
| 04/05/2012 | WO2012022869A3 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 04/05/2012 | US20120079803 Exhaust plume heat effect reducing method and apparatus |
| 04/04/2012 | EP2435685A1 Turbine engine comprising an exhaust-gas guide cone with a sound suppressor |
| 04/04/2012 | EP2435307A1 Aircraft engine nacelle comprising a mobile cowl moved by electric motors |
| 03/29/2012 | WO2010145918A3 Temperature activatable actuator |
| 03/28/2012 | EP2433864A1 Air-discharge device for an airplane turbofan engine |
| 03/28/2012 | EP2432981A1 Cowling for a turbine engine nozzle provided with side fins for reducing the noise of the jet |
| 03/28/2012 | CN102395777A Thrust reversal device |
| 03/28/2012 | CN102395776A Control system for a turboreactor nacelle |
| 03/28/2012 | CN102395509A Actuator system for a mobile panel of a nacelle of a turbojet |
| 03/27/2012 | US8141366 Gas turbine engine with variable area fan nozzle |
| 03/27/2012 | US8141353 Exhaust gas additive/treatment system and mixer for use therein |
| 03/22/2012 | WO2012035223A1 Locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle for aircraft engine nacelle |
| 03/22/2012 | US20120067975 Thrust reversing device |
| 03/22/2012 | US20120067052 Deployable divergent nozzle for a propulsive unit |
| 03/22/2012 | DE102010045697A1 Blütenmischer für ein Turbofantriebwerk Bloom mixer for a turbofan engine |
| 03/22/2012 | CA2807679A1 Locking/unlocking device for a thrust reverser with sliding cover and adaptive nozzle for aircraft engine nacelle |
| 03/21/2012 | EP2431599A2 Daisy type mixer for a turbofan engine |
| 03/21/2012 | CN102383971A Multilevel hot stamping engine |
| 03/21/2012 | CN102383970A Turbofan engine |
| 03/21/2012 | CN101466940B Engine exhaust system |
| 03/20/2012 | US8136342 Arrangement for controlling fluid jets injected into a fluid stream |
| 03/20/2012 | CA2649523C Thrust reverser for a turbofan gas turbine engine |
| 03/15/2012 | US20120060467 Fastener fitting between the movable portion of a deployable diverging bell for a thruster and a mechanism for deploying said movable portion |
| 03/14/2012 | CN102374070A Injection jet engine |
| 03/14/2012 | CN102374069A Hot-stamping engine |
| 03/13/2012 | US8135503 Ground proximity sensor |
| 03/13/2012 | US8132756 Device with plane jets for reducing the noise generated by an aircraft engine |
| 03/13/2012 | CA2449469C Exhaust flow guide for jet noise reduction |
| 03/08/2012 | WO2011014250A8 Nested fairing thrust reverser |
| 03/08/2012 | US20120056038 Mechanism for Changing the Shape of a Control Surface |
| 03/08/2012 | US20120056005 Shape memory material actuation |
| 03/08/2012 | DE102010044483A1 Bloom mixer for turbofan engine of aircraft for mixture of primary current and secondary current, has projections and recesses arranged adjacent to each other in circumferential direction and formed by walls that are formed asymmetrically |
| 03/07/2012 | EP2426342A2 Turbofan engine with variable bypass nozzle exit area and method of operation |
| 03/07/2012 | EP2074317B1 Nacelle assembly for a gas turbine engine comprising a pylon located in the fan bypass flow path with a variable area flow system |
| 03/06/2012 | US8127530 Thrust reverser for a turbofan gas turbine engine |
| 03/06/2012 | CA2466795C Combined exhaust duct and mixer for a gas turbine engine |
| 03/06/2012 | CA2359924C Noise reduction sandwich panel, notably for aircraft turbojet engine |
| 03/01/2012 | WO2012025690A2 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 03/01/2012 | CA2807913A1 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same |
| 02/29/2012 | EP2423495A2 Valve system for a gas turbine engine |
| 02/29/2012 | EP2422114A1 Torque limiter in particular for an actuator of the nacelle of an aircraft turbojet engine |
| 02/29/2012 | EP2152582B1 Propulsion assembly for aircraft with sliding nacelle |
| 02/28/2012 | US8122723 Adjustment assembly |
| 02/28/2012 | US8122722 Exhaust nozzle seal with segmented basesheet disposed between side rails |
| 02/23/2012 | WO2012022900A1 Beam for a cascade thrust reverser |
| 02/23/2012 | WO2012022869A2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 02/23/2012 | US20120042628 Robotic manipulator |
| 02/23/2012 | CA2807430A1 Beam for a cascade thrust reverser |
| 02/23/2012 | CA2803746A1 Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 02/22/2012 | EP2420665A1 Variable area fan nozzle |
| 02/22/2012 | EP2419620A1 Thrust reversal device |
| 02/22/2012 | EP2419619A1 Control system for a turboreactor nacelle |
| 02/22/2012 | EP2419330A1 Actuator system for a mobile panel of a nacelle of a turbojet |
| 02/22/2012 | CN102362085A Bent connecting rod fitted with at least one self-aligning means |
| 02/21/2012 | US8117847 Hybrid missile propulsion system with reconfigurable multinozzle grid |
| 02/21/2012 | CA2517563C Rotary adjustable exhaust nozzle |
| 02/21/2012 | CA2445828C Electromechanical thrust reverser for a turboreactor used to control door movement |
| 02/21/2012 | CA2444986C Maintenance and inhibitor plate for thrust reverser |
| 02/16/2012 | US20120037723 Torque limiter in particular for an actuator of the nacelle of an aircraft turbojet engine |
| 02/09/2012 | US20120031995 Actuator system for a mobile panel of a nacelle of a turbojet |
| 02/09/2012 | US20120031071 Control system for a turboreactor nacelle |
| 02/08/2012 | EP2415971A2 A seal assembly |
| 02/08/2012 | CN102349101A Aircraft acoustic attenuation member and method for forming said member |
| 02/07/2012 | US8109468 Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle |
| 02/07/2012 | US8109467 Thrust reverser assembly with shaped drag links |
| 02/07/2012 | US8109466 Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion |
| 02/01/2012 | EP2411686A1 Bent connecting rod fitted with at least one self-aligning means |
| 02/01/2012 | CN202132128U 多级热冲压发动机 Multi-stage heat ramjet |
| 02/01/2012 | CN202132101U 动力流体气体工质压缩系统 Dynamic fluid refrigerant gas compression system |
| 02/01/2012 | CN101652556B 用于喷气发动机的推力反向器 For jet engine thrust reverser |
| 01/31/2012 | US8104263 Actuator arrangement for vectorable nozzles of gas turbine |
| 01/31/2012 | US8104260 Deswirling exhaust mixer |
| 01/26/2012 | WO2012010774A2 Turbojet engine nacelle |
| 01/26/2012 | WO2012010124A1 Device for reducing jet noise |
| 01/25/2012 | EP2410165A2 Gas turbine with noise attenuating variable area fan nozzle |
| 01/25/2012 | EP2410139A1 Exhaust gas diffusor for a gas turbine |
| 01/25/2012 | EP2409921A2 Nacelle for Aircraft |
| 01/25/2012 | CN101313139B Control method for driving pushing force commutator |
| 01/24/2012 | CA2467842C Nozzle flap for aircraft turbojets |
| 01/19/2012 | WO2011142866A3 Articulating slider track |
| 01/19/2012 | US20120011828 Propulsion system |
| 01/19/2012 | US20120011826 Turbojet engine with an element of the nacelle attached to the intermediate casing |
| 01/19/2012 | US20120011825 Gas turbine engine with noise attenuating variable area fan nozzle |
| 01/18/2012 | EP2407659A2 Gas turbine exhaust cone |
| 01/18/2012 | EP2406786A1 Aircraft acoustic attenuation member and method for forming said member |
| 01/17/2012 | US8096501 Aircraft nacelle which includes thrust reverser system and aircraft incorporating at least one such nacelle |
| 01/17/2012 | US8096105 Turbojet engine with attenuated jet noise |
| 01/17/2012 | US8096104 Fluidic vectoring for exhaust nozzle |
| 01/12/2012 | WO2012004486A1 Thrust reverser having an aerodynamic coupling for a front frame |
| 01/12/2012 | US20120006614 Gas-turbine exhaust cone |