| 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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| 02/18/2014 | US8650855 System for controlling at least one actuator of the cowlings of a turbojet engine thrust reverser |
| 02/18/2014 | US8650854 Bifurcation and aft vent used to vary fan nozzle exit area |
| 02/18/2014 | CA2580179C Turbine exhaust strut airfoil profile |
| 02/13/2014 | WO2014023901A1 Structural part made of a composite material, such as a rail for a slidable cowl of a thrust reverser of an aircraft engine nacelle |
| 02/13/2014 | WO2014023890A1 Composite strap for connection between two parts |
| 02/11/2014 | US8647048 Flexible seal for gas turbine engine system |
| 02/11/2014 | US8646725 Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow |
| 02/11/2014 | US8646251 Flutter sensing system for a gas turbine engine |
| 02/06/2014 | WO2014022344A1 Cmc core cowl and method of fabricating |
| 02/06/2014 | WO2014021973A2 Liner assembly |
| 02/06/2014 | WO2014020367A1 Motor-powered fan drives for vehicles of all types |
| 02/06/2014 | WO2014020286A1 Method for manufacturing of a metal part |
| 02/05/2014 | EP2691625A1 Anti-fire seal assembly and nacelle comprising such a seal |
| 02/05/2014 | CN103561948A Method for manufacturing sound attenuation panel |
| 02/05/2014 | CN103557090A Jet engine |
| 02/04/2014 | US8640820 High-speed jet noise reduction via fluidic injection |
| 01/30/2014 | WO2014018198A1 Air-cooled engine surface cooler |
| 01/30/2014 | WO2014016512A1 Flap-driving device, especially for an adaptive nozzle |
| 01/30/2014 | US20140027538 Variable geometry structure |
| 01/30/2014 | US20140027537 Integrated variable area fan nozzle and thrust reverser |
| 01/30/2014 | US20140027536 Translating cascades |
| 01/30/2014 | US20140026582 Anti-fire seal assembly and nacelle comprising such a seal |
| 01/30/2014 | US20140026536 Variable area fan nozzle position and skew sensing |
| 01/29/2014 | EP2690273A2 Thrust reverser-integrated track beam and inner fixed structure |
| 01/29/2014 | EP2690272A2 Variable area fan nozzle position and skew sensing |
| 01/29/2014 | CN103541831A CL spray tube used on spacecraft |
| 01/29/2014 | CN101815857B Method and system for controlling at least one actuator or actuating the cowlings of a thrust inverter in a turbojet engine |
| 01/29/2014 | CN101784444B Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 01/28/2014 | US8635851 Grid thrust reverser cover comprising a seal support and associated seal |
| 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 |
| 01/22/2014 | CN102448822B Aircraft engine nacelle comprising a mobile cowl moved by electric motors |
| 01/21/2014 | US8632033 Thrust reverser actuation |
| 01/21/2014 | US8631640 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser |
| 01/15/2014 | EP2683918A1 Device and method for carrying out a temperature compensation between turbine housing regions that are at different temperatures |
| 01/15/2014 | CN102536514B Binary plug nozzle of turbofan engine with afterburning |
| 01/14/2014 | US8627644 Thrust reverser for a jet engine |
| 01/09/2014 | WO2014007994A1 Airfoil for improved flow distribution with high radial offset |
| 01/09/2014 | WO2014007907A2 Variable immersion lobe mixer for turbofan jet engine exhauts and method of fabricating the same |
| 01/09/2014 | WO2014006321A1 Coupling and uncoupling mechanism for a turbojet engine nacelle onboard device |
| 01/09/2014 | WO2014006303A1 Method for controlling a variable nozzle section of an aircraft |
| 01/09/2014 | US20140007554 Rocket motor with means for user adjustable thrust |
| 01/09/2014 | CA2877836A1 Method for controlling a variable nozzle section of an aircraft |
| 01/08/2014 | EP2682590A2 Turbine generator assembly for thrust vector control |
| 01/08/2014 | CN103502580A Integrated variable geometry flow restrictor and heat exchanger |
| 01/03/2014 | WO2014001726A1 Thrust-reversal device for an aircraft including at least two thrust reversers |
| 01/03/2014 | WO2014001682A1 Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing device |
| 01/03/2014 | CA2877204A1 Gas turbine engine comprising a composite component and a metal component which are connected by a flexible fixing device |
| 01/03/2014 | CA2876975A1 Thrust-reversal device for an aircraft including at least two thrust reversers |
| 01/02/2014 | US20140001284 Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber |
| 01/02/2014 | US20140000238 Locking/unlocking device for a thurst reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle |
| 01/02/2014 | US20140000237 Thrust reverser maintenance actuation system |
| 01/01/2014 | EP2679793A1 Flow channel for a gaseous medium and corresponding exhaust-gas liner of a gas turbine |
| 01/01/2014 | EP2679780A1 Diffuser for the exhaust section of a gas turbine and gas turbine with such a diffuser |
| 01/01/2014 | CN103492696A Thrust reverser for an aircraft jet engine |
| 01/01/2014 | CN103492676A Tertiary locking assembly for a thrust reverser |
| 01/01/2014 | CN102037232B Device for reducing noise generated by an aircraft jet engine with curve ducts |
| 12/31/2013 | US8615982 Integrated electric variable area fan nozzle thrust reversal actuation system |
| 12/27/2013 | WO2013190246A1 Gas turbine engine comprising an exhaust cone attached to the exhaust casing |
| 12/25/2013 | CN103477054A Anti-fire seal assembly and nacelle comprising such a seal |
| 12/25/2013 | CN103470400A Design method of exhaust nozzle with controllable inlet and outlet shapes for air-breathing hypersonic flight vehicle |
| 12/25/2013 | CN102108915B Turbofan engine for stol aircraft |
| 12/25/2013 | CN102105669B Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle |
| 12/25/2013 | CN101970843B Turboshaft engine with reduced noise emission for aircraft |
| 12/24/2013 | US8613398 Apparatus and methods for linear actuation of flow altering components of jet engine nozzle |
| 12/24/2013 | US8613185 Method and device for the detection of a thrust dissymmetry of an aircraft during a braking |
| 12/24/2013 | CA2581532C Crankcase housing in a turbojet engine |
| 12/19/2013 | WO2013186476A1 Method for producing foam panels, especially for the field of aeronautics |
| 12/19/2013 | WO2013186475A1 Thrust reverser comprising retractable cascade vanes |
| 12/19/2013 | CA2875489A1 Method for producing foam panels, especially for the field of aeronautics |
| 12/18/2013 | EP2673545A1 Reduced pressure-drop pipe element |
| 12/17/2013 | US8607574 Turbine engine exhaust nozzle flap |
| 12/17/2013 | US8607452 Method for reducing sound output at the back of a turbo engine and turbo engine improved by this method |
| 12/17/2013 | CA2611556C Control system for the nacelle of a turboreactor |
| 12/12/2013 | WO2013182820A1 Locking/unlocking device for a one-piece cover of a thrust reverser of a turbojet engine nacelle |
| 12/12/2013 | WO2013158180A3 Variable area fan nozzle fan flutter management system |
| 12/12/2013 | US20130327847 Turbine engine exhaust nozzle flap |
| 12/12/2013 | US20130327047 Gas turbine engine variable area exhaust nozzle |
| 12/11/2013 | CN203335275U Binary injection thrust vectoring nozzle |
| 12/11/2013 | CN203335274U Square ring connecting rod type two-dimensional nozzle contraction section control mechanism |
| 12/11/2013 | CN203335273U Control mechanism for two-dimensional converging-diverging nozzle and with single-actuation system |
| 12/11/2013 | CN203335272U Sliding-beam connecting-rod type control mechanism of expansion section of binary contraction-and-expansion thrust-vectoring nozzle |
| 12/11/2013 | CN203335271U Sliding beam cam type two-dimensional nozzle contraction section control mechanism |
| 12/11/2013 | CN203335270U Square ring and connecting rod type control mechanism for expansion section of binary convergence-expansion vectoring nozzle |
| 12/11/2013 | CN103437911A Partition-bearing fluid control binary vector nozzle tube and vector thrust generation and control method thereof |
| 12/11/2013 | CN102037231B Device with secondary jets reducing the noise generated by an aircraft jet engine |
| 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 | WO2013180778A2 Seal assembly |
| 12/05/2013 | US20130318944 Jet Exhaust Noise Reduction |
| 12/04/2013 | EP2669500A2 Jet exhaust noise reduction |
| 12/04/2013 | CN203321699U Square ring cam type binary spraying pipe contraction section control mechanism |
| 12/04/2013 | CN103429880A Turbomachine with fan(s) for aircraft, with mobile jet nozzle |
| 12/04/2013 | CN103423031A Pulse detonation engine tail nozzle |
| 12/04/2013 | CN103423030A Tapered plug mechanism realizing axial symmetry spray pipe all-direction vector regulation |
| 12/04/2013 | CN103423029A 推力反向器系统 Thrust reverser system |
| 12/04/2013 | CN103423028A Two-dimensional nozzle throat area control mechanism |
| 12/04/2013 | CN103423027A Two-dimensional thrust vectoring nozzle expanding section control mechanism |
| 12/04/2013 | CN103423026A Vector cascade mechanism capable of enhancing stealth of S-shaped bent two-dimensional nozzle |
| 12/04/2013 | CN103423025A Convergent nozzle |