| 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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| 04/20/2011 | CN201802507U Supersonic-speed rotor engine |
| 04/20/2011 | CN102022222A Silencer |
| 04/19/2011 | US7926285 Modular chevron exhaust nozzle |
| 04/19/2011 | CA2648765C Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods |
| 04/14/2011 | WO2011042642A1 Circuit for supplying fuel to an aircraft engine |
| 04/14/2011 | DE19711679B4 Vorrichtung und Verfahren zur Regelung einer Luftströmung Apparatus and method for controlling an air flow |
| 04/14/2011 | CA2776314A1 Circuit for supplying fuel to an aircraft engine |
| 04/13/2011 | CN102016280A Exhaust washed structure and associated composite structure and method of fabrication |
| 04/12/2011 | CA2464830C Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 04/07/2011 | WO2011018569A3 Thrust reversal device |
| 04/07/2011 | WO2011014346A3 Integrated thrust reverser assembly |
| 04/06/2011 | EP2304211A1 Method for synchronizing the actuators of a movable thrust reverser cowl |
| 04/06/2011 | CN102007363A Wall cooling device |
| 04/06/2011 | CN102007284A Bypass turbojet engine nacelle |
| 04/06/2011 | CN101624945B Jet pressing burning splitting ring curled turbine engine |
| 03/30/2011 | EP2302189A1 Module arranged at the downstream end of a bypass turbofan engine |
| 03/30/2011 | EP2301845A2 Thrust reverser actuation |
| 03/30/2011 | EP2270312A9 Aero- or hydrodynamic construction |
| 03/24/2011 | WO2011034469A1 A noise attenuation panel and a gas turbine component comprising a noise attenuation panel |
| 03/23/2011 | EP2297445A1 Dual-flow turbine engine for aircraft with low noise emission |
| 03/23/2011 | EP2297438A2 Method and device for implementing the thrust reversers of an aircraft |
| 03/23/2011 | EP1882096B1 Method of reducing noise emissions at the rear of a turbofan engine and turbofan engine thus improved |
| 03/17/2011 | US20110062279 Hybrid beam for a thrust reverser unit |
| 03/16/2011 | EP2294303A1 Exhaust washed structure and associated composite structure and method of fabrication |
| 03/16/2011 | EP2181039B1 Device and method for controlling the power supply of at least one aircraft maintenance actuator |
| 03/16/2011 | CN101985903A Two-stage engine thrust steering mechanism |
| 03/10/2011 | WO2011027072A1 Structuring assembly for an exhaust nozzle |
| 03/10/2011 | WO2011026516A1 A mounting apparatus |
| 03/10/2011 | US20110056183 Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan |
| 03/10/2011 | CA2770257A1 Structuring assembly for an exhaust nozzle |
| 03/09/2011 | CN101501319B Engine exhaust system with directional nozzle |
| 03/08/2011 | US7900460 Outlet device for a jet engine and a jet engine comprising such an outlet device |
| 03/08/2011 | US7900459 Inner plenum dual wall liner |
| 03/08/2011 | US7900433 Fan exhaust nozzle for turbofan engine |
| 03/03/2011 | US20110048847 Noise attenuation device for reducing noise attenuation in a jet engine test cell |
| 03/03/2011 | US20110048025 Nozzle plasma flow control utilizing dielectric barrier discharge plasma actuators |
| 03/02/2011 | EP2288862A1 Wall cooling device |
| 02/23/2011 | EP1941148B1 Turbofan engine for stol aircraft |
| 02/23/2011 | CN101981300A Device for reducing the noise generated by an aircraft jet engine with fluid jets of the same orientation |
| 02/22/2011 | US7891195 Central body of a turbojet nozzle |
| 02/17/2011 | WO2011018569A2 Thrust reversal device |
| 02/17/2011 | US20110036068 Gas turbine engine exhaust mixer |
| 02/17/2011 | CA2768931A1 Thrust reversal device |
| 02/17/2011 | CA2713317A1 Gas turbine engine exhaust mixer |
| 02/17/2011 | CA2713316A1 Turbine section architecture for gas turbine engine |
| 02/16/2011 | EP2179167B1 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser |
| 02/16/2011 | EP1825126B1 Vectoring transition duct for turbine engine |
| 02/16/2011 | EP1529163B1 Rocket engine with swivelling nozzle |
| 02/16/2011 | CN101977814A Device for reducing turboprop infrared emissions |
| 02/16/2011 | CN101975122A Stabilized knocking engine with magnetic fluid energy bypath system |
| 02/16/2011 | CN101549758B Intake and exhaust device of air breathing supersonic/hypersonic aerocraft |
| 02/15/2011 | US7886543 Central body for a turbojet exhaust channel, turbojet |
| 02/15/2011 | US7886518 Turbofan engine cowl assembly and method of operating the same |
| 02/10/2011 | WO2011016973A2 High stiffness shape memory alloy actuated aerostructure |
| 02/10/2011 | US20110030380 High stiffness shape memory alloy actuated aerostructure |
| 02/10/2011 | US20110030341 Device with secondary jets reducing the noise generated by an aircraft jet engine |
| 02/10/2011 | US20110030339 Multifunctional propulsive system for an airplane |
| 02/10/2011 | DE102008023052B4 Brennkammerwand bzw. Heißgaswand einer Brennkammer und Brennkammer mit einer Brennkammerwand Combustion chamber wall or hot gas wall of a combustion chamber and combustion chamber with a combustion chamber wall |
| 02/10/2011 | CA2767049A1 High stiffness shape memory alloy actuated aerostructure |
| 02/09/2011 | EP2282016A2 Turbofan temperature control with variable area nozzle |
| 02/09/2011 | CN101970843A Turboshaft engine with reduced noise emission for aircraft |
| 02/09/2011 | CN101473130B Thrust reverser forming an adaptive nozzle |
| 02/08/2011 | US7883049 Jet nozzle having noise attenuating shield and method therefor |
| 02/08/2011 | US7882696 Integrated support and mixer for turbo machinery |
| 02/03/2011 | WO2011014250A1 Nested fairing thrust reverser |
| 02/03/2011 | CA2769589A1 Nested fairing thrust reverser |
| 02/02/2011 | EP2279341A2 Device for reducing noise generated by an aircraft jet engine with curve ducts |
| 02/02/2011 | EP2074303B1 Core cowl airfoil for a gas turbine engine |
| 02/02/2011 | CN101479461B Guiding carrier for jet engine linings |
| 02/01/2011 | US7878451 Low-leakage seal system for pivot door type thrust reverser |
| 01/27/2011 | US20110017843 System for actuating and controlling the mobile cowling of a turbojet engine nacelle |
| 01/27/2011 | US20110016880 Retainer for suspended thermal protection elements in a gas turbine engine |
| 01/27/2011 | DE102009034598A1 Thrust reverser for gas turbine, has flow guidance element symmetrically arranged at inner wall of deflection doors and adjacent to pivot axle, where flow guidance element includes base plate and bar fastened to base plate |
| 01/27/2011 | DE102009034530A1 Querschnittsprofil für die Stützen oder die Verkleidung von Stützen und Versorgungsleitungen eines Turbofantriebwerks Cross-sectional profile of the posts or the lining of supports and supply lines of a turbofan engine |
| 01/26/2011 | EP2278147A2 Translating variable area fan nozzle providing an upstream bypass flow exit |
| 01/26/2011 | EP2278146A2 Actuation system for a translating variable area fan nozzle |
| 01/26/2011 | EP2276926A1 Electric thruster for a spacecraft |
| 01/26/2011 | EP2074307B1 Translating core cowl having aerodynamic flap sections |
| 01/26/2011 | EP1633935B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 01/26/2011 | CN101960131A Trailing edge for an aircraft engine, of the type with moving chevrons |
| 01/25/2011 | US7874160 Nozzle-area ratio float bias |
| 01/20/2011 | DE102009032841A1 Geräuschreduziertes Flugzeugtriebwerk sowie Verfahren zur Verminderung von Geräuschemissionen eines Flugzeugtriebwerks Reduced noise aircraft engine and method for reducing noise emissions of an aircraft engine |
| 01/19/2011 | EP2126322B1 Self-calibration method for the electric jacks of a turbojet nacelle |
| 01/19/2011 | CN101952580A System for controlling a plurality of functions of a turbojet engine |
| 01/19/2011 | CN101529072B Cascade-type thrust reverser for jet engine |
| 01/18/2011 | US7870741 Turbine engine valve assembly and method of assembling the same |
| 01/13/2011 | WO2011004095A1 Actuating system for a movable aircraft engine nacelle element, such as a thrust reverser cover |
| 01/13/2011 | US20110005858 Noise-reduced aircraft engine and method for reducing noise emissions of an aircraft engine |
| 01/13/2011 | CA2765217A1 Actuating system for a movable aircraft engine nacelle element, such as a thrust reverser cover |
| 01/12/2011 | EP2271835A2 Device with secondary jets reducing the noise generated by an aircraft jet engine |
| 01/12/2011 | CN101946081A System for controlling the cowl of a turbojet engine nacelle thrust reverser |
| 01/12/2011 | CN101946080A Stave and ring cmc nozzle |
| 01/12/2011 | CN101946079A Control system for turbojet engine nacelle |
| 01/11/2011 | US7866440 System for joining acoustic cellular panel sections in edge-to-edge relation |
| 01/11/2011 | US7866158 Exhaust liner attachment arrangement |
| 01/11/2011 | US7866141 Cooling device for the primary nozzle of a dual-flow turbojet engine |
| 01/11/2011 | CA2478198C Methods and apparatus for flade engine nozzle |
| 01/06/2011 | US20110000548 Airflow separation initiator |
| 01/06/2011 | US20110000217 Managing spool bearing load using variable area flow nozzle |
| 01/05/2011 | EP2270326A2 Turbofan engine |