| 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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| 04/23/2013 | US8424312 Exhaust system for gas turbine |
| 04/18/2013 | US20130092756 Variable area nozzle for gas turbine engine |
| 04/18/2013 | US20130092755 Thrust Reverser Cascade Assembly With Flow Deflection Shelf |
| 04/18/2013 | US20130092754 Nacelle for a power plant with a variable-area fan nozzle |
| 04/18/2013 | US20130091825 Turbojet engine nacelle including a device for absorbing circumferential stresses |
| 04/17/2013 | EP2581593A2 Thrust Reverser Cascade Assembly with Flow Deflection Shelf |
| 04/17/2013 | EP2580459A1 Self-mounted cascade for a thrust reverser |
| 04/17/2013 | EP2580433A1 Cooled conduit for conveying combustion gases in a gas turbine engine |
| 04/17/2013 | CN103047048A Thrust reverser cascade assembly with flow deflection shelf |
| 04/17/2013 | CN101787937B Porous wall expanding type dual throat nozzle |
| 04/16/2013 | US8418437 Jet flow discharge nozzle and jet engine |
| 04/13/2013 | CA2792065A1 Thrust reverser cascade assembly with flow deflection shelf |
| 04/11/2013 | WO2012117197A3 Air cushion aircraft |
| 04/11/2013 | US20130086907 Jet flow nozzle and jet engine |
| 04/10/2013 | EP2578864A1 Variable area fan nozzle with bypass flow |
| 04/10/2013 | EP2578495A2 Acoustic treatment panel including hot-air channels and at least one stabilising chamber |
| 04/10/2013 | EP2577033A1 Thrust reverser having a lockable variable nozzle section |
| 04/10/2013 | EP2577032A1 Assembly including a reverse thrust device and system for actuating said device |
| 04/10/2013 | CN103038484A Multi-layer acoustic treatment panel |
| 04/09/2013 | US8413443 Flow control through a resonator system of gas turbine combustor |
| 04/04/2013 | WO2013045787A1 Thrust reverser gates having side openings |
| 04/04/2013 | DE102011114705A1 Schalldämpfer für ein Hilfstriebwerk eines Flugzeugs Silencer for an auxiliary power unit of an aircraft |
| 04/04/2013 | CA2849233A1 Thrust reverser gates having side openings |
| 04/03/2013 | EP2574766A2 VAFN actuation system with improved drive coupling and brake |
| 04/03/2013 | EP2574765A2 Variable area fan nozzle with locking assembly |
| 04/03/2013 | CN101535622B Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with the device |
| 04/02/2013 | US8408356 Storage box for electronic apparatus |
| 03/28/2013 | WO2013041818A1 Primary cowl of a turbofan comprising a rotating ring having micro-jets |
| 03/28/2013 | US20130075493 Airplane jet engine thrust reverser having gratings or cascades |
| 03/28/2013 | US20130075193 Seamless acoustic liner |
| 03/27/2013 | EP2573375A2 Thrust reverser for the fan of a gas turbine engine |
| 03/27/2013 | EP2572097A1 Airplane jet engine thrust reverser having gratings or cascades |
| 03/27/2013 | CN103003872A Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 03/27/2013 | CN101784447B Device and method for controlling the power supply of at least one aircraft maintenance actuator |
| 03/26/2013 | US8403629 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine |
| 03/26/2013 | US8403264 Air inlet valve for an airplane and manufacturing method for an air inlet valve |
| 03/26/2013 | US8402765 Translating variable area fan nozzle providing an upstream bypass flow exit |
| 03/26/2013 | US8402744 Valve system for a gas turbine engine |
| 03/26/2013 | US8402736 Method and apparatus for suppressing aeroengine contrails |
| 03/21/2013 | WO2013038093A1 Rear nacelle assembly for a turbojet engine |
| 03/21/2013 | US20130067885 Fan case thrust reverser |
| 03/21/2013 | US20130067884 Thrust reverser for a gas turbine engine |
| 03/21/2013 | CA2845031A1 Rear nacelle assembly for a turbojet engine |
| 03/20/2013 | EP2570641A2 Fan case with thrust reverser cascade section, corresponding fan section and gas turbine engine |
| 03/20/2013 | EP2570640A2 A variable geometry structure |
| 03/20/2013 | EP2570606A2 Ceramic matrix composite turbine exhaust case for a gas turbine engine and corresponding gas turbine engine |
| 03/20/2013 | EP2569527A1 Device for reducing the noise emitted by the jet of an aircraft propulsion engine |
| 03/20/2013 | CA2789329A1 Tiltrotor vectored exhaust system |
| 03/19/2013 | US8397513 Device for tapping cooling air in a turbomachine |
| 03/19/2013 | US8397493 Method for recovering waste heat from exhaust |
| 03/19/2013 | US8397485 Morphing structure and method |
| 03/19/2013 | CA2625068C Turbojet engine with attenuated jet noise |
| 03/14/2013 | US20130062435 Nacelle for an aircraft engine with cascade-type thrust reverser and variable-geometry nozzle |
| 03/14/2013 | US20130062434 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
| 03/14/2013 | US20130062433 Nacelle for an aircraft engine with variable cross-section nozzle |
| 03/14/2013 | US20130061572 Hydraulic control system for a thrust reversal device |
| 03/13/2013 | EP2568151A2 Serrated nozzle trailing edge for exhaust noise suppression |
| 03/13/2013 | EP2568150A1 Cable-actuated variable area fan nozzle with elastomeric seals |
| 03/13/2013 | EP2566757A1 Unit for an aircraft thruster |
| 03/13/2013 | CN102966463A Magnetic heat shielding method for large-thrust orbit maneuver motor venture of satellite |
| 03/13/2013 | CN101975122B Stabilized knocking engine with magnetic fluid energy bypath system |
| 03/12/2013 | US8393435 Trailing edge for an aircraft engine, of the type with moving chevrons |
| 03/12/2013 | CA2536693C Nested latch thrust reverser |
| 03/12/2013 | CA2511892C Cowling for turbine engine nozzle with jet noise reduction patterns |
| 03/07/2013 | US20130056553 Method for mixing airflows in a turbofan and engine outlet for operation |
| 03/07/2013 | US20130055718 Device for reducing the noise emitted by the jet of an aircraft propulsion engine |
| 03/06/2013 | EP2565435A2 Multi axis slide carriage system |
| 03/06/2013 | EP2565400A2 Exhaust gas duct for a gas turbine with heat resistant liner and gas turbine having such a gas duct |
| 03/06/2013 | EP2564051A1 Airfoil combination for aircraft turbofan |
| 03/06/2013 | EP2564050A1 Turbojet engine nacelle |
| 03/06/2013 | EP2563667A1 Reverser having doors |
| 03/06/2013 | CN102959223A Thrust reverser having aerodynamic coupling for front frame |
| 03/06/2013 | CN102953865A Plug cooling structure of plug type axisymmetric nozzle |
| 03/06/2013 | CN102953864A Spherical dynamic seal structure of spherical nozzle |
| 03/05/2013 | US8387360 Integral thrust vector and roll control system |
| 02/28/2013 | US20130048749 Flap seal for gas turbine engine movable nozzle flap |
| 02/28/2013 | US20130048414 Soundproofing panel for turbomachine and turbomachine comprising such a panel |
| 02/27/2013 | EP2562405A1 Gas turbine engine access door |
| 02/27/2013 | EP2562363A2 Flap seal for gas turbine engine movable nozzle flap |
| 02/27/2013 | EP2561209A1 Hydraulic control system for a thrust reversal device |
| 02/27/2013 | EP2561208A1 Nacelle for an aircraft engine with variable cross-section nozzle |
| 02/27/2013 | EP2560877A1 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle |
| 02/26/2013 | US8381510 Method and systems for controlling engine thrust using variable trim |
| 02/21/2013 | WO2013024231A1 Method of determining the performance of at least one propeller of a turbomachine in an air stream under gyration |
| 02/21/2013 | WO2013024218A1 Exhaust cone for aircraft turbojet engine |
| 02/21/2013 | WO2013024216A1 Exhaust plug for an aircraft turbojet engine |
| 02/21/2013 | CA2842874A1 Exhaust cone for aircraft turbojet engine |
| 02/21/2013 | CA2842871A1 Exhaust plug for an aircraft turbojet engine |
| 02/20/2013 | EP2558702A1 System for controlling an electrical device of a nacelle |
| 02/19/2013 | CA2608373C Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved |
| 02/19/2013 | CA2492418C Methods and apparatus for operating gas turbine engines |
| 02/14/2013 | WO2013021136A1 Thrust reverser device for compact jet pipe |
| 02/14/2013 | WO2013021120A1 Method for monitoring the locking means of an electrical thrust reversal system for a turbine engine |
| 02/14/2013 | WO2013021111A1 Reverser having movable cascades, and translatably variable nozzle |
| 02/14/2013 | WO2013021110A1 Thrust reverser device |
| 02/14/2013 | WO2013021108A1 Turbojet engine nacelle having a variable nozzle |
| 02/14/2013 | CA2843581A1 Method for monitoring the locking means of an electrical thrust reversal system for a turbine engine |
| 02/14/2013 | CA2843046A1 Thrust reverser device for compact jet pipe |
| 02/14/2013 | CA2842749A1 Thrust reverser device |
| 02/14/2013 | CA2842540A1 Turbojet engine nacelle having a variable nozzle |