Patents
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)
12/2006
12/20/2006EP1733134A2 Spider actuated thrust reverser
12/19/2006CA2292750C Backblast gas structure equipped with thrust reverser with two rear doors and planar exhaust area
12/14/2006WO2006131083A1 Ejector power plant
12/14/2006US20060277914 Combi-Supersonic-Adjusting-Nozzle
12/14/2006US20060277895 Aircraft systems including cascade thrust reversers
12/13/2006EP1731747A1 Jet exhaust noise reduction system and method
12/13/2006CN1876242A Low noise pneumatic jet nozzle
12/12/2006US7146796 Nested latch thrust reverser
12/12/2006CA2245526C Cross bar centring mechanism for slave petals in convergent divergent nozzles with thrust vectoring capability
11/2006
11/30/2006US20060266045 Protection process and control system for a gas turbine
11/29/2006EP1726813A1 Axial divergent section slot nozzle
11/29/2006EP1726812A2 Thrust reverser system for an aircraft
11/29/2006EP1726811A2 System and method for cooling lateral edge regions of a divergent seal of an axisymmetric nozzle
11/29/2006EP1726788A2 A rotor blade containment assembly for a gas turbine engine
11/29/2006EP1726004A1 Assembly for reducing noise in turbofan engines
11/29/2006EP1725763A2 Jet nozzle mixer
11/29/2006EP1552131B1 Electro-hydraulic thrust reverser lock actuation system
11/29/2006EP1478836B1 Gearless electric thrust reverser actuator and actuation system incorporating the same
11/28/2006US7140840 Turboshaft engine comprising two elements connected to each other with the interposition of a seal
11/23/2006WO2006123035A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved
11/23/2006WO2006088437A9 Passive exhaust suppressor and method
11/23/2006CA2608373A1 Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved
11/21/2006CA2180501C Ramjet engine for supersonic and/or hypersonic aircraft
11/16/2006DE102005021781A1 Gas turbine, especially aviation engine, has at least one oscillatory element positioned in region of exhaust duct and is excitable into oscillations in such way that noise radiated from especially low pressure turbine is minimized
11/15/2006CN1864003A Thrust reverser lock comprising locking device
11/15/2006CN1863703A Annular acoustic panel
11/09/2006WO2006116907A1 Air compression aeroengine
11/09/2006WO2006028516B1 Thrust vector control system for a plug nozzle rocket engine
11/09/2006CA2606525A1 Air compression type engine for aviation
11/08/2006EP1719878A2 Gas turbine engine air valve assembly
11/08/2006CN1858425A Bushing for thermally independent bypass air metering valve
11/02/2006US20060242944 Jet nozzle mixer
11/02/2006EP1717432A1 Rotable exhaust nozzle for an aircraft engine
10/2006
10/31/2006US7128532 Transpiration cooling system
10/31/2006US7127880 Induction coupled variable nozzle
10/26/2006US20060236676 Swivelling exhaust nozzle for an aircraft engine
10/25/2006EP1715172A2 Acoustic liner assembly and corresponding fabrication method
10/25/2006EP1715158A2 Duct liner acoustic splice
10/25/2006EP1714021A2 Passive exhaust suppressor and method
10/24/2006US7124981 Thrust reverser utilizing integrated structural bypass duct
10/19/2006WO2006110184A1 System for controlling a position of jet engine exhaust mixing tabs and corresponding jet engine nacelle and operating method
10/19/2006WO2006110123A2 Vectoring transition duct for turbine engine
10/19/2006US20060230744 Exhaust nozzle for an engine of a flying craft
10/18/2006EP1712769A1 Exhaust nozzle of an aircraft engine
10/18/2006EP1320674B1 Jet engine with unsteady flow ejector
10/14/2006CA2542717A1 Aircraft engine exhaust nozzle
10/12/2006WO2006107341A1 Morphing structure
10/12/2006WO2006088437A3 Passive exhaust suppressor and method
10/12/2006US20060225427 Jet engine with a variable section nozzle of which at least one flap pivots about a pin, pins for flaps
10/12/2006US20060225426 Turobjet axisymmetric nozzle controlled hot flap shutter
10/12/2006US20060225405 Cooling scheme for scramjet variable geometry hardware
10/10/2006US7117974 Electronically controlled dual chamber variable resonator
10/10/2006US7117682 Turbojet axisymmetric nozzle controlled hot flap shutter
10/10/2006US7117681 Thrust control valve
10/10/2006US7117680 Cooling scheme for scramjet variable geometry hardware
10/04/2006EP1707787A2 Reduced radar cross section exhaust nozzle assembly
10/04/2006EP1707760A2 Thrust reverser mounting structure
10/04/2006CN1278062C Thermally stressable wall and method for sealing gap in thermally stressed wall
10/03/2006US7114323 Jet exhaust noise reduction system and method
09/2006
09/28/2006US20060213199 Convergent turbojet exhaust nozzle
09/28/2006US20060213198 Reduced radar cross section exhaust nozzle assembly
09/27/2006EP1705361A2 System for the deviation of a gas flow in a nozzle
09/27/2006EP1705343A2 Low leakage finger seal
09/26/2006US7111448 Jet nozzle mixer
09/26/2006CA2318373C Thrust reverser with turning vanes capable of being superposed
09/26/2006CA2168631C Sealing device between an air inlet and a fan frame of a turbofan engine
09/23/2006CA2540259A1 Gas stream deflection system in a nozzle
09/21/2006WO2005026518A3 Induction coupled variable nozzle
09/21/2006US20060207239 Compact mixer with trimmable open centerbody
09/20/2006EP1703114A1 Engine noise
09/19/2006US7107757 Aircraft provided with thrust reversers
09/19/2006US7107756 Turbofan arrangement
09/13/2006EP1701028A2 Acoustic liner with a nonuniform depth backwall
09/13/2006EP1701016A1 Acoustic liner with nonuniform impedance
09/12/2006US7104500 Thrust reverser with sliding pivot joints
09/12/2006CA2180502C Ramjet engine for supersonic and/or hypersonic aircraft
09/05/2006US7100736 Serviceable muffler
08/2006
08/31/2006US20060191267 Shape memory alloy actuated adaptive exhaust nozzle for jet engine
08/30/2006EP1696116A2 Thrust vectoring using fluid jets
08/29/2006US7096662 Variable area throat exhaust nozzle with vectorable sideways shifting of exhaust flow
08/29/2006US7096661 Axial divergent section slot nozzle
08/24/2006WO2006028516A3 Thrust vector control system for a plug nozzle rocket engine
08/22/2006US7093996 Methods and apparatus for mounting a gas turbine engine
08/22/2006US7093424 Thrust reverser system electro-mechanical brake manual release mechanism
08/22/2006US7093423 Methods and apparatus for operating gas turbine engines
08/22/2006CA2238469C Load strut for a variable geometry nozzle
08/16/2006EP1691064A2 Cooled dual wall liner closeout
08/16/2006EP0946827B1 A hollow nozzle actuating ring
08/15/2006US7090165 Aeroengine nacelle
08/08/2006US7086219 Cowl structure for a gas turbine engine
08/02/2006EP1686255A2 Turbine engine nozzle
07/2006
07/27/2006WO2006077290A1 Method for fixing a flexible drive shaft in a thrust reverser and a thrust reverser of this type
07/27/2006US20060162339 Gas turbine engine component having bypass circuit
07/27/2006CA2588578A1 Method for fixing a flexible drive shaft in a thrust reverser and a thrust reverser of this type
07/26/2006CN2799873Y Combustion type engine
07/26/2006CN1266419C Coolable segment for a turbine set and combustion turbine
07/19/2006EP1680589A1 Localized arc filament plasma actuators for noise mitigation and mixing enhancement
07/13/2006US20060150613 Thrust reverser actuator system flex shaft assembly
07/13/2006US20060150612 Thrust vector control
07/12/2006EP1427933B1 Device for controlling propulsive flow mixture for aircraft reactor
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