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