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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03/11/2004 | US20040045765 Tubular acoustic attenuation piece for an aircraft jet engine air intake |
03/10/2004 | EP1395741A1 System and method for sustaining electic power during a momentary power interruption in an electric thrust reverser actuation system |
03/04/2004 | US20040040308 Methods for retaining gas turbine engine nozzle basesheets |
02/26/2004 | WO2003081013A3 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
02/26/2004 | US20040035653 Thrust reverser system with a pass-through torque activated brake |
02/25/2004 | EP1391597A2 Noise reduction conduit for static components in aircraft engines |
02/25/2004 | EP1390613A1 Jet engine nozzle with variable thrust vectoring and exhaust area |
02/25/2004 | CN2604529Y Mixture pressure type pulse detonation injector |
02/24/2004 | US6695094 Acoustic muffler for turbine engine |
02/19/2004 | WO2003092946B1 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers |
02/19/2004 | US20040031258 Jet engine noise suppressor |
02/14/2004 | CA2437155A1 Noise reduction conduit for static components in aircraft engines |
02/12/2004 | WO2004013481A1 Thrust reverser system with a pass-through torque activated brake |
02/12/2004 | CA2494866A1 Thrust reverser system with a pass-through torque activated brake |
02/10/2004 | US6688099 Variable area thrust reverser nozzle |
02/10/2004 | US6688098 Backup locking system for a thrust reverser door |
02/10/2004 | CA2204825C Jet turbine engine thrust reverser employing doors fitted with upstream panel |
02/05/2004 | US20040020214 Control strategy for gas turbine engine |
02/04/2004 | EP1386072A1 Device for controlling the deployment of jet engine thrust reversers |
02/04/2004 | EP1386071A1 System for controlling the stowage of jet engine thrust reversers |
02/03/2004 | US6684623 Gearless electric thrust reverser actuators and actuation system incorporating same |
02/03/2004 | US6684622 Rocket exhaust plume signature tailoring |
01/29/2004 | US20040017045 Fluid seal |
01/27/2004 | US6681561 Outlet device for a jet engine |
01/27/2004 | US6681560 Nozzle throat area control apparatus and method |
01/27/2004 | US6681559 Thrust reverser position determination system and method |
01/27/2004 | US6681558 Method of increasing engine temperature limit margins |
01/22/2004 | US20040011045 Ramjet for a supersonic and hypersonic aircraft |
01/22/2004 | US20040011018 Assistance and emergency drive for electrically-driven accessories |
01/21/2004 | EP1382817A1 Assistance to the driving of accessories in a turbo-engine |
01/20/2004 | US6679048 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection |
01/20/2004 | CA2190197C Thrust inverter of a turbojet with downstream obstacles tending to balancing |
01/15/2004 | WO2004005690A1 Swivelling nozzle for a rocket engine |
01/15/2004 | US20040006969 Variable area nozzle |
01/15/2004 | US20040006968 Lobe mixer for jet engine |
01/14/2004 | EP1380746A1 Lobe mixer for jet engine |
01/13/2004 | CA2152883C Turbofan thrust reverser, with obstructions linked to the primary enclosure |
01/08/2004 | WO2004002821A1 Ducted air power plant |
01/08/2004 | US20040003585 Cooled variable geometry exhaust nozzle |
01/08/2004 | CA2490886A1 Ducted air power plant |
01/07/2004 | EP1378651A2 Cooled variable geometry exhaust nozzle |
01/06/2004 | US6672424 Acoustically treated turbomachine multi-duct exhaust device |
01/06/2004 | US6672068 Ramjet for a supersonic and hypersonic aircraft |
01/02/2004 | EP1376534A1 Manufacturing process for a double resonator acoustic panel |
01/02/2004 | EP1373702A1 Tortuous path exhaust eductor system |
12/31/2003 | WO2003068597A3 Control system for vertical take off and land (vtol) aircraft |
12/31/2003 | CN2596043Y Diffuser with tornado sand-dune combined stabilizer |
12/30/2003 | US6668542 Pulse detonation bypass engine propulsion pod |
12/30/2003 | CA2153560C External deflector reverse thrust system for bypass engine |
12/24/2003 | WO2003107325A1 Method for making a soundproofing panel with at least one double resonator |
12/24/2003 | WO2003106263A1 An acoustic liner, use of such a liner and method for manufacturing an acoustic liner |
12/23/2003 | US6666307 Thrust reverser system with a pass-through torque activated brake |
12/23/2003 | US6666016 Mixing enhancement using axial flow |
12/23/2003 | CA2213049C Turbojet thrust reverser with doors forming scoops |
12/23/2003 | CA2207836C Exhaust pipe for turboreactor with variable geometry |
12/16/2003 | US6663042 Aircraft propulsive power unit |
12/16/2003 | US6662549 Propulsion system |
12/16/2003 | US6662548 Jet blade ejector nozzle |
12/09/2003 | US6658854 Methods and apparatus for retaining gas turbine engine nozzle basesheets |
12/09/2003 | US6658839 Convergent/divergent segmented exhaust nozzle |
12/04/2003 | WO2003100241A1 Variable area thrust reverser nozzle |
12/04/2003 | WO2003099654A2 Bifurcated turbofan exhaust nozzle |
12/04/2003 | US20030221411 Deployable segmented exhaust nozzle for a jet engine |
12/04/2003 | CA2486175A1 Bifurcated turbofan exhaust nozzle |
12/03/2003 | EP1367249A1 Deployable segmented exhaust nozzle for a jet engine |
12/02/2003 | US6655125 System architecture for electromechanical thrust reverser actuation systems |
12/02/2003 | US6655124 External system and method for rocket exhaust plume signature tailoring |
12/02/2003 | US6655123 Device for economizing fuel supply in a fuel supply circuit |
11/27/2003 | US20030218094 Variable area thrust reverser nozzle |
11/25/2003 | US6651929 Passive cooling system for auxiliary power unit installation |
11/20/2003 | US20030213227 Segmented mixing device for jet engines and aircraft |
11/18/2003 | US6648268 Control system for vertical take off and land (VTOL) aircraft |
11/13/2003 | WO2003092946A1 Method for the production of soldered heat-exchanger structures, particularly regeneratively cooled combustion chambers |
11/13/2003 | WO2003036063A3 Confluent variable exhaust nozzle |
11/06/2003 | WO2003057561A3 Variably angled propulsion/steering system |
11/05/2003 | EP1359309A1 Gas turbine with a gas mixing device comprising lobes and pipes |
11/04/2003 | US6640544 Gas turbine combustor, gas turbine, and jet engine |
11/04/2003 | US6640537 Aero-engine exhaust jet noise reduction assembly |
11/04/2003 | CA2191179C Jet engine thrust reserver with articulated rear door |
10/30/2003 | US20030201364 Bi-fold thrust reverser door assembly |
10/28/2003 | US6637187 Rotary inlet flow controller for pulse detonation combustion engines |
10/23/2003 | US20030196425 Jet nozzle mixer |
10/15/2003 | EP1352170A1 Rocket engine member and a method for manufacturing a rocket engine member |
10/15/2003 | EP1352169A1 Rocket engine member and a method for manufacturing a rocket engine member |
10/15/2003 | EP1352168A1 Rocket engine member and method for manufacturing a rocket engine member |
10/15/2003 | EP1352167A1 Method for manufacturing outlet nozzles for rocket engines |
10/15/2003 | EP1352166A1 An outlet nozzle and a method for manufacturing an outlet nozzle |
10/02/2003 | WO2003081013A2 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
10/02/2003 | US20030183799 Porous sound absorbing material and method of manufacturing the material |
10/02/2003 | US20030183723 Propulsion system for a vertical and short takeoff and landing aircraft |
10/02/2003 | US20030182929 Cooling system for a gas turbine engine post-combustion jet nozzle |
10/02/2003 | US20030182925 Duplex mixer exhaust nozzle |
10/02/2003 | DE20306279U1 Noise blocking system for jet-propelled aircraft has water mist spraying device in funnel form as nozzle insert, and on lower end has orifice for forcing through of water |
09/30/2003 | US6625987 Control strategy for gas turbine engine |
09/30/2003 | US6625973 Lock mechanism |
09/30/2003 | US6625972 Thrust reverser sleeve lock |
09/30/2003 | CA2204589C Jet turbine engine thrust reverser employing doors fitted with deflector vanes |
09/24/2003 | CN1443927A Equipment for fixing supporting blades of disributor component arround circumferential curved line |
09/23/2003 | US6622964 System for the synchronized locking of the doors of a thrust reverser |
09/23/2003 | US6622474 Synchronization cross-feed system |