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