Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
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)
04/2003
04/17/2003US20030070417 Apparatus and method for thrust vector control
04/17/2003US20030070416 Jet engine thrust reverser system having torque limited synchronization
04/16/2003EP1302640A2 Variable cycle boost propulsor
04/15/2003US6546716 Jet engine nozzle with variable thrust vectoring and exhaust area
04/15/2003US6546715 Cascade-type thrust reverser
04/10/2003US20030066284 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism
04/10/2003US20030066283 System and method for controlling the deployment of jet engine thrust reversers
04/08/2003CA2065677C Axisymmetric vectoring exhaust nozzle thermal shield
04/03/2003WO2003027475A1 Converging nozzle thrust reverser
04/03/2003WO2003027474A1 Locking system on a grid thrust reverser
04/02/2003EP1298309A1 Locking system for a thrust reverser with a sliding fan housing
03/2003
03/27/2003WO2003025378A2 Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine
03/27/2003WO2003025377A1 Device for controlling propulsive flow mixture for aircraft reactor
03/27/2003US20030056493 Converging nozzle thrust reverser
03/25/2003US6536556 Noise reduction sandwich panel, notably for aircraft turbojet engine
03/20/2003WO2003023215A1 Trust reverser actuator including an integrated locking mechanism
03/19/2003EP1077871B1 Ir suppressor
03/18/2003US6532729 Shelf truncated chevron exhaust nozzle for reduction of exhaust noise and infrared (IR) signature
03/13/2003US20030049470 Ceramic containing hafnia, germanium oxide on metallic substrate
03/13/2003US20030047878 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
03/06/2003US20030042358 Out-of-plane thrust reverser sleeve lock
03/05/2003EP1288480A1 Ramjet for supersonic and hypersonic aircraft
03/05/2003EP1288479A2 Thrust reverser sleeve lock
03/05/2003EP1288478A1 Synchronization cross-feed system
03/05/2003EP1286885A1 Propulsion system
03/04/2003US6526744 System and method for controlling the stowage of jet engine thrust reversers
02/2003
02/26/2003EP1286037A1 Lock for the turbofan engine thrust reverser
02/20/2003US20030033798 VTOL aircraft propulsion systems and forward flight thrust vectoring
02/18/2003US6520450 V/STOL aircraft
02/18/2003US6519929 System and method for controlling the deployment of jet engine thrust reversers
02/13/2003WO2002036944A9 Turbogenerator exhaust silencer
02/11/2003US6516606 Aeroengine nacelle afterbodies
02/06/2003WO2003010430A1 Thrust reverser position determination system and method
02/06/2003US20030024236 Lock for the translating sleeve of a turbofan engine thrust reverser
02/06/2003US20030024235 Control strategy for gas turbine engine
02/06/2003CA2455554A1 Thrust reverser position determination system and method
02/05/2003EP1281846A2 Control strategy for gas turbine engine
01/2003
01/30/2003US20030019206 Thrust reverser position determination system and method
01/29/2003CN2533277Y Water and fuel mixed combustion high-efficiency energy-saving engine with infrared silencer for flying boat and vehicles
01/29/2003CN1394263A Thermally stressable wall and method for sealing gap in thermally stressed wall
01/28/2003US6511284 Methods and apparatus for minimizing gas turbine engine thermal stress
01/28/2003CA2099502C Thrust reverser with a planar exit opening
01/23/2003WO2003006883A1 Coolable segment for a turbomachinery and combustion turbine
01/21/2003US6509081 No-septum acoustic sandwich panel, and apparatus and method for suppressing noise in a nozzle
01/21/2003US6508055 Variable mode jet engine—suitable for STOVL
01/16/2003WO2003004852A1 Rocket vehicle thrust augmentation within divergent section of nozzle
01/16/2003US20030013356 Propulsion system
01/16/2003US20030012939 Fiber reinforced composite article, fiber member, and method for making
01/14/2003US6505706 Exhaust flow guide for jet noise reduction
01/09/2003US20030005701 Rocket vehicle thrust augmentation within divergent section of nozzle
01/08/2003CN1098412C Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same
01/07/2003US6502383 Stub airfoil exhaust nozzle
12/2002
12/27/2002WO2002103189A1 System and method for sustaining electic power during a momentary power interruption in an electric thrust reverser actuation system
12/27/2002WO2002103188A1 Exhaust flow guide for jet noise reduction
12/19/2002WO2002101222A1 Pivot fairing thrust reverser
12/19/2002US20020189896 Exhaust flow guide for jet noise reduction
12/19/2002US20020189232 Outlet device for a jet engine
12/19/2002US20020189230 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation
12/18/2002EP1267064A1 Variable cycle propulsion device for supersonic airplanes using diverted exhaust gas and operation method thereof
12/18/2002EP1266044A2 Nickel vapour deposition manufacture of aircraft engine parts
12/17/2002US6494033 Sequentially operated actuator with brake arrangement
12/12/2002US20020184874 Pivot fairing thrust reverser
12/05/2002US20020182058 Methods and apparatus for minimizing gas turbine engine thermal stress
12/05/2002US20020178711 Truncated chevron exhaust nozzle
12/04/2002EP1262636A2 Gas turbine engine exhaust frame for minimizing the thermal stress and method for assembling it
12/04/2002CN1382903A Supersonic swirl boosted propulsion engine
12/03/2002US6487848 Gas turbine engine jet noise suppressor
12/03/2002US6487847 Gas turbine engine fuel control system
12/03/2002US6487846 Thrust reverser actuator including an integrated locking mechanism
12/03/2002US6487845 Pivot fairing thrust reverser
11/2002
11/27/2002EP1260696A1 Synchronised latch system for thrust reverser blocker doors
11/19/2002US6482485 Structural part including a portion made of thermostructural composite material cooled by fluid circulation
11/14/2002US20020166718 Acoustically treated turbomachine multi-duct exhaust device
11/14/2002US20020166318 Pulse detonation bypass engine propulsion pod
11/13/2002EP1256705A2 Engine interface for axisymmetric vectoring nozzle
11/13/2002EP0991861B1 Turbo-shaft engine having an exhaust nozzle for suppressing infrared radiation
11/07/2002WO2002088540A1 Device for controlling the deployment of jet engine thrust reversers
11/07/2002WO2002088539A1 Jet engine nozzle with variable thrust vectoring and exhaust area
11/07/2002WO2002088538A1 System for controlling the stowage of jet engine thrust reversers
11/07/2002US20020164249 Gas turbine engine exhaust nozzle
11/06/2002EP1222380A4 Swing pivot thrust reverser
11/05/2002US6474059 Thrust reverser
11/05/2002CA2127261C Exhaust eductor cooling system
10/2002
10/31/2002WO2002086303A1 Lobe mixer for jet engine
10/31/2002US20020158146 Jet engine nozzle with variable thrust vectoring and exhaust area
10/31/2002US20020157377 System and method for controlling the stowage of jet engine thrust reversers
10/31/2002US20020157376 System for controlling the deployment of jet engine thrust reversers
10/29/2002US6472346 Photocatalytic nuisance organism inhibitor agents
10/29/2002US6471469 Methods and apparatus for sealing gas turbine engine variable nozzles
10/24/2002US20020152752 Apparatus for controlling the flow separation line of rocket nozzles
10/23/2002EP1251262A1 System for security door lock of a thrust reverser
10/23/2002EP1099050B1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same
10/22/2002US6468594 Method for thermal protection of a surface against a thermally and mechanically aggressive environment
10/17/2002WO2002081893A1 Exhaust thrust booster for a thrust generator
10/16/2002EP1248924A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
10/15/2002US6463992 Method of manufacturing seamless self-supporting aerodynamically contoured sheet metal aircraft engine parts using nickel vapor deposition
10/10/2002WO2002079631A1 Tortuous path exhaust eductor system
10/10/2002US20020145078 System for the synchronized locking of the doors of a thrust reverser
10/10/2002US20020144499 Backup locking system for a thrust reverser door
10/09/2002EP0868596B1 Sound suppressor exhaust structure
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