| 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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| 05/08/2007 | US7213393 Device for supplying cooling air to exhaust nozzle flaps |
| 05/04/2007 | CA2562452A1 Duct for reducing shock related noise |
| 05/03/2007 | WO2007049032A1 Turbofan engine for stol aircraft |
| 05/03/2007 | US20070095049 Synchronized motor thrust reverser actuation system |
| 05/02/2007 | EP1780394A2 Syncronized motor thrust reverser actuation system |
| 05/02/2007 | EP1780124A2 Eductor swirl buster |
| 05/02/2007 | EP1440004B1 Passive cooling system for auxiliary power unit installation |
| 05/02/2007 | CN1313769C Streamlined body, use thereof, and combustion apparatus for burning fuel mixture |
| 05/01/2007 | US7210900 Gas turbine engine component having bypass circuit |
| 05/01/2007 | US7210897 Actively-controlled sound absorption panel system using movement-controlled reflective plate |
| 05/01/2007 | US7210283 Maintenance and inhibition plate for a thrust reverser |
| 04/26/2007 | WO2007045754A1 Turbojet engine with attenuated jet noise |
| 04/26/2007 | CA2625068A1 Turbojet engine with attenuated jet noise |
| 04/19/2007 | US20070084191 Closure and locking detection system for turbojet thrust reverser |
| 04/18/2007 | EP1775485A2 Apparatus for moving rotatable components |
| 04/18/2007 | EP1313937B1 High frequency excitation apparatus and method for reducing jet and cavity noise |
| 04/11/2007 | EP1771648A1 Method for opening a mobile cowl equipping a thrust reverser |
| 04/05/2007 | WO2007037725A1 An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
| 04/04/2007 | EP1770078A2 Process for wear protectiion of a high temperature resistant ceramic matrix composite material workpiece and coating and workpiece obtained thereby |
| 04/04/2007 | EP1451461B1 Jet nozzle mixer |
| 04/04/2007 | CN1942665A Jet nozzle mixer |
| 04/03/2007 | CA2326790C System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies |
| 03/28/2007 | EP1767768A2 Turbine engine nozzle |
| 03/28/2007 | EP1767753A1 Infrared discretion device of a motor vehicle exhaust duct |
| 03/28/2007 | EP1766219A1 Cooling device for the primary nozzle of a dual-flow turbojet engine |
| 03/28/2007 | EP1766218A1 Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 03/28/2007 | EP1470328B1 Turbofan exhaust nozzle and method of reducing noise in such a nozzle |
| 03/28/2007 | CA2561227A1 Anti-wear protection process for a thermostructural part made of composite matrix ceramic material, coating and the part obtained through this process |
| 03/27/2007 | CA2364377C Gas turbine combustor, gas turbine, and jet engine |
| 03/22/2007 | WO2007031618A1 Method for attenuating the noise of a turbofan |
| 03/22/2007 | WO2007031616A1 Dynamically self-locking catching device |
| 03/22/2007 | WO2005113970A3 Method of evaluation of space systems for safety assurance and residual risk to flight crew |
| 03/22/2007 | US20070063098 Passive cooling system for auxiliary power unit installation |
| 03/22/2007 | CA2620494A1 Dynamically self-locking catching device |
| 03/22/2007 | CA2619292A1 Method for attenuating the noise of a turbofan |
| 03/21/2007 | EP1764499A1 Thrust reverser including a latching mechanism and method of manufacturing such a thrust reverser |
| 03/21/2007 | EP1764498A2 Convergent divergent nozzle with interlocking divergent flaps |
| 03/13/2007 | US7188477 High temperature dynamic seal for scramjet variable geometry |
| 03/13/2007 | US7188417 Advanced L-channel welded nozzle design |
| 03/07/2007 | EP1760271A2 Valve assembly for a gas turbine engine |
| 02/28/2007 | EP1755867A1 Method for production of elements such as thrust-reverser cascade vanes by moulding of a composite material |
| 02/27/2007 | US7181915 High temperature centerbody for temperature reduction by optical reflection and process for manufacturing |
| 02/22/2007 | US20070039328 Turbine engine nozzle |
| 02/22/2007 | US20070039327 Monobloc flameholder arm for an afterburner device of a bypass turbojet |
| 02/20/2007 | US7178338 Variable area nozzle |
| 02/20/2007 | US7178325 Divergent flap for a gas turbine engine |
| 02/15/2007 | WO2007018627A1 Radially expanding turbine engine exhaust cylinder interface |
| 02/15/2007 | US20070033922 Serrated nozzle trailing edge for exhaust noise suppression |
| 02/14/2007 | EP1752649A2 Serrated nozzle trailing edge of a gas turbine |
| 02/14/2007 | EP1752648A2 Aircraft engine exhaust flap curved strut slot |
| 02/14/2007 | EP1752637A2 Architecture for an acoustic liner |
| 02/14/2007 | EP1751415A2 Method of evaluation of space systems for safety assurance and residual risk to flight crew |
| 02/14/2007 | CN1912372A Serrated nozzle trailing edge for exhaust noise suppression |
| 02/13/2007 | US7174718 Device for controlling propulsive jet mixing for aircraft jet engines |
| 02/13/2007 | US7174704 Split shroud exhaust nozzle |
| 02/10/2007 | CA2551929A1 Serrated nozzle trailing edge for exhaust noise supression |
| 02/07/2007 | EP1750003A2 Infrared suppressor apparatus |
| 02/07/2007 | EP1750002A2 One-piece baffle infrared suppressor apparatus |
| 02/07/2007 | EP1750001A2 An exhaust nozzle for a gas turbine engine |
| 02/07/2007 | EP1040736B1 Synthetic jet actuators for cooling heated bodies and environments |
| 02/07/2007 | CN1298987C Vectoring nozzle control system |
| 02/03/2007 | CA2554385A1 One-piece baffle infrared suppressor apparatus and method |
| 02/03/2007 | CA2554151A1 Infrared suppressor apparatus and method |
| 01/31/2007 | EP1748177A1 Compact, light weight eductor oil cooler plenum and surge flow plenum design |
| 01/30/2007 | US7168253 Monobloc flameholder arm for an afterburner device of a bypass turbojet |
| 01/25/2007 | US20070017209 Newtonian thrust cowl array |
| 01/24/2007 | EP1745207A2 Pulse jet engines |
| 01/24/2007 | CN1900507A Steam booster of rocket propeller |
| 01/17/2007 | EP1744033A2 Acoustic liner assembly |
| 01/16/2007 | US7163206 Fluid seal |
| 01/16/2007 | US7162859 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 01/13/2007 | CA2548719A1 Impact resistance acoustic treatment |
| 01/11/2007 | WO2007005520A2 Jet nozzle mixer |
| 01/11/2007 | WO2007003749A1 Aircraft pod and aircraft equipped with at least one such pod |
| 01/11/2007 | US20070007388 Thrust reversers including locking assemblies for inhibiting deflection |
| 01/11/2007 | CA2612117A1 Aircraft pod and aircraft equipped with at least one such pod |
| 01/10/2007 | EP1741915A1 Nozzle with orientable thrust |
| 01/09/2007 | US7159383 Apparatus, method and system for gas turbine engine noise reduction |
| 01/09/2007 | CA2422553C Valve assembly for gas turbine engine |
| 01/09/2007 | CA2332467C Thrust reverser with bladed deflection grilles with a fixed rear structure |
| 01/09/2007 | CA2317707C Heat exchanger in composite material and method for making same |
| 01/09/2007 | CA2239462C Bypass turbojet thrust reverser with doors fitted with a movable spoiler with optimized drive |
| 01/07/2007 | CA2545761A1 Methods and apparatus for assembling gas turbine engines |
| 01/04/2007 | WO2005094227A3 Spider actuated thrust reverser |
| 01/04/2007 | US20070000234 Jet nozzle mixer |
| 01/04/2007 | US20070000233 Thrust orienting nozzle |
| 01/03/2007 | EP1739299A1 Locking device for a jet engine thrust reverser |
| 01/03/2007 | EP1739281A2 Arrangement for controlling fluid jets injected into a fluid stream |
| 01/03/2007 | EP1738112A1 Damping of vibration of a combustion chamber by resonators |
| 01/02/2007 | US7155898 Thrust vector control system for a plug nozzle rocket engine |
| 12/30/2006 | CA2551343A1 Thrust vectoring nozzle |
| 12/28/2006 | US20060288688 Turbofan core thrust spoiler |
| 12/27/2006 | EP1735532A2 Thrust vector control system for a plug nozzle rocket engine |
| 12/27/2006 | EP1735531A2 Method and device for reducing engine noise |
| 12/26/2006 | US7153054 Fastener assembly for attaching a non-metal component to a metal component |
| 12/21/2006 | WO2006135402A1 Thrust reverser system electro-mechanical brake manual release mechanism |
| 12/21/2006 | WO2006134253A1 Control system for the nacelle of a turboreactor |
| 12/21/2006 | WO2006110123A3 Vectoring transition duct for turbine engine |
| 12/21/2006 | US20060283188 Suppression of part of the noise from a gas turbine engine |
| 12/21/2006 | CA2611556A1 Control system for the nacelle of a turboreactor |