| 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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| 02/24/2009 | US7494153 Anti-roll thrust system for vehicles |
| 02/23/2009 | CA2639169A1 Turbofan engine with reduced jet noise |
| 02/19/2009 | US20090044541 Apparatus and method for reduction of jet noise from single jets |
| 02/17/2009 | CA2359239C Aircraft propulsive power unit |
| 02/12/2009 | WO2008152259A3 Acoustic panel having a variable acoustic characteristic |
| 02/12/2009 | WO2008113900A3 Self-calibration method for the electric jacks of a turbojet nacelle |
| 02/12/2009 | DE102007036527A1 Düsenanordnung für ein Gasturbinentriebwerk Nozzle arrangement for a gas turbine engine |
| 02/11/2009 | EP2021610A1 Turbojet nacelle equipped with means for reducing the noise produced by said turbojet |
| 02/05/2009 | WO2008111992A8 Monolithic thrust reverser components |
| 02/05/2009 | US20090031730 Nozzle Arrangement for a Gas Turbine Engine |
| 02/03/2009 | US7484355 Thrust reverser comprising optimized deflector gratings |
| 02/03/2009 | CA2308131C Exit area control mechanism for convergent divergent nozzles |
| 01/29/2009 | WO2008139048A3 Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 01/29/2009 | US20090026283 Thrust vectoring system and method |
| 01/29/2009 | US20090025393 Auxiliary power unit assembly |
| 01/29/2009 | US20090025362 Infrared suppression system with spiral septum |
| 01/27/2009 | US7481038 Yaw vectoring for exhaust nozzle |
| 01/27/2009 | CA2360885C Fuel-saving circuit |
| 01/22/2009 | US20090019857 Modular chevron exhaust nozzle |
| 01/21/2009 | EP2016274A1 Nacelle for bypass engine with high bypass ratio |
| 01/20/2009 | US7478525 System and method for controlling the temperature and infrared signature of an engine |
| 01/15/2009 | US20090013664 Actuator Arrangement |
| 01/14/2009 | EP2013466A1 Sound-absorbing exhaust nozzle center plug |
| 01/14/2009 | CN100450631C Low noise pneumatic jet nozzle |
| 01/13/2009 | US7475550 Method and device for reducing engine noise |
| 01/13/2009 | US7475548 Vectorable nozzle with pivotable triangular panels |
| 01/13/2009 | US7475547 Convergent turbojet exhaust nozzle |
| 01/08/2009 | WO2009004143A2 Dual flow turboshaft engine and improved hot flow nozzle |
| 01/07/2009 | CN101341326A Exhaust dispersion device |
| 01/06/2009 | US7472543 Jet engine noise suppressor |
| 01/01/2009 | US20090000304 Integrated support and mixer for turbo machinery |
| 12/31/2008 | WO2008097247A8 Engine exhaust system |
| 12/31/2008 | CN101333977A Engines tail jet flow plasma arc temperature-increasing jet tube |
| 12/30/2008 | US7469529 Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
| 12/30/2008 | US7469528 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/24/2008 | WO2008155480A1 Multiple-acting linear actuator |
| 12/24/2008 | WO2008107605A3 Aircraft nacelle incorporating a thrust-reversing device |
| 12/24/2008 | EP1797311B1 Quiet chevron/tab exhaust eductor system |
| 12/24/2008 | CA2690907A1 Actionneur lineaire a action multiple |
| 12/23/2008 | US7467684 Anti-roll thrust system for hydrogen powered vehicles |
| 12/18/2008 | WO2008067000B1 Pintle-controlled propulsion system with external dynamic seal |
| 12/18/2008 | US20080308345 Assembly for Reducing Noise in Turbofan Engines |
| 12/18/2008 | CA2685287A1 Acoustic panel having a variable acoustic characteristic |
| 12/11/2008 | WO2008148999A2 Exhaust system for gas turbine |
| 12/11/2008 | WO2008111992A3 Monolithic thrust reverser components |
| 12/11/2008 | US20080302083 Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines |
| 12/11/2008 | CA2682991A1 Exhaust system for gas turbine |
| 12/10/2008 | EP1999022A1 Air inlet shroud structure |
| 12/10/2008 | CN101319641A Rotating wheel type jet engine |
| 12/09/2008 | CA2538806C Annular acoustic panel |
| 12/04/2008 | WO2008145725A1 Propulsion assembly for aircraft with sliding nacelle |
| 12/04/2008 | US20080295481 Fluidic vectoring for exhaust nozzle |
| 12/04/2008 | CA2689111A1 Propulsion assembly for aircraft with sliding nacelle |
| 12/03/2008 | EP1998035A2 Fluidic vectoring for exhaust nozzle |
| 12/03/2008 | EP1998029A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operating method |
| 12/03/2008 | EP1998007A2 Single actuator controlled rotational flow balance system |
| 12/02/2008 | US7458221 Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths |
| 11/27/2008 | WO2008143558A1 A system for mixing gas flows in a gas turbine engine, gas turbine engine and an aircraft engine |
| 11/27/2008 | WO2008143556A1 A masking arrangement for a gas turbine engine |
| 11/27/2008 | WO2008142243A1 Door with movable spoiler for door-type thrust reverser |
| 11/27/2008 | WO2008142218A1 Grid thrust reverser cover comprising a seal support and associated seal |
| 11/27/2008 | WO2008100712A3 Systems and methods for reducing noise from jet engine exhaust |
| 11/27/2008 | US20080290213 Turbofan Engine for Stol Aircraft |
| 11/27/2008 | US20080289317 Control Method For Actuating a Thrust Reverser |
| 11/27/2008 | CA2687518A1 Door with movable spoiler for door-type thrust reverser |
| 11/27/2008 | CA2682213A1 Grid thrust reverser cover comprising a seal support and associated seal |
| 11/26/2008 | EP1995441A2 Fluted chevron exhaust nozzle |
| 11/26/2008 | EP1995415A1 Gas turbine exhaust duct installation |
| 11/26/2008 | EP1673530B1 Thrust reverser lock comprising locking device |
| 11/26/2008 | CN101313139A Control method for driving pushing force commutator |
| 11/20/2008 | WO2008139114A1 Cmc mixer with structural outer cowling |
| 11/20/2008 | WO2008139095A2 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained |
| 11/20/2008 | WO2008139048A2 Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 11/20/2008 | CA2683168A1 A cmc mixer having a structural outer cowling |
| 11/20/2008 | CA2680265A1 Nacelle for turbojet jet fitted with a single door thrust reverser system |
| 11/20/2008 | CA2680117A1 Method for assembling end-to-end two parts having different thermal expansion coefficients and assembly thus obtained |
| 11/19/2008 | EP1992807A2 Variable geometry nacelle for an aircraft engine and corresponding operating method |
| 11/19/2008 | CN101307734A Rocket engine noise reducer |
| 11/18/2008 | CA2461207C Locking system on a grid thrust reverser |
| 11/18/2008 | CA2379192C Thrust reverser door emergency locking system |
| 11/13/2008 | WO2008135644A1 Thrust reverser for a jet engine |
| 11/13/2008 | WO2008102079A3 Nacelle for aircraft jet engine and aircraft including such nacelle |
| 11/13/2008 | CA2680485A1 Thrust reverser for a jet engine |
| 11/12/2008 | EP1989109A2 Infrared suppression system with spiral septum |
| 11/12/2008 | EP1588102B1 Heat shield element, combustion chamber and gas turbine |
| 11/06/2008 | WO2008132297A2 Rear nacelle structure for a jet engine, such as a thrust reverser |
| 11/06/2008 | WO2008132294A1 Device for varying the cross section of a secondary nozzle associated with a gate reverser and jet smoothing device |
| 11/06/2008 | WO2008104692A3 Method of manufacturing a cmc flow mixer lobed structure for a gas turbine aeroengine |
| 11/06/2008 | US20080271431 Turbojet Engine with Attenuated Jet Noise |
| 11/06/2008 | DE10145489B4 Anordnung zum Vermischen von zwei ursprünglich getrennt geführten Fluidströmen in einem Zweikreis-Strahltriebwerk Arrangement for mixing two initially separate fluid flows out in a two-circuit jet engine |
| 11/06/2008 | CA2681354A1 Device for varying the cross section of a secondary nozzle associated with a gate reverser and jet smoothing device |
| 11/05/2008 | EP1988273A2 Power unit including a voltage limiting circuit for tertiary lock system |
| 11/05/2008 | CN201144919Y Hydraulic actuating cylinder |
| 11/05/2008 | CN201144903Y Mechanical synchronous hydraulic actuation system |
| 10/30/2008 | WO2008129177A1 Method for reducing noise output at the back of a turboshaft engine and turboshaft engine improved by this method |
| 10/30/2008 | WO2008128422A1 A nuclear reactor |
| 10/30/2008 | WO2008067000A3 Pintle-controlled propulsion system with external dynamic seal |
| 10/30/2008 | WO2008063153A3 Managing low pressure turbine maximum speed in a turbofan engine |
| 10/30/2008 | US20080264718 Jet nozzle having noise attenuating shield and method therefor |
| 10/30/2008 | US20080264034 System and method for controlling the temperature and infrared signature of an engine |