| 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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| 12/29/2004 | EP1491752A1 Ventilation channels in the confluence plate of an afterburning chamber |
| 12/29/2004 | EP1179131B1 An apparatus for controlling the flow separation line of rocket nozzles |
| 12/25/2004 | CA2470268A1 Ventilation duct on the confluence plate of an afterburner |
| 12/23/2004 | US20040255573 Combined exhaust duct and mixer for a gas turbine engine |
| 12/23/2004 | US20040255572 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls |
| 12/22/2004 | EP1488999A1 Aircraft engine cowling with reduced gap |
| 12/16/2004 | US20040251379 Rear fastening device for aircraft engine |
| 12/15/2004 | EP1485600A1 Duplex mixer exhaust nozzle |
| 12/09/2004 | US20040245770 Full port externally gimballed joint |
| 12/09/2004 | US20040244357 Divergent chevron nozzle and method |
| 12/08/2004 | EP1484495A2 Externally gimballed joint of a jet pipe |
| 12/08/2004 | EP1407193B1 Coolable segment for a turbomachinery and combustion turbine |
| 12/08/2004 | EP1068438B1 System for activating an adjustable tube by means of an elastic ring for a thrust nozzle |
| 12/07/2004 | US6827180 Noise attenuation panel |
| 12/07/2004 | US6826901 Convergent/divergent segmented exhaust nozzle |
| 12/02/2004 | WO2004104377A2 Rotary adjustable exhaust nozzle |
| 12/02/2004 | US20040238687 Aeroengine nacelle |
| 12/02/2004 | US20040237534 Engine nozzle |
| 12/02/2004 | US20040237501 Apparatus method and system for gas turbine engine noise reduction |
| 12/01/2004 | EP1482160A1 Noise reducing nozzle for a jet engine |
| 12/01/2004 | EP1482159A2 Engine nozzle and engine with such a nozzle |
| 12/01/2004 | EP1482158A1 Movable exhaust nozzle flap of a turbomachine with extended durability |
| 12/01/2004 | EP1482127A1 Sealing system for the bypass flow at the inlet of the afterburner nozzle of a turbomachine |
| 12/01/2004 | EP1481895A1 Rear suspension device for an aircraft engine |
| 12/01/2004 | CN1177999C Apparatus for controlling flow separation line of rocket engine nozzles |
| 11/30/2004 | US6824101 Apparatus and method for mounting a cascade support ring to a thrust reverser |
| 11/30/2004 | CA2126272C Fixed geometry mixer/ejector noise suppression system for turbofan aircraft engines |
| 11/27/2004 | CA2469853A1 Secondary flow sealing system at the entrance of a turbomachine nozzle with post-combustion chamber |
| 11/27/2004 | CA2429884A1 Turbojet automobile and aircraft propulsion system |
| 11/25/2004 | US20040231317 Locking system on a grid thrust reverser |
| 11/24/2004 | EP1478836A1 Electric thrust reverser actuation system |
| 11/24/2004 | EP1040265B1 Vectoring nozzle calibration |
| 11/23/2004 | US6820410 Bifurcated turbofan nozzle |
| 11/18/2004 | WO2004099602A2 Self-aligning thrust reverser system lock assembly |
| 11/18/2004 | US20040228976 Sprayable noble metal coating for high tempreature use on ceramic and smoothcoat coated aircraft engine parts |
| 11/18/2004 | DE10342840A1 Method for generating mechanical or electric energy utilizing thermal potentials of natural or artificial origin by compressed flow of compressible medium through diffuser with integrated heat exchanger |
| 11/11/2004 | WO2004097202A2 Toggle interlocked thrust reverser |
| 11/11/2004 | CA2517434A1 Toggle interlocked thrust reverser |
| 11/10/2004 | EP1474328A2 Control system for vertical take off and land (vtol) aircraft |
| 11/09/2004 | US6814191 Thrust reverser system with a pass-through torque activated brake |
| 11/09/2004 | US6813877 Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators |
| 11/04/2004 | US20040216461 Methods and apparatus for mounting a gas turbine engine |
| 11/04/2004 | US20040216446 Device for controlling propulsive jet mixing for aircraft jet engines |
| 11/03/2004 | EP1473441A2 Apparatus for mounting a gas turbine engine |
| 11/03/2004 | EP1472449A2 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
| 11/02/2004 | US6810656 Thrust reverser system power drive unit with dual sequential torque decoupler and method |
| 10/27/2004 | EP1470329A1 Nozzle throat area control apparatus and method |
| 10/27/2004 | EP1470328A1 Turbofan variable fan nozzle |
| 10/27/2004 | EP1470327A1 Variable area plug nozzle |
| 10/26/2004 | US6807803 Gas turbine exhaust diffuser |
| 10/21/2004 | WO2004036020A3 Thrust vectoring and variable exhaust area for jet engine nozzle |
| 10/21/2004 | US20040206066 Lock assembly that inhibits thrust reverser movement at or near the stowed position |
| 10/20/2004 | EP1469184A1 Turbo jet engine |
| 10/20/2004 | CN1538051A Long service life jet deflection plate for turbine jet motor of aircraft |
| 10/20/2004 | CN1538047A Augmentor |
| 10/20/2004 | CN1172143C Thermal resistance coating system and its material |
| 10/19/2004 | US6804948 Lobe mixer for jet engine |
| 10/19/2004 | US6804947 Device for cooling the common nozzle of a turbojet pod |
| 10/19/2004 | CA2230010C Door-type thrust reverser of a jet turbine engine with doors associated with a control synchronization device |
| 10/13/2004 | EP1068437B1 System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies |
| 10/07/2004 | US20040195443 Self stowing thrust reverser |
| 10/07/2004 | US20040195434 Thrust reverser utilizing integrated structural bypass duct |
| 10/07/2004 | US20040195432 Electro-hydraulic thrust reverser lock actuation system and method |
| 10/07/2004 | US20040195397 Ejector device for direct injection fuel jet |
| 10/06/2004 | EP1464822A2 Methods and apparatus for operating gas turbine engines |
| 10/05/2004 | US6799418 Rocket engine member and method for manufacturing a rocket engine member |
| 09/30/2004 | US20040188211 Thrust reverser system with sequential torque decoupler |
| 09/30/2004 | US20040187476 Bifurcated turbofan nozzle |
| 09/30/2004 | US20040187474 Methods and apparatus for operating gas turbine engines |
| 09/29/2004 | EP1462642A1 Thrust reverser utilizing integrated structural bypass duct |
| 09/29/2004 | CN1532395A AIr jet engine attached device |
| 09/23/2004 | WO2004068035A3 Heat shield element, combustion chamber and gas turbine |
| 09/22/2004 | EP1458968A1 A component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 09/21/2004 | US6792748 Cooling system for a gas turbine engine post-combustion jet nozzle |
| 09/16/2004 | US20040177616 Augmentor |
| 09/16/2004 | DE10219502B4 Verfahren zum Herstellen gelöteter Wärmetauscherstrukturen, insbesondere regenerativ gekühlter Brennkammern A method for producing brazed heat exchanger structures, especially regenerative cooled combustors |
| 09/15/2004 | EP1457738A2 Afterburner |
| 09/15/2004 | EP1457660A1 Closing and locking device for thrust reverser doors |
| 09/15/2004 | EP1457659A2 Apparatus and method for mounting a cascade support ring to a thrust reverser |
| 09/15/2004 | EP1457648A1 Exhaust gas dilution device |
| 09/14/2004 | US6789316 Method for manufacturing outlet nozzles for rocket engines |
| 09/13/2004 | CA2458280A1 Augmentor |
| 09/10/2004 | WO2004077400A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 09/08/2004 | CN1527922A Coolable segment for a turbomachinery and combustion turbine |
| 09/07/2004 | US6786315 Thrust reverser system with sequential torque decoupler |
| 09/07/2004 | US6786039 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
| 09/07/2004 | US6786038 Duplex mixer exhaust nozzle |
| 09/07/2004 | US6786037 Segmented mixing device having chevrons for exhaust noise reduction in jet engines |
| 09/01/2004 | EP1451462A1 System architecture for electromechanical thrust reverser actuation systems |
| 09/01/2004 | EP1451461A1 Jet nozzle mixer |
| 09/01/2004 | CN2637749Y Direct jetting engine |
| 08/26/2004 | US20040163888 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 08/25/2004 | EP1448883A1 Noise attenuator arrangement |
| 08/24/2004 | US6779336 Cooled variable geometry exhaust nozzle |
| 08/19/2004 | US20040159741 Apparatus and method for mounting a cascade support ring to a thrust reverser |
| 08/19/2004 | US20040159092 Jet nozzle mixer |
| 08/19/2004 | US20040159091 Apparatus and method for mounting a cascade support ring to a thrust reverser |
| 08/18/2004 | EP1446611A1 Flow-type body and combustion device provided with a flow-type body of this type |
| 08/18/2004 | EP1402166A4 Rocket vehicle thrust augmentation within divergent section of nozzle |
| 08/18/2004 | CN1521087A Maintenance and inhibition plate for a thrust reverser |