| 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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| 04/21/2005 | US20050082112 Annular acoustic panel |
| 04/21/2005 | US20050081509 Flade gas turbine engine with fixed geometry inlet |
| 04/21/2005 | DE102004012929B3 Noise reduction system for gas turbine engine for aircraft has surface cladding for hot gas channel downstream of turbine, with circular perforated plates covering large ends of frustoconical spaces |
| 04/21/2005 | CA2445934A1 Jet engine nozzle with variable thrust vectoring and exhaust area |
| 04/20/2005 | CN1607323A Operated hot flap of asymmetrical nozzle of turbojet |
| 04/19/2005 | CA2169874C Downstream air flaps thrust reverser for turbojet |
| 04/13/2005 | EP1522772A1 Turbine containing two components connected by a sealing |
| 04/13/2005 | EP1522680A1 Cooling system for a convergent divergent nozzle |
| 04/07/2005 | US20050072876 Variably angled propulsion/steering system |
| 04/07/2005 | DE19721429B4 Verfahren zur Verminderung der Zielsignatur von Luftfahrzeugen A method for reducing the target signature of aircraft |
| 04/06/2005 | EP1141534B1 Exhaust mixer and apparatus using same |
| 03/31/2005 | WO2005028842A2 Controlled autoignition propellant systems |
| 03/31/2005 | WO2005028815A2 Device for the generation of mechanical or electrical energy using any thermal potential |
| 03/31/2005 | WO2005028303A2 Self stowing thrust reverser |
| 03/31/2005 | US20050067218 Noise attenuator arrangement |
| 03/31/2005 | CA2515888A1 Self stowing thrust reverser |
| 03/30/2005 | EP1519009A1 Turbomachine with cabin bleed air through a tube with ball joint |
| 03/30/2005 | CN1601067A Turbomachine with cabin bleed air through a tube with bi-ball joint |
| 03/29/2005 | US6871797 Turbine engine nozzle |
| 03/29/2005 | US6871725 For use in a sound attenuation panel in the high velocity air flow region of an engine nacelle |
| 03/29/2005 | CA2237843C Dichotomous reheat system reducing losses in dry operation |
| 03/24/2005 | WO2005026518A2 Induction coupled variable nozzle |
| 03/24/2005 | US20050061005 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 03/24/2005 | US20050060984 Convergent-divergent turbojet nozzle |
| 03/23/2005 | EP1517032A1 Operated flap for an axisymmetrical exhaust nozzle of a jet engine |
| 03/23/2005 | EP1517006A1 Gas turbine brush seal arrangement for cabin air supply |
| 03/23/2005 | EP1517005A1 Gas turbine sealing joint having lamellar structure |
| 03/23/2005 | EP1515888A1 An acoustic liner, use of such a liner and method for manufacturing an acoustic liner |
| 03/23/2005 | CN1598272A Gas turbine brush seal arrangement for cabin air supply |
| 03/23/2005 | CN1598271A Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 03/19/2005 | CA2480538A1 Operated hot flap of asymmetrical nozzle of turbojet |
| 03/17/2005 | US20050056025 Provision of sealing for the cabin-air bleed cavity using a segment seal |
| 03/16/2005 | EP1515035A2 A jet engine thrust reverser device |
| 03/16/2005 | EP1515004A1 Piston ring type seal for the compressor of a gas turbine |
| 03/16/2005 | EP1451462B1 System architecture for electromechanical thrust reverser actuation systems |
| 03/16/2005 | EP1240421B1 Turbojet engine |
| 03/16/2005 | CN1594845A Provision of sealing for the cabin-air bleed cavity using a segment seal |
| 03/15/2005 | CA2236044C Thrust reverser with protection in the event of accidental shutter release |
| 03/10/2005 | WO2005021934A2 Ventilated confluent exhaust nozzle |
| 03/10/2005 | WO2003106263A8 An acoustic liner, use of such a liner and method for manufacturing an acoustic liner |
| 03/09/2005 | EP1512627A1 Aircraft with thrust reversers |
| 03/09/2005 | CN1192352C Fluidic element structure body for controlling noise and vibration, and control method thereof |
| 03/08/2005 | WO2006088437A2 Passive exhaust suppressor and method |
| 03/03/2005 | US20050045306 Transpiration cooling system |
| 03/02/2005 | EP1509447A2 Bifurcated turbofan nozzle |
| 03/02/2005 | CN1589383A Streamlined body and combustion apparatus having such a streamlined body |
| 03/01/2005 | US6860712 Control strategy for gas turbine engine |
| 02/24/2005 | US20050042081 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle |
| 02/24/2005 | US20050040284 Thrust reverser system actuator having an integral torque limiter |
| 02/24/2005 | US20050039438 Toggle interlocked thrust reverser |
| 02/24/2005 | US20050039437 Turbofan variable fan nozzle |
| 02/23/2005 | EP1507971A1 Variable area thrust reverser nozzle |
| 02/23/2005 | CN1584316A Fuel atomizing nozzles |
| 02/22/2005 | US6857600 Infrared suppressing two dimensional vectorable single expansion ramp nozzle |
| 02/22/2005 | US6857597 Control system for vertical take off and land (VTOL) aircraft |
| 02/22/2005 | CA2200053C Jet engine fan noise reduction system utilizing electro-pneumatic transducers |
| 02/16/2005 | EP1507080A1 Convergent-divergent turboreactor nozzle |
| 02/15/2005 | US6854260 Jet nozzle mixer |
| 02/15/2005 | CA2150222C Silencer |
| 02/12/2005 | CA2478781A1 Convergent-divergent nozzle for jet turbine engine |
| 02/10/2005 | WO2004077400A3 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 02/10/2005 | DE102004032709A1 Turbinenmaschinendüse Turbinenmaschinendüse |
| 02/09/2005 | EP1470329A4 Nozzle throat area control apparatus and method |
| 02/09/2005 | EP1470328A4 Turbofan variable fan nozzle |
| 02/09/2005 | CN1576560A Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 02/09/2005 | CN1576519A Flexible flap for a variable-section turbomachine nozzle |
| 02/08/2005 | CA2204823C Turbofan reverse thruster with obstructions connected to primary cowling |
| 02/03/2005 | US20050026096 Streamlined body and combustion apparatus having such a streamlined body |
| 02/03/2005 | US20050022532 Flexible flap for a variable-section turbomachine nozzle |
| 02/03/2005 | US20050022502 Device for mixing two flows of fluid which are initially guided separate from one another in a two-circuit reaction engine |
| 02/02/2005 | EP1503068A1 Resilient flap for a variable exhaust nozzle of a turbomachine |
| 02/02/2005 | CN1573194A Full port externally gimballed joint |
| 02/02/2005 | CN1573054A System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber |
| 02/01/2005 | US6848651 Electro-hydraulic thrust reverser lock actuation system and method |
| 01/27/2005 | US20050016158 Swivelling nozzle for a rocket engine |
| 01/26/2005 | EP1500880A2 A transpiration cooling system |
| 01/26/2005 | CN1570365A Methods and apparatus for mounting a gas turbine engine |
| 01/25/2005 | US6845946 Self stowing thrust reverser |
| 01/25/2005 | US6845945 Thrust reverser with sliding pivot joints |
| 01/25/2005 | US6845607 Variable area plug nozzle |
| 01/25/2005 | US6845606 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation |
| 01/20/2005 | WO2005005815A1 Thrust reverser system with sequential torque decoupler |
| 01/20/2005 | WO2004097202A3 Toggle interlocked thrust reverser |
| 01/20/2005 | US20050011988 Aircraft configuration |
| 01/20/2005 | US20050011195 Turbine engine nozzle |
| 01/13/2005 | US20050006522 Control system for vertical take off and land (vtol) aircraft |
| 01/13/2005 | US20050005608 Long life nozzle flap for aircraft turbojets |
| 01/13/2005 | US20050005607 System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber |
| 01/13/2005 | US20050005594 Dilution and dispersion device for the exhaust and/or cooling gases of a vehicle's engine |
| 01/12/2005 | EP1496238A1 Apparatus for the reduction of the jetflow noise of a turboengine |
| 01/08/2005 | CA2472878A1 Flexible seal for variable section turbine engine nozzle |
| 01/06/2005 | WO2005001247A2 Confluent exhaust nozzle |
| 01/06/2005 | US20050001095 Self-aligning thrust reverser system lock assembly |
| 01/05/2005 | EP1493912A1 Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 01/05/2005 | EP1493911A2 Four-bar mechanism and gas turbine engine with a variable area nozzle |
| 01/05/2005 | EP1493665A1 Aircraft configuration for attenuation of engine noise |
| 01/04/2005 | US6837054 Actuator assembly with synchronized hydraulic actuators |
| 01/04/2005 | US6837038 Variable cycle boost propulsor |
| 12/30/2004 | US20040262447 Fluidic chevrons and configurable thermal shield for jet noise reduction |
| 12/29/2004 | WO2004113707A1 Thrust reverser system actuator having an integral torque limiter |