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)
09/2003
09/23/2003US6622472 Apparatus and method for thrust vector control
09/17/2003EP1344928A2 Variable area nozzle
09/17/2003EP1343962A2 Aero-engine exhaust jet noise reduction assembly
09/17/2003EP1343956A1 Bypass duct fan noise reduction assembly
09/16/2003US6619916 Methods and apparatus for varying gas turbine engine inlet air flow
09/09/2003US6615576 Tortuous path quiet exhaust eductor system
09/04/2003WO2003072923A1 Duplex mixer exhaust nozzle
09/04/2003WO2003072922A1 Electric thrust reverser actuation system
09/04/2003US20030163985 Cowl structure for a gas turbine engine
09/03/2003EP1340901A2 Noise attenuating segmented exhaust nozzle
09/03/2003EP1340894A2 Variable inlet guide vanes for varying gas turbine engine inlet air flow
09/03/2003EP1340736A1 Porous sound absorbing material and method of manufacturing the material
09/02/2003US6612106 Segmented mixing device having chevrons for exhaust noise reduction in jet engines
08/2003
08/28/2003US20030161724 Methods and apparatus for varying gas turbine engine inlet air flow
08/28/2003US20030159430 Thrust vectoring and variable exhaust area for jet engine nozzle
08/28/2003US20030159429 Gearless electric thrust reverser actuators and actuation system incorporating same
08/28/2003US20030159428 Convergent/divergent segmented exhaust nozzle
08/28/2003US20030159427 External system and method for rocket exhaust plume signature tailoring
08/28/2003US20030159426 Rocket exhaust plume signature tailoring
08/27/2003EP1338784A1 Lobe mixer for jet flow
08/26/2003US6609592 Noise attenuation panel
08/21/2003WO2003068597A2 Control system for vertical take off and land (vtol) aircraft
08/21/2003US20030154707 Rotary inlet flow controller for pulse detonation combustion engines
08/20/2003EP1248924B1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall
08/19/2003US6606854 Exhaust mixer and apparatus using same
08/14/2003US20030150954 Control system for vertical take off and land (vtol) aircraft
08/14/2003US20030150214 Variable area plug nozzle
08/13/2003EP1335113A1 Fastening device for gas turbine distributor sectors
08/12/2003US6604355 Thrust reverser hook latch system
08/07/2003US20030146578 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
08/07/2003US20030146296 Active noise reducing nozzle
08/07/2003US20030145600 Methods and apparatus for retaining gas turbine engine nozzle basesheets
08/07/2003US20030145599 Methods and apparatus for sealing gas turbine engine nozzles
08/07/2003US20030145578 Lobe mixer for jet flow
08/07/2003US20030145577 System and method of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
08/06/2003EP1333172A1 Cooling system for an afterburner nozzle of a turbomachine
08/06/2003EP1333164A1 Exhaust apparatus for internal combustion engine
07/2003
07/31/2003US20030141144 Noise attenuation panel
07/31/2003US20030140615 Device for cooling the common nozzle of a turbojet pod
07/30/2003EP1331404A1 Actuation assembly with synchronized hydraulic actuators
07/29/2003US6599092 Methods and apparatus for cooling gas turbine nozzles
07/29/2003US6598386 Jet engine thrust reverser system having torque limited synchronization
07/24/2003WO2003060313A1 Nozzle throat area control apparatus and method
07/24/2003WO2003060312A1 Turbofan variable fan nozzle
07/24/2003WO2003060311A1 Variable area plug nozzle
07/24/2003US20030136129 Actuator assembly with synchronized hydraulic actuators
07/24/2003CA2472604A1 Variable area plug nozzle
07/17/2003WO2003057561A2 Variably angled propulsion/steering system
07/16/2003EP1327767A1 Cooling device for a common nozzle of a turbofan engine
07/16/2003CN1429968A Method and device for cooling gas turbine nozzle
07/15/2003US6592074 System driving the displaceable fairing of a turbojet-engine thrust reverser
07/10/2003US20030129054 Methods and apparatus for cooling gas turbine nozzles
07/10/2003US20030126861 Nozzle throat area control apparatus and method
07/10/2003US20030126856 Confluent variable exhaust nozzle
07/09/2003EP1326006A2 Methods and apparatus for cooling gas turbine nozzles
07/02/2003EP1322854A1 Apparatus, method and system for gas turbine engine noise reduction
07/02/2003CN1113164C Heat exchanger in composite material and method for making same
07/01/2003US6584766 Methods and apparatus for minimizing thermal stresses in a centerbody
07/01/2003US6584763 Lock for the translating sleeve of a turbofan engine thrust reverser
07/01/2003US6584762 Gas turbine engine fuel control method
06/2003
06/26/2003WO2003052255A1 A component for being subjected to high thermal load during operation and a method for manufacturing such a component
06/26/2003US20030115852 Segmented mixing device having chevrons for exhaust noise reduction in jet engines
06/25/2003EP1321542A1 Thermal barrier coating systems and materials
06/25/2003EP1320674A1 Jet engine with unsteady flow ejector
06/19/2003WO2003050404A1 System architecture for electromechanical thrust reverser actuation systems
06/19/2003WO2003050403A1 Jet nozzle mixer
06/17/2003US6578355 Bloom mixer for a turbofan engine
06/10/2003US6574952 Apparatus for controlling the flow separation line of rocket nozzles
06/05/2003WO2003046358A1 Noise attenuator arrangement
06/05/2003US20030101712 System architecture for electromechanical thrust reverser actuation systems
06/05/2003CA2468141A1 Noise attenuator arrangement
06/03/2003US6574534 6-degree-of-freedom control apparatus for spacecraft
06/03/2003US6571549 Jet noise suppressor
05/2003
05/30/2003WO2003044431A1 Flow-type body and combustion device provided with a flow-type body of this type
05/30/2003WO2003025378A3 Device for mixing two flows of fluid, which are initially guided separate from one another, in a two-circuit reaction engine
05/28/2003EP1313937A1 High frequency excitation apparatus and method for reducing jet and cavity noise
05/27/2003US6568172 Converging nozzle thrust reverser
05/27/2003US6568171 Rocket vehicle thrust augmentation within divergent section of nozzle
05/21/2003CN1419044A Stopper type jet pipe
05/20/2003US6564541 Method for controlling the deployment of jet engine thrust reversers
05/20/2003CA2126313C Thrust reverser integrating a variable exhaust area nozzle
05/15/2003US20030089824 Acoustic treated thrust reverser bullnose fairing assembly
05/14/2003EP1310658A2 Acoustic treated thrust reverser bullnose fairing assembly
05/08/2003WO2003037715A1 Passive cooling system for auxiliary power unit installation
05/08/2003CA2766010A1 Passive cooling system for auxiliary power unit installation
05/08/2003CA2703166A1 Passive cooling system for auxiliary power unit installation
05/08/2003CA2703108A1 Passive cooling system for auxiliary power unit installation
05/06/2003US6557799 Acoustic treated thrust reverser bullnose fairing assembly
05/06/2003US6557338 Two plates and a plurality of flow directing vanes
05/01/2003WO2003036063A2 Confluent variable exhaust nozzle
05/01/2003US20030080244 Passive cooling system for auxiliary power unit installation
04/2003
04/29/2003US6554224 Out-of-plane thrust reverser sleeve lock
04/24/2003WO2003033899A1 Apparatus and method for thrust vector control
04/24/2003WO2003033898A1 Jet engine thrust reverser system having torque limited synchronization
04/24/2003US20030074884 Gas turbine engine fuel control system and method
04/24/2003CA2463817A1 Jet engine thrust reverser system having torque limited synchronization
04/23/2003EP1304472A1 Gas turbine engine two dimensional exhaust nozzle mechanism with reverse exhaust capability
04/23/2003EP1141534A4 Exhaust mixer and apparatus using same
04/23/2003EP0932755B1 An axisymmetric vectoring nozzle actuating system having multiple power control circuits
04/17/2003US20030070418 Variable cycle boost propulsor
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