| 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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| 09/13/2000 | EP1035317A2 Apparatus for the Suppression of Infra Red Emissions from an Engine |
| 09/13/2000 | EP1035316A1 Vectoriable jet nozzle |
| 09/12/2000 | US6117560 A ceramic surface coatings has a cubic pyrochlore structure |
| 09/10/2000 | CA2299670A1 Ejection nozzle for an axisymmetrical, multi-direction turbojet |
| 09/07/2000 | DE19909793A1 Mixer for twin-circuit jet engine, with intermediate channels coming out in pre-mixing plane before main mixing plane |
| 09/07/2000 | DE19909792A1 Mixer for twin circuit jet engine, with outward radial channels offset alternately from each other in flow direction |
| 09/05/2000 | US6112513 Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow |
| 09/05/2000 | US6112512 Method and apparatus of pulsed injection for improved nozzle flow control |
| 08/31/2000 | WO2000050759A2 Thrust vectoring techniques |
| 08/30/2000 | EP1031724A2 Plug for a rocket combustion chamber |
| 08/30/2000 | EP1031510A2 Turbo fan engine nacelle exhaust system with concave primary nozzle plug |
| 08/29/2000 | US6109663 Joint seal for a gas turbine engine exhaust duct |
| 08/29/2000 | US6109562 Aircraft construction |
| 08/29/2000 | US6109021 Vectoring nozzle calibration |
| 08/22/2000 | US6105901 Thrust vectoring system |
| 08/17/2000 | WO2000047918A1 Flex seal for gas turbine expansion joints |
| 08/15/2000 | US6102610 Brittle composite structure for resiliently accomodating thermal expansion |
| 08/15/2000 | US6102329 Flow diverter system for multiple streams for gas turbine engine |
| 08/15/2000 | US6102307 Load strut for a variable geometry nozzle |
| 08/15/2000 | US6101807 Gas flow guide for an aircraft thrust reverser |
| 08/09/2000 | EP1026388A1 Rear ejection block with thrust reverser for a jet engine |
| 08/09/2000 | EP1026387A2 Contoured thrust reverser blocker doors matching lobed noise suppressor nozzle |
| 08/08/2000 | US6098402 Infra-red stealth masking device (IRSMD) |
| 08/08/2000 | US6098401 Afterburner flame holder with rotationally-splitting radial arms |
| 08/08/2000 | US6098400 Divergent petal for gas turbine engine nozzle |
| 08/03/2000 | WO2000045398A2 Injector mixer |
| 08/03/2000 | WO2000045040A1 System for activating an adjustable tube by means of an elastic ring for a thrust nozzle |
| 08/03/2000 | WO2000045039A1 System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies |
| 08/01/2000 | US6094908 Synchronizing control system for aircraft jet engine thrust reversers |
| 08/01/2000 | US6094907 Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness |
| 07/20/2000 | WO2000042308A1 Turbofan jet nozzle with integrated reversal |
| 07/19/2000 | EP1020631A1 Ejection nozzle for turbojet with integrated thrust reverser |
| 07/13/2000 | WO2000040851A1 Exhaust mixer and apparatus using same |
| 07/04/2000 | US6082635 Undulated nozzle for enhanced exit area mixing |
| 07/04/2000 | US6082096 Turbo-jet engine thrust-reverser fitted with scoop-doors linked to a movable cascade |
| 06/28/2000 | EP1013412A1 Integrally woven ceramic composites |
| 06/27/2000 | US6079201 Self-closing pivoting door thrust reverser |
| 06/21/2000 | EP1010884A1 Turbomachine multi-annular exhaust duct with acoustic lining |
| 06/21/2000 | EP1010618A2 Integrated muffler and exhaust cone for aircraft tailcone |
| 06/20/2000 | US6076347 Turbojet engine thrust reverser having scoop doors and movable upstream visors |
| 06/14/2000 | EP1007835A1 Backblast gas structure equipped with thrust reverser with two rear doors and planar exhaust area |
| 06/08/2000 | DE19855708A1 Acoustic tubular damper has outer casing, inner pipe with transverse lot and rectangular cavity, knitted fabric damping and volume cavities |
| 06/06/2000 | US6070830 Faceted exhaust nozzle |
| 06/02/2000 | WO2000031401A1 Thrust reverser with turning vanes capable of being superposed |
| 05/31/2000 | EP1004798A1 Actuator |
| 05/31/2000 | EP1004766A1 Thrust reverser with telescopic cascades |
| 05/30/2000 | US6068213 Aircraft engine ducted fan cowling with thrust reverser section and fairings for fan shroud brace members in fan exhaust duct |
| 05/30/2000 | US6067793 Variable geometry axisymmetric nozzle with 2-d thrust vectoring intended for a gas turbine engine |
| 05/24/2000 | CN1253878A Thermal resistance coating system and its material |
| 05/23/2000 | US6065756 Flex seal for gas turbine expansion joints |
| 05/23/2000 | US6065285 Thrust reverser for turbojet engine having scoop-forming doors cooperating with movable flow deflecting baffles |
| 05/23/2000 | CA2132255C Axisymmetric nozzles of variable geometry and orientation of the flow which are intended for gas turbine engines |
| 05/23/2000 | CA2089981C Thrust vectoring variable geometry exhaust nozzle for gas turbines |
| 05/18/2000 | WO2000028202A1 Heat exchanger in composite material and method for making same |
| 05/16/2000 | CA2077232C Variable section exhaust nozzle |
| 05/10/2000 | EP0999358A2 Gas turbine engine jet noise suppressor |
| 05/10/2000 | EP0998628A1 Turning vane arrangement for ir suppressors |
| 05/09/2000 | US6058846 Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section |
| 05/09/2000 | US6058696 Inlet and outlet module for a heat exchanger for a flowpath for working medium gases |
| 05/03/2000 | EP0997630A2 Deployment inhibiting arrangement for a thrust reverser system |
| 05/02/2000 | US6056204 Synthetic jet actuators for mixing applications |
| 05/02/2000 | US6055804 Turning vane arrangement for IR suppressors |
| 04/19/2000 | EP0994304A2 Thermally compliant liner |
| 04/19/2000 | EP0868596A4 Sound suppressor exhaust structure |
| 04/18/2000 | US6051302 Thermally conductive nonmetallic carbon pitch fiber honeycomb core sandwiched between a top and bottom layer. the core is adhered by a reticulated layer of adhesive to a perforated carbon fiber top layer |
| 04/18/2000 | US6050522 Thrust reverser for a high bypass turbofan engine |
| 04/12/2000 | EP0992603A1 Thermal barrier coating systems and materials |
| 04/12/2000 | EP0991861A1 Exhaust nozzle for suppressing infrared radiation |
| 04/12/2000 | EP0991860A1 Multi-stage mixer/ejector for suppressing infrared radiation |
| 04/04/2000 | US6045091 Thrust reverser with improved impact strength |
| 04/04/2000 | US6044641 Locking system for an aircraft jet engine thrust reverser door including a plurality of locking devices arranged to prevent deformation of the thrust reverser door |
| 03/29/2000 | EP0988446A1 Device for anchoring a member activating an adjustable nozzle |
| 03/28/2000 | US6042053 Automatic restow system for aircraft thrust reverser |
| 03/28/2000 | US6041590 Jet pipe liner |
| 03/22/2000 | EP0799376B1 Compact thrust reverser |
| 03/21/2000 | US6039287 Detachable integral aircraft tailcone and power assembly |
| 03/14/2000 | US6036142 Vectorable nozzle for aircraft |
| 03/08/2000 | EP0984152A2 Tabbed nozzle for jet noise suppression |
| 03/08/2000 | EP0984151A2 Guiding mechanism for variable geometry vectoring nozzles |
| 03/08/2000 | EP0984150A2 Vectoring ring support and actuation mechanism for axisymmetric vectoring nozzle |
| 03/08/2000 | EP0983939A1 Turbofan nacelle with grounded mobile part |
| 03/07/2000 | US6032901 Linkage system for an aircraft turbojet engine |
| 02/29/2000 | US6029439 Gas flow guide for an aircraft thrust reverser |
| 02/24/2000 | DE19919549A1 Thrust and propulsion production and producer works off subsonic subcritical fluid input for acceleration and heat input for ensuing deceleration and temperature increase for thrust output |
| 02/23/2000 | EP0958452A4 Ramjet engine for power generation |
| 02/22/2000 | US6027071 Thrust reverser with throat trimming capability |
| 02/22/2000 | US6026638 Thrust reverser door with isolated outer panel |
| 02/17/2000 | DE19937812A1 Composite heat exchanger, which uses materials that enable it to operate at high elevated temperatures, such as for in a nuclear fusion reactor |
| 02/09/2000 | EP0791141B1 Self-locking sealing device |
| 02/08/2000 | US6021637 Integrated fluidic CD nozzle for gas turbine engine |
| 02/08/2000 | US6021636 Lightweight tertiary thrust reverser lock assembly with a blocking member |
| 02/03/2000 | WO2000005497A1 Vectoring nozzle calibration |
| 02/03/2000 | WO2000005496A1 Vectoring nozzle control system |
| 02/03/2000 | WO2000005494A1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
| 02/03/2000 | CA2338232A1 Apparatus and method for active reduction of the noise emission from je t engines and for their diagnosis |
| 02/01/2000 | CA2122536C Orientable axisymmetric nozzle of variable geometry for gas turbine propulsors |
| 02/01/2000 | CA2082780C Two-shaft turbofan inverter |
| 01/25/2000 | US6016996 Airborne apparatus for ground erosion reduction |
| 01/25/2000 | US6016651 Multi-stage mixer/ejector for suppressing infrared radiation |
| 01/25/2000 | CA2013932C Axisymmetric vectoring exhaust nozzle |