| 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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| 03/16/2006 | WO2006029058A1 Integrated axially varying engine muffler, and associated methods and systems |
| 03/16/2006 | WO2006028516A2 Thrust vector control system for a plug nozzle rocket engine |
| 03/16/2006 | US20060053769 Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle |
| 03/16/2006 | US20060053767 Method and device for reducing engine noise |
| 03/15/2006 | EP1633935A2 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/15/2006 | EP1390613A4 Jet engine nozzle with variable thrust vectoring and exhaust area |
| 03/14/2006 | US7010905 Ventilated confluent exhaust nozzle |
| 03/09/2006 | DE102004042518A1 Airplane`s e.g. military airplane, turbofan engine testing device, has deflecting device deflecting exhaust gas stream from thrust reverser and including deflecting and outlet areas, where inner boundary wall has curve in deflecting area |
| 03/07/2006 | US7007483 Turbine engine nozzle |
| 03/07/2006 | US7007454 Locking system on a cascade thrust reverser |
| 03/02/2006 | US20060042230 Vectorable nozzle with sideways pivotable ramp |
| 03/02/2006 | US20060042229 Thrust reverser system electro-mechanical brake manual release mechanism |
| 03/01/2006 | EP1630399A2 Vectorable nozzle with sideways pivotable ramp |
| 03/01/2006 | EP1629188A2 Rotary adjustable exhaust nozzle |
| 02/28/2006 | US7004047 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 02/23/2006 | US20060038064 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop |
| 02/23/2006 | US20060037812 Acoustic fluid machine |
| 02/21/2006 | US7000378 Gas turbine engine exhaust nozzle having a noise attenuation device driven by shape memory material actuators |
| 02/16/2006 | WO2006016017A1 Cooling device for the primary nozzle of a dual-flow turbojet engine |
| 02/16/2006 | WO2005040589A3 Nested latch thrust reverser |
| 02/16/2006 | CA2564508A1 Cooling device for the primary nozzle of a dual-flow turbojet engine |
| 02/14/2006 | US6996973 Method of achieving jet separation of an un-separated flow in a divergent nozzle body of a rocket engine |
| 02/14/2006 | CA2234437C Thrust reverser with unlock protection for aircraft turbine engine |
| 02/09/2006 | WO2006013243A1 Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 02/09/2006 | US20060027704 Internal duct VTOL aircraft propulsion system |
| 02/09/2006 | CA2572698A1 Aircraft jet engine provided with a device for reducing propulsion jet noise |
| 02/07/2006 | US6993914 Convergent-divergent turbojet nozzle |
| 02/02/2006 | WO2006010803A1 Method for opening a mobile cowl equipping a thrust reverser |
| 02/02/2006 | US20060024154 Zero acoustic splice fan case liner |
| 02/02/2006 | US20060021351 Method for resistance welding two sheet metal elements together |
| 02/01/2006 | EP1621815A1 Microcombustor |
| 02/01/2006 | EP1621752A2 Noise attenuation at a splice in a fan case liner |
| 02/01/2006 | EP1621751A1 Jet engine convergent nozzle |
| 02/01/2006 | EP1620643A2 Self-aligning thrust reverser system lock assembly |
| 02/01/2006 | CN1727698A Noise attenuation at a splice in a fan case liner |
| 01/31/2006 | CA2275099C Supersonic coherent gas jet for providing gas into a liquid |
| 01/31/2006 | CA2224621C Divergent petal for gas turbine engine nozzle |
| 01/27/2006 | CA2507082A1 Zero acoustic splice fan case liner |
| 01/26/2006 | US20060016171 Split shroud exhaust nozzle |
| 01/26/2006 | CA2796895A1 Turbine exhaust case and method of making |
| 01/25/2006 | EP1619489A1 Test equipment for the development of an aircraft gas turbine engine |
| 01/25/2006 | EP1619376A2 Split shroud exhaust nozzle |
| 01/24/2006 | US6988692 Rear fastening device for aircraft engine |
| 01/24/2006 | US6988674 Method and apparatus for suppressing infrared signatures |
| 01/24/2006 | CA2225794C A device and procedure for the thermal protection of a surface against a thermally and mechanically harsh environment |
| 01/19/2006 | US20060011411 Acoustic compressor |
| 01/19/2006 | US20060010853 Turbomachine nozzle cover for reducing jet noise |
| 01/19/2006 | US20060010852 Turbine exhaust case and method of making |
| 01/18/2006 | EP1617068A1 Turbomachine cowl having noise suppression tabs |
| 01/17/2006 | US6986940 Fiber reinforced composite article, fiber member, and method for making |
| 01/17/2006 | US6986246 Side thruster valve and side thruster device |
| 01/13/2006 | CA2511892A1 Cowling for turbine engine nozzle with jet noise reduction patterns |
| 01/12/2006 | US20060005545 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 01/12/2006 | US20060005530 Thrust reverser comprising optimised deflector gratings |
| 01/11/2006 | EP1613854A1 Thrust reverser system with sequential torque decoupler |
| 01/10/2006 | US6983602 Ejector cooled nozzle |
| 01/10/2006 | US6983588 Turbofan variable fan nozzle |
| 01/05/2006 | US20060000211 Shape memory material actuation |
| 01/04/2006 | EP1612769A2 High admittance acoustic liner |
| 01/04/2006 | EP1612416A1 Shape memory material actuator |
| 01/04/2006 | CN1234966C Jet rotary engine |
| 01/03/2006 | US6981365 Supersonic revolving nozzle |
| 01/03/2006 | CA2181857C Turbofan with thrust reversal doors not submitted to bypass air in their inactive position |
| 01/03/2006 | CA1341492C Tubular structure ramjet, and missile propelled by such ramjet |
| 12/29/2005 | US20050284690 High admittance acoustic liner |
| 12/29/2005 | CA2471887A1 Aero hoverjet mk-1 |
| 12/28/2005 | EP1609719A1 Method for braking aircraft and turbo fan jet engine for implementing the method |
| 12/22/2005 | US20050279081 Aircraft braking method and ducted fan jet engine for implementing the method |
| 12/21/2005 | EP1607611A2 Aircraft propulsion system comprising an apparatus for suppressing infrared signatures |
| 12/21/2005 | EP1607610A1 Two-dimensional vectorable single expansion ramp nozzle |
| 12/21/2005 | EP1607603A2 Gas turbine engine inlet with noise reduction features |
| 12/21/2005 | EP1606504A2 Toggle interlocked thrust reverser |
| 12/20/2005 | US6976361 Ventilation channels in an afterburner chamber confluence sheet |
| 12/20/2005 | US6976352 Toggle interlocked thrust reverser |
| 12/15/2005 | WO2004104377A3 Rotary adjustable exhaust nozzle |
| 12/15/2005 | US20050274114 Ventilation channels in an afterburner chamber confluence sheet |
| 12/15/2005 | US20050274103 Gas turbine engine inlet with noise reduction features |
| 12/14/2005 | EP1605152A1 Divergent flap for a gas turbine engine |
| 12/14/2005 | EP1286885A4 Propulsion system |
| 12/13/2005 | US6974107 Thrust reverser system actuator having an integral torque limiter |
| 12/08/2005 | WO2005039978A3 Aircraft protection method and system |
| 12/08/2005 | WO2004077400A8 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 12/08/2005 | US20050268595 Method and apparatus for suppressing infrared signatures |
| 12/08/2005 | DE102005022824A1 Elektronisch gesteuerter variabler Zweikammer-Resonator Electronically controlled variable two-chamber resonator |
| 12/06/2005 | US6971240 Methods and apparatus for exhausting gases from gas turbine engines |
| 12/06/2005 | US6971229 Confluent exhaust nozzle |
| 12/01/2005 | WO2005113970A2 Method of evaluation of space systems for safety assurance and residual risk to flight crew |
| 12/01/2005 | US20050263643 Cowl structure for a gas turbine engine |
| 12/01/2005 | US20050262826 Jet nozzle mixer |
| 11/29/2005 | US6969028 Scarf nozzle for a jet engine and method of using the same |
| 11/29/2005 | US6968694 Augmentor |
| 11/29/2005 | US6968675 Cascadeless fan thrust reverser with plume control |
| 11/24/2005 | WO2005110723A1 Method for production of elements such as thrust-reverser cascade vanes by moulding of a composite material |
| 11/24/2005 | US20050260034 Fastener assembly for attaching a non-metal component to a metal component |
| 11/24/2005 | US20050260033 Fastener assembly for attaching a non-metal component to a metal component |
| 11/24/2005 | US20050257529 Divergent flap for a gas turbine engine |
| 11/24/2005 | US20050257527 Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance |
| 11/24/2005 | DE102004004076B4 Turboflugtriebwerk mit internem Mischer Turbo aero engine with internal mixer |
| 11/24/2005 | DE10158295B4 Strömungskörper Flow body |
| 11/24/2005 | CA2564617A1 Method for production of elements such as thrust-reverser cascade vanes by moulding of a composite material |