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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10/09/2002 | CN1092289C Ramjet engine for power generation |
10/03/2002 | WO2002050415A3 Aero-engine exhaust jet noise reduction assembly |
10/03/2002 | US20020139120 Tortuous path quiet exhaust eductor system |
10/03/2002 | US20020139108 Exhaust thrust booster for a thrust generator |
10/02/2002 | EP0938624B1 Turbofan aircraft engine |
10/02/2002 | CN1091842C Convertible ejector cooled nozzle |
10/01/2002 | US6457654 Micromachined synthetic jet actuators and applications thereof |
09/26/2002 | US20020134070 Method of increasing engine temperature limit margins |
09/26/2002 | DE10109274A1 Vorrichtung zur Verminderung der IR-Zielsignatur von Luftfahrzeugen Apparatus for reducing IR target signature of aircraft |
09/24/2002 | US6455467 Photocatalytic nuisance organism inhibitor agents |
09/18/2002 | EP1240421A1 Turbojet engine |
09/18/2002 | EP1240420A1 An outlet device for a jet engine |
09/12/2002 | US20020125370 System driving the displaceable fairing of a turbojet-engine thrust reverser |
09/12/2002 | US20020125340 Gas turbine engine exhaust nozzle |
09/12/2002 | US20020124550 Thrust reverser |
09/12/2002 | DE10126632A1 Combination propulsion system pref. for aircraft has thrust vector control, also useable as lifting device, located behind multistage vacuum system or ram jet engines |
09/11/2002 | EP1239139A1 Thrust reverser actuating system in a turbojet engine |
09/05/2002 | US20020121090 Gas turbine engine jet noise suppressor |
09/05/2002 | DE10106772A1 Combustion chamber used for a rocket propulsion system is made from a composite ceramic |
09/04/2002 | EP1236881A1 Lock mechanism |
09/03/2002 | CA2065650C Support for a translating nozzle vectoring ring |
08/28/2002 | EP1234764A2 Aircraft infrared suppressor |
08/27/2002 | US6440521 Method for transferring heat in an aircraft engine thrust reverser |
08/27/2002 | US6439840 Bypass duct fan noise reduction assembly |
08/27/2002 | US6439504 System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system |
08/27/2002 | US6438942 Cascade-type reversers for jet engines |
08/27/2002 | CA2296833C Turbo fan engine nacelle exhaust system with concave primary nozzle plug |
08/27/2002 | CA2061938C Nozzle load management |
08/20/2002 | US6434927 Thrust reverser |
08/20/2002 | US6434924 Ramjet engine for power generation |
08/20/2002 | US6434851 Constant pressure mechanism of probe |
08/14/2002 | CN1364217A Apparatus for controlling flow separation line of rocket nozzles |
08/08/2002 | US20020104707 Acoustic muffler for turbine engine |
08/07/2002 | EP1229237A2 Cascade-type thrust reverser |
08/01/2002 | US20020100837 Aircraft propulsive power unit |
07/31/2002 | EP1007835B1 Backblast gas structure equipped with thrust reverser with two rear doors and planar exhaust area |
07/25/2002 | US20020096393 Turbogenerator exhaust silencer |
07/18/2002 | WO2002055864A1 Rocket engine member and a method for manufacturing a rocket engine member |
07/18/2002 | WO2002055863A1 Rocket engine member and a method for manufacturing a rocket engine member |
07/18/2002 | WO2002055862A1 Rocket engine member and method for manufacturing a rocket engine member |
07/18/2002 | WO2002055861A1 Method for manufacturing outlet nozzles for rocket engines |
07/18/2002 | WO2002055860A1 An outlet nozzle and a method for manufacturing an outlet nozzle |
07/18/2002 | US20020092948 Apparatus and method for reducing jet engine noise |
07/17/2002 | EP1222380A2 Swing pivot thrust reverser |
07/16/2002 | US6418973 Integrally woven ceramic composites |
07/09/2002 | US6415599 Engine interface for axisymmetric vectoring nozzle |
07/09/2002 | US6415598 Exhaust nozzle for by-pass gas turbine engines |
07/03/2002 | EP0865570B1 Noise suppression system for a jet engine |
07/02/2002 | US6412283 Deep lobed deswirling diffuser tailpipe |
06/27/2002 | WO2002050415A2 Aero-engine exhaust jet noise reduction assembly |
06/27/2002 | US20020079404 Method and apparatus for planar actuation of a flared surface to control a vehicle |
06/20/2002 | US20020077732 6-degree-of-freedom control apparatus for spacecraft |
06/20/2002 | US20020073691 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
06/20/2002 | US20020073690 Aero-engine exhaust jet noise reduction assembly |
06/19/2002 | CN1354322A Jet rotary engine |
06/12/2002 | EP1213539A1 Gas turbine combustor, gas turbine, and jet engine |
06/11/2002 | US6402092 Turbojet-engine thrust reverser with doors mounted on centered pivots |
06/11/2002 | US6401557 Screw actuator |
06/06/2002 | WO2002044539A1 Bypass duct fan noise reduction assembly |
06/06/2002 | WO2002044105A1 Porous sound absorbing material and method of manufacturing the material |
06/06/2002 | US20020066272 Gas turbine combustor, gas turbine, and jet engine |
06/06/2002 | US20020066268 Mixing enhancement using axial flow |
06/05/2002 | EP1211406A1 Methods and apparatus for sealing gas turbine engine variable nozzles |
06/05/2002 | EP0998628B1 Turning vane arrangement for ir suppressors |
06/04/2002 | US6398129 Throat configuration for axisymmetric nozzle |
06/04/2002 | US6397581 Heat exchanger in composite material and method for making same |
05/30/2002 | US20020064455 Methods and apparatus for sealing gas turbine engine variable nozzles |
05/30/2002 | US20020064453 Bypass duct fan noise reduction assembly |
05/23/2002 | US20020061110 Actively-controlled sound absorption panel system using movement-controlled reflective plate |
05/14/2002 | US6385965 System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies |
05/14/2002 | US6385964 Thrust reverser having a bypass vane-cascade and fitted with a stationary rear structure |
05/10/2002 | WO2002036944A1 Turbogenerator exhaust silencer |
05/07/2002 | US6383445 Supersonic coherent gas jet for providing gas into a liquid |
05/07/2002 | US6382559 Thrust vectoring mechanism |
05/07/2002 | US6381950 Engine nozzle arrangement for an aircraft |
05/02/2002 | US20020050420 Noise reduction sandwich panel, notably for aircraft turbojet engine |
05/02/2002 | US20020050140 Device and process for economizing fuel supply in a fuel supply circuit |
05/02/2002 | EP1201420A1 Sound absorbing panel particularly for aircraft engine |
04/30/2002 | US6378781 Exit area control mechanism for convergent divergent nozzles |
04/30/2002 | US6378294 System for activating an adjustable tube by means of an elastic ring for a thrust nozzle |
04/30/2002 | CA2077815C Cooling air transfer apparatus for aircraft gas turbine engine exhaust nozzles |
04/24/2002 | EP0923488B1 Detachable integral aircraft tailcone and power assembly |
04/23/2002 | US6375118 High frequency excitation apparatus and method for reducing jet and cavity noise |
04/23/2002 | US6375095 Swiveling, converging-diverging, axisymmetric exhaust nozzle |
04/11/2002 | WO2002029232A1 Apparatus, method and system for gas turbine engine noise reduction |
04/10/2002 | EP1195512A2 Flow blocking exhaust nozzle |
04/04/2002 | WO2002027177A1 Jet engine with unsteady flow ejector |
04/03/2002 | EP1193682A1 Acoustic sandwich panel with no septum and apparatus and method for suppressing noise in a turbojet nozzle |
04/03/2002 | EP1192348A1 Engine nozzle arrangement for an aircraft |
03/28/2002 | US20020036241 Throat configuration for axisymmetric nozzle |
03/28/2002 | US20020036115 Noise attenuation panel |
03/27/2002 | EP1191214A2 Exhaust nozzle with stub airfoils |
03/26/2002 | US6360844 Aircraft engine acoustic liner and method of making the same |
03/26/2002 | US6360528 Chevron exhaust nozzle for a gas turbine engine |
03/26/2002 | US6360527 Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring |
03/21/2002 | WO2001057382A3 Locking device for a thrust reverser |
03/19/2002 | US6358590 Noise attenuation panel |
03/19/2002 | US6357672 Sealing means for a multi-axis nozzle |
03/13/2002 | EP1185779A1 Apparatus and methods for active flow control of a nozzle exhaust plume |
03/07/2002 | WO2002018771A1 High frequency excitation apparatus and method for reducing jet and cavity noise |