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