| 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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| 05/29/2001 | US6237325 Bypass turbojet-engine cowling comprising an electrically grounded displaceable component |
| 05/22/2001 | US6233920 Contoured thrust reverser and lobed nozzle noise suppressor for gas turbine engines |
| 05/16/2001 | EP1099050A1 Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
| 05/15/2001 | US6231991 Ceramic on superalloy turbine |
| 05/10/2001 | DE19952797A1 Flow mixer for the flows in a turbofan jet aircraft engine has a flower petal shape with structured alternating radial trough channels for an increased mixing action without loss of pressure |
| 05/02/2001 | CN2428402Y Universal vector spraying tube |
| 05/01/2001 | CA1341218C Radiation suppression |
| 04/25/2001 | EP0739291B1 Engine exhaust gas deflection system |
| 04/19/2001 | DE19949241A1 Device for reducing sound conducted through air and solids caused by turbosuperchargers in internal combustion engines comprises tubes sliding into an outer jacket with a center flange to form a chamber |
| 04/18/2001 | EP1092859A1 Thrust reverser for a turbojet-engine |
| 04/17/2001 | US6216980 System for closing a pivoting thrust reverser door |
| 04/10/2001 | US6212877 Vectoring ring support and actuation mechanism for axisymmetric vectoring nozzle with a universal joint |
| 04/03/2001 | US6210773 Non-metallic thermally conductive honeycomb thrust reverser inner wall |
| 04/03/2001 | US6209679 Aircraft engine acoustic liner and method of making same |
| 03/27/2001 | US6206136 Acoustic liner and method of making an acoustic liner |
| 03/27/2001 | CA2072118C Dual flow turbine engine muffler |
| 03/22/2001 | WO2001019674A2 Swing pivot thrust reverser |
| 03/20/2001 | US6202405 Wall construction for a combustion chamber or a nozzle of a high performance propulsion plant |
| 03/15/2001 | WO2001018376A2 Thrust vectoring mechanism |
| 03/14/2001 | CN1287592A Heat exchanger in composite material and method for making same |
| 03/13/2001 | US6200660 Device and method for thermal protection of a surface against a thermally and mechanically aggressive environment |
| 03/13/2001 | US6199772 Linear actuation and vectoring ring support mechanism for axisymmetric vectoring nozzle |
| 03/13/2001 | US6199371 Thermally compliant liner |
| 03/13/2001 | CA2010934C Sustained release bolus effective for the prolonged prevention, treatment or control of nematode, acarid and endo- and ectoparasitic infestations of ruminants |
| 03/06/2001 | US6195981 Vectoring nozzle control system |
| 02/28/2001 | EP1079093A2 Support mechanism and linear actuator for a unison ring of a vectoriable axisymmetric nozzle |
| 02/28/2001 | EP1077871A1 Ir suppressor |
| 02/27/2001 | US6192671 Cross bar centering mechanism for slave petals in covergent divergent nozzles with variable geometry |
| 02/21/2001 | EP1076765A1 Bloom mixer for a turbofan engine |
| 02/13/2001 | US6185926 Turbojet engine thrust reverser and exhaust nozzle assembly |
| 02/06/2001 | US6182442 Combustion chamber wall construction for high power engines and thrust nozzles |
| 02/06/2001 | US6182440 Infrared radiation coanda suppressor |
| 01/31/2001 | EP1071609A1 Jet engine exhaust nozzle |
| 01/30/2001 | US6179225 Turbo jet engine exhaust nozzle with masked gas jet |
| 01/30/2001 | US6178742 Rear mixer ejector for a turbomachine |
| 01/30/2001 | US6178740 Turbo fan engine nacelle exhaust system with concave primary nozzle plug |
| 01/24/2001 | EP1071072A2 Acoustic liner and method of making an acoustic liner |
| 01/23/2001 | US6177200 Thermal barrier coating systems and materials |
| 01/23/2001 | US6176894 High velocity gas streams |
| 01/18/2001 | WO2001004485A1 Engine nozzle arrangement for an aircraft |
| 01/18/2001 | WO2001004484A1 Convergent-divergent axisymmetric turbojet exhaust nozzle |
| 01/17/2001 | EP1069302A1 Axisymmetric convergent divergent vectoring nozzle |
| 01/17/2001 | EP1068438A1 System for activating an adjustable tube by means of an elastic ring for a thrust nozzle |
| 01/17/2001 | EP1068437A1 System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies |
| 01/12/2001 | CA2314169A1 Axisymmetric, convergent-divergent jet deviation turbojet vectoring nozzle |
| 01/09/2001 | US6170257 Variable thrust nozzle system |
| 01/09/2001 | US6170256 Anchor device for a member for actuating a steerable nozzle |
| 01/09/2001 | US6170255 Turbojet thrust reverser with downstream obstacles |
| 01/09/2001 | US6170254 Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft |
| 01/09/2001 | US6170253 Cascade structure arrangement for a gas turbine engine |
| 01/02/2001 | US6167694 Actuator |
| 01/02/2001 | CA2022439C Turbojet engine thrust reverser with flaps related to an upstream panel |
| 12/26/2000 | US6164563 Converging exhaust nozzle fitted with translating cold flaps |
| 12/26/2000 | US6164059 Multi-expansion ejector nozzle with diverging walls |
| 12/21/2000 | WO2000077380A1 Apparatus and methods for active flow control of a nozzle exhaust plume |
| 12/21/2000 | WO2000050759A3 Thrust vectoring techniques |
| 12/20/2000 | CN1277657A Vectoring nozzle control system |
| 12/20/2000 | CN1277656A Vectoring nozzle calibration |
| 12/19/2000 | US6161839 Valve seal assembly |
| 12/19/2000 | US6161646 Turbo-generator exhaust noise silencer |
| 12/14/2000 | WO2000074831A1 Method and device for mixing gases |
| 12/12/2000 | US6160892 Active muffler |
| 12/12/2000 | US6158211 Turbojet-engine thrust reverser with scoop-doors of adjustable exhaust cross-section |
| 11/28/2000 | US6151886 Turbo jet-engine thrust reverser with scoop doors linked to a displaceable external cowling panel |
| 11/28/2000 | US6151885 Turbojet-engine thrust reverser with internal clamshells |
| 11/28/2000 | US6151884 Turbojet engine thrust reverser door spoilers with motion controlling drive system |
| 11/28/2000 | US6151883 Aircraft propulsive power unit thrust reverser with separation delay means |
| 11/28/2000 | CA2019802C An acoustic liner |
| 11/21/2000 | US6148608 Divergent petal arrangement for a convergent-divergent aircraft engine nozzle |
| 11/21/2000 | US6148607 Thrust reverser with lock-status display |
| 11/16/2000 | DE4041026A1 Gekühlte dünne Verkleidung aus Metall Chilled thin cladding metal |
| 11/15/2000 | EP1052472A2 Constant pressure mechanism of probe |
| 11/15/2000 | EP1052428A2 Screw actuator |
| 11/15/2000 | EP1052427A2 Actuator |
| 11/15/2000 | EP1052395A1 Exit area control mechanism for convergent divergent nozzles |
| 11/15/2000 | CN1273357A Constant pressure mechanism of contact |
| 11/14/2000 | US6145786 Latching mechanism for a jet engine thrust reverser door |
| 11/14/2000 | US6145301 Thrust reverser for fan type turbojet engines using independently actuated pivoted thrust deflectors |
| 11/08/2000 | EP1050678A2 Exhaust vane |
| 11/07/2000 | US6142416 Hydraulic failsafe system and method for an axisymmetric vectoring nozzle |
| 10/31/2000 | US6138449 Lock for a thrust reverser mechanism and a thrust reverser mechanism |
| 10/25/2000 | EP1046806A1 Vectoriable gimbal nozzle |
| 10/25/2000 | EP1045971A1 Heat exchanger in composite material and method for making same |
| 10/24/2000 | US6135238 Extended reaction acoustic liner for jet engines and the like |
| 10/24/2000 | US6134879 Suppression system for a gas turbine engine |
| 10/24/2000 | CA2034381C Exhaust nozzle flap seal |
| 10/18/2000 | EP1045130A1 Axisymmetric vectoriable convergent - divergent nozzle actuated by a unison ring |
| 10/18/2000 | EP1045129A1 Axisymmetric vectoriable convergent - divergent nozzle |
| 10/15/2000 | CA2305024A1 Aximetric converging-diverging vectoring nozzle with guide ring steering |
| 10/15/2000 | CA2305023A1 Steerable aximetric converging-diverging vectoring nozzle |
| 10/11/2000 | EP1043492A2 Lock for a thrust reverser |
| 10/11/2000 | EP1042602A1 Vectoring nozzle control system |
| 10/04/2000 | EP1040736A1 Synthetic jet actuators for cooling heated bodies and environments |
| 10/04/2000 | EP1040265A1 Vectoring nozzle calibration |
| 10/03/2000 | CA2022448C Suringing plate register inverter for turbojet engine |
| 09/26/2000 | US6123290 Helicopters equipped with jet dilution/deflection means for the combustion gases |
| 09/26/2000 | US6123145 Synthetic jet actuators for cooling heated bodies and environments |
| 09/26/2000 | US6122907 IR suppressor |
| 09/26/2000 | US6122892 Ventilated honeycomb cell sandwich panel and ventilation process for such a panel |
| 09/14/2000 | WO2000053915A1 Bloom mixer for a turbofan engine |