| 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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| 03/07/2002 | DE10033653A1 Drive system for e.g. aircraft, is formed multistage with drives units such that the drive system is combined with at least one negative pressure system |
| 03/06/2002 | CN1080375C Axisymmetric vectoring nozzle actuating system having multiple power control circuits |
| 03/05/2002 | US6352790 Substrate containing silicon and a barrier layer which functions as a protective/thermal barrier coating |
| 03/05/2002 | US6352211 Flow blocking exhaust nozzle |
| 03/05/2002 | US6351941 Methods and apparatus for reducing thermal stresses in an augmentor |
| 02/27/2002 | CN1079902C Lock for nozzle control in event of hydraulic failure |
| 02/26/2002 | US6349539 Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzle |
| 02/21/2002 | US20020020167 Variable mode jet engin - suitable for STOVL |
| 02/19/2002 | US6347510 Axi-nozzle ejector seal |
| 02/13/2002 | EP1179131A1 An apparatus for controlling the flow separation line of rocket nozzles |
| 02/05/2002 | US6343769 Deployment inhibiting arrangement for a thrust reverser system |
| 01/30/2002 | EP1176302A1 Thrust reverser for a jet engine |
| 01/30/2002 | EP1176127A2 Fiber reinforced composite article, fiber containing member, and method for making |
| 01/30/2002 | CN1078664C Double door thurst reverser assembly |
| 01/24/2002 | WO2001071056A3 Nickel vapour deposition manufacture of aircraft engine parts |
| 01/24/2002 | US20020010097 Photocatalytic nuisance organism inhibitor agents |
| 01/24/2002 | US20020007625 Cascade-type reversers for jet engines |
| 01/23/2002 | EP1174341A1 Aircraft jet engine nacelle with an enhanced rear ejection block with common nozzle |
| 01/17/2002 | US20020006333 Aeroengine nacelle afterbodies |
| 01/08/2002 | US6336319 Fluidic nozzle control system |
| 01/02/2002 | EP1167322A1 Article comprising a substrate containing silicon and a barrier layer which functions as a protective/thermal barrier coating |
| 01/02/2002 | EP0786131B1 Jet engine fan noise reduction system utilizing electro pneumatic transducers |
| 01/02/2002 | CN1077217C Thrust reverster synchronization shaft lock mechanism |
| 01/01/2002 | US6334299 Ramjet engine for power generation |
| 12/20/2001 | WO2001018376A3 Thrust vectoring mechanism |
| 12/18/2001 | CA2016346C Fringed thermal protection device and method of manufacturing it |
| 12/13/2001 | WO2001094197A1 Propulsion system |
| 12/11/2001 | US6327846 Universal-joint vectoring system for a turbojet-engine exhaust nozzle |
| 12/05/2001 | EP1160439A1 Mixing device for jet engines |
| 12/05/2001 | EP0870104B1 Lock for nozzle control in the event of hydraulic failure |
| 12/05/2001 | EP0852669B1 Convertible ejector cooled nozzle |
| 11/28/2001 | EP1158156A2 Fluidic nozzle control system |
| 11/20/2001 | US6318668 Thrust vectoring techniques |
| 11/20/2001 | US6318072 Apparatus for reducing noise produced by supersonic jet |
| 11/20/2001 | US6318070 Variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 11/13/2001 | US6314721 Tabbed nozzle for jet noise suppression |
| 11/06/2001 | US6311928 Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor |
| 11/06/2001 | US6311478 Guiding mechanism for variable geometry vectoring nozzles |
| 11/01/2001 | US20010035004 Segmented mixing device for jet engines |
| 10/30/2001 | US6308915 Detachable integral aircraft tailcone and power assembly |
| 10/30/2001 | US6308914 Apparatus for the suppression of infra red emissions from an engine |
| 10/30/2001 | US6308898 Apparatus and methods for active flow control of a nozzle exhaust plume |
| 10/18/2001 | DE10017040A1 Device for thrust increase of turbojets with regeneration has convergent-divergent nozzle which accelerates bypass flow to supersonic speed |
| 10/17/2001 | EP0991860B1 Multi-stage mixer/ejector for suppressing infrared radiation |
| 10/16/2001 | US6301877 Ejector extension cooling for exhaust nozzle |
| 10/11/2001 | WO2001019674A3 Swing pivot thrust reverser |
| 10/10/2001 | EP1141534A1 Exhaust mixer and apparatus using same |
| 10/09/2001 | US6299077 Actuation system for convergent/divergent nozzle |
| 10/09/2001 | US6298658 Multi-stable thrust vectoring nozzle |
| 10/09/2001 | US6298653 Ramjet engine for power generation |
| 10/02/2001 | US6295805 Exhaust induced ejector nozzle system and method |
| 09/27/2001 | WO2001071056A2 Nickel vapour deposition manufacture of aircraft engine parts |
| 09/27/2001 | US20010023582 Apparatus and method for active reduction of the noise emission from jet engines and for jet engine diagnosis |
| 09/26/2001 | EP1136687A2 Methods and apparatus for minimizing thermal stresses in a centerbody |
| 09/25/2001 | US6293495 Pivoting door thrust reverser system for turbofan aircraft jet engine |
| 09/25/2001 | US6293489 Lock for a trust reverser |
| 09/25/2001 | US6293091 Axisymmetrical annular plug propulsion system for integrated rocket/ramjet or rocket/scramjet |
| 09/20/2001 | WO2001069069A1 An apparatus for controlling the flow separation line of rocket nozzles |
| 09/18/2001 | US6292763 Methods for designing variable cycle gas turbine engines |
| 09/18/2001 | US6289671 Plug for a liquid-propellant rocket engine chamber |
| 09/18/2001 | US6289670 Turbojet engine thrust reverser and exhaust nozzle |
| 09/18/2001 | US6289669 Lateral-thrust control arrangement for missiles with solid-fuel hot-gas generator |
| 09/12/2001 | EP1132687A1 Methods and apparatus for reducing thermal stresses in an augmentor |
| 09/11/2001 | US6286784 Automatic restow system for aircraft thrust reverser |
| 09/05/2001 | EP1130243A2 A variable area nozzle for gas turbine engines driven by shape memory alloy actuators |
| 09/05/2001 | EP0828934B1 Double door thrust reverser assembly |
| 09/04/2001 | US6284323 Thermal barrier coating systems and materials |
| 08/30/2001 | US20010017232 Aircraft engine acoustic liner and method of making the same |
| 08/29/2001 | EP1128052A1 Thrust reverser with bladed cascades and fixed rear structure |
| 08/29/2001 | CN1310785A Device and method for actively reducing the noise emissions of jet engines and for diagnosing the same |
| 08/21/2001 | US6276127 Noise suppressing mixer for jet engines |
| 08/21/2001 | US6276126 Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle |
| 08/09/2001 | WO2001057382A2 Locking device for a thrust reverser |
| 08/07/2001 | US6270037 Rapid response attitude control logic for shaft-driven lift fan STOVL engine |
| 08/07/2001 | US6269627 Rapid thrust response control logic for shaft-driven lift fan STOVL engine |
| 08/02/2001 | US20010010148 Thrust reverser having a bypass vane-cascade and fitted with a stationary rear structure |
| 07/26/2001 | WO2001053729A1 Thermally stressable wall and method for sealing a gap in a thermally stressed wall |
| 07/26/2001 | US20010009642 Flow directing element and a method of manufacturing a flow directing element |
| 07/25/2001 | EP1118806A1 Thermally charged wall structure and method to seal gaps in such a structure |
| 07/25/2001 | EP1118763A2 A flow directing element and a method of manufacturing a flow directing element |
| 07/17/2001 | US6260801 Swing pivot thrust reverser |
| 07/17/2001 | US6260800 Aircraft power plant with two air intake fans |
| 07/17/2001 | US6260794 Dolphin cascade vane |
| 07/17/2001 | US6260352 Turbofan aircraft engine |
| 07/12/2001 | US20010007719 Mixed oxide overcoating metal or alloy; gas turbine engine |
| 07/12/2001 | DE19962617A1 Turbostrahltriebwerk Turbojet |
| 07/10/2001 | US6257366 Exhaust device for a turbine engine |
| 07/10/2001 | US6256980 Thrust reverser with turning vanes capable of being superposed |
| 07/10/2001 | US6256979 Backblast gas structure equipped with thrust reverser with two rear doors and planar exhaust area |
| 07/05/2001 | WO2001048365A1 Turbojet engine |
| 07/03/2001 | US6253540 Removable baffle infrared suppressor |
| 06/28/2001 | WO2001046580A1 An outlet device for a jet engine |
| 06/28/2001 | WO2000045398A9 Injector mixer |
| 06/12/2001 | US6244539 Detachable integral aircraft tailcone and power assembly |
| 06/12/2001 | CA2048727C Gas turbine engine multi-hole film cooled combustor liner |
| 06/07/2001 | US20010002537 Nozzle |
| 06/06/2001 | EP1104847A2 Inclined jet nozzle |
| 06/05/2001 | US6240720 Hybrid-composite gas turbine exhaust nozzle compression link |
| 06/01/2001 | CA2327166A1 Improved nozzle |
| 05/31/2001 | WO2000045398A3 Injector mixer |