| 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) |
|---|
| 08/10/2005 | EP1561939A2 Sinuous chevron exhaust nozzle |
| 08/09/2005 | US6926234 Electromechanical turbojet thrust reverser with continuous position control |
| 08/09/2005 | CA2384651C Swing pivot thrust reverser |
| 08/04/2005 | US20050166575 Gas turbine engine exhaust nozzle |
| 08/03/2005 | EP1559539A1 Integrally woven ceramic composites |
| 08/03/2005 | EP1558840A2 Bifold door thrust reverser |
| 08/02/2005 | US6924040 Ceramic containing hafnia, germanium oxide on metallic substrate |
| 07/28/2005 | WO2005068796A1 Exhaust gas temperature moderator |
| 07/28/2005 | US20050161527 Convergent/divergent nozzle with modulated cooling |
| 07/28/2005 | US20050160718 Square ultra thrust reverser system |
| 07/27/2005 | EP1557553A1 Monobloc arm for a postcombustion device of a double flow turboengine |
| 07/27/2005 | EP1557552A1 Gas turbine engine and method for assembling and operating such a gas turbine engine |
| 07/27/2005 | CN1644904A Methods and apparatus for operating gas turbine engines |
| 07/26/2005 | US6920958 Annular acoustic panel |
| 07/26/2005 | US6920750 Rocket engine member and a method for manufacturing a rocket engine member |
| 07/26/2005 | CA2223529C Thrust reverser for jet turbine engine with doors held within nacelle lines |
| 07/21/2005 | WO2005028303A3 Self stowing thrust reverser |
| 07/21/2005 | US20050155352 Multiple sectioned duct |
| 07/21/2005 | US20050155343 Methods and apparatus for operating gas turbine engines |
| 07/21/2005 | US20050155341 Axisymmetric flap on gas turbine exhaust centerbody |
| 07/20/2005 | EP1555406A1 Cooling system for hot elements of aircraft engines and aircraft engine equipped with such a cooling system. |
| 07/20/2005 | EP1555393A2 Gas turbine engine component having bypass circuit |
| 07/20/2005 | EP1554484A1 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism |
| 07/20/2005 | CA2492418A1 Methods and apparatus for operating gas turbine engines |
| 07/19/2005 | US6918244 Vertical takeoff and landing aircraft propulsion systems |
| 07/14/2005 | US20050151012 Spider actuated thrust reverser |
| 07/14/2005 | US20050150970 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/14/2005 | US20050150234 Gas turbine engine component having bypass circuit |
| 07/14/2005 | US20050150207 Fluidic diverter valve with a variable valve-bore clearance |
| 07/13/2005 | EP1553282A1 Device for feeding cooling air to flap nozzle |
| 07/13/2005 | EP1553281A1 A device for reducing jet engine exhaust noise using oscillating jets |
| 07/13/2005 | EP1552131A1 Electro-hydraulic thrust reverser lock actuation system |
| 07/13/2005 | CN1637262A Device for reducing jet engine exhaust noise using oscillating jets |
| 07/13/2005 | CN1637261A Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith |
| 07/13/2005 | CA2491935A1 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/12/2005 | US6915984 Apparatus and method for mounting a cascade support ring to a thrust reverser |
| 07/12/2005 | CA2222470C Device for linking a thrust reverser to a turbine engine |
| 07/07/2005 | WO2005028815A3 Device for the generation of mechanical or electrical energy using any thermal potential |
| 07/07/2005 | WO2004077400B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 07/07/2005 | US20050147790 Method for making a soundproofing panel with at least one double resonator |
| 07/07/2005 | US20050144935 Device for reducing jet engine exhaust noise using oscillating jets |
| 06/30/2005 | US20050138932 Aircraft protection method and system |
| 06/30/2005 | US20050138915 Turbomachine nozzle with noise reduction |
| 06/29/2005 | EP1548266A1 Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith |
| 06/28/2005 | US6911158 Ceramics with porosities of 75% to 85%; material retains strength while maintaining prescribed sound absorbing effect; efficiently absorbs noises over wide range of sound frequencies, such as from jet engines |
| 06/28/2005 | US6910328 Vectorable variable area nozzle |
| 06/23/2005 | US20050132714 Compact fastening collar and stud for connecting walls of a nozzle liner and method associated therewith |
| 06/23/2005 | US20050132709 Exhaust nozzle segmented basesheet and production method thereof |
| 06/22/2005 | EP1544448A2 Exhaust nozzle segmented basesheet and production method thereof |
| 06/16/2005 | US20050127135 Support structure |
| 06/16/2005 | US20050126174 Rotary adjustable exhaust nozzle |
| 06/15/2005 | EP1540164A2 Thrust vectoring and variable exhaust area for jet engine nozzle |
| 06/14/2005 | CA2180402C One clamshell-door type turbojet thrust reverser |
| 06/09/2005 | US20050120702 Two-axis thrust vectoring nozzle |
| 06/08/2005 | EP1538239A2 Sprayable noble metal coating for high temperature use on ceramic and smoothcoat coated aircraft engine parts |
| 06/08/2005 | CN1624307A Cooling system for high-temperature unit of aircraft engine and aircraft engine mounted with the system |
| 06/07/2005 | US6902692 Process for making a fiber reinforced article |
| 06/02/2005 | WO2005049997A1 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 06/02/2005 | US20050116096 Aircraft provided with thrust reversers |
| 06/02/2005 | US20050116061 Method and apparatus for arresting a crack within a body |
| 06/02/2005 | US20050115245 Device for reducing the jet noise of a turbomachine |
| 06/01/2005 | EP1536126A1 Support structure adapted for thermal expansion |
| 06/01/2005 | EP1534590A1 Ducted air power plant |
| 06/01/2005 | EP1430212A4 Converging nozzle thrust reverser |
| 05/26/2005 | WO2004099602A3 Self-aligning thrust reverser system lock assembly |
| 05/26/2005 | US20050109557 Soundproofing panel with beads, and a method of manufacture |
| 05/25/2005 | EP1533787A1 Sound insulation panel containing balls and method for producing it |
| 05/24/2005 | US6896100 Noise reducing apparatus and exhaust nozzle for jet engine |
| 05/24/2005 | US6895742 Bifold door thrust reverser |
| 05/19/2005 | US20050102996 Nested latch thrust reverser |
| 05/19/2005 | US20050102994 Provision of sealing for the cabin-air bleed cavity of a jet engine using a brush seal |
| 05/17/2005 | US6892526 Cowl structure for a gas turbine engine |
| 05/12/2005 | US20050097899 Provision of sealing in a jet engine for bleeding air to the cabin using a tube with a double ball joint |
| 05/12/2005 | US20050097893 Method and apparatus for increasing a durability of a body |
| 05/12/2005 | US20050097892 Method and apparatus for arresting a crack within a body |
| 05/12/2005 | US20050097883 Ablative baffle for a liquid rocket engine thrust chamber |
| 05/11/2005 | EP1529950A1 Method and apparatus for arresting a crack within an exhaust nozzle flap seal body |
| 05/11/2005 | EP1529949A1 Method and apparatus for increasing a durability of an exhaust nozzle flap seal |
| 05/11/2005 | EP1529925A2 Method and apparatus for arresting a crack within a ceramic matrix composite body |
| 05/11/2005 | EP1529163A1 Swivelling nozzle for a rocket engine |
| 05/11/2005 | EP1240420B1 An outlet device for a jet engine |
| 05/07/2005 | CA2486014A1 Method and apparatus for increasing a durability of a body |
| 05/06/2005 | WO2005040589A2 Nested latch thrust reverser |
| 05/06/2005 | WO2005039978A2 Aircraft protection method and system |
| 05/06/2005 | CA2536693A1 Nested latch thrust reverser |
| 05/05/2005 | US20050095123 Turboshaft engine comprising two elements connected to each other with the interposition of a seal |
| 05/05/2005 | US20050091983 Methods and apparatus to reduce turbine engine nozzle basesheet stresses |
| 05/05/2005 | US20050091982 Methods and apparatus for flade engine nozzle |
| 05/05/2005 | US20050091964 Ventilation system for a convergent divergent exhaust nozzle |
| 05/05/2005 | US20050091963 Aircraft turbine engine and an air ejection assembly for use therewith |
| 05/04/2005 | EP1528248A1 Methods and apparatus for flade engine nozzle |
| 05/04/2005 | EP1528247A2 Methods and apparatus to reduce turbine engine nozzle base sheet stresses |
| 05/04/2005 | EP1527997A2 Flade gas turbine engine with fixed geometry inlet |
| 05/04/2005 | EP1527268A1 Thrust reverser system with a pass-through torque activated brake |
| 05/04/2005 | CN1611762A Methods and apparatus to reduce turbine engine nozzle base sheet stresses |
| 05/04/2005 | CN1611761A Super combustion pressed engine |
| 04/28/2005 | US20050086927 Induction coupled variable nozzle |
| 04/26/2005 | US6883302 Methods and apparatus for generating gas turbine engine thrust with a pulse detonation thrust augmenter |
| 04/26/2005 | CA2113367C Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
| 04/21/2005 | WO2005035964A1 Thrust reverser lock comprising locking device |