| 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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| 01/16/2008 | EP1878903A1 Air compression aeroengine |
| 01/16/2008 | EP1878877A2 Shape memory material actuator |
| 01/11/2008 | CA2592911A1 Gas turbine engine and method of operating same |
| 01/10/2008 | WO2008003889A2 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 01/10/2008 | CA2656279A1 Method for reversing the thrust produced by a power plant of an aircraft, device for implementing it and nacelle equipped with said device |
| 01/09/2008 | CN100360786C AIr jet engine attached device |
| 01/08/2008 | CA2305927C Universal joint-type vectoring turbojet exhaust nozzle |
| 01/03/2008 | US20080000236 Seal assembly |
| 01/03/2008 | US20080000235 Fan variable area nozzle for a gas turbine engine fan nacelle |
| 01/02/2008 | EP1873389A1 Turbomachine nozzle cowl with triangular noise suppression tabs having an inflexion point |
| 01/02/2008 | EP1873388A1 Turbomachine cowl having noise suppression triangular tabs with double crests |
| 01/02/2008 | EP1873387A2 Purged flameholder fuel shield |
| 01/02/2008 | EP1873386A2 Fan variable area nozzle for a gas turbine engine fan nacelle |
| 01/02/2008 | EP1873385A2 Exhaust cone for channeling a gas stream downstream of a turbine |
| 01/01/2008 | US7313910 Jet vane thrust vector control system |
| 12/27/2007 | WO2007148001A1 Aircraft propulsion assembly comprising a jet pipe with a notched trailing edge |
| 12/27/2007 | WO2007147954A1 Thrust reverser forming an adaptive nozzle |
| 12/27/2007 | WO2007147193A1 Guiding carrier for jet engine linings |
| 12/27/2007 | US20070295860 Propulsion System, Aircraft Comprising the Propulsion System and an Outlet Device for a Jet Engine |
| 12/27/2007 | CA2655601A1 Aircraft propulsion assembly comprising a jet pipe with a notched trailing edge |
| 12/27/2007 | CA2655369A1 Track beam for the cowling of jet engines |
| 12/27/2007 | CA2654362A1 Thrust reverser forming an adaptive nozzle |
| 12/26/2007 | EP1870589A1 Flow mixing nozzle with curved lobes for a turbomachine |
| 12/26/2007 | EP1870588A1 Swirling flow mixing nozzle for a turbomachine |
| 12/26/2007 | CN100357569C Equipment for fixing supporting blades of disributor component arround circumferential curved line |
| 12/26/2007 | CA2592794A1 Cowling for turbine engine nozzle with triangular inflection point patterns to reduce jet noise |
| 12/26/2007 | CA2592484A1 Cowling for turbine engine nozzle with triangular double top patterns to reduce jet noise |
| 12/26/2007 | CA2592483A1 Exhaust cone for channeling a gas stream downstream from a turbine |
| 12/25/2007 | US7310949 Method and apparatus for arresting a crack within a body |
| 12/25/2007 | US7310939 Device for reducing the jet noise of a turbomachine |
| 12/19/2007 | EP1386072B1 Device for controlling the deployment of jet engine thrust reversers |
| 12/19/2007 | CA2592272A1 Rotary movement mixer for a confluent flow nozzle of a turbine engine |
| 12/19/2007 | CA2592200A1 Curved lobe mixer for a confluent flow nozzle of a turbine engine |
| 12/18/2007 | US7308966 Device for reducing jet engine exhaust noise using oscillating jets |
| 12/12/2007 | EP1595068B1 Ventilated confluent exhaust nozzle |
| 12/11/2007 | US7305817 Sinuous chevron exhaust nozzle |
| 12/06/2007 | DE102006023827A1 Thrust-direction turning device of airplane with vertical take-off-landing, and with short-distance take-off-landing, has extension attachment piece, which leads downward during vertical flight |
| 12/05/2007 | CN101084370A Method for fixing a flexible drive shaft in a thrust reverser and a thrust reverser of this type |
| 12/04/2007 | US7302794 Rocket engine member and a method for manufacturing a rocket engine member |
| 12/04/2007 | US7302793 Methods and apparatus to reduce turbine engine nozzle basesheet stresses |
| 11/29/2007 | WO2007135257A1 Turbojet nacelle equipped with means for reducing the noise produced by said turbojet |
| 11/29/2007 | US20070273159 Thrust Reverser Lock Comprising Locking Device |
| 11/29/2007 | US20070271901 An outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine |
| 11/29/2007 | CA2652363A1 Turbojet nacelle equipped with means for reducing the noise produced by said turbojet |
| 11/28/2007 | EP1860313A1 Central body for the exhaust channel of a jet engine |
| 11/28/2007 | EP1860301A2 Micro-perforated acoustic liner |
| 11/27/2007 | US7299636 Extendible exhaust nozzle bell for a rocket engine |
| 11/27/2007 | US7299635 Device for mixing two flows of fluid which are initially guided separate from one another in a bypass jet engine |
| 11/27/2007 | US7299622 Component for being subjected to high thermal load during operation and a method for manufacturing such a component |
| 11/23/2007 | CA2588950A1 Central body for a turbojet engine exhaust channel |
| 11/22/2007 | US20070266712 Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft |
| 11/21/2007 | EP1857656A2 Multi-splice acoustic liner |
| 11/21/2007 | CN101076659A Acoustic absorber for aircraft engines |
| 11/21/2007 | CN100350147C Electromechanical turbojet thrust reverser with containuous position control |
| 11/21/2007 | CN100350146C Turbojet engine electromechanical thrust reverse with synchronous locking device |
| 11/20/2007 | US7296656 Acoustic mechanical retainer |
| 11/20/2007 | US7296655 Duct liner acoustic splice |
| 11/20/2007 | US7296411 Method and system for regulating internal fluid flow within an enclosed or semi-enclosed environment |
| 11/20/2007 | US7296397 Ventilation system for a convergent divergent exhaust nozzle |
| 11/20/2007 | CA2477627C Electric thrust reverser actuation system |
| 11/15/2007 | WO2007130768A1 Sound-absorbing exhaust nozzle center plug |
| 11/15/2007 | WO2007128890A1 Nacelle for bypass engine with high bypass ratio |
| 11/15/2007 | CA2651103A1 Nacelle for bypass engine with high bypass ratio |
| 11/14/2007 | EP1854989A2 Cover of a bleed air relief system in a turbomachine |
| 11/13/2007 | US7293401 Jet engine noise suppressor |
| 11/08/2007 | US20070256419 Nozzle with an adjustable throat |
| 11/08/2007 | DE102006019299B3 Aircraft turbofan jet engine, with a primary and a ring-shaped side jet, has an adjustment mechanism of rings to reduce noise emissions on take-off |
| 11/07/2007 | EP1852614A2 Low noise ejector motive nozzle |
| 11/07/2007 | EP1852595A2 Aeroengine thrust reverser |
| 11/06/2007 | US7290982 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle |
| 11/01/2007 | WO2007123556A2 Turbofan core thrust spoiler |
| 11/01/2007 | WO2007122368A1 Variable area exhaust nozzle |
| 11/01/2007 | US20070251211 Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft |
| 11/01/2007 | CA2612532A1 Turbofan core thrust spoiler |
| 10/31/2007 | EP1849987A2 Gas turbine engine with acoustic liners |
| 10/31/2007 | EP1849986A1 Jet engine comprising an afterburner cooled by a ventilation flow with variable flow |
| 10/31/2007 | EP1849985A1 Twisted elbow-shaped propelling gas exhaust assembly in an aircraft |
| 10/31/2007 | EP1849984A1 Propelling gas exhaust assembly in an aircraft with two elbow-shaped channels |
| 10/31/2007 | EP1849983A1 Elbow-shaped propelling gas exhaust assembly in an aircraft |
| 10/31/2007 | EP1849974A2 Turbine engine tailcone resonator |
| 10/31/2007 | CN100346066C System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber |
| 10/30/2007 | US7287369 Method for extending a nozzle and extended nozzle for rocket drives |
| 10/28/2007 | CA2585920A1 Exhaust assembly forming a horizontal elbow for propulsion gases in an aircraft |
| 10/28/2007 | CA2585893A1 Jet turbine engine having a post-combustion channel cooled by a variable-flow rate ventilation flow |
| 10/28/2007 | CA2585879A1 Exhaust assembly for propulsion gases in an aircraft with twist elbow |
| 10/28/2007 | CA2585878A1 Exhaust assembly for propulsion gases in an aircraft forming an elbow |
| 10/25/2007 | US20070246293 Method and device for reducing engine noise |
| 10/24/2007 | EP1847707A2 Actuation system for two mobile crowls of a thrust reverser, and thrust reserver equipped with such a system |
| 10/24/2007 | EP1846649A1 Outlet device for a jet engine and a craft comprising such an outlet device |
| 10/24/2007 | EP1846295A1 Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner |
| 10/24/2007 | EP1846294A1 Procedure for replacement of acoustic liner in integrated exhaust duct muffler for use with airborne auxiliary power units |
| 10/18/2007 | DE102006017739A1 Jet engine for use at subsonic speeds has thrust nozzle with inwardly-tapering section formed by end of turbine shaft surrounded by outwardly-tapering section of nozzle wall |
| 10/17/2007 | CN101054932A Nuclear power engine and aerocraft produced thereby and spacecraft |
| 10/11/2007 | WO2007025047A3 Performance improvements for pulse detonation engines using ejectors |
| 10/11/2007 | US20070234728 Convergent divergent nozzle with interlocking divergent flaps |
| 10/11/2007 | DE102006012977A1 Thermal-insulating layer system for use in e.g. gas turbine, has active thermal-insulating layer counteracting heat flow, which is defined by intrinsic thermal conductivity of passive poor heat conducting thermal-insulating layer |
| 10/10/2007 | EP1843032A1 Central body of jet engine nozzle |
| 10/10/2007 | EP1843031A1 Aeroengine thrust reverser |
| 10/10/2007 | EP1843030A2 Flow control device |
| 10/09/2007 | US7278258 Floating flexible firewall seal |