Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
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)
07/2010
07/07/2010EP2084062B1 Side-opening jet engine nacelle
07/07/2010CN101772635A Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise, and turbojet and motor assembly associated therewith
07/07/2010CN101772634A Mobile thrust reverser cowl and thrust reverser provided with such a cowl
07/01/2010US20100162683 Turbofan engine
07/01/2010US20100162679 Gas turbine engine with ejector
06/2010
06/30/2010CA2689176A1 Gas turbine engine with ejector
06/30/2010CA2689174A1 Gas turbine engine with ejector
06/24/2010WO2010055213A8 System for controlling the cowl of a turbojet engine nacelle thrust reverser
06/24/2010WO2010046704A3 Method and system for altering engine air intake geometry
06/23/2010EP2198143A1 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator
06/22/2010US7739872 Cooled dual wall liner closeout
06/22/2010US7739865 Gas turbine engine inlet with noise reduction features
06/22/2010CA2688673A1 Exhaust gas discharge system and plenum
06/18/2010CA2686898A1 Method and apparatus for forming a turbofan mixer
06/17/2010WO2010066957A1 A turbojet engine nacelle with variable nozzle section
06/17/2010US20100146980 masking arrangement for a gas turbine engine
06/17/2010US20100146932 Gas turbine engine variable area exhaust nozzle
06/16/2010CN101737194A Adjustable front duct ejector in variable cycle engine mode switching mechanism
06/16/2010CN101733614A Method for preparing rocket engine jet pipe and special equipment thereof
06/15/2010US7735778 Pivoting fairings for a thrust reverser
06/15/2010US7735601 Engine noise
06/15/2010US7735600 Monolithic acoustically-treated engine nacelle inlet panels
06/15/2010CA2429461C Bypass duct fan noise reduction assembly
06/10/2010US20100140388 Air cushion landing system and method of operation
06/10/2010US20100139285 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
06/10/2010US20100139284 Jet nozzle plug with varying, non-circular cross sections
06/10/2010US20100139240 Bladder type variable area fan nozzle
06/09/2010EP2193594A2 Double-acting telescopic linear actuator with single-motor drive system
06/09/2010CN101446244B Single-valve core double-channel solenoid valve
06/08/2010US7730995 Acoustic apparatus
06/08/2010US7730714 Turbofan gas turbine engine with variable fan outlet guide vanes
06/03/2010WO2010061107A1 Thrust reverser for a turbofan engine nacelle
06/03/2010US20100133378 Acoustic panel having a variable acoustic characteristic
06/03/2010CA2743445A1 Thrust reverser for a turbofan engine nacelle
06/02/2010EP2192289A1 Intake silencer for gas turbine
06/02/2010EP2192269A2 Interturbine duct strut and vane ring for gas turbine engine
06/02/2010EP2191124A1 Gas ejection cone for an aircraft turbojet equipped with a device for generating turbulence in a primary flow limiting jet noise, and turbojet and motor assembly associated therewith
06/02/2010DE4007875A1 Schubstrahlauslaß Schubstrahlauslaß
06/02/2010DE102008049055A1 Verfahren zur Reparatur eines Gehäuseflanschs eines Flugzeugtriebwerks Method for repairing a housing flange of an aircraft engine
06/02/2010CN101718235A Synthetic jet actuator with double films, single chamber and single spout
06/02/2010CN101307734B Rocket engine noise reducer
05/2010
05/26/2010EP2188514A1 Turboshaft engine with reduced noise emission for aircraft
05/26/2010CN201486689U Turbojet engine silencer
05/25/2010US7721551 Fan variable area nozzle for a gas turbine engine fan nacelle
05/25/2010US7721550 Aircraft engine exhaust flap curved strut slot
05/25/2010US7721549 Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
05/25/2010US7721526 Turbofan engine
05/20/2010WO2010056666A1 Radially translating fan nozzle nacelle
05/20/2010WO2010055213A1 System for controlling the cowl of a turbojet engine nacelle thrust reverser
05/20/2010WO2010036412A3 Robotic manipulator
05/20/2010WO2010026354A3 Flexible abutment links for attaching a part made of cmc
05/20/2010WO2009060295A8 A device and method for controlling vortex structures in a turbulent air jet
05/20/2010US20100122868 Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
05/20/2010CA2711945A1 System for controlling the cowl of a turbojet engine nacelle thrust reverser
05/19/2010CN101709679A Adjustable rear culvert channel injector in mode switching mechanism of variable cycle engine
05/18/2010US7717229 Gas turbine exhaust sound suppressor and associated methods
05/18/2010US7716932 Dilating fan duct nozzle
05/18/2010US7716912 Propulsion thrust control system and method
05/14/2010WO2009138681A3 Turbojet engine nacelle downstream assembly
05/13/2010US20100115964 Noise reduction device
05/13/2010US20100115958 Radially translating fan nozzle nacelle
05/13/2010US20100115915 Method for controlling electric motors of a thrust reverser
05/13/2010US20100115914 Translating core cowl having aerodynamic flap sections
05/12/2010EP2184481A2 Gas turbine engine with variable area exhaust nozzle
05/12/2010EP2184480A2 A gas turbine engine with variable area exhaust nozzle and method of operating such a gas turbine engine
05/06/2010US20100108802 Sail wing aircraft which includes an engine mounted on a pylon
05/06/2010US20100107646 Shape memory alloy actuated adaptive exhaust nozzle for jet engine
05/06/2010US20100107600 Gas turbine engine variable area exhaust nozzle
05/06/2010US20100107599 Thrust reverser for a jet engine
05/06/2010DE102008037513A1 Baffle seal for deflector flap arrangement of thrust-reverser for gas turbine, has sealing edge including outer peripheral area that extends-out over outer peripheral area of central section, in order to define exposed sealing surface
05/05/2010EP2182289A2 Method and apparatus for affecting a recirculation zone in a combustor cross flow
05/05/2010EP2181373A1 System for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser
05/05/2010EP2181371A2 System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system
05/05/2010EP2181364A1 Method and system for controlling at least one actuator for the cowlings of a turbojet engine thrust reverser
05/05/2010EP2181262A2 Variable area fan nozzle with bypass flow
05/05/2010EP2181039A1 Device and method for controlling the power supply of at least one aircraft maintenance actuator
05/04/2010US7711124 Method and device for attenuating the noise generated at the outlet of an exhaust line
05/04/2010US7707820 Control and/or drive device for a flying body
05/04/2010CA2642777A1 Baffle seal for gas turbine engine thrust reverser
04/2010
04/29/2010US20100102144 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained
04/28/2010EP2179194A1 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
04/28/2010EP2179167A2 System for controlling at least one actuator of the cowlings of a turbojet engine thrust reverser
04/28/2010EP2179166A2 Method and system for controlling at least one actuator or actuating the cowlings of a thrust inverter in a turbojet engine
04/28/2010EP2179165A1 Mobile thrust reverser cowl and thrust reverser provided with such a cowl
04/28/2010EP2179164A1 Thrust reverser with a system for braking the actuators
04/28/2010EP2179163A1 Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron
04/28/2010EP2179144A2 Structure for thrust inverter
04/28/2010EP2178753A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
04/22/2010US20100096474 Gas Turbine Ejector and Method of Operation
04/20/2010US7698896 exhaust system of a gas turbine engine has primary nozzle, which is configured to accelerate and discharge turbine exhaust gas through the exhaust duct and exits the aircraft via the exhaust opening; used in aircraft;
04/15/2010US20100089031 System, method and apparatus for vectoring nozzle exhaust plume with external actuation
04/15/2010US20100089028 Corrugated core cowl for a gas turbine engine
04/14/2010EP2175123A2 Actuator and corresponding thrust reverser system
04/13/2010CA2486237C Method and apparatus for arresting a crack within a body
04/07/2010EP2172716A2 Sound attenuation systems
04/07/2010EP2171244A2 Modular chevron exhaust nozzle
04/07/2010EP2171218A2 Dual flow turboshaft engine with advanced hot flow nozzle
04/06/2010US7690195 Dilution and dispersion device for the exhaust and/or cooling gases of a vehicle's engine
04/06/2010CA2460854C Converging nozzle thrust reverser
04/01/2010WO2010034893A1 Nacelle with a variable nozzle section
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