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)
10/2010
10/05/2010CA2486024C Method and apparatus for arresting a crack within a body
10/02/2010CA2697741A1 Combined acoustic absorber and heat exchanging outlet guide vanes
09/2010
09/30/2010WO2010109109A1 Bent connecting rod fitted with at least one self-aligning means
09/30/2010CA2756101A1 Bent connecting rod fitted with at least one self-aligning means
09/29/2010EP2233728A2 Fuel-cooled heat exchanger with thermoelectric device compression
09/29/2010EP2233727A2 Fuel-cooled flexible heat exchanger with thermoelectric device compression
09/29/2010EP2232040A2 Door-type thrust reverser for a jet engine
09/29/2010EP2231475A2 Twelve-hour structure for thrust reverser, in particular with grids
09/29/2010CN101849094A A device and method for controlling vortex structures in a turbulent air jet
09/28/2010US7802752 Jet engine noise suppressor
09/28/2010US7802432 Multiple vane variable geometry nozzle
09/23/2010US20100236862 Engine inlet deep acoustic liner section
09/22/2010EP2230455A1 Burner for a gas turbine and method for locally cooling a hot gases flow passing through a burner
09/22/2010CN101842571A Control and monitoring system and method
09/22/2010CN101443543B Turbojet nacelle equipped with means for reducing the noise produced by said turbojet
09/21/2010US7798285 Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
09/21/2010US7797944 Gas turbine engine having slim-line nacelle
09/21/2010US7797809 Zero acoustic splice fan case liner
09/16/2010WO2010103302A1 Aircraft acoustic attenuation member and method for forming said member
09/16/2010US20100232932 Air inlet shroud structure
09/16/2010US20100229528 Actuation system for a translating variable area fan nozzle
09/16/2010DE102009013150A1 Bauteil zum Einsatz in Heißgasströmungen Component for use in streams of hot gas
09/16/2010CA2754782A1 Aircraft acoustic attenuation member and method for forming said member
09/15/2010CN101835969A Grid-type thrust reverser
09/14/2010US7793504 Nozzle with an adjustable throat
09/09/2010US20100223906 Component for use in streams of hot gas
09/08/2010EP2226486A1 Method for manufacturing an ejector nozzle tube
09/08/2010EP2225453A1 Nacelle for aircraft engine having a nozzle with a variable section
09/07/2010CA2475208C Control system for vertical take off and land (vtol) aircraft
09/02/2010US20100218483 Controlled fan stream flow bypass
09/02/2010US20100218480 Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator
08/2010
08/31/2010US7784735 Aircraft pod and aircraft equipped with at least one such pod
08/31/2010US7784285 Apparatus and method for reduction of jet noise from single jets
08/31/2010US7784284 Exhaust assembly forming a horizontal propulsion gas elbow in an aircraft
08/31/2010US7784283 Sound-absorbing exhaust nozzle center plug
08/31/2010US7784270 Rotary motion mixer for a converging-stream nozzle of a turbomachine
08/26/2010WO2010096087A1 Magnetic advanced generation jet electric turbine
08/26/2010US20100215479 Gas turbine engine inlet with noise reduction features
08/26/2010US20100212998 Cellular-core structure for an acoustic panel
08/26/2010US20100212288 Jet Engine Exhaust Nozzle and Associated System and Method of Use
08/26/2010US20100212287 Thrust reverser with a system for braking the actuators
08/25/2010EP1446611B1 Use of an aerodynamic body and combustion device provided with an aerodynamic body of this type
08/25/2010CN101815973A System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system
08/25/2010CN101815857A Method and system for controlling at least one actuator or actuating the cowlings of a thrust inverter in a turbojet engine
08/24/2010US7779965 Absorbent structure for attenuating noise particular by a rotor-generator noise, and a rotor duct including such a structure
08/19/2010US20100205931 Double-acting telescopic linear actuator with single-motor drive system
08/19/2010US20100205930 Exhaust system for gas turbine
08/18/2010EP2218894A2 Arrangement for fixing stator vane
08/18/2010EP2218893A2 Cooled vane for gas turbine exhaust duct
08/18/2010EP2218892A2 Cooled vane for gas turbine exhaust duct
08/18/2010CN101809849A Double-acting telescopic linear actuator with single-motor drive system
08/18/2010CN101809311A Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
08/18/2010CN101809273A Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator
08/18/2010CN101809272A Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron
08/17/2010US7775460 Combustion nozzle fluidic injection assembly
08/17/2010US7775048 Seal assembly
08/12/2010WO2010089505A1 Thermoelectric generation for a gas turbine
08/12/2010CA2751395A1 Thermoelectric generation for a gas turbine
08/10/2010US7770399 Gas turbine engine nozzle liner with thermally compliant attachment brackets
08/10/2010US7770379 Apparatus for moving rotatable components
08/10/2010CA2584447C Shape changing structure
08/05/2010WO2010088069A2 Thermally balanced materials
08/05/2010WO2010088068A2 Thermally balanced aero structures
08/05/2010WO2010086536A1 Soundproof exhaust pipe for a turbine engine
08/05/2010US20100193632 Integral composite slider for aircrafts
08/05/2010US20100193628 Continuous composite fan duct and thrust reverser
08/05/2010US20100193605 Thermally balanced aero structures
08/05/2010US20100192590 Thermally balanced materials
08/05/2010DE102009006579A1 Sound absorber for auxiliary engine of aircraft, has inlet, outlet, housing, and flow channel which has porous wall material and is arranged in housing
08/05/2010DE102008049055B4 Verfahren zur Reparatur eines Gehäuseflanschs eines Flugzeugtriebwerks Method for repairing a housing flange of an aircraft engine
08/05/2010CA2750130A1 Soundproof exhaust pipe for a turbine engine
08/05/2010CA2749815A1 Thermally balanced materials
08/05/2010CA2749811A1 Thermally balanced aero structures
07/2010
07/29/2010US20100186369 Dual flow turboshaft engine and improved hot flow nozzle
07/28/2010EP2211038A1 Apparatus for cooling overheated gas in engine room
07/28/2010EP2209980A1 Grid-type thrust reverser
07/28/2010CN101787937A Porous wall expanding type dual throat nozzle
07/27/2010US7762078 Nozzle with temperature-responsive throat diameter
07/22/2010US20100180571 Modulating flow through gas turbine engine cooling system
07/21/2010CN101784972A System for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter
07/21/2010CN101784964A Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter
07/21/2010CN101784782A System for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter
07/21/2010CN101784781A Thrust reverser with a system for braking the actuators
07/21/2010CN101784755A Structure for thrust inverter
07/21/2010CN101784447A Device and method for controlling the power supply of at least one aircraft maintenance actuator
07/21/2010CN101784444A Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
07/21/2010CN101782026A Divergent dual-throat nozzle with gas-injection divergent section
07/20/2010US7757477 Convergent divergent nozzle with slot cooled nozzle liner
07/15/2010WO2010026354A4 Flexible abutment links for attaching a part made of cmc
07/15/2010US20100175383 Dilating fan duct nozzle
07/14/2010EP2206893A2 Combined Surface Cooler and Acoustic Absorber for Turbomachines
07/14/2010EP2205848A2 Monitoring system and monitoring method
07/14/2010EP2205847A1 A device and method for controlling vortex structures in a turbulent air jet
07/13/2010US7753311 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
07/08/2010WO2010040837A3 Sound absorber for an auxiliary engine of an aircraft
07/08/2010US20100170984 Engine assembly for aircraft with sliding nancelle
07/08/2010US20100170265 Variable Geometry Ejector
07/08/2010US20100170261 Engine noise
07/07/2010EP2204568A2 Gas turbine engine with ejector and corresponding operating method
07/07/2010EP2204567A2 Gas turbine engine with ejector and corresponding operating method
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