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)
04/2014
04/23/2014EP2721277A1 Actuating assembly for a thrust reverser of an aircraft engine
04/23/2014EP2721276A1 Variable jet engine outlet with a mainly circle sector-formed cross section
04/22/2014US8701386 Aircraft nacelle that incorporates a thrust reversal device
04/22/2014US8701385 Method and apparatus for the operation of a turboprop aircraft engine provided with pusher propellers
04/22/2014CA2663231C Cascade-type thrust reverser for jet engine
04/17/2014WO2014056913A1 Actuating device including a primary locking device
04/17/2014WO2014007907A3 Variable immersion lobe mixer for turbofan jet engine exhauts and method of fabricating the same
04/17/2014US20140103141 Variable jet engine outlet with a mainly circle sector-formed cross section
04/17/2014US20140102112 One-piece fuel nozzle for a thrust engine
04/17/2014US20140102108 Seal assembly for liners of exhaust nozzle
04/16/2014CN203547987U Engine
04/16/2014CN103732949A Double-acting linear actuator
04/16/2014CN103732900A Thrust reverser device
04/16/2014CN103732899A Nacelle for an aircraft bypass turbojet engine
04/16/2014CN102459856B Thrust reversing device
04/16/2014CN102449294B Thrust reverser for a dual-flow turbine engine nacelle
04/16/2014CN102144084B Flexible abutment links for attaching a part made of CMC
04/15/2014CA2554385C One-piece baffle infrared suppressor apparatus and method
04/10/2014WO2014028078A3 A gas turbine engine and nacelle noise attenuation structure
04/10/2014WO2014021973A3 Liner assembly
04/10/2014US20140097271 Aircraft engine with an apparatus for pulsating expiration of gas into the exhaus nozzle
04/10/2014DE102012109647A1 Flugtriebwerk mit einer Einrichtung zum pulsierenden Ausblasen eines Gases in die Abgasdüse Aircraft engine including means for pulsating blowing a gas into the exhaust nozzle
04/09/2014EP2716879A1 Turbine exhaust plume mitigation system
04/09/2014EP2715099A1 Nacelle for an aircraft bypass turbojet engine
04/09/2014EP2714384A1 Method for manufacturing a sound attenuation panel
04/09/2014CN103717870A Exhaust cone for aircraft turbojet engine
04/09/2014CN103717869A Method for monitoring the locking means of an electrical thrust reversal system for a turbine engine
04/09/2014CN103717868A Thrust reverser device for compact jet pipe
04/09/2014CN103717867A Aircraft propulsion unit including at least one turbojet engine and a nacelle
04/09/2014CN103717866A Turbojet engine nacelle having a variable nozzle
04/09/2014CN102216597B Thrust reverser for turbofan engine nacelle
04/08/2014US8689933 Helmholtz resonator for a gas turbine combustion chamber
04/08/2014CA2561227C Anti-wear protection process for a thermostructural part made of composite matrix ceramic material, coating and the part obtained through this process
04/03/2014WO2014052281A1 Gas turbine engine assembly including a thrust reverser
04/03/2014WO2014052061A1 Turbomachine thrust reverser
04/03/2014WO2014051671A1 Geared gas turbine engine integrated with a variable area fan nozzle with reduced noise
04/03/2014WO2014051667A1 Divot for blocker doors of thrust reverser system
04/03/2014US20140090359 Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it
04/03/2014US20140090358 Replaceable thrust generating structures attached to an air vehicle
04/02/2014CN103703237A Device for connecting front frame to fan casing
04/02/2014CN103703236A Reverser having movable cascades, and translatably variable nozzle
04/02/2014CN103696880A Thin-wall whirl central body structure
04/02/2014CN103696879A Two-dimensional aerospike vectoring nozzle
04/02/2014CN103696878A Axisymmetric convergent and divergent exhaust nozzle
04/02/2014CN103696877A Reverse thrusting device with capacity of adjusting area of spray pipe
04/02/2014CN103696876A Sawtoothed angle regulation mechanism for two-dimensional spray pipe
04/02/2014CN103696875A Sawtooth angle-adjustable two-dimensional vectoring nozzle
04/02/2014CN103696874A Outer flap of axisymmetric vectoring exhaust nozzle
04/02/2014CN103696873A Axisymmetric vectoring nozzle with good stealth function
04/02/2014CN103696872A Thrust vectoring nozzle with rectangular jet engine tail cross section
04/01/2014US8684130 Damping system for combustor
04/01/2014US8683807 Jet engine exhaust nozzle flow effector
04/01/2014CA2554151C Infrared suppressor apparatus and method
03/2014
03/27/2014WO2014046842A1 System for decoupling drive shaft of variable area fan nozzle
03/27/2014WO2014044964A1 Thrust reverser device fixed structure
03/27/2014US20140086738 Nacelle for an aircrft bypass turbojet engine
03/27/2014US20140084080 Infrared Suppressing Exhaust System
03/27/2014DE102005022824B4 Elektronisch gesteuerter variabler Zweikammer-Resonator Electronically controlled variable two-chamber resonator
03/26/2014EP2711506A1 Infrared suppressing exhaust system
03/26/2014CN102362085B Bent connecting rod fitted with at least one self-aligning means
03/25/2014US8677758 Dilating fan duct nozzle
03/25/2014CA2756214C Jet engine nozzle exit configurations and associated systems and methods
03/25/2014CA2618812C Variable area fan nozzle and thrust reverser
03/20/2014WO2014041297A1 Method for mounting an acoustic panel in a housing of a turbomachine and turbomachine comprising an acoustic panel
03/20/2014US20140076999 Tertiary locking assembly for a thrust reverser
03/20/2014US20140076998 System for decoupling drive shaft of variable area fan nozzle
03/20/2014US20140075919 Tec mixer with variable thicknesses
03/19/2014EP2707589A1 Tail cone for a microjet rotary turbine engine
03/19/2014CN103644043A Mass gain type spray pipe
03/19/2014CN103644042A Jet rotor engine
03/18/2014US8671693 Thermally conductive structure
03/17/2014CA2826478A1 Tec mixer with variable thicknesses
03/13/2014WO2014007875A3 Gas turbine engine thrust reverser system
03/13/2014WO2012074648A3 Thrust reverser and variable area fan nozzle actuation system and method
03/12/2014DE202013011243U1 Mantelstromtriebwerk das eine Schubvektorsteuerung mit mindestens einer schwenkbaren Antriebsdüse an der Seite hat Turbofan engine having a thrust vector control with at least one propulsion nozzle at the side of the pivotable
03/12/2014CN103635681A Actuating assembly for thrust reverser of aircraft engine
03/12/2014CN103629012A Propeller
03/12/2014CN103629011A Engine
03/11/2014US8667802 Variable fan duct nozzle translatable core/inner cowl including two overlapping portions made of different materials
03/06/2014WO2014033412A1 Front frame for a cascade thrust reverser structure
03/06/2014WO2014033398A1 Assembly for holding the interface of a front frame of a nacelle and a turbojet casing
03/06/2014WO2014033387A1 Method and device for testing a system for actuating a mobile structure of a thrust reverser
03/06/2014WO2014011279A3 Turbine engine exhaust nozzle flap
03/06/2014WO2013180778A3 Seal assembly
03/06/2014US20140061332 Thrust reverser for an aircraft jet engine
03/06/2014US20140061331 Discharge system of a separated twin-flow turbojet for an aircraft, corresponding turbojet and associated design method
03/05/2014EP2702249A2 Tertiary lock system for thrust reversing mechanism
03/05/2014CN101985903B Two-stage engine thrust steering mechanism
03/04/2014US8662417 Gas turbine engine fan variable area nozzle with swivable insert system
03/04/2014US8661795 Exhaust system having multiple inlets and multiple outlets
02/2014
02/27/2014WO2014029929A1 Cascade thrust reverser for an aircraft turbofan
02/27/2014US20140053533 Reverse flow gas turbine engine with thrust reverser
02/26/2014EP2700068A1 Multi-degree of freedom resonator array
02/25/2014CA2585893C Jet turbine engine having a post-combustion channel cooled by a variable-flow rate ventilation flow
02/25/2014CA2576694C Bypass engine ejection system
02/19/2014EP2697497A1 Thrust reverser for an aircraft jet engine
02/19/2014CN203441627U Supersonic/hypersonic aerocraft engine overexpansion nozzle bypass type device
02/19/2014CN103597196A Thrust reverser and variable area fan nozzle actuation system and method
02/19/2014CN103597195A Tail cone for a microjet rotary turbine engine
02/18/2014US8651142 Flow modulating device
1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 ... 67