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)
07/2014
07/02/2014CN103899432A 一种改进的具有两股二次流喷射气动矢量喷管结构 An improved secondary injection has two strands vectoring nozzle structure
07/01/2014US8763930 Twin-nozzle bow thruster for hovercraft
07/01/2014US8763751 Silencer for an auxiliary power unit of an aircraft
06/2014
06/26/2014WO2014100684A1 Thermally compliant dual wall liner for a gas turbine engine
06/26/2014WO2014096634A1 Removable acoustic panels for turbojet engine casing
06/26/2014WO2014096619A1 Optimising the availability of a thrust reverser
06/25/2014EP2745223A1 Method of determining the performance of at least one propeller of a turbomachine in an air stream under gyration
06/25/2014EP2744999A2 Nozzle arrangement and method of making the same
06/25/2014CN203670026U 航空发动机附面偏转矢量喷口装置 Aero-engine plane deflection vector nozzle attached device
06/25/2014CN103890366A 用于附接中空部件的设备 A device for attaching the hollow member
06/25/2014CN102278233B 超音速转子发动机 Supersonic rotary engine
06/25/2014CN101815973B 控制一涡轮喷气发动机上推力反向器整流罩的至少一致动器的系统以及用于测试此系统的方法 Control of a turbojet engine thrust reverser cowling at least an actuator system and a method for testing this system
06/24/2014US8756936 Exhaust diffuser adjustment system for a gas turbine engine
06/19/2014WO2014092595A1 Power device
06/19/2014WO2014091140A1 Nacelle thrust reverser and nacelle equipped with at least one reverser
06/19/2014WO2014091139A1 Synchronization system for a thrust reverser
06/19/2014US20140172201 Method for monitoring the locking means of an electrical thrust reversal system for a turbine engine
06/19/2014US20140165574 Exhaust plug for an aircraft turbojet engine
06/19/2014US20140165532 System and method for improving the efficiency of a jet engine
06/18/2014EP2742230A1 Exhaust cone for aircraft turbojet engine
06/18/2014EP2742229A1 Thrust reverser device for compact jet pipe
06/18/2014EP2742228A1 Thrust reverser device
06/18/2014EP2742227A1 Exhaust plug for an aircraft turbojet engine
06/18/2014CN102131705B Nacelle with a variable nozzle section
06/12/2014US20140158458 Exhaust cone for aircraft turbojet engine
06/12/2014DE102012220358A1 Düse mit Leitvorrichtungen Nozzle with louvers
06/11/2014EP2740923A1 Exhaust Diffuser
06/11/2014EP2739842A1 Method for monitoring the locking means of an electrical thrust reversal system for a turbine engine
06/11/2014EP2739841A1 Reverser having movable cascades, and translatably variable nozzle
06/11/2014EP2739840A1 Turbojet engine nacelle having a variable nozzle
06/05/2014WO2014084986A1 Thrust reverser system with translating rotating blocker doors and method of operation
06/05/2014WO2014083278A1 Active lock with mobilisation assistance and thrust reverser incorporating such a lock
06/05/2014US20140154064 Thrust reverser device
06/05/2014US20140150404 Thrust reverser device for compact jet pipe
06/05/2014US20140150403 Thrust reverser system with translating-rotating cascade and method of operation
06/04/2014EP2737231A1 Double-acting linear actuator
06/04/2014EP2737194A1 Device for connecting a front frame to a fan casing
06/04/2014EP2737193A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle
06/03/2014US8739548 Sliding ramp nozzle system for a gas turbine engine
06/03/2014US8739515 Variable area fan nozzle cowl airfoil
06/03/2014CA2728527C Duplex tab exhaust nozzle
05/2014
05/29/2014US20140145008 Gas turbine engine exhaust nozzle
05/29/2014US20140145001 Method and apparatus for nozzle thrust vectoring
05/28/2014CN203614268U 一种用于航空发动机控制系统的主-备控制模式切换阀 Main engine control system for aviation - the device control mode switching valve
05/28/2014CN103827473A 带有侧面开口的推力反向器门 With side openings of the thrust reverser door
05/28/2014CN102444499B 膛线形气动突条喷管的排气掺混方法及其装置 Pneumatic linear ridges bore exhaust nozzle blending method and apparatus
05/28/2014CN102434315B 旁路式双喉道无源矢量喷管 Bypass dual passive vectoring nozzle throat
05/27/2014US8733698 Method and device for implementing the thrust reversers of an aircraft
05/27/2014US8733496 Acoustic damper, combustor, and gas turbine
05/27/2014US8733107 Nozzle-area ratio float bias
05/27/2014US8733080 Thrust reverser and VAFN arrangement
05/22/2014WO2014078570A1 Engine and thrust reverser actuation system
05/22/2014US20140137541 Aircraft propulsion unit including at least one turbojet engine and a nacelle
05/20/2014US8727275 Nacelle
05/20/2014US8726634 Nacelle for an aircraft engine with variable cross-section nozzle having a rack and pinion actuator assembly
05/15/2014WO2014072655A1 Turbojet engine nacelle comprising a unit assembly capable of moving along a guide assembly
05/15/2014US20140131515 Aircraft turbojet engine thrust reverser with a reduced number of latches
05/15/2014US20140131481 Threaded rod for system for deploying a deployable divergent segment of a thruster
05/15/2014US20140131480 Thrust reverser device without a control rod in the stream
05/15/2014US20140131479 Aircraft turbojet engine thrust reverser with a lower number of actuators
05/15/2014US20140130503 Turbofan engine with convergent - divergent exhaust nozzle
05/14/2014EP2730773A2 A gas turbine engine exhaust nozzle
05/14/2014EP2730772A2 Nozzle with baffles
05/14/2014EP2730771A2 Nozzle with baffles
05/14/2014CN103796919A 涡轮喷气发动机的机舱后部组件 Turbojet engine nacelle rear assembly
05/14/2014CN103790733A 一种能降低喷气式飞机喷气噪声的装置 One kind of a jet to reduce the jet noise reduction device
05/14/2014CN102301122B 用于飞行器发动机机舱的声衰减板 For aircraft engine nacelle acoustic attenuation plate
05/13/2014US8720818 Thrust reverser and nacelle for aircraft equipped with at least one such reverser
05/13/2014US8720183 Thrust reverser translating sleeve assembly
05/13/2014US8720182 Integrated variable area nozzle and thrust reversing mechanism
05/13/2014CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes
05/13/2014CA2551343C Thrust vectoring nozzle
05/08/2014WO2014028088A3 Liner hanger with spherical washers
05/08/2014WO2013062664A3 Nozzle arrangement and method of making the same
05/08/2014US20140127010 Nozzle with guiding devices
05/08/2014US20140124289 Nozzle with guiding devices
05/08/2014US20140123625 Engine control parameter trimming
05/08/2014DE102012220360A1 Düse mit Leitvorrichtungen Nozzle with louvers
05/07/2014EP2728154A2 Methods and apparatus for sealing variable area fan nozzles of jet engines
05/07/2014EP2728153A2 Actuator arrangement
05/07/2014EP2728152A2 Thrust reversers and methods to provide reverse thrust
05/07/2014CN103775244A 喷射双流转子发动机 Shuangliu rotor jet engine
05/07/2014CN102235266B 排气消声器对流冷却 Convection cooled exhaust muffler
05/06/2014US8714919 Inlet and exhaust system
05/06/2014US8713911 System and method for operating a thrust reverser for a turbofan propulsion system
05/06/2014US8713910 Integrated thrust reverser/pylon assembly
05/01/2014US20140117113 Methods and apparatus for sealing variable area fan nozzles of jet engines
05/01/2014US20140117106 Thrust reversers and methods to provide reverse thrust
05/01/2014US20140116026 Aeroengine thrust reverser arrangement
05/01/2014US20140116025 Aeroengine thrust reverser arrangement
05/01/2014US20140116024 Lock for a translating sleeve of a nacelle
04/2014
04/30/2014EP2725218A2 Aeroengine thrust reverser arrangement
04/30/2014EP2725217A2 Aeroengine thrust reverser arrangement
04/30/2014DE102012219541A1 Nozzle e.g. exhaust nozzle of aircraft jet engine, comprises a turbulence and/or swirl-generating structure which projects radially from the nozzle walls to the inside and/or on the outer side of the nozzle walls
04/30/2014CN103764985A Exhaust plug for an aircraft turbojet engine
04/30/2014CA2822240A1 Methods and apparatus for sealing variable area fan nozzles of jet engines
04/30/2014CA2822165A1 Thrust reversers and methods to provide reverse thrust
04/29/2014US8707675 Pressure assisted direct drive proportional hot-gas thruster
04/29/2014CA2581542C Central portion of turbine engine nozzle
04/24/2014US20140110503 Thrust reverser and nacelle for aircraft equipped with at least one such reverser
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