Patents
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)
01/2012
01/12/2012US20120006000 Bent connecting rod fitted with at least one self-aligning means
01/12/2012DE102010026834A1 Gasturbinenabgaskonus Gas turbine exhaust cone
01/12/2012CA2802655A1 Thrust reverser having an aerodynamic coupling for a front frame
01/11/2012CN101451556B Hydraulic pressure moving tube with emergency back function
01/10/2012US8091827 Thrust reverser door
01/10/2012US8091335 Swept fan ramp for pivot door thrust reverser
01/10/2012US8091334 Method of operating a turbofan engine cowl assembly
01/05/2012WO2011066365A3 Variable area fan nozzle bearing track
01/05/2012US20120000179 Rear section of aircraft nacelle and nacelle equipped with such rear section
01/05/2012DE102010026083A1 Damping device for sealing machine for rotation friction welding of e.g. airplane thruster, has damping element arranged between housing and rotatable spindle which receives to-be-welded component
01/05/2012DE102010026000A1 Producing three-dimensional metallic component such as component of aircraft engine, comprises applying of droplets that contain organometallic compound; and removing organic part of the organometallic compound in applied droplets
01/04/2012EP1745207B1 Pulse jet engines
01/04/2012CN102308401A Thermoelectric generation for a gas turbine
01/04/2012CN102305153A Novel heat engine
01/03/2012US8087491 Vane type silencers in elbow for gas turbine
01/03/2012US8087250 Duplex tab exhaust nozzle
01/03/2012US8087229 Variable supersonic mach number air heater utilizing supersonic combustion
01/03/2012CA2600289C Device for actuating the mobile cowlings of a thrust reverser
01/03/2012CA2515852C Ventilated confluent exhaust nozzle
01/03/2012CA2469943C Aircraft engine rear hanging device
12/2011
12/29/2011WO2011160441A1 Thermal ramjet
12/29/2011DE102010025014A1 Vorrichtung zur Reduzierung von Strahllärm Device for reducing jet noise
12/28/2011EP2399827A2 Guide system for nacelle assembly
12/28/2011CN102301123A 用于涡轮引擎的隔音排气管 For a turbine engine exhaust noise
12/28/2011CN102301122A 用于飞行器发动机机舱的声衰减板 Sound attenuation for aircraft engine nacelle board
12/24/2011CA2742548A1 Ejector purge of cavity adjacent exhaust flowpath
12/22/2011WO2011066368A3 Nacelle assembly for a variable area fan nozzle of a gas turbine engine
12/22/2011US20110308232 Method and device to increase thrust and efficiency of jet engine
12/22/2011DE102010023998A1 Flow channel for e.g. aircraft engine, has slat whose floating bearing is adjusted under elastic deformation of slats in radial direction to extent and/or axial direction of flow channel relative to fixed wall portion
12/21/2011EP2153049B1 System for mixing gas flows in a gas turbine engine, corresponding gas turbine engine and aircraft engine
12/21/2011EP2074308B1 Integrated variable area nozzle and thrust reversing mechanism
12/21/2011CN101403349B 高速机车喷气式发动机排气管及其近净成型铸造法 High-speed locomotive jet engine exhaust pipe and near net shape casting
12/15/2011WO2011156078A1 Cooled conduit for conveying combustion gases in a gas turbine engine
12/15/2011WO2011154644A1 Self-mounted cascade for a thrust reverser
12/15/2011US20110302905 Eyeball seals for gimbaled rocket engines, and associated systems and methods
12/15/2011DE202008018190U1 Motor Motor
12/15/2011CA2801603A1 Self-mounted cascade for a thrust reverser
12/14/2011EP2395222A1 Gas turbine engine system and corresponding controlling method
12/14/2011EP2394309A1 Thermoelectric generation for a gas turbine
12/14/2011CN202073656U 一种水下气液两相发动机 Underwater gas-liquid two-phase engine
12/14/2011CN102278233A 超音速转子发动机 Supersonic rotary engine
12/14/2011CN102278231A 用于发动机舱总成的导引系统 A nacelle assembly for a guide system
12/14/2011CN101558230B 用于喷气发动机的可平移的推力反向装置 For jet engine thrust reverse translating means
12/08/2011WO2011151579A1 Assembly including a reverse thrust device and system for actuating said device
12/08/2011WO2011151563A1 Thrust reverser having a lockable variable nozzle section
12/08/2011US20110296813 Variable area fan nozzle with bypass flow
12/08/2011US20110296812 Thrust reverser actuation system architecture
12/08/2011CA2799367A1 Assembly including a reverse thrust device and system for actuating said device
12/08/2011CA2799361A1 Thrust reverser having a lockable variable nozzle section
12/07/2011EP2392814A2 External flap retaining mechanism for an exhaust nozzle
12/07/2011EP2391811A1 Soundproof exhaust pipe for a turbine engine
12/07/2011EP2391810A2 Thermally balanced materials
12/07/2011EP2391809A2 Thermally balanced aero structures
12/07/2011EP2391804A1 Fluid expansion device and method with noise attenuation
12/07/2011CN101733614B 一种火箭发动机喷管的制备方法以及其专用设备 Preparation of a rocket engine nozzle and its special equipment
12/06/2011US8069666 System for generating shaft horsepower using waste heat
12/06/2011US8069648 Impingement cooling for turbofan exhaust assembly
12/06/2011US8069647 Jet nozzle mixer
12/01/2011US20110289900 Thrust reversing variable area nozzle
11/2011
11/29/2011US8065868 System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft
11/29/2011CA2592676C Jet engine nozzle exit configurations and associated systems and methods
11/24/2011WO2011144837A1 Airplane jet engine thrust reverser having gratings or cascades
11/24/2011US20110284660 Thrust reverser for a turbofan engine nacelle
11/24/2011US20110284318 Soundproof exhaust pipe for a turbine engine
11/24/2011CA2799543A1 Multi-layer acoustic treatment panel
11/23/2011EP2388193A2 Guide system for nacelle assembly
11/23/2011CN102251880A Underwater gas-liquid two-phase engine
11/23/2011CN102251879A Differential adjustable unilateral expansion nozzle
11/22/2011US8061145 Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine
11/22/2011US8061144 Gas turbine engines
11/22/2011US8061143 Gas turbine engine reheat systems
11/22/2011US8061119 Actuation mechanism for a convertible gas turbine propulsion system
11/17/2011WO2011142866A2 Articulating slider track
11/17/2011WO2011141678A1 Device for reducing the noise emitted by the jet of an aircraft propulsion engine
11/17/2011CA2789438A1 Articulating slider track
11/16/2011EP2315928B1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
11/16/2011CN101605978B Method of manufacturing a CMC flow mixer lobed structure for a gas turbine aeroengine
11/16/2011CN101451553B Mechanical synchronous hydraulic pressure moving system
11/15/2011CA2492149C Nozzle flap cooling air supply system
11/15/2011CA2439555C Acoustically resistive layer for a sound attenuation panel, panel using such a layer
11/10/2011WO2011138571A1 Unit for an aircraft thruster
11/10/2011US20110271686 Exhaust silencer convection cooling
11/10/2011US20110271685 Variable fan duct nozzle
11/09/2011EP2385221A1 Sealing assembly
11/09/2011EP2288862B1 Wall cooling device
11/09/2011CN102235266A Exhaust silencer convection cooling
11/08/2011US8052086 Thrust reverser door
11/08/2011US8052085 Thrust reverser for a turbofan gas turbine engine
11/03/2011WO2011135238A1 Turbojet engine nacelle
11/03/2011WO2011135216A1 Reverser having doors
11/03/2011US20110266366 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
11/03/2011US20110265448 Jet nozzle mixer
11/03/2011CA2796017A1 Reverser having doors
11/02/2011EP2383456A1 Single acting hydraulic cylinder
11/02/2011EP2383455A2 Gas turbine engine exhaust mixer
11/02/2011EP2383180A1 Actuator arrangement
11/02/2011EP2179165B1 Mobile thrust reverser cowl and thrust reverser provided with such a cowl
11/01/2011US8047884 Propulsion system
11/01/2011US8047004 Stave and ring CMC nozzle
10/2011
10/29/2011CA2738100A1 Gas turbine engine exhaust mixer
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