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)
09/2012
09/04/2012US8256225 Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method
09/04/2012US8256204 Aircraft engine thrust reverser
08/2012
08/30/2012US20120219415 Metallic annular connection structure for aircraft turbomachine
08/29/2012CN101627202B Self-calibration method for the electric jacks of a turbojet nacelle
08/28/2012US8251306 Turbofan engine for stol aircraft
08/22/2012EP2489859A1 Free gas turbine with constant temperature-corrected gas generator speed
08/22/2012EP2489856A2 Micro-perforated acoustic liner
08/21/2012US8245516 Shape memory alloy actuated adaptive exhaust nozzle for jet engine
08/21/2012US8245496 Control and/or drive device for a flying body
08/16/2012WO2012107687A1 Reduced pressure-drop pipe element
08/16/2012DE102011011220A1 Raketentriebwerk mit einer ausfahrbaren Düsenerweiterung Rocket engine with an extendable nozzle expansion
08/15/2012EP2486261A1 Circuit for supplying fuel to an aircraft engine
08/15/2012EP2074319B1 Gas turbine engine with a variable exit area fan nozzle, nacelle assembly of such a engine, and corresponding operating method
08/15/2012CN102635445A Acoustic panel treatment with a junction between two parties and repair method of an acoustic panel
08/14/2012US8240223 Actuator arrangement
08/14/2012US8240126 Valve system for a gas turbine engine
08/14/2012US8240125 Thrust vectoring system and method
08/09/2012US20120199670 Reduced drag afterburner nozzle actuation system
08/08/2012EP2484881A1 Turbine engine tailcone resonator
08/08/2012CN102630272A Assembly for an aircraft turbojet engine comprising a thrust reversal cowl
08/07/2012US8235170 Integrated tailcone muffler assemblies and methods
08/07/2012US8234869 Aviation engine inlet with tangential blowing for buzz saw noise control
08/07/2012CA2550458C Valve assembly for a gas turbine engine
08/01/2012EP2074305B1 Gas turbine engine system comprising a translating core cowl and operational method thereof
08/01/2012EP1817490B1 Cooled exhaust duct
08/01/2012EP1507971B1 Variable area thrust reverser nozzle
07/2012
07/31/2012US8230967 Vane type silencers in elbow for gas turbine
07/26/2012WO2012098328A1 Aircraft turbojet engine thrust reverser with a reduced number of latches
07/26/2012WO2012098322A2 Nacelle for an aircraft bypass turbojet engine
07/26/2012WO2012098321A2 Nacelle for an aircraft bypass turbojet engine
07/26/2012WO2012097998A1 Sound absorber for a gas turbine exhaust cone, and method for the production thereof
07/26/2012WO2012097996A1 Aviation gas turbine thrust reversing device
07/26/2012WO2012097995A1 Aviation gas turbine thrust reversing device
07/26/2012US20120186224 Aircraft jet engine comprising a system for reducing the noise generated by the ejection of the gases
07/26/2012US20120186223 Pressure assisted direct drive proportional hot-gas thruster
07/26/2012CA2824372A1 Aircraft turbojet engine thrust reverser with a reduced number of latches
07/26/2012CA2824369A1 Nacelle for an aircraft bypass turbojet engine
07/26/2012CA2824367A1 Nacelle for an aircraft bypass turbojet engine
07/25/2012EP2479415A1 Aircraft jet engine including a system for reducing the noise generated by the discharge of gases
07/25/2012EP2479414A2 Variable area fan nozzle with bypass flow
07/25/2012EP2478202A1 A noise attenuation panel and a gas turbine component comprising a noise attenuation panel
07/25/2012EP1585896B1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
07/25/2012CN102606344A Electromagnetic aerospace engine
07/25/2012CN101438048B Nacell for bypass engine with high bypass ratio
07/24/2012US8225592 Microjet noise suppression system for jet engines
07/24/2012CA2704366C Deswirling exhaust mixer
07/24/2012CA2669280C Turbofan gas turbine engine and nacelle arrangement
07/24/2012CA2480584C Turbine engine with two sections connected by a joint
07/19/2012WO2012095600A1 Device for linking a front frame to a fan casing
07/19/2012WO2012095599A1 Door for thrust reverser of an aircraft nacelle
07/19/2012WO2012059677A3 Aircraft turbojet engine thrust reverser with a lower number of actuators
07/19/2012DE102011008921A1 Gasturbinenabgaskonus Gas turbine exhaust cone
07/19/2012DE102011008920A1 Schallabsorber, insbesondere für einen Gasturbinenabgaskonus und Verfahren zu dessen Herstellung A sound absorber, in particular for a gas turbine exhaust cone and process for its preparation
07/19/2012DE102011008919A1 Fluggasturbinenschubumkehrvorrichtung Aircraft gas turbine thrust reverser
07/19/2012DE102011008918A1 Aircraft gas turbine thrust reverser, has detour elements arranged at peripheral region of cowl, and lever swingably arranged at rear end region of detour elements, where lever enables pivoting doors with displacement of detour elements
07/19/2012DE102011008917A1 Fluggasturbinenschubumkehrvorrichtung Aircraft gas turbine thrust reverser
07/19/2012CA2824005A1 Device for linking a front frame to a fan casing
07/19/2012CA2824004A1 Door for thrust reverser of an aircraft nacelle
07/18/2012CN202338414U 一种新型脉冲发动机 A new impulse engines
07/18/2012CN102597477A A noise attenuation panel and a gas turbine component comprising a noise attenuation panel
07/18/2012CN102597476A Thrust Inverter
07/18/2012CN102597475A Reverse thrust device
07/18/2012CN102597474A Noise reduction device
07/18/2012CN102597429A Metal annular connecting structure for an aircraft turbine engine
07/18/2012CN102588145A Air-breathing rotary detonation wave injection and multimode ram detonation coupled circulating propulsion system
07/18/2012CN102588112A Jet-flow efficient thermal power system
07/18/2012CN102588080A Dynamic fluid gas working medium compression system
07/18/2012CN101784782B System for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter
07/18/2012CN101646857B Aircraft nacelle incorporating a thrust-reversing device
07/17/2012US8220586 Noise-reduced aircraft engine and method for reducing noise emissions of an aircraft engine
07/17/2012CA2617719C Radially expanding turbine engine exhaust cylinder interface
07/11/2012EP2473727A1 Structuring assembly for an exhaust nozzle
07/11/2012EP2473712A1 A mounting apparatus
07/11/2012EP2242921B1 Control system for turbojet engine nacelle
07/11/2012EP1554484B1 Thrust reverser actuator with an automatic relock and lock drop prevention mechanism
07/11/2012CN102575616A Noise reduction device with chamber
07/11/2012CN102575586A Circuit for supplying fuel to an aircraft engine
07/10/2012US8215097 Rocket thruster assembly comprising load-balanced pintle valve
07/10/2012US8215096 Outlet device for a jet engine and a craft comprising such an outlet device
07/10/2012CA2536759C Induction coupled variable nozzle
07/05/2012WO2012092219A1 Flight vehicle, propulsion system and thrust vectoring system
07/05/2012WO2011144842A3 Multi-layer acoustic treatment panel
07/05/2012US20120167575 Rocket engine with extendable divergent
07/05/2012US20120167550 Thrust augmented gas turbine engine
07/04/2012EP2472089A2 Flade discharge in 2-d exhaust nozzle
07/04/2012EP2472067A1 Integration of a surface heat exchanger with controlled air flow in an airplane engine
07/04/2012CN102536514A Binary plug nozzle of turbofan engine with afterburning
07/04/2012CN102536513A System and method for operating a thrust reverser for a turbofan propulsion system
07/04/2012CN102536512A Method and apparatus for variable exhaust nozzle exit area
07/04/2012CN102536511A High thrust aircraft engine
07/04/2012CN101589217B Systems and methods for reducing noise from jet engine exhaust
07/03/2012US8210307 Sonic absorption device for an air pipeline of an aircraft, in particular of an air conditioning system of an aircraft
06/2012
06/30/2012CA2762397A1 Linear actuator and method of operation thereof
06/28/2012WO2012085379A1 Inner structure for an aircraft nacelle
06/28/2012US20120160933 Structuring assembly for an exhaust nozzle
06/28/2012US20120160600 Tubular acoustic insulating element
06/28/2012CA2821402A1 Inner structure for an aircraft nacelle
06/27/2012EP2071930B1 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area
06/27/2012EP2064434B1 Operational line management of low pressure compressor in a turbofan engine
06/26/2012US8205454 Convergent divergent nozzle with edge cooled divergent seals
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