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)
01/2010
01/07/2010US20100000220 Fan variable area nozzle with electromechanical actuator
01/07/2010US20100000219 Systems and Methods for Supplying Cooling Air to a Gas Turbine
01/07/2010DE112007001683T5 Kernreflexdüse für eine Turbofanmaschine Kernreflexdüse for a Turbofanmaschine
01/07/2010CA2729685A1 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
12/2009
12/31/2009US20090326783 Fluid-powered thrust reverser actuation system speed control
12/31/2009US20090321561 Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle
12/31/2009US20090320488 Gas turbine engine with noise attenuating variable area fan nozzle
12/31/2009US20090320487 Systems and methods for reducing noise from jet engine exhaust
12/31/2009US20090320486 Duplex tab exhaust nozzle
12/31/2009US20090320446 Performance improvements for pulse detonation engines
12/31/2009US20090320445 Method and device for the detection of a thrust dissymmetry of an aircraft during a braking
12/31/2009DE102008030020A1 Thermokinetic engine e.g. ramjet engine, for actuating airplane, has combustion chamber found completely in air lock, where increased oxygen content is supplied during supply of air into chamber at specific temperature
12/30/2009WO2009133272A3 Device for reducing the noise generated by an aircraft jet engine with fluid jets of the same orientation
12/30/2009EP2138697A2 Aft cascade ring with flow deflector portion, corresponding thrust reverser cascade assembly and aircraft engine nacelle
12/30/2009EP2138696A1 Gas turbine engine with noise attenuating variable area fan nozzle
12/30/2009EP2137394A1 Device for varying the cross section of a secondary nozzle associated with a gate reverser and jet smoothing device
12/30/2009EP2078152B1 Cascade-type thrust reverser for jet engine
12/30/2009CN100575690C Reverse thrust device including locking mechanism and producing method thereof
12/24/2009US20090314887 Thrust reverser cascade assembly and aft cascade ring with flow deflector portion
12/24/2009US20090314885 System, method and apparatus for fluidic effectors for enhanced fluid flow mixing
12/24/2009US20090313998 Axially split nozzle liner for convergent nozzle
12/23/2009WO2009133273A3 Device with secondary jets reducing the noise generated by an aircraft jet engine
12/23/2009EP2134950A1 Pintle-controlled propulsion system with external ring actuator
12/23/2009EP2134949A1 Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system
12/23/2009CN100572882C Full port externally gimbal joint
12/17/2009WO2009150312A1 Electric thruster for a spacecraft
12/16/2009EP2132427A2 Nacelle for turbojet jet fitted with a single door thrust reverser system
12/16/2009EP2132426A1 Cmc mixer with structural outer cowling
12/16/2009CN101605978A Method of manufacturing a CMC flow mixer lobed structure for a gas turbine aeroengine
12/15/2009US7631486 Thrust orienting nozzle
12/10/2009WO2009147333A1 Method for synchronizing the actuators of a movable thrust reverser cowl
12/10/2009US20090301094 Gas turbine engine exhaust nozzle having a composite article having a shape memory material member
12/10/2009DE102008025826A1 Device for reduction of jet noise generated by nozzle, particularly by jet engine, has nozzle, where one or more units are provided for active boundary layer impact of nozzle flow before leaving nozzle
12/09/2009EP2131179A2 An apparatus and method for evaluating a hydrocarbon to determine the propensity for coke formation
12/09/2009EP2129901A1 Thrust reverser for a jet engine
12/09/2009EP2129878A2 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained
12/09/2009CN101600623A Jack with integrated locking device
12/08/2009US7628356 Yaw control device for a nozzle having a rectangular outlet section
12/03/2009WO2009125157A3 Turbofan engine nacelle
12/03/2009WO2009112749A3 Thrust reverser for bypass turbojet engine nacelle
12/03/2009US20090297338 Variable area nozzle assisted noise control of a gas turbine engine
12/03/2009DE102008023052A1 Combustion chamber wall for combustion chamber, has inner wall, outer wall and cooling channel located between inner wall and outer wall, where bridges are arranged and formed between inner wall and outer wall
12/02/2009EP2126322A2 Self-calibration method for the electric jacks of a turbojet nacelle
12/02/2009EP2126321A1 Gas turbine comprising a guide ring and a mixer
12/02/2009CN101595292A Method for controlling electric motors of a thrust reverser
12/02/2009CN100564859C Method of reducing noise emissions at the rear of a turboshaft engine and turboshaft engine thus improved
12/01/2009US7624579 Convergent divergent nozzle with supported divergent seals
12/01/2009US7624567 Convergent divergent nozzle with interlocking divergent flaps
11/2009
11/26/2009WO2009142674A1 Rocket nozzles for unconventional vehicles
11/26/2009US20090288389 Integral thrust vector and roll control system
11/26/2009US20090288387 Gas turbine engine bifurcation located in a fan variable area nozzle
11/26/2009US20090288386 Tri-body variable area fan nozzle and thrust reverser
11/26/2009DE102008022271A1 Nozzle i.e. jet-nozzle, for e.g. gas turbine of aircraft, has one-piece tubular body including wall that forms convergent and divergent channel parts by radial contraction of cross-section dimension of nozzle
11/25/2009EP2123894A1 Jet flow discharge nozzle and jet engine
11/25/2009EP2121435A1 Jack with integrated locking device
11/25/2009CN101589217A Systems and methods for reducing noise from jet engine exhaust
11/24/2009US7621371 Method for attenuating the noise of a turbofan
11/19/2009WO2009138613A1 Wall cooling device
11/19/2009WO2009138598A2 Method and device for implementing the thrust reversers of an aircraft
11/19/2009WO2009138597A1 Dual-flow turbine engine for aircraft with low noise emission
11/19/2009WO2009138068A1 Mixer nozzle structure
11/19/2009US20090282806 Integrated airbreathing and non-airbreathing engine system
11/19/2009DE102008023816A1 Mischdüsenaufbau Mixing nozzle assembly
11/19/2009CA2721381A1 Wall cooling device
11/19/2009CA2721378A1 Method and device for implementing the thrust reversers of an aircraft
11/19/2009CA2721227A1 Dual-flow turbine engine for aircraft with low noise emission
11/18/2009EP2118477A1 Device for acoustically treating turbine and combustion noise
11/18/2009EP2118476A2 Method for controlling electric motors of a thrust reverser
11/18/2009EP2118475A2 Systems and methods for reducing noise from jet engine exhaust
11/18/2009EP2118474A2 Method of manufacturing a cmc flow mixer lobed structure for a gas turbine aeroengine
11/17/2009US7617685 Quick change fastener system for attaching liner bracket to convergent flap and seal in turbine nozzle
11/12/2009WO2009136096A2 Bypass turbojet engine nacelle
11/12/2009US20090277714 Gas turbine exhaust sound suppressor and associated methods
11/12/2009US20090277181 Aircraft propulsion unit that comprises an exhaust pipe with a scalloped trailing edge
11/12/2009CA2719155A1 Bypass turbojet engine nacelle
11/11/2009EP2116714A1 Low noise aircraft
11/11/2009EP2115290A2 Nacelle for aircraft jet engine and aircraft including such nacelle
11/11/2009EP2115289A1 Gas turbine engine with rotationally overlapped fan variable area nozzle
11/11/2009CN101576025A Multi-mode spraying pipe with adjustable throat for ramjet engine
11/10/2009US7614236 Positioning bridge guide and its utilisation for the nozzle support pipe of a turboprop
11/05/2009WO2009133273A2 Device with secondary jets reducing the noise generated by an aircraft jet engine
11/05/2009WO2009133272A2 Device for reducing the noise generated by an aircraft jet engine with fluid jets of the same orientation
11/05/2009WO2009133271A2 Device for reducing noise generated by an aircraft jet engine with curve ducts
11/05/2009WO2009106763A3 Twelve-hour structure for thrust reverser, in particular with grids
11/04/2009EP2113649A2 A gas turbine engine exhaust nozzle having a composite article comprising a shape memory material member
11/04/2009EP1485600B1 Duplex mixer exhaust nozzle
11/03/2009US7610747 Side thruster module
10/2009
10/29/2009WO2009131793A1 Exhaust washed structure and associated composite structure and method of fabrication
10/29/2009WO2009092872A3 Monitoring system and monitoring method
10/29/2009US20090269497 Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications
10/29/2009US20090266642 Engine Assembly, Acoustical Liner And Associated Method Of Fabrication
10/29/2009CA2713168A1 Exhaust washed structure and associated composite structure and method of fabrication
10/28/2009EP2112362A2 Rear fan case for a gas turbine engine
10/28/2009EP1343956B1 Bypass duct fan noise reduction assembly
10/27/2009US7607306 Infrared suppressor apparatus and method
10/27/2009US7607305 One-piece baffle infrared suppressor apparatus and method
10/22/2009DE102008020198A1 Nozzle extension for rocket engine, has nozzle cover provided with two shell elements made of ceramic fiber reinforced composite material, where shell elements are fixed relative to each other
10/21/2009EP2109712A2 Aircraft nacelle incorporating a thrust-reversing device
10/21/2009EP2032830B1 Guiding carrier for jet engine linings
10/20/2009US7603842 Method for reducing the nonsteady side loads acting on a nozzle of a rocket engine
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