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)
02/2013
02/14/2013CA2842059A1 Reverser having movable cascades, and translatably variable nozzle
02/13/2013EP2557304A1 Jet flow nozzle and jet engine
02/13/2013EP2556237A1 Aircraft propulsion system provided with reverse thrust means
02/13/2013CN102933829A Self-mounted cascade for a thrust reverser
02/13/2013CN102933828A Nacelle for an aircraft engine with variable cross-section nozzle
02/13/2013CN102926888A Stealth exhaust system
02/12/2013US8371806 Gas turbine engine having core auxiliary duct passage
02/12/2013US8371521 Low noise exhaust ducting system
02/12/2013US8371124 Jet nozzle plug with varying, non-circular cross sections
02/12/2013US8371104 System and apparatus for vectoring nozzle exhaust plume from a nozzle
02/12/2013CA2502374C Methods and apparatus for exhausting gases from gas turbine engines
02/07/2013WO2013017771A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle
02/07/2013WO2013017756A1 Double-acting linear actuator
02/07/2013CA2842537A1 Double-acting linear actuator
02/07/2013CA2841167A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle
02/06/2013CN102918252A Thrust reverser having a lockable variable nozzle section
02/06/2013CN102918251A Hydraulic control system for thrust reversal device
01/2013
01/31/2013WO2013014365A1 Device for connecting a front frame to a fan casing
01/31/2013WO2013014350A1 Rear frame for a deflection cascade-type thrust reverser structure for a turbo jet engine nacelle
01/31/2013US20130026301 Nacelle for variable section nozzle propulsion unit
01/31/2013US20130025962 Gas-turbine exhaust cone with three-dimensionally profiled partition wall and plate-type wall element
01/31/2013US20130025260 Aircraft propulsion system provided with reverse thrust means
01/31/2013US20130025259 Ducted fan gas turbine assembly
01/31/2013DE102011108533A1 Abgasturbinenkonus mit dreidimensional profilierter Trennwand sowie plattenartiges Wandelement Turbine exhaust cone with three-dimensionally profiled partition wall and plate-like element
01/31/2013CA2842064A1 Device for connecting a front frame to a fan casing
01/30/2013EP2551507A2 Waste gas turbine cone with three dimensional profiled partition wall and board-shaped wall element
01/30/2013EP2551506A2 Thrust reverser for a turbofan engine
01/30/2013EP2550471A1 Reverse thrust device
01/30/2013CN202707277U Air exhaust heating nozzle used for gas turbine air intake filter
01/30/2013CN102906407A Assembly including a reverse thrust device and system for actuating said device
01/30/2013CN102900564A Blade top air injection stability controller for axial flow compression system
01/30/2013CN102900471A Efficient low-resistant structural or efficient energy-gathered structural or efficient engine
01/29/2013US8359825 Microjet creation and control of shock waves
01/29/2013CA2729685C Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
01/26/2013CA2783790A1 Gas turbine engine with ejector
01/24/2013WO2013012316A1 Turbofan engine with convergent - divergent exhaust nozzle
01/24/2013US20130020408 Cable-Actuated Variable Area Fan Nozzle with Elastomeric Seals
01/24/2013CA2875090A1 Turbofan engine with convergent - divergent exhaust nozzle
01/23/2013EP2549105A1 Synthetic jet apparatus
01/23/2013EP2548804A1 Nacelle for propulsion assembly with variable ejector nozzle
01/23/2013CN102893010A Airplane jet engine thrust reverser having gratings or cascades
01/23/2013CN102893009A Device for reducing the noise emitted by the jet of an aircraft propulsion engine
01/22/2013US8356483 Gas turbine engine systems involving variable nozzles with sliding doors
01/22/2013US8356468 Gas turbine engine nozzle configurations
01/22/2013CA2703108C Passive cooling system for auxiliary power unit installation
01/16/2013EP2546505A2 A Gas Turbine Engine Exhaust Nozzle
01/16/2013CN102877982A Thrust reverser of aero-engine
01/15/2013US8353164 Gas turbine engine having slim-line nacelle
01/15/2013CA2703166C Passive cooling system for auxiliary power unit installation
01/10/2013US20130009005 Reverse thrust device
01/10/2013US20130009004 Internal gas turbine propulsion thrust reverser
01/10/2013US20130008147 Aircraft gas turbine with variable bypass nozzle
01/10/2013US20130008145 Integrated electric variable area fan nozzle thrust reversal actuation system
01/10/2013DE102011106959A1 Fluggasturbine mit variabler Nebenstromdüse Aircraft gas turbine with variable Nebenstromdüse
01/09/2013EP2543864A2 Aircraft propulsion assembly with a heat shield for thermal protection of a rear aerodynamic fairing of a pylon and a cooling method for the heat shield
01/09/2013EP2543863A2 Integrated variable area fan nozzle and thrust reversal actuation system
01/09/2013EP2543862A2 Thrust reverser
01/09/2013EP2543861A2 Gas turbine engine with variable bypass nozzle
01/09/2013EP2543600A2 Sound absorber for an auxiliary engine of an aircraft
01/09/2013EP2542772A1 Flow mixer and corresponding gas turbine engine
01/09/2013CN102865156A Integrated variable area fan nozzle and thrust reversal actuation system
01/08/2013US8347601 Device for pivoting at least one pivotable element in a gas turbine engine
01/08/2013CA2713168C Exhaust washed structure and associated composite structure and method of fabrication
01/03/2013WO2013001185A2 Tertiary locking assembly for a thrust reverser
01/03/2013DE102011105955A1 Jet propulsion unit, has thrust nozzle consisting of two parts, where one part is tapered in flow direction and another part is designed as diffuser such that gas flows through thrust nozzle at subsonic speed
01/03/2013CA2831488A1 Tertiary locking assembly for a thrust reverser
01/02/2013EP2540984A2 Impingement Cooled Nozzle Liner
01/02/2013CN102859168A Turbojet engine nacelle
01/02/2013CN102858636A Reverser having doors
01/02/2013CN102858634A Unit for an aircraft thruster
01/02/2013CN102852668A Self-air-entraining jet mechanism for axial fan/compressor
01/01/2013US8341934 Infrared suppression system with spiral septum
12/2012
12/27/2012WO2012175841A1 Actuating assembly for a thrust reverser of an aircraft engine
12/27/2012WO2012175329A1 Device and method for carrying out a temperature compensation between turbine housing regions that are at different temperatures
12/27/2012CA2837612A1 Actuating assembly for a thrust reverser of an aircraft engine
12/26/2012EP2537171A1 Circuit for detecting the positions of contactors in a turbine engine
12/26/2012EP2536941A2 Articulating slider track
12/26/2012CN102844557A System for controlling an electrical device of a nacelle
12/26/2012CN102844527A Exhaust gas diffuser of gas turbine
12/26/2012CN102844239A Arrangement of thrust reverser flap link rods on internal fixed structure of turbojet engine nacelle
12/20/2012WO2012173546A1 Variable jet engine outlet with a mainly circle sector-formed cross section
12/20/2012US20120318380 Turbojet engine nacelle provided with a cooling assembly for cooling a component
12/20/2012US20120317957 Aircraft powerplant
12/20/2012US20120317956 Constant Volume Combustion Chamber
12/19/2012EP2535547A2 Apparatus for linear actuation of flow altering components of jet engine nozzle
12/19/2012EP2534361A1 Gas-guiding pipe comprising a noise-attenuating covering with variable porosity
12/19/2012EP2534360A1 Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser
12/19/2012EP2534359A1 Aircraft control system
12/19/2012EP2534358A1 Device for ejecting gas from a gas turbine engine and gas turbine engine
12/19/2012CN202611925U Engine of high-thrust aircraft
12/19/2012CN202611856U High-pressure air source compression system
12/19/2012CN102828850A Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
12/18/2012CA2654751C Engine exhaust system
12/18/2012CA2652685C Engine exhaust system with directional nozzle
12/18/2012CA2495166C Axisymmetric flap on gas turbine exhaust centerbody
12/18/2012CA2460598C Confluent variable exhaust nozzle
12/17/2012CA2779811A1 Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
12/12/2012EP2532872A2 Clamping system and method for thrust reverser attachment
12/12/2012CN202596922U Venturi tube
12/12/2012CN102822492A Jet flow nozzle and jet engine
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