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