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)
12/2012
12/11/2012US8327617 Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine
12/06/2012WO2012164189A1 Method for manufacturing a sound attenuation panel
12/06/2012WO2012164186A1 Nacelle for an aircraft bypass turbojet engine
12/06/2012US20120304621 Clamping system and method for thrust reverser attachment
12/06/2012DE102010007567B4 Kerndiffusor Core diffuser
12/06/2012CA2837635A1 Nacelle for an aircraft bypass turbojet engine
12/06/2012CA2832526A1 Method for manufacturing a sound attenuation panel
12/06/2012CA2778592A1 Clamping system and method for thrust reverser attachment
12/05/2012CN202578941U Bubble generator for underwater gas-liquid two-phase engine
12/05/2012CN102812273A Reverse thrust device
12/04/2012US8322653 Hybrid beam for a thrust reverser unit
12/04/2012US8322144 Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise
12/04/2012US8322127 Nozzle assembly with flow conduits
11/2012
11/29/2012US20120297791 Ceramic matrix composite turbine exhaust case for a gas turbine engine
11/29/2012US20120297779 Corrosion resistant catalysts for decomposition of liquid monopropellants
11/28/2012CN102804307A Circuit for detecting the positions of contactors in a turbine engine
11/28/2012CN102799739A Method for regulating and designing engine jet pipe throat area by taking installation performance into account
11/27/2012US8316646 Fan variable area nozzle for a gas turbine engine fan nacelle with drive ring actuation system
11/22/2012US20120292126 Method for processing a surface element
11/22/2012US20120291443 Rocket propulsion device and method for assembling rocket propulsion device
11/22/2012US20120291415 Dual function cascade integrated variable area fan nozzle and thrust reverser
11/21/2012EP2525069A2 Crack and delamination stoppers for aircraft propulsion system components
11/21/2012CN102792001A Aircraft propulsion system provided with reverse thrust means
11/21/2012CN101809311B Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
11/15/2012WO2012153074A1 Tail cone for a microjet rotary turbine engine
11/15/2012US20120285138 Aircraft gas-turbine engine with oil cooler in the engine cowling
11/15/2012DE102011101342A1 Fluggasturbinentriebwerk mit Ölkühler in der Triebwerksverkleidung Aircraft gas turbine engine with oil cooler in the engine cowling
11/15/2012CA2835353A1 Tail cone for a microjet rotary turbine engine
11/14/2012EP2522831A2 Turbojet engine with oil cooler in the engine nacelle
11/14/2012CN102777252A High-pressure gas source compression system
11/14/2012CN101297107B Turbofan engine for stol aircraft
11/13/2012US8307945 Gas-turbine exhaust cone
11/13/2012US8307659 Nozzle with guiding elements
11/08/2012US20120279225 Flow evacuation system for an aircraft engine
11/07/2012EP2519729A1 Exhaust for a gas turbine engine
11/07/2012EP2519724A2 Gas turbine engine and cooling system
11/07/2012CN102052254B Power generator utilizing wind energy and fuel chemical energy
11/06/2012US8302907 Hybrid torque box for a thrust reverser
11/01/2012US20120273611 Exhaust silencer with baffles
11/01/2012US20120272637 Replacing an aperture in a laminated component
10/2012
10/31/2012CN102762844A Gas-guiding pipe comprising a noise-attenuating covering with variable porosity
10/31/2012CN102760193A Method for adjusting and designing outlet area of engine jet pipe based on installation performance
10/31/2012CN102758704A Exhaust silencer with baffles
10/31/2012CN102758667A Integrated tailcone muffler assemblies and methods
10/30/2012US8297404 Soundproof exhaust pipe for a turbine engine
10/26/2012WO2012145141A1 Multi-degree of freedom resonator array
10/26/2012WO2012066210A3 Nacelle for an aircraft bypass turbojet engine
10/25/2012US20120269633 Closed gas generator and micro power unit including the same
10/24/2012EP2513463A1 Stub frame for a cascade thrust reverser structure
10/24/2012EP2512928A1 Supporting structure for thrust reverser, in particular having cascades
10/24/2012CN102753808A Secondary-air nozzle of a two-flow jet engine having separated flows including a grid thrust reverser
10/24/2012CN102753807A Device for ejecting gas from a gas turbine engine and gas turbine engine
10/24/2012CN102748160A Flexible connector assembly for flexible spraying pipe of solid rocket engine and manufacture method thereof
10/23/2012US8291710 Gas turbine engine exhaust nozzle having a composite article having a shape memory material member
10/18/2012WO2012140368A1 Thrust reverser for an aircraft jet engine
10/18/2012CA2831187A1 Thrust reverser for an aircraft jet engine
10/16/2012US8286654 Gas turbine engine inlet with noise reduction features
10/16/2012US8286416 Valve system for a gas turbine engine
10/11/2012US20120256051 Stub frame for a cascade thrust reverser structure
10/11/2012US20120256044 Flight vehicle, propulsion system and thrust vectoring system
10/11/2012US20120255806 Noise reduction of supersonic jet engines
10/10/2012EP2508716A2 Improvements in or relating to gas turbine engine transition ducts
10/09/2012US8285467 Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine
10/09/2012US8281603 Fastener assembly for connecting rocket engine nozzles
10/04/2012WO2012131209A1 Anti-fire seal assembly and nacelle comprising such a seal
10/04/2012US20120247110 Device for mixing fuel and air of a jet engine
10/04/2012CA2829267A1 Anti-fire seal assembly and nacelle comprising such a seal
10/03/2012EP2505791A1 Securing system and corresponding gas turbine engine
10/03/2012EP2504554A1 Assembly for an aircraft turbojet engine comprising a thrust reversal cowl
10/03/2012EP2504553A2 Nacelle assembly for a variable area fan nozzle of a gas turbine engine
10/03/2012EP2504552A2 Variable area fan nozzle with a bearing track
10/03/2012CN102712546A Low-thickness thermostructural composite material part, and manufacture method
09/2012
09/27/2012US20120240587 Noise reduction system
09/26/2012EP2501920A1 Thrust inverter
09/26/2012CN102695868A 飞行器控制系统 Aircraft Control System
09/26/2012CN101198785B Control system for the nacelle of a turboreactor
09/25/2012US8272202 Gas turbine engine fan variable area nozzle with swivalable insert system
09/20/2012WO2012125895A1 System and method for operating a precooler in an aircraft
09/20/2012WO2012123681A1 Turbomachine with fan(s) for aircraft, with mobile jet nozzle
09/20/2012WO2012097999A3 Method for the production of a sound absorber, especially for a gas turbine exhaust cone
09/20/2012WO2012097997A3 Gas turbine exhaust cone
09/20/2012US20120233983 Rocket Nozzles for Unconventional Vehicles
09/20/2012CA2829074A1 Turbomachine with fan(s) for aircraft, with mobile jet nozzle
09/19/2012EP2500270A2 Aircraft capable of hovering
09/19/2012EP2499341A1 Metal annular connecting structure for an aircraft turbine engine
09/18/2012US8268438 Component for use in streams of hot gas
09/18/2012CA2489627C Inboard cooled nozzle doublet
09/13/2012WO2012120227A1 Pipe having an upstream core having a sharp curvature
09/13/2012WO2012098322A3 Nacelle for an aircraft bypass turbojet engine
09/13/2012WO2012098321A3 Nacelle for an aircraft bypass turbojet engine
09/13/2012US20120228050 Helmholtz resonator for a gas turbine combustion chamber
09/13/2012US20120228049 Arrangement of a silencer on a combustion motor with improved coupling to the cylinder
09/12/2012EP2497934A1 Flow evacuation system for an aircraft engine
09/12/2012EP2496817A1 Reverse thrust device
09/07/2012WO2012117197A2 Air cushion aircraft
09/05/2012EP2495424A1 Noise reduction device with chamber
09/05/2012EP2495423A1 Noise reduction device
09/05/2012EP2493832A1 Low-thickness thermostructural composite material part, and manufacture method
09/05/2012CN102656357A Stub frame for a cascade thrust reverser structure
09/05/2012CN102656087A Supporting structure for thrust reverser, in particular having cascades
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