Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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10/10/2012 | CN101844621B Airborne combined cooling and heating and power system of multi-electric aircraft |
10/09/2012 | US8282037 Nacelle flow assembly |
10/04/2012 | WO2012135300A2 Airborne cooling system |
10/04/2012 | WO2012131211A1 Method of inspecting impacts observed in fan casings |
10/04/2012 | WO2012130418A1 Aircraft tail region with a cooling system installed in aircraft tail region |
10/04/2012 | CA2830834A1 Method of inspecting impacts observed in fan casings |
10/02/2012 | CA2471259C Nacelle inlet lip anti-icing with engine oil |
09/27/2012 | US20120241249 Panel for the acoustic treatment with a progressive thickness |
09/27/2012 | US20120241248 Two-stroke engine with a silencer |
09/27/2012 | DE102011015126A1 Flugzeugheckbereich mit einem in dem Flugzeugheckbereich installierten Kühlsystem Aircraft tail region with a cooling system installed in the aircraft tail region |
09/26/2012 | CN202449214U Protective cover |
09/26/2012 | CN102689691A Aircraft capable of hovering |
09/20/2012 | US20120233988 Aircraft capable of hovering |
09/19/2012 | EP2500270A2 Aircraft capable of hovering |
09/19/2012 | EP2500269A1 Aircraft capable of hovering |
09/19/2012 | CN102686481A Acoustic treatment panel having scalable thickness |
09/19/2012 | CN102686480A Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel together |
09/19/2012 | CN102673793A Exhaust ejector system of airplane auxiliary power unit |
09/19/2012 | CN102673792A Cocoon packaged fire-proof cover of auxiliary power unit |
09/13/2012 | WO2012120227A1 Pipe having an upstream core having a sharp curvature |
09/13/2012 | WO2012098322A3 Nacelle for an aircraft bypass turbojet engine |
09/13/2012 | WO2012098321A3 Nacelle for an aircraft bypass turbojet engine |
09/13/2012 | US20120228403 Assembly for an aircraft turbojet engine comprising a thrust reversal cowl |
09/12/2012 | EP2497713A2 Heat exchanger in a free air stream |
09/12/2012 | CN202429355U Engine cooling channel |
09/11/2012 | US8262018 Drag-optimised ram-air duct and process for controlling a mass flow of ambient air or cooling air through a ram-air duct |
09/11/2012 | CA2546685C Aircraft fluid cooling system and an aircraft provided with said system |
09/07/2012 | WO2012118516A1 Ceramic matrix composite structures, components formed therewith, and methods of producing |
09/07/2012 | CA2799049A1 Ceramic matrix composite structures, components formed therewith, and methods of producing |
09/05/2012 | CN202417680U Radiator for unmanned helicopter |
09/05/2012 | CN202414168U Multipurpose unmanned helicopter capable of effectively removing resonance |
09/04/2012 | US8256706 Integrated hypersonic inlet design |
08/23/2012 | WO2012110845A1 Aircraft with improved aerodynamic performance |
08/22/2012 | EP2488412A2 Flow body, in particular for aircraft |
08/21/2012 | CA2706815C Apparatus and method for starting a helicopter turbine engine using an electrical energy source and comprising reserve discharge means |
08/16/2012 | WO2012065713A3 Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |
08/15/2012 | EP2487111A1 Device for ventilating a compartment of an aircraft engine |
08/15/2012 | CN102632996A Device for ventilating a compartment of an aircraft engine |
08/09/2012 | WO2012104560A1 Method for manufacturing an air-intake structure for a turbojet-engine nacelle |
08/09/2012 | US20120199212 Isentropic compression inlet for supersonic aircraft |
08/09/2012 | CA2825982A1 Method for manufacturing an air-intake structure for a turbojet-engine nacelle |
08/08/2012 | EP2484591A2 Aircraft engine nozzle |
08/08/2012 | EP1718857B1 Integrated air inlet system for multi-propulsion aircraft engines |
08/07/2012 | CA2563815C Multi-engine aircraft |
08/01/2012 | EP2344381B1 Air intake for an aeroplane engine with unducted propellers |
08/01/2012 | EP1507971B1 Variable area thrust reverser nozzle |
08/01/2012 | CN202358306U Thermal protection structure for tail segment of aircraft |
08/01/2012 | CN102616382A Connecting device mainly suitable for connecting an engine of an aircraft nacelle and an air intake pipe |
07/26/2012 | WO2012098322A2 Nacelle for an aircraft bypass turbojet engine |
07/26/2012 | WO2012098321A2 Nacelle for an aircraft bypass turbojet engine |
07/26/2012 | US20120187214 Converging blocker door system for use with a thrust reverser |
07/26/2012 | CA2824369A1 Nacelle for an aircraft bypass turbojet engine |
07/26/2012 | CA2824367A1 Nacelle for an aircraft bypass turbojet engine |
07/25/2012 | CN102602542A Aircraft capable of lifting off in floating manner |
07/19/2012 | WO2012095592A1 Turbofan engine |
07/19/2012 | US20120181389 Passive control of ice shedding |
07/19/2012 | CA2819384A1 Turbofan engine |
07/18/2012 | EP2476618A2 Integrated bleed and engine controller |
07/18/2012 | EP2476617A1 Passive control of ice shedding |
07/11/2012 | EP2474474A2 Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly |
07/11/2012 | CN102562827A High-speed bearing cooling system of turbine/compressor for aviation and method and application thereof |
07/10/2012 | US8215589 Reversible space plane |
07/05/2012 | WO2012010116A3 Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature |
07/05/2012 | WO2011144842A3 Multi-layer acoustic treatment panel |
07/04/2012 | EP2222561B1 Aircraft cooling system |
07/04/2012 | CN202295291U 一种基于naca构型的飞机短舱进气口 An intake port configuration based naca aircraft nacelle |
07/04/2012 | CN202295290U Novel separating channel structure of air inlet channel |
07/03/2012 | US8210474 Multi-path inlet for aircraft engine |
06/30/2012 | CA2762598A1 Integration of a surface heat-exchanger with regulated air flow in an airplane engine |
06/28/2012 | WO2012085379A1 Inner structure for an aircraft nacelle |
06/28/2012 | DE102011112941A1 Engine assembly for aircraft, has engine that is arranged either before air wings or behind the air wings, where engine flame is directed around or on or below air wings if engine is arranged before air wings |
06/28/2012 | CA2821402A1 Inner structure for an aircraft nacelle |
06/27/2012 | CN102514715A Cooling channel of motor |
06/26/2012 | CA2472935C Device for reducing jet noise from a turbine engine |
06/14/2012 | WO2012077857A1 Airplane equipped with a wing booster |
06/14/2012 | CA2758211A1 Aircraft comprising a reversible rotary electrical machine |
06/13/2012 | EP2463197A1 Air intake for propulsion system of an aircraft with a structure withstanding overpressure and method for repairing an air intake of an aircraft propulsion system |
06/12/2012 | US8196704 Linear acoustic liner |
06/12/2012 | CA2585918C Drive installation for rotary-wing aircraft |
06/07/2012 | WO2012072457A1 An air intake system for an air vehicle |
06/07/2012 | CA2820122A1 An air intake system for an air vehicle |
06/06/2012 | EP2460729A1 An air intake system for an air vehicle |
06/06/2012 | CN101228069B Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
05/30/2012 | EP2457632A1 Inlet particle separator system |
05/30/2012 | CN202244089U Constant-speed turbine air outlet louver of plane |
05/30/2012 | CN102483170A 飞行器小余隙流体止回阀 Small aircraft fluid valve clearance |
05/30/2012 | CN102483169A 具有指引的飞行器流体止回阀组件 Aircraft fluid check valve assembly having Guidelines |
05/30/2012 | CN101573524B Nacelle for aircraft jet engine and aircraft including such nacelle |
05/29/2012 | CA2759191A1 Combination low spool generator and ram air turbine generator |
05/24/2012 | WO2012066211A1 Turbojet engine nacelle reinforcing structure |
05/24/2012 | WO2012066210A2 Nacelle for an aircraft bypass turbojet engine |
05/24/2012 | CA2816455A1 Turbojet engine nacelle reinforcing structure |
05/24/2012 | CA2816255A1 Nacelle for an aircraft bypass turbojet engine |
05/23/2012 | EP2454154A1 Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
05/23/2012 | CN102470929A Leading edge structure, in particular for the air intake of the nacelle of an aircraft engine |
05/23/2012 | CN101415607B Air inlet lip for a pod with electric defrosting |
05/22/2012 | US8181905 Aircraft engine nacelle with translating inlet cowl |
05/17/2012 | US20120118419 Aircraft low clearance fluid check valve |
05/16/2012 | EP2452876A2 Aircraft propulsion system and system for taxiing an aircraft |
05/16/2012 | DE102010051517A1 Flugzeugaußenhautwärmetauscher, Flugzeugkühlsystem und Verfahren zum Betreiben eines Flugzeugaußenhautwärmetauschers Aircraft outer skin heat exchanger, aircraft cooling system and method for operating an aircraft outer skin heat exchanger |