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