Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
09/2012
09/26/2012CN102689690A Flying saucer airplane provided with own force point
09/26/2012CN102689444A Dry preform, annular structure made of a composite material, and manufacturing method for the annular structure
09/26/2012CN101111419B Device for fastening passenger seats on a seat track break in an aircraft
09/25/2012US8274024 Control surface assemblies with torque tube base
09/25/2012CA2618858C Continuous fuselage connection
09/20/2012WO2012125233A1 Method and system for insulating frame member
09/20/2012US20120234979 Method and system for insulating frame member
09/20/2012US20120234978 Load transfer devices at a stringer run-out
09/20/2012US20120234977 Coupling structure for airframe components
09/20/2012US20120234975 Fairing transition and vehicle with a movable body and a fixed body comprising a fairing transition
09/20/2012DE102011001267A1 Airliner, has hydrophilic manifold connected with hot gas source through connector, and outlet arranged at end of hydrophilic manifold, where end of manifold is turned away from connector of hot gas source
09/19/2012EP2500706A1 Device for detecting impacts on a structure
09/19/2012EP2498973A2 Thermoplastic composite window panel for aircraft applications
09/19/2012EP2271477B1 Device for producing a component and method
09/19/2012EP1750929B1 Structural panels for use in aircraft fuselages and other structures
09/19/2012CN202439303U Ultra-light glass cotton felt with ultralow volume weight
09/19/2012CN102686478A Adaptive structural core for morphing panel structures
09/19/2012CN102673773A Vehicle panel provided with mobile window, and associated vehicle
09/19/2012CN102673052A Hot-stamping preparation method of Al layer coating type TPU (thermoplastic polyurethane) film friction reduction micro-groove for airship skin
09/18/2012US8271179 System and method for aiding airdrop computations
09/18/2012US8267354 Fitting
09/18/2012US8267352 Structure of the load introduction zone in the rear end of an aircraft
09/18/2012CA2632264C Aircraft pressurized cabin door made of fiber composite
09/18/2012CA2547756C Insulation arrangement for the internal insulation of a vehicle
09/14/2012DE202009018690U1 Dekompressionselementbefestigungssystem für ein Flugzeug Dekompressionselementbefestigungssystem for an aircraft
09/13/2012WO2012121825A1 Diamond shaped window for a composite and/or metallic airframe
09/13/2012WO2012121813A1 Hoop load bearing aircraft transparency
09/13/2012WO2012098331A3 Fish joint device having an improved mechanical hold
09/13/2012WO2012085359A3 Aluminium-copper-lithium alloy with improved compressive strength and toughness
09/13/2012WO2012061498A3 Method and apparatus for making and using a self-sealing fastener
09/13/2012US20120228431 Fastening arrangement for fastening a component on a fuselage
09/13/2012US20120228430 Torsion stop deployment system for airborne object
09/13/2012US20120228429 Vehicle door lock
09/13/2012US20120228428 Hoop load bearing aircraft transparency
09/13/2012US20120228427 Pressure fuselage of an aircraft with dome-shaped pressure bulkhead
09/13/2012US20120227325 Vehicle panel provided with a movable window, and an associated vehicle
09/13/2012CA2826143A1 Diamond shaped window for a composite and/or metallic airframe
09/12/2012EP2497623A1 Jig for manufacture of composite material structure
09/12/2012EP2496476A2 Aircraft cabin comprising a flight deck security system
09/12/2012EP2496411A1 Electromagnetic hazard protector for composite materials
09/12/2012EP2496410A1 Electromagnetic hazard protector for composite materials
09/12/2012CN202429343U Front body of unmanned aerial vehicle and unmanned aerial vehicle
09/12/2012CN102666274A Device and method for maintaining parallelism between the two glazings of an aircraft double glazing
09/12/2012CN102666273A Aircraft ring frame and method for the production thereof
09/12/2012CN102658863A Flying object anti-drag acceleration design
09/12/2012CN102658694A Preparation method of TiO2 plated type PU (polyurethane) or TPU (thermoplastic polyurethane) film anti-drag micro groove for airship skin
09/12/2012CN102658693A Hot-pressing preparation method for aluminum-coated TPU (thermoplastic polyurethane) film resistance reduction microgrooves for airship skin
09/11/2012US8262823 High strength; lightweight; radiation transparent; preimpregnated tape with fibers; multilayer; with metal sheet; aircraft
09/11/2012US8262025 Aircraft structure
09/11/2012US8262024 Aircraft frames
09/11/2012US8262023 Aircraft frame element connected to an air-conditioning system
09/11/2012CA2671602C Auxiliary power unit inlet door actuation mechanism
09/07/2012WO2012116918A1 Door frame construction, fuselage portion and aircraft or spacecraft
09/07/2012WO2012116739A1 A draining device
09/07/2012CA2828130A1 A draining device
09/06/2012US20120223188 Movable connecting plate for connecting two overhead storage compartment elements
09/06/2012US20120223187 Diamond shaped window for composite and/or metallic airframe
09/06/2012US20120223183 Aerospace articles made from quasi-isotropic chopped prepreg
09/05/2012CN202414154U Non-bearing shifting-type quick-release covering cap device
09/05/2012CN202414153U Multi-purpose unmanned aerial vehicle airframe
09/05/2012CN101842267B Aeroplane with improved acoustic comfort
09/04/2012US8256716 Aircraft flight termination system and method
09/04/2012US8256715 Devices, systems and methods for modular payload integration for unmanned aerial vehicles
09/04/2012US8256714 Modularized airplane structures and methods
09/04/2012US8256713 Aircraft fuselage section
09/04/2012US8256702 Aircraft landing gear provided with at least one noise reducing means
08/2012
08/30/2012WO2012114022A1 Heat exchanger built into a wall of an aircraft
08/30/2012US20120217368 Fastener device, a seat provided with said device, and a vehicle
08/30/2012US20120217347 aircraft fuel tank access cover and an aircraft fuel tank
08/30/2012US20120217346 Foam window mount having an electric conductive layer over a light blocking layer
08/30/2012US20120217345 Observation port and a helicopter cabin
08/30/2012DE102011004844A1 Türrahmenverbund, Rumpfabschnitt sowie Luft- oder Raumfahrzeug Door frame assembly, body section and aircraft or spacecraft
08/30/2012DE102009012429B4 Bodenmodul eines Frachtdecks im Rumpf eines Flugzeugs Base module of a cargo deck in the fuselage of an aircraft
08/29/2012EP2492197A1 Attachment device, seat provided with said device and vehicle
08/29/2012EP2492190A2 Decompression arrangement for an aircraft
08/29/2012EP2492189A2 Observation channel and helicopter cabin
08/29/2012EP2492087A1 Composite structure comprising a first section, a second section and a curved corner
08/29/2012CN102649474A Decompression arrangement for an aircraft
08/28/2012US8251314 Cargo receiving arrangement for an aircraft hold
08/28/2012US8251312 Method and system for control of upstream flowfields of vehicle in supersonic or hypersonic atmospheric flight
08/24/2012CA2763175A1 Panel member, aircraft main wing, and method for forming panel member
08/23/2012WO2012112212A1 Common bulkhead for composite propellant tanks
08/23/2012WO2012111704A1 Carbon-fiber-reinforced plastic structure and method for producing same
08/23/2012WO2012110845A1 Aircraft with improved aerodynamic performance
08/23/2012WO2012110569A2 Door system having an actuator
08/23/2012WO2012110568A1 Arrangement for passing a line in a load-free manner through a pressure frame of a fuselage of an aircraft or spacecraft
08/23/2012US20120213955 Method for manufacturing a shell body and corresponding body
08/23/2012US20120211605 System and method for converting a passenger aircraft to a cargo aircraft
08/23/2012US20120211602 Frame for an opening provided in an aircraft fuselage
08/23/2012US20120211601 Aircraft nose section including a lock for accessing the cockpit
08/23/2012US20120211597 System for attaching an impeller engine
08/23/2012DE102011011976A1 Dekompressionsanordnung für ein Luftfahrzeug Decompression assembly for an aircraft
08/23/2012DE102011004385A1 Anordnung zum lastfreien Durchführen einer Leitung durch einen Druckspant eines Rumpfes eines Luft- oder Raumfahrzeuges Arrangement for the load-free management of a line through a pressure frame of a fuselage of an aircraft or spacecraft
08/23/2012DE102010048365B4 Flächengebilde und Flugzeugrumpf mit einem derartigen Flächengebilde Fabrics and fuselage with such fabrics
08/23/2012DE102010019380B4 Leitungshalter zur Befestigung eines Leitungsstrangs Conductor holder for attaching a cable loom
08/23/2012CA2827396A1 Carbon-fiber-reinforced plastic structure and method for producing same
08/22/2012EP2489590A1 Wing panel and aircraft main wing
08/22/2012EP2489471A1 Stringer manufacturing method
08/22/2012EP2488410A2 Aircraft elevator system and method
08/22/2012CN102648129A Front portion of an aircraft, comprising a vestibule for accessing the cockpit
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