Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
08/2012
08/22/2012CN102642611A Actively deformed stressed-skin structure based on pneumatic muscles
08/22/2012CN102642610A Mofei private plane
08/22/2012CN102642609A Connecting device of wing box rectification covering cap
08/22/2012CN101578220B Section of aircraft fuselage and aircraft including one such section
08/21/2012US8246770 Copper grid repair technique for lightning strike protection
08/21/2012US8245981 Ice shed reduction for leading edge structures
08/21/2012US8245977 Apparatus for the pivotal fastening of an active surface, in particular a spoiler on a wind tunnel model of an aircraft
08/21/2012US8245976 Door assembly for laminar flow control system
08/21/2012US8245975 Load-supporting and damage-tolerant laminated aircraft window
08/21/2012US8245974 Drainage device, aircraft, and method for letting out a fluid that is present between the exterior skin and the interior lining of an aircraft
08/21/2012US8245973 Methods and systems for improving aircraft visibility
08/21/2012US8245971 Curved element, wing, control surface and stabilizer for aircraft
08/16/2012US20120207968 Selective tinting method
08/15/2012EP2487107A1 Anti-condensation method and device for aircraft
08/15/2012EP2487106A1 Composite material structure, as well as aircraft wing and fuselage provided therewith
08/15/2012EP2485941A2 Pressure fuselage of an aircraft comprising a tail-face pressure calotte
08/15/2012CN102639394A A controllable buoyancy system
08/15/2012CN101189118B Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft
08/14/2012US8240608 Device for installing windshield panes
08/14/2012US8240607 Aircraft-fuselage assembly concept
08/14/2012US8240606 Integrated aircraft floor with longitudinal beams
08/13/2012DE202012006668U1 Flugzeugrumpf-Öffnung mit automatischer Evakuierung der Passagiere im Notfall. Fuselage opening with automatic passenger evacuation in an emergency. Ein-und Ausstieg erfolgt ohne Flugzeugtüren, über die hintere Flugzeugrumpf-Öffnung. Entry and exit is made without aircraft doors on the rear fuselage opening.
08/09/2012WO2012105691A1 Composite material structure, and aircraft wing and fuselage provided therewith
08/09/2012WO2012105415A1 Composite material structure, and aircraft wing and fuselage provided therewith
08/09/2012WO2012104182A1 Fuselage segment for a fuselage of an aircraft, aircraft fuselage and aircraft
08/09/2012WO2012104064A2 Aircraft interior component system and method for mounting an interior component system in an aircraft
08/09/2012WO2012052589A3 Hermetic fitting for holding the vertical stabiliser of the tail unit of an aircraft
08/09/2012US20120199269 Contact Stiffeners for Structural Skins
08/09/2012DE102011010539A1 Aufrüstvorrichtung und Verfahren zur Herstellung einer aus einem Faserverbundwerkstoff bestehenden Rumpftonne für ein Luftfahrzeug Aufrüstvorrichtung and method for making a fiber consisting of a composite material for an aircraft fuselage barrel
08/09/2012CA2815966A1 Composite material structure, and aircraft wing and fuselage provided therewith
08/08/2012EP2484585A1 Window mounted raft system
08/08/2012EP2484584A2 Aircraft frame and method for obtaining it
08/08/2012EP2344378B1 System and method for integrally forming a substructure element with a fiber metal laminate
08/08/2012EP2219941B1 Interconnection device connecting an aircraft internal structure component to the fuselage of this aircraft
08/08/2012EP2219940B1 Safety cabin system, method for manufacture and use
08/08/2012EP2051905B1 Aircraft tail cone
08/08/2012EP2040979B1 Method, apparatus and plant for manufacturing shell structures
08/08/2012CN101568468B Wing/fuselage connection for an aircraft
08/08/2012CA2763186A1 Methods and apparatus for mechanically joining metal components and composite components
08/07/2012CA2495989C Method and apparatus for machining by fenestration of thin, non-developable panels
08/02/2012WO2012102789A1 Composite structures having integrated stiffeners with smooth runouts and method of making the same
08/02/2012WO2012101439A1 Stringer, aircraft wing panel assembly, and method of forming thereof
08/02/2012WO2012101313A2 Flexible, fire-resistant apu drain device
08/02/2012WO2012100985A1 Door assembly with two door leaves
08/02/2012US20120193476 Removable fastener device equipped with attachment means for attaching an external load and with fastener means for fastening said attachment means to an aircraft, an associated aircraft, and an associated method
08/02/2012US20120193475 Connector for stiffening frames between an aircraft fuselage and a wing box
08/02/2012US20120193474 Window Mounted Raft System
08/02/2012US20120193472 Stairway for an aircraft
08/02/2012US20120193471 Modular adapter plate system
08/02/2012DE102011009806A1 Rumpfsegment für einen Luftfahrzeugrumpf, Luftfahrzeugrumpf und Luftfahrzeug Fuselage section for an aircraft fuselage aircraft fuselage and aircraft
08/02/2012DE102007046478B4 Blechlaminat, insbesondere für Rumpfhautbleche für Flugzeuge Laminations, in particular for fuselage panels for aircraft
08/02/2012DE102007044388B4 Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs Pressure bulkhead and method for dividing an aircraft or spacecraft
08/02/2012DE102007021076B4 Interkostal für ein Luft- oder Raumfahrzeug Intercostal for an aircraft or spacecraft
08/02/2012DE102007003277B4 Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen Fuselage of an aircraft or spacecraft in CFRP-metal hybrid construction with a metal frame
08/02/2012DE102006019123B4 Bodenstruktur für einen Rumpf Soil structure for a fuselage
08/02/2012CA2822577A1 Composite structures having integrated stiffeners with smooth runouts and method of making the same
08/01/2012EP2482352A2 Sinkless thermoelectric energy generator
08/01/2012EP2481768A2 Aircraft sealant
08/01/2012EP2481668A1 Connection of stiffening frames between an aircraft fuselage and a wing box
08/01/2012EP2481667A1 Stiffened structure including an opening
08/01/2012EP2200899B1 Splicing of omega-shaped stiffeners at a circumferential joint in an aircraft fuselage
08/01/2012EP1748922B1 Composite barrel sections for aircraft fuselages
08/01/2012CN102616379A Fastener device, associated aircraft, and associated method
08/01/2012CN102616366A Connection of stiffening frames between an aircraft fuselage and a wing box
08/01/2012CN102616365A Stiffened structure integrating an opening
07/2012
07/31/2012US8231751 Repair technique for lightning strike protection
07/31/2012US8231081 Electronic display mount
07/31/2012US8231080 Distributing power in systems having a composite structure
07/31/2012US8230770 Apparatus to energetically remove a ballistic tolerant window
07/31/2012CA2765085A1 Stiffened structure integrating an orifice
07/31/2012CA2438417C Lightweight structural component made of metallic ply materials
07/26/2012WO2012098331A2 Fish joint device having an improved mechanical hold
07/26/2012US20120187248 Method and device for the installation of systems, and a freight loading system
07/26/2012US20120187247 Manhole assembly in the lower skin of an aircraft wing made of a composite material
07/26/2012US20120187245 Fuselage segment, and method for the production of a fuselage segment
07/26/2012DE102011009481A1 Türanordnung mit zwei Türblättern Door assembly with two door leaves
07/26/2012DE102007025984B4 Bodenschienenbeschlag für Flugzeugsitze Bottom rail fitting for aircraft seats
07/26/2012CA2824375A1 Fish joint device having an improved mechanical hold
07/25/2012EP2477891A2 Covering device for an interior of an aircraft and a method for covering an interior of an aircraft
07/25/2012EP2477890A1 Removable horizontal stabilizer for helicopter
07/25/2012CN102612466A Fuselage element comprising a fuselage segment and junction means
07/25/2012CN102602546A Aircraft stringer positioning method and mechanism
07/25/2012CN102602544A Aircraft stringer positioning mechanism
07/25/2012CN102602528A Orthogonal grating cylindrical shell provided with reinforcement ribs and circular opening and made of composite materials
07/24/2012US8226039 Vibration isolation devices and associated systems and methods
07/24/2012US8226038 Microvanes for aircraft aft body drag reduction
07/24/2012US8226037 Aircraft door assembly, and aircraft fuselage comprising such an aircraft door assembly
07/24/2012US8226036 ECU mounting system for a light aircraft
07/24/2012US8226035 Blended wing aircraft
07/24/2012US8226034 Cargo deck and a method for assembling said deck
07/24/2012US8226032 Pivoting equipment carrier in combination with a modified luggage rack
07/24/2012CA2489783C Rivet assembly apparatus and process for assembling panels, specifically aircraft fuselage, using the apparatus
07/21/2012CA2762748A1 Vent stringer and aircraft main wing
07/19/2012WO2012097176A1 Systems and methods for installing motorized window shade mechanism in aircraft
07/19/2012WO2012095300A1 Support strut for supporting primary components as well as guiding systems with such a support strut and method for manufacturing such a support strut
07/19/2012US20120181797 Latching Mechanism
07/19/2012CA2824054A1 Systems and methods for installing motorized window shade mechanism in aircraft
07/18/2012EP2476162A1 Radome and device for attaching said radome to an aircraft
07/18/2012EP2415662B1 Fuselage structure made of composite material
07/18/2012CN102596714A Covering device for an interior of an aircraft and a method for covering an interior of an aircraft
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