Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
02/2012
02/16/2012DE102010039135A1 Vorrichtung zur Halterung von Systemen sowie Luft- oder Raumfahrzeug Device for holding systems and aircraft or spacecraft
02/16/2012DE102010036982A1 Frachtraumboden sowie Flugzeug mit einem Frachtraumboden Cargo compartment floor and the aircraft with a cargo compartment floor
02/16/2012DE102010034080A1 Beschlagfreies Fahrzeugfenster Free fitting vehicle window
02/16/2012CA2801701A1 System and method for supporting a load across a plurality of non-intersecting beams
02/15/2012EP2418145A2 Freight deck floor and aircraft with same
02/15/2012EP2417021A1 Center fuselage bellows
02/14/2012US8114501 Fiber reinforced core panel having natural contour
02/14/2012US8113751 Locking device for fastening a container
02/14/2012US8113466 System and method for drag reduction
02/14/2012US8113465 Trailing edge aircraft structure with overhanging cover
02/14/2012US8113464 Autonomous plane architecture for the transport and the replacement of propulsion engines
02/11/2012CA2746878A1 Sandwich board for an inner wall cladding of a passenger cabin
02/09/2012WO2012016900A1 Facing arrangement and aircraft or spacecraft
02/09/2012US20120032028 Actuating mechanism for a vent door
02/09/2012US20120032024 Wing-to-body fairing with spray-on foam and noise reduction method
02/09/2012DE102010033271A1 Sandwich element for sound-absorbing inner liner of transportation medium, particular aircraft, has multiple passageways introduced in core structure or partially in top layers for sound transmission
02/09/2012DE102007030422B4 Halterung zur lösbaren Befestigung einer Verkleidungsplatte in einem Luftfahrzeug Bracket for releasably securing a trim panel in an aircraft
02/08/2012EP2415668A1 Integration of an aircraft fairing
02/08/2012EP2415664A2 Wing-to-body fairing with spray-on foam and noise reduction method
02/08/2012EP2415663A1 Actuating mechanism for a vent door
02/08/2012EP2415662A1 Fuselage structure made of composite material
02/08/2012EP2415661A1 Structure for assembly of the pressure bulkhead of an aircraft
02/08/2012EP2415575A1 Closed injection moulded lightweight grid structure
02/08/2012EP2414229A1 Aircraft comprising an insulation system for thermal and acoustic insulation
02/08/2012EP2414227A2 Fuselage segment, and method for the production of a fuselage segment
02/08/2012EP2209710B1 Transversal butt strap and method for connecting two especially wound cfk fuselage sections in order to create a fuselage cell
02/08/2012EP2089272B1 Wing/fuselage connection for an aircraft
02/08/2012EP2021236B1 Aircraft fuselage structure and method for its production
02/08/2012CN202138535U 一种外开式增压舱门 One kind outside the open door Booster
02/08/2012CN102348548A Closed structure consisting of composite material
02/07/2012US8108980 Hinge cover integration into door seal edges
02/07/2012CA2653134C Fastener
02/02/2012WO2011158015A3 Aircraft wing box joint
02/02/2012US20120025024 Device for the mounting of connectors
02/02/2012US20120025023 Longitudinal junction for aircraft fuselage panels in composite materials
02/02/2012US20120025022 Fuselage structure made of composite material
02/02/2012US20120025021 Payload door and elevator system
02/02/2012US20120025020 Fasteners made of a polymer material
02/02/2012US20120025016 Aircraft propeller
02/02/2012DE10251579B4 Verfahren zur Herstellung einer umlaufenden dreidimensionalen Faserverstärkungsstruktur A process for producing a rotating three-dimensional fiber reinforcing structure
02/02/2012DE102010032402A1 Verfahren zum Verbinden von zwei Luftfahrzeugrumpfsegmenten mittels Rührreibschweißen A method of joining two aircraft fuselage segments friction stir
02/02/2012CA2743372A1 Fuselage structure made of composite material
02/01/2012EP2411280A1 Aeroplane structure comprising air guiding shafts built into structural elements
02/01/2012EP2411267A1 Integrated aircraft floor with longitudinal beams
02/01/2012EP2094561B1 Window element for inserting in a structural part and method of integration of a window element in a structural part
02/01/2012CN102342195A Method of applying an electric conductive layer to selected portions of a mounting frame
02/01/2012CN102341304A Decompression assembly for aircraft
01/2012
01/31/2012US8104715 Window arrangement for installing larger aircraft windows
01/31/2012US8104712 Aircraft fuselage element
01/31/2012US8104709 Lateral force joint
01/26/2012WO2012010882A1 Aircraft thermal insulation
01/26/2012WO2012010306A1 Main-load-bearing planking shell and structural component and flow body comprising such a main-load-bearing planking shell
01/26/2012WO2012010305A1 Structural component comprising at least one main-load-bearing covering shell and a carrier structure for fixing the main-load-bearing covering shell, and flow body comprising such a structural component
01/26/2012WO2012010304A1 Lining shell carrying a main load and structural component having at least one lining shell carrying a main load
01/26/2012US20120018589 Method For Carrying Out An Aircraft And Aircraft So Obtained
01/26/2012US20120018580 Insulating blanket for an aircraft and assembly integrating such a blanket
01/26/2012US20120018579 Self-righting frame and aeronautical vehicle
01/26/2012US20120017514 Aircraft opening window and aircraft equipped with at least one such window
01/26/2012DE102010031690A1 Covering plate for sandwich component in planar extending interior region of airplane, has control line coupled to two ports for creation of optical check signal, where control line is provided with specific amount of tear resistance
01/26/2012DE102010027696A1 Main load-bearing sheeting shell for structural component of flow body, has inner main section, outer main section and core layer that is shear-loaded between main sections
01/26/2012DE102009015856B4 Rumpfsegment und Verfahren zur Herstellung des Rumpfsegments Fuselage segment and method for producing the hull segment
01/26/2012DE102009013585B4 Rumpfzellenstruktur für ein Flugzeug in Hybridbauweise Fuselage structure for an aircraft in hybrid construction
01/25/2012EP2410004A1 Transparent Polyurethane Protective Coating, Film and Laminate Compositions with Enhanced Electrostatic Dissipation Capability, and Methods for Making Same
01/25/2012EP2409914A1 Aircraft thermal insulation
01/25/2012EP2408666A2 Under-flap stiffener for aircraft
01/25/2012EP2408665A2 Fuselage cell structure for an aircraft in hybrid design
01/25/2012CN202124115U Glass opening cover
01/24/2012US8101284 Fibre metal laminate panel
01/24/2012US8100363 Hatch equipped with at least one locking socket capable of being actuated on each side of the hatch
01/24/2012US8100362 Cockpit and aircraft including such cockpit
01/24/2012US8100361 Hull structure
01/24/2012US8100360 Light rail system for powered introduction of large loads in a structure
01/24/2012CA2508839C Door which is intended to be positioned between the cockpit and the cabin of an aircraft
01/19/2012WO2012007449A1 Beam
01/19/2012US20120014741 Cushioned sliding joint
01/19/2012US20120012712 Aircraft assembly and spar
01/19/2012US20120012698 Aircraft comprising an insulation system for thermal and acoustic insulation
01/19/2012DE102010046932A1 Base assembly for interior equipment of air craft, has base plate and seat rail running in longitudinal direction of aircraft, and base plate is mounted at seat rail
01/19/2012DE102010027005A1 Elemente zur Signal- und/oder Leistungsübertragung in oder an Kabinenbauteilen Elements for signal and / or power transfer in or on car parts
01/19/2012CA2802980A1 Beam
01/18/2012EP2407375A1 Interior panel of an aircraft cabin integrating at least one system.
01/18/2012EP2407018A2 Method of applying an electric conductive layer to selected portions of a mounting frame
01/18/2012EP2406071A1 Composite structures employing quasi-isotropic laminates
01/18/2012EP2406069A1 Multilayer board for sound insulation
01/18/2012EP2258143B1 Layered heater system with honeycomb core structure
01/17/2012US8096848 Collapsible toy airplane
01/17/2012US8096507 Methods and apparatus for optical propagation improvement system
01/17/2012US8096506 Method for making window frame
01/17/2012US8096504 Integrated aircraft structure in composite material
01/17/2012US8096503 Structuring construction for an aircraft fuselage
01/17/2012US8096092 Lightweight structural panel
01/17/2012CA2543788C An apparatus for automatically pointing a device at a target
01/12/2012WO2012004490A1 Method for producing a central wing box
01/12/2012US20120006942 Coupling assembly
01/12/2012US20120006940 Method for realization of an aircraft structure and resulting structure
01/12/2012US20120006937 Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage
01/12/2012DE102010026839A1 Aerodynamic outer lining device for use in airplane component arrangement to mount at airplane structure, has covering part whose connection section forms flap, and fastening device accommodating connecting element to connect covering parts
01/12/2012DE102010026683A1 Interieurkomponententrägersystem, Flugzeuginterieurkomponentenmodul und Montageverfahren Interior component carrier system, aircraft interior components and module assembly method
01/12/2012CA2803974A1 Method for producing a central wing box
01/11/2012EP2404826A1 Amphibious large aircraft without airstairs
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