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