Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
10/2011
10/27/2011US20110259998 Configuration of a rear fuselage tail cone of an aircraft with an auxiliary power unit
10/27/2011DE102009014973B4 Schalungselement Sideform
10/27/2011CA2769734A1 Cockpit window of aircraft having electromagnetic shield, and aircraft
10/26/2011EP2379829A1 Wireless self-sufficient monitoring system for a door lock mechanism
10/26/2011EP2379313A1 Composite l-shaped fitting and method and mould for the production thereof
10/26/2011EP2167377B1 Corrosion-resistant connection between a first component and a second component
10/26/2011CN102227350A Shell component for aircraft or spacecraft
10/25/2011US8043554 Manufacturing process using bladderless mold line conformal hat stringer
10/25/2011US8043445 High strength; toughness; noncracking; aluminum alloy
10/25/2011US8042770 Structural element, method for producing such a structural element, and aircraft having such a structural element
10/25/2011US8042769 Modular aircraft window
10/25/2011US8042768 Systems and methods for reducing noise in aircraft fuselages and other structures
10/25/2011US8042767 Composite fabric with rigid member structure
10/25/2011CA2615590C Sound absorbing element and method for producing a sound absorbing element
10/20/2011WO2011129721A1 Fuselage and method for reducing resistance
10/20/2011WO2011128858A2 Acoustic insulation device and method for producing same
10/20/2011WO2011127899A2 Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a fuselage
10/20/2011US20110253878 Supporting pillar for an aircraft's structural component manufactured by a selective laser melting process
10/20/2011US20110253840 Method for installing an inertial reference unit in an aircraft, and aircraft equipped in this way
10/20/2011US20110253839 Door entry head guard
10/20/2011US20110253834 Flexible Mounting Assembly for an Air Frame Structure
10/20/2011US20110252954 Jettisonable armor
10/20/2011DE102010027859A1 Stay device for cell that is impact-endangered or crash-endangered of vehicle, comprises stay made of plastic material, particularly fiber reinforced plastic, and energy absorption unit made of metallic material with energy absorption area
10/20/2011DE102010015638A1 Plattenabsorber Plate absorber
10/20/2011CA2795863A1 Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a fuselage
10/19/2011DE202011102487U1 Sicherheitsschwenkmechanismus Safety hinge mechanism
10/19/2011CN102224393A Structural element for a fuselage cell structure of an aircraft, comprising at least one positioning aid
10/19/2011CN102224070A Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft
10/18/2011US8039115 Metallic aircraft component
10/18/2011US8038100 Paneled partition with track for linear and rotational movement
10/18/2011US8038099 Bonded metal fuselage and method for making the same
10/18/2011US8038098 Overhead luggage bin for aircraft interior
10/18/2011CA2475799C Laminated panel with discontinuous internal layer
10/13/2011WO2011127265A2 Structural connectors and methods of using same
10/13/2011WO2011126519A2 Cnt-tailored composite sea-based structures
10/13/2011WO2011126518A2 Cnt-tailored composite air-based structures
10/13/2011WO2011126517A2 Cnt-tailored composite land-based structures
10/13/2011WO2011124215A1 Connecting element and fastening arrangement for seat rails in an aircraft
10/13/2011WO2011124207A1 Aircraft, and fastening arrangement for a floor structure in an aircraft
10/13/2011WO2011080320A3 Aircraft or spacecraft casing
10/13/2011WO2011080286A3 Aircraft fuselage and skin section
10/13/2011WO2011064356A3 Cargo hold floor for a cargo hold of an aircraft, functional element for installing in a cargo hold floor, side guide, fixing device for introducing a tensile load, and device for ejecting cargo items
10/13/2011US20110248119 Structural connectors and methods of using same
10/13/2011US20110248117 Multilayer board for acoustic insulation
10/13/2011DE102010014641A1 Wall section for structure component for flow components of airplanes, has external cover, which is formed permeable for air flow, where internal cover is arranged with openings
10/13/2011DE102010014640A1 Structural component for use with flow components of airplane, has air duct staying in fluid-communicating connection with permeable metal braided fabric arrangement above openings for extracting air from outside outer cover
10/13/2011DE102010014639A1 Method for manufacturing reinforced hollow-chamber profile with permeable surface for use with components for flow influence at components of airplanes, involves arranging lower cover in tool
10/13/2011DE102010014638A1 Luftfahrzeug mit einer integrierten energieaufnehmenden Verformungsstruktur und Luftfahrzeug mit einem derartigen Rumpf Aircraft with an integrated energy-absorbing deformation structure and aircraft with such a hull
10/13/2011DE102010014302A1 Luftfahrzeug und Befestigungsanordnung für eine Fußbodenstruktur in einem Luftfahrzeug Aircraft and mounting arrangement for a floor structure in an aircraft
10/13/2011DE102010014301A1 Befestigungsanordnung und Verbindungselement für eine Befestigungsanordnung Mounting assembly and connecting element for a fastening arrangement
10/13/2011DE102010014265A1 Türrahmenanordnung und Tür, insbesondere für Luft- oder Raumfahrzeuge Door frame and door assembly, particularly for air and space vehicles
10/13/2011CA2795912A1 Aircraft and fastening arrangement for a floor structure in an aircraft
10/13/2011CA2795307A1 Connecting element and fastening arrangement for seat rails in an aircraft
10/13/2011CA2776999A1 Cnt-tailored composite air-based structures
10/12/2011EP2374713A2 Door frame assembly and door, in particular for aircraft or spacecraft
10/12/2011EP2373542A2 Transparency having sensors
10/12/2011EP2373541A2 A method of and system for maintaining operating performance of a transparency
10/12/2011EP2373540A2 Monomolecular carbon-based film for forming lubricious surface on aircraft parts
10/12/2011EP2373539A1 Longitudinal joint for aircraft fuselage panels made of composite materials
10/12/2011EP2373531A1 Modular floor section for aircraft
10/12/2011CN102211659A Explosive cutting rope protection method for airframe truss or frame structure
10/11/2011US8033505 Aircraft door window
10/11/2011US8033503 Pressure bulkhead for an aerospace fuselage
10/06/2011WO2011121340A1 Composite structural member
10/06/2011WO2011120503A2 Wall component for an aircraft
10/06/2011WO2011039402A3 Joining of structural aircraft elements
10/06/2011US20110241359 Electromechanical blocking device, particularly for the door of an airplane
10/06/2011DE102010013715A1 Verriegelungsmechanismus für eine Luftfahrzeugtür sowie Verfahren zum Verriegeln einer Luftfahrzeugtür Locking mechanism for an air vehicle door and method for locking an aircraft door
10/06/2011DE102010013714A1 Method for assembling outer shell of aircraft with cab window, involves connecting window frame to outer shell portion in hardened condition for definition of window section, where window section is detached from window frame
10/06/2011DE102010013479A1 Einrichtung und Verfahren zur Herstellung zweidimensional gewölbter Strukturbauteile aus einem Faserverbundwerkstoff Means and methods for making two-dimensionally curved structural members made of a fiber composite material
10/06/2011DE102010013478A1 Einrichtung und Verfahren zur Herstellung mehrfach gewölbter Strukturbauteile aus einem Faserverbundwerkstoff Apparatus and method for preparing multiple curved structural members made of a fiber composite material
10/06/2011DE102010013370A1 Wandbauteil für ein Luftfahrzeug Wall member for an aircraft
10/05/2011EP2372170A1 Assembling device for cabin interior components
10/05/2011EP2371705A2 Horizontal stabilising surface of an aircraft
10/05/2011EP2371704A1 Structure of the load-introduction area in the fuselage rear section of an aircraft
10/05/2011EP2370315A2 Planar component of an aircraft and method for producing the same
10/05/2011EP2276663B1 Aircraft door with locking device
10/05/2011EP1723033B1 Device and method for supporting a galley
10/05/2011EP1648764B1 Sliding door comprising a frame and a guiding mechanism
10/05/2011CN102209665A Method and system for emergency ventilation of an aircraft cabin in case of a leak in the area of an air mixer
10/04/2011US8028955 Landing gear casing provided with a box structure
10/04/2011US8028951 Hydrogen powered aircraft
10/04/2011CA2466003C Method for avoiding air pockets in a joint between two structural components
09/2011
09/29/2011WO2011119720A2 Passenger seat assembly and associated floor panel structure
09/29/2011WO2011118558A1 Cap, fastened structure using same, and aircraft having said fastened structure
09/29/2011WO2011117454A1 Structure for joining torsion boxes in an aircraft using a triform fitting made from non-metal composite materials
09/29/2011WO2011081830A3 Fireproof bidirectional decompression panel
09/29/2011US20110233339 Passenger seat assembly and associated floor panel structure
09/29/2011US20110233338 Joint
09/29/2011US20110233336 Fuselage structure for combined fixing of insulation blankets and items of equipment, aircraft incorporating such a structure
09/29/2011US20110233335 Impact resistant and damage tolerant aircraft fuselage
09/29/2011US20110233334 Structure, especially a fuselage structure of an aircraft or a spacecraft
09/29/2011DE102010003356A1 Component manufacturing method for e.g. aircraft, involves impregnating added reinforcement fibers with polymer matrix for forming component from elements, where reinforcement fibers are disrupted along parting plane
09/29/2011CA2792105A1 Cap, fastening structure using the same, and aircraft including the fastening structure
09/28/2011EP2367681A1 Reinforced foam-filled composite stringer
09/28/2011EP2217495B1 Carrier tube for ceiling elements
09/28/2011EP2167378B1 Differential pressure-controlled locking mechanism
09/28/2011CN201989945U 模块式快速拼接式无人机 Modular fast tiled UAV
09/28/2011CN102202973A Airplane having engines partially encased in the fuselage
09/28/2011CN102202965A Fitting for trimming the horizontal stabiliser of an aircraft
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