Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
02/2011
02/03/2011US20110024572 Device for reducing aerodynamic drag
02/03/2011US20110024565 Aircraft Component Assembly System
02/03/2011US20110024564 Injection-molded window panel and related methods
02/03/2011US20110024563 Pressure fuselage of an aircraft or spacecraft with pressure calotte
02/03/2011US20110024562 Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft
02/03/2011US20110024561 Frame element, aircraft air-conditioning system and method for the installation of a frame element in an aircraft
02/03/2011DE102009035265A1 Druckrumpf eines Luft- oder Raumfahrzeuges mit Druckkalotte Pressure hull of an aircraft or spacecraft with pressure cap
02/02/2011EP2279116A2 Aircraft flight termination system and method
02/02/2011EP2279115A1 Impact resistant aircraft fuselage
02/02/2011EP2279073A1 Composite and structure, particularly in the aerospace sector
02/02/2011EP1893478B1 Reinforcement beam as well as method and fiber laminate for manufacturing the reinforcement beam
02/02/2011CN101203374B Process for producing a substantially shell-shaped component
02/02/2011CN101137541B Aircraft structural element provided with a cavity and drainage element
02/01/2011US7881833 Airplane emergency navigational system
02/01/2011US7879276 Foam stiffened hollow composite stringer
02/01/2011US7878454 Doors of aircraft cabins
01/2011
01/27/2011WO2011009983A1 Method for assembling aircraft fuselage sections
01/27/2011WO2011009916A2 Method and device for system installation, and freight loading system
01/27/2011WO2011009474A1 Floor element for a loading deck of an aircraft
01/27/2011US20110017871 Load-supporting and damage-tolerant laminated aircraft window
01/27/2011US20110017870 Section of aircraft fuselage and aircraft including one such section
01/27/2011US20110017866 Locking device
01/27/2011DE10230710B4 Schweißbare hochfeste Al-Mg-Si-Legierung Weldable high strength Al-Mg-Si alloy
01/27/2011DE102009034416A1 Verfahren und Vorrichtung zur Systeminstallation sowie Frachtladesystem Method and apparatus for system installation and cargo loading system
01/27/2011DE102009033444A1 Schalensegment zur Herstellung einer Rumpfzellensektion für eine Rumpfzelle eines Flugzeugs Shell segment of manufacturing a fuselage section for a fuselage cell of an aircraft
01/27/2011CA2768885A1 A method and a device for the installation of systems, and also a freight loading system
01/26/2011EP2277773A2 Self-supporting interior cabin structure with integrated installation elements
01/26/2011EP2276663A1 Aircraft door closing device and aircraft comprising such a device
01/26/2011EP1796960B1 Aircraft provided with a cabin differential pressure warning system
01/26/2011CN101959753A Transverse butt connection between two fuselage sections
01/26/2011CN101596933B Civil aircraft fuselage bottom structure based on impact strength tests
01/25/2011US7874518 Aircraft structure including composite beam and composite panel with metal foil therebetween
01/25/2011US7874516 Structural frame for an aircraft fuselage
01/20/2011WO2011006954A2 Shell segment for producing a fuselage cell section for a fuselage cell of an airplane
01/20/2011WO2010112527A3 Fuselage segment, and method for the production of a fuselage segment
01/20/2011US20110011980 Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component
01/20/2011US20110011978 Floor system for a fuselage airframe of an aircraft
01/20/2011US20110011976 Connection of cabin components, cabin component and method for connecting cabin components
01/20/2011US20110011975 Aerospace articles made from quasi-isotropic chopped prepreg
01/20/2011CA2767945A1 A shell segment for the purpose of manufacturing a fuselage cell section for a fuselage cell of an aeroplane
01/19/2011EP2275692A2 Method for using an expandable collet anchor system
01/19/2011CN101952168A Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle
01/19/2011CN101952167A Floor system for a fuselage section of an aircraft
01/19/2011CN101952166A Structural component with rib and cross member element
01/19/2011CN101384850B Device for protecting and guiding a cable of an openable window of an aircraft flight cabin
01/18/2011US7871041 System, method, and apparatus for leading edge structures and direct manufacturing thereof
01/18/2011US7871040 Composite aircraft structures with hat stiffeners
01/13/2011WO2011005600A2 Seat track fitting
01/13/2011WO2011005350A2 Skin panel joint for improved airflow
01/13/2011WO2011003844A2 Stringer
01/13/2011WO2010116168A3 Coupling assembly
01/13/2011US20110006159 Fuselage of an aircraft or spacecraft and corresponding aircraft or spacecraft
01/13/2011US20110006158 Pivoting equipment carrier in combination with a modified luggage rack
01/13/2011DE102009032497A1 Sound insulation for cabin of vehicle, particularly aircraft, is provided with sound insulation index installed at cabin wall for increasing passive insulation in lower frequency range
01/13/2011DE102004025383B4 Fensterrahmen für Flugzeuge Frames for aircraft
01/13/2011DE102004025380B4 Fensterrahmen für Flugzeuge Frames for aircraft
01/13/2011DE102004025378B4 Fensterrahmen für Flugzeuge Frames for aircraft
01/13/2011DE102004025376B4 Fensterrahmen für Flugzeuge Frames for aircraft
01/13/2011DE102004009020B4 Zwischenkostal für Flugzeuge Between Kostal for aircraft
01/13/2011CA2765568A1 Skin panel joint for improved airflow
01/13/2011CA2765202A1 Seat track fitting
01/12/2011EP2271477A1 Device for producing a component and method and component
01/12/2011EP1888323B1 Method for manufacturing a reinforced shell for forming component parts for aircraft
01/12/2011EP1719084B1 Improvements in aircraft doors
01/12/2011CN1435355B Light buzzard-type wing jet plane and its use
01/12/2011CN101945807A Method of connecting two fuselage sections with the formation of a transverse joint, and transverse joint connection
01/12/2011CN101941522A Flying device
01/12/2011CN101941521A Light airplane body structure made of high-strength high-safety composite materials
01/12/2011CN101342942B Disposal solidifying and forming technique for frame and outer panel skin of wing profile
01/12/2011CN101321664B Aircraft pressurized cabin door made of fiber composite
01/11/2011US7867929 electrically insulant, compressible impermeable cloth formed by impregnating an electrically insulant woven fiber with a sealant, and curing; airframe structures may be assembled by positioning the cloth between a substructure and an outer skin on substructure, and assembling outer skin to substructure
01/11/2011US7867621 Wide area lightning diverter overlay
01/11/2011US7866605 Energy absorbing impact band and method
01/11/2011CA2515149C Contact stiffeners for structural skins
01/06/2011WO2011002628A1 Integrated multilayer insulation
01/06/2011WO2011002331A1 Small unmanned aircraft system
01/06/2011WO2011002309A1 Flying, gliding and/or airdrop craft
01/06/2011WO2011001081A2 Frame for an opening provided in an aircraft fuselage
01/06/2011WO2011001050A1 Fuselage element comprising a fuselage segment and junction means
01/06/2011WO2011001049A1 Fuselage element comprising a fuselage segment and junction means, fuselage portion, fuselage and aircraft
01/06/2011WO2011000987A1 Reinforcing frame for an aircraft fuselage
01/06/2011WO2010112270A4 Aircraft comprising an insulation system for thermal and acoustic insulation
01/06/2011US20110001010 Arrangement of two fuselage sections of an aircraft and a connecting structure for connecting fuselage skins
01/06/2011US20110001008 Aircraft floor of optimized compactness
01/06/2011US20110001007 Method and system for controlling swaying of an object
01/06/2011US20110001006 Process for making an aircraft having a floor
01/06/2011US20110001004 Landing Gear
01/06/2011CA2766007A1 Fuselage element comprising a fuselage segment and junction means
01/06/2011CA2765214A1 Fuselage element comprising a fuselage segment and junction means, fuselage portion, fuselage and aircraft
01/06/2011CA2765205A1 Frame for an opening provided in an aircraft fuselage
01/05/2011EP2269857A1 Emergency Jettison window pane and associated ejection system
01/05/2011EP2268474A2 Curved structural part made of composite material and method of manufacturing such a part
01/05/2011EP2179117B1 Locking device
01/05/2011EP2102060B1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect
01/05/2011DE102010010686A1 Verfahren und Vorrichtung zum klebtechnischen Fügen großflächiger Komponenten im Fahrzeugbau Method and apparatus for adhesive joining of large-scale components in vehicle
01/05/2011DE102009031523A1 Cabin window lining for airplane, has ring-like lining element arranged between side lining and window frame that is inserted in fuselage section, and centering device provided for automatically centering lining element for cabin window
01/05/2011CN201694384U Retracting mechanism of aircraft cargo door
01/05/2011CN101939218A Load-supporting and damage-tolerant laminated aircraft window
01/05/2011CN101939217A Method for producing a fibre composite component fibre composite component and a fibre composite fuselage component of an aircraft
01/04/2011US7862903 A stringer (support) for aircraft comprising an aluminum alloy base and a body of a heat-treatable, aluminium alloy having different properties; coextruded alloys by machining from a single piece of extruded partly finished product which includes a diffusion zone 116 mu m wide; welding the skin
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