Patents
Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562)
07/2008
07/03/2008US20080156933 Collapsible staircase, notably for a vehicle such as an aircraft
07/03/2008US20080155931 Space truss structure surface slab assembly
07/02/2008EP1939389A1 Motorized window shade
07/02/2008EP1937551A1 Floor panel and installation for fixing layout elements comprising such panels
07/02/2008CN101213130A Device for fixing a seat rail on a floor, and aircraft equipped with such a fixing device
06/2008
06/26/2008WO2008076147A2 Building made of hexagonal layers
06/26/2008WO2008076019A1 Microwave power distribution system for an airborne radar system
06/26/2008US20080149769 Compliant panel for aircraft
06/26/2008US20080149768 Multi-ring system for fuselage barrel formation
06/26/2008US20080149767 Fuel range for an aircraft
06/26/2008US20080149763 Air transport with scalloped underbody
06/26/2008US20080149758 Modular unmanned air-vehicle
06/26/2008DE102007046479A1 Fire protection device for aircraft or spacecraft, has adjusting device adjusting fire wall from ventilation position to partitioning position, where fire wall in ventilation position releases gap between partitioning and external walls
06/26/2008DE102006060364A1 Fuselage component for an aircraft or spacecraft comprises a heat stopper having low heat conductivity for connecting a structural part to the skin
06/26/2008DE102006060361A1 Transportation gripper for transporting flexible surface material of location surface on target form, comprises rolling body with winding rolling surface and deactivated operating device, which pulls surface material to location surface
06/26/2008DE102006060360A1 Fuselage section for forming a fuselage cell of an airplane comprises longitudinal slots for equalizing tolerances in an end region of an outer skin surrounding the fuselage section
06/26/2008DE102006058377A1 Samer rod for structural reinforcement of fuselage structure of airplane, has shaft and double sided eyes that are arranged at shaft ends for connection of samer rod
06/26/2008DE102006058005A1 Thermal insulating element for an aircraft has two plates that are connected to each other via frame structure which establishes its assembled geometry and forms an air filled insulation with vent opening
06/25/2008EP1935782A1 Mounting layer for mounting loading devices on the loading deck of an aircraft
06/25/2008EP1934089A1 Molded sliding window assembly
06/25/2008EP1843941B1 Aircraft interior module
06/19/2008WO2008073668A2 Thermal insulation materials and applications of the same
06/19/2008WO2008073150A2 Window assembly and method for a mobile platform
06/19/2008WO2008053041B1 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer
06/19/2008US20080145528 Methods of preparing wetting-resistant surfaces and articles incorporating the same
06/19/2008US20080144158 Power supply for an electric window dimming device
06/19/2008US20080142641 Airplane configuration
06/19/2008US20080142635 Aircraft safety system
06/19/2008US20080142634 Landing Gear Noise Attenuation
06/19/2008DE202007014079U1 Verbesserungen an einem Mini-Jet Luftfahrtzeug Improvements to a mini-jet aviation stuff
06/19/2008DE102007003274B3 Method e.g. for reinforcing foam material, involves providing processing area and creating processing area with laminar for partial surrounding gap and fiber-surface material is arranged into gap and has foam material
06/19/2008DE102006057255A1 Method for repairing damage in aircraft skin using patches applied from inside the hull and with outer flush filling
06/19/2008DE102004013966B4 Aktives Element zur Schwingungsreduktion von Bauteilen, insbesondere für Flugzeugkomponenten Active element for vibration reduction of components, particularly for aircraft components
06/18/2008EP1932758A1 Absorbent coating
06/18/2008EP1932757A1 Bonded aluminium window frame on fibre metal laminate fuselage skin
06/18/2008EP1931565A1 Polyurethane lacquers as abrasion-resistant coatings
06/18/2008CN101203374A Process for producing a substantially shell-shaped component
06/18/2008CN101200217A Driving-cabin protecting chamber
06/17/2008US7387276 Aerial sensor pod deployment system
06/17/2008CA2329718C Window shade assembly with a motorized window shade mechanism
06/12/2008WO2008068523A1 Composite structure
06/12/2008WO2008068045A1 Oscillation damper for installed parts in aircraft
06/12/2008WO2008043940A3 Aircraft fuselage made from longitudinal panels and method of producing such a fuselage
06/12/2008US20080135684 Reduced Door Opening Force and Enhanced Security Flight Deck Door Mechanism
06/12/2008US20080135683 Thermal Insulating Element
06/12/2008US20080135682 Arrangement And Method For Installing A Component In An Aircraft
06/12/2008DE102006058006A1 Anordnung und Verfahren zur Montage eines Bauelements in einem Flugzeug Arrangement and method for mounting a component in an aircraft
06/12/2008DE102004043664B4 Schwingungskraftgenerator Vibration power generator
06/12/2008CA2671166A1 Composite structure
06/11/2008EP1930519A2 Sandwich panel
06/11/2008EP1930237A1 Deformable floor substructure for a helicopter
06/11/2008EP1928735A1 Sound absorbing element and method for producing a sound absorbing element
06/11/2008EP1928734A1 Cooling system for an aircraft, aircrft comprising the cooling system and cooling method
06/11/2008EP1928733A1 Aircraft safety system
06/11/2008EP1928732A1 Laminated passenger window for reduced noise transmission
06/11/2008EP1928731A1 Water deflector and system having multiple water deflectors of this type
06/11/2008EP1685023B1 Architectural archway for an aircraft
06/11/2008CN101198519A Helicopter one-piece door
06/11/2008CN101198518A Reinforcement beam as well as method and fiber laminate for manufacturing the reinforcement beam
06/10/2008US7384015 Aircraft nose with shield
06/05/2008WO2008065654A2 Wall effects on vtol vehicles
06/05/2008WO2008065214A1 Composite pressure bulkhead for aircraft
06/05/2008US20080131661 Resin infused transparent skin panel and method of making same
06/05/2008US20080128559 Optimal sun safe attitude for satellite ground tracking
06/05/2008US20080128555 Ejection device, ejectable hatch and aircraft having at least one ejectable hatch
06/05/2008US20080128554 Composite shear tie
06/05/2008US20080128551 Aircraft archway architecture
06/05/2008US20080128550 Stiffening element for an aircraft or spacecraft, and method for its production
06/05/2008US20080128549 Assembly for securing a stringer to a substrate
06/05/2008DE102006056568A1 Core structure manufacturing method for airplane, involves positioning core layers with defined distance, and inserting reinforcement unit in hollow space between layers, where reinforcement unit and layers form integral core structure
06/05/2008DE102006056442A1 Türschloss für Türen von Luftfahrzeugen, insbesondere von Hubschraubern Door lock for doors of aircraft, especially helicopters
06/05/2008DE102006056440A1 Crash-Energieabsorber-Element, Anbindungselement mit einem solchen Crash-Engergieabsorber-Element, sowie Luftfahrzeug Crash energy absorber element, connecting element with such a crash Engergieabsorber element, as well as aircraft
06/05/2008DE102006040298B4 Leichtbau-Strukturbauteil, insbesondere für Flugzeuge Lightweight structural element, in particular for aircraft
06/04/2008EP1927464A2 Sandwich panel
06/04/2008EP1926659A2 Composite thermoplastic matrix airframe structure and method of manufacture therefor
06/04/2008CN101194082A Ladder system, especially for vehicles
06/04/2008CN101190712A Anti-hijacking airplane
06/03/2008US7380753 Composite material structure
06/03/2008US7380752 Aircraft interior architecture
05/2008
05/29/2008US20080121758 Reinforced cover for gaps in an aerodynamic contour
05/29/2008DE102006056441A1 Verriegelungsvorrichtung für Schiebetüren von Luftfahrzeugen, insbesondere von Hubschraubern Locking device for sliding doors of aircraft, especially helicopters
05/29/2008DE102006056137A1 Door e.g. cargo door, arrangement, for air plane, has pressure reducing device comprising channel, pipe line and vacuum pump and provided for lowering pressure in gap formed between sealing lips
05/29/2008DE102006054431A1 Türbeschlag für das Lagern von Flugzeugtüren Door hardware for the storage of aircraft doors
05/29/2008CA2656521A1 Improved composite resin window frame constructions for airplanes
05/28/2008EP1924491A1 Aircraft fuselage
05/28/2008CN101189160A Glazing comprising an electronic device and method of reading/writing information in said device
05/28/2008CN101189118A Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft
05/22/2008WO2008058746A1 Window element for inserting in a structural part and method of integration of a window element in a structural part
05/22/2008WO2007117260A3 Aircraft with belly flaps
05/22/2008US20080116319 Fitting And Associated Grommet For Supporting A Conduit Penetrating A Panel
05/22/2008US20080116094 Receptacle for fasteners and an associated installation method
05/22/2008CA2669173A1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect
05/22/2008CA2669110A1 Window element for inserting in a structural part and method of integration of a window element in a structural part
05/21/2008DE102007039895A1 Luftfracht-Kraftantriebseinheit zum wahrnehmen einer Bewegung eines über ihr befindlichen Frachtcontainers Air cargo power drive unit to perform a movement of a located above her cargo container
05/21/2008DE102006053967A1 Fensterelement zur Befestigung in einem Fensterausschnitt Window element for mounting in a pane
05/21/2008DE102006053966A1 Universal line holder for aircraft, has function module fastened to base module, which has attachment surface with hole and locking surface, and bolt attached for fixing holder in borehole in reinforcement structure
05/21/2008CN101184666A Long-range aircraft
05/20/2008US7374132 Insulation product and system suitable for use in an aircraft
05/20/2008US7374131 Support device for a galley
05/20/2008CA2481929C Equipment apparatus for a hole in a panel and the panel so equipped
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