| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 02/07/2008 | CA2658317A1 Aircraft doorway |
| 02/06/2008 | EP1884047A2 De-rotation system for counter-rotating, coaxial rotor hub shaft fairing |
| 02/05/2008 | US7325772 Aircraft heat sink and electronics enclosure |
| 02/05/2008 | US7325771 Splice joints for composite aircraft fuselages and other structures |
| 01/31/2008 | WO2007138082B1 Line system arrangement in an aircraft or spacecraft having a fuselage |
| 01/31/2008 | WO2007107520B1 Bolted joint |
| 01/31/2008 | US20080023584 Hinge device of a nacelle cowling of an aircraft engine on a supporting structure |
| 01/31/2008 | US20080023583 Composite anti-crash structure with lateral retention, for an aircraft |
| 01/31/2008 | US20080023582 Composite anti-crash structure with controlled buckling for an aircraft |
| 01/31/2008 | DE102006034862A1 Vehicle cabin i.e. passenger aircraft, reconfiguring method, involves inserting cabin module through vehicle opening into vehicle cabin, fastening inserted module to vehicle cabin, and moving module from driven rollers to vehicle cabin |
| 01/31/2008 | DE102006026168A1 Flugzeugrumpfstruktur und Verfahren zu deren Herstellung Aircraft fuselage structure and process for their preparation |
| 01/30/2008 | EP1881928A1 Helicopter one-piece door |
| 01/29/2008 | US7324747 Aircraft fuselage element and method of taking a number of pictures |
| 01/24/2008 | WO2007100601A3 Door pod assembly |
| 01/24/2008 | DE102006028956A1 Side fairing for an aircraft includes gastight film that surrounds the component with the hollow chambers in a gastight manner after application of a vacuum to evacuate the hollow chambers of the component |
| 01/23/2008 | CN201010045Y Ground-effect aircraft |
| 01/23/2008 | CN101111419A Device for fastening passenger seats on a seat track break in an aircraft |
| 01/22/2008 | CA2482732C Method of manufacturing window having at least one of radio wave stealth property and electromagnetic wave shield property, and window material having at least one of radio wave stealth property and electromagnetic wave shield property |
| 01/17/2008 | WO2008007043A1 Composite manufacturing method |
| 01/17/2008 | WO2008006956A1 Storage compartment for the nose gear of an aircraft |
| 01/17/2008 | WO2008006955A1 Aircraft tail cone |
| 01/17/2008 | WO2007046905A3 Rf shielding for aircraft windows |
| 01/17/2008 | DE102006003638B4 Flugkörper für den Überschallbereich Missiles to supersonic |
| 01/17/2008 | CA2658277A1 Composite manufacturing method |
| 01/17/2008 | CA2657218A1 Aircraft tail cone |
| 01/16/2008 | EP1878657A2 Aircraft archway architecture |
| 01/16/2008 | EP1877309A1 Improvements in aircraft doors |
| 01/16/2008 | CN101107506A Pressure-difference warning system |
| 01/15/2008 | US7318566 Aircraft with a lift system |
| 01/10/2008 | WO2008003733A1 Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby |
| 01/10/2008 | US20080006742 Airplane Protected Against Projections of Tire Debris |
| 01/10/2008 | US20080006741 Structural element, method for producing such a structural element, and aircraft having such a structural element |
| 01/10/2008 | DE10324648B4 Vorrichtung zur Aufnahme von Zurrvorrichtungen für ein Frachtladesystem eines Transportmittels, insbesondere eines Flugzeuges Device for receiving lashing devices for a cargo loading system of a transportation means, in particular of an aircraft |
| 01/10/2008 | DE10017699B4 Verwendung eines transparenten Scheibenpaketes als Verglasung für Sichtfenster in Raumstationen, Flugkörpern sowie Polarstationen in arktischen und antarktischen Breiten Using a transparent disc set as glazing window in space stations, missiles and polar stations in the Arctic and Antarctic latitudes |
| 01/10/2008 | CA2655709A1 Method for producing a fibre composite component for aviation and spaceflight |
| 01/09/2008 | EP1874622A1 Glazing comprising an electronic device and method of reading/writing information in said device |
| 01/09/2008 | EP1874621A2 Multi-ring system for fuselage barrel formation |
| 01/09/2008 | EP1874537A2 Layered, transparent thermoplastic for flammability resistance |
| 01/09/2008 | CN101102931A 货运飞机 Cargo aircraft |
| 01/08/2008 | US7316372 Fuselage spar for aircraft and central sparbox provided with such a spar |
| 01/03/2008 | WO2008000670A2 Pressure bulkhead for an aerospace fuselage |
| 01/03/2008 | WO2008000286A1 Aircraft-fuselage assembly concept |
| 01/03/2008 | US20080001033 Fuselage structure |
| 01/03/2008 | DE102006029231A1 Pressure bulkhead for e.g. securing pressure tight inner side in tail section of aircraft, has frame carrying bulkhead main section and netlike unit with strip units that are interlaced strips, which forms fabric in air-tight manner |
| 01/03/2008 | DE102006002248B4 Strukturgebende Konstruktion für einen Flugzeugrumpf Structuring construction for an aircraft fuselage |
| 01/03/2008 | CA2654646A1 Aircraft-fuselage assembly concept |
| 01/03/2008 | CA2651518A1 Pressure bulkhead for an aerospace fuselage |
| 01/02/2008 | EP1873059A2 Airplane with multi-level cabins for cargos or passengers and method of loading cargos into same |
| 01/02/2008 | EP1871662A1 Integrated aircraft structural floor |
| 01/02/2008 | EP1871661A1 Seals and fasteners |
| 01/02/2008 | EP1871579A2 Novel decorative panel based on wood, for interior design |
| 01/01/2008 | US7314198 Aircraft evacuation slide with thermally actuated gas relief valve |
| 12/27/2007 | WO2007147885A1 Vacuum insulation panels for aircraft interiors |
| 12/27/2007 | WO2007115690A8 Aircraft door with oversizing |
| 12/27/2007 | US20070295861 Carrier system for receiving components |
| 12/27/2007 | DE102006026918A1 Fuselage structure for aircraft construction, comprises multiple elements, which are mounted by welded connections in longitudinal direction at each other, where multiple rotating ribs are connection with multiple elements |
| 12/27/2007 | DE102006026170A1 Flugzeugrumpfstruktur und Verfahren zu deren Herstellung Aircraft fuselage structure and process for their preparation |
| 12/27/2007 | DE102006026169A1 Flugzeugrumpfstruktur und Verfahren zu deren Herstellung Aircraft fuselage structure and process for their preparation |
| 12/27/2007 | CA2649899A1 Vacuum insulation panels for aircraft interiors |
| 12/26/2007 | EP1868886A2 Method of reducing drag and increasing lift due to flow of a fluid over solid objects |
| 12/26/2007 | EP1868885A1 Aircraft structural element provided with a cavity and drainage element |
| 12/26/2007 | EP1868795A1 Multi-axial laminate composite structures and methods of forming the same |
| 12/26/2007 | CN100357160C System and method for inspecting a beam using micro fiber-optic technology |
| 12/25/2007 | US7311287 Methods for incorporating area ruled surfaces in a supersonic aircraft |
| 12/25/2007 | US7311175 Acoustic liner with bypass cooling |
| 12/21/2007 | WO2007145512A1 Laminate of metal sheets and polymer |
| 12/21/2007 | WO2007144377A1 Tail structure for an aircraft or spacecraft |
| 12/21/2007 | WO2007115804A8 Aircraft fuselage with circular-arc-shaped exterior contour |
| 12/21/2007 | WO2007110647A3 Aircraft fuselage interior |
| 12/21/2007 | CA2650512A1 Tail structure for an aircraft or spacecraft |
| 12/20/2007 | US20070292203 Fastening system for fastening an object in a vehicle |
| 12/20/2007 | DE102006027707A1 Tail structure for e.g. spacecraft, has separation unit for pressure-tight locking of trunk section, where separation unit is coupled with support construction and with trunk section for forming force-flow path |
| 12/18/2007 | US7309046 Method for determination of fuselage shape of supersonic aircraft, and fuselage front section shape |
| 12/18/2007 | US7309044 Device and method for improving security during the operation of air traffic |
| 12/18/2007 | US7308762 Method and apparatus for rotatably supporting movable components, including canards |
| 12/13/2007 | WO2007142354A1 Fastener |
| 12/13/2007 | WO2007141291A1 Aircraft fuselage structure and method for its production |
| 12/13/2007 | WO2007141268A1 Aircraft fuselage structure and method for producing it |
| 12/13/2007 | WO2007141176A1 Fuselage structure and method for the production of a fuselage structure |
| 12/13/2007 | US20070284481 Aircraft luggage handling system |
| 12/13/2007 | US20070283512 Boarding ramp device for aircraft |
| 12/13/2007 | DE102006026167B3 Leichtbau-Strukturpanel Lightweight structural panel |
| 12/13/2007 | DE102006025930A1 Fuselage structure for aircraft or spacecraft has an inner shell system with upper and lower inner shells and a window hinge plate with a window pane device and a grid structure |
| 12/13/2007 | CA2654045A1 Aircraft fuselage structure and method for its production |
| 12/13/2007 | CA2650509A1 Aircraft fuselage structure and method for producing it |
| 12/13/2007 | CA2649339A1 Fuselage structure and method for the production of a fuselage structure |
| 12/13/2007 | CA2649240A1 Aircraft fuselage structure and method for its production |
| 12/12/2007 | EP1864792A1 Peel progression preventing structure of sandwich panel |
| 12/12/2007 | EP1332961B1 Aircraft provided with carrying fuselage |
| 12/12/2007 | EP1250257B1 Emergency vision apparatus |
| 12/12/2007 | CN101087716A Aircraft windshield defogging/deicing system and method of use thereof |
| 12/06/2007 | WO2007138082A1 Line system arrangement in an aircraft or spacecraft having a fuselage |
| 12/06/2007 | WO2007137607A1 Sandwich element for sound-absorbing inner cladding of transport means, especially for sound-absorbing inner cladding of aircraft fuselage cells |
| 12/06/2007 | WO2007092371A3 Fabrication process for thermoplastic composite parts and products obtained thereby |
| 12/06/2007 | US20070278350 Aircraft walkway |
| 12/06/2007 | US20070278348 Apparatus for opening airframe of missile by pyrotechnical power |
| 12/06/2007 | DE102006025388A1 Leitungssystemanordnung in einem einen Rumpf aufweisenden Luft- oder Raumfahrzeug Piping arrangement in a hull having an aircraft or spacecraft |
| 12/06/2007 | DE102006013069B3 Bolzenverbindung Bolted connection |
| 12/06/2007 | CA2651742A1 Sandwich element for sound-absorbing inner cladding of transport means, especially for sound-absorbing inner cladding of aircraft fuselage cells |
| 12/06/2007 | CA2650445A1 Line system arrangement in an aircraft or spacecraft having a fuselage |