| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 03/01/2006 | EP1628877A1 Crashworthiness structure and method |
| 02/28/2006 | US7005175 Ventilated double-walled composite aircraft fuselage shell |
| 02/28/2006 | US7004430 Threat-resistant aircraft tray |
| 02/23/2006 | US20060039765 Process and mechanical device for machining flexible panels, in particular with a complex shape |
| 02/23/2006 | US20060038077 Aircraft cargo locating system |
| 02/23/2006 | US20060038075 Holder for interior installations in airplanes |
| 02/23/2006 | US20060038074 Connecting element for connecting a conduit system to cooling aggregates in aircraft cabins |
| 02/23/2006 | US20060038072 Aircraft fuselage training device for fire fighters |
| 02/23/2006 | US20060038070 Seat power outlets integrated into floor |
| 02/23/2006 | DE112004000582T5 Verfahren zum Reduzieren kinetischer Reibung A method for reducing kinetic friction |
| 02/23/2006 | DE102004039189A1 Power distribution system e.g. for electrical supply of rail-mounted aircraft fittings, has locking bolt of seat rail forming clamping piece for fixture on seat rail |
| 02/21/2006 | US7003374 Aircraft cargo loading logistics system using machine readable identifiers |
| 02/21/2006 | US7000870 Laminar flow wing for transonic cruise |
| 02/21/2006 | US7000869 Cross section for a supersonic airplane |
| 02/16/2006 | WO2005110842A3 Airfoil box and associated method |
| 02/16/2006 | WO2005084156A3 Hydrogen powered aircraft |
| 02/16/2006 | WO2005011886A3 Tubular metal fitting expandable in a wall opening and method of installation |
| 02/16/2006 | US20060032982 Method of joining structural elements in an aircraft |
| 02/16/2006 | US20060032981 Aerodynamic airflow deflector for aircraft landing gear |
| 02/16/2006 | US20060032980 Aircraft window case that can be artificially illuminated in an indirect manner |
| 02/16/2006 | DE102004036184A1 Flugzeugtür-Anordnung mit einer um 180° schwenkenden Flugzeugtür Aircraft door assembly having a pivoting 180 ° aircraft door |
| 02/16/2006 | DE102004035161A1 Airplane for transporting goods has upper and lower tail boards that may be respectively swiveled upwards and downwards simultaneously |
| 02/16/2006 | DE102004034903A1 Covering device for door hinge of aircraft, includes flexible covering set across gap between two hinge pieces of door hinge and which can adjust between stretched and unstretched conditions based on size of gap between hinge pieces |
| 02/15/2006 | EP1626470A2 Current distribution system for electric supply of rail-mounted installations in an aircraft |
| 02/14/2006 | US6997414 Cargo door modification to ease emergency egress |
| 02/09/2006 | WO2006012716A2 A device for fastening passenger seats on a seat track break in an aircraft |
| 02/09/2006 | US20060027707 Drain particularly for engine support strut |
| 02/09/2006 | DE202005017097U1 Stiffening or stabilizing system for hollow profile or hollow body, especially profile useful for road or rail vehicle or water, air or space craft, has supports of loose material of random orientation, bonded at contact areas and with wall |
| 02/09/2006 | DE102004034684A1 Small aircraft for air freight transport has goods container which is variably sized to match load requirements |
| 02/09/2006 | DE102004033068A1 Verkehrsflugzeug mit einem Hauptdeck und einem Unterdeck Airliner with a main deck and lower deck |
| 02/07/2006 | US6994916 Friction stir grain refinement of structural members |
| 02/07/2006 | CA2355366C Forming reinforcing components |
| 02/02/2006 | WO2006010817A1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 02/02/2006 | WO2006010437A1 Aircraft door arrangement comprising a pivotable aircraft door |
| 02/02/2006 | WO2005115837B1 Window frame for aircraft |
| 02/02/2006 | WO2005115836B1 Window frame for aircraft |
| 02/02/2006 | US20060022090 Carry-on luggage system for an operational ground support system |
| 02/02/2006 | US20060022089 High altitude platform control system |
| 02/02/2006 | US20060022088 Aircraft nose with shield |
| 02/02/2006 | US20060022082 Static port skin applique apparatus and method |
| 02/02/2006 | US20060021560 Tail fairing designed with features for fast installation and/or for suppression of vortices addition between fairings, apparatus incorporating such fairings, methods of making and using such fairings and apparatus, and methods of installing such fairings |
| 02/02/2006 | CA2570618A1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 02/01/2006 | EP1620310A1 Aircraft comprising a lift-generating fuselage |
| 02/01/2006 | EP1316409B1 Crash-structure made of fibre reinforced composite material and uses of such a structure |
| 02/01/2006 | EP0757647B1 Main rotor system for helicopters |
| 02/01/2006 | CN1729308A Method for making structural elements by machining thick plates |
| 01/31/2006 | US6991280 Airflow control devices based on active materials |
| 01/31/2006 | US6991082 Ball panel |
| 01/26/2006 | WO2006009489A1 Laminated composite material and a product made thereof |
| 01/26/2006 | WO2006008106A1 Method for the production of a cylindrically bent sheet metal part, particularly an outer sheet metal part of a flying object |
| 01/26/2006 | WO2005039972A3 Ducted fan vtol vehicles |
| 01/26/2006 | US20060018710 Device for joining composite structure elements with metallic structure elements |
| 01/26/2006 | US20060016927 Method and apparatus for rotatably supporting movable components, including canards |
| 01/26/2006 | DE102004032554A1 Verschluss zum Verschließen einer Bauteilöffnung in einem Bauteil Closure for closing an opening component in a component |
| 01/25/2006 | EP1619120A1 Device for the attachment of a partition panel to an interior panel in the interior of a vehicle |
| 01/25/2006 | EP1619116A1 Fish-plating device between composite and metallic structural members |
| 01/25/2006 | EP1436193B1 Aircraft configuration with improved aerodynamic performance |
| 01/24/2006 | CA2247635C Engine parameter activated airplane exit locking system |
| 01/24/2006 | CA2225794C A device and procedure for the thermal protection of a surface against a thermally and mechanically harsh environment |
| 01/22/2006 | CA2511847A1 Fish-jointed unit for composite structure elements with metal structure elements |
| 01/19/2006 | WO2006005550A1 Commercial aircraft with a main deck and a lower deck |
| 01/19/2006 | US20060010769 Emergency door actuator system |
| 01/19/2006 | CA2572460A1 Insulation process |
| 01/19/2006 | CA2570917A1 Commercial aircraft with a main deck and a lower deck |
| 01/18/2006 | EP1616061A2 Contact stiffeners for structural skins |
| 01/18/2006 | CN1236911C Joint construction in laminate of metal and plastic layer |
| 01/17/2006 | US6986484 VTOL aircraft external load drag reduction system |
| 01/12/2006 | WO2005115839B1 Window frame for aircraft |
| 01/12/2006 | WO2005110843A3 Architectural archway for an aircraft |
| 01/12/2006 | US20060006287 Fairing and airfoil apparatus and method |
| 01/12/2006 | US20060006286 Hinge cover integration into door seal edges |
| 01/12/2006 | US20060006285 Device for warning of differential pressure during the opening of a pressurized closing device pertaining to an opening in the fuselage of an aeroplane |
| 01/12/2006 | US20060006284 Floor for aircraft |
| 01/12/2006 | US20060006283 Cockpit floor for aircraft |
| 01/11/2006 | EP1614942A1 Seal for sealing a component opening in a component |
| 01/11/2006 | EP1614625A1 Aircraft floor |
| 01/11/2006 | EP1614624A1 Aircraft floor |
| 01/11/2006 | EP1614623A1 Aircraft door and an aircraft with such a door |
| 01/11/2006 | EP1614622A1 Aircraft cockpit floor |
| 01/11/2006 | EP1614531A2 Titanium-polymer hybrid laminates |
| 01/11/2006 | EP1406813B1 Method and device for positioning freight containers on a loading surface |
| 01/10/2006 | US6983912 Hybrid exhaust heat shield for pylon mounted gas turbine engines |
| 01/08/2006 | CA2511864A1 Floor for aircraft |
| 01/08/2006 | CA2511862A1 Floor for aircraft |
| 01/05/2006 | WO2006001859A1 Structural panels for use in aircraft fuselages and other structures |
| 01/05/2006 | US20060000075 Assembly of sealed components |
| 01/05/2006 | CA2857682A1 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| 01/05/2006 | CA2562632A1 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| 01/04/2006 | EP1612139A1 Device and method for mouting the radome of an aircraft |
| 01/04/2006 | EP1612138A1 Holder for a panel in an aircraft |
| 01/03/2006 | CA2240542C Adjustable length brace for cyclic loads |
| 12/29/2005 | WO2005124267A1 Shielding composite material |
| 12/29/2005 | WO2005113333A3 Load bearing window |
| 12/29/2005 | WO2005084152A3 Aircraft fuselage |
| 12/29/2005 | WO2003106796A3 Pressure responsive blowout latch with reservoir |
| 12/29/2005 | DE102004026228A1 Bonded titanium-aluminum component for aircraft, e.g. seat rail, is formed by deep-welding process in aluminum, combined with diffusion process driven by heat flux toward titanium |
| 12/29/2005 | DE102004025383A1 Window frame for aircraft, includes downholders made from fiber-reinforced synthetic resin materials and which support window pieces e.g. window panes to inner flange or vertical flange |
| 12/29/2005 | CA2510908A1 Device and method for fastening an aircraft radome |
| 12/28/2005 | EP1608553A1 Integral frame member for an aircraft |
| 12/28/2005 | EP1240077B1 Sound-proofing panel, in particular a rotorcraft structural or lining panel |