Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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07/19/2006 | EP1681236A1 Structural element for an aircraft |
07/18/2006 | CA2170609C Structural cellular component |
07/13/2006 | WO2006072749A2 Improvement to aircraft cabin doors |
07/13/2006 | WO2006072131A1 Panel and clamping fasteners |
07/13/2006 | WO2005096721A3 Landing gear noise attenuation |
07/13/2006 | US20060151668 Pivot mechanism for quick installation of stowage bins or rotating items |
07/13/2006 | DE10335483B4 Hohlkörper bestehend aus mindestens zwei miteinander verbundenen Bauteilen Hollow body consisting of at least two connected components |
07/13/2006 | DE102004032554B4 Verschluss zum Verschließen einer Bauteilöffnung in einem Bauteil Closure for closing an opening component in a component |
07/13/2006 | CA2591112A1 Apparatus, system and method for drag reduction |
07/12/2006 | EP1678460A2 System and method with adaptive angle-of-attack autopilot |
07/11/2006 | US7076341 Autonomous manoeuvring for spinning spacecraft |
07/11/2006 | US7073994 Cargo deck for an aircraft |
07/11/2006 | CA2414700C Aircraft windows and associated methods for installation |
07/11/2006 | CA2405923C Snap-in window assembly and method |
07/11/2006 | CA2326314C Burn through resistant systems for transportation, especially aircraft |
07/06/2006 | WO2006071207A2 Dynamic cmg array and method |
07/06/2006 | WO2006070016A1 Monolithic composite panel with multicell box shape |
07/06/2006 | WO2006070014A1 Aircraft with a rear fuselage protection shield |
07/06/2006 | WO2005102839A3 Method and apparatus for braking and maneuvering |
07/06/2006 | US20060147704 Method to eliminate undulations in a composite panel |
07/06/2006 | US20060145013 Sealing device for a flap track in a belly fairing of an aircraft for a flap-actuating shaft |
07/06/2006 | US20060145012 Reinforced cover for gaps in an aerodynamic contour |
07/06/2006 | US20060145009 Penetration- and fire-resistant fabric materials and structures |
07/06/2006 | US20060145008 Airplane surface protection film kits |
07/06/2006 | US20060145002 Modular galley for an aircraft or train as well as wall and modular for such a galley and aircraft or train equipped therewith |
07/06/2006 | DE10117964B4 Kabinenfensterverkleidung für Passagierkabinen, insbesondere in einem Verkehrsflugzeug Cabin window trim for passenger cars, especially in a commercial aircraft |
07/06/2006 | CA2592594A1 Monolithic composite panel with multicell box shape |
07/05/2006 | EP0912394B8 Ball mat |
07/05/2006 | CN1798686A Crashworthiness structure and method |
07/05/2006 | CN1798682A Fluid handling component with ultraphobic surfaces |
07/04/2006 | US7070850 backing layer having an outer, exposed patterned surface that reduces drag, an adhesive bonding layer, and an intermediate layer between them; free of a reinforcing layer. |
06/29/2006 | WO2006069291A2 System and method for utilizing stored electrical energy for vtol aircraft thrust enhancement and attitude control |
06/29/2006 | US20060138281 Flight lock actuator with dual energy sources |
06/29/2006 | US20060138280 Arrangement and method for utilizing the heat of waste air for heating the bilge area of aircraft |
06/28/2006 | EP1674650A2 Window shade assembly with a motorized window shade mechanism |
06/28/2006 | EP1673218A2 Cross-reference to related applications |
06/28/2006 | EP1620310B1 Aircraft with a lift-generating fuselage |
06/22/2006 | CA2530901A1 Adhesive joint for joining components of transport craft, in particular of aircraft, and method for determining minimum mechanical load capacity and/or mechanical strength of an adhesive joint |
06/20/2006 | US7063898 A metal fastener having a first layer comprising a chemical conversion coating and a second layer derived from a sol gel of an organometal polymer on the first layer which separates the metal from the cured sol gel film; aircraft rivets having improved adhesion to paint; corrosion resistance |
06/20/2006 | US7063763 Tubular members integrated to form a structure |
06/20/2006 | US7063562 Seat power outlets integrated into floor |
06/15/2006 | WO2006061617A1 A trussed structure |
06/15/2006 | WO2006001860A3 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
06/15/2006 | CA2589043A1 A trussed structure |
06/14/2006 | EP1668271A2 A vibration isolation mount and method |
06/13/2006 | US7059664 Airflow control devices based on active materials |
06/13/2006 | US7059568 Panel for a vehicle |
06/13/2006 | US7059566 Unmanned aerial vehicle for logistical delivery |
06/13/2006 | US7059565 Aircraft frame hole patterns and brackets, and associated methods |
06/13/2006 | US7059090 Fairing access door with reinforcement and method of manufacture |
06/13/2006 | US7059034 One-piece closed-shape structure and method of forming same |
06/08/2006 | WO2006060321A1 Determinant assembly features for vehicle structures |
06/08/2006 | WO2005084152A8 Aircraft fuselage |
06/08/2006 | US20060118676 Integrated window belt system for aircraft cabins |
06/08/2006 | US20060118675 Transformable fluid foil with pivoting spars and ribs |
06/08/2006 | DE112004000995T5 Hoch schadenstolerantes Aluminiumlegierungsprodukt, insbesondere für Luft- und Raumfahrtanwendungen High damage tolerant aluminum alloy product, particularly for aerospace applications |
06/08/2006 | DE102004058014A1 Structural component for aircraft shells has reinforcement element, which is partly coated with cladding element, embedded in the carrier element |
06/07/2006 | EP1666354A1 Structural component, process for manufacturing a structural component and use of a structural component for an aircraft skin |
06/07/2006 | EP1666353A1 Method for fabricating a curved beam from composite material |
06/07/2006 | EP1663776A2 A resin infused transparent skin panel and method of making same |
06/07/2006 | EP1663623A1 Reaction injection molded members and method of forming |
06/06/2006 | US7055781 Cooled insulation surface temperature control system |
06/06/2006 | CA2353229C Aircraft door |
06/01/2006 | US20060113442 Clamp holder for a support structure |
06/01/2006 | DE10145687B4 Anordnung zur Verhinderung des Aufbaus von einem invers wirkenden Differenzluftdruck in einem Flugzeug Arrangement for preventing the build of an inverse-acting differential air pressure in a plane |
06/01/2006 | CA2596429A1 Lifting-type aeroplane fuselage |
05/31/2006 | EP1660307A2 Window skin panel and method of making same |
05/31/2006 | EP1250257A4 Emergency vision apparatus |
05/30/2006 | US7052573 Method to eliminate undulations in a composite panel |
05/30/2006 | US7051979 Auxiliary fuel tank systems for aircraft and methods for their manufacture and use |
05/30/2006 | US7051978 Adaptable payload processes |
05/30/2006 | US7051780 Latch assembly for a bifold cockpit door |
05/30/2006 | CA2527545A1 Retainer and method for attaching lines to lightweight elements of means of transport, in particular to sandwich panels of aircraft |
05/25/2006 | US20060108474 Hollow assembly structure and fabrication method therefor |
05/24/2006 | EP1467910B1 Joint for connecting a longitudinal side to an upper side of components and flexible strip for use in such a joint |
05/24/2006 | EP0912394B1 Ball mat |
05/24/2006 | DE102004056287A1 Vorrichtung und Verfahren zur Fertigung von Sektionen für Verkehrsmittel, insbesondere für Luftfahrzeuge Device and method for the production of the sections for transport, in particular for aircraft |
05/24/2006 | DE102004056286A1 Assembly device for sections of aircraft has several positioning devices by which individual components are positioned relative to each other in space |
05/24/2006 | DE102004056285A1 Components e.g. riveting fixtures, connecting device for aircraft, has handling systems that are positioned in place by positioning mechanisms, where system has articulated robot with handling mechanism |
05/24/2006 | DE102004056284A1 Transporting device for components of aircraft has positioning stand with at least one positioner for alignment in work station |
05/24/2006 | CA2527253A1 Cover skin for a variable-shape aerodynamic area |
05/23/2006 | US7048230 Laminar flow nacelle for an aircraft engine |
05/18/2006 | WO2006051235A1 Structural frame for an aircraft fuselage |
05/18/2006 | US20060102802 Aircraft with forward opening inlay spoilers for yaw control |
05/18/2006 | US20060102792 Pressurized sonobuoy deployment system |
05/18/2006 | US20060102789 Linear shock wave absorber |
05/18/2006 | US20060102788 Increased security flight deck door strike apparatus and method |
05/18/2006 | US20060102787 Aircraft archway |
05/18/2006 | US20060102786 Joint cover in aircraft |
05/18/2006 | US20060102784 Cut to fit powered seat track cover |
05/18/2006 | US20060101771 Modular monolithic bulkhead panel |
05/18/2006 | CA2585869A1 Structural frame for an aircraft fuselage |
05/17/2006 | EP1657453A2 Apparatus, system and method of joining structural components with a tapered tension bond joint |
05/17/2006 | EP0923452B1 Metal sandwich structure with integral hardpoint |
05/16/2006 | CA2420174C Dead bolt lock assembly for flight deck door of an aircraft |
05/11/2006 | WO2005039977A3 A simple, forward-rolling canopy for small airplanes |
05/11/2006 | WO2004076769A3 Contact stiffeners for structural skins |
05/11/2006 | US20060097110 Non-threaded structural insert for component attachment |
05/09/2006 | US7043345 System and method with adaptive angle-of-attack autopilot |
05/09/2006 | US7040577 Attachment apparatus for injection-molded frameless canopies |