| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 01/15/2009 | CA2690009A1 Conveyor device intended in particular for luggage in an aircraft hold |
| 01/15/2009 | CA2675274A1 Aircraft window erosion shield |
| 01/14/2009 | EP1668271B1 A vibration isolation mount and method |
| 01/14/2009 | CN101346277A Locking device for fastening a container |
| 01/14/2009 | CN101346275A Method of dimensioning and producing stiffened structural components, use of structural condition sensors and an aircraft |
| 01/14/2009 | CN101342942A Disposal solidifying and forming technique for frame and outer panel skin of wing profile |
| 01/14/2009 | CN101342941A Disposal solidifying and molding method for fuselage ring and outer panel skin |
| 01/13/2009 | US7475853 Method and system for regulating external fluid flow over an object's surface, and particularly a wing and diffuser |
| 01/13/2009 | US7475850 Cockpit floor for aircraft |
| 01/13/2009 | CA2356802C In-flight calibration of air data systems using a nose-mask sensor |
| 01/08/2009 | WO2009004200A1 Reduced dimension landing gear casing |
| 01/08/2009 | WO2009003954A1 Cover for an aircraft access opening |
| 01/08/2009 | WO2009003870A2 Structural component with rib and cross member element |
| 01/08/2009 | US20090008502 Aircraft Fuselage Interior |
| 01/08/2009 | CA2692291A1 Cover for an aircraft access opening |
| 01/08/2009 | CA2691148A1 Reduced dimension landing gear casing |
| 01/08/2009 | CA2690590A1 Structural component with rib and cross member element |
| 01/07/2009 | EP2010384A1 Laminated glazing and sealing and peripheral reinforcing means for same |
| 01/07/2009 | EP1544099B1 Method of joining structural elements in an aircraft |
| 01/07/2009 | CN101341070A A joint for use in aircraft construction |
| 01/07/2009 | CN101341069A Aircraft door assembly, and aircraft fuselage comprising such an aircraft door assembly |
| 01/07/2009 | CN101341068A Safety system for reducing the impact energy of a container |
| 01/07/2009 | CN101341067A Method for producing a fuselage cell of an aircraft |
| 01/07/2009 | CN100448744C Device and method for floor heating in an aircraft |
| 01/06/2009 | US7472867 Support roller arrangement for use in an aircraft cargo hold |
| 01/06/2009 | CA2314162C Assembly procedure for a flexible panel for an open structure and system for implementing the procedure |
| 01/02/2009 | DE102007030422A1 Retaining bracket for detachably fixing cladding panel to passenger airplane, has retainer linearly movable relative to another retainer to introduce former retainer' connecting elements partially into connecting elements of latter retainer |
| 01/02/2009 | DE102007030026A1 Strukturbauteil mit Spant- und Querträgerelement Structural component with direction of the ribs and cross member |
| 01/02/2009 | DE102007029762A1 Verfahren und Vorrichtung zur Verbindung eines trockenen Faserbands mit einem trockenen Faserstrang Method and apparatus for connection of a dry fiber tape with a dry fiber strand |
| 01/02/2009 | DE102007029500A1 Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil Method for coupling stiffening profile elements and structural component |
| 01/02/2009 | DE102007029337A1 Korrosionsfeste Verbindung zwischen einem ersten Bauteil und einem zweiten Bauteil Corrosion-resistant connection between a first component and a second component |
| 01/02/2009 | DE102007028918A1 Verfahren zur Herstellung einer Rumpfzelle eines Flugzeugs sowie Vorrichtung A process for producing a fuselage cell of an aircraft, as well as apparatus |
| 01/02/2009 | DE102004014745B4 Frachtdeck Cargo deck |
| 01/01/2009 | US20090001217 Pre-fabricated article for eme protection of an aircraft |
| 12/31/2008 | WO2009000873A1 Aeronautical component and method to produce it |
| 12/31/2008 | WO2009000863A1 Corrosion-resistant connection between a first component and a second component |
| 12/31/2008 | WO2009000761A2 Method and device for producing a fuselage cell of an airplane |
| 12/31/2008 | WO2009000734A2 Method for coupling stiffening profile elements and structural component |
| 12/31/2008 | WO2008115301A3 Composite laminate having a damping interlayer and method of making the same |
| 12/31/2008 | EP2007622A1 Aircraft floor, use of said floor and aircraft section fitted with said floor |
| 12/31/2008 | EP2007621A1 Locking system for an aircraft door, especially for an airplane passenger door |
| 12/31/2008 | EP1537993B1 Method for making a laminated structure and aeroplane provided with such a structure |
| 12/31/2008 | CN101336191A Extended decompression flap arrangement |
| 12/31/2008 | CN100447469C Tubular metal fitting expandable in a wall opening and method of installation |
| 12/31/2008 | CN100447051C Window frame for aircraft |
| 12/31/2008 | CN100447050C Window frame for aircraft |
| 12/31/2008 | CN100447049C Commercial aircraft with a main deck and a lower deck |
| 12/31/2008 | CA2688655A1 Corrosion-resistant connection between a first component and a second component |
| 12/31/2008 | CA2688137A1 Method and device for producing a fuselage cell of an airplane |
| 12/31/2008 | CA2687553A1 Method for coupling stiffening profile elements and structural component |
| 12/30/2008 | US7469860 Aircraft archway architecture |
| 12/25/2008 | US20080317562 Aircraft Payload Retention System For Interior Loads |
| 12/25/2008 | US20080315037 Safety System for Reducing the Impact Energy of a Container |
| 12/25/2008 | US20080315036 Aircraft Having Multiple Seating Configurations and Associated Systems and Methods |
| 12/24/2008 | WO2008157075A1 Method of forming panels using an in-situ tape placement process and panels formed therefrom |
| 12/24/2008 | WO2008156966A1 Radio frequency shielding apparatus system and method |
| 12/24/2008 | WO2008156802A1 Asset protection method and apparatus |
| 12/24/2008 | EP2004481A1 Aircraft door with oversizing |
| 12/24/2008 | EP2004480A2 Aircraft fuselage with circular-arc-shaped exterior contour |
| 12/24/2008 | DE102007028098A1 Flugzeug mit Rumpfschale und Fußbodenstruktur Aircraft hull and floor structure |
| 12/23/2008 | US7467764 Fuselage mounted evacuation slide system |
| 12/18/2008 | WO2008154066A2 Methods and apparatus for aircraft |
| 12/18/2008 | WO2008152248A2 Aircraft structural element located at the interface between a wing and the fuselage |
| 12/18/2008 | WO2008151756A1 Differential pressure-controlled locking mechanism |
| 12/18/2008 | WO2008127418A3 Sol-gel coating method and composition |
| 12/18/2008 | WO2008113612A3 Gap covering device |
| 12/18/2008 | US20080308682 Automatic Velocity Control System For Aircraft |
| 12/18/2008 | US20080308678 Application of insulating coating |
| 12/18/2008 | US20080308677 Radio frequency shielding apparatus system and method |
| 12/18/2008 | US20080308676 Aircraft Fuselage |
| 12/18/2008 | DE102008026096A1 Kraftantriebseinheit mit exzentrischem Rollenhebesystem Power unit with eccentric roller lifting system |
| 12/18/2008 | DE102007027735A1 Aircraft window, has protection device for incident light rays and formed such that protection against sun and ultra violet rays is provided based on angle of incidence of light rays on window |
| 12/18/2008 | DE102007027550A1 Differenzdruckgesteuerter Verriegelungsmechanismus Differential pressure controlled locking mechanism |
| 12/18/2008 | DE102007027113A1 Verfahren zur Fertigung von Rumpfzellenabschnitten für Flugzeuge mit Faserverbundwerkstoffen sowie Vorrichtung Process for the production of fuselage sections for aircraft with composite fiber materials and device |
| 12/18/2008 | CA2687437A1 Aircraft structural element located at the interface between a wing and the fuselage |
| 12/17/2008 | EP2002076A1 Door stop pin assembly |
| 12/17/2008 | CN101323370A Joint of body and wing of large-sized civil aeroplane |
| 12/17/2008 | CN100443370C Covering device for a hinge of an aircraft |
| 12/11/2008 | WO2008151195A1 Method of extending length of aircraft to increase interior space |
| 12/11/2008 | WO2008150714A1 Bladderless mold line conformal hat stringer |
| 12/11/2008 | WO2008150712A1 Manufacturing process using bladderless mold line conformal hat stringer |
| 12/11/2008 | WO2008150688A1 Apparatus and methods for securing a first structural member and a second structural member to one another |
| 12/11/2008 | US20080305000 Aluminum-magnesium-silver based alloys |
| 12/11/2008 | US20080304931 Overrideable guide and vertical restraint for an air cargo system |
| 12/11/2008 | US20080302915 Manufacturing Process Using Bladderless Mold Line Conformal Hat Stringer |
| 12/11/2008 | US20080302914 Connection element for power transmission between a flap actuator and a flap mounted on a wing of an aircraft so as to swivel |
| 12/11/2008 | US20080302913 Cargo floor, system, and method |
| 12/11/2008 | US20080302912 Bladderless Mold Line Conformal Hat Stringer |
| 12/11/2008 | US20080302909 Cargo roller tray shear fitting |
| 12/11/2008 | DE102007026099A1 Vorrichtung und Verfahren zum Bearbeiten einer Faserverbundstruktur Apparatus and method for processing a fiber compound structure |
| 12/11/2008 | CA2687891A1 Method of extending length of aircraft to increase interior space |
| 12/10/2008 | EP1999013A1 Aircraft component |
| 12/10/2008 | EP1999012A2 Aircraft fuselage interior |
| 12/10/2008 | EP1861311B1 Device and method for non-symmetrical mixed carbon-metal assembly |
| 12/10/2008 | EP1766102B1 Method for making high-tenacity and high-fatigue strength aluminium alloy products |
| 12/10/2008 | CN101321665A Conductive gasket apparatus and method |
| 12/10/2008 | CN101321664A Aircraft pressurized cabin door made of fiber composite |
| 12/09/2008 | US7461816 Internal arrangement of the walls of the fuselage of an aircraft |
| 12/09/2008 | CA2337725C Integral structural shell component for an aircraft and method of manufacturing the same |
| 12/04/2008 | WO2008147754A1 Hybrid composite material having damping generating metallic fibers and method for making the same |