| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 08/26/2009 | CN100532196C Fairing for an aircraft structure |
| 08/25/2009 | US7578478 Attaching panels to support structures in an aircraft |
| 08/25/2009 | US7578477 Internal security door for an aircraft |
| 08/25/2009 | US7578476 Aircraft door arrangement |
| 08/25/2009 | US7578475 Pressure responsive blowout latch |
| 08/25/2009 | US7578474 Sealed structural passenger window assembly and method of forming same |
| 08/25/2009 | US7578468 Acoustic absorption system for an aircraft airframe |
| 08/25/2009 | CA2524372C Crashworthiness structure and method |
| 08/25/2009 | CA2421415C Method for producing a fiber composite structural component |
| 08/20/2009 | WO2009102372A2 Fluid resistant composite sandwich panel |
| 08/20/2009 | WO2009101372A1 Energy-absorbing structural element made of a composite material and aircraft fuselage having said absorber |
| 08/20/2009 | WO2008109763A9 Compliant panel for aircraft |
| 08/20/2009 | US20090206202 Energy absorbing structure for aircraft |
| 08/20/2009 | US20090206193 Ballistically deployed telescoping aircraft wing |
| 08/19/2009 | EP2089272A1 Wing/fuselage connection for an aircraft |
| 08/19/2009 | EP2089218A1 Composite structure |
| 08/19/2009 | EP1856498B1 Pressure-difference warning system |
| 08/19/2009 | EP1651518B1 Surface temperature control system |
| 08/19/2009 | CN201292009Y Space shuttle cabin door unlock mechanism |
| 08/19/2009 | CN101511674A Aircraft doorway |
| 08/19/2009 | CN101511673A Panel assembly and method of erecting a panel assembly |
| 08/18/2009 | US7575195 Hinge cover integration into door seal edges |
| 08/18/2009 | US7575194 Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures |
| 08/13/2009 | WO2009100030A2 Tool operated channel latch |
| 08/13/2009 | WO2009098374A2 Interconnection device connecting an aircraft internal structure component to the fuselage of this aircraft |
| 08/13/2009 | WO2009098159A1 Load-supporting and damage-tolerant laminated aircraft window |
| 08/13/2009 | WO2009098098A2 Floor system for a fuselage section of an aircraft |
| 08/13/2009 | WO2009098088A2 Method for producing a fibre composite component fibre composite component and a fibre composite fuselage component of an aircraft |
| 08/13/2009 | WO2009056643A4 Structure, especially a fuselage structure of an aircraft or a spacecraft |
| 08/13/2009 | WO2008078026A3 Functional glazing |
| 08/13/2009 | US20090200431 Aircraft wing tip having a variable incidence angle |
| 08/13/2009 | US20090200425 Fitting |
| 08/13/2009 | US20090200424 Lateral Force Joint |
| 08/13/2009 | DE102008008406A1 Female mold for use in aircraft part i.e. glider body, has partial molds, where each mold is made of paper honeycombs that are laid over pair of shape-suitable supports such that molds form female half shell |
| 08/13/2009 | DE102008008386A1 Verfahren zur Herstellung eines FVW-Bauteils A method for producing a fiber-composite component |
| 08/13/2009 | DE102008007421A1 Verriegelungseinrichtung Locking device |
| 08/13/2009 | DE102007062873A1 Luftfrachtcontainer und Flugzeug Air freight containers and aircraft |
| 08/13/2009 | CA2714175A1 Method for manufacturing a fibre-composite component, fibre-composite component and fibre-composite fuselage component of an aircraft |
| 08/13/2009 | CA2713334A1 Floor system for a fuselage section of an aircraft |
| 08/13/2009 | CA2712398A1 Load-supporting and damage-tolerant laminated aircraft window |
| 08/12/2009 | CN201287827Y Aircraft capable of hiding in side direction |
| 08/12/2009 | CN101506036A Frame element, aircraft component assembly system and method of fitting a component in an aircraft |
| 08/12/2009 | CN101506035A Frame element, aircraft air-conditioning system and method for the installation of a frame element in an aircraft |
| 08/12/2009 | CN101506034A Aircraft with optimised utility volume and method for optimising the utility volume of an aircraft |
| 08/12/2009 | CN101506033A Method, apparatus and plant for manufacturing shell structures |
| 08/12/2009 | CN100526157C Window element for insertion in a window cutout in an outer skin of an aircraft |
| 08/11/2009 | CA2413349C Decompression unit for equalizing an explosive air pressure |
| 08/11/2009 | CA2348113C Friction stir grain refinement of structural members |
| 08/06/2009 | WO2009095133A2 Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component |
| 08/06/2009 | WO2008155720A3 Method and equipment for forming and assembling uncured spars for the horizontal stabilizers of aircraft |
| 08/06/2009 | US20090194640 Apparatus system and method for drag reduction |
| 08/06/2009 | US20090194638 Frangible fasteners and associated systems and methods |
| 08/06/2009 | US20090194637 Aircraft door |
| 08/06/2009 | DE102008007586A1 Electrical energy generating method for airplane, involves subjecting solar modules to solar radiations treading through window pane and partially convert solar radiations into electrical energy |
| 08/06/2009 | CA2712062A1 Connecting arrangement for joining two stiffening elements having different cross-sectional profiles for an aircraft or spacecraft, and shell component |
| 08/05/2009 | EP2084057A2 Composite aircraft structures with hat stiffeners |
| 08/05/2009 | EP1753655B1 Window frame for aircraft |
| 08/05/2009 | CN101500797A Laminate of metal sheets and polymer |
| 08/05/2009 | CN101500787A Improved composite resin window frame constructions for airplanes |
| 08/05/2009 | CA2652746A1 Avionics rack arrangement |
| 08/04/2009 | US7568659 Door which is intended to be positioned between the cockpit and the cabin of an aircraft |
| 07/30/2009 | WO2009092964A1 Pressurised aircraft carrier with open air exposure flap |
| 07/30/2009 | WO2008106585A3 Adherends with enhanced surfaces |
| 07/30/2009 | US20090189019 Rib for aircraft wing and methods for the manufacture thereof |
| 07/30/2009 | US20090189018 Method for isolating a cabin wall of an aircraft or for cooling or heating of cabin air and a cabin wall suitable therefore |
| 07/30/2009 | US20090189017 Releasable fastening of a component in an aircraft |
| 07/30/2009 | US20090189013 Non-handed engine cowl doors for fuselage mounted turbine engines |
| 07/30/2009 | DE10319503B4 Frachtdeck für ein Flugzeug Cargo deck for an aircraft |
| 07/30/2009 | DE102008005595A1 Cargo compartment door for use in fuselage of aircraft, has opening in fuselage closed by cargo compartment door and reinforced with door frame, and two door wings are provided for reducing space required for cargo compartment door |
| 07/30/2009 | DE102007059148B4 Haltenocken für einen Drehverschluss Cam lock for a screw cap |
| 07/30/2009 | DE102006048518B4 Vorrichtung zum weitgehend rückstandsfreien Entfernen von geklebten Fensterrahmen Apparatus for substantially residue-free removal of bonded Frames |
| 07/30/2009 | DE102006045635B4 Verfahren zum Anbinden von vor- bzw. ausgehärteten Stringern an mindestens ein Strukturbauteil eines Luft- oder Raumfahrzeuges Mechanism for attaching forward or cured stringers at least one structural component of an aircraft or spacecraft |
| 07/30/2009 | DE10109638B4 Druckbelastbare Außenhaut einer Flugzeugtür Compression resistant outer skin of an aircraft door |
| 07/30/2009 | CA2712453A1 Pressurised aircraft carrier with open air exposure flap |
| 07/29/2009 | EP2081820A1 Fitting |
| 07/29/2009 | EP2081785A1 Modular airplane cabin window |
| 07/29/2009 | EP1960264B1 Landing gear casing provided with a dissociated structure |
| 07/29/2009 | CN201280225Y Air transportation oil sac mooring apparatus |
| 07/28/2009 | US7566489 Impact-absorbing structural component |
| 07/28/2009 | US7565778 Composite protection for revealing damage to a core in a vehicle such as an aircraft |
| 07/23/2009 | WO2009056476A4 Emergency exit hatch for exiting a cabin module in an emergency and entering the same |
| 07/23/2009 | WO2009056319A4 Transversal butt strap and method for connecting two especially wound cfk fuselage sections in order to create a fuselage cell |
| 07/23/2009 | US20090184206 Particle-filled wing-to-body fairing |
| 07/23/2009 | US20090184202 Structrual element made of an aluminum alloy including an optical sensor |
| 07/23/2009 | US20090184201 Joining fuselage skins using friction stir welding |
| 07/23/2009 | US20090184200 Vibration damping for wing-to-body aircraft fairing |
| 07/23/2009 | DE102008003779A1 Haltevorrichtung Holding device |
| 07/23/2009 | DE102007062747A1 Base plate for covering floor structure in aircraft, has connection point provided for fastening component assembly on plate independent of assembly site on floor structure, and system port arranged in region of plate |
| 07/23/2009 | DE102007062082A1 Core composite, particularly for use in aerospace area, has upper cover layer, lower cover layer and core element arranged between cover layers, where core element is formed as honeycomb structure |
| 07/23/2009 | DE102007060514A1 Device for limiting deflection of door arranged in fuselage cabin of aircraft, particularly hatch or cargo gate, has retaining element arranged preferably in area of door jamb or in area of door sheet edge |
| 07/22/2009 | EP2080699A2 Pressure bulkhead for an airplane |
| 07/22/2009 | EP2080612A1 Distribution of point loads in honeycomb panels |
| 07/22/2009 | CN201276209Y Once solidified and molded wing type frame and covering |
| 07/22/2009 | CN101489868A Aircraft tail cone |
| 07/22/2009 | CN101489867A Storage compartment for the nose gear of an aircraft |
| 07/21/2009 | US7562846 Window retaining system |
| 07/21/2009 | US7562845 Rudder unit connection to a fuselage without a bolt-fairing structure |
| 07/16/2009 | WO2009089282A2 Distortion resistant transparent reinforcing fibers for use in transparent reinforced composites |
| 07/16/2009 | WO2009089193A2 Aircraft trim panel with integrated adjustable acoustic properties |
| 07/16/2009 | US20090181203 Laminated glazing and sealing and peripheral reinforcing means for same |