| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 10/30/2008 | DE102007019692A1 Flügel-Rumpf-Sektion eines Flugzeugs Wing-fuselage section of an aircraft |
| 10/30/2008 | DE102007018753A1 Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten Fire protection area for aircraft passengers using Rumpfbehäutung of fiber-metal laminates |
| 10/30/2008 | DE102007018325A1 Mounting device for supporting trunk section of air or spacecraft, has stiffener holder for locking stiffener of trunk section and rotating support supports stiffener holder in rotatable manner |
| 10/30/2008 | DE102007018279A1 Flugzeugtürfenster eines Verkehrsflugzeugs Aircraft door window of a commercial aircraft |
| 10/30/2008 | DE102006046518B4 Verfahren zum Beschichten eines Substrates A method for coating a substrate |
| 10/30/2008 | CA2678644A1 Attachment arrangement for attaching a component to the fuselage of an aircraft, aircraft and method for constructing an attachment arrangement |
| 10/30/2008 | CA2630071A1 Dual action structural latch |
| 10/30/2008 | CA2624214A1 Rib structure for torsion boxes of a wing or horizontal stabiliser of an aircraft |
| 10/29/2008 | EP1984243A1 Double-walled floor segment for a means of locomotion for accommodating system components |
| 10/29/2008 | EP1984242A1 Oscillation damper for installed parts in aircraft |
| 10/29/2008 | EP1984241A1 Method for autoclave-free adhesive bonding of components for aircraft |
| 10/29/2008 | EP1984204A1 Floor structure in an aircraft with continuous panels |
| 10/29/2008 | EP1720767B1 Force feedback refueling system for unmanned aircraft |
| 10/28/2008 | US7441726 Flight deck security pocket door system |
| 10/28/2008 | US7441725 Aircraft wet wing |
| 10/23/2008 | WO2008127481A2 Fuel range for an aircraft |
| 10/23/2008 | WO2008103665A3 Modular galley unit including beverage maker |
| 10/23/2008 | WO2008096088A3 Aircraft cabin window assembly method |
| 10/23/2008 | WO2008096087A3 Section of aircraft fuselage and aircraft including one such section |
| 10/23/2008 | WO2008073150A3 Window assembly and method for a mobile platform |
| 10/23/2008 | WO2007089302A3 Tool for use with ski boots, bindings and boards |
| 10/23/2008 | US20080258016 Nacelle assembly without lower bi-fi splitter |
| 10/23/2008 | US20080258009 Leading edge for aircraft made of reinforced composite material |
| 10/23/2008 | US20080258008 Joint for Use in Aircraft Construction |
| 10/23/2008 | US20080258007 Attaching panels to support structures in an aircraft |
| 10/23/2008 | DE102006045633B4 Verfahren zum Anbinden eines Stringers an ein Strukturbauteil eines Luft- oder Raumfahrzeugs A method for attaching a stringer to a structural component of an aircraft or spacecraft |
| 10/22/2008 | CN101291846A Aircraft safety system |
| 10/21/2008 | US7438263 Optimal aircraft window shape for noise control |
| 10/21/2008 | CA2315335C High performance insulations and methods of manufacturing the same |
| 10/16/2008 | US20080251641 Commercial Aircraft With a Main Deck and a Lower Deck |
| 10/16/2008 | DE202008008215U1 Krafteinleitungselement für Faserverbundstreben in Flugzeugen Force transmission element for composite struts in aircraft |
| 10/15/2008 | EP1979231A1 Cargo receiving arrangement for an aircraft hold |
| 10/15/2008 | EP1979230A1 Flight deck and airplane comprising such a flight deck |
| 10/15/2008 | CN201132606Y Travelling stair self-mounted on aeroplane |
| 10/14/2008 | CA2280413C Device for positioning a break in a transparent panel that consists of a minimum of two layers, and the resulting panel |
| 10/09/2008 | WO2008121418A1 A passive drag modification system |
| 10/09/2008 | WO2008121005A1 Aircraft component manufacture and assembly |
| 10/09/2008 | WO2008119698A1 Under-floor system for an aircraft |
| 10/09/2008 | WO2008099097A3 Aircraft wing including a plurality of dismountable members |
| 10/09/2008 | WO2008090144B1 Connecting element and use of such a connecting element for fastening aircraft components in the case of a cfk-metal hybrid construction |
| 10/09/2008 | WO2008059168A3 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 10/09/2008 | US20080245929 Systems and Methods for Fabricating Multi-Material Joining Mechanisms |
| 10/09/2008 | CA2677717A1 Under-floor system for an aircraft |
| 10/08/2008 | EP1976752A1 Extended decompression flap arrangement |
| 10/08/2008 | EP1976751A2 Deformable forward pressure bulkhead for an aircraft |
| 10/08/2008 | CN100423990C Reverse pulse explosion heat-resistant and damping method for high supersonic aerocraft |
| 10/08/2008 | CN100423989C Ablation-free self-adaptive heat-resistant and damping system for high supersonic aerocraft |
| 10/07/2008 | US7431239 One-piece closed-shape structure and method of forming same |
| 10/07/2008 | CA2449285C Infrared segmented rf signature managed window |
| 10/07/2008 | CA2399719C Pitch-based carbon foam and composites and uses thereof |
| 10/02/2008 | WO2008118732A1 Flexible composite multiple layer fire-resistant insulation structure |
| 10/02/2008 | WO2008118076A1 System for transportation of goods in a loading space |
| 10/02/2008 | WO2008096073A3 Aircraft fuselage |
| 10/02/2008 | WO2008090097B1 Fuselage structural component of an aircraft or spacecraft, with a foam layer as thermal insulation |
| 10/02/2008 | WO2008090089B1 Fuselage of an aircraft or spacecraft of crp/metal hybrid construction with a metal framework |
| 10/02/2008 | WO2008090039B1 Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component |
| 10/02/2008 | WO2008088708A3 Composite aircraft window frame |
| 10/02/2008 | US20080237922 Composite components with integral protective casings |
| 10/02/2008 | US20080237442 Multi-ring system for fuselage barrel formation |
| 10/02/2008 | US20080237404 Hydrogen powered aircraft |
| 10/02/2008 | US20080236708 Preparing metal sheet or plate comprising heat treatable alloy by casting a rolling ingot, homogenizing; hot or cold rolling; reheating, cutting, finishing; pre-maching; solution heat treatment; quenching |
| 10/02/2008 | DE102007015520A1 Unterbodensystem für ein Flugzeug Underbody system for an aircraft |
| 10/02/2008 | DE102007015517A1 Verfahren zur Herstellung eines Strukturbauteils A process for producing a structural component |
| 10/02/2008 | DE102007015007A1 Door frame component for door opening in external panel and for fuselage structure part for aircraft or spacecraft, has contact surface for attaching external panel, in which contact surface is formed |
| 10/02/2008 | DE102007013819A1 Innenaustattungsbauteil für eine Flugzeugkabine Innenaustattungsbauteil for an aircraft cabin |
| 10/02/2008 | DE102005016653B4 Sandwichelement zur schallabsorbierenden Innenverkleidung von Verkehrsmitteln, insbesondere zur schallabsorbierenden Innenverkleidung von Rumpfzellen von Luftfahrzeugen Sandwich panel for sound-absorbing interior lining of transport, particularly for sound absorbing interior lining of fuselage of aircraft |
| 10/02/2008 | CA2679952A1 Flexible composite multiple layer fire-resistant insulation structure |
| 10/02/2008 | CA2666595A1 Hybrid composite-metal aircraft landing gear and engine support beams |
| 10/01/2008 | EP1975061A2 Aircraft internal insulation structure |
| 10/01/2008 | EP1973776A1 Structuring construction for an aircraft fuselage |
| 10/01/2008 | EP1720764B1 Cargo-hold floor for aircraft |
| 10/01/2008 | CN101277869A Polyurethane lacquers as abrasion-resistant coatings |
| 09/30/2008 | US7429074 Airflow control devices based on active materials |
| 09/30/2008 | US7429019 Auxiliary nose undercarriage, a force-transmission structure, and a rotary wing aircraft |
| 09/30/2008 | US7429018 Variable fluid intake with ramp and inflatable bag |
| 09/30/2008 | US7429015 Acoustic absorption blanket mounting system for an aircraft cabin |
| 09/30/2008 | CA2396436C An aircraft window of synthetic resin having hard coated film and a method for producing the same |
| 09/30/2008 | CA2372166C Aircraft wing and fuselage contours |
| 09/25/2008 | WO2008113613A2 Interior trim component for an aircraft cabin |
| 09/25/2008 | WO2008113612A2 Gap covering device |
| 09/25/2008 | WO2008063247A3 Improved composite resin window frame constructions for airplanes |
| 09/25/2008 | WO2008039168A3 Composite thermoplastic matrix airframe structure and method of manufacture therefor |
| 09/25/2008 | WO2007106863A3 Methods and apparatus for reducing noise via a plasma fairing |
| 09/25/2008 | US20080230653 Self-Powered Dimmable Windows with Integrated Controls |
| 09/25/2008 | US20080230652 Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
| 09/25/2008 | DE102007013904A1 Spaltabdeckvorrichtung Spaltabdeckvorrichtung |
| 09/25/2008 | DE102004033068B4 Verkehrsflugzeug mit einem Hauptdeck und einem Unterdeck Airliner with a main deck and lower deck |
| 09/25/2008 | CA2684629A1 Gap covering device |
| 09/24/2008 | EP1971797A1 Device for protecting and guiding a cable of an openable window of an aircraft flight cabin |
| 09/24/2008 | EP1971522A2 Process and system for controlling the pressure in an aircraft cabin |
| 09/24/2008 | CN101272949A Sound absorbing element and method for producing the same |
| 09/24/2008 | CN101272948A Floor panel and installation for fixing layout elements comprising such panels |
| 09/24/2008 | CN101272947A Water deflector and system having multiple water deflectors of this type |
| 09/24/2008 | CN100420607C Aircraft frame |
| 09/23/2008 | CA2444560C Method and apparatus for rotatably supporting movable components, including canards |
| 09/18/2008 | WO2008090084A3 Lining for an aircraft |
| 09/18/2008 | WO2008087194A3 Method of welding a thermoplastic material to a fibre composite material and device manufactured therewith |
| 09/18/2008 | US20080223986 Trussed Structure |
| 09/18/2008 | US20080223985 Splicing Fuselage Sections without Shims |
| 09/18/2008 | DE102007010692A1 Eccentric bush arrangement for use during aircraft mounting, has eccentric bushes including projections provided in sections in respective recesses to obtain anti-twist protection of bushes in relation to each other |