| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 08/06/2008 | EP1812288B1 Structural frame for an aircraft fuselage |
| 08/06/2008 | EP1549545B1 Lightning strike protection and grounding of a composite aircraft panel |
| 08/06/2008 | CN101238030A Window element for insertion in a window cutout in an outer skin of an aircraft |
| 08/06/2008 | CN100408429C Perforated skin structure for laminar-flow systems |
| 08/05/2008 | US7408629 Passive measurement of terrain parameters |
| 08/05/2008 | US7407136 Static port skin applique apparatus and method |
| 08/05/2008 | US7407134 Auxiliary nose undercarriage, a force-transmission structure, and a rotary wing aircraft |
| 08/05/2008 | US7407131 Method for creating an aeronautic sound shield having gas distributors arranged on the engines, wings, and nose of an aircraft |
| 08/05/2008 | CA2436810C Automated fabrication of an integral fiber reinforced composite structural component using a positioning and assembly support |
| 07/31/2008 | WO2008091347A1 Embedded conductor honeycomb core and sandwich panel incorporating same |
| 07/31/2008 | WO2008090176A1 Shell element as part of an aircraft fuselage |
| 07/31/2008 | WO2008090144A1 Connecting element and use of such a connecting element for fastening aircraft components in the case of a cfk-metal hybrid construction |
| 07/31/2008 | WO2008090097A1 Fuselage structural component of an aircraft or spacecraft, with a foam layer as thermal insulation |
| 07/31/2008 | WO2008090089A1 Fuselage of an aircraft or spacecraft of crp/metal hybrid construction with a metal framework |
| 07/31/2008 | WO2008090084A2 Lining for an aircraft |
| 07/31/2008 | WO2008090039A1 Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component |
| 07/31/2008 | WO2008039230A3 Aircraft window assembly |
| 07/31/2008 | US20080179461 Stiffening element for an aircraft or spacecraft, and method for its production |
| 07/31/2008 | US20080179460 Aircraft load frame made of a composite material |
| 07/31/2008 | US20080179459 Pressure bulkhead made of composite material for an aircraft |
| 07/31/2008 | US20080179450 Lifting-Type Aeroplane Fuselage |
| 07/31/2008 | US20080179448 Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein |
| 07/31/2008 | DE102007011627A1 Innenverkleidung für ein Luftfahrzeug Interior trim for an aircraft |
| 07/31/2008 | DE102007011621A1 Vorrichtung, insbesondere Samerstange, zur Aussteifung einer Rumpfzellenstruktur eines Luftfahrzeugs und/oder zur Befestigung eines Bauteils Device, especially Samer rod for stiffening a fuselage structure of an aircraft and / or for fastening a component |
| 07/31/2008 | DE102007011619A1 Bodenplatte zur Bildung einer Ladefläche in einem Frachtraum eines Luftfahrzeugs Bottom plate to form a loading area in a cargo space of an aircraft |
| 07/31/2008 | DE102007011618A1 Crashpaddel zur Verstärkung einer primären Rumpfstruktur eines Flugzeugs Crash paddle to gain a primary fuselage structure of an aircraft |
| 07/31/2008 | DE102007004554A1 Seat rail for fixing components in aircraft, has rail base section and bearing surface section, where both sections are connected by connecting section |
| 07/31/2008 | DE102007004314A1 Method for manufacturing fiber composite component with interspersed area for aircraft or spacecraft, involves transforming tape clutch in area of break-through for forming interspersed range |
| 07/31/2008 | DE102007004313A1 Method for manufacturing construction unit for airplane or spacecraft, involves providing panel which has fiber connected material, and cross bracing elements are fixed on panel |
| 07/31/2008 | DE102007004312A1 Fiber composite component producing method for e.g. spacecraft, involves hardening component together with multiple packed reinforcement elements subjected to vacuum for forming fiber composite component |
| 07/31/2008 | DE102007003276A1 Verbindungselement und Verwendung eines derartigen Verbindungselementes zum Befestigen von Flugzeugbauteilen bei einer CFK-Metall Hybridkonstruktion Connector and use of such a connecting element for attaching aircraft components at a CFRP-metal hybrid construction |
| 07/31/2008 | CA2672029A1 Lining for an aircraft |
| 07/31/2008 | CA2671942A1 Device, in particular connection rod, for bracing a fuselage structure of an aircraft and/or for fastening a component |
| 07/31/2008 | CA2671920A1 Shell element as part of an aircraft fuselage |
| 07/31/2008 | CA2671917A1 Connecting element and use of such a connecting element for fastening aircraft components in the case of a cfk-metal hybrid construction |
| 07/31/2008 | CA2671908A1 Fuselage structural component of an aircraft or spacecraft, with a foam layer as thermal insulation |
| 07/31/2008 | CA2671896A1 Fuselage of an aircraft or spacecraft of crp/metal hybrid construction with a metal framework |
| 07/30/2008 | EP1948503A1 Integrally damped composite aircraft floor panels |
| 07/30/2008 | EP1948502A1 Method for producing a fuselage cell of an aircraft |
| 07/30/2008 | EP1888870B1 Ladder system, especially for vehicles |
| 07/30/2008 | CN101233289A Control device for locking and unlocking and aircraft door and aircraft door that integrates such a device |
| 07/29/2008 | US7406403 Systems and methods for automatically generating 3D wireframe CAD models of aircraft |
| 07/29/2008 | CA2331441C Crash energy absorbing glareshield and method of protecting against head injury in aircraft crashes |
| 07/29/2008 | CA2328573C Composite junction for the assembly of at least one external device on a sandwich panel and panel incorporating at least one such junction |
| 07/24/2008 | WO2008088708A2 Composite aircraft window frame |
| 07/24/2008 | WO2008087194A2 Method of welding a thermoplastic material to a fibre composite material and device manufactured therewith |
| 07/24/2008 | WO2007053362A3 Single piece fuselage barrel |
| 07/24/2008 | US20080174126 Latch device for mounting sheet-like linings |
| 07/24/2008 | US20080173765 Airframe structure of an aircraft or spacecraft |
| 07/24/2008 | US20080173761 Fitting for introducing high forces into a fuselage cell of an aircraft |
| 07/24/2008 | US20080173760 System for opening and closing a landing-gear compartment for an aircraft |
| 07/24/2008 | US20080173758 Crash paddle for reinforcing a primary fuselage structure of an aircraft |
| 07/24/2008 | US20080173757 Rib support for wing panels |
| 07/24/2008 | US20080173755 Floor panel for forming a loading area in a cargo hold of an aircraft |
| 07/24/2008 | US20080172959 Bonded aluminum window frame on fibre metal laminate fuselage skin |
| 07/24/2008 | DE10319504B4 Fördereinrichtung an einem Fracht-Deck eines Flugzeugs Conveyor at a cargo deck of an aircraft |
| 07/24/2008 | DE102007011613A1 Beschlag zur Einleitung von hohen Kräften in eine Rumpfzelle eines Flugzeugs Fitting for the introduction of high forces in a fuselage airframe of an aircraft |
| 07/24/2008 | DE102007011611A1 Befestigungsanordnung für Verzurrbügel in einem Frachtraumboden eines Flugzeugs Mounting arrangement for Verzurrbügel in a cargo compartment floor of an aircraft |
| 07/24/2008 | DE102007003793A1 Vorrichtung mit Spreizbandantrieb und deren Verwendung im Flugzeugbau Device with Spreizbandantrieb and their use in aircraft |
| 07/24/2008 | DE102007003358A1 Method for bonding thermoplastic material with fibre-reinforced material, e.g. for making composite articles such as side panels and hat-rack casings in aircraft cabins, involves welding the components together |
| 07/24/2008 | DE102007003357A1 Verfahren zum Verbinden eines thermoplastischen Materials mit einem Faserverbundmaterial A method of joining a thermoplastic material with a fibrous composite material |
| 07/24/2008 | DE102007003278A1 Rumpfstrukturbauteil eines Luft- oder Raumfahrzeuges mit einer Schaumstoffschicht als thermische Isolierung Hull structural component of an aircraft or space vehicle with a foam layer as a thermal insulator |
| 07/24/2008 | DE102007003277A1 Rumpf eines Luft- oder Raumfahrzeuges in CFK-Metall Hybridbauweise mit einem Metallrahmen Fuselage of an aircraft or spacecraft in CFRP-metal hybrid construction with a metal frame |
| 07/24/2008 | DE102007003275A1 Schalenelement als Teil eines Flugzeugrumpfes Shell element as part of an aircraft fuselage |
| 07/24/2008 | DE10145272B4 Flugzeug, insbesondere Passagierflugzeug, mit einem auf der Basis von Faserverbundbauteilen aufgebauten Rumpf Aircraft, especially passenger aircraft, with a built up on the basis of composite components hull |
| 07/24/2008 | CA2676317A1 Method of joining a thermoplastic material to a fibre composite material |
| 07/24/2008 | CA2675206A1 Composite aircraft window frame |
| 07/23/2008 | EP1945500A1 Window arrangement for installing larger aircraft windows |
| 07/23/2008 | CN101228066A Lateral force joint |
| 07/22/2008 | US7402973 Power drive unit with unit load device sensor |
| 07/22/2008 | US7401751 Fluid flow regulator with overpressure relief function |
| 07/22/2008 | US7401682 Architecture for an acoustic liner |
| 07/17/2008 | WO2008085547A2 Aerodynamic integration of a payload container with a vertical take-off and landing aircraft |
| 07/17/2008 | WO2008084089A1 Coating of an aircraft seat mounting rail or a aircraft seat stud |
| 07/17/2008 | US20080169382 Sealing system for the gap existing between the fuselage and the elevator of an aircraft with orientable horizontal stabiliser |
| 07/17/2008 | US20080169381 Aircraft window erosion shield |
| 07/17/2008 | US20080169380 Composite aircraft window frame |
| 07/17/2008 | US20080168619 Process For Production of Aircraft Stops, and Aircraft Door Stops Made of Carbon Composite Material |
| 07/17/2008 | DE202007014781U1 Ablenkvorflügel Ablenkvorflügel |
| 07/17/2008 | CA2672833A1 Coating of an aircraft seat mounting rail or a aircraft seat stud |
| 07/16/2008 | CN101223080A Monolithic self-stiffened panels |
| 07/16/2008 | CN101222999A Method for connection at least two pieces of sheet material, particularly at least two metal sheets for a lightweight structure as well a joining and lightweight structure |
| 07/16/2008 | CN101219587A Composite stressed-skin construction for fuselage and technique of preparing the same |
| 07/10/2008 | WO2008058746B1 Window element for inserting in a structural part and method of integration of a window element in a structural part |
| 07/10/2008 | US20080164376 Leading edge skin height difference adjusting structure and method of assembling leading edge skin |
| 07/10/2008 | US20080164375 Arrangement for coupling a coupling pivot for a trimmable horizontal stabiliser to the tail fuselage of an aircraft |
| 07/10/2008 | US20080164374 Air discharge device for an aircraft |
| 07/10/2008 | US20080164373 Door arrangement and aircraft |
| 07/10/2008 | US20080164372 Method of optimizing stiffened panels under stress |
| 07/10/2008 | US20080164371 System and method for converting a passenger aircraft to a cargo aircraft |
| 07/10/2008 | DE102004003773B4 Optisches System und Verfahren zur Aufnahme einer Anzahl von Bildern Optical system and method for receiving a number of images |
| 07/09/2008 | EP1942052A1 Rib support for wing panels |
| 07/09/2008 | CN101214852A Connecting structure for unmanned aerial vehicle body and wing |
| 07/08/2008 | US7395989 Aircraft fuselage and corresponding aircraft |
| 07/08/2008 | CA2281130C A process for making a dismountable and/or fixed traction-compression coupling to be applied to composite materials |
| 07/08/2008 | CA2256887C Environment control system for aircraft having interior condensation problem reduction, cabin air quality improvement, fire suppression and fire venting functions |
| 07/03/2008 | WO2008080027A1 Seat track assembly |
| 07/03/2008 | WO2008079181A2 Mounting device for a line replaceable unit in an aircraft and a method for using the same |
| 07/03/2008 | US20080156935 Composite internal beam for reinforcing the structrue of an aircraft |
| 07/03/2008 | US20080156934 Apparatus and methods of attaching panels to support structures |