| Patents for B64C 1 - Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like (12,562) |
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| 05/15/2008 | WO2008057986A1 Combined thermal protection and surface temperature control system |
| 05/15/2008 | WO2007001715A3 System and method for landing a tailless aircraft in a crosswind |
| 05/15/2008 | US20080111027 Sol-gel coating method and composition |
| 05/15/2008 | US20080111026 Splice Joints for Composite Aircraft Fuselages and Other Structures |
| 05/15/2008 | US20080111025 Latch device of cockpit door of an aircraft |
| 05/15/2008 | US20080111024 Composite Aircraft Structures With Hat Stiffeners |
| 05/15/2008 | DE102007051567A1 Selbsteinstellende Führungs- und Haltevorrichtung für das Laden von ULDs Self-guiding and holding device for loading of ULDs |
| 05/15/2008 | DE102006051989A1 Fiber-metal laminate stringer for use in aircraft or spacecraft, has synthetic fiber layers produced from Zylon fibers, and provided between metallic layers, and straight side portions and middle region merge with one another |
| 05/15/2008 | DE102006051462A1 Reinforcement element for shell component of aircraft or spacecraft, has shape stiffener part, which has light metal material, and base part, which has high-corrosion resistant material |
| 05/15/2008 | DE102006051457A1 Stiffening element e.g. for air or space vehicle, has base section and made of fiber composite material with material filling in sub-structure fiber |
| 05/14/2008 | EP1921006A2 Latch device of cockpit door of an aircraft |
| 05/14/2008 | EP1748923B1 Window frame for aircraft |
| 05/14/2008 | EP1735210B1 Foam composite insulation for aircraft |
| 05/14/2008 | CN101180208A Apparatus, system and method for drag reduction |
| 05/13/2008 | US7371304 Apparatuses and methods for joining structural members, such as composite structural members |
| 05/13/2008 | US7370832 Payload to support track interface and fitting apparatus and methods |
| 05/13/2008 | US7370831 Power strip for seats |
| 05/08/2008 | WO2008053041A1 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
| 05/08/2008 | WO2008052801A1 Wing/fuselage connection for an aircraft |
| 05/08/2008 | WO2008010159A3 Method, apparatus and plant for manufacturing shell structures |
| 05/08/2008 | WO2007133182A3 Modular aerospace plane |
| 05/08/2008 | US20080105785 Optimized fuselage structure |
| 05/08/2008 | US20080105783 Fuselage design for sonic boom suppression of supersonic aircraft |
| 05/08/2008 | DE102007025984A1 Bodenschienenbeschlag für Flugzeugsitze Bottom rail fitting for aircraft seats |
| 05/08/2008 | DE102006052082A1 Method for compensation of mechanical stresses in aircraft structure, involves generating of signals, which represents mechanical stresses are developed in aircraft structure |
| 05/08/2008 | DE102006051600A1 Aircraft fuselage structure for tailless aircraft, has structure reinforcements with three dimentional frame work bending support extending over area of small curvature and belts are connected with each other by coupling elements |
| 05/08/2008 | DE102006051572A1 Flügel-Rumpf-Verbindung eines Flugzeugs Wing-fuselage connection of an airplane |
| 05/08/2008 | CA2668358A1 Wing/fuselage connection of an aircraft |
| 05/08/2008 | CA2662141A1 Stiffened casing for an aircraft or spacecraft with a laminate stringer of high rigidity and corresponding laminate stringer |
| 05/07/2008 | EP1918194A2 Ventral fairing for an aircraft |
| 05/07/2008 | EP1917186A2 Aircraft with belly flaps |
| 05/07/2008 | EP1917185A2 Sound-absorbing element for transport means, in particular for aircraft |
| 05/07/2008 | EP1917184A1 Scalable freight loading system, especially for an aircraft |
| 05/07/2008 | CN101172523A Auxiliary power unit assembly |
| 05/07/2008 | CN101172520A 辅助动力装置总成 Auxiliary power unit assembly |
| 05/07/2008 | CN100386245C Transportation means for marine, land and air |
| 05/06/2008 | US7367528 Airport system for operations, safety, and security |
| 05/06/2008 | US7367527 Reinforced insulation product and system suitable for use in an aircraft |
| 05/02/2008 | WO2008049138A1 Modular airplane cabin window |
| 05/02/2008 | CA2666169A1 Modular airplane cabin window |
| 05/01/2008 | US20080099621 Fuselage mounted evacuation slide system |
| 05/01/2008 | US20080099620 Self-adjusting uld loading guide and restraint |
| 05/01/2008 | US20080099616 Electrical interlock and indication system for aircraft |
| 05/01/2008 | US20080099615 Modular aircraft window |
| 05/01/2008 | US20080099614 Unitary one-piece windshield |
| 05/01/2008 | US20080099612 Actuation system for tail section of aircraft |
| 05/01/2008 | US20080099611 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof |
| 05/01/2008 | US20080099610 Ventral fairing for an aircraft |
| 05/01/2008 | US20080099609 Tunable acoustic absorption system for an aircraft cabin |
| 05/01/2008 | US20080099605 Boarding ramp device for aircraft |
| 04/30/2008 | EP1915290A1 Continuous fuselage connection |
| 04/30/2008 | DE102006050534A1 Electrical/optical line system for aircraft, has electrical lines that are integral parts of aircraft component having fuselage sections to form fuselage cells, and wing shells, where lines are connected between components by coupling unit |
| 04/30/2008 | CA2608270A1 Device indicating non-closure of an internal compartment door not visible from the outside |
| 04/30/2008 | CA2590892A1 Tail cone for aircraft with movable fairing and support structure for auxiliary power unit and the ancillary elements thereof |
| 04/29/2008 | US7366592 System for automatically controlling lift-enhancing devices of an aircraft, in particular wing leading edge slats |
| 04/29/2008 | CA2297266C Method for making parts in composite material with thermoplastic matrix |
| 04/24/2008 | US20080093504 Doors of Aircraft Cabins |
| 04/24/2008 | US20080093503 Structural frame for an aircraft fuselage |
| 04/24/2008 | DE102006048641A1 Connecting structure for aircraft or spacecraft, has stringer connected with structure component, and high-impact strength material for local increase of power consumption ability of connecting areas attached in one of connecting areas |
| 04/24/2008 | DE102006048518A1 Device for removing bonded window frames in aircraft, particularly in passenger planes, has support plate and guiding device arranged in area of support plate, by which tool is guided into area of window frame |
| 04/23/2008 | EP1912860A2 Rf shielding for aircraft windows |
| 04/23/2008 | EP1912859A1 Window element for insertion in a window cutout in an outer skin of an aircraft |
| 04/23/2008 | EP1912759A1 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 |
| 04/23/2008 | EP1608553B1 Integral frame member for an aircraft |
| 04/17/2008 | WO2008043940A2 Aircraft fuselage made from longitudinal panels and method of producing such a fuselage |
| 04/17/2008 | WO2008043557A1 Self-supporting interior cabin structure with integrated installation elements |
| 04/17/2008 | US20080087768 Aircraft component |
| 04/17/2008 | DE102006049075A1 Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen Adjusting device for aligning bearing parts of structures subject to tolerance |
| 04/17/2008 | DE102006048376A1 Cabin structure unit for mounting cabin installation unit for airplane, has reinforcing rib arranged between support frames, where structure unit is designed in self-supportable manner and is mounted in airplane and floor structures |
| 04/17/2008 | DE102006047238A1 Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen Adjusting device for aligning bearing parts of structures subject to tolerance |
| 04/17/2008 | DE102006047237A1 Stelleinrichtung zum Ausrichten von Lagerteilen an toleranzbehafteten Strukturen Adjusting device for aligning bearing parts of structures subject to tolerance |
| 04/17/2008 | DE10017699B9 Verwendung eines transparenten Scheibenpaketes als Verglasung für Sichtfenster in Raumstationen, Flugkörpern sowie Polarstationen in arktischen und antarktischen Breiten Using a transparent disc set as glazing window in space stations, missiles and polar stations in the Arctic and Antarctic latitudes |
| 04/17/2008 | CA2664780A1 Self-supporting interior cabin structure with integrated installation elements |
| 04/17/2008 | CA2663415A1 Aircraft fuselage made from longitudinal panels and method of producing such a fuselage |
| 04/16/2008 | CN101161548A Firewall of aircraft |
| 04/15/2008 | US7358466 Localized heat treating apparatus for blisk airfoils |
| 04/15/2008 | US7357354 Aircraft door hinge assembly |
| 04/15/2008 | US7357353 Method of joining structural elements in an aircraft |
| 04/15/2008 | US7357351 Linear shock wave absorber |
| 04/15/2008 | CA2349122C Aircraft fuselage shell component with crack propagation resistance |
| 04/10/2008 | WO2008041023A1 A door for opening and closing a door aperture in an aircraft |
| 04/10/2008 | WO2008041019A1 Fitting |
| 04/10/2008 | WO2008040868A1 Aircraft comprising a fuselage with a floor extending in the longitudinal plane of the fuselage |
| 04/10/2008 | US20080083850 Method for joining a profiled first structural component to a second structural component |
| 04/10/2008 | US20080083849 Adjustment device for the alignment of supporting parts on structures having inherent dimensional tolerances |
| 04/10/2008 | DE102006046518A1 Coating a substrate comprises depositing an uncured resin film on a release film, depositing a protective layer on the resin film, removing the release film, applying the resin film onto the substrate, and curing the resin film |
| 04/10/2008 | DE102006045596A1 Passenger stairway for integration with the fuselage of an aircraft has one stairway segment that is insertable into the link of another stairway segment so that the stairway segments come to rest lying one on top of another |
| 04/10/2008 | DE10145276B4 Flugzeug, insbesondere Passagierflugzeug, mit einem Rumpf, der eine tragende Primärstruktur und einen Frachtraum umfasst Aircraft, especially passenger aircraft having a fuselage, comprising a supporting primary structure and a cargo hold |
| 04/10/2008 | CA2663873A1 Aircraft comprising a fuselage with a floor extending in the longitudinal plane of the fuselage |
| 04/10/2008 | CA2663611A1 Fitting |
| 04/10/2008 | CA2662719A1 A door for opening and closing a door aperture in an aircraft |
| 04/09/2008 | EP1907278A1 Lateral force joint |
| 04/09/2008 | EP1448374B1 Manufacture and assembly of structures |
| 04/08/2008 | US7356389 Vehicle data services |
| 04/03/2008 | WO2008039168A2 Composite thermoplastic matrix airframe structure and method of manufacture therefor |
| 04/03/2008 | WO2008037847A1 Curved element, wing, control surface and stabilizer for aircraft |
| 04/03/2008 | WO2008000670B1 Pressure bulkhead for an aerospace fuselage |
| 04/03/2008 | US20080078881 System and method for aiding airdrop computations |
| 04/03/2008 | US20080078879 Aircraft wing coupling arrangement |
| 04/03/2008 | US20080078878 Window Frame for Aircraft |