Systems and methods are provided for assembling aircraft fuselages. One embodiment is a method for assembling a fuselage of an aircraft. The method includes indexing an arcuate section (120) of the fuselage to a frame installation station (140), feeding a frame (142) at the frame installation station into a concavity (126) defined by the arcuate section, placing the frame against an Inner Mold Line (IML) (128) of the arcuate section while the frame is within the concavity, and affixing the frame to the arcuate section.
FRAME INSTALLATION STATION FOR AIRCRAFT FUSELAGE SEGMENTS
RAHMENMONTAGESTATION FÜR FLUGZEUGRUMPFSEGMENTE
STATION D'INSTALLATION DE CADRE POUR SEGMENTS DE FUSELAGE D'AÉRONEF
2022-05-25
Patent
Elektronische Ressource
Englisch
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B21J FORGING , Schmieden / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B65G TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS , Transport- oder Lagervorrichtungen, z.B. Förderer zum Laden oder Abladen / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL |
FRAME INSTALLATION STATION FOR AIRCRAFT FUSELAGE SEGMENTS
Europäisches Patentamt | 2022
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