The objective of the present invention is to provide an aircraft panel production method and aircraft panel production system with which an aircraft panel can be assembled accurately. This aircraft panel production method has: a step in which a holding jig (1) holds a body panel (10), which has a plurality of plate-like members having a curved cross-sectional shape, such that the cross section of the body panel (10) has an upwardly bulging curved shape; a step in which the plate-like members of the body panel (10) held by the holding jig (1) are overlapped with each other and the overlapping portions are joined by a rivet; a step in which the holding jig (1), which is holding the body panel (10) of which the plate-like members have been joined to each other, is moved; and a step in which a frame (32) that follows the curved shape of the body panel (10) is joined, by a rivet, to the plate-like members of the body panel (10) which is held by the holding jig (1) which has been moved.


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    Titel :

    AIRCRAFT PANEL PRODUCTION METHOD


    Weitere Titelangaben:

    VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGPANELS
    PROCÉDÉ DE FABRICATION DE PANNEAU D'AÉRONEF


    Beteiligte:
    HIRAI MAKOTO (Autor:in) / TANEDA HIROSHI (Autor:in) / GOTO TAKUYA (Autor:in) / KANEKO TSUYOSHI (Autor:in)

    Erscheinungsdatum :

    2021-03-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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 / B21J FORGING , Schmieden / B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B64C AEROPLANES , Flugzeuge



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