A method (M) for joining two fuselage sections (FS1, FS2) of aircraft or spacecraft involves fastening (M1) a crossbeam (CB) to an elliptical interface frame (IF) to form an intermediate coupling assembly; temporarily fastening (M2) the intermediate coupling assembly to a planar mounting frame (MF) at a number of fixation holes (H) formed in the planar mounting frame (MF); temporarily fastening (M3) a buttstrap (BS) circumferentially around the interface frame (IF); permanently attaching (M4) the intermediate coupling assembly and the buttstrap (BS) to a first fuselage section (FS1); disengaging (M5) the intermediate coupling assembly from the mounting frame (MF); and permanently attaching (M6) a second fuselage section (FS2) to the first fuselage section (FS1) at the buttstrap (BS); a mounting device comprising a planar mounting frame (MF) and at least one mounting beam (MB; MB') extending substantially perpendicularly to the plane of extension of the mounting frame (MF) is also disclosed.


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    Titel :

    Method for joining two fuselage sections


    Weitere Titelangaben:

    Verfahren zum Verbinden zweier Rumpfabschnitte
    Procédé pour relier deux sections de fuselage


    Beteiligte:
    EILKEN WOLFGANG (Autor:in) / SAUER MICHAEL (Autor:in) / TIRYAKI MEMIS (Autor:in)

    Erscheinungsdatum :

    2016-07-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B21J FORGING , Schmieden / 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



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