A method for assembling an aircraft pylon having a primary structure and at least one internal system at least partially positioned within the primary structure, wherein the internal system is positioned inside the primary structure before the last lateral panel of the primary structure is attached. The absence of one of the lateral panels facilitates the installation of the internal systems.


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    Titel :

    Method For Assembling An Aircraft Pylon


    Beteiligte:
    MARTINEL FRANÇOIS (Autor:in) / DEDIEU JOEL (Autor:in) / THERON THIERRY (Autor:in) / MOULIS JULIEN (Autor:in) / DEFORET THOMAS (Autor:in) / BENABEN AUDREY (Autor:in) / WHIFFEN ROBERT (Autor:in)

    Erscheinungsdatum :

    23.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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