A component for a structure of an aircraft interior, wherein at least a portion of the component extends between a first point and a second point, defining a longitudinal axis of the component. The component includes at least one bushing. The at least one bushing is located at the first point and/or the second point. The component further includes a fibrous material that extends between the first point and the second point. The component further includes a thermoplastic that at least partially encases the at least one bushing and the fibrous material.


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    Titel :

    COMPONENT FOR AIRCRAFT INTERIORS


    Beteiligte:
    CHRISTIE DAMIAN (Autor:in) / BALLOCCHI PAOLO (Autor:in)

    Erscheinungsdatum :

    10.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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