An aircraft with a fuselage that comprises at least one hollow beam element, wherein the at least one hollow beam element accommodates at least one hollow duct element that comprises a tubular duct element wall, and wherein at least one protective spacer is arranged between the tubular duct element wall and the at least one hollow beam element such that free space is available between the tubular duct element wall and the at least one hollow beam element.


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    Titel :

    AIRCRAFT WITH A FUSELAGE THAT COMPRISES AT LEAST ONE HOLLOW BEAM ELEMENT


    Beteiligte:
    VINKE CHRIS (Autor:in) / SCHEJBAL PETR (Autor:in) / HAASE DANIEL (Autor:in)

    Erscheinungsdatum :

    2018-09-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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