A rotary wing aircraft comprising a fuselage tail boom, a tail cone and an interface frame, the interface frame in turn having a connecting structure directly attached to the tail cone by means of a tail cone mechanical connection and a connecting sleeve fitting axially the fuselage tail boom, the connecting sleeve and the fuselage tail boom being directly attached by means of a one boom mechanical connection; the interface frame thereby joining the fuselage tail boom and the tail cone.


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    Titel :

    Rotary wing aircraft with an interface frame joining the fuselage tail boom and the tail cone


    Beteiligte:
    PROBST STEFAN (Autor:in) / WALCH PHILIPP (Autor:in) / NOTHEN MARC (Autor:in) / BUXEL CHRISTIAN (Autor:in) / SCHWEIZER ROMED (Autor:in) / WUERFL THOMAS (Autor:in)

    Erscheinungsdatum :

    20.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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