The invention is related to an aircraft with a composite tail boom (3) that comprises at least partly a tubular tail boom cone with an outer skin (8) and an inner skin (9), wherein the inner skin (9) delimits a hollow interior (3c) of the composite tail boom (3), wherein a plurality of rod-shaped stiffening elements (10) and a plurality of ring-shaped stiffening elements (11) are arranged between the outer skin (8) and the inner skin (9), the plurality of rod-shaped stiffening elements (10) being oriented in longitudinal direction of the composite tail boom (3) and the plurality of ring-shaped stiffening elements (11) being distributed along the longitudinal direction in the tubular tail boom cone.


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    Titel :

    A HELICOPTER WITH A FUSELAGE AND A COMPOSITE TAIL BOOM


    Weitere Titelangaben:

    HUBSCHRAUBER MIT EINEM RUMPF UND EINEM VERBUNDSTOFFHECKAUSLEGER
    HÉLICOPTÈRE AVEC UN FUSELAGE ET UNE POUTRE DE QUEUE COMPOSITE


    Beteiligte:
    FINK AXEL (Autor:in)

    Erscheinungsdatum :

    17.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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