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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    Title :

    A HELICOPTER WITH A FUSELAGE AND A COMPOSITE TAIL BOOM


    Additional title:

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


    Contributors:
    FINK AXEL (author)

    Publication date :

    2019-04-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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