The present invention refers to a tail cone of an aircraft, more specifically to a tail cone made of composite materials comprising: - an internal skin (3), - an external skin (4) which surrounds the internal skin (3), - longitudinal structural members (1) located on the inner face of the internal skin (3) in the longitudinal direction of the tail cone, and - transversal structural members (2) located between the external skin (4) and the internal skin (3) in the transverse direction of the tail cone.


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    Title :

    Tail cone of an aircraft


    Additional title:

    Heckkonus eines Flugzeugs
    Cône de queue d'un aéronef


    Contributors:

    Publication date :

    2017-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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