An aircraft tail including: a leading edge, a trailing edge, a tip and a root, and a single protrusion protruding from the leading edge, wherein the single protrusion protrudes from the leading edge only in a direction opposite to the trailing edge and is closer to the tip than to the root, and includes a first lateral side and a second lateral side that originate from different points of the leading edge along the tail span, wherein the first lateral side is closer to the tip than to the second lateral side, and the protrusion is entirely in a section of the leading edge between 50% and 95% of the tail span from the root.


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    Titel :

    AIRCRAFT TAIL SURFACE


    Beteiligte:

    Erscheinungsdatum :

    22.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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