Aircraft with a fuselage, wings, horizontal stabilizers and a vertical stabilizer, wherein on the front portion of the vertical stabilizer an elongated one-piece nose element (20) is mounted which forms lateral air guide surfaces, and to the front end of the nose element (20) a perforated metal plate nose member (25) is attached, and wherein the front end of the nose element (20) is closed and between this closed front end and the nose member (25) an elongated air channel (9) is formed.


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    Titel :

    Leading edge nose structure on the vertical stabilizer of an aircraft


    Weitere Titelangaben:

    Anströmkantennasenstruktur am Seitenleitwerk eines Flugzeugs
    Structure de bec de bord d'attaque sur le stabilisateur vertical d'un aéronef


    Beteiligte:
    GERBER MARTIN (Autor:in)

    Erscheinungsdatum :

    2018-02-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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