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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    Title :

    Leading edge nose structure on the vertical stabilizer of an aircraft


    Additional title:

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


    Contributors:

    Publication date :

    2018-02-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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