A pitch stabilizer (10) with box configuration suitable for providing stability to a rotorcraft comprising a vertical mid-plane (15) and a fuselage (14); the pitch stabilizer (10) comprising one or two pitch stabilizing assemblies, with no more than one pitch stabilizing assembly on each side of the vertical mid-plane (15), wherein each pitch stabilizing assembly comprises upper pitch stabilizing means (11), lower pitch stabilizing means (12) and a wing tip element (13).


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    Title :

    Advanced pitch stabilizer


    Additional title:

    Erweiterter Steigungsstabilisator
    Stabilisateur de pas avancé


    Contributors:

    Publication date :

    2017-05-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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