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


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    Titel :

    Advanced pitch stabilizer


    Beteiligte:
    MORES SEBASTIAN (Autor:in) / D ALASCIO ALESSANDRO (Autor:in) / KIESEWETTER UWE (Autor:in) / PROBST STEFAN (Autor:in) / WEHLE CHRISTIAN (Autor:in) / BEBESEL MARIUS (Autor:in)

    Erscheinungsdatum :

    05.07.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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