A rotor (8a) comprises at least two rotor blades (10), and each rotor blade (10) of the at least two rotor blades (10) rotates around a rotor axis (Y) and performs pitching around a pitch axis (X). The rotor axis (Y) and the pitch axis (X) intersect in a rotor center (P0). The rotor (8a) is characterized in that each rotor blade (10) comprises at least one permanent magnet (25) having a first spherical magnet surface (19). Each rotor blade (10) further comprises a pitch control apparatus (20) for controlling the pitching of the at least two rotor blades (10). The pitch control apparatus (20) comprises electrically controlled magnets (24) having a second spherical magnet surface (15).


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    Title :

    A ROTOR WITH PITCH CONTROL APPARATUS


    Additional title:

    ROTOR MIT BLATTVERSTELLUNGSVORRICHTUNG
    ROTOR À APPAREIL DE COMMANDE DE PAS


    Contributors:
    RIES TOBIAS (author)

    Publication date :

    2022-12-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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