The present embodiments relate to a cyclic pitch angle adjustment apparatus 200 for a rotor 110 or propeller, to a rotor 110 with such a cyclic pitch angle adjustment apparatus 200, and to a rotorcraft with such a rotor 110. The cyclic pitch angle adjustment apparatus 200 may include levers that rotate rotor blades around associated pitch axes, rods 240 that mechanically link the levers with a bearing 220 such that the rods 240 are movable relative to a central point 223, the bearing 220 being attached to a central rod 250 that is movable by means of a motor 510 and adapted for adjusting the cyclic pitch angle of the rotor blades from one pitch angle in one position to another pitch angle in another position.


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    Title :

    A CYCLIC PITCH ANGLE ADJUSTMENT APPARATUS


    Additional title:

    VORRICHTUNG ZUR ZYKLISCHEN NEIGUNGSWINKELEINSTELLUNG
    APPAREIL DE RÉGLAGE D'ANGLE DE PAS CYCLIQUE


    Contributors:

    Publication date :

    2023-11-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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