Systems and methods directed to a rotor blade assembly for an unmanned aerial vehicle (UAV) are provided. A system may include a rotor blade assembly including an axle assembly (414A,B), a first rotor arm (410) supporting a first rotor blade (422) and coupled to rotate about the axle assembly, a second rotor arm (412) supporting a second rotor blade (424) and coupled to rotate about the axle assembly, and a torsion spring (446) coupled to the first rotor arm (410) and the second rotor arm (412), such that a rotation of one of the first rotor arm (410) or the second rotor arm (412) about the axle assembly applies a spring force to the other of the first rotor arm (410) or the second rotor arm (412). Additional systems and related methods are also provided.


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    Title :

    ROTOR BLADE ASSEMBLY FOR UNMANNED AERIAL VEHICLE SYSTEMS AND METHODS


    Contributors:

    Publication date :

    2025-07-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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