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.
ROTOR BLADE ASSEMBLY FOR UNMANNED AERIAL VEHICLE SYSTEMS AND METHODS
2025-07-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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