Rotor mount assembly
    1.
    发明授权

    公开(公告)号:US12162593B2

    公开(公告)日:2024-12-10

    申请号:US17035380

    申请日:2020-09-28

    Abstract: An unmanned aerial vehicle (UAV) including a fuselage frame and a propulsion system coupled to the fuselage frame. The propulsion system includes a first propulsion device and a second propulsion device. The first propulsion device includes a first rotor blade assembly and a first rotor mount assembly, and the second propulsion device includes a second rotor blade assembly and a second rotor mount assembly. The first rotor mount assembly is configured to not allow the second rotor blade assembly to be assembled to the first rotor mount assembly.

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