| CPC B64U 30/29 (2023.01) | 16 Claims |

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1. An unmanned aerial vehicle (UAV) arm, comprising:
a cantilever having a first end and a second end;
a mounting base, connected to the first end of the cantilever, and configured for a power driving unit of an UAV; and
a connecting portion, connected to the second end of the cantilever, and connected to a fuselage of the UAV;
wherein an upper end of a cross section of the cantilever is arc-shaped, a lower end of the cross section of the cantilever is pointed, and the cross section of the cantilever is a section generally perpendicular to a direction from the first end of the cantilever toward the second end of the cantilever; and
the cantilever is obliquely arranged, and the upper end is inclined toward a direction in which the UAV flies forward.
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