CPC B64C 39/024 (2013.01) [B64U 60/30 (2023.01); B64U 50/34 (2023.01); B64U 2101/60 (2023.01)] | 3 Claims |
1. An energy-load assembly configured to attach to an unmanned aerial vehicle, said energy-load assembly comprising:
an accommodating box (1) having four side panels and four corners;
four guide connecting pieces, each respectively connected to one of the four corners of the accommodating box;
wherein an upper portion of each of the four guide connecting pieces is configured to attach to a body of the unmanned aerial vehicle;
a power source (2), the power source (2) being arranged in the accommodating box (1) and capable of providing power to the unmanned aerial vehicle;
a load (3) directly connected to a bottom of the accommodating box (1);
an undercarriage (4) having four tubular struts, the four struts each being directly connected to a lower portion of a respective one of the four guide connecting pieces;
wherein a first of the four struts has a straight body, a neck region, and a foot region, wherein a top of the straight body is directly connected to the neck region that has a bend, wherein the neck region is directly connected to one of said four corners of the accommodating box;
a first horizontal tubular bar located vertically lower than a bottom of the load (3) and is connected to two of the four struts;
a second horizontal tubular bar located vertically lower than the bottom of the load (3) and is connected to another two of the four struts;
wherein the foot region has a bend and is connected to a terminal end of the first horizontal bar;
wherein each of the first and second horizontal bars has a length longer than any of the four side panels of the accommodating box; and
a charging port (111) disposed on one of the four side panels.
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