CPC B64C 29/0025 (2013.01) [B64C 1/22 (2013.01); B64C 29/0033 (2013.01); B64C 39/024 (2013.01); B64U 10/25 (2023.01); B64U 30/10 (2023.01)] | 13 Claims |
1. A fixed-wing unmanned aerial vehicle (UAV) comprising:
a left hind wing and a right hind wing;
a left forewing coupled to a right forewing;
a cabin coupled to the left hind wing and the right hind wing;
a left linear support coupled to at least one of said left hind wing and said left forewing;
a right linear support coupled to at least one of said right hind wing and said right forewing;
the left linear support has a first, a second, a third lifting propellers disposed thereon;
the right linear support has a fourth, a fifth, a sixth lifting propellers disposed thereon;
a left traction propeller disposed at a front end of the left linear support;
a right traction propeller disposed at a front end of the right linear support;
wherein the left linear support is parallel to the right linear support, and there are no other linear supports disposed parallel to said left and right linear supports; and
wherein when the UAV is in an upright position on a ground, the left and right linear supports are disposed from the ground at a distance longer than a distance of a top of said cabin to said ground.
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