CPC B60F 5/02 (2013.01) [B64C 37/00 (2013.01); B64C 39/024 (2013.01); B64D 1/12 (2013.01); B64D 27/24 (2013.01); B60B 19/00 (2013.01); B64U 10/13 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 2201/10 (2023.01); G05D 1/101 (2013.01)] | 20 Claims |
1. An unmanned aerial vehicle (UAV) comprising:
(a) a body with at least two extending arms;
(b) a land/air drive assembly attached to each arm, each drive assembly including:
(i) a multi-speed motor assembly;
(ii) a propeller driven by the motor assembly at a first speed, the propeller having a first diameter;
(iii) a ground drive wheel driven by the motor assembly at a second speed slower than the first speed, the ground drive wheel having a second diameter greater than the first diameter; and
(c) a drive assembly orientation servo positioned between each arm and each drive assembly, wherein the orientation servo is configured to, on command, rotate the drive assembly between a flight position and a ground drive position approximately perpendicular to the flight position.
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