Offset drag reduction device

Abstract

In one aspect an uncrewed aerial vehicle (UAV) is provided. The uncrewed aerial vehicle includes a fuselage and a drag reduction device. The fuselage has a front end, a rear end, a top, and a bottom. The drag reduction device includes a proximal end and a distal end. The proximal end of the drag reduction device is coupled to the bottom of the fuselage. The drag reduction device is rotatable between a rest position and an active position in which the drag reduction device extends downward. A standoff is disposed on a rear side of the drag reduction device and is configured to engage a payload secured under the fuselage and hold the drag reduction device at a distance from the payload when the drag reduction device is in the active position.

Dependencies are inferred from the claim text.