The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 01, 2026

Filed:

Dec. 16, 2025
Applicant:

Wing Aviation Llc, Palo Alto, CA (US);

Inventors:

Aaron Bryce Christian, Redwood City, CA (US);

André Peter Prager, Margraten, NL;

Elizabeth Chase Marshman, Brooklyn, NY (US);

Christina Lee Ngo, San Jose, CA (US);

Assignee:

Wing Aviation LLC, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64U 101/64 (2023.01); B64C 7/00 (2006.01); B64C 21/08 (2023.01); B64U 30/40 (2023.01);
U.S. Cl.
CPC ...
B64U 30/40 (2023.01); B64C 21/08 (2013.01); B64C 7/00 (2013.01); B64U 2101/64 (2023.01);
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.


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