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:
Jul. 22, 2025

Filed:

Jan. 29, 2024
Applicant:

Anduril Industries, Inc., Costa Mesa, CA (US);

Inventors:

Nicholas Robert Alley, Marietta, GA (US);

Joshua Lemming Steele, Marietta, GA (US);

Jesse Owen Williams, Marietta, GA (US);

Daniel Kuehme, Marietta, GA (US);

Jonathan Caleb Phillips, Marietta, GA (US);

Assignee:

Anduril Industries, Inc., Costa Mesa, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/40 (2006.01); B64C 1/36 (2006.01); B64C 3/54 (2006.01); B64C 5/02 (2006.01); B64C 5/12 (2006.01); B64C 5/16 (2006.01); B64C 11/28 (2006.01); B64C 13/24 (2006.01); B64C 13/30 (2006.01); B64U 30/12 (2023.01); B64U 50/13 (2023.01); B64U 20/60 (2023.01); B64U 50/19 (2023.01); B64U 101/31 (2023.01);
U.S. Cl.
CPC ...
B64C 3/40 (2013.01); B64C 1/36 (2013.01); B64C 3/54 (2013.01); B64C 3/546 (2013.01); B64C 5/02 (2013.01); B64C 5/12 (2013.01); B64C 5/16 (2013.01); B64C 11/28 (2013.01); B64C 13/24 (2013.01); B64C 13/30 (2013.01); B64U 30/12 (2023.01); B64U 50/13 (2023.01); B64C 2211/00 (2013.01); B64U 20/60 (2023.01); B64U 50/19 (2023.01); B64U 2101/31 (2023.01); B64U 2201/20 (2023.01); Y02T 50/10 (2013.01); Y02T 50/40 (2013.01);
Abstract

An unmanned aerial vehicle (UAV) having wings stowed against a fuselage of the UAV in a first arrangement is disclosed. Methods and systems for deploying the wings into a second arrangement are disclosed. For example, after a launch of the UAV, the UAV monitors for at least one precondition. The at least one pre-condition being a pre-condition associated with deploying wings of the UAV into the second arrangement. Upon detecting the at least one precondition, the wings of the UAV are deployed into a second arrangement. Deploying the wings comprises activating, in response to detecting the at least one precondition associated with the UAV, a gearbox configured to transition the wings from the first arrangement to the second arrangement. Roll control may be maintained throughout launch and deployment.


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