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:
May. 27, 2025

Filed:

Oct. 10, 2023
Applicant:

Swift Engineering, Inc., San Clemente, CA (US);

Inventor:

Christopher Noskowicz, San Clemente, CA (US);

Assignee:

SWIFT ENGINEERING, INC., San Clemente, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 9/00 (2006.01); B64U 10/25 (2023.01); B64U 20/50 (2023.01); B64U 30/10 (2023.01); B64U 70/50 (2023.01); B64U 80/70 (2023.01); B64U 50/13 (2023.01); B64U 101/31 (2023.01);
U.S. Cl.
CPC ...
B64C 9/00 (2013.01); B64U 10/25 (2023.01); B64U 20/50 (2023.01); B64U 70/50 (2023.01); B64C 2009/005 (2013.01); B64U 30/10 (2023.01); B64U 50/13 (2023.01); B64U 80/70 (2023.01); B64U 2101/31 (2023.01);
Abstract

A method of deploying an unmanned aerial vehicle (UAV) includes launching a UAV and deploying at least one portion of a wing assembly from a stowed configuration to a deployed configuration in which the at least one portion of the wing assembly extends away from a body of the UAV. Deploying the portion of the wing assembly, which may be an outboard portion of a wing assembly, includes deflecting an aerodynamic control surface on the at least one portion of the wing assembly to cause an aerodynamic force to move the portion of the wing assembly into the deployed configuration without assistance from a spring or motor. An unmanned aerial vehicle (UAV) includes a UAV having a body and a plurality of wing assemblies carried by the body, at least a portion of a wing assembly is deployable using aerodynamic forces and without assistance form a spring or motor.


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