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:
Dec. 17, 2024

Filed:

Jul. 07, 2023
Applicant:

Saildrone, Inc.;

Inventors:

Richard Elliott Jenkins, Alameda, CA (US);

Dylan Owens, Oakland, CA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B63H 9/061 (2020.01); B63B 1/10 (2006.01); B63B 1/12 (2006.01); B63B 43/00 (2006.01); B63B 43/02 (2006.01); B63B 71/20 (2020.01); B63G 8/00 (2006.01); B63G 8/22 (2006.01); B63G 8/28 (2006.01); B63G 8/38 (2006.01); B63H 9/08 (2006.01); B63H 25/04 (2006.01); B63H 25/38 (2006.01); G05D 1/00 (2006.01); G05D 1/02 (2020.01); G05D 1/08 (2006.01); H02S 40/38 (2014.01); B63B 35/00 (2020.01);
U.S. Cl.
CPC ...
B63H 9/061 (2020.02); B63B 1/10 (2013.01); B63B 1/12 (2013.01); B63B 1/125 (2013.01); B63B 43/00 (2013.01); B63B 43/02 (2013.01); B63B 71/20 (2020.01); B63G 8/001 (2013.01); B63G 8/22 (2013.01); B63G 8/28 (2013.01); B63G 8/38 (2013.01); B63H 9/08 (2013.01); B63H 25/04 (2013.01); B63H 25/38 (2013.01); G05D 1/0206 (2013.01); G05D 1/0875 (2013.01); H02S 40/38 (2014.12); B63B 2035/007 (2013.01); B63G 2008/004 (2013.01); B63H 9/0635 (2020.02); B63H 2009/082 (2013.01); B63H 2025/045 (2013.01);
Abstract

An unmanned sailing vehicle comprising: a primary hull; a rigid wing rotationally coupled with said primary hull that freely rotates about a rotational axis of said rigid wing; a boom comprising a first end extending from a leading edge of said rigid wing and a second end extending from a trailing edge of said rigid wing, said first end of said boom comprising a counterweight configured to dynamically balance a wing system comprising said rigid wing, said boom, and said tail with respect to said rotational axis of said rigid wing; a tail coupled to said second end of said boom; a control surface element disposed on said tail and configured to aerodynamically control a wing angle of said rigid wing based on a position of said control surface element; and a controller configured to determine a control surface angle and generate a signal to position said control surface element.


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