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:
Apr. 14, 2020

Filed:

Aug. 09, 2016
Applicant:

Gopro, Inc., San Mateo, CA (US);

Inventors:

Scott Patrick Campbell, Belmont, CA (US);

Leo Baldwin, Seattle, WA (US);

Gary Fong, Cupertino, CA (US);

Assignee:

GoPro, Inc., San Mateo, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/34 (2006.01); B64C 11/20 (2006.01); B64C 11/26 (2006.01); B64C 39/02 (2006.01);
U.S. Cl.
CPC ...
B64C 11/20 (2013.01); B64C 11/26 (2013.01); B64C 11/34 (2013.01); B64C 39/024 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01);
Abstract

A variable pitch propeller is designed to adjust the pitch of the propeller blade during flight to maximize the propeller efficiency. The propeller blade may comprise airfoil cross-sections. Each cross-section may be composed of different materials at the leading edge and trailing edge. In various embodiments, these materials are selected and oriented to achieve the necessary elastic moduli of the leading and trailing edge for the airfoil cross-section. During liftoff, the airfoil at the blade tip possesses a high blade pitch (e.g. 20 degrees), thereby increasing the generated lift on the propeller blades. During flight or hover conditions when maximal lift is no longer required, the trailing edge of the airfoil displaces upward and reduces the blade pitch to minimize the drag forces on the blade tip.


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