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:
Nov. 17, 2020

Filed:

Jun. 08, 2018
Applicant:

Sanmina Corporation, San Jose, CA (US);

Inventors:

Max Edward Klein, Huntsville, AL (US);

Walter Thomas Castleberry, Hampton Cove, AL (US);

Nathan Trey McFerrin, Huntsville, AL (US);

Assignee:

Sanmina Corporation, San Jose, CA (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/34 (2006.01); B64C 27/52 (2006.01); B64C 11/30 (2006.01); B64C 39/02 (2006.01); B64C 27/80 (2006.01); B64C 27/08 (2006.01); B64C 27/605 (2006.01);
U.S. Cl.
CPC ...
B64C 11/34 (2013.01); B64C 11/305 (2013.01); B64C 27/08 (2013.01); B64C 27/52 (2013.01); B64C 27/605 (2013.01); B64C 27/80 (2013.01); B64C 39/024 (2013.01); B64C 2201/027 (2013.01); B64C 2201/108 (2013.01); B64C 2203/00 (2013.01);
Abstract

Aircraft are configured to facilitate propeller blade pitch adjustability. According to one example, an aircraft can include a plurality of propellers, where each propeller includes plurality of blades. At least one pitch adjust mechanism may be associated with at least on propeller, where the pitch adjust mechanism is configured to adjust a pitch of the plurality of blades for at least one propeller in response to airflow from at least one other propeller influencing an airflow at the at least one propeller. Other aspects, embodiments, and features are also included.


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