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:
Jan. 30, 2018

Filed:

Dec. 11, 2015
Applicant:

Amazon Technologies, Inc., Seattle, WA (US);

Inventors:

Jack Erdozain, Jr., Miami, FL (US);

Louis LeRoi LeGrand, III, Seattle, WA (US);

Joshua White Traube, Seattle, WA (US);

Assignee:

Amazon Technologies, Inc., Seattle, WA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/00 (2006.01); B64C 27/58 (2006.01); B64C 27/12 (2006.01); B64C 39/02 (2006.01); H02K 7/114 (2006.01); H02K 49/10 (2006.01);
U.S. Cl.
CPC ...
B64C 27/58 (2013.01); B64C 27/12 (2013.01); B64C 39/024 (2013.01); H02K 7/114 (2013.01); H02K 49/10 (2013.01); B64C 2201/024 (2013.01); B64C 2201/042 (2013.01); B64C 2201/108 (2013.01);
Abstract

A propeller alignment device is described. The propeller alignment device can include a second retainer attached to a propeller and a motor. The propeller alignment device can also include a first retainer that does not rotate, but that is aligned with the second retainer. The first retainer can include two or more magnets oppositely orientated relative to each other. The second retainer can also include two or more magnets oppositely orientated relative to each other. As the second retainer rotates relative to the first retainer, the magnets may alternatingly align with each other. In the absence of a current applied to the motor, the magnets may magnetically bias the second retainer into a predetermined orientation relative to the first retainer. The predetermined orientation can be predetermined to correspond to an alignment of the propeller that is desirable (e.g., that minimizes aerodynamic drag on the propeller).


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