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:
Jun. 01, 2021

Filed:

May. 25, 2017
Applicant:

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

Inventors:

Christopher Gornall, Essex, GB;

David Moro Ludena, Madrid, ES;

Cyriel Notteboom, Cambridge, GB;

Michael Piedmonte, Kirkland, WA (US);

James Thomas, Cambridgeshire, GB;

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/36 (2006.01); F16H 1/46 (2006.01); B64C 11/30 (2006.01); B64C 27/54 (2006.01); B64C 27/18 (2006.01); B64C 27/59 (2006.01); B64C 27/80 (2006.01); B64C 11/06 (2006.01);
U.S. Cl.
CPC ...
B64C 11/36 (2013.01); B64C 11/30 (2013.01); B64C 27/54 (2013.01); F16H 1/46 (2013.01); B64C 11/06 (2013.01); B64C 27/18 (2013.01); B64C 27/59 (2013.01); B64C 27/80 (2013.01);
Abstract

Various mechanisms for adjusting pitches of propeller blades are described. For example, the pitch adjustment mechanism may include a propeller hub enclosing a geared mechanism that cooperates with a compound gearbox having first and second planetary stages to adjust pitches of propeller blades. Alternatively, the pitch adjustment mechanism may include a propeller hub enclosing a pitch adjustment assembly that utilizes tension cables and torsion springs, or rack-and-pinion structures, to adjust pitches of propeller blades. Using any of the various mechanisms, the pitches of propeller blades may be rotated at least 90 degrees, and up to and exceeding 360 degrees, in order to effect thrust reversals and/or adjust thrust profiles.


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