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. 09, 2020

Filed:

Aug. 27, 2015
Applicant:

Sikorsky Aircraft Corporation, Stratford, CT (US);

Inventors:

Kevin L. Bredenbeck, Jr., Stuart, FL (US);

Bryan S. Cotton, Poplar Grove, IL (US);

Mark K. Wilson, West Palm Beach, FL (US);

Assignee:

SIKORSKY AIRCRAFT CORPORATION, Stratford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/57 (2006.01); B64C 11/30 (2006.01); B64C 27/82 (2006.01); B64C 11/40 (2006.01); B64C 11/34 (2006.01); B64C 27/56 (2006.01);
U.S. Cl.
CPC ...
B64C 27/57 (2013.01); B64C 11/30 (2013.01); B64C 11/305 (2013.01); B64C 11/34 (2013.01); B64C 11/40 (2013.01); B64C 27/56 (2013.01); B64C 27/82 (2013.01); B64C 2027/8236 (2013.01);
Abstract

A pitch control system configured to vary a pitch angle of at least one of a plurality of propeller blades of a propeller system is provided including a switch movable between a neutral position and a plurality of non-neutral positions. Movement of the switch to a first non-neutral position generates a command to move the propeller blades in a first direction. Movement of the switch to a second non-neutral position generates a command to move the propeller blades in a second direction. Movement of the switch to a third non-neutral position generates a command to move the propeller blades to a zero thrust position.


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