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:
Mar. 22, 2022

Filed:

Jul. 16, 2018
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Joseph Ernesto Marone, Montreal, CA;

Olivier Basse, Saint-Bruno, CA;

Martin Dobson, Brossard, CA;

Martin Clermont, Montreal, CA;

Marc Lavoie, Otterburn Park, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 45/02 (2006.01); B64C 11/30 (2006.01); B64C 1/12 (2006.01); H05F 3/00 (2006.01); H02H 9/06 (2006.01); H02H 3/22 (2006.01); H01H 47/00 (2006.01);
U.S. Cl.
CPC ...
B64C 11/301 (2013.01); B64C 1/12 (2013.01); B64C 11/30 (2013.01); B64D 45/02 (2013.01); H01H 47/00 (2013.01); H02H 3/22 (2013.01); H02H 9/06 (2013.01); H05F 3/00 (2013.01);
Abstract

A blade angle feedback ring assembly for an aircraft engine propeller having adjustable angle blades is provided. The feedback ring assembly comprises a feedback ring coupled to rotate with the propeller, the engine configured such that a first electrically-conductive path is defined between the propeller and the engine via the feedback ring, and an electric current conduction element provided between the propeller and the engine to define a second electrically-conductive path between the propeller and the engine in parallel to the first path, the second electrically-conductive path configured with a lower electrical resistance to conduction between the propeller and the engine than the first electrically-conductive path.


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