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. 28, 2022

Filed:

Jan. 09, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Sean Durand, Brossard, CA;

Richard Kudrna, Carignan, CA;

Ian Farrell, Greenfield Park, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 11/30 (2006.01); G01B 7/30 (2006.01); B64D 31/00 (2006.01); F01D 5/02 (2006.01); G01B 7/00 (2006.01); G01D 5/14 (2006.01);
U.S. Cl.
CPC ...
G01B 7/30 (2013.01); B64D 31/00 (2013.01); F01D 5/02 (2013.01); G01B 7/003 (2013.01); G01D 5/145 (2013.01); F05D 2240/30 (2013.01); F05D 2270/80 (2013.01);
Abstract

A blade angle feedback assembly for an aircraft-bladed rotor is provided. The rotor is rotatable about a longitudinal axis and having an adjustable blade pitch angle. The assembly comprises a feedback device coupled to rotate with the rotor with adjustment of the blade pitch angle, the feedback device comprising a non-magnetically permeable body defining a root surface and a plurality of magnetically permeable position markers circumferentially disposed on the root surface, and at least one sensor mounted adjacent the feedback device and configured to detect a passage of the plurality of position markers as the feedback device rotates about the longitudinal axis.


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