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. 07, 2023

Filed:

Nov. 26, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Dana Tomescu, Brampton, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
G01D 5/20 (2006.01); G01D 5/247 (2006.01); G01B 7/14 (2006.01); G01B 7/30 (2006.01); B64C 13/16 (2006.01); B64C 11/30 (2006.01); G01D 5/245 (2006.01);
U.S. Cl.
CPC ...
B64C 13/16 (2013.01); B64C 11/30 (2013.01); B64C 11/301 (2013.01); G01D 5/2013 (2013.01); G01D 5/2451 (2013.01);
Abstract

A blade angle feedback system for an aircraft-bladed rotor rotatable about a longitudinal axis and having an adjustable blade pitch angle is provided. A feedback device is coupled to rotate with the rotor and to move along the axis with adjustment of the blade angle. At least one position marker is affixed to a core of the feedback device and extends along a direction angled relative to the axis. The core is made of a first material having a first magnetic permeability and the position marker comprises a second material having a second magnetic permeability greater than the first magnetic permeability. A sensor is positioned adjacent the feedback device and produces, as the feedback device rotates about the axis, a sensor signal in response to detecting passage of the position marker. A control unit generates a feedback signal indicative of the blade angle in response to the sensor signal.


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