Feedback system for pitch-adjustable blades of aircraft bladed rotor

Patent metadata

Field	Value
Publication number	US-10889367-B2
Application number	US-201715495070-A
Country	US
Kind code	B2
Filing date	Apr 24, 2017
Priority date	Apr 24, 2017
Publication date	Jan 12, 2021
Grant date	Jan 12, 2021

Abstract

Systems and methods for providing pitch position feedback for pitch-adjustable blades of an aircraft bladed rotor are disclosed. In one embodiment, the systems include a sensor comprising a magnet having a magnetic field, a pole piece coupled to a first pole of the magnet and directing the magnetic field toward the feature and a coil mounted in the magnetic field. The coil generates a sensor signal indicative of a variation in the magnetic field caused by movement of the feature in the magnetic field. The sensor also includes a magnetic shield mounted in the magnetic field. The magnetic shield defines a magnetic return path for some magnetic flux of the magnetic field exiting the pole piece toward an opposite second pole of the magnet.

First claim

What is claimed is:

1. An engine having a feedback system for pitch-adjustable blades of an aircraft bladed rotor, the system comprising:
a feedback rotor configured to rotate with the aircraft bladed rotor about a rotation axis, the feedback rotor being axially displaceable along the rotation axis to a plurality of axial positions, the axial position of the feedback rotor corresponding to a respective pitch position of the pitch-adjustable blades, the feedback rotor comprising elongated features spaced circumferentially around the feedback rotor, each elongated feature having an axial edge where the elongated feature terminates along the rotation axis;
a sensor including:
a sensor housing;
a stationary magnet mounted in the engine adjacent the rotating feedback rotor, the magnet having a magnetic field;
a pole piece coupled to a first pole of the magnet and configured to direct the magnetic field toward the elongated features along a sensor axis, part of the pole piece being disposed in the sensor housing;
a coil mounted in the magnetic field and being stationary relative to the magnet, the coil being configured to generate a sensor signal indicative of a variation in the magnetic field caused by movement of one or more of the elongated features in the magnetic field as the feedback rotor rotates relative to the magnet; and
a magnetic shield disposed inside or outside of the sensor housing, the magnetic shield mounted in the magnetic field and being stationary relative to the magnet, the magnetic shield defining a magnetic return path for some magnetic flux of the magnetic field exiting the pole piece toward an opposite second pole of the magnet, the magnetic shield having a side wall and a bottom wall cooperatively defining part of a receptacle receiving the part of the pole piece, the bottom wall defining an aperture for permitting passage of the magnetic field through the magnetic shield via the aperture; and

a detection unit operatively connected to the coil and configured to generate a feedback signal indicative of the respective pitch position of the pitch-adjustable blades in response to the sensor signal received from the coil;
wherein:
the feedback rotor is axially displaceable between a first position and a second position relative to the sensor;
the first position corresponds to the sensor being axially distal of a first axial edge of a first of the elongated features; and
the second position corresponds to the sensor axially overlapping the first axial edge of the first elongated feature where the first elongated feature provides an asymmetric magnetic permeability for the magnetic field about the sensor axis.

2. The engine as defined in claim 1 , wherein the pole piece is disposed between the magnet and the feedback rotor.

3. The engine as defined in claim 1 , wherein the pole piece extends into the aperture in the magnetic shield.

4. The engine as defined in claim 1 , wherein at least part of the magnetic shield is disposed inside the sensor housing, the sensor housing containing the magnet and the coil.

5. The engine as defined in claim 1 , wherein at least part of the magnetic shield is disposed outside the sensor housing, the sensor housing containing the magnet and the coil.

6. The engine as defined in claim 3 , wherein the pole piece is disposed between the magnet and the feedback rotor.

7. The engine as defined in claim 1 , wherein the receptacle receives part of the coil.

8. The engine as defined in claim 1 , wherein:
the coil is a first coil and the sensor signal is a first sensor signal indicative of the variation in the magnetic field on a first channel;
the system comprises a second coil configured to generate a second sensor signal indicative of the variation in the magnetic field on a second channel;
the first and second coils are disposed at different axial locations along the sensor axis.

9. The engine as defined in claim 1 , wherein the bottom wall of the magnetic shield is disposed between the coil and the feedback rotor.

10. The engine as defined in claim 1 , wherein the magnetic shield has a relative permeability value that is between 20,000 and 100,000.

11. A method for providing pitch position feedback for pitch-adjustable blades of an aircraft bladed rotor, the method comprising:
rotating a feedback rotor with the aircraft bladed rotor about a rotation axis;
axially displacing the feedback rotor along the rotation axis based on a pitch of the pitch-adjustable blades between a first position and a second position relative to a sensor having a sensor axis, the first position corresponding to the sensor being axially distal of a first axial edge of a first of a plurality of moving elongated features of the feedback rotor, the second position corresponding to the sensor axially overlapping the first axial edge of the first elongated feature where the first elongated feature provides an asymmetric magnetic permeability for a magnetic field generated by the sensor along the sensor axis;
directing the magnetic field from a first pole of a magnet of the sensor toward a location that the moving elongated features, which are indicative of the pitch of the pitch-adjustable blades, are expected to occupy as the moving elongated features move relative to the magnet, the magnetic field including first magnetic flux intersecting the location that the moving elongated features are expected to occupy and second magnetic flux not intersecting the location that the moving elongated features are expected to occupy;
guiding the second magnetic flux toward an opposite second pole of the magnet along one or more magnetic return paths defined by a magnetic shield having a side wall and a bottom wall cooperatively defining part of a receptacle receiving part of a pole piece disposed in a sensor housing and coupled to the first pole of the magnet, the bottom wall defining an aperture for permitting passage of the magnetic field through the magnetic shield via the aperture, the magnetic shield disposed inside or outside of the sensor housing;
detecting a variation in the magnetic field caused by movement of one or more of the moving elongated features in the magnetic field; and
generating a signal indicative of the pitch of the pitch-adjustable blades based on the detection of the variation in the magnetic field.

Assignees

• Pratt & Whitney Canada

Inventors

• Kudrna Richard
• Farrell Ian

Classifications

• G01D2205/40

  Position sensors comprising arrangements for concentrating or redirecting magnetic flux · CPC title

• G01D5/147

  influenced by the movement of a third element, the position of Hall device and the source of magnetic field being fixed in respect to each other · CPC title

• G01P3/488

  delivered by variable reluctance detectors · CPC title

• G01D5/20

  by varying inductance, e.g. by a movable armature · CPC title

• B64C11/30

  Blade pitch-changing mechanisms · CPC title