Blade angle position feedback system with extended markers

Patent metadata

Field	Value
Publication number	US-10829201-B2
Application number	US-201916359276-A
Country	US
Kind code	B2
Filing date	Mar 20, 2019
Priority date	Mar 20, 2019
Publication date	Nov 10, 2020
Grant date	Nov 10, 2020

Abstract

A blade angle feedback assembly for an aircraft-bladed rotor and an aircraft-bladed rotor system are provided. The rotor is rotatable about a longitudinal axis and has an adjustable blade pitch angle. A feedback device is coupled to rotate with the rotor, the feedback device having a root surface having an edge. At least one position marker extends from the root surface and extends laterally beyond the edge. At least one sensor is mounted adjacent the feedback device and configured to detect a passage of the at least one position marker as the feedback device rotates about the longitudinal axis.

First claim

The invention claimed is:

1. A blade angle feedback assembly comprising:
an aircraft-bladed rotor, the rotor rotatable about a longitudinal axis and having an adjustable blade pitch angle, the blade angle feedback assembly further comprising:
a feedback device coupled to rotate with the rotor, the feedback device having a root surface having an edge;
at least one position marker extending from the root surface and extending laterally beyond the edge; and
at least one sensor mounted adjacent the feedback device and configured to detect a passage of the at least one position marker as the feedback device rotates about the longitudinal axis.

2. The feedback assembly of claim 1 , wherein the root surface has a first edge and a second edge opposite the first edge, and the at least one position marker extends axially from a first end to a second end, at least one of the first end and the second end extending laterally beyond a corresponding at least one of the first edge and the second edge.

3. The feedback assembly of claim 2 , wherein the at least one sensor is configured to detect, as the feedback device rotates about the longitudinal axis, a change in magnetic flux caused by passage of the at least one position marker in a sensing zone of the at least one sensor, the at least one of the first end and the second end extending laterally beyond the at least one of the first edge and the second edge resulting in an increase in a density of the magnetic flux as the feedback device is displaced along the longitudinal axis.

4. The feedback assembly of claim 3 , wherein the at least one sensor is mounted adjacent the feedback device between the first edge and the second edge, the first end of the at least one position marker extending laterally beyond the first edge and the second end of the at least one position marker extending laterally beyond the second edge.

5. The feedback assembly of claim 3 , wherein the at least one sensor is mounted adjacent a given one of the first edge and the second edge, the at least one position marker extending laterally beyond the other one of the first edge and the second edge.

6. The feedback assembly of claim 2 , wherein the feedback device comprises at least one support member configured to extend away from the at least one of the first edge and the second edge and to support the at least one of the first end and the second end thereon.

7. The feedback assembly of claim 2 , wherein the at least one of the first end and the second end is substantially parallel to the corresponding at least one of the first edge and the second edge.

8. The feedback assembly of claim 1 , wherein the at least one position marker comprises a first plurality of projections extending from the root surface and oriented substantially parallel to the longitudinal axis and at least one second projection extending from the root surface and positioned between two adjacent first projections, the first plurality of projections circumferentially spaced from one another and the at least one second projection disposed on the root surface at an oblique angle relative to the first plurality of projections, and further wherein the first plurality of projections and the at least one second projection extend laterally beyond the at least one of the first edge and the second edge.

9. An aircraft-bladed rotor system, comprising:
a rotor rotatable by a shaft about a longitudinal axis, the rotor having blades with adjustable blade pitch angle; and
a feedback device coupled to rotate with the rotor, the feedback device having a root surface having an edge, at least one position marker extending from the root surface and extending laterally beyond the edge.

10. The system of claim 9 , wherein the root surface has a first edge and a second edge opposite the first edge, and the at least one position marker extends axially along the root surface from a first end to a second end, at least one of the first end and the second end extending laterally beyond a corresponding at least one of the first edge and the second edge.

11. The system of claim 10 , further comprising at least one sensor mounted adjacent the feedback device, the at least one sensor configured to detect, as the feedback device rotates about the longitudinal axis, a change in magnetic flux caused by passage of the at least one position marker in a sensing zone of the at least one sensor, the at least one of the first end and the second end extending laterally beyond the at least one of the first edge and the second edge resulting in an increase in a density of the magnetic flux as the feedback device is displaced along the longitudinal axis.

12. The system of claim 11 , wherein the at least one sensor is mounted adjacent the feedback device between the first edge and the second edge, the first end of the at least one position marker extending laterally beyond the first edge and the second end of the at least one position marker extending laterally beyond the second edge.

13. The system of claim 11 , wherein the at least one sensor is mounted adjacent a given one of the first edge and the second edge, the at least one position marker extending laterally beyond the other one of the first edge and the second edge.

14. The system of claim 10 , wherein the feedback device comprises at least one support member configured to extend away from the at least one of the first edge and the second edge and to support the at least one of the first end and the second end thereon.

15. The system of claim 10 , wherein the at least one of the first end and the second end is substantially parallel to the corresponding at least one of the first edge and the second edge.

16. The system of claim 9 , wherein the at least one position marker comprises a first plurality of projections extending from the root surface and oriented substantially parallel to the longitudinal axis and at least one second projection extending from the root surface and positioned between two adjacent first projections, the first plurality of projections circumferentially spaced from one another and the at least one second projection disposed on the root surface at an angle relative to the first plurality of projections, and further wherein the first plurality of projections and the at least one second projection extend laterally beyond the at least one of the first edge and the second edge.

Assignees

• Pratt & Whitney Canada

Inventors

• Tomescu Dana

Classifications

• G01D5/145

  influenced by the relative movement between the Hall device and magnetic fields (see G01R33/06) · CPC title

• B64C11/301 Primary

  characterised by blade position indicating means · CPC title

• B64C11/30

  Blade pitch-changing mechanisms · CPC title

• B64C27/78

  in association with pitch adjustment of blades of anti-torque rotor · CPC title

• G01P3/488

  delivered by variable reluctance detectors · CPC title