IP Library › Granted Patent US 8,549,931
Granted Patent B2
US 8,549,931 · App. 13/067,651 · Granted Oct 8, 2013

Speed or torque probe for gas turbine engines

Inventor: Robert Michael George Bodin (Hampshire, GB)
Assignee: Weston Aerospace Limited
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Quick Facts
Patent No.
US 8,549,931
App. No.
13/067,651
Granted
Oct 8, 2013
Kind
B2
Abstract

There is provided a variable reluctance sensor for sensing the speed or torque of a shaft in a gear box or gas turbine engine, comprising a magnetic pole piece a conductive wire wrapped around the pole piece a housing surrounding the pole piece, the housing having a front face and at least one side wall, wherein, in use, the front face is positioned proximate to an object to be sensed wherein the pole piece is rigidly fixed to the side wall of the housing. This arrangement reduces microphony in the sensor.

Claims (34)

1. A variable reluctance sensor for sensing the speed or torque of a shaft in a gear box or gas turbine engine, comprising:

a magnetic pole piece;

a conductive wire wrapped around the pole piece;

a housing surrounding the pole piece, the housing having a front face and at least one side wall, wherein, in use, the front face is positioned proximate to an object to be sensed,

wherein the pole piece is rigidly fixed to the side wall of the housing.

2. A variable reluctance sensor according to claim 1 , wherein the pole piece is rigidly fixed to a plurality of points on the housing.

3. A variable reluctance sensor according to claim 1 , wherein the pole piece is welded to the housing.

4. A variable reluctance sensor according to claim 1 , wherein the pole piece is mechanically fixed to the housing.

5. A variable reluctance sensor according to claim 1 , further comprising a rigid intermediate structure wherein the pole piece is rigidly fixed to the rigid intermediate structure, and the rigid intermediate structure is rigidly fixed to the housing.

6. A variable reluctance sensor according to claim 1 , wherein the pole piece extends through and is fixed to the front of the housing.

7. A variable reluctance sensor according to claim 6 , wherein the pole piece is welded to the front face of the housing.

8. A variable reluctance sensor according to claim 1 , wherein the pole piece extends through the front face of the housing but is not fixed to the front face of the housing.

9. A variable reluctance sensor according to claim 1 , wherein the front face of the housing is substantially less rigid than the side wall of the housing.

10. A variable reluctance sensor according to claim 1 , further comprising a permanent magnet, the permanent magnet positioned within the housing adjacent to the pole piece.

11. A variable reluctance sensor according to claim 10 , wherein the permanent magnet is rigidly fixed to a side wall of the housing.

12. A variable reluctance sensor according to claim 10 , wherein the pole piece has a front end adjacent to the front face of the housing and a rear end positioned adjacent to the permanent magnet, and wherein the rear end of the pole piece is fixed to the side wall of the housing.

13. A variable reluctance sensor according to claim 1 , wherein the pole piece is formed in one piece and comprises a longitudinally extending shaft around which the conductive wire is wrapped, and a rear end which is rigidly fixed to the housing.

14. A variable reluctance sensor according to claim 1 , wherein the conductive wire is held in place relative to the pole piece by a packing material surrounding the conductive wire and a portion of the pole piece.

15. A gas turbine engine comprising:

a rotating shaft;

a phonic wheel mounted to the shaft for rotating with the shaft; and

a variable reluctance sensor according to claim 1 , wherein the front face of the housing is positioned proximate to the phonic wheel.

16. A variable reluctance sensor for sensing the speed or torque of a shaft in a gear box or gas turbine engine, comprising:

a magnetic pole piece;

a conductive wire wrapped around the pole piece;

a permanent magnet adjacent to the pole piece;

a housing surrounding the pole piece and the permanent magnet, the housing having a front face and at least one side wall, wherein, in use, the front face is positioned proximate to an object to be sensed,

wherein the pole piece is rigidly fixed to the side wall of the housing.

17. A variable reluctance sensor for sensing the speed or torque of a shaft in a gear box or gas turbine engine, comprising:

a magnetic pole piece;

a conductive wire wrapped around the pole piece;

a housing surrounding the pole piece, the housing having a front face and at least one side wall, wherein, in use, the front face is positioned proximate to an object to be sensed,

wherein the pole piece extends through the front face of the housing and the front face of the housing is substantially less rigid than the side wall of the housing.

18. A variable reluctance sensor according to claim 17 wherein the pole piece is fixed to the front face of the housing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 18, 2011
From: BODIN, ROBERT MICHAEL GEORGE
To: WESTON AEROSPACE LIMITED
Reel/Frame 026799/0113 →
Priority Claims (1)
GB 1010497.4 · Jun 22, 2010 · national
Continuity (1)
Related Publication 20110308331A1 · Dec 22, 2011