Magnetic control of guide vanes

Patent metadata

Field	Value
Publication number	US-9828871-B2
Application number	US-201414546646-A
Country	US
Kind code	B2
Filing date	Nov 18, 2014
Priority date	Nov 18, 2014
Publication date	Nov 28, 2017
Grant date	Nov 28, 2017

Abstract

A system for controlling an angular position of a component of an aircraft includes a component having a shaft that includes at least one magnet. The system also includes a housing configured to receive the shaft and including at least one coil configured to generate a magnetic field based on a current through the at least one coil.

First claim

What is claimed is:

1. A system for controlling an angular position of a component of an aircraft comprising:
a component having a shaft that includes a first row of magnets that includes a first plurality of magnets equally spaced about a circumference of the shaft and a second row of magnets axially adjacent the first row of magnets and wherein the second row of magnets includes a second plurality of magnets equally spaced about the circumference of the shaft; and
a housing configured to receive the shaft and including at least one coil and a magnetic position sensor, wherein the at least one coil is configured to generate a magnetic field based on a current through the at least one coil and wherein the magnetic position sensor is positioned circumferentially about the shaft and configured to detect an angular position of the shaft within the housing, wherein a first coil is positioned circumferentially around and aligned with the first row of magnets and the magnetic position sensor is positioned circumferentially around and aligned with the second row of magnets.

2. The system of claim 1 , wherein the component is a variable vane in a turbine system.

3. The system of claim 1 , further including a controller configured to control the angular position of the component by controlling the current through the at least one coil such that the magnetic field causes a torque on the shaft.

4. The system of claim 3 , wherein the shaft has a longitudinal axis.

5. The system of claim 4 , wherein the housing has a longitudinal axis and the at least one coil includes a first coil and a second coil circumferentially adjacent the first coil such that a different current may flow through the first coil than the second coil.

6. The system of claim 5 , further comprising a first power supply coupled to the controller and the first coil and a second power supply coupled to the controller and the second coil, wherein the controller is configured to control the first power supply to generate the current through the at least one coil and the controller is configured to control the second power supply to generate the current through the second coil.

7. A system for controlling an angular position of a component of an aircraft, the system comprising:
a component having a shaft having a longitudinal axis, the shaft including a first row of magnets that includes a first plurality of magnets equally spaced about a circumference of the shaft and a second row of magnets axially adjacent the first row of magnets and wherein the second row of magnets includes a second plurality of magnets equally spaced about the circumference of the shaft;
a first power supply configured to generate a first current;
a second power supply configured to generate a second current;
a third power supply configured to generate a third current;
a housing configured to receive the shaft and including a first coil coupled to the first power supply and configured to receive the first current and generate a first magnetic field based on the first current, wherein the housing further includes a second coil coupled to the second power supply and configured to receive the second current and generate a second magnetic field based on the second current, wherein the housing further includes a third coil coupled to the third power supply and configured to receive the third current and generate a third magnetic field based on the third current, wherein the housing further includes a magnetic position sensor; and
a controller coupled to the first power supply, the second power supply, and the third power supply, wherein the controller is configured to control the first current, the second current, and the third current, wherein the magnetic position sensor is coupled to the controller and is configured to detect the angular position of the shaft relative to the housing, wherein the first coil is positioned circumferentially around and aligned with the first row of magnets and the magnetic position sensor is positioned circumferentially around and aligned with the second row of magnets.

8. The system of claim 7 , wherein the controller is configured to control the first power supply to generate a selectable level of negative and positive current.

9. The system of claim 7 , wherein each circumferentially adjacent pair of magnets of the first plurality of magnets have opposite polarities.

10. The system of claim 7 , wherein the housing further includes a magnetic position sensor coupled to the controller and configured to detect the angular position of the shaft relative to the housing.

11. The system of claim 10 , wherein the housing has a longitudinal axis and the first coil is positioned circumferentially opposite the magnetic position sensor.

12. The system of claim 10 , wherein the magnetic position sensor is positioned circumferentially about the longitudinal axis of the shaft of the component.

13. The system of claim 10 , wherein the shaft is configured to rotate about the longitudinal axis, wherein the magnetic position sensor does not rotate with the shaft.

14. The system of claim 7 , wherein an angular distance between adjacent magnets of the first plurality of magnets is different than an angular distance between the first coil and the second coil.

15. The system of claim 7 , wherein each angular distance between each pair of circumferentially adjacent coils of the first coil, the second coil, and the third coil is different.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Poisson Richard A
• Mantese Joseph V

Classifications

• F01D17/165

  for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F01D21/003 Primary

  Arrangements for testing or measuring (for measuring vibrations G01H) · CPC title

• F01D17/162 Primary

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• H02K26/00

  Machines adapted to function as torque motors, i.e. to exert a torque when stalled · CPC title

• H01F7/145

  Rotary electromagnets with variable gap (with fixed gap or torque motors H02K26/00) · CPC title