Fault-tolerant magnetic bearing position sensing and control system

• US 20060055259A1
• Filed: 09/14/2004
• Published: 03/16/2006
• Est. Priority Date: 09/14/2004
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hanlon, Casey, Potter, Calvin C., Wingett, Paul T.
• Application Number:
  US10/941,179
• Publication Number:
  US 20060055259A1
• Time in Patent Office: Days
• US Class Current: 310/90.500
• CPC Class Codes: F16C 32/0442 with devices affected by abnormal, undesired or non-standard conditions such as shock-load, power outage, start-up or touchdown
• CPC Class Codes: F16C 32/0446 Determination of the actual position of the moving member, e.g. details of sensors
• CPC Class Codes: G05B 9/03 with multiple-channel loop, i.e. redundant control systems

Abstract

A magnetic bearing sensing and control system and method provides increased tolerance to faults associated with the associated displacement sensors. The system includes a plurality of redundant displacement sensor sets to provide dual or triple displacement sensor redundancy, or higher if desired, and implements a process for determining when one or more displacement sensors is faulty. The system also compensates for determined sensor-related faults.

Claims

1. An active magnetic bearing sensing and control system for rotationally suspending a rotor that is configured to rotate about a rotational axis, the system comprising:

a first primary displacement sensor configured to sense rotor displacements in a first axis that is perpendicular to the rotational axis and supply a displacement signal representative thereof;

a second primary displacement sensor configured to sense rotor displacements in a second axis that is perpendicular to the rotational axis and supply a displacement signal representative thereof;

a first secondary displacement sensor configured to sense rotor displacements in the first axis and supply a displacement signal representative thereof;

a second secondary displacement sensor configured to sense rotor displacements in the second axis and supply a displacement signal representative thereof; and

a controller coupled to receive the displacement signals from each of the displacement sensors and a speed signal representative of a rotational speed of the rotor, the controller operable, in response to receipt of the displacement signals and the speed signal, to determine whether each of the displacement signals is valid.

2. The system of claim 1, wherein the controller is further operable, in response to the displacement signals, to determine the rotational speed of the rotor and supply the speed signal representative thereof.

3. The system of claim 1, further comprising:

a rotational speed sensor operable to sense the rotational speed of the rotor and supply the speed signal representative thereof.

4. The system of claim 1, wherein the controller is further operable to selectively disregard one or more of the displacement signals based on the determined validity thereof.

5. The system of claim 1, wherein the controller is further operable to determine a cause of invalidity of one or more of the displacement signals.

6. The system of claim 1, wherein:

each displacement sensor comprises a displacement sensor set that includes a first individual displacement sensor and a second individual displacement sensor disposed in opposing relation to one another with the rotor interposed there between;

each individual displacement sensor in each displacement sensor set is configured to sense rotor displacements relative thereto and supply an individual sensor displacement signal representative thereof; and

each displacement signal is based on a difference between the individual sensor displacement signals associated with each individual displacement sensor in each displacement sensor set.

7. The system of claim 6, wherein the controller is further operable, in response to receipt of the displacement signals and the speed signal, to selectively disregard only one of the individual sensor displacement signals from one of the individual displacement sensors in each displacement sensor set.

8. The system of claim 1, further comprising:

a first tertiary displacement sensor configured to sense rotor displacements in the first axis and supply a displacement signal representative thereof; and

a second tertiary displacement sensor configured to sense rotor displacements in the second axis and supply a displacement signal representative thereof.

9. The system of claim 1, further comprising:

a sensor target coupled to the rotor,

wherein each displacement sensor senses rotor displacement based on a displacement between the displacement sensor and the sensor target.

10. The system of claim 1, wherein the controller is further operable, in response to receipt of the displacement signals and the speed signal, to determine whether one or more of the sensors is faulty or at least a portion of the sensor target is faulty.

11. The system of claim 10, wherein the controller is further operable, in response to the displacement signals and the speed signal, to (i) determine rotor position using a position determination algorithm and (ii) selectively supply rotor position command signals representative of a commanded rotor position based at least in part on the determined rotor position.

12. The system of claim 11, further comprising:

one or more electromagnets, each electromagnet coupled to receive one or more of the rotor position command signals and operable, in response thereto, to position the rotor to the commanded rotor position.

13. The system of claim 11, wherein, if the controller determines that at least a portion of the sensor target is faulty, the controller determines rotor position using an altered position determination algorithm.

14. The system of claim 11, wherein:

the first and second primary displacement sensors are disposed orthogonal relative to one another; and

the first and second secondary displacement sensors are disposed orthogonal relative to one another.

15. In a system including at least a rotor that is configured to rotate about a rotational axis, and one or more active magnetic bearings configured to rotationally suspend the rotor, a method of determining system operability, comprising the steps of:

sensing a first primary rotor displacement in a first axis that is perpendicular to the rotational axis;

sensing a second primary rotor displacement in a second axis that is perpendicular to the rotational axis;

sensing a first secondary rotor displacement in the first axis;

sensing a second secondary rotor displacement in the second axis;

determining a rotational speed of the rotor; and

determining a validity of each of the sensed rotor displacements based, at least in part on, the sensed rotor displacements and the determined rotational speed.

16. The method of claim 15, wherein the rotational speed is determined based at least in part on the sensed rotor displacements.

17. The method of claim 15, further comprising:

selectively disregarding one or more of the sensed rotor displacement signals based on the determined validity of each of the sensed rotor displacements.

18. The method of claim 15, further comprisings:

determining a cause of invalidity of one or more of the sensed rotor displacements.

19. The method of claim 15, wherein the sensed rotor displacements are generated using a sensor target coupled to the rotor, and a plurality of sensors, and wherein the method further comprises:

determining whether one or more of the sensors is faulty or at least a portion of the sensor target is faulty.

20. The method of claim 19, further comprising:

determining rotor position using a position determination algorithm; and

selectively supplying actuator position command signals representative of a commanded rotor position based at least in part on the determined rotor position.

21. The method of claim 20, further comprising:

determining rotor position using an altered position determination algorithm, if the sensor target is determined to be degraded.