System and method for measuring dynamic loads in a magnetic bearing

• US 6,518,770 B2
• Filed: 05/15/2001
• Issued: 02/11/2003
• Est. Priority Date: 05/16/2000
• Status: Expired due to Fees

• Current Assignee: Texas A&M University System
• Original Assignee: Texas A&M University System
• Inventors: Childs, Dara W.
• Primary Examiner(s): Oda, Christine
• Assistant Examiner(s): KERVEROS, JAMES C
• Application Number:
  US09/858,275
• Publication Number:
  US 20020005724A1
• Time in Patent Office: 637 Days
• Field of Search: 324/545, 324/772, 324/96, 324/117.H, 310/68.B, 310/90.5, 738/624.9, 385/26, 356/81, 250/205
• US Class Current: 324/545
• CPC Class Codes: F16C 32/0444 Details of devices to control the actuation of the electromagnets
• CPC Class Codes: F16C 41/00 Other accessories, e.g. devices integrated in the bearing not relating to the bearing function as such
• CPC Class Codes: G01B 11/18 using photoelastic elements
• CPC Class Codes: G01D 5/35303 using a reference fibre, e.g. interferometric devices
• CPC Class Codes: G01L 5/0009 Force sensors associated with a bearing testing of bearings G01M13/04

Abstract

A system for measuring dynamic loads in a rotordynamic system having a rotor includes a magnetic bearing disposed around the rotor and having a plurality of magnets and at least one fiber optic strain gage associated with a pole of a respective magnet. The fiber optic strain gage is operable to detect a strain on the respective pole resulting from the dynamic loads. The detected strain is indicative of the dynamic loads.

Claims

1. A system for measuring dynamic loads in a rotordynamic system having a rotor, comprising:

a magnetic bearing disposed around the rotor and having a plurality of magnets; and

at least one fiber optic strain gage associated with a pole of a respective one of the plurality of magnets, the fiber optic strain gage operable to detect a strain on the pole resulting from the dynamic loads.

2. The system of claim 1, wherein a first end of the fiber optic strain gage is disposed proximate an end of the pole proximate the rotor.

3. The system of claim 1, wherein the fiber optic strain gage is coupled to an outside surface of the pole.

4. The system of claim 1, wherein the fiber optic strain gage is disposed within the pole.

5. The system of claim 1, wherein the at least one fiber optic strain gage comprises two fiber optic strain gages associated with poles of two of the magnets, the two fiber optic strain gages oriented, with respect to the rotor, approximately ninety degrees from one another.

6. The system of claim 1, wherein the at least one fiber optic strain gage comprises four fiber optic strain gages associated with poles of four of the magnets, the four fiber optic strain gages oriented, with respect to the rotor, approximately ninety degrees from one another.

7. The system of claim 1, wherein the at least one fiber optic strain gage comprises three fiber optic strain gages associated with poles of three of the magnets, the three fiber optic strain gages oriented, with respect to the rotor, approximately 120 degrees from one another.

8. A system for measuring dynamic loads in a rotordynamic system having a rotor, comprising:

a magnetic bearing disposed around the rotor and having a plurality of magnets, each magnet having two poles and formed from a plurality of metal plates;

a first fiber optic strain gage disposed within a pole of a first magnet such that an end of the first fiber optic strain gage is proximate an end of the pole of the first magnet;

a second fiber optic strain gage disposed within a pole of a second magnet such that an end of the second fiber optic strain gage is proximate an end of the pole of the second magnet, the second fiber optic strain gage oriented approximately ninety degrees from the first fiber optic strain gage with respect to the rotor; and

wherein the first and second fiber optic strain gages are operable to detect first and second strains on their respective poles resulting from the dynamic loads.

9. The system of claim 8, further comprising:

a third fiber optic strain gage disposed within a pole of a third magnet such that an end of the third fiber optic strain gage is proximate an end of the pole of the third magnet, the third fiber optic strain gage oriented approximately 180 degrees from the first fiber optic strain gage with respect to the rotor; and

a fourth fiber optic strain gage disposed within a pole of a fourth magnet such that an end of the fourth fiber optic strain gage is proximate an end of the pole of the fourth magnet, the fourth fiber optic strain gage oriented approximately 180 degrees from the second fiber optic strain gage with respect to the rotor.

10. The system of claim 8, further comprising a third fiber optic strain gage disposed within a pole of a third magnet such that an end of the third fiber optic strain gage is proximate an end of the pole of the third magnet, and wherein the first, second, and third fiber optic strain gages are oriented approximately 120 degrees from one another with respect to the rotor.

11. A method for measuring dynamic loads in a rotordynamic system having a rotor, comprising:

disposing a magnetic bearing around the rotor, the magnetic bearing having a plurality of magnets;

associating at least one fiber optic strain gage with a pole of a respective one of the plurality of magnets; and

detecting, via the fiber optic strain gage, a strain on the pole resulting from the dynamic loads.

12. The method of claim 11, further comprising disposing a first end of the fiber optic strain gage proximate an end of the pole proximate the rotor.

13. The method of claim 11, further comprising coupling the fiber optic strain gage to an outside surface of the pole.

14. The method of claim 11, further comprising disposing the fiber optic strain gage within the pole.

15. The method of claim 11, wherein associating the at least one fiber optic strain gage with the pole of the respective one of the plurality of magnets comprises:

associating two fiber optic strain gages with poles of two of the magnets; and

orienting, with respect to the rotor, the two fiber optic strain gages approximately ninety degrees from one another.

16. The method of claim 11, wherein associating the at least one fiber optic strain gage with the pole of the respective one of the plurality of magnets comprises:

associating four fiber optic strain gages with poles of four of the magnets; and

orienting, with respect to the rotor, the four fiber optic strain gages approximately ninety degrees from one another.

17. The method of claim 11, wherein associating the at least one fiber optic strain gage with the pole of the respective one of the plurality of magnets comprises:

associating three fiber optic strain gages with poles of three of the magnets; and

orienting, with respect to the rotor, the three fiber optic strain gages approximately 120 degrees from one another.

18. A method for measuring dynamic loads in a rotordynamic system having a rotor, comprising:

disposing a magnetic bearing around the rotor, the magnetic bearing having a plurality of magnets, each magnet having two poles and formed from a plurality of metal plates;

disposing a first fiber optic strain gage within a pole of a first magnet such that an end of the first fiber optic strain gage is proximate an end of the pole of the first magnet;

disposing a second fiber optic strain gage within a pole of a second magnet such that an end of the second fiber optic strain gage is proximate an end of the pole of the second magnet;

orienting, with respect to the rotor, the second fiber optic strain gage approximately ninety degrees from the first fiber optic strain gage; and

detecting, via the first and second fiber optic strain gages, first and second strains on their respective poles resulting from the dynamic loads.

19. The method of claim 18, further comprising:

disposing a third fiber optic strain gage within a pole of a third magnet such that an end of the third fiber optic strain gage is proximate an end of the pole of the third magnet;

orienting the third fiber optic strain gage approximately 180 degrees from the first fiber optic strain gage with respect to the rotor;

disposing a fourth fiber optic strain gage within a pole of a fourth magnet such that an end of the fourth fiber optic strain gage is proximate an end of the pole of the fourth magnet; and

orienting the fourth fiber optic strain gage approximately 180 degrees from the second fiber optic strain gage with respect to the rotor.

20. The method of claim 18, further comprising:

disposing a third fiber optic strain gage within a pole of a third magnet such that an end of the third fiber optic strain gage is proximate an end of the pole of the third magnet; and

orienting the first, second, and third fiber optic strain gages approximately 120 degrees from one another with respect to the rotor.

21. A method for calibrating a fiber optic strain gage associated with a magnetic bearing supporting a shaft, the method comprising:

applying a force to the shaft;

measuring a first magnitude of the force with a calibrated system associated with the magnetic bearing;

detecting a strain on a pole of a magnet of the magnetic bearing with the fiber optic strain gage;

determining a second magnitude of the force based on the detected strain;

comparing the first magnitude and the second magnitude; and

adjusting the fiber optic strain gage based on the comparison.

22. The method of claim 21, wherein applying the force to the shaft comprises applying the force to the shaft at a generally low frequency.

23. The method of claim 22, wherein applying the force to the shaft at the generally low frequency comprises applying the force to the shaft at a frequency between approximately one and five hertz.

24. The method of claim 21, wherein applying the force to the shaft comprises inputting an error signal into a controller associated with the magnetic bearing.

25. The method of claim 21, wherein measuring the first magnitude of the force with the calibrated system associated with the magnetic bearing comprises measuring the first magnitude of the force with a calibrated load cell associated with the magnetic bearing.

26. The method of claim 21, wherein comparing the first magnitude and the second magnitude comprises producing a transfer function by utilizing Fourier transforms.