Monitoring rotating machinery using radio frequency probes

• US 10,280,787 B2
• Filed: 11/09/2015
• Issued: 05/07/2019
• Est. Priority Date: 11/09/2015
• Status: Active Grant

• Current Assignee: University of Notre DAME Du Lac
• Original Assignee: University of Notre DAME Du Lac
• Inventors: Pratt, Thomas G., Mueller, Jeffrey G., Kossler, Robert D., Dodson, Neil, Morris, Scott C.
• Primary Examiner(s): Ahn, Sung S
• Application Number:
  US14/936,523
• Publication Number:
  US 20170134154A1
• Time in Patent Office: 1,275 Days
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H

Abstract

Systems and methods for monitoring rotating machinery are disclosed. Transmitter and receiver antennas can be provided with access to the rotating machinery. At least one receiver signal resulting from at least one transmitter signal that has propagated through a portion of the rotating machinery can be obtained. A first signal pair can be formed from a first receiver signal and a first transmitter signal, or from first and second receiver signals obtained from spatially-separated receiver antennas, or from first and second receiver signals which are attributable to different transmitter signals. Amplitude and phase information of a plurality of frequency components for each signal in the first signal pair can be determined. A set of comparison values for the first signal pair can be determined by comparing respective frequency component phases or respective frequency component amplitudes. A characteristic of the rotating machinery can then be analyzed using the comparison values.

Claims

1. A method for monitoring rotating machinery, the method comprising:

providing at least one transmitter antenna with access to at least a portion of the rotating machinery;

providing at least one receiver antenna with access to the portion of the rotating machinery;

obtaining at least one receiver signal resulting from at least one transmitter signal that has propagated from the transmitter antenna to the receiver antenna by way of the portion of the rotating machinery;

forming at least a first signal pair which comprises

a first receiver signal and a first transmitter signal, or

first and second receiver signals which are obtained from spatially-separated receiver antennas, or

first and second receiver signals which are attributable to different transmitter signals, or

first and second receiver signals which are obtained from non-orthogonally polarized portions of one or more receiver antennas, or

a coherent beam signal associated with a plurality of receiver antennas or a coherent beam signal associated with a plurality of transmitter antennas, or

a combination transmitter signal comprising a combination of two or more transmitter signals or a combination receiver signal comprising a combination of two or more receiver signals;

determining amplitude and phase information of a plurality of frequency components for each signal in the first signal pair;

determining a set of comparison values for the first signal pair by comparing respective frequency component phases and respective frequency component amplitudes of the signals in the first signal pair; and

analyzing a characteristic of the rotating machinery using the set of comparison values,

wherein the rotating machinery comprises a gas turbine engine.

2. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to a turbine stage of the rotating machinery, including on opposite sides, on the same side, or about a rotation axis of the turbine stage.

3. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to a compressor stage of the rotating machinery, including on opposite sides, on the same side, or about a rotation axis of the compressor stage.

4. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to a bypass fan of the rotating machinery, including on opposite sides, on the same side, or about a rotation axis of the bypass fan.

5. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to a bearing of the rotating machinery.

6. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to a combustor of the gas turbine engine.

7. The method of claim 1, further comprising positioning the transmitter antenna and the receiver antenna with access to an exit nozzle of the gas turbine engine.

8. The method of claim 1, further comprising coherently receiving the first and second receiver signals, whether they are attributable to a common transmitter signal or different transmitter signals.

9. The method of claim 8, wherein coherently receiving the first and second receiver signals comprises frequency down-converting the first and second receiver signals using a common local oscillator.

10. The method of claim 8, wherein coherently receiving the first and second receiver signals comprises performing synchronous digital sampling of the first and second receiver signals.

11. The method of claim 1, wherein the first and second receiver signals, whether attributable to a common transmitter signal or different transmitter signals, are obtained using co-polarized portions of one or more receiver antennas.

12. The method of claim 1, wherein the first and second receiver signals, whether attributable to a common transmitter signal or different transmitter signals, are obtained using orthogonally-polarized portions of one or more receiver antennas.

13. The method of claim 1, wherein the first and second receiver signals are respectively attributable to first and second transmitter signals, and wherein the first and second transmitter signals are separable.

14. The method of claim 13, wherein the separable first and second transmitter signals are coherently synthesized.

15. The method of claim 13, wherein the separable first and second transmitter signals overlap in time.

16. The method claim 13, wherein the separable first and second transmitter signals are sent using orthogonally-polarized portions of a common transmitter antenna.

17. The method claim 13, wherein the separable first and second transmitter signals are sent using spatially-separated transmitter antennas.

18. The method of claim 1, wherein the first signal pair comprises the first receiver signal and the first transmitter signal, and wherein the first receiver signal is attributable to a second transmitter signal.

19. The method of claim 1, wherein comparing respective frequency component phases and respective frequency component amplitudes of the signals in the first signal pair comprises calculating Jones vectors or Stokes parameters.

20. The method of claim 1, wherein analyzing a characteristic of the transmitter, receiver, or propagation channel using the set of comparison values comprises identifying a characteristic of a curve formed from the comparison values at a given time or identifying a time-varying change in the comparison values.

21. The method of claim 1, wherein the at least one receiver signal and the at least one transmitter signal comprise radio frequency (RF) signals, and where the propagation channel comprises a multipath propagation channel.

22. The method of claim 1, further comprising controlling an operating condition of the rotating machinery based on the characteristic.

36. The method of claim 1, wherein the first signal pair comprises the first receiver signal and the first transmitter signal.

37. The method of claim 1, wherein the first signal pair comprises the first and second receiver signals which are obtained from spatially-separated receiver antennas.

38. The method of claim 1, wherein the first signal pair comprises the first and second receiver signals which are attributable to different transmitter signals.

39. The method of claim 1, wherein the first signal pair comprises the first and second receiver signals which are obtained from non-orthogonally polarized portions of one or more receiver antennas.

40. The method of claim 1, wherein the first signal pair comprises the coherent beam signal associated with a plurality of receiver antennas or the coherent beam signal associated with a plurality of transmitter antennas.

41. The method of claim 1, wherein the first signal pair comprises the combination transmitter signal or the combination receiver signal.

42. The method of claim 1, wherein the first signal pair comprises signals that are time delayed or frequency offset with respect to one another.

43. The method of claim 13, wherein the first and second transmitter signals are made separable using time multiplexing, frequency multiplexing, or code multiplexing.

23. A system for monitoring rotating machinery, the system comprising:

at least one transmitter antenna configured to access to at least a portion of the rotating machinery;

at least one receiver antenna configured to access to the portion of the rotating machinery; and

a processor configured to

obtain at least one receiver signal resulting from at least one transmitter signal that has propagated from the transmitter antenna to the receiver antenna by way of the portion of the rotating machinery;

form at least a first signal pair which comprises a first receiver signal and a first transmitter signal, or first and second receiver signals which are obtained from spatially-separated receiver antennas, or first and second receiver signals which are attributable to different transmitter signals, or first and second receiver signals which are obtained from non-orthogonally polarized portions of one or more receiver antennas, or a coherent beam signal associated with a plurality of receiver antennas or a coherent beam signal associated with a plurality of transmitter antennas, or a combination transmitter signal comprising a combination of two or more transmitter signals or a combination receiver signal comprising a combination of two or more receiver signals;

determine amplitude and phase information of a plurality of frequency components for each signal in the first signal pair;

determine a set of comparison values for the first signal pair by comparing respective frequency component phases and respective frequency component amplitudes of the signals in the first signal pair; and

analyze a characteristic of the rotating machinery using the set of comparison values,

wherein the rotating machinery comprises a gas turbine engine.

24. The system of claim 23, wherein at least one of the transmitter antenna and the receiver antenna is configured to be inserted into the rotating machinery from outside the machinery.

25. The system of claim 23, wherein at least one of the transmitter antenna and the receiver antenna is configured to be internally integrated with the rotating machinery.

26. The system of claim 23, further comprising receiver circuitry to coherently receive the first and second receiver signals.

27. The system of claim 26, wherein the receiver circuitry comprises a common local oscillator to frequency down-convert the first and second receiver signals, and one or more analog-to-digital converters to perform synchronous digital sampling of the first and second receiver signals.

28. The system of claim 23, further comprising transmitter circuitry to coherently synthesize first and second transmitter signals.

29. The system of claim 23, wherein the at least one transmitter antenna and the at least one receiver antenna comprise dual polarization antennas.

30. The system of claim 23, wherein the first signal pair comprises the first receiver signal and the first transmitter signal.

31. The system of claim 23, wherein the first signal pair comprises the first and second receiver signals which are obtained from spatially-separated receiver antennas.

32. The system of claim 23, wherein the first signal pair comprises the first and second receiver signals which are attributable to different transmitter signals.

33. The system of claim 23, wherein the first signal pair comprises the first and second receiver signals which are obtained from non-orthogonally polarized portions of one or more receiver antennas.

34. The system of claim 23, wherein the first signal pair comprises the coherent beam signal associated with a plurality of receiver antennas or the coherent beam signal associated with a plurality of transmitter antennas.

35. The system of claim 23, wherein the first signal pair comprises the combination transmitter signal or the combination receiver signal.