Surface mounted and scanning spatially periodic eddy-current sensor arrays

• US 6,952,095 B1
• Filed: 09/20/2000
• Issued: 10/04/2005
• Est. Priority Date: 09/20/1999
• Status: Expired due to Term

• Current Assignee: Jentek Sensors, Inc.
• Original Assignee: Jentek Sensors, Inc.
• Inventors: Goldfine, Neil J., Schlicker, Darrell E., Washabaugh, Andrew P., Zilberstein, Vladimir A., Tsukernik, Vladimir
• Primary Examiner(s): PATIDAR, JAY M
• Application Number:
  US09/666,524
• Time in Patent Office: 1,840 Days
• Field of Search: 324/227, 324/232, 324/239, 324/202, 324/240, 324/241, 324/242, 324/243
• US Class Current: 324/240
• CPC Class Codes: G01B 7/24 using change in magnetic properties
• CPC Class Codes: G01B 7/34 for measuring roughness or irregularity of surfaces
• CPC Class Codes: G01N 27/72 by investigating magnetic variables
• CPC Class Codes: G01N 27/90 using eddy currents
• CPC Class Codes: G01N 27/902 by moving the sensors
• CPC Class Codes: G01R 33/12 Measuring magnetic properties of articles or specimens of solids or fluids involving magnetic resonance G01R33/20

Abstract

Inductive sensors measure the near surface properties of conducting and magnetic material. A sensor may have primary windings with parallel extended winding segments to impose a spatially periodic magnetic field in a test material. Those extended portions may be formed by adjacent portions of individual drive coils. Sensing elements provided every other half wavelength may be connected together in series while the sensing elements in adjacent half wavelengths are spatially offset. Certain sensors include circular segments which create a circularly symmetric magnetic field that is periodic in the radial direction. Such sensors are particularly adapted to surround fasteners to detect cracks and can be mounted beneath a fastener head. In another sensor, sensing windings are offset along the length of parallel winding segments to provide material measurements over different locations when the circuit is scanned over the test material. The distance from the sensing elements to the ends of the primary winding may be kept constant as the offset space in between sensing elements is varied. An image of the material properties can be provided as the sensor is scanned across the material.

Claims

1. A method of monitoring damage at a fastener through the test substrate comprising:

mounting respective spatially periodic field eddy-current sensors to the test substrate at both ends of a fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensors.

2. A method as claimed in claim 1 where the damage is in the form of a crack.

3. A method as claimed in claim 2, wherein an action is taken at a predetermined sensor response level.

4. A method as claimed in claim 1 wherein at least one sensor from the eddy-current sensors is placed in an area likely to see damage and at least one sensing element is placed in an area unlikely to see damage.

5. A method as claimed in claim 1 wherein the eddy-current sensors are located at different radial distances from the fastener center.

6. A method as claimed in claim 1 wherein the eddy-current sensors are located at different circumferential positions around the fastener.

7. A method for monitoring damage at a fastener comprising:

mounting at least two eddy-current sensor arrays on a test substrate around respective fasteners;

connecting drive and sense conductors of the eddy-current sensors with a single cable to a data acquisition system; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensors.

8. A method as claimed in claim 7 where the each sensor provides a separate output.

9. A method as claimed in claim 8 where the output is an absolute property measurement.

10. A method as claimed in claim 7 where the drive conductors of at least two sensors are connected in series.

11. A method as claimed in claim 10 where sense conductors of the at least two eddy-current sensor arrays are connected together to provide a differential measurement.

12. A method as claimed in claim 7 where separate drive connections are made to each sensor.

13. A method as claimed in claim 12 where the sense conductors are connected together to provide a common output connection.

14. A method as claimed in claim 7 where the drive conductors are connected together to provide a common drive signal.

15. A method as claimed in claim 14 where the sense conductors are connected together to provide a common output connection.

16. A method as claimed in claim 7 wherein at least one eddy-current sensor is placed in an area likely to see damage and at least one eddy-current sensor is placed in an area unlikely to see damage.

17. A method as claimed in claim 7 wherein the eddy-current sensors are located at different circumferential positions around the fastener.

58. A method as claimed in claim 7 wherein the eddy-current sensors are located at different radial distances from the fastener center.

18. A method for monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a test substrate under the head of a fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

19. A method as claimed in claim 18 where at least one sensor is a circular spatially periodic field sensor.

20. A method as claimed in claim 18 where at least one eddy-current sensor is placed in an area likely to see damage and at least one eddy-current sensor is placed in an area unlikely to see damage.

21. A method as claimed in claim 18, wherein the test substrate is a test specimen.

22. A method for performing fatigue testing at a fastener comprising:

mounting an eddy current sensor array to a test substrate under the head of a fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

23. A method as claimed in claim 22 where the sensor further comprises a drive having at least two conductors where the current changes direction in at least one conductor.

24. A method as claimed in claim 22, wherein the test substrate is a test specimen.

25. A method of monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener, and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

26. A method as claimed in claim 25 wherein the test substrate is a test specimen.

27. A method of monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a test specimen, the sensor being mounted between layers of the test coupon attached by the fastener; and

sensing response of the test specimen to a magnetic field imposed by the eddy-current sensor array.

28. A method as claimed in claim 27 wherein the sensor is thin and conforms to the shape of the test specimen.

29. A method as claimed in claim 27 wherein the sensor is mounted using an adhesive.

30. A method as claimed in claim 27 wherein the sensor is mounted by pressing the sensor against the surface of the test specimen and using pressure to hold the sensor in place, the pressure being provided by an opposing surface whose shape matches the shape of the test specimen.

31. A method for performing fatigue testing at a fastener comprising:

mounting an eddy current sensor array to a test substrate under the head of a fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

32. A method of monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a structure near a fastener, the sensor array being mounted between layers of the structure attached by the fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array, each eddy-current sensor having at least two drive conductors and the current changing direction in at least one conductor.

33. A method of monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener;

sensing response of the structure to a magnetic field imposed by the eddy-current sensor; and

calibrating each sense element of the eddy-current sensor array by adjusting the response to an appropriate level.

34. A method as claimed in claim 33 where the calibration involves placing the sensor on the test structure and measuring the response of each sense element.

35. A method as claimed in claim 34 where the calibration further involves a second response measurement for each sense element with a nonconductive material placed between the sensor and the test material.

36. A method as claimed in claim 34 wherein the calibration includes varying the temperature of the test material.

37. A method of monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener; and

sensing response of the structure to a magnetic field imposed by the eddy-current sensor array, each eddy current sensor having a periodic magnetic field produced by linear segments of its drive winding.

38. A method of monitoring damage at a fastener comprising:

mounting an eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener; and

sensing response of the structure to a magnetic field imposed by the eddy-current sensor array, the sensor array having a magnetic field produced by a drive winding formed from concentric conductors within the same plane.

39. A method as claimed in claim 38, wherein there is one or more sense elements per each conductor.

40. A method for monitoring damage at a fastener comprising:

mounting a spatially periodic field eddy current sensor array with a cylindrical support material shaped in the form of a washer;

mounting the cylindrical support to a test substrate under a fastener head; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor.

41. A method as claimed in claim 40 where the test substrate withstands compressive loads.

42. A method for monitoring damage under the head of a fastener comprising:

mounting an eddy current sensor array to a test substrate under the head of a fastener with sense elements located at different radial distances from the fastener center; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensors.

43. A method for monitoring damage under the head of a fastener comprising:

mounting an eddy current sensor array to a test substrate under the head of a fastener with sense elements located at different circumferential positions around the fastener; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensors.

44. A method of monitoring damage at a fastener comprising:

mounting an eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener with at least one sensing element placed in an area likely to see damage and at least one sensing element placed in an area unlikely to see damage; and

sensing response of the structure to a magnetic field imposed by the eddy-current sensors.

45. A method of monitoring damage at a fastener comprising:

mounting an eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener with sense elements located at different radial distances from the fastener center; and

sensing response of the structure to a magnetic field imposed by the eddy-current sensors.

46. A method of monitoring damage at a fastener comprising:

mounting an eddy-current sensor array to a structure near a fastener, the sensor being mounted between layers of the structure attached by the fastener with sense elements located at different circumferential positions around the fastener; and

sensing response of the structure to a magnetic field imposed by the eddy-current sensors.

47. A method for monitoring damage at a fastener comprising:

mounting an eddy-current sensor array with a cylindrical support material shaped in the form of a washer with at least one sensing element placed in an area likely to see damage and at least one sensing element placed in an area unlikely to see damage;

mounting the cylindrical support to a test substrate under a fastener head; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

48. A method for monitoring damage at a fastener comprising:

mounting an eddy-current sensor array with a cylindrical support material shaped in the form of a washer the sense elements being located at different radial distances from the fastener center;

mounting the cylindrical support to a test substrate under a fastener head; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

49. A method for monitoring damage at a fastener comprising:

mounting an eddy-current sensor array with a cylindrical support material shaped in the form of a washer the sense elements being located at different circumferential positions around the fastener;

mounting the cylindrical support to a test substrate under a fastener head; and

sensing response of the test substrate to a magnetic field imposed by the eddy-current sensor array.

50. A method for monitoring damage at a fastener comprising:

mounting at least two eddy-current sensor arrays on a test substrate around fasteners;

connecting drive windings of the eddy-current sensor arrays in series; and

sensing a response of the test substrate to a magnetic field imposed by the eddy-current sensor arrays.

51. A method as claimed in claim 50 wherein each sensor has one or more sensing elements.

52. A method as claimed in claim 51 where the response from all of the sensing elements are monitored in parallel at essentially the same time.

53. A method as claimed in claim 50 where the sensors are used to monitor material properties at different locations to detect response changes.

54. A method as claimed in claim 53 where the changes in the response are related to damage in material.

55. A method as claimed in claim 53 where the response is used to detect the initiation of a crack.

56. A method as claimed in claim 53 where the response is used to monitor the growth of a crack.

57. A method as claimed in claim 53 where the response is used to estimate the length of a crack.