Fiber optic strain gauge patch

• US 5,649,035 A
• Filed: 11/03/1995
• Issued: 07/15/1997
• Est. Priority Date: 11/03/1995
• Status: Expired due to Fees

• Current Assignee: BAE Systems Simula, Inc. (Safariland LLC)
• Original Assignee: BAE Systems Simula, Inc. (Safariland LLC)
• Inventors: Zimmerman, Bernd Dieter, Stevens, Donald Clark, Hardtmann, Dirk Jeffery, Yaniv, Gershon, Lou, Ken-An
• Primary Examiner(s): Bovernick, Rodney B.
• Assistant Examiner(s): Sanghavi, Hemang
• Application Number:
  US08/552,692
• Time in Patent Office: 620 Days
• Field of Search: 385/12-13, 356/32, 356/345, 356/352, 356/35.5, 73/800, 250/227.14-227.19
• US Class Current: 385/13
• CPC Class Codes: G01B 11/18 using photoelastic elements
• CPC Class Codes: G01D 5/35383 using multiple sensor devices using multiplexing techniques
• CPC Class Codes: G01L 1/242 the material being an optical fibre
• CPC Class Codes: G01M 11/086 Details about the embedment of the optical fiber within the DUT

Abstract

A fiber optic sensor for measuring strain on and within structures. The sensor includes an optical fiber, two reflective markers, and two thin layers of carrier material. The optical fiber is looped multiple times within the two thin layers of the carrier material. The optical signal circulates multiple times through the sensing region, as it is travels through the multiple loops of optical fiber within the carrier layers. The fiber optic sensor can be embedded within a structure, as that structure is being fabricated, or it can be attached onto a preexisting structure. An optical signal generated from a source such as a laser is input into one end of the optical fiber. The signal is reflected at reflective markers at predetermined positions in the optical fiber. The time delay of the signals received back is then analyzed to calculate the strain in the structure.

Claims

1. A fiber optic strain gauge patch comprising:

(a) a first layer of protective carrier material;

(b) an optical fiber having a first end and a second end, formed in a plurality of loops, and disposed onto the first layer of protective carrier material;

(c) a first reflective marker in the optical fiber in proximity to the first end of the optical fiber;

(d) a second reflective marker in the optical fiber in proximity to the second end of the optical fiber; and

(e) a second layer of protective carrier material disposed onto the optical fiber,

wherein the first and second layers of protective carrier material hold the optical fiber in position with respect to the first and second layers of protective carrier material.

2. The fiber optic strain gauge patch of claim 1, wherein the second layer of protective carrier material is substantially identical in size and material to the first layer of protective carrier material.

3. The fiber optic strain gauge patch of claim 1, further comprising flexible protective cover placed over at least one of the first and the second ends of the optical fiber.

4. The fiber optic strain gauge patch of claim 1, wherein the first end of the optical fiber is routed outside of the fiber optic strain gauge patch.

5. The fiber optic strain gauge patch of claim 4, wherein the first and the second ends of the optical fiber are routed outside of the fiber optic strain gauge patch.

6. The fiber optic strain gauge patch of claim 1, wherein the first layer of protective carrier material is selected such that it holds the optical fiber in position without the use of any adhesive.

7. The fiber optic strain gauge patch of claim 1, wherein the first layer of protective carrier material is a thermoset material.

8. The fiber optic strain gauge patch of claim 1, wherein the optical fiber terminates at the second reflective marker.

9. The fiber optic strain gauge patch of claim 1, wherein the protective carrier material is a composite material.

10. The fiber optic strain gauge patch of claim 1, wherein the optical fiber is kept in its position using an adhesive.

11. A system for measuring strain comprising:

(a) a fiber optic strain gauge patch comprising a first layer and a second layer of protective carrier material, an optical fiber having a first end and a second end, formed in a plurality of loops, and disposed onto the first layer of protective carrier material, first and second reflective markers on the optical fiber in proximity to the first and second ends, respectively, of the optical fiber, wherein the first and second layers of protective carrier material hold the optical fiber in position with respect to the first and second layers of protective carrier material;

(b) a monitor connected to the optical fiber in the fiber optic strain gauge patch by a connecting optical fiber, said monitor comprising a light source, a delay generator, a fast rise-time photodetector and a fiber optic splitter;

(c) means for analyzing data derived from optical signals reflected by the reflective markers to calculate strain in the optical fiber.

12. The system of claim 11, further comprising a personal computer in communication with the optical time domain reflectometer.

13. The system of claim 12, further comprising a modem in communication with the personal computer.

14. The system of claim 11, wherein the second layer of protective carrier material is substantially identical in size and material to the first layer of protective carrier material.

15. The system of claim 11, further comprising flexible protective cover placed over at least one of the first and the second ends of the optical fiber.

16. The system of claim 11, wherein the first layer of carrier material is selected such that it holds the optical fiber in position without the use of any adhesive.

17. The system of claim 11, wherein the first layer of carrier material is a thermoset material.

18. The system of claim 11, wherein the light source is a laser having a wavelength in the range of 700 to 1600 nanometers.

19. The system of claim 11, wherein the carrier material is a composite material.

20. The system of claim 11, further comprising a 1×

N fiber optic splitter having a single input end and N-multiple output ends optically connected at its single end to the optical time domain reflectometer, wherein the fiber optic strain gauge patch is one of a plurality of fiber optic strain gauge patches optically connected to the N-multiple end of the 1×

N fiber optic splitter.

21. A method for making a fiber optic strain gauge patch comprising:

(a) preparing a first and a second layer of protective carrier material;

(b) preparing an optical fiber having a first end and a second end, and having a first reflective marker in proximity to the first end and a second reflective marker in proximity to the second end;

(c) placing the optical fiber in multiple loops on the first layer of protective carrier material;

(d) encasing the first end of the optical fiber in protective flexible cover;

(e) placing the second layer of protective carrier material over the optical fiber; and

(f) pressing the first and second layers of protective carrier material against each other at a pressure ranging from about 0 psi to about 20 psi.

22. The method of claim 21, wherein the pressure ranges from about 10 to about 13 psi.

23. The method of claim 21, wherein the first and second layers of protective materials are composite materials comprising a first resin.

24. The method of claim 21, wherein the protective carrier materials are uncured during steps (a)-(f), further comprising

(g) curing the protective carrier materials.

25. The method of claim 21, wherein the protective carrier materials are uncured during steps (a)-(f), further comprising:

(g) embedding the fiber optic strain gauge patch in a structure;

(h) routing at least one end of the optical fiber outside of the structure; and

(i) curing the embedded fiber optic strain gauge patch.

26. The method of claim 25, wherein the structure is a composite material comprising a second resin.

27. The method of claim 26, wherein the composite material of the structure and the protective carrier layers are cured simultaneously.

28. The method of claim 26, wherein the first resin and the second resin are the same resin.

29. The method of claim 21, wherein the carrier material is selected from one of epoxy, polyester, vinylester, polyphenylene sulfide, polycarbonate and nylon carrier materials.

30. The method of claim 21, wherein the protective flexible cover is selected from one of polyimide-coated glass and high-modulus plastic tubing.

31. A method for measuring strain in a structure comprising:

(a) providing a fiber optic strain gauge patch having a first layer of protective carrier material, multiple loops of an optical fiber with a first end, a second end, a first reflective marker in proximity to the first end, a second reflective marker in proximity to the second end, and a second layer of protective carrier material, said first and second layers of protective materials covering and enclosing said multiple loops of the optical fiber;

(b) optically connecting the first end of the optical fiber to a time domain reflectometer having a light source, a delay generator, a fast rise-time photo-detector and a fiber optic splitter;

(c) using the optical time domain reflectometer to input a first light pulse into the first end of the optical fiber;

(d) using the optical time delay reflectometer to detect light pulses reflected by the first and second reflective markers;

(e) measuring the time delay between light pulses reflected by the first reflective marker and light pulses reflected by the second reflective marker; and

(f) calculating the strain in the structure from the time delay between light pulses.

32. The method of claim 31, wherein the optical fiber is characterized by its strain sensitivity, and wherein the multiple loops of the optical fiber are characterized by the number of straight sections of optical fiber in the optical fiber strain gauge patch, the length of each such straight section, and a geometric factor, and wherein the strain in the structure is calculated from the number of straight sections of optical fiber in the fiber optic strain gauge patch, the length of each such straight section, the strain sensitivity of the optical fiber, and the geometric factor.

33. The method of claim 31, wherein a plurality of fiber optic strain gauge patches monitoring the same plurality of regions are optically connected to the optical time domain reflectometer, and wherein the strain in the structure in each region is calculated from the time delay of pulses reflected from reflective markers in the fiber optic strain gauge patch mounted on that region.

34. The method of claim 31, wherein the wavelength of the light source ranges from about 700 nanometers to about 1600 nanometers.

35. The method of claim 31, wherein the carrier material is a composite material.

36. The method of claim 31, wherein the optical fiber is kept in its position using an adhesive.

37. The method of claim 31, wherein the carrier material is selected from one of epoxy, polyester, vinylester, polyphenylene sulfide, polycarbonate and nylon carrier materials.

38. The method of claim 31, wherein the carrier material is a thermoset material.

39. The method of claim 31, wherein the step of calculating the strain in the structure comprises obtaining the geometrical factor of the multiple loops of optical fiber by calibration.

40. The method of claim 31, wherein the optical fiber is a multi-mode fiber.

41. The method of claim 31, wherein the optical fiber is a single mode fiber.

42. A fiber optic strain gauge patch for installation in a composite material comprising:

(a) an optical fiber having a first end and a second end, disposed in loops onto a first layer of protective carrier material;

(b) a first reflective marker in the optical fiber in proximity to the first end of the optical fiber;

(c) a second reflective marker in the optical fiber in proximity to the second end of the optical fiber; and

(d) a second layer of protective carrier material disposed onto the optical fiber,

wherein the first and second layers of protective carrier material hold the optical fiber in position with respect to the first and second layers of protective carrier material, and

wherein the protective carrier material is selected such that the curing characteristics of the carrier material match the curing characteristics of the composite material sufficiently such that the carrier material can be cured as the composite material is cured.

43. The fiber optic strain gauge patch of claim 42, further comprising flexible protective cover placed over at least one of the first and the second ends of the optical fiber.

44. The fiber optic strain gauge patch of claim 42, wherein the first end of the optical fiber is routed outside of the fiber optic strain gauge patch, and the second end of the optical fiber is terminated within the fiber optic strain gauge patch.

45. The fiber optic strain gauge patch of claim 42, wherein the first layer of protective carrier material is selected such that it holds the optical fiber in position without the use of any adhesive.

46. The fiber optic strain gauge patch of claim 42, wherein the first layer of protective carrier material is a thermoset material.

47. The fiber optic strain gauge patch of claim 42, wherein the response of the optical fiber is characterized by a geometric factor.

48. The fiber optic strain gauge patch of claim 42, wherein the optical fiber is a multi-mode optical fiber.

49. The fiber optic strain gauge patch of claim 42, wherein the optical fiber is a single mode optical fiber.