Damage evaluation system and method using optical fibers

• US 4,936,649 A
• Filed: 01/25/1989
• Issued: 06/26/1990
• Est. Priority Date: 01/25/1989
• Status: Expired due to Term

• Current Assignee: University of Toronto Innovations Foundation
• Original Assignee: University of Toronto Innovations Foundation
• Inventors: Tennyson, Roderick C., Measures, Raymond M., Lymer, John D., Glossop, Neil D. W., Hogg, W. Dayle
• Primary Examiner(s): Sikes, William L.
• Assistant Examiner(s): HEALY, BRIAN
• Application Number:
  US07/301,294
• Time in Patent Office: 517 Days
• Field of Search: 350/320, 350/96.10, 350/96.15, 350/96.19, 350/96.20, 350/96.29, 350/96.30, 350/96.33, 250/227, 156/625, 156/632, 156/158, 65/3.1, 65/3.11, 65/4.1, 65/4.2, 65/4.3, 65/31, 219/121.68
• US Class Current: 385/13
• CPC Class Codes: G01M 11/086 Details about the embedment of the optical fiber within the DUT
• CPC Class Codes: G01M 5/0091 by using electromagnetic excitation or detection
• CPC Class Codes: G01V 8/24 using optical fibres
• CPC Class Codes: G02B 6/00 Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
• CPC Class Codes: G02B 6/3502 involving direct waveguide displacement, e.g. cantilever type waveguide displacement involving waveguide bending, or displacing an interposed waveguide between stationary waveguides
• CPC Class Codes: G02B 6/3536 involving evanescent coupling variation, e.g. by a moving element such as a membrane which changes the effective refractive index mode converters G02B6/14; adjustable lateral coupling between waveguides G02B6/283; electro- optical refractive index variations G02F1/0118

Abstract

A damage detection and evaluation system utilizes optical fibers to detect and assess damage to a structure. The optical fibers are intermittently etched in a controlled manner to weaken them so they fracture when a desired load is applied to the structure. Where visual inspection of the optical fibers is used to check for damage, a reference set of optical fibers is used. Where photodetection is used and minimal connections to the structure are required, one end of the optical fiber is made reflecting so an optical connection is only made to the other end. To further simplify the connection, a single input/output optical connection to a demultiplexing/multiplexing chip mounted on or within the structure is provided. Where orthogonal grids of fibers are not possible, the invention provides interdigitated optical fibers and volume backscattering to locate the position of the first fracture along the length of the optical fiber. The entire periphery of a damaged area can then be determined with a set of such interdigitated optical fibers. Again, a single optical interface to the structure can be provided using a demultiplexing/multiplexing chip. In the case of composite materials, the optical fibers are located between specified plys and at a specified orientation for optimum sensitivity.

Claims

1. A method of treating optical fibers to alter the fracture strength of the optical fibers, for use in a DESIFOR system, the method comprising:

(a) applying a protective coating to a plurality of first, selected parts of an optical fiber;

3. A method as claimed in claim 1, wherein at least one portion of the optical fiber, having a length substantially greater than the length of each of the first and second parts, is coated with the protective coating, so as to be left unetched.

4. A method as claimed in claim 1, wherein the optical fiber initially includes an original protective jacket, and wherein the protective jacket is removed, before step (a).

6. A method as claimed in claim 1,. 3 or 4, wherein the etchant comprises a liquid acid.

8. A method b as claimed in claim 1, wherein the etching is effected by one of a laser and flash heating.

48. A method as claimed in claim 1 or 7, wherein the transitional parts are formed with a generally frusto-conical shape.

50. A method as claimed in claim 1 or 2, wherein after step (b) the protective coating is removed.

52. A damage evaluation system as claimed in claim 50, in combination with an object comprising a fiber reinforced composite material, which comprises a plurality of layers of reinforcing fibers and a polymer binding the reinforcing fibers together, with the optical fibers bound to the composite material by the polymer.

53. A damage evaluation system as claimed in claim 50 or 51, wherein the transitional parts are sufficiently abrupt to form said substantial stress concentrations.

54. A damage evaluation system as claimed in claim 50 or 51, wherein the transition parts are such as to include at least one of minor perturbations and cracking of the surfaces of the damage sensing portions to give a desired reduction in the fracture strength of the ptical fibers.

55. A damage evaluation system as claimed in claim 50 or 51, wherein the transition parts are generally frustro-conical.

56. A damage evaluation system as claimed in claim 50 or 51, wherein the composite material has a surface which is subject to the greatest tensile load, and wherein the optical fibers are located adjaacent to said surface subject to the greatest tensile load and are oriented to extend transversely across cracks commencing between reinforcing fibers adjacent said surface.

57. A damage evaluataion system as claimed in claim 50 or 51, wherein the optical fibers comprise a first group of optical fibers which extends across one edge of a pre-determined area to a generally opposite edge of the pre-determined area, and a second group of optical fibers which extend across said second, generally opposite edge to said one edge and which are intidigitated with the first group of optical fibers.

58. A damage evaluataion system as claimed in claim 50 or 51, wherein the optical fibers comprise volume backscattering optical fibers.

59. A damage evaluation system as claimed in claim 50 or 51, wherein, for eachoptical fiber, there is provided a light source, a directional coupler coupling the light source to the respective optical fiber, a reference photodetector connected to the directional coupler for detecting the magnitude of light transmitted to the optical fiber from the light source, and a return signal photodetector connected to the directional coupler for detecting the returned light emitted from the optical fiber.

60. A damage evaluation system as claimed in claim 50 or 5I, which includes a light source, a directional coupler having an input connected to the light source and an output, a DMD which is connected to the optical fibers and to the directional coupler, a reference photodetector connected to the directional coupler for detecting the magnitude of light transmitted to the DMD, and a return signaI photodetector connected to the directionaI coupler for sensing the magnitude of the return light from an optical fiber transmitted through the DMD, whereby the light source and the DMD operate together to illuminate the optical fibers individually and successively, and the DMD and the return signal photodetector operate to interrogate the optical fibers individually and successively.

61. A damage evaluation systemn as claimed in claim 50 or 51, wherein for the sensing portion of each optical fiber, the first and second parts are of generally similara length to one another, with the transition parts being substantially shorter than the first and second parts.

2. (b) subjecting the optical fiber to an etchant, to etch a plurality of second parts of the optical rfiber which are not protected, to produce second parts of reduced external diameter whilst leaving the first parts with the diameter of the optical fiber prior to etching, the etching being carried out so as to form transitional parts, between the first and second parts, which are such as to provide substantial stress concentrations and sufficiently weaken the optical fiber to, reduce the fracture strength of the optical fiber

5. A method as claimed in claim 2, wherein the optical fiber initially includes an original protective jacket, which, with the exception of the portion of the protective jacket covering said one portion of the optical fiber, is removed before carrying out step (a).

7. A method as claimed in claim 5, wherein the optical fiber is immersed in the liquid acid for a predetermined time to give a predetermined reduction in the diameter of the second parts, to give a desired damage sensitivity.

9. A method as claimed in claim 7, wherein the optical fiber initially has a protective jacket, which is removed before effecting the etching or weakening to the second parts thereof.

11. A composite material as claimed in claim 9, wherein the composite material is formed into a component having a surface which is subject to the greatest tensile load, and wherein the optical fibers and said two adjacent layers are located adjacent said surface having the greatest tensile load.

15. A composite material as claimed in claim 9, wherein each optical fiber includes a damage sensing portion, which comprises first and second parts alternating with one another and transition parts extending between the first and second parats, with the second parts having a reduced diameter relative the first parts so as to provide substantial stress concentrations and sufficiently weaken the optical fiber to reduce the fracture strength of the optical fibers, the diameter of the second parts is selected to give a desired degree of damage sensitivity, and the transition parts are generally frustro-conical and such as to lock the damage sensing portions into the polymer.

20. A composite material as claimed in claim 9, wherein the optical fibers are volume backscattering optical fibers.

22. A composite material as claimed in claim 20, which is formed into a component having a surface, which is subject to the greatest tensile load, and wherein the two layers of reinforcing fibers and the optical fibers are located adjacent said surface having the greatest tensile load.

25. A composite material as claimed in claim 22 or 23, which is formed as a component having a surface, which is subject to the greatest tensile load, and wherein the optical fibers and said two layers of reinforcing fibers are located adjacent said surface, having the greatest tensile load.

26. A composite material as claimed in claim 9, wherein each optical fiber has one end adapted for connection to a light source and a photodetector, and another end which is highly reflecting.

27. A composite material as claimed in claim 25, wherein the optical fibers are arranged in a grid, with a first group of fibers extending in one direction and a second group of fibers extending in another direction and intersecting the first group of fibers, wherein the two groups of fibers are sufficiently spaced to avoid excessive microbend loss and damage to the fibers.

31. A composite material as claimed in claim 27, wherein each of the optical fibers includes a portion, which comprises first and second parts alternating with one another, with each second part having a smaller diameter than the first parts to reduce the fracture strength of the optical fibers, the diameter of the second parts being selected to give a desired damage sensitivity.

36. A composite material as claimed in claim 9, wherein each damage sensing optical fiber includes a first end mounted for receiving illumination and a second end mounted for visual inspection, and which includes a plurality of reference optical fibers each of which includes a first end for receiving illumination and a second end for providing a reference light point, each second end of the reference optical fibers being associated and located adjacent a second end of a respective first-mentioned optical fiber.

38. A composite material as claimed in claim 36, which is formed as a component with a surface, which is subject to the greatest tensile load, and wheerein the optical fibers and said two layers of reinforcing fibers are located adjacent said surface having the gratest tensile load.

10. A fiber reinforced composite material, which comprises:

a plurality of layers of reinforcing fibers, with the reinforcing each two adjacent layers extending in one direction within that layer, and a polymer binding the reinforcing fibers together;

a plurality of damage sensing optical fibers extending generally parallel to one another and spaced apart from one another between said two layers of reinforcing fibers with the optical fibers extending at the largest possible angle relative to the reinforcing fibers of each of said two layers, and with the angle between the optical fibers and the reinforcing fibers of one of said two layers being substantiall,y equal to the angle between the optical fibers and the reinforcing fibers of the other of said two layers.

12. A composite material as claimed in claim 10, wherein the number of layers of reinforcing fibers is less than or equal to 16, and which does not include any substantial reinforcement on the rear surface therof, whereby the material is free to flex.

13. A composite material as claimed in claim 9 or 10, wherein the two adjacent layers of reinforcing fibers are parallel to one another and the optical fibers are substantially perpendicular to those layers of reinforcing fibers.

14. a composite materiaI as claim 9, 10 or 11, wherein each optical fiber, includes a damage sensing portion which comprises first and second parts alternating witb one another, with the second parts having a reduced diameter relative to the first parts so as to provide substantial stress concentrations and sufficiently weaken the optical fiber to reduoe the fracture strength of the optical fibers, the diameter of the second parts being selected, to give a desired damage sensitivity.

16. A composite material as claimed in claim 14, wherein the transition parts are such as to provide stress concentrations, giving a desired local increase in the loading on the damage sensing portions.

33. A composite material as claimed in claim 9 or 10, which includes a light source, a directional coupler having an input connected to the light source and an output, a DMD connected to the output of the directional coupler and connected to the optical fibers, a reference photodetector connncted to the directional coupler for detecting the magnitude of the light from the light source, and a return signal photodetector connected to the directional coupler, for determining the magnitude of the return light from an individual optical fiber, the light source and the DMD operating together to illuminate the optical fibers individually and successively, and the DMD and the return signal photodetector operating to interrogate the optical fibers individually and successively.

35. A composite material as claimed in claim 33, wherein each optical fiber is a volume backscattering optical fiber, and the directional coupler is an asymmetric coupler, which couples the majority of the light backscattered from each individual optical fiber to the return signal photodetector and the majority of the light from the light source to each optical fiber in turn, and wherein the optical fibers comprise first and second groups of fibers extending across a predetermined area, with the first group of fibers extending across one edge of the predetermined area to another, generally opposite edge thereof, and with the second group of fibers extending across said another edge to said one edge, the first and second groups of fibers being interdigitated with one another.

17. A composite material as claimed inclaim 14 or 15 wherein the transition parts are such as to provide minor perturbations and/or cracking of the surfaces of the damage sensing portions, to give a desired reduction in the fracture strength of the damage sensing portions.

19. A composite material as claimed in claim 17, wherein the composite material is formed into a component having a surface which is subject to the greatest tensile load, and wherein the optical fibers and said two layers are located adjacent said surface having the greatest tensile load.

23. A composite material as claimed in claim 19, wherein the first and second groups of optical fibers extend across a predetermined area, with the first group of optical fibers extending across one edge of the predetermined area to another, generally opposite edge of the predetermined area, and with the second group of optical fibers extending across said opposite edge to said one edge, and being interdigitated with the first group of optical fibers.

24. A composite material as claimed in claim 17, wherein the optical fibers comprise volume backscattering optical fibers, and the first and second groups of optical fibersi extend across a predetermined area, with the first group of optical fibers extending across one edge of the predetermined area to another, generally opposite edge of the predetermined area, and with the second group of optical fibers extending across said opposite edge to said one edge, and being interdigitated with the first group of optical fibers.

28. A composite material as claimed in claim 19, 20, 22 or 25, wherein, for each optical fiber, there is provided a light source, a directional coupler coupling the light source to the respective optical fiber, a reference photodetector connected to the directional coupler for detecting the magnitude of light transmitted to the optical fiber from the light source, and a return signal photodetector connected to the directional coupler for detecting the returned light emitted from the optical fiber.

29. A composite material as claimed in claim 19, 20, 22 or 25, which comprises a light source, a directional coupler having an input connected to the light source and an output, a DMD which is connected to the optical fibers and to the directional coupler, a reference photodetector connected to the directional coupler for detecting the magnitude of light transmitted to the DMD, and a return signal photodetector connected to the directional coupler for sensing the magnitude of the return light from an optical fiber through the DMD, whereby the light source and the DMD operate together to illuminate the optical fibers individually and successively, and the. DMD and the return signal photodetector operate to interrogate the optical fibers individually and successively.

30. A composite material as claimed in claim 19, 20, 22 or 25, wherein each of the optical fibers includes a portion, which comprises first and second parts alternating with one another, with each second part having a smaller diameter than the first parts, the diameter of the second parts being selected to give a desired damage sensitivity.

32. A composite material as claimed in claim 28, wherein each of the optical fibers includes a portion, which comprises first and second parts alternating with one another, with each second part having a smaller diameter than the first parts to reduce the fracture strength of the optical fibers, the diameter of the second parts being selected to give a desired damage sensitivity.

34. A composite material as claimed in claim 32, wherein each of the optical fibers includes a portion which comprises first and second parts alternating with one another, with each second part having a smaller diameter than the first parts, the diameter of the second parts being selected to give the desired damage sensitivity.

18. A fiber reinforced composite material, which comprises:

a plurality of layers of reinforcing fibers, with the reinforcing fibers of each of two adjacent layers extending in one within that layer, and with the reinforcing fibers of the two layers being at an angle to one another, and a polymer binding the reinforcing fibers together;

a plurality of optical fibers extending generally parallel to one another and spaced apart from one another between said two layers, with the optical fibers extending perpendicularly to the reinforcing fibers of one of said two layers.

21. A fiber reinforced composite material, which comprises:

a plurality of layers of reinforcing fibers, and a polymer binding the layers of reinforcing fibers together;

a plurality of volume backscattering optical fibers located between two adjacent layers of reinforcing fibers and extending across a predetermined area, with the optical fibers comprising a first group of optical fibers which extend across one edge of a predetermined area to a second, generally opposite edge of the predetermined area, and a second group of optical fibers which extend across said second, generally opposite edge to said one edge and which are interdigitated with the first group optical fibers.

37. A fiber reinforced composite material which comprises:

a plurality of layers of reinforcing fibers and a polymer binding the reinforcing fibers together;

a plurality of optical fibers extending between two adjacent layers of reinforcing fibers and across a predetermined area for detecting damage therein;

a light source, a directional coupler having an input connected to the light source and an output, a DMD connected to the output of the directional coupler and to each of the optical fibers, a reference photodetector magnitude of the light from the light source, and a return signal photodetector connected to the directiona-4 coupler, for detecting the magnitude of return light back from each optical fiber, the light source and the DMD operating together to illuminate each of the optical fibers individually and successively, and the DMD and the return signal photodetector operating together to interrogate .the optical fibers individually and successively.

39. A fiber reinforced composite material which comprises:

a pIuralityof layers of reinforcing fibers and a polymeer binding the reinforcing fibers together;

a pluralityof volume backscattering optical fibers extending, spaced apart from one another between two adjacent layers of reinforcing fibesrs, each optical fibesr including a damage sensing portion comprising a plurality of first parts, a plurality of second parts having a smaller diameter than the diameter of the first parts and alternating therewith, ad a plurality of transition parts extending between the first and second parts, the transition parts being such as to provide substantial stress concentrations and sufficiently weaken the optical fibers to give the optical fibers a reduced fracture strength relative to optical fibers of uniform diameter and similar material, and the transition parts locking the optical fibers to the composite material, whereby the optical fibers are subjected to the same strain as the compoeite mterial;

illumination and interrogation means connected to both ends of each optical fiber, for alternately illuminating each end of each optical fiber, to determine the location of a fracture of the optical fiber.

41. An optical fiber as claimed in claim 39, wherein a portion of the optical fiber, with a length considerably greater than each of the first parts, has a uniform diameter equal to the diameter of the first parts.

42. An optical fiber as claimed in claim 39 or 40, wherein some of the second parts have one second diameter, and others of the second parts have another second diameter different from said one second diameter.

44. A method as claimed in claim 42, wherein the pins are frictionally mounted in bores in the support surface, whereby during step (c), the pins are depressed until they are flush with the support surface.

40. An optical fiber which includes, a damage sensing portion comprising a plurality of first parts, a plurality of second parts having a smaller diameter than the diameter of the first parts and alternating therewith, and a pIurality of transition parts extending between the first and second parts, the transition parts being such as to provide substantial stress concentrations and sufficiently weaken the optical fibers to give the optical fibers a reduced fracture strength relative to optical fibers of uniform diameter and similar material, and the transition parts being capable of locking the optical fibers to an object, whereby the optical fibers are subjected to the same strain as the object.

43. A method of mounting optical fibers in a composite material, the method comprising:

(a) providing a support surface with a plurality of pins defining the desired pattern for the optical fibers;

(b) positioning optical fibers around the pins in the desired pattern;

(c) placing a sheet with an adhesive surface onto the optical fibers, whereby the optical fibers adhere to the sheet;

(d) removing the sheet with the optical fibers adhered thereto.

45. A method as claimed in claim 43, wherein after step (d), the sheet bearing the optical fibers is placed in a mold and laminated with other layers of reinforcing fibers to form a composite material with the optical fibers embedded therein.

46. A method as claimed in claim 43 or 44, wherein said sheet comprises a sheet of resin.

47. A method as claimed in claim 43 or 44, wherein said sheet comprises a pre-impregnated layer of reinforcing fibers.

49. A method as claimed in claim 47, wherein the etching is such as to form an uneven surface on the transitional parts, relative to the surfaces of the first and second parts.

51. A damage evaluation system for anobject, the damage evaluation system comprising a plurality of damage sensing optical fibers for bonding to the object, each of which optical fibers includes a damage sensing portion oomprising a plurality of first parts, a pluralityof second parts having a smaller diameter than the diameter of the first parts and alternating therewith, and a plurality of transition parats extending between the first and second parts, the transition parts being such as to provide substantial stress concentrations and sufficiently weaken the optical fibers, to give the optical fibers a reduced fracture strength relative to optical fibers of uniform diameter and similar material, and the transition parts being capable of locking the optical fibers to the object, whereby the optical fibers are subjected to the same strain as the object.