Crack growth measurement network with primary and shunt optical fibers

• US 5,142,141 A
• Filed: 09/19/1990
• Issued: 08/25/1992
• Est. Priority Date: 09/19/1990
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Biando, Gary J., Talat, Kausar
• Primary Examiner(s): Nelms, David C.
• Application Number:
  US07/585,003
• Time in Patent Office: 706 Days
• Field of Search: 250/227.11, 250/227.15, 250/227.18, 250/227.23, 340/550, 340/555, 73/800
• US Class Current: 250/227.15
• CPC Class Codes: G01M 11/085 the optical fiber being on or near the surface of the DUT
• CPC Class Codes: G01M 11/086 Details about the embedment of the optical fiber within the DUT

Abstract

A fiber optic crack propagation measurement apparatus including an input optical fiber for receiving light energy and an output optical fiber connected to deliver light energy to a detector is disclosed. A plurality of shunt optical fibers are connected in parallel between the input and output optical fibers. The input optical fibers, output optical fibers and shunt optical fibers are secured to a structure in which stresses are expected to cause the advancement of a crack. As the crack grows, individual shunt fibers are broken, reducing the amount of light energy delivered to the detector. Detector signals are generated indicative of the light energy received thereby to report the advancement of the crack. In one embodiment, wavelength division multiplexing techniques are employed so that multiple crack measuring units can be monitored over a single monitoring optical fiber.

Claims

1. An apparatus for optically measuring the propagation of a crack in a structure, comprising:

a substrate attachable to the structure in which the crack is expected to propagate;

a primary optical fiber attached to said substrate, said primary optical fiber having means for receiving light energy at a first end and means for delivery light energy at a second end; and

a shunt optical path optically connected to said primary optical fiber in optical parallel with a portion of said primary optical fiber so that as the crack propagates the shunt optical path will be stressed by crack propagation causing a change in the light energy available at the second end of the primary optical path.

2. The apparatus of claim 1 comprising a detector responsive to changes in the amount of light energy delivered to said second end for generating crack propagation signals.

3. The apparatus of claim 1 wherein said shunt optical path comprises a plurality of shunt optical fibers each optically connected to said primary optical fiber in optical parallel with said portion of said primary optical fiber and attached to said substrate in a predetermined spatial arrangement.

4. The apparatus of claim 1 wherein said shunt optical path comprises a plurality of shunt optical fibers optically connected to said primary optical fiber in optical parallel with said portion of said primary optical fiber and attached to said substrate in parallel spatially with said portion of said primary optical fiber.

5. The apparatus of claim 3 wherein each optical connection between said primary optical fiber an one of said shunt optical fibers is a fused optical coupling.

6. The apparatus of claim 3 wherein each of said shunt optical fibers is optically connected to said primary optical fiber to receive a unique portion of light energy conveyed by said primary optical fiber, the unique light energy portion connected to each shunt optical fiber being different than the unique portion connected to the others of said shunt optical fibers whereby each shunt fiber has a unique light energy signature discernible by said detector.

7. The apparatus of claim 3 wherein said detector comprises means for generating a system integrity failure signal when the amount of light energy received by said detector from said primary optical fiber is below a predetermined amount.

13. The apparatus of claim 7 wherein said attaching means attaches said shunt optical fibers to said structure in lines parallel with one another and spaced apart by predetermined distances.

8. An apparatus for measuring the propagation of a crack in a structure, comprising:

an input optical fiber for receiving light energy;

an output optical fiber for delivering light energy to a detector;

a plurality of shunt optical fibers, each shunt optical fiber having a first end optically connected to receive light energy from said input optical fiber and having a second end optically connected to deliver light energy received from said input optical fiber to said output optical fiber;

means for attaching said shunt optical fibers to said structure in a predetermined spatial pattern in an area of potential structural stress; and

said detector comprising means responsive to the amount of light energy received from said output optical fiber for detecting the propagation of a crack in the area of potential structural stress.

9. The apparatus of claim 8 comprising a substrate to which said input optical fiber, said output optical fiber and said shunt optical fibers are attached and said attachment means comprises means for attaching said substrate to said structure.

10. The apparatus of claim 8 wherein each optical connection between said shunt optical fibers and said input and output optical fibers is a fused optical coupling.

11. The apparatus of claim 10 wherein each of said shunt optical fibers is optically connected by one of said fused optical couplings to receive a unique portion of the light energy conveyed by said input optical fiber whereby each of said shunt optical fibers has a unique signature discernible by said detector.

12. The apparatus of claim 8 wherein said detector comprises means for generating a system integrity failure signal when the amount of light energy received by said detector from said output optical fiber is below a predetermined amount.

14. An apparatus for measuring the propagation of a crack in a structure, comprising:

a stress sensing optical fiber means embedded in said structure in a predetermined spatial pattern, said stress sensing means comprising an input optical fiber, an output optical fiber, and a plurality of shunt path optical fibers, each shunt path optical fiber having a first end optically connected to receive light energy from said input optical fiber and having a second end optically connected to deliver light energy received from said input optical fiber to said output optical fiber;

connecting means for connecting light energy to said input optical fiber and for connecting light energy from said output optical fiber to a detector; and

said detector comprising means responsive to the amount of light energy received from said output optical fiber for detecting the propagation of a crack in said structure.

15. The apparatus of claim 14 further comprising at least one flexible, hollow tube for receiving at least one of said input optical fiber and said output optical fiber, said tube extending from a first end embedded in said structure to a second end outside of said structure.

16. An optical system for measuring crack propagation in a structure, comprising:

a plurality of crack propagation measuring means each having an input optical fiber for receiving input light energy, an output optical fiber and a shunt optical path for conveying from said input optical fiber to said output optical fiber an amount of light energy indicative of the propagation of a crack in said structure;

a monitoring fiber optically connected to the output optical fibers of each of said plurality of crack propagation measuring means for receiving light energy conveyed thereby;

optical source means for coupling an individual one of a plurality of optically distinctive light energy signals to each of said input optical fibers; and

detection means connected to receive light energy signals from said monitoring fiber for separately detecting changes in the amount of light energy of each of said optically distinctive light energy signals and for generating signals representing such changes in detected light energy.

17. The apparatus of claim 16 wherein said optical source means comprises means for coupling optically distinctive light energy signals each having a different one of a plurality of wavelengths to each of said input optical fibers, and said detection means comprises means for separating received light energy by wavelength, and means for detecting changes in the amount of light energy received at each of said plurality of wavelengths.

18. The apparatus of claim 16 wherein the shunt optical path of each of said plurality of crack propagation measuring means comprises a plurality of shunt optical fibers, each shunt optical fiber having a first end optically connected to receive light from said input optical fiber and having a second end optically connected to deliver light energy received from said input optical fiber to said output optical fiber.

19. The apparatus of claim 16 wherein said shunt optical path of each of said plurality of crack measuring means comprises a plurality of shunt optical fibers optically connected in parallel between said input optical fiber and said output optical fiber and attached to said structure in lines parallel with one another and spaced apart by predetermined distances.

20. The apparatus of claim 18 comprising means for attaching said input optical fiber, said output optical fiber and said shunt path fibers to said structure in an area of potential structural stress.

21. An optical system for measuring crack propagation in a structure, comprising:

a plurality of crack propagation measuring means each having an input optical fiber for receiving input light energy, an output optical fiber and a shunt optical path for conveying from said input optical fiber to said output optical fiber, an amount of light energy indicative of the propagation of a crack in said structure;

a monitoring fiber optically connected to the output optical fibers of each of said plurality of crack propagation measuring means for receiving light energy conveyed thereby;

optical source means for coupling distinctive light energy signals to each of said input fibers; and

detection means connected to receive said distinctive light energy signals from said monitoring fiber, for separately detecting changes in the amount of light energy in each of said received distinctive light energy signals and for generating signals representing such changes in detected light energy.

22. A method of optically measuring the propagation of a crack in a structure, said method comprising:

attaching a plurality of crack detection fibers to said structure in an area of anticipated crack propagation;

optically connecting each of said crack detection fibers to an input optical fiber;

optically connecting each of said crack detection fibers to an output optical fiber;

applying optical energy to said input optical fiber; and

detecting reductions in the amount of optical energy conveyed by said output optical fiber to measure crack propagation.

23. The method of claim 22 wherein said attaching step comprises attaching said plurality of crack detection fibers to said structure in a predetermined spatial pattern.

24. The method of claim 22 wherein said attaching step comprises attaching said plurality of crack detection fibers to a substrate in a predetermined spatial pattern and attaching said substrate to said structure.

25. The method of claim 23 wherein the step of optically connecting said crack detection fibers to said input optical fiber comprises connecting each of said crack detection fibers to said input optical fiber such that each of said crack detection fibers receives a unique amount of light energy from said input optical fiber, the unique light energy amount connected to each crack detection fiber being different than the unique amount connected to the others of said crack detection fibers whereby each of said crack detection fibers has a unique light energy signature.

26. The method of claim 25 wherein said detecting step comprises identifying the breakage of one of said crack detection fibers from a reduction in the amount of optical energy conveyed by said output optical fiber substantially equal to the unique optical energy signature of said one crack detection fiber.