Composite structures, such as coated wiring assemblies, having integral fiber optic-based condition detectors and systems which employ the same

• US 7,154,081 B1
• Filed: 11/25/2003
• Issued: 12/26/2006
• Est. Priority Date: 11/26/2002
• Status: Expired due to Fees

• Current Assignee: Luna Innovations, Inc.
• Original Assignee: Luna Innovations, Inc.
• Inventors: Wavering, Thomas A., Friedersdorf, Fritz
• Primary Examiner(s): Allen, Stephone B.
• Assistant Examiner(s): Lee, Patrick J.
• Application Number:
  US10/720,694
• Time in Patent Office: 1,127 Days
• Field of Search: 250/227.14, 250/227.16, 385/10, 385/12, 385/13, 385/37, 385/73.1
• US Class Current: 250/227.14
• CPC Class Codes: D07B 1/145 comprising elements for indicating or detecting the rope or cable status
• CPC Class Codes: D07B 2301/5577 using light guides
• CPC Class Codes: G01B 11/18 using photoelastic elements
• CPC Class Codes: G01M 11/086 Details about the embedment of the optical fiber within the DUT
• CPC Class Codes: G02B 6/022 using mechanical stress, e.g. tuning by compression or elongation, special geometrical shapes such as "dog-bone" or taper G02B6/02204 takes precedence; optical modulation using photo-elastic effect G02F1/0131
• CPC Class Codes: G02B 6/02204 using thermal effects, e.g. heating or cooling of a temperature sensitive mounting body optical modulation using thermo-optic effect G02F1/0147

Abstract

Integral fiber optic-based condition sensors detect conditions of a composite structure, e.g., a coated wire assembly so as to detect damage or conditions that may damage the same. Preferably, at least one optical fiber sensor having a plurality of Bragg gratings written into the fiber at spaced-apart locations along its axial length is integrated into the electrical insulator coating of a wire, wire bundle or wiring harness. The fiber optic sensor may thus be employed to measure the environmental loads on the electrical wiring including stresses from bending, axial loading, pinch points, high temperature excursions and chemical damage. The system is capable of detecting and locating transient conditions that might cause damage to a wiring system or permanent changes in state associated with damage events. The residual stress in the electrical insulator coating of a wire, wire bundle, or wiring harness are used to monitor the evolution of damage by wear or chaffing processes. Detected stress relief on one or more Bragg gratings will thus be indicative of damage to the insulator coating on the conductor. As such, the magnitude of such stress relief may be detected and used as an alert that the wire insulation is damaged to an unsafe extent.

Claims

1. A composite structure comprising:

a coated element, and

at least one fiber optic condition sensor embedded physically within a coating of said coated element, wherein

the at least one fiber optic condition sensor exhibits an initial wavelength at a zero state prior to being embedded physically within the coating, and wherein

each of the coating and the at least one fiber optic condition sensor has a coefficient of thermal expansion (CTE) which is sufficiently different from one another so as to induce compressive stress on the at least one fiber optic condition sensor to achieve a wavelength change thereof during a normal state which is greater than about 0.1 nm relative to the initial wavelength of the at least one fiber optic condition sensor at the zero state to thereby achieve a predetermined strain characteristic which is responsive to a selected condition of the composite structure to be sensed, and wherein

said sensor detects a change in the predetermined strain characteristic which is indicative of the condition of said composite structure during an abnormal condition due to the induced compressive stress achieved by the different CTE of the coating and the sensor.

2. The structure of claim 1, wherein said coating is a polymeric coating, and wherein said element is an electrical conductor, and wherein the polymeric coating and the at least one fiber optic condition sensor have different coefficients of thermal expansion so as to impart said predetermined strain characteristic.

3. The structure of claim 1 or 2, wherein said at least one fiber optic condition sensor comprises a series of axially spaced apart Bragg gratings written therein.

4. The structure of claim 1, comprising a plurality of said fiber optic condition sensors each embedded in said coating.

5. The structure of claim 4, wherein each of said fiber optic condition sensors comprises a series of axially spaced apart Bragg gratings written therein.

6. The structure of claim 4 or 5, wherein at least one of said fiber optic condition sensors detects the change in the strain characteristic so as to sense a condition of the structure other than a temperature condition, and wherein at least one other fiber optic sensor detects a temperature condition of said structure.

7. The structure of claim 1, wherein the coating is a magnetorestrictive coating, and wherein said at least one fiber optic condition sensor detects a change in the strain characteristic in response to the presence of the structure in a magnetic field.

8. A condition detection system comprising:

a composite structure comprised of a coated element, and at least one fiber optic condition sensor embedded physically within a coating of said coated element, wherein the at least one fiber optic condition sensor exhibits an initial wavelength at a zero state prior to being embedded physically within the coating, and wherein each of the coating and the at least one fiber optic condition sensor has a coefficient of thermal expansion (CTE) which is sufficiently different from one another so as to induce compressive stress on the at least one fiber optic condition sensor to achieve a wavelength change thereof during a normal state which is greater than about 0.1 nm relative to the initial wavelength of the at least one fiber optic condition sensor at the zero state to thereby achieve a predetermined strain characteristic which is responsive to a selected condition of the composite structure to be sensed, and wherein said sensor detects a change in the predetermined strain characteristic which is indicative of the condition of said composite structure during an abnormal condition due to the induced compressive stress achieved by the different CTE of the coating and the sensor,

a data acquisition system operatively connected to said fiber optic sensor for outputting a signal indicative of the change in the predetermined strain characteristic of the at least one fiber optic condition sensor, and

a monitor for receiving the signal and providing an indication of said predetermined condition.

9. The system of claim 8, wherein said monitor provides a visual and/or aural indication of said predetermined condition.

10. The system of claim 8, wherein said monitor stores data associated with said predetermined condition.

11. A wire assembly having integral condition detection capabilities, comprising:

a wire element which includes at least one electrical conductor;

an electrical insulator formed of a polymeric material surrounding said wire element; and

a fiber optic condition sensor in operative association with said electrical insulator to detect a selected condition of said wire assembly, wherein

the fiber optic condition sensor exhibits a predetermined strain characteristic which is responsive to the selected condition of the wire assembly to be detected, and wherein

the fiber optic condition sensor detects a change in the predetermined strain characteristic which is indicative of the selected sensed condition of said wire assembly; and

wherein

the fiber optic condition sensor exhibits an initial wavelength at a zero state prior to being operatively associated with the electrical insulator, and wherein

each of the electrical insulation and the fiber optic condition sensor has a coefficient of thermal expansion (CTE) which is sufficiently different from one another so as to induce compressive stress on the fiber optic condition sensor to achieve a wavelength change thereof during a normal state which is greater than about 0.1 nm relative to the initial wavelength of the fiber optic condition sensor at the zero state to thereby achieve the predetermined strain characteristic which is responsive to the selected condition of the wire assembly to be detected, and wherein

the sensor detects a change in the predetermined strain characteristic which is indicative of the condition of the wire assembly during an abnormal condition due to the induced compressive stress achieved by the different CTE of the electrical insulation and the sensor.

12. The wire assembly as in claim 11, wherein said fiber optic condition sensor is embedded physically within said electrical insulator.

13. The wire assembly as in claim 11, wherein said wire element includes a plurality of electrical conductors, and wherein said fiber optic condition sensor is associated physically with said plurality of electrical conductors so as to be surrounded by said electrical insulator.

14. The wire assembly of claim 11, comprising a plurality of fiber optic condition sensors each in operative association with said electrical insulator and each having a series of axially spaced apart Bragg gratings written therein for detecting the change in the predetermined strain characteristic indicative of the selected sensed condition of the wire assembly.

15. The wire assembly of claim 11, wherein the fiber optic condition sensor is oriented substantially parallel to or spirally wound around the electrical conductor.

16. The wire assembly of claim 11, wherein the polymeric material is extruded as a coating onto the electrical conductor.

17. The wire assembly of claim 11, wherein the polymeric material is a heat-shrunk tube, tape wrap or woven sleeve.

18. The wire assembly of claim 11, wherein the polymeric material is a polyolefin, polytetrafluoroethylene, fluorinated ethylene propylene, polyvinylidene fluoride, ethylene-tetrafluoroethylene, or polyimide.

19. The wire assembly of claim 18, wherein the polymeric material is a heat shrunk tube, tape wrap or woven sleeve.

20. An insulation wear detector system comprising:

a wire assembly comprising a wire element which includes at least one electrical conductor;

an electrical insulator formed of a polymeric material surrounding said wire element; and

a fiber optic condition sensor in operative association with said electrical insulator, wherein the fiber optic condition sensor exhibits a predetermined strain characteristic which is responsive to a wear condition of the electrical insulator, and wherein the fiber optic condition sensor detects a change in the predetermined strain characteristic which is indicative of the wear condition of said electrical insulator;

a data acquisition system operatively connected to said fiber optic sensor for outputting a signal indicative of a change in the predetermined strain characteristic of the fiber optic sensor, and

a monitor for receiving the signal and providing an indication of the wear condition of the electrical insulator;

wherein

the fiber optic condition sensor exhibits an initial wavelength at a zero state prior to being operatively associated with the electrical insulator, and wherein

each of the electrical insulation and the fiber optic condition sensor has a coefficient of thermal expansion (CTE) which is sufficiently different from one another so as to induce compressive stress on the fiber optic condition sensor to achieve a wavelength change thereof during a normal state which is greater than about 0.1 nm relative to the initial wavelength of the fiber optic condition sensor at the zero state to thereby achieve the predetermined strain characteristic which is responsive to the selected condition of the wire assembly to be detected, and wherein

the sensor detects a change in the predetermined strain characteristic which is indicative of the condition of the wire assembly during an abnormal condition due to the induced compressive stress achieved by the different CTE of the electrical insulation and the sensor.

21. The system of claim 20, wherein said monitor provides a visual and/or aural indication of said predetermined change in strain.

22. The system of claim 20, further comprising at least one other said fiber optic condition sensor for detecting a temperature condition of the wire assembly and for outputting a temperature signal indicative of the temperature condition of the wire assembly.

23. The system of claim 22, wherein the data acquisition system receives the temperature signal and compares the temperature signal to the signal indicative of the wear condition of the electrical insulator.

24. A magnetic field strength sensor assembly comprising:

a magnetorestrictive coating material, and

at least one fiber optic condition sensor associated physically with the magnetorestrictive coating material, wherein the at least one fiber optic condition sensor exhibits an initial wavelength at a zero state prior to being associated physically with the magnetorestrictive coating material, and wherein

each of the magneto restrictive coating material and the at least one fiber optic condition sensor has a coefficient of thermal expansion (CTE) which is sufficiently different from one another so as to induce compressive stress on the at least one fiber optic condition sensor to achieve a wavelength chance thereof during a normal state which is greater than about 0.1 nm relative to the initial wavelength of the at least one fiber optic condition sensor at the zero state to thereby achieve a predetermined strain characteristic which is responsive to exposure to a magnetic field, the magnetorestrictive coating material thereby inducing a strain characteristic on the at least one fiber optic condition sensor in response to exposure to the magnetic field such that the sensor detects the strain characteristic which is indicative of magnetic field strength.

25. A system for detecting magnetic field strength comprising a sensor assembly as in claim 24, a data acquisition system operatively connected to said fiber optic sensor for outputting a signal indicative of the detected strain characteristic induced by the magnetic field, and a monitor for receiving the signal and providing an indication of magnetic field strength.