Fiber optic sensor using a hollow core fiber

• US 8,233,151 B2
• Filed: 09/12/2011
• Issued: 07/31/2012
• Est. Priority Date: 08/20/2002
• Status: Expired due to Term

• Current Assignee: Board of Trustees of the Leland Stanford Junior University (Stanford University)
• Original Assignee: Board of Trustees of the Leland Stanford Junior University (Stanford University)
• Inventors: Digonnet, Michel J. F.
• Primary Examiner(s): Chowdhury, Tarifur
• Assistant Examiner(s): Hansen, Jonathan
• Application Number:
  US13/230,740
• Publication Number:
  US 20120062902A1
• Time in Patent Office: 323 Days
• Field of Search: 356/460
• US Class Current: 356/460
• CPC Class Codes: G01C 19/722 of the mechanical construction
• CPC Class Codes: G02B 6/02328 Hollow or gas filled core
• CPC Class Codes: G02B 6/02361 Longitudinal structures forming multiple layers around the core, e.g. arranged in multiple rings with each ring having longitudinal elements at substantially the same radial distance from the core, having rotational symmetry about the fibre axis

Abstract

An optical sensor includes at least a portion of an optical waveguide having a hollow core generally surrounded by a cladding. The cladding substantially confines a first optical signal and a second optical signal within the hollow core as the first optical signal and the second optical signal counterpropagate through the optical waveguide. Interference between the first optical signal and the second optical signal is responsive to perturbation of the at least a portion of the optical waveguide.

Claims

1. An optical sensor system comprising:

an optical coupler configured to split a first optical signal into a second optical signal and a third optical signal; and

an optical waveguide having a hollow core generally surrounded by a cladding, the optical waveguide receiving the second optical signal and the third optical signal, the cladding of the optical waveguide substantially confining the second optical signal and the third optical signal within the hollow core, wherein interference between the second optical signal and the third optical signal after the second optical signal and the third optical signal have counterpropagated through the optical waveguide is responsive to perturbation of at least a portion of the optical waveguide.

2. The optical sensor system of claim 1, further comprising a light source in optical communication with the optical coupler, the light source configured to emit the first optical signal.

3. The optical sensor system of claim 2, wherein the light source comprises a superfluorescent light source.

4. The optical sensor system of claim 3, wherein the superfluorescent light source comprises an erbium-doped superfluorescent fiber source.

5. The optical sensor system of claim 2, wherein the light source has a spectral distribution with a full width at half maximum of about 1 nanometer or larger.

6. The optical sensor system of claim 2, wherein the light source has a spectral distribution with a full width at half maximum of less than 1 nanometer.

7. The optical sensor system of claim 1, further comprising an optical detector in optical communication with the optical coupler, the optical detector receiving the second optical signal and the third optical signal after having counterpropagated through the optical waveguide.

8. The optical sensor system of claim 1, wherein the optical waveguide comprises a Bragg fiber.

9. The optical sensor system of claim 1, wherein the hollow core is gas-filled.

10. The optical sensor system of claim 1, wherein the hollow core is evacuated.

11. The optical sensor system of claim 1, wherein the hollow core comprises vacuum.

12. The optical sensor system of claim 1, wherein the hollow core comprises one or more gases.

13. The optical sensor system of claim 1, wherein the optical waveguide is a coil.

14. The optical sensor system of claim 13, wherein the coil is wound around a spool such that differential phase shifts due to asymmetric variations of the temperature of the coil with respect to a mid-point of the coil are reduced.

15. An optical sensor comprising at least a portion of an optical waveguide having a hollow core generally surrounded by a cladding, wherein the cladding substantially confines a first optical signal and a second optical signal within the hollow core as the first optical signal and the second optical signal counterpropagate through the at least a portion of the optical waveguide, wherein interference between the first optical signal and the second optical signal is responsive to perturbation of the at least a portion of the optical waveguide.

16. The optical sensor of claim 15, wherein the optical sensor comprises a Sagnac interferometer.

17. The optical sensor of claim 15, wherein the perturbation is selected from the group consisting of:

magnetic field, electric field, pressure, displacement, rotation, twisting, and bending applied to at least a portion of the optical waveguide.

18. The optical sensor of claim 15, further comprising a source of the first optical signal and the second optical signal.

19. The optical sensor of claim 18, wherein the source comprises a superfluorescent light source.

20. The optical sensor of claim 15, further comprising an optical detector configured to receive the first optical signal and the second optical signal after having counterpropagated through the optical waveguide.

21. The optical sensor of claim 15, wherein the hollow core is gas-filled.

22. The optical sensor of claim 15, wherein the hollow core is evacuated.

23. The optical sensor of claim 15, wherein the hollow core comprises vacuum.

24. A method for sensing a perturbation, the method comprising:

counterpropagating two portions of a light signal through an optical waveguide having a hollow core generally surrounded by a cladding;

optically interfering the two portions of the light signal after having counterpropagated through the optical waveguide, thereby producing an optical interference signal;

subjecting at least a portion of the optical waveguide to a perturbation; and

measuring variations in the optical interference signal caused by the perturbation.

25. The method of claim 24, wherein the perturbation is selected from the group consisting of:

magnetic field, electric field, pressure, displacement, rotation, twisting, and bending applied to at least a portion of the optical waveguide.

26. The method of claim 24, wherein the hollow core is gas-filled.

27. The method of claim 24, wherein the hollow core is evacuated.

28. The method of claim 24, wherein the hollow core comprises vacuum.