Intrusion detecting system with polarization dependent sensing elements

• US 8,319,957 B2
• Filed: 04/29/2009
• Issued: 11/27/2012
• Est. Priority Date: 04/29/2009
• Status: Expired due to Fees

• Current Assignee: Corning Incorporated
• Original Assignee: Corning Incorporated
• Inventors: Chen, Xin, Etienne, Michael, Nolan, Daniel Aloysius
• Primary Examiner(s): Chowdhury, Tarifur
• Assistant Examiner(s): Nur, Abdullahi
• Application Number:
  US12/432,222
• Publication Number:
  US 20100277719A1
• Time in Patent Office: 1,308 Days
• Field of Search: 356/73.1
• US Class Current: 356/73.1
• CPC Class Codes: G08B 13/186 using light guides, e.g. optical fibres

Abstract

A detection system includes a length of optical fiber and an OTDR coupled to the optical fiber. The OTDR includes a radiation source providing pulsed radiation to the fiber, a detector detecting radiation that is backscattered through the fiber, and a processor capable of analyzing the variation of the radiation that is backscattered through the fiber. At least two polarization dependent sensing elements are positioned along the length of optical fiber.

Claims

1. A detection system comprising:

(i) a length of optical fiber; and

(iii) an OTDR coupled to said fiber, said OTDR comprising (a) a radiation source providing pulsed radiation to said fiber, (b) a detector detecting radiation that is backscattered through the fiber, and (c) a processor capable of analyzing the variation of the radiation that is backscattered through the fiber;

wherein at least two polarization dependent sensing elements are positioned along the length of optical fiber.

2. The detection system of claim 1, wherein at least one polarization dependent sensing element comprises optical fiber subjected to mechanically induced microbending.

3. The detection system of claim 2, wherein at least one polarization dependent sensing element comprises a microbending gear rack.

4. The detection system of claim 3, wherein the microbending gear rack is at least 1 centimeter in length and induces a bend period of from 0.5 millimeters to 2 millimeters to the optical fiber and induces a bend amplitude of from 25 μ

m to 2 millimeters to the optical fiber.

5. The detection system of claim 1, wherein the length of the optical fiber comprises a plurality of airlines and at least one polarization dependent sensing element comprises a region wherein the airlines are absent.

6. The detection system of claim 1, wherein said detection system is capable of detecting a fiber disturbance within 20 meters of the actual location of the disturbance.

7. The detection system of claim 1, wherein each polarization dependent sensing element induces a polarization dependent loss of at least 0.2 dB along the length of optical fiber.

8. The detection system of claim 1, wherein each polarization dependent sensing element induces a polarization dependent loss of at least 10 dB along the length of optical fiber.

9. The detection system of claim 1, wherein at least four polarization dependent sensing elements are positioned along the length of optical fiber, wherein the distance between each polarization dependent sensing element is at least 50 meters.

10. A method for detecting a disturbance along a length of optical fiber comprising the steps of:

(i) emitting pulsed radiation into a length of optical fiber;

(ii) measuring radiation that is backscattered through the optical fiber; and

(iii) analyzing the variation of said measured radiation to produce information related to change in said measured radiation over time along the length of the fiber;

wherein at least two polarization dependent sensing elements are positioned along the length of optical fiber.

11. The method of claim 10, wherein at least one polarization dependent sensing element comprises optical fiber subjected to mechanically induced microbending.

12. The method of claim 11, wherein at least one polarization dependent sensing element comprises a microbending gear rack.

13. The method of claim 12, wherein the microbending gear rack is at least 1 centimeter in length and induces a bend period of from 0.5 millimeters to 2 millimeters to the optical fiber and induces a bend amplitude of from 25 μ

m to 2 millimeters to the optical fiber.

14. The method of claim 10, wherein the length of the optical fiber comprises a plurality of airlines and at least one polarization dependent sensing element comprises a region wherein the airlines are absent.

15. The method of claim 10, wherein the step of measuring radiation that is backscattered through the optical fiber comprises measuring at least one background reference trace and the step of analyzing the variation of said measured radiation comprises analyzing the variation of the difference between the at least one background reference trace and radiation backscattered over time along the length of the fiber.

16. The method of claim 10, wherein said method is capable of detecting a fiber disturbance within 20 meters of the actual location of the disturbance.

17. The method of claim 10, wherein each polarization dependent sensing element induces a polarization dependent loss of at least 0.2 dB along the length of optical fiber.

18. The method of claim 10, wherein each polarization dependent sensing element induces a polarization dependent loss of at least 10 dB along the length of optical fiber.

19. The method of claim 10, wherein at least four polarization dependent sensing elements are positioned along the length of optical fiber, wherein the distance between each polarization dependent sensing element is at least 50 meters.

20. The method of claim 10, wherein said step of analyzing the variation of said measured radiation comprises calculating:

(i) a sliding standard deviation trace;

or (ii) an auto correlation function of processed OTDR traces.