Electrical fault detector and method of use

Patent metadata

Field	Value
Publication number	US-10928435-B2
Application number	US-201916511984-A
Country	US
Kind code	B2
Filing date	Jul 15, 2019
Priority date	Jul 15, 2019
Publication date	Feb 23, 2021
Grant date	Feb 23, 2021

Abstract

An electrical system is provided. The electrical system includes an insulated electrical conductor installed in an aircraft and configured to conduct a current over a length of the insulated electrical conductor. The electrical system includes an optical fiber includes a jacket surrounding an optical core, the optical fiber installed adjacent to the insulated electrical conductor. The electrical system includes a photo detector coupled to the optical fiber and configured to detect an electromagnetic signal carried by the optical fiber and at least partially generated as a function of an electrical fault that occurs at a point along the length of the insulated electrical conductor.

First claim

What is claimed is:

1. An electrical system, comprising:
an insulated electrical conductor installed in an aircraft and configured to conduct a current over a length of the insulated electrical conductor;
an optical fiber comprising a jacket surrounding an optical core, the optical fiber installed adjacent to the insulated electrical conductor; and
a photo detector coupled to the optical fiber and configured to detect an electromagnetic signal carried by the optical fiber and at least partially generated as a function of an electrical fault that occurs at a point along the length of the insulated electrical conductor.

2. The electrical system of claim 1 further comprising:
an optical transmitter coupled to the optical fiber and configured to transmit a base signal through the optical fiber; and
a processor coupled to the optical transmitter and the photo detector, the processor configured to detect a difference between the base signal and the electromagnetic signal at least partially generated as a function of the electrical fault.

3. The electrical system of claim 1 further comprising:
an optical transmitter coupled to the optical fiber and configured to transmit a measurement signal through the optical fiber in response to detecting the electromagnetic signal; and
a processor coupled to the optical transmitter and the photo detector, the processor configured to determine a location of the electrical fault along the length of the insulated electrical conductor based on an optical time-domain reflectometry measurement using the measurement signal.

4. The electrical system of claim 1 further comprising an optical transmitter coupled to the optical fiber and configured to transmit an identification signal through the optical fiber in response to detecting the electromagnetic signal, the identification signal configured to illuminate a location of the electrical fault along the length of the insulated electrical conductor using at least one frequency band of light.

5. The electrical system of claim 4 , wherein the at least one frequency band of light is infrared.

6. The electrical system of claim 1 further comprising a processor coupled to the photo detector and configured to initiate a maintenance message for the insulated electrical conductor in response to detecting the electromagnetic signal.

7. The electrical system of claim 1 further comprising a processor coupled to the photo detector and configured to de-energize the insulated electrical conductor in response to detecting the electromagnetic signal.

8. The electrical system of claim 1 further comprising:
an acoustic sensor system configured to detect the electrical fault; and
a processor coupled to the acoustic sensor system and the photo detector, the processor configured to determine the electrical fault has occurred based on both detection by the photo detector and detection by the acoustic sensor system.

9. An electrical fault detector, comprising:
an optical fiber comprising a jacket surrounding an optical core, the optical fiber configured to be installed adjacent to an insulated electrical conductor installed in an aircraft and configured to conduct a current over a length of the insulated electrical conductor;
a photo detector coupled to the optical fiber and configured to detect an electromagnetic signal carried by the optical fiber and at least partially generated as a function of an electrical fault that occurs at a point along the length of the insulated electrical conductor, the photo detector further configured to transmit an electrical signal indicative of detecting the electromagnetic signal; and
a processor coupled to the photo detector and configured to receive the electrical signal and determine the electrical fault has occurred in response to the electrical signal.

10. The electrical fault detector of claim 9 , wherein the jacket surrounding the optical core comprises a jacket material sensitive to heat and radiant energy emitted by the electrical fault and configured to degrade at a location proximate the electrical fault in response to the electrical fault.

11. The electrical fault detector of claim 10 , wherein the jacket material is further configured to degrade in response to at least one of an electrical arc or a corona discharge, thereby at least partially generating the electromagnetic signal carried by the optical fiber.

12. The electrical fault detector of claim 9 further comprising an optical transmitter coupled to the optical fiber and coupled to the processor, the optical transmitter configured to transmit a base signal through the optical fiber, and wherein the processor is further configured to detect a difference between the base signal and the electromagnetic signal at least partially generated as a function of the electrical fault to determine the electrical fault has occurred.

13. The electrical fault detector of claim 9 further comprising an optical transmitter coupled to the optical fiber and coupled to the processor, the optical transmitter configured to transmit a measurement signal through the optical fiber in response to detecting the electromagnetic signal, and wherein the processor is further configured to determine a location of the electrical fault based on an optical time-domain reflectometry measurement using the measurement signal.

14. The electrical fault detector of claim 9 further comprising an optical transmitter coupled to the optical fiber and coupled to the processor, the optical transmitter configured to transmit an identification signal through the optical fiber in response to detecting the electromagnetic signal, the identification signal configured to illuminate a location of the electrical fault along the length of the insulated electrical conductor using at least one frequency band of light.

15. A method of detecting an electrical fault occurring at a point along a length of an insulated electrical conductor installed in an aircraft and configured to conduct a current over its length, the method comprising:
installing an optical fiber adjacent to the insulated electrical conductor, the optical fiber having a jacket material configured to degrade at a location proximate the electrical fault in response to the electrical fault;
receiving, at a photo detector coupled to the optical fiber, an electromagnetic signal carried by the optical fiber and at least partially generated as a function of the electrical fault;
transmitting an electrical signal indicative of detecting the electromagnetic signal to a processor coupled to the photo detector; and
determining, by the processor, the electrical fault has occurred in response to the electrical signal.

16. The method of claim 15 further comprising:
transmitting, by an optical transmitter coupled to the optical fiber and the processor, a base signal through the optical fiber; and
detecting, by the processor, a difference between the base signal and the electromagnetic signal at least partially generated as a function of the electrical fault to determine the electrical fault has occurred.

17. The method of claim 15 further comprising:
transmitting, by an optical transmitter coupled to the optical fiber and the processor, a measurement signal through the optical fiber in response to determining the electrical fault has occurred; and
determining, by the processor, a location of the electrical fault along the length of the insulated electrical conductor based on an optical time-domain reflectometry measurement using the measurement signal.

18. The method of claim 15 furthe

Assignees

• Boeing Co

Inventors

• Severns Christopher Mark
• Khozikov Vyacheslav

Classifications

• G01R31/58 Primary

  Testing of lines, cables or conductors (testing of electric windings G01R31/72) · CPC title

• G01R31/1218

  using optical methods; using charged particle, e.g. electron, beams or X-rays · CPC title

• G01R31/1209

  using acoustic measurements (acoustic measurements G01H3/00) · CPC title

• G01R31/11 Primary

  using pulse reflection methods · CPC title

• G01R31/083

  in cables, e.g. underground · CPC title