Overheat detection with clamp health monitoring

Patent metadata

Field	Value
Publication number	US-11906369-B2
Application number	US-202117529868-A
Country	US
Kind code	B2
Filing date	Nov 18, 2021
Priority date	Sep 22, 2021
Publication date	Feb 20, 2024
Grant date	Feb 20, 2024

Abstract

A detection system in an aircraft includes an optical fiber arranged along a structure of the aircraft and affixed to the structure with clamps that are spaced apart along the structure. The optical fiber includes two or more sets of fiber Bragg gratings (FBGs). The system also includes a light source to generate light with two or more wavelengths for injection into the optical fiber, and processing circuitry to identify an overheat condition and monitor vibration experienced by the optical fiber based on reflected signals generated by the two or more sets of FBGs. Integrity of the clamps is indicated by monitoring the vibration.

First claim

What is claimed is:

1. A detection system in an aircraft comprising:
an optical fiber arranged along a structure of the aircraft and affixed to the structure with clamps that are spaced apart along the structure, wherein the optical fiber includes two or more sets of fiber Bragg gratings (FBGs);
a light source configured to generate light with two or more wavelengths for injection into the optical fiber; and
processing circuitry configured to identify an overheat condition and monitor vibration experienced by the optical fiber based on reflected signals generated by the two or more sets of FBGs, wherein integrity of the clamps is indicated by monitoring the vibration;
wherein each of the two or more FBGs of the optical fiber has a different grating pitch than others of the two or more FBGs and generates the reflected signals with a different reflected wavelength than the others of the two or more FBGs; and
wherein the overheat condition and the vibration cause a shift in the reflected wavelength of the reflected signals produced by affected ones of the two or more FBGs, the shift being periodic over a predefined duration when based on the vibration and the shift being non-periodic over the predefined duration when based on the overheat condition.

2. The system according to claim 1 , further comprising one or more photodetectors configured to detect an amplitude of the reflected signals at different wavelengths.

3. The system according to claim 2 , further comprising a circulator configured to direct the light from the light source into the optical fiber and to direct the reflected signals to the one or more photodetectors.

4. The system according to claim 1 , wherein the light source is configured to generate the light as pulses, with each pulse having one of the two or more wavelengths.

5. The system according to claim 1 , wherein the optical fiber is first optical fiber, the system further comprising a second optical fiber arranged in parallel with the first optical fiber along the structure and affixed with the clamps.

6. The system according to claim 5 , wherein the second optical fiber includes the two or more sets of FBGs.

7. The system according to claim 6 , wherein the processing circuitry is configured to identify the first optical fiber to identify the overheat condition and the processing circuitry is configured to use the second optical fiber to identify the vibration.

8. The system according to claim 1 , wherein the processing circuitry identifies a portion of the optical fiber that experiences the overheat condition or the vibration and one or more of the clamps that are affected based on identifying which of the two or more FBGs are the affected ones of the two or more FBGs.

9. A method of assembling a detection system in an aircraft comprising:
arranging an optical fiber along a structure of the aircraft and affixed to the structure with clamps that are spaced apart along the structure, wherein the optical fiber includes two or more sets of fiber Bragg gratings (FBGs);
arranging a light source to generate light with two or more wavelengths for injection into the optical fiber; and
configuring processing circuitry to identify an overheat condition and monitor vibration experienced by the optical fiber based on reflected signals generated by the two or more sets of FBGs, wherein integrity of the clamps is indicated by monitoring the vibration;
wherein the arranging the optical fiber includes each of the two or more FBGs of the optical fiber having a different grating pitch than others of the two or more FBGs and generating the reflected signals with a different reflected wavelength than the others of the two or more FBGs; and
wherein the configuring the processing circuitry to identify the overheat condition and monitor the vibration includes identifying that the overheat condition and the vibration cause a shift in the reflected wavelength of the reflected signals produced by affected ones of the two or more FBGs, the shift being periodic over a predefined duration when based on the vibration and the shift being non-periodic over the predefined duration when based on the overheat condition.

10. The method according to claim 9 , further comprising arranging one or more photodetectors to detect an amplitude of the reflected signals at different wavelengths.

11. The method according to claim 10 , further comprising arranging a circulator to direct the light from the light source into the optical fiber and to direct the reflected signals to the one or more photodetectors.

12. The method according to claim 9 , wherein the arranging the light source includes configuring the light source to generate the light as pulses, with each pulse having one of the two or more wavelengths.

13. The method according to claim 9 , wherein the optical fiber includes a first optical fiber and a second optical fiber, wherein arranging the optical fiber includes arranging the first and second optical fibers in parallel along the structure and affixed with the clamps.

14. The method according to claim 13 , wherein the second optical fiber includes the two or more sets of FBGs.

15. The method according to claim 14 , wherein the configuring the processing circuitry includes configuring the processing circuitry to use the first optical fiber to identify the overheat condition and configuring the processing circuit to use the second optical fiber to identify the vibration.

16. The method according to claim 9 , wherein the configuring the processing circuitry includes the processing circuitry identifying a portion of the optical fiber that experiences the overheat condition or the vibration and one or more of the clamps that are affected based on identifying which of the two or more FBGs are the affected ones of the two or more FBGs.

Assignees

• Kidde Tech Inc

Inventors

• Vallamkondu Aswin Kumar
• Miller Mark Sherwood
• Coreth Stefan

Classifications

• G01K11/3206 Primary

  at discrete locations in the fibre, e.g. using Bragg scattering · CPC title

• B64D45/00

  Aircraft indicators or protectors not otherwise provided for · CPC title

• G01H9/004

  using fibre optic sensors (light guides per se G02B6/00, acousto-optical devices specially adapted for gating or modulating in optical wave guides G02F1/125) · CPC title

• B64D2045/009

  Fire detection or protection; Erosion protection, e.g. from airborne particles · CPC title

• B64D2045/0085

  Devices for aircraft health monitoring, e.g. monitoring flutter or vibration · CPC title