Detecting fluid leakage at aircraft hatch

Patent metadata

Field	Value
Publication number	US-12158394-B2
Application number	US-202217980701-A
Country	US
Kind code	B2
Filing date	Nov 4, 2022
Priority date	Nov 11, 2021
Publication date	Dec 3, 2024
Grant date	Dec 3, 2024

Abstract

An assembly is provided for an aircraft. This aircraft assembly includes a fuselage and a second system. The fuselage includes a wall and a hatch configured to close an opening in the wall. The sensor system includes an optical fiber, a transmitter and a receiver. The optical fiber is arranged at an interface between the hatch and the wall. The transmitter is configured to transmit first electromagnetic radiation into the optical fiber. The receiver is configured to detect second electromagnetic radiation received from the optical fiber to provide receiver data. The sensor system is configured to detect fluid leakage across the interface between the hatch and the wall based on the receiver data.

First claim

What is claimed is:

1. An assembly for an aircraft, comprising:
a fuselage including a wall and a hatch configured to close an opening in the wall; and
a sensor system including an optical fiber, a transmitter and a receiver, the optical fiber arranged at an interface between the hatch and the wall, the transmitter configured to transmit first electromagnetic radiation into the optical fiber, the receiver configured to detect second electromagnetic radiation received from the optical fiber to provide receiver data, and the sensor system configured to detect fluid leakage across the interface between the hatch and the wall based on the receiver data.

2. The assembly of claim 1 , wherein the sensor system is further configured to
process the receiver data to determine a difference between the second electromagnetic radiation and expected electromagnetic radiation; and
detect the fluid leakage based on the difference between the second electromagnetic radiation and the expected electromagnetic radiation.

3. The assembly of claim 2 , wherein the difference between the second electromagnetic radiation and the expected electromagnetic radiation comprises a wavelength shift between the second electromagnetic radiation and the expected electromagnetic radiation.

4. The assembly of claim 1 , wherein the sensor system is further configured to determine a flowrate of the fluid leakage across the interface between the hatch and the wall based on the receiver data.

5. The assembly of claim 4 , wherein the sensor system is further configured to provide an indicator signal when the flowrate of the fluid leakage across the interface is greater than a threshold.

6. The assembly of claim 1 , wherein the sensor system is further configured to determine a location of the fluid leakage across the interface.

7. The assembly of claim 1 , wherein the optical fiber comprises a grating configured to shift a wavelength of the first electromagnetic radiation.

8. The assembly of claim 7 , wherein the first electromagnetic radiation interacts with and passes through the grating to at least partially provide the second electromagnetic radiation.

9. The assembly of claim 7 , wherein the second electromagnetic radiation comprises a reflection of at least a portion of the first electromagnetic radiation by the grating.

10. The assembly of claim 1 , wherein
the optical fiber comprises a plurality of gratings arranged at discrete locations along the interface between the hatch and the wall;
the plurality of gratings comprises a first grating and a second grating;
the first grating is configured to reflect a first wavelength of electromagnetic radiation; and
the second grating is configured to reflect a second wavelength of electromagnetic radiation.

11. The assembly of claim 1 , wherein
the optical fiber comprises a plurality of gratings arranged at discrete locations along the interface between the hatch and the wall; and
each of the plurality of gratings is associated with unique electromagnetic radiation transmitted into the optical fiber.

12. The assembly of claim 1 , wherein
the optical fiber extends longitudinally between a first end and a second end; and
the transmitter and the receiver are arranged at the first end.

13. The assembly of claim 1 , wherein
the optical fiber extends longitudinally between a first end and a second end;
the transmitter is arranged at the first end; and
the receiver is arranged at the second end.

14. The assembly of claim 1 , further comprising:
a seal element arranged at the interface between the hatch and the wall;
the optical fiber disposed along and outside of the seal element.

15. The assembly of claim 1 , further comprising:
a seal element arranged at the interface between the hatch and the wall; and
at least a portion of the optical fiber disposed within the seal element.

16. The assembly of claim 1 , wherein the optical fiber is disposed at an exterior side or an interior side of the interface between the hatch and the wall.

17. The assembly of claim 1 , further comprising:
a second sensor system including a second optical fiber, a second transmitter and a second receiver;
the second optical fiber arranged at the interface between the hatch and the wall;
the second transmitter configured to transmit third electromagnetic radiation into the second optical fiber;
the second receiver configured to detect fourth electromagnetic radiation received from the second optical fiber to provide second receiver data; and
the second sensor system configured to detect fluid leakage across the interface between the hatch and the wall based on the second receiver data.

18. An assembly for an aircraft, comprising:
a fuselage including a wall and a hatch configured to close an opening in the wall; and
a sensor system including an optical fiber, a transmitter and a receiver, the optical fiber arranged at an interface between the hatch and the wall, the transmitter configured to transmit first electromagnetic radiation into the optical fiber, the receiver configured to detect second electromagnetic radiation received from the optical fiber to provide receiver data, the sensor system configured to determine temperature data at the interface between the hatch and the wall based on the receiver data, and the sensor system further configured to process the temperature data to detect fluid leakage across the interface between the hatch and the wall.

19. A method involving an aircraft fuselage including a wall and a hatch, the method comprising:
transmitting first electromagnetic radiation into an optical fiber, the optical fiber arranged at an interface between the hatch and the wall, and the hatch configured to close an opening in the wall;
detecting actual second electromagnetic radiation received from the optical fiber; and
detecting a fluid leak across the interface between the hatch and the wall based on a wavelength shift between the actual second electromagnetic radiation and expected second electromagnetic radiation.

Assignees

• Rohr Inc

Inventors

• Goyal Nitin Kumar
• Jacob Robin

Classifications

• H04B10/40

  Transceivers · CPC title

• G01L1/246

  using integrated gratings, e.g. Bragg gratings · CPC title

• G01K13/00

  Thermometers specially adapted for specific purposes · CPC title

• G01K11/3206

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

• B64C1/14

  Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens {accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers}(fairings movable in conjunction with undercarriage elements B64C25/16; bomb doors B64D1/06) · CPC title