Measuring fuel in a fuel tank

Patent metadata

Field	Value
Publication number	US-10551237-B2
Application number	US-201715726771-A
Country	US
Kind code	B2
Filing date	Oct 6, 2017
Priority date	Oct 10, 2016
Publication date	Feb 4, 2020
Grant date	Feb 4, 2020

Abstract

A method of measuring a height of a fuel in an aircraft fuel tank ( 21 ) b including illuminating the fuel in the aircraft fuel tank and detecting reflected light from the fuel. Optical coherence tomography is used to determine the height of a surface of fuel in the fuel tank. An apparatus ( 30 ) is used to measure a height of a surface of fuel in an aircraft fuel tank, and an aircraft fuel tank system with a fuel tank and an apparatus for measuring a height of a surface of fuel in the aircraft fuel tank.

First claim

The invention claimed is:

1. A method of determining a height of liquid in an aircraft fuel tank, the method comprising:
illuminating the liquid in the aircraft fuel tank,
detecting reflected light from the liquid, and
using optical coherence tomography to determine a depth profile of the liquid in the fuel tank, and
determining a height of the liquid in the fuel tank based on the determined depth profile.

2. The method according to claim 1 , wherein the liquid is a liquid fuel.

3. The method according to claim 1 , wherein the method comprises analysing the depth profile to identify a gas/liquid boundary in the fuel tank, and determining the height of the liquid in the fuel tank in dependence on the determined gas/liquid boundary.

4. The method according to claim 3 , wherein the method comprises analysing the depth profile to identify a tank/liquid boundary, and the determining the height of the liquid in the fuel tank depends on the determined gas/liquid boundary and the tank/liquid boundary.

5. The method according to claim 3 , wherein the method comprises analysing the depth profile to identify a liquid fuel/water boundary, and the determining the height of the liquid in the fuel tank depends on the determined gas/liquid boundary and the liquid fuel/water boundary.

6. The method according to claim 1 , wherein the method comprises determining an interference spectrum pattern in the wavelength domain of the reflected light, and analysing the interference spectrum pattern to determine the depth profile of the liquid in the fuel tank.

7. The method according to claim 6 , wherein the method comprises applying a Fast Fourier Transform to the interference spectrum pattern to determine the depth profile of the liquid in the fuel tank.

8. The method according to claim 6 , wherein the method comprises directing light from a light source along a sample path into the fuel tank to illuminate the liquid and directing the reflected light from the fuel tank to an optical detector.

9. The method according to claim 8 , wherein the method comprises directing light from the light source along a reference path split from the sample path, and recombining the light from the reference path with the reflected light from the fuel tank to generate the interference spectrum pattern.

10. The method according to claim 8 , wherein the method comprises using a swept laser source as the light source and a photodetector as the detector, or using a broadband light source as the light source and a spectrometer as the detector.

11. The method according to claim 1 , wherein the method further comprises directing light illuminating the liquid in the fuel tank from a bottom side of the fuel tank.

12. The method according to claim 1 , wherein
the method comprises splitting light illuminating the liquid in the fuel tank into two or more projecting paths in the fuel tank, and
determining the depth profile of the liquid in the fuel tank at two or more positions in the fuel tank.

13. The method according to claim 12 , wherein the method comprises determining the attitude of a surface of the liquid in the fuel tank in dependence on the two or more depth profiles of the liquid in the fuel tank at two or more positions in the fuel tank.

14. The method according to claim 1 , wherein the method comprises scanning light illuminating the liquid in the fuel tank across a portion of the fuel tank, and determining a depth profile of the liquid in the fuel tank at two or more positions in the fuel tank.

15. A fuel tank measuring apparatus for measuring a depth of a liquid in an aircraft fuel tank, the apparatus comprising an optical coherence tomography system including:
a light source configured to illuminate the liquid in the aircraft fuel tank, and
a detector configured to detect reflected light reflected from within the aircraft fuel tank,
wherein the optical coherence tomography system is configured to analyse the reflected light using optical coherence tomography to determine a depth profile of the liquid in the fuel tank, and determine a depth of the liquid in the fuel tank based on the depth profile.

16. The apparatus according to claim 15 , further comprising a display device arranged to receive and display an output from the optical coherence tomography system.

17. An aircraft fuel tank system comprising an aircraft fuel tank, and an optical coherence tomography system including:
a light source configured to illuminate liquid in the aircraft fuel tank,
a detector configured to detect reflected light reflected from within the aircraft fuel tank, and
wherein the optical coherence tomography system is configured to analyse the reflected light using optical coherence tomography to determine a depth profile of the liquid in the fuel tank, and determining a height of the liquid in the fuel tank using the depth profile.

18. The system according to claim 17 , wherein the aircraft fuel tank comprises a window, and the optical coherence tomography system is positioned outside the aircraft fuel tank and arranged to illuminate the liquid in the fuel tank and detect reflect light through the window.

19. The system according to claim 17 , wherein the aircraft fuel tank comprises a reflector in the aircraft fuel tank which is configured to reflect the light illuminating the liquid in the aircraft fuel tank.

20. A method comprising:
illuminating a fuel tank containing a liquid,
detecting light reflected from within the fuel tank due to the illumination, and
determining a depth profile of the liquid in the fuel tank by analyzing the detected light using optical coherence tomography.

21. The method of claim 20 further comprising determining depth of the liquid in the fuel tank using the depth profile.

22. The method of claim 20 wherein the illumination of the fuel tank includes projecting from or into one end of the fuel tank and towards a reflective surface at on opposite end of the fuel tank.

23. The method of claim 20 wherein the illumination of the fuel tank includes projecting light through a collimating lens which directs collimated light towards the fuel tank.

24. The method of claim 20 further comprising generating information indicating the depth profile of the liquid in the fuel tank and sending the information to a display device.

Assignees

• Airbus Operations Ltd
• Univ Aston

Inventors

• Cipullo Alessio
• Gordon Neil Thomson
• Zhou Kaiming

Classifications

• G01C9/005

  specially adapted for use in aircraft · CPC title

• G01B11/0608

  Height gauges · CPC title

• G01F23/292 Primary

  Light {, e.g. infrared or ultraviolet} · CPC title

• G01C9/18

  by using liquids · CPC title

• G01F23/2928 Primary

  using light reflected on the material surface · CPC title