FUEL SURFACE HEIGHT MEASUREMENT

• US 20150153212A1
• Filed: 11/28/2014
• Published: 06/04/2015
• Est. Priority Date: 11/29/2013
• Status: Abandoned Application

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: CIPULLO, Alessio, TICHBORNE, Franklin, LAM, Joseph K-W, LEIGH, Timothy
• Application Number:
  US14/555,818
• Publication Number:
  US 20150153212A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01F 23/292 Light , e.g. infrared or ultraviolet
• CPC Class Codes: G01F 23/802 Particular electronic circuits for digital processing equipment
• CPC Class Codes: G06V 10/143 Sensing or illuminating at different wavelengths
• CPC Class Codes: G06V 10/75 Organisation of the matching processes, e.g. simultaneous or sequential comparisons of image or video features; Coarse-fine approaches, e.g. multi-scale approaches; using context analysis; Selection of dictionaries
• CPC Class Codes: G06V 20/52 Surveillance or monitoring of activities, e.g. for recognising suspicious objects recognising microscopic objects G06V20/69

Abstract

A method of measuring a height of a fuel surface of fuel in an aircraft fuel tank. One or more images of the fuel surface are captured, each image including a fuel surface line where the fuel surface meets a structure. Each image is analysed in order to determine a height of the fuel surface line at three or more points in the image. If the fuel surface line is not a straight line, then an average angle of the fuel surface line can be determined from the points in the image by spatial averaging. Preferably a series of images of the fuel surface are captured over a time period, and an average height of the fuel surface is determined from the series of images by time averaging. The height of the fuel surface line(s) at three or more points is used to determine a volume of the fuel, a mass of the fuel, and/or an attitude of the fuel surface.

Claims

1. A method of measuring a height of a fuel surface in an aircraft fuel tank, the method comprising:

capturing one or more images of the fuel surface, each image including a fuel surface line where the fuel surface meets a structure; and

analysing each image in order to determine a height of the fuel surface line at three or more points in the image, wherein at least one of the fuel surface lines is not straight, and an average angle of that fuel surface line is determined from the points in the image by spatial averaging.

2. The method of claim 1 wherein each image is analysed by determining a height of the fuel surface line at ten or more points in the image.

3. The method of claim 1 wherein the method comprises capturing a series of two or more images of the fuel surface over a time period, and determining an average height of the fuel surface from the series of images by time averaging.

4. The method of claim 3 wherein the time period is greater than one minute.

5. The method of claim 3 wherein the time period is less than ten seconds.

6. The method of claim 1 further comprising using the height of the fuel surface line(s) at three or more points to determine a volume of the fuel, and/or a mass of the fuel, and/or an attitude of the fuel surface.

7. The method of claim 1, wherein each image is analysed by determining a height of the fuel surface line at three or more points in the image relative to a feature in the image.

8. The method of claim 7, wherein the feature in the image is a grid line carried by the structure.

9. The method of claim 7 wherein each image is analysed by counting a number of pixels between the fuel surface line and the feature in the image.

10. The method of claim 1 wherein the image is captured by a fiberscope comprising a bundle of optical fibres.

11. The method of claim 1 further comprising applying distortion correction to the image.

12. The method of claim 1 further comprising displaying at least one of the images.

13. Apparatus for measuring a height of a fuel surface in an aircraft fuel tank, the method comprising:

an image capture device arranged to capture one or more images of the fuel surface, each image including a fuel surface line where the fuel surface meets a structure; and

a processor arranged to analyse each image in order to determine a height of the fuel surface line at three or more points in the image, wherein at least one of the fuel surface lines is not straight, and the processor is arranged to determine an average angle of that fuel surface line from the points in the image by spatial averaging.

14. The apparatus of claim 13 further comprising a display device arranged to receive and display at least one of the images.

15. An aircraft fuel tank system comprising a fuel tank, and apparatus according to claim 13 for measuring a height of a fuel surface in the fuel tank.

16. A system according to claim 15 wherein the fuel tank comprises a window, and the image capture device is positioned outside the fuel tank and arranged to capture the image(s) of the fuel surface through the window.

17. A system according to claim 15 wherein the fuel tank comprises a structure which carries one or more features, and wherein the processor is arranged to analyse each image by determining a height of the fuel surface line at one or more points in the image relative to one of said features in the image.