Aircraft fuel measurement

Patent metadata

Field	Value
Publication number	US-10480986-B2
Application number	US-201615189511-A
Country	US
Kind code	B2
Filing date	Jun 22, 2016
Priority date	Jun 30, 2015
Publication date	Nov 19, 2019
Grant date	Nov 19, 2019

Abstract

A method of estimating a quantity of a liquid fuel in a fuel tank of an aircraft is disclosed. A surface of the fuel is illuminated with light so that the light is reflected or scattered by the surface of the fuel onto an array of sensors. The light travels to and from the surface of the fuel via a measurement path containing a transmission medium. A measured time of flight is made at each sensor for the light which travels via the measurement path to that sensor. At least one of the sensors is illuminated with light via a reference path containing a transmission medium with substantially the same refractive index as the transmission medium in the measurement path, the reference path having a known reference distance which does not vary in accordance with the quantity of the fuel.

First claim

The invention claimed is:

1. An aircraft fuel tank system, comprising:
a fuel tank;
an array of sensors;
a light source arranged to illuminate a surface of a liquid fuel in the fuel tank with light so that the light is reflected or scattered by the surface of the fuel onto the array of sensors, the light travelling to and from the surface of the fuel via a measurement path containing a transmission medium, wherein the light source is also arranged to illuminate at least one sensor of the array of sensors with light via a reference path containing a transmission medium with substantially the same refractive index as the transmission medium in the measurement path, the reference path having a known reference distance which does not vary in accordance with the quantity of the fuel; and
a processing system arranged to determine a measured time of flight of the light which travels via the measurement path to each sensor of the array of sensors, measure a reference time of flight of the light which travels via the reference path to said at least one sensor, and estimate the quantity of the fuel in the fuel tank in accordance with the measured times of flight, the reference time of flight and the known reference distance,
a reflector mounted in fixed relation to the array of sensors, so that the light travelling via the reference path is reflected onto said at least one sensor by the reflector,
wherein the reflector is a semi-transparent window arranged such that some of the light from the light source is transmitted through the semi-transparent window and illuminates the surface of the fuel to provide the measurement path, and some of the light from the light source is reflected by the semi-transparent window onto said at least one sensor to provide the reference path.

2. A system according to claim 1 , wherein the light source is arranged for pulsed operation so that the light which illuminates the surface of the liquid fuel in the fuel tank is emitted by the light source in pulses.

3. A system according to claim 1 , wherein the surface of the fuel is illuminated from above so that the transmission medium in the measurement path comprises tillage gas.

4. A system according to claim 1 , wherein the surface of the fuel is illuminated from below so that the transmission medium in the measurement path comprises the liquid fuel.

5. A system according to claim 1 , further comprising a lens arranged so that the light travelling to and from the surface of the fuel via the measurement path passes through the lens.

6. A system according to claim 5 wherein the lens is arranged so that the light travelling to said at least one sensor via the reference path also passes through the lens.

7. A system according to claim 1 , wherein the processing system is arranged to estimate the quantity of the fuel in the fuel tank in accordance with the measured times of flight, the reference time of flight, the known reference distance, and a known geometry of the fuel tank.

8. An aircraft comprising a fuel tank system according to claim 1 .

9. A method of estimating a quantity of a liquid fuel in a fuel tank of an aircraft, the method comprising:
illuminating a surface of the fuel with light so that the light is reflected or scattered by the surface of the fuel onto an array of sensors, the light travelling to and from the surface of the fuel via a measurement path containing a transmission medium;
for each sensor of the array of sensors, determining a measured time of flight of the light which travels via the measurement path to that sensor;
illuminating at least one sensor of the array of sensors with light via a reference path containing a transmission medium with substantially the same refractive index as the transmission medium in the measurement path, the reference path having a known reference distance which does not vary in accordance with the quantity of the fuel;
measuring a reference time of flight of the light which travels via the reference path to said at least one sensor;
estimating the quantity of the fuel in the fuel tank in accordance with the measured times of flight, the reference time of flight and the known reference distance;
providing a reflector mounted in fixed relation to the array of sensors, so that the light travelling via the reference path is reflected onto said at least one sensor by the reflector,
wherein the reflector is a semi-transparent window arranged such that some of the light from the light source is transmitted through the semi-transparent window and illuminates the surface of the fuel to provide the measurement path, and some of the light from the light source is reflected by the semi-transparent window onto said at least one sensor to provide the reference path.

Assignees

• Airbus Operations Ltd

Inventors

• Cipullo Alessio
• Burnell Stephen
• Lam Joseph K-W

Classifications

• G01F23/2928 Primary

  using light reflected on the material surface · CPC title

• G01F23/292 Primary

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

• G01S7/497

  Means for monitoring or calibrating · CPC title

• G01S17/10

  using transmission of interrupted, pulse-modulated waves (determination of distance by phase measurements G01S17/32) · CPC title

• B64D37/005

  Accessories not provided for in the groups B64D37/02 - B64D37/28 · CPC title