FUEL QUANTITY MEASUREMENT

• US 20140053645A1
• Filed: 08/08/2013
• Published: 02/27/2014
• Est. Priority Date: 08/22/2012
• Status: Abandoned Application

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: WARD, Ian, HASKINS, RIchard
• Application Number:
  US13/962,306
• Publication Number:
  US 20140053645A1
• Time in Patent Office: Days
• US Class Current: 73/302
• CPC Class Codes: G01F 23/14 by measurement of pressure
• CPC Class Codes: G01F 23/22 by measuring physical variables, other than linear dimensions, pressure or weight, dependent on the level to be measured, e.g. by difference of heat transfer of steam or water involving the use of floats G01F23/30
• CPC Class Codes: G01F 23/804 containing circuits handling parameters other than liquid level

Abstract

The present invention provides a method, device and apparatus for determining a quantity of fuel within a fuel tank having a drain valve penetrating a lower boundary of the fuel tank. The method includes inserting a pressure measurement probe having a pressure sensor into the drain valve to permit contact between the pressure sensor and fuel within the tank, and measuring a pressure of the fuel with the pressure sensor. The measured pressure is used to determine the quantity of fuel within the tank, e.g. by consulting look-up tables comprising data indicating the relationship between measured pressure and fuel quantity, or by using one or more conversion equations.

Claims

1. A method of determining a quantity of fuel within a fuel tank having a drain valve penetrating a lower boundary of the fuel tank, the method including:

interconnecting a pressure measurement probe with the drain valve to permit direct or indirect contact between a pressure sensor and fuel within the tank;

measuring a pressure of the fuel with the pressure sensor; and

using the measured pressure and information relating to the geometry of the fuel tank to determine the quantity of fuel within the tank.

2. A method according to claim 1, wherein the step of using the measured pressure and information relating to the geometry of the fuel tank to determine the quantity of fuel within the tank includes one of:

consulting a look-up table comprising a matrix of corresponding pressures and fuel quantities for said fuel tank; and

using one or more conversion equations.

3. A method according to claim 1, including detecting an identifier associated with said fuel tank, wherein the step of determining the quantity of fuel within the tank includes using the detected identifier and measured pressure and information relating to the geometry of the fuel tank to determine the quantity of fuel.

4. A method according to claim 3, wherein the step of detecting an identifier associated with said fuel tank includes interrogating an identification device attached to said fuel tank.

5. A method according to claim 1, including detecting a temperature of either fuel within said fuel tank or air external to said fuel tank, wherein the step of determining the quantity of fuel within the tank includes using the detected temperature and measured pressure to determine the quantity of fuel.

6. A method according to claim 1, including detecting an attitude of said fuel tank, wherein the step of determining the quantity of fuel within the tank includes using the detected attitude and measured pressure to determine the quantity of fuel.

7. A method according to claim 1, including interconnecting a drain probe with the drain valve to drain some or all of the fuel from the fuel tank.

8. A method according to claim 1, wherein the fuel tank is arranged to supply fuel to one or more engines of an aircraft.

9. Equipment for determining a quantity of fuel within a fuel tank having a drain valve penetrating a lower boundary of the fuel tank, the equipment comprising:

a device including a pressure measurement probe and a pressure sensor, the pressure measurement probe being adapted to interconnect with the drain valve to permit direct or indirect contact between the pressure sensor and fuel within the tank; and

quantity calculation means for generating a value indicative of the quantity of fuel using a pressure measured by the pressure sensor and information relating to the geometry of the fuel tank.

10. Equipment according to claim 9, including a fuel duct arranged to provide fluid communication between the drain valve and the pressure sensor when the pressure measurement probe is interconnected with the drain valve.

11. Equipment according to claim 9, wherein the device includes a power source arranged to provide operating power to the pressure measurement probe.

12. Equipment according to claim 9, wherein the device includes a computation module arranged to convert a measured pressure from the pressure sensor into the quantity of said fuel.

13. Equipment according to claim 12, including an identity detection module arranged to interrogate an identification device of the fuel tank to determine an identify of the fuel tank, wherein the computation module is arranged to receive from the identity detection module identification data indicative of a detected identity of the fuel tank, and to use that identification data to convert the measured pressure into the quantity of said fuel.

14. Equipment according to claim 12, including a temperature sensor arranged to detect a temperature of either fuel within the fuel tank or air external to the fuel tank, wherein the computation module is arranged to receive from the temperature sensor temperature data indicative of a detected temperature, and to use that temperature data to convert the measured pressure into the quantity of said fuel.

15. Equipment according to claim 12, wherein the computation module is arranged to receive attitude data indicative of an attitude of the fuel tank, and to use that attitude data to convert the measured pressure into the quantity of said fuel.

16. Equipment according to any claim 12, wherein the computation module is arranged to calculate an error band representative of an accuracy of the determined quantity of said fuel.

17. Equipment according to claim 9, wherein the quantity calculation means comprises at least one of:

a look-up table comprising a matrix of corresponding pressures and fuel quantities for said fuel tank; and

one or more conversion equations.

18. A device according to claim 9, wherein the fuel tank is arranged to supply fuel to one or more engines of an aircraft.

19. Apparatus for determining a quantity of fuel within a fuel tank, the apparatus including:

a drain valve penetrating a lower boundary of the fuel tank, the drain valve being biased towards a closed configuration in which fuel is prevented from flowing through the drain valve;

equipment according to claim 9, wherein the pressure measurement probe is adapted to interconnect with the drain valve to urge the drain valve to a measurement configuration in which fuel is permitted to flow within the drain valve to directly or indirectly contact the pressure sensor and thereby permit measurement of a pressure of the fuel.

20. Apparatus according to claim 19, wherein the quantity calculation means comprises one of:

a look-up table comprising a matrix of corresponding pressures and fuel quantities for said fuel tank; and

a computation module arranged to receive a measured pressure from the pressure sensor and to use that measured head of pressure to calculate the fuel quantity.

21. Apparatus according to claim 19, wherein the drain valve has an open configuration in which it permits draining of fuel from the fuel tank through the drain valve.

22. Apparatus according to claim 19, including a drain device adapted to interconnect with the drain valve to urge the drain valve to the open configuration, the drain device optionally having a sampling container arranged to collect a sample volume of fuel draining from the fuel tank via the drain valve.

23. Apparatus according to claim 19, wherein the fuel tank is arranged to supply fuel to one or more engines of an aircraft.