Measuring the volume of fluid in a vessel

Patent metadata

Field	Value
Publication number	US-9846068-B2
Application number	US-201314397127-A
Country	US
Kind code	B2
Filing date	Apr 26, 2013
Priority date	Apr 27, 2012
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

A method and apparatus is disclosed for measuring the volume of fluid in a variable volume vessel.

First claim

The invention claimed is:

1. A method for measuring the volume of fluid in a variable volume vessel comprising two or more parts arranged to move relative to each other, the method comprising the steps of:
extracting a measured volume of gas from the variable volume vessel into an extraction chamber in an extraction phase to decrease the pressure of the gas in the variable volume vessel;
recording pressure data and temperature data representing the temperature and pressure of gas in the variable volume vessel during the extraction phase;
inserting the measured volume of gas in the extraction chamber into the variable volume vessel in an insertion phase to increase the pressure of the gas in the variable volume vessel;
recording pressure data and temperature data representing the temperature and pressure of gas in the variable volume vessel during the insertion phase;
determining, from the recorded temperature and pressure data, which of the insertion phase and the extraction phase corresponds to the maximum pressure change for the gas in the variable volume vessel;
identifying a region in the recorded temperature and pressure data representing substantially constant volume of the variable volume vessel due to stiction between the two or more moving parts during the determined one of the insertion phase and the extraction phase;
calculating the volume of gas in the variable volume vessel from the measured volume and the temperature and pressure data based on a plural of data points selected from the identified region; and
outputting the calculated gas volume.

2. A method according to claim 1 in which the variable volume vessel is partially filled with a liquid and the method comprises the further steps of:
identifying an internal volume of the variable volume vessel; and
calculating the volume of the liquid from the difference between the calculated volume of gas and the internal volume.

3. A method according to claim 1 in which an interface between the two or more parts comprises a gas-tight seal providing friction against the relative movement of the two or more parts such that the volume of the variable volume vessel may vary, in response to changes in its internal pressure or loading, when the friction is overcome.

4. A method according to claim 1 in which the variable volume vessel is externally loaded so as to pressurise the variable volume vessel.

5. A method according to claim 1 in which the gas is extracted from the variable volume vessel by a displacement pump.

6. A method according to claim 5 in which the displacement pump is operable by a control system, the control system being further operable to record the pressure and temperature data, select the data points, calculate the volume of gas and output the calculated volume.

7. A method according to claim 1 in which the gas is arranged to provide a gas spring.

8. A method according to claim 2 in which the liquid is arranged to provide damping for a gas spring.

9. A method according to claim 1 in which the variable volume vessel comprises a suspension strut for a vehicle.

10. A method according to claim 9 in which the vehicle is an aircraft.

11. A method according to claim 1 in which the region in the pressure data representing substantially constant volume of the variable volume vessel is identified by the rate of change of the pressure data being substantially linear.

12. A method according to claim 1 in which the region in the pressure data representing substantially constant volume of the variable volume vessel is identified using data representing an externally measured dimension for the variable volume vessel.

13. Apparatus for measuring the volume of fluid in a variable volume vessel comprising two or more parts arranged to move relative to each other, the apparatus, comprising:
a displacement pump to extract a measured volume of gas from the variable volume vessel into an extraction chamber in an extraction phase to decrease the pressure of the gas in the vessel, and insert the measured volume of gas in the extraction chamber into the variable volume vessel in an insertion phase to increase the pressure of the gas in the vessel, and
a control system configured to record pressure data and temperature data representing the temperature and pressure of gas in the variable volume vessel during the extraction phase;
record pressure data and temperature data representing the temperature and pressure of gas in the variable volume vessel during the insertion phase;
determine, from the recorded temperature and pressure data, which of the insertion phase and the extraction phase corresponds to the maximum pressure change for the gas in the variable volume vessel;
identify a region in the recorded temperature and pressure data representing substantially constant volume of the variable volume vessel due to stiction between the two or more moving parts during the determined one or the insertion phase and the extraction phase;
calculate the volume of gas in the variable volume vessel from the measured volume and the temperature and pressure data based on a plurality of data points selected from the identified region; and
output the calculated gas volume.

14. Apparatus according to claim 13 in which the variable volume vessel is partially filled with a liquid and the apparatus is further operable to:
identify an internal volume of the variable volume vessel; and
calculate the volume of the liquid from the difference between the calculated volume of gas and the internal volume.

15. Apparatus according to claim 13 in which an interface between the two or more parts comprises a gas-tight seal providing friction against the relative movement of the two or more parts such that the volume of the variable volume vessel may vary, in response to changes in its internal pressure or loading, when the friction is overcome.

16. Apparatus according to claim 13 in which the variable volume vessel is externally loaded so as to pressurise the variable volume vessel.

17. Apparatus according to claim 13 in which the gas is extracted from the variable volume vessel by the displacement pump.

18. Apparatus according to claim 17 in which the displacement pump is operable by a control system, the control system being further operable to record the pressure and temperature data, select the data points, calculate the volume of gas and output the calculated volume.

19. Apparatus according to claim 13 in which the gas is arranged to provide a gas spring.

20. Apparatus according to claim 14 in which the liquid is arranged to provide damping for a gas spring.

21. Apparatus according to claim 13 in which the vessel comprises a suspension strut for a vehicle.

22. Apparatus according to claim 21 in which the vehicle is an aircraft.

23. Apparatus according to claim 13 in which the region in the pressure data representing substantially constant volume of the variable volume vessel is identified by the rate of change of the pressure data being substantially linear.

24. Apparatus according to claim 13 in which the region in the pressure data representing substantially constant volume of the variable volume vessel is identified using data representing an externally measured dimension for the variable volume vessel.

Assignees

• Airbus Operations Ltd

Inventors

• Shepherd Alan
• Duncan Julian

Classifications

• F16F9/3264

  Arrangements for indicating, e.g. fluid level; Arrangements for checking dampers (F16F9/3292 takes precedence; testing of vehicle damping G01M17/04) · CPC title

• B64C25/60

  Oleo legs · CPC title

• G01F22/02 Primary

  involving measurement of pressure · CPC title

• G01F22/00 Primary

  Methods or apparatus for measuring volume of fluids or fluent solid material, not otherwise provided for · CPC title

• B64F5/60

  Testing or inspecting aircraft components or systems · CPC title