System and method for measuring a mass of fuel within a variable geometry container

• US 9,429,459 B2
• Filed: 10/27/2014
• Issued: 08/30/2016
• Est. Priority Date: 10/28/2013
• Status: Expired due to Fees

• Current Assignee: EADS Construcciones Aeronauticas SA (Airbus SE)
• Original Assignee: EADS Construcciones Aeronauticas SA (Airbus SE)
• Inventors: Marcos Montes, Jose Luis, Angibaud, Guillaume, De La Fuente Lopez, Samuel, Espinosa Sanchez, Martin
• Primary Examiner(s): Macchiarolo, Peter
• Assistant Examiner(s): JENKINS, JERMAINE L
• Application Number:
  US14/524,794
• Publication Number:
  US 20150114103A1
• Time in Patent Office: 673 Days
• Field of Search: None
• US Class Current: 1/1
• CPC Class Codes: G01F 22/00 Methods or apparatus for measuring volume of fluids or fluent solid material, not otherwise provided for
• CPC Class Codes: G01F 23/20 by measurement of weight, e.g. to determine the level of stored liquefied gas
• CPC Class Codes: G01F 23/80 Arrangements for signal processing

Abstract

A system and method for measuring a mass of fuel contained in a variable geometry container. The container comprises a container assembly, formed by a variable geometry container disposed on a rigid support, a three-axis load cell coupled with the rigid support and providing a first set of three signals with a magnitude proportional to the force exerted by the container assembly, a three-axis accelerometer coupled with the rigid support and providing a second set of three signals with a magnitude proportional to the acceleration to which the container assembly is subjected, and a signal processing device configured to convert the first and the second set of signals into force and acceleration data, for three perpendicular directions of the space, and configured to calculate a measure relative to the mass of fuel contained in the variable geometry container.

Claims

1. A system for measuring a mass of fuel contained in a variable geometry container, comprising:

a container assembly formed by a variable geometry container disposed on a rigid support so that a weight of the container rests on the rigid support,

at least one three-axis load cell coupled with the rigid support, wherein the three-axis load cell provides a first set of three signals, each one of the three signals having a magnitude proportional to the force exerted by the container assembly in one of three perpendicular directions of the space,

at least one three-axis accelerometer coupled with the rigid support, wherein the three-axis accelerometer provides a second set of three signals, each one of the three signals having a magnitude proportional to the acceleration to which the container assembly is subjected in one of the three perpendicular directions of the space, and

a signal processing device configured to convert the first and the second set of signals to obtain force and acceleration data, for each one of the directions of the three perpendicular directions of the space, and also configured to calculate a measure relative to the mass of fuel contained in the variable geometry container.

2. The system according to claim 1, wherein the signal processing device is configured to calculate the mass as the result of dividing a sum of the forces exerted on a direction of the three common directions of the space, by the acceleration to which the container assembly is subjected by the same direction, additionally subtracting the known container assembly empty weight.

3. The system according to claim 1, wherein the signal processing device comprises an analog to digital converter for converting the first and the second set of signals to force and acceleration data.

4. The system according to claim 1, wherein the at least one three-axis load cell comprises four three-axis load cells arranged at opposing extremes of the rigid support.

5. The system according to claim 1, wherein the rigid support is a pallet.

6. The system according to claim 1, wherein the three-axis load cell is a strain gauge load cell and is configured to provide analog voltage signals corresponding to the first set of three signals.

7. The system according to claim 1, wherein the variable geometry container is a portable container, and it is made of a flexible material.

8. The system according to claim 1, further comprising a display system configured to display and monitor the mass of fuel calculated.

9. A method for measuring a mass of fuel contained in a variable geometry container, comprising the steps:

providing a container assembly formed by a variable geometry container disposed on a rigid support so that a weight of the container rests on the rigid support,

generating at least a first set of three signals, by means of a three-axis load cell coupled with the rigid support, wherein each one of the three signals has a magnitude proportional to a force exerted by the container assembly in one of three perpendicular directions of a space enclosed by the container,

generating at least a second set of three signals, by means of a three-axis accelerometer coupled with the rigid support, wherein each one of the three signals has a magnitude proportional to the acceleration to which the container assembly is subjected in one of the directions of the three directions of the space,

converting the first and the second set of signals into digital data, representative of measured forces and acceleration subjected by the container assembly, for each one of the three directions of the space,

calculating, for each one of the three directions of the space, a value relative to the mass of fuel contained in the variable geometry container, from the digital data relative to the measured forces and acceleration,

calculating, a total value relative to the mass of fuel contained in the variable geometry container.

10. The method according to claim 9, wherein the step of calculating the value relative to the mass of fuel contained in the variable geometry container comprises dividing the sum of the measured forces exerted on a direction of the three directions of the space, by the acceleration to which the container assembly is subjected in the same direction.

11. The method according to claim 9, wherein the step of calculating the total value relative to the mass of fuel contained in the variable geometry container comprises the step of determining the global mass of fuel as a result of a function that relates all the calculated values relatives to the mass of fuel contained in the variable geometry container for each of the three directions of the space, and the step of subtracting the known container assembly empty weight from the global mass.

12. The method according to claim 11, wherein the function that relates all the calculated values relatives to the mass of fuel contained in the variable geometry container for each of the three directions of the space, comprises one of an arithmetic mean, or a median, or a weighting function.

13. The method according to claim 9, further comprising the step of displaying and monitoring the total value relative to the mass of fuel contained in the variable geometry container measured with a display system.