Fill level measurement system and method for determining a fill level

• US 9,395,230 B2
• Filed: 11/25/2013
• Issued: 07/19/2016
• Est. Priority Date: 11/28/2012
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Operations GmbH (Airbus SE)
• Inventors: Rieger, Ulrich
• Primary Examiner(s): WILLIAMS, HEZRON
• Assistant Examiner(s): Eyassu, Marrit
• Application Number:
  US14/089,131
• Publication Number:
  US 20140150549A1
• Time in Patent Office: 967 Days
• Field of Search: 733/06, 732/91
• US Class Current: 1/1
• CPC Class Codes: G01F 23/296 Acoustic waves
• CPC Class Codes: G01F 23/2962 Measuring transit time of reflected waves
• CPC Class Codes: G01F 23/64 of the free float type without mechanical transmission elements

Abstract

A measurement system for determining a liquid fill level of a tank, including a floating sensor configured to float on the surface of a liquid contained in the tank, at least three reference sensors mounted at a hull of the tank in a spatially fixed arrangement, and a control device to control the floating sensor and the reference sensors, wherein at least one of the floating sensor and the reference sensors can emit an acoustic signal to the remaining sensors, wherein the remaining sensors can receive the emitted acoustic signal, and wherein the control device is configured to determine signal travelling times of the acoustic signal from the emitting sensor to the receiving sensor, to compute a spatial position of the floating sensor with respect to the reference sensors from the signal travelling times, and to determine the liquid fill level using the computed spatial position of the floating sensor.

Claims

1. A measurement system for determining a liquid fill level of a tank, comprising:

a floating sensor configured to float on the surface of a liquid contained in the tank;

at least three reference sensors mounted at a hull of the tank in a spatially fixed arrangement; and

a control device configured to control the floating sensor and the reference sensors,

wherein at least one of the floating sensor and the reference sensors is configured to emit an acoustic signal to the remaining sensors,

wherein the remaining sensors are each configured to receive the emitted acoustic signal, and

wherein the control device is configured to determine signal travelling times of the acoustic signal from the emitting sensor to the receiving sensor, to compute a spatial position of the floating sensor with respect to the reference sensors using the signal travelling times of the acoustic signal, to determine the liquid fill level on the basis of the computed spatial position of the floating sensor, to control a first one of the at least three reference sensors to emit a test acoustic signal which is received by a second of the at least three reference sensors, to determine a travelling time of the test acoustic signal between the first and the second one of the at least three reference sensors, and to compute a speed of sound in the tank using the travelling time of the test acoustic signal.

2. The measurement system of claim 1, wherein the acoustic signals comprise ultrasonic signals.

3. The measurement system of claim 1, wherein the control device is an integral component of the floating sensor.

4. The measurement system of claim 1, wherein the control device is an integral component of one of the reference sensors.

5. The measurement system of claim 1, wherein the control device is connected to the floating sensor by a cable.

6. The measurement system of claim 1, wherein the control device is connected to the floating sensor by a wireless communication channel.

7. The measurement system of claim 6, wherein the floating sensor is supplied with electrical energy by a battery.

8. The measurement system of claim 1, wherein the tank comprises a potable water tank, a waste water tank or a fuel tank of an aircraft or spacecraft.

9. The measurement system of claim 8, wherein the control device is configured to receive declination parameters of the aircraft or spacecraft and to determine the liquid fill level on the basis of the declination parameters.

10. A method for determining a liquid fill level of a tank, comprising:

emitting a first acoustic signal by a floating sensor floating on the surface of a liquid contained in the tank;

receiving the first acoustic signal by at least three reference sensors mounted at a hull of the tank in a spatially fixed arrangement;

determining signal travelling times of the first acoustic signal between the floating sensor and each of the reference sensors;

computing the spatial position of the floating sensor with reference to the reference sensors from the determined signal travelling times;

determining the liquid fill level on the basis of the computed spatial position of the floating sensor,

emitting a test acoustic signal by a first one of the at least three reference Sensors;

receiving the test acoustic signal by a second one of the at least three reference sensors;

determining a signal travelling time of the test acoustic signal between the first and the second one of the at least three reference sensors; and

computing a speed of sound in the tank using the signal travelling time of the test acoustic signal.

11. The method of claim 10, wherein the first and second one of the reference sensors are mounted at the hull of the tank at or above the surface of the liquid, and wherein the computed speed of sound is the speed of sound in the atmosphere above the liquid in the tank.

12. The method of claim 10, wherein the first and second one of the reference sensors are mounted at the hull of the tank below the surface of the liquid, and wherein the computed speed of sound is the speed of sound in the liquid in the tank.

13. The method of claim 10, wherein the first and/or test acoustic signal comprises a series of pulsed acoustic signals.

14. The method of claim 10, wherein the first and/or test acoustic signal comprises a message signal comprising information about the time of emitting and the identity of the emitting sensor.