FUEL DENSITY MEASURING DEVICE, SYSTEM, AND METHOD USING MAGNETOSTRICTIVE PROBE BUOYANCY

• US 20070282540A1
• Filed: 08/14/2007
• Published: 12/06/2007
• Est. Priority Date: 05/31/2005
• Status: Active Grant

• Current Assignee: Veeder-Root Co (Vontier Corp.)
• Original Assignee: Veeder-Root Co (Vontier Corp.)
• Inventors: Hart, Robert
• Granted Patent: US 7,403,860 B2
• Time in Patent Office: Days
• US Class Current: 702/25
• CPC Class Codes: G01F 23/2963 magnetostrictive
• CPC Class Codes: G01F 23/68 using electrically actuated indicating means
• CPC Class Codes: G01F 23/72 using magnetically actuated indicating means
• CPC Class Codes: G01N 9/18 Special adaptations for indicating, recording, or control
• CPC Class Codes: G01N 9/20 by balancing the weight of the bodies

Abstract

A magnetostrictive fuel level probe includes a spring-loaded foot. The probe shaft of the fuel level probe moves up and down within the spring-loaded foot as a function of fuel density. The spring-loaded foot includes a reference magnet whose height relative to the bottom of a fuel storage tank is fixed. Currents generated by the fuel level probe allow measurement of how much of the fuel level probe is positioned above the reference magnet, and from this measurement, the buoyancy of the fuel level probe may be measured. From the buoyancy of the fuel level probe, the fuel density may be calculated.

Claims

1-13. -13. (canceled)

14. A method of detecting fuel density for fuel within a fuel storage tank, comprising:

measuring, with a magnetostrictive fuel probe having a probe shaft, a distance associated with an amount of the probe shaft positioned above a reference magnet;

calculating a buoyancy associated with the probe shaft;

calculating from the buoyancy of the probe shaft, the fuel density for fuel within the fuel storage tank; and

reporting the fuel density to a location removed from the magnetostrictive fuel probe.

15. The method of claim 14, wherein measuring the distance associated with the amount of the probe shaft positioned above the reference magnet comprises allowing the probe shaft to move up and down within a spring-loaded foot associated with the magnetostrictive fuel probe.

16. The method of claim 15, wherein the probe shaft moves up and down within the spring-loaded foot as a function of the buoyancy of the probe shaft.

17. The method of claim 16, wherein calculating according to the algorithm comprises calculating a force exerted by a spring on the probe shaft, namely F_s=K_s*(H_s0−

H_s), wherein F_s is the force exerted by the spring, K_s is a spring constant of the spring, H_s0 is an unloaded height of the spring, and H_s is a loaded height of the spring.

18. The method of claim 17, wherein calculating according to the algorithm comprises subtracting the force exerted by the spring on the probe shaft from the weight of the probe shaft, namely W_p−

K_s*(H_s0−

H_s), where W_p is the weight of the probe shaft.

19. The method of claim 18, wherein calculating according to the algorithm comprises dividing a quantity of the weight of the probe shaft minus the force exerted by the spring by a volume of the probe shaft within the fuel, namely

20. The method of claim 15, wherein measuring comprises, at least in part, measuring a time component associated with a torsional reflection.

21. The method of claim 15, wherein measuring comprises, at least in part, measuring a fuel depth with the magnetostrictive fuel probe.

22. The method of claim 15, wherein reporting the fuel density to a location removed from the magnetostrictive fuel probe comprises encrypting data from the magnetostrictive fuel probe such that it cannot be altered by a fueling site operator.

23. The method of claim 15, further comprising measuring a distance to a probe reference magnet associated with a terminal end of the probe shaft and comparing this distance to the distance associated with the amount of the probe shaft positioned above the reference magnet.

24-37. -37. (canceled)