Load cell assembly with linearization and common mode discrimination of complementary force-responsive signals

• US 5,629,489 A
• Filed: 02/06/1995
• Issued: 05/13/1997
• Est. Priority Date: 02/06/1995
• Status: Expired due to Fees

• Current Assignee: Avery Weigh-Tronix LLC (Illinois Tool Works Inc.)
• Original Assignee: Weigh-Tronix, Inc. (Illinois Tool Works Inc.)
• Inventors: Hipkiss, Victor E., Strom, Miles O.
• Primary Examiner(s): Dougherty, Elizabeth L.
• Assistant Examiner(s): Biegel, Ronald
• Application Number:
  US08/383,967
• Time in Patent Office: 827 Days
• Field of Search: 73/766, 73/862.59, 73/DIG. 1, 73/862.622, 73/765, 364/571.01, 364/571.03, 364/573, 364/508
• US Class Current: 73/862.622
• CPC Class Codes: G01G 3/165 Constructional details
• CPC Class Codes: G01G 3/18 Temperature-compensating arrangements

Abstract

A load cell assembly includes a load cell body having a pair of sensors mounted therein which provide complementary output signals in response to a force applied to the load cell body. A linearization and common mode discrimination routine analyzes changes in the sensor outputs and characterizes the changes as being either primarily due to applied force or primarily due to common mode effects. A force value, indicative of the applied force on the load cell body, is updated only for changes in the sensor outputs which are primarily due to applied force. However, changes which are primarily due to common mode effects are not incorporated into force value calculations, whereby common mode effects are rejected.

Claims

1. A load cell assembly for generating a force value indicative of an applied force, the load cell assembly comprising:

a load cell body adapted to receive the applied force;

first and second sensing means, coupled to the load cell body, for respectively providing first and second sensed signals which react in a complementary manner in response to the applied force on the load cell body;

means for sampling the first and second sensed signals at predetermined intervals of time to produce first and second change values representative of changes in the values of the first and second sensed signals over such predetermined time interval, each of said first and second change values having a magnitude value and a direction of change;

means for determining when the directions of change in the first and second change values are different; and

force calculating means, responsive to the determining means, for calculating the force value of the applied force from the magnitudes of the first and second change values.

2. The load cell assembly of claim 1, wherein the first and second sensing means respectively comprise:

(a) first and second force transducers, each of the type having a resonant frequency that varies with a force applied thereto;

(b) first and second driving means for driving the first and second transducers at their resonant frequencies and thereby respectively providing the first and second sensed signals; and

(c) converting means for converting the first and second sensed signals into digital first and second sensed values, respectively.

3. The load cell assembly of claim 2, wherein the load cell body comprises:

(a) an interior opening defined in the load cell body by an upper wall and a lower wall joined by first and second side walls;

(b) a base positioned within the opening and affixed to at least one of the opening walls;

(c) a first cantilever beam affixed to the base;

(d) a second cantilever beam affixed to the base; and

(e) wherein the first transducer is affixed between the first cantilever beam and the base and the second transducer is affixed between the second cantilever beam and the base.

4. The load cell assembly of claim 3, wherein the first and second transducers each comprise a double-ended tuning fork resonator.

5. The load cell assembly of claim 1, wherein the first and second sensing means each comprise a strain gauge.

6. The load cell assembly of claim 1, further comprising span correction means for correcting the force value for span effects.

7. The load cell assembly of claim 1, wherein the determining means comprises:

(a) means for calculating first and second difference values, the first difference value being representative of the difference between the first sensed value and a first reference value, and the second difference value being representative of the difference between the second sensed value and a second reference value; and

(b) means for comparing the signs of the first and second difference values, wherein same signs represent common mode effect changes and different signs represent applied force changes.

8. The load cell assembly of claim 7, further comprising reference value updating means for updating the first and second reference values to be equivalent to the first and second sensed values, respectively, after each sampling of the first and second sensed signals.

9. The load cell assembly of claim 8, wherein the force calculating means comprises adding a force change value to the force value responsive to an applied force change, wherein the force change value is representative of the difference between (1) the first difference value and (2) the second difference value multiplied by a scaling factor.

10. The load cell assembly of claim 1, wherein the determining means comprises:

(a) means for calculating a force sample value, the force sample value being representative of the difference between (1) the difference between the first sensed value and a first reference value and (2) a scaled difference between the second sensed value and a second reference value; and

(b) means for calculating a common mode sample value, the common mode sample value being representative of the sum of (1) the difference between the first sensed value and a first reference value and (2) a scaled difference between the second sensed value and a second reference value.

11. The load cell assembly of claim 10, wherein the determining means further comprises:

(a) means for calculating a force change value, the force change value being representative of the difference between force sample values taken in successive samples;

(b) means for calculating a common mode change value, the common mode change value being representative of the difference between common mode sample values taken in successive samples; and

(c) means for comparing the relative magnitudes of the force change value and common mode change value, wherein a greater magnitude for the common mode change value represents common mode effect changes and a greater magnitude for the force change value represents applied force changes.

12. The load cell assembly of claim 11, further comprising means for updating a common mode value by adding the common mode change value to the common mode value when the magnitude of the common mode change value exceeds that of the force change value.

13. The load cell assembly of claim 11, wherein the force calculating means comprises means for adding the force change value to the force value when the magnitude of the force change value exceeds that of the common mode change value.

14. The load cell assembly of claim 13, wherein the force calculating means further comprises means for comparing the force change value to a creep threshold value, the creep threshold value being representative of a rate that is characteristic of creep, and wherein the force calculating means adds the force change value to the force value only when the force change value exceeds the creep threshold value.

15. The load cell assembly of claim 13, further comprising reference value updating means for updating the first and second reference values to be equivalent to the first and second sensed values, respectively.

16. The load cell assembly of claim 15, wherein the reference value updating means updates the first and second reference values when the magnitude of the common mode change value is greater than or equal to that of the force change value.

17. The load cell assembly of claim 16, wherein the reference value updating means further comprises means for comparing the common mode change value to a noise threshold value, wherein the reference value updating means updates the first and second reference values when the common mode change value is greater than the noise threshold value.

18. The load cell assembly of claim 16, wherein the reference value updating means further comprises means for accumulating the common mode change values to provide an accumulated common mode change value, and means for comparing the accumulated common mode change value to a common mode error threshold value, and wherein the reference value updating means updates the first and second reference values when the accumulated common mode change value exceeds the common mode error threshold value.

19. A driver for generating a force value indicative of a force that is applied to a load cell assembly of the type including first and second force sensors which have complementary sensitivity to the applied force, the driver comprising:

first and second sampling means, coupled to the first and second force sensors, for periodically providing first and second sensed values, respectively, each of said first and second sensed values having a magnitude value and a direction of change;

means for determining when the directions of change in the first and second sensed values are different; and

force accumulating means, responsive to the determining means, for calculating the force value of the applied force from the magnitudes of the first and second change values.

20. The driver of claim 19, further comprising reference value updating means for updating the first and second reference values to respectively equal the first and second sensed values.

21. The driver of claim 19, wherein the characterizing means comprises:

(a) means for calculating the force change value, wherein the force change value is representative of the difference in applied force between the pair of samples;

(b) means for calculating a common mode change value representative of the difference in common mode effects between the pair of samples; and

(c) means for comparing absolute values of the force change value and the common mode change value, wherein a greater absolute value for the force change value represents a force change, and a greater absolute value for the common mode change value represents a non-force change.

22. The driver of claim 21, wherein:

(a) the force change value is representative of the difference between force sample values for the pair of samples, each force sample value for a sample being representative of the difference between (1) the difference between the first sensed value at the sample and a first reference value and (2) a scaled difference between the second sensed value at the sample and a second reference value; and

(b) the common mode change value is representative of the difference between common mode sample values for the pair of samples, each common mode sample value at a sample being representative of the sum of (1) the difference between the first sensed value at the sample and the first reference value and (2) a scaled difference between the second sensed value at the sample and the second reference value.

23. The driver of claim 22, wherein the force accumulating means further comprises means for comparing the force change value to a creep threshold value, and wherein the force calculating means only sums the force change value with the force value when the force change value exceeds the creep threshold value.

24. A method for generating a force value indicative of an applied force in a load cell assembly of the type including first and second force sensors mounted in a load cell body to exhibit complementary sensitivity to the applied force, comprising:

driving the first and second force sensors to generate first and second sensed signals, respectively;

calculating first and second change values representative of respective changes in the first and second sensed signals over a predetermined time period, each of said first and second change values having a magnitude value and a direction of change;

determining when the directions of change in the first and second change values are different; and

calculating the force value of the applied force from the magnitudes of the first and second change values.

25. The method of claim 24, further comprising the step of updating the first and second reference values to respectively equal the first and second sensed values.

26. The method of claim 24, wherein the first and second force sensors each comprise a double-ended tuning fork resonator having a resonant frequency which varies with force applied thereto, the method further comprising the step of converting the first and second sensed signals into digital first and second sensed values, respectively.

27. The method of claim 24, wherein:

(a) the calculating step includes the steps of calculating force and common mode change values, wherein the force change value is representative of the difference in applied force between a pair of force sample values, each force sample value being representative of the difference between (1) the difference between a first sensed value at the sample and a first reference value and (2) a scaled difference between a second sensed value at the sample and a second reference value, and wherein the common mode change value is representative of the difference in common mode effects between a pair of common mode sample values, each common mode sample value being representative of the sum of (1) the difference between the first sensed value at the sample and the first reference value and (2) a scaled difference between the second sensed value at the sample and the second reference value, the first and second sensed values being digital representations of the first and second sensed signals at the sample; and

(c) the determining step includes the step of comparing the absolute values of the force and common mode change values, wherein a greater absolute value for the force change value represents a force change, and a greater absolute value for the common mode change value represents a non-force change.

28. The method of claim 27, further comprising the step of comparing the force change value to a creep threshold value, and wherein the updating step sums the force change value with the force value only when the force change value exceeds the creep threshold value.

29. The method of claim 27, further comprising the step of updating a common mode value by adding the common mode change value to the common mode value when the magnitude of the common mode change value exceeds that of the force change value.

30. The method of claim 27, further comprising the step of updating the first and second reference values to be equivalent to the first and second sensed values, respectively, when the magnitude of the common mode change value is greater than or equal to that of the force change value.

31. The method of claim 30, wherein the reference value updating step includes the step of comparing the common mode change value to a noise threshold value, and wherein the reference value updating step updates the first and second reference values only when the common mode change value is less than the noise threshold value.

32. The method of claim 30, wherein the reference value updating step includes the steps of accumulating the common mode change values to provide an accumulated common mode change value and comparing the accumulated common mode change value to a common mode error threshold value, and wherein the reference value updating step updates the first and second reference values only when the accumulated common mode change value exceeds the common mode error threshold value.

33. The method of claim 24, further comprising the step of correcting the force value for span effects.