Dynamic payload monitor

• US 5,070,953 A
• Filed: 08/20/1990
• Issued: 12/10/1991
• Est. Priority Date: 08/20/1990
• Status: Expired due to Fees

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Worrell, Dean A., Kyrtsos, Christos T.
• Primary Examiner(s): MILLER JR, GEORGE
• Application Number:
  US07/569,794
• Time in Patent Office: 477 Days
• Field of Search: 177/25, 177/14, 177/139, 177/141
• US Class Current: 177/25.14
• CPC Class Codes: E02F 9/264 Sensors and their calibration for indicating the position of the work tool
• CPC Class Codes: G01G 19/083 lift truck scale

Abstract

A dynamic payload monitor measures and displays payload weight for a loader vehicle operated on a slope by sensing the hydraulic pressure and position of the lift arm cylinders. The payload weight is computed by curve fitting the sensed cylinder pressure and position data to a second order polynomial, and then performing interpolation or extrapolation with a pair of pressure versus position reference parabolas obtained during calibration. Payload weight is corrected for errors caused by operating the loader vehicle on a slope. The weight computation algorithms used in the dynamic payload monitor are applicable to a number of work vehicles having at least one work implement linkage and at least one hydraulic cylinder for modifying the linkage geometry.

Claims

1. A method for dynamically measuring and indicating payload weight for a vehicle having at least one implement linkage and at least one cylinder for modifying said implement linkage geometry, said method comprising the steps of:

sensing the hydraulic pressure of said cylinder and responsively producing a first signal;

sensing said implement linkage geometry and responsively producing a second signal;

receiving said first and second signals and responsively deriving a preliminary payload weight in response to said first and second signals;

deriving a slope value; and

calculating a final payload weight in response to said preliminary payload weight and said slope value.

2. A method, as set forth in claim 1, wherein said step of deriving a preliminary payload weight includes the step of deriving a preliminary second order polynomial expressing lift cylinder pressure with respect to lift cylinder extension.

3. A method, as set forth in claim 2, wherein said step of deriving a slope value includes the steps of:

integrating said preliminary second order polynomial;

obtaining an ideal second order polynomial in response to said integration of said preliminary second order polynomial; and

differentiating said preliminary and ideal second order polynomials at a given lift cylinder extension thereby obtaining the slope of said preliminary and ideal second order polynomials at the given lift cylinder extension.

4. A method, as set forth in claim 3, including the step of calculating a slope function in response to said slope value.

5. A method, as set forth in claim 4, wherein said slope function is a linear function of the difference between said slope of said preliminary second order polynomial and said slope of said ideal second order polynomial.

6. A method, as set forth in claim 4, including the step of calculating a correction factor in response to said slope function and said preliminary payload weight.

7. A method, as set forth in claim 6, wherein said correction factor is a second order function of said preliminary payload weight.

8. A method, as set forth in claim 1, wherein said implement linkage includes a linkage connection pivot pin and said step of sensing said implement linkage geometry includes the step of sensing rotation of said implement linkage about said linkage connection pivot pin.

9. An apparatus for dynamically measuring and indicating payload weight for a vehicle having at least one implement linkage and at least one cylinder for modifying said implement linkage geometry, said apparatus comprising:

means for sensing the hydraulic pressure of said cylinder and responsively producing a first signal;

means for sensing said implement linkage geometry and responsively producing a second signal;

means for receiving said first and second signals and responsively deriving a preliminary payload weight in response to said first and second signals;

means for producing a slope value; and

means for calculating a final payload weight in response to said preliminary payload weight and said slope value.

10. An apparatus, as set forth in claim 9, wherein said means for receiving said first and second signals and responsively deriving a preliminary payload weight includes a means for deriving a preliminary second order polynomial expressing lift cylinder pressure with respect to lift cylinder extension and said means for producing a slope value includes:

means for integrating said preliminary second order polynomial;

means for obtaining an ideal second order polynomial in response to said integration of said preliminary second order polynomial;

means for differentiating said preliminary and ideal second order polynomials at a given lift cylinder extension thereby obtaining the slope of said preliminary and ideal second order polynomials at the given lift cylinder extension; and

means for calculating a slope function in response to said slopes of said preliminary and ideal second order polynomials.

11. An apparatus, as set forth in claim 9, wherein said implement linkage includes a linkage connection pivot pin and said means for sensing said implement linkage geometry senses rotation of said implement linkage about said linkage connection pivot pin.