Dynamic payload monitor

• US 5,067,572 A
• Filed: 08/20/1990
• Issued: 11/26/1991
• Est. Priority Date: 08/20/1990
• Status: Expired due to Term

• Current Assignee: Caterpillar Incorporated
• Original Assignee: Caterpillar Incorporated
• Inventors: Worrell, Dean A., Kyrtsos, Christos T.
• Primary Examiner(s): Miller, Jr., George H.
• Application Number:
  US07/569,899
• Time in Patent Office: 463 Days
• Field of Search: 177/25.14, 177/139, 177/141
• US Class Current: 177/139
• 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 during tip loading by sensing the hydraulic pressure of the lift and tilt cylinders and the geometry of an implement linkage. The payload weight is computed by curve fitting the sensed lift cylinder pressure and geometry data to a second order polynomial, and then performing interpolation or extrapolation with a pair of pressure versus position reference parabolas obtained during calibration. Tilt cylinder curves are derived by curve fitting tilt cylinder pressure and lift cylinder geometry data to a third order polynomial. The tilt cylinder curves are then compared to a plurality of tabulated tilt cylinder curves. Tip loading conditions are detected and the computed payload weight is modified in response to the magnitude of the tilt cylinder pressure. 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 two hydraulic cylinders for modifying the linkage geometry.

Claims

1. An apparatus for dynamically measuring and indicating payload weight for a vehicle having at least one implement linkage including a linkage connection pivot pin, said vehicle including at least one lift cylinder and at least one tilt cylinder for modifying said implement linkage geometry, said apparatus comprising:

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

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

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

means for receiving said first, second, and third signals and responsively deriving a payload weight.

2. An apparatus, as set forth in claim 1, wherein said means for sensing implement linkage geometry senses rotation of said linkage about said linkage connection pivot pin.

3. An apparatus, as set forth in claim 1, wherein said means for receiving said first, second, and third signals and responsively deriving a payload weight produces first and second reference payload curves, and calculates an actual payload curve by interpolating between said first and second reference payload curves in response to said first signal value being within the area bounded by said reference payload curves, and by extrapolating beyond said first and second reference payload curves in response to said first signal value being outside of the area bounded by said reference payload curves.

4. An apparatus, as set forth in claim 3, wherein said means for receiving said first, second, and third signals and responsively deriving payload weight includes means for detecting tip loading conditions and modifying said payload weight in response to detecting said tip loading conditions.

5. An apparatus, as set forth in claim 3, wherein said payload curves are represented by quadratic equations.

6. An apparatus, as set forth in claim 3, wherein said means for receiving said first, second and third signals and responsively deriving payload weight includes:

means for storing a plurality of tabulated tilt cylinder curves representing tilt cylinder pressure versus lift cylinder extension;

means for deriving actual tilt cylinder curves in response to said second and third signals;

means for comparing said actual tilt cylinder curves with said tabulated tilt cylinder curves; and

means for modifying said payload weight in response to said comparison between said actual and tabulated tilt cylinder curves.

7. An apparatus, as set forth in claim 6, wherein said tilt cylinder curves are represented by third order polynomials.

8. An apparatus, as set forth in claim 3, wherein said means for receiving said first, second, and third signals and responsively deriving payload weight compensates for variable lift cylinder extension velocity by linearly shifting said payload curves.

9. A method for dynamically measuring and indicating payload weight for a vehicle having at least one implement linkage including a linkage connection pivot pin, said vehicle including at least one lift cylinder and at least one tilt cylinder for modifying said implement linkage geometry, said method comprising the steps of:

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

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

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

receiving said first, second, and third signals and responsively deriving a payload weight.

10. A method, as set forth in claim 9, wherein said step of sensing said implement linkage geometry includes the step of sensing rotation of said linkage about said linkage connection pivot pin.

11. A method, as set forth in claim 9, wherein said step of receiving said first, second, and third signals and responsively deriving payload weight includes the steps of:

producing first and second reference payload curves; and

calculating an actual payload curve by interpolating between said first and second reference payload curves in response to said first signal value being within the area bounded by said reference payload curves, and by extrapolating beyond said first and second reference payload curves in response to said first signal value being outside of the area bounded b said reference payload curves.

12. A method, as set forth in claim 11, wherein said step of receiving said first, second, and third signals and responsively deriving payload weight includes the steps of detecting tip loading conditions and modifying said payload weight in response to detecting said tip loading conditions.

13. A method, as set forth in claim 11, wherein said step of receiving said first, second, and third signals and responsively deriving payload weight includes the steps of:

deriving actual tilt cylinder curves in response to said second and third signals;

comparing said actual tilt cylinder curves with tabulated tilt cylinder curves; and

modifying said payload weight in response to said comparison between said actual and tabulated tilt cylinder curves.

14. A method, as set forth in claim 11, wherein said step of receiving said first, second, and third signals and responsively deriving payload weight includes the step of compensating for variable lift cylinder extension velocity by linearly shifting said payload curves.