Dynamic payload monitor

• US 4,919,222 A
• Filed: 03/15/1989
• Issued: 04/24/1990
• Est. Priority Date: 03/15/1989
• 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
• Application Number:
  US07/324,517
• Time in Patent Office: 405 Days
• Field of Search: 177/139, 177/141, 177/146, 177/147, 177/25.14
• 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 19/10 having fluid weight-sensitive devices
• CPC Class Codes: G01G 5/04 with means for measuring the pressure imposed by the load on a liquid pressure gauges per se G01L

Abstract

A dynamic payload monitor measures and displays payload weight for a loader vehicle 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. 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. An apparatus for dynamically measuring and indicating payload weight for a vehicle having at least one implement linkage including a linkage connection pivot pin, and at least one cylinder for modifying said implement linkage geometry, said apparatus comprising:

means for delivering a first signal in response to sensing the hydraulic pressure of said cylinder;

means for delivering a second signal in response to sensing rotation of said implement linkage about said linkage connection pivot pin; and

means for deriving payload weight in response to said first and second signals.

2. The apparatus, as set forth in claim 1, wherein said second signal represents said cylinder extension.

3. The apparatus, as set forth in claim 1, wherein said payload weight deriving means produces first and second reference payload parabolic curves, receives said first and second signals, and calculates an actual payload parabolic 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. The apparatus, as set forth in claim 3, wherein said payload weight deriving means calculates said first and second reference payload curves in response to measuring respective first and second reference payload weights.

5. The apparatus, as set forth in claim 4, wherein said vehicle includes a payload carrier, said first reference payload weight is the empty weight of said carrier and said second reference payload weight is the weight of said carrier loaded with a predetermined known mass.

6. The apparatus, as set forth in claim 3, wherein each of said payload curves is represented by a second order polynomial equation.

7. A method for dynamically measuring and indicating payload weight for a vehicle having at least one lift cylinder for elevating a payload carrier, said vehicle generally executing a work cycle including lifting said payload carrier, said method comprising the steps of:

sensing said lift cylinder hydraulic pressure during said work cycle;

delivering a plurality of first signals in response to said sensed pressure;

sensing said lift cylinder extension during said work cycle;

delivering a plurality of second signals in response to said sensed extension;

deriving a second order polynomial geometric representation for said plurality of first and second signals;

comparing said geometric representation to at least one other second order polynomial geometric representation of a known reference payload weight; and

calculating an actual payload weight in response to said comparison.

8. A method, as set forth in claim 7, wherein said lift cylinder pressure and extension sensing steps are performed only during the payload lifting portion of said work cycle.

9. A method, as set forth in claim 7, wherein said polynomial is obtained by filtering said first and second signals.

10. A method, as set forth in claim 7, wherein said geometric representation of a known payload weight includes a second order polynomial derived from a plurality of first and second signals sensed during a lift of an empty payload carrier.

11. A method, as set forth in claim 10, wherein said geometric representation of a known payload weight further includes another second order polynomial derived from a plurality of first and second signals sensed during a lift of a payload carrier having a predetermined known weight.

12. A method, as set forth in claim 11, wherein said comparing step includes one of interpolation between and extrapolation beyond said empty payload carrier polynomial and said predetermined known weight payload carrier polynomial.

13. A method, as set forth in claim 12, wherein said comparing step interpolates between said empty and known payload polynomials in response to said first signal value being within the area bounded by said polynomials, and extrapolates beyond said polynomials in response to said first signal value being outside of the area bounded by said polynomials.

14. A method, as set forth in claim 7, wherein said vehicle further includes a lift arm, said lift arm being pivotally attached to said vehicle by a rotatable pivot pin, whereby said lift cylinder extension sensing step includes sensing rotation about said rotatable pin.

15. A method, as set forth in claim 7, wherein said payload weight calculation step includes compensating for variable cylinder extension velocity by linearly shifting said second order polynomials.

16. 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 delivering a first signal in response to sensing the hydraulic pressure of said cylinder;

means for delivering a second signal in response to sensing said linkage geometry with respect to said vehicle;

means for deriving payload weight in response to said first and second signals; and

wherein said payload weight deriving means produces first and second reference payload parabolic curves, receives said first and second signals, and calculates an actual payload parabolic 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.

17. The apparatus, as set forth in claim 16, wherein said payload weight deriving means calculates said first and second reference payload curves in response to measuring first and second reference payload weights.

18. The apparatus, as set forth in claim 17, wherein said vehicle includes a payload carrier, said first reference payload weight is the empty weight of said carrier and said second reference payload weight is the weight of said carrier loaded with a predetermined known mass.

19. The apparatus, as set forth in claim 16, wherein each of said payload curves is represented by a second order polynomial equation.

20. The apparatus, as set forth in claim 19, wherein said payload weight driving means compensates for variable cylinder extension velocity by linearly shifting said second order polynomials.