Torque-insensitive load cell

• US 4,454,770 A
• Filed: 12/24/1981
• Issued: 06/19/1984
• Est. Priority Date: 12/24/1981
• Status: Expired due to Term

• Current Assignee: Weigh-Tronix, Inc. (Illinois Tool Works Inc.)
• Original Assignee: Kistler-Morse Corp. (Danaher Corporation)
• Inventors: Kistler, Walter P.
• Primary Examiner(s): Hartary, Joseph W.
• Application Number:
  US06/334,252
• Time in Patent Office: 908 Days
• Field of Search: 177/211, 177/229, 73/862.65, 338/2, 338/5
• US Class Current: 73/862.633
• CPC Class Codes: G01G 21/24 Guides or linkages for ensuring parallel motion of the weigh-pans
• CPC Class Codes: G01G 3/1412 the supports being parallelogram shaped
• CPC Class Codes: G01L 1/2243 the supports being parallelogram-shaped

Abstract

A load cell having a parallelogram configuration formed by a pair of spaced-apart, generally parallel force-receiving members interconnected by a cantilever beam and a parallel spacer beam. The cantilever beam projects perpendicularly from one of the force-receiving members, and its end is secured to the other beam by a flexure hinge. The ends of the spacer beam are secured to the force-receiving members by respective flexure hinges. In order to maintain the parallelogram configuration of the load cell, the length of the spacer beam is equal to the length of the cantilever beam from the beam'"'"'s virtual pivot point to its end. Rotational moments imparted to the force-receiving members apply forces to the beams along their longitudinal axes without deflecting the cantilever beam, thus making the load cell insensitive to such moments. A reduced thickness portion instrumented with semiconductor strain gauges is formed in the cantilever beam near its point of attachment with the force-receiving member. The reduced thickness portion accurately positions the virtual pivot point of the beam and it concentrates the stress at the strain gauges. The load cell may be used in a scale by securing one of the load-receiving members on a base and mounting a load-receiving tray on the other load-receiving member.

Claims

1. A torque-insensitive load cell, comprising:

first and second spaced-apart force-receiving members;

a cantilever beam extending between said first and second force-receiving members, one end of said beam being connected to said first member in cantilever fashion so that the angle between said first member and said beam at the area of attachment therebetween is substantially constant, the other end of the said beam being connected to said second member through a relatively thin flexure hinge which is capable of transmitting forces to said beam while allowing said beam to freely pivot with respect to said second member;

a second beam extending between said first and second force-receiving members and having at least one of its ends connected to a respective force-receiving member by a flexure hinge which is capable of transmitting forces to said beam while allowing said beam to freely pivot with respect to said first and second members, said second beam having an effective length which is equal to the length of said first beam from its virtual pivot point to the flexure hinge connecting the end of said beam to said second member, said first and second force-receiving members being spaced apart solely by said cantilever beam and said spacer beam so that the longitudinal stress on said cantilever beam is unaffected by variations in the relative lengths of said cantilever beam and said spacer beam;

strain-sensing means mounted on said cantilever beam for providing an electrical indication of the flexing of said beam; and

means for applying a force between said first and second force-receiving members having a component which is perpendicular to said beams, thereby flexing said cantilever beam and causing said strain-sensing means to generate an electrical indication of the force applied between said force-receiving members.

2. The load cell of claim 1 wherein said second beam is a spacer beam having each of its ends connected to respective force-receiving members by flexure hinges.

3. The load cell of claim 2, further including a gauging area formed on said cantilever beam on which said strain-sensing means is mounted, said gauging area having a reduced cross-sectional area, thereby fixing the position of the virtual pivot point of said beam and concentrating the flex of said beam at said strain-sensing means.

4. The load cell of claim 3 wherein said gauging area is located closely adjacent the junction of said cantilever beam with said force-receiving member.

5. The load cell of claim 2 wherein said force-receiving members and said beams are integrally formed from a single piece of resilient material.

6. The load cell of claim 2 wherein said flexure hinges are formed by respective pairs of parallel cylindrical bores formed closely adjacent the juncture between said beams and force-receiving members, said bores being spaced apart from each other by a relatively small distance to form a relatively thin web therebetween which is highly compliant about an axis parallel to the said bores.

7. The load cell of claim 2 wherein said strain-sensing means are a pair of semiconductor strain gauges mounted on opposite surfaces of said cantilever beam from the neutral bending axis of said beam.

8. The load cell of claim 2 wherein said gauging area is located closely adjacent the juncture of said cantilever beam with said force-receiving member.

9. The load cell of claim 2, further including a base to which one of said force-receiving members is secured, a load-receiving tray mounted on the other of said force-receiving members, a bridge circuit formed at least in part by said strain-sensing means, amplifier means receiving the output of said bridge circuit, and indicator means for providing a visual indication of the magnitude of the output of said amplifier means whereby said indicator means provides an indication of the load carried by said tray.

10. A method of fabricating a load cell, comprising:

providing first and second spaced-apart force-receiving members;

providing a cantilever beam extending between said first and second force-receiving members, one end of said beam being connected to said first member in cantilever fashion so that the angle between said first member and said beam at the area of attachment therebetween is substantially constant, the other end of said beam being connected to said second member through a relatively thin flexure hinge which is capable of transmitting forces to said beam while allowing said beam to freely pivot with respect to said second member;

providing a spacer beam extending between said first and second force-receiving members and having at least one of its ends connected thereto by a flexure hinge which is capable of transmitting forces to said beam while allowing said beam to freely pivot with respect to said first and second members, said second beam having an effective length which is equal to the length of said cantilever beam from its virtual pivot point to the flexure hinge connecting the end of said beam to said second member, said first and second force-receiving members being spaced apart solely by said cantilever beam and said second beam so that the longitudinal stress on said cantilever beam is unaffected by variations in the relative lengths of said cantilever beam and said second beam;

providing strain-sensing means mounted on said beam for generating an electrical indication of the flexing of said cantilever beam; and

removing material from said cantilever beam to modify the virtual pivot point of said beam so that said load cell is insensitive to rotational moments applied between said first and second members.

11. The method of claim 10 wherein said material is removed on one side or the other of the neutral bending axis of said beam to minimize the sensitivity of said load cell to moments applied to said members about an axis parallel to the pivot axis of said virtual pivot point.

12. The method of claim 10 wherein said material is removed from one or the other lateral surface of said beam to minimize the sensitivity of said load cell to moments applied to said members about an axis parallel to the longitudinal axis of said beam.