Cable load sensing device

• US 5,728,953 A
• Filed: 10/04/1996
• Issued: 03/17/1998
• Est. Priority Date: 10/04/1996
• Status: Expired due to Fees

• Current Assignee: Michael J. Beus
• Original Assignee: United States Department of Energy (Government of the United States of America)
• Inventors: Beus, Michael J., McCoy, William G.
• Primary Examiner(s): Dougherty, Elizabeth L.
• Assistant Examiner(s): Noori, Max H.
• Application Number:
  US08/726,226
• Time in Patent Office: 529 Days
• Field of Search: 73/827, 73/828, 73/831, 73/833, 73/862.392, 73/862.391, 73/862.451, 73/862.46, 73/862.471, 73/862.472, 73/862.474
• US Class Current: 73/862.472
• CPC Class Codes: G01G 3/12 wherein the weighing element is in the form of a solid body stressed by pressure or tension during weighing
• CPC Class Codes: G01L 5/102 using sensors located at a non-interrupted part of the flexible member
• CPC Class Codes: G01L 5/107 for measuring a reaction force applied on an element disposed between two supports, e.g. on a plurality of rollers or gliders

Abstract

Apparatus for sensing the magnitude of a load on a cable as the cable is employed to support the load includes a beam structure clamped to the cable so that a length of the cable lies along the beam structure. A spacer associated with the beam structure forces a slight curvature in a portion of the length of cable under a cable "no-load" condition so that the portion of the length of cable is spaced from the beam structure to define a cable curved portion. A strain gauge circuit including strain gauges is secured to the beam structure by welding. As the cable is employed to support a load the load causes the cable curved portion to exert a force normal to the cable through the spacer and on the beam structure to deform the beam structure as the cable curved portion attempts to straighten under the load. As this deformation takes place, the resistance of the strain gauges is set to a value proportional to the magnitude of the normal strain on the beam structure during such deformation. The magnitude of the normal strain is manipulated in a control device to generate a value equal to the magnitude or weight of the load supported by the cable.

Claims

1. Load sensor apparatus for sensing the magnitude of a load on a cable as the cable is employed to support the load, comprising;

(a) a non-load bearing beam structure, wherein the beam structure does not bear a load in the axial direction of the cable;

(b) means for slidably attaching said beam structure to said cable so that a length of cable lies along said beam structure;

(c) spacer means associated with said beam structure for forcing a slight curvature in a portion of said length of cable under a no-load condition so that said portion of said length of cable is spaced from said beam structure to define a cable curved portion; and

(d) sensing means secured to said beam structure;

whereby as said cable is employed to support a load the load causes said cable curved portion to exert a force normal to said cable through said spacer means and on said beam structure to deform said beam structure as said cable curved portion attempts to straighten under the load and said sensing means detects the magnitude of the normal strain on said beam structure during said deformation which is proportional to the magnitude of the load on said cable.

2. The load sensor apparatus as recited in claim 1, wherein said beam structure is an elongated structure having a substantially flat first surface portion, first and second end portions and means at said first and second end portions for clamping said beam structure to said cable so that said length of cable lies along said first surface portion.

3. The load sensor apparatus as recited in claim 2, wherein said means at each of said first and second end portions for clamping said beam structure to said cable is a generally "U"-shaped clamp.

4. The load sensor apparatus as recited in claim 2, wherein said beam structure is made from a titanium alloy material.

5. The load sensor apparatus as recited in claim 4, wherein said beam structure is made from titanium alloy 6A14V.

6. The load sensor apparatus as recited in claim 4, wherein said beam structure is a laminated assembly formed from flat bars of titanium alloy.

7. The load sensor apparatus as recited in claim 2, wherein said spacer means is positioned on said first surface portion of said beam structure midway between said first and second end portions thereof and forces a curvature of less than one degree in said portion of said length of cable upon clamping said beam structure to said cable.

8. The load sensor apparatus as recited in claim 1, wherein:

said sensing means includes at least one strain gauge that provides a resistance value which is proportional to the magnitude of the normal strain on said beam structure during deformation; and

said resistance value is a component of a control device which generates a millivolt signal proportional to said resistance value and representative of the magnitude of said load supported by said cable.

9. The load sensor apparatus as recited in claim 1, wherein said beam structure, sensing means and said length of cable are all disposed within a protective housing made from a metal material and filled with a polyfoam insulation.

10. The load sensor apparatus as recited in claim 1, wherein said beam structure is elongated and said spacer means is located on and midway between the opposite ends of said elongated beam structure.