PLANAR LOAD CELL ASSEMBLY

Abstract

An assembly including a load cell body having contiguous cutout windows, each formed by a pair of cutout lines and connected by a cutout base, the second window being transversely bounded by the first window,; measuring beams, disposed generally along edges of the body, each defined by a respective line of the first pair of cutout lines; first and second arrangements, each having a pair of flexure beams connected by first and second bases, respectively; a loading element, extending from the second base; and strain gages, attached to the beams, and a transverse flexural arrangement.

Claims

1. A planar load cell assembly comprising: at least one load cell arrangement disposed on a single metal load cell body, said load cell body having a primary axis, a central longitudinal axis, and a transverse axis disposed transversely with respect to said primary and central longitudinal axes, a broad dimension of said load cell body being disposed perpendicular to said primary axis; each said load cell arrangement including: (a) a first contiguous cutout window passing through said broad dimension and formed by a first pair of cutout lines disposed generally along or parallel to said central longitudinal axis, and connected by a first cutout base; (b) a pair of measuring beams, disposed along opposite edges of said load cell body, and generally parallel to said central longitudinal axis, each of said measuring beams longitudinally defined by a respective cutout line of a first pair of cutout lines, each of said pair of cutout lines disposed generally along or parallel to said central longitudinal axis; (c) at least one strain gage, fixedly attached to a surface of a measuring beam of said measuring beams; (d) a loading element, longitudinally defined by an innermost pair of said cutout lines, and extending from an innermost flexure base, said transverse axis passing through said loading element, said loading element adapted to receive a vertical load; and at least one of the following structural limitations: (i) a hinge disposed in said metal load cell body, said hinge having a transverse orientation with respect to said primary and central longitudinal axes; (ii) at least one transverse flexure beam disposed in said metal load cell body, said hinge having a transverse orientation with respect to said primary and central longitudinal axes; and (iii) a transverse flexure arrangement disposed within said first contiguous cutout window.

2. The planar load cell assembly of claim 1, wherein an angle of deviation from the transverse axis of said transverse orientation is within a range of 0° to 70°, 0° to 60°, 0° to 45°, 0° to 40°, 0° to 35°, 0° to 30°, 0° to 25°, or 0° to 20°.

3. The planar load cell assembly of claim 1, wherein said transverse flexure arrangement is disposed so as to mechanically bridge or connect between said loading element and a spring arrangement of said load cell arrangement.

4. A planar load cell assembly comprising: at least one load cell arrangement disposed on a single metal load cell body, said load cell body having a primary axis, a central longitudinal axis, and a transverse axis disposed transversely with respect to said primary and central longitudinal axes, a broad dimension of said load cell body being disposed perpendicular to said primary axis; each said load cell arrangement including: (a) at least a first pair of cutout lines, including an outermost pair of cutout lines, said outermost pair of cutout lines disposed generally along or generally parallel to said central longitudinal axis, and passing through said broad dimension, said outermost pair of cutout lines intercommunicating via a first transverse cutout base, to form a first contiguous cutout window passing through said broad dimension; (b) a pair of measuring beams, disposed along opposite edges of said load cell body, and generally parallel to said central longitudinal axis, each of said measuring beams longitudinally defined by a respective cutout line of said outermost pair of said cutout lines; (c) at least one strain gage, fixedly attached to a surface of a measuring beam of said measuring beams; (d) a loading element, defined by a cutout arrangement, said transverse axis passing through said loading element, said loading element adapted to receive a vertical load; and (e) a transverse flexure arrangement.

5. A double-ended load cell assembly having two load cell arrangements disposed on a single metal load cell body, each of said load cell arrangements being in accordance with

6. The planar load cell assembly of claim 1, wherein said metal load cell body is made of a magnesium alloy, wherein a magnesium content of said magnesium alloy, by weight or by volume, is within a range of 85% to 98%, 88% to 98%, 90% to 98%, or 92% to 98%.

7. The planar load cell assembly of claim 6, wherein said magnesium alloy is selected or adapted such that an elastic module (E) thereof is lower than that of load-cell grade aluminum alloy 2023.

8. The planar load cell assembly of claim 1, wherein said loading element, said second pair of flexure beams, said first pair of flexure beams, and said pair of measuring beams are mechanically disposed in series, such that a load disposed on said loading element acts upon said second pair of flexure beams prior to said first pair of flexure beams, and on said first pair of flexure beams prior to said pair of measuring beams.

9. A double-ended load cell assembly having two load cell arrangements disposed on a single metal load cell body, each of said load cell arrangements being in accordance with claim 4.

10. The planar load cell assembly of claim 4, wherein said loading element, said second pair of flexure beams, said first pair of flexure beams, and said pair of measuring beams are mechanically disposed in series, such that a load disposed on said loading element acts upon said second pair of flexure beams prior to said first pair of flexure beams, and on said first pair of flexure beams prior to said pair of measuring beams.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0054] The invention is herein described, by way of example only, with reference to the accompanying drawings. With specific reference now to the drawings in detail, it is stressed that the particulars shown are by way of example and for purposes of illustrative discussion of the preferred embodiments of the present invention only, and are presented in the cause of providing what is believed to be the most useful and readily understood description of the principles and conceptual aspects of the invention. In this regard, no attempt is made to show structural details of the invention in more detail than is necessary for a fundamental understanding of the invention, the description taken with the drawings making apparent to those skilled in the art how the several forms of the invention may be embodied in practice. Throughout the drawings, like-referenced characters are used to designate like elements.

[0055] In the drawings:

[0056] FIG. 1 is a block diagram of showing a series connection between the loaded loading beam and the measuring beam, via a flexure arrangement having at least two flexures, within a spring arrangement of a load cell assembly, according to embodiments of the present invention;

[0057] FIG. 2 is a conventional schematic diagram of the strain gage electronics;

[0058] FIG. 3A is a top, schematic view of a planar load cell assembly, according to embodiments of the present invention;

[0059] FIG. 3B is a side, schematic view of the planar load cell assembly of FIG. 1A;

[0060] FIG. 4 is an exemplary displacement plot showing a deflection of a flexure and load cell arrangement similar to that of FIG. 3A, in response to a vertical load, according to embodiments of the present invention;

[0061] FIG. 5A is a partial, schematic view of the planar load cell assembly of FIG. 3A;

[0062] FIG. 5B is a partial, top schematic view of a planar load cell assembly similar to that of FIG. 3A, and having a pair of slots disposed on the loading element;

[0063] FIG. 5C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 5B, in response to a vertical load;

[0064] FIG. 5D is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 5B, in response to a moment along the transverse (Z) axis;

[0065] FIG. 5E is an exemplary pivot structure of the flexure arrangement and the load cell arrangement of FIG. 5B;

[0066] FIG. 6A is a partial, top schematic view of a planar load cell assembly similar to that of FIG. 3A, and having a pair of slots ending in pivot cutout lines disposed on the loading element;

[0067] FIG. 6B is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 6A, in response to a vertical load;

[0068] FIG. 6C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 6A, in response to a moment (Mz) along the transverse (Z) axis;

[0069] FIG. 6D is an exemplary pivot structure of the flexure arrangement and the load cell arrangement of FIG. 6A;

[0070] FIG. 7A is a partial, schematic view of a planar load cell assembly having three flexure beams between the loading element and the measuring beam;

[0071] FIG. 7B is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 7A, in response to a vertical load;

[0072] FIG. 7C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 7A, in response to a moment (Mz) along the transverse (Z) axis;

[0073] FIG. 8A and 8B are schematic top and side views of a double-ended planar assembly load cell assembly having two planar load cells sharing a single, integral load cell body;

[0074] FIG. 9 is a schematic top view of an inventive planar load cell assembly having four planar load cells sharing a single, integral load cell body, each planar load cell assembly having three flexure beams between the loading element and the measuring beam, as in FIG. 7A;

[0075] FIG. 10 is a block diagram of a weighing scale or load cell assembly, according to embodiments of the present invention;

[0076] FIG. 11 is an exploded perspective view of a planar weighing scale or load cell assembly, according to embodiments of the present invention;

[0077] FIG. 12A is an exploded perspective view of a planar weighing scale or load cell assembly having a base plate, according to embodiments of the present invention; and

[0078] FIG. 12B is schematic cross-sectional view of the planar weighing scale or load cell assembly of FIG. 12A.

[0079] FIG. 13 is a block diagram of showing a series connection between the loaded loading beam and the measuring beam, via a flexure arrangement having at least two flexures, within a spring arrangement of a load cell assembly, according to embodiments of the present invention;

[0080] FIG. 14 is a conventional schematic diagram of the strain gage electronics;

[0081] FIG. 15A is a top, schematic view of a planar load cell arrangement, according to embodiments of the present invention;

[0082] FIG. 15B is a top, schematic view of a planar load cell body, according to embodiments of the present invention;

[0083] FIG. 16 is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell body of FIG. 3A, in response to a moment (Mz) along the transverse (Z) axis;

[0084] FIGS. 17A-17E provide top, schematic views of various planar load cell bodies, according to embodiments of the present invention;

[0085] FIG. 18 is a block diagram of a weighing scale or load cell assembly, according to embodiments of the present invention;

[0086] FIG. 19 is an exploded perspective view of a planar weighing scale or load cell assembly, according to embodiments of the present invention;

[0087] FIG. 20 is an exploded perspective view of a planar weighing scale or load cell assembly having a base plate, according to embodiments of the present invention;

[0088] FIGS. 21A and 21B are top views of (as yet unpublished) planar load cell assemblies of the inventor;

[0089] FIG. 21C is a top view of a planar load cell assembly according to the present invention; and

[0090] FIG. 21D is a top, schematic view of the inventive planar load cell assembly of FIG. 21C.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0091] The principles and operation of the low-profile or planar load cell assembly according to the present invention may be better understood with reference to the drawings and the accompanying description.

[0092] Before explaining at least one embodiment of the invention in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of the components set forth in the following description or illustrated in the drawings. The invention is capable of other embodiments or of being practiced or carried out in various ways. Also, it is to be understood that the phraseology and terminology employed herein is for the purpose of description and should not be regarded as limiting.

[0093] Load cells with low profiles may have a characteristically low amplitude signal. Given limitations in the total weight to be measured, and the inherent sensitivity of load cells, the performance of such devices may be compromised by a high noise-to-signal ratio and by unacceptable settling times. Various embodiments of the present invention resolve, or at least appreciably reduce, parasitic noise issues associated with typical low profile load cells and enable high accuracy weight measurements.

[0094] FIG. 1 is a block diagram schematically showing the operation of a spring arrangement, in loaded or operative mode, according to aspects of the present invention. Loading of the spring arrangement is effected by placing a load on, or below, the loading beam, depending on whether the loading beam is anchored to the weighing platform, or to the weighing base. The loading beam may also be referred to as the “loading element” or as the “load-receiving element” or “load-supporting element” (depending on the configuration) of the load cell assembly. The spring arrangement has at least one flexure arrangement having at least two flexures or flexural elements operatively connected in series. The flexure arrangement is operatively connected, at a first end, to the loading beam, and at a second end, to the free or adaptive end of at least one measuring beam.

[0095] Substantially as shown, the flexure arrangement has n flexures (n being an integer) operatively connected in series, the first of these flexures being operatively connected to the loading beam, and the ultimate flexure of the n flexures being operatively connected in series to a second flexure, which in turn, is operatively connected to the first flexure in an assembly of m flexures (m being an integer), operatively connected in series. The ultimate flexure of the m flexures is operatively connected, in series, to a measuring beam of the spring arrangement. Associated with the measuring beam is at least one strain gage, which produces weighing information with respect to the load.

[0096] The inventor has discovered that at least two of such flexure arrangements, disposed in parallel, may be necessary for the loading element to be suitably disposed substantially in a horizontal position (i.e., perpendicular to the load). In some embodiments, and particularly when extremely high accuracy is not necessary, a single flexure disposed between the loading beam and the measuring beam may be sufficient.

[0097] This single flexure load cell arrangement may also exhibit increased crosstalk with other load cell arrangements (weighing assemblies may typically have 4 of such load cell arrangements for a single weighing platform). For a given nominal capacity, the overload capacity may also be compromised with respect to load cell arrangements having a plurality of flexures disposed in series between the load receiving beam and the measuring beam. This reduced overload capacity may be manifested as poorer durability and/or shorter product lifetime, with respect to load cell arrangements having a plurality of flexures disposed in series. Nonetheless, the overall performance of the single-flexure arrangement may compare favorably with conventional weighing apparatus and load cell arrangements. In any event, for this case, m+n=−1, which is the lowest value of m+n flexures for the present invention.

[0098] Typically, there are 4 strain gages per loading beam. FIG. 2 provides a conventional schematic diagram of the strain gage electronics, which may be used in, or with, the load cell assemblies and weighing modules of the present invention. The strain gages may be configured in a Wheatstone bridge configuration, a configuration that is well known to those of skill in the art. The load cell system may further include a processing unit, such as a central processing unit (CPU). The processing unit may be configured to receive the load or strain signals (e.g., from 4 strain gages SG1-SG4) from each particular load cell and to produce a weight indication based on the load signals, as is known to those of ordinary skill in the art.

[0099] With reference now to the FIGS. 3A and 3B, FIG. 3A is a top, schematic view of a planar load cell assembly 100, according to an embodiment of the present invention; FIG. 3B is a side, schematic view of the planar load cell assembly of FIG. 3A.

[0100] Referring collectively to FIGS. 3A and 3B, a load cell body 125 may be made from a block of load cell quality metal or alloy. Particularly advantageous embodiments employing particular magnesium alloys will be described hereinbelow.

[0101] Load cell body 125 may be fixed to a weighing assembly via one or more mounting holes or elements 142. A 1.sup.st contiguous cutout window 116 passes from a top face 110 through a bottom face 112, perpendicularly through the broad dimension (i.e., with respect to the other 2 dimensions of a three-dimensional Cartesian system) of load cell body 125. 1.sup.st contiguous cutout window 116 may be generally C-shaped or U-shaped, and may have arms or a pair of cutout lines 118a, 118b running generally parallel to a central longitudinal axis 102 of load cell body 125, and connected or made contiguous by a cutout line or cutout base 118c. Both central longitudinal axis 102 and a transverse axis 104, disposed transversely thereto, run generally parallel to the broad dimension of load cell body 125. Both of these axes are oriented in perpendicular fashion with respect to a primary axis 114. The thickness of load cell body 125 perpendicular to primary axis 114 is typically within a range of 2 mm to 10 mm, and is designated W.sub.LCB.

[0102] Long sides 105a and 105b of load cell body 125 run generally along, or parallel to, central longitudinal axis 102.

[0103] As shown, measuring beams or spring elements 107a and 107b are each disposed between respective cutout lines 118a and 118b, and respective long sides 105a and 105b of load cell body 125, distal to cutout lines 118a and 118b with respect to transverse axis 104. When planar load cell assembly 100 is disposed in a vertically loaded position, the free end of each of beams 107a and 107b may be held in a fixed relationship, substantially perpendicular to the vertical load, by an end block 124 disposed at a free end 123 of load cell body 125.

[0104] A 2.sup.nd contiguous cutout window 126 also passes from top face 110 through bottom face 112, perpendicularly through the broad dimension of load cell body 125. 2.sup.nd contiguous cutout window 126 may be generally C-shaped or U-shaped, and may have arms or a pair of cutout lines 128a, 128b running generally parallel to central longitudinal axis 102, and connected or made contiguous by a cutout line or cutout base 128c. 2.sup.nd contiguous cutout window 126 may be enveloped on three sides by 1.sup.st contiguous cutout window 116 (such that the 2.sup.nd contiguous cutout window is transversely bounded by the 1.sup.st contiguous cutout window). The orientation of 2.sup.nd contiguous cutout window 126 may be 180° (i.e., generally opposite) with respect to 1.sup.st contiguous cutout window 116.

[0105] A 3.sup.rd contiguous cutout window 136 also passes from top face 110 through bottom face 112, perpendicularly through the broad dimension of load cell body 125. 3.sup.rd contiguous cutout window 136 may be generally C-shaped or U-shaped, and may have arms or a pair of cutout lines 138a, 138b running generally parallel to central longitudinal axis 102, and connected or made contiguous by a cutout line or cutout base 138c. 3.sup.rd contiguous cutout window 136 may be enveloped on three sides by 2.sup.nd contiguous cutout window 126 (such that the 3.sup.rd contiguous cutout window is transversely bounded by the 2.sup.nd contiguous cutout window). The orientation of 3.sup.rd contiguous cutout window 136 may be 180° (i.e., generally opposite) with respect to 2.sup.nd contiguous cutout window 126 (and generally aligned with 1.sup.st contiguous cutout window 116).

[0106] Load cell body 125 has a first flexure arrangement having a first pair of flexure beams 117a, 117b disposed along opposite sides of central longitudinal axis 102, and distal and parallel thereto. First pair of flexure beams 117a, 117b may be longitudinally disposed between the first pair of cutout lines and the second pair of cutout lines, and mechanically connected or coupled by a first flexure base 119.

[0107] Load cell body 125 has a second flexure arrangement having a second pair of flexure beams 127a, 127b disposed along opposite sides of central longitudinal axis 102, and distal and parallel thereto. Second pair of flexure beams 127a, 127b may be longitudinally disposed between the first pair of cutout lines and the second pair of cutout lines, and mechanically connected or coupled by a second flexure base 129.

[0108] Contiguous cutout window 136 defines a loading element 137 disposed therein. Loading element 137 is longitudinally defined by 3.sup.rd pair of cutout lines 138a and 138b, and is connected to, and extends from, second flexure base 129.

[0109] The various cutout lines described above may typically have a width (W.sub.CO) of 0.2 mm to 5 mm, and more typically, 0.2 mm to 2.5 mm, 0.2 mm to 2.0 mm, 0.2 mm to 1.5 mm, 0.2 mm to 1.0 mm, 0.2 mm to 0.7 mm, 0.2 mm to 0.5 mm, 0.3 mm to 5 mm, 0.3 mm to 2.5 mm, 0.3 mm to 2.0 mm, 0.3 mm to 1.5mm, 0.3 mm to 1.0 mm, 0.3 mm to 0.7 mm, 0.3 mm to 0.6 mm, or 0.3 mm to 0.5 mm.

[0110] In some embodiments, the ratio of W.sub.CO to W.sub.LCB (W.sub.CO/W.sub.LCB) is at most 0.5, at most 0.4, at most 0.3, at most 0.25, at most 0.2, at most 0.15, at most 0.12, at most 0.10, at most 0.08, at most 0.06, or at most 0.05.

[0111] In some embodiments, the ratio of W.sub.CO to W.sub.LCB (W.sub.CO/W.sub.LCB) is within a range of 0.03 to 0.5, 0.03 to 0.4, 0.03 to 0.3, 0.03 to 0.2, 0.03 to 0.15, 0.03 to 0.10, 0.04 to 0.5, 0.04 to 0.4, 0.04 to 0.3, 0.04 to 0.2, 0.04 to 0.15, 0.04 to 0.10, 0.05 to 0.5, 0.05 to 0.4, 0.05 to 0.3, 0.05 to 0.2, 0.05 to 0.15, or 0.05 to 0.10. Loading element 137 may also include a hole 140, which may be a threaded hole, for receiving a load, e.g., for receiving or connecting to an upper, weighing platform, or for supporting a load, e.g., connecting to a base, leg, or support (disposed below load cell body 125) of a weighing system (described with respect to FIG. 11). Load-receiving hole 140 may be positioned at an intersection of central longitudinal axis 102 and transverse axis 104.

[0112] In the exemplary embodiment provided in FIGS. 3A and 3B, first and second flexure arrangements form a flexure arrangement 180, mechanically disposed between loading element 137 and measuring beams or spring elements 107a and 107b.

[0113] At least one strain gage, such as strain (or “strain-sensing”) gages 120, may be fixedly attached to a surface (typically a top or bottom surface) of each of measuring beams 107a and 107b. Strain gages 120 may be adapted and positioned to measure the strains caused by a force applied to the top of the “free” or “adaptive” side 123 of load cell body 125. When a vertical load acts on free end (i.e., an end unsupported by the base, as shown in FIG. 4) 123 of load cell body 125, load cell body 125 undergoes a slight deflection or distortion, with the bending beams assuming a double-bending configuration having an at least partial, and typically primarily or substantially, double-bending behavior. The distortion is measurably sensed by strain gages 120.

[0114] It may thus be seen that planar load cell assembly 100 is a particular case of a load cell assembly having the load beam and spring arrangement of FIG. 1. In this case, the number of intermediate flexures is 2, such that m and n both equal zero. In addition, the intermediate flexures are intermediate flexure beam pairs connected by a flexure base. Similarly, the measuring beams are connected at a first end by the fixed end of load cell body 125, and at the opposite end by adaptive end 124 of load cell body 125.

[0115] A load cell body 125 may be made from a block of load cell quality metal or alloy. For example, load cell quality aluminum is one conventional and suitable material. In some embodiments, the alloy may advantageously be a magnesium alloy, typically containing at least 85%, at least 90%, and in some cases, at least 92%, at least 95%, or at least 98% magnesium, by weight or by volume. The magnesium alloy should preferably be selected to have an elastic module (E) that is lower, and preferably, significantly lower, than that of aluminum.

[0116] FIG. 4 is an exemplary displacement plot showing a deflection of the flexure arrangements and measuring beams, according to embodiments of the present invention. The flexure arrangements and measuring beams of the planar load cell assembly should be dimensioned and structured such that under loading in an operative mode, the broad face of loading element 137 is close to 90° (within ±5° within ±3°, or within ±2°, within ±1.5 °, within ±1.0°, within ±0.5°, within ±0.3°, within ±0.25°, within ±0.20°, within ±0.15°, within ±0.12°, or within ±0.10°, with respect to the vertical or the direction of the load (denoted in FIG. 4 by the 4 arrows pointing down towards the measuring beams of the load cell assembly), at “full capacity” or “nominal capacity” of the load cell. The closer such a configuration is to 90°, the greater the weighing accuracy.

[0117] As used herein in the specification and in the claims section that follows, the term “nominal capacity”, and the like, as known in the art, is the load that effects 1 microstrain (0.1% of the strain) in the length of the measuring beam.

[0118] Alternatively, with the low-profile load cell assembly disposed in an operative or weighing mode, and with a load disposed on the loading element so as to achieve the nominal load capacity, an angle of a top surface of the loading element, with respect to horizontal, is within ±3°, within ±2°, within ±1.5°, within ±1°, within ±0.8°, within ±0.5°, within ±0.3°, within ±0.25°, within ±0.20°, within ±0.15°, within ±0.12°, within ±0.10°, within ±0.08°, within ±0.06°, within ±0.05°, within ±0.04°, within ±0.035°, within ±0.030°, within ±0.025°, or within ±0.020°.

[0119] FIG. 5A is a partial, schematic view of the planar load cell assembly of FIG. 3A, in which the lengths and widths of measuring beams 107a-b (L.sub.mb, W.sub.mb) are defined. Similarly, the lengths and widths of the first pair of flexure beams 117a, 117b (L.sub.F1, W.sub.F1) and the second pair of flexure beams 127a, 127b (L.sub.F2, W.sub.F2) are defined.

[0120] For these variables, a set of dimensionless ratios K.sub.mb, K.sub.F1, and K.sub.F2 are defined as:

K.sub.mb=W.sub.mb/L.sub.mb; K.sub.F1=W.sub.F1/L.sub.F1; and K.sub.F2=W.sub.F2/L.sub.F2;

Typically, at least one or both of K.sub.F1/K.sub.mb and K.sub.F2/K.sub.mb are within a range of 0.75 to 1.25, 0.8 to 1.2, 0.85 to 1.15, 0.9 to 1.1, or 0.92 to 1.08.

[0121] In FIG. 5A, a length D3 of second flexure base 129, as shown, is defined as the minimum distance, parallel to central longitudinal axis 102, between cutout base 128c of 2.sup.nd contiguous cutout window 126 and cutout lines 138a, 138b of 3.sup.rd contiguous cutout window 126 (all shown in FIG. 3A). Also defined is a length L3, which as shown, is the length of loading element 137 parallel to central longitudinal axis 102 (ending at the end of cutout lines 138a or 138b juxtaposed with second flexure base 129).

[0122] The inventor has discovered that in various embodiments of the present invention, and optionally, to achieve improved weighing accuracy, the ratio L3/D3 is preferably within a range of 3 to 7 or 3.5 to 6.5, and more typically, within a range of 3.8 to 6.4 to 5.8, 4.2 to 5.6, 4.4 to 5.4, or 4.6 to 5.2.

[0123] FIG. 5B is a partial, top schematic view of a planar load cell assembly 500 similar to that of FIG. 3A, and having a pivot structure 590 including a pair of slots such as rounded or curved slots (585, 586) disposed on the loading element 537. The rounded slots may be disposed such that the slot arms (such as 587a, 587b of slot 585) face each other, to form a detached generally rounded, circular or generally oval or ovoid structure. The shortest distance between the slot arms of curved slots 585 and 586 is denoted by D1. The diameter, or largest distance between the slot arms 587a, 587b of an individual curved slot 585 is denoted by Lslot. The height, or largest distance between the slot arms 587a, 587b of an individual curved slot 585 is denoted by Hslot. The width of an individual slot 585 is denoted by Wslot, and may be as narrow as practically possible, typically 0.2-1.0 mm and more typically, 0.2-0.5 mm. The width of the loading element is denoted by W.sub.LE. Typically, D1 is less than Hslot, Wslot and W.sub.LE.

[0124] Curved slots 585 and 586 may appreciably increase the elasticity of the load cell arrangement, particularly when moments having a significant component parallel to the Z-Z axis (the “transverse axis”) are applied. Curved slots 585 and 586 may be somewhat rotated in orientation so as to further increase the elasticity of the load cell arrangement, particularly when moments having a significant component perpendicular to the Z-Z axis (parallel to the central longitudinal axis) are applied.

[0125] FIG. 5C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 5B.

[0126] FIG. 5D is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 5B, in response to a moment along the transverse (Z) axis. The arrangement includes an exemplary pivot structure, better viewed in FIG. 5E. Such a pivot structure may provide additional, appreciable flexibility when a moment Mz is applied at or near the transverse Z-Z axis (shown in FIG. 5B). This additional elastic and reversible flexibility may appreciably reduce, or make insignificant, the deleterious effects of such a moment on the measurement beams/strain gages.

[0127] FIG. 6A is a partial, top schematic view of a planar load cell assembly 600 similar to that of FIGS. 3A and 5B, and having a pivot structure 690 including slots or curved slots (typically a pair of curved slots such as slot 685) whose arms end in pivot cutout lines 691 disposed on the loading element. The length (Lsec-slot) of such pivot cutout lines 691 exceeds the width of the curved slots (Wslot shown in FIG. 5B), e.g., by at least 1 mm, at least 2 mm, at least 3 mm, or at least 4 mm. Typically, Lsec-slot is at most 20 mm, at most 15 mm, at most 10 mm, or at most 8 mm. FIG. 6B is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 6A, in response to a vertical load.

[0128] FIG. 6C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 6A, in response to a moment (Mz) along the transverse (Z) axis. The deflection is an elastic deflection. The arrangement includes an exemplary pivot structure, better viewed in FIG. 6D. As described above, such a pivot structure may provide additional, appreciable flexibility when a moment Mz is applied at or near the transverse Z-Z axis. This additional elastic and reversible flexibility may appreciably reduce, or make insignificant, the deleterious effects of such a moment on the measurement beams/strain gages. Moreover, the additional one or more pivot cutout lines 691 in the arrangement of FIGS. 6C-D may provide the pivot structure with appreciably increased flexibility with respect to the pivot structure provided in FIG. 5E.

[0129] It will be appreciated that the cutout lines on the pivot structure may be oriented so as to exhibit increased flexibility to moments applied along the longitudinal axis as well.

[0130] FIG. 6D is an exemplary pivot structure of the flexure arrangement and the load cell arrangement of FIG. 6A.

[0131] FIG. 7A is a partial, schematic view of a planar load cell assembly 700 having three flexure beams 717b, 727b, 737b, disposed in series with respect to the loading element 747 and the measuring beam 707b. In terms of the schematic arrangement shown in FIG. 1, m+n=1.

[0132] FIG. 7B is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 7A, in response to a vertical load, according to embodiments of the present invention. As described hereinabove, the flexure arrangements and measuring beams of the planar load cell assembly should be dimensioned and structured such that under loading in an operative mode, the broad face of the loading element is close to 90° (within ±5° within ±3°, or within ±2°, within ±1.5°, within ±1.0°, within ±0.5°, within ±0.3°, within ±0.25°, within ±0.20°, within ±0.15°, within ±0.12°, or within ±0.10°, with respect to the vertical or the direction of the load (denoted in FIG. 4 by the 4 arrows pointing down towards the measuring beams of the load cell assembly), at “full capacity” or “nominal capacity” of the load cell. The closer such a configuration is to 90°, the greater the weighing accuracy.

[0133] FIG. 7C is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 7A, in response to a moment (Mz) along the transverse (Z-Z) axis.

[0134] FIG. 8A and 8B are schematic top and side views of a double-ended planar load cell assembly 500 having two planar load cell assemblies 100A, 100B, substantially similar or identical to those described hereinabove, but sharing a common, integral load cell body, and generally disposed at opposite ends thereof, optionally symmetrically about a central transverse axis (Z-Z) of the load cell body.

[0135] FIG. 9 is a schematic top view of an inventive planar load cell assembly having four planar load cells sharing a single, integral load cell body, each planar load cell assembly having three flexure beams between the loading element and the measuring beam, as in FIG. 7A. Typically, a load cell assembly may employ solely these four planar load cells. Such an arrangement may exhibit appreciably reduced crosstalk between load cells, with respect to 4 individual load cell bodies, or with respect to 2 double-ended planar load cell assemblies.

[0136] FIG. 10 is a block diagram of a weighing scale or load cell assembly. An object to be weighed is placed on the top plate of a weighing scale of the present invention. During operation, vertical forces applied to the top plate are transferred to one or more of the inventive load cell assemblies (e.g., load cell assembly 100) configured to measure vertical forces. Electrical signals containing, or correlated with, weight information, are communicated with a processor. The processor processes the signals, or adaptations thereof, to produce weight information, and may then transmit this weight information, for example, to a display device. A processor port may also be available for maintenance, calibration or firmware updates.

[0137] FIG. 11 is an exploded view of an exemplary weighing scale or load cell assembly 700, according to one embodiment of the present invention. Weighing scale 700 is typically a low-profile or (ultra-low profile) planar weighing scale, substantially as shown. Weighing scale 700 may include at least one load cell assembly such as load cell assembly 705 (e.g., 4 of load cell assemblies 105, as provided and described hereinabove), or at least one double-ended planar load cell assembly (as shown in FIG. 5B), by way of example, 2 of such double-ended planar load cell assemblies.

[0138] Weighing scale 700 has a solid top plate 720 disposed above load cell assemblies 705, which may attach to load cell assembly 705 via mounting holes or elements 742, with shims or adapter plates 730 disposed therebetween. In the embodiment shown in FIG. 7, each load cell assembly 705 is supported by a base such as weighing scale leg 750. In this embodiment, leg 750 may be attached to, or associated with, load cell assembly 705 via hole 740. Typically, an upper portion of leg 750, or an element associated therewith (not shown), may protrude up through hole 740.

[0139] FIG. 12A is an exploded perspective view of a planar weighing scale or load cell assembly having a base plate, according to embodiments of the present invention. FIG. 12B is schematic cross-sectional view of the planar weighing scale or load cell assembly of FIG. 12A. With collective reference now to FIGS. 12A and 12B, each load cell assembly 805 may be attached to a (typically single) base plate or base element 890. Such a base plate 890 may support top plate or weighing surface 820 via at least one load cell assembly 805. In some embodiments, top plate or weighing surface 820 may integrally include, or be attached to, a protruding element 822, adapted to pass through hole 840 of load cell assembly 805, so as to deliver a load to loading element 837.

[0140] Base plate 890 may be supported by one or more supports such as leg 850, which may be further adapted to make contact with a flooring or flat surface. Each load cell assembly 805 is anchored to base plate or base element 890 via mounting holes or elements 842, e.g., using fastening elements such as bolts (not shown), and using shims or adapter plates 830, or the like, as necessary.

[0141] In the embodiment provided in FIGS. 3A-3B, load cell assembly 100 may be adapted, when secured within a weighing module (e.g., as described in FIG. 11 or in FIGS. 12A-12B), such that a vertical impact (e.g., an object that is slammed down with great force onto weighing platform 720) acts mainly upon flexures 127a-b and 117a-b, while measuring beams 107a-b remain largely or substantially completely unaffected. Thus, flexures 127a-b and 117a-b may serve as a vertical shock-protection mechanism for the measuring beams.

[0142] FIG. 13 is a block diagram schematically showing the operation of a spring arrangement, in loaded or operative mode, according to aspects of the present invention. Loading of the spring arrangement is effected by placing a load on, or below, the loading beam, depending on whether the loading beam is anchored to the weighing platform, or to the weighing base. As used herein and in the appended claims section, the loading beam may also be referred to as the “loading element” or as the “load-receiving element” or “load-supporting element” (depending on the configuration) of the load cell assembly. The spring arrangement may include—in addition to the measuring beam—a flexure arrangement (including at least one flexural element) operatively connected in series with the measuring beam. The flexure arrangement may be operatively connected, at a first end, to the loading beam, and at a second or opposite end, to the free or adaptive end of at least one measuring beam.

[0143] Substantially as shown, the flexure arrangement has n flexures (n being an integer) operatively connected in series, the first of these flexures being operatively connected to the loading beam, and the ultimate flexure of the n flexures being operatively connected in series to a second flexure, which in turn, is operatively connected to the first flexure in an assembly of m flexures (m being an integer), operatively connected in series. The ultimate flexure of the m flexures is operatively connected, in series, to a measuring beam of the spring arrangement. Associated with the measuring beam is at least one strain gage, which produces weighing information with respect to the load.

[0144] At least two of such flexure arrangements, disposed in parallel, may be necessary for the loading element to be suitably disposed substantially in a horizontal position (i.e., perpendicular to the load). In some embodiments, and particularly when extremely high accuracy is not necessary, a single flexure disposed between the loading beam and the measuring beam may be sufficient. This single flexure load cell arrangement may also exhibit increased crosstalk with other load cell arrangements (weighing assemblies may typically have 4 of such load cell arrangements for a single weighing platform). For a given nominal capacity, the overload capacity may also be compromised with respect to load cell arrangements having a plurality of flexures disposed in series between the load receiving beam and the measuring beam. This reduced overload capacity may be manifested as poorer durability and/or shorter product lifetime, with respect to load cell arrangements having a plurality of flexures disposed in series. Nonetheless, the overall performance of the single-flexure arrangement may compare favorably with conventional weighing apparatus and load cell arrangements. In any event, for this case, m+n=−1.

[0145] When no intermediate longitudinal flexures are present (i.e., m+n=−2), the inventor has found that the arrangement is yet more compromised by crosstalk with other load cell arrangements, and the overload capacity may be yet further compromised.

[0146] Moreover, the inventor has found that when no intermediate longitudinal flexures are present, the planar load cell may exhibit poor or insufficient flexibility to transverse rotation.

[0147] The inventor has surprisingly found that by connecting the load-receiving element or tip to the measuring beams via a transverse (transversely disposed with respect to the longitudinal face of the load cell body) flexure arrangement, the overload protection is significantly increased.

[0148] Such planar load cells may be fabricated from sheet metal typically having a thickness of 1.5 to 10 mm Typical materials of construction include aluminum and aluminum alloys (e.g., 2024 aluminum T3) for lower capacities, and steel (e.g., 17-4 PH steel H900) for larger capacities. Magnesium alloys (e.g., E675) may also be employed, typically for ultra-low, low and medium capacities.

[0149] Fabrication may be effected using various techniques known in the art.

[0150] The inventor has found that planar load cell sensitivity to various parasitical moments may be significantly reduced by increasing the load receiving element's rotational flexibility in the transverse plane.

[0151] The inventor has discovered that by connecting the load-receiving element or tip to the weighing beams via at least one transverse flexure arrangement, the planar load cell may exhibit appreciably increased transverse flexibility, thereby reducing the parasitical moments. In addition, as described briefly hereinabove, this increased transverse flexibility may significantly contribute to the vertical displacement achieved by the load cell, thereby increasing the overload capacity of the load cell.

[0152] Typically, there are 4 strain gages per loading beam. FIG. 14 provides a conventional schematic diagram of the strain gage electronics, which may be used in, or with, the load cell assemblies and weighing modules of the present invention. The strain gages may be configured in a Wheatstone bridge configuration, a configuration that is well known to those of skill in the art. The load cell system may further include a processing unit, such as a central processing unit (CPU). The processing unit may be configured to receive the load or strain signals (e.g., from 4 strain gages SG1-SG4) from each particular load cell and to produce a weight indication based on the load signals, as is known to those of ordinary skill in the art.

[0153] With reference now to the FIGS. 15, FIG. 15A is a top, schematic view of a planar load cell assembly 100, according to an embodiment of the present invention;

[0154] A load cell body 125 of planar load cell assembly 100 may be made from a block of load cell quality metal or alloy. Particularly advantageous embodiments employing particular magnesium alloys will be described hereinbelow.

[0155] Load cell body 125 may be fixed to a weighing assembly via one or more mounting holes or elements 142. A 1.sup.st, typically contiguous cutout window 116 passes from a top face 110 through a bottom face 112, perpendicularly through the broad dimension (i.e., with respect to the other 2 dimensions of a three-dimensional Cartesian system) of load cell body 125. 1.sup.st contiguous cutout window 116 may be generally C-shaped or U-shaped, and may have arms or a pair of cutout lines 118a, 118b running generally parallel to a central longitudinal axis 102 of load cell body 125, and connected or made contiguous by a cutout line or cutout base 118c. Both central longitudinal axis 102 and a transverse axis 104, disposed transversely thereto, run generally parallel to the broad dimension of load cell body 125. Both of these axes may be oriented in generally perpendicular fashion with respect to a primary axis 114. The thickness of load cell body 125 perpendicular to primary axis 114 is typically within a range of 1.5 mm to 10 mm, or 2 mm to 10 mm, and is designated W.sub.LCB.

[0156] Long sides 105a and 105b of load cell body 125 run generally along, or generally parallel to, central longitudinal axis 102.

[0157] As shown, measuring beams or spring elements 107a and 107b are each disposed between respective cutout lines 118a and 118b, and respective long sides 105a and 105b of load cell body 125, distal to cutout lines 118a and 118b with respect to transverse axis 104. When planar load cell assembly 100 is disposed in a vertically loaded position, the free end of each of beams 107a and 107b may be held in a fixed relationship, substantially perpendicular to the vertical load, by an end block 124 disposed at a free end 123 of load cell body 125.

[0158] A 2.sup.nd, typically contiguous cutout window 126 also passes from top face 110 through bottom face 112, perpendicularly through the broad dimension of load cell body 125. 2.sup.nd cutout window 126 may be generally C-shaped or U-shaped, and may have arms or a pair of cutout lines 128a, 128b running generally parallel to central longitudinal axis 102, and connected or made contiguous by a cutout line or cutout base 128c. 2.sup.nd cutout window 126 may be enveloped on three sides by 1.sup.st cutout window 116 (such that the 2.sup.nd cutout window is transversely bounded by the 1.sup.st contiguous cutout window). The orientation of 2.sup.nd cutout window 126 may be 180° (i.e., generally opposite) with respect to 1.sup.st cutout window 116.

[0159] Load cell body 125 has a first flexure arrangement having a first pair of flexure beams 117a, 117b disposed along opposite sides of central longitudinal axis 102, and distal and parallel thereto. First pair of flexure beams 117a, 117b may be longitudinally disposed between the first pair of cutout lines and the second pair of cutout lines, and mechanically connected or coupled by a first flexure base 119.

[0160] As shown, load cell body 125 has a second flexure arrangement 126 that may optionally be generally longitudinal. The second flexure arrangement may have a second pair of flexure beams 127a, 127b disposed along opposite sides of central longitudinal axis 102, and distal and optionally generally parallel thereto. Second pair of flexure beams 127a, 127b may be longitudinally disposed between the first pair of cutout lines and the second pair of cutout lines, and mechanically connected or coupled by a second flexure base 129.

[0161] A transverse flexure arrangement 136 may be disposed within 1.sup.st (outermost) cutout window 116, and more typically, within 2.sup.nd (or innermost) cutout window 126 as well. Typically, transverse flexure arrangement 136 may be disposed so as to mechanically bridge or connect between loading element 137 and the spring arrangement, e.g., to or via second flexure base 129 and/or first flexure base 119.

[0162] Transverse flexure arrangement 136 may include at least one transverse flexure beam such as transverse flexure beams 138a, 138b and 138c. Such beams may be disposed on either side or both sides of a loading area or load-contact area 140, which is described in further detail hereinbelow.

[0163] As used herein in the specification and in the claims section that follows, the term “transverse flexure beam” is used as would be understood to those of skill in the art. For the avoidance of doubt, such a transverse flexure beam may be a flexure beam disposed at an angle with respect to the traverse axis, such that the beam has a transverse component (e.g., related to the cosine of the angle of deviation from the transverse axis). Typically, the angle of deviation from the transverse axis of such transverse flexure beams is within a range of 0° to 70°, 0° to 60°, 0° to 45°, 0° to 40°, 0° to 35°, 0° to 30°, 0° to 25°, or 0° to 20°.

[0164] Transverse flexure beams 138a, 138b and 138c may be formed by one or more cutout structures 179a, 179a having comb-like cutout lines including a cutout backbone line 180a, 180b, and one or more transverse cutout lines 181a, substantially as shown. Typically, the angle of deviation from the transverse axis of such transverse cutout lines is within a range of 0° to 70°, 0° to 60°, 0° to 45°, 0° to 40°, 0° to 35°, 0° to 30°, 0° to 25°, or 0° to 20°.

[0165] Cutout structures 179a, 179a may be spaced and dimensioned such that transverse flexure arrangement 136 has a labyrinth or labyrinth-like transverse flexure beam structure.

[0166] More generally, the transverse flexure beams may be disposed and dimensioned to form a transverse hinge having a transverse character or component. Typically, the angle of deviation from the transverse axis of such a transverse hinge is within a range of 0° to 70°, 0° to 60°, 0° to 45°, 0° to 40°, 0° to 35°, 0° to 30°, 0° to 25°, or 0° to 20°.

[0167] A dimensionless parameter (D.sub.tb) characterizing transverse beam length (L.sub.tb) may be defined as follows:

D.sub.tb=L.sub.tb/W.sub.Lcb

where W.sub.Lcb is the width of the load cell body in the transverse direction. The inventor has found that the length of such beams in the transverse direction may be such that D.sub.tb is at least 0.03 or at least 0.05, and more typically, at least 0.07 at least 0.10, at least 0.12 at least 0.15, or at least 0.20.

[0168] In some embodiments, D.sub.tb is within a range of 0.03 to 0.60, 0.03 to 0.50, 0.05 to 0.60, 0.05 to 0.50, 0.05 to 0.40, 0.07 to 0.60, 0.07 to 0.50, 0.10 to 0.60, 0.10 to 0.50, 0.12 to 0.60, 0.12 to 0.50, 0.12 to 0.40, 0.15 to 0.60, 0.15 to 0.50, or 0.15 to 0.40.

[0169] The various cutout lines described above may typically have a width (W.sub.CO) of 0.2 mm to 5 mm, and more typically, 0.2 mm to 2.5 mm, 0.2 mm to 2.0 mm, 0.2 mm to 1.5 mm, 0.2 mm to 1.0 mm, 0.2 mm to 0.7 mm, 0.2 mm to 0.5 mm, 0.3 mm to 5 mm, 0.3 mm to 2.5 mm, 0.3 mm to 2.0 mm, 0.3 mm to 1.5 mm, 0.3 mm to 1.0 mm, 0.3 mm to 0.7 mm, 0.3 mm to 0.6 mm, or 0.3 mm to 0.5 mm.

[0170] In some embodiments, the ratio of W.sub.CO to W.sub.LCB (W.sub.CO/W.sub.LCB) is at most 0.5, at most 0.4, at most 0.3, at most 0.25, at most 0.2, at most 0.15, at most 0.12, at most 0.10, at most 0.08, at most 0.06, or at most 0.05.

[0171] In some embodiments, the ratio of W.sub.CO to W.sub.LCB (W.sub.CO/W.sub.LCB) is within a range of 0.03 to 0.5, 0.03 to 0.4, 0.03 to 0.3, 0.03 to 0.2, 0.03 to 0.15, 0.03 to 0.10, 0.04 to 0.5, 0.04 to 0.4, 0.04 to 0.3, 0.04 to 0.2, 0.04 to 0.15, 0.04 to 0.10, 0.05 to 0.5, 0.05 to 0.4, 0.05 to 0.3, 0.05 to 0.2, 0.05 to 0.15, or 0.05 to 0.10. Loading element 137 may also include a loading area or load-contact area 140, which may be the threading of a hole (e.g., the threading being for receiving a load, e.g., for receiving or connecting to an upper, weighing platform, or for supporting a load, e.g., connecting to a base, leg, or support (disposed below load cell body 125) of a weighing system. Loading area or load-contact area 140 may be positioned at an intersection of central longitudinal axis 102 and transverse axis 104.

[0172] In the exemplary embodiment provided in FIG. 15A, first and second flexure arrangements may form a generally longitudinal flexure arrangement 180, mechanically disposed between loading element 137 and measuring beams or spring elements 107a and 107b.

[0173] At least one strain gage, such as strain (or “strain-sensing”) gages 120, may be fixedly attached to a surface (typically a top or bottom surface) of each of measuring beams 107a and 107b. Strain gages 120 may be adapted and positioned to measure the strains caused by a force applied to the top of the “free” or “adaptive” side 123 of load cell body 125. When a vertical load acts on free end (i.e., an end unsupported by the base) 123 of load cell body 125, load cell body 125 undergoes a slight deflection or distortion, with the bending beams assuming a double-bending configuration having an at least partial, and typically primarily or substantially, double-bending behavior. The distortion is measurably sensed by strain gages 120.

[0174] It may thus be seen that planar load cell assembly 100 is a particular case of a load cell assembly having the load beam and spring arrangement of FIG. 13. In this case, the number of intermediate flexures is 2, such that m and n both equal zero. In addition, the intermediate flexures are intermediate flexure beam pairs connected by a flexure base. Similarly, the measuring beams are connected at a first end by the fixed end of load cell body 125, and at the opposite end by adaptive end 124 of load cell body 125.

[0175] A load cell body 125 may be made from a block of load cell quality metal or alloy. For example, load cell quality aluminum is one conventional and suitable material. In some embodiments, the alloy may advantageously be a magnesium alloy, typically containing at least 85%, at least 90%, and in some cases, at least 92%, at least 95%, or at least 98% magnesium, by weight or by volume. The magnesium alloy should preferably be selected to have an elastic module (E) that is lower, and preferably, significantly lower, than that of aluminum.

[0176] The flexure arrangements and measuring beams of the planar load cell assembly should be dimensioned and structured such that under loading in an operative mode, the broad face of loading element 137 is close to 90° (within ±5° within ±3°, or within ±2°, within ±1.5°, within ±1.0°, within ±0.5°, within ±0.3°, within ±0.25°, within ±0.20°, within ±0.15°, within ±0.12°, or within ±0.10°, with respect to the vertical or the direction of the load, at “full capacity” or “nominal capacity” of the load cell. The closer such a configuration is to 90°, the greater the weighing accuracy.

[0177] As used herein in the specification and in the claims section that follows, the term “nominal capacity”, and the like, as known in the art, is the load that effects 1 microstrain (0.1% of the strain) in the length of the measuring beam.

[0178] Alternatively, with the low-profile load cell assembly disposed in an operative or weighing mode, and with a load disposed on the loading element so as to achieve the nominal load capacity, an angle of a top surface of the loading element, with respect to horizontal, is within ±3°, within ±2°, within ±1.5°, within ±1°, within ±0.8°, within ±0.5°, within ±0.3°, within ±0.25°, within ±0.20°, within ±0.15°, within ±0.12°, within ±0.10°, within ±0.08°, within ±0.06°, within ±0.05°, within ±0.04°, within ±0.035°, within ±0.030°, within ±0.025°, or within ±0.020°.

[0179] FIG. 15B is a top, schematic view of a planar load cell body, according to embodiments of the present invention. FIG. 16 is an exemplary displacement plot showing a deflection of the flexure arrangement and the load cell arrangement of FIG. 15B, in response to a moment (Mz) along the transverse (Z) axis. The deflection reveals a mechanical hinge disposed in a generally transverse direction.

[0180] FIGS. 17A-17E provide top, schematic views of various planar load cell bodies, according to embodiments of the present invention.

[0181] In some embodiments, two of the inventive load cell arrangements may form a double-ended planar load cell assembly having two planar load cell assemblies, substantially similar or identical to those described hereinabove, but sharing a common, integral load cell body, and generally disposed at opposite ends thereof, optionally symmetrically about a central transverse axis (Z-Z) of the load cell body.

[0182] In one typical configuration, the inventive planar load cell assembly includes a plurality of planar load cells sharing a single, integral load cell body, each planar load cell assembly having a transverse flexure arrangement mechanically bridging or connecting between the loading element and the measuring beam. Typically, a load cell assembly may employ solely these four planar load cells. Such an arrangement may exhibit appreciably reduced crosstalk between load cells, with respect to 4 individual load cell bodies, or with respect to 2 double-ended planar load cell assemblies.

[0183] FIG. 18 is a block diagram of a weighing scale or load cell assembly. An object to be weighed is placed on the top plate of a weighing scale of the present invention. During operation, vertical forces applied to the top plate are transferred to one or more of the inventive load cell assemblies (e.g., load cell assembly 100) configured to measure vertical forces. Electrical signals containing, or correlated with, weight information, are communicated with a processor. The processor processes the signals, or adaptations thereof, to produce weight information, and may then transmit this weight information, for example, to a display device. A processor port may also be available for maintenance, calibration or firmware updates.

[0184] FIG. 19 is an exploded view of an exemplary weighing scale or load cell assembly 700, according to one embodiment of the present invention. Weighing scale 700 is typically a low-profile or (ultra-low profile) planar weighing scale, substantially as shown. Weighing scale 700 may include at least one load cell assembly such as load cell assembly 705 (e.g., 4 of load cell assemblies 105, as provided and described hereinabove, but shown only schematically here), or at least one double-ended planar load cell assembly (as described hereinabove), by way of example, 2 of such double-ended planar load cell assemblies.

[0185] Weighing scale 700 may have a solid top plate 720 disposed above load cell assemblies 705, which may attach to load cell assembly 705 via mounting holes or elements 742, with shims or adapter plates 730 disposed therebetween. In the embodiment shown in FIG. 19, each load cell assembly 705 is supported by a base such as weighing scale leg 750. In this embodiment, leg 750 may be attached to, or associated with, load cell assembly 705 via a load contacting area 740. Typically, an upper portion of leg 750, or an element associated therewith (not shown), may protrude up through load contacting area 740.

[0186] FIG. 20 is an exploded perspective view of a planar weighing scale or load cell assembly having a base plate, according to embodiments of the present invention. Each schematically-shown load cell assembly 805 may be attached to a (typically single) base plate or base element 890. Such a base plate 890 may support top plate or weighing surface 820 via at least one load cell assembly 805. In some embodiments, top plate or weighing surface 820 may integrally include, or be attached to, a protruding element 822, adapted to pass through a load contacting area 840 of load cell assembly 805, so as to deliver a load to loading element 837.

[0187] Base plate 890 may be supported by one or more supports such as leg 850, which may be further adapted to make contact with a flooring or flat surface. Each load cell assembly 805 is anchored to base plate or base element 890 via mounting holes or elements 842, e.g., using fastening elements such as bolts (not shown), and using shims or adapter plates 830, or the like, as necessary.

[0188] In the embodiment provided in FIG. 15A, load cell assembly 100 may be adapted, when secured within a weighing module (e.g., as described in FIG. 19 or in FIG. 20), such that a vertical impact (e.g., an object that is slammed down with great force onto weighing platform 720) acts mainly upon flexures 127a-b and 117a-b, while measuring beams 107a-b remain largely or substantially completely unaffected. Thus, flexures 127a-b and 117a-b may serve as a vertical shock-protection mechanism for the measuring beams.

EXAMPLES

[0189] Reference is now made to the following examples, which together with the description provided herein, illustrate the invention in a non-limiting fashion.

[0190] The vertical displacement of various planar load cells was evaluated experimentally. In these examples, the load cell bodies were fabricated from aluminum 2024 T3 having a sheet thickness of 2.0 mm. The capacity of each exemplary load cell was approximately 4 kg. Evaluation was performed by applying a transverse torque of 0.7 kg*cm, and measuring the relative angle of inclination in the transverse direction.

Comparative Example 1

[0191] For a load cell having 2 intermediate longitudinal flexures disposed between the measuring beam and the load receiving element, shown in FIG. 21A, the relative angle of inclination in the transverse direction was 0.59°/(kg.Math.cm).

Comparative Example 2

[0192] For a load cell having 3 intermediate longitudinal flexures disposed between the measuring beam and the load receiving element, shown in FIG. 21B, the relative angle of inclination in the transverse direction was 0.91°/(kg.Math.cm), an improvement of 0.32°/(kg.Math.cm) with respect to the more simple design of FIG. 21A. However, the machining cost is increased, and perhaps more significantly, there are physical machining limitations with respect to the distance between cutout lines, such that this approach of increasing the number of intermediate longitudinal flexures is of limited value.

Example 3

[0193] The inventive load cell shown in FIG. 21C (the structure of this load cell may be more clearly viewed in the schematic drawing provided in FIG. 21D) has only 1 intermediate longitudinal flexure disposed between the measuring beam and the load receiving element. However, the load cell further includes a transverse flexure pattern adapted to increase transverse flexibility. The relative angle of inclination in the transverse direction for this inventive load cell was 2.0°/(kg.Math.cm), an improvement of about 1.4°/(kg.Math.cm) with respect to the more simple design of FIG. 21A, over 4 times the improvement attained utilizing the design of FIG. 21B.

[0194] Significantly, the vertical displacement achieved by this inventive load cell was approximately 1.5 times larger than the vertical displacement achieved by the load cells of the comparative examples. One ramification of this feature is that overload protection may be significantly increased.

[0195] As used herein in the specification and in the claims section that follows, the terms “spring element” and “measuring beam” refer to a beam having one or more strain gages attached or directly attached therewith. Such strain gages are not considered to be part of the “spring element” or “measuring beam”.

[0196] As shown in the figures and described herein, the spring element or measuring beam is disposed along a longitudinal section of the load cell body that is defined by a length of the cutout window of the spring element along the long dimension of the load cell body. The at least one strain gage associated with the spring element is longitudinally positioned within this longitudinal section of the load cell body, typically between this cutout window and the closest longitudinal edge (i.e., generally parallel to the longitudinal axis) of the load cell body.

[0197] As used herein in the specification and in the claims section that follows, the term “flexure beam”, and the like, refers to a spring element that is devoid of strain gages.

[0198] As used herein in the specification and in the claims section that follows, the terms “flexure beam” and “spring element” refer to beams having a length L.sub.b, a width W.sub.b, and a height H.sub.b, for which L.sub.b>W.sub.b, and for which L.sub.b>H.sub.b. More typically, L.sub.b>3.Math.W.sub.b, L.sub.b>5.Math.W.sub.b, or L.sub.b>7.Math.W.sub.b, and/or L.sub.b>3.Math.H.sub.b, L.sub.b>5.Math.H.sub.b, L.sub.b>7.Math.H.sub.b, or L.sub.b>10.Math.H.sub.b.

[0199] As used herein in the specification and in the claims section that follows, the term “generally”, with respect to orientations and measurements such as “parallel”, “along”, and “central”, is meant to limit the deviation to within ±30%. More typically, this deviation is within ±25%, ±20%, ±15%, ±10%, ±5%, ±3%, ±2%, ±1%, ±0.5%, ±0.2%, or less.

[0200] It will be appreciated that certain features of the invention, which are, for clarity, described in the context of separate embodiments, may also be provided in combination in a single embodiment. Conversely, various features of the invention, which are, for brevity, described in the context of a single embodiment, may also be provided separately or in any suitable sub-combination.

[0201] Although the invention has been described in conjunction with specific embodiments thereof, it is evident that many alternatives, modifications and variations will be apparent to those skilled in the art. Accordingly, it is intended to embrace all such alternatives, modifications and variations that fall within the spirit and broad scope of the appended claims.