Title of Invention

WEIGHING DEVICE, IN PARTICULAR MULTIPLE TRACK WEIGHING DEVICE

Abstract The invention relates to a weighing device with several weighing cells (3) which are mechanically rigidly interconnected, and which in each case have a load sensor (7) that has a predetermined load insertion direction and can be acted on by a load, with at least one acceleration sensor (9) for the detection of at least one acceleration disturbance and with at least one evaluating unit to which the weight signals generated by the weighing cells (3) and the disturbance signals generated by the acceleration sensors (9) can be transmitted. The evaluating unit is configured such that, by using a predetermined rule for each weighing cell (3), a correcting quantity is determined from the disturbance signal of the at least one acceleration sensor (9) as a function of the geometric location of the relevant weighing cell (3) relative to the geometric location of the at least one acceleration sensor (9), where this correcting quantity takes into account the influence, operating at the geometric location of the relevant weighing cell (3), of the at least one acceleration disturbance, and in that the weight signal, which is affected by the at least one acceleration disturbance, of the relevant weighing cell (3) is combined, or processed conventionally, with the correcting quantity in such a way that the influence of the at least one acceleration disturbance on the weight signal is substantially compensated.
Full Text 1
WEIGHING DEVICE, IN PARTICULAR, MULTIPLE-TRACK WEIGHING DEVICE
The invention relates to a weighing device with several weighing cells, allowing
simultaneous weighing processes to be carried out. Such multiple-track weighing devices are
used, for example, in the pharmaceutical industry, and they are configured to weigh products of
small weight, particularly tablets, coated tablets, and similar items at a high cycle rate.
To keep the number of weighing processes per hour as high as possible, a low-pass filter
with a relatively low limit frequency cannot be applied to the measurement signal with such
weighing devices. Although such low-pass filters would improve the accuracy of the weighing
process, and in particular, would allow the accuracy required in the pharmaceutical industry in
the first place, the result would not be achievable.
Therefore, rather than use low-pass filters with very low limit frequency in such multiple-
track weighing devices, it is commonly known to instead correct the output signal of the force
sensor itself of the weighing cell by the detection of disturbing accelerations, and to compensate
in this way for the influence of disturbing accelerations.
Such compensation methods are known, for example, from DE 32 30 998 Al for scales
with a single weighing cell. In this weighing device, an acceleration sencer is arranged in the
housing of the weighing cell in the immediate vicinity of the moving measurement mechanisms.
With this acceleration sensor, substantially the same disturbing accelerations are detected that
also act on the load and the mass of the measurement mechanisms. The sensor signal is then
amplified to adapt the sensor sensitivity to the sensitivity of the weighing cell, and it is
subtracted from the signal of the weighing cell. In this way, a measurement signal is obtained
which is corrected by the detected disturbing acceleration, and which ideally depends only on the
mass of the load to be weighed. The acceleration sensor is arranged here in such a way that it
detects the components of disturbing accelerations that act in the load insertion direction.
From DE 40 01 614 Al a compensation scale is known in which at least one acceleration
sensor is arranged on a mobile part of the scale. The acceleration sensor delivers a signal to an
arrangement which processes a correction signal, and which determines at least one correction
signal for influencing the measurement result which appears at the output as a measure of weight
or of the mass of the load acting on the mobile part. This state of the art also describes the
compensation and elimination, respectively, of the influence of translational and rotational
disturbing accelerations that act on the base plate of the scale.

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However, the use of such weighing cells, with in each case one or more measurement
recorders, to construct a multiple-track weighing system would be associated with high costs as a
result of the corresponding high number of acceleration sensors.
Therefore, in the construction of multiple-track weighing systems, an appropriate number
of weighing cells is arranged on a common base plate, and a single acceleration sensor is
arranged on this base plate. The position of the acceleration sensor is chosen here such that it is
as characteristic as possible for the disturbing accelerations that can usually be expected, i.e., in
such a way that it is possible to use the signal of the single acceleration sensor to correct with
sufficient accuracy the measurement signals of the individual weighing cells, which signals have
been affected by the disturbing accelerations that have occurred.
However, such multiple-track weighing systems have the disadvantage that in the case
where the disturbing accelerations do not affect the individual weighing cells in the same way, a
sufficiently exact compensation of the disturbing accelerations is not possible, and in some
circumstances an unacceptable error is applied to the generated, corrected weight signals of the
individual weighing cells.
Therefore, the invention is based on the problem of producing a weighing device with
several weighing cells that are mechanically rigidly interconnected, where the weight signals of
the individual weighing cells can be corrected with sufficient accuracy even if disturbing
accelerations occur that do not affect all the weighing cells in the same way, and where the
device has a simple and cost effective construction.
The invention solves this problem with the characteristics of Claim 1.
The invention is based on the finding that a sufficiently exact compensation of disturbing
accelerations is enabled by using at least one acceleration sensor that detects at least one
acceleration disturbance, if in addition in each case a correcting quantity which takes into
account the influence of the detected acceleration disturbance is determined, using a
predetermined rule for each weighing cell, from the disturbing quantity signaLof the at least one
acceleration sensor as a function of the geometric location of the relevant weighing cell relative
to the geometric location of the at least one acceleration sensor. Using this correcting quantity,
which is determined for each individual weighing cell, the weight signal of the relevant weighing
cell, to which the influence of the disturbing acceleration has been applied, can then be corrected.
For this purpose, the correcting quantity can be combined or connected by means of circuit
technology, for example, analog circuit technology, with the measurement signal of the force
measuring device itself of the weighing cell. However, it is naturally also possible to use a purely
computational correction of the weight signal by means of an appropriately configured
evaluating unit. The latter can receive the digitized signal of the acceleration sensor and of the
force sensor.

3
The acceleration sensor can be connected rigidly with the weighing cells, which are
rigidly interconnected. This arrangement ensures that although the disturbing accelerations that
occur may affect the individual weighing cells differently, the occurrence of oscillations within
the system of the weighing cells and of the acceleration sensor(s) is avoided. Indeed, in the latter
case it would be impossible to reach a conclusion with sufficient reliability regarding the effect
of this acceleration disturbance at the locations of the weighing cells, and thus on the weighing
cells themselves, by means of detection of the at least one acceleration disturbance.
In principle, however, it is conceivable to provide the moving measurement mechanism
of one or more weighing cells also with the at least one acceleration sensor or at least one of the
acceleration sensors. In this way, the influence of acceleration disturbances on the load side of
the relevant weighing cell can be detected. From this detected acceleration disturbance, it is then
also possible to derive the effect of the detected acceleration disturbance on the other weighing
cells in each case as a function of the geometric data and the characteristic data of the individual
cells.
A weighing device according to the invention can be produced, for example, in a simple
way by connecting all the weighing cells, and preferably also the at least one acceleration sensor,
mechanically rigidly with a support element, for example, by arranging them on a common rigid
base plate.
As is usually done, it is preferred to arrange the weighing cells in such a way that the load
insertion directions or action directions of the weighing cells are substantially parallel.
According to the preferred embodiment of the invention, the number and type of
acceleration sensors is fixed such that it is possible to detect and/or determine both the
component of a purely translational acceleration disturbance that exists in the load insertion
direction of each weighing cell, and also those components of rotational acceleration
disturbances that exist in the load insertion direction and are generated by a single- or multiple-
axis rotational disturbing movement of the weighing cell.
In this case, the evaluating unit is preferably configured so that, using a predetermined
rule for each weighing cell, a correcting quantity is determined in each case from the disturbing
quantity signals of the acceleration sensors as a function of the geometric location of the relevant
weighing cell relative to the geometric location of the acceleration sensors, where this correcting
quantity takes into account the influence, operating at the geometric location of the relevant
weighing cell, of the components of the acceleration disturbances in the load insertion direction
of the relevant weighing cell. In this way, the weight signal, which is affected by the disturbing
quantity, of the relevant weighing cell can then be combined with the correcting quantity, or
processed computationally, in such a way that the influence on the weight signal of the

4
components of the acceleration disturbances in the load insertion direction of the relevant
weighing cell can be substantially compensated.
According to an additional embodiment of the invention, the number and the type of
acceleration sensors can be established such that, in addition to the acceleration components in
the load insertion direction of each weighing cell, single- or multiple-axis rotational acceleration
disturbances at the location of each weighing cell can be detected and/or determined that affect
the inertial moment(s) of the measurement mechanisms of the weighing cells about
corresponding axes.
If the influence of rotational acceleration disturbances on the inertial moments of the
measurement mechanisms of the weighing cells about corresponding axes is also compensated,
the accuracy of the weighing device is improved further.
In this case, the evaluating unit is preferably configured so that, using a predetermined
rule for each weighing cell, a correcting quantity is determined in each case from the disturbing
quantity signals of the acceleration sensors as a function of the geometric location of the relevant
weighing cell relative to the geometric location of the acceleration sensors, which in addition
takes into account the influence, operating at the geometric location of the relevant weighing
cell, of the single- or multiple-axis rotational acceleration disturbances on the inertial moment(s)
of the measurement mechanisms of the relevant weighing cell. The weight signal of the relevant
weighing cell that is affected by the disturbing quantity can then again be linked, or nrocessed
computationally, with the correcting quantity, so that the influence of the rotational acceleration
disturbances on the weight signal is substantially compensated. Naturally, it is possible to
provide several evaluating units instead of a single evaluating unit, or even one evaluating unit
per weighing cell, with these units performing signal processing, or the single evaluating unit can
be implemented as an evaluating unit with a distributed arrangement.
According to an embodiment of the invention that is easy to produce, several weighing
cells can be arranged on a line x connecting two translational acceleration sensors that are
arranged at a certain separation from each other. The expression translational acceleration sensor
here denotes an acceleration sensor whose sensor signal reflects, or is proportional to, the
components of any acceleration disturbances where the components occur in an action direction
or detection direction of the acceleration sensor. On the other hand, a rotational acceleration
sensor detects a purely rotational disturbing acceleration about a predetermined axis (action
direction of the rotational acceleration sensor).
In this simplified embodiment of a weighing device according to the invention, it is
possible to use only two translational acceleration sensors to determine in a simple way by
calculation the influence of acceleration disturbances which have components in the load

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insertion direction of the weighing cells. In many cases, a sufficiently accurate correction of the
weight signals is already achieved with only two translational acceleration sensors.
According to a preferred embodiment of the invention, it is possible to provide, in
addition to the two translational acceleration sensors on the line on which the weighing cells are
also provided, an additional translational acceleration sensor that is at a predetermined distance
from the connecting line. In this embodiment, it is not absolutely necessary for all the weighing
cells to be on one line with the first two translational acceleration sensors. This is because using
three translational acceleration sensors also enables determining the influence of any acceleration
disturbances having components in the weighing cell load insertion direction at the locations of
the individual weighing cells. However, by placing the weighing cells on a line with two of the
translational acceleration sensors, a simple computational correction of the weight signals can be
achieved.
If the additional translational acceleration sensor is arranged on a central normal line onto
the interval between the first two translational acceleration sensors, then it is also possible to
determine a simple correction of the influence of a single rotational acceleration disturbance,
namely the rotational acceleration disturbance whose axis is parallel to the line on which the
weighing cells are arranged. In principle, however it is naturally possible to use three
translational acceleration sensors to also determine the influence of rotational disturbing
accelerations whose axis is parallel to the plane defined by the three translational acceleration
sensors.
Another simplification of the correction and accuracy improvement can be achieved by
designing and arranging the weighing cells such that the measurement mechanisms have
rotational oscillation sensitivity substantially only about an axis that is parallel to the line on
which the weighing cells are arranged.
In the embodiment with three acceleration sensors, where the weighing cells are located
on the line connecting two of the acceleration sensors, and the third acceleration sensor is located
on the central normal line onto the interval between the two first acceleration sensors, a very
simple computational compensation of the influence of both rotational disturbing accelerations
and also a very simple computational correction of the influence of translational disturbing
acceleration in the load insertion direction of the weighing cells can be achieved.
According to one embodiment of the invention, one can use as acceleration sensors, in
particular translational acceleration sensors, capacitive acceleration sensors, in which the
deflection of a seismic mass from a starting position is determined by using capacitance and the
seismic mass is reset to the starting position by the generation of an electrostatic force using a
closed loop system, where the resetting force required for this purpose represents a measure of
the detected acceleration.

6
The acceleration sensors produce very minimal noise, even at high resolution. In
addition, no phase shift occurs with these sensors even at frequencies much higher than 100 Hz.
Consequently, it is simpler to design filters that adapt the frequency response of the sensor to the
frequency response of the weighing cells, since the frequency response of these sensors is
constant in the range of interest.
Such capacitive acceleration sensors naturally need not be used only in weighing devices
with several weighing cells according to the present invention. In fact, one or more such
capacitive acceleration sensors can also be used for the detection of disturbing accelerations in
weighing devices with a single weighing cell. The sensors here can be connected rigidly to the
weighing cells in known fashion, or they can be provided on a moving element of the
measurement mechanisms of the weighing cell.
Additional embodiments of the invention can be obtained from the dependent claims. The
invention is explained in greater detail below with reference to an embodiment example
represented in the drawing. In the drawing,
Figure 1 shows a schematic representation of a multiple-track weighing device according
to the present invention with two translational acceleration sensors;
Figure 2 shows a schematic block diagram for representing the signal combination with
the correction of the weight signals of the device in Figure 1;
Figure 3 shows a schematic representation of an additional embodiment of a multinle-
track weighing device according to the invention with three acceleration sensors in top view, and
Figure 4 shows a schematic block diagram for representing the combination of the
individual signals for the correction of the weight signals of the multiple-track weighing device
in Figure 3.
The weighing device 1, which is represented diagrammatically in a front view in Figure
1, comprises several weighing cells 3, which are also marked with the abbreviation WZ. The
weighing cells 3 are arranged along a line or straight line on a rigid support plate 5. The
Cartesian coordinate system, which is also represented in Figure 1, was chosen to describe the
geometry of the weighing device 1. In this coordinate system, the line along which the weighing
cells 3 are arranged, preferably at equidistant intervals, runs in the direction of the x axis. The
force insertion direction, along which a load (not shown) in each case exerts weight on a load
sensor 7 of the weighing cell 3, runs in the direction of the z axis of the coordinate system.
To correct influences from acceleration disturbances that have components in the
direction of the z axis of the weighing cells 3, only two translational acceleration recorders or
acceleration sensors 9 are arranged in the weighing device 1 represented in Figure 1. The
acceleration sensors are also provided with the reference numbers BA1 and BA2.

7
To compensate for the above-mentioned acceleration disturbances, the acceleration
sensors 9 are arranged on the same line on which the weighing cells 3 are also positioned. In the
represented embodiment example, the acceleration sensors 9 are positioned in each case at one
end of the series of weighing cells 3. As a result of the relatively large separation between the
two acceleration sensors 9, the desired high accuracy is achieved in the computation of the
correction factors, as explained below.
The effect on the signals of the individual weighing cells caused by acceleration
disturbances having z-axis direction components can be taken into account because the geometry
of the weighing device 1 is known. The weight Gk(t), which is usually (in the strict sense
incorrectly) indicated in kilograms, on a weighing cell in position k that is adulterated or
superposed by acceleration components can be described by the equation

Here mk stands for the mass of the load, which is located on the load sensor 7 of the weighing
cell in position k, and mvLk takes into account the influence of a preload that is ontionally
mounted on the weighing cell and the unladen masses of the weighing cell mechanism which are
involved in acceleration. The gravitation; istant (gravitational acceleration) is
denoted as g.
For the geometry of this special arrangement, the anreleration in the z direction
can be calculated from the accelerations at the two locations XBAI and XRA2
of the two translational acceleration sensors 9, or BA1 and BA2, respectively, using the
following equation:

In this equation, the geometric location of the weighing cell in position k is denoted Xwzk-
In this special geometry of the arrangement of all the weighing cells 3 and of the two
translational acceleration sensors 9 on a line, all the components of any acceleration disturbances

8
in the load insertion weighing cells can be determined and corrected with only two translational
acceleration sensors.
It should be noted here that a translational acceleration sensor means an acceleration
sensor that can determine the acceleration in a predetermined direction of action. Thus, the
direction of action of the acceleration sensors 9 in the embodiment in Figure 1 is provided as
being in the direction of the z axis of the chosen coordinate system, i.e., parallel to the load
insertion direction of the weighing cells 3.
To compensate for the influence of the acceleration disturbances having components in
the z direction, which is described by the product of the second partial term of the above
equation 1 with the determined disturbing acceleration zv must be subtracted from the weight
signal Gk(t) that is affected by error and is generated by the force sensor itself of each weighing
cell 3. The schematic signal path in question is shown in the block diagram represented in Figure
2. To simplify, only the signal path for the first two weighing cells 3 WZ1 and WZ2 is
represented here.
The two acceleration signals generated by the translational acceleration sensors 3, or BA1
and BA2, respectively, are proportional to the detected disturbing acceleration in the z direction.
For each weighing cell 3, these signals in each case are input to an amplifier VBAI and VBA2,
respectively. Here, the factor which can be seen from equation II is applied in each case to both
signals. At the same time, the sensitivities of the two acceleration sensors BA1 and BA2 are
adapted by means of the amplifiers VBAI and VBA2 to the sensitivity of the weighing cell that
delivers the weight signal Gk(t) which is affected by error. The signals that are present at the
output of each amplifier VBAI and VBA2, and which in each case correspond to a summand of the
above equation II, are added in accordance with this equation. This signal is input to a filter 11
that adapts the frequency responses of the two acceleration sensors to the frequency response of
the weighing cell to ensure a phase-correct combination of these signals. Then, the factor 1/g of a
corresponding multiplier unit is applied to the output signal of the filter 11. However, this
multiplication can naturally also be integrated into the relevant filter 11. The product of the
output signal of the multiplier unit with the mass mvLk is subtracted from the weight signal Gk(t)
that is affected by error. This result is then divided by the output signal of the multiplier unit plus
one. This corrected weight signal Gk,kon-(t) can then be transmitted to a display unit and/or to an
additional data processing unit.
In Figure 3, an additional embodiment of a multiple-track weighing device is represented
that is largely identical to the embodiment according to Figure 1. An additional acceleration
sensor 9 is provided however, which is also denoted BA3.
This embodiment also allows the detection and correction of rotational accelerations of
the support plate 5 and thus of the weighing cells 3. With the three translational acceleration

9
sensors, which in each case have a direction of action in the load insertion direction of the
weighing cells 3, it is theoretically possible to detect all the acceleration disturbances that have a
component in the direction of the z axis as well as a two-axis rotational acceleration of the
support plate 5 and thus of the weighing cells 3. The two axes of the rotational acceleration are
here parallel to the plane, or in the plane of the support plate 5, or in the plane in which the
weighing cells 3 are arranged (or in a plane that is perpendicular to the load insertion direction of
the weighing cells 3). Thus, any wobbling motion of the support plate 5 and of the weighing cells
3 arranged on it can be detected.
Below, it is assumed that the weighing cells 3 are constructed such that they are sensitive
only to rotating oscillations or rotational disturbing accelerations about an axis parallel to the x
axis. This is the case, for example, in compensation scales whose lever mechanisms have centers
of rotation for the levers exclusively about axes that are parallel to the x axis. If the weighing
cells 3 are arranged so that the rotation axes of the lever mechanisms run parallel to the x axis,
then a rotational acceleration disturbance that can have a corrupting effect on the measurement
result can only be one which contains at least one component of a rotational disturbing
acceleration about this axis.
For an arrangement of the additional acceleration sensor BA3 on the central normal line

This equation corresponds to the above explained equation I, but it has been expanded by
the last partial term to take into account the rotational disturbing acceleration about an axis
parallel to the x axis, where kk denotes the rotational sensitivity of the measurement mechanisms
of the weighing cells in position k about an axis parallel to the x axis, and denotes the
rotational disturbing acceleration about this axis.
The translational disturbing acceleration must again be determined according to
the previously explained equation II.
For the geometry chosen in Figure 3, the rotational disturbing acceleration is
obtained from the relation

10
In this relation, denote the measurement signals of the
two translational acceleration sensors BA1 and BA2, and of the additional translational
acceleration sensor BA3, respectively, VBAI, YBA2 and VBA3 refer to the geometric locations of the
translational acceleration sensors in a direction perpendicular to the x axis or in the direction of
the y axis.
Naturally, the chosen geometry can also be chosen to be more complicated than shown in
Figure 3. However, this geometry in particular leads to relatively simple relations for those
quantities required for correction of the weight signals affected by error of the measurement cells
3.
In general, however, the present invention is based on the principle, starting from a
preselected number and type of acceleration sensors that are mechanically rigidly connected with
the weighing cells which are also interconnected rigidly, of evaluation of the sensor signals
taking into account the geometry such that the disturbing acceleration of interest in each case, or
its components at the location of each individual weighing cells, is (are) determined and used for
correction of the weight signal affected by error of the relevant weighing cell.
In Figure 4, the signal path for the generation of a corrected weight signal Gk,kon-(t) of the
individual weighing cells 3 is again represented using the signal of the three translational
acceleration sensors BA1, BA2 and BA3 (to simplify, only for the first weighing cell 3 WZ1).
For the generation of the signal corresponding to the translational acceleration in the z
direction, normalized for gravitational acceleration, which is present at the output of the filter 11,
reference is made to the above explanations in connection with Figure 2. The rotational
acceleration according to the above equation IV is determined from the signals of all three
translational acceleration sensors 9, where an amplifier V'BAU V'BA2 and V'BA3 acts on each signal
of these sensors. The amplifiers here adapt the sensitivity of the acceleration sensors to the
sensitivity of the relevant weighing cell 3, and at the same time take into account the factors of


11
For the generation of a corrected weight signal Gk,kon{t) that corresponds to the mass
mk(t) in equation III, the signal at the output of the filter 13, with the factor kk applied to it, is
subtracted from the erroneous weight signal Gk(t) of the weighing cell at the position 1, as is
apparent from solving equation III for the quantity mk(t). The filter 13 again adjusts the
frequency response of the acceleration sensors BA1, BA2, BA3 to the frequency response of the
relevant weighing cell WZk in position k. If different acceleration sensors are used, this
frequency response adaptation can naturally also be integrated into the respective amplifiers and
carried out separately for each acceleration sensor. In addition, the filter 13 can incorporate the
application of the rotational disturbing acceleration about the x axis with the rotational sensitivity
kk of the weighing cell WZk in position k, which application is achieved in Figure 4 by means of
a separately represented multiplication unit. In addition, the product of the output of the filter 11
with the mass mvuc and the factor 1/g is also subtracted from the signal Gk(t) affected by error.
This result in turn is divided by the output signal of the filter 11, increased by plus one.
To simplify, Figure 4 shows this signal course only for the weighing cell WZ1 in the
position 1. With identical weighing cells, a block with the identical signal course plan can be
used for each weighing cell. With different weighing cells, different parameters may have to be
taken into account, such as different sensitivities of the weighing cells, different frequency
responses, and different rotational sensitivities.
Naturally, it is not necessary to provide a corresponding number of hardware circuits to
implement in each case the signal course, represented in Figure 3 for the weighing cell WZ1,
separately for each weighing cell. Rather, the signals of the acceleration sensors and the
erroneous signals of the weighing cells can also be digitized and transmitted to a central
evaluating unit, which consists substantially of a controller which can also be configured as an
independent computer. The controller can then carry out the required computations from the
rules of the previous equations, which are known to the controller, and deliver the corrected
weight signal in digital form, or again in analog form after digital-analog conversion, which is
represented in Figure 3 for the weighing cell WZ1. Naturally, it is also possible to provide
several evaluating units, which in each case correct the weight signals affected by error of a
group of weighing cells 3.

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Claims
1. Weighing device
(a) with several weighing cells (3), which are mechanically rigidly interconnected and in
each case have a load sensor (7) that can be acted on by a load, and which have a predetermined
load insertion direction,
(b) with at least one acceleration sensor (9) for the detection of at least one acceleration
disturbance, and
(c) with at least one evaluating unit to which the weight signals generated by the
weighing cells (3) and the disturbance signals generated by the acceleration sensors (9) are
transmitted,
(d) where the at least one evaluating unit is configured so that,
(i) using a predetermined rule for each weighing cell (3), a correcting quantity is
determined in each case from the disturbance signal of the at least one acceleration sensor (9) as
a function of the geometric location of the relevant weighing cell (3) relative to the geometric
location of the at least one acceleration sensor (9), where this correcting quantity takes into
account the influence, operating at the geometric location of the relevant weighing cell (3), of the
at least one acceleration disturbance,
(ii) the weight signal of the relevant weighing cell (3), that is affected by the at least one
acceleration disturbance is combined with the correcting quantity, or processed computationally,
so that the influence of the at least one acceleration disturbance on the weight signal is
substantially compensated.
2. Weighing device according to Claim 1, characterized in that the at least one
acceleration sensor (9) is rigidly connected to the weighing cells (3).
3. Weighing device according to Claim 1 or 2, characterized in that the weighing cells (3)
and preferably also the at least one acceleration sensor (9) are rigidly connected mechanically
with a rigid support element (5), for example, a common rigid base plate,
4. Weighing device according to one of the preceding claims, characterized in that the
load insertion directions of the weighing cells (3) run substantially parallel.
5. Weighing device according to one of the preceding claims, characterized in that the
number and type of the acceleration sensors (9) is established so that it is possible to detect
and/or determine both a component of a purely translational acceleration disturbance that exists
in the load insertion direction of each weighing cell (3), and also those components of rotational
acceleration disturbances that exist in the load insertion direction, where the components are
generated by a one- or multiple-axis rotational disturbance movement of the weighing cells (3).
6. Weighing device according to Claim 5, characterized in that the at least one evaluating
unit is configured so that,

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(a) using a predetermined rule for each weighing cell (3), in each case a correcting
quantity is determined from the disturbance signals of the acceleration sensors (9) as a function
of the geometric location of the relevant weighing cells (3) relative to the geometric locations of
the acceleration sensors (9), where this correcting quantity takes into account the influence,
operating at the geometric location of the relevant weighing cell (3), of those components of the
acceleration disturbances which are in the load insertion relevant weighing cell (3), and
(b) the weight signal affected by the disturbing quantity of the relevant weighing cell (3)
is combined with the correcting quantity, or processed computationally, such that the influence
on the weight signal of those components of the acceleration disturbances in the load insertion
relevant weighing cell (3), is substantially compensated.

7. Weighing device [according to] Claim 5 or 6, characterized in that the number and
type of the acceleration sensors (9) are fixed so that, in addition to the acceleration components
in the load insertion direction of each weighing cell (3), at the location of each weighing cell,
single- or multiple-axis rotational acceleration disturbances can be detected and/or determined
that have an effect on the inertial moment(s) of the parts of the weighing cells (3) that are
movable about corresponding axes with respect to a fixed foundation body.
8. Weighing device according to Claim 7, characterized in that the at least one evaluating
unit is configured so that

(a) using a predetermined rule for each weighing cell (3), in each case a correcting
quantity is determined from the disturbance signals of the acceleration sensors (9) as a function
of the geometric location of the relevant weighing cells (3) with respect to the geometric
locations of the acceleration sensors (9), where this correcting quantity in addition takes into
account the influence, operating at the geometric location of the relevant weighing cell (3), of the
single- or multiple-axis rotational acceleration disturbances on the inertial moment(s) of the
measurement mechanisms of the relevant weighing cell (3) about corresponding axes, and
(b) the weight signal, affected by the disturbance, of the relevant weighing cell (3) is
combined, or processed computationally, with the correcting quantity in such a way that the
influence of the rotational acceleration disturbances on the weight signal is substantially
compensated.
9. Weighing device according to Claims 5 and 6, characterized in that two translational
acceleration sensors (9), arranged at a predetermined separation from each other, are provided,
and in that the weighing cells (3) are arranged on the line connecting the two translational
acceleration sensors.
10. Weighing device according to Claim 9, characterized in that the at least one
evaluating unit determines the weight signal Gk(t) of a weighing cell (3) in position k according
to the relation

14

where nik(t) denotes the mass of the load on the weighing cell (3), mvLk denotes the unladen
mass of the relevant moved masses of the measurement mechanisms and the mass of an optional
preload on the weighing cell (3) in position k, denotes the total translational disturbing
acceleration in the detection direction of the weighing cell (3) at the location of the weighing cell
(3), and g denotes the gravitational acceleration; and in that the weighing cell (3) determines the
translational disturbing acceleration according to the relation

where denote the measurement signals of the two translational acceleration
sensors 9, and XBAI, XBA2, xwzk denote the geometric locations of the two translational
acceleration sensors and of the relevant weighing cell (3) on the line.
11. Weighing device according to Claim 9, characterized in that in addition at least one additional
translational acceleration sensor (9) is provided having a predetermined separation from the
connecting line.
12. Weighing device according to Claim 11, characterized in that at least bn£ translational
acceleration sensor (9) is arranged on a central normal line onto the interval between the two
translational acceleration sensors (9).
13. Weighing device according to Claim 11 or 12, characterized in that the weighing cells
(13) are configured and arranged so that the measurement mechanisms have a rotational
oscillation sensitivity essentially only about an axis that is parallel to the line x on which the
weighing cells (3) are arranged.
14. Weighing device according to Claim 13, characterized in that the at least one
evaluating unit determines the weight signal Gk(t) of a weighing cell (3) in position k according
to the relation

15

where mk(t) denotes the mass of the load of the weighing cell, mvLk denotes the unladen mass of
the relevant moved mass of the measurement mechanisms and the mass of an optional preload of
the weighing cell (3), denotes the total translational disturbing acceleration in the
detection direction of the weighing cell (3) at the location of this weighing cell, g denotes the
gravitational acceleration, kk denotes the rotational sensitivity of the measurement mechanisms
of the weighing cell (3) at the location k about a line that is parallel to the connecting line, and
the rotational disturbing acceleration about this axis; in that the at least one evaluating
unit determines the translational disturbing acceleration according to the relation

where denote the measurement signals of the two translational acceleration
sensors (9) and XBAI, XBA2, Xwzk denote the geometric locations of the two translational
acceleration sensors (9) and of the relevant weighing cell (3) on the line, and in that the at least
one evaluating unit determines the rotational disturbing acceleration according to the
relation

where denote the measurement signals of the two translational
acceleration sensors (9) and of the additional translational acceleration sensor (9), and VBAI, YBA2
and yBA3 denote the geometric locations of the translational acceleration sensors (9) in a direction
perpendicular to the line x.
15. Weighing device according to one of the preceding claims, characterized in that the
acceleration sensors (9) are formed as capacitive acceleration sensors, where the deflection of a
seismic mass from a starting position is determined by using capacitance, and the seismic mass is

16
reset to the starting position by the generation of an electrostatic force using a closed loop
system, where the resetting force required for this purpose represents a measure of the detected
acceleration.
16. Weighing device according to one of the preceding claims, characterized in that an
evaluating unit is provided for each weighing cell, or in each case an evaluating unit is provided
for a group of weighing cells.

The invention relates to a weighing device with several weighing cells (3) which are
mechanically rigidly interconnected, and which in each case have a load sensor (7) that has a
predetermined load insertion direction and can be acted on by a load, with at least one
acceleration sensor (9) for the detection of at least one acceleration disturbance and with at least
one evaluating unit to which the weight signals generated by the weighing cells (3) and the
disturbance signals generated by the acceleration sensors (9) can be transmitted.
The evaluating unit is configured such that, by using a predetermined rule for each
weighing cell (3), a correcting quantity is determined from the disturbance signal of the at least
one acceleration sensor (9) as a function of the geometric location of the relevant weighing cell
(3) relative to the geometric location of the at least one acceleration sensor (9), where this
correcting quantity takes into account the influence, operating at the geometric location of the
relevant weighing cell (3), of the at least one acceleration disturbance, and in that the weight
signal, which is affected by the at least one acceleration disturbance, of the relevant weighing
cell (3) is combined, or processed conventionally, with the correcting quantity in such a way that
the influence of the at least one acceleration disturbance on the weight signal is substantially
compensated.

Documents:

http://ipindiaonline.gov.in/patentsearch/GrantedSearch/viewdoc.aspx?id=7TBYifTlGl6cdNpDWBbP3g==&loc=wDBSZCsAt7zoiVrqcFJsRw==


Patent Number 268392
Indian Patent Application Number 4409/KOLNP/2007
PG Journal Number 36/2015
Publication Date 04-Sep-2015
Grant Date 27-Aug-2015
Date of Filing 16-Nov-2007
Name of Patentee WIPOTEC WIEGE-UND POSITIONIERSYSTEME GMBH
Applicant Address ADAM-HOFFMANN-STRASSE 26 67657 KAISERSLAUTERN
Inventors:
# Inventor's Name Inventor's Address
1 GOTTFRIEDSEN JAN AUF DEM ASPEN 30, 67714 WALDISCHBACH-BURGALBEN
2 URSCHEL PATRICK BEETHOVENWEG 3, 67886 MACKENBACH
PCT International Classification Number G01G 23/12
PCT International Application Number PCT/DE2006/000633
PCT International Filing date 2006-04-10
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 102005018708.0 2005-04-21 Germany