Information
-
Patent Grant
-
6363895
-
Patent Number
6,363,895
-
Date Filed
Friday, February 23, 200124 years ago
-
Date Issued
Tuesday, April 2, 200223 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 123 9011
- 251 12901
- 251 1291
- 251 12915
- 251 12916
- 361 156
-
International Classifications
-
Abstract
An actuator comprises a gas exchange valve and an electromagnetic actuating drive, having at least one electromagnet which has a coil, having an armature, whose armature plate can move between a first bearing surface on the electromagnet and a second bearing surface. A device for controlling the actuator comprises a power output stage provided for driving the coil. The power output stage has an electrical energy store which is charged by the coil in a predetermined operating state. The control unit controls the power output stage in an operating state of rapid energization when a predetermined condition is met indicating the striking of the armature plate on the first bearing surface or an imminent fallback of the armature plate to a rest position, the energy stored in the electrical energy store being fed to the coil in the operating state of rapid energization.
Description
FIELD OF THE INVENTION
The invention relates to a device for controlling an actuator, in particular, for controlling an internal combustion engine.
BACKGROUND OF THE INVENTION
A known actuator (DE 195 26 683 A1) has an actuating element, designed as a gas exchange valve, and an actuating drive. The actuating drive has two electromagnets between which, in each case counter to the force of a restoring means, an armature plate can be moved by switching off the coil current at the holding electromagnets and switching on the coil current at the capturing electromagnet. The coil current of the respective capturing electromagnet is regulated to a predetermined capture value, to be precise during a predetermined period of time which is dimensioned such that the armature plate strikes a bearing surface on the capturing electromagnet within the period of time. The coil current of the capturing electromagnet is subsequently regulated to a holding value.
The force acting on the armature plate essentially depends on the position of the armature plate and the excitation of the coil of the respective capturing electromagnet. The excitation of the coil depends, in turn, on the current through the coil. The gradient of the current rise of the current through the coil is given by the voltage drop across the coil.
Motor vehicles usually have a voltage supply which makes a predetermined operating voltage available to the electrical loads of the motor vehicle. At the customary operating voltages of from 12 to a maximum of 42 volts, an undesirable fallback of the armature plate to a rest position can thus occur. Likewise, if appropriate, the point in time of “gas exchange valve open” or “gas exchange valve closed” cannot be set sufficiently accurately.
DE 197 01 471 A1 discloses an apparatus for driving an electromagnetic load, with a capacitor which is discharged in each case at the beginning of load driving. This leads to a high current rise in the electromagnetic load.
Furthermore, DE 44 13 240 A1 discloses an apparatus for driving an electromagnetic load which comprises a half-bridge and an energy-storing element arranged between the half-bridge and a voltage source.
SUMMARY OF THE INVENTION
In one embodiment of the invention there is a device for controlling an actuator which is simple and ensures certain and reliable operation of the actuator.
BRIEF DESCRIPTION OF THE DRAWINGS
Exemplary embodiments of the invention are explained in more detail with reference to the schematic drawing, in which:
FIG. 1
shows an arrangement of an actuator and a control device in an internal combustion engine,
FIG. 2
a
shows a power output stage of the control device in an operating state of normal energization,
FIG. 2
b
shows the power output stage in the operating state of freewheeling,
FIG. 2
c
shows the power output stage in the operating state of rapid current reduction,
FIG. 2
d
shows the power output stage in the operating state of rapid energization,
FIG. 2
e
shows a table of the operating states of a first power output stage,
FIG. 2
f
shows a table of the operating states of a second power output stage,
FIG. 3
shows the first power output stage and a second power output stage,
FIG. 4
shows a flow diagram for controlling the first coil,
FIG. 5
shows a flow diagram of a diagram for controlling the second coil, and
FIGS. 6
a
-
6
e
show signal profiles of the current and of the voltages.
Elements having the same construction and function are provided with the same reference symbols throughout the figures.
DETAILED DESCRIPTION OF THE INVENTION
An actuator
1
(
FIG. 1
) comprises an actuating drive
11
and an actuating element
12
, which is preferably designed as a gas exchange valve and has a stem
121
and a disk
122
. The actuating drive
11
has a housing
111
, in which a first and a second electromagnet are arranged. The first electromagnet has a first core
112
, in which a first coil
113
is embedded in an annular groove. The second electromagnet has a second core
114
, in which a second coil
115
is embedded in a further annular groove. An armature is provided, whose armature plate
116
is arranged in the housing
111
in a manner allowing it to move between a first bearing surface
115
a
of the first electromagnet and a second bearing surface
115
b
of the second electromagnet. The armature furthermore comprises an armature stem
117
, which is guided through cutouts in the first and second cores
112
,
114
and can be mechanically coupled to the stem
121
of the actuating element
12
. A first restoring means
118
a
and a second restoring means
118
b
prestress the armature plate
116
into a predetermined rest position N. The actuator
1
is rigidly connected to a cylinder head
21
. The cylinder head
21
is assigned an intake duct
22
and a cylinder
23
with a piston
24
. The piston
24
is coupled to a crankshaft
26
via a connecting rod
25
.
A control device
3
is provided, which acquires signals from sensors and/or acquires signals from a superordinate control device (not illustrated) for engine operating functions and generates actuating signals, depending on which the first and second coils
113
,
115
of the actuator
1
are controlled. The sensors assigned to the control device
3
are designed as a first current measuring device
34
, which detects an actual value I_AV
1
of the current through the first coil, or a second current measuring device
35
, which detects an actual value I_AV
2
of the current through the second coil
115
. In addition to the sensors mentioned there may also be still further sensors.
The control device furthermore comprises a control unit
31
and a first power output stage
32
and a second power output stage
33
. Depending on control commands from the superordinate control device and depending on the actual values I_AV
1
, I_AV
2
of the current through the first and second coils
113
,
115
, the control unit
31
generates control signals for the control lines L
1
, L
2
, L
3
, via which the control unit
31
is electrically conductively connected to the first output stage
32
, and control signals for the control lines L
1
′, L
2
′, L
3
′, via which the control unit
31
is electrically conductively connected to the second output stage
33
. The first and second power output stages
32
,
33
differ merely by the fact that the first power output stage
32
is provided for driving the first coil
113
and the second power output stage is provided for driving the second coil
115
. The circuit arrangement and method of operation of their components is equivalent.
The first power output stage
32
is described below by way of example. The first power output stage
32
(
FIG. 2
a
) has a first transistor T
1
, whose gate terminal is electrically conductively connected to the control line L
1
, a second transistor T
2
, whose gate terminal is electrically conductively connected to the control line L
2
, and a third transistor T
3
, whose gate terminal is electrically conductively connected to a control line L
3
. The first power output stage
32
furthermore comprises diodes D
1
, D
3
, D
4
, a freewheeling diode D
2
, an electrical energy store designed as a capacitor C, and a resistor, which is provided as a measuring resistor for the current measuring device
34
. The first power output stage can be controlled into five different operating states BZ
1
which are each characterized by the respective switching state of the transistors T
1
, T
2
, T
3
. If a high voltage potential is present at the gate terminals of the transistors T
1
, T
2
, T
3
, which are preferably designed as MOS transistors, then the respective transistor T
1
, T
2
, T
3
is in the on state (ON) from its drain terminal toward the source terminal. By contrast, if a low voltage potential is present at the gate terminal of the respective transistor T
1
, T
2
, T
3
, then the transistor is in the off state (OFF) from its drain terminal to its source terminal. The five operating states BZ
1
are entered in
FIG. 2
e
with the associated switching states of the transistors T
1
, T
2
, T
3
. The five operating states BZ
1
are a quiescent state RZ, normal energization NB, freewheeling FL, rapid current reduction SSR and rapid energization SB. The operating states BZ
1
of the power output stage
32
will be explained in more detail below with reference to
FIGS. 2
a
to
2
d.
In the operating state BZ
1
of the quiescent state RZ, the transistors T
1
, T
2
, T
3
are all in the off state. The actual value I_AV
1
of the current through the first coil is zero and the voltage drop U
L
across the first coil is likewise.
In the operating state BZ
1
of normal energization NB, the transistors T
1
and T
2
are operated in the on state (ON) and the transistor T
3
is operated in the off state (OFF). Current then flows from a voltage source with the potential of the supply voltage U
B
through the transistor T
1
, the diode D
1
, the terminal AL
1
of the first coil
113
, through the first coil
113
toward the terminal AL
2
of the first coil
113
, through the transistor T
2
and the resistor R toward a ground terminal, which is at a reference-ground potential. As long as the coil is not operated at saturation, virtually the entire supply voltage U
B
is dropped across the first coil
113
. The current rises in accordance with the ratio of the voltage drop UL across the first coil
113
and the inductance of the first coil
113
.
In the operating state of freewheeling FL, the transistor T
2
is operated in the on state (ON), whereas the transistors T
1
, T
3
are operated in the off state (OFF). If, at the instant of the transition to the operating state of freewheeling FL, a current flows from the terminal AL
1
through the first coil
113
toward the terminal AL
2
, then the freewheeling diode D
2
is turned on and the current through the first coil
113
decreases in a manner dependent on the losses in the coil
113
, in the transistor T
2
, the resistor R and the freewheeling diode D
2
. The voltage drop U
L
across the first coil
113
is then given by the forward voltages of the freewheeling diode and of the transistor T
2
and the voltage drop across the resistor R (in total 2 volts, for example).
In an operating state BZ
1
of rapid current reduction SSR (
FIG. 2
c
) of the first power output stage
32
, the transistors T
1
, T
2
, and T
3
are operated in the off state. If, in the event of the transition to the operating state BZ
1
of rapid current reduction SSR, a current flows through the first coil
113
, then the freewheeling diode D
2
and the diode D
3
are turned on. The current then flows from the reference-ground potential via the freewheeling diode D
2
toward the terminal AL
1
of the first coil
113
and then through the first coil
113
toward the terminal AL
2
. From there, the current flows via the diode D
3
toward the capacitor C and charges the latter. The current through the first coil decreases significantly more rapidly in the operating state of rapid current reduction SSR than in the operating state BZ
1
of freewheeling FL, since the negative supply voltage U
B
reduced by the voltage drop U
C
across the capacitor C and the forward voltages of the freewheeling diode D
2
and of the diode D
3
is dropped across the first coil
113
. In the operating state of rapid current reduction SSR, the first coil
113
and the capacitor C form a first resonant circuit.
In the operating state of rapid energization SB (
FIG. 2
d
), the first transistor T
1
is operated in the off state (OFF) and the transistors T
2
and T
3
are operated in the on state (ON). Current flows from the voltage source via the capacitor C, which is discharged in the process, the transistor T
3
toward the terminal AL
1
of the first coil, through the first coil toward the terminal AL
2
of the first coil
113
, through the transistor T
2
and the resistor R to the reference-ground potential. In the operating state of rapid energization SB, the voltage drop U
L
across the first coil
113
is equal to the sum of the supply voltage U
B
and the voltage drop U
C
across the capacitor C reduced by the forward voltages of the transistor T
2
and T
3
and the voltage drop across the resistor R.
The voltage drop U
L
across the first coil
113
is then about 80 V, for example, given a supply voltage U
V
of about 42 V. The rise of the current through the first coil
113
is then approximately twice as high as when merely the supply voltage U
B
is dropped across the first coil
113
.
A diode D
4
is connected in parallel with the capacitor C, and this ensures that the voltage potential at the drain terminal of the transistor T
3
does not fall below the supply voltage U
B
by more than the forward voltage of the diode D
4
.
FIG. 3
shows the first and second power output stages
32
,
33
in an embodiment in which both power output stages
32
,
33
are assigned a common capacitor C. This embodiment has the advantage that just one capacitor is provided, as a result of which the power output stages overall are cost-effective, and the capacitor C can be charged in an operating state Z
1
of the first power output stage
32
of rapid current reduction SSR, and can subsequently be discharged again in an operating stage BZ
2
of rapid energization SB of the second power output stage
34
. This is likewise possible in a converse manner. The reference symbols of the elements of the second power output stage
33
which correspond to the first power output stage
32
are in each case provided with a “′”.
FIG. 4
illustrates a flow diagram of a first program which is processed in the control unit
31
. The program is started in a step S
1
. The present desired position of the armature plate
116
is read in, this being predetermined by the superordinate control device. In a step S
2
, a check is made to determine whether the desired position of the armature plate
116
has changed from the closed position S to the open position O since the last calling of the first program. If this is the case, then the first power output stage
32
is controlled into the operating state BZ
1
of rapid current reduction SSR in a step S
3
. The first power output stage
32
changes over to the operating state BZ
1
of the quiescent state RZ as soon as the current through the first coil
113
becomes zero. The first program is then ended in step S
5
.
If the condition of step S
2
is not met, then in a step S
7
a check is made to determine whether there has been a transition in the desired position of the armature plate
116
from the open position O to the closed position S since the last calling of the first program. If this is the case, then a first regulator R
1
is activated in a step S
8
. The regulated quantity of the first regulator R
1
is the current through the first coil
113
. A capture value I_F is assigned to a desired value I_SP
1
of the current through the first coil
113
. A regulation difference RD is calculated from the difference between the desired value I_SP
1
and the actual value I_AV
1
of the current through the first coil
113
. The first regulator R
1
is preferably designed as a two-point regulator. The first regulator R
1
controls the first output stage
32
into the operating state BZ
1
either of normal energization NB or of freewheeling FL, depending on the regulation difference RD. The regulator R
1
remains activated until a predetermined condition is met indicating the striking of the armature plate
116
on the first bearing surface
115
a.
The predetermined condition may be, for example, that the armature plate has reached or exceeds a predetermined position. In this case, this predetermined position is chosen such that it is very near the closed position S.
As soon as the predetermined condition is met, the processing is continued in a step S
9
, in which the first regulator is activated again, the desired value I_SP
1
of the current through the first coil
113
being an increased holding value I_HE. In step S
9
, depending on the regulation difference RD, the first regulator R
1
controls the first power output stage
32
either into the operating state BZ
1
of rapid energization SB or into the operating state BZ
1
of freewheeling FL or, if the capacitor C is discharged, into the operating state BZ
1
of normal energization NB. Since the increased holding value I_HE is preferably greater than the capture value I_F, in step S
9
the first regulator controls the first power output stage
32
firstly into the operating state of rapid energization SB, until the actual value I_AV
1
of the current through the first coil is greater than the increased holding value I_HE, and/or into the operating state of normal energization as soon as the capacitor C is discharged, to be precise until the actual value I_AV
1
of the current through the first coil is greater than the increased holding value I_HE.
At the instant of the activation of the first regulator R
1
in step S
9
, the actual position of the armature plate
116
is very near or at the closed position S. For certain and reliable operation of the actuator, it must be ensured that the armature plate bears reliably on the first bearing surface and neither bounces off nor falls back to the rest position N before the closed position S has been reached. The controlling of the operating state BZ
1
of rapid energization SB makes it possible to set the actual value I_AV
1
of the current through the first coil
113
very rapidly to the increased holding value I_HE. This has the advantage that the first regulator R
1
, in step S
9
, can be activated immediately before the armature plate
116
strikes the first bearing surface
115
a,
with the result that the speed of the armature plate is no longer significantly increased and the noise of the armature plate striking the first bearing surface
115
a
is thus low. After a predetermined period of time has elapsed, which is preferably determined by experiments, the processing is continued in a step S
10
.
In step S
10
, the first regulator R
1
is activated, the desired value I_SP
1
of the current through the first coil
113
is the holding value I_H and the regulator controls the first power output stage
32
, depending on the regulation difference RD, either into the state of the operating state BZ
1
of normal energization NB or freewheeling FL until a transition takes place in the desired position of the armature plate from the closed position S to the open position O. The processing of the program is subsequently ended in step S
5
.
If the condition of step S
7
is not met, then the processing is continued in a step S
11
, in which a check is made to determine whether the desired position of the armature plate
116
is the closed position S or whether the capacitor C is charged to a predetermined value. Checking whether the capacitor C is charged to the predetermined value can be effected in a particularly simple manner by evaluation of a counter which is incremented each time a step S
13
is processed, and is reset in step S
8
. It is advantageous if a sensor is provided which detects the voltage drop U
C
across the capacitor C, and the charge of the capacitor C is determined from the voltage drop U
C
detected. If the condition of step S
11
is met, then the first regulator R
1
remains active, as in step S
10
, if the desired position of the armature plate
116
is the closed position S, and the first program is ended in step S
11
. If the condition of step S
11
is not met, however, then the processing is continued in a step S
13
, in which the first power output stage
32
is controlled into an operating state BZ
1
of normal energization NB, to be precise either for a fixedly predetermined period of time or until the actual value I_AV
1
of the current through the first coil
113
has reached a predetermined value. Afterward, in a step S
14
, the power output stage
32
is controlled in the operating state BZ
1
of rapid current reduction SSR. Thus, the capacitor C can simply be charged while the first coil
113
is not energized for capturing or holding the armature plate
116
. The processing of the program is then ended in step S
5
.
The first program is called cyclically, to be precise either at predetermined time intervals or after a predetermined change in the crankshaft angle. While the desired position of the armature plate
116
is the open position O, the first power output stage
32
is thus controlled into the operating state BZ
1
of rapid current reduction SSR once in step S
3
, and into the operating state BZ
1
of rapid current reduction a number of times in step S
14
, and the capacitor C is thus charged to the predetermined value within a predetermined period of time.
It is advantageous if, in step S
8
, the first coil
113
is controlled into the operating state of freewheeling as soon as the energy necessary for reaching the closed position has been fed to the armature plate. The first coil
113
is then in the state of freewheeling FL if the predetermined condition is met, indicating the striking of the armature plate
116
on the first bearing surface
115
a.
A flow diagram of a second program for controlling the second coil
115
is illustrated in
FIG. 5
, which program is processed in the control unit
31
. The second program has the same structure as the first program (FIG.
4
). Only the differences from the first program are described below.
In a step S
2
′, a check is made to determine whether the desired position of the armature plate
116
has changed from the open position O to the closed position S since the last calling of the first program. If this is the case, then the second power output stage is controlled into the operating state BZ
2
of rapid current reduction SSR in a step S
3
′. The second power output stage
34
changes over to the operating state BZ
2
of the quiescent state RZ as soon as the current through the second coil
115
becomes zero.
If the condition of step S
2
′ is not met, then a check is made in a step S
7
′ to determine whether there has been a transition in the desired position of the armature plate
116
from the closed position S to the open position O since the last calling of the second program.
In a step S
8
′, a second regulator R
2
is activated, whose regulated quantity is the current through the second coil
115
. A regulation difference RD′ is calculated from the difference between the desired value I_SP
2
and the actual value I_AV
2
of the current through the second coil
115
. The second regulator R
2
is preferably designed as a two-point regulator. The second regulator R
2
controls the second output stage
33
in a manner depending on the regulation difference RD′ in a corresponding way to how the first regulator R
1
controls the first output stage.
The regulator R
2
remains activated in step S
8
′ until a predetermined condition is met, indicating the striking of the armature plate
116
on the second bearing surface
115
b.
At the instant of the activation of the second regulator R
2
in step S
9
′, the actual position of the armature plate
116
is very near or at the open position O. For certain and reliable operation of the actuator, it must be ensured that the armature plate bears reliably on the second bearing surface and neither bounces off nor falls back into the rest position N before the open position O is reached.
If the condition of step S
7
′ is not met, then the processing is continued in a step S
11
′, in which a check is made to determine whether the desired position of the armature plate
116
is the open position O or whether the capacitor C is charged to a predetermined value.
If the condition of step S
11
′ is not met, then the processing is continued in a step S
13
′ in which the second power output stage
33
is controlled into an operating state BZ
1
of normal energization NB, to be precise either for the fixedly predetermined period of time or until the actual value I_AV
2
of the current through the second coil
115
has reached a predetermined value. Afterward, in a step S
14
′, the second power output stage
33
is controlled into the operating state BZ
2
of rapid current reduction SSR.
In
FIGS. 6
a
to
6
e,
signal profiles are plotted against time t. The time profile of the actual value I_AV
1
of the current through the first coil
113
is plotted in
FIG. 6
a.
The time profile of the voltage difference UGS
T1
between the gate and source terminals of the transistor T
1
is plotted in
FIG. 6
b.
The time profile of the voltage difference UGS
T2
between the gate terminal and the source terminal of the transistor T
2
is plotted in
FIG. 6
c.
The time profile of the voltage difference UGS
T3
between the gate terminal and the source terminal at the transistor T
3
is plotted in
FIG. 6
d.
If the voltage difference UGS
T1
has a high level HI, the transistor T
1
is in the on state (T
1
=ON) . If the voltage difference UGS
T1
at the transistor T
1
has a low level LO, the transistor turns off, that is to say is in the off state (T
1
=OFF). Likewise, the transistor T
2
turns on if the voltage difference UGS
T2
has a high level HI (T
2
=ON) and the transistor T
2
turns off if the voltage difference UGS
T2
has a low level LO (T
2
=OFF). If the voltage difference UGS
T3
between the gate terminal and the source terminal of the transistor T
3
has a high level, then the transistor T
3
is in the on state (T
3
=ON). If the voltage difference UGS
T3
between the gate terminal and the source terminal of the transistor T
3
has a low level, then the transistor T
3
turns off, that is to say it is in the off state (T
3
=OFF).
At an instant to, the desired position of the armature plate
116
is the open position O. The actual value I_AV
1
of the current through the coil is zero. At an intant t
1
, the first power output stage
32
is controlled into an operating state of normal energization NB, to be precise until the instant t
2
.
From the instant t
2
, the first power output stage
32
is controlled into the operating state BZ
1
of rapid current reduction SSR. Until the instant t
3
the voltage drop U
C
across the capacitor C has increased to a value U
C1
. Starting from the instant t
3
, the first power output stage
32
is then again controlled into the operating state BZ
1
of normal energization NB, to be precise until an instant t
4
. Starting from the instant t
5
, the first power output stage
32
is then again controlled into the operating state BZ
1
of rapid current reduction SSR, with the result that the voltage drop U
C
across the capacitor C has the value U
C2
at the instant t
5
.
Starting from the instant t
5
, the first power output stage
32
is then again controlled into the operating state BZ
1
of normal energization, to be precise until an instant t
6
, in which it is then again controlled into the operating state BZ
1
of rapid current reduction SSR until the instant t
7
. Starting from the instant t
7
, the desired value I_SP
1
of the current through the first coil is the capture value I_F and the first regulator R
1
is activated as in step S
8
(FIG.
4
), to be precise until an instant t
10
the position of the armature plate
116
has reached a predetermined value near or directly on the first bearing surface
115
a.
Starting from the instant t
10
, the first power output stage
32
is controlled into the operating state of rapid energization SB in order very rapidly to bring the actual value I_AV
1
of the current through the first coil to the new desired value I_SP
1
, to be precise of the increased holding value I_HE, and thus, if appropriate to prevent an imminent fallback of the armature into the rest position N or severe bouncing of the armature plate
116
. In this case, the capacitor C is discharged and the voltage drop across the capacitor U
C
decreases accordingly to the value zero at the instant t
11
. The first coil
113
is then energized with the increased holding current I_HE until the instant t
12
. Starting from the instant t
12
, the holding value I_H is predetermined as the desired value I_SP
1
of the current through the first coil, and starting from the instant t
14
, the open position O is predetermined as the desired position. Accordingly, the first power output stage
32
is controlled into the operating state BZ
1
of rapid current reduction SSR starting from the instant t
14
. In this case, the energy stored in the first coil
113
is fed to the capacitor C, whose voltage drop is increased to a value U
C1
* until an instant t
15
. Between the instant t
17
and t
18
and the instants t
19
, t
20
, the capacitor C is again charged until the capacitor has a voltage drop having the value U
C3
at the instant t
20
. The capacitor then has the predetermined charge and is charged further again only when the charge of the capacitor C has decreased.
Claims
- 1. A device for controlling an actuator which comprises a gas exchange valve and an electromagnetic actuating drive, having one electromagnet which has a coil, having an armature, whose armature plate can move between a first bearing surface on the electromagnet and a second bearing surface, the device comprising a power output stage provided for driving the coil,wherein the power out stage has an electrical energy store which is charged by the coil in a predetermined operating state, and wherein a control unit controls the power output stage into an operating state of rapid energization when a predetermined second condition is met indicating the striking of the armature plate or the first bearing surface or an imminent fallback of the armature plate from the first bearing surface to a rest position, the energy stored in the electrical energy store being fed to the coil in the operating state of rapid energization.
- 2. The device as claimed in claim 1, wherein the power output stage is charged in an operating state of rapid current reduction.
- 3. The device as claimed in claim 2, wherein the power output stage is controlled into the operating state of rapid current reduction within a period of time in which the desired position of the armature plate is on the second bearing surface.
- 4. The device as claimed in claim 1, further comprising the control unit, which controls the power output stage after a change of the desired position of the armature plate toward the second bearing surface into the operating state of rapid current reduction from a holding value to a zero value of the current through the coil, the electrical energy store being simultaneously charged.
- 5. The device as claimed in claim 4, wherein the control unit controls the power output stage alternately into an operating state of normal energization and of rapid current reduction during the movement of the armature plate away from the first bearing surface, or the bearing of the armature plate on the second bearing surface, to be precise until a predetermined first condition is met, which is characteristic of a predetermined charge of the electrical energy store.
- 6. The device as claimed in claim 1, wherein the power output stage has a first resonant circuit, which is a series circuit comprising a freewheeling diode, the coil, a diode and the electrical energy store in an order of enumeration from a reference-earth potential through to a terminal of a voltage source.
- 7. The device as claimed in claim 6, wherein the power output stage has a second resonant circuit, which is a series circuit comprising a first switching means, the coil, a second switching means and the electrical energy store in an order of enumeration from a reference-ground potential through to the voltage source.
- 8. The device as claimed in claim 1, wherein the actuating drive comprises a second electromagnet having a second coil and is provided with a second power output stage.
- 9. The device as claimed in claim 8, wherein a common electrical energy store is provided for both the power output stages.
- 10. The device as claimed in claim 9 wherein the electrical energy store is a capacitor.
Priority Claims (1)
Number |
Date |
Country |
Kind |
198 36 779 |
Aug 1998 |
DE |
|
PCT Information
Filing Document |
Filing Date |
Country |
Kind |
PCT/DE99/02085 |
|
WO |
00 |
Publishing Document |
Publishing Date |
Country |
Kind |
WO00/09867 |
2/24/2000 |
WO |
A |
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