Information
-
Patent Grant
-
6354253
-
Patent Number
6,354,253
-
Date Filed
Wednesday, September 1, 199925 years ago
-
Date Issued
Tuesday, March 12, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 123 9011
- 123 9055
- 123 9049
- 123 9052
- 251 12901
- 251 1291
- 251 12915
- 251 12916
-
International Classifications
-
Abstract
A solenoid valve device includes an engine valve which can move in an axial direction thereof, an armature which moves with the engine valve, an electromagnet which attracts the engine valve so that the engine valve moves in the axial direction, and a zero-lash adjuster mechanism which is interposed between the engine valve and the armature. Thus, the solenoid valve can positively actuate an engine valve between a fully closed position and a fully opened position without formation of a clearance between the engine valve and the armature. A current supplied to the electromagnet may be set in accordance with a value which is related to a relative position of the armature and the electromagnet.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to a solenoid valve device, and particularly to a solenoid valve which actuates an engine valve by an armature attracted by an electromagnet.
2. Description of the Related Art
Conventionally, as disclosed in Japanese Laid-Open Patent Application No. 7-332044, there is known a solenoid valve having an engine valve which functions as an intake valve or an exhaust valve of an internal combustion engine. In this solenoid valve, an armature is connected to the engine valve, and electromagnets are disposed above and below the armature, respectively. The electromagnets exert electromagnetic forces on the armature in a valve-closing direction and a valve-opening direction, respectively. The engine valve is so constructed that it is seated on a valve seat provided to a cylinder head of the engine when the armature is in contact with the electromagnet for closing. Thus, according to the above-mentioned conventional solenoid valve, the engine valve can be moved between a fully opened position and a fully closed position by alternately energizing the electromagnets.
Generally, the cylinder head of the engine is heated to a high temperature in association with combustion in a combustion chamber. Thus, the engine valve is also heated to a high temperature by heat transferred from the cylinder head. In this case, the cylinder head and the engine valve thermally expand to different extents due to a difference in a thermal capacity and a thermal expansion coefficient. If the engine valve thermally expands to a greater extent than the cylinder head, the engine valve may not be seated on the valve seat when the armature is in contact with the electromagnet for closing. In this case, a clearance is generated between the engine valve and the valve seat. Similarly, when the valve seat or the engine valve is worn away, the engine valve may not be seated on the valve seat.
SUMMARY OF THE INVENTION
It is a first object of the present invention to provide a solenoid valve device which can positively actuate an engine valve between a fully closed position and a fully opened position without formation of a clearance between the engine valve and an armature.
It is a second object of the present invention to properly control a current supplied to an electromagnet of the solenoid valve device.
The first object of the present invention can be achieved by a solenoid valve device, comprising:
an engine valve which can move in an axial direction thereof;
an armature which moves with the engine valve;
an electromagnet which attracts the engine valve so that the engine valve moves in the axial direction; and
a zero-lash adjuster mechanism which is interposed between the engine valve and the armature.
In this invention, the zero-lash adjuster mechanism is interposed between the engine valve and the armature. Thus, a change in a spacing between the engine valve and the armature can be compensated for by the zero-lash adjuster mechanism so that formation of a clearance between the engine valve can be prevented. Therefore, according to this invention, it is possible to positively actuate the engine valve while preventing formation of a clearance between the armature and the engine valve. When there is no clearance between the armature and the engine valve, the armature does not impact on the engine valve when the engine valve is actuated. Thus, according to the present invention, it is also possible to reduce an operating sound of the solenoid valve.
In this case, the zero-lash adjuster mechanism may be a displacement-compensating mechanism which can expand in accordance with an increase in a spacing between the engine valve and the armature.
In this invention, an increase in the spacing between the engine valve and the armature can be compensated for by an expansion of the zero-lash adjuster mechanism. Thus, formation of a clearance between the engine valve can be prevented irrespective of a change in the spacing therebetween. Therefore, according to this invention, it is possible to positively actuate the engine valve while reducing an operating sound of the solenoid valve device.
In this case, the displacement-compensating mechanism may be constituted so that it can expand when the engine valve is in a closed position.
In this invention, the displacement-compensating mechanism can expand when the engine valve is in a closed position. A change in a spacing between the engine valve and the armature is generated when the engine valve reaches a closed position. Thus, formation of a clearance between the engine valve and the armature can be effectively prevented by the displacement-compensating mechanism expanding when the engine valve is in a closed position.
In the solenoid valve device of the present invention, at least part of the displacement-compensating mechanism may be disposed inside the electromagnet.
In this invention, since at least a part of the displacement-compensating mechanism is disposed inside the electromagnet, a total height of the solenoid valve device need not be enlarged by a full height of the displacement-compensating mechanism. Thus, according to this invention, it is possible to reduce the total height of the solenoid valve device.
Additionally, in the solenoid valve device of the present invention, the zero-lash adjuster mechanism may comprise:
a displacement-compensating mechanism which can expand when no compressing force is exerted thereon;
a swing arm which is connected to one end of the displacement-compensating mechanism so that the swing arm can swing around the one end and is in contact with both the armature and the engine valve so that the armature moves in a valve-closing direction when the displacement-compensating mechanism expands.
In this invention, in a state where the engine valve is opened, the armature exerts a force on the swing arm in the valve-opening direction. Since the swing arm is in contact with both the armature and the engine valve so that the armature moves in the valve-closing direction when the displacement-compensating mechanism expands, the force exerted on the swing arm in the valve-opening direction by the armature is transmitted to the displacement-compensating mechanism as a compressing force. In this case, the displacement-compensating mechanism is not allowed.
On the other hand, in a state where the engine valve is closed, the armature does not exert a force on the swing arm in the valve-opening direction. In this case, the displacement-compensating mechanism is allowed to expand since no compressing force is exerted thereon. Thus, when a spacing between the engine valve and the armature increases, that is, when the armature shifts in the valve-closing direction relative to the engine valve, in a state where the engine valve is closed, the displacement-compensating mechanism expands so that the swing arm swings so as to maintain a state in which the swing arm is in contact with both the armature and the engine valve.
In this way, formation of a clearance between the engine valve and the armature can be prevented. Additionally, since only the swing arm moves in accordance of a movement of the engine valve and the displacement-compensating mechanism is maintained still, a mass of a movable part of the solenoid valve device can be reduced. Thus, according to this invention, it is possible to improve a response of the solenoid valve device.
Additionally, the displacement-compensating mechanism may be a hydraulic zero-lash adjuster which can expand by being supplied with an oil pressure.
In this case, the solenoid valve device may further comprise an oil pressure supplying mechanism for supplying an oil pressure to the hydraulic zero-lash adjuster when the engine valve is closed.
In this invention, in a state where the engine valve is closed, an oil pressure in the hydraulic zero-lash adjuster is maintained to be relatively low since no compressing force is exerted thereon. Thus, by supplying an oil pressure to the hydraulic zero-lash adjuster in such a state, it is possible to reduce a required oil pressure to be supplied to the hydraulic zero-lash adjuster.
The above-mentioned second object of the present invention can be achieved by the solenoid valve device further comprising:
a current source which supplies a current to the electromagnet;
a current setting part which sets the current supplied to the electromagnet by the current source to be a value which is different from a value used in a regular situation for a predetermined period after the hydraulic zero-lash adjuster starts being supplied with an oil pressure.
In this invention, immediately after the hydraulic zero-lash adjuster starts being supplied with an oil pressure, the hydraulic zero-lash adjuster does not sufficiently expand. In this case, a position of the armature is shifted toward the engine valve as compared to a regular state (that is, a state in which the hydraulic zero-lash adjuster has expanded so as to cancel a clearance between the engine valve and the armature). On the other hand, a current to be supplied to the electromagnet to exert a required electromagnetic force on the armature changes in accordance with a distance between the armature and the electromagnet. Thus, according to this invention, it is possible to exert a proper electromagnetic force on the armature by setting a current supplied to the electromagnet to be a value which is different from a value used in a regular situation for a predetermined period after the hydraulic zero-lash adjuster starts being supplied with an oil pressure.
The above-mentioned second object of the present invention can also be achieved by a controller for controlling the solenoid valve device comprising:
a current source which supplies a current to the electromagnet;
a relative position detector which detects a value which is related to a relative position of the armature and the electromagnet; and
a current setting part which sets the current supplied to the electromagnet by the current source in accordance with the value detected by the relative position detector.
In this invention, a current to be supplied to the electromagnet is set in accordance with a distance between the armature and the electromagnet. Thus, according to this invention, since the current supplied to the electromagnet is set in accordance with a value related to a relative position of the armature and the electromagnet, a proper force can be exerted on the armature so that the engine valve can be positively actuated.
In this case, the value related to the relative position of the armature and the electromagnet may be a time which has elapsed after the hydraulic zero-lash adjuster stops being supplied with an oil pressure until the hydraulic zero-lash adjuster starts being supplied with an oil pressure.
In this invention, in a state where the hydraulic zero-lash adjuster is supplied with no oil pressure, the hydraulic zero-lash adjuster gradually contracts with a passage of time since oil leaks out from the hydraulic zero-lash adjuster. The relative position of the armature and the engine valve changes in accordance with the contraction of the hydraulic zero-lash adjuster. Thus, the time which has elapsed after the hydraulic zero-lash adjuster stops being supplied with an oil pressure until the hydraulic zero-lash adjuster starts being supplied with an oil pressure is related to the relative position of the engine valve and the armature.
Additionally, the value related to the relative position of the armature and the electromagnet may be an oil pressure which is supplied to the hydraulic zero-lash adjuster.
In this invention, an amount of expansion of the hydraulic zero-lash adjuster changes in accordance with an oil pressure supplied to the hydraulic zero-lash adjuster. The relative position of the armature and the engine valve changes in accordance with the contraction of the hydraulic zero-lash adjuster, as mentioned above. Thus, an oil pressure which is supplied to the hydraulic zero-lash adjuster is related to a relative position of the armature and the electromagnet.
The solenoid valve device may further comprise a failure detector which detects a failure in a system for supplying an oil pressure to the hydraulic zero-lash adjuster, wherein the value related to the relative position of the armature and the electromagnet is related to the failure detected by the failure detector.
In this invention, when a failure has occurred in the system for supplying an oil pressure to the hydraulic zero-lash adjuster, the oil pressure supplied to the hydraulic zero-lash adjuster decreases. An amount of expansion of the hydraulic zero-lash adjuster changes in accordance with the oil pressure supplied to the hydraulic zero-lash adjuster and a relative position of the armature and the electromagnet changes in accordance with an amount of expansion of the hydraulic zero-lash adjuster. Thus, the value related to a relative position of the armature and the electromagnet can be related to the failure in the system for supplying an oil pressure to the hydraulic zero-lash adjuster.
Other objects and further features of the present invention will be apparent from the following detailed description when read in conjunction with the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a diagram showing a cross section of a solenoid valve device according to a first embodiment of the present invention;
FIG. 2
is a diagram showing a relationship between a tappet clearance and an operating sound of the solenoid valve device;
FIG. 3
is a diagram showing an enlarged cross section of a zero-lash adjuster and neighboring parts thereof;
FIG. 4A
is a diagram showing a displacement of the engine valve moving between a fully closed position and a fully opened position;
FIGS. 4B and 4C
are diagrams showing waveforms of vibrations generated in association with the movement of the engine valve in a case where the zero-lash adjuster is not provided and in a case where the zero-lash adjuster is provided, respectively;
FIG. 5
is a cross-sectional view showing a process of assembling the zero-lash adjuster;
FIG. 6
is a cross-sectional view showing another process of assembling the zero-lash adjuster;
FIG. 7
is a diagram showing cross section of a solenoid valve device of a second embodiment according to the present invention;
FIG. 8
is a diagram showing a cross section of a solenoid valve device of a third embodiment according to the present invention;
FIG. 9
is a diagram showing an enlarged axial cross section of the zero-lash adjuster;
FIG. 10
is a diagram showing a cross section of a solenoid valve device of a fourth embodiment according to the present invention;
FIG. 11
is a diagram showing an enlarged cross section of a zero lash adjuster and neighboring parts thereof in the present embodiment;
FIG. 12
is a diagram schematically showing a top view of an arrangement in which an armature shaft and the zero-lash adjuster are offset with respect to the engine valve in an outwardly radial direction of a cylinder bore of an engine;
FIGS. 13A and 13B
are diagrams showing instruction currents supplied to an upper coil and a lower coil, respectively, after an ignition switch is turned on until the engine valve starts being actuated between the fully closed position and the fully opened position in a fifth embodiment of the present embodiment;
FIG. 13C
is a diagram showing a displacement of the engine valve when the instruction currents shown in
FIGS. 13A and 13B
are supplied to the respective coils;
FIG. 14
is a diagram showing a relationship between a position of the armature and an electromagnetic force acting between the armature and a lower core when a current supplied to the lower coil is changed in three steps;
FIG. 15
is a diagram showing a map which is referred to so as to determine the instruction currents I
L
and I
U
in an initial actuation in accordance with a position of the armature;
FIG. 16
is a diagram showing a perspective view of an arrangement for detecting a position of the armature;
FIG. 17
is a diagram showing an axial cross section of a valve guide and a valve shaft in the present embodiment;
FIG. 18
is a diagram showing changes in a relative position of gap sensors and a recessed part provided on a valve shaft when the engine valve moves from the fully closed position to the fully opened position;
FIG. 19
is a diagram showing a change in the output voltage V when the engine valve moves from the fully closed position to the fully opened position;
FIG. 20
is a flowchart performed by an ECU in the present embodiment;
FIG. 21
is a diagram showing an example of an arrangement for directly detecting a position of the armature using a gap sensor;
FIG. 22
is a diagram showing an example of an arrangement for directly detecting a position of the armature using a laser distance sensor;
FIGS. 23A and 23B
are diagrams schematically showing the solenoid valve device when the armature is in the fully opened position in a case where leak-down of the zero-lash adjuster has not occurred and in a case where leak-down of the zero-lash adjuster has occurred, respectively;
FIGS. 24A and 24B
are diagrams showing instruction currents supplied to the upper coil and the lower coil, respectively, in a sixth embodiment of the present invention;
FIG. 25
is a diagram showing a flowchart of a routine performed by the ECU in the present embodiment;
FIG. 26
is a diagram showing an example of a relationship between a valve stopping time T
S
and a displacement of the armature toward the lower core from a reference neutral position;
FIG. 27
is a map which is referred to so as to determine the values I
A1
, I
A2
of the attracting current I
A
and the values I
H1
, I
H2
of the holding current I
H
based on the valve stopping time T
s
in a seventh embodiment of the present invention;
FIG. 28
is diagram showing a flowchart of a routine performed by the ECU in the present embodiment;
FIGS. 29A
to
29
E are diagrams showing changes in an engine speed, a supplied oil pressure P, a tappet clearance, an attracting current to the upper coil, and an attracting current to the lower coil
62
in an eighth embodiment of the present invention;
FIG. 30
is diagram showing a flowchart of a routine performed by the ECU in the present embodiment;
FIG. 31
is a diagram showing an example of a map which is referred to so as to determine correction values ΔI
1
and ΔI
2
in the routine shown in
FIG. 30
;
FIG. 32
is a diagram showing a flowchart of a routine performed by the ECU in a ninth embodiment of the present invention;
FIG. 33
is a diagram showing an example of a map which is referred to so as to determine the correction values ΔI
1
and ΔI
2
in the routine shown in
FIG. 32
; and
FIG. 34
is a routine performed by the ECU
11
in a tenth embodiment of the present invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1
is a diagram showing a cross section of a solenoid valve device
10
according to a first embodiment of the present invention. The solenoid valve device
10
of the present embodiment is provided to each of intake valves and exhaust valves of an internal combustion engine. The solenoid valve device
10
is controlled by an electronic control unit (hereinafter referred to as an ECU)
11
.
As shown in
FIG. 1
, the solenoid valve device
10
has an engine valve
12
which functions as an intake valve or an exhaust valve. The engine valve
12
is disposed in a lower head
16
so that the engine valve
12
is exposed in a combustion chamber
14
of the engine. A port
18
is formed in the lower head
16
. An opening part of the port
18
into the combustion chamber
14
is provided with a valve seat
20
associated with the engine valve
12
. The port
18
communicates with the combustion chamber
14
when the engine valve
12
is released from the valve seat
20
, and the port
16
is disconnected from the combustion chamber
14
when the engine valve
12
is seated on the valve seat
20
.
A cylinder head spacer
24
is provided on a top of the lower head
16
via a thermal insulation plate
22
. The thermal insulation plate
22
is a sheet-like member formed from a thermally insulating material such as Bakelite, and functions to prevent heat generated in the combustion chamber
14
from being transferred to the cylinder head spacer
24
. An upper head
25
is provided on a top of the cylinder head spacer
24
.
The engine valve
12
comprises a valve shaft
26
extending upwardly. The valve shaft
26
is guided by a valve guide
28
so that the valve shaft
26
can move in an axial direction. The valve guide
28
is held in the lower head
16
. The lower head
16
is provided with a spring containing space
30
which is cylindrically formed and surrounds a substantially upper-half part of the valve shaft
26
. An upper end part of the valve guide
28
is exposed in the spring containing space
30
. A valve stem seal
31
is mounted on an upper end of the valve guide
28
.
A cotter
32
is mounted on the valve shaft
26
at a position near an upper end thereof. The cotter
32
is a substantially cylindrical member having a taper-shaped outer surface whose diameter increases toward an upward direction. A projection is formed on an inner surface of the cotter
32
. The projection is fitted into a recess formed on a surface of the valve shaft
26
. A lower retainer
34
is fitted around the cotter
32
.
A spring seat
36
is disposed on a bottom face of the spring containing space
30
. A lower spring
38
is disposed between the spring seat
36
and the lower retainer
34
. The lower spring
38
exerts a resilient force on the lower retainer
34
so as to push the engine valve
12
in an upward direction, that is, in a direction in which the engine valve
12
approaches the valve seat
20
. In this specification, an upward direction, that is, a direction in which the engine valve
12
approaches the valve seat
20
may also be referred to as a valve-closing direction. Additionally, a downward direction, that is, a direction in which the engine valve
12
moves away from the valve seat
20
may also be referred to as a valve-closing direction.
An armature shaft
42
is disposed coaxially with the valve shaft
26
. A zero-lash adjuster
40
is interposed between the armature shaft
42
and the valve shaft
26
. A detailed description of the zero-lash adjuster
40
will be given later.
A cotter
44
is mounted on an upper end part of the armature shaft
42
. The cotter
44
has a structure which is symmetric to the cotter
32
in the axial direction. An upper retainer
46
is fitted around the cotter
44
. A lower end of an upper spring
48
abuts on a top surface of the upper retainer
46
. A cylindrical upper case
50
is provided around the upper spring
48
. An adjuster bolt
52
is screwed on a top part of the upper case
50
. An upper end of the upper spring
48
is supported by a spring guide
54
which is interposed between the adjuster bolt
52
and the upper spring
48
. The upper spring
48
pushes the armature shaft
42
via the upper retainer
48
in a downward direction.
An armature
56
is fixed to the armature shaft
42
at a substantially center position in the axial direction. The armature
56
is an annular member which is formed from a soft magnetic material. An upper coil
58
and an upper core
60
are disposed above the armature
56
. Additionally, a lower coil
62
and a lower coil
64
are disposed below the armature
56
. The upper coil
58
and the lower coil
62
are contained in annular recesses
60
a
,
64
a
, respectively, formed in the upper core
60
and the lower core
64
a,
respectively.
The upper coil
58
and the lower coil
62
are electrically connected to an actuating circuit
65
. The actuating circuit
65
supplies instruction currents in accordance with control signals supplied from the ECU
11
.
The upper core
60
and the lower core
64
have through holes
60
b
and
64
b
, respectively, which go though the center parts thereof. An upper bush
66
is disposed in an upper end part of the through hole
60
b
. Additionally, a lower bush
68
is disposed in a lower end part of the through hole
64
b
. The armature shaft
42
is guided by the upper bush
66
and the lower bush
68
so that the armature shaft
42
can move in the axial direction. The upper core
60
includes a flange
60
c
formed at an upper end part thereof.
Similarly, the lower core
64
includes a flange
64
c
formed at a lower end part thereof.
A lash-adjuster containing space
24
a
is cylindrically formed in the cylinder head spacer
24
. The lash-adjuster containing space
24
a
goes through the cylinder head spacer
24
coaxially with the above-mentioned spring containing space
30
. The zero-lash adjuster
40
is supported in the lash-adjuster containing space
24
a
. A raised part
24
b
which is upwardly raised is formed on an upper surface of the cylinder head spacer
24
around an opening part of the lash-adjuster containing space
24
a
. Further, a cylindrical part
24
c
is formed on a top of the raised part
24
b.
A cylindrical core containing space
25
a
is formed in the upper head
25
. The core containing space
25
a
goes through the upper head
25
coaxially with the spring containing space
30
and the lash-adjuster containing space
24
a
. The upper core
60
is inserted into the core containing space
25
a
so that the flange
60
c
abuts on an upper face of the upper head
25
via a shim
70
. On the other hand, the lower core
64
is inserted into the core containing space
25
a
so that the flange
64
c
abuts on a lower face of the upper head
25
. The flange
60
c
of the upper core
60
is supported between the upper head
25
and a flange
50
a
formed at a lower end of the upper case
50
. Additionally, the flange
64
c
of the lower core
64
is supported between the upper head
25
and a lower bracket
72
.
The upper case
50
and the lower bracket
72
are fixed to the upper head
25
by fixing bolts
74
,
76
so that the upper core
60
and the lower core
64
are fixed with a predetermined spacing being formed therebetween. In such a state, a predetermined clearance is provided between the raised part
24
b
of the cylinder head spacer
24
and a lower surface of the lower core
64
. A neutral position of the armature
56
is adjusted by the above-mentioned adjuster bolt
52
so as to be at a central position between the upper core
60
and the lower core
64
.
Oil supply passages
80
and
82
are formed in the cylinder head spacer
24
. The oil supply passages
80
and
82
are connected to each other. Pressurized oil is supplied to the oil supply passage
82
from an oil pump
83
. The oil pump
83
is actuated by, for example, using a rotation of an output shaft of the engine as a power source. The oil supply passage
80
opens on an inner wall of the lash-adjuster containing space
24
a
at a predetermined position.
A pressure sensor
84
is provided to a passage connecting the oil pump
83
and the oil supply passage
82
. The pressure sensor
84
delivers a signal to the ECU
11
in accordance with an oil pressure in the passage, that is, an oil pressure which is supplied to the zero-lash adjuster
40
. Hereinafter, this oil pressure is referred to as a supplied oil pressure P. The ECU
11
detects the supplied oil pressure P based on the signal delivered by the pressure sensor
84
. The pressure sensor
84
may be provided to the oil supply passage
82
or
80
.
An oil collecting passage
85
is also formed in the cylinder head spacer
24
. An upper end of the oil collecting passage
85
opens on an upper surface of the cylinder head spacer
24
at a part near the raised part
24
b
, and a lower end of the oil collecting passage
85
opens into the spring containing space
30
. The upper end part of the oil collecting passage
85
is constituted by drilled holes
85
a
,
85
b
so that the oil collecting passage
85
has a large opening area on the upper surface of the cylinder head spacer
24
. The oil collecting passage
85
functions to collect oil which has flown out above the zero-lash adjuster
40
and to supply the collected oil into the spring containing space
30
so as to provide lubrication of the valve shaft
26
.
Next, a description will be given of an operation of the solenoid valve device
10
.
When a current is supplied to the upper coil
58
, an electromagnetic force is exerted on the armature
56
in a direction toward the upper core
60
. Thus, the armature
56
moves upwardly against the resilient force of the upper spring
48
until the armature
56
comes into contact with the upper core
60
, as shown in FIG.
1
. In this state, the engine valve
12
is seated on the valve seat
20
. Hereinafter, a position of the armature
56
or the engine valve
12
in the above-mentioned state where the armature is in contact with the upper core
60
is referred to as a fully closed position.
When the current to the upper coil
58
is cut off in the state where the engine valve
12
is in the fully closed position, an electromagnetic force which is required to maintain the armature
56
in the fully closed position disappears. In this case, the armature shaft
42
starts moving downwardly together with the engine valve
12
due to the resilient force of the upper spring
48
. Thus, the engine valve
12
is released from the valve seat
20
. When a current is supplied to the lower coil
62
at a time when the armature shaft
42
reaches a predetermined position, an electromagnetic force is generated which pushes the armature
56
toward the lower core
64
.
When the above electromagnetic force is exerted on the armature
56
, the armature
56
moves further downwardly against the resilient force of the lower spring
38
until the armature
56
comes into contact with the lower core
64
. Hereinafter, a position of the armature
56
or the engine valve
12
in a state where the armature
56
is in contact with the lower core
64
is referred to as a fully opened position. When the current to the lower coil
62
is cut off in this state, an electromagnetic force which is required to maintain the armature
56
in the fully opened state disappears. In this case, the armature shaft
42
starts moving upwardly together with the engine valve
12
by the resilient force of the lower spring
38
.
When a current is supplied to the upper coil
58
at a time when the armature shaft
42
reaches a predetermined position, the armature
56
moves upwardly by an electromagnetic force generated by the upper coil
58
until the armature
56
comes into contact with the upper core
60
. In the state where the armature
56
is in contact with the upper core
60
, the engine valve
12
is seated on the valve seat
20
, as mentioned above.
In this way, according to the present embodiment, it is possible to actuate the engine valve
12
between the fully closed position and the fully opened position by alternately supplying currents to the upper coil
58
and the lower coil
62
at proper timings.
As mentioned above, the engine valve
12
is exposed in the combustion chamber
14
of the engine. Thus, the engine valve
12
is rapidly heated by high heat in the combustion chamber
14
being directly transferred thereto. On the other hand, since the lower head
16
has a relatively large thermal capacity, the lower head
16
is moderately heated as compared to the engine valve
12
. Accordingly, a temperature of the engine valve
12
becomes higher than a temperature of the lower head
16
, and as a result, the engine valve
12
thermally expands to a greater extent than the lower head
16
.
In such a situation, if the engine valve
12
and the armature shaft
42
are rigidly connected to each other in the fully closed state, the engine valve
12
is prevented from expanding in the valve-closing direction by the armature shaft
42
, and, thus, the engine valve
12
expands in the valve-opening direction. That is, the engine valve
12
moves in the valve-opening direction with respect to the valve seat
20
, and a clearance is formed between the engine valve
12
and the valve seat
20
. Similarly, when contacting surfaces of the engine valve
12
and the valve seat
20
are worn, a clearance is formed between the engine valve
12
and the valve seat
20
. In this way, if the engine valve
12
and the armature shaft
42
are rigidly connected to each other, it may not be possible to fully close the engine valve
12
due to a difference in the thermal expansion between the engine valve
12
and the lower head
16
or wear of the engine valve
12
and the valve seat
20
.
The above problem can be avoided by providing a clearance between the armature shaft
42
and the valve shaft
26
in a state where the armature
56
is in contact with the upper core
60
and the engine valve
12
is seated on the valve seat
20
, that is, in a state where the armature
56
and the engine valve
12
are in the fully closed position. This clearance is generally called a tappet clearance. However, when the tappet clearance is provided, an operating sound of the solenoid valve device
10
becomes large for the following reason.
That is, when the engine valve
12
moves from the fully closed position to the fully opened position, a first impact sound is generated when the armature shaft
42
impacts on the valve shaft
26
, and then a second impact sound is generated when armature
56
impacts on the lower core
64
. On the other hand, when the engine valve
12
moves from the fully opened position to the fully closed position, a first impact sound is generated when the engine valve
12
impacts on the valve seat
20
, and then a second impact sound is generated when the armature
56
impacts or on the upper core
60
. In this way, impact sounds are generated twice in each case, resulting in an increased operating sound of the solenoid valve device
10
.
FIG. 2
is a diagram showing a relationship between the tappet clearance and an operating sound of the solenoid valve device
10
. As shown in
FIG. 2
, a larger operating sound is generated for a larger tappet clearance. This is due to a fact that, as the tappet clearance becomes larger, a speed with which the armature shaft
42
impacts on the valve shaft
26
becomes higher and thus a larger impact sound is generated. Therefore, if a larger tappet clearance is provided so as to compensate for a larger difference in the thermal expansion between the engine valve
12
and the lower head
16
or larger wear of the engine valve
12
or the valve seat
20
, the operating sound of the solenoid valve device
10
becomes larger.
For the above-mentioned reason, it is not desirable to provide a tappet clearance between the valve shaft
26
and the armature shaft
42
in view of reducing the operating sound of the solenoid valve device.
In the solenoid valve device
10
of the present embodiment, the zero-lash adjuster
40
which is interposed between the armature shaft
42
and the valve shaft
26
functions to positively move the engine valve
12
to the fully closed position irrespective of the above-mentioned difference in the thermal expansion of the engine valve
12
and the lower head
16
or wear of the engine valve
12
and the valve seat
20
, without causing an increase in the operating sound of the solenoid valve device
10
. Now, a detailed description will be given of the zero-lash adjuster
40
.
FIG. 3
is a diagram showing an enlarged cross section of the zero-lash adjuster
40
and neighboring parts thereof. The state shown in
FIG. 3
is achieved when the armature
56
is in contact with the upper core
60
.
As shown in
FIG. 3
, the zero-lash adjuster
40
includes a plunger body
100
. The plunger body
100
is a cylindrical member with a lower end thereof being closed. The plunger body
100
is supported in the lash-adjuster containing space
24
a
so that it can slide in the axial direction. A spring retaining part
100
a
is formed inside the plunger body
100
in a lower part thereof. Additionally, a plunger retaining part
100
b
having a larger diameter than that of the spring retaining part
100
a
is formed inside the plunger body
100
above the spring retaining part
100
a.
A plunger
102
is supported in the plunger retaining part
100
b
so that it can slide in the axial direction. A hydraulic pressure chamber
104
is defined by a bottom surface of the plunger
102
and a bottom surface of the spring retaining part
100
a.
The plunger
102
has a large-diameter part
102
a
which slides on an inner surface of the plunger retaining part
100
b
. Additionally, the plunger
102
has a small-diameter part
102
b
provided at an upper end thereof. A stopper ring
106
is pressed in an upper end of the plunger retaining space
100
b
. The stopper ring
106
has a diameter which is smaller than a diameter of the large-diameter part
102
a
of the plunger
102
. Therefore, an upward movement of the plunger
102
inside the plunger body
100
is limited by the stopper ring
106
being engaged with a step between the large-diameter part
102
a
and the small-diameter part
102
b
. The plunger
102
also has a reservoir
108
which outwardly opens and a connecting passage
110
which connects the reservoir
108
and the hydraulic pressure chamber
104
.
A retainer
112
and a plunger spring
114
are disposed in the hydraulic chamber
104
. The plunger spring
114
pushes the plunger
102
in an upward direction via the retainer
112
. A check ball
116
and a check ball spring
118
are disposed inside the retainer
112
. The check ball spring
118
pushes the check ball
116
toward an opening of the connecting passage
110
. The check ball
116
and the check ball spring
118
function as a check valve which opens only when a pressure in the hydraulic pressure chamber
104
is lower than a pressure in the reservoir
108
by a predetermined value.
The zero-lash adjuster
40
also includes a reservoir cap
120
. The reservoir cap
120
is a substantially cylindrical member with a lower end thereof being closed. The reservoir cap
120
is disposed inside the lash-adjuster containing space
24
a
so that it can slide in the axial direction with an outer bottom face of the reservoir cap
120
being in contact with a upper end face of the plunger
102
. A part of the outer bottom face of the reservoir cap
120
is cut off to form an overflow recess
122
. The overflow recess
122
always communicates with the reservoir
108
.
A lower end face of the armature shaft
42
is in contact with an inner bottom face of the reservoir cap
120
. On the other hand, an upper end face of the valve shaft
26
is in contact with an outer bottom face of the plunger body
100
. The above-mentioned oil supply passage
82
opens on an internal wall of the lash-adjuster containing space
24
a
so that the oil supply passage
82
communicates with the overflow recess
122
in a state shown in
FIG. 3
(that is, a state where the armature
56
is in contact with the upper core
60
).
When the upper coil
58
is de-energized in the state shown in
FIG. 3
, an actuating force is exerted on the armature shaft
42
in the valve-opening direction, as mentioned above. This force is transmitted to the plunger
102
via the reservoir cap
120
. When the force transmitted to the plunger
102
exceeds a resilient force
114
of the plunger spring
114
, oil contained in the hydraulic pressure chamber
104
is pressurized by the plunger
102
being pressed in a downward direction. Thus, a pressure in the hydraulic pressure chamber
104
becomes higher than a pressure in the reservoir
108
, and, as a result, the connecting passage
110
is closed by a check ball
116
. When the connecting passage
110
is thus closed, a flow of oil between the hydraulic pressure chamber
104
and the reservoir
108
is prohibited. In this case, the actuating force is transmitted to the plunger body
100
via the hydraulic pressure chamber
104
, and, thus, the zero-lash adjuster
40
moves in the valve-opening direction together with the armature shaft
42
and the engine valve
12
.
In a process in which the zero-lash adjuster
40
moves in the valve-opening direction, oil in the hydraulic pressure chamber
104
gradually leaks out through the sliding surface between the plunger
102
and the plunger body
100
. Thus, the zero-lash adjuster
40
slightly contracts in the axial direction in accordance with the leakage of oil.
When the lower coil
62
is de-energized after the armature has come into contact with the lower core
64
, the armature
56
starts moving in the valve-closing direction. After the valve
12
is seated on the valve seat
20
, a resilient force of the lower spring
38
is no longer exerted on the plunger body
100
, while the armature
56
moves in the valve-closing direction by a small distance corresponding to an amount of the contraction of the zero-lash adjuster
40
. In this case, the plunger
102
is pushed toward the reservoir cap
120
by a resilient force of the plunger spring
114
, and, as a result, a pressure in the hydraulic pressure chamber
104
is decreased. When the pressure in the hydraulic pressure chamber
104
becomes lower than a pressure in the reservoir
108
, the hydraulic pressure chamber
104
and the reservoir
108
are connected to each other by the check ball
116
being released from an opening of the connecting passage
110
. As mentioned above, when the engine valve
12
is seated on the valve seat
20
, the overflow recess
122
communicates with the oil supply passage
82
. Thus, when the hydraulic pressure chamber
104
and the reservoir
108
are connected to each other, pressured oil is supplied to the hydraulic pressure chamber
104
from the oil supply passage
82
via the reservoir
108
. In this case, the plunger
102
moves in an upward direction until the armature
56
comes into contact with the upper core
60
, with a state where the plunger
102
is in contact with the reservoir cap
120
being maintained.
As mentioned above, the zero-lash adjuster is a mechanism having the following function:
in a state where the engine valve
12
is released from the valve seat
20
and thus a force is exerted on the plunger body
100
in the valve opening direction by the reservoir cap
120
as a reaction force to the resilient force of the lower spring
38
, that is, in a state where an axial compressing force is exerted on the zero-lash adjuster
40
, the zero-lash adjuster moves together with the armature shaft
42
and the engine valve
12
while gradually contracting; and
in a state where the engine valve
12
is seated on the valve seat
20
and thus no compressing force is exerted on the zero-lash adjuster
40
, the plunger
102
is allowed to move relative to the plunger body
100
so that the zero-lash adjuster
40
axially expands.
According to this function of the zero-lash adjuster
40
, it is possible to prevent a clearance from being formed between the valve shaft
26
and the armature shaft
42
when the engine valve
12
is in the fully closed position.
It should be noted that a change in a distance between the valve shaft
26
and the armature shaft
42
due to a difference in the thermal expansion between the engine valve
12
and the lower head
16
or wear of the engine valve
12
and the valve seat
20
occurs slowly. Therefore, an amount of the change in the distance between the valve shaft
26
and the armature shaft
42
is quite small during a period in which the engine valve
12
moves back and forth between the fully closed position and the fully opened position. Such a small change in the distance can be compensated for by the zero-lash adjuster
40
, which has been slightly contracted when the engine valve
12
is opened, expanding when the engine valve
12
has returned to the fully-closed position.
Thus, according to the solenoid valve device
10
of the present embodiment, it is possible to positively actuate the engine valve
12
between the fully closed position and the fully opened position without formation of a clearance between the armature shaft
42
and the valve shaft
26
.
FIG. 4A
is a diagram showing a displacement of the engine valve moving between a fully closed position and a fully opened position, and
FIGS. 4B and 4C
are diagrams showing waveforms of vibrations generated in association with the movement of the engine valve
12
in a case where the zero-lash adjuster
40
is not provided (that is, in a case where a tappet clearance is provided) and in a case where the zero- lash adjuster
40
is provided (that is, in a case of the solenoid valve device
10
of the present embodiment), respectively.
As shown in
FIG. 4B
, in a case where the zero-lash adjuster
40
is not provided, a vibration due to an impact between the armature shaft
42
and the valve shaft
26
(marked with “a”) and a vibration due to an impact between the armature
56
and the lower core
64
(marked with “b”) occur when the engine valve
12
moves in the valve-opening direction. Additionally, a vibration due to an impact between the engine valve
12
and the valve seat
20
(marked with “c”) and a vibration due to an impact between the armature
56
and the upper core
60
(marked with “d”) occur when the engine valve
12
moves in the valve-closing direction.
On the contrary, according to the solenoid valve device
10
of the present embodiment, since no clearance exists between the armature shaft
42
and the valve shaft
26
, no impact occurs therebetween when the engine valve
12
moves in the valve-opening direction. Additionally, the zero-lashadjuster
40
is designed so that the amount of the contraction due to the leakage of oil when the engine valve
12
is opened is as small as approximately one tenth of a typical value, which is 0.2 to 0.3 mm, for example, of the tappet clearance. Thus, the impact between the engine valve
12
and the valve seat
20
and the impact between the armature
56
and the upper core
60
occur substantially at the same time. For these reasons, a vibration occurs only once in each of the cases where the engine valve
12
is moving in the valve-opening direction and where the engine valve
12
is moving in the valve-closing direction, as shown in FIG.
4
C. Thus, according to the present embodiment, it is possible to reduce the operating sound of the solenoid valve device
10
as compared to a case where a tappet clearance is provided.
Additionally, in the present embodiment, oil is supplied to the reservoir
108
and the hydraulic pressure chamber
104
when the armature
56
is in contact with the upper core
60
, that is, when the engine valve
12
is in the fully-closed position. When the armature
56
is in contact with the upper core
60
, a pressure in the hydraulic pressure chamber
104
becomes low since no force is exerted on the reservoir cap
120
in the valve-opening direction. According to the present embodiment, since oil is supplied to the hydraulic pressure chamber
104
in such a state, it is possible to reduce an oil pressure required to be supplied to the oil supply passages
80
,
82
and thus to miniaturize the oil pump
83
.
Additionally, in the present embodiment, a clearance between an inner wall of the lash-adjuster containing space
24
a
and the zero-lash adjuster
40
is selected so that the clearance becomes zero in a possible coldest condition. Thus, under a normal temperature, a clearance is formed around the zero-lash adjuster
40
and oil can leak out through the clearance above and below the zero-lash adjuster
40
. In the present embodiment, oil which has leaked out above the zero-lash adjuster
40
and accumulated in the reservoir cap
120
provides lubrication between the armature shaft
42
and the lower bush
68
. Additionally, oil which has leaked out above the zero-lash adjuster
40
and flown into the spring containing space
30
via the oil collecting passage
85
and oil which has leaked out below the zero-lash adjuster
40
and directly flown into the spring containing space
30
provide lubrication between the valve shaft
26
and the valve guide
28
. In this way, it is possible to effectively utilize the oil which has leaked out from the zero-lash adjuster
40
as a lubricant of the armature shaft
42
and the valve shaft
26
.
In this connection, since an oil pressure supplied to the zero-lash adjuster
40
can be set to be low as mentioned above, it is possible to reduce an amount of the oil leakage.
In the solenoid valve device
10
, if air is mixed into oil in the hydraulic pressure chamber
104
, the zero-lash adjuster
40
becomes less rigid by the mixed air being compressed when the hydraulic pressure chamber
104
is pressurized. In order to avoid such a problem, it is necessary to prevent air from being mixed into oil when the solenoid valve device
10
is assembled.
FIG. 5
is a cross-sectional view showing a process of assembling the zero-lash adjuster
40
. As shown in
FIG. 5
, the zero-lash adjuster
40
is assembled by inserting the reservoir cap
120
into the zero-lash-adjuster containing space
24
a
after fitting a cylindrical cap
122
around the cylindrical part
24
c
of the cylinder head spacer
24
, inserting the plunger body
100
into the lash-adjuster containing space
24
a
, and filling the lash-adjuster containing space
24
a
with oil.
In this process, since the solenoid valve device
10
is mounted to the engine with the axial direction of the solenoid valve device
10
being inclined with respect to a vertical direction, a surface of the oil filled in the lash-adjuster containing space
24
a
is inclined with respect to a top surface of the cylindrical part
24
c
. Therefore, if the cap
122
is not provided, an opening part of the lash-adjuster containing space
24
a
is exposed to air above a surface of the oil in the lash-adjuster containing space
24
a
which is indicated by a dotted line A in FIG.
5
. If the reservoir cap
120
is inserted into the lash-adjuster containing space
24
a
in such a state, air is mixed into the oil via the exposed part.
According to the process shown in
FIG. 5
, since the cap
122
is provided, the lash-adjuster containing space
24
a
is completely submerged below the surface of the oil which is indicated by a solid line B in FIG.
5
. Thus, by inserting the reservoir cap
122
into the lash-adjuster containing space
24
a
in such a state, it is possible to prevent air from being mixed into oil.
FIG. 6
is a cross-sectional view showing another process of assembling the zero-lash adjuster
40
. In the process shown in
FIG. 6
, an annual recess
123
is formed on a top surface of the raised part
24
b
instead of providing the cylindrical part
24
c
, and a pin ring
124
is fitted into the annual recess
123
. According to this process, the reservoir cap
120
can be inserted into the lash-adjuster containing space
24
a
in a state where an opening part of the lash-adjuster containing space
24
a
is submerged below a surface of oil, as a case of the process shown in FIG.
5
. Thus, it is possible to prevent air from being mixed into oil.
It should be noted that the cap
122
or the pin ring
124
is removed after the zero-lash adjuster
40
has been assembled by the process shown in
FIG. 5
or FIG.
6
. Thus, it is possible to prevent an increase in a total height of the cylinder head spacer
24
due to the provision of the cap
122
or the pin ring
124
.
As mentioned above, according to the processes shown in
FIGS. 5 and 6
, it is possible to prevent air from being mixed into oil in the process of assembling the zero-lash adjuster
40
. However, when oil supplied to the zero-lash adjuster is heated, air which has been dissolved in the oil may become bubbles and the rigidity of the zero-lash adjuster
40
may be lowered due to the bubbles.
In the present embodiment, since the heat insulating plate
22
is interposed between the lower head
16
and the cylinder head spacer
24
, heat in the combustion chamber
16
is not easily transferred to the cylinder head spacer
24
. Thus, according to the present embodiment, it is possible to suppress an increase in the temperature of oil in the oil supply passages
80
and
82
and the zero-lash adjuster
40
, thereby preventing generation of bubbles in the oil.
Next, a description will be given of a second embodiment of the present invention.
FIG. 7
is a diagram showing a cross section of a solenoid valve device
200
of the present embodiment. In
FIG. 7
, parts that are the same as the parts shown in
FIG. 1
are given the same reference numerals, and descriptions thereof will be omitted. As shown in
FIG. 7
, in the present embodiment, the cylinder head spacer
24
of the first embodiment is omitted and the upper head
25
is mounted on the lower head
16
via the heat insulating plate
22
. Additionally, in the present embodiment, the lower core
64
of the first embodiment is replaced by a lower core
202
.
The lower core
202
has a lash-adjuster containing hole
203
which axially goes through a center of the lower core
202
. The zero-lash adjuster
40
is supported in the lash-adjuster containing hole
203
so that it can slide in the axial direction.
An outer bottom face of the plunger body
100
is in contact with an upper end face of the valve shaft
26
. Additionally, an inner bottom face of the reservoir cap
120
is in contact with a lower end face of an armature shaft
204
. Since the zero-lash adjuster
40
is disposed inside the lower core
202
, the armature shaft
204
has a structure achieved by cutting off a lower end part of the armature shaft
42
of the first embodiment by a length corresponding to an axial length of the zero-lash adjuster
40
.
An oil supply passage
206
is provided in the upper head
25
corresponding to each cylinder of the engine. An oil supply passage
207
corresponding to each zero-lash adjuster
40
is connected to the oil supply passage. Oil is supplied to the oil supply passage
206
by the oil pump
83
.
Oil supply passages
208
and
210
which are connected to each other are provided in the lower core
202
. The oil supply passage
208
is connected to the oil supply passage
207
. On the other hand, the oil supply passage
210
opens on an inner wall of the lash-adjuster containing hole
203
so as to be connected to the overflow recess
122
when the engine valve
12
is in the fully closed position. Thus, the zero-lash adjuster
40
is supplied with an oil pressure via the oil supply passages
206
,
207
,
208
, and
210
.
An O ring
212
is provided between an upper surface of a flange of the lower core
202
and a lower surface of the upper head
25
so as to surround a connecting portion of the oil supply passages
207
and
208
. The O ring
212
functions to prevent oil flowing through the oil supply passages
206
,
208
from leaking out.
In the solenoid valve device
200
of the present embodiment, when the engine valve
12
is opened, the zero-lash adjuster
40
slightly contracts with oil leaking out through a sliding surface between the plunger body
100
and the plunger
102
, as in the case of the solenoid valve device
10
of the first embodiment. When the engine valve
12
is seated on the valve seat
20
, the zero-lash adjuster
40
expands until the armature
56
comes into contact with the upper core
60
, being supplied with an oil pressure. Thus, according to the present embodiment, it is possible to positively actuate the engine valve
12
between the fully closed position and the fully opened position without forming a clearance between the engine valve
12
and the armature shaft
204
, as in a case of the solenoid valve device
10
of the first embodiment.
Additionally, in the present embodiment, since the zero-lash adjuster
40
is contained inside the lower core
202
, a full length of the solenoid valve device
200
is smaller than that of the solenoid valve device
10
of the first embodiment by an axial length of the zero-lash adjuster
40
. Thus, according to the present embodiment, it is possible to reduce a total height of the engine while obtaining the above-mentioned effect by the zero-lash adjuster
40
.
Further, in the present embodiment, part of oil which has leaked out above the zero-lash adjuster
40
stays on a top surface of the lower core
202
and intervenes between the armature
56
and the lower core
202
when the armature
56
impacts on the lower core
202
. Thus, according to the present embodiment, it is possible to damp the impact between the armature
56
and the lower core
202
by viscosity of oil so that an operating sound of the solenoid valve device
200
can be reduced. It should be noted that oil which has leaked out below the zero-lash adjuster
40
flows into the spring containing space
30
and provides lubrication between the valve shaft
26
and the valve guide
28
.
Additionally, in the present embodiment, since the oil supply passages
208
,
210
are provided inside the lower core
202
, the lower core
202
can be cooled by oil flowing through the oil supply passages
208
,
210
. In particular, when the engine valve
12
constitutes an exhaust valve, it is necessary to supply a large current to the lower coil
62
to actuate the engine valve
12
in the valve-opening direction against a high pressure in the combustion chamber
14
. In this case, high heat is generated in the lower core
202
. Thus, according to the present embodiment, since the lower core
202
can be cooled by oil flowing through the oil supply passages
208
,
210
as mentioned above, an increase in a temperature of the lower core
202
can be suppressed, and therefore the solenoid valve device
200
can be applied to an engine which operates with a high revolution and a high load.
Next, a description will be given of a solenoid valve device
300
of a third embodiment of the present invention.
FIG. 8
is a diagram showing a structure of the solenoid valve device
300
. The solenoid valve device
300
is achieved by providing a lower core
302
, an armature shaft
304
, a valve shaft
306
and a zero-lash adjuster
308
instead of the lower core
64
, the armature shaft
42
, the valve shaft
28
and the zero-lash adjuster
40
, respectively, of the solenoid valve device
10
of the first embodiment.
The lower core
302
has a lash-adjuster containing hole
310
which axially goes through a center thereof. A part of the zero-lash adjuster
308
is contained in the lash-adjuster containing hole
310
.
The armature shaft
304
has a structure achieved by removing a part of the armature shaft
42
below the armature
56
, and the zero-lash adjuster
308
is disposed immediately below the armature
56
. Thus, the valve shaft
306
is upwardly extended into the lash adjuster-containing hole
310
of the lower core
302
, as compared to the valve shaft
28
of the first embodiment. A cylindrical part
304
a
is provided on a lower end face of the armature shaft
304
. An upper end part
308
of the zero-lash adjuster
308
is fitted into the cylindrical part
304
a.
The zero-lash adjuster
308
which is provided to the solenoid valve device
300
of the present embodiment has a sealed structure.
FIG. 9
is a diagram showing an enlarged axial cross section of the zero-lash adjuster
308
.
As shown in
FIG. 9
, the zero-lash adjuster
308
has a plunger body
350
. The plunge body
350
is a substantially cylindrical member with a lower end thereof being closed. A cylindrical part
350
a
is provided on an outer bottom face of the plunger body
350
. An upper end part of the valve shaft
306
is fitted into the cylindrical part
350
a.
A plunger
352
is supported inside the plunger body
350
so that it can slide in the axial direction. A hydraulic pressure chamber
354
is defined between an outer bottom face of the plunger
352
and an inner bottom face of the plunger body
350
. The plunger
352
is provided with a reservoir
356
which upwardly opens and a connecting passage
360
which connects the reservoir
356
and the hydraulic pressure chamber
354
.
A retainer
362
and a plunger spring
364
are disposed in the hydraulic pressure chamber
354
. The plunger spring
364
upwardly presses the plunger
352
via the retainer
362
. A check ball
366
and a check ball spring
368
are disposed inside the retainer
362
. The check ball spring
368
presses the check ball
366
toward an opening of the connecting passage
360
. The check ball
366
and the check ball spring
368
function as a check valve which opens only when a pressure in the hydraulic pressure chamber
364
is lower than a pressure in the reservoir
356
.
The zero-lash adjuster
308
also includes a reservoir cap
370
. The reservoir cap
370
is a substantially cylindrical member with an upper end thereof being closed. The reservoir cap
370
is supported inside the plunger body
350
so that it can slide in the axial direction with a lower end face of the reservoir cap
370
being in contact with an upper end face of the plunger
352
. The reservoir
356
of the plunger
352
and an inner space of the reservoir cap
370
constitute a reservoir chamber
372
. The zero-lash adjuster
308
contains oil to a predetermined level in the reservoir chamber
372
.
A small diameter part
370
a
is provided on an upper end part of the reservoir cap
370
. The small diameter part
370
a
upwardly projects from the plunger body
350
and is fitted into the cylindrical part
304
a
of the armature shaft
304
. Connecting holes
374
are provided on a bottom part of the small diameter part
370
a
. The connecting holes
374
connect the reservoir chamber
372
and a space outside the reservoir cap
370
.
An annular recess
376
is formed on an outer circumferential surface of the reservoir cap
370
. The annular recess
376
is connected to the reservoir chamber
372
via connecting holes
378
which open on a bottom of the annular recess
376
. On the other hand, an annular recess
380
is formed on an internal circumferential surface of the plunger body
350
. The annular recess
376
and the annular recess
380
are positioned so that they communicate with each other in a normal operating state of the solenoid valve device
300
.
An annular seal member
382
is provided on an upper end of the plunger body
350
. An inner circumferential face of the seal member
382
is engaged with an outer circumferential surface of the small diameter part
370
a
of the reservoir cap
370
. As will be described below, the seal member
382
functions to prevent oil which has upwardly leaked out through the sliding surface between the reservoir cap
370
and the plunger body
350
from leaking out to the outside of the zero-lash adjuster
308
.
According to the above-mentioned structure of the zero-lash adjuster
308
, when the engine valve
12
is actuated in the valve-opening direction, oil in the hydraulic pressure chamber
354
is pressurized by a force acting on the plunger
370
in the valve-opening direction. In this case, a flow of oil between the hydraulic pressure chamber
354
and the reservoir chamber
372
is prohibited by the check ball
366
closing the connecting passage
360
. Thus, the zero-lash adjuster
308
moves in the valve-opening direction together with the armature shaft
304
and the engine valve
12
while allowing oil to gradually leak out through the sliding surface between the plunger
352
and the plunger body
350
. In this process, the zero-lash adjuster
308
contracts by a slight extent corresponding to an amount of oil which has leaked out.
Oil which has leaked out downwardly through the sliding surface between the plunger
352
and the plunger body
350
is collected to the reservoir chamber
372
via the connecting holes
378
. Additionally, oil which has leaked out upwardly through the sliding surface between the reservoir cap
370
and the plunger body
350
is prevented from flowing out by the seal member
382
and collected to the reservoir chamber
372
via the connecting holes
374
.
When the valve
12
returns to be seated on the valve seat
20
, a resilient force of the lower spring
38
is no longer exerted on the plunger body
350
. On the other hand, the armature
56
continues to move in the valve-closing direction by a slight distance corresponding to an extent of the contraction of the zero-lash adjuster
308
after the valve
12
is seated on the valve seat
20
. In this case, since the plunger
350
and the reservoir cap
370
are upwardly pressed toward the armature shaft
304
by a resilient force of the plunger spring
364
, an oil pressure in the hydraulic pressure chamber
354
is decreased. Due to this pressure decrease, the check ball
366
is released from the opening of the connecting passage
360
, and thus the hydraulic pressure chamber
354
and the reservoir chamber
372
are connected to each other. In such a situation, since oil is allowed to flow from the reservoir chamber
372
into the hydraulic pressure chamber
354
, the zero-lash adjuster
308
expands until the armature
56
comes into contact with the upper core
60
. Thus, it is possible to maintain a state in which the armature shaft
304
and the reservoir cap
370
are in contact with each other and the plunger
352
and the valve shaft
306
are in contact with each other.
Additionally, a change in a distance between the valve shaft
26
and the armature shaft
304
due to a difference in the thermal expansion between the engine valve
12
and the lower head
16
or wear of the engine valve
12
and the valve seat
20
can be compensated for by the zero-lash adjuster
308
, which has been slightly contracted when the engine valve
12
is opened, expanding when the engine valve
12
is closed, as in the case of the zero-lash adjuster
40
.
Thus, according to the zero-lash adjuster
308
, it is possible to positively actuate the engine valve
12
between the fully closed position and the fully opened position while preventing formation of a clearance between the armature shaft
304
and the engine valve
12
.
Additionally, since the zero-lash adjuster
308
is of a sealed type in which all of oil which has leaked out from the hydraulic pressure chamber
354
is collected to the reservoir chamber
372
via the connecting holes
378
or
374
, it is unnecessary to supply oil to the zero-lash adjuster
308
. Thus, contrary to the solenoid valve devices
10
, 200 of the first and second embodiments, oil supply passages and an oil pump for supplying oil to the zero-lash adjuster
308
need not be provided and thus a cost of the solenoid valve device
300
can be reduced.
Further, since the zero-lash adjuster need not slide on an inner wall of the lash-adjuster containing hole
310
, an energy loss caused by a sliding resistance can be avoided.
Additionally, due to the sealed structure of the zero-lash adjuster
308
, the zero-lash adjuster
308
may project from the lower core
308
when the engine valve
12
is in the fully closed position, as shown in FIG.
8
.
Next, a description will be given of a fourth embodiment of the present invention.
FIG. 10
is a diagram showing a cross section of solenoid valve device
400
of the fourth embodiment according to the present invention. In
FIG. 10
, parts that are the same as the parts shown in
FIG. 1
are given the same reference numerals, and descriptions thereof will be omitted. The solenoid valve device
400
of the present embodiment is achieved by offsetting center axes of the armature shaft
42
and the valve shaft
26
to each other and replacing the zero-lash adjuster
40
of the first embodiment with a swing arm
402
and a zero-lash adjuster
404
.
As shown in
FIG. 10
, a lash-adjuster containing space
406
is formed in the cylinder head spacer
24
. The swing arm
402
is contained in the lash-adjuster containing space
406
. Additionally, a lash-adjuster supporting hole
408
is formed on an upper surface of the lower head
16
. The zero-lash adjuster
404
is supported in the lash-adjuster supporting hole
408
.
FIG. 11
is a diagram showing an enlarged cross section of the zero lash adjuster
404
and neighboring parts thereof. As shown in
FIG. 11
, the zero-lash adjuster
404
has a plunger body
410
. The plunger body
410
is a substantially cylindrical member with one end (lower end in
FIG. 11
) being closed. The plunger body
410
is fitted into the lash-adjuster containing hole
408
so that an upper end part of the plunger body
410
upwardly projects from the lash-adjuster containing hole
408
. A plunger
412
is disposed inside the plunger body
410
so that it can slide in the axial direction. The plunger
412
is a substantially cylindrical member which includes a reservoir space
414
therein. A pivot part
412
a
having a hemispheric shape is provided on an upper end of the plunger
412
.
A space inside the plunger body
410
below the plunger
412
constitutes a hydraulic pressure chamber
416
. The plunger
412
is provided with a connecting passage
418
which connects the reservoir space
414
and the hydraulic pressure chamber
416
.
A retainer
420
and a plunger spring
422
are disposed in the hydraulic chamber
416
. The plunger spring
422
upwardly presses the plunger
412
via the retainer
420
. A check ball
424
and a check ball spring
426
are disposed inside the retainer
420
. The check ball spring
426
presses the check ball
424
toward an opening of the connecting passage
424
.
Annular recesses
428
and
430
are provided on an outer circumferential surface and an inner circumferential surface, respectively, of the plunger body
410
. The annular recesses
428
and
430
are connected to each other by a connecting hole
432
.
An oil supply passage
434
is formed in the lower head
16
corresponding to each cylinder of the engine. An oil supply passage
436
corresponding to each zero-lash adjuster
404
is connected to the oil supply passage
434
. The oil supply passage
436
opens on a inner wall of the lash-adjuster containing hole
408
so as to be connected to the annular recess
428
. The oil supply passage
434
is supplied with oil from the oil pump
83
not shown in FIG.
11
.
An annular recess
438
is provided on an outer circumferential surface of the plunger
412
. The annular recess
438
is positioned so as to communicate with the annular recess
430
of the plunger body
410
in a normal operating state of the solenoid valve device
400
. Additionally, the annular recess
438
is connected to the reservoir space
414
via connecting holes
440
which open on a bottom of the annular recess
438
.
An adjuster connecting part
402
a
is provided on a bottom surface of the swing arm
402
near a left end thereof in FIG.
11
. The adjuster connecting part
402
a
is a recessed part having a substantially hemispheric shape corresponding to a shape of the pivot part
412
a
of the plunger
412
. Additionally, a valve-shaft contacting part
402
b
is provided on a bottom face of the swing arm
402
near a right end thereof in FIG.
11
. The valve-shaft contacting part
402
b
is a raised part having a curved surface (a spherically shaped surface, for example). Further, an armature contacting part
402
c
is provided on an upper surface of the swing arm
402
at a position corresponding to an intermediate position between the adjuster connecting part
402
a
and the valve-shaft contacting part
402
b
. The armature contacting part
402
c
is a part having a moderately curved (or planer) surface.
The pivot part
412
a
of the plunger
412
is fitted in the adjuster connecting part
402
s
of the swing arm
402
. Thus, the swing arm
402
can swing relative to the zero-lash adjuster
404
around an apex of the pivot part
402
a
. On the other hand, an upper end face of the valve shaft
26
is in contact with the valve-shaft contacting part
402
b
. Additionally, a lower end face of the armature shaft
42
, which end face has a raised and curved (spherical, for example) surface, is in contact with the armature-shaft contacting part
402
c
. Thus, the swing arm
402
can smoothly swing while maintaining a state in which the swing arm
402
is in contact with the armature shaft
42
and the valve shaft
26
.
Hereinafter, a distance between a contact point of the armature contacting part
402
c
and armature shaft
42
and an apex of the pivot part
412
a
is indicated by L
1
, and a distance between a contact point of the armature contacting part
402
c
and the armature shaft
42
and a contact point of the valve-shaft shaft contacting part
402
b
and the valve shaft
28
is indicated by L
2
.
According to the above-mentioned structure, when the upper coil
58
is de-energized in a state where the armature
56
and the engine valve
12
are maintained in the fully closed position, a resilient force of the upper spring
48
is transmitted to the armature
56
as a force in the valve-opening direction. This force is in turn transmitted to the plunger
412
of the zero-lash adjuster
404
as a downward force by leverage of the swing arm
402
with the contact point of the valve-contacting point
402
b
and the valve shaft
26
being a fulcrum. When a downward force is transmitted to the plunger
412
, the connecting passage
418
is closed by the check ball
424
since the hydraulic pressure chamber
416
is pressurized. In this case, a flow of oil between the reservoir chamber
414
and the hydraulic pressure chamber
416
is prohibited. Thus, the zero-lash adjuster
404
contracts to a slight extent corresponding to an amount of oil which leaks out through a sliding surface between the plunger
412
and the plunger body
410
.
Therefore, when a force is transmitted to the armature
56
in the valve-opening direction, the swing arm
402
downwardly swings around the pivot part
412
a
of the plunger
412
. In this case, a force transmitted to the armature
56
in the valve-opening direction (that is, a force transmitted to the armature contacting part
402
c
of the swing arm
402
from the armature shaft
42
) divided by a lever ratio R=(L
1
+L
2
)/L
1
is transmitted to the valve shaft
26
from the valve-shaft contacting part
402
b
, and thus the engine valve
12
is actuated in the valve-opening direction.
When the engine valve
12
is actuated in the valve-closing direction, a resilient force of the lower spring
38
is transmitted to the valve-contacting part
402
b
of the swing arm
402
from the valve shaft
26
as an upward force. In this case, a downward force is transmitted to the plunger
412
of the zero-lash adjuster
404
from the adjuster connecting part
402
a
by a leverage of the swing arm
402
with the contact point of the armature shaft
42
and the armature contacting part
402
c
being a fulcrum. Thus, the swing arm
402
upwardly swings around the pivot part
412
a
with the zero-lash adjuster
404
slightly contracting, as in the above-mentioned case where the engine valve
12
is opened. The force transmitted to the valve-shaft contacting part
402
b
multiplied by the above-mentioned lever ratio R is transmitted to the armature shaft
42
and thus the armature shaft
42
and the engine valve
12
are actuated together in the valve-closing direction.
When the engine valve
12
is seated on the valve seat
20
, the downward force is no longer exerted on the plunger
412
of the zero-lash adjuster
402
since the resilient force of the lower spring
38
is not transmitted to the valve-shaft contacting part
402
b
of the swing arm
402
. In this state, the swing arm
402
is downwardly inclined around the valve-shaft contacting part
402
b
to a slight extent corresponding to an extent of the contraction of the zero-lash adjuster
404
as compared to a state at a time when the engine valve
12
started moving in the valve-opening direction from the fully closed position. Thus, the armature
56
further moves in the valve-closing direction by a distance corresponding to the extent of the inclination of the swing arm
402
until the armature
56
comes into contact with the upper core
60
.
In this case, since the plunger
412
is upwardly pushed by a resilient force of the plunger spring
422
, an oil pressure in the hydraulic chamber
416
is decreased. Thus, the check ball
424
is released from the opening of the connecting passage
418
allowing a flow of oil from the reservoir space
414
into the hydraulic pressure chamber
416
, and the plunger
412
moves in an upward direction. As a result, the swing arm
402
upwardly swings around the valve-shaft contacting part
402
b
while maintaining a state in which the armature shaft
42
is in contact with the armature-shaft contacting part
402
c.
Thus, according to the solenoid valve device
400
of the present embodiment, clearances are prevented from being formed between the swing arm
402
and the armature shaft
42
by the swing arm
402
swinging in association with the expansion of the zero-lash adjuster
404
when the engine valve
12
is seated on the valve seat
20
. Additionally, a change in a distance between the valve shaft
26
and the armature shaft
42
due to a difference in the thermal expansion between the engine valve
12
and the lower head
16
or wear of the engine valve
12
and the valve seat
20
can be compensated for by the zero-lash adjuster
404
, which has been slightly contracted when the engine valve
12
is opened, expanding when the engine valve
12
is seated on the valve seat
20
, as in the case of the zero-lash adjuster
40
.
In this way, it is possible to positively actuate the engine valve
12
between the fully closed position and the fully opened position while preventing formation of a clearance between the engine valve
12
and the armature shaft
42
, that is, while maintaining a state in which both the engine valve
12
and the armature shaft
42
are in contact with the swing arm
402
.
Additionally, only the swing arm
402
, which has a sufficiently small height as compared to a height of the zero-lash adjuster
404
, is interposed between the engine valve
12
and the armature shaft
42
. Thus, according to the present embodiment, it is possible to reduce a total length of the solenoid valve device
400
and thus to suppress an increase in a height of the engine, as compared to a structure in which a zero-lash adjuster is interposed between the engine valve
12
and the armature shaft
42
.
Further, in the present embodiment, the swing arm
402
swings in association with the movement of the engine valve
12
while the zero-lash adjuster
404
is maintained still. That is, a mass of the zero-lash adjuster
404
is not included in a mass of a movable part of the solenoid valve device
400
but only an equivalent inertial mass of the swing arm
402
swinging around the pivot part
412
a
is included in the mass of the movable part. Thus, according to the present embodiment, it is possible to reduce an inertial mass of the movable part of the solenoid valve device
400
thereby improving a response of the solenoid valve device
400
.
Additionally, due to the arrangement in which center axes of the zero-lash adjuster
404
, the armature shaft
42
and the valve shaft
26
are offset with respect to each other, the solenoid valve device
400
can be mounted to the engine with a higher degree of freedom. That is, the offset directions of the armature shaft
42
and the zero-lash adjuster
404
with respect to the engine valve
12
can be arbitrarily changed in accordance with a structure of the engine.
FIG. 12
is a diagram schematically showing a top view of an arrangement in which the armature shaft
42
and the zero-lash adjuster
404
are offset with respect to the engine valve
12
in an outwardly radial direction of a cylinder bore
450
of the engine.
FIG. 12
shows a positional relationship between the armature shafts
42
, the upper and lower cores
60
,
64
(generally referred to as cores
452
), center axes
404
a
of the zero-lash adjusters
404
, the swing arms
402
, intake valves
454
constituted by the engine valves
12
, and exhaust valves
456
constituted by the engine valves
12
. In the arrangement shown in
FIG. 12
, since the armature shafts
42
and the zero-lash adjusters
404
are disposed in radially outward positions with respect to the engine valves
12
, relatively large spacings are provided between the cores
452
, and thus solenoid valve devices having a larger size can be mounted to the engine.
In the present embodiment, the zero-lash adjuster
404
has a structure in which oil is supplied from an external oil-pressure source. However, a zero-lash adjuster of a sealed type as the zero-lash adjuster
308
of the third embodiment can be used instead of the zero-lash adjuster
404
.
Additionally, although hydraulic zero-lash adjusters are used in the first to the fourth embodiments, a mechanical zero-lash adjuster can be used instead. The mechanical zero-lash adjuster has a first member connected to an actuating mechanism (corresponding to the armature shaft
42
in the first embodiment) and a second member connected to an engine valve. Screw threads are provided to the respective first and second members. The first and second members are connected to each other by the screw threads being engaged with each other with an axial spacing being provided therebetween. The screw threads are constructed so as to prohibit a relative rotation of the first and second members when a force is exerted on the first member in the valve-opening direction and to allow a relative rotation of the first and second members when a force is not exerted on the first member in the valve-opening direction. Thus, when the engine valve is actuated in the valve-opening direction, the first and second members move with the engine valve as a rigid body without a relative axial movement between the two members. On the other hand, when the engine valve is actuated in the valve-closing direction or is in the fully closed or fully opened position, the first and second members move relative to each other by a relative rotation so that a clearance between the engine valve and the actuating mechanism is adjusted to be zero. According to such a mechanical zero-lash adjuster, it is possible to reduce weight of the zero-lash adjuster since components such as a hydraulic chamber and a check valve are not required. Thus, it is possible to improve a response of a solenoid and thus to apply the solenoid valve device to high-speed engines.
Additionally, in the above-mentioned embodiments, the solenoid valve devices
10
,
200
,
300
,
400
are constructed as intake valves or exhaust valves. However, the present invention can be constructed as other valve devices which actuate an engine valve by an electromagnetic force.
Next, a description will be given of a fifth embodiment of the present invention. In the present embodiment and in the following embodiments, current control of the upper coil
58
and the lower coil
62
will be described with reference to the solenoid valve device
10
of the first embodiment.
When an ignition switch of a vehicle in which the engine is mounted is turned off, neither the upper coil
58
nor the lower coil
62
can be energized. Thus, at a time when the ignition switch is turned on, the engine valve
12
is supported by the upper spring
48
and the lower spring
38
at a neutral position between the fully closed position and the fully opened position. When the engine valve
12
is at the neutral position, the armature
56
is spaced away from both the upper coil
58
and the lower coil
62
. In this state, resilient forces of the upper spring
48
and the lower spring
38
exerted on the armature
56
are balanced. Thus, in order to start actuating the engine valve
12
situated in the neutral position, it is necessary to attract the armature
56
spaced away from the upper coil
58
and the lower coil
62
without using the resilient forces of the springs. In this case, it is difficult to effectively actuate the engine valve
12
at desired timings. Thus, in order to smoothly start the engine, it is necessary to move the engine valve to the fully closed position or the fully opened position immediately after the ignition switch is turned on.
FIGS. 13A and 13B
are diagrams showing instruction currents supplied to the upper coil
58
and the lower coil
62
, respectively, after the ignition switch is turned on until the engine valve
12
starts being actuated between the fully closed position and the fully opened position in the present embodiment.
FIG. 13C
is a diagram showing a displacement of the engine valve when the above instruction currents are supplied to the respective coils.
As shown in
FIGS. 13A
to
13
C, actuation of the engine valve
12
is performed in three period, namely, a starting period, a holding period, and an operating period. In the starting period, the upper coil
58
is supplied with an instruction current having a pulse waveform which changes between “0” and a predetermined value I
U
with a predetermined period T, and the lower coil
62
is supplied with an instruction current having a pulse waveform which changes between “0” and a predetermined value I
L
with the predetermined period T delayed 180° in phase with respect to the instruction current supplied to the upper coil
58
, as shown in
FIGS. 13A and 13B
. The predetermined period T is set to be equal to a natural vibration period of a spring-mass system defined by a mass of a movable part of the solenoid valve device
10
(that is, the armature
56
and parts moving with the armature
56
), the upper spring
48
, and the lower spring
38
.
Thus, in the starting period, electromagnetic forces are alternately exerted on the armature
56
in the valve-opening direction and the valve-closing direction with a period equal to the natural vibration period of the movable part so that a natural vibration of the movable part is excited. As a result, the amplitude of vibration of the engine valve
12
gradually increases in the starting period, and the engine valve
12
ultimately reaches the fully closed position, as shown in FIG.
13
C. Hereinafter, the above-mentioned process performed in the starting period to move the engine valve
12
to the fully closed position by exciting a natural vibration of the movable part is referred to as an initial actuation.
In the next holding period, the instruction current to the lower coil
62
is set to be “0” and the instruction current to the upper coil
58
is set to be a predetermined holding current I
H
. Thus, the armature
56
and the engine valve
12
are held in the fully closed position.
When the operating period is started following the holding period, the instruction current to the upper coil
58
is set to be “0” so that the engine valve
12
starts moving in the valve-opening direction. Then, an instruction current having a pattern comprising an attracting current I
A
, a transition current I
T
and the holding current I
H
is supplied to the lower coil
62
at a proper timing. According to the instruction current having such a pattern, after the armature
56
is actuated to come close to the lower core
64
by the attracting current I
A
, the armature
56
is attracted to come into contact with the lower core
64
while being decelerated by the transition current I
T
, and ultimately, the armature
56
is held in contact with the lower core
64
by the holding current I
H
. Thereafter, the engine valve
12
is actuated between the fully opened position and the fully closed position by alternately supplying the instruction current having the above-mentioned pattern to the upper coil
58
and the lower coil
62
.
As mentioned in the first embodiment, the zero-lash adjuster
40
has a function to expand by being supplied with an oil pressure from the oil supply passage
80
when the engine valve
12
reaches near the fully closed position so as to prevent formation of a clearance (that is, a tappet clearance) between the engine valve
12
and the armature shaft
42
in a state where the armature
56
and the engine valve
12
are in the fully closed position. Hereinafter, a state where the tappet clearance is cancelled by the above-mentioned function of the zero-lash adjuster
40
is referred to as a zero-lash state. Additionally, a position of the armature
56
in a state where both the upper coil
58
and the lower coil
62
are de-energized in the zero-lash lash state is referred to as a reference neutral position.
When the ignition switch is turned off, the zero-lash adjuster
40
cannot be supplied with an oil pressure, since neither the upper coil
58
nor the lower coil
62
is supplied with a current and the armature
56
is held near the reference neutral position. In the state where the armature
56
is held near the reference neutral position, a compressing force is exerted on the zero-lash adjuster
40
by the upper spring
48
and the lower spring
38
. Thus, the zero-lash adjuster
40
gradually contracts since oil leaks out from the hydraulic pressure chamber
104
while the ignition switch is turned off. Hereinafter, the phenomenon in which the zero-lash adjuster
40
contracts due to leakage of oil from the hydraulic pressure chamber
104
is referred to as a leak-down of the zero-lash adjuster
40
. When the leak-down has occurred, a position of the armature
56
shifts toward the lower core
64
from the reference neutral position in accordance with an extent of the leak-down. Thus, distances from the armature
56
to the upper core
60
and the lower core
64
at a time when the ignition switch is turned on change in accordance with an extent of the leak-down of the zero-lash adjuster
40
.
FIG. 14
is a diagram showing a relationship between a position of the armature
56
and an electromagnetic force acting between the armature
56
and the lower core
64
when a current supplied to the lower coil
62
is changed in three steps, namely, large, medium, and small. As shown in
FIG. 14
, when a current supplied to the lower coil
62
is constant, the electromagnetic force acting between the armature
56
and the lower core
64
becomes smaller as the armature
56
shifts toward the upper core
60
. Additionally, when a position of the armature
56
is constant, the electromagnetic force acting between the armature
56
and the lower core
64
becomes larger as a larger current is supplied to the lower coil
62
.
Due to such characteristics, a current to be supplied to the lower coil
62
to exert a required force on the armature
56
in the valve-opening direction becomes smaller as the armature
56
shifts toward the lower core
58
. Similarly, a current to be supplied to the upper coil
58
to exert a required force on the armature
56
in the valve-closing direction becomes larger as the armature
56
shifts toward the lower core
58
.
For this reason, if constant currents are used as the instruction currents I
U
and I
L
to the upper coil
58
and the lower coil
62
, respectively, in the initial actuation irrespective of a position of the armature
56
, the following problems occur. First, since the armature
56
has shifted toward the lower core
64
in accordance with the leak-down of the zero-lash adjuster
40
when the ignition switch is turned on, the initial actuation may not be properly performed due to an insufficient electromagnetic force to actuate the armature
56
toward the upper core
60
. Second, since the lower coil
62
is supplied with a current which is larger than a required value, power consumption of the solenoid valve device
10
is unnecessarily increased.
In order to avoid these problems, the instruction currents I
U
and I
L
in the initial actuation are changed in accordance with a position of the armature
56
in the present embodiment.
FIG. 15
is a diagram showing a map which is referred to so as to determine the instruction currents I
L
and I
U
in the initial actuation in accordance with a position of the armature
56
. As shown in
FIG. 15
, since the instruction current I
L
to the lower coil
62
is set to be larger as the armature
56
shifts toward the upper core
60
, a sufficient force can be generated to actuate the armature
56
toward the lower core
64
. Additionally, since the instruction current I
U
to the upper coil
58
is set to be smaller as the armature
56
shifts toward the upper core
60
, the upper coil
58
can be prevented from being supplied with an unnecessarily large current and thus power consumption of the solenoid valve device
10
can be reduced.
FIG. 16
is a diagram showing a perspective view of an arrangement for detecting a position of the armature
56
. As mentioned above, the armature
56
shifts toward the lower core
64
due to the leak-down of the zero-lash adjuster
40
. When the leak-down of the zero-lash adjuster
40
has occurred, the armature shaft
42
and the engine valve
12
shift downwardly and upwardly, respectively, to the same extent from both sides of the zero-lash adjuster
40
. Thus, in the present embodiment, a position of the armature
56
is indirectly detected by detecting a position of the valve shaft
26
.
As shown in
FIG. 16
, a cut-out part
28
a
is formed in the valve guide
28
. A pair of gap sensors
150
,
152
are mounted in the cut-out part
28
a
via sensor holders
154
,
156
, respectively, so as to be positioned to face to each other from both sides of the valve shaft
26
in the radial direction. Additionally, a terminal film
158
for delivering output signals of the gap sensors
150
,
152
is mounted in the cut-out part
28
a
.
FIG. 16
shows a state in which the gap sensors
150
,
152
, the sensor holders
154
,
156
, and the terminal film
158
are taken away from the cut-out part
28
a
. The gap sensors
150
,
152
are eddy-current gap sensors, for example, and deliver electric signals to the ECU
11
in accordance with distances to the circumferential surface of the valve shaft
26
. It should be noted that other types of gap sensors such as electrostatic gap sensors can be used as the gap sensors
150
,
152
.
FIG. 17
is a diagram showing an axial cross section of the valve guide
28
and the valve shaft
26
. As shown in
FIG. 17
, a recessed part
160
having a rectanglar cross section is formed on a circumference of the valve shaft
26
. The gap sensors
150
,
152
and the recessed part
160
are positioned so that center parts of the gap sensors
150
,
152
face a lower step
160
a
of the recessed part
160
when the engine valve
12
is in the fully closed position and the center parts of the gap sensors
150
,
152
face an upper step
160
b
of the recessed part
160
when the engine valve
12
is in the neutral position. Thus, an axial length of the recessed part
160
substantially corresponds to a half of a displacement of the engine valve
12
between the fully closed position and the fully opened position.
The output voltage V of the gap sensors
150
,
152
becomes a minimum value V
min
when the whole surfaces of the gap sensors
150
,
152
face a circumferential part of the valve shaft
28
other than the recessed part
160
(hereinafter referred to as a general part of the valve shaft
28
) and becomes a maximum value V
max
when the whole surfaces of the gap sensor a
150
,
152
face to recessed part
160
. It should be noted that the output voltage V of the gap sensors
150
,
152
is defined as a mean value of the output voltages of the respective sensors.
FIG. 18
is a diagram showing changes in a relative position of the gap sensors
150
,
152
and the recessed part
160
when the engine valve
12
moves from the fully closed position to the fully opened position.
FIG. 19
is a diagram showing a change in the output voltage V when the engine valve
12
moves from the fully closed position to the fully opened position.
As shown in a state (1) of the
FIG. 18
, when the engine valve
12
is in the fully closed position, substantially half surfaces of the gap sensors
150
,
152
face the general part of the valve shaft
28
and the other half surfaces face the recessed part
160
. In this state, the output voltage V is an intermediate value V
s
(≈(V
max
+V
min
) /2).
After the engine valve
12
has started moving from the fully closed position in the valve-opening direction, the output voltage V increases as shown in a period I of
FIG. 19
since areas of the gap sensors
150
,
152
facing the recessed part
160
increases. After the engine valve
12
has moved until the whole surfaces of the gap sensors
150
,
152
face the recessed part
160
as shown in a state (2) of the
FIG. 18
, the output voltage V is maintained to be the maximum voltage V
max
as shown in a period II of FIG.
19
.
When the engine valve
12
has reached near the neutral position, the gap sensors
150
,
152
face the upper step
160
b
of the recessed part
160
as shown in a state (3) of FIG.
18
. In this state, the output voltage V decreases as the engine valve
12
moves in the valve-opening direction as shown in a period III of FIG.
19
. After the engine valve
12
has further moved in the valve-opening direction until the whole surfaces of the gap sensors
150
,
152
face the general part of the valve shaft
28
, the output voltage V is maintained to be the minimum voltage V
min
until the engine valve
12
reaches the fully opened position as shown in a period IV of FIG.
19
.
As mentioned above, when the engine valve
12
is moving near the neutral position as shown in the period III of
FIG. 19
, the output voltage V changes in accordance with a position of the engine valve
12
. That is, as the engine valve
12
moves in an upward direction in association with the leak-down of the zero-lash adjuster
40
, the output voltage V becomes larger as compared to a value of the output voltage V in the zero-lash state. Accordingly, the ECU
11
can detect a position of the engine valve
12
at a time when the ignition switch is turned on based on the output voltage V at that time and thus can indirectly detect a displacement of the armature
56
from the reference neutral position toward the lower core
64
based on the detected position of the engine valve
12
.
It should be noted that the value V
s
of the output voltage V in a state where the engine valve
12
is in the fully closed position changes in accordance with a relative position of the armature
56
and the engine valve
12
. Thus, it can be determined whether or not the zero-lash state is achieved based on the value V
s
of the output voltage V at a time when the initial actuation is completed. If it is determined that the zero-lash state is not yet achieved after the initial actuation is completed, instruction currents supplied to the upper coil
58
may be increased as compared to a regular situation for a certain period after the operating period has started so that the engine valve
12
can be positively actuated between the fully closed position and the fully opened position.
Additionally, a position of the recessed part
160
of the valve shaft
28
changes in accordance with thermal expansion of the engine valve
12
. Thus, thermal expansion of the engine valve
12
can be detected based on the value V
s
of the output voltage V when the engine valve
12
is in the fully closed position.
Further, since the mean value of the outputs voltages of the gap sensors
150
,
152
is used as the output voltage V, it is possible to compensate for a change in the output voltages of the respective sensors due to a radial displacement of the engine valve
28
. Thus, it is possible to precisely detect a position of the engine valve
12
.
FIG. 20
is a flowchart performed by the ECU
11
so as to determine the instruction currents I
L
and I
U
in the initial actuation. The routine shown in
FIG. 20
is performed once immediately after the ignition switch is turned on. When the routine shown in
FIG. 20
is started, the process of step
500
is performed first.
In step
500
, a position of the armature
56
is detected based on the output voltage V, as mentioned above.
In step
502
, the instruction currents I
L
and I
U
in the initial actuation are determined based on the detected position of the armature
56
by referring to the map shown in FIG.
15
.
In step
504
, a process is performed for starting the initial actuation using the instruction currents I
L
and I
U
determined in step
502
. When the process of step
504
is finished, the present routine is ended.
As mentioned above, the instruction currents I
L
, I
U
in the initial actuation are determined in accordance with a position of the armature
56
before the initial actuation is started. Thus, according to the present embodiment, it is possible to properly perform the initial actuation while suppressing the power consumption in the initial actuation, irrespective of a change in a position of the armature
56
due to the leak-down of the zero-lash adjuster
40
.
In the present embodiment, a position of the armature
56
is indirectly detected by detecting a position of the valve shaft
28
based on a fact that the valve shaft
28
and the armature
56
shift by substantially the same distance in association with the leak-down of the zero-lash adjuster
40
. However, a position of the armature
56
may also be directly detected.
FIG. 21
is a diagram showing an example of an arrangement for directly detecting a position of the armature
56
by using a gap sensor
250
. In the arrangement shown in
FIG. 21
, the armature shaft
42
is provided with an extended part
42
a
upwardly extending through the adjuster bolt
52
. A measurement target
252
is fixed to an end face of the extended part
42
a
. The gap sensor
250
, which can be an eddy-current gap sensor for example, is supported above the measurement target
252
. The gap sensor
250
delivers an electric signal to the ECU
11
in accordance with a distance to the measurement target
252
. Thus, according to the arrangement shown in
FIG. 11
, a position of the armature
56
can be directly detected.
FIG. 22
shows an example of an arrangement for directly measuring a position of the armature
56
by using a laser distance sensor
260
. The laser distance sensor
260
projects a laser light emitted by a laser diode on a target to be measured, and detects a distance to the target based on a position of the reflected light from the target using a principle of triangulation. The armature shaft
42
is provided with the extended part
42
a
upwardly extending through the adjuster bolt
52
as the arrangement shown in
FIG. 21. A
laser light from the laser distance sensor
260
is projected on an end face of the extended part
42
a
. Since the laser light has a small diameter, only a small surface is required for the measurement as compared to a case of an eddy-current gap sensor. Thus, in the arrangement shown in
FIG. 22
, the measured target
252
of the arrangement shown in
FIG. 21
need not be provided.
Next, a description will be given of a sixth embodiment of the present invention. In the present embodiment, if the zero-lash state is not achieved at a time when the initial actuation is completed, the instruction currents to the upper coil
58
and the lower coil
62
are changed as compared to a regular situation for a predetermined period after start of the actuating period.
FIGS. 23A and 23B
are diagrams schematically showing the solenoid valve device
10
when the armature
56
is in the fully opened position in a case where the leak-down of the zero-lash adjuster
40
has not occurred and in a case where leak-down of the zero-lash adjuster
40
has occurred, respectively.
In a case where the leak-down has occurred as shown in
FIG. 23B
, the engine valve
12
shifts toward the armature
56
as compared to a case where the leak-down has not occurred as shown in FIG.
23
A. Thus, an amount of contraction of the lower spring
38
decreases in accordance with an extent of the leak-down. In this case, since a resilient force acting on the engine valve
12
in the valve-closing direction decreases, a current to be supplied to the upper coil
58
for actuating the engine valve
12
in the valve-closing direction increases. Additionally, in a case where the leak-down has occurred, a distance for which the armature
56
must actuate the engine valve
12
becomes smaller by an amount of the tappet clearance when the engine valve
12
is actuated from the fully closed position in the valve-opening direction. Thus, a current to be supplied to the lower coil
62
for opening the engine valve
12
is smaller as compared to a case where no leak-down has occurred.
As mentioned above, when the leak-down of the zero-lash adjuster
40
has occurred, a current to be supplied to the upper coil
58
increases and a current to be supplied to the lower coil
62
decreases, as compared to a case where no leak-down has occurred. Thus, in the present embodiment, an instruction current to the lower coil
62
is set to be smaller than an instruction current to the upper coil
58
for a predetermined period after the initial actuation is completed, so that the engine valve
12
can be positively actuated between the fully closed position and the fully opened position while suppressing power consumption of the solenoid valve device
10
.
FIGS. 24A and 24B
are diagrams showing the instruction currents supplied to the upper coil
58
and the lower coil
62
, respectively. In
FIGS. 24A and 24B
, instruction currents used in a regular situation (that is, when the zero-lash state is being achieved) is indicated by dotted lines.
As shown in
FIGS. 24A and 24B
, for predetermined N cycles after the operating period is started, the attracting current I
A
and the holding current I
H
to the lower coil
62
are set to be values I
A1
and I
H1
, respectively, which are smaller than the respective base values I
A0
and I
H0
used in the regular situation, and the attracting current I
A
and the holding current I
H
to the upper coil
58
are set to be values I
A2
and I
H2
, respectively, which are larger than the respective base values I
A0
and I
H0
. Here, one cycle means a process in which the engine valve
12
moves back and forth between the fully closed position and the fully opened position. The predetermined number N is set to be a number of the cycles required to supply a sufficient oil pressure to the zero-lash adjuster
40
for achieving the zero-lash state.
After the N cycles have finished after start of the actuating period, the attracting current I
A
and the holding current I
H
to the upper coil
58
are gradually decreased from I
A2
and I
H2
to I
A0
and I
H0
, respectively, and the attracting current I
A
and the holding current I
H
to the lower coil
62
are increased from I
A1
and I
H1
to I
A0
and I
H0
, respectively, for a predetermined N
1
cycles.
It should be noted that each of the base values I
A0
and I
H0
may be different for the upper coil
58
and the lower coil
62
.
FIG. 25
is a diagram showing a flowchart of a routine performed by the ECU
11
so as to achieve the above-mentioned operation. The routine shown in
FIG. 25
is performed once at a time when the initial actuation is completed. When the routine shown in
FIG. 25
is started, the process of step
500
is performed first.
In step
600
, a variable n indicating a number of the cycles is initialized to be “1”.
In step
602
, it is determined whether or not a request to open the engine valve
12
is generated. The process of step
602
is repeatedly performed until the request is generated. If the request to open the engine valve
12
is generated, then the process of step
604
is performed.
In step
604
, a process for supplying a smaller current to the lower coil
62
as compared to the regular situation, that is, a process for supplying an instruction current to the lower coil
62
with the attracting current I
A
being I
A1
and the holding current I
H
being I
H1
, is performed.
In step
606
, it is determined whether or not a request to close the engine valve
12
is generated. The process of step
606
is repeatedly performed until the request is generated. If the request to close the engine valve
12
is generated in step
606
, then the process of step
608
is performed.
In step
608
, a process for supplying a larger current to the upper coil
58
as compared to the regular situation, that is, a process for supplying an instruction current to the upper coil
58
with the attracting current I
A
being I
A2
and the holding current I
H
being I
H2
, is performed.
In step
610
, it is determined whether or not a relationship n>N is established. If n>N is not established, the valuable n is increased by one in step
612
and then the process of step
602
is performed again. On the other hand, if n>N is established in step
610
, then the process of step
614
is performed.
In step
614
, the variable n is initialized to be “1” again.
In step
616
, it is determined whether or not a request to open the engine valve
12
is generated. The process of step
616
is repeatedly performed until the request is generated. If the request to open the engine valve
12
is generated in step
616
, then the process of step
618
is performed.
In step
618
, an instruction current is supplied to the lower coil
62
with the attracting current I
A
being I
A1
+n·ΔI
A1
and the holding current I
H
being I
H1
+n·ΔI
H1
. The values ΔI
A1
and ΔI
H1
are set to be (I
A0
−I
A1
)/N
1
and (I
H0
−I
H1
)/N
1
, respectively. According to the process of step
618
, the attracting current I
A
and the holding current I
H
to the lower coil
62
are gradually increased to the base values I
A0
and I
H0
, respectively.
In step
620
, it is determined whether or not a request to close the engine valve
12
is generated. The process of step
620
is repeatedly performed until the request is generated. If the request to close the engine valve
12
is generated in step
620
, then the process of step
622
is performed.
In step
622
, an instruction current is supplied to the upper coil
58
with the attracting current I
A
being I
A2
−n·ΔI
A2
and the holding current I
H
being I
H2
−n·ΔI
H2
. The values ΔI
A2
and ΔI
H2
are set to be (I
A2
−I
A0
)/N
1
and (I
H2
−I
H0
)/N
1
, respectively. According to the process of step
622
, the attracting current I
A
and the holding current I
H
to the lower coil
62
are gradually decreased to the base values I
A0
and I
H0
, respectively.
In step
624
, it is determined whether a relationship n>N
1
is established. If n>N
1
is not established, the variable n is increased by one in step
626
and then the process of step
616
is performed again. On the other hand, if n>N
1
is established in step
624
, then a process for achieving a regular operation of the engine valve
12
is performed in step
628
. Specifically, in step
628
, instruction currents are supplied to the lower coil
62
and the upper coil
58
with the attracting current I
A
being I
A0
and the holding current I
H
being I
H0
each time when requests to open and close the engine valve
12
, respectively, are generated.
As mentioned above, in the present embodiment, since the attracting current I
A
and the holding current I
H
which are larger than the respective values in the regular situation are supplied to the upper coil
58
for the predetermined N cycles after the initial actuation is completed, the armature
56
can be moved until the armature
56
is in contact with the upper core
60
in a situation where the leak-down of the zero-lash adjuster
40
has occurred. Thus, according the present embodiment, it is possible to positively actuate the engine valve
12
between the fully closed position and the fully opened position.
Additionally, if the armature
56
is not attracted to be in contact with the upper core
60
by the attracting current I
A
and the armature
56
is re-attracted to the upper core
60
by the transition current I
T
or the holding current I
H
, a large impact sound may be generated by the armature
56
impacting on the upper core
60
with a high speed. According to the present embodiment, since the armature
56
can be positively attracted by the attracting current I
A
until the armature
56
comes into contact with the upper core
56
, it is possible to prevent generation of the above-mentioned large impact sound.
Further, since the attracting current I
A
and the holding current I
H
which are smaller than the respective values in the regular situation are supplied to the lower coil
62
for the N cycles, it is possible to prevent an excessive electromagnetic force from acting on the armature
56
in the valve-opening direction. Thus, according to the present embodiment, it is possible to prevent a generation of a large impact sound due to a high-speed impact of the armature
56
and the lower core
64
while suppressing power consumption in the lower coil
62
.
In the present embodiment, the instruction currents to the respective coils are changed after the initial actuation which is performed when the engine is started. However, when a desynchronization (a phenomenon in which the armature
56
cannot be attracted to the upper core
60
or the lower core
64
and the armature
56
is held in the neutral position) of the solenoid vale
10
has occurred, a process similar to the initial actuation is performed for actuating the armature
56
to the fully closed position so that the solenoid valve device
10
can be recovered from the desynchronization. Thus, the instruction currents to the respective coils may be changed for a predetermined cycles after the process for recovering the solenoid valve device
10
from the desynchronization is finished.
Additionally, in the present embodiment, both the attraction current I
A
and the holding current I
H
are changed. However, it is also possible to change only the attracting current I
A
while always using the base value I
H0
as the holding current I
H
.
Further, in the present embodiment, the attracting current I
A
and the holding current I
H
are fixed to be I
A1
or I
A2
and I
H1
or I
H2
, respectively, for the N cycles, and gradually changed toward the base values I
A0
and I
H0
, respectively, in the next N
1
cycles. However, it is also possible to gradually change the attracting current I
A
and the holding current I
H
toward the base values I
A0
and I
H0
, respectively, immediately after start of the operating period.
Next, a description will be given of a seventh embodiment of the present invention. In the present embodiment, the values I
A1
and I
A2
of the attracting current I
A
and the values I
H1
and I
H2
of the holding current are set in accordance with an elapsed time for which the actuation of the engine valve
12
has been stopped, in view of a fact that an amount of the leak-down of the zero-lash adjuster
40
changes in accordance with the above-mentioned elapsed time.
As mentioned above, the leak-down of the zero-lash adjuster
40
is a phenomenon in which oil gradually leaks out from the zero-lash adjuster
40
in a state where the armature
56
is held near the neutral position, that is, in a state where the zero-lash adjuster
40
cannot be supplied with an oil pressure. Accordingly, an amount of the leak-down of the zero-lash adjuster
40
becomes larger as the armature
56
is held near the neutral position (that is, the ignition switch is maintained to be turned off, for example) for a longer time. Thus, in the present embodiment, the values I
A1
and I
A2
of the attracting current I
A
and the values I
H1
and I
H2
of the holding current to the upper coil
58
and the lower coil
62
are set in accordance with an elapsed time after the zero-lash adjuster
40
was stopped being supplied with an oil pressure. Hereinafter, this elapsed time is referred to as a valve stopping time T
s
.
FIG. 26
is a diagram showing an example of a relationship between the valve stopping time T
s
and a displacement of the armature
56
toward the lower core
64
from the reference neutral position. The relationship shown in
FIG. 26
can be experimentally obtained by measuring positions of the armature
56
for various values of valve stopping time T
s
.
FIG. 27
is a map which is referred to so as to determine the values I
A1
, I
A2
of the attracting current I
A
and the values I
H1
, I
H2
of the holding current I
H
based on the valve stopping time T
s
.
As shown in
FIG. 26
, a displacement of the armature
56
toward the lower core
64
from the reference neutral position becomes larger for a longer valve stopping time T
s
. In accordance with this, the value I
A2
of the attracting current I
A
and the value I
H2
of the holding current I
H
to the upper coil
58
are set to be larger and the value I
A1
of the attracting current I
A
and the value I
H1
of the holding current I
H
to the lower coil
62
are set to be smaller for a longer valve stopping time T
s
, as shown in FIG.
27
. Thus, according to the present embodiment, it is possible to more properly set the instruction currents to the respective coils in accordance with a position of the armature
56
.
FIG. 28
is diagram showing a flowchart of a routine performed by the ECU
11
so as to determine the values I
A1
, I
A2
and I
H1
, I
H2
as mentioned above. The routine shown in
FIG. 28
is performed once when the ignition switch is turned on. In the present embodiment, the above-mentioned routine shown in
FIG. 25
is performed together with the routine shown in FIG.
28
. When the routine shown in
FIG. 28
is started, the process of step
700
is performed first.
In step
700
, the valve stopping time Ts (that is, a time for which the ignition switch has been turned off) is detected. The ECU
11
includes a counter which counts an elapsed time. Thus, the ECU
11
can detect the valve stopping time T
s
based on the counter value by resetting the counter when the ignition switch is turned off.
In step
702
, the values I
A1
, I
A2
of the attracting current I
A
and the values I
H1
, I
H2
of the holding current I
H
to the respective coils are determined based on the valve stopping time T
s
by referring to the map shown in FIG.
27
.
In step
704
, a process for achieving the initial actuation is performed. When the process of step
704
is finished, the present routine is ended and then the routine shown in
FIG. 25
is performed using the values I
A1
, I
A2
, I
H1
, I
H2
determined in step
702
.
In the present embodiment, the attracting current I
A
and the holding current I
H
are changed in accordance with the valve stopping time T
s
when the operating period is started. However, it is also possible to change the instruction currents I
U
and I
L
supplied to the respective coils in the initial actuation in accordance with the valve stopping time T
s
.
Additionally, in the present embodiment, the valve stopping time T
s
is set to be a time for which the ignition switch has been turned off in view of a fact that the leak-down of the zero-lash adjuster
40
is caused when the ignition switch is turned off. However, the leak-down of the zero-lash adjuster
40
is also caused when the desynchronization of the solenoid valve device
10
has occurred. Thus, the valve stopping time T
s
may be set to be an elapsed time after the desynchronization was detected.
The desynchronization can be detected by, for example, comparing an actual current flowing trough the upper coil
58
or the lower coil
62
with an instruction current to that coil. That is, when the desynchronization has occurred, an inductance of the upper coil
58
or the lower coil
62
becomes small since the armature
56
is not in contact with the corresponding core
60
or
64
a,
and thus the actual current to that coil is highly responsive to a change in the instruction current as compared to a case where the armature
56
is in contact with the corresponding core
60
or
64
. Thus, the desynchronization can be detected based on a change in the actual current when, for example, the holding current I
H
is shut off.
Next, a description will be given of an eighth embodiment of the present invention. In the present embodiment, the instruction currents to the respective coils are set in accordance with the supplied oil pressure P detected by the pressure sensor
84
.
As mentioned above, since the oil pump
83
is operated by using a rotation of the output shaft of the engine as a power source, it takes a certain time for a discharge pressure of the oil pump
83
to reach a desired value after the engine is started. Additionally, a time delay occurs in transmission of an oil pressure from the oil pump
83
to the zero-lash adjuster
40
. Thus, a tappet clearance is generated for a certain period after the armature
56
has moved to the fully closed position by the initial actuation, since the zero-lash adjuster is not supplied with a sufficient oil pressure for that period.
FIGS. 29A
to
29
E are diagrams showing changes in the engine speed, the supplied oil pressure P, the tappet clearance, the attracting current I
A
to the upper coil
58
, and the attracting current I
A
to the lower coil
62
.
As shown in
FIG. 29A
, the engine speed increases in response to start of combustion through a cranking after the ignition switch is turned on at a time t
0
. Since the discharge pressure of the oil pump
83
increases in accordance with the increase in the engine speed, the supplied oil pressure P starts increasing as shown in FIG.
29
B. The tappet clearance gradually decreases with the increase in the supplied oil pressure P and the zero-lash state is achieved at a time t
1
, as shown in FIG.
29
C.
In the present embodiment, the attracting current I
A
to the upper coil
58
is set to be larger and the attracting current I
A
to the lower coil
62
is set to be smaller as compared to the regular situation in accordance with the supplied oil pressure P as shown in
FIGS. 29D and 29E
, in view of the above-mentioned fact that the tappet clearance decreases as the supplied oil pressure P increases.
FIG. 30
is a diagram showing a flowchart of a routine performed by the ECU
11
so as to determined the values of attracting current I
A
to the upper coil
58
and the lower coil
62
. The routine shown in
FIG. 30
is started at predetermined time intervals after the initial actuation is finished. When the routine shown in
FIG. 30
is started, the process of step
800
is performed first.
In step
800
, the supplied oil pressure P is detected.
In step
802
, a difference ΔP between the supplied oil pressure P and a predetermined reference pressure P
0
is calculated as ΔP=P−P
0
. The reference pressure P
0
is set to be a value of the supplied oil pressure P required to achieve the zero-lash state.
In step
804
, it is determined whether or not the difference ΔP is a positive value. If ΔP>0 is established, then the process of step
806
is performed. On the other hand, if ΔP>0 is not established in step
804
, then the process of step
808
is performed.
In step
806
, a correction value ΔI
1
(<0) for the attracting current I
A
to the lower coil
62
is determined based on the difference ΔP, and, in the subsequent step
810
, a correction value ΔI
2
(>0) for the attracting current I
A
to the upper coil
58
is determined based on the difference ΔP.
FIG. 31
is a diagram showing an example of a map which is referred to so as to determine the correction values ΔI
1
and ΔI
2
in the above-mentioned steps
506
and
510
. The map shown in
FIG. 31
can be obtained by experimentally determining optimal values of the attracting current I
A
to the respective coils for various values of the difference ΔP and calculating differences between the determined values and the base values I
A1
—
base
, I
A2
—
base
, respectively. As shown in
FIG. 31
, the correction value ΔI
2
is set to be larger and the correction value ΔI
1
is set to be smaller for a larger value of the difference ΔP.
In step
812
, a value I
A1
of the attracting current I
A
to the lower coil
62
is calculated as I
A1
=I
A1
—
base
+ΔI
1
, and in the subsequent step
814
, a value I
A2
of the attracting current I
A
to the upper coil
58
is calculated as I
A2
=I
A2
—
base
+ΔI
2
. The base values I
A1
—
base
and I
A2
—
base
base are set to be values of the attracting current I
A
to the lower coil
62
and the upper coil
58
, respectively, in the zero-lash state, as mentioned in the sixth embodiment. When the process of step
814
is finished, the present routine is ended.
In step
808
, the correction value ΔI
1
is set to be “0”, and in the subsequent step
816
, the correction value ΔI
2
is set to be “0”. After the process of step
816
is finished, the process of the above-mentioned step
812
is performed. Thus, the base values I
A1
—
base
and I
A2
—
base
are used as values of the attracting current I
A
to the lower coil
62
and the upper coil
58
, respectively, when ΔP≦0 is established, that is, when the supplied oil pressure P is equal to or larger than the reference pressure P
0
.
As mentioned above, in the present embodiment, the attracting current I
A
to the lower coil
62
is set to be smaller and the attracting current to the upper coil
58
is set to be larger for a larger value of the difference ΔP, in view of the fact that the armature
56
shifts toward the lower core
64
as the supplied oil pressure P becomes lower (that is, as the difference ΔP becomes larger). Thus, according to the present embodiment, the optimal attracting currents I
A
can be supplied to the lower coil
62
and the upper coil
58
for actuating the armature
56
to the fully opened position and the fully closed position, respectively, so that the engine valve
12
can be positively actuated between the fully closed position and the fully opened position.
Next, a description will be given of a ninth embodiment of the present invention.
As shown in the above-mentioned
FIGS. 29B and 29C
, the supplied oil pressure P increases as a passage of time after the ignition switch is turned on, and the tappet clearance gradually decreases in accordance with the increase in the supplied oil pressure P. Thus, in the present embodiment, values of the attracting current I
A
to the respective coils are determined in accordance with an elapsed time Th after the ignition switch is turned on.
FIG. 32
is a diagram showing a flowchart of a routine performed by the ECU
11
so as to determine values of the attracting current I
A
to the upper coil
58
and the lower coil
62
in the present embodiment. In the routine shown in
FIG. 32
, steps which performs the same process as steps of the routine shown in
FIG. 30
are given the same reference numerals and descriptions thereof will be omitted. The routine shown in
FIG. 32
is started at predetermined time intervals. When the routine is started, the process of step
900
is performed first.
In step
900
, the elapsed time T
g
after the ignition switch was turned on is detected.
In step
902
, a difference ΔT between the elapsed time T
g
and a predetermined reference time T
0
is calculated as ΔT=T
0
−T
g
. The reference time T
0
is set to be a time required to achieve the zero-lash state after the ignition switch is turned on.
In step
904
, it is determined whether or not the difference ΔT is a positive value. If ΔT>0 is established, then the process of step
906
is performed. On the other hand, if ΔT>0 is not established, then the process of step
808
is performed.
In step
906
, the correction value ΔI
1
(<0) for the attracting current I
A
to the lower coil
62
is determined based on the difference ΔT, and in the subsequent step
908
, the correction value ΔI
2
(>0) for the attracting current I
A
to the upper coil
58
is determined based on the difference ΔP. When the process of step
908
is finished, the process of step
812
is performed.
FIG. 33
is a diagram showing an example of a map which is referred to so as to determine the correction values ΔI
1
and ΔI
2
in the above-mentioned steps
606
and
608
. The map shown in
FIG. 33
can be obtained by experimentally determining optimal values of the attracting current I
A
to the respective coils for various values of the difference ΔT and calculating differences between the determined values and the base values I
A1
—
base
, I
A2
—
base
, respectively. As shown in
FIG. 33
, the correction value ΔI
2
is set to be larger and the correction value ΔI
1
is set to be smaller for a larger value of the difference ΔP.
As mentioned above, in the present embodiment, the attracting current I
A
to the lower coil
62
is set to be smaller and the attracting current to the upper coil
58
is set to be larger for a larger value of the difference ΔT, in view of the fact that a displacement of the armature
56
toward the lower core
64
becomes smaller as the elapsed time Th becomes longer (that is, as the difference ΔT becomes larger). Thus, according to the present embodiment, the engine valve
12
can be positively actuated between the fully closed position and the fully opened position without a necessity of providing the pressure sensor for detecting the supplied oil pressure P.
In the above-mentioned eighth and ninth embodiments, only the attracting current I
A
is changed. However, it is also possible to change both the attracting current I
A
and the holding current I
H
as in the fifth to seventh embodiments.
Additionally, in the eighth and ninth embodiments, descriptions are given for a case where the oil pump
83
is operated by using a rotation of the engine as a power source. However, in a case where the oil pump
83
is an electric pump operated by using a battery as a power source, a discharge pressure of the oil pump
83
is not immediately increased after the ignition switch is turned on. Thus, in the case where the oil pump
83
is an electric pump, it is possible to positively actuate the engine valve
12
by changing the attracting current I
A
in accordance with the supplied oil pressure P or the elapsed time Th as in the eighth and ninth embodiments.
Further, although values of instruction currents to the respective coils are changed in the fifth to the ninth embodiments, a time for which the respective coils are supplied with instruction currents may be changed.
Next, a description will be given of a tenth embodiment of the present embodiment.
If a failure of a system for supplying an oil pressure to the zero-lash adjuster
40
, such as a trouble of the oil pump
83
or a damage of the oil supply passages
80
,
82
, has occurred, it is possible that a sufficient oil pressure is not supplied to the zero-lash adjuster
40
or no oil pressure is supplied to the zero-lash adjuster
40
. Hereinafter, such a failure is referred to as an oil-supply failure. The oil-supply failure may occur before the engine is started or after the operating period has started.
If the oil-supply failure has occurred before the engine is started, the zero-lash adjuster
40
is not supplied with a proper oil pressure when the armature
56
is moved to the fully closed position by the initial actuation and the zero-lash adjuster
40
communicates with the oil supply passage
82
. In this case, the leak-down of the zero-lash adjuster
40
cannot be cancelled.
Similarly, if the oil-supply failure has occurred during the operating period, the leak-down of the zero-lash adjuster
40
starts being caused since the zero-lash adjuster
40
is not supplied with a proper oil pressure.
As mentioned above with reference to
FIGS. 23A and 23B
, when the leak-down of the zero-lash adjuster
40
has occurred, a current to be supplied to the upper coil
58
becomes larger and a current to be supplied to the lower coil
62
becomes smaller as compared to a case where no leak-down has occurred.
In the present embodiment, the solenoid valve device
10
can be operated in one of a regular operation mode and a compensating operation mode. The regular operation mode is achieved when the reference oil pressure P is supplied to the zero-lash adjuster
40
so that the zero-lash state is maintained. When the oil-supply failure is detected, an operation mode of the solenoid valve device
10
is switched from the regular operation mode to the compensating operation mode. In the compensating operation mode, an instruction current to the lower coil
62
is set to be a smaller value and an instruction current to the upper coil
58
is set to be a larger value as compared to a case of the regular operation mode. Thus, according to the compensating operation mode, it is possible to actuate the engine valve
12
between the fully closed position and the fully opened position while suppressing power consumption of the solenoid valve device
10
when the oil-supply failure has occurred. In the present embodiment, the oil-supply failure is detected when the supplied oil pressure P is lower than the reference oil pressure P.
FIG. 34
is a routine performed by the ECU
11
in the present embodiment. The routine shown in
FIG. 34
is performed once when the ignition switch is turned on. When the routine is started, the process of step
1000
is performed first.
In step
1000
, a process for achieving the initial actuation is performed.
In step
1002
, the supplied oil pressure P is detected.
In step
1004
, it is determined whether or not the supplied oil pressure P is equal to or larger than the reference oil pressure P
0
. If P≧P
0
is established, then the process of step
1006
is performed. On the other hand, if P≧P
0
is not established, then the process of step
1008
is performed.
In step
1006
, an operation mode of the solenoid valve device
10
is set to be the regular operation mode. Specifically, in step
1006
, the attracting currents I
A
to the lower coil
62
and the upper coil
58
are set to be the base values I
A1
—
base
and I
A2
—
base
, respectively, and the holding currents I
H
to the lower coil
62
and the upper coil
58
are set to be the base values I
H1
—
base
and I
H2
—
base
, respectively, which base values were described in the above-mentioned eighth embodiment. When the process of step
1006
is finished, then the process of step
1010
is performed.
In step
1010
, it is determined whether or not the ignition switch is turned off. If the ignition is not turned off, then the process of step
1004
is performed again. Thus, the oil-supply failure can be detected after the operating period is started. On the other hand, if the ignition switch is turned off, the operation of the solenoid valve device
10
is stopped in step
1012
and then the routine is ended.
In step
1008
, the operation mode of the solenoid valve device
10
is set to be the compensating operation mode. Specifically, in step
1008
, the attracting current I
A
and the holding current I
H
to the lower coil
62
are set to be values which are smaller than the base values I
A1
—
base
and I
H1
—
base
, respectively, and the attracting current I
A
and the holding current I
H
to the upper coil
58
are set to be values which are larger than the base values I
A2
—
base
and I
H2
—
base
, respectively. When the process of step
1008
is finished, then the process of step
1014
is performed.
In step
1014
, it is determined whether or not the ignition switch is turned off. If the ignition switch is not turned off, then the process of step
1008
is performed again. On the other hand, if the ignition switch is turned off, the operation of the solenoid valve device
10
is stopped in step
1012
and then the routine is ended.
In the present embodiment, the oil-supply failure is detected based on the supplied oil pressure P. However, when an electric pump is used as the oil pump
83
, it is possible to detect a trouble of the oil pump
83
when a rotation speed of a pump motor is smaller than a predetermined value or a cutoff of the pump motor is detected.
Additionally, in the present embodiment, the instruction currents to the respective coils are set to be constant values in the compensating operation mode. However, if oil gradually leaks out from the oil supply passage
80
or
82
due to a crack of the passage, for example, the supplied oil pressure P changes in accordance with an extent of the crack. The instruction currents to be supplied to the respective coils change in accordance with the supplied oil pressure P, as mentioned in the eighth embodiment. Thus, the instruction currents to the respective coils may be changed based on the supplied oil pressure P by the ECU
11
performing the abovementioned mentioned routine shown in FIG.
30
.
In the above-mentioned fifth to tenth embodiments, descriptions were given of current controls with respect to the solenoid valve device
10
. However, it should be noted that these current controls can be applied to the solenoid valve devices
200
,
400
.
Additionally, the present invention is not limited to these embodiments, but variations and modifications may be made without departing from the scope of the present invention.
The present application is based on japanese priority applications no. 10-331548 filed on Nov. 20, 1998, No. 11-54173 filed on Mar. 2, 1999, No. 11-84896 filed on Mar. 26, 1999, and No. 11-105555 file on Apr. 13, 1999, the entire contents of which are hereby incorporated by reference.
Claims
- 1. A valve device comprising:an engine valve which can move in an axial direction thereof and being in operative engagement with an armature; an electromagnet which attracts said armature so that said engine valve moves in the axial direction; and a zero-lash adjuster mechanism which is interposed between said engine valve and said armature, said zero-lash adjuster mechanism being connected between a valve shaft of said engine valve and an armature shaft of said armature, wherein at least a part of said zero-lash adjuster mechanism is disposed inside said electromagnet.
- 2. The solenoid valve device as claimed in claim 1, wherein said zero-lash adjuster mechanism is a displacement-compensating mechanism which expands in accordance with an increase in a spacing between said valve shaft and said armature shaft.
- 3. The solenoid valve device as claimed in claim 2, wherein said displacement-compensating mechanism expands when said engine valve is in a closed position.
- 4. The solenoid valve device as claimed in claim 2, wherein said displacement-compensating mechanism is a hydraulic zero-lash adjuster.
- 5. The solenoid valve device as claimed in claim 4, wherein said hydraulic zero-lash adjuster expands by being supplied with an oil pressure.
- 6. The solenoid valve device as claimed in claim 5, further comprising an oil pressure supplying mechanism for supplying an oil pressure to said hydraulic zero-lash adjuster when said engine valve is closed.
- 7. The solenoid valve device as claimed in claim 1, wherein said zero-lash adjuster mechanism includes a hydraulic zero-lash adjuster which expands in accordance with an increase in a spacing between said engine valve and said armature by being supplied with an oil pressure.
- 8. The solenoid valve device as claimed in claim 1, wherein said electromagnet includes an upper core and a lower core positioned closer to said engine valve than said upper core so that said armature moves between said upper core and said lower core, and said zero-lash adjuster mechanism is disposed inside said lower core of said electromagnet.
- 9. The solenoid valve device as claimed in claim 8, wherein said zero-lash adjuster mechanism is operated by an hydraulic pressure supplied through an oil supply passage provided in said lower core.
Priority Claims (4)
Number |
Date |
Country |
Kind |
10-331548 |
Nov 1998 |
JP |
|
11-054173 |
Mar 1999 |
JP |
|
11-084896 |
Mar 1999 |
JP |
|
11-105555 |
Apr 1999 |
JP |
|
US Referenced Citations (12)
Foreign Referenced Citations (3)
Number |
Date |
Country |
7-332044 |
Dec 1995 |
JP |
0722039 |
Oct 1996 |
JP |
11-30113 |
Feb 1999 |
JP |