TECHNICAL FIELD
[0001] This disclosure relates to a valve opening/closing timing control device capable
of adjusting the opening/closing timing of the intake valves or exhaust valves of
an internal combustion engine used in vehicles such as automobile, and more particularly
to a valve opening/closing timing control device including a driving side rotational
member synchronously rotatable with a crankshaft, a driven side rotational member
arranged coaxially with the driving side rotational member in a relatively rotational
manner and integrally rotatable with a camshaft that opens and closes valves of an
internal combustion engine, a retarded angle chamber and an advanced angle chamber
which are formed by the driving side rotational member and the driven side rotational
member, in which the retarded angle chamber moves a relative rotational phase of the
driven side rotational member to the driving side rotational member in a retarded
angle direction, and the advanced angle chamber moves the relative rotational phase
of both rotational members in an advanced angle direction, and a lock mechanism confining
the relative rotational phase to a predetermined lock phase, specifically, a technique
for biasing the driving side rotational member and the driven side rotational member
in a direction of a lock phase.
BACKGROUND DISCUSSION
[0002] JP-A-2000-345816 (Patent Document 1; paragraphs [0057] to [0067], and Figs. 1, 2, 3 and 6) discloses
a valve opening/closing timing control device including a driving side rotational
member (a shoe housing in Patent Document 1) and a driven side rotational member (a
vane rotor in Patent Document 1), in which an accommodation chamber is divided into
two parts, an advanced angle chamber and a retarded angle chamber, by a vane provided
on the driven side rotational member. The valve opening/closing timing control device
further includes a fitting type restriction means for setting a phase difference between
the driving side rotational member and the driven side rotational member to an optimum
intermediate position, and a spring as an advanced angle means for rotating the driven
side rotational member with respect to the driving side rotational member in the advanced
angle direction. One end portion of the spring is locked to a locking hole of the
driving side rotational member, and the other end portion of the spring is locked
to a locking hole of an elongated hole shape (second embodiment).
[0003] With the above configuration, if the engine starts up in a state in which the driven
side rotational member (camshaft side) is more to the retarded angle side than an
intermediate position, the driven side rotational member is rotated in the direction
of the intermediate position by the biasing force of the spring to fit the restriction
means, and thus the engine starts up quickly. After the engine starts up, operating
oil is supplied to the restriction means to release the fitting, and the operating
oil is supplied to any one of the advanced angle chamber and the retarded angle chamber
to achieve a relative rotation between the driving side rotational member and the
driven side rotational member.
[0004] In Patent Document 1, when the driven side rotational member is relatively rotated
toward the advanced angle side with respect to the driving side rotational member
by releasing the fitting of the restriction means, the other end portion of the spring
is moved in the engaging hole with the elongated hole shape, so that the biasing force
of the spring does not act.
[0005] Further, a valve opening/closing timing control device disclosed in
JP-A-2009-074384 (Patent Document 2; paragraphs [0026] to [0028], and Figs. 3 to 7) includes a driving
side rotational member and a driven side rotational member, in which an accommodation
chamber is divided into two parts, an advanced angle chamber and a retarded angle
chamber, by a vane provided on the driven side rotational member. The valve opening/closing
timing control device further includes a lock mechanism for fixing and maintaining
the driving side rotational member and the driven side rotational member to an intermediate
lock phase, and a torsion spring to bias the driving side rotational member and the
driven side rotational member in the direction of the intermediate lock phase which
generates an assisting force.
[0006] The torsion spring serves to suppress displacement of the retarded angle side in
a region between an intermediate regulation phase which is placed in the direction
of the retarded angle phase than the intermediate lock phase, and a most retarded
angle phase, and has the role of a stopper at the displacement from the intermediate
lock phase to the intermediate regulation phase after the engine starts up.
[0007] In Patent Document 2, one end portion of the torsion spring is fixed to the driving
side rotational member, and the other end portion can abut against an opening formed
diametrically in the driven side rotational member. A spring receiving groove to which
the other end portion is inserted is formed in the driving side rotational member.
As the other end portion of the torsion spring abuts against an abutting surface of
the opening in an effective range between the intermediate regulation phase and the
most retarded angle phase by the configuration, the biasing force acts on the driven
side rotational member. Further, the other end portion abuts against a stopper surface
of the spring receiving groove in the intermediate regulation phase, so that no biasing
force acts on the driven side rotational member.
[0008] As disclosed in Patent Document 1 or Patent Document 2, the torsion spring is used
between the driving side rotational member and the driven side rotational member as
the biasing means for biasing the rotational members in the direction of the lock
phase from the most retarded angle phase. The number of turns in a coil portion of
the torsion spring is required to some degree, thereby causing the whole valve opening/closing
timing control device to become larger.
[0009] That is, so as not to vary spring load significantly in the relative rotational region
of the driven side rotational member with respect to the driving side rotational member
from the most retarded angle phase to the lock phase, the number of turns in the coil
portion is required to some degree. Therefore, there is a need for a space in the
direction of a shaft core by a dimension corresponding to the number of turns, which
causes the whole valve opening/closing timing control device to become larger.
[0010] A need thus exists for a valve opening/closing timing control device without impairing
the function of biasing the driving side rotational member and the driven side rotational
member from a most retarded angle phase to the direction of a predetermined phase.
SUMMARY
[0011] According to an aspect of this disclosure, there is provided a valve opening/closing
timing control device including a driving side rotational member synchronously rotatable
with a crankshaft of an internal combustion engine, a driven side rotational member
arranged coaxially with the driving side rotational member in a relatively rotational
manner and integrally rotatable with a camshaft that opens and closes valves of the
internal combustion engine, a retarded angle chamber and an advanced angle chamber
which are formed by the driving side rotational member and the driven side rotational
member, in which the retarded angle chamber moves a relative rotational phase of the
driven side rotational member to the driving side rotational member in a retarded
angle direction in accordance with volume increase, and the advanced angle chamber
moves the relative rotational phase in an advanced angle direction in accordance with
volume increase, a lock mechanism confining the relative rotational phase to a predetermined
lock phase, and a spiral spring providing a biasing force in a predetermined phase
direction in a retarded angle region of the relative rotational phase from a most
retarded angle phase to a predetermined phase of the driven side rotational member
to the driving side rotational member, and not providing the biasing force to a most
advanced angle phase from the predetermined phase.
[0012] At the time of starting of the internal combustion engine, it is preferable that
the relative rotational phase of the driven side rotational member to the driving
side rotational member is at the predetermined lock phase, but is not necessary at
the predetermined lock phase. For example, it may be at the retarded angle region
side near the predetermined lock phase or at the advanced angle region side near the
predetermined lock phase, on the basis of the predetermined lock phase. That is, at
the time of starting of the internal combustion engine, if the relative rotational
phase of the driven side rotational member to the driving side rotational member is
in a predetermined region including the predetermined lock phase, proper starting
is achieved.
[0013] In this aspect of this disclosure, if the internal combustion engine starts up in
a state in which the relative rotational phase of the driven side rotational member
to the driving side rotational member is in the retarded angle region, the relative
rotational phase acts in the predetermined phase direction by the biasing force of
the spiral spring, so that the relative rotational phase is early moved in the predetermined
phase direction to enhance the starting ability of the internal combustion engine.
Further, in a case in which the relative rotational phase is more towards the advanced
angle region than the predetermined phase, the biasing force of the spiral spring
does not act. In particular, since no space corresponding to the coil portion of the
torsion spring is required by using the spiral spring, it is possible to suppress
the device from becoming larger. As a result, the valve opening/closing timing control
device can be compactly configured without impairing the function of biasing the driving
side rotational member and the driven side rotational member in the predetermined
phase direction from the most retarded angle phase.
[0014] The aspect this disclosure may include the spiral spring providing the biasing force
in the predetermined lock phase direction in the retarded angle region of the relative
rotational phase from the most retarded angle phase to the predetermined lock phase,
and not providing the biasing force to the most advanced angle phase from the predetermined
lock phase.
[0015] If the internal combustion engine starts up in a state in which the relative rotational
phase of the driven side rotational member to the driving side rotational member is
in the retarded angle region, the relative rotational phase acts in the predetermined
lock phase direction as the predetermined phase by the biasing force of the spiral
spring, so that the relative rotational phase is maintained early to the predetermined
lock phase to enhance the starting ability of the internal combustion engine. Further,
in a case in which the relative rotational phase is in the advanced angle region than
the predetermined lock phase, the biasing force of the spiral spring does not act.
[0016] In the aspect of this disclosure, the outer circumference of a shaft-shaped body
which rotates integrally with the driven side rotational member is provided with an
engaging concave portion having a region distance corresponding to the advanced angle
region from the predetermined lock phase to the most advanced angle phase. An engaging
portion formed by bending an inner end portion of the spiral spring is engaged to
the engaging concave portion, and a support portion of an outer end portion of the
spiral spring is supported by a support body which rotates integrally with the driving
side rotational member. The engaging portion is biased in a direction of engaging
the engaging concave portion by the spiral spring.
[0017] In the configuration, in accordance with the setting of the positional relationship
between the engaging portion of the spiral spring and the engaging concave portion
of the shaft-shaped body, the biasing force can act to rotate the driven side rotational
member in the predetermined lock phase direction in a case in which the relative rotational
phase of the driven side rotational member to the driving side rotational member is
in the retarded angle region. Further, in a case in which the relative rotational
phase of the driven side rotational member to the driving side rotational member is
in the advanced angle phase, the free rotation of the driven side rotational member
is allowed. In addition, since the engaging portion is biased in a direction of a
shaft core, it does not lead to problems in which the engaging portion becomes released
from the engaging concave portion.
[0018] The aspect of this disclosure may include a regulation piece to restrict displacement
of the engaging portion in the direction of the advanced angle region by abutment
of the engaging portion.
[0019] In the configuration, since the position of the engaging portion is restricted by
the regulation piece, it is possible to set the range of which the biasing force of
the spiral spring acts.
[0020] The aspect of this disclosure may include a suppression piece to suppress displacement
of the engaging portion in the direction in which the spiral spring bulges.
[0021] In the configuration, since the suppression piece suppresses displacement of the
engaging portion of the spiral spring in a releasing direction from the engaging concave
portion, it does not lead to problems of the engaging portion releasing from the engaging
concave portion.
[0022] According to the aspect of this disclosure, the support portion is formed in a concave
surface which is concave in the center direction of the spiral spring, and the support
body is formed in a protruding surface which fits into the concave surface. The concave
surface and the engaging portion may be disposed at a position in which a spring body
is sandwiched in a radial direction.
[0023] In the configuration, when the protruding surface is fitted into the concave surface
and the engaging portion is engaged to the engaging concave portion, a force acts
in the direction of compressing the spring body in the radial direction. By the spring
load generated by the action of the force, the biasing force is generated from the
spring body so that the protruding surface is fitted into the concave surface and
the engaging portion is fitted into the engaging concave portion. Consequently, it
is possible to reliably support the spiral spring and provide the biasing force between
the driving side rotational member and the driven side rotational member reliably.
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] The foregoing and additional features and characteristics of this disclosure will
become more apparent from the following detailed description considered with the reference
to the accompanying drawings, wherein:
[0025] Fig. 1 is a cross-sectional view illustrating a valve opening/closing timing control
device including an electromagnetic control valve;
[0026] Figs. 2A and 2B are cross-sectional views taken along the line IIa-IIa and the line
IIb-IIb in Fig. 1 in a most retarded angle phase;
[0027] Figs. 3A and 3B are cross-sectional views illustrating an outer rotor and an inner
rotor at a lock phase, and a spiral spring at the lock phase;
[0028] Figs. 4A and 4B are cross-sectional views illustrating the outer rotor and the inner
rotor at a most advanced angle phase, and the spiral spring at the most advanced angle
phase; and
[0029] Fig. 5 is a perspective view illustrating the shape of the spiral spring.
DETAILED DESCRIPTION
[0030] Embodiments disclosed here will now be described with reference to the accompanying
drawings.
(Basic configuration)
[0031] As shown in Fig. 1 and Figs. 2A and 2B, a valve opening/closing timing control device
includes an outer rotor 1 serving as a driving side rotational member and synchronously
rotatable with a crankshaft (not shown) of an engine (an internal combustion engine),
an inner rotor 2 serving as a driven side rotational member and coaxially and synchronously
rotatable with a camshaft 3 which opens and closes an intake valve or an exhaust valve
in a combustion chamber of the engine, and an electromagnetic control valve V.
[0032] The valve opening/closing timing control device includes a configuration in which
the inner rotor 2 (driven side rotational member) is inserted in the outer rotor 1
(driving rotational member). Consequently, the outer rotor 1 and the inner rotor 2
can be relatively freely rotated around a core X of a rotational shaft in the range
of a predetermined relative rotational phase. A fluid pressure chamber is formed between
the outer rotor 1 and the inner rotor 2, the fluid pressure chamber is partitioned
into a retarded angle chamber 11 and an advanced angle chamber 12 by a vane 5 installed
therein.
[0033] The vane 5 is inserted into a vane groove formed in the outer circumference of the
inner rotor 2, and is biased in a protruding direction by a leaf spring. Consequently,
at the time of relative rotation of the outer rotor 1 and the inner rotor 2, an outer
end portion of the vane 5 is slidable on an inner surface of the outer rotor in the
fluid pressure chamber.
[0034] The camshaft 3 is coaxially arranged with the core X of the rotational shaft. The
camshaft 3 is connected to the inner rotor 2 by a connecting bolt 4. A front plate
6 is placed on one surface of the outer rotor 1, and a rear plate 7 is placed on the
other surface of the outer rotor 1. The front plate 6 and the rear plate 7 are fixed
to the outer rotor 1 by a plurality of fixing bolts 8. With the configuration, the
inner rotor 2 is interposed between the front plate 6 and the rear plate 7.
[0035] Further, the front plate 6 includes a spiral spring S to provide a biasing force
on the outer rotor 1 (driving side rotational member) and the inner rotor 2 (driven
side rotational member), and a cover 9 to cover the spiral spring. The detailed configuration
of the spiral spring S will be described below.
[0036] A timing sprocket 7S is integrally installed on the outer circumference of the rear
plate 7. Between the timing sprocket 7S and a gear attached to the crankshaft of the
engine, there is provided a power transmission member (not shown) such as a timing
chain or a timing belt.
[0037] In the configuration, upon start-up of the engine, a rotational driving force of
the crankshaft is transmitted to the timing sprocket 7S through the power transmission
member, and the outer rotor 1 rotates in a rotational direction T shown in Fig. 2A
or the like. As the inner rotor 2 rotates in the rotational direction T in conjunction
with the rotation, the camshaft 3 rotates, and the intake valve or the exhaust valve
of the engine is opened or closed by the driving rotation of a cam (not shown) provided
on the camshaft 3.
[0038] In the valve opening/closing timing control device, when the engine operates, if
the advanced angle chamber 12 is supplied with operating oil, the volume of the advanced
angle chamber 12 is enlarged by the pressure acting on the vane 5, and thus the inner
rotor 2 is moved in a direction denoted by an arrow T1 with respect to the outer rotor
1. Consequently, the relative rotational phase of the outer rotor 1 and the inner
rotor 2 is shifted in the advanced angle direction. In contrast, if the retarded angle
chamber 11 is supplied with the operating oil, the volume of the retarded angle chamber
11 is enlarged by the pressure acting on the vane 5 in an adverse direction, and thus
the inner rotor 2 is moved in a direction denoted by an arrow T2 with respect to the
outer rotor 1. Consequently, the relative rotational phase of the outer rotor 1 and
the inner rotor 2 is shifted in the retarded angle direction. The opening and closing
timing of the intake vale or exhaust valve is controlled by changing a rotational
phase of the camshaft 3 with respect to the rotational phase of the crankshaft.
[0039] Engine oil is used as the operating oil, and the valve opening/closing timing control
device includes a lock mechanism L to maintain the relative rotational phase between
the outer rotor 1 and the inner rotor 2 at a lock phase suitable for the start-up
of the engine. In other words, the lock mechanism L restricts the relative rotation
between the outer rotor 1 and the inner rotor 2 when the relative rotational phase
between the outer rotor 1 and the inner rotor 2 becomes the predetermined phase, i.e.,
the predetermined lock phase. The lock mechanism L confines (locks) the outer rotor
1 and the inner rotor 2 at a set relative rotational phase in circumstances in which
the pressure of the operating oil is an unstable state immediately after the start-up
of the engine. Therefore, the rotational phase of the camshaft 3 with respect to the
rotational phase of the crankshaft is maintained at a phase suitable for the start-up
of the engine, thereby providing the stable start-up of the engine.
[0040] The lock mechanism L is constituted of a pair of lock pieces 14 of a plate shape
extendable and withdrawing freely to and from the outer rotor 1, a spring 15 biasing
each of the lock pieces 14 in a protruding direction (direction of the inner rotor
2), and a pair of lock concave portions 16 formed on the outer circumferential portion
of the inner rotor 2 in a concave shape so as to be engaged to each of the lock pieces
14. In this instance, as the shape of the lock pieces 14, a pin shape may be employed,
as well as the plate shape shown in this embodiment.
[0041] In the valve opening/closing timing control device, the inner rotor 2 is provided
with a retarded angle chamber side oil passage 11a through which the operating oil
is distributed to a plurality of retarded angle chambers 11, an advanced angle chamber
side oil passage 12a through which the operating oil is distributed to a plurality
of advanced angle chambers 12, and a lock release oil passage 16a through which the
operating oil is distributed to the lock concave portion 16.
[0042] As shown in Fig. 1 and Figs. 2A and 2B, the cam shaft 3 is fitted with a bush 18,
and the bush 18 is relatively rotated with respect to the camshaft 3. There is an
oil passage system to supply sequentially the operating oil to an internal oil passage
3a of the camshaft 3 and an internal oil passage 2a of the inner rotor 2 from a supply
oil passage 18a of the bush 18. The operating oil supplied from a hydraulic pump P
to the supply oil passage 18a is supplied to a cylindrical space 2S of the inner rotor
2 by the oil passage system. Further, the operating oil supplied to the inner rotor
2 is supplied to the retarded angle chamber side oil passage 11a, the advanced angle
chamber side oil passage 12a, and the lock release oil passage 16a by the electromagnetic
control valve V, and is discharged from the retarded angle chamber side oil passage
11a, the advanced angle chamber side oil passage 12a and the lock release oil passage
16a by the electromagnetic control valve V.
(Electromagnetic control valve)
[0043] The electromagnetic control valve V includes an operating oil control portion Va
having a spool valve 22 which is operated by an electromagnetic solenoid 21, and an
operating oil supply/discharge portion Vb of a cylindrical shape to perform distribution
of the operating oil, in which the operating oil control portion and the operating
oil supply/discharge portion are integrally formed. The operating oil supply/discharge
portion Vb includes a check valve C provided in a main oil passage 23 to receive the
operating oil from the above-described inner oil passage 2a. In an entire circumference
of an outer surface of the operating oil supply/discharge portion Vb, three ports
24, 25 and 26 are formed in a groove shape, in which the distribution of the operating
oil is controlled by the spool valve 22. An oil seal 27 is fitted from outside on
the outer circumference of the operating oil supply/discharge portion Vb to suppress
leakage of the operating oil from each of the ports 24, 25 and 26.
[0044] The above-described cylindrical space 2S is formed in the inner rotor 2 so as to
form a cylindrical shape around the core X of the rotational shaft, and the above-described
operating oil supplying/discharging portion Vb of the electromagnetic control valve
V is relatively rotatably fitted in the cylindrical space 2S. In this instance, the
retarded angle chamber side oil passage 11a, the advanced angle chamber side oil passage
12a and the lock release oil passage 16a are in communication with the ports 24, 25
and 26 in the figure, but the relative disposition of the oil passages is not limited
thereto.
[0045] In the valve opening/closing timing control device, a gap is formed between the inner
rotor 2 and the front plate 6 and between the inner rotor 2 and the rear plate 7,
in which the operating oil slightly leaks there through. The operating oil slightly
leaks through the other movable portion. The leaked operating oil is collected by
an oil pan (not shown).
(Outline of control system)
[0046] Although not shown in the figures, the control system of the valve opening/closing
timing control device includes a crank angle sensor detecting the rotational angle
of the crankshaft of the engine, a camshaft angle sensor detecting the rotational
angle of the camshaft 3, and an ECU (not shown) controlling the electromagnetic control
valve V
[0047] The ECU is provided with a signal system acquiring ON/OFF information of an ignition
key, information from an oil temperature sensor detecting the temperature of the engine
oil, or the like, and control information of the optimum relative rotational phase
according to the driving state of the engine is stored in a nonvolatile memory.
[0048] The ECU detects the relative phase of the outer rotor 1 and the inner rotor 2 based
on information of the driving state (e.g., revolutions of engine, temperature of cooling
water or the like) and the detected result of the above-described crank angle sensor
and camshaft angle sensor. The distribution of the operating oil to the retarded angle
chamber side oil passage 11a, the advanced angle chamber side oil passage 12a and
the lock release oil passage 16a is performed by operating the electromagnetic control
valve V based on the information, thereby controlling the relative rotational phase
of the outer rotor 1 and the inner rotor 2. Consequently, the phase control is achieved
between the most retarded angle phase (relative rotational phase in which the volume
of the retarded angle chamber 11 is maximized) and the most advanced angle phase (relative
rotational phase in which the volume of the advanced angle chamber 12 is maximized),
and the lock state and the unlock state by the lock mechanism L are achieved.
[0049] If an operation is performed to stop the engine, the ECU moves the relative phase
of the outer rotor 1 and the inner rotor 2 in the lock phase direction by supplying
the operating oil to the retarded angle chamber 11 or the advanced angle chamber 12
in a state in which the operating oil is discharged from the lock release oil passage
16a. Consequently, the engine stops in a state in which the pair of lock pieces 14
is engaged to the pair of the corresponding lock concave portions 16. When the engine
starts up after stopping, the engine starts up reliably by confining (restricting)
the outer rotor 1 and the inner rotor 2 with the lock mechanism L to hold the relative
rotation (to the predetermined lock phase).
[0050] After the start-up of the engine, the ECU supplies the operating oil to the lock
release oil passage 16a to lift the lock pieces 14 up from the lock concave portions
16 to thereby release the lock. The ECU changes the relative phase of the outer rotor
1 and the inner rotor 2 in a state in which the pressure of the operating oil acts
on the lock release oil passage 16a, so that the control of the opening and closing
timing of the intake valve and the exhaust valve is performed by the ECU.
[0051] In a case where the inner rotor 2 with respect to the outer rotor 1 is in the retarded
angle side region than the lock phase, the above-described spiral spring S has a function
of providing the biasing force in the lock phase direction (direction of the predetermined
phase) with respect to the inner rotor 2. Therefore, a problem in which the relative
phase of the inner rotor 2 integrally rotating with the camshaft 3 is retarded with
respect to the rotation of the outer rotor 1 since the camshaft 3 receives resistance
from the valve spring is solved.
[0052] In a case where the engine is in the stop state since excessive load is applied to
the engine, the inner rotor 2 may reach the most retarded angle phase with respect
to the outer rotor 1. When the engine starts up in this situation, the ECU controls
the phase of the inner rotor 2 with respect to the outer rotor 1 to move to the lock
phase early and thus set the phase in a lock state so as to perform reliable start-up
of the engine.
[0053] As a detailed control mode, the electromagnetic control valve V discharges the operating
oil from the lock release oil passage 16a, discharges the operating oil from the retarded
angle side oil passage 11a and supplies the operating oil to the advanced angle chamber
side oil passage 12a by the control of the ECU, so that the inner rotor 2 with respect
to the outer rotor 1 is moved in the lock phase direction. Under the control, the
lock pieces 14 are engaged to the lock concave portions 16 at the timing in which
the outer rotor 1 and the inner rotor 2 reach the lock phase, so that the lock mechanism
L is in the lock state. In this instance, the rotational phase of the most retarded
angle phase, in which the inner rotor 2 is disposed at the most retarded angle side,
is referred to as a super-retarded angle phase.
[0054] However, in a case in which the engine starts up in the state in which the inner
rotor 2 is at the most retarded angle phase, the time is needed until the relative
rotational phase reaches the lock phase, so that the start-up of the engine is not
smoothly performed. In particular, the operating oil is cold at the time of stopping
the engine in cold climates, the viscosity of the operating oil is high, and thus
the distribution of the operating oil to each of the retarded angle chamber 11 and
the advanced angle chamber 12 is not smoothly performed. For this reason, the start-up
of the engine is not smoothly performed. In order to address the above problem, it
is aimed to shorten the time required to reach the lock phase by assisting the relative
movement of the outer rotor 1 and the inner rotor 2 in the direction of the lock phase
by the above-described spiral spring S.
(Spiral spring)
[0055] As shown in Fig. 2B and Fig. 5, the spiral spring S operates to bias the relative
rotational phase of the inner rotor 2 (driven side rotational member) with respect
to the outer rotor 1 (driving side rotational member) in the direction of the lock
phase in a retarded angle region A from the most retarded angle phase to the lock
phase. In addition, the spiral spring S operates so as not to provide the biasing
force in an advanced angle region B from the lock phase to the most advanced angle
phase. In this instance, it is not necessary for the spiral spring S to provide the
biasing force in the direction of the lock phase in the whole area of the retarded
angle region A. For example, the biasing force may act from the super-retarded angle
phase to near the lock phase, or the biasing force may act in the advanced angle side
on the basis of the lock phase to the advanced angle region A near the lock phase.
The phase on which the biasing force of the spiral spring S acts is the predetermined
phase of the embodiment disclosed here and thus becomes a proper phase (region) suitable
for the start-up of the engine (internal combustion engine).
[0056] Since the spiral spring S is formed in a spiral shape from a strap of spring material,
the thickness (dimension of the rotational shaft in the direction of core X) can be
thinned as compared with one including a coil portion such as a torsion spring. In
a case where the spiral spring S is installed, since a large space is not required
in the direction of the core X of the rotational shaft, it is possible to downsize
the valve opening/closing timing control device.
[0057] The outer circumference of an axial portion 10 (one example of the axial body) of
the inner rotor 2 is provided with an engaging concave portion 10G having an opening
width (opening width in a circumferential direction) of a region distance corresponding
the advanced angle region B. The front plate 6 connected to the outer rotor 1 is provided
with a protruding surface 6T protruding in the direction of the core X of the rotational
shaft.
[0058] The spiral spring S has a spring body 30 of a spiral shape. An engaging portion 31
is formed by bending the inner end portion of the spiral spring and is engaged to
the engaging concave portion 10G, and a concave surface 32 (one example of the support
portion) is formed on an outer end portion of the spiral spring in a concaved shape
in a center direction (core X of the rotational shaft) of the spiral spring S so that
the protruding surface 6T (one example of the support body) is inserted into the concave
surface.
[0059] The front plate 6 is provided with a suppression piece 33 constituted of a pin which
abuts against the engaging portion 31 to suppress a displacement of the engaging portion
31 in the direction of the advanced angle region B. In addition, the front plate 6
is provided with a suppression piece 34 constituted of a pin which abuts against an
adjacent portion of the engaging portion 31 of the spiral spring S to suppress a displacement
of the engaging portion 31 in a direction in which the diameter of the spiral spring
S is bulged.
[0060] In the region of the same direction on the basis of the center position of the spiral
spring S, the engaging portion 31 and the concave surface 32 described above are positioned
in a position to which the spring body 30 is sandwiched. Further, the spiral spring
S is set in such a manner that the distance from the engaging portion 31 to the concave
surface 32 is slightly longer than that from the engaging concave portion 10G to the
protruding surface 6T in a no-load free state. In addition, spacers 35 are inserted
into a gap of the spring body 30 in the vicinity of the outer circumference of the
spiral spring S.
[0061] According to the arrangement and the feature of the spiral spring S, the above-described
biasing force is obtained by compressing the spring body 30 in a radial direction
so as to shorten the distance of the engaging portion 31 and the concave surface 32
slightly when the spiral spring S is set. Consequently, the engaging portion 31 is
biased in a direction (direction of the core X of the rotational shaft) of fitting
it into the engaging concave portion 10G by the resilient force of the spring body
30. Simultaneously, the concave surface 32 is biased in a direction of pressing it
against the protruding surface 6T. Further, the appropriate gap is formed in the spring
body 30 by the spacers 35. Therefore, both ends of the spiral spring S can be supported
reliably and the biasing force can provide between the outer rotor 1 and the inner
rotor 2 reliably.
[0062] As shown in Fig. 2A, in a state in which the engine stops at the relative phase of
the inner rotor 2 with respect to the outer rotor 1 which is at the super-retarded
angle, an opened end portion of the engaging concave portion 10G abuts against the
engaging portion 31, as shown in Fig. 2B, and the spiral spring S provides the biasing
force to move the relative rotational phase of the outer rotor 1 and the inner rotor
2 in the lock phase.
[0063] In a case where the engine stops in this state, the biasing force of the spiral spring
S is provided on the outer rotor 1 and the inner rotor 2 continuously through the
protruding surface 6T and the axial portion 10 until reaching the lock phase. As shown
in Fig. 3A, if the relatively rotational phase of the outer rotor 1 and the inner
rotor 2 reaches the lock phase, the engaging portion 31 abuts against the regulation
piece 33, as shown in Fig. 3B. The region, on which the biasing force of the spiral
spring S acts, corresponds to the retarded angle region A.
[0064] If the relative rotational phase reaches the lock phase and the engaging portion
31 abuts against the regulation piece 33, the biasing force of the spiral spring S
does not act on the axial portion 10. Further, the lock pieces 14 of the lock mechanism
L fit into the lock concave portions 16 to reach the lock state, the stable start-up
of the engine is achieved. Since the engaging portion 31 of the spiral spring S abuts
against the suppression piece 34, it is possible to suppress the displacement of the
spiral spring S in the bulging direction, so that the engaging portion 31 is not released
from the engaging concave portion 10G.
[0065] After the engine starts, as shown in Fig. 4A, in a case where the inner rotor 2 moves
to the advanced angle region B in the direction of the advanced angle, the inner rotor
reaches a position in which the engaging portion 31 is spaced apart from the opened
end portion of the engaging concave portion 10G, as shown in Fig. 4B. Therefore, the
biasing force of the spiral spring S does not act on the inner rotor 2, and the appropriate
relative movement is achieved by supply of the operating oil to any one of the outer
rotor 1 and the inner rotor 2.
[0066] In particular, the outer end portion of the spiral spring S may be formed to have
a support structure in such a manner that the front plate 6 is provided with a concave
portion or a hole for engagement, and the outer end portion of the spiral spring S
is bent to be engaged to the concave portion or the hole. Further, the configuration
may be formed in such a manner that a pin or the like serving as the engaging portion
31 protrudes from the inner end portion of the spiral spring S to be engaged to the
engaging concave portion 10G.
[0067] Since the valve opening/closing timing control device disclosed here includes the
spiral spring S to bias the relative rotational phase of the outer rotor 1 and the
inner rotor 2 in the lock phase direction, the space corresponding to the coil portion
such as the torsion spring is not required, thereby suppressing the device from becoming
larger.
[0068] The spiral spring S applies the biasing force in the lock phase direction at the
relative rotational phase only in a case where the relative rotational phase of the
inner rotor 2 (driven side rotational member) to the outer rotor 1 (driving side rotational
member) is in the retarded angle region A from the most retarded angle phase to near
the lock phase. Consequently, if the engine starts up in the state in which the relative
rotational phase of the inner rotor 2 to the outer rotor 1 is at the most retarded
angle phase, the movement of the inner rotor 2 with respect to the outer rotor 1 is
assisted until reaching the lock phase.
[0069] In a case where the relative rotational phase of the outer rotor 1 and the inner
rotor 2 exceeds the lock phase and is in the advanced angle region B, the biasing
force of the spiral spring S does not act, and the relative rotation is smoothly performed.
[0070] The embodiment disclosed here can be used in the whole valve opening/closing timing
control devices capable of setting opening and closing timing of any one of an intake
valve and an exhaust valve of an engine.
[0071] The principles, preferred embodiment and mode of operation of the present invention
have been described in the foregoing specification. However, the invention which is
intended to be protected is not to be construed as limited to the particular embodiments
disclosed. Further, the embodiments described herein are to be regarded as illustrative
rather than restrictive. Variations and changes may be made by others, and equivalents
employed, without departing from the spirit of the present invention. Accordingly
it is expressly intended that all such variations, changes and equivalents which fall
within the spirit and scope of the present invention as defined in the claims, be
embraced thereby.
It is explicitly stated that all features disclosed in the description and/or the
claims are intended to be disclosed separately and independently from each other for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention independent of the composition of the features in the embodiments and/or
the claims. It is explicitly stated that all value ranges or indications of groups
of entities disclose every possible intermediate value or intermediate entity for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention, in particular as limits of value ranges.