TECHNICAL FIELD
[0001] The present invention relates to a variable displacement vane pump used as a fluid
pressure source.
BACKGROUND ART
[0002] JP2013-194692A describes a variable displacement vane pump that is capable of changing an amount
of working fluid discharged by changing an amount of eccentricity of a cam ring with
respect to a rotor.
[0003] In order to move the cam ring, this variable displacement vane pump includes a first
fluid pressure chamber and a second fluid pressure chamber that are formed on the
outer circumferential side of the cam ring; a metering orifice that is provided in
a discharge passage; a control valve that introduces control pressure to the first
fluid pressure chamber in accordance with movement of a spool that slides in accordance
with a differential pressure between upstream and downstream of the metering orifice;
and a cam spring that always biases the cam ring towards the first fluid pressure
chamber side from the second fluid pressure chamber. The cam ring is provided so as
to be movable between a maximum-eccentric position in which the amount of eccentricity
is maximized when the cam ring is moved towards the first fluid pressure chamber side
and a minimum-eccentric position in which the amount of eccentricity is minimized.
SUMMARY OF INVENTION
[0004] In the above-described conventional technique, while the control pressure is introduced
to the first fluid pressure chamber from the control valve, suction pressure is always
introduced to the second fluid pressure chamber. Therefore, when the cam ring is moved
in the direction in which the amount of eccentricity is reduced, the cam ring is moved
by the control pressure introduced to the first fluid pressure chamber. However, when
the cam ring is moved in the direction in which the amount of eccentricity is increased,
the cam ring is moved by biasing force exerted by the cam spring. Thus, there is a
risk in that, when the cam ring is moved in the direction in which the amount of eccentricity
is increased, the movement of the cam ring may be delayed, causing a follow-up delay.
[0005] The present invention has been conceived in light of such technical problems, and
an object thereof is to provide a variable displacement vane pump capable of preventing
the follow-up delay of a cam ring.
[0006] According to one aspect of the present invention, a variable displacement vane pump
includes: a rotor that is linked to a driving shaft; a plurality of vanes provided
so as to be movable in a reciprocating manner in the radial direction with respect
to the rotor; a cam ring in which tip-end portions of the vanes are in sliding contact
with a cam face on an inner circumference of the cam ring with rotation of the rotor
arranged in the cam ring, the cam ring being capable of being made eccentric with
respect to the rotor; pump chambers that are defined between the rotor and the cam
ring by being partitioned by the plurality of vanes; a first fluid pressure chamber
and a second fluid pressure chamber that are defined in an accommodating space on
an outer circumferential side of the cam ring; a biasing member configured to always
bias the cam ring in a direction in which an amount of eccentricity is increased;
a restrictor configured to impart resistance to flow of working fluid discharged from
the pump chambers; a control valve configured to reduce the amount of eccentricity
of the cam ring by introducing the working fluid that has been discharged from the
pump chambers to the first fluid pressure chamber as a differential pressure between
upstream and downstream of the restrictor is increased, the control valve being configured
to increase the amount of eccentricity of the cam ring by discharging the working
fluid in the first fluid pressure chamber as the differential pressure between upstream
and downstream of the restrictor is reduced; a suction passage configured to guide
the working fluid to be sucked into the pump chambers, the suction passage being configured
to always communicate with the second fluid pressure chamber; and a guiding passage
configured to allow communication between the control valve and the second fluid pressure
chamber, the guiding passage being configured to guide the working fluid, which is
discharged from the first fluid pressure chamber to the control valve, to the second
fluid pressure chamber.
BRIEF DESCRIPTION OF DRAWINGS
[0007]
[FIG. 1] FIG. 1 is a sectional view showing a cross section perpendicular to a driving
shaft in a variable displacement vane pump according to a first embodiment of the
present invention.
[FIG. 2] FIG. 2 is a sectional view showing a cross section parallel to the driving
shaft in the variable displacement vane pump according to the first embodiment of
the present invention.
[FIG. 3] FIG. 3 is a hydraulic circuit diagram of the variable displacement vane pump
according to the first embodiment of the present invention.
[FIG. 4] FIG. 4 is a hydraulic circuit diagram of the variable displacement vane pump
according to the first embodiment of the present invention and shows a state in which
an amount of eccentricity of a cam ring with respect to a rotor is at a maximum level.
[FIG. 5] FIG. 5 is a hydraulic circuit diagram of the variable displacement vane pump
according to the first embodiment of the present invention and shows a state in which
the amount of eccentricity of the cam ring with respect to the rotor is at an intermediate
level.
[FIG. 6] FIG. 6 is a hydraulic circuit diagram of the variable displacement vane pump
according to the first embodiment of the present invention and shows a state in which
the amount of eccentricity of the cam ring with respect to the rotor is at a minimum
level.
[FIG. 7] FIG. 7 is a sectional view showing a cross section perpendicular to a driving
shaft in a variable displacement vane pump according to a second embodiment of the
present invention.
[FIG. 8] FIG. 8 is a sectional view showing a cross section parallel to the driving
shaft in the variable displacement vane pump according to the second embodiment of
the present invention.
DESCRIPTION OF EMBODIMENTS
[0008] The following describes embodiments of the present invention with reference to the
drawings.
<First Embodiment>
[0009] A variable displacement vane pump 100 according to a first embodiment of the present
invention will be described with reference to FIGs. 1 to 3.
[0010] The variable displacement vane pump 100 (hereinafter, simply referred to as "the
vane pump 100") is used as a hydraulic pressure source for a hydraulic apparatus mounted
on a vehicle, such as, for example, a power steering apparatus, a continuously variable
transmission, and the like.
[0011] As shown in FIG. 1, in the vane pump 100, motive force from a driving source (not
shown) is transmitted to a driving shaft 1, and a rotor 2 that is linked to the driving
shaft 1 is rotated. In FIGs. 1 and 3, the rotor 2 is rotated in the counterclockwise
direction as indicated by an arrow.
[0012] The vane pump 100 includes a plurality of vanes 3 that are provided so as to be movable
in a reciprocating manner in the radial direction with respect to the rotor 2 and
a cam ring 4 in which tip-end portions of the vanes 3 are in sliding contact with
a cam face 4a, forming an inner circumference of the cam ring 4, by rotation of the
rotor 2 arranged in the cam ring 4. The cam ring 4 is can be made eccentric with respect
to the center of the rotor 2.
[0013] As shown in FIG. 2, the driving shaft 1 is rotatably supported by a pump body 6 via
a bush 5. A pump accommodating recessed portion 6a serving as a recessed portion for
accommodating the cam ring 4 is formed in the pump body 6. In an end portion of the
pump body 6, a seal 7 is provided for preventing leakage of lubricating oil between
an outer circumference of the driving shaft 1 and an inner circumference of the bush
5.
[0014] A side plate 8 that comes into contact with first side portions of the rotor 2 and
the cam ring 4 is arranged on a bottom surface 6b of the pump accommodating recessed
portion 6a. An opening portion of the pump accommodating recessed portion 6a is sealed
with a pump cover 9 that comes into contact with second side portions of the rotor
2 and the cam ring 4. The pump cover 9 is fastened to the pump body 6 by bolts 10
(see FIG. 1).
[0015] As described above, the pump cover 9 and the side plate 8 are arranged so as to sandwich
the rotor 2 and the cam ring 4 at both side surfaces thereof. With such a configuration,
pump chambers 11 are defined between the rotor 2 and the cam ring 4 by being partitioned
by the respective vanes 3.
[0016] As shown in FIGs. 1 and 3, the cam ring 4 is an annular member and has a suction
region in which volumes of the pump chambers 11 partitioned by and between the respective
vanes 3 are expanded by the rotation of the rotor 2 and a discharge region in which
the volumes of the pump chambers 11 partitioned by and between the respective vanes
3 are contracted by the rotation of the rotor 2. The pump chambers 11 suck working
oil serving as working fluid in the suction region and discharge the working oil in
the discharge region. In FIG. 1, an upper part of the cam ring 4 corresponds to the
suction region and a lower part corresponds to the discharge region.
[0017] An annular adapter ring 12 is fitted to an inner circumferential surface of the pump
accommodating recessed portion 6a so as to surround the cam ring 4. The adapter ring
12 is sandwiched by the pump cover 9 and the side plate 8 at both side surfaces thereof
in the same way as the rotor 2 and the cam ring 4.
[0018] A support plate 13 that extends in parallel with the driving shaft 1 is supported
on an inner circumferential surface of the adapter ring 12. The cam ring 4 is supported
by the support plate 13, and the cam ring 4 swings around inside the adapter ring
12 with the support plate 13 as a supporting point.
[0019] A groove 12a extending in parallel with the driving shaft 1 is formed at an axisymmetric
position to the support plate 13 in the inner circumferential surface of the adapter
ring 12. A seal member 14, which is in sliding contact with the outer circumferential
surface of the cam ring 4 when the cam ring 4 swings around, is fitted in the groove
12a in a state in which an elastic member 15 is compressed.
[0020] As described above, in a space between the outer circumferential surface of the cam
ring 4 and the inner circumferential surface of the adapter ring 12, which is an accommodating
space on the outer circumference of the cam ring 4, a first hydraulic chamber 16 serving
as a first fluid pressure chamber and a second hydraulic chamber 17 serving as a second
fluid pressure chamber are defined by the support plate 13 and the seal member 14.
[0021] As shown in FIG. 1, a cam spring 18 serving as a biasing member is provided on the
second hydraulic chamber 17 side of the outer circumferential surface of the cam ring
4. The cam spring 18 is fitted to a spring plug 19 that is screwed into the pump body
6 from the side and always biases the cam ring 4 towards the first hydraulic chamber
16 side via a through hole 12b formed in the adapter ring 12. In other words, the
cam ring 4 is always biased by the cam spring 18 in the direction in which an amount
of eccentricity is increased.
[0022] The cam ring 4 swings around with the support plate 13 as the supporting point in
such a manner that a differential pressure of the working oil between the first hydraulic
chamber 16 and the second hydraulic chamber 17, biasing force exerted by the cam spring
18, and the internal pressure of the cam ring 4 are balanced. As the cam ring 4 swings
around with the support plate 13 as the supporting point, the amount of eccentricity
of the cam ring 4 with respect to the rotor 2 is changed. As the amount of eccentricity
of the cam ring 4 is changed, a pump displacement volume per rotation of the rotor
2 is changed.
[0023] When the pressure in the first hydraulic chamber 16 is increased, the amount of eccentricity
of the cam ring 4 with respect to the rotor 2 is reduced. In this case, the pump displacement
volume per rotation of the rotor 2 is reduced. In contrast, when the pressure in the
first hydraulic chamber 16 is reduced, the amount of eccentricity of the cam ring
4 with respect to the rotor 2 is increased. In this case, the pump displacement volume
per rotation of the rotor 2 is increased. As described above, in the vane pump 100,
the pump displacement volume is changed in accordance with the amount of eccentricity
of the cam ring 4 with respect to the rotor 2.
[0024] The pump cover 9 is provided with a suction port 20 having an arc-shaped opening
so as to correspond to the suction region of the pump chambers 11. In addition, the
side plate 8 is provided with a discharge port 21 having an arc-shaped opening so
as to correspond to the discharge region of the pump chambers 11.
[0025] As shown in FIG. 2, the suction port 20 is formed so as to communicate with a suction
passage 22 formed in the pump cover 9 and guides the working oil in the suction passage
22 to the suction region of the pump chambers 11. The discharge port 21 is formed
so as to communicate with a high-pressure chamber 23 formed in the pump body 6 and
guides the working oil discharged from the discharge region of the pump chambers 11
to the high-pressure chamber 23.
[0026] The high-pressure chamber 23 is defined by closing a groove portion 6c, which is
formed so as to open at the bottom surface 6b of the pump accommodating recessed portion
6a, with the side plate 8. The working oil in the high-pressure chamber 23 is guided
to an external hydraulic apparatus of the vane pump 100 through a discharge passage
24 (see FIG. 3) formed in the pump body 6.
[0027] The pump body 6 is provided with a low-pressure chamber 25, serving as a first guiding
passage, that is formed at a position corresponding to the suction region of the pump
chambers 11 on the bottom surface 6b of the pump accommodating recessed portion 6a.
The low-pressure chamber 25 is defined by closing a groove portion 6d, which is formed
so as to open at a position corresponding to the suction region of the pump chambers
11, with the side plate 8. The low-pressure chamber 25 is formed in a straight line
parallel to the driving shaft 1, and its back-most end portion communicates with a
boundary between the bush 5 and the seal 7. The low-pressure chamber 25 is always
connected to the second hydraulic chamber 17, and the working oil that has leaked
out between the outer circumference of the driving shaft 1 and the inner circumference
of the bush 5 is recovered and returned to the pump chambers 11 in the suction region.
[0028] As shown in FIGs. 1 and 2, the pump body 6 is provided with a valve accommodating
hole 26 that is formed in the direction perpendicular to the axial direction of the
driving shaft 1. In the valve accommodating hole 26, a control valve 27 that controls
the working oil pressures in the first hydraulic chamber 16 and the second hydraulic
chamber 17 is accommodated. The valve accommodating hole 26 is sealed by a plug 28.
[0029] The control valve 27 includes a spool 29 that is slidably inserted into the valve
accommodating hole 26, a first pilot chamber 30 that faces one end of the spool 29,
a second pilot chamber 31 that faces the other end of the spool 29, and a return spring
32 that is accommodated in the second pilot chamber 31 and biases the spool 29 in
the direction in which the volume of the second pilot chamber 31 is expanded.
[0030] The spool 29 includes a first land portion 29a and a second land portion 29b that
slide along an inner circumferential surface of the valve accommodating hole 26, an
annular groove 29c that is formed between the first land portion 29a and the second
land portion 29b, a first rod portion 29d that is connected to the first land portion
29a and extends within the first pilot chamber 30, and a second rod portion 29e that
is connected to the second land portion 29b and extends within the second pilot chamber
31.
[0031] The first rod portion 29d comes into contact with the plug 28 when the spool 29 is
moved in the direction in which the volume of the first pilot chamber 30 is contracted.
When the spool 29 is moved in the direction in which the volume of the second pilot
chamber 31 is contracted, the second rod portion 29e comes into contact with an end
surface of the valve accommodating hole 26 on the opposite side from the plug 28.
The return spring 32 surrounds the second rod portion 29e and is received in the second
pilot chamber 31.
[0032] As shown in FIG. 3, a first passage 35 and a second passage 36, which serves as a
guiding passage, that communicate with the first hydraulic chamber 16 and the second
hydraulic chamber 17, respectively; a first pressure guiding passage 38 that guides
to the first pilot chamber 30 the working oil that has been discharged from the high-pressure
chamber 23 to the upstream side of an orifice 37 serving as a restrictor; and a second
pressure guiding passage 39 that guides to the second pilot chamber 31 the working
oil that has been discharged from the high-pressure chamber 23 to the downstream side
of the orifice 37 are connected to the control valve 27. A drain passage 40 that is
always in communication with the suction passage 22 is connected to the second hydraulic
chamber 17.
[0033] The first passage 35 and the second passage 36 are formed so as to open at the valve
accommodating hole 26 and to open at the first hydraulic chamber 16 and the second
hydraulic chamber 17, respectively, by penetrating through the adapter ring 12.
[0034] The spool 29 slides to a position at which the thrust force exerted by the differential
pressure between the first pilot chamber 30 and the second pilot chamber 31, which
face the respective ends of the spool 29, is balanced with the biasing force exerted
by the return spring 32. The first passage 35 is opened/closed by the first land portion
29a, and the working oil in the first hydraulic chamber 16 is supplied/discharged
depending on the position of the spool 29. The second passage 36 always opens to the
annular groove 29c regardless of the position of the spool 29.
[0035] When the biasing force exerted by the return spring 32 is greater than the thrust
force exerted by the differential pressure between the first pilot chamber 30 and
the second pilot chamber 31, a state in which the return spring 32 is elongated is
achieved. In this state, as shown in FIGs. 1 and 3, the first passage 35 and the second
passage 36 open at the annular groove 29c. With such a configuration, the communication
between the first hydraulic chamber 16 and the first pilot chamber 30 is shut off.
[0036] Here, a state in which the first hydraulic chamber 16 communicates with the drain
passage 40 through the first passage 35, the annular groove 29c, the second passage
36, and the second hydraulic chamber 17 is achieved. Because the cam ring 4 is always
biased by the cam spring 18 in the direction in which the amount of eccentricity is
increased, the amount of eccentricity of the cam ring 4 with respect to the rotor
2 is maximized.
[0037] In contrast, when the thrust force exerted by the differential pressure between the
first pilot chamber 30 and the second pilot chamber 31 is greater than the biasing
force exerted by the return spring 32, the spool 29 is moved against the biasing force
exerted by the return spring 32. In this case, the first passage 35 is shifted into
an open state, communicates with the first pilot chamber 30, and communicates with
the first pressure guiding passage 38 through the first pilot chamber 30. In addition,
the second passage 36 is held in the open state and communicates with the annular
groove 29c. With such a configuration, the first hydraulic chamber 16 communicates
with the high-pressure chamber 23. Because the second hydraulic chamber 17 communicates
with the suction passage 22 through the drain passage 40, as the pressure in the first
hydraulic chamber 16 is increased, the amount of eccentricity of the cam ring 4 is
reduced. In other words, when the pressure in the first hydraulic chamber 16 is increased
and the force received by the cam ring 4 from the first hydraulic chamber 16 exceeds
the sum of the force received by the cam ring 4 from the cam spring 18 and the force
received by the cam ring 4 from the internal pressure of the cam ring 4, the cam ring
4 is moved in the direction in which the amount of eccentricity with respect to the
rotor 2 is reduced.
[0038] As described above, when the thrust force exerted by the differential pressure between
the first pilot chamber 30 and the second pilot chamber 31 exceeds the biasing force
exerted by the return spring 32, the spool 29 of the control valve 27 is moved so
as to compress the return spring 32.
[0039] The working oil at the upstream side and the downstream side of the orifice 37 serving
as the restrictor, which is interposed in the discharge passage 24 and imparts resistance
to the flow of the working oil, is respectively guided to the first pilot chamber
30 and the second pilot chamber 31. In other words, the working oil in the high-pressure
chamber 23 is guided directly to the first pilot chamber 30 through the first pressure
guiding passage 38 without passing through the orifice 37, and is also guided to the
second pilot chamber 31 through the orifice 37. Therefore, the spool 29 is moved in
accordance with the differential pressure between upstream and downstream of the orifice
37.
[0040] Next, operation of the vane pump 100 will be described with reference to FIGs. 4
to 6. FIGs. 4 to 6 are hydraulic circuit diagrams of the vane pump 100 and respectively
show states in which the amount of eccentricity of the cam ring 4 with respect to
the rotor 2 is at maximum, intermediate, and minimum levels.
[0041] As the rotor 2 is rotated by motive force transmitted from the driving source to
the driving shaft 1, the working oil is sucked from the suction passage 22 through
the suction port 20 into the pump chambers 11 whose spaces are expanded between the
respective vanes 3 with the rotation of the rotor 2. In addition, the working oil
is discharged through the discharge port 21 to the high-pressure chamber 23 from the
pump chambers 11 whose spaces are contracted between the respective vanes 3. The working
oil that has been discharged to the high-pressure chamber 23 is supplied to the hydraulic
apparatus through the discharge passage 24.
[0042] When the working oil passes through the discharge passage 24, the differential pressure
is generated between upstream and downstream of the orifice 37, which is interposed
in the discharge passage 24, and the pressures at the upstream and downstream sides
of the orifice 37 are guided to the first pilot chamber 30 and the second pilot chamber
31, respectively. The spool 29 of the control valve 27 slides to the position at which
the thrust force exerted by the differential pressure between the first pilot chamber
30 and the second pilot chamber 31 is balanced with the biasing force exerted by the
return spring 32.
[0043] Because the rotation speed of the rotor 2 is low and a pump discharge flow amount
is small at a pump starting time at which the rotation speed of the rotor 2 is equal
to or lower than a predetermined rotation speed, the differential pressure between
upstream and downstream of the orifice 37 is small, and the thrust force exerted by
the differential pressure between the first pilot chamber 30 and the second pilot
chamber 31 is small. Therefore, the biasing force exerted by the return spring 32
is greater than the thrust force exerted by the differential pressure between the
first pilot chamber 30 and the second pilot chamber 31, and the return spring 32 is
in an elongated state.
[0044] In this case, as shown in FIG. 4, because the first passage 35 and the second passage
36 open at the annular groove 29c, the first hydraulic chamber 16 communicates with
the drain passage 40 through the annular groove 29c and the second hydraulic chamber
17. In this state, because the hydraulic pressure that makes the cam ring 4 swing
around does not act on the first hydraulic chamber 16 and the second hydraulic chamber
17, the cam ring 4 is biased by the cam spring 18 in the direction in which the amount
of eccentricity with respect to the rotor 2 is increased. With such a configuration,
the amount of eccentricity of the cam ring 4 with respect to the rotor 2 is maximized.
[0045] In a region in which the rotation speed of the rotor 2 is equal to or lower than
the predetermined rotation speed, the amount of eccentricity of the cam ring 4 with
respect to the rotor 2 is maximized to cause the pump displacement volume per rotation
of the rotor 2 to be maximized, and the pump discharge flow amount of the vane pump
100 becomes the flow amount substantially in proportion to the rotation speed of the
rotor 2. Therefore, even when the rotation speed of the rotor 2 is low, it is possible
to supply the working oil to the hydraulic apparatus at a sufficient flow amount.
[0046] As the rotation speed of the rotor 2 is increased, the differential pressure between
upstream and downstream of the orifice 37 is increased, and thereby, the thrust force
exerted by the differential pressure between the first pilot chamber 30 and the second
pilot chamber 31 is balanced with or becomes slightly greater than the biasing force
exerted by the return spring 32. With such a configuration, the spool 29 starts to
move against the biasing force exerted by the return spring 32.
[0047] Furthermore, when the rotation speed of the rotor 2 is increased and reaches the
predetermined rotation speed, as shown in FIG. 5, by the movement of the spool 29,
the first passage 35 is shifted into the open state and communicates with the first
pilot chamber 30 and the annular groove 29c, and the second passage 36 is held in
the open state. With such a configuration, because the first hydraulic chamber 16
communicates with the high-pressure chamber 23 and the second hydraulic chamber 17
communicates with the drain passage 40, as the pressure in the first hydraulic chamber
16 is increased, the cam ring 4 starts to move in the direction in which the amount
of eccentricity with respect to the rotor 2 is reduced.
[0048] In a region in which the rotation speed of the rotor 2 exceeds the predetermined
rotation speed, the pump discharge flow amount of the vane pump 100 becomes substantially
constant. In other words, when the first passage 35 and the second passage 36 are
shifted into the open state and the cam ring 4 starts to move in the direction in
which the amount of eccentricity with respect to the rotor 2 is reduced, the pump
discharge flow amount is reduced and the differential pressure between upstream and
downstream of the orifice 37 is reduced. With such a configuration, the return spring
32 is elongated, and the first passage 35 is closed again. When the first passage
35 is closed, the cam ring 4 is moved in the direction in which the amount of eccentricity
with respect to the rotor 2 is increased and the pump discharge flow amount is increased.
When the pump discharge flow amount is increased, the differential pressure between
upstream and downstream of the orifice 37 is increased, and the spool 29 is moved
so as to compress the return spring 32, and thereby, the first passage 35 and the
second passage 36 are again shifted into the open state. As described above, because
a control is performed such that the first passage 35 is opened/closed to make the
differential pressure between upstream and downstream of the orifice 37 constant,
the pump discharge flow amount becomes substantially constant.
[0049] In a region in which the rotation speed of the rotor 2 exceeds the predetermined
rotation speed, as the rotation speed of the rotor 2 is increased, because the amount
of movement of the spool 29 while compressing the return spring 32 is increased and
an opening degree of the first passage 35 is increased, the amount of eccentricity
of the cam ring 4 with respect to the rotor 2 is reduced gradually, causing a gradual
reduction in the pump displacement volume per rotation of the rotor 2.
[0050] When the rotation speed of the rotor 2 is further increased, as shown in FIG. 6,
the amount of eccentricity of the cam ring 4 with respect to the rotor 2 is minimized,
and the pump displacement volume per rotation of the rotor 2 is minimized.
[0051] Even in a state shown in FIG. 6 in which the amount of eccentricity of the cam ring
4 with respect to the rotor 2 is minimized, because the amount of eccentricity does
not become zero, the vane pump 100 discharges the working oil at the minimum discharge
capacity.
[0052] As described above, the spool 29 is moved in accordance with the change in the rotation
speed of the rotor 2 and the first passage 35 is opened/closed by the movement of
the spool 29, and thereby, the pump discharge flow amount is adjusted. More specifically,
at the pump starting time at which the rotation speed of the rotor 2 is equal to or
lower than the predetermined rotation speed, because the first passage 35 is closed
by the spool 29, the amount of eccentricity of the cam ring 4 with respect to the
rotor 2 is maximized, and the pump discharge flow amount is increased along with the
increase in the rotation speed of the rotor 2. In addition, when the rotation speed
of the rotor 2 exceeds the predetermined rotation speed, because a control is performed
such that the opening degree of the first passage 35 is adjusted by the movement of
the spool 29 and the differential pressure between upstream and downstream of the
orifice 37 becomes constant, the pump discharge flow amount becomes substantially
constant.
[0053] Here, when the rotation speed of the rotor 2 is reduced from the region in which
the rotation speed of the rotor 2 is greater than the predetermined rotation speed,
the thrust force exerted by the differential pressure between the first pilot chamber
30 and the second pilot chamber 31 is reduced, and the spool 29 slides in the direction
in which the return spring 32 is elongated. When the communication between the first
passage 35 and the first pilot chamber 30 is shut off by the slide of the spool 29,
the high-pressure working oil that has been guided to the first hydraulic chamber
16 is discharged to the annular groove 29c, and then, supplied to the second hydraulic
chamber 17 through the second passage 36. The working oil in the second hydraulic
chamber 17 is subsequently returned to the suction passage 22 through the drain passage
40 (see FIGs. 4 and 5).
[0054] With such a configuration, when the amount of eccentricity of the cam ring 4 is increased
as the rotation speed of the rotor 2 is reduced, the cam ring 4 receives the force
exerted, in the direction in which the amount of eccentricity is increased, by the
working oil pressure that has been guided from the first hydraulic chamber 16 to the
second hydraulic chamber 17 through the annular groove 29c.
[0055] Because the working oil pressure that has been guided to the second hydraulic chamber
17 is greater than the working oil pressure in the suction passage 22 that always
communicates with the second hydraulic chamber 17 through the drain passage 40, it
is possible to make the cam ring 4 eccentric with higher responsiveness compared to
a case in which the amount of eccentricity of the cam ring 4 is increased only by
the biasing force exerted by the cam spring 18 and the force exerted by the internal
pressure of the cam ring 4. Thus, it is possible to prevent a follow-up delay of the
cam ring 4 when the rotation speed of the rotor 2 is reduced.
[0056] With the above-mentioned first embodiment, the following effects can be afforded.
[0057] When the working oil in the first hydraulic chamber 16 is discharged to increase
the amount of eccentricity of the cam ring 4 as the differential pressure between
upstream and downstream of the orifice 37 is reduced, the working oil that has been
discharged from the first hydraulic chamber 16 to the annular groove 29c is guided
to the second hydraulic chamber 17 through the second passage 36.
[0058] With such a configuration, when the rotation speed of the rotor 2 is reduced and
the amount of eccentricity of the cam ring 4 is increased, in addition to the biasing
force exerted by the cam spring 18, the force exerted by the working oil pressure
in the second hydraulic chamber 17 that has been guided from the first hydraulic chamber
16 through the annular groove 29c acts on the cam ring 4. Therefore, it is possible
to prevent the follow-up delay of the cam ring 4.
[0059] Furthermore, because the second passage 36 opens at the valve accommodating hole
26 and opens at the inner circumferential surface of the adapter ring 12 in the second
hydraulic chamber 17 by penetrating through the adapter ring 12, it is possible to
shorten a distance between the control valve 27, which is arranged radially outside
of the adapter ring 12 so as to be adjacent to the adapter ring 12, and the second
hydraulic chamber 17.
[0060] With such a configuration, when the rotation speed of the rotor 2 is reduced and
the amount of eccentricity of the cam ring 4 is increased, it is possible to reduce
the time required for the working oil pressure, which has been discharged to the annular
groove 29c from the first hydraulic chamber 16, to be supplied to the second hydraulic
chamber 17. Thus, it is possible to improve a startup of the working oil pressure
in the second hydraulic chamber 17 that biases the cam ring 4 in the direction in
which the amount of eccentricity is increased and prevent the follow-up delay of the
cam ring 4 more reliably.
[0061] <Second Embodiment>
[0062] A variable displacement vane pump 200 according to a second embodiment of the present
invention will be described with reference to FIGs. 7 and 8.
[0063] The variable displacement vane pump 200 in this embodiment differs from that in the
first embodiment in a configuration of a second passage 136, and other points are
the same as those in the first embodiment. Therefore, components that are the same
as those in the first embodiment are assigned the same reference signs, and descriptions
thereof shall be omitted.
[0064] The second passage 36 is formed so as to open at the valve accommodating hole 26
and to open at the second hydraulic chamber 17 by penetrating through the adapter
ring 12 in the first embodiment, whereas in this embodiment, the second passage 136
serving as a guiding passage is constituted of the low-pressure chamber 25 and a straight
passage 101, which serves as a second guiding passage that connects the back-anost
end portion of the low-pressure chamber 25 and the annular groove 29c of the control
valve 27 in a straight line.
[0065] With such a configuration, the working oil that has been discharged from the first
hydraulic chamber 16 to the annular groove 29c of the control valve 27 is guided to
the second hydraulic chamber 17 through the straight passage 101 and the low-pressure
chamber 25.
[0066] With the above-mentioned second embodiment, the following effects can be afforded.
[0067] Because the second passage 136 opens at the bottom surface 6b of the pump accommodating
recessed portion 6a in the suction region in which the volumes of the pump chambers
11 are expanded, a through hole needs not be provided in the adapter ring 12, which
defines an accommodating space on the outer circumferential side of the cam ring 4.
Thus, there is no need to provide the through hole in the adapter ring 12, and in
addition to that, there is no need to perform alignment of the through hole of the
adapter ring 12 and a hole formed in the pump body 6 so as to communicate with the
annular groove 29c of the control valve 27. Therefore, it is possible to prevent the
follow-up delay of the cam ring 4 while reducing the manufacturing cost.
[0068] Furthermore, because the second passage 136 is constituted of the low-pressure chamber
25 that is formed in a straight line parallel to the driving shaft 1 and the straight
passage 101 that connects the back-most end portion of the low-pressure chamber 25
and the annular groove 29c of the control valve 27 in a straight line, it is possible
to form the second passage 136 in the pump body 6 only by providing two straight passages.
Therefore, it is possible to improve the ease of processing for providing the second
passage 136 and to reduce the manufacturing cost.
[0069] Furthermore, because a part of the second passage 136 is constituted of the low-pressure
chamber 25, it is possible to form the second passage 136 only by providing the straight
passage 101. Therefore, it is possible to further improve the ease of processing for
providing the second passage 136 and to further reduce the manufacturing cost.
[0070] Embodiments of this invention were described above, but the above embodiments are
merely examples of applications of this invention, and the technical scope of this
invention is not limited to the specific constitutions of the above embodiments.
[0071] For example, in the above-mentioned embodiment, although a case in which the working
oil is used as the working fluid has been described, other fluids than the working
oil, such as water, aqueous alternative fluid, and so forth, may be used.
[0072] Furthermore, in the above-mentioned embodiment, although a case in which the low-pressure
chamber 25 and the straight passage 101 are both formed in a straight line is described,
the configuration is not limited thereto, and at least one of the low-pressure chamber
25 and the straight passage 101 may be formed to have a curved shape or a shape having
a bent portion at an intermediate position.
[0073] This application claims priority based on Japanese Patent Application No.
2014-239200 filed with the Japan Patent Office on November 26, 2014, the entire contents of which
are incorporated into this specification.