BACKGROUND OF THE INVENTION
Field of the Invention:
[0001] The present invention relates to a hydraulic servo device for converting a small-torque
angular displacement into a large-load linear displacement, and more particularly
to a hydraulic servo device for use in controlling the operation of a scoop tube as
a speed control mechanism for a variable-speed fluid coupling.
Description of the Prior Art:
[0002] Figure 11 shows an actuator for a water feeding device for supplying water to a high-capacity
boiler. As shown in Figure 11, the rotation of an input shaft 121 is accelerated and
transmitted through a large-diameter gear 122 and a small-diameter gear 124 to a drive
shaft 123, from which the rotation is transmitted through a fluid coupling C to a
driven shaft 125. The rotation is then accelerated and transmitted from the driven
shaft 125 through a large-diameter gear 131 and a small-diameter gear 133 to an output
shaft 132. The fluid coupling C comprises an impeller 126 and an impeller casing 128
which are mounted on the drive shaft 123, and a runner 127 mounted on the driven shaft
125. When working oil is introduced into a working chamber defined in the impeller
casing 128, the impeller 126 and the runner 127 interlockingly rotate due to the viscosity
of the working oil so as to transmit the rotation from the drive shaft 123 to the
driven shaft 125.
[0003] A scoop tube 130 for regulating the rate of the working oil is disposed in the working
chamber. The torque transmitted by the fluid coupling C can be controlled by moving
the scoop tube 130 into and out of the working chamber. The fluid coupling C, which
is of a simple structure, is capable of continuously changing the rotational speed
of the load side shaft (output shaft) from a minimum level to a maximum level.
[0004] The scoop tube needs to resist against forces applied by the working oil thereby
to be positioned accurately. One actuating device for the scoop tube comprises, for
example, a hydraulic servo device for amplifying and transmitting a displacement produced
under a small force by an electric actuator, as disclosed in Japanese laid-open patent
publication No. 7-208499, for example. The disclosed hydraulic servo device has a
piston slidably mounted on a pilot shaft disposed in a cylinder, with oil passages
defined in a surface of the pilot shaft and inside the piston. A rotation of the pilot
shaft is converted into a displacement of the piston, which is outputted from the
hydraulic servo device. The scoop tube is positionally controlled under feedback control
based on a signal from a displacement sensor located in a predetermined position.
[0005] It is necessary that the above hydraulic servo device be reduced in size for an overall
balance, and to meet such a requirement, the pilot shaft needs to be reduced in diameter.
If the diameter of the pilot shaft is reduced, however, the width of the oil passage
defined as a groove in the surface of the pilot shaft is also reduced. When the rotational
speed of the pilot shaft is increased, the oil passage in the surface of the pilot
shaft is displaced out of alignment in the oil passage in the piston, tending to cause
a control failure. Consequently, the control response of the hydraulic servo device
is limited.
SUMMARY OF THE INVENTION
[0006] It is therefore an object of the present invention to provide a hydraulic servo device
which will keep oil passages in alignment with each other even though its pilot shaft
is of a small diameter, and which has a sufficient control response even though the
overall size is relatively small.
[0007] According to an aspect of the present invention, there is provided a hydraulic servo
device comprising a cylinder, a pilot shaft disposed angularly movably and extending
axially in the cylinder, the pilot shaft having a pair of communication passages defined
in an outer circumferential surface thereof, a piston movably mounted on the pilot
shaft for axial movement in the cylinder, the piston having a pair of oil passages
defined therein, and an actuator for angularly moving the pilot shaft about its own
axis to bring at least one of the communication passages into communication with at
least one of the oil passages to apply a fluid under pressure to the piston for axially
moving the piston in the cylinder. The communication passages and the oil passages
are relatively small in diameter and width, and can be held in communication with
each other in a relatively large angular range of the pilot shaft, so that the hydraulic
servo device can be controlled with a high response.
[0008] The communication passages and the oil passages are relatively positioned such that
the communication passages and the oil passages are brought into communication with
each other in different angular ranges of the pilot shaft.
[0009] Each of the communication passages is angularly nonlinear in a configuration thereof.
[0010] The oil passages include an oil supply passage for supplying a working oil under
pressure and an oil drain passage connected to a drain.
[0011] According to another aspect of the present invention, there is provided a hydraulic
servo device comprising a cylinder, a pilot shaft disposed angularly movably and extending
axially in the cylinder, the pilot shaft having a communication passage defined in
an outer circumferential surface thereof, a piston movably mounted on the pilot shaft
for axial movement in the cylinder, the piston having an oil passage defined therein,
an actuator for angularly moving the pilot shaft about its own axis to bring the communication
passage into communication with the oil passage to apply a fluid under pressure to
the piston for axially moving the piston in the cylinder, the cylinder having an interior
space compartmented by the piston into a first space communicating with a pressurized
oil hole and a second space which can selectively be brought into and out of communication
with the oil passage by the communication passage, and an air bleeder pipe connected
to an upper region of the cylinder in communication with the second space. Highly
compressible air which has been trapped in the second space can be discharged through
the air bleeder pipe for thereby allowing the hydraulic servo device to have a high
response.
[0012] The air bleeder pipe has an orifice and vented to the atmosphere therethrough.
[0013] The air bleeder pipe has a check valve and vented to the atmosphere therethrough.
[0014] According to still another aspect of the present invention, there is provided a hydraulic
servo device comprising a cylinder, a pilot shaft disposed angularly movably and extending
axially in the cylinder, the pilot shaft having a communication passage defined in
an outer circumferential surface thereof, a piston movably mounted on the pilot shaft
for axial movement in the cylinder, the piston having an oil passage defined therein,
and an actuator for angularly moving the pilot shaft about its own axis to bring the
communication passage into communication with the oil passage to apply a fluid under
pressure to the piston for axially moving the piston in the cylinder, the cylinder
having an interior space compartmented by the piston into a first space communicating
with a pressurized oil hole and a second space which can selectively be brought into
and out of communication with the oil passage by the communication passage, the cylinder
having a recess for collecting particles therein, the recess being defined in a lower
region of an inner cylindrical surface thereof respectively in the first space and/or
the second space. Since particles produced upon sliding movement of the piston against
the cylinder are collected in the recess, they are prevented from being caught between
the piston and the cylinder, so that the hydraulic servo device can operate stably.
[0015] The cylinder has a discharge hole defined in a cylindrical wall thereof for discharging
particles collected in the recess.
[0016] According to yet still another aspect of the present invention, there is provided
a hydraulic servo device comprising a cylinder, a pilot shaft disposed angularly movably
and extending axially in the cylinder, the pilot shaft having a communication passage
defined in an outer circumferential surface thereof, a piston movably mounted on the
pilot shaft for axial movement in the cylinder, the piston having an oil passage defined
therein, an actuator for angularly moving the pilot shaft about its own axis to bring
the communication passage into communication with the oil passage to apply a fluid
under pressure to the piston for axially moving the piston in the cylinder, the cylinder
having an interior space compartmented by the piston into a first space communicating
with a pressurized oil hole and a second space which can selectively be brought into
and out of communication with the oil passage by the communication passage, and an
oil reservoir disposed in covering relation to an end wall of the cylinder which defines
the first space.
[0017] According to a further aspect of the present invention, there is provided a hydraulic
servo device comprising a cylinder, a pilot shaft disposed angularly movably and extending
axially in the cylinder, the pilot shaft having a communication passage defined in
an outer circumferential surface thereof, a piston movably mounted on the pilot shaft
for axial movement in the cylinder, the piston having an oil passage defined therein,
and an actuator for angularly moving the pilot shaft about its own axis to bring the
communication passage into communication with the oil passage to apply a fluid under
pressure to the piston for axially moving the piston in the cylinder, the piston having
engaging means on an end face thereof for engaging a piston remover for pulling out
the piston from the cylinder. The piston can easily be removed from the cylinder by
the piston remover which is engaged by the engaging means on the piston. As a result,
the piston, the cylinder, and a scoop tube mounted on the piston can easily be inspected,
service, for maintenance, or can easily be replaced.
[0018] According to a still further aspect of the present invention, there is provided a
fluid coupling comprising an impeller and an impeller casing which are adapted to
be mounted on a drive shaft, the impeller casing defining a working chamber therein,
a runner adapted to be mounted on a driven shaft, a scoop tube disposed for movement
into and out of the working chamber for generating the rate of a working oil introduced
into the working chamber, and any of the hydraulic servo devices described above for
positionally controlling the scoop tube.
[0019] The above and other objects, features, and advantages of the present invention will
become apparent from the following description when taken in conjunction with the
accompanying drawings which illustrate preferred embodiments of the present invention
by way of example.
BRIEF DESCRIPTION OF THE DRAWINGS
[0020]
Figure 1 is a perspective view, partly cut away, of a hydraulic servo device according
to a first embodiment of the present invention;
Figure 2A is a transverse cross-sectional view showing a positional relationship between
an oil passage and a communication passage when a pilot shaft is in an angular position;
Figure 2B is a transverse cross-sectional view showing a positional relationship between
the oil passage and the communication passage when a pilot shaft is in another angular
position;
Figure 3A is a transverse cross-sectional view showing a positional relationship between
the oil passage and the communication passage when a pilot shaft is in still another
angular position;
Figure 3B is a transverse cross-sectional view showing a positional relationship between
an oil passage and a communication passage in a conventional hydraulic servo device;
Figure 4 is a diagram showing a two-dimensional shape of the communication passage;
Figure 5 is a graph showing angular ranges in which oil supply and drain passages
and communication passages communicate with each other;
Figure 6 is a longitudinal cross-sectional view of a hydraulic servo device according
to a second embodiment of the present invention;
Figure 7 is a longitudinal cross-sectional view of a hydraulic servo device according
to a third embodiment of the present invention;
Figure 8 is a longitudinal cross-sectional view of a hydraulic servo device according
to a fourth embodiment of the present invention;
Figure 9 is a longitudinal cross-sectional view of a hydraulic servo device according
to a fifth embodiment of the present invention;
Figure 10 is a longitudinal cross-sectional view of a hydraulic servo device according
to a sixth embodiment of the present invention; and
Figure 11 is a cross-sectional view of a fluid coupling for use in combination with
a hydraulic servo device.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0021] As shown in Figure 1, a hydraulic servo device according to a first embodiment of
the present invention, which is typically used as an actuating device for the scoop
tube of the fluid coupling shown in Figure 11, comprises a cylinder 10 as a pressure
casing, a pilot actuating device 12 mounted on a proximal end of the cylinder 10 and
connected to a controller (not shown), a pilot shaft 14 projecting from the pilot
actuating device 12 into the cylinder 10, and a piston 16 disposed in a space defined
between the cylinder 10 and the pilot shaft 14. The piston 16 is slidably movable
axially along the pilot shaft 14, but is prevented from rotating around the pilot
shaft 14. The piston 16 comprises a large-diameter portion 18 closer to the proximal
end of the cylinder 10 and a small-diameter portion 20 closer to the distal end of
the cylinder 10. The small-diameter portion 20 projects axially out of the cylinder
10 through a slide hole 24 that is defined in an end wall 22 on the distal end of
the cylinder 10. The small-diameter portion 20 supports on its projecting end an attachment
portion 26 for supporting the scoop tube that is to be actuated by the hydraulic servo
device.
[0022] The piston 16 compartments the space within the cylinder 10 into a first space 28
defined around the small-diameter portion 20 and a second space 30 defined in and
on the free end of the large-diameter portion 18. A pressurized oil passageway 32
is defined radially in the distal end of the cylinder 10 in communication with the
first space 28. The cylinder 10 has an annular step 34 on an inner cylindrical wall
thereof which serves as a stop for defining a stop position for the piston 16 on its
axial movement towards the distal end of the cylinder 10. With the cylinder 10 being
held in the stop position, the first space 28 is still maintained in the distal end
of the cylinder 10 while being kept in communication with the first space 28.
[0023] As also shown in Figure 2A, the small-diameter portion 20 of the piston 16 has an
axial central hole 36 defined therein which receives the pilot shaft 14 slidably therein,
and a pair of oil supply passages 38a, 38b defined radially therein near the large-diameter
portion 18 and extending from the first space 28 into the axial central hole 36. The
oil supply passages 38a, 38b are positioned substantially symmetrically with respect
to the central axis of the small-diameter portion 20. The small-diameter portion 20
also has a pair of oil drain passages 40a, 40b defined therein substantially symmetrically
with respect to a plane passing through the central axis of the small-diameter portion
20 parallel to the oil supply passages 38a, 38b. The oil drain passages 40a, 40b are
open at the attachment portion 26. The axial central hole 36 and the oil drain passages
40a, 40b are both connected to an external drain (not shown).
[0024] The pilot shaft 14 has a pair of communication passages 42a, 42b defined in an outer
circumferential surface thereof for providing communication between the oil supply
passages 38a, 38b and the second space 30 depending upon angular location of the pilot
shaft 14. The communication passages 42a, 42b are positioned substantially symmetrically
with respect to the central axis of the pilot shaft 14. Each of the communication
passages 42a, 42b extends substantially axially over a length which corresponds to
the stroke of the piston 16, and also extends helically circumferentially over a substantially
half the full circumference of the pilot shaft 14. In this embodiment, the oil supply
passages 38a, 38b and the oil drain passages 40a, 40b have a diameter equal to the
width of the communication passages 42a, 42b. In Figure 1, one of the oil supply passages
38a, 38b is shown as an oil supply passage 38, one of the oil drain passages 40a,
40b as an oil drain passage 40, and one of the communication passages 42a, 42b as
a communication passage 42.
[0025] The piston 16 has a pressure bearing area in the first space 28 which is represented
by the difference between the cross-sectional area of the large-diameter portion 18
and the cross-sectional area of the small-diameter portion 20. The piston 16 has a
pressure bearing area in the second space 30 which is represented by the difference
between the cross-sectional area of the large-diameter portion 18 and the cross-sectional
area of the pilot shaft 14. Therefore, the pressure bearing area of the piston 16
in the second space 30 is greater than the pressure bearing area of the piston 16
in the first space 28. When an identical working oil pressure acts in both the first
space 28 and the second space 30 from the pressurized oil passageway 32 when the communication
passages 42 communicates the oil supply passages 38 and the second space 30, the piston
16 moves axially towards the distal end of the cylinder 10, i.e., towards the pilot
actuating device 12. When a working oil pressure from the pressurized oil passageway
32 acts only in the first space 28 with the communication passages 42 held in communication
with the oil drain passages 40 and the second space 30, the piston 16 moves axially
towards the proximal end of the cylinder 10, i.e., towards the end wall 22.
[0026] As shown in Figure 4, each of the communication passages 42 is angularly nonlinear
in its configuration for thereby allowing the piston 16 to move axially through a
linear stroke in response to an angular displacement of the pilot shaft 14. The large-diameter
portion 18 of the piston 16 is hollow so that, even when the piston 16 is axially
displaced fully to the proximal end of the cylinder 10, the communication passages
42 are not covered by the piston 16.
[0027] As shown in Figures 2A, 2B and 3A, the oil supply passage 38a and the oil drain passage
40a adjacent thereto are spaced more closely from each other than the oil supply passage
38b and the oil drain passage 40b adjacent thereto are spaced from each other. This
angular positional relationship between these passages 38a, 40a and 38b, 40b ensures
that when the pilot shaft 14 is angularly moved about its own axis, the communication
passage 42a starts to overlap or communicate with the oil supply passage 38a or the
oil drain passage 40a earlier than the communication passage 42b starts to overlap
or communicate with the oil supply passage 38b or the oil drain passage 40b. Specifically,
as shown in Figure 5, the communication passage 42a overlaps or communicates with
the oil supply passage 38a or the oil drain passage 40a when the pilot shaft 14 is
angularly moved about its own axis through an angular range 2θ where θ corresponds
to the diameter of the passages 38a, 38b, 40a, 40b and hence the width of the passages
42a, 42b. The angular range 2θ through which the pilot shaft 14 is angularly moved
about its own axis when the communication passage 42b overlaps or communicates with
the oil supply passage 38b or the oil drain passage 40b is delayed by an angle α which
is not in excess of the angle θ. As a result, the overall angle range through which
the pilot shaft 14 is angularly moved about its own axis when the communication passages
42a, 42b overlap or communicate with the oil supply passages 38a, 38b or the oil drain
passages 40a, 40b is represented by (2θ + α). This overall angular range (2 θ + α)
is greater than the angular range through which the pilot shaft 14 is angularly moved
about its own axis when a communication passage 42 overlaps or communicates with one
oil supply passage 38 or one oil drain passage 40 in the conventional hydraulic servo
device as shown in Figure 3B. Consequently, the possibility for both the communication
passages 42a, 42b to be brought out of communication with the oil supply passages
38a, 38b or the oil drain passages 40a, 40b is reduced, and the hydraulic servo device
is less likely to suffer a control failure.
[0028] Operation of the hydraulic servo device according to the first embodiment will be
described below. When the controller applies a control signal to the pilot actuating
device 12, the pilot shaft 14 is angularly moved by the pilot actuating device 12
from the position where the communication passages 42a, 42b are out of communication
with the oil supply passages 38a, 38b or the oil drain passages 40a, 40b as shown
in Figure 2A, clockwise in the direction indicated by the arrow in Figure 2B. As shown
in Figure 2B, the communication passage 42a starts to communicate with the oil supply
passage 38a. A working oil starts to be introduced under pressure from the first space
28 through the oil supply passage 38a and the communication passage 42a into the second
space 30, and the piston 16 is axially displaced towards the distal end of the cylinder
10 due to the pressure area difference on both directions of the piston 16. Since
the communication passage 42a is inclined with respect to the ridge line of the pilot
shaft 14, when the piston 16 is axially displaced towards the distal end of the cylinder
10, the communication passage 42a is again brought out of communication with the oil
supply passage 38a as shown in Figure 2A so that the axial displacement of the piston
16 is stopped.
[0029] When the pilot shaft 14 is further angularly moved to the position shown in Figure
2B, the piston 16 is also axially displaced towards the distal end of the cylinder
10. In this manner, the pilot shaft 14 is continuously angularly moved under feedback
control while the axial position of the piston 16 is being detected, until the piston
16 comes to a desired axial position.
[0030] If the load on the piston 16 is so large that the piston 16 cannot be axially displaced
or if the axial displacement of the piston 16 is too small even in the position shown
in Figure 2B, then the controller issues a control signal to the pilot actuating device
12 which angularly moves the pilot shaft 14 further clockwise into the position shown
in Figure 3A. In this position, both the communication passages 42a, 42b communicate
with the oil supply passages 38a, 38b, respectively, allowing the working oil to flow
under pressure from the first space 28 through the oil supply passages 38a, 38b and
the communication passages 42a, 42b into the second space 30. The piston 16 is axially
displaced by an increased working oil flow rate to produce an increased drive power
with an increased response. Even when the controller further applies a control signal
to the pilot actuating device 12, the communication passages 42a, 42b are less liable
to be brought out of communication with the oil supply passages 38a, 38b because the
angular range of the pilot shaft 14 in which the communication passages 42a, 42b communicate
with the oil supply passages 38a, 38b is larger than when only one communication passage
42 and one oil supply passage 38 are provided.
[0031] For axially moving the piston 16 towards the proximal end of the cylinder 10, the
pilot shaft 14 is angularly moved from the position shown in Figure 2A counterclockwise
in the direction opposite to the direction indicated by the arrow in Figure 2B. The
communication passage 42a starts to communicate with the oil drain passage 40a, connecting
the second space 30 to the drain. Since the oil pressure in the second space 30 drops,
the piston 16 is axially displaced towards the proximal end of the cylinder 10 under
the oil pressure in the first space 28 until the communication passage 42a is brought
out of communication with the oil drain passage 40a as shown in Figure 2A. The pilot
shaft 14 is continuously angularly moved under feedback control while the axial position
of the piston 16 is being detected, for thereby controlling the axial position of
the piston 16. Since the oil drain passages 40a, 40b are positioned relatively to
each other in the same manner as the oil supply passages 38a, 38b, the piston 16 is
axially displaced towards the proximal end of the cylinder 10 with an increased response
and without the danger of the communication passages 42a, 42b being brought out of
communication with the oil drain passages 40a, 40b.
[0032] Figure 6 shows a hydraulic servo device according to a second embodiment of the present
invention. In Figure 6, an air bleeder pipe 44 is connected at an upper region of
the proximal end of the cylinder 10 in communication with the second space 30. The
air bleeder pipe 44 is vented to the atmosphere through an orifice 46. Air contained
in the working oil flowing from the pressurized oil passageway 32 and trapped in the
second space 30 can be discharged through the air bleeder pipe 44. Therefore, the
response of the hydraulic servo device is prevented from being adversely affected
by such trapped air. Since the orifice 46 has a small air passage hole, it can discharge
the trapped air while keeping the oil pressure in the second space 30.
[0033] Figure 7 shows a hydraulic servo device according to a third embodiment of the present
invention. The hydraulic servo device shown in Figure 7 is an improvement in the hydraulic
servo device shown in Figure 6. The air bleeder pipe 44 vented to the atmosphere by
the orifice 46 is connected to the upper region of the proximal end of the cylinder
10, and the slide hole 24 in the end wall 22 is covered with an oil reservoir 48.
The oil reservoir 48 is defined by a bottom plate 50 and a wall 52 which are attached
to the end wall 22. The wall 52 has a hole (not shown) defined therein for the passage
therethrough of the scoop tube that is to be actuated by the hydraulic servo device.
The oil reservoir 48 has a height which is preferably the same as or greater than
the height of the lower end of the air bleeder pipe 44 that is connected to the cylinder
10.
[0034] In the embodiment shown in Figure 6, since the air bleeder pipe 44 is vented to the
atmosphere through the orifice 46, when no oil pressure acts in the second space 30
while the hydraulic servo device is at rest, the working oil seeps through the gap
between the small-diameter portion 20 of the piston 16 and the end wall 22 because
of the head of the working oil in the second chamber 30. Therefore, air tends to flow
from the air bleeder pipe 44 into the second space 30. Such air is responsible for
unstable operation or reduced response of the hydraulic servo device when it starts
to operate next time. In the embodiment shown in Figure 7, the oil reservoir 48 covering
the slide hole 24 is effective to prevent the working oil from seeping from the second
space 30 through the gap between the small-diameter portion 20 and the end wall 22,
so that the hydraulic servo device can start to operate stably or with desired response.
[0035] Figure 8 shows a hydraulic servo device according to a fourth embodiment of the present
invention. The hydraulic servo device shown in Figure 8 is also an improvement in
the hydraulic servo device shown in Figure 6. In Figure 8, the air bleeder pipe 44
has a check valve 50 connected between its end coupled to the cylinder 10 and the
orifice 46. The check valve 50 serves to prevent air from flowing into the second
space 30 through the air bleeder pipe 44 while the hydraulic servo device is at rest.
The check valve 50 may be replaced with a remotely controlled or automatically operated
on-off valve, which can be open only when necessary.
[0036] Figure 9 shows a hydraulic servo device according to a fifth embodiment of the present
invention. In Figure 9, two recesses 56 are defined in lower regions of an inner cylindrical
surface of the cylinder 10 respectively in the first and second spaces 28, 30 near
the distal and proximal ends of the cylinder 10. The recesses 56 serve to collect
particles that are produced as the piston 16 slides against the inner cylindrical
surface of the cylinder 10. The cylinder 10 also has two discharge holes 58 defined
in its cylindrical wall in communication with the bottoms of the respective recesses
56, for discharging particles P collected on the bottoms of the respective recesses
56. The discharge holes 58 are normally closed by respective pressure-tight plugs
60. Since particles produced as the piston 16 slides against the inner cylindrical
surface of the cylinder 10 are gathered and collected in the recesses 56, they are
less likely to remain on the inner cylindrical surface of the cylinder 10, and hence
less liable to be caught between the piston 56 and the cylinder 10. The collected
particles P can be discharged when the plugs 10 are removed and the interior of the
cylinder 10 is cleaned with working oil, etc. while the hydraulic servo device is
not in use.
[0037] Figure 10 shows a hydraulic servo device according to a sixth embodiment of the present
invention. The hydraulic servo device shown in Figure 10 is designed for easy maintenance.
In Figure 10, the large-diameter portion 18 of the piston 16 has threaded holes 64
defined in an end face thereof, and elongate bolts 62 are threaded in the respective
threaded holes 64 as piston removers for pulling the piston 10 out of the cylinder
10. After the working oil is drawn out of the cylinder 10, an end wall is detached
from the proximal end of the cylinder 10, and the pilot shaft 14 is removed. Thereafter,
the elongate bolts 62 are threaded into the respective threaded holes 64, and axially
drawn to pull out the piston 16 from the cylinder 10. The elongate bolts 62 can remove
the piston 16 from the cylinder 10 without disassembling the cylinder 10, so that
the worker can easily inspect and service the piston 16, the cylinder 10, the scoop
tube mounted on the piston 16 for maintenance, or easily replace them.
[0038] Although certain preferred embodiments of the present invention have been shown and
described in detail, it should be understood that various changes and modifications
may be made therein without departing from the scope of the appended claims.
[0039] According to its broadest aspect the invention relates to a hydraulic servo device
comprising: a cylinder; a pilot shaft, said pilot shaft having a pair of communication
passages; and a piston movably mounted on said pilot shaft for axial movement in said
cylinder.
[0040] It should be noted that the objects and advantages of the invention may be attained
by means of any compatible combination(s) particularly pointed out in the items of
the following summary of the invention and the appended claims.
SUMMARY OF THE INVENTION
[0041]
1. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a pair of communication passages defined in an outer circumferential
surface thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having a pair of oil passages defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring at least
one of said communication passages into communication with at least one of said oil
passages to apply a fluid under pressure to said piston for axially moving said piston
in said cylinder.
2. A hydraulic servo device
wherein said communication passages and said oil passages are relatively positioned
such that said communication passages and said oil passages are brought into communication
with each other in different angular ranges of said pilot shaft.
3. A hydraulic servo device
wherein each of said communication passages is angularly nonlinear in a configuration
thereof.
4. A hydraulic servo device
wherein said oil passages include an oil supply passage for supplying a working oil
under pressure and an oil drain passage connected to a drain.
5. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an air bleeder pipe connected to an upper region of said cylinder in communication
with said second space.
6. A hydraulic servo device
wherein said air bleeder pipe has an orifice and vented to the atmosphere therethrough.
7. A hydraulic servo device
wherein said air bleeder pipe has a check valve and vented to the atmosphere therethrough.
8. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage, said cylinder having a recess for collecting particles therein, said recess
being defined in a lower region of an inner cylindrical surface thereof respectively
in said first space and/or said second space.
9. A hydraulic servo device
wherein said cylinder has a discharge hole defined in a cylindrical wall thereof for
discharging particles collected in said recess.
10. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an oil reservoir disposed in covering relation to an end wall of said cylinder which
defines said first space.
11. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said piston having engaging means on an end face thereof for engaging a piston remover
for pulling out the piston from said cylinder.
12. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a pair of communication passages defined in an outer circumferential
surface thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having a pair of oil passages defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring at least
one of said communication passages into communication with at least one of said oil
passages to apply a fluid under pressure to said piston for axially moving said piston
in said cylinder.
13. A fluid coupling wherein said communication passages and said oil passages are
relatively positioned such that said communication passages and said oil passages
are brought into communication with each other in different angular ranges of said
pilot shaft.
14. A fluid coupling wherein each of said communication passages is angularly nonlinear
in a configuration thereof.
15. A fluid coupling wherein said oil passages include an oil supply passage for supplying
a working oil under pressure and an oil drain passage connected to a drain.
16. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an air bleeder pipe connected to an upper region of said cylinder in communication
with said second space.
17. A fluid coupling wherein said air bleeder pipe has an orifice and vented to the
atmosphere therethrough.
18. A fluid coupling wherein said air bleeder pipe has a check valve and vented to
the atmosphere therethrough.
19. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage, said cylinder having a recess for collecting particles therein, said recess
being defined in a lower region of an inner cylindrical surface thereof respectively
in said first space and/or said second space.
20. A fluid coupling wherein said cylinder has a discharge hole defined in a cylindrical
wall thereof for discharging particles collected in said recess.
21. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an oil reservoir disposed in covering relation to an end wall of said cylinder which
defines said first space.
22. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said piston having engaging means on an end face thereof for engaging a piston remover
for pulling out the piston from said cylinder.
1. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a pair of communication passages defined in an outer circumferential
surface thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having a pair of oil passages defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring at least
one of said communication passages into communication with at least one of said oil
passages to apply a fluid under pressure to said piston for axially moving said piston
in said cylinder.
2. A hydraulic servo device according to claim 1, wherein said communication passages
and said oil passages are relatively positioned such that said communication passages
and said oil passages are brought into communication with each other in different
angular ranges of said pilot shaft,
and/or wherein preferably
each of said communication passages is angularly nonlinear in a configuration thereof,
and/or wherein preferably
said oil passages include an oil supply passage for supplying a working oil under
pressure and an oil drain passage connected to a drain.
3. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an air bleeder pipe connected to an upper region of said cylinder in communication
with said second space.
4. A hydraulic servo device according to any of the preceding claims wherein said air
bleeder pipe has an orifice and vented to the atmosphere therethrough,
and/or wherein preferably
said air bleeder pipe has a check valve and vented to the atmosphere therethrough.
5. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage, said cylinder having a recess for collecting particles therein, said recess
being defined in a lower region of an inner cylindrical surface thereof respectively
in said first space and/or said second space.
6. A hydraulic servo device according to any of the preceding claims wherein said cylinder
has a discharge hole defined in a cylindrical wall thereof for discharging particles
collected in said recess.
7. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an oil reservoir disposed in covering relation to an end wall of said cylinder which
defines said first space.
8. A hydraulic servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said piston having engaging means on an end face thereof for engaging a piston remover
for pulling out the piston from said cylinder.
9. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a pair of communication passages defined in an outer circumferential
surface thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having a pair of oil passages defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring at least
one of said communication passages into communication with at least one of said oil
passages to apply a fluid under pressure to said piston for axially moving said piston
in said cylinder.
10. A fluid coupling according to any of the preceding claims wherein said communication
passages and said oil passages are relatively positioned such that said communication
passages and said oil passages are brought into communication with each other in different
angular ranges of said pilot shaft,
and/or wherein preferably
each of said communication passages is angularly nonlinear in a configuration thereof,
and/or wherein preferably
said oil passages include an oil supply passage for supplying a working oil under
pressure and an oil drain passage connected to a drain.
11. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an air bleeder pipe connected to an upper region of said cylinder in communication
with said second space.
12. A fluid coupling according to any of the preceding claims wherein said air bleeder
pipe has an orifice and vented to the atmosphere therethrough,
and/or wherein preferably
said air bleeder pipe has a check valve and vented to the atmosphere therethrough.
13. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage, said cylinder having a recess for collecting particles therein, said recess
being defined in a lower region of an inner cylindrical surface thereof respectively
in said first space and/or said second space.
14. A fluid coupling according to any of the preceding claims wherein said cylindrical
has a discharge hole in a cylindrical wall thereof for discharging particles collected
in said recess.
15. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to be mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein;
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said cylinder having an interior space compartmented by said piston into a first space
communicating with a pressurized oil hole and a second space which can selectively
be brought into and out of communication with said oil passage by said communication
passage; and
an oil reservoir disposed in covering relation to an end wall of said cylinder which
defines said first space.
16. A fluid coupling comprising:
an impeller and an impeller casing which are adapted to be mounted on a drive shaft,
said impeller casing defining a working chamber therein;
a runner adapted to he mounted on a driven shaft;
a scoop tube disposed for movement into and out of said working chamber for generating
the rate of a working oil introduced into said working chamber; and
a hydraulic servo device for positionally controlling said scoop tube, said hydraulic
servo device comprising:
a cylinder;
a pilot shaft disposed angularly movably and extending axially in said cylinder, said
pilot shaft having a communication passage defined in an outer circumferential surface
thereof;
a piston movably mounted on said pilot shaft for axial movement in said cylinder,
said piston having an oil passage defined therein; and
an actuator for angularly moving said pilot shaft about its own axis to bring said
communication passage into communication with said oil passage to apply a fluid under
pressure to said piston for axially moving said piston in said cylinder;
said piston having engaging means on an end face thereof for engaging a piston remover
for pulling out the piston from said cylinder.
17. A hydraulic servo device comprising:
a cylinder;
a pilot shaft, said pilot shaft having a pair of communication passages; and
a piston movably mounted on said pilot shaft for axial movement in said cylinder.