U.S. patent number 3,574,493 [Application Number 04/817,827] was granted by the patent office on 1971-04-13 for vane-type pumps.
This patent grant is currently assigned to Abex Corporation. Invention is credited to William M. Hamilton.
United States Patent |
3,574,493 |
Hamilton |
April 13, 1971 |
VANE-TYPE PUMPS
Abstract
A rotary vane fluid power unit in which a plurality of vanes
slidably supported in a rotor are individually maintained in
engagement with an encircling cam surface by fluid pressure acting
radially on the inner surfaces of pistons which engage the vanes. A
fluid passageway is provided internally of the pump which includes
a valve for maintaining under pressure the fluid that reacts
against the pistons.
Inventors: |
Hamilton; William M. (Hilliard,
OH) |
Assignee: |
Abex Corporation (New York,
NY)
|
Family
ID: |
25223968 |
Appl.
No.: |
04/817,827 |
Filed: |
April 21, 1969 |
Current U.S.
Class: |
418/268 |
Current CPC
Class: |
F01C
21/0863 (20130101) |
Current International
Class: |
F01C
21/08 (20060101); F01C 21/00 (20060101); F04c
001/00 () |
Field of
Search: |
;103/136,136 (R-1)/
;103/135,42,4 ;230/152 ;71/136,138 ;418/268 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Croyle; Carlton R.
Assistant Examiner: Goodlin; Wilbur J.
Claims
I claim:
1. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low and high-pressure ports in the
walls;
a rotor supported on a shaft for rotation in the chamber;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating with the side and peripheral walls to form fluid
transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high pressure port by a fluid passage
means, said passage means including a portion within said shaft
into which pressure fluid is applied from said pressure port;
and
one-way valve means in said passage means within said shaft for
preventing release of fluid acting on the end surface of each
piston.
2. The fluid energy-translating device of claim 1 wherein the
passage means includes a portion on the axis of said shaft and said
one-way valve means is in that axial portion.
3. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low- and high-pressure ports in the
walls;
a rotor supported by a shaft for rotation in the chamber;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating with the side and peripheral walls to form fluid
transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high-pressure port by a fluid passage means
internally of the shaft and rotor;
said passage means including a portion extending longitudinally
within said shaft into which pressure fluid is admitted radially
through said shaft, said passage means also including a portion in
said rotor which opens to the end surfaces of the pistons; and
valve means in said longitudinal portion of said passage means for
controlling the fluid acting on the end surface of each piston.
4. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low- and high-pressure ports in the
walls;
a rotor supported by a shaft for rotation in the chamber;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating with the side and peripheral walls to form fluid
transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high-pressure port by a fluid passage means
internally of the shaft and rotor; and
valve means for controlling the fluid acting on the end surface of
each piston, said valve means being disposed in the fluid passage
means internally of the shaft.
5. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low- and high-pressure ports in the
walls;
a rotor supported by a shaft for rotation in the chamber;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating with the side and peripheral walls to form fluid
transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high-pressure port by a fluid passage means
internally of the shaft and rotor; and
valve means for controlling the fluid acting on the end surface of
each piston, said valve means being a spring biased ball-type check
valve.
6. A fluid energy-translating device of the rotary vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced fluid inlet and outlet ports in the wall,
the peripheral wall having a cam surface;
a rotor disposed upon a shaft and supported for rotation in the
chamber;
vanes projecting from the rotor in slots, the vanes engaging the
sidewalls and cam surface to form fluid transfer pockets;
a piston disposed in the rotor in relation to each vane such that a
force applied to the pistons will be applied outwardly to each
vane;
conduit means provided internally of the rotor and the shaft for
supplying fluid under pressure from the outlet port to end surface
of the pistons; and
a valve disposed in the conduit means in the shaft for controlling
the fluid acting on the end surface of each piston.
7. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low- and high-pressure ports in the
walls;
a rotor supported by a shaft for rotation in the chamber, said
rotor being integral with the shaft;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating with the side and peripheral walls to form fluid
transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high-pressure port by a fluid passage means
internally of the shaft and rotor; and
valve means for controlling the fluid acting on the end surface of
each piston, said valve means being disposed in the passage means
internally of the integral shaft and rotor.
8. A fluid energy-translating device of the vane type
comprising:
a casing having side and peripheral walls forming a rotor chamber,
circumferentially spaced low- and high-pressure ports in the
walls;
a unitary shaft and rotor supported by bearing means for rotation
in the chamber;
vanes mounted in vane slots in the rotor, the vanes and rotor
cooperating to form fluid transfer pockets;
imperforate piston means disposed in the rotor and operable to urge
each vane outwardly, each piston having an end surface
interconnected with the high-pressure port by a fluid passage means
internally of the unitary shaft and rotor and bearing means;
and
valve means for controlling the fluid acting on the end surface of
each piston.
9. A fluid energy-translating device, as defined in claim 8,
wherein the fluid passageway passes through the sidewall of the
bearing means.
10. A fluid energy-translating device of the rotary vane type
comprising:
a casing forming side and peripheral walls forming a rotor chamber,
circumferentially spaced fluid inlet and outlet ports in the wall,
the peripheral wall forming a cam surface;
a rotor connectedly disposed upon a shaft and supported for
rotation in the chamber;
a resilient seal disposed between and in sealing engagement with
the shaft and rotor;
vanes projecting from the rotor in slots, the vanes engaging the
sidewalls and cam surface to form fluid transfer pockets;
pistons disposed in the rotor in relation to each vane such that a
force applied to the pistons will be applied outwardly to each
vane;
conduit means provided in the shaft, resilient seal and the rotor
for supplying fluid under pressure from the outlet port to the
underside of the pistons; and
a valve disposed in the conduit means in the shaft for controlling
the fluid acting on the end surface of each piston.
Description
BACKGROUND OF THE INVENTION
This invention is directed to improvements in fluid pressure energy
translating devices of the vane type which include hydraulic means
for vane control and which are known in the art as "three-area"
devices. More specifically, the invention relates to valve means in
a vane pump for preventing damage to the vane tips and the cam ring
such as is normally encountered where there is an insufficient
total force acting outwardly on the vanes as the vanes traverse the
cam ring surface. A typical hydraulic pump of the vane type
includes a rotor having a plurality of radially movable vanes
carried in slots around its periphery. The vanes engage the cam
ring surface of a fixed stator or cam ring which surrounds the
rotor. Inlet and outlet ports open at spaced positions into the
area between the periphery of the rotor and the cam surface and are
swept or traversed sequentially by the vanes as the rotor turns,
whereby fluid received at the inlet port is transferred by the
vanes to the outlet port.
In a vane pump of the three-area type, fluid pressures act on the
three areas associated with each vane and the forces resulting from
these pressures cooperate to urge each vane into operative
engagement with the cam surface, i.e., to maintain a dynamic seal
between the vane tip and the cam surface. By utilization of the
three-area vane control principle, a limited predetermined
hydraulic force for urging or moving the vanes outwardly is
obtained.
The fluid pressures acting on two of the areas associated with each
vane are substantially equal but act in opposite directions. And
the forces resulting from these pressures thus tend to counteract
each other. The first area comprises a surface on the radially
outer end of the vane and is subjected to pressure which urges the
vane inwardly in its slot. The second vane area comprises a surface
and on the radially inner end of the vane. The second area is
subjected to a pressure equal but opposed to that acting on the
first area, which pressure urges the vane outwardly in its
slot.
A third area associated with each vane is also subjected to fluid
pressure which urges the vane outwardly. Pressure on this third
area provides a controlling hydraulic force which, in addition to
centrifugal force, urges the vane outwardly to effect and maintain
a fluid seal between the outer end of the vane or vane tip and cam
ring surface.
Three-area pumps of the type to which this invention relates
include a rotor assembly having an internal pressure chamber and a
pressure operated pin or piston associated with each vane, the
piston being slidable in a bore intersecting the pressure chamber
and leading radially to the vane. Fluid pressure in the chamber
acts on the pistons and provides the third area force holding the
vanes outwardly against the cam surface. Pressure is supplied to
this chamber through passageways from a high-pressure zone of the
pump whenever the pressure in the chamber tends to drop
sufficiently below the pressure in the high-pressure zone.
The basic principles of the three-area concept for controlling
vanes are taught in U.S. Pat. No. 2,832,293 for a "Vane Pump,"
Cecil E. Adams et al. According to one form of the three-area
device as disclosed in the Adams et al. patent, there is associated
with each vane a piston mounted in the rotor for sliding movement
in the radial direction to engage the inner end of the vane. Fluid
under pressure for operating the pistons is supplied through a
channel or chamber in the rotor adjacent the operating shaft which
in turn is fed through grooves formed in the cheek plate surfaces
adjacent the rotor and leading from the high-pressure zone. Because
the fluid being fed to the rotor channel must pass from or through
the cheek plates across the clearance gaps between the rotor and
cheek plate, considerable quantities of fluid under pressure can
escape through these clearance gaps. This loss of fluid under
pressure reduces the overall efficiency of the device.
Prior to the present invention, no satisfactory means had been
known for supplying fluid under pressure to the third area means of
the type shown in U.S. Pat. No. 2,832,293 without an excessive
amount of leakage. As previously suggested, one object of this
invention includes the provision of a pump including the three-area
vane control principle in which the passageway through which fluid
under pressure is supplied to the third area is contained wholly
within the rotating assembly including the rotor body and shaft
and, therefore, is not exposed to leakage paths (such as the
mentioned clearance gaps) from which leakage of high-pressure fluid
from the high-pressure fluid passageway can occur.
A further object of the present invention is to provide a valve
means disposed in the internal passageway or conduit means for
maintaining under pressure the fluid acting upon the pistons.
Further objects and advantages of the present invention will be
apparent from the following description, reference being had to the
accompanying drawings wherein preferred embodiments of the present
invention are clearly shown.
IN THE DRAWINGS
FIG. 1 is a vertical longitudinal or axial sectional view of a
three-area vane-type pressure energy-translating device including
the invention;
FIG. 2 is a view in section taken generally on line 2-2 of FIG. 1
and showing an enlarged view of the relative positions of the fluid
ports;
FIG. 3 is an enlarged perspective view depicting the resilient
sleeve structure used in one embodiment of the invention; and
FIG. 4 is an enlarged view of another embodiment showing a unitary
shaft and rotor element which includes the features of this
invention.
GENERAL CONSTRUCTION
The three-area vane pump of this invention is a first described
with reference to FIG. 1 of the drawings. It includes a housing or
casing formed by a body casing 10 having a generally cylindrical
interior chamber. An end cap 11 having a cylindrical boss 12
telescopes into the end of the body and is sealed by an O-ring
13.
The end wall 14 of the body opposite end cap 11 includes a bore
through which the pump operating shaft 15 extends. Shaft 15 is
supported for rotation in this bore by a bearing (not shown) which
is secured against axial movement in the bore. Shaft 15 extends
from the body 10 into end cap 11 and is carried for rotation
therein by a plain bearing 16 mounted within a central bore 17 in
the end cap 11. The bearing 16 is held against axial movement at
one end by a snap ring 18. Cylindrical boss 12 of end cap 11 is
finished to form a flat inner surface which is clamped against a
side or radial face 19 of a cam ring or stator 20. It may be
mentioned here that the cam ring itself as well as the housing and
cam ring together is sometimes referred to in the art as a
stator.
A fluid intake passageway 21 extends radially into body 14 and
communicates with a pair of annular channels 22, 23 which encircle
the internal cavity within the body 14. These annular channels 22,
23 distribute fluid from the intake passageway 21 to suction ports
later to be described in detail.
The cam ring 20 is supported radially by an annular rib 24 formed
in the body 11 between the annular channels 22, 23. The cam ring 20
encircles a rotor 25 which is connected to and supported by the
shaft 15 through a motion permitting spline joint 26 that permits
proper running alignment between the rotor, the flat surface of the
cylindrical boss 19, and a movable cheek or port plate 27. The
rotor 25 is provided with a plurality of radial vane slots 28 in
each of which a radially pressure balanced vane 29 is mounted. This
may best may be seen in FIG. 2 of the drawings.
The cam ring 20 has a cam surface 30 that is contoured to provide a
balanced or symmetrical pump construction in which there are
diametrically opposite low-pressure or suction zones 31, fluid
transfer zones 32, high-pressure or exhaust zones 33, and sealing
zones 34 formed between the cam surface and the rotor 25. In order
to provide the opposed zones, the cam surface 30 is formed in part,
by a first pair of arcs of equal radii which extend across the
fluid transfer zones 32 and, in part, by a second pair of arcs of
shorter radii than the first pair of arcs which extends across the
sealing zones 34. These pairs of arcs are interconnected by cam
surfaces which extend across the low- and high-pressure zones 31
and 33, respectively.
Cheek plate 27 is finished to provide a smooth flat radial surface
on the inner side thereof which abuts the cam ring 20. A central
bore 35 in cheek plate 27 is surrounded by a cylindrical boss 36
which extends into the bore in the wall 14 of the body 10 and is
sealed by an O-ring 37. The outer cylindrical surface of cheek
plate 27 is sealed with respect to body 10 by an O-ring 38. The
cheek plate 27 is movable axially in the body 10 and is urged
toward rotor 25 by fluid pressure supplied from the high-pressure
zone 33 through passageways 39 and 40 to a pressure chamber 41
formed between the body and the outer face 31 of the cheek plate.
The cheek plate functions in the nature of an axially movable,
nonrotatable piston, under pressure supplied by the fluid in
chamber 41 to maintain it in engagement with the adjacent side face
of the cam ring 20.
Intake passageway 21 communicates through annular channels 22 and
23 around cam ring 20 to suction ports spaced 180.degree. apart.
Two suction ports, 43 and 44 shown in FIG. 2, are formed in cheek
plate 27 and are fed by channel 23. Two additional suction ports
(not shown) are formed in end cap 11 and are fed by channel 22.
These suction ports in the end cap and cheek plate are identical in
shape and are axially aligned with the suction zone 31 between the
rotor 25 and cam surface 30. Each suction port has a branch
passage, the opening of one of which is designated at 45, and the
other of which is designated at 46, whereby these suction ports
communicate with the inner ends 47 of vane slots 28 in the rotor 25
as well as with the inlet zones 31.
As shown in FIG. 1, the end cap 11 includes two diametrically
opposed crescent-shaped exhaust or pressure ports 48 which are
based substantially 90.degree. from the suction ports. Similarly,
pressure ports 49 are formed in cheek plate 27 and are axially
aligned with the pressure zones 33 and with ports 48 in the end cap
11. Each pressure port 48 and 49 communicates with the inner ends
47 of the vane slots 28 in the rotor 25 as the vane slots pass the
ports through branch ports 50 and 51. Pressure ports 48 are
connected with a fluid outlet or delivery port 52 by passageway 53
in the end cap 11.
OPERATION
In the direction of rotor movement (clockwise as shown by the arrow
in FIG. 2), the cam surface 30 progressively recedes from the
periphery of the rotor 25 across the suction zones 31. In the
transfer zones 32, cam surface 30 has nearly constant radial
spacing from the rotor, and across the exhaust zones 33 the cam
surface progressively approaches the rotor 25 as it comes into
close proximity with the periphery of the rotor 25 in the sealing
zone 34. Fluid from the suction ports 43 and 44 is drawn into the
fluid transport pockets defined between the successive vanes as
those pockets become larger when the vanes 29 move through the
suction zones 31. As the vanes move through the pressure zones 33,
the volume of the pockets between the vanes diminishes and the
fluid is positively displaced to effect a pumping action.
Each vane 29 is provided with grooves 54 which are formed in the
radially outer surface 70 and opposite side surfaces 71. One ore
more channels or bores 55 are also provided in each vane which
communicate between the outer groove 54 of the vane and the inner
end 47 of the vane slot. The grooves 54 and channels or bores 55
insure that fluid pressure acting on the first area or outer end
surface of any given vane will be substantially balanced at all
times by the pressure acting on the secondary or inner end surface
of that vane.
For the pump to operate at high efficiency, it is necessary to
maintain a continuous sealing engagement between the cam surface 30
and the outer end surfaces 70 of the vane, regardless of changes in
the arcuateness of the cam surface. To provide the hydraulic
pressure for this purpose, one or more radial bores or piston
cylinders 56 is formed in the rotor 25, extending inwardly from the
inner end 47 of each vane slot 28. The bores 56 are interconnected
at their inner ends with an annular pressure chamber 57 formed in a
cylindrical resilient seal 58 disposed between the rotor 25 and
shaft 15. The seal 58, best seen in FIG. 3 of the drawings, may be
constructed from neoprene or any similar material. With some
materials it may be desirable to bond seal 58 to rotor 25.
A generally cylindrical piston or hydraulic actuator 59 is
slidingly and sealingly disposed within the cylinder 56. Each
piston 59 is closely fitted to the bore 56 so that leakage of fluid
along the external walls of the piston is negligible. Fluid which
is admitted under pressure to the radial bores 56 flows from the
high-pressure chamber or exhaust port 53, through passageways 60 in
end cap 11, ports 61 in bushing 16, ports 62 in shaft 15, port 63
in bushing 64, around check valve 65, spring 65', passageway 66 and
into radially interconnecting passageways 67 through ports 68 in
resilient seal 58 and thus into bores 56. The bushing 64, check
valve 65 and spring 65' are retained within the shaft 15 by a
threaded plug 69. Once the interconnecting passageways 56, 57, 68,
67, 66 have been charged with high-pressure fluid, the check valve
65 will maintain that fluid under pressure. If for any reason, the
pressure of the fluid in the aforesaid mentioned passageway should
become less than the pressure of the fluid in the outlet chamber
53, then high-pressure fluid will flow from chamber 53 past the
check valve 65 and into the passageways previously described, thus
maintaining the fluid in those passageways at a pressure
substantially equal to the pressure in the outlet or exhaust
chamber 53.
The basic elements of the pump are included in a modified
embodiment of the invention which is illustrated in FIG. 4.
Component elements of the pump 10 similar to components of the pump
structure previously described are identified by the same reference
numbers used in FIG. 1. The embodiment illustrated in FIG. 4 of the
drawings differs from the one shown in FIG. 1 in that the shaft and
rotor in FIG. 4 is one unitary element 15', i.e., the rotor and
shaft are made of one piece of metal. By using the unitary rotor
and shaft element 15' as illustrated in FIG. 4, it is possible to
eliminate the need for the seal 58 and spline connection 26, that
are required with the multiple piece structure (rotor 25 and shaft
15) shown in FIG. 1.
From the foregoing, it will be obvious to those skilled in the art
that by this invention I have provided a fluid pressure energy
translating device including the three-area principle described in
the previously mentioned Adams et al. patent wherein there is no
material volumetric loss of fluid from that portion of the
passageway means which is constantly pressurized to act upon the
third area means and that the valve means in the internal
passageway means opens only when it is necessary to maintain
pressure in the constantly pressurized portion of the passageway
means and that the valve means need only open slightly to
accomplish this function.
* * * * *