GOVERNMENT LICENSE RIGHTS
[0001] This invention was made with government support under contract number AATD W911 W6-06-D-0005-0004
awarded by the U.S. Army. The government has certain rights in the invention.
BACKGROUND OF THE INVENTION
1. Field of the Intention
[0002] The subject disclosure is directed to rotary vane pumps, and more particularly, to
a balanced split discharge vane pump that provides a combined discharge flow for high
fluid demand conditions and a first (primary) discharge flow for low fluid demand
conditions, and stili more particularly to a multi-discharge vane pump that has an
inlet port and four discharge ports, includes a floating side wear disk and a cam
ring with internal flow passages, and a rotor assembly with improved under-vane pumping
features.
2. Description of Related Art
[0003] Rotary hydraulic vane pumps are well known in the art, as disclosed for example in
U.S. Patent No. 4,274,817 to Sakamaki et al. and
U.S. Patent No. 5,064,362 to Hansen. A typical rotary vane pump includes a circular rotor mounted for rotation within a larger
circular pumping chamber. The centers of these two circles are typically offset, causing
eccentricity. Vanes are mounted to slide in and out of the rotor to create a plurality
of volume chambers or vane buckets that perform the pumping work. On the intake side
of the pump, the vane buckets increase in volume. These increasing volume vane buckets
are filled with fluid that is forced into the pumping chamber by an inlet pressure.
On the discharge side of the pump, the vane buckets decrease in volume, forcing pressurized
fluid out of the pumping chamber.
[0004] It is desirable to match the fluid displacement of a vane pump to the operating characteristics
of the system with which the pump is to be associated. For example, the maximum displacement
of a fuel pump should be coordinated with the maximum fuel requirements of the associated
engine application. However, system requirements typically vary with operating conditions,
so that a fixed displacement fuel pump that is designed as a function of the most
demanding engine operating conditions may function with less than desired efficiency
under other operating conditions.
[0005] In the case of a fuel pump associated with a gas turbine engine of an aircraft, fuel
flow requirements, as quantified by pump displacement per rotational speed, under
engine starting conditions greatly exceed fuel flow requirements during other less
demanding engine operating conditions, such as cruise, idle, decent and taxi. Various
attempts have been made to improve fuel pump efficiency over the operating envelope
of a gas turbine engine, by utilizing different valve arrangements at the pump outlet
to meter a portion of the pump discharge to the engine as a function of engine demand.
However, these prior art arrangements are typically complex and thus add cost to the
pumping system. In other implementations, variable displacement pumps have been utilized
to match pump output flow to system demand. However, these implementations are at
the expense of pump size/weight and reliability because of an increase in pump radial/axial
loading and the incorporation of additional moving parts.
[0006] U.S. Patent Application Publication No. 2010/0316507, entitled Split Discharge Vane Pump and Fluid Metering System Therefor, discloses
a positive displacement vane pump that is adapted and configured to more closely match
the operating characteristics of the system with which it is associated, as well as,
a valving arrangement for effectively managing the flow of fluid from the pump depending
upon the fluid demand conditions of the system with which it is associated. The disclosure
of
U.S. Patent Application Publication No. 2010/0316507 is hereby incorporated by reference in its entirety.
[0007] The pump disclosed in
U.S. Patent Application Publication No. 2010/0316507 solves many of the problems noted above with respect to prior art pump constructions.
However, there is need for a positive displacement vane pump design that further increses
pumping efficiency over the operation range of fuel requirements and reduces component
degradation by more effectively balancing the forces within the pumping chamber.
SUMMARY OF THE INVENTION
[0008] The present invention is directed to a hydraulic vane pump that includes,
inter alia, a pump body that defines an interior pumping chamber and an inlet port for allowing
fluid to be provided to the interior pumping chamber and at least one discharge port
for allowing pressurized fluid to be discharged from the interior pumping chamber.
The pump further includes a cam ring that is disposed within the interior pumping
chamber and defines a continuous peripheral cam surface; and a rotor mounted for axial
rotation within the interior pumping chamber and defining a pump axis. A plurality
of circumferentially spaced apart radially extending vanes are mounted for radial
movement within slots formed in the rotor, the plurality of vanes define an equal
number of circumferentially spaced apart volume chambers which extend between an outer
periphery of the rotor and the cam surface for carrying pressurized fluid. Still further,
the pump includes axially opposed first and second wear disks disposed within the
interior pumping chamber. The first wear disk has an outer periphery which is positioned
radially inward of the cam surface and is adapted and configured to slide axially
with respect to the cam surface, so as to provide for thermal expansion of the rotor
and vanes. The second wear disk is fixedly positioned adjacent to a second end surface
of the rotor. However, as will be discussed below, the second wear disk can also be
a floating disk (i.e., adapted for sliding in the axial direction).
[0009] In a preferred embodiment, the pump is a multi-discharge hydraulic vane pump and
the pump body defines four radially-oriented discharge ports, each discharge port
allowing pressurized fluid to be discharged from the interior pumping chamber.
[0010] It is envisioned that the first wear disk is biased towards the first end surface
of the rotor using a spring element. Moreover, the first wear disk can be biased towards
the first end surface of the rotor using pressurized fluid discharged from the volume
chambers defined by the vanes.
[0011] In certain constructions of the present invention, the pump body further includes
a rear side plate and the inlet port extends axially through the rear side plate to
the interior chamber.
[0012] Preferably, the cam surface includes four quadrantal cam segments, wherein diametrically
opposed cam segments have identical cam profiles, and each cam segment defines an
inlet arc, a discharge are and two seal arcs.
[0013] In a preferred embodiment, the cam ring includes a plurality of inlet chambers arranged
and configured to receive fluid from the inlet port and distribute the fluid to the
inlet arc of each cam segment. The cam ring can also includes a plurality of discharge
chambers which communicate with the discharge arc of each cam segment and are arranged
and configured to facilitate the discharge of pressurized fluid from the interior
pumping chamber.
[0014] It is presently preferred that each vane slot has an under-vane pocket for receiving
pressurized fluid based on an angular position of the rotor. Additionally, in certain
embodiments, the rotor includes a plurality of axially-extending under-vane passages,
each under-vane passage communicating with an under-vane pocket through a connector
passage.
[0015] Preferably, each wear disk includes flow passages for communicating fluid into the
under-vane pockets and under-vane passages associated with each vane slot. The pressure
of the undervane pocket is dependent on an angular position of the rotor. Preferably,
the fluid in the rotor under-vane passage whilst positioned in the inlet arc segment
is about equal to pump inlet pressure and the fluid in the rotor under-vane passage
whilst positioned in the discharge arc segment is about equal to pump discharge pressure.
[0016] Certain constructions of the vane pump of present invention include a fluid metering
system for extracting fluid flow from the discharge arcs of the four cam segments.
It is envisioned that the metering system has a first operating condition in which
fluid is extracted from the discharge arcs of all four cam segments and combined for
delivery to a source of fluid demand. The fluid metering system can also include a
second operating condition wherein fluid is extracted from a first (primary) pair
of diametrically opposed discharge arcs for delivery to a source of fluid demand and
fluid from a second pair of diametrically opposed discharge arcs bypasses the source
of fluid demand and returns to the pumping chamber.
[0017] The present invention is also directed to a multi-discharge hydraulic vane pump that
includes, among other elements, a pump body that has an interior pumping chamber and
defines a axially extending inlet port for allowing fluid to be provided to the interior
pumping chamber and four radially-extending discharge ports for allowing pressurized
fluid to be discharged from the interior pumping chamber. The vane pump further includes
a cam ring disposed within the interior pumping chamber that defines a continuous
peripheral cam surface and a rotor mounted for axial rotation within the interior
pumping chamber that defines a pump axis. A plurality of circumferentially spaced
apart and radially extending vanes are mounted for radial movement within slots formed
in the rotor. The plurality of vanes define an equal number of circumferentially spaced
apart volume chambers which extend between an outer periphery of the rotor and the
cam surface for carrying pressurized fluid. The pump further includes axially opposed
first and second wear disks which are disposed within the interior pumping chamber.
[0018] In a preferred embodiment, the first wear disk has an outer periphery which is positioned
radially inward of the cam surface and is mounted for sliding movement with respect
to the cam surface, so as to provide for thermal expansion of the rotor and vanes.
The second wear disk is positioned adjacent to a second end surface of the rotor.
[0019] It is envisioned that the first wear disk is biased towards the first end surface
of the rotor using a spring element. Moreover, the first wear disk can be biased towards
the first end surface of the rotor using pressurized fluid discharged from the volume
chambers defined by the vanes.
[0020] In certain constructions of the present invention, the pump body further includes
a rear housing with an inlet port that extends axially through the rear side plate
to the interior chamber.
[0021] Preferably, the cam surface includes four quadrantal cam segments, wherein diametrically
opposed cam segments have identical cam profiles, and each cam segment defines an
inlet arc, a discharge arc and two seal arcs.
[0022] In a preferred embodiment, the cam ring includes a plurality of inlet chambers arranged
and configured to receive fluid from the inlet port and distribute the fluid to the
inlet arc of each cam segment. The cam ring also includes a plurality of discharge
chambers which communicate with the discharge arc of each cam segment and are arranged
and configured to facilitate the discharge of pressurized fluid from the interior
pumping chamber.
[0023] It is presently preferred that each vane slot has an under-vane pocket for receiving
either low inlet or discharging high outlet pressurized fluid based on an angular
position of the rotor. Additionally, in certain embodiments, the rotor includes a
plurality of axially-extending under-vane passages, each under-vane passage communicating
with an under-vane pocket through a connector passage.
[0024] It is envisioned that each wear disk can includes flow passages for communicating
fluid into the under-vane pockets and under-vane passages associated with each vane
slot. The pressure of the undervane pocket in dependent on an angular position of
the rotor. Preferably, the pressurized fluid in the rotor under-vane passage whilst
positioned in the inlet arc segment is about equal to pump inlet pressure and the
fluid in the rotor under-vane passage whilst positioned in the discharge arc segment
is about equal to pump discharge pressure.
[0025] Certain constructions of the vane pump of present invention include a fluid metering
system for extracting fluid flow from the discharge arcs of the four cam segments.
It is envisioned that the metering system has a first operating condition in which
fluid is extracted from the discharge arcs of all four cam segments and combined for
delivery to a source of fluid demand. The fluid metering system can also include a
second operating condition wherein fluid is extracted from a first pair of diametrically
opposed discharge arcs for delivery to a source of fluid demand and fluid from a second
pair of diametrically opposed discharge arcs bypasses the source of fluid demand and
returns to the pumping chamber.
[0026] The present invention is further directed to a hydraulic vane pump that includes,
inter atia, a pump body that defines an interior pumping chamber, an inlet port for allowing
fluid to be provided to the interior pumping chamber and at least one discharge port
for allowing pressurized fluid to be discharged from the interior pumping chamber.
The hydraulic vane pump further includes a cam ring disposed within the interior pumping
chamber that defines a continuous peripheral cam surface, the cam ring also defining
a plurality of inlet chambers and discharge chambers. The inlet chambers are arranged
and configured to receive fluid from the inlet port and to distribute the fluid to
the interior pumping chamber and the discharge chambers communicate with the interior
pumping chamber and are arranged and configured to facilitate the discharge of pressurized
fluid from the interior pumping chamber.
[0027] A rotor is mounted for axial rotation within the interior pumping chamber and defines
a pump axis. A plurality of circumferentially spaced apart and radially extending
vanes are mounted for radial movement within slots formed in the rotor. The plurality
of vanes define an equal number of circumferentially spaced apart volume chambers
which extend between an outer periphery of the rotor and the cam surface for carrying
pressurized fluid. Each vane slot has an under-vane pocket for communicating fluid.
The pressure in the undervane pockets are dependent on an angular position of the
rotor.
[0028] Axially opposed first and second wear disks are disposed within the interior pumping
chamber, the first wear disk has an outer periphery which is positioned radially inward
of the cam surface and is axially biased towards a first end surface of the rotor,
so as to provide for thermal expansion of the rotor and vanes. The second wear disk
is positioned adjacent to a second end surface of the rotor. Preferably, each wear
disk includes flow passages for communicating fluid into the under-vane pockets associated
with each vane slot. The pressure of the undervane pockets is dependant on an angular
position of the rotor.
[0029] These and other features and benefits of the subject invention and the manner in
which it is assembled and employed will become more readily apparent to those having
ordinary skill in the art from the following enabling description of the preferred
embodiments of the subject invention taken in conjunction with the several drawings
described below.
BRIEF DESCRIPTION OF THE DRAWINGS
[0030] So that those skilled in the art to which the subject invention appertains will readily
understand how to make and use the methods, devices and systems of the subject invention
without undue experimentation, preferred embodiments thereof will be described in
detail hereinbelow with reference to certain figures, wherein:
[0031] FIG. 1 is a perspective view of a multi-discharge pump assembly which has been constructed
in accordance with a preferred embodiment of the present invention;
[0032] FIG. 2 is a partially exploded perspective view of the pump assembly of FIG. 1 in
which a front side plate has been removed for ease of illustration;
[0033] FIG. 3 is an exploded perspective view of the cam ring, the rotor assembly, the annular
spacer and the rear side plate used in the pump assembly of FIG. 1;
[0034] FIGS. 4 provides a end view of a rear side plate used in the pump assembly of FIG.
1;
[0035] FIG. 5 provides a cross-sectional view of the rear side plate shown in FIG. 4 taken
along cut line 5-5;
[0036] FIG. 6 provides a cross-sectional view of the rear side plate shown in FIG. 4 taken
along cut line 6-6;
[0037] FIG. 7 is an exploded view of a portion of the pump assembly of FIG. 1 which illustrates
the front side fixed wear plate, the rotor assembly, the cam ring and the rear side
sliding wear plate;
[0038] FIG. 8 is a perspective view of the rotor assembly used in the pump assembly of FIG.
1;
[0039] FIG. 9 is a cross-sectional view of the rotor assembly of FIG. 8 taken along cut
line 9-9;
[0040] FIG. 10 is a perspective view of the cam ring used in the pump assembly of FIG. 1;
[0041] FIG. 11 is an end view of the cam ring of FIG. 10;
[0042] FIG. 12 provides a perspective view of the rear side floating disk used in the pump
assembly of FIG. 1;
[0043] FIG. 13 is a front end view of the floating wear disk of FIG. 12;
[0044] FIG. 14 is a rear end view of the floating wear disk of FIG. 12;
[0045] FIG. 15 is a cross-sectional view taken along cut line 15-15 of the floating wear
disk of FIG. 12;
[0046] FIG. 16 provides a perspective view of the front side fixed wear disk used in the
pump assembly of FIG. 7;
[0047] FIG. 17 is a front end view of the fixed wear disk of FIG. 16;
[0048] FIG. 18 is a rear end view of the fixed wear disk of FIG. 16;
[0049] FIG. 19 is sectional view of the pump assembly shown in FIG. 1 which illustrates
that when the vanes are within the seal arc, the under-vane cavities are connected
to pump discharge passages;
[0050] FIG. 20 is a cross-sectional view of the pump assembly shown in FIG. 1 taken along
cut line 20-20 in FIG. 19;
[0051] FIG. 21 is sectional view of the pump assembly shown in FIG. 1 taken along cut line
21-21 which illustrates that when the vanes are within the discharge ramp/arc, the
over-vane and under-vane cavities are connected to pump discharge passages;
[0052] FIG. 22 is sectional view of the pump assembly shown in FIG. 1 taken along cut line
22-22 which illustrates that when the vanes are within the inlet ramp/are, the over-vane
and under-vane cavities are connected to pump inlet passages; and
[0053] FIG. 23 provides a cross-sectional view of the rotor assembly and a portion of the
cam ring.
[0054] These and other aspects of the subject invention will become more readily apparent
to those having ordinary skill in the art from the following detailed description
of the invention taken in conjunction with the drawings.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS
[0055] Disclosed herein are detailed descriptions of specific embodiments of the devices,
systems and methods of the present invention. It will be understood that the disclosed
embodiments are merely examples of the way in which certain aspects of the invention
can be implemented and do not represent an exhaustive list of all of the ways the
invention may be embodied. Indeed, it will be understood that the systems, devices,
and methods described herein may be embodied in various and alternative forms. The
figures are not necessarily to scale and some features may be exaggerated or minimized
to show details of particular components. Well-known components, materials or methods
are not necessarily described in great detail in order to avoid obscuring the present
disclosure. Any specific structural and functional details disclosed herein are not
to be interpreted as limiting, but merely as a basis for the claims and as a representative
basis for teaching one skilled in the art to variously employ the invention.
[0056] For ease of description, the components of this invention are described in an upright
operating position, and terms such as upper, lower, front, rear, horizontal, etc.,
are used with reference to this position. It will be understood, however, that the
components of this invention may be manufactured, stored, transported, used, and sold
in an orientation other than the position described.
[0057] Figures illustrating the components show some mechanical elements that are known
and will be recognized by one skilled in the art. The detailed descriptions of such
elements arc not necessary to an understanding of the invention, and accordingly,
are herein presented only to the degree necessary to facilitate an understanding of
the novel features of the present invention.
[0058] Referring now to the drawings wherein like reference numerals identify similar structural
features or elements of the subject invention, there are illustrated in FIG. 1 an
embodiment of the hydrostatically-balance, multi-discharge hydraulic vane pump of
the present invention designated generally by reference numeral 10 which includes
a cartridge assembly pumping element (item 90 in Fig. 7). The cartridge assembly 90
is configured to fit within a reusable housing (annular space 16). In other words,
the pump element 90 can be readily replaced when worn or in need of repair. FIGS.
2 through 18 provide views of the various component parts that form the pump element
90 and FIGS. 19 through 23 provide cross-sectional and elevational views for pump
assembly 10 in a variety of operating configurations.
[0059] Pump assembly 10 includes a single inlet port 24 (see FIGS. 19-22) for admitting
low pressure fluid into the pump assembly 10. Pump assembly 10 also includes four
discharge ports 30a-d for discharging pressurized fluid from the pump assembly 10.
Discharge ports 30a and 30c diametrically oppose each other. Similarly, discharge
ports 30b and 30d diametrically oppose each other. Normally, 30a/30c or 30b/30d for
one of two pumps.
[0060] By passing through the pump assembly 10, the low pressure fluid becomes high pressure
fluid and exits the pump assembly through either two diametrically opposed discharge
ports 30a-d or through all of the discharge ports. The manner in which the low pressure
fluid proceeds from the inlet port 24 into the interior pump chamber 42, is pressurized
and is supplied to the discharge ports 30a-d will be discussed in detail herein below.
By having diametrically opposed discharge ports 30a-d, the forces generated in the
pumping process thereby effectively cancel to provide a balanced pump assembly 10.
[0061] The pump assembly 10 also includes fixed front and rear side plates 80s, 80b, which
are separated from one another by an annular spacer 16. The inlet port 24 is formed
in the rear side plate 80b. The discharge ports 30a-30d are formed in the annular
spacer 16.
[0062] An end plate 22 is fixed to the front side plate 80a using a series of bolts 27a-f
and defines an axial passageway 26 through which a drive shaft 28a passes to attach
to a rotor assembly 70. The front and rear side plates 80a, 80b, along with the annular
spacer 16, combine to form an interior or pumping chamber 42 that houses a cam ring
90, a floating side wear disk 50, a fixed side wear disk 60 and the rotor assembly
70 (see FIG. 3).
[0063] Referring to FIG. 2, a perspective view of the pump assembly 10 is shown with the
front side plate 80a removed to illustrate the rotor assembly 70 and the cam ring
90 housed in the pumping chamber 42 and having a front end abutting the fixed side
wear disk 60. FIG. 3 provides an additional exploded perspective view in which the
cam ring 90, fixed side wear disk 60, floating wear disk 50 and the rotor assembly
70 have been removed from within the interior pumping chamber 42.
[0064] The rotor assembly 70, which is best viewed in FIGS. 8 and 9, is mounted on a drive
shaft 28b for axial rotation within the pumping chamber 42. The rotor assembly is
supported for rotation within the pumping chamber 42 by two journal bearings which
are associated with the side wear disks 50/60. As shown in FIG. 19, rotor drive shaft
28b engages with drive shaft 28a which extends outside of the front side plate 80a.
[0065] Rotor assembly 70 includes a rotor body 71, which fits within a pumping chamber surface
35 defined by cam ring 90 (best shown in FIG. 11). The rotor body 71 includes a plurality
of radially outwardly acting vane elements 36 which normally contact the elliptical
pumping chamber surface 35. As described in more detail below, a plurality of circumferential
vane buckets or volume chambers 44 are formed between the rotor body 71, the elliptical
pumping chamber surface 35, the vane assemblies 36 and the wear disks 50/60 (see FIG.
20).
[0066] For each vane element 36, rotor body 71 includes a vane slot 38 into which the vane
element is slidably received, an axially extending under-vane pumping pocket 73 and
an axially extending under-vane pumping passage 75. Radially extending, but angled,
connector passages 77, allow fluid to communicate between the under-vane pumping pocket
73 and under-vane pumping passage 75. The manner in which the under-vane pumping occurs
and the benefits associated with the configuration of the under-vane pumping of the
present invention will also be described below.
[0067] Referring now to FIGS. 4 through 6, which provide several views of rear housing plate
80b. Eight through holes 82 are provided in the outer flanges of the front and rear
housing plates 80a/80b which allow the rear housing plate 80b and the front housing
plate 80a to be secured to the annular spacer 16 using through bolts and associated
nuts (see FIG. 1). As discussed above, the axial inlet port 24 for the pump assembly
10 is formed in the rear side plate 80b and branches off into four diametrically opposed
angled inlet channels 84. These inlet channels 84 can also been viewed in FIG. 3 and
as will be discussed below are arranged and configured so as to distribute the incoming
fluid into four axially extending inlet chambers 92 formed in cam ring 90.
[0068] Referring now to FIGS. 10 and 11, in addition to the axially extending inlet chambers
92, cam ring 90 also defines axially extending discharge chambers 94. Still further,
the outer periphery 96 of the cam ring 90 also includes a plurality of access slots
108 which are used to enable the formation of radially extending ports 104/106 which
extend through the inner wall 102 of the cam ring 90 to the pumping chamber surface
35. Ports 104 extend radially inward from the inlet chambers 92 and ports 106 extend
radially inward from the discharge chambers 94. The purpose of the flow ports 104/106
will also be discussed below.
[0069] The cam ring 90 is also provided with a number of seal grooves. For example, the
outer periphery 96 of the cam ring 12 includes a plurality of seal grooves 98 which
are adapted and configured for receiving linear sealing elements. Each end of the
cam ring 90 also includes a circular seal groove 99 and the pumping chamber surface
35 includes front and rear circumferential seal grooves 97. Those skilled in the art
will readily appreciate the seals inserted into the seal grooves 97/98/99 are designed
to prevent cross port leakage throughout the pump assembly 10.
[0070] Referring now to FIGS. 12 through 15 where there is illustrated floating wear disk
50. As shown in FIG. 19, unlike prior art wear disks, which are fixedly positioned
outside and adjacent to the end of the cam ring, floating wear disk 50 is positioned
entirely within the inside profile of the cam ring 90 and is adapted for sliding in
an axial direction to allow for thermal expansion of the rotor assembly during operation.
However, unlike prior art devices wherein the axial gap between the wear disk and
the rotor must be minimized in order to prevent cross port leakage, in pump assembly
10 it is the circumferential gap between the floating wear disk 50 and the pumping
chamber surface which must be sealed. Since the circumferential gap is much less impacted
by thermal expansion during operation of the pump, it is easier to maintain the seal
in this location.
[0071] Like cam ring 90, floating wear disk 50 includes a plurality of fluid ports which
allow fluid to communicate with pump assembly 10. For example, eight radial holes
52 are provided which extend from the outer periphery of the floating wear disk 50.
Four of the radial holes 52 connect with four axially extending discharge fluid ports
54 and the other four radial holes 52 connect with four axially extending inlet fluid
ports 56. As will be discussed in detail below, the discharge fluid ports 54 are used
to allow pressurized discharge fluid to be provided to the under-vane slots and under-vane
passages to used for under-vane pumping and the inlet fluid ports 56 are used to allow
low pressure inlet fluid to be provided to the under-vane slots and under-vane passages
to be used for under-vane pumping.
[0072] The floating wear disk 50 is also provided with a journal bearing 58 which supports
one end of the rotor assembly 70 within the pumping chamber 52. Four seal grooves
53 are provided on the rear face of the floating wear disk 50 and are adapted for
receiving a face seal, Additionally, eight spring cavities 55 are formed in the rear
face of the floating wear disk 50 and contain a spring element or biasing mechanism
for urging the floating wear disk 50 in the direction of the rotor assembly 70. Moreover,
a small hole 59 extends from each of the discharge fluid ports 54 to the rear face
of the floating wear disk 50. As a result, pressurized discharge fluid is supplied
to the back side of the floating wear disk 50 and further urges/biases the floating
wear disk 50 in the direction of the rotor assembly 70. The configuration and location
of the seal grooves 53 defines a load area against which the pressurized discharge
fluid works in order to urge the floating wear disk 50 towards the rotor assembly
70. As a result, the amount of pressure applied to the back side of the wear disk
50 can be adjusted by adjusting the load area upon which the discharge fluid works.
[0073] Referring now to FIGS. 16 through 18 which illustrate the fixed side wear disk 60
used in the pump assembly 10 of the present invention. Like the floating wear disk
50, the fixed side wear disk 60 includes a journal bearing 68 and a plurality of radial
holes 62. Four axially extending discharge fluid ports 64 communicate with four of
the radial holes 62 and four radially extending inlet fluid ports 66 communicate with
the remaining four radial holes 62. Similar to the floating wear disk 50, discharge
fluid ports 64 and inlet fluid ports 66 are used to provide fluid in support of under-vane
pumping.
[0074] The back side of the fixed side wear disk 60 includes circular pressure relief groves
67a/67b and four radially extending pressure relief grooves 69a-d. It should be noted
that both the floating side wear disk and the fixed side wear disk include slots for
receiving a pin which prevents the disks 50/60 from rotating with respect to the cam
ring 90.
[0075] Referring now to FIGS. 19 through 23 which illustrate the arrangement of the component
parts used in pump assembly 10 and the manner in which the pump assembly operates
to increase the pressure of the inlet fluid. In operation, fluid is received in inlet
port 24 and is diverted into the four inlet channels 84. The four inlet channels 84
provide the fluid to the four axially extending inlet chambers 92 formed in the cam
ring 90. From the inlet chambers 92 the fluid is directed radially inward through
the radially extending inlet ports 104. The end two ports 104 provide fluid to four
radial holes 52/62 formed in the wear disks 50 and 60 respectively, and this fluid
is used for under-vane pumping. The fluid proceeding through the remaining ports 104
formed in the cam ring 90 is supplied into vane buckets 44 which are in the four inlet
arc regions "I" shown in FIG. 23. As the rotor assembly 70 rotates the fluid is displaced
and exits the vane buckets 44 in the discharge arc region "D" through the interior-most
ports 106 formed in the cam ring 90 and is received into the four axially extending
discharge chambers 94. A portion of the pressurized fluid contained in the discharge
chamber 94 is provided to the discharge fluid ports 54/64 of the wear disks 50/60
via radial holes 52/62 and is used for under-vane pumping. The remaining pressurized
fluid contained with the four axially extending discharge chambers 94 formed in the
cam ring 90 is provided to the four discharge ports 30a-d of the pump assembly 10.
[0076] FIG. 19 is sectional view of the pump assembly shown in FIG. 1 which illustrates
that when the vanes 36 are within the seal are "S", the under-vane slot 75 and the
under-vane passage 73 are connected to pump discharge passages which are formed in
the wear disks 50/60 and the cam ring 90. FIG. 20 is a cross-sectional view of the
pump assembly shown in FIG. 1 taken along cut line 20-20 in FIG. 19.
[0077] FIG. 21 is sectional view of the pump assembly shown in FIG. 1 which illustrates
that when the vanes 36 are within the discharge ramp/are "D", the over-vane 44 and
under-vane cavities 73/75/77 are connected to pump discharge passages which are formed
in the wear disks 50/60 and the cam ring 90.
[0078] Lestly, FIG. 22 is sectional view of the pump assembly shown in FIG. 1 which illustrates
that when the vanes 36 are within the inlet ramp/are "I", the over-vane and under-vane
cavities are connected to pump inlet passages which are formed in the wear disks 50/60
and the cam ring 90.
[0079] Typically, in prior art vane pumps, the wear disks are fixedly mounted within the
interior pumping chamber and abut the axial ends of the cam ring and rotor blade.
As shown in these figures, the front side wear disk 50 is a floating wear disk which
is located radially inside of the pumping chamber surface 35 defined by the cam ring
90.
[0080] Previously disclosed vane pump designs usually have a fixed axial clearance between
the wear disk and the rotor. Moreover, the wear plates/disks at both side of the rotor/vane
are fixed. For a fixed axial clearance design, the longer the rotor, the more axial
clearance is needed considering free thermal expansion of the rotor and vanes. At
high operating temperatures, the amount of available clearance between the rotor and
wear disks could be significantly reduced due to rotor/vane expansion. As a result,
mechanical galling and premature wear could occur at rotor ends if the axial clearance
is not sufficient
[0081] Moreover, as discussed previously, cross-port leakage occurs due to above described
fixed axial clearance. Excessive leakage could then take place at high pump operating
pressures. This leakage could have significant effect on the minimum allowable operation
speed of the pump, in addition to significant energy loss of the pump. In other terms,
the pump could have little or no discharge flow due to its excessive internal re-circulated
cross-port leakage at a low input speed.
[0082] Therefore, it is preferred to have a vane pump with at least one pressure compensated
side wear disk. In the present invention, during pump operation, the pressure overbalanced
side wear disk 50 is subject to a net clamping force that pushes the wear disk against
the rotor/vanes (rotating group) tightly. This net force comes from mechanical spring
force and/or hydraulic pressure acting on the back side of the floating wear disk
50 at the side opposite to the rotor 70. Usually, the higher the operating pressure,
the higher the net clamping force. In a pump of good design, the clamping force closes
the axial gap and squeezes the oil film between rotor and the wear disk to a minimum
film thickness without mechanical contact between two parts that rotate close to each
other.
[0083] To allow the floating wear disk 50 to move freely inside the cam ring 90 as a result
of the above described net biased force, the outer shape of the wear disk 50 generally
has the same shape (with adequate radial clearance for free relative movement) as
the inner pumping chamber surface 35 of the cam ring 90. Thus, the floating wear disk
50 requires precision manufacturing similar to the cam ring inner diameter 35.
[0084] Typically, the inner pumping chamber surface of a cam ring has an elliptical shape
for a single balance (dual action) fixed displacement vane pump. As shown in FIG.
23, in the present invention, the cross-section of the inner pumping chamber surface
35 is close to a circle because it has two balanced pumps in a same pumping element.
Alignment pins could be used to ensure proper orientation of the wear disk and the
cam profile.
[0085] Those skilled in the art will readily appreciate that the fixed side wear disk 60
could also be a floating wear disk if cost is not a concern. Preferably, both disks
50/60 are made of steel, alumiaum, or other light weight materials for weight reduction
and have hard coated layers applied on the wear surfaces (rotor side). It also should
be appreciated that the back side of the floating wear disk 50 is connected to corresponding
pump discharge pressure all the time.
[0086] When a rotor rotates, vanes are expected to maintain contact with the inner surface
of the cam ring. Since the inner surface of the cam ring has a varying radius at different
angular positions, each vane, which behaves as a piston, will slide into and out of
the rotor inside the rotor vane slot. This radial movement of the vane stokes fluid
into and out the cavity beneath it. To let each vane work as a positive displacement
piston pump, a porting device is needed. The porting device assures that when the
cavity volume increases, the under-vane pumping passages are linked to a pump inlet
pressure; and conversely, when the bucket volume is reduced, the under-vane pumping
passages are linked to its corresponding pump discharge line.
[0087] Conventional vane pumps usually incorporate flow passages that directly connect an
under-vane cavity to corresponding over-vane volume chambers. Thus, under-vane cavities
can be linked to the inlet and discharge ports of the pump at the same time as their
corresponding over-vane volume chambers. Those flow passages could be inside the rotor
or use the interface between rotor and the side wear plate. The disadvantage of the
conventional design is that there are significant dynamic pressure losses along and
through the flow passages and cavitation damage could result in these areas when the
pump is operated at very high speed.
[0088] Vane pump assembly 10 provides a separate porting mechanism to link inlet and discharge
ports of each pump (over-vane) to its corresponding under-vane cavities. When a cavity
volume increases, it is linked to pump inlet pressure. When the cavity is reduced,
it is linked to a corresponding discharge line.
[0089] Over vane volume chambers (16 total for pump assembly 10) are separated by vane/cam
sealing. As shown in FIG. 19 when a vane 36 is sweeping on the seal arc "S" (the constant
radius portion of the cam ring profile located between inlet and discharge ports),
its under-vane passage 73 and under-vane slot/pocket 75 are linked to a pump discharge
pressure port to assure that the vane 36 can be pushed out by under-vane hydraulic
pressure forces. When a vane 36 is sweeping on the inlet ramp "I", as shown in FIG.
22, its under-vane passage 73 and under-vane slot 75 are connected to inlet pressure.
When a vane 36 is sweeping the discharge ramp, as shown in FIG. 21, its under-vane
passage 73 and under-vane slot 75 are connected to its corresponding discharge line.
As a result, the pressure ports on the wear disks are longer in the circumferential
direction in the discharge ports 54/64 than the inlet ports 56/66.
[0090] As discussed previously, there are radial holes 52/62 on the outer surfaces of the
wear disks 50/60. Those radial holes 52/62 are used to connect the under-vane passage
73 and under-vane slot 75 (for under-vane pump porting) to pump inlet lines 92 and
discharge lines 94, which are integrated into the cam ring 90.
[0091] Vanes pump under-vane cavity fluid at very rapid speed. To avoid excessive pressure
build up or de-compression due to resistance of the under-vane cavities and flow passages,
unlike a conventional design, which has only one axial slot to connect under-vane
cavity to pump system ports or over-vane volume chamber, the pump assembly 10 has
both an under-vane passage 73 and an under-vane slot 75 for a single under-vane pumping
element. This arrangement reduces the pressure loss inside the under-vane cavity and
flow passages.
[0092] The outer axial slot 75 is a primary one and the inner axial passage 73 is the second
link to under-vane cavities and pump ports. The second passage 73 is linked to the
primary slot inside the rotor via a number of radial connector passages 77. Those
radial connector passages 77 are slanted with an angle to reduce the energy loss of
merging flow.
[0093] As will be readily appreciated, pump assembly 10 is a split discharge pump and is
essentially a main fuel pump that consists of four separate pumps. Each pump can discharge
flow both from over-vane volume chambers and under-vane volume chambers. All volume
chambers need separate timely porting to assure volume chambers are connected to an
inlet line when their volume is expanding and connected to a pump discharge line when
its volume is contracting.
[0094] As discussed above, the cam ring 90 is designed to receive fluid from a common pump
inlet 24 (four pumps share the same pump inlet) and it ports it to the inlet ports
56/66 of the wear disk, along with performing porting for the over-vane volume chambers.
In addition, it receives discharge flow from the wear plates 56/60 and combines the
flow with corresponding over-vane discharge flow and then provides for discharge from
one of the four corresponding discharge ports 94 in the cam ring.
[0095] To assure the minimum timing error for over-vane porting, the angular location of
the ports on the inner surface of the cam ring is very critical and requires precision
manufacturing. To reduce the manufacturing cost, these ports are machined from the
outer surface of the cam ring 90. When the cam ring is inserted into its housing/annular
space 16, some construction openings on the outer surface will be covered by the inner
surface of the annular spacer 16. As discussed previously, multiple seal cords are
used to seal circumferential cross-port leakage between the cam ring and the housing.
[0096] Those skilled in the art will readily appreciate that the cam ring 90 could have
been designed differently with multiple pieces for ease of manufacturing. For instance,
a hardened sleeve/ring could be used as vane running wear surface and inserted into
a separate block inclusive of the flow ports, thereby simplifying manufacturing of
the cam running surface and the flow passages.
[0097] Moreover, unlike prior vane pump constructions, vane pump assembly 10 includes single
inlet port 24 oriented in the axial direction and multiple discharge ports 30a-30d
oriented in the radial direction. There are a total four vane pumps for this split-discharge
vane pump. All four pumps share the same pump inlet volume. For each pump, the over-vane
volume chamber discharges flow into the cam ring. There, flow merges with the discharge
flow from its corresponding under-vane cavity. Then, the total flow is expended from
the pump from a pump discharge port. There are total of four discharge ports, one
for each pump.
[0098] To form two balanced dual action vane pumps, the flow from two diagonally opposite
discharge ports of the main pump could be combined by external plumbing. Alternatively
the two ports could be linked internally inside a main pump housing by design, along
with necessary control valves, as illustrated in
U.S. Patent Application Publication No. 2010/0316507, the disclosure of which is incorporated by reference.
[0099] While the subject invention has been described with respect to preferred embodiments,
those skilled in the art will readily appreciate that changes and modifications may
be made thereto without departing from the spirit and scope of the subject invention
as defined by the appended claims.
1. A hydraulic vane pump, comprising:
a) a pump body including an interior pumping chamber and defining an inlet port for
allowing fluid to be provided to the interior pumping chamber and at least one discharge
port for allowing pressurized fluid to be discharged from the interior pumping chamber,
b) a cam ring disposed within the interior pumping chamber and defining a continuous
peripheral cam surface;
c) rotor mounted for axial rotation within the interior pumping chamber and defining
a pump axis;
d) a plurality of circumferentially spaced apart radially extending vanes mounted
for radial movement within slots formed in the rotor, the plurality of vanes defining
an equal number of circumferentially spaced apart volume chambers which extend between
an outer periphery of the rotor and the cam surface for carrying pressurized fluid;
and
e) axially opposed first and second wear disks disposed within the interior pumping
chamber, the first wear disk having an outer periphery which is positioned radially
inward of the cam surface and is adapted and configured to slide axially with respect
to the cam surface, so as to provide for thermal expansion of the rotor and vanes,
and the second wear disk being positioned adjacent to a second end surface of the
rotor.
2. A hydraulic vane pump as recited in Claim 1, wherein the vane pump is a multi-discharge
hydraulic vane pump and the pump body defines four radially-oriented discharge ports,
each port allowing pressurized fluid to be discharged from the interior pumping chamber.
3. A hydraulic vane pump as recited in Claim 1, wherein at least one of a) and b):-
a) the first wear disk is biased towards the first end surface of the rotor using
a spring element towards the first end surface of the rotor;
b) the first wear disk is biased towards the first end surface of the rotor using
pressurized fluid discharged from the volume chambers defined by the vanes.
4. A hydraulic vane pump as recited in Claim 1, wherein the pump body further includes
a rear housing plate and the inlet port extends axially through the rear housing plate
to the interior chamber.
5. A hydraulic vane pump as recited in Claim 1, wherein the cam surface includes four
quadrantal cam segments, wherein diametrically opposed cam segments have identical
cam profiles, and each cam segment defines an inlet arc, a discharge are and two seal
arcs.
6. A hydraulic vane pump as recited in Claim 5, wherein at least one of a) and b):-
a) the cam ring includes a plurality of inlet chambers arranged and configured to
receive fluid from the inlet port and distribute the fluid to the inlet arc of each
cam segment;
b) the cam ring includes a plurality of discharge chambers which communicate with
the discharge arc of each cam segment and are arranged and configured to facilitate
the discharge of pressurized fluid from the interior pumping chamber.
7. A hydraulic vane pump as recited in Claim 1, wherein each vane slot has an under-vane
pocket for receiving fluid and the pressure of the undervane pocket is dependent on
an angular position of the rotor.
8. A hydraulic vane pump as recited in Claim 7, wherein the rotor includes a plurality
of axially-extending under-vane passages, each under-vane passage communicating with
an under-vane pocket through a connector passage, and
optionally:-
each wear disk includes flow passages for communicating fluid into the under-vane
pockets and under-vane passages associated with each vane slot and the pressure of
the undervane pocket is dependent on an angular position of the rotor.
9. A hydraulic vane pump as recited in Claim 7, wherein at least one of a) and b):-
a) the pressure of the fluid in the rotor under-vane passage whilst positioned in
the inlet arc segment is about equal to pump inlet pressure;
b) the pressure of the fluid in the rotor under-vane passage whilst positioned in
the discharge arc segment is about equal to pump discharge pressure.
10. A hydraulic vane pump as recited in Claim 5, further comprising a fluid metering system
for extracting fluid flow from the discharge arcs of the four cam segments.
11. A hydraulic vane pump as recited in Claim 10, wherein at least one of a) and b):-
a) the fluid metering system has a first operating condition in which fluid is extracted
from the discharge arcs of all four cam segments and combined for delivery to a source
of fluid demand;
b) the fluid metering system has a second operating condition wherein fluid is extracted
from a first pair of diametrically opposed discharge arcs for delivery to a source
of fluid demand and fluid from a second pair of diametrically opposed discharge arcs
bypasses the source of fluid demand and returns to the pumping chamber.
12. A multi-discharge hydraulic vane pump, comprising:
a) a pump body including an interior pumping chamber and defining a axially extending
inlet port for allowing fluid to be provided to the interior pumping chamber and four
discharge ports for allowing pressurized fluid to be discharged from the interior
pumping chamber;
b) a cam ring disposed within the interior pumping chamber and defining a continuous
peripheral cam surface;
c) rotor mounted for axial rotation within the interior pumping chamber and defining
a pump axis;
d) a plurality of circumferentially spaced apart radially extending vanes mounted
for radial movement within slots formed in the rotor, the plurality of vanes defining
an equal number of circumferentially spaced apart volume chambers which extend between
an outer periphery of the rotor and the cam surface for carrying pressurized fluid;
and
e) axially opposed first and second wear disks disposed within the interior pumping
chamber.
13. A multi-discharge hydraulic vane pump as recited in Claim 12, wherein the first wear
disk has an outer periphery which is positioned radially inward of the cam surface
and is mounted for sliding movement with respect to the cam surface, so as to provide
for thermal expansion of the rotor and vanes, and the second wear disk being positioned
adjacent to a second end surface of the rotor.
14. A multi-discharge hydraulic vane pump as recited in Claim 13, wherein at least one
of a) and b);-
a) the first wear disk is biased towards the first end surface of the rotor using
a spring element towards the first end surface of the rotor;
b) the first wear disk is biased towards the first end surface of the rotor using
pressurized fluid discharged from the volume chambers defined by the vanes.
15. A multi-discharge hydraulic vane pump as recited in Claim 12, wherein at least one
of a) and b):-
a) the pump body further includes a rear housing plate and the inlet port extends
axially through the side plate towards the interior chamber;
b) the cam surface includes four quadrantal cam segments, wherein diametrically opposed
cam segments have identical cam profiles, and each cam segment defines an inlet are,
a discharge arc and two seal ares.
16. A multi-discharge hydraulic vane pump as recited in Claim 12, wherein:-
the cam ring includes a plurality of inlet chambers arranged and configured to receive
fluid from the inlet port and distribute the fluid to the inlet are of each cam segment;
and/or
the cam ring includes a plurality of discharge chambers which communicate with the
discharge are of each cam segment and are arranged and configured to facilitate the
discharge of pressurized fluid from the interior pumping chamber; and/or
17. A multi-discharge hydraulic vane pump as recited in Claim 12, wherein each vane slot
has an under-vane pocket for receiving fluid and the pressure in the undervane pocket
is dependent on an angular position of the rotor.
18. A multi-discharge hydraulic vane pump as recited in Claim 17, wherein the rotor includes
a plurality of axially-extending under-vane passages, each under-vane passage communicating
with an under-vane pocket through a connector passage, and
optionally:-
each wear disk includes flow passages for communicating fluid into the under-vane
pockets and under-vane passages associated with each vane slot based and the pressure
of the undervane pocket is dependent on an angular position of the rotor.
19. A multi-discharge hydraulic vane pump as recited in Claim 17, wherein at least one
of a) and b):-
a) the pressurized fluid in the rotor under-vane pocket whilst positioned in the inlet
are segment is about equal to pump inlet pressure;
b) the pressurized fluid in the rotor under-vane pocket whilst positioned in the discharge
arc segment is about equal to pump discharge pressure.
20. A multi-discharge hydraulic vane pump as recited in Claim 15, further comprising a
fluid metering system for extracting fluid flow from the discharge ares of the four
cam segments.
21. A multi-discharge hydraulic vane pump as recited in Claim 20, wherein at least one
of a) and b):-
a) the fluid metering system has a first operating condition in which fluid is extracted
from the discharge arcs of all four cam segments and combined for delivery to a source
of fluid demand;
b) the fluid metering system has a second operating condition wherein fluid is extracted
from a first pair of diametrically opposed discharge ares for delivery to a source
of fluid demand and fluid from a second pair of diametrically opposed discharge arcs
bypasses the source of fluid demand and returns to the pumping chamber.
22. A hydraulic vane pump, comprising:
a) a pump body including an interior pumping chamber and defining an inlet port for
allowing fluid to be provided to the interior pumping chamber and at least one discharge
port for allowing pressurized fluid to be discharged from the interior pumping chamber;
b) a cam ring disposed within the interior pumping chamber and defining a continuous
peripheral cam surface, the cam ring also defining a plurality of inlet chambers and
discharge chambers, the inlet chambers being arranged and configured to receive fluid
from the inlet port and to distribute the fluid to the interior pumping chamber, the
discharge chambers communicating with the interior pumping chamber and are arranged
and configured to facilitate the discharge of pressurized fluid from the interior
pumping chamber;
c) a rotor mounted for axial rotation within the interior pumping chamber and defining
a pump axis;
d) a plurality of circumferentially spaced apart radially extending vanes mounted
for radial movement within slots formed in the rotor, the plurality of vanes defining
an equal number of circumferentially spaced apart volume chambers which extend between
an outer periphery of the rotor and the cam surface for carrying pressurized fluid,
wherein each vane slot has an under-vane pocket for receiving pressurized fluid based
on an angular position of the rotor, and
e) axially opposed first and second wear disks disposed within the interior pumping
chamber, the first wear disk having an outer periphery which is positioned radially
inward of the cam surface, and is axially biased towards a first end surface of the
rotor so as to provide for thermal expansion of the rotor and vanes and the second
wear disk being positioned adjacent to a second end surface of the rotor.
23. The hydraulic vane pump as recited in Claim 22, wherein each wear disk includes flow
passages for feeding fluid into the under-vane pockets associated with each vane slot
and the pressure of the undervane pocket is dependent on an angular position of the
rotor.