Information
-
Patent Grant
-
6547531
-
Patent Number
6,547,531
-
Date Filed
Wednesday, January 16, 200222 years ago
-
Date Issued
Tuesday, April 15, 200321 years ago
-
Inventors
-
-
Examiners
Agents
-
CPC
-
US Classifications
Field of Search
US
- 060 449
- 060 452
- 092 122
- 417 63
- 417 2221
- 417 269
-
International Classifications
-
Abstract
A conventional variable-displacement, axial piston-type hydraulic fluid pump having a pump housing is provided with co-operating pump rotational speed, thrust plate position, and working pressure operating-condition sensor assemblies that are partially contained within the pump housing, that are partially contained within a separate position sensor housing which is removably secured to the pump housing, and that are sealed against high-pressure fluid leakage using only static resilient fluid pressure seals.
Description
CROSS-REFERENCES
None
FIELD OF THE INVENTION
This invention relates generally to fluid pumps, and particularly concerns an improved variable-displacement axial piston pump that advantageously achieves reduced auxiliary sensor fluid leakage over prolonged periods of pump operating life, and that also facilitates efficient pump assembly operations.
BACKGROUND OF THE INVENTION
It has become increasingly important that the pump component of high-pressure hydraulic systems include one or more sensors that continuously monitor the status of pump operation. In the case of high-pressure hydraulic systems utilizing a variable-displacement, axial piston-type pump it is common practice to measure pump volumetric pumping rate by sensing both pump rate of rotation and pump thrust plate angular position. In addition it has been common practice to also provide the variable-displacement, axial piston-type pump component of the hydraulic system with included pressure sensors that monitor pump output (working) pressure and pump load pressure with the latter being a feedback pressure utilized for effecting control of the relative angular position of the pump thrust plate element.
Heretofore, it also has been common practice to utilize both dynamic and static resilient pressure seals in connection with mounting the different pump operating condition sensors on the pump with the dynamic resilient seals being in contact with sensor rotating elements and thus subjected to wear erosion and consequent fluid leakage over extended periods of pump operation.
It is therefore a primary objective of the present invention to provide a variable-displacement, axial piston-type hydraulic pump with an installation of multiple sensors that utilizes static resilient pressure seals exclusively.
It also is an objective of the present invention to provide a variable-displacement, axial piston-type hydraulic pump with multiple sensors that may be efficiently constructed and installed in the pump.
Other objectives of the invention will become apparent from consideration of the detailed descriptions, drawings, and claims which follow.
SUMMARY OF THE INVENTION
The instant hydraulic pump invention essentially is comprised of a conventional variable-displacement hydraulic fluid pump contained within a pump housing and of co-operating pump operating-condition sensor assemblies contained partially within the pump housing and partially within a separate position sensor housing that is removably secured to the pump housing. The hydraulic fluid pump includes multiple variable-stroke fluid-pumping pistons contained within a rotationally-driven pump barrel, an angularly-adjustable piston thrust plate co-operating with the fluid-pumping pistons to vary pump volumetric output, and various conventional internal fluid passageways.
The co-operating pump operating-condition sensor assemblies include a piston thrust plate position sensor assembly responsive to pump thrust plate position changes, a pump barrel rotational speed sensor assembly, and a pump working or output pressure sensor assembly. Advantageously, the installation of pump operating-condition sensor assemblies may optionally include a pump load feedback pressure sensor assembly. In each instance only a static (i.e., non-eroded) resilient pressure seal is utilized to seal the pump and position sensor assembly housings against fluid leakage from around the sensor body.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
is a perspective view of a rocker cam type pump which incorporates a preferred embodiment of the instant invention looking at the pump intake and discharge ports;
FIG. 2
is a perspective view of the pump of
FIG. 1
with the pump housing removed to illustrate the pump variable-position rocker cam and other internal parts;
FIG. 3
is an axial sectional view of the
FIG. 1
pump taken at lines
3
—
3
of
FIG. 2
;
FIG. 4
is a side view, partially sectioned, of the pump of
FIG. 1
;
FIG. 5
is a section view taken at line
5
—
5
of
FIG. 4
;
FIG. 6
is a section view taken at line
6
—
6
of
FIG. 5
;
FIG. 7
is a section view taken at line
7
—
7
of
FIG. 5
; and
FIG. 8
is a section view taken at line
8
—
8
of FIG.
6
.
DESCRIPTION OF THE PREFERRED EMBODIMENT
FIGS. 1 through 4
of the drawings disclose construction details of a typical pressure-compensated, variable displacement, axial piston pump
10
to which the present invention has found application. Pump
10
has a rocker cam pivotally mounted in a cam support or cradle may be seen to include a central pump housing
12
, having a mounting pilot end
14
and a port cap
16
at the other end. Bolts
17
connect port cap
16
to housing
12
.
Housing
12
defines a cavity which houses a rotatable barrel
18
mounted on a drive shaft
20
. The inner end of drive shaft
20
is supported in a bearing
22
mounted in the port cap
16
. Drive shaft
20
also is supported in a bearing
24
mounted within pump housing
12
and has a splined drive end
26
which projects outwardly of pump housing
12
.
Barrel
18
has a plurality of bores
28
equally spaced circumferentially about its rotational axis. Each bore
28
contains a piston
30
having a ball shaped head
32
. A shoe
34
is swaged onto head
32
of piston
30
such that the shoe can pivot about the end of the piston. Each of the shoes is clamped against a flat thrust plate or swash plate surface
36
formed on the face of a pivotal rocker cam
38
utilizing a conventional shoe retainer assembly of the type described in detail in U.S. Pat. No. 3,904,318 assigned to the predecessor in interest of the assignee of the subject invention.
Turning to
FIGS. 2 through 4
, it may be seen that rocker cam
38
has a pair of arcuate bearing surfaces
40
which are received in complementary arcuate bearing surfaces
42
which comprise a rocker cam support or cradle
44
formed in mounting pilot end
14
in pump housing
12
. Rocker cam
38
pivots about a fixed axis perpendicular to the axis of rotation of barrel
18
to change the displacement of pump
10
. In operation, the prime mover, not shown, affixed to spline drive end
26
rotates drive shaft
20
and barrel
18
within pump housing
12
. When thrust surface
36
on the rocker cam
38
is perpendicular to the axis of rotation of barrel
18
, rotation of barrel
18
will cause the shoes to slide across the surface of thrust surface
36
but no pumping action will occur inasmuch as the pistons
30
will not reciprocate within bores
28
. In other words, when thrust surface
36
is perpendicular to the axis of drive shaft
20
, the pump is in a position of minimum fluid displacement. As rocker cam
38
and thrust surface
36
are inclined from this position, the pistons
30
will reciprocate within bores
28
as shoes
34
slide over the surface of thrust plate
36
. As the pistons
30
move inwardly of bores
28
i.e. away from port plate
46
, low pressure fluid is drawn into cylinder bores
28
from inlet port
48
. As piston shoes
34
slide across thrust surface
36
and move toward port plate
46
, high pressure fluid is expelled through outlet port
50
. It should be noted that fluid displacement increases as the angle of inclination of thrust surface
36
increases.
Referring to
FIG. 3
, it may be seen that rocker cam
38
and thrust surface
36
are shown in a position of maximum fluid displacement. Rocker cam
38
may be pivoted clockwise to reduce the displacement of pump
10
. Although, pump
10
of the instant invention embodiment is depicted as a pressure-compensated pump which does not cross center, the instant invention described below applies equally to a rocker cam type variable displacement axial piston where rocker cam
38
may be pivoted clockwise across center such that the intake and exhaust ports are reversed and the device is providing maximum fluid displacement in the opposite direction. Such a pump may be seen in U.S. Pat. No. 5,076,145 assigned to the predecessor in interest of the subject invention. The instant invention also applies equally to a rocker cam type, variable displacement pump having a rotary servo or linear servo type control.
In the instant embodiment, in which pump
10
is depicted as a pressure compensated device, a piston
52
is slidably mounted in a bore
54
formed in a cylinder
56
rigidly mounted within port cap
16
. A spring
58
around cylinder
56
biases piston
52
against a button
60
mounted on one side of rocker cam
38
to force the rocker cam to pivot to a position of maximum fluid displacement. A stroking piston
62
is slidably mounted in a bore
64
of a cylinder
66
rigidly secured in port cap
16
at a position within pump housing
12
diametrically opposite that of biasing piston
52
. Stroking piston
62
engages a button
68
mounted in rocker cam
38
at a position diametrically opposite that of button
60
.
In a pressure-compensated pump it is necessary to reduce the displacement of the pump when the pressure of the discharge fluid becomes excessive. When this condition occurs, pressure fluid is supplied to the end of stroking piston
62
to force it to move outwardly of bore
64
and thereby cause rocker cam
38
to pivot clockwise (as viewed in
FIG. 3
) towards a position of reduced fluid displacement. Stroking piston
62
will continue to pivot rocker cam
38
until such time as the discharge pressure of working fluid falls below a maximum setting. When this occurs, pressure fluid no longer is supplied to stroking piston
62
and biasing spring
58
moves stroking piston
62
outwardly to thereby pivot rocker cam
38
in a counterclockwise direction and thereby increase the displacement of the pump. Inasmuch as the instant invention is for any type of rocker cam type pump independent of its displacement control, a further description of the pressure compensated mechanism of pump
10
is not required.
As mentioned above, when rocker cam
38
is pivoted counterclockwise sufficiently to cause working pressure fluid to be expelled from pump
10
at a relatively high pressure, large pumping forces are exerted through pistons
30
to rocker cam
38
. These forces are transmitted through the complementary arcuate bearing surfaces
40
and
42
into rocker cam support
44
. The large pumping forces cause large friction forces to occur at the interface of rocker cam bearing surfaces
40
and rocker support bearing surfaces
40
and rocker support bearing surfaces
42
to make movement of rocker cam
38
within rocker support
44
very difficult. In an attempt to reduce the friction forces between rocker cam
38
and rocker support
44
plain bushings
70
are inserted between rocker cam arcuate bearing surfaces
40
and rocker support arcuate bearing surfaces
42
as depicted in FIG.
4
. While plain bushings
70
reduce the aforementioned frictional forces to some extent, they are inadequate by themselves to reduce the frictional forces to a satisfactory level.
Accordingly, working pressure fluid is supplied to counterbalance pockets
72
and
74
formed in the rear faces
76
of rocker cam
38
as depicted in FIGS. in
2
and
4
. The areas of the counterbalance pockets
72
and
74
are designed such that when they receive working pressure fluid they reduce the force required to pivot rocker cam
38
within cam support
44
to within desirable levels. Heretofore, working pressure fluid has been supplied to counterbalance pockets in rocker cam where the working pressure fluid source is a pumping piston and fluid is supplied to the piston shoe and thereafter to bores in the thrust plate which bores connect to the counterbalance pockets.
Pump
10
has a unique means for supplying working pressure fluid to the counterbalanced pockets
72
and
74
formed in the rear face
76
of rocker cam
38
where the fluid source is in pump housing
12
.
Turning to the
FIG. 4
, it may be seen that a fluid passage
78
connected to a source, not shown, of working pressure fluid is formed in pump housing
12
. Fluid passage
78
opens into fluid passage
80
formed in pump housing
12
, one end of which is closed by a plug
82
which may be replaced with a sensor or other device utilizing working pressure fluid for control purposes.
A hollow roll pin
84
is mounted in a central bore of plain bushing
70
, in cam support arcuate bearing surface
42
and in a corresponding bore in housing
12
. Roll pin
84
serves two purposes. It anchors plain bushing
70
on cam support or cradle
44
and it intersects fluid passage
80
to thereby connect that passage to a fluid passage
86
formed in rocker cam
38
and in arcuate cam surface
40
. Fluid passage
86
intersects an angled fluid passage
88
formed in rocker cam
38
. Fluid passage
88
intersects an oppositely angled passage
92
. The fluid passage
96
which parallels fluid passage
86
has one end which intersects fluid passage
92
at a right angle and another end which opens into fluid pocket
74
formed in rear face
76
of rocker cam
38
. Turning to
FIG. 4
, it may be seen that a roll pin
98
anchors plain bushing
70
to cam support surface
44
.
As indicated initially, the present invention includes an installation of sensor assemblies, designated
100
in the drawings, which is combined with pump
10
to facilitate the measurement of pump operating performance. A pump control block
101
overlies and is electrically connected to said sensor assemblies
100
. The sensor assembly installation preferably includes a pump output or working fluid pressure sensor assembly
102
, a pump rate of rotation sensor assembly
104
, a pump piston thrust plate cam angular position sensor assembly
106
, and, optionally, a load fluid pressure sensor assembly
108
that senses the magnitude of a system feedback pressure utilized for adjustment control of the piston thrust plate angular position. Such sensor assemblies are partially contained within position sensor housing
110
(which in turn is removably secured to pump housing
12
using the screw fasteners referenced by the numeral
112
), and are partially contained within pump housing
12
using circular static fluid pressure seals
114
exclusively. Such static fluid pressure seals are preferably “O-ring”-type resilient synthetic rubber fluid pressure seals that surround and are compressed against included non-rotating sensor assembly body elements or housing elements to thereby eliminate leakage of high-pressure hydraulic fluid that would otherwise potentially arise out of seal wear due to seal erosion.
Although various different types of position, speed, and pressure sensors may be incorporated in the present invention, the drawings illustrate only conventional forms of such devices. Specifically, speed sensor
104
is a conventional, Hall-effect type of electromagnetic sensor that detects uniformly-spaced blind hole discontinuities
116
provided in the surface of pump barrel element
18
, and provides output pulses that are used in pump rotation rate and volumetric pumping rate computations. Position sensor
106
also is a Hall-effect electromagnetic sensor with the included permanent magnets. The spaced and position sensors
104
and
106
may be any type of electromagnetic sensors. Fluid pressure sensors
102
and
108
are conventional strain gage bridge type devices.
Various changes in size, proportions, or material of construction may be incorporated into the different invention elements described herein without departing from the meaning, scope, or intent of the claim which follows.
Claims
- 1. In a variable-displacement hydraulic pump having a pump housing and having contained within the pump housing a rotationally-driven pump barrel, multiple, variable stroke, fluid-pumping pistons contained within the rotationally-driven pump barrel, and an angularly-positioned piston thrust plate that co-operates with the fluid-pumping pistons, in combination:a position sensor housing removably secured to the pump housing; an electromagnetic position sensor assembly partially contained within said position sensor housing, partially contained within the pump housing; an electromagnetic rotational speed sensor assembly partially contained within said position sensor housing, partially contained within the pump housing, and positioned to sense surface discontinuities in the rotationally-driven pump barrel; a hydraulic fluid pressure sensor assembly partially contained within said position sensor housing; and multiple resilient fluid pressure seals engaging only static surfaces of each said sensor assemblies, said electromagnetic position sensor assembly, said electromagnetic rotational speed sensor assembly, and said hydraulic fluid pressure sensor assembly each having a respective static resilient pressure seal that is compressed sufficiently to preclude the leakage of pressurized hydraulic fluid to regions positioned between said position sensor housing and the pump housing.
US Referenced Citations (5)
Foreign Referenced Citations (1)
Number |
Date |
Country |
5-231306 |
Sep 1993 |
JP |