Variable-displacement axial piston pump

Information

  • Patent Grant
  • 6547531
  • Patent Number
    6,547,531
  • Date Filed
    Wednesday, January 16, 2002
    22 years ago
  • Date Issued
    Tuesday, April 15, 2003
    21 years ago
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)
Number Name Date Kind
4265603 Chiyoda et al. May 1981 A
4393966 Kono et al. Jul 1983 A
5073091 Burgess et al. Dec 1991 A
6102490 Ko Aug 2000 A
6375433 Du et al. Apr 2002 B1
Foreign Referenced Citations (1)
Number Date Country
5-231306 Sep 1993 JP