Fluid translating device

Information

  • Patent Grant
  • 6651545
  • Patent Number
    6,651,545
  • Date Filed
    Thursday, December 13, 2001
    23 years ago
  • Date Issued
    Tuesday, November 25, 2003
    21 years ago
Abstract
It is desirable to deliver only the fluid that is used to do useful work and not waste energy. In the subject arrangement, selected ones of a plurality of pistons are held at their top dead center positions when delivery therefrom is not needed. This is accomplished by having a valving arrangement disposed between the associated pressure chambers and first and second inlet/outlet ports. The valving arrangement is movable from a neutral, flow blocking position to an operative flow passing position. At the flow blocking position, fluid flow into and out of the associated pressure chamber is blocked, thus the associated piston is maintained at the top dead center position. By holding selected ones of the pistons at the top dead center position, the effective volume of fluid being used is reduced and energy is saved due to the fact that the selected pistons are not moving any fluid.
Description




TECHNICAL FIELD




The subject invention generally relates to controlling energy losses in fluid translating devices and more particularly to controlling the motion of the respective pistons when they are not in use.




BACKGROUND




Fluid translating devices are well known in the art and may be in the form of a fluid pump or a fluid motor. Piston types of fluid translating devices are normally used in systems to provide high operating torques and/or pressures. They may be in the form of radial piston designs, axial piston designs, bent axis designs or other known designs. In either of the types, a plurality of pistons are used and they reciprocate in and out of respective piston bores. When it is desired to change the flow displacement within the fluid translating device, energy is wasted by having to move the respective pistons in and out of the piston bores. It has been known to inactivate all of the pistons during use in order to hold the pistons in a predetermined position so that energy may be saved when the fluid is not needed to do useful work. One example of such a system is illustrated in the brochure entitled “We can help you pump up performance on the road, off the road, and down the road” published by Deere Inc. in April 1988. In the brochure, it teaches subjecting the internal cavity with pressurized fluid that forces each of the pistons to retract into their respective piston bores when the fluid flow into their respective pressure chambers is shut off. The pressurized fluid in the internal cavity is effective to move the respective pistons into their piston bores but the pressurized fluid within the internal cavity induces extra leakage paths and also creates unwanted drag forces therein.




The present invention is directed to overcoming one or more of the problems set forth above.




SUMMARY OF THE INVENTION




In one aspect of the present invention, a variable displacement fluid translating device is provided and comprises a housing, a rotating cam, a plurality of piston bores, a plurality of pistons, a plurality of pressure chambers and a valving arrangement. The housing has first and second inlet/outlet ports and defines a reference axis therethrough. The rotating cam is disposed in the housing along the reference axis and has a cam surface. The plurality of piston bores are defined in the housing about the reference axis and each bore of the plurality of piston bores has a bottom portion. The plurality of pistons are slideably disposed in the plurality of piston bores and are selectively in mating contact with the cam surface of the rotating cam. The plurality of pressure chambers are defined in the housing between the respective one of the plurality of pistons and the bottom portion of the respective ones of the plurality of piston bores. The valving arrangement is connected between selected pressure chambers of the plurality of pressure chambers and the respective first and second inlet/outlet ports. The valving arrangement is operative to selectively block fluid flow in and out of each pressure chamber to hold the respective piston at a predetermined position.




In another aspect of the present invention, a method is provided to control the relative position of respective ones of a plurality of pistons within a variable displacement fluid translating device. The method comprises the following steps: provide a housing having first and second inlet/outlet ports and a reference axis; provide a rotating cam having a cam surface in the housing along the reference axis; form a plurality of piston bores in the housing about the reference axis; provide a plurality of pistons in the plurality of piston bores that are slideably disposed in the respective piston bores and that are selectively in mating contact with the cam surface of the rotating cam; establish a plurality of pressure chambers between the respective one of the plurality of pistons and the respective ones of the plurality of piston bores; and provide a valving arrangement between selected pressure chamber of the plurality of pressure chambers and the respective first and second inlet/outlet ports. In the method each valving arrangement is operative to selectively block the fluid flow in and out of each pressure chamber to maintain the associated piston at a predetermined position.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a schematic representation of a work system utilizing the subject invention;





FIG. 2

is a schematic representation of another work system utilizing the subject invention;





FIG. 3

is a schematic representation of yet another work system utilizing the subject invention;





FIG. 4

is a diagrammatic representation of an embodiment of the subject invention;





FIG. 5

is a diagrammatic representation of another embodiment of the subject invention; and





FIG. 6

is a diagrammatic representation of yet another embodiment of the subject invention.











DETAILED DESCRIPTION




Referring to

FIG. 1

of the drawings, a work system


10


is illustrated and includes a variable displacement fluid translating device


12


, such as a fluid pump, that is driven by a power source


14


. The variable displacement fluid translating device


12


draws fluid from a reservoir


16


and delivers pressurized fluid to a work element


18


, such as a fluid cylinder, through a directional control valve


20


. The variable displacement fluid translating device


12


could be a fluid pump or a fluid motor and will be described in more detail herein after. Likewise the variable displacement fluid translating device could be radial, wobble plate, axial or bent axis design. The work system


10


of the subject embodiment could be, for example, an implement system.




A speed and position sensor


22


is associated with the variable displacement fluid translating device


12


and is operative to detect the speed of the variable displacement fluid translating device


12


and the rotational position of its internal mechanism. It is recognized that the speed and position sensor


22


could be disposed within the variable displacement fluid translating device


12


. The detected speed and position is delivered to a controller


24


. The controller


24


is also operatively connected by a wiring harness


25


to the variable displacement fluid translating device


12


.




A source of low pressure fluid


26


, such as a low pressure accumulator, and a high pressure accumulator


28


are also operatively connected by respective conduits


27


,


29


to the variable displacement fluid translating device


12


.




Referring to

FIG. 2

, another embodiment of a work system


10


is illustrated. Like elements have like element numbers. The work system


10


of

FIG. 2

includes the power source


14


drivingly connected to the variable displacement fluid translating device


12


. The work element


18


of the subject embodiment is a second variable displacement fluid translating device


12


′, such as a fluid motor, and is fluidity connected to the first variable displacement fluid translating device by conduits


30


,


32


.




The speed and position sensor


22


functions in the same manner as that of

FIG. 1. A

second speed and position sensor


22


′ is associated with the second variable displacement fluid translating device


12


′ and is also connected to the controller


24


. The second speed and position sensor


22


′ functions in the same manner as the first speed and position sensor


22


. A second wiring harness


25


′ connects the controller


24


to the second variable displacement fluid translating device


12


′.




The source of low pressure


26


is operatively connected to both of the first and second variable displacement fluid translating devices


12


,


12


′ and is also connected through first and second one way check valves


34


,


36


to the respective conduits


30


,


32


. In the subject embodiment, the source of low pressure fluid


26


is a pilot pump


37


.




The high pressure accumulator


28


is connected to the both the first and second variable displacement fluid translating devices


12


,


12


′ and is also connected to the first and second conduits


30


,


32


through the resolver valve


38


.




The variable displacement fluid translating device


12


of

FIG. 1

could be the same as that of

FIG. 2

, but the variable displacement fluid translating device


12


of

FIG. 1

needs to only function in two quadrants. That is, the variable displacement fluid translating device


12


of

FIG. 1

need only be capable of pump fluid only in one direction and motoring in the opposite direction. This means that the high pressure port of the variable displacement fluid translating device


12


of

FIG. 1

will always be the high pressure port and the low pressure port will always be the low pressure port. The variable displacement fluid translating device of

FIG. 2

, however must be able to function in all four quadrants. That is, it must be capable of pumping and motoring fluid in both directions. This means that the high and low pressure ports must be able to be reversed during operation depending on the operating parameters of the work system


10


. Reversing of the low and high pressure ports effectively is a change in flow direction within the variable displacement fluid translating device


12


.




Referring to the work system


10


in the embodiment of

FIG. 3

, the power source


14


is drivingly connected to the variable displacement fluid translating device


12


which in turn is fluidity connected to the work element


18


the conduits


30


,


32


. The variable displacement fluid translating device


12


of

FIG. 3

is capable of functioning in all four quadrants. The work element


18


of the subject embodiment is a typical fluid cylinder or it could be a well known fluid motor.




The speed and position sensor


22


is connected and functions the same as the speed and position sensor


22


of

FIGS. 1 and 2

. Likewise, the controller


24


is connected to the variable displacement fluid translating device


12


by the wiring harness


25


.




In the subject embodiment of

FIG. 3

, the reservoir


16


is a pressurized reservoir and serves as the source of low pressure fluid


26


. The first and second one way check valves


34


,


36


of the subject embodiment are pilot operated one way check valves


34


′,


36


′ and the source of low pressure fluid


26


is connected through the first and second pilot operated one way check valves


34


′,


36


′ with the conduits


30


,


32


. The first pilot operated one way check valves


34


′ is responsive to pressurized fluid in the conduit


32


while the second pilot operated one way check valve


36


′ is responsive to pressurized fluid in the conduit


34


.




The high pressure accumulator


28


is connected with the variable displacement fluid translating device


12


and connected with the first and second conduits


30


,


32


through the resolver valve


38


in the same manner as that of FIG.


2


.




Referring to

FIGS. 4-6

, different embodiments of the variable displacement fluid translating device


12


are illustrated. The variable displacement fluid translating device


12


of each embodiment includes a housing


40


, a rotating cam


42


, a plurality of piston bores


44


, a plurality of pistons


46


, a plurality of pressure chambers


48


and a valving arrangement


50


. It is recognized that any number of pistons


46


and piston bores


44


could be utilized in the subject embodiments. The housing


40


has first and second inlet/outlet ports


52


,


54


and a reference axis


56


extending therethrough.




The plurality of piston bores


44


defined in the housing


40


each has a bottom portion


58


and is defined therein extending radially outward from and about the reference axis


56


. Each of the respective piston bores


44


is evenly spaced from one another about the reference axis


56


. The plurality of pistons


46


are slideably disposed within the plurality of piston bores


44


to define the plurality of pressure chambers


48


between the bottom portion


58


of each piston bore of the plurality of piston bores


44


and one end of the associated piston of the plurality of pistons


46


.




The rotating cam


42


has a cam surface


60


disposed thereon eccentric from the reference axis


56


. The amount of eccentricity of the cam surface


60


relative to the reference axis


56


determines the maximum displacement or movement of the respective pistons of the plurality of pistons


46


within their respective plurality of piston bores


44


. The other end of the respective pistons


46


is in selective engagement with the cam surface


60


of the rotating cam


42


. Once the cam surface


60


on the rotating cam


42


moves the associated one of the pistons


46


into its associated piston bore


44


as far as possible, the one piston


46


is at a top dead center position ‘TDC’. When the piston


46


is furthest from the bottom portion


58


of the associated piston bore


44


, the piston is at its bottom dead center position ‘BDC’.




Each of the valving arrangements


50


is disposed between the respective pressure chambers


48


and the first and second inlet/out ports


52


,


54


. Each of the valving arrangements


50


is movable from a neutral, flow blocking position to an operative, flow passing position in response to respective electrically controlled actuator arrangements


62


. The respective electrically controlled actuator arrangements


62


are connected to the controller


24


through the wiring harness


25


. Each of the valving arrangements


50


is operative to control the direction of fluid flow between the respective pressure chambers


48


and the first and second inlet/outlet ports


52


,


54


. When the valving arrangement


50


is at its neutral, flow blocking position, the associated piston


46


is held at a predetermined position. The predetermined position in the subject arrangements is at top dead center ‘TDC’.




Each of the valving arrangements


50


of

FIG. 4

includes first and second valving assemblies


64


,


66


. The first valving assembly


64


is disposed between the respective pressure chambers


48


and the first inlet/outlet port


52


and the second valving assembly


66


is disposed between the respective pressure chambers


48


and the second inlet/outlet port


54


. Each of the first and second valving assemblies


64


,


66


is movable from a neutral, flow blocking position towards an operative, flow passing position.




Each of the first and second valving assemblies


64


,


66


has first and second valve seats


68


,


70


disposed therein with a ball check


72


disposed therebetween and operative to be selectively seated between or in one of the first and second valve seats


68


,


70


. A biasing member


74


biasing the respective ball checks


72


into engagement with the first valving seat


68


.




Each of the electrically controlled actuator arrangements


62


of the subject embodiment includes first and second electrically controlled actuators


76


,


78


. Each of the electrically controlled actuators


76


,


78


are connected through the wiring harness


25


to the controller


24


and operative to move the respective ball checks


72


between the first and second valve seats


68


,


70


.




The respective pressure chambers


48


are each connected to the high pressure accumulator


28


through respective relief valves


80


and the conduit


29


. It is recognized that the relief valves


80


serve only to vent minimal amounts of fluid at a very low differential pressure since the line


29


is connected to the high pressure accumulator


28


. The respective pressure chambers


48


are also connected to the source of low pressure fluid through respective orifices


82


and one way check valves


84


.




Referring to the embodiment of

FIG. 5

, like elements have like element numbers. Each of the first and second valving assemblies


64


,


66


of the valving arrangement


50


in

FIG. 5

includes a single valve seat


86


and a pilot operated poppet valve


88


. Each of the pilot operated poppet valves


88


is urged into seating engagement with the single valve seat


86


in response to actuation of respective pilot valves


90


. The respective pilot valves


90


are disposed between the associated pilot operated poppet valves


88


and the associated electrically controlled actuators


76


,


78


and each is operative in response to the associated electrically controlled actuators


76


,


78


to hold the pilot operated poppet valve


88


in the neutral, flow blocking position or to permit it to open to the operative, flow passing position. The respective pilot valves


90


of each of the first and second valving assemblies


64


,


66


are connected between the associated pressure chamber


48


and the associated one of the first and second inlet/outlet ports


52


,


54


. Movement of the respective pilot valves


90


function to control the pressure of fluid in a pilot control chamber


92


behind the respective pilot operated poppet valves


88


. A light weight spring


94


is disposed in the pilot control chamber


92


and functions to urge the pilot operated poppet valve


88


to the neutral, flow blocking position. It is recognized that the pilot valves


90


could be removed and the respective first and second electrically controlled actuators


76


,


78


could be connected directly to the associated pilot operated poppet valves


88


.




Referring to the embodiment of

FIG. 6

, like elements have like element numbers. The valving arrangement


50


of

FIG. 6

has a single valving element


94


and a single electrically controlled actuator


96


associated therewith through a single pilot valve


98


. It is recognized that the single electrically controlled actuator


96


could be connected directly to the single valving element. The single valving element


94


is disposed between the respective pressure chambers


48


and the first and second inlet/outlet ports


52


,


54


and is movable between a neutral, flow blocking position and first and second operative positions. At the neutral position, all flow to and from the respective pressure chambers


48


is blocked. In the first operative position, the first inlet/out port


52


is in communication with the associated pressure chamber


48


and the second inlet/outlet port


54


is blocked therefrom. In the second operative position, the second inlet/out port


54


is in communication with the associated pressure chamber


48


and the first inlet/outlet port


52


is blocked therefrom.




The single pilot valve


98


is disposed between the single valving element


94


and the single electrically controlled actuator


96


and operative to control the fluid within a single pilot control chamber


100


. The single pilot valve


98


controls communication of fluid between the source of low pressure fluid


26


, the single pilot control chamber


100


and the reservoir


16


.




FIGS. 1-6 set forth a method of controlling the relative position of respective ones of a plurality of pistons within a variable displacement fluid translating device. Various ones of the following steps are utilized in accomplishing this method. For example, some of the steps include providing a housing


40


having first and second inlet/outlet ports


52


,


54


with a reference axis


56


extending therethough; providing a rotating cam


42


having a cam surface


60


in the housing


40


along the reference axis


56


; forming a plurality of pressure chambers


48


in the housing


40


; providing a plurality of pistons


46


in the plurality of pressure chambers


48


that are slideably disposed therein and that are selectively in mating contact with the cam surface


60


of the rotating cam


42


; establishing a plurality of pressure chambers


48


between the plurality of pistons


46


and the respective ones of the plurality of pressure chambers


48


; and providing a valving arrangement


50


between each pressure chambers


48


and the respective ones of the first and second inlet/outlet ports


52


,


54


. Each of the valving arrangements


50


being operative to selectively block the fluid flow in and out of each pressure chamber


48


to maintain the associated piston


46


at a predetermined position. Other steps include moving the respective pistons


46


a predetermined distance within the associated piston bore


44


and controlling the direction of flow into and out of the respective pressure chambers


48


for only a portion of the predetermined distance. Another step includes providing a controller


24


operatively connected to the variable displacement fluid translating device


12


and a speed and position sensor


22


associated with the variable displacement fluid translating device


12


that is operative to sense the speed and rotational position of the variable displacement fluid translating device


12


and direct a signal representative thereof to the controller


24


.




It is recognized that various other embodiments of the variable displacement fluid translating device


12


and combinations of the work system


10


could be utilized without departing from the essence of the present invention.




INDUSTRIAL APPLICABILITY




In the operation of the work system


10


of

FIG. 1

, the pump


12


draws fluid from the reservoir


16


and delivers pressurized fluid to the fluid cylinder


18


through a directional control valve


20


. As noted above, the fluid pump


12


of

FIG. 1

operates only in the two quadrant mode. The first inlet/outlet port


52


(

FIG. 4

) is always the high pressure port and the second inlet/outlet port


54


(FIG.


4


)is always the low pressure port or as illustrated in this embodiment, it is connected to the reservoir


16


. The exhaust flow from the fluid cylinder


18


is directed across the directional control valve


20


to the reservoir


16


in a well known manner.




In the work system


10


of

FIG. 2

, the variable displacement fluid translating device


12


(pump) and the second variable displacement fluid translating device


12


′ (motor) each operate in the four quadrant mode. Consequently, each of the first and second inlet/outlet ports


52


,


54


serve as high and low pressure ports depending on the operating parameters of the work system


10


. The work system


10


of

FIG. 2

is a typical hydrostatic system in which the fluid pump


12


and the fluid motor


12


′ are fluidity connected together. The pilot pump


37


provides low pressure fluid through the first and second one way check valves


34


,


36


to both the conduits


30


,


32


and the fluid pump


12


and fluid motor


12


′. The high pressure accumulator


28


is maintained at the highest system pressure level by its connection through the resolver valve


38


to the respective conduits


30


,


32


and is also connected to the fluid pump


12


and fluid motor


12


′ in order to receive any fluid resulting from an overpressure condition within the pump


12


or motor


12


′ and also functions to reduce fluid pressure ripples and/or fluid borne noise.




The speed and position sensors


22


,


22


′ functions to continually sense and deliver a signal to the controller


24


representative of the speed of the fluid pump


12


and the fluid motor


12


′. Likewise, it also functions to continually monitor and deliver a signal to the controller


24


representative of the position of the rotating cam


42


within the fluid pump


12


and the fluid motor


12


′. The controller


24


functions to control the displacement of the fluid pump


12


and fluid motor


12


′ relative to the operating parameters of the total work system


10


.




In the work system


10


of

FIG. 3

, the variable displacement fluid translating device or pump


12


operates in the four quadrant mode like that of FIG.


2


. However, the work element


18


of

FIG. 3

is a typical fluid actuator


18


. The pressurized fluid reservoir


16


serves as the source of low pressure fluid


26


and is connected to the conduits


30


,


32


through the respective pilot operated one way check valves


34


′,


36


′. When the pressure in the conduit


30


is at a higher pressure level than that in conduit


32


, the pilot operated one way check valve


36


′ is forced to open in response to the higher pressure in conduit


30


and the pressure in the conduit


32


is maintained at least at the level of the pressure in the pressurized reservoir


16


. When the pressure in the conduit


32


is higher than that in the conduit


30


the opposite occurs. The pressurized fluid in the pressurized reservoir


16


is also connected to the fluid pump


12


to provide the source of low pressure fluid


26


that will be explained below. All other operating aspects of the work system


10


of

FIG. 3

is the same as that of FIG.


2


.




Referring to the variable displacement fluid translating device


12


of

FIG. 4

, hereinafter referred to as a fluid pump


12


, the operation thereof is described with it being used as a fluid pump


12


. However, it is recognized that it is also applicable as a fluid motor. As the rotating cam


42


of the fluid pump


12


rotates, the plurality of pistons


40


are forced to reciprocate within the plurality of piston bores


44


due to the fact that they are in mating contact with the cam surface


60


of the rotating cam


42


. As the rotating cam


42


rotates with respect to the plurality of pistons


46


from the bottom dead center position BDC towards the top dead center position TDC, the fluid in the respective ones of the plurality of pressure chambers


48


is forced out towards the first inlet/outlet port


52


. In order for the fluid within the respective pressure chambers


48


to get to the first inlet/outlet port


52


, the fluid must pass through the first valve seat


68


pass by the ball check


72


to the first inlet/outlet port


52


or pressure side of the fluid pump


12


leading to the work element


18


. Simultaneously, fluid must be received from the second inlet/outlet port


54


or low pressure side and delivered to the pressure chambers


48


from which the associated pistons


46


are moving from the top dead center TDC position towards the bottom dead center position BDC. In order for fluid from the low pressure side to get to the pressure chambers


48


that are being filled, the ball check


72


seated on the second valve seat


70


must be moved. This is accomplished by the controller


24


directing a signal to the second electrically controlled actuator


78


which then forces the ball check


72


thereof to the operative, flow passing position. In this pumping mode, the ball check


72


is moved to a position between the first and second valve seats


68


,


70


. As long as the pumping mode remains active pressurized fluid at full displacement is pumped through the first inlet/outlet port


52


to the work element


18


.




When the fluid pump


12


is operating in a work system requiring the four quadrant mode and the fluid direction is reversed, the opposite occurs. That is, the first valving assembly


64


is actuated and the second valving assembly


66


remains in its unactuated position with the ball check


72


seated against the first valve seat


68


.




In order for the fluid pump


12


, to operate in the motoring mode, both of the first and second electrically controlled actuators


76


,


78


need to be energized at the same time during the intake stroke to move the ball checks


72


of the first and second valving assemblies


64


,


66


against their respective second valve seats


66


. During the exhaust stroke, both of the first and second electrically controlled actuators


76


,


78


are de-energized to permit both of the ball checks


72


to return to the respective first valve seats


64


.




In the event of over pressurization within either of the pressure chambers


48


, the associated relief valve


80


opens to vent fluid therefrom to the high pressure accumulator


28


thus removing the over pressure condition. During initial startup of the subject fluid pump


12


, it may be necessary to introduce pressurized fluid into the respective pressure chambers


48


. The orifice


82


and one way check


84


function to permit a small amount of low pressure fluid to be introduced into the respective pressure chambers


48


during startup. After startup, the one way check


84


blocks reverse flow from the pressure chambers


48


to the source of low pressure fluid


26


.




In order to vary the displacement of the fluid pump


12


, any one or more of the plurality of pistons


46


are selectively stopped thus removing its effective volume of fluid from the total volume. This is accomplished by continuously holding the ball check


72


of the second valving assembly


66


in a position between the first and second valve seats


68


,


70


while leaving the ball check


72


of the first valving assembly


64


seated against the first valve seat


68


. This permits the selected piston or pistons


46


to continue to reciprocate in and out. However, during the pumping stroke the fluid being expelled is being directed back to the second inlet/outlet port


54


through the second, open valving assembly


66


. If the flow direction through the fluid pump


12


is reversed, the ball check


72


of the first valving assembly


66


is positioned between the first and second valve seats


68


,


70


while the ball check


72


of the second valving assembly


66


remains against the first valve seat


68


thereof.




The displacement of the fluid pump


12


can also be varied by controlling the volume that each piston


46


can produce. This is accomplished by permitting the selected one or ones of the pistons


46


to effectively pump a portion of their total volume and bypass the remaining portion. Likewise, it is possible to pump a first portion of the volume, bypass an intermediate portion and pump the remaining portion of the total volume of fluid. This is accomplished by the controller


24


selectively controlling actuation of the second valving assembly


66


between it neutral and operative positions.




In order to totally stop the flow of fluid into and out of the selected piston or piston


46


in either direction of fluid flow, both of the first and second electrically controlled actuators


76


,


78


are de-energized just prior to the respective selected piston or pistons


46


reaching their top dead center TDC positions. Consequently, the respective selected piston or pistons


46


are hydraulically locked or stopped at the top dead center position TDC and do not reciprocate in and out until it is desired to recombine their flows into the total flow output. When it is desired to activate the deactivated selected piston or pistons


46


, the second electrically controlled actuator


78


is energized near top dead center TDC, assuming that the flow direction is towards the first inlet/outlet port


52


, to move the ball check


72


of the second valve assembly


66


towards the second valve seat


70


.




In the operation of the variable displacement fluid translating device


12


of

FIG. 5

, all aspects with respect to the operation of

FIG. 4

is the same except the first and second valving assemblies


64


,


66


are different. When the pressurized fluid flow is in the direction of the first inlet/outlet port


52


, the second valving assembly


66


that is associated with each of the pistons that are forcing fluid out of the respective pressure chambers


48


is actuated and the first valving assembly


64


of each remain unactuated. Consequently, the pressurized fluid in the associated pressure chambers


48


act on the pilot operated poppet valve


88


urging it towards the operative, flow passing position to direct the pressurized fluid to the inlet/outlet port


52


. The pilot valve


90


of the first valving assembly


64


acts to block the pressure in the respective pressure chamber


48


from the pilot control chamber


92


and permit the pressure at the inlet/outlet port


52


to be communicated with the pilot control chamber


92


. The pressure in the pressure chamber


48


acting on the pilot operated poppet valve


88


is sufficient to move the pilot operated poppet valve


88


towards its open position.




At the same time, the pilot valve


90


of the second valving assembly


66


is actuated to move it to a position to communicate the pressure in the pressure chamber


48


to the pilot control chamber


92


of the second valving assembly


66


and blocks the communication of the pressure at the second inlet/outlet port


54


with the pilot control chamber


92


thereof. Consequently, the higher pressure being subjected to the pilot control chamber


92


of the second valving assembly


66


maintains the pilot operated poppet valve


88


of the second valving assembly


66


in its neutral, flow blocking position.




Once all of the fluid has been expelled from the respective pressure chambers


48


and the associated pistons


46


begin to retract, the pressure within the pressure chambers


48


thereof is quickly reduced. Since the pressure of the fluid at the first inlet/outlet port


52


is communicated with the pilot control chamber


92


of the first valving assembly


64


, the pilot operated poppet valve


88


thereof is held firmly against its valve seat


86


. Since the pressure of the fluid in the pilot control chamber


92


of the second valving assembly


66


is also in communication with the lowered pressure in the pressure chambers


48


, the pressure of the fluid at the second inlet/outlet port


54


is sufficient to open the pilot operated poppet valve


88


of the second valving assembly


66


to fill the pressure chambers


48


as they retract. If fluid flow is in the opposite direction, the opposite operation would occur.




In the motoring mode of operation, both of the first and second valving assemblies


64


,


66


are actuated during the intake stroke, i. e. when receiving high pressure. During the exhaust stroke, both are returned to their unactuated positions. Typically, to aid in timing, just before BDC the electrically controlled actuator


76


/


78


of the associated valving assembly


64


/


66


on the high pressure side of the pump


12


is de-energized and the electrically controlled actuator


76


/


78


of the associated valving assembly


64


/


66


on the low pressure side of the pump


12


is de-energized at BDC. Likewise, just before TDC the valving assembly


64


/


66


of the low pressure side is actuated and the valving assembly


64


/


66


on the high pressure side is actuated at TDC. Thereafter, the whole cycle repeats.




In the event of an over pressure condition within the respective pressure chambers


48


, the respective pilot control chambers


92


of the first and second valving assemblies


64


,


66


are connected to the relief valve


80


. Consequently, any over pressure condition can be released across the associated one of the pilot operated poppet valves


88


of the first and second valve assemblies


64


,


66


to one of the first and second inlet/outlet ports


52


,


54


.




In order to vary the displacement of the fluid pump


12


with the direction of fluid flow being towards the first inlet/outlet port


52


, the second valving assembly


66


of a selected one or ones of the pistons


46


that are expelling fluid remains unactuated along with the first valving assembly being unactuated. Consequently, the fluid being pressurized in the associated pressure chamber


48


acts on the pilot operated poppet valve


88


of the second valving assembly


66


and urges it towards its open position thus directing the fluid to the second, low pressure inlet/outlet port


54


. Once the associated piston


46


reaches the TDC position, the second valving assembly


66


is actuated and the pressure chamber


48


fills with fluid as the piston


46


retracted from the piston bore


44


.




The displacement of the fluid pump


12


can also be varied by permitting a selected one or ones of the pistons


46


to pump only a portion of their total volume and bypass the remaining portion to the low pressure side. This is accomplished by the controller


24


selectively controlling the actuation of the second valving element


66


. Since the velocity of the respective pistons


46


are their highest at a position between the bottom dead center position BDC and the top dead center positions TDC, it may be advantageous to use only the first and/or last portions of the total volumes and bypass the mid portion thereof.




In order to reduce the total required energy in the work system


10


, the fluid flow that is not being used for useful work can be eliminated. By leaving the second valving assembly


66


unactuated when the piston


46


reaches the TDC position, the piston


46


is hydraulically locked at the TDC position. When it is desired to once again increase the pumps displacement, the second valving assembly


66


is actuated at the TDC position so that the pressure chamber


48


can refill and the piston


46


again contacts the cam surface


60


and retracts as the rotating cam turns. Naturally, if the flow direction is in the direction of the second inlet/outlet port


54


, the operation would be just the opposite.




In the operation of the embodiment of

FIG. 6

, all aspects with respect to the operation of

FIG. 5

is the same except the valving arrangement


50


of

FIG. 6

only has a single valving element


94


connected between the respective pressure chambers


48


and the first and second inlet/outlet ports


52


,


54


and the respective pressure chambers


48


are connected through respective relief valves


80


to the high pressure accumulator


28


to control overpressure conditions.




When the flow of fluid is towards the first inlet/outlet port


52


, the single valving element


94


is moved from its neutral, flow blocking position towards its first operative position to direct pressurized fluid from the pressure chamber


48


of the pistons


46


that are expelling fluid to the first inlet/outlet port


52


. At the same time, the single valving element


94


of the pressure chambers


48


that are being filled due to the pistons


46


retracting is moved from its flow blocking position to its second operative position to connect the associated pressure chambers


48


to the second inlet/outlet port


54


. When the pistons


46


that are pumping pressurized fluid reaches their respective TDC positions, the single valving element


94


associated therewith moves from the first operative position towards the second operative position. Likewise, when the pistons


46


that are retracting reaches their respective BDC positions, the single valving element


94


associated therewith moves from their second operative position towards their first operative positions. If the flow direction is changed towards the second inlet/outlet port


54


, the reverse operation occurs.




When it is desired to reduce the displacement from the pump


12


with the flow in the direction of the first inlet/outlet port


52


, a selected one or ones of the single valving elements


94


is moved from its neutral, flow blocking position towards its second operative position to connect the associated pressure chamber


48


to the second inlet/outlet port


54


that is functioning as the low pressure port. The single valve element


94


of the selected one or ones of the pistons that are not being used to provide useful flow remains in the second operative position until the flow therefrom is again needed to do useful work.




As set forth with respect to

FIGS. 4 and 5

, it is also possible to vary the volume of fluid delivered from the embodiment of

FIG. 6

by using only a portion of the total volume being pumped from the respective pressure chambers


48


. The controller


24


controls the operation of the respective single valving members


94


to direct portions of the pumped fluid to the high pressure side and to bypass other portions thereof to the low pressure side.




In order to eliminate the wasted energy in the system due to the pumping of flow that is not being used to do useful work, the piston


46


that is being bypassed is stopped at TDC and not permitted to move. This is accomplished by maintaining the single valving element


94


of the selected one or ones of the pistons


46


being bypassed in its neutral, flow blocking position. With the single valving element


94


in its neutral position, the associated piston is hydraulically locked at that position. Consequently, the cam surface


60


separates from the piston


46


. Once the flow from the stopped piston is needed, the single valving element


94


is moved to its first operative position as set forth above.




In view of the above, it is readily apparent that the fluid translating device


12


provides a pump/motor in which the displacement thereof is changed by not using fluid flow from selected one(s) of the pistons therein. It also conserves energy within the work system by stopping the motion of the selected one or ones of the pistons when the displacement therein is being varied thus not permitting unused fluid to be unnecessarily pumped at low pressure through the work system


10


.




Other aspects, objects and advantages of the invention can be obtained from a study of the drawings, the disclosure and the appended claims.



Claims
  • 1. A variable displacement fluid translating device, comprising:a housing having first and second inlet/outlet ports and defining a reference axis therethrough a rotating cam disposed in the housing along the reference axis and having a cam surface; a plurality of piston bores defined in the housing about the reference axis and each bore of the plurality of piston bores having a bottom portion; a plurality of pistons slideably disposed in the plurality of piston bores and selectively in mating contact with the cam surface of the rotating cam; a plurality of pressure chambers defined in the housing between the respective one of the plurality of pistons and the bottom portion of the respective ones of the plurality of piston bores; a valving arrangement connected between selected pressure chambers of the plurality of pressure chambers and the respective first and second inlet/outlet ports and being operative to selectively block fluid flow in and out of each pressure chamber to hold the respective piston at a predetermined position, each of the valving arrangements including first and second valving assemblies; and first and second electrically controlled actuators operatively connected to each of the first and second valving assemblies.
  • 2. The variable displacement fluid translating device of claim 1 wherein, the first valving assembly is disposed between the associated pressure chamber and the first inlet/outlet port and the second valving assembly is disposed between the associated pressure chamber and the second inlet/outlet port.
  • 3. The variable displacement fluid translating device of claim 2 wherein each of the first and second valving assemblies are movable from a neutral, flow blocking position towards an operative, flow passing position in response to actuation of the associated electrically controlled actuator.
  • 4. The variable displacement fluid translating device of claim 3 wherein each of the pistons has a top dead center position and when the first and second valving assemblies are held in their neutral, flow blocking positions, fluid flow in and out of the respective pressure chambers is blocked and the associated piston is held at its top dead center position.
  • 5. The variable displacement fluid translating device of claim 4 wherein the variable displacement fluid translating device is a radial variable displacement fluid translating device.
  • 6. The variable displacement fluid translating device of claim 4 wherein the variable displacement fluid translating device is a fluid pump.
  • 7. The variable displacement fluid translating device of claim 4 wherein the variable displacement fluid translating device is a fluid motor.
  • 8. The variable displacement fluid translating device of claim 4 in combination with a controller operatively connected to the variable displacement fluid translating device and a speed and position sensor operatively associated with the variable displacement fluid translating device and operative to sense the speed and position of rotation of the variable displacement fluid translating device and deliver a signal representative thereof to the controller.
  • 9. A method of controlling the relative position of respective ones of a plurality of pistons within a variable displacement fluid translating device, comprising the steps:providing a housing having first and second inlet/outlet ports and a reference axis; providing a rotating cam having a cam surface in the housing along the reference axis; forming a plurality of piston bores in the housing about the reference axis; providing a plurality of pistons in the plurality of piston bores that are slideably disposed in the respective piston bores and that are selectively in mating contact with the cam surface of the rotating cam; establishing a plurality of pressure chambers between the respective one of the plurality of pistons and the respective ones of the plurality of piston bores; and providing first and second valving assemblies between one selected pressure chamber of the plurality of pressure chambers and the respective first and second inlet/outlet ports, the first and second valving assemblies being operative to selectively block the fluid flow in and out of the one pressure chamber to maintain the associated piston at a predetermined position.
  • 10. The method of claim 9 including the step of holding the selected pistons at a top dead center position.
  • 11. The method of claim 9 wherein the step of providing a plurality of pistons slideably disposed in the plurality of piston bores includes the step of moving the respective pistons a predetermined distance within the associated piston bore of the plurality of piston bores and the step of providing first and second valving assemblies includes the step of controlling the direction of flow into and out of the pressure chamber for only a portion of the predetermined distance.
  • 12. The method of claim 11 including the step of providing a controller operatively connected to the variable displacement fluid translating device and a speed and position sensor associated with the variable displacement fluid translating device and operative to sense the speed of and the rotational position of the variable displacement fluid translating device and direct a signal representative thereof to the controller.
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Number Date Country
0 651 159 May 1995 IT
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