METHOD FOR INCREASING COMPRESSED AIR EFFICIENCY IN A PUMP

Abstract
One or more techniques and/or systems are disclosed for increasing compressed air efficiency in a pump utilizes an air efficiency device in order to optimize the amount of a compressed air in a pump. The air efficiency device may allow for controlling the operation of the air operated diaphragm pump by reducing the flow of compressed air supplied to the pump as the pump moves between first and second diaphragm positions. A sensor may be used to monitor velocity of the diaphragm assemblies. In turn, full position feedback is possible so that the pump self-adjusts to determine the optimum, or close to optimum, turndown point of the diaphragm assemblies. As such, air savings is achieved by minimizing the amount of required compressed air.
Description
BACKGROUND

Fluid-operated pumps, such as diaphragm pumps, are widely used particularly for pumping liquids, solutions, viscous materials, slurries, suspensions or flowable solids. Double diaphragm pumps are well known for their utility in pumping viscous or solids-laden liquids, as well as for pumping plain water or other liquids, and high or low viscosity solutions based on such liquids. Accordingly, such double diaphragm pumps have found extensive use in pumping out sumps, shafts, and pits, and generally in handling a great variety of slurries, sludges, and waste-laden liquids. Fluid driven diaphragm pumps offer certain further advantages in convenience, effectiveness, portability, and safety. Double diaphragm pumps are rugged and compact and, to gain maximum flexibility, are often served by a single intake line and deliver liquid through a short manifold to a single discharge line.


U.S. Pat. No. 5,332,372 to Reynolds teaches a control system for an air operated diaphragm pump. The control system utilizes sensors to monitor pump speed and pump position and then controls the supply of compressed air to the pump in response thereto. Because pump speed and pump position are effected by pumped fluid characteristics, the control unit is able to change the pump speed or the cycle pattern of the pump assembly in response to changes in pumped fluid characteristics to achieve desired pump operating characteristics. The sensors provide a constant feedback that allows the control system to immediately adjust the supply of compressed air to the pump in response to changes in pump operating conditions without interrupting pump operation. Position sensors may be used to detect pump position. For example, the sensors can comprise a digitally encoded piston shaft operatively connected to the diaphragm assembly that provides a precise signal corresponding to pump position that can be used to detect changes in pump speed and pump position. Flow condition sensors can be utilized to determine flow rate, leakage, or slurry concentration. The sensors transmit signals to a microprocessor that utilizes the transmitted signals to selectively actuate the pump's control valves. By sensing changes in pump position, the control system can control the supply of compressed air to the pump by modifying the settings of the control valves thereby controlling both pump speed and pump cycle pattern at any point along the pump stroke. Digital modulating valves can be utilized to increase the degree of system control provided by the control system. The desired optimal pump conditions can be programmed into the control system and, utilizing information transmitted by the sensors, the control system can experiment with different stroke lengths, stroke speeds, and onset of pumping cycle to determine the optimal pump actuation sequence to achieve and maintain the desired predetermined pumping conditions.


U.S. Pat. No. 5,257,914 to Reynolds teaches an electronic control interface for a fluid powered diaphragm pump. Further, the '372 patent is incorporated into the '914 patent by reference. The supply of compressed air is controlled for the purpose of allowing changes in pump speed or a cycle pattern. This is accomplished by detecting the position and acceleration of the diaphragms. More specifically, the pump utilizes sensors to detect certain pump characteristics, such as pump speed, flow rate, and pump position, but not limited thereto, and sends those signals to the control unit. Because the position and rate of movement of the diaphragm is effected by pumped fluid characteristics, the control unit is able to change the pump speed or cycle pattern of the pump assembly in response to changes in pumped fluid characteristics. The control unit determines elapsed time between pulse signals, which leads to calculations for the speed of reciprocation of the rod and the diaphragms. The control unit, utilizing the changes in the speed of travel of the diaphragms, calculates acceleration and other speed-dependent characteristics of the pump.


U.S. Patent Publication No. 2006/0104829 to Reed et al. discloses a control system for operating and controlling an air operated diaphragm pump. Reed does not use position or acceleration of the diaphragms, but is dependent upon other considerations such as a predetermined time period.


What is needed then is an air operated diaphragm pump that utilizes a self-learning process by velocity detection at a floating point or a set point to minimize the amount of compressed air needed to effectively operate the pump.


SUMMARY

This Summary is provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. This Summary is not intended to identify key factors or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter.


As provided herein, a method for increasing compressed air efficiency in a pump. More specifically, the inventive method utilizes an air efficiency device in order to minimize the amount of a compressed air in a pump. A principal object of this invention is to improve upon the teachings of the aforementioned Reynolds U.S. Pat. No. 5,257,914 and its incorporated teaching of Reynolds U.S. Pat. No. 5,332,372 by utilizing velocity and position sensing of the movement of the diaphragm assemblies to control the utilization of the pressure fluid which causes movement of the diaphragm assemblies and to do so utilizing control algorithms that accommodate changing condition influences to achieve a more optimally controlled pump.


In one implementation, a pump is provided having diaphragm chambers and diaphragm assemblies. Each diaphragm assembly may comprise a diaphragm. An air efficiency device may allow for controlling the operation of an air operated diaphragm. A minimum and termination velocity may be defined. As one of the diaphragm chambers is filled with the compressed air, the diaphragm assembly passes a turndown position. Upon passing the turndown position, the air efficiency device stops or decreases the flow of compressed air into the pump. The air efficiency device monitors the velocity of the diaphragm assembly until it reaches its end of stroke position and redefines the turndown position if it determines that the velocity of the diaphragm assembly exceeded the defined termination velocity or fell below the defined minimum velocity. The air efficiency device then performs the same method independently for the other diaphragm assembly. Upon the other diaphragm assembly reaching its end of stroke position, the method is again repeated for the first diaphragm assembly utilizing any redefined turndown positions as appropriate.


To the accomplishment of the foregoing and related ends, the following description and annexed drawings set forth certain illustrative aspects and implementations. These are indicative of but a few of the various ways in which one or more aspects may be employed. Other aspects, advantages and novel features of the disclosure will become apparent from the following detailed description when considered in conjunction with the annexed drawings.





BRIEF DESCRIPTION OF THE DRAWINGS

What is disclosed herein may take physical form in certain parts and arrangement of parts, and will be described in detail in this specification and illustrated in the accompanying drawings which form a part hereof and wherein:



FIG. 1 is a component diagram illustrating a sectional view of an example implementation of an air operated double diaphragm pump.



FIG. 2 is component diagram illustrating a schematic view of an example implementation of an air operated double diaphragm pump comprising a first pump state.



FIG. 3 is component diagram illustrating a schematic view of an example implementation of an air operated double diaphragm pump shown.



FIG. 4 shows a partial sectional view of a pilot valve assembly and a main valve assembly according to one embodiment of the invention.



FIG. 5 is a component diagram illustrating a partial sectional view of an example implementation of a pilot valve assembly and a main valve assembly.



FIG. 6
a is a component diagram illustrating a partial sectional view of an example implementation of an air efficiency device operatively connected to an air operated double diaphragm pump.



FIG. 6
b is a component diagram illustrating a schematic view of an example implementation of an air efficiency device operatively connected to an air operated double diaphragm pump.



FIG. 7 is a component diagram illustrating a perspective view an example implementation of a linear displacement device.



FIG. 8 is a flow chart diagram illustrating an exemplary method for operating an air operated double diaphragm according to one or more implementations described herein.



FIG. 9 is a flow diagram illustrating an exemplary method for optimizing an amount of supply compressed air utilized during operation of a pump.



FIG. 10 is a flow diagram illustrating an example embodiment where one or more portions of one or more techniques, described herein, may implemented.





DETAILED DESCRIPTION

The claimed subject matter is now described with reference to the drawings, wherein like reference numerals are generally used to refer to like elements throughout. In the following description, for purposes of explanation, numerous specific details are set forth in order to provide a thorough understanding of the claimed subject matter. It may be evident, however, that the claimed subject matter may be practiced without these specific details. In other instances, structures and devices are shown in block diagram form in order to facilitate describing the claimed subject matter.


Referring now to the drawings wherein the showings are for purposes of illustrating embodiments of the invention only and not for purposes of limiting the same, FIGS. 1-8 illustrate the present invention. FIG. 1 shows an air operated double diaphragm pump 10 comprising an air efficiency device 1 according to one embodiment of the invention. The air efficiency device 1 may enable the pump 10 to operate at an increased efficiency by controlling or regulating the supply of compressed air or compressed fluid provided to the pump 10 from a compressed air or fluid supply. Hereinafter, the term “compressed air” and “compressed fluid” may be used interchangeably. The air efficiency device 1 may reduce or temporarily halt the supply of compressed air to the pump 10 beginning at a predetermined shutoff or turndown point prior to the pump's 10 end of stroke position as more fully described below. By reducing or completely halting the supply of compressed air at the turndown point, the pump 10 utilizes the natural expansion of the compressed air within the pump's chambers to reach the end of stroke position. Although the invention is described in terms of an air operated double diaphragm pump, the invention may be utilized with any type pump chosen with sound judgment by a person of ordinary skill in the art. The designations left and right are used in describing the invention for illustrative purposes only. The designations left and right are used to distinguish similar elements and positions and are not intended to limit the invention to a specific physical arrangement of the elements.


With reference now to FIG. 1, the pump 10 will generally be described. The pump 10 may comprise a housing 11, a first diaphragm chamber 12, a second diaphragm chamber 13, a center section 14, a power supply 15, and the air efficiency device 1. The first diaphragm chamber 12 may include a first diaphragm assembly 16 comprising a first diaphragm 17 and a first diaphragm plate 24. The first diaphragm 17 may be coupled to the first diaphragm plate 24 and may extend across the first diaphragm chamber 12 thereby forming a movable wall defining a first pumping chamber 18 and a first diaphragm chamber 21. The second diaphragm chamber 13 may be substantially the same as the first diaphragm chamber 12 and may include a second diaphragm assembly 20 comprising a second diaphragm 23 and a second diaphragm plate 25. The second diaphragm 23 may be coupled to the second diaphragm plate 25 and may extend across the second diaphragm chamber 13 to define a second pumping chamber 26 and a second diaphragm chamber 22. A connecting rod 30 may be operatively connected to and extend between the first and second diaphragm plates 24, 25.


With reference now to FIGS. 2 and 3, the connecting rod 30 may at least partially allow the first and second diaphragm assemblies 16, 20 to reciprocate together between a first end of stroke position EOS1, as shown in FIG. 2, and a second end of stroke position EOS2, as shown in FIG. 3. The first and second end of stroke positions EOS1, EOS2 may represent a hard-stop or physically limited position of the first and second diaphragm assemblies 16, 20, as restricted by the mechanics of the pump as is well known in the art. Next, each of the diaphragm assemblies 16, 20 within respective first and second diaphragm chambers 12, 13 may have a first diaphragm position DP1L, DP1R and a second diaphragm position DP2L, DP2R, respectively. The first and second diaphragm positions DP1L, DP1R, DP2L, DP2R may correspond to a predetermined and/or detected position of the first and second diaphragm assemblies 16, 20 that is reached prior to the respective end of stroke position EOS 1, EOS2. In one embodiment, the first diaphragm position DP1L, DP1R and the second diaphragm positions DP2L, DP2R may comprise a position that is about 0.01 mm to about 10 mm from the first and second end of stroke positions EOS 1, EOS2, respectively. In another embodiment, the first diaphragm position DP1L, DP1R and the second diaphragm positions DP2L, DP2R may comprise a position that is about 5 mm from the first and second end of stroke positions EOS 1, EOS2, respectively. It is important that measurement of velocity, as described in more detail below, is never measured at the end of stroke positions, EOS1 and EOS2. Rather, velocity is measured just prior to the end of stroke positions EOS1 and EOS2.


With continued reference now to FIGS. 2 and 3, in one embodiment, the first diaphragm position DP1L, DP1R may comprise a position wherein the compressed air has been substantially exhausted from the diaphragm chamber 21, 22 and a pumped fluid has been suctioned or otherwise communicated into the pumping chamber 18, 26. In the first diaphragm position DP1L, DP1R the diaphragm plate 24, 25 may contact an end portion of an actuator pin 27 thereby initiating the movement of a pilot valve spool 29. The second diaphragm position DP2L, DP2R may comprise a position wherein the first and second diaphragm chambers 21, 22 are substantially filled with compressed air and the pumped fluid has been substantially exhausted from the first and second pumping chambers 18, 26. In the second diaphragm position DP2L, DP2R the first and second diaphragm plates 24, 25 may be positioned completely out of contact with the actuator pin 27.


With reference now to FIGS. 1-5, the center section 14 may include a pilot valve housing 28, a main fluid valve assembly 34, and the air efficiency device 1. The pilot valve housing 28 may comprise a pilot inlet 31, the actuator pin 27, a pilot valve spool 29, a first main channel 36, a second main channel 41, a first signal port channel 42, and a second signal port channel 45. The pilot valve housing 28 may at least partially allow for the control of the movement of the main fluid valve assembly 34 between a first and a second main valve position, thereby causing the compressed air to flow into either the first or second diaphragm chambers 21, 22 as more fully described below. In one embodiment, the movement of the pilot valve spool 29 may be caused by the actuator pin 27 being contacted by the first or second diaphragm plates 24, 25. The pilot inlet 31 may communicate compressed air to the first main channel 36, the second main channel 41, and the pilot valve spool 29. The pilot valve spool 29 may be movable between a first pilot position FP1, shown in FIGS. 2 and 4, and a second pilot position FP2, shown in FIG. 3. The pilot valve spool 29 may comprise a first pilot passageway 64 and a second pilot passageway 65 configured such that movement of the pilot valve spool 29 into the first pilot position FP1 allows the first pilot passageway 64 to communicate compressed air from the pilot inlet 31 to the first signal port channel 42. Further, in the first pilot position FP1, the pilot valve spool 29 may be positioned to prevent the communication of compressed air from the pilot inlet 31 to the second pilot passageway 65 and therefore the second signal port channel 45. The movement of the pilot valve spool 29 to the right or into the second pilot position FP2 may allow the second pilot passageway 65 to communicate compressed air from the pilot inlet 31 to the second signal port channel 45 while preventing the communication of compressed air to the first pilot passageway 64 and therefore the first signal port channel 42.


With continued reference to FIGS. 1-5, the main fluid valve assembly 34 may comprise a first pilot signal port 33, a second pilot signal port 46, a main fluid valve spool 35, a first inlet port 37, a second inlet port 39, a first outlet port 68, a second outlet port 69, and an exhaust port 32. The communication of compressed air to the first or second pilot signal port 33, 46 may cause the main fluid valve assembly 34 to move between a first and second main position MP1, MP2, respectively. In one embodiment, the communication of compressed air to the first pilot signal port 33 may cause the main fluid valve spool 35 to move from the first main position MP1 to the second main position MP2, shown in FIG. 3. The main fluid valve spool 35 may comprise a first main passageway 66 and a second main passageway 67. The movement of the main fluid valve spool 35 to the second main position MP2 may cause the second main passageway to be positioned to allow the communication of compressed air from the second main channel 41 through the second inlet port 39, out the second outlet port 69, and into the second diaphragm chamber 22 thereby causing the second diaphragm chamber 22 to be filled with compressed air, as illustrated by the line 44. Additionally, the first main passageway 66 of the main fluid valve spool 35 may be positioned to allow compressed air to be exhausted from the first diaphragm chamber 21 via the exhaust port 32, as illustrated by the line 48. The communication of compressed air to the second pilot signal port 46 may cause the main fluid valve spool 35 to move from the second main position MP2 to the first main position MP1 shown in FIG. 2. The movement of the main fluid valve spool 35 to the first main position MP1 may cause the first main passageway 66 to be positioned to allow the communication of compressed air from the first main channel 36 through the first inlet port 37, out the first outlet port 68, and into the first diaphragm chamber 21 thereby causing the second diaphragm chamber 22 to be filled with compressed air, as illustrated by the line 38. Additionally, the second main passageway 67 of the main fluid valve spool 35 may be positioned to allow compressed air to be exhausted from the second diaphragm chamber 22 via the exhaust port 32, as illustrated by the line 43. In another embodiment, the movement of the main valve spool 35 may be controlled electronically, for example, utilizing a solenoid and a controller, as disclosed in U.S. Pat. No. 6,036,445, which is herein incorporated by reference.


With reference now to FIGS. 1, 2, 3, 6a, 6b and 7, the air efficiency device 1 may comprise a sensor 2, a controller 5, and a valve assembly 4. The sensor 2 may comprise a contacting potentiometer or resistance sensor; an inductance sensor, such as a linear variable differential transformer (LVDT) sensor or an eddy current sensor; or, a non-contacting potentiometer displacement sensor. In one embodiment, the sensor 2 may comprise an embedded sensor sold by Sentrinsic LLC. Such sensor is described in U.S. patent application having publication number US 20070126416. In one embodiment, the sensor 2, as shown in FIG. 7, may comprise a sensor housing 50, a resistive member 51, a signal strip 52, and a sensor rod 53. The sensor housing 50 may be fixedly attached to the housing 11 and may enclose the resistive member 51, the signal strip 52, and a portion of the sensor rod 53. The sensor rod 53 may comprise an elongated, rigid structure similar to that of the connecting rod 30. The sensor rod 53 may extend through the sensor housing 50 and may be operatively connected to the first and second diaphragm assemblies 16, 20 such that the movement of the diaphragm assemblies 16, 20 causes the movement of the sensor rod 53 relative to the sensor housing 50. The resistive member 51 may comprise a variable resistant film that is fixedly coupled to the sensor housing and positioned substantially parallel to the sensor rod 53. The signal strip 52 may be fixedly attached to the sensor rod 53 such that the signal strip 52 extends substantially perpendicular relative to the resistive member 51. The signal strip 52 may extend at least partially across the resistive member 51 and may be capacitively coupled to the resistive member 51. In one embodiment, the sensor rod 53 may extend through the sensor housing 50 and may be fixedly attached at its respective ends to the first and second diaphragm plates 24, 25. The movement of the first and second diaphragm assemblies 16, 20 may cause the movement of the sensor rod 53 within the sensor housing 50 thereby causing the signal strip 52 to travel across at least a portion of the length of the resistive member 51.


With continued reference now to FIGS. 1, 2, 3, 6a, 6b and 7, the sensor 2 may be positioned to measure or detect the diaphragm motion of the first and second diaphragm assemblies 16, 20. The diaphragm motion may be defined as the motion of the respective diaphragm assemblies 16, 20 or, stated differently, the motion of the diaphragm 17, 23, the base plate 24, 25, and the connecting rod 30 moving as a single unit. The sensor 2 may continuously measure and detect the diaphragm motion as the diaphragm assemblies 16, 20 move between the first and second end of stroke positions EOS 1, EOS2, i.e., over the entire stroke of the diaphragm assembly. The sensor 2 may measure or detect the diaphragm motion for the first and second diaphragm assemblies 16, 20 independently from each other as the diaphragm assembly 16, 20 moves from the second end of stroke position EOS2 to the first end of stroke position EOS 1. In one embodiment, the sensor 2 may be positioned to detect the motion of the control rod 30. In another embodiment, the sensor 2 may be positioned to detect the motion of the first and second diaphragm plates 24, 25. In yet another embodiment, the air efficiency device 1 may comprise a plurality of sensors 2 wherein each sensor 2 is positioned within the housing 11 to independently detect the diaphragm motion of either the first diaphragm assembly 16 or the second diaphragm assembly 20 or a component thereof. Optionally, each of the sensors 2 may detect only a specific component of the diaphragm motion. For example, in one embodiment, a first sensor 2 may be positioned to detect the motion of the first diaphragm plate 24, a second sensor 2 may be positioned to detect the motion of the second diaphragm plate 25, and a third sensor 2 may be positioned to detect the motion of the control rod 30. U.S. Pat. No. 6,241,487, herein incorporated by reference, discloses the use of proximity sensors and an electrical interface positioned within the main fluid valve housing. U.S. Pat. No. 5,257,914, herein incorporated by reference, discloses the use of a sensor mechanism for sensing the position and rate of movement of the diaphragm assembly. The air efficiency device 1 may comprise any type and number of sensors 2 positioned to detect, measure, or sense the diaphragm motion, or a component thereof, with respect to any portion of the first or second diaphragm assemblies 16, 20 chosen with sound judgment by a person of ordinary skill in the art.


With continued reference to FIGS. 1, 2, 3, 6a, 6b and 7, the controller 5 may comprise a microprocessor or microcontroller that is operatively connected to the sensor 2 and the valve assembly 4. The controller 5 may comprise a processing unit, not shown, and an internal memory portion, not shown, and may perform calculations in accordance with the methods described herein. The controller 5 may receive and store a plurality of input signals transmitted by the sensor 2. The input signals may at least partially provide the controller 5 with information relating to the diaphragm motion of the first and second diaphragm assemblies 16, 20. The controller 5 may utilize a pre-programmed algorithm and the plurality of input signals to determine and transmit a plurality of output signals to control the operation of the valve assembly 4. The controller 5 may provide for the independent control of the valve assembly 4 such that the air efficiency device 1 optimizes the flow of compressed air into the pump 10 for each diaphragm assembly 16, 20 independently. In one embodiment, the controller 5 may comprise a 16-bit digital signal controller having a high-performance modified reduced instruction set computer (RISC) which is commercially available from a variety of suppliers known to one of ordinary skill in the art, such as but not limited to a motor control 16-bit digital signal controller having model number dsPIC30F4013-301/PT and supplied by Microchip Technology Inc. The controller 5 may be in communication with the sensor 2 and the valve assembly 4 via connections 8a and 8b respectively. In one embodiment, the connections 8a, 8b may comprise an electrically conductive wire or cable. The connections 8a, 8b may comprise any type of connection chosen with sound judgment by a person of ordinary skill in the art.


With continued reference to FIGS. 1, 2, 3, 6a, 6b and 7, the valve assembly 4 may comprise an air inlet valve 6 and an AED pilot valve 7. The valve assembly 4 may allow for the control of the flow of compressed air to the pump 10. The valve assembly 4 may be controlled by the controller 5 to allow the pump 10 to operate in a conventional mode CM, a learning mode LM, and an optimization mode OM as is more fully discussed below. The conventional mode CM may comprise the pump 10 operating in a conventional manner wherein the valve assembly 4 does not restrict the flow of compressed air into the pump 10 during the operation of the pump 10. In one embodiment, the air inlet valve 6 may comprise a normally open poppet valve and the AED pilot valve 7 may comprise a normally closed pilot valve thereby allowing the pump 10 to operate in the conventional mode CM during any period of operational failure of the air efficiency device 1. In another embodiment, the air inlet valve 6 may comprise a normally closed poppet valve and the AED pilot valve 7 may comprise a normally open pilot valve. The valve assembly 4 can comprise any type of valve assembly comprising any number and type of valves that allow for the conventional operation of the pump 10 during any period of operational failure of the air efficiency device 1 chosen with sound judgment by a person of ordinary skill in the art.


With continued reference now to FIGS. 1, 2, 3, 6a, 6b, and 7, in one embodiment, the AED pilot valve 7 may receive an output signal from the controller 5 that actuates a solenoid, not shown, in order to open the AED pilot valve 7. The opening of the AED pilot valve 7 may cause compressed air to flow from the compressed air supply 9 and into the AED pilot valve 7. The flow of compressed air into the AED pilot valve 7 may contact a stem, not shown, of the air inlet valve 6, thereby closing the air inlet valve 6. The closing of the air inlet valve 6 may prevent compressed air from entering into the pump 10. Similarly, the controller 5 may transmit, or cease transmitting, an output signal that then causes the AED pilot valve 7 to close. The closing of the AED pilot valve 7 may stop the flow of compressed air into the AED pilot valve 7 and allow the air inlet valve 6 to return to its normally open position wherein compressed air is again allowed to flow into the pump 10 to move the diaphragm assemblies 16, 20 to respective end of stroke left and end of stroke right positions.



FIGS. 6
a and 6b show yet another embodiment of the present invention where the pump receives a continuous flow of compressed air. As shown in FIG. 6a, the air inlet valve 6 may include a leakage or bypass for allowing a reduced amount of compressed air to be continuously and/or selectively supplied to the pump 10. In one embodiment, the air inlet valve 6 may comprise a poppet valve having an air bypass 6a formed therein that allows the reduced amount of compressed air to be supplied to the pump 10 while the air inlet valve 6 is closed. In another embodiment shown in FIGS. 6b, the air inlet valve 6 may comprise a 2-position valve that allows for a reduced amount of compressed air to be selectively provided to the pump 10. The 2-position valve comprises a large flow position and a reduced flow position such that the large flow position enables a less restrictive compressed air flow than the reduced flow position. In one embodiment, the air inlet valve 6 may comprise a flow restrictor 6b. The flow restrictor 6b may comprise a flow restrictor, a pressure restrictor, a variable flow restrictor, a variable pressure restrictor, or any other type of restrictor suitable for providing a reduced or restricted flow of compressed air chosen with sound judgment by a person of ordinary skill in the art. The air inlet valve 6 may comprise any type of valve chosen with sound judgment by a person of ordinary skill in the art. For example, the air inlet valve 6 may comprise a fully variable air supply valve where the degree of air flow reduction could be determined from any preset or predetermined percentage of available full flow, the initial air supply flow to a lesser percentage determined by, for example, determining the degree of velocity difference between Vmin and Vmax at XSL or XSR or at any other point chosen with sound judgment by a person of ordinary skill in the art. The pressure reduction could take place in one or more discrete steps or as a continuum from a high to a low pressure. To assure that the diaphragm assembly always has sufficient velocity to cause a pressure air reversal to occur at end of stroke where the diaphragm assembly physically actuates an end of stroke sensor, the minimum reduced pressure being supplied should not drop below the pressure necessary to cause activation of the end of stroke sensor which may, for example, be a standard pilot valve moved by contact with a portion of the valve assembly.


With continued reference to FIGS. 1, 2, 3, 6a, 6b and 7, the power supply 15 may comprise an integrated power supply attached to the pump housing 11. In one embodiment, the power supply 15 may be an integrated electric generator. The electric generator 15 may be operated by either pump inlet compressed air supply, pump exhaust, or an external power source. One advantage of the on board generator 15 is it renders the pump 10 portable. Often, the location or environment in which the pump 10 is utilized makes it impracticable to connect the pump 10 to a power outlet or stationary power source via external electrical wiring. It is also contemplated to be within the scope of the present invention that the pump 10 may be utilized in connection with a power outlet, such as a conventional wall socket, or a stationary power source via external electrical wiring.


With reference now to FIGS. 2, 3 and 8, the operation of the pump 10 will generally be described. The table below provides a partial listing and description of the reference figures used in describing the operation of the pump 10.













Reference



Figure
Description







XCL
Current position of the first diaphragm assembly


XCR
Current position of the second diaphragm assembly


XSL
Turndown position associated with the first diaphragm



assembly


XSR
Turndown position associated with the second diaphragm



assembly


VMINL
Minimum coast velocity associated with the first diaphragm



assembly


VMINR
Minimum coast velocity associated with the second diaphragm



assembly


VTERML
Termination velocity associated with the first diaphragm



assembly determined either as an instantaneous peak over a



stroke or as an average of multiple velocities taken over



the stroke


VTERMIL
Termination velocity associated with the second diaphragm



assembly (same as other)


VCL
Current velocity of the first diaphragm assembly


VCR
Current velocity of the second diaphragm assembly


S1R
First constant displacement value used to redefine the first



turndown position


S2R
Second constant displacement value used to redefine the first



turndown position


S3R
Third constant displacement value used to redefine the first



turndown position


S1L
Fourth constant displacement value used to redefine the



second turndown position


S2L
Fifth constant displacement value used to redefine the second



turndown position


S3L
Sixth constant displacement value used to redefine the second



turndown position









Generally, the pump 10 may operate by continuously transitioning between a first pump state PS1 and a second pump state PS2. The first pump state PS1, shown in FIG. 2, may comprise the pilot valve spool 29 in the first pilot position FP1; the main fluid valve spool 35 in the second main position MP2 (shown in FIG. 3); and, the first and second chambers 12, 13 in the first end of stroke position EOS 1. The second pump state PS2, shown in FIG. 3, may comprise the pilot valve spool 29 in the second pilot position FP2; the main fluid valve spool 35 in the first main position MP1; and, the first and second chambers 12, 13 in the second end of stroke position EOS2. The transition of the pump 10 from the first pump state PS1 to the second pump state PS2 may begin by a compressed air supply 9 supplying compressed air through the AED valve assembly 4 to the pump 10 via the air inlet valve 6, step 100. The compressed air may flow into the pilot valve housing 28 via the pilot inlet 31. With the pilot valve spool 29 in the first pilot position FP1, a portion of the compressed air is communicated to the first pilot signal port 33 of the main fluid valve assembly 34, as illustrated by the line 40, as well as to the first and second main channels 36, 41. In one embodiment, the main fluid valve spool 35 may initially be in the first main position MP1 and the initial communication of the compressed air to the first pilot signal port 33 may cause the main fluid valve spool 35 to move from the first main position MP1 to the second main position MP2. The second main channel 41 may be in fluid communication with the second inlet port 39. In the second main position MP2, the second main passageway 67 of the main fluid valve spool 35 may allow compressed air to flow through the pilot valve housing 28 and into the second diaphragm chamber 22 as described above, step 110. Additionally, the main fluid valve spool 35 may prevent or block compressed air from being communicated through the pilot valve housing 28 to the first diaphragm chamber 21. Instead, the main fluid valve spool 35 may allow compressed air to be vented or exhausted from the first diaphragm chamber 21 through the exhaust port 32 as described above, step 112.


With continued reference to FIGS. 2, 3 and 8, the compressed air may continue to be communicated into the second diaphragm chamber 22 and exhausted from the first diaphragm chamber 21. The continued communication and exhaustion of compressed air into the second diaphragm chamber 22 and from the first diaphragm chamber 21 may cause the second diaphragm assembly 20 to move away from the first diaphragm position DP1R and towards the second diaphragm position DP2R and may cause the first diaphragm assembly 16 to move away from the second diaphragm position DP2L and towards the first diaphragm position DP1L. The sensor 2 may substantially continuously measure or detect the diaphragm motion of the second diaphragm assembly 20 as the second diaphragm assembly 20 moves from the first diaphragm position DP1R to the second diaphragm position DP2R, step 114. In one embodiment, the sensor 2 may substantially continuously transmit data representing the current displacement and velocity of the second diaphragm plate 25 as the second diaphragm assembly 20 moves from the first diaphragm position DP1R to the second diaphragm position DP2R. The controller 5 may receive the data transmitted by the sensor 2 and may determine when the second diaphragm assembly 20, or a component thereof, reaches a first predetermined turndown position XSR, step 116. The first turndown position XSR may be located between the first diaphragm position DP1R and the second diaphragm position DP2R.


With continued reference to FIGS. 2, 3, and 8, in one embodiment, the first turndown position XSR may be determined by the pump 10 initially operating in the learning mode LM. The learning mode LM may comprise the pump 10 operating in the conventional mode CM for a predetermined number of pump strokes or pump cycles, for example, 4 pump cycles. The sensor 2 may continuously monitor the diaphragm motion of the first and/or second diaphragm assemblies 16, 20 and transmit the data to the controller 5. The controller 5 may utilize the data transmitted by the sensor 2 to determine an average velocity Vavg. The average velocity Vavg may comprise the average velocity of the first and/or second diaphragm assemblies 16, 20 at the second diaphragm position DP2R, DP2L while operating in the learning mode LM. In another embodiment, the average velocity Vavg may comprise the average velocity of the first and/or second diaphragm assembly 16, 20 as the first and/or second diaphragm assembly 16, 20 moves between the first diaphragm position DP1R, DP1L and the second diaphragm position DP2R, DP2L. The controller 5 may determine the average velocity Vavg independently for the first and second diaphragm assembly 16, 20. The first turndown position XSR may comprise a position that is calculated to at least partially cause the velocity of the first and/or second diaphragm assembly 16, 20 at the second diaphragm position DP2R, DP2L to be a predetermined percentage of the average velocity Vavg. For example, in one embodiment, the first turndown position XSR may comprise a position that is calculated to at least partially cause the velocity of the first and/or second diaphragm assembly 16, 20 to be about 95% of the average velocity Vavg. The controller 5 may allow for the user to selectively change the predetermined percentage of the average velocity Vavg during the operation of the pump 10 thereby adjusting or redefining the first turndown point XSR. In another embodiment, the first turndown position XSR may initially comprise an arbitrarily selected point that is dynamically refined and/or adjusted by the air efficiency device 1 to substantially reach an optimum value as described below.


With continued reference to FIGS. 2, 3 and 8, upon determining that the second diaphragm assembly 20 has reached or passed the first turndown position XSR, the air efficiency device 1 may cause the flow of compressed air into the pump 10 to be turned down to a lower flow rate, step 118. In one embodiment, the controller 5 may cause an output signal to be transmitted to the AED pilot valve 7, which in turn may cause the air inlet valve 6 to at least partially close thereby causing the flow of compressed air into the pump 10 to decrease. In another embodiment, the AED pilot valve 7 may cause the air inlet valve 6 to partially close thereby uniformly decreasing the amount of compressed air entering into the pump 10 over a predetermined period. The sensor 2 may continue to transmit detected diaphragm motion data to the controller 5 as the second diaphragm assembly 20 continues to move from the first turndown position XSR to the second diaphragm position DP2R, step 120. The controller 5 may receive the transmitted data from the sensor 2 and may determine if a current second diaphragm velocity VCR falls below a predetermined minimum coast velocity VMINR, step 122. The minimum coast velocity VMINR may comprise the minimum diaphragm assembly velocity allowed after the diaphragm assembly has reached the first turndown position XSR. If the controller 5 determines that the current second diaphragm velocity VCR is less than the predetermined minimum coast velocity VMINR, the controller 5 may cause the air inlet valve 6 to open or to be turned up to provide an increased flow rate of compressed air into the pump 10, step 124. It should be understood that the minimum coast velocity VMINR or VMINL may be detected at any selected point, or continuously, to the extent the sensor 2 is able to provide feedback to the controller 5. If the minimum coast velocity VMINR or VMINL is reached at any point before end of stroke, additional compressed air will be supplied if it has been reduced. In another embodiment where the compressed air is reduced, the restrictor 6b will need to be adjusted to increase flow of the compressed air, and hence, result in a longer time period before diaphragm assembly reaches end of stroke. More specifically, the continuously supplied lower flow compressed air will increase enough pressure to continue to move the diaphragm assembly and will build sufficient pressure when the diaphragm assembly contacts the pilot valve, which will shift the pilot valve. Pressure will continue to increase upon any stoppage in the diaphragm assembly back to a maximum line pressure.


With continued reference to FIGS. 2, 3, and 8, in one embodiment, the controller 5 may transmit an output signal to the AED pilot valve 7 that causes the AED pilot valve 7 to close thereby allowing the air inlet valve 6 to return to its normally open position. The controller 5 may detect the potential for the pump 10 to stall and may adjust or redefine the first turndown position XSR to keep the air inlet valve 6 open in order to increase the amount of compress air provided to the pump 10. The controller 5 may adjust or redefine the first turndown position XSR by adding a first constant displacement value S1R to the first turndown position XSR, thereby increasing the amount of time the air inlet valve 6 remains fully open, step 125. The potential for the pump 10 to stall may be detected by determining that the current second diaphragm velocity VCR is less than the predetermined minimum coast velocity VMINR before the second diaphragm assembly 20 reaches the second diaphragm position DP2R. If the controller 5 determines that the current second diaphragm velocity VCR is less than the predetermined minimum coast velocity VMINR before the second diaphragm assembly 20 reaches the second diaphragm position DP2R, the controller 5 may cause the diaphragm motion data received from the sensor 2 relating to that specific stroke to be discarded and not stored or saved.


With continued reference to FIGS. 2, 3, and 8, the controller 5 may next determine when the second diaphragm assembly 20 substantially reaches the second diaphragm position DP2R and may then determine the second diaphragm velocity VCR, step 126. If the controller 5 determines that the second diaphragm velocity VCR is greater than a predetermined maximum termination velocity VTERMIL or less than the predetermined minimum coast velocity VMINR, the controller 5 may adjust or redefine the first turndown position XSR, step 128. The second diaphragm velocity VCR being greater than the predetermined maximum termination velocity VTERMIL as the second diaphragm assembly 20 substantially reaches the second diaphragm position DP2R indicates an opportunity to save air by utilizing a lesser amount of compressed air on the next stroke. If the controller 5 determines that the second diaphragm velocity VCR is greater than the predetermined maximum termination velocity VTERMIL as the second diaphragm assembly 20 substantially reaches the second diaphragm position DP2R, thereby indicating that the second diaphragm assembly 20 is running too quickly when nearing end of stroke, the controller 5 may adjust or redefine the first turndown position XSR by moving the first turndown position XSR closer to the first diaphragm position DP1R. In one embodiment, the controller 5 may redefine the first turndown position XSR by subtracting a second constant displacement value S2R from the first turndown position XSR. The controller 5 may determine that the second diaphragm velocity VCR is less than the predetermined minimum coast velocity VMINR as the second diaphragm assembly 20 substantially reaches the second diaphragm position DP2R thereby indicating that the first diaphragm assembly 16 is running too slowly when nearing end of stroke. As such, the pump 10 is using very little compressed air but sacrificing significant output flow. The controller 5 may adjust or redefine the first turndown position XSR in order to cause a greater amount of compressed air to enter the pump 10. In one embodiment, the controller 5 may redefine the first turndown position XSR by adding a third constant displacement value S3R to the first turndown position XSR. Upon passing the second diaphragm position DP2R and reaching the second end of stroke position EOS2, the second diaphragm assembly 20 may turnaround or begin moving in the opposite direction toward the first diaphragm position DP1R, step 130. The controller 5 may save or store the data received from the sensor 2 as well as any redefined first turndown position XSR.


With continued reference to FIGS. 2, 3, and 8, upon the second diaphragm assembly 20 reaching the second end of stroke position EOS2, the pump 10 may comprise the second pump state PS2. The first diaphragm plate 24 may be in contact with the actuator pin 27 causing the pilot valve spool 29 to move to the second pilot position FP2 wherein compressed air is communicated through the pilot valve housing 28 to the second pilot signal port 46 of the main fluid valve assembly 34, as shown in FIG. 3. The continued communication of compressed air to the second pilot signal port 46 may cause the main fluid valve spool 35 to shift or move to the left, away from the second main position MP2 and into the first main position MP1, shown in FIG. 2. In the first main position MP1, the main fluid valve spool 35 of the main fluid valve 34 may thereby block or prevent the communication of compressed air through the second inlet port 39 and may position the first inlet port 37 to allow compressed air to be communicated from the first main channel 36 to the first diaphragm chamber 21 as described above. While the first diaphragm chamber 21 is being filled with compressed air, the second diaphragm chamber 22 may be vented through the exhaust port 32 of the main fluid valve assembly 34 as described above. The sensor 2 may substantially continuously monitor, measure, and/or detect the diaphragm motion of the first diaphragm assembly 16 as the first diaphragm assembly 16 moves from the first diaphragm position DP1L to the second diaphragm position DP2L. The controller 5 may receive the data transmitted by the sensor 2 and may determine when the first diaphragm assembly 16, or a component thereof, reaches a second predetermined turndown position XSL. The second turndown position XSL may be located between the first position DP1L and the second position DP2L. The second turndown position XSL may be calculated while the pump 10 is operating in the learning mode LM in a similar manner as that of the first turndown position XSR. In one embodiment, the air efficiency device 1 may utilize the same turndown position for both the first and second diaphragm assemblies 16, 20 throughout the operation of the pump 10. In other words, the first turndown position is determined on one side (left or right) and used as the reference. The other side is derived based on general symmetry of the pump. This results in an independent turndown position and a dependent turndown position. In another embodiment, the second turndown position XSL may initially comprise an arbitrarily selected point that is dynamically refined and/or adjusted by the air efficiency device 1 to substantially reach an optimum value.


With continued reference to FIGS. 2, 3, and 8, upon determining that the first diaphragm assembly 16 has reached or passed the second turndown position XSL, the air efficiency device 1 may cause the flow of compressed air into the pump 10 to be turned down to a lower flow rate which may or may not be the same as the lower flow rate utilized for the second diaphragm assembly 20. The sensor 2 may continue to transmit detected diaphragm motion data to the controller 5 as the first diaphragm assembly 16 continues to move from the second turndown position XSL to the second diaphragm position DP2L. The controller 5 may receive the transmitted data from the sensor 2 and may determine if a current first diaphragm velocity VCL falls below a second predetermined minimum coast velocity VminL before the first diaphragm assembly 16 reaches the second diaphragm position DP2L. The second minimum coast velocity VminL may or may not comprise the same minimum diaphragm coast velocity VminR corresponding to the second diaphragm assembly 20. If the controller 5 determines that the current first diaphragm velocity VCL is less than the second predetermined minimum coast velocity VminL before the first diaphragm reaches the second diaphragm position DP2L, the controller 5 may cause the air inlet valve 6 to open or to be turned up to an increased flow rate that may or may not be the same as the increased flow rate utilized with the second diaphragm assembly 20. The controller 5 may detect the potential for the pump 10 to stall and may adjust or redefine the second turndown position XSL. In one embodiment, the controller 5 may redefine the second turndown position XSL by adding a fourth constant displacement value S1L to the second turndown position XSL. The fourth constant displacement value S1L may or may not be the same as the first constant displacement value S1R utilized with the second diaphragm assembly 20. If the controller 5 determines that the current first diaphragm velocity VCL is less than the second predetermined minimum coast velocity VMINL before the first diaphragm assembly 16 reaches the second diaphragm position DP2L, the controller 5 may cause the diaphragm motion data received from the sensor 2 relating to that specific stroke to be discarded and not stored or saved.


With continued reference to FIGS. 2, 3, and 8, the controller 5 may next determine the second diaphragm velocity VCL as the first diaphragm assembly 16 substantially reaches the second diaphragm position DP2L. If the controller 5 determines that the first diaphragm velocity VCL is greater than a second predetermined maximum termination velocity VTERML or less than the second predetermined minimum coast velocity VMINL, the controller 5 may redefine the second turndown position XSL. If the controller 5 determines that the second diaphragm velocity VCL is greater than the second predetermined maximum termination velocity VTERML as the first diaphragm assembly 16 substantially reaches the second diaphragm position DP2L, thereby indicating that the first diaphragm assembly 16 is running too quickly when nearing end of stroke, the controller 5 may redefine the second turndown position XSL by subtracting a fifth constant displacement value S2L from the second turndown position XSL. The fifth constant displacement valve S2L may or may not be the same as the second constant displacement value S2R utilized with the second diaphragm assembly 20. If the controller 5 determines that the second diaphragm velocity VCL is less than the second predetermined minimum coast velocity VMINL as the first diaphragm assembly 16 substantially reaches the second diaphragm position DP2L, thereby indicating that the first diaphragm assembly 16 is running too slowly when nearing end of stroke, the controller 5 may redefine the second turndown position XSL by adding a sixth constant displacement value S3L to the first turndown position XSL. Upon passing the second diaphragm position DP2L and reaching the first end of stroke position EOS1, the first diaphragm assembly 16 may turnaround or begin moving in the opposite direction toward the first diaphragm position DP1L, wherein the sensor 2 monitors the diaphragm motion of the second diaphragm assembly 20 moving from the first diaphragm position DP1R to the second diaphragm position DP2R and the method repeats itself utilizing any redefined values of XSR as necessary.


The controller 5 may save or store the data received from the sensor 2 as well as any redefined turndown positions XSR, XSL for the diaphragm motion of the first and second diaphragm assemblies 16, 20. The data stored relating to the diaphragm motion of the second diaphragm assembly 20 may be stored separately from the data relating to the diaphragm motion of the first diaphragm assembly 16. In another embodiment, the air efficiency device 1 may utilize a single turndown position for both the first and second diaphragm assemblies 16, 20 such that the first turndown position XSR, and any adjustments made thereto, is utilized as the second turndown position XSL and any adjustments then made to the second turndown position XSL subsequently comprises the first turndown position XSR such that the turndown position is dynamically adjusted to optimize the flow of compressed air into the pump 10. In one embodiment, the second turndown position is dependent of the first turndown position, wherein the second turndown position may be determined by the symmetry of the pump 10. The controller 5 may utilize the same or different predetermined values for any or all of the predetermined values utilized to adjust or optimize the diaphragm motion of the first and second diaphragm assemblies 16, 20. The predetermined values may be dependent upon the type of pump and the material to be pumped by the pump 10. Additionally, the predetermined values may be may be specific to the pump 10. The predetermined values can be determined by a person of ordinary skill in the art without undue experimentation. In one embodiment, the air efficiency device 1 may comprise an output device, not shown, that allows the user to download or otherwise access the data relating to the diaphragm motion of the first and second diaphragm assemblies 16, 20. Additionally, the air efficiency device 1 may comprise an input device, not shown, that allows the user to define or change the predetermined values, for example the first turndown point XSR or the predetermined percentage of time the air inlet valve is open.


While operating in the optimization mode OM, the controller 5 may cause the pump 10 to periodically operate in the learning mode LM in order to re-define the first and/or second turndown positions XSR, XSL. In one embodiment, the controller 5 may cause the pump 10 to periodically operate in the learning mode LM after the pump 10 operates for a predetermined number of strokes or cycles in the optimization mode OM. In another embodiment, the controller 5 may cause the pump 10 to re-enter the learning mode LM upon determining that the velocity of the first and/or second diaphragm assemblies 16, 20 at the second diaphragm position DP2R, DP2L is outside of a predetermined range of velocities. Optionally, the air efficiency device 1 may allow the user to selectively cause the pump 10 to operate in the learning mode LM.


In summary, the air efficiency device 1 monitors the diaphragm motion of the pump 10 as the first and second diaphragm assemblies transition between the two end of stroke positions in order to optimize the amount of compressed air supplied to the pump 10. The air efficiency device 1 may substantially continuously monitor the velocity of one of the diaphragm assemblies 16, 20 of the pump 10 to determine the current position of the diaphragm assembly as the diaphragm assembly travels between a first and second diaphragm positions. Upon determining that the diaphragm assembly has reached a predetermined position, the air efficiency device 1 may cause the supply or flow rate of compressed air to be reduced while the diaphragm assembly continues to move to the second diaphragm position. The air efficiency device 1 continues to monitor the diaphragm motion of the diaphragm assembly until the diaphragm assembly reaches the second diaphragm position. If the air efficiency device determines that the velocity of the diaphragm assembly falls below a predetermined minimum velocity prior to the diaphragm assembly reaching the second diaphragm position, the supply or flow rate of compressed air to the pump is increased and the predetermined position is redefined as described above. If the air efficiency device determines that the velocity of the diaphragm assembly is either greater than a predetermined termination velocity or less than the predetermined minimum velocity the predetermined position is redefined. The diaphragm assembly then reaches end of stroke and the air efficiency device 1 monitors the diaphragm motion of the other diaphragm assembly as the diaphragm assemblies move in the opposite direction and similarly redefines a second predetermined position as described above. In one embodiment, subsequent monitoring of either diaphragm assembly by the air efficiency device 1 may utilize any redefined positions previously determined for that specific diaphragm assembly. In another embodiment, the subsequent monitoring of either diaphragm assembly by the air efficiency device 1 may utilized any redefined positions previously determined for the opposite diaphragm assembly. By utilizing the inventive method described herein, the pump self-adjusts to determine the optimum turndown point so as to provide for air savings, and thus energy savings.



FIG. 9 is a flow diagram illustrating an exemplary method 900 for optimizing an amount of supply compressed air utilized during operation of a pump. One or more portions of one or more implementations of exemplary method 900 are described above in FIGS. 1-8. The exemplary method 900 begins at 902. At 904, a determination may be made as to whether the first current position (XCL) for the first diaphragm assembly (e.g., 16 of FIGS. 1-3) of a pump has met a first turndown position (XSL). In one implementation, a first sensor that is configured to detect the first diaphragm assembly at the first turndown position (XSL) can be used to determination whether the first current position (XCL) has met a first turndown position (XSL)


In one implementation, the first diaphragm assembly of the pump may be disposed in a first diaphragm chamber, and may comprises the first end-of-stroke position (EOS1) and the first turndown position (XSL), where the first turndown position (XSL) comprises a different position of the first diaphragm assembly in the first diaphragm chamber than the first end-of-stroke position (EOS1). Further, the pump can comprise a second diaphragm assembly (e.g., 20 of FIGS. 1-3) that is disposed in a second diaphragm chamber. The second diaphragm assembly can comprises a second end-of-stroke position (EOS2) and a second turndown position (XSR), where the second turndown position-(XSR) comprises a different position of the second diaphragm assembly in the second diaphragm chamber than the second end-of-stroke position (EOS2).


At 906 in the exemplary method 900, the supply compressed air to the first diaphragm chamber can be decreased upon determining that the first current position (XCL) has met the first turndown position (XSL). At 908, a determination may be made as to whether the first current position (XCL) has met the first end-of-stroke position (EOS1). In one implementation, a second sensor that is configured to detect the first diaphragm assembly at the first end-of-stroke position (EOS1) can be used to determine whether the first current position (XCL) has met the first end-of-stroke position (EOS1). At 910, upon determining that the first current position (XCL) has met the first end-of-stroke position (EOS1), supply compressed air can be increased to the second diaphragm chamber.


Having increased the supply compressed air to the second diaphragm chamber, the exemplary method 900 ends at 912.



FIG. 10 is a flow diagram illustrating an example embodiment 1000 where one or more portions of one or more techniques, described herein, may implemented. One or more portions of one or more implementations of example embodiment 1000 are described above in FIGS. 1-8. At 1002 of the exemplary embodiment 100, the pump may be operated. For example the pump may be energized (e.g., with compressed air, electricity, and/or some other form of power), thereby enabling the pump to operate in an intended manner. At 1004, compressed supply air can be provided to first pump chamber, comprising the first diaphragm assembly. For example, supplying compressed air to the first pump chamber may result in the first diaphragm assembly translating toward the first end-of-stroke position (EOS1).


At 1006, the first diaphragm assembly can operably connect with the first sensor. In one implementation, the first sensor can be configured to detect that the first diaphragm assembly has met the first turndown position (XSL). For example, the first sensor may comprise a mechanical sensor (e.g., 27 of FIGS. 2 and 3), and/or the first sensor may comprise an electrical-based sensor (e.g., 2 of FIG. 7). Further, in one implementation, the first diaphragm assembly contacting the first sensor may result in a first signal being transmitted (e.g., by the sensor). For example, the first signal may comprise a mechanical-based signal, and/or may comprise an electrical-based signal.


At 1008, upon the first diaphragm assembly operably connecting with the first sensor (e.g., and receiving the first signal), the compressed supply air may be reduced to the first pump chamber. At 1010, the first diaphragm assembly may contact the second sensor, where the second sensor detects the first end-of-stroke position (EOS1) of the first diaphragm assembly. For example, the first diaphragm assembly can continue translating toward the first end-of-stroke position (EOS1), even though the process air has been reduced in the first chamber. In this example, the first diaphragm assembly can continue translating until it contacts the second sensor, indicating that it has met the first end-of-stroke position (EOS1).


At 1012, upon the first diaphragm assembly operably connecting with the second sensor (e.g., and receiving a second signal, such as a mechanical-based and/or electrical-based signal), the compressed supply air may be increased to the second pump chamber. In this way, for example, the second diaphragm assembly may be translating toward the second end-of-stroke position (EOS2). At 1014, the second diaphragm assembly can contact a third sensor, where the third sensor can be used to detect that the second diaphragm assembly has met the second turndown position-(XSR). For example, the third sensor may comprise a mechanical sensor, and/or the third sensor may comprise an electrical-based sensor. Further, in one implementation, the second diaphragm assembly contacting the third sensor may result in a second signal being transmitted (e.g., by the sensor). For example, the second signal may comprise a mechanical-based signal, and/or may comprise an electrical-based signal.


At 1016, upon the second diaphragm assembly operably connecting with the third sensor (e.g., and receiving the second signal), the compressed supply air may be reduced to the second pump chamber. At 1018, the second diaphragm assembly may contact a fourth sensor, where the fourth sensor detects the second end-of-stroke position (EOS2) of the second diaphragm assembly. For example, the second diaphragm assembly can continue translating toward the second end-of-stroke position (EOS2), even though the process air has been reduced in the second chamber. In this example, the second diaphragm assembly can continue translating until it contacts the fourth sensor, indicating that it has met the second end-of-stroke position (EOS2). In one implementation, the process 1004-1018 may be iterated, for example, at least until the pump is shut-down (e.g., de-energized).


The word “exemplary” is used herein to mean serving as an example, instance or illustration. Any aspect or design described herein as “exemplary” is not necessarily to be construed as advantageous over other aspects or designs. Rather, use of the word exemplary is intended to present concepts in a concrete fashion. As used in this application, the term “or” is intended to mean an inclusive “or” rather than an exclusive “or.” That is, unless specified otherwise, or clear from context, “X employs A or B” is intended to mean any of the natural inclusive permutations. That is, if X employs A; X employs B; or X employs both A and B, then “X employs A or B” is satisfied under any of the foregoing instances. Further, at least one of A and B and/or the like generally means A or B or both A and B. In addition, the articles “a” and “an” as used in this application and the appended claims may generally be construed to mean “one or more” unless specified otherwise or clear from context to be directed to a singular form.


Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms of implementing the claims. Of course, those skilled in the art will recognize many modifications may be made to this configuration without departing from the scope or spirit of the claimed subject matter.


Also, although the disclosure has been shown and described with respect to one or more implementations, equivalent alterations and modifications will occur to others skilled in the art based upon a reading and understanding of this specification and the annexed drawings. The disclosure includes all such modifications and alterations and is limited only by the scope of the following claims. In particular regard to the various functions performed by the above described components (e.g., elements, resources, etc.), the terms used to describe such components are intended to correspond, unless otherwise indicated, to any component which performs the specified function of the described component (e.g., that is functionally equivalent), even though not structurally equivalent to the disclosed structure which performs the function in the herein illustrated exemplary implementations of the disclosure.


In addition, while a particular feature of the disclosure may have been disclosed with respect to only one of several implementations, such feature may be combined with one or more other features of the other implementations as may be desired and advantageous for any given or particular application. Furthermore, to the extent that the terms “includes,” “having,” “has,” “with,” or variants thereof are used in either the detailed description or the claims, such terms are intended to be inclusive in a manner similar to the term “comprising.”


The implementations have been described, hereinabove. It will be apparent to those skilled in the art that the above methods and apparatuses may incorporate changes and modifications without departing from the general scope of this invention. It is intended to include all such modifications and alterations in so far as they come within the scope of the appended claims or the equivalents thereof.

Claims
  • 1. A method for optimizing an amount of supply compressed air utilized during operation of a pump, comprising: determining that a first current position (XCL) for a first diaphragm assembly of a pump has met a first turndown position (XSL), using a first sensor configured to detect the first diaphragm assembly at the first turndown position (XSL), the pump comprising: the first diaphragm assembly disposed in a first diaphragm chamber, wherein the first diaphragm assembly comprises a first end-of-stroke position (EOS1) and the first turndown position (XSL), the first turndown position (XSL) comprising a different position of the first diaphragm assembly in the first diaphragm chamber than the first end-of-stroke position (EOS1); anda second diaphragm assembly disposed in a second diaphragm chamber, wherein the second diaphragm assembly comprises a second end-of-stroke position (EOS2) and a second turndown position-(XSR), the second turndown position-(XSR) comprising a different position of the second diaphragm assembly in the second diaphragm chamber than the second end-of-stroke position (EOS2);decreasing supply compressed air to the first diaphragm chamber upon determining that the first current position (XCL) has met the first turndown position (XSL); andincreasing supply compressed air to the second diaphragm chamber upon determining that the first current position (XCL) has met the first end-of-stroke position (EOS1), using a second sensor configured to detect the first diaphragm assembly at the first end-of-stroke position (EOS1).
  • 2. The method of claim 1, comprising adjusting the first sensor, resulting in an adjustment of the first turndown position (XSL).
  • 3. The method of claim 1, comprising: receiving a first signal from the first sensor;decreasing the supply compressed air acting on the first diaphragm assembly upon receiving the first signal;receiving a second signal from the second sensor; andincreasing supply compressed air acting on the second diaphragm assembly upon receiving the second signal.
  • 4. The method of claim 3, one or more of: receiving the first signal from the first sensor comprising the first diaphragm assembly in operative communication with the first sensor; andreceiving the second signal from the second sensor comprising the first diaphragm assembly in operative communication with the second sensor.
  • 5. The method of claim 3, one or more of: receiving the first signal from the first sensor comprising receiving an electrical-based signal from the first sensor; andreceiving the second signal from the second sensor comprising receiving an electrical-based signal from the second sensor.
  • 6. The method of claim 3, one or more of: receiving the first signal from the first sensor comprising receiving a mechanical-based signal from the first sensor; andreceiving the second signal from the second sensor comprising receiving a mechanical-based signal from the second sensor.
  • 7. The method of claim 1, comprising: determining that a second current position (XCR) for the second diaphragm assembly has met the second turndown position (XSR) using a third sensor configured to detect the second diaphragm assembly at the second turndown position (XSR); anddecreasing supply compressed air to the second diaphragm chamber.
  • 8. The method of claim 7, comprising: determining that a second current position (XCR) for the second diaphragm assembly has met the second end-of-stroke position (EOS2) using a fourth sensor configured to detect the second diaphragm assembly at the second end-of-stroke position (EOS2); andincreasing supply compressed air to the first diaphragm chamber.
  • 9. The method of claim 8, comprising: receiving a third signal from the third sensor;decreasing supply compressed air acting on the second diaphragm assembly upon receiving the third signal;receiving a fourth signal from the fourth sensor; andincreasing supply compressed air acting on the first diaphragm assembly upon receiving the fourth signal.
  • 10. The method of claim 7, comprising adjusting the third sensor, resulting in an adjustment of the second turndown position-(XSR).
  • 11. The method of claim 1, comprising identifying the first turndown position (XSL) based at least upon a velocity of the first diaphragm assembly.
  • 12. The method of claim 1, comprising the first current position (XCL) meeting the first turndown position (XSL).
  • 13. The method of claim 1, comprising calculating the first turndown position (XSL) based at least upon a first current velocity (VCL), a first minimum velocity (VMINL) and a first termination velocity (VTERML).
  • 14. The method of claim 13, calculating the first turndown position (XSL) comprising one of: indicating that the first turndown position (XSL) has met the first current position (XCL) if the first current velocity (VCL) is less than or equal to the first termination velocity (VTERML) and greater than or equal to the first minimum velocity (VMINL); orredefining the first turndown position (XSL) if the first current velocity (VCL) is one of: less than the first minimum velocity (VMINL); andgreater than the first termination velocity (VTERML).
  • 15. The method of claim 14, redefining the first turndown position (XSL) resulting in a first redefined first turndown position (XSL1) that comprises a sum of the first turndown position (XSL) and a first constant displacement value (SIL), wherein the first redefined first turndown position (XSL1) is utilized during a subsequent pump stroke when the first diaphragm assembly is translated from the first end-of-stroke position (EOS1) toward the second end-of-stroke position (EOS2).
  • 16. The method of claim 1, comprising operating the pump in a start-up mode, comprising the pump operating with a preset first turndown position (XSL).
  • 17. The method of claim 1, comprising operating the pump in a turndown position determination mode, comprising pump operation during which a desired first turndown position (XSL) is determined.
  • 18. The method of claim 17, comprising operating the pump in an efficiency mode, comprising pump operation during which said desired first turndown position (XSL) is utilized.
  • 19. The method of claim 1, comprising operating the pump in a conventional mode, comprising pump operation that does not utilize the first turndown position (XSL).
  • 20. A method for optimizing an amount of supply compressed air utilized during operation of a pump, comprising: operating a first diaphragm assembly disposed in a first diaphragm chamber of the pump, the first diaphragm assembly comprising a first end-of-stroke position (EOS1) and a different first turndown position (XSL), comprising: detecting that the first diaphragm assembly has met the first turndown position (XSL) in the first diaphragm chamber using a first sensor; andreducing supply compressed air to the first diaphragm chamber; andoperating a second diaphragm assembly disposed in a second diaphragm chamber of the pump, the second diaphragm assembly comprising a second turndown position (XSR), comprising: detecting that the first diaphragm assembly has met the first end-of-stroke position (EOS1) in the first diaphragm chamber using a second sensor; andincreasing supply compressed air to the second diaphragm chamber;detecting that the second diaphragm assembly has met the second turndown position (XSR) in the second diaphragm chamber using a third sensor; andreducing supply compressed air to the second diaphragm chamber.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation application of, and claims priority to, U.S. Ser. No. 13/912,818, filed Jun. 7, 2013, which is a continuation application of, and claims priority to, U.S. Ser. No. 12/693,044, filed Jan. 25, 2010, which claims priority to a provisional application having Ser. No. 61/146,959, filed Jan. 23, 2009, all of which are incorporated herein by reference.

Provisional Applications (1)
Number Date Country
61146959 Jan 2009 US
Continuations (2)
Number Date Country
Parent 13912818 Jun 2013 US
Child 14050973 US
Parent 12693044 Jan 2010 US
Child 13912818 US