The invention relates to a seal-less piston pump, and more particularly, to a seal-less liquid propane injection pump for an engine such as a diesel engine on a vehicle.
In conventional diesel engines, it is known to inject liquid propane (LPG) into the fuel-air mixture in the fuel header or manifold of the engine. This is done to reduce emissions and increase performance of the vehicle. Typically, the vehicle would include an LPG tank and a pump which is in fluid communication with the LPG tank and pumps the LPG or other fluid into the engine manifold. In a known configuration, such a pump may be an in-tank, submersible turbine pump. However, such a configuration is known to have disadvantages associated therewith.
It therefore is an object of the invention to overcome disadvantages associated with prior art pumps used to deliver liquefied gases.
The invention relates to a fuel supply system for a vehicle, which uses an externally-mounted positive displacement pump to supply the LPG from the storage tank to the engine. More particularly, the invention relates to a dual-acting, seal-less LPG injection pump, which is formed as a piston pump for pumping the fluid from the storage tank to the engine intake manifold. The term seal-less shall refer to a pump that has only stationary seals, and no moving or dynamic seals. In the preferred embodiment, the pump is provided in a dual-acting, single piston configuration, wherein the pump piston is driven by a pneumatic drive actuator which may be formed as a pneumatic drive cylinder or other mechanical drive mechanism that reciprocates the piston. The drive actuator is operated using the vehicle's pneumatic air system, wherein the pressurized air of this system alternatingly drives or reciprocates the pneumatic drive actuator, which in turn drives the piston. The pressure cylinder of the actuator is operatively connected to the pump piston through a seal-less connection, such that movement of one end of the drive cylinder effects a direct, corresponding movement of the piston.
As to the seal-less connection, the inventive pump uses a contained, tubular pump housing, which is formed as a thin-walled pump tube that internally defines a pump chamber. The piston is wholly contained within the elongate pump chamber wherein the piston is driven in a reciprocating manner. Preferably, the piston is dual acting so that each direction of movement defines a pumping stroke. The vehicle's air system is used to pressurize and drive the piston through both pumping strokes.
More particularly, to drivingly connect the pump piston and drive cylinder, an inner magnet set is provided on the piston within the pump chamber, and an outer magnet set is positioned outside of the pump housing adjacent the inner magnet set to form an indirect, magnetic connection through the attractive magnetic fields defined by the magnet sets. Preferably, the tube is made from non-magnetic material, such as stainless steel, but can be constructed from any non-magnetic material. The outer magnet set is carried in a movable main body which in turn is directly connected to the drive cylinder. Reciprocation of the main body also reciprocates the piston due to the magnetic connection therebetween. Since the magnetic connection between the magnet sets requires no penetrations through the pump housing, a seal-less connection is formed between the piston and the drive actuator.
As the main body is moved in one direction, fluid is pumped out of one piston side that is being constricted, which is the outlet side, while fluid is drawn into the opposite suction side of the piston that is being expanded during piston movement, which is the inlet side. When the pneumatic actuator is reversed, pumping action within tube is also reversed, such that the inlet and outlet sides also reverse.
In another aspect of the invention, the pump outlet pressure is a direct result of the motivating input force supplied by the actuator in addition to any inlet pressure supplied to an inlet side of the piston. In the case of high inlet pressures, which can be encountered when pumping a liquefied gas supplied by a pressurized tank, the inlet pressure will assist the pump in reaching higher discharge pressures. Therefore, in the case of a pressurized inlet, a lower motivating force is necessary, which makes the pump more energy efficient.
As a result of the inventive pump design, the alternating operation of the piston generates a continuous, uninterrupted flow of the LPG discharged from the opposite ends of the pump since the piston is always moving through one piston stroke or the other.
Other objects and purposes of the invention, and variations thereof, will be apparent upon reading the following specification and inspecting the accompanying drawings.
Certain terminology will be used in the following description for convenience and reference only, and will not be limiting. For example, the words “upwardly”, “downwardly”, “rightwardly” and “leftwardly” will refer to directions in the drawings to which reference is made. The words “inwardly” and “outwardly” will refer to directions toward and away from, respectively, the geometric center of the arrangement and designated parts thereof. Said terminology will include the words specifically mentioned, derivatives thereof, and words of similar import.
Referring to
As to the vehicle 11, this vehicle 11 is powered by a conventional diesel engine 12, which includes a diesel engine intake 14 that may be constructed in the form of a fuel header or manifold. This engine intake 14 is supplied through one or more fuel injectors 15 wherein a representative one of such injectors 15 is illustrated in
More particularly, a conventional vehicle may also include a supply tank 16, which is mounted to a vehicle body and is pressurized so as to store the LPG or other fuel additive therein. To deliver the injection fluid to the injectors 15 and to the engine intake 14, the inventive injection pump 17 preferably is a seal-less LPG piston pump that is pneumatically driven by a drive actuator 18 and provides a continuous supply of the injection fluid. Preferably, the drive actuator 18 is a double acting pneumatic cylinder that is connected to and operated by the air supply system 20 of the vehicle 11 as will be described in greater detail hereinafter.
While the air supply system 20 is the driving means of the pneumatic cylinder, it will be understood that the pump 17 could also be driven by other pressurized fluid sources such as an “under the hood” air compressor on the vehicle 11, a hydraulic fluid supply system driving a hydraulic actuator, or by mechanical means such as linear actuators or other mechanical actuators having a similar structure and function. The particular construction of the inventive pump 17 provides a low flow, high pressure pumping of the LPG or propane. Further, the pump 17 readily accommodates changes in environmental temperature, which can vary the pressure or psi of the propane depending upon whether environmental conditions are hot or cold.
Generally as to the inventive pump 17, the pump 17 is a dual-acting LPG injection pump, which is formed as a piston pump for pumping the fluid from the storage tank 16 to the engine intake 14. As will be described in more detail herein, the drive actuator 18 is operatively connected to the pump piston through a seal-less connection, which uses an indirect magnetic connection to translate pressure cylinder movement of the actuator 18 into piston movement within the pump 17. This provides significant advantages as will be understood from the following discussion.
Next as to the piping system connected between the supply tank 16, injection pump 17 and engine intake 14, these components are piped together in fluid communication with each other to define the supply lines for the delivery of LPG or any other process or injection fluid from the supply tank 16 to the engine intake 14. The pump 17 is particularly suitable for use with liquefied gases.
The piping system 21 also includes various system controls to control the delivery of the injection fluid. More particularly, the supply tank 16 is connected to the injection pump 17 by a first supply line 22 that is connected upstream of the injection pump 17 to an inlet 23 thereof and receives the LPG or other injection fluid therethrough.
Specifically, the supply line 22 supplies fluid to the pump 17 through inlet 23 wherein the pump 17 and actuator 18 are operatively controlled by a system controller 27, which may take the form of a PLC (Programmable Logic Controller) controlling the operation of the various mechanical components and the various system controls provided therein. The system controller 27 may take other forms, such as different types of electrical or mechanical system controllers, although most preferably, a computer-based controller is provided to generate the necessary electronic signals to drive the various controls, as will be described further herein.
When the pump 17 is in an open operative condition, the injection fluid is able to flow through the supply line 22 from the upstream supply tank 16 to the process fluid side of the downstream injection pump 17. The injection pump 17, during operation thereof, preferably draws the injection fluid through the supply line 22 and then pumps the fluid through a pump outlet 31 to another downstream supply line 32, which connects the injection pump 17 to the engine intake 14. The downstream supply line 32 exits the outlet 31 from the process fluid side of the injection pump 17 and extends to the injectors 15. The injectors 15 inject the LPG injection fluid into the engine intake 14 as diagrammatically indicated by reference arrow 32A. The injectors 15 serve to constrict the fluid flow therethrough so that the injector flow 32A essentially is pressurized and sprayed into the engine intake 14 in an appropriate condition for use by the diesel engine 12.
Preferably, the injection pump 17 pressurizes the injection fluid to generate a specific constant pressure, which pressure is used to supply the engine intake 14. To optimize operation of the diesel engine 12, the specific constant pressure should be maintained by operation of the system and excessive process fluid pressures are undesirable. In order to accommodate the possibility of excessive pressures within the supply line 32, the piping system 21 further includes a return line 33, which is fluidly connected to the supply line 32 upstream of the injectors 15. The return line 33 connects to a pressure regulator 34, which is normally closed, but opens if a pressure limit is reached and exceeded. The pressure regulator 34 therefore is connected to an upstream segment 33A of the return line 33, as well as a downstream segment 33B, which thereby defines the pressure bypass line 33. If the pressure regulator 34 encounters pressure in the upstream segment 33A which exceeds the pressure limit, the pressure bypass valve 34 then opens in response to the excessive pressure to allow the injection fluid to flow through the downstream segment 33B back to the supply tank 16. As the injection fluid flows through the bypass segment 33B, this reduces and stabilizes the line pressure to the desired specific constant pressure that is to be developed within the engine intake 14. If the excessive pressure condition continues, the pressure regulator 34 would maintain an open condition to allow excessive pressure to be relieved through the bypass line 33B. Should the pressure drop below the preset pressure limit of the pressure regulator 34, the regulator 34 is then able to close to allow pressure to build back up within the supply line 32 and be maintained at the specific constant pressure desired for the engine intake 14. The pressure bypass valve 34 may be mechanically adjusted to set the pressure limit, although it is also possible to control the pressure regulator 34 through electronic connections and settings controlled by the system controller 27.
In one potential scenario, the system may be turned off which might result in an increase in temperature within the line 32. This condition may cause expansion of the process fluid in line 32, which in turn causes the undesirable increase in line pressure, which pressure increase preferably is relieved by the pressure regulator 34. It will also be understood that in some situations it may be desirable to eliminate the pressure bypass line 33 and the associated pressure regulator 34.
Generally as to the injection pump 17, the pump operates to supply the injection fluid through the piping system 21. In order to operate the injection pump 17, the pump 17 is connected to and is operatively driven by an actuator 18 that is driven by the air supply system 20 of the vehicle 11. Typically, the air supply system 11 is already provided on the vehicle 11 such that installation of the injection pump 17 does not require substantial changes to the vehicle systems.
The air supply system 20 illustrated in
Still further, the valve 43 connects to a discharge line 50 which can vent to atmosphere. When the control valve 43 is in the first operative condition, as diagrammatically shown in
Operation of the valve 43 is effected by the system controller 27 through a control line 55, which serves as an output from the system controller 27 in order to selectively activate the solenoid 44. Accordingly, the system controller 27 is able to control switching of the valve 43 between the first and second operative positions and thereby control reciprocal operation of the actuator 18.
Turning next to
As seen in
The cylinder 52 includes a mounting bracket 58 which is configured to be fixed to the pump 17 by fasteners 59 (
As to the pump 17, the pump 17 includes a pair of end caps 65 and 66, which are axially spaced apart and joined in fixed relation to each other by four connector members 67, preferably formed as elongate bolts or cap screws. Two of the connector members 67 are best seen at two of the corners of the end caps 65 and 66. The other two connector members 67 are on the back side of the pump 17 in
Generally as to
The above-described support flange 62 is mounted on the one end cap 65 by bolts 78, which engage bolt holes 79 (as seen on end cap 66). The end cap 65 rigidly supports the piston rod end 60 by the support flange 62. The piston mounting bracket 58 in turn is affixed to the main pump body 76 by the bolts 59 so that reciprocating movement of the drive cylinder 52 along path 63 causes the main body 76 to reciprocate along path 77. This movement of the main body 76 causes dual action pumping as will be described below. Since the cylinder 52 moves axially past the end cap 66, only the one end cap 65 has the support flange 62 to provide clearance for cylinder 52.
As seen in
Referring to
As referenced above, the pump 17 essentially is a seal-less piston pump. Generally, the pump 17 includes a dual-acting piston 90, which is slidably received within the pump tube 75 and effects pumping of the injection fluid. The piston sub-divides the interior pump bore 91 of the pump tube 75 into first and second pump chambers 92 and 93.
To effect reciprocation of the piston 90, an indirect, magnetic connection is formed between the main body 76 located exteriorly of the pump tube 75 and the piston 90 located within the interior bore 91 of the pump tube 75. To form this magnetic connection, the main body 76 includes an outer magnet set 95 and the piston 90 includes an inner magnet set 96, which magnetically attract each other through the thin wall of the pump tube 75. The pump tube 75 is preferably formed of a non-magnetic, durable material such as stainless steel. As the main body 76 reciprocates the magnetic interaction and attractive force between the outer and inner magnet sets 95 and 96 drive the piston 90 in unison with the main body 75 to effect pumping of the injection fluid.
The outer magnet set 95 comprises an alternating stack of multiple annular magnets 97 and annular spacers 98, which are slid within the interior chamber 83. The end caps 84 are affixed to the outer housing 82 by fasteners to close off and seal the interior chamber 83 from outside contaminants and dust. If desired, an axial spring may be provided within the chamber 83 to bias the outer magnets 97 tightly together in assembly.
Since the connection between the main body 76 and the piston 90 is accomplished magnetically, there are no wall penetrations of the pump tube 75 needed for the connection with the actuator 18. Since there are no wall penetrations needed for the actuator 18 to drive the piston 90, there are no dynamic seals required between moving parts which thereby makes the pump 17 a seal-less pump. This eliminates the need for secondary seals which would otherwise be required if an actuator required a direct connection to a piston within a pump chamber. Such secondary seals can create problems if the secondary seal fails and flammable injector fluid is able to escape from a pump chamber.
Next, the piston 90 is discussed in greater detail relative to
When coupled with the outer magnet set 95, a large axial force is required to separate the inner magnet set 96 from the outer magnet set 95. This is the primary driving force needed to pump fluid at elevated pressure. However, the maximum differential pressure also can be limited by the magnet holding power of the magnet sets 95 and 96. When differential pressure on the pumping side in comparison to the drive side exceeds the holding power of magnets 97 and 100, the inner and outer magnet sets 95 and 96 can decouple without damaging the pump components. The outer magnet set 95 and main body 76 will continue to move past the piston 90 but can recouple with the piston 90 on the return stroke. As such, if the system returns to lower pressure, the magnet sets 95 and 96 can be recoupled and the pump 17 restarted. This is an inherent safety feature;
The magnets 100 and spacers 101 extend along a threaded stud 102, which includes piston end caps 103 fastened to the opposite ends thereof. The stud 102 axially joins the spacers 101, inner magnets 100 and end caps 103 together in a cohesive unit that moves together during pump operation.
The piston 90 axially separates the pump chambers 92 and 93 from each other. The end caps 103 include piston guide bushings 104, which are restrained axially by retainers 105 and locate the piston 90 within the inner bore 91 of the pump tube 75. Further, annular gaskets or seals 141 are provided in contact with the inner bore 91 so as to prevent axial leakage or migration of injector fluid between the pump chambers 92 and 93 that are alternatingly being filled and pumped out during reciprocation of the piston 90. Essentially, the seals 141 keep product on the high pressure side of the piston 90 from migrating to the low pressure side of piston 90.
Therefore, in operation, the piston 90 subdivides the inner bore 91 into pump chambers 92 and 93, wherein the chamber volumes increase and decrease as the piston 90 reciprocates.
Referring to
To control the time at which the valve 43 switches between the first and second operative conditions, proximity sensors 99 are able to detect the main body 76 as it approaches the sensor 99 through interaction with the inserts 103 or 104. In one example, each of the metallic insert or plugs 103 and 104 preferably is formed as a magnet and is detected as they approach one proximity sensor 99 or the other to trip the proximity switch therein. In this regard, the sensor 99 may be of the type, such as a Reed switch, that detects the presence of magnetic body when the main body 76 and sensor 99 are close together, for example, as seen in
While the proximity sensors are illustrated as a preferred embodiment for reversing the movement of the piston 90, other sensing or control means may be used to reciprocate these piston 90. In one example, the system controller 27 may simply control the solenoid 44 using a timing signal or circuit wherein the valve 43 may be switched between its operative conditions after preselected time periods which are calculated based upon the time that the piston 90 reciprocates through its pumping strokes. Preferably, the time period as selected serves to limit or prevent bottoming out of the piston 90 against one end cap 65/66 or the other. Other methods may be used to determine the time or location at which the piston stroke should be reversed. For example, it also may be desirable to monitor the discharge pressure in line 32, which would indicate when the piston 90 bottoms out wherein detection of a pressure drop in such line 32 would indicate that the piston 90 had reached the end of its pumping stroke.
As seen in
Keeping in mind the operation of the piston 90, the following disclosure relates to the inlet and outlet paths defined through the pump 17.
As noted above, the guide tubes 74 provide a first function of guiding and supporting the main body 76. However, as seen in
The pump tube 75 is similarly mounted within bores formed in the end caps 65 and 66 and are sealed therein by annular gaskets or seals 108. During assembly, the guide tubes 74 and pump tube 75 are restrained axially within such end cap bores by installation of the connector members 67 described above. The connectors 67 are formed as bolts which tightly draw the end caps 65 and 66, guide tubes 74 and pump tube 75 axially together to prevent any leakage from the hollow passages formed within the tubes 74 and 75. Notably, there is no relative motion between the tubes 74/75 and the end caps 65 and 66 during pump operation, such that the seals 106 and 108 are static seals that are much less prone to leakage in comparison to dynamic seals. As described above, this pump 17 is a seal-less pump in that it does not require any moving parts which project into the pump chamber and which require dynamic seals.
More particularly as to the flow passages, the tube passages 105 open into axial bores 109 that open through the sides of transverse passages 110, 111, 112, and 113. The transverse passages 110, 111, 112, and 113 are formed through the end caps 65 and 66 and open through respective ports 110A, 111A, 112A, and 113A. In addition, chamber ports 114 and 115 open respectively into pump chambers 92 and 93, as well as the passages 110/111 and passages 112/113. The chamber ports 114 and 115 are formed by boring into the end caps 65 and 66 respectively, which bores are then closed by plugs 116. All of these passages and ports are constructed so as to be in fluid communication with each other. However, flow control devices are inserted into the passages to selectively control flow therethrough during piston operation and provide for a continuous outflow of injector fluid from the pump 17 during reverse movement of the piston 90.
In more detail, the port 110A can be selected as the inlet port 23 and any one of the other ports such as port 113A can be selected as the outlet port 31. These functions could be changed if desired, since the overall fluid flow through the ports and passages depends upon the flow control devices.
Where the two ports are selected as the inlet and outlet (such as ports 110A and 113A), the other two ports would then be closed by threaded plugs 117. Before installing plugs 117, appropriate check valves are installed in each of the passages 110, 111, 112, and 113, which check valves would include two check valves 118 and 119 on the outlet side and two check valves 120 and 121 on the inlet side. The check valves open and close in dependence on the pump chambers 92 and 93, which generate high pressure during pumping that is greater than the inlet and outlet pressures.
The inlet check valves 120 and 121 open to permit one-way in-flow of the LPG process fluid into the piston chambers 92 and 93 during suction, but automatically close when pressurized to prevent discharge or out-flow of any process fluid from the piston chambers 92 and 93. Hence, when the piston moves to the right in
Hence, as the piston 90 reciprocates through its dual action pumping strokes, this will generate a continuous flow of fluid through the outlet port 113A by opening either of the outlet check valves 118 or 119 so that the process fluid can flow through the outlet passage 113A to the supply line 32 for subsequent injection into the engine intake 14 described above. During this time, one or the other inlet check valves 120 or 121 opens such that the other of the pumping chambers 92 and 93 is refilling to allow continuous refilling of the other of the pump chambers 92 and 93. In this manner, the reciprocating movement of the piston 90 effects simultaneous refilling and pumping through the respective inlet port 110A and outlet passage 113A. This therefore provides a continuous low flow, high pressure supply of fuel additive, which is supplied through the supply line 32 to the engine intake 14.
Since the end caps 65 and 66 are bored out to form these passages, this allows for a small pump package and simplified plumbing for customer interface.
It will be understood that the outlet pressure from outlet port 113A is a direct result of the motivating input force from the actuator 18 (which may be a pneumatic actuator, hydraulic actuator, mechanical actuator or the like) in addition to inlet pressure received through inlet port 110A. In the case of a high inlet pressure, which would occur with a liquefied gas supplied by the pressurized tank 16, the inlet pressure will assist the pump 17 in reaching higher discharge pressures since the inlet pressure helps motivate the piston 90. Therefore, in the case of a pressurized inlet, a lower motivating force by the actuator 18 is necessary, which makes the pump 17 more energy efficient. Additionally, it is preferred that the system controller 27 monitor the pressure on the outlet 113A, which allows the controller to control the air pressure being provided to the cylinder 52 and thereby modify the motivating force provided thereby to control the outlet pressure.
Referring back to
Based upon the foregoing, the present invention provides significant advantages. The pump 17 and actuator 18 are connected indirectly by a non-mechanical connection and most preferably, by a magnetic connection. This allows the pump 17 to be driven pneumatically, hydraulically, or mechanically, such as by a screw/gear drive provided in place of the air cylinder, and yet the a seal-less axial piston pump 17 has no dynamic seal between atmosphere and product. As such, this inventive design is safer than pumps using dynamic seals since there are no dynamic seals to wear out and fail causing leakage of potentially dangerous products.
If the internal seals 141 actually do fail, this will simply allow leakage or cross flow between the pump chambers 92 and 93 but there will be no leakage outside of the pump 17. The pump 17 may cease to operate effectively or will operate at a reduced capacity but the failure of seals 141 will not cause potentially hazardous leakage to atmosphere.
This design also allows for easy replacement of drive components since the dual acting axial actuators 18 are readily and commercially available.
In a further aspect of the invention, the guide tubes 74 are used as both a locating feature and for internal fluid movement. This makes the pump package smaller and allows for a simpler customer interface (one inlet, one outlet).
Further, the discharge or outlet pressure is a result of a combination of the inlet pressure and the motivating force of the actuator 18. Discharge pressure can be monitored and used to vary the air/hydraulic pressure driving actuator 18 to maintain constant system pressure. This could reduce energy needed to maintain constant system pressure in applications using a pressurized inlet.
The modular construction offers many options including:
Use of a wide range of materials necessary for pumping a wide range of fluids;
Low weight materials in areas not sensitive to wear;
Tube length of pump tube 75 could be changed to easily increase or decrease pump displacement;
Pump discharge pressure is controlled by the air pressure provided to the pneumatic actuator 18 (or hydraulic pressure to a hydraulic actuator). This is inherently safer than relief valves although a hydrostatic relief valve may still be required in closed systems to prevent system overpressure when heated.
The structure of the system wherein the mounting bolts 67 are outside of the guide tubes 74 and pump tube 75 provides rigidity and protects pressure containing elements from physical damage;
The structure also allows for simplified guarding against pinch points for operator/technician safety during maintenance since all sliding components are buried within the pump frame;
The maximum differential pressure can be limited by magnet holding power of the magnet sets 95 and 96. When differential pressure exceeds the holding power of magnets 97 and 100, the inner and outer magnet sets 95 and 96 can decouple. If the system returns to lower pressure, the magnet sets 95 and 96 can be recoupled and the pump 17 restarted. This is an inherent safety feature;
Relative slow moving fluid and the large surface area of guide tubes 74 could be used in conjunction with pump tube 75 to either heat or cool the fluid;
The pneumatic actuator size could be used to control maximum pressure generated by the piston 90. As an example, it will be noted that the injection pump 17 governs or dictates the outlet pressure in line 32 by the construction of the piston area and the piston stroke length.
Further, the above design provides an improved ability to refurbish the pump 17. In this regard, the end caps 65 and 66 can be readily removed to allow for replacement of the various tubes, seals, check valves and other components.
Next, the modular construction also allows for alternate configurations of pumps.
The pump 17 could also be constructed of multiple tubes, bodies, or pistons to allow for higher flow rate or plumbed in series for higher overall differential pressure capability. The pumping system of the present invention lends itself to be configured for high pressure, and very low flow applications.
For example, referring to
In this design, two pumps 17 are provided in series. These pumps 17 are constructed virtually the same as the pump 17 illustrated in
In the right pump, the ports 111A and 112A are blocked by plugs 117, while port 113A serves as the system outlet. In the left pump 17, the inlet check valves 118 and 119 close when their respective pump chambers 92 and 93 are pressurized and the other outlet check valves 120 and 121 would then open to allow fluid flow from port 112A of the left pump 17 to port 110A of the right pump 17. In the right pump 17, the inlet valves 120 and 121 would then supply the pump chambers 92 and 93 but close when their respective chambers 92 and 93 are pressurized. The outlet check valves 118 and 119 in the right pump 17 then open to allow discharge of fluid from outlet port 113A. This modified design allows the pumps 17 to be connected in series and thereby increase the total pressure of the fluid discharged from outlet port 113A.
In other alternate designs, the actuator 18 could be a screw drive instead of pneumatics/hydraulics for precise position control, rate of flow, and discharge pressure.
While the pump 17 preferably is dual acting, it will be understood these components could be modified to form a single acting pump. In this regard, the piston 90 could act in one direction by replacing the check valves in the end caps 65 and 66 with a single check valve within the inner piston 90. This would reduce number of check valves but would eliminate the benefit of lower pulsations due to the dual pumping action and would effectively lower the overall flow rate.
Although particular preferred embodiments of the invention have been disclosed in detail for illustrative purposes, it will be recognized that variations or modifications of the disclosed apparatus, including the rearrangement of parts, lie within the scope of the present invention.
This application asserts priority from provisional application 61/791,881, filed on Mar. 15, 2013, which is incorporated herein by reference.
Number | Date | Country | |
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61791881 | Mar 2013 | US |