Centrifugal pump apparatus and method for using a single impeller with multiple passes

Information

  • Patent Grant
  • 6447244
  • Patent Number
    6,447,244
  • Date Filed
    Wednesday, May 10, 2000
    24 years ago
  • Date Issued
    Tuesday, September 10, 2002
    22 years ago
Abstract
A method of increasing the pressure of a fluid in an aircraft centrifugal pump by forcing the fluid to make multiple passes through one impeller of the aircraft centrifugal pump is provided. It includes providing fluid through a pump inlet to an aircraft impeller inlet. The fluid then exits the impeller through a first set of discharge ports and the exiting fluid is directed to a second inlet on the same impeller. The fluid then exits the impeller through a second set of discharge ports to a pump outlet. Each pass through the impeller by the fluid increases the pressure thereof.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to centrifugal pumps, and more particularly, to an improved impeller for use in a centrifugal pump. The present invention finds particular application in conjunction with an aircraft fuel pump, and it will be described with particular reference thereto. However, it is to be appreciated that the present invention is also amenable to other like applications.




2. Discussion of the Art




The structure and operation of centrifugal pumps is well known in the art. Briefly, fluid generally enters a pump inlet in an axial direction and due to the rotation of the impeller the fluid centrifugally flows radially outward through a set of channels defined between impeller blades. The fluid discharges from the impeller around the peripheral edge of the impeller. The centrifugal action of the fluid flowing outwardly through the channels creates a suction at the central area of the impeller which serves to continuously draw more fluid into the inlet of the pump.




The fluid discharged from the impeller is at a significantly higher pressure than the fluid entering the pump inlet. The major portion of the energy imparted to the fluid is converted to a pressure head by means of a volute, diffuse, or other system.




Impellers may generally be classified according to their flow arrangements. Single-suction impellers receive fluid through a single inlet on one face of the impeller. Double-suction impellers generally have fluid flowing onto opposed faces of the impeller. The fluid streams flowing into each face of a double-suction impeller are usually commingled within impeller fluid channels or at the periphery of the impeller before exiting the pump.




Centrifugal pumps may additionally be classified as either single-stage pumps or multi-stage pumps. Single-stage pumps are generally defined as those in which the pressure head was developed by a single pass through only a single impeller. Multi-stage pumps generally refer to pumps using two or more impellers operating in series. Additionally, a single impeller, double suction pump has been, heretofore, generally classified as a single-stage pump.




Multi-stage pumps are often used in applications that require large volumes of liquid to be delivered at high pressures. Each stage incrementally imparts rotational energy into the fluid thereby increasing the amount of pressure of the fluid at each stage. Although the delivery of a high volume of fluid at high pressures is desirable, several disadvantages are present in the prior art.




One disadvantage of multi-stage pumps is that substantial internal energy losses result from using additional impellers because each impeller frictionally interfaces with the surrounding pump casing or housing. The mechanical drag results in lower pump efficiency.




Another disadvantage is that each additional impeller stage adds volume and weight to the overall pump assembly. Increased volume or size may prevent installation of the pump unit in tight-fitting applications. Increased weight may cause inefficiencies in particular applications such as for use as an aircraft fuel pump where the load capacity of the aircraft is limited.




Therefore, it is desirable to provide an improved impeller for use in a centrifugal multi-stage pump that overcomes these problems and others.




BRIEF SUMMARY OF THE INVENTION




In accordance with the present invention, an improved impeller for use in a single-impeller, multi-stage centrifugal pump is provided for minimizing these and other disadvantages of the prior art.




More particularly, a preferred embodiment of the present invention has an impeller provided with multiple inlets and corresponding sets of discharge ports. Multiple pump stages are accomplished by successively passing the fluid through the impeller by entry into the various inlets of the impeller.




A preferred embodiment of the centrifugal pump includes a housing having a pump inlet and a pump outlet that communicate with an internal chamber. A rotatable shaft drives a generally cylindrical impeller operatively received in the internal chamber. The impeller includes a first impeller face, a second impeller face opposite from the first impeller face, and a radial peripheral edge extending around the circumference of the impeller and interconnecting the first and second impeller faces. The impeller also includes a first impeller inlet located on one of the first and second impeller faces and a second impeller inlet located on one of the first and second impeller faces. Additionally, a first and second set of impeller outlet ports are located on the impeller. The first set of channels communicate between the first impeller inlet and the first set of impeller outlet ports disposed in the impeller while the second set of channels communicate between the second impeller inlet and the second set of impeller outlet ports disposed in the impeller.




According to a preferred method of the present invention increased pressure of a fluid in a centrifugal pump having a single impeller is provided. The method includes the steps of providing fluid through a pump inlet to a first impeller inlet. Fluid exiting the impeller through a first set of discharge ports is directed to a second inlet for a second pass through the same impeller. The fluid then exits the impeller through a second set of discharge ports at an increased pressure. Finally, the fluid is directed to a pump outlet. Of course, additional passes through the same impeller are possible.




A primary advantage of the present invention is reduced overall efficiency losses due to mechanical drag from using the subject single-impeller, multi-stage pump of the present invention.




A further advantage is realized by the multi-pass single impeller obtaining high discharge pressures without requiring a large impeller diameter.




Another advantage of the present invention over the prior art is that the overall pump weight is reduced.




Still another advantage is that the overall size of the pump is reduced.




Still other features and benefits of the invention will be apparent to those skilled in the art upon reading and understanding the following detailed description.











BRIEF DESCRIPTION OF THE DRAWINGS




The structure, operation and advantages of the presently preferred embodiment of this invention will become further apparent upon consideration of the following description, taken in conjunction with the accompanying drawings. Of course, the drawings are only for purposes of illustrating preferred embodiments and are not to be construed as limiting the invention.





FIG. 1

illustrates a partial cross-sectional view of the impeller in one embodiment of the present invention.





FIG. 2

illustrates a partial cross-sectional view of the impeller in a second embodiment of the present invention.





FIG. 3

illustrates an exploded perspective view of the impeller in a third embodiment of the present invention.











DETAILED DESCRIPTION OF THE INVENTION




Referring now to the drawings wherein like reference characters represent like elements. The impeller of the present invention may have any number of inlets on one or both of its faces. Each inlet represents the beginning of a separate pump stage. Thus, in a first pump stage the fluid enters a specific or first impeller inlet and is discharged from a first set of discharge ports in operative communication with the first inlet. The fluid is then routed to a second or successive impeller inlet to begin the second pump stage. Each stage, or pass through the impeller, incrementally increases the pressure of the fluid. The number of stages or passes that may be accomplished through a single impeller is theoretically unlimited, but in accordance with the present invention two or three passes are preferred.




Multiple passes through the improved single impeller of this invention provide high discharge pressures to be attained without many of the disadvantages of the prior art. As will be evident to those skilled in the art, a single impeller capable of multiple passes can be accomplished in a variety of manners.




With reference to

FIG. 1

, a centrifugal pump indicated generally by reference numeral


10


illustrates one embodiment of the present invention. The rotational components of the pump


10


includes an impeller


12


and a shaft


14


. The impeller


10


is connected to the shaft


14


by any known means. The shaft interconnects a drive output from a motor (not shown) to rotatably drive the impeller


12


. A housing or casing


16


includes an internal chamber


18


for operatively receiving the impeller


12


and the shaft


14


. The housing


16


also includes a pump inlet


20


and a pump outlet (not shown).




The pump inlet


20


is an axial inlet disposed adjacent a rotational axis of the impeller. The inlet


20


is in fluid communication with a first impeller inlet


22


located on a first face


24


of the impeller


12


. The first impeller inlet


22


is annularly disposed between a distal end


14


a of the shaft


14


and an interior wall


26


of the impeller


12


. The first impeller inlet leads to a first set of fluid channels


28


that extend through the impeller and connect the first impeller inlet to a first set of discharge ports


30


. The fluid channels may be of any variety as is well known in the art.




The first set of discharge ports


30


are located on a peripheral edge


32


of the impeller. Specifically, the first set of discharge ports


30


are axially spaced from a central axis


34


that extends perpendicular to the rotational axis of the impeller and generally parallel to the first face


24


of the impeller


12


. A first discharge chamber


36


is provided in the housing


16


. The first discharge chamber


36


receives the fluid from the first set of discharge ports


30


as it exits from the impeller.




The first discharge chamber


36


is connected to a second inlet chamber


38


by any known fluid communication means (not shown). For example, passages in the housing direct the fluid from the first discharge chamber to the second inlet chamber (shown in

FIG. 1

as being located on an axially opposite end of the impeller from the first inlet chamber). The second inlet chamber


38


redirects fluid to a second impeller inlet


40


such that the fluid may enter the impeller


12


in a generally axial direction. The second impeller inlet


40


, located on a second face


42


of the impeller


12


, is annularly disposed between the shaft and the interior wall


44


of the impeller. The second impeller inlet


40


leads to a second set of fluid channels


46


. The fluid channels


46


proceed through the impeller and connect the second impeller inlet


40


to a second set of discharge ports


48


. Again, the fluid channels may be of any variety as is well known(i.e., radial, axial, circumferential, or a combination of these).




The second set of discharge ports


48


are located on the peripheral edge


32


of the impeller. Specifically, the second set of discharge ports


48


are axially offset from the central axis


34


in the direction of the second face


42


of the impeller. A second discharge chamber


50


is provided in the housing and is in fluid communication with the second set of discharge ports


48


to receive fluid as it exits the impeller from the second set of channels


46


.




Third and fourth inlet chambers


52


,


54


are provided in the impeller to provide an actuator stage. The inlets are disposed on opposite ends or faces of the impeller and communicate with axially extending impeller inlets


56


,


64


, respectively. The impeller inlets


56


,


64


are located radially outward relative to the first impeller inlet


22


and communicate with a third set of fluid channels


58


. The fluid channels


58


extend radially through the impeller connecting the third impeller inlet to a third set of discharge ports


60


. As with the first and second set of discharge ports, the third set of discharge ports


60


are located on the peripheral edge


32


of the impeller and are axially offset on opposite sides of the central axis


34


in the direction of the first face and second faces of the impeller. Third discharge chambers


62


,


70


are provided in the housing


16


and fluidly connect to the third set of discharge ports for receiving fluid as it exits the impeller from the third set of channels


58


.




The third and fourth discharge chambers


62


and


70


are connected to an actuator outlet (not shown). At a point before the actuator outlet, the fluid from the third and fourth discharge chambers


62


and


70


reconvenes and exits the pump


10


as a single fluid stream.




In operation, fluid enters the pump


10


through the pump inlet


20


and is axially directed into the first impeller inlet


22


. The motor (not shown) rotates the impeller


12


via the shaft


14


. The rotation of the impeller causes the fluid entering the first impeller inlet


22


to be centrifugally forced radially outwardly through the first set of fluid channels


28


. The fluid then exits the impeller


12


through the first set of discharge ports


30


and is received in the first discharge chamber


36


. As a result of the centrifugal forces, the fluid received in the first discharge chamber


36


is at a higher pressure than when the fluid first entered the impeller.




The fluid is then directed to the second inlet chamber


38


where the fluid is axially directed for reentry into the impeller. Fluid enters the second impeller inlet


40


and is again forced radially outwardly through a second set of fluid channels


46


due to the rotation of the impeller


12


. The fluid exits the impeller


12


through the second set of discharge ports


68


and is received in a second discharge chamber


50


. The fluid received in the second discharge chamber


50


is at an even higher pressure than when the fluid entered the impeller for the second time.




Although the third and fourth inlets, fluid channels, and discharge ports are intended for use as an actuator in

FIG. 1

, this embodiment illustrates how additional passages can be formed in the impeller without adversely affecting the function of the impeller. It will be understood by one skilled in the art that these additional passages could also be converted to third and fourth stages if appropriate.




With reference to

FIG. 2

, a second embodiment of the present invention is shown. Where possible, components in the

FIG. 2

embodiments are identified by a “100” series to correspond with like components having the same last two digits in the embodiment of

FIG. 1

(e.g., impeller


12


from

FIG. 1

generally corresponds to impeller


112


in FIG.


2


). A centrifugal pump


110


has an impeller


112


and a shaft


114


. The pump


110


includes a housing or casing


116


which includes an internal chamber


118


for operatively receiving the impeller


112


and the shaft


114


. Additionally, the casing


116


includes a pump inlet


120


and a pump outlet (not shown).




The pump inlet


120


is in fluid communication with a first impeller inlet


122


located on a first face


124


of the impeller


112


. The first impeller inlet


122


is annularly disposed on the first face


124


. The first impeller inlet


122


is in fluid communication with a first set of channels


128


that axially and radially extend and thereby connect the first impeller inlet to a first set of discharge ports


130


. The first set of discharge ports


130


are preferably located on a chamfered peripheral edge


131


which is located between an outer diameter


132


of the impeller and a second face


142


of the impeller.




A fluid communication means or passage


137


receives fluid from the first set of discharge ports


130


and redirects the fluid into a second impeller inlet


140


. The second impeller inlet


140


is annularly disposed on the second face


142


of the impeller and is in fluid communication with a second set of channels


146


. The fluid channels run through the impeller connecting the second impeller inlet


140


to a second set of discharge ports


140


. The first and second set of fluid channels


128


and


146


cross-over one another but are not in fluid communication with one another. In this manner, each pass through the impeller increases the pressure and a multi-stage pump is achieved with a single impeller. The second set of discharge ports


140


are located on the radial peripheral edge


132


and in fluid communication with the pump outlet such that fluid may be discharged from the pump upon completion of two passes through the impeller.




In operation, fluid enters the pump


110


through the pump inlet


120


and is axially directed into the first impeller inlet


122


. The impeller


112


rotates via the shaft


114


causing the fluid entering the first impeller inlet to be centrifugally forced radially outwardly through the first set of fluid channels


128


and exit the impeller


112


through the first set of discharge ports


130


. The exiting fluid is at a higher pressure than the fluid first entering the impeller.




The fluid is then directed through the fluid passage


137


to the second impeller inlet


140


where the fluid again enters the impeller. The rotation of the impeller imparts further energy to the fluid and forces the fluid radially outwardly. The fluid flows through the second set of fluid channels


146


and exits the impeller through the second set of discharge ports


168


. The fluid exiting the impeller for a second time is at an even higher pressure than the fluid exiting the impeller after the first pass. The fluid is then directed to the pump outlet after two passes through the impeller in which each pass incrementally increases the pressure of the fluid.




A third embodiment of the present invention is shown in FIG.


3


. An impeller


200


of the centrifugal pump is shown in a disassembled state and includes a first and second member


202


and


204


. Each member


202


and


204


includes a substantially planar face


202




a


and


204




a


disposed in facing relation and that allow members


202


and


204


to be abutted together.




The first member includes a hub


206


having a circular opening


208


that receives a drive shaft for rotational engagement. A first impeller inlet


210


is annularly disposed around the hub and is in fluid communication with a first set of flow channels


212


. The second member


204


defines the remainder of the first set of flow channels


212


. The first set of flow channels


212


connects the first impeller inlet


210


to a first set of discharge ports located on the first chamfered edge of the second member


204


. The second member


204


is substantially a mirror image of the first member. That is, a second impeller inlet (not shown) is annularly disposed around a second hub portion (not shown) in the same manner as the hub portion


206


of the first member


202


. A second set of flow channels


216


is partially defined by the second member


204


. The first member


202


defines the remainder of the second set of flow channels


216


. The second set of flow channels


216


connects the second impeller inlet to a second set of discharge ports


218


located on the second chamfered edge.




The first and second members


202


and


204


are joined together in any conventional manner. For example, the members


202


and


204


are brazed together once the fluid flow channels


212


and


216


are aligned. The respective sets of channels


212


and


216


cross over one another but are not in fluid communication with one another for reasons described above. The resultant impeller


200


has the capability of a two-stage pump achieved with only a single impeller.



Claims
  • 1. A method of increasing the pressure of a fluid in a centrifugal pump by forcing the fluid to make multiple passes through one impeller of the centrifugal pump, the method comprising the steps:providing fluid to a first inlet of a centrifugal pump impeller; rotating the impeller to increase the pressure of the fluid and cause the fluid to exit from the impeller; directing exiting fluid to a second inlet of the same impeller to make a second pass through the impeller and further increase the fluid pressure and cause the fluid to again exit from the impeller, wherein the first and second inlets are generally parallel to the axis of rotation of the impeller and radially aligned with one another.
  • 2. The method according to claim 1 further comprising the step of:directing fluid to a third inlet of the same impeller.
  • 3. The method according to claim 2 wherein the step of directing fluid to the third inlet includes directing the fluid again exiting the impeller after the second pass therethrough to the third inlet of the impeller.
  • 4. The method according to claim 3, further comprising the step of:directing fluid to a fourth inlet of the same impeller.
  • 5. The method according to claim 1 wherein the step of rotating the impeller to increase the pressure of the fluid from the first inlet includes the sub-step of:directing the fluid from the first inlet located on a first face of the impeller to a first set of outlet ports located on a second face of the impeller axially spaced relative to the first face of the impeller.
  • 6. The method according to claim 1 wherein the step of directing exiting fluid to a second inlet of the same impeller to make a second pass through the impeller includes the sub-step of:directing the fluid making the second pass through the impeller to cross over the fluid making the first pass through the impeller.
  • 7. A centrifugal pump comprising:a housing having an internal chamber, a pump inlet, and a pump outlet; an impeller operatively received in the internal chamber having first and second impeller faces, the impeller includes a first impeller inlet located on the first impeller face, a first set of impeller outlet ports located on the second impeller face, and a first set of channels for fluid communication between the first impeller inlet on the first impeller face and the first set of impeller outlet ports disposed in the impeller on the second impeller face.
  • 8. The centrifugal pump of claim 7 wherein the impeller includes a second impeller inlet located on one of the first and second impeller faces, a second set of impeller outlet ports, and a second set of channels for fluid communication between the second impeller inlet and the second set of impeller outlet ports.
  • 9. The centrifugal pump of claim 8 wherein the first set of impeller outlet ports is in fluid communication with the second impeller inlet.
  • 10. The centrifugal pump of claim 8 where in the second impeller inlet is located on the second impeller face and the second set of impeller outlet ports is located on the first impeller face.
  • 11. The centrifugal pump of claim 8 wherein one of the first and second sets of channels axially crosses over the other of the first and second sets of channels.
  • 12. The centrifugal pump of claim 8 wherein the second impeller face is axially spaced in relation to the first impeller face.
  • 13. The centrifugal pump of claim 7 wherein the second impeller face includes a chamfered peripheral edge located at an angle between a general axial plane of the second impeller face and a general radial plane of an outer diameter of the impeller.
  • 14. The centrifugal pump of claim 13 wherein the impeller includes a second impeller inlet located on the second impeller face in fluid communication with the first set of discharge ports.
  • 15. A centrifugal pump comprising:a housing having an internal chamber, a pump inlet, and a pump outlet; an impeller operatively received in the internal chamber having first and second impeller faces, the impeller includes a first impeller inlet located on one of the first and second impeller faces, a second impeller inlet located on one of the first and second impeller faces, a first set of impeller outlet ports located on the impeller, a second set of impeller outlet ports located on the impeller, a first set of channels for fluid communication between the first impeller inlet and the first set of impeller outlet ports, and a second set of channels for fluid communication between the second impeller inlet and the second set of impeller outlet ports; wherein the first set of impeller outlet ports is in fluid communication with the second impeller inlet; wherein the impeller includes a third impeller inlet located on one face of the impeller in fluid communication with the second set of outlet ports, a third set of outlet ports located on the impeller, and a third set of fluid channels fluidly connecting the third impeller inlet with the third set of fluid outlet ports; and wherein the impeller includes a fourth impeller inlet located on one face of the impeller, a fourth set of outlet ports located on the impeller, and a fourth set of fluid channels fluidly connecting the fourth impeller inlet with the fourth set of fluid outlet ports.
  • 16. The centrifugal pump of claim 15 wherein the fourth impeller inlet is in fluid communication with the second set of discharge ports allowing the fluid to divide between the third and fourth impeller inlets.
  • 17. An impeller for use in a centrifugal pump of an aircraft fuel system, comprising:a first impeller half member having a first half first face that defines a first face portion of a central shaft opening, a first half inlet annularly disposed around and adjacent to the first face portion, and a plurality of first half discharge ports annularly disposed around the first half inlet near a peripheral radial edge of the first half member; a second impeller half member having a second half first face that defines a second face portion of the central shaft opening, a second half inlet annularly disposed around and adjacent to the second face portion, and a plurality of second half discharge ports annularly disposed around the second half inlet near a peripheral radial edge of the second half member; and first and second sets of fluid passages together defined by the first and second impeller half members, the first set of fluid passages fluidly connecting the first inlet of the first half member and the plurality of second half discharge ports of the second half member and the second set of fluid passages fluidly connecting the second inlet of the second half member and the plurality of first half discharge ports of the first half member.
  • 18. The impeller according to claim 17 wherein:the first set of fluid passages a redefined by a first set of channels defined within a second face of the first half member connecting the first inlet to the second face of the first half member and a second set of channels defined within a second face of the second half member connecting the second half discharge ports to the second face of the second half member; and the second set of fluid passages are defined by a third set of channels defined within the second face of the second half member connecting the second inlet to the second face of the second half member and a fourth set of channels defined within the second face of the first half member connecting the first half discharge ports to the first face of the first half member.
  • 19. The impeller according to claim 17 wherein the first and second impeller half member s are brazed together.
  • 20. The impeller according to claim 17 wherein the first set of fluid passages axially crosses over the second set of fluid passages without fluidly communicating directly with one another.
Parent Case Info

This application claims the benefit of U.S. Provisional Application Serial No. 60/134,271, filed on May 14, 1999.

US Referenced Citations (7)
Number Name Date Kind
1309282 Frame Jul 1919 A
1743348 Hollander Jan 1930 A
2944785 Sampietro Jul 1960 A
4408952 Schweinfurter Oct 1983 A
4664592 Grzina May 1987 A
4720242 Lovisetto Jan 1988 A
5082425 Reil et al. Jan 1992 A
Provisional Applications (1)
Number Date Country
60/134271 May 1999 US