US3516758A - Liquid displacement pumps - Google Patents

Liquid displacement pumps Download PDF

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Publication number
US3516758A
US3516758A US734441A US3516758DA US3516758A US 3516758 A US3516758 A US 3516758A US 734441 A US734441 A US 734441A US 3516758D A US3516758D A US 3516758DA US 3516758 A US3516758 A US 3516758A
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Prior art keywords
recess
cavity
rotor
inlet
outlet
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Expired - Lifetime
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US734441A
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Robert Thomas John Skinner
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ZF International UK Ltd
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Lucas Industries Ltd
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D15/00Control, e.g. regulation, of pumps, pumping installations or systems
    • F04D15/0027Varying behaviour or the very pump
    • F04D15/005Varying behaviour or the very pump the pumps being of the circumferential flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D15/00Control, e.g. regulation, of pumps, pumping installations or systems
    • F04D15/0005Control, e.g. regulation, of pumps, pumping installations or systems by using valves
    • F04D15/0022Control, e.g. regulation, of pumps, pumping installations or systems by using valves throttling valves or valves varying the pump inlet opening or the outlet opening

Definitions

  • a liquid displacement pump in which a body is provided with an interior cavity, a bladed rotor cavity, an inlet and an outlet disposed at respective angularly spaced positions in the cavity, and the side wall of the cavity defines a part annular recess adjacent to the rotor edge, and extending between the inlet and the outlet.
  • Control means is actuable to vary the effective combined volume of the cavity and the recess which is available for the flow of liquid between the inlet and the outlet.
  • a liquid displacement pump of the type having a body, a bladed rotor mounted within a cavity in the body, an inlet and and outlet in the body communicating with the cavity and a part annular recess in the side wall of the cavity in the body adjacent to the rotor periphery, with the recess extending around the rotor intermediate the position of the inlet and that of the outlet.
  • the present application relates to a liquid displacement pump of this type generally as disclosed in my earlier application and in addition discloses parts and features of the pump not referred to in the original application.
  • the object of the invention is to provide a pump of the kind specified, in a convenient form.
  • a liquid displacement pump of the type specified is characterized by the provision of control means whereby the effective combined volume of the cavity and recess in the body which is available for the flow of liquid between the inlet and the outlet, can be varied.
  • FIG. 1 is a cross-sectional view of a pump incorporating the present invention
  • FIG. 2 is an end elevation view
  • FIG. 3 is a fragmentary cross-sectional view on the line III--III in FIG. 2.
  • the pump is suitable for supplying liquid fuel to a gas turbine engine.
  • the pump has a multi-part body which defines a generally cylindrical internal cavity 11 within which is mounted a bladed rotor 12 connected to a shaft 13 which can be driven by the engine to which the pump is intended to supply fuel.
  • the rotor blades in this example, extend radially and are flat on both faces except at the outer end of the leading face of each blade.
  • the blade is formed with a concave recess indicated at 12a of part cylindrical cross-section, to form a scoop at the outer end of the blade.
  • the axial depth of the rotor is equal tothe width of the recess so that, except for the center, the whole of the cavity is swept by the rotor blades.
  • In the cylindrical wall of the cavity are a pair of diametrically opposite tangential outlets 14a communicating with respective outlet passages 14- as illustrated in FIG. 2.
  • One sidewall of the cavity 11 is defined by an inlet plate 15 having a pair of diametrically opposite inlet openings 15a which communicate with a central inlet port 16 formed in the body 10. These inlet openings 15a in the plate 15 are disposed near the inner edges of the rotor blades and are angularly spaced from the outlets 14:: respectively.
  • the opposite sidewall of the cavity 11 has an annular recess 17 of rectangular channel shape in cross-section.
  • the outer peripheral edge of this coincides with the cylindrical wall of the cavity 11 and the radial width of the recess is approximately a quarter of the radius of the rotor 12.
  • the recess 17 is divided by a pair of fixed abutments 23 secured in the body to form a pair of semicircular recess portions. Radially aligned with one end of the recesses is one of the inlet openings 15a and radially aligned with the other end of each is one of the outlets 14a.
  • the base wall of the recess 17 is constituted by the crown of an annular piston 18 mounted in the body 10, with this piston being movable in a direction parallel to the axis of the rotor toward and away from the rotor under control of springs 24 acting beneath the abutments 23.
  • At the opposite end of the piston 18 is defined a space to which fluid under pressure can be admitted to control the position of the piston 18 against the action of its springs 24.
  • the volume of the recess 17 available for liquid flow can be increased or decreased and it is known that the smaller the recess, the less will be the increase in pressure generated by the toroidal flow.
  • the recess 17 is completely filled by the piston 18, there will be no tendency for toroidal flow to be generated and the pump will operate in the manner of a normal centrifugal pump.
  • the pump thus far described can be used as such, but alternatively or additionally to the arrangements for controlling the pressure in the outlet, the position of the inlet plate 15 may be varied.
  • the inlet plate 15 has a flange and is urged toward the rotor 12 by a spring 19.
  • the outer periphery of the inlet plate 15 is stepped and engages in a stepped bore in the body 10.
  • annular space 25 Between the respective shoulders of the body and inlet plate is defined an annular space 25, with which communicates a fluid pressure inlet passage 26, shown in FIG. 3.
  • admission of fluid under pressure to the space causes the inlet plate 15 to be moved against the action of the spring 19. This moves the inlet openings 15a away from the rotor so that the volume of the cavity available for flow is increased.
  • the flow of fluid liquid will now take place, not from two specific points around the rotor, but towards the outlets 14a before entering the spaces between the blades.
  • the pump will operate more like a conventional centrifugal pump, having no recess 17, than when the inlet plate 15 is adjacent to the rotor side face.
  • the pressure rise across the pump will under these circumstances, be less than when the inlet plate 15 is closely adjacent to the rotor.
  • the flange of the plate 15 has a plurality of elongated slots 20 engaged by a pair of screws 21, 22.
  • the inlet plate 15 is angularly adjustable to move the inlet openings 15a towards and away from the outlets 14a respectively, thus varying the effective lengths of the recesses which are available for flow between the inlet openings and the outlets respectively. Releasing of the screws 21, 22 engaging in the slots 20 in the inlet plate enables the angular adjustment of the inlet plate 15 to be effected.
  • the body 10 will be provided with a fixed recess 17.
  • outlets are formed in a ring defining the outer peripheral wall of the cavity.
  • This ring is angularly movable to vary the distance between the inlet openings and outlets. Adjustments may be achieved in the manner adopted for angular adjustment of the inlet plate 15 in the form illustrated.
  • a liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor rotatably mounted in the cavity in the body, said body having an inlet and an outlet disposed at respective positions, spaced angularly about the rotor rotational axis, the outlet being disposed in the cylindrical wall of the cavity, a part annular recess being provided in one side wall of the cavity, the recess having an outer peripheral edge adjacent to the cylindrical wall of the cavity, said recess extending around the rotor intermediate the position of the inlet and that of the outlet, and control means actuable to vary the effective combined volume of the cavity and the recess which is available for flow of liquid between the inlet and the outlet.
  • a liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor rotatably mounted in the cavity in the body, an inlet and an outlet in the body disposed at respective positions, spaced angularly about the rotor rotational axis, the outlet being disposed in the cylindrical wall of the cavity, a part annular recess in one side wall of the cavity, the recess having an outer peripheral edge adjacent to the cylindrical wall of the cavity, said recess extending around the rotor intermediate the position of the inlet and that of the outlet, and control means comprising a piston forming the base of the recess in the body, and means for moving said piston in a direction parallel to the rotor rotational axis to vary the volume of said recess which is available for flow of liquid between the inlet and the outlet.
  • liquid displacement pump as claimed in claim 2 in which there are two inlets and two outlets in the body and the recess is divided into two portions extending between the respective inlets and outlets.
  • a liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor mounted for rotation in the cavity, said body having an inlet and an outlet disposed'at respective positions spaced angularly about the rotational axis of the rotor, said outlet being disposed in the cylindrical wall of the cavity, one side wall of the cavity having an annular recess of rectangular channel shape in cross section, the outer peripheral edge of the recess coinciding with the cylindrical wall of the cavity, a pair of fixed abutments secured in the body and dividing the recess into a pair of semi-circular portions, the inlet being radially aligned with one end of the recess and the outlet with the other end, and control means for varying the volume of the recess which is available for liquid flow between the inlet and the outlet, said control means including an annular piston having a crown mounted in the body, with the crown defining the base wall of the recess, spring means beneath the abutments for moving the piston in a direction parallel to the axi

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

June 23, 1970 1 R. 11.1. SKINNER 3,516,758
LIQUID DISPLACEMENT PUMPS' Filed June 4. 1968 v 2 Sheets-Sheet 1 BY, W ATTORNEYS June 23, 1970 R. T. J. SKINNER LIQUID DISPLACEMENT PUMPS 2 Sheets-Sheet Filed June 4, 1968 vgwrorz BY ATTORNEYS United States Patent 3,516,758 LIQUID DISPLACEMENT PUMPS Robert Thomas John Skinner, Kenilworth, England, assignor to Joseph Lucas (Industries) Limited, Birmingham, England Continuation-impart of application Ser. No. 557,043, June 13, 1966. This application June 4, 1968, Ser. No. 734,441 The portion of the term of the patent subsequent to Dec. 24, 1985, has been disclaimed Int. Cl. F04d 15/00, 27/100 U.S. Cl. 415-126 4 Claims ABSTRACT OF THE DISCLOSURE A liquid displacement pump in which a body is provided with an interior cavity, a bladed rotor cavity, an inlet and an outlet disposed at respective angularly spaced positions in the cavity, and the side wall of the cavity defines a part annular recess adjacent to the rotor edge, and extending between the inlet and the outlet. Control means is actuable to vary the effective combined volume of the cavity and the recess which is available for the flow of liquid between the inlet and the outlet.
BACKGROUND OF THE INVENTION This application is a continuation-in-part of my application No. 557,043, filed June 13, 1966, now abandoned, and entitled: Liquid Displacement Pumps.
In my earlier application I have disclosed a liquid displacement pump of the type having a body, a bladed rotor mounted within a cavity in the body, an inlet and and outlet in the body communicating with the cavity and a part annular recess in the side wall of the cavity in the body adjacent to the rotor periphery, with the recess extending around the rotor intermediate the position of the inlet and that of the outlet.
The present application relates to a liquid displacement pump of this type generally as disclosed in my earlier application and in addition discloses parts and features of the pump not referred to in the original application.
The object of the invention is to provide a pump of the kind specified, in a convenient form.
SUMMARY OF THE INVENTION In accordance with the present invention, a liquid displacement pump of the type specified is characterized by the provision of control means whereby the effective combined volume of the cavity and recess in the body which is available for the flow of liquid between the inlet and the outlet, can be varied.
The invention will now be described by way of example with reference to the accompanying drawings in which:
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a cross-sectional view of a pump incorporating the present invention,
FIG. 2 is an end elevation view, and
FIG. 3 is a fragmentary cross-sectional view on the line III--III in FIG. 2.
DETAILED DESCRIPTION OF THE INVENTION These drawings illustrate a pump which incorporates altenative arrangements as will be described, and it is to be understood that certain parts can, if desired, be omitted. The pump is suitable for supplying liquid fuel to a gas turbine engine. The pump has a multi-part body which defines a generally cylindrical internal cavity 11 within which is mounted a bladed rotor 12 connected to a shaft 13 which can be driven by the engine to which the pump is intended to supply fuel. The rotor blades, in this example, extend radially and are flat on both faces except at the outer end of the leading face of each blade. At this position, the blade is formed with a concave recess indicated at 12a of part cylindrical cross-section, to form a scoop at the outer end of the blade. The axial depth of the rotor is equal tothe width of the recess so that, except for the center, the whole of the cavity is swept by the rotor blades. In the cylindrical wall of the cavity are a pair of diametrically opposite tangential outlets 14a communicating with respective outlet passages 14- as illustrated in FIG. 2.
One sidewall of the cavity 11 is defined by an inlet plate 15 having a pair of diametrically opposite inlet openings 15a which communicate with a central inlet port 16 formed in the body 10. These inlet openings 15a in the plate 15 are disposed near the inner edges of the rotor blades and are angularly spaced from the outlets 14:: respectively.
The opposite sidewall of the cavity 11 has an annular recess 17 of rectangular channel shape in cross-section. The outer peripheral edge of this coincides with the cylindrical wall of the cavity 11 and the radial width of the recess is approximately a quarter of the radius of the rotor 12. The recess 17 is divided by a pair of fixed abutments 23 secured in the body to form a pair of semicircular recess portions. Radially aligned with one end of the recesses is one of the inlet openings 15a and radially aligned with the other end of each is one of the outlets 14a.
The base wall of the recess 17 is constituted by the crown of an annular piston 18 mounted in the body 10, with this piston being movable in a direction parallel to the axis of the rotor toward and away from the rotor under control of springs 24 acting beneath the abutments 23. At the opposite end of the piston 18 is defined a space to which fluid under pressure can be admitted to control the position of the piston 18 against the action of its springs 24. These springs 24 urge the piston away from the rotor 12 so that when no fluid pressure exists in the space at the end of the piston, the recess 17 will be of maximum depth.
In use, as the rotor 12 rotates, flow of liquid takes place through the inlet openings 15a, between the rotor blades and into the respective portions of the recess 17, and thence again through the spaces between the rotor blades to the outlets 14a. As the liquid flows through the spaces between the blades and through the recess 17 it tends to follow a generally part-toroidal path about a center coincident with the rotor axis between the inlet openings and the outlets respectively; the magnitude of this toroidal movement and therefore the pressure and rate of flow of the liquid leaving the outlets are dependent upon the physical dimensions of the respective recess portions. By varying the position of the annular piston 18, the volume of the recess 17 available for liquid flow can be increased or decreased and it is known that the smaller the recess, the less will be the increase in pressure generated by the toroidal flow. When the recess 17 is completely filled by the piston 18, there will be no tendency for toroidal flow to be generated and the pump will operate in the manner of a normal centrifugal pump.
The pump thus far described can be used as such, but alternatively or additionally to the arrangements for controlling the pressure in the outlet, the position of the inlet plate 15 may be varied. For this purpose, the inlet plate 15 has a flange and is urged toward the rotor 12 by a spring 19. The outer periphery of the inlet plate 15 is stepped and engages in a stepped bore in the body 10.
Between the respective shoulders of the body and inlet plate is defined an annular space 25, with which communicates a fluid pressure inlet passage 26, shown in FIG. 3.
Admission of fluid under pressure to the space causes the inlet plate 15 to be moved against the action of the spring 19. This moves the inlet openings 15a away from the rotor so that the volume of the cavity available for flow is increased. The flow of fluid liquid will now take place, not from two specific points around the rotor, but towards the outlets 14a before entering the spaces between the blades. The pump will operate more like a conventional centrifugal pump, having no recess 17, than when the inlet plate 15 is adjacent to the rotor side face. The pressure rise across the pump will under these circumstances, be less than when the inlet plate 15 is closely adjacent to the rotor. To guide the inlet plate 15 and limit the permitted travel towards and away from the rotor, the flange of the plate 15 has a plurality of elongated slots 20 engaged by a pair of screws 21, 22.
The inlet plate 15 is angularly adjustable to move the inlet openings 15a towards and away from the outlets 14a respectively, thus varying the effective lengths of the recesses which are available for flow between the inlet openings and the outlets respectively. Releasing of the screws 21, 22 engaging in the slots 20 in the inlet plate enables the angular adjustment of the inlet plate 15 to be effected.
If the movable inlet plate is employed instead of the movable piston 18, the body 10 will be provided with a fixed recess 17.
In an alternative construction, there is one recess with one abutment only and the inlet opening is at one side of it and the outlet at the other. The double arrangement described and illustrated affords a better distribution of loads on the piston thus reducing the risk of this jammmg.
In a still further form the outlets are formed in a ring defining the outer peripheral wall of the cavity. This ring is angularly movable to vary the distance between the inlet openings and outlets. Adjustments may be achieved in the manner adopted for angular adjustment of the inlet plate 15 in the form illustrated.
It is to be understood that in the form illustrated two forms of volume variation are provided. In practice only one would be provided in a pump.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
1. A liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor rotatably mounted in the cavity in the body, said body having an inlet and an outlet disposed at respective positions, spaced angularly about the rotor rotational axis, the outlet being disposed in the cylindrical wall of the cavity, a part annular recess being provided in one side wall of the cavity, the recess having an outer peripheral edge adjacent to the cylindrical wall of the cavity, said recess extending around the rotor intermediate the position of the inlet and that of the outlet, and control means actuable to vary the effective combined volume of the cavity and the recess which is available for flow of liquid between the inlet and the outlet.
2. A liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor rotatably mounted in the cavity in the body, an inlet and an outlet in the body disposed at respective positions, spaced angularly about the rotor rotational axis, the outlet being disposed in the cylindrical wall of the cavity, a part annular recess in one side wall of the cavity, the recess having an outer peripheral edge adjacent to the cylindrical wall of the cavity, said recess extending around the rotor intermediate the position of the inlet and that of the outlet, and control means comprising a piston forming the base of the recess in the body, and means for moving said piston in a direction parallel to the rotor rotational axis to vary the volume of said recess which is available for flow of liquid between the inlet and the outlet.
3. The liquid displacement pump as claimed in claim 2 in which there are two inlets and two outlets in the body and the recess is divided into two portions extending between the respective inlets and outlets.
4. A liquid displacement pump comprising a body defining an interior cylindrical cavity, a bladed rotor mounted for rotation in the cavity, said body having an inlet and an outlet disposed'at respective positions spaced angularly about the rotational axis of the rotor, said outlet being disposed in the cylindrical wall of the cavity, one side wall of the cavity having an annular recess of rectangular channel shape in cross section, the outer peripheral edge of the recess coinciding with the cylindrical wall of the cavity, a pair of fixed abutments secured in the body and dividing the recess into a pair of semi-circular portions, the inlet being radially aligned with one end of the recess and the outlet with the other end, and control means for varying the volume of the recess which is available for liquid flow between the inlet and the outlet, said control means including an annular piston having a crown mounted in the body, with the crown defining the base wall of the recess, spring means beneath the abutments for moving the piston in a direction parallel to the axis of the rotor, a space at the opposite end of the piston into which pressure fluid can be introduced to control the piston position against the action of the spring means, and said spring means normally urging the piston away from the rotor when no fluid pressure exists in the space.
References Cited UNITED STATES PATENTS 1,768,313 6 /1930 Ferguson et al 10396 X 2,765,745 10/1956 Sadler et a1. 10342 2,957,424 10/ 1960 Brundage et a1. 10397 3,417,705 12/1968 Skinner 103-97 LEONARD H. GERIN, Primary Examiner US. Cl. X.R.
US734441A 1968-06-04 1968-06-04 Liquid displacement pumps Expired - Lifetime US3516758A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3678147A (en) * 1970-04-13 1972-07-18 Lee H Patchen A method for making reinforced grating
US3973867A (en) * 1975-04-09 1976-08-10 Chien Fu Lee Radial flow type pump

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1768313A (en) * 1930-06-24 Pumping apparatus
US2765745A (en) * 1955-02-21 1956-10-09 Harry J Sadler Pump
US2957424A (en) * 1958-11-19 1960-10-25 Gen Motors Corp Centrifugal pump
US3417705A (en) * 1966-06-13 1968-12-24 Lucas Industries Ltd Liquid displacement pumps

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1768313A (en) * 1930-06-24 Pumping apparatus
US2765745A (en) * 1955-02-21 1956-10-09 Harry J Sadler Pump
US2957424A (en) * 1958-11-19 1960-10-25 Gen Motors Corp Centrifugal pump
US3417705A (en) * 1966-06-13 1968-12-24 Lucas Industries Ltd Liquid displacement pumps

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3678147A (en) * 1970-04-13 1972-07-18 Lee H Patchen A method for making reinforced grating
US3973867A (en) * 1975-04-09 1976-08-10 Chien Fu Lee Radial flow type pump

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