US1941442A - Multistage centrifugal pump - Google Patents

Multistage centrifugal pump Download PDF

Info

Publication number
US1941442A
US1941442A US655926A US65592633A US1941442A US 1941442 A US1941442 A US 1941442A US 655926 A US655926 A US 655926A US 65592633 A US65592633 A US 65592633A US 1941442 A US1941442 A US 1941442A
Authority
US
United States
Prior art keywords
stages
pump
stage
impellers
centrifugal pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US655926A
Inventor
Daniel J Moran
Edwin O Bennett
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ConocoPhillips Co
Original Assignee
Continental Oil Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Continental Oil Co filed Critical Continental Oil Co
Priority to US655926A priority Critical patent/US1941442A/en
Application granted granted Critical
Publication of US1941442A publication Critical patent/US1941442A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/06Multi-stage pumps

Definitions

  • the customary design for centrifugal Vpumps is one in which the stages are placed in series along the shaft with the low pressure or intake stage at one end and the high pressure or discharge stage at the other end.
  • the disadvantage inherent in this design is that the axial thrust is in one direction.
  • the hydraulic unbalance of this type of construction requires special balancing disks or cylinders on the shaft.
  • specially designed thrust bearings are used in order to hold the rotating elements in their correct spatial relation to the stationary parts.
  • the outlet or discharge pressure is usually very high. This necessitates the packing of the discharge end against atmospheric pressure.
  • the high pressure within the pump tends to promote leakage.
  • Our invention contemplates a multi-stage centrifugal pump design in which the number of stages is odd. While we prefer to use an odd number of stages, it is to be remembered that an even number of stages can be used within thespirit of our invention.
  • Figure 1 shows a diagrammatic sectional elevation of a pump embodying one mode of carrying out our invention.
  • Figure 2 is a sectional view taken on the line 2-2 of Figure 1.
  • Figure 3 is a sectional view taken on the line 3 3 of Figure 1.
  • a shaft l is mounted for rotation within a suiti able casing or housing 2.
  • a pair oi centrifugal impellers 3 and 3a are keyed to the shaft l by keys 4 and 5.
  • the impellers 3 and 3a are dis- 13a from impeller 3a. It will be observed that 65 the capacity of impellers 3 and 3a is one half that i of the remaining impellers of the pump.
  • the two stages 3 and 3a will handle a volume of iiuid equivalent to that handled by any one of the remaining stages of the pump.
  • the fluid from the 79 two divided stages 3 and 3c passes from duct 13a to stage 10 of the pump, thence to stages 9 and 8 as can readily be seen by reference to Figure 1.-
  • the fluid from stage 8 passes through duct 14 to stage 5 and thence through stages 6 and 'l as can be seen by reference to Figure l.
  • stages 5, 6, and 7 are opposed to stages 8, 9, and 10 so that the thrust will be balanced.
  • the iiow of the iiuid through the stages of each group is toward the center of the pump.
  • 'f lIhe final stage 7 communicates with eduction tubing 15.
  • the impellers may be of any suitable design and may be provided with blades 16 as can be seen by reference to Figure 2.
  • the transfer lines 13 and 14 may be external of the pump if desired. Likewise, line 13 may be formed by a bore in the pump casing if it is desired.
  • a multi-stage centrifugal pump having an odd number of stages and an even number of impellers, two of said impellers having half the capacity of the other impellers and being disposed at opposite ends of said pump, and means for splitting the induction fow of the liquid being pumped to said impellers of half capacity.
  • a multi-stage centrifugal pump comprising ⁇ stages on one side in combination a casing, n+1 centrifugal impeling stages, n+2 impellers, two of said impellers having half the capacity of the other impellers, said half capacity impeliers being disposed at the ends of the pump and adapted to form the rst stage, the other stages being distributed in the following manner:

Landscapes

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

Description

Dec., 26, 1933. D. J. MoRAN ET AL Y MULTISTAGE CENTRIFUGAL PUMP Filed Feb. 9. 1933 Patented Dec. 26, 1933 PATENT ,o1-Flos 1,941,442 l f' MULTISTAGE CENTRIFUGAL PUMP Daniel J. Moran and Edwin 0. Bennett, Ponca l City, kla., assignors to Continental Oil -Company, Ponca City, Okla., a corporation of Dela- Ware Application February 9, 1933. Serial No. 655,926
2 Claims. (Cl. 10S-109) Our invention relates to multi-stage centrifugal pumps and more particularly to a balanced centrifugal pump construction.
The customary design for centrifugal Vpumps is one in which the stages are placed in series along the shaft with the low pressure or intake stage at one end and the high pressure or discharge stage at the other end. The disadvantage inherent in this design is that the axial thrust is in one direction. The hydraulic unbalance of this type of construction requires special balancing disks or cylinders on the shaft. Sometimes specially designed thrust bearings are used in order to hold the rotating elements in their correct spatial relation to the stationary parts. y
Where many stages are used, the outlet or discharge pressure is usually very high. This necessitates the packing of the discharge end against atmospheric pressure. The high pressure within the pump tends to promote leakage. In' order to preclude the escape of the fluid being pumped, it is necessary to keep the discharge end stuiiing box extremely tight especially when volatile liquids are used. This creates friction and entails power losses. The result is that the operating 'emciency is lowered.
Our invention contemplates a multi-stage centrifugal pump design in which the number of stages is odd. While we prefer to use an odd number of stages, it is to be remembered that an even number of stages can be used within thespirit of our invention. We propose with an odd number of stages to split the first stage. The remaining impellers are divided into two groups and placed along the shaft in back to back relationship. Each section of the split stage has one half the volume capacity of one of the remaining stages of the pump.
In the accompanying drawing which forms part of the instant specification and which is t0 be read in conjunction therewith, and in which\ like reference numerals are used to indicate like parts in the various views;
Figure 1 shows a diagrammatic sectional elevation of a pump embodying one mode of carrying out our invention.
Figure 2 is a sectional view taken on the line 2-2 of Figure 1.
Figure 3 is a sectional view taken on the line 3 3 of Figure 1.
More particularly referring now to the draw-a ing, a shaft l is mounted for rotation within a suiti able casing or housing 2. A pair oi centrifugal impellers 3 and 3a are keyed to the shaft l by keys 4 and 5. The impellers 3 and 3a are dis- 13a from impeller 3a. It will be observed that 65 the capacity of impellers 3 and 3a is one half that i of the remaining impellers of the pump. The two stages 3 and 3a will handle a volume of iiuid equivalent to that handled by any one of the remaining stages of the pump. The fluid from the 79 two divided stages 3 and 3c passes from duct 13a to stage 10 of the pump, thence to stages 9 and 8 as can readily be seen by reference to Figure 1.- The fluid from stage 8 passes through duct 14 to stage 5 and thence through stages 6 and 'l as can be seen by reference to Figure l. It is to ybe remembered that stages 5, 6, and 7 are opposed to stages 8, 9, and 10 so that the thrust will be balanced. The iiow of the iiuid through the stages of each group is toward the center of the pump. 'f lIhe final stage 7 communicates with eduction tubing 15. The impellers may be of any suitable design and may be provided with blades 16 as can be seen by reference to Figure 2. The transfer lines 13 and 14 may be external of the pump if desired. Likewise, line 13 may be formed by a bore in the pump casing if it is desired. Y
It will be noted that our arrangement provides for an even number of impellers at all, times and that the ow through the pump is such that the thrust at the opposite ends of the pump equalize. This feature makes for a pump having a long life. The introduction of the iluid to the low pressure impellers and their disposition at the ends of the pump require that the stuing boxes 17 and-18 hold back only such pressure as is occasioned by the differential between the atmospheric pressure and that existing in the first stage. This is a great advantage as obviously this pressure will be much lower than that ex- 190 isting at the high pressure or discharge stage. 'l
If an even number of stages is used, we may introduce the liquid to one outboard stage, transfer it to the second outboard stage, and
then continue as shown. This method has the disadvantage of requiring a packing at one end which will withstand the pressure developed in the second stage which is considerably higher than that developed in the rst stage. This modification ci' our invention is not shown but it il@ The uuid to 6:0,-
is to be understood that it is Within the spirit thereof.
It will be understood that certain features and subcombinations are of utility and may be employed without reference to other features and sub-combinations. This is contemplated by and is within the scope of our claims. t is further obvious that various changes may be made in details Within the scope of our claims Without departing from the spirit of our invention. Xt is, therefore, to be understood that our invention is not to be limited to the specific details shown and described.
Having thus described our invention, what We claim is:
1. A multi-stage centrifugal pump having an odd number of stages and an even number of impellers, two of said impellers having half the capacity of the other impellers and being disposed at opposite ends of said pump, and means for splitting the induction fow of the liquid being pumped to said impellers of half capacity.
2. A multi-stage centrifugal pump comprising `stages on one side in combination a casing, n+1 centrifugal impeling stages, n+2 impellers, two of said impellers having half the capacity of the other impellers, said half capacity impeliers being disposed at the ends of the pump and adapted to form the rst stage, the other stages being distributed in the following manner:
of the center of said pump and NIB
stages opposed to the rst stages, means for dividing the induction iiuid to said first stage and the last stage of the pump being disposed near the central part thereof, wherein n is any even number.
DANIEL J. MORAN. EDWEN O. BENNETT.
US655926A 1933-02-09 1933-02-09 Multistage centrifugal pump Expired - Lifetime US1941442A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US655926A US1941442A (en) 1933-02-09 1933-02-09 Multistage centrifugal pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US655926A US1941442A (en) 1933-02-09 1933-02-09 Multistage centrifugal pump

Publications (1)

Publication Number Publication Date
US1941442A true US1941442A (en) 1933-12-26

Family

ID=24630958

Family Applications (1)

Application Number Title Priority Date Filing Date
US655926A Expired - Lifetime US1941442A (en) 1933-02-09 1933-02-09 Multistage centrifugal pump

Country Status (1)

Country Link
US (1) US1941442A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2668502A (en) * 1949-10-26 1954-02-09 Allis Chalmers Mfg Co Double casing pump
WO2006021560A1 (en) * 2004-08-23 2006-03-02 Frank Mohn Flatøy As Rotodynamic fluid machine
US20070154304A1 (en) * 2005-12-29 2007-07-05 Abdallah Shaaban A Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of rotor blades
US11326607B2 (en) * 2019-02-05 2022-05-10 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11359472B2 (en) 2019-02-05 2022-06-14 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser
US11994016B2 (en) 2021-12-09 2024-05-28 Saudi Arabian Oil Company Downhole phase separation in deviated wells
US12012550B2 (en) 2021-12-13 2024-06-18 Saudi Arabian Oil Company Attenuated acid formulations for acid stimulation

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2668502A (en) * 1949-10-26 1954-02-09 Allis Chalmers Mfg Co Double casing pump
WO2006021560A1 (en) * 2004-08-23 2006-03-02 Frank Mohn Flatøy As Rotodynamic fluid machine
US20070212238A1 (en) * 2004-08-23 2007-09-13 Frank Mohn Flatoy As Rotodynamic Fluid Machine
US20070154304A1 (en) * 2005-12-29 2007-07-05 Abdallah Shaaban A Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of rotor blades
US7600961B2 (en) * 2005-12-29 2009-10-13 Macro-Micro Devices, Inc. Fluid transfer controllers having a rotor assembly with multiple sets of rotor blades arranged in proximity and about the same hub component and further having barrier components configured to form passages for routing fluid through the multiple sets of rotor blades
US11326607B2 (en) * 2019-02-05 2022-05-10 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11359472B2 (en) 2019-02-05 2022-06-14 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11686312B2 (en) 2019-02-05 2023-06-27 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser
US11994016B2 (en) 2021-12-09 2024-05-28 Saudi Arabian Oil Company Downhole phase separation in deviated wells
US12012550B2 (en) 2021-12-13 2024-06-18 Saudi Arabian Oil Company Attenuated acid formulations for acid stimulation

Similar Documents

Publication Publication Date Title
US5599164A (en) Centrifugal process pump with booster impeller
US2319730A (en) Pump
EP3527830A1 (en) System for moving fluid with opposed axial forces
US2194054A (en) Pumping system
US1941442A (en) Multistage centrifugal pump
US1927543A (en) Sealing device
US2233825A (en) Pump
US2475316A (en) Fluid pumping system
US2601828A (en) Centrifugal pump
US2340787A (en) Means for balancing rotary pumps
US2678606A (en) Centrifugal pump or compressor
US2393691A (en) Pumping unit
US1979621A (en) Balanced turbulence pump
US2635547A (en) Axial gap electric motor-driven pump
US2046226A (en) Centrifugal pump
US3132595A (en) Axial flow pump
US2472010A (en) Hermetically sealed power transmitting mechanism
US2502173A (en) Fluid balancing means
GB1364117A (en) Multistage centrifugal pumps
CN206874490U (en) Axial subdivision three-level centrifugal pump
US2662479A (en) Turbine pump or motor
US3273906A (en) Rotating shaft seal
US1849217A (en) Pump
CN205136033U (en) Multistage low temperature liquid oxygen pump of vertical radial subdivision
US2455460A (en) Rotary pump for liquefied gases