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US2764944A - Centrifugal pumps - Google Patents

Centrifugal pumps Download PDF

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Publication number
US2764944A
US2764944A US485054A US48505455A US2764944A US 2764944 A US2764944 A US 2764944A US 485054 A US485054 A US 485054A US 48505455 A US48505455 A US 48505455A US 2764944 A US2764944 A US 2764944A
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United States
Prior art keywords
impeller
diffuser
centrifugal pumps
cross sectional
sectional area
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
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US485054A
Inventor
Owen N Lawrence
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
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Publication date
Application filed by Lucas Industries Ltd filed Critical Lucas Industries Ltd
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Publication of US2764944A publication Critical patent/US2764944A/en
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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
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/445Fluid-guiding means, e.g. diffusers especially adapted for liquid pumps

Definitions

  • This invention relates to centrifugal pumps for pumping liquids, and more particularly pumps for supplying liquid fuel oil to jet propulsion engines, gas turbines or the like.
  • the object of the present invention is to provide an improved pump which will obviate the aforesaid condition over a desired range of variation of the rate of outflow, which latter is controlled by a valve.
  • a pump embodying the invention comprises the combination of a rotary impeller, a diffuser ring surrounding the impeller and having therein a plurality of nozzlelike divergent passages the axes of which are substantially tangential to the periphery of the impeller, and a housing having therein a spiral chamber of stepped configuration, each step subtending an angular distance equal to the angular distance between the outlet ends of an adjacent pair of the said diffuser passages, the cross sectional area of the first step being equal to the area of the 40 outlet end of the adjacent difiuser passage, and the cross sectional area of each of the other steps being equal to its number times the cross sectional area of the first step.
  • the rotary impeller a is provided with four equi-spaced radial vanes 12.
  • a fixed diffuser ring 0 having in it any convenient number of (for example eight) equispaced nozzle-like divergent passages d, the axes of which ice are substantially tangential to the periphery of the impeller.
  • a spiral chamber consisting of a series of steps as f of progressively increasing radial depth.
  • Each of the steps subtends an angular distance equal to the angular distance between the discharge ends of a pair of adjacent diffuser passages d, and the cross sectional area of the first step is equal to the area of the discharge end of the first diffuser passage.
  • the cross sectional area of the second step is twice that of the first step, and that of the third step is three times that of the first step, and so on.
  • this passage may be made of divergent form to increase the pressure of the efiluent liquid to the desired amount.
  • liquid under the control of a valve can be discharged at a substantially uniform pressure over a wide range of variation of rate of flow.
  • the invention is not, however, limited to the example above described, as the number and shape of the vanes on the impeller, and the number of passages and steps in the diffuser and housing respectively may be varied to meet different requirements.
  • a centrifugal pump for pumping liquids comprising the combination of a rotary impeller, a diffuser ring surrounding the impeller and having therein a plurality of nozzle-like divergent passages the axes of which are substantially tangential to the periphery of the impeller, and a housing having therein a spiral chamber of stepped configuration, each step subtending an angular distance equal to the angular distance between the outlet ends of an adjacent pair of the said diffuser passages, the cross sectional area of the first step being equal to the area of the outlet end of the adjacent diffuser passage, and the cross sectional area of each of the other steps being equal to its number times the cross sectional area of the first step.

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

Description

Oc 1956 o. N. LAWRENCE CENTRIFUGAL PUMPS Filed Jan; 31, 1955 CENTRIFUGAL PUMPS Owen N. Lawrence, Dorridge, England, assignor to Joseph Lucas (Industries) Limited, Birmingham, England Application January 31, 1955, Serial No. 485,054
Claims priority, application Great Britain February 3, 1954" 1 Claim. (Cl. 103-103) This invention relates to centrifugal pumps for pumping liquids, and more particularly pumps for supplying liquid fuel oil to jet propulsion engines, gas turbines or the like.
It has been found that when a pump of conventional form is run at a constant speed, and the outflow is controlled by a valve, the pressure of the discharged liquid varies in a capricious manner with variation of the rate of outflow.
The object of the present invention is to provide an improved pump which will obviate the aforesaid condition over a desired range of variation of the rate of outflow, which latter is controlled by a valve.
A pump embodying the invention comprises the combination of a rotary impeller, a diffuser ring surrounding the impeller and having therein a plurality of nozzlelike divergent passages the axes of which are substantially tangential to the periphery of the impeller, and a housing having therein a spiral chamber of stepped configuration, each step subtending an angular distance equal to the angular distance between the outlet ends of an adjacent pair of the said diffuser passages, the cross sectional area of the first step being equal to the area of the 40 outlet end of the adjacent difiuser passage, and the cross sectional area of each of the other steps being equal to its number times the cross sectional area of the first step.
The accompanying drawing illustrates diagrammatically a typical embodiment of the invention.
Referring to the drawing, the rotary impeller a is provided with four equi-spaced radial vanes 12. Around the impeller is mounted a fixed diffuser ring 0 having in it any convenient number of (for example eight) equispaced nozzle-like divergent passages d, the axes of which ice are substantially tangential to the periphery of the impeller.
In the housing e is formed around the diffuser ring a spiral chamber consisting of a series of steps as f of progressively increasing radial depth. Each of the steps subtends an angular distance equal to the angular distance between the discharge ends of a pair of adjacent diffuser passages d, and the cross sectional area of the first step is equal to the area of the discharge end of the first diffuser passage. The cross sectional area of the second step is twice that of the first step, and that of the third step is three times that of the first step, and so on.
At its discharge end the spiral chamber is provided with a discharge passage. If desired, this passage may be made of divergent form to increase the pressure of the efiluent liquid to the desired amount.
By the use of a diffuser and stepped spiral chamber as above described, liquid under the control of a valve can be discharged at a substantially uniform pressure over a wide range of variation of rate of flow.
The invention is not, however, limited to the example above described, as the number and shape of the vanes on the impeller, and the number of passages and steps in the diffuser and housing respectively may be varied to meet different requirements.
Having thus described my invention what I claim as new and desire to secure by Letters Patent is:
A centrifugal pump for pumping liquids, comprising the combination of a rotary impeller, a diffuser ring surrounding the impeller and having therein a plurality of nozzle-like divergent passages the axes of which are substantially tangential to the periphery of the impeller, and a housing having therein a spiral chamber of stepped configuration, each step subtending an angular distance equal to the angular distance between the outlet ends of an adjacent pair of the said diffuser passages, the cross sectional area of the first step being equal to the area of the outlet end of the adjacent diffuser passage, and the cross sectional area of each of the other steps being equal to its number times the cross sectional area of the first step.
References Cited in the file of this patent UNITED STATES PATENTS 1,233,115 Osborne July 10, 1917 FOREIGN PATENTS 219,739 Switzerland June 1, 1942 419,544 Great Britain Nov. 18, 1934
US485054A 1954-02-03 1955-01-31 Centrifugal pumps Expired - Lifetime US2764944A (en)

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GB2764944X 1954-02-03

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123284A (en) * 1964-03-03 greenawalt
US3289598A (en) * 1965-10-21 1966-12-06 Ingersoll Rand Co Centrifugal pumps
US3642379A (en) * 1969-06-27 1972-02-15 Judson S Swearingen Rotary gas-handling machine and rotor therefor free of vibration waves in operation
US3775024A (en) * 1970-05-20 1973-11-27 Airtex Prod Division Of United Submersible fuel pump
US3904312A (en) * 1974-06-12 1975-09-09 Avco Corp Radial flow compressors
US3905721A (en) * 1974-09-03 1975-09-16 Gen Motors Corp Centrifugal compressor diffuser
US4234290A (en) * 1978-11-30 1980-11-18 Binks Manufacturing Company Turbine pump
US4278396A (en) * 1978-05-15 1981-07-14 John Vander Horst Hub seals for thrust-assisted centrifugal pump
FR2544402A1 (en) * 1983-04-15 1984-10-19 Ingersoll Rand Co CENTRIFUGAL PUMP COMPRISING A VOLUME TYPE DIFFUSER
US20130047606A1 (en) * 2010-04-07 2013-02-28 Daimler Ag Internal combustion engine
WO2013072997A1 (en) * 2011-11-14 2013-05-23 五大産業株式会社 Pump device
DE102013218410A1 (en) * 2013-09-13 2015-04-02 Technochem Im- Und Export Gmbh centrifugal pump

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1233115A (en) * 1916-04-08 1917-07-10 Clarence N Mack Centrifugal conveyer-fan.
GB419544A (en) * 1934-01-12 1934-11-14 G & J Weir Ltd Improvements in centrifugal pumps
CH219739A (en) * 1941-01-16 1942-02-28 Oerlikon Maschf Centrifugal hoist with volute casing.

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1233115A (en) * 1916-04-08 1917-07-10 Clarence N Mack Centrifugal conveyer-fan.
GB419544A (en) * 1934-01-12 1934-11-14 G & J Weir Ltd Improvements in centrifugal pumps
CH219739A (en) * 1941-01-16 1942-02-28 Oerlikon Maschf Centrifugal hoist with volute casing.

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3123284A (en) * 1964-03-03 greenawalt
US3289598A (en) * 1965-10-21 1966-12-06 Ingersoll Rand Co Centrifugal pumps
US3642379A (en) * 1969-06-27 1972-02-15 Judson S Swearingen Rotary gas-handling machine and rotor therefor free of vibration waves in operation
US3775024A (en) * 1970-05-20 1973-11-27 Airtex Prod Division Of United Submersible fuel pump
US3904312A (en) * 1974-06-12 1975-09-09 Avco Corp Radial flow compressors
US3905721A (en) * 1974-09-03 1975-09-16 Gen Motors Corp Centrifugal compressor diffuser
US4278396A (en) * 1978-05-15 1981-07-14 John Vander Horst Hub seals for thrust-assisted centrifugal pump
US4234290A (en) * 1978-11-30 1980-11-18 Binks Manufacturing Company Turbine pump
FR2544402A1 (en) * 1983-04-15 1984-10-19 Ingersoll Rand Co CENTRIFUGAL PUMP COMPRISING A VOLUME TYPE DIFFUSER
US20130047606A1 (en) * 2010-04-07 2013-02-28 Daimler Ag Internal combustion engine
US9097173B2 (en) * 2010-04-07 2015-08-04 Daimler Ag Internal combustion engine
WO2013072997A1 (en) * 2011-11-14 2013-05-23 五大産業株式会社 Pump device
DE102013218410A1 (en) * 2013-09-13 2015-04-02 Technochem Im- Und Export Gmbh centrifugal pump
DE102013218410B4 (en) 2013-09-13 2022-07-14 Technochem Im- Und Export Gmbh centrifugal pump

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