US2764944A - Centrifugal pumps - Google Patents
Centrifugal pumps Download PDFInfo
- 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
- Authority
- US
- 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
Links
- 239000007788 liquid Substances 0.000 description 6
- 238000005086 pumping Methods 0.000 description 2
- 239000000295 fuel oil Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/445—Fluid-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.
Landscapes
- 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
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2764944X | 1954-02-03 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2764944A true US2764944A (en) | 1956-10-02 |
Family
ID=10914918
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US485054A Expired - Lifetime US2764944A (en) | 1954-02-03 | 1955-01-31 | Centrifugal pumps |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2764944A (en) |
Cited By (12)
| 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)
| 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. |
-
1955
- 1955-01-31 US US485054A patent/US2764944A/en not_active Expired - Lifetime
Patent Citations (3)
| 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)
| 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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2764944A (en) | Centrifugal pumps | |
| US3289921A (en) | Vaneless diffuser | |
| GB1350471A (en) | Gas turbine engine | |
| GB1400761A (en) | Axial or semi-axial flow impeller pump | |
| GB1510629A (en) | Centrifugal compressor or centripetal turbine | |
| GB1291235A (en) | Fluid flow machine | |
| US1020699A (en) | Centrifugal pump. | |
| US3392675A (en) | Centrifugal pump | |
| GB1387480A (en) | Energy transfer machine | |
| US4236867A (en) | Friction reducing arrangement for hydraulic machines | |
| US3493169A (en) | Bleed for compressor | |
| CA1086137A (en) | Jet flap controlled fuel pump | |
| US2157002A (en) | Diffuser for centrifugal compressors | |
| GB1043168A (en) | Improvements in or relating to turbo-compressors | |
| GB1145895A (en) | Centrifugal pump | |
| GB1440551A (en) | Pitot pump with slotted inlet passages in rotor case | |
| US3356034A (en) | Fluid pump flow bypass control | |
| US2399072A (en) | Centrifugal compressor | |
| GB1599908A (en) | Centrifugal pumps | |
| GB1432974A (en) | ||
| US2190245A (en) | Pump for compressible fluids | |
| US2981516A (en) | Turbine housing | |
| GB1503905A (en) | Centrifugal fluid pumps | |
| GB2074662A (en) | Rotary Impeller for a Centrifugal Pump | |
| US3164369A (en) | Multistage multiple-reentry turbine |