EP2503156A1 - Impeller for centrifugal pump - Google Patents
Impeller for centrifugal pump Download PDFInfo
- Publication number
- EP2503156A1 EP2503156A1 EP11002276A EP11002276A EP2503156A1 EP 2503156 A1 EP2503156 A1 EP 2503156A1 EP 11002276 A EP11002276 A EP 11002276A EP 11002276 A EP11002276 A EP 11002276A EP 2503156 A1 EP2503156 A1 EP 2503156A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- shield diameter
- diameter
- frontal
- blades
- 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.)
- Withdrawn
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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
- F04D29/18—Rotors
- F04D29/22—Rotors specially for centrifugal pumps
- F04D29/2205—Conventional flow pattern
- F04D29/2216—Shape, geometry
Definitions
- the subject of invention is a rotor of impeller pump, especially centrifugal or screw pump with blades of spatial curvature.
- a typical rotor of centrifugal pump generally consists of a hub and frontal as well as rear shield mounted on it, joined with blades forming internal discharge channels.
- the number of blades in rotors is from two to mostly eight or ten pieces, depending on demanded capacity and delivery head.
- centrifugal rotors with blades of two-dimensional curvature there are used centrifugal rotors with blades of two-dimensional curvature, whereas frontal and rear shields have an equal diameter.
- centrifugal rotors with blades of spatial curvature and the rear shield diameter is equal or smaller than the frontal shield diameter, whereas outlet blade edges are a straight parallel line or a line diagonal to an axis of rotation, joining shield edges in order to get a diagonal direction of liquid flow to a stator inserting liquid to the next stage of pumping.
- a rotor type and diameter as well as in less degree a body diameter determines two nominal pump parameters - its capacity (m3/s) and delivery head (m).
- a smaller rotor diameter of impeller pump means less power consumption from a drive shaft as a result of less liquid friction losses on frontal and rear rotor shields as well as smaller surface of blades transferring the momentum moment to the flowing liquid and it causes a smaller delivery head.
- the solution point of rotor, in which out let blade edges are parallel on its all length to the axis of rotor rotation, is that the rear shield diameter is from 0.99 to 0.70 of the frontal shield diameter.
- the solution point of rotor, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation, is that the rear shield diameter is from 0.99 to 0.70 of the frontal shield diameter and outlet blade edges have got skips to be a1 wide, being from 0.01 to 0.9 of rotor discharge channel width, however its height a2 is from 0.01 to 0.5 of its width.
- fig. 1 shows a rotor in an end view in the form of work, in which outlet blade edges are parallel on its all length to the axis of rotor rotation
- fig. 2 shows a rotor in a perspective view, in which outlet blade edges are parallel on its all length to the axis of rotor rotation
- fig. 3 shows a rotor in an end view, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation
- fig. 4 shows a perspective view of rotor, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation.
- FIG. 5 shows a graph of rotor work parameters according to the invention, in which outlet blade edges are parallel on its all length to the axis of rotor rotation and in which the rear shield diameter is 0.96 of the frontal shield diameter, in comparison with the work of standard rotor.
- fig. 6 shows a graph of rotor work parameters according to the invention, in which the rear shield diameter is 0.86 of the frontal shield diameter and a1 skip width is 0.4 of discharge channel width, and its height makes up 0.2 of its width.
- a rotor of impeller pump has got a hub (1), a front a1 shield ( 2 ), a rear shield ( 3 ) joined with blades (4) of outlet edges ( 5 ) parallel to the axis of rotor rotation and having got a skip ( 6 ).
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A pump rotor is characterized by the fact that the rear shield diameter ( 1 ) is from 0.99 to 0.70 of the frontal shield diameter ( 2 ), whereas outlet blade( 2 ) edges ( 2 ) are parallel on its all length to the axis of rotor rotation. Outlet blade edges have got skips to be al wide, being from 0.01 to 0.9 of rotor discharge channel width; however its height a2 is from 0.01 to 0.5 of its width.
Description
- The subject of invention is a rotor of impeller pump, especially centrifugal or screw pump with blades of spatial curvature.
- A typical rotor of centrifugal pump generally consists of a hub and frontal as well as rear shield mounted on it, joined with blades forming internal discharge channels. The number of blades in rotors is from two to mostly eight or ten pieces, depending on demanded capacity and delivery head. In single-stage pumps there are used centrifugal rotors with blades of two-dimensional curvature, whereas frontal and rear shields have an equal diameter. In multi-stage submersible and deep-well pumps there are used centrifugal rotors with blades of spatial curvature and the rear shield diameter is equal or smaller than the frontal shield diameter, whereas outlet blade edges are a straight parallel line or a line diagonal to an axis of rotation, joining shield edges in order to get a diagonal direction of liquid flow to a stator inserting liquid to the next stage of pumping.
- A rotor type and diameter as well as in less degree a body diameter determines two nominal pump parameters - its capacity (m3/s) and delivery head (m).
- A smaller rotor diameter of impeller pump means less power consumption from a drive shaft as a result of less liquid friction losses on frontal and rear rotor shields as well as smaller surface of blades transferring the momentum moment to the flowing liquid and it causes a smaller delivery head.
- The solution point of rotor, in which out let blade edges are parallel on its all length to the axis of rotor rotation, is that the rear shield diameter is from 0.99 to 0.70 of the frontal shield diameter.
- It is advantageously, when the rear shield diameter is from 0.99 to 0.70 of the frontal shield diameter, whereas outlet blade edges are parallel on its all length to the axis of rotor rotation and out let blade edges have got skips to be al wide, being from 0.01 to 0.9 of rotor discharge channel width, however its height a2 is from 0.01 to 0.5 of its width.
- It is advantageously, when the rear shield diameter makes up from 0.98 to 0.85 of the frontal shield diameter.
- It is advantageously, when the rear shield diameter of pump rotor according to the invention makes up from 0.96 to 0.90 of the frontal shield diameter.
- It is very advantageously, when the rear shield diameter of pump rotor according to the invention makes up 0.95 of the frontal shield diameter.
- The solution point of rotor, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation, is that the rear shield diameter is from 0.99 to 0.70 of the frontal shield diameter and outlet blade edges have got skips to be a1 wide, being from 0.01 to 0.9 of rotor discharge channel width, however its height a2 is from 0.01 to 0.5 of its width.
- It is advantageously, when the rear shield diameter of pump rotor is from 0.9 to 0.70 of the frontal shield diameter and outlet blade edges have got skips to be a1 wide, being from 0.1 to 0.6 of b2 rotor discharge channel width, however its height a2 is from 0.2 to 0.5 of its a1 width.
- It is very advantageously, when the rear shield diameter of
pump 5 rotors is from 0.80 to 0.70 of the frontal shield diameter and outlet blade edges have got skips to be a1 wide, being from 0.4 to 0.5 of rotor discharge channel width; however its height a2 is from 0.4 to 0.5 of its a1 width. - The invention was presented in work examples in the figure, not limiting them in any way, on which
fig. 1 shows a rotor in an end view in the form of work, in which outlet blade edges are parallel on its all length to the axis of rotor rotation,fig. 2 shows a rotor in a perspective view, in which outlet blade edges are parallel on its all length to the axis of rotor rotation,fig. 3 shows a rotor in an end view, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation,fig. 4 shows a perspective view of rotor, in which outlet blade edges are on its all length directed askew to the axis of rotor rotation.Fig. 5 shows a graph of rotor work parameters according to the invention, in which outlet blade edges are parallel on its all length to the axis of rotor rotation and in which the rear shield diameter is 0.96 of the frontal shield diameter, in comparison with the work of standard rotor. However,fig. 6 shows a graph of rotor work parameters according to the invention, in which the rear shield diameter is 0.86 of the frontal shield diameter and a1 skip width is 0.4 of discharge channel width, and its height makes up 0.2 of its width. - A rotor of impeller pump has got a hub (1), a front a1 shield ( 2 ), a rear shield ( 3 ) joined with blades (4) of outlet edges ( 5 ) parallel to the axis of rotor rotation and having got a skip ( 6 ).
- Broken lines presented in
fig. 5 illustrate the rise of rotor efficiency, which the rear shield diameter is 0.96 of the frontal shield diameter. It is caused by the decrease of whirling shield friction loss without decreasing the surface of rotor blades. As a result, power consumption is decreasing without a significant decrease of delivery head, what causes, as a last resort, the efficiency rise of the whole impeller pump. The second observed result of such rotor construction is loosening the outlet rotor blade grid, causing lowering a speed value and decreasing the outlet loss from the rotor as well as the inlet loss to the element of liquid draining, having also an impact on the efficiency rise. In case of multi-stage pumps there is being observed a mating improvement of rotor and stator as a result of faster change of liquid flow direction in the direction of rotor axis and decreasing flow losses in the flow system. - In
fig. 6 there is shown a rotor profile with a skip from the side of rear shield by means of broken line. There has been observed a significant decrease of power consumed by a rotor with insignificant lowering the delivery head, what finally gives the rise of pump efficiency. It is caused by decreasing liquid friction losses of whirling shields as well as partial power decrease, transferred by blades to pumped liquid. Apart from the efficiency increase, there has been observed a profile e form improvement of pump flow. In case of unstable profiles, in which a delivery head for - Q=0 is smaller than for a pump efficiency Q>0 the applied rotor according to the invention causes the rise of delivery head for small pump capacity.
Claims (8)
- A rotor of impeller pump including a hub, a frontal shield, a rear shield joined with blades, characterized in that the rear shield diameter ( 1 ) is from 0.99 to 0.70 of the frontal shield diameter
( 9 ), whereas outlet edges (5) of blades ( 4 ) are parallel on its all length to the axis of rotor rotation. - A pump rotor according to the claim 1 characterized in that the rear shield diameter ( 3 ) is from 0.99 to 0.70 of the frontal shield diameter ( 2 ), whereas outlet edges ( 5 ) of blades ( 4 ) are parallel on its all length to the axis of rotor rotation and outlet blade edges have got skips ( 6 ) to be a1 wide, being from 0.01 to 0.9 of rotor discharge channel width, however its height a2 is from 0.01 to 0.5 of its width.
- A pump rotor according to the claim 1 or 2 characterized in that the rear shield diameter ( 3 ) makes up from 0.98 to 0.85 of the frontal shield diameter ( 2 ).
- A pump rotors according to the claim 3 characterized in that the rear shield diameter ( 3 ) makes up from 0.96 to 0.90 of the frontal shield diameter ( 2 ).
- A pump rotor according to the claim 4 characterized in that the rear shield diameter ( 3 ) makes up 0.92 of the frontal shield diameter ( 2 ).
- A rotor of impeller pump including a hub, a frontal shield, a rear shield joined with blades, characterized in that the rear shield diameter ( 3 ) is from 0.99 to 0.70 of the frontal shield diameter
( 2 ), whereas outlet blade edges are on its all length directed askew to the axis of rotor rotation and outlet edges ( 5 ) of blades ( 4 ) have got skips
( 6 ) to be a1 wide, being from 0.01 to 0.9 of rotor discharge channel width, however its height a2 is from 0.01 to 0.5 of its width. - A pump rotor according to the claim 6 characterized in that the rear shield diameter ( 3 ) is from 0.9 to 0.70 of the frontal shield diameter ( 2 ) and outlet edges (5) of blades ( 4 ) have got skips to be al wide, being from 0.1 to 0.6 of rotor discharge channel width, however its height a2 is from 0.2 to 0.5 of its width.
- A pump rotor according to the claim 7 characterized in that the rear shield diameter ( 3 ) is from 0.80 to 0.70 of the frontal shield diameter ( 2 ) and outlet edges ( 5 ) of blades ( 4 ) have got skips to be a1 wide, being from 0.4 to 0.5 of its width.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11002276A EP2503156A1 (en) | 2011-03-20 | 2011-03-20 | Impeller for centrifugal pump |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11002276A EP2503156A1 (en) | 2011-03-20 | 2011-03-20 | Impeller for centrifugal pump |
Publications (1)
Publication Number | Publication Date |
---|---|
EP2503156A1 true EP2503156A1 (en) | 2012-09-26 |
Family
ID=45444339
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11002276A Withdrawn EP2503156A1 (en) | 2011-03-20 | 2011-03-20 | Impeller for centrifugal pump |
Country Status (1)
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EP (1) | EP2503156A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105508292A (en) * | 2015-12-17 | 2016-04-20 | 江苏国泉泵业制造有限公司 | Semi-open type vortex pump impeller structure design method |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5216009A (en) * | 1975-07-29 | 1977-02-07 | Shinko Kikai Seisakusho:Kk | Centrifugal fan |
US4886417A (en) * | 1988-12-06 | 1989-12-12 | Sundstrand Corporation | Fuel pump and radial-flow impeller therefor |
JP2001003888A (en) * | 1999-06-22 | 2001-01-09 | Teral Kyokuto Inc | Impeller of submersible motor pump for deep well |
US6481961B1 (en) * | 2001-07-02 | 2002-11-19 | Sea Chung Electric Co., Ltd. | Stage for a centrifugal submersible pump |
JP2009167990A (en) * | 2008-01-21 | 2009-07-30 | Mitsubishi Heavy Ind Ltd | Centrifugal pump |
US20090280013A1 (en) * | 2008-05-06 | 2009-11-12 | Minel Kupferberg | Frustoconical centrifugal wheel |
WO2011089512A2 (en) * | 2010-01-22 | 2011-07-28 | Itt Manufacturing Enterprises, Inc. | Centrifugal pump |
-
2011
- 2011-03-20 EP EP11002276A patent/EP2503156A1/en not_active Withdrawn
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5216009A (en) * | 1975-07-29 | 1977-02-07 | Shinko Kikai Seisakusho:Kk | Centrifugal fan |
US4886417A (en) * | 1988-12-06 | 1989-12-12 | Sundstrand Corporation | Fuel pump and radial-flow impeller therefor |
JP2001003888A (en) * | 1999-06-22 | 2001-01-09 | Teral Kyokuto Inc | Impeller of submersible motor pump for deep well |
US6481961B1 (en) * | 2001-07-02 | 2002-11-19 | Sea Chung Electric Co., Ltd. | Stage for a centrifugal submersible pump |
JP2009167990A (en) * | 2008-01-21 | 2009-07-30 | Mitsubishi Heavy Ind Ltd | Centrifugal pump |
US20090280013A1 (en) * | 2008-05-06 | 2009-11-12 | Minel Kupferberg | Frustoconical centrifugal wheel |
WO2011089512A2 (en) * | 2010-01-22 | 2011-07-28 | Itt Manufacturing Enterprises, Inc. | Centrifugal pump |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105508292A (en) * | 2015-12-17 | 2016-04-20 | 江苏国泉泵业制造有限公司 | Semi-open type vortex pump impeller structure design method |
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Effective date: 20130327 |