EP0466350A2 - Multi-stage centrifugal pumps - Google Patents
Multi-stage centrifugal pumps Download PDFInfo
- Publication number
- EP0466350A2 EP0466350A2 EP91305692A EP91305692A EP0466350A2 EP 0466350 A2 EP0466350 A2 EP 0466350A2 EP 91305692 A EP91305692 A EP 91305692A EP 91305692 A EP91305692 A EP 91305692A EP 0466350 A2 EP0466350 A2 EP 0466350A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- pin
- bushing
- casing
- ring
- split
- 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.)
- Granted
Links
- 230000006835 compression Effects 0.000 claims abstract description 4
- 238000007906 compression Methods 0.000 claims abstract description 4
- 238000007789 sealing Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 239000012530 fluid Substances 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 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
- F04D29/08—Sealings
- F04D29/16—Sealings between pressure and suction sides
- F04D29/165—Sealings between pressure and suction sides especially adapted for liquid pumps
- F04D29/167—Sealings between pressure and suction sides especially adapted for liquid pumps of a centrifugal flow wheel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D1/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D1/06—Multi-stage pumps
Definitions
- This invention relates to multi-stage centrifugal pumps, and more particularly to means for preventing rotation of an inter-stage bushing or ring in a multi-stage centrifugal pump with an axially split casing which houses a shaft carrying impellers.
- a multi-stage centrifugal pump has a number of inter-stage bushings and rings, sometimes called stage pieces and wear rings, which fit within the casing and have to be accurately positioned radially and locked against axial and rotational movement.
- These bushings and rings have essentially the same function as one another, namely to seal each side of each impeller, but the bushings have a larger radial thickness and may carry integral guide vanes for the incoming fluid whereas the rings have a smaller radial thickness and lack guide vanes.
- Radial positioning is by means of a close fit between the periphery of the bushing or ring and a bore machined in the casing.
- Axial location is by means of a flange on the bushing or ring which engages in an annular groove machined in the casing.
- each bushing or ring has been prevented from rotating by means of a small pin fitted into a radial hole drilled in the base of the annular groove, said pin protruding into an axial slot machined in the flange.
- the pins have been fitted in the lower half of the casing in the vertical plane containing the pump axis, so that the axial slots in the bushings and rings could be engaged with the pins during the assembly of the shaft and impellers into the lower half of the casing.
- the object of the present invention is to avoid the aforesaid disadvantages.
- means for preventing rotation of an inter-stage bushing or ring in a multi-stage centrifugal pump with an axially split casing which houses a shaft carrying impellers are characterised by a tangential pin fitted into a hole provided in either half of the casing at its join face, the centre-line of the pin being normal to the join face and the exposed end of the pin being flush with said face, and a recess in which the pin engages provided in the periphery of the bushing or ring.
- a multi-stage centrifugal pump has a casing indicated generally at 10 which is split axially in a horizontal plane and houses a power-driven shaft 12 on which there are rigidly secured a plurality of impellers 14.
- Each impeller 14 is disposed in a chamber 16 having an axial inlet 18 and a radial outlet 20, the chambers 16 being connected in series in well-known manner.
- An inter-stage ring 22 is disposed at the inlet side of each impeller 14, and an inter-stage bushing 24 carrying integral guide means 25 for the incoming fluid is disposed at the other side thereof.
- each bushing 24 and ring 22 is diametrically split in a plane 26 incline at, say, 10° to the horizontal, the split being below the joint face 28 of the casing 10 at that side of the casing 10 where the periphery of the rotating shaft 12 moves upwardly.
- the two halves of each bushing 24 (and ring 22) are located together by dowels 30.
- Each bushing 24 (and ring 22) is prevented from rotating by a tangential pin 32 (see Figure 2) driven into a hole 34 machined in the upper half 36 of the casing 10 at its joint face 28, the centre-line 29 of the pin 32 being normal to the joint face 28 and the exposed end 37 of the pin 32 being flush with the joint face 28.
- the pin 32 engages in a recess 38 machined in a flange 40 on the upper half 42 of the bushing 24 (or ring 22) the recess 38 including a shoulder 44 against which the exposed end 37 of the pin 32 abuts.
- the flange 40 engages in known manner in an annular groove 45 machined in the casing 10.
- the exposed end 37 of the pin 32 may be slightly short of the joint face 28 of the casing 10 without departing from the scope of the invention, but it must not protrude beyond said face.
- the pin 32 is positioned at that side of the casing 10 which places said pin under compression if the bushing 24 (or ring 22) tends to rotate in the same direction as the shaft 12.
- the recess 38 is machined in a suitable part of the periphery of the bushing 24 (or ring 22) other than the axial location flange 40 thereon.
- the pin 32 can be much larger than the radial pin used hitherto and is in compression, not shear, so that it will readily withstand all anticipated loadings; there is a greater certainty of correct engagement of the pin 32 in the recess 38, and if engagement is not achieved further assembly of the pump is prevented; and, in cases where the bushing 24 (or ring 22) is diametrically split and the pin 32 is fitted in the upper half 36 of the casing 10, the lower half 48 of the bushing 24 or ring 22 can be rotated to enable it to be removed without lifting the shaft.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
Abstract
Description
- This invention relates to multi-stage centrifugal pumps, and more particularly to means for preventing rotation of an inter-stage bushing or ring in a multi-stage centrifugal pump with an axially split casing which houses a shaft carrying impellers.
- A multi-stage centrifugal pump has a number of inter-stage bushings and rings, sometimes called stage pieces and wear rings, which fit within the casing and have to be accurately positioned radially and locked against axial and rotational movement. These bushings and rings have essentially the same function as one another, namely to seal each side of each impeller, but the bushings have a larger radial thickness and may carry integral guide vanes for the incoming fluid whereas the rings have a smaller radial thickness and lack guide vanes. Radial positioning is by means of a close fit between the periphery of the bushing or ring and a bore machined in the casing. Axial location is by means of a flange on the bushing or ring which engages in an annular groove machined in the casing.
- Hitherto, each bushing or ring has been prevented from rotating by means of a small pin fitted into a radial hole drilled in the base of the annular groove, said pin protruding into an axial slot machined in the flange. The pins have been fitted in the lower half of the casing in the vertical plane containing the pump axis, so that the axial slots in the bushings and rings could be engaged with the pins during the assembly of the shaft and impellers into the lower half of the casing. This arrangement has the disadvantages that the pin is necessarily small and is liable to shear if large or cyclic loads are applied to it during operation of the pump; it can be difficult to ensure correct engagement of the pin in the axial slot during assembly; and, in cases where the bushing or ring has been diametrically split to permit its easy removal, the pin does not allow rotation of the lower half to enable it to be removed without lifting the shaft.
- The object of the present invention is to avoid the aforesaid disadvantages.
- According to the invention, means for preventing rotation of an inter-stage bushing or ring in a multi-stage centrifugal pump with an axially split casing which houses a shaft carrying impellers are characterised by a tangential pin fitted into a hole provided in either half of the casing at its join face, the centre-line of the pin being normal to the join face and the exposed end of the pin being flush with said face, and a recess in which the pin engages provided in the periphery of the bushing or ring.
- The invention will now be described, by way of example only, with reference to the accompanying drawings, of which :-
- Figure 1 is a sectional side elevation of a multi-stage centrifugal pump with a casing which is split axially in a horizontal plane;
- Figure 2 is a cross-section through the upper half of the casing on the line 2-2 in Figure 1;
- Figure 3 is an end view of a diametrically split inter-stage bushing;
- Figure 4 is a view of one half of the bushing in the direction of the
arrow 4 in Figure 3; - Figure 5 is an end view of an inter-stage ring which is not diametrically split; and
- Figure 6 is a side elevation of the ring shown in Figure 5.
- Referring now to Figures 1 to 4 of the drawings, in a preferred embodiment of the invention a multi-stage centrifugal pump has a casing indicated generally at 10 which is split axially in a horizontal plane and houses a power-driven
shaft 12 on which there are rigidly secured a plurality ofimpellers 14. Eachimpeller 14 is disposed in achamber 16 having anaxial inlet 18 and aradial outlet 20, thechambers 16 being connected in series in well-known manner. Aninter-stage ring 22 is disposed at the inlet side of eachimpeller 14, and an inter-stage bushing 24 carrying integral guide means 25 for the incoming fluid is disposed at the other side thereof. As exemplified in Figures 3 and 4, each bushing 24 andring 22 is diametrically split in aplane 26 incline at, say, 10° to the horizontal, the split being below thejoint face 28 of thecasing 10 at that side of thecasing 10 where the periphery of the rotatingshaft 12 moves upwardly. The two halves of each bushing 24 (and ring 22) are located together bydowels 30. Each bushing 24 (and ring 22) is prevented from rotating by a tangential pin 32 (see Figure 2) driven into ahole 34 machined in theupper half 36 of thecasing 10 at itsjoint face 28, the centre-line 29 of thepin 32 being normal to thejoint face 28 and the exposedend 37 of thepin 32 being flush with thejoint face 28. Thepin 32 engages in arecess 38 machined in aflange 40 on theupper half 42 of the bushing 24 (or ring 22) therecess 38 including ashoulder 44 against which the exposedend 37 of thepin 32 abuts. Theflange 40 engages in known manner in anannular groove 45 machined in thecasing 10. In practice, due to manufacturing tolerances, the exposedend 37 of thepin 32 may be slightly short of thejoint face 28 of thecasing 10 without departing from the scope of the invention, but it must not protrude beyond said face. Thepin 32 is positioned at that side of thecasing 10 which places said pin under compression if the bushing 24 (or ring 22) tends to rotate in the same direction as theshaft 12. - In a modification exemplified by the
ring 22 shown in Figures 5 and 6, thebushing 24 andrings 22 are not diametrically split, in which case thepins 32 can equally well be fitted in thelower half 46 of thecasing 10. - In another modification, the
recess 38 is machined in a suitable part of the periphery of the bushing 24 (or ring 22) other than theaxial location flange 40 thereon. - Arrangements in accordance with the invention have the advantages that the
pin 32 can be much larger than the radial pin used hitherto and is in compression, not shear, so that it will readily withstand all anticipated loadings; there is a greater certainty of correct engagement of thepin 32 in therecess 38, and if engagement is not achieved further assembly of the pump is prevented; and, in cases where the bushing 24 (or ring 22) is diametrically split and thepin 32 is fitted in theupper half 36 of thecasing 10, thelower half 48 of thebushing 24 orring 22 can be rotated to enable it to be removed without lifting the shaft. - The reader's attention is directed to all papers and documents which are filed concurrently with or previous to this specification in connection with this application and which are open to public inspection with this specification, and the contents of all such papers and documents are incorporated herein by reference.
- All of the features disclosed in this specification (including any accompanying claims, abstract and drawings), and/or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and/or steps are mutually exclusive.
- Each feature disclosed in this specification (including any accompanying claims, abstract and drawings), may be replaced by alternative features serving the same, equivalent or similar purpose, unless expressly stated otherwise. Thus, unless expressly stated otherwise, each feature disclosed is one example only of a generic series of equivalent or similar features.
- The invention is not restricted to the details of the foregoing embodiment(s). The invention extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims, abstract and drawings), or to any novel one, or any novel combination, of the steps of any method or process so disclosed.
Claims (4)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9015047 | 1990-07-07 | ||
GB909015047A GB9015047D0 (en) | 1990-07-07 | 1990-07-07 | Multi-stage centrifugal pumps |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0466350A2 true EP0466350A2 (en) | 1992-01-15 |
EP0466350A3 EP0466350A3 (en) | 1992-02-26 |
EP0466350B1 EP0466350B1 (en) | 1994-06-08 |
Family
ID=10678810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP91305692A Expired - Lifetime EP0466350B1 (en) | 1990-07-07 | 1991-06-24 | Multi-stage centrifugal pumps |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0466350B1 (en) |
AT (1) | ATE106994T1 (en) |
CA (1) | CA2046465C (en) |
DE (1) | DE69102357T2 (en) |
ES (1) | ES2057773T3 (en) |
GB (1) | GB9015047D0 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2410297A (en) * | 2004-01-21 | 2005-07-27 | Weir Pumps Ltd | Split casing for a multi-stage pump |
DE102008033073B3 (en) * | 2008-07-15 | 2009-12-03 | Ruhrpumpen Gmbh | Centrifugal pump, has flow channel provided between inlet and outlet, and positioning unit attached at separating wall in selectable angle distance from guiding device and accommodated in region of mold parting line |
CN103291462A (en) * | 2013-01-05 | 2013-09-11 | 中国航空工业集团公司西安飞机设计研究所 | Oil drainage method of split type fuel pump |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB100858A (en) * | 1916-03-29 | 1916-07-20 | G & J Weir Ltd | Improvements in Centrifugal or the like Pumps. |
US1639279A (en) * | 1923-05-16 | 1927-08-16 | Frederick Iron And Steel Compa | Wearing ring for rotary elements |
US1743348A (en) * | 1928-05-07 | 1930-01-14 | Byron Jackson Pump Co | Centrifugal-pump assembly |
FR850685A (en) * | 1938-05-21 | 1939-12-22 | G & J Weir | Improvements to rotary pumps |
DE2158518B2 (en) * | 1970-12-21 | 1980-03-27 | Borg-Warner Corp., Chicago, Ill. (V.St.A.) | Horizontal multistage centrifugal pump |
-
1990
- 1990-07-07 GB GB909015047A patent/GB9015047D0/en active Pending
-
1991
- 1991-06-24 ES ES91305692T patent/ES2057773T3/en not_active Expired - Lifetime
- 1991-06-24 EP EP91305692A patent/EP0466350B1/en not_active Expired - Lifetime
- 1991-06-24 AT AT91305692T patent/ATE106994T1/en not_active IP Right Cessation
- 1991-06-24 DE DE69102357T patent/DE69102357T2/en not_active Expired - Lifetime
- 1991-07-08 CA CA002046465A patent/CA2046465C/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB100858A (en) * | 1916-03-29 | 1916-07-20 | G & J Weir Ltd | Improvements in Centrifugal or the like Pumps. |
US1639279A (en) * | 1923-05-16 | 1927-08-16 | Frederick Iron And Steel Compa | Wearing ring for rotary elements |
US1743348A (en) * | 1928-05-07 | 1930-01-14 | Byron Jackson Pump Co | Centrifugal-pump assembly |
FR850685A (en) * | 1938-05-21 | 1939-12-22 | G & J Weir | Improvements to rotary pumps |
DE2158518B2 (en) * | 1970-12-21 | 1980-03-27 | Borg-Warner Corp., Chicago, Ill. (V.St.A.) | Horizontal multistage centrifugal pump |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2410297A (en) * | 2004-01-21 | 2005-07-27 | Weir Pumps Ltd | Split casing for a multi-stage pump |
GB2410297B (en) * | 2004-01-21 | 2007-08-29 | Weir Pumps Ltd | Pump casing |
DE102008033073B3 (en) * | 2008-07-15 | 2009-12-03 | Ruhrpumpen Gmbh | Centrifugal pump, has flow channel provided between inlet and outlet, and positioning unit attached at separating wall in selectable angle distance from guiding device and accommodated in region of mold parting line |
CN103291462A (en) * | 2013-01-05 | 2013-09-11 | 中国航空工业集团公司西安飞机设计研究所 | Oil drainage method of split type fuel pump |
CN103291462B (en) * | 2013-01-05 | 2015-08-05 | 中国航空工业集团公司西安飞机设计研究所 | A kind of split type fuel pump method of discharge |
Also Published As
Publication number | Publication date |
---|---|
DE69102357D1 (en) | 1994-07-14 |
EP0466350B1 (en) | 1994-06-08 |
CA2046465C (en) | 1998-09-22 |
DE69102357T2 (en) | 1995-01-19 |
CA2046465A1 (en) | 1992-01-08 |
ES2057773T3 (en) | 1994-10-16 |
ATE106994T1 (en) | 1994-06-15 |
EP0466350A3 (en) | 1992-02-26 |
GB9015047D0 (en) | 1990-08-29 |
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