WO2017155972A2 - Center bushing to balance axial forces in multi-stage pumps - Google Patents
Center bushing to balance axial forces in multi-stage pumps Download PDFInfo
- Publication number
- WO2017155972A2 WO2017155972A2 PCT/US2017/021123 US2017021123W WO2017155972A2 WO 2017155972 A2 WO2017155972 A2 WO 2017155972A2 US 2017021123 W US2017021123 W US 2017021123W WO 2017155972 A2 WO2017155972 A2 WO 2017155972A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- pockets
- center bushing
- stage
- wall
- stage pump
- Prior art date
Links
Classifications
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- 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
-
- 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
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/16—Centrifugal pumps for displacing without appreciable compression
- F04D17/164—Multi-stage fans, e.g. for vacuum cleaners
-
- 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
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/041—Axial thrust balancing
-
- 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
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/041—Axial thrust balancing
- F04D29/0413—Axial thrust balancing hydrostatic; hydrodynamic thrust bearings
-
- 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
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/051—Axial thrust balancing
Definitions
- the present invention relates to a multi-stage pump; and more particularly relates to a center bushing for a multi-stage pump.
- a normal center bushing acts as a controlled leakage point between the different stages of the pump, as well as acts to minimize generated axial thrust.
- the center bushing acts as a divide between the different stages and only allows minimal balancing though the small leakage point between the rotating and stationary element.
- the higher pressures must be able to flow to an area of lower pressure, e.g., via balance holes, pump out vanes, or other similar thrust reducing designs which may allow this pressure to be reduced.
- the introduction of these passages increases the leakage between the stages which may negatively affect the efficiency. If these forces are not reduced, it may lead to increasing the size of the bearing system. A larger bearing/frame system may cost more and these larger bearings may use more power, therefore reducing the overall efficiency.
- the present invention provides a new and unique center bushing that still has a small controlled leakage between the stationary and rotating elements.
- the present invention will increase the axial forces in the higher pressure section of the pump, by introducing pockets to the center bushing.
- the velocity that is on the backside of the high pressure stage is reduced, which will increase the pressure locally on the backside of the respective stage. Since the pressure in this section is now being increased, a new way of balancing is introduced.
- the pressure on the high pressure side is increased due to a decreased velocity, this helps to create an axial force balance between the different stages.
- the results are a force with a magnitude and a direction.
- the present invention will be directionally
- the present invention will allow for a placement so it can always be located on the desired side to help increase the local pressure which will help to balance the axial forces.
- the center bushing or device will only need to be pinned in one locating to prevent rotation, and with running tight tolerances between the center bushing or device and the pump's casing these tight clearances allow for the removal of O-ring features or devices that aid in the prevention of leakage.
- no diameter difference is introduced that may create another location for axial forces to act upon. Also by removing the extra balance holes drilled through the center bushing, which helps offset the axial forces, there is less of a leakage path.
- the original and alternate center bushing configurations disclosed herein are designed to reduce velocity behind the stage of higher pressure which will proportionally increase the pressure behind the respective stage. This pressure increase may help to offset the larger axial forces generated from the pressure rise across the stage which will help to balance resultant axial forces.
- the present invention may take the form of a multi-stage pump, featuring:
- a pump having different stages configured to pump a fluid from a pump suction and to a pump discharge;
- center bushing configured between the different stages, having a center bushing side configured with pockets to balance axial forces between the different stages of the multistage pump.
- the multi-stage pump according to the present invention may include one or more of the following features:
- the pockets may include, or take the form of, radially-formed rib pockets.
- the center bushing side may include a center bushing surface having an inner wall, an outer wall and a plurality of radial walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent radial walls connecting the inner wall portion and the corresponding outer wall portion.
- the inner wall may include, or form part of, an inner circular wall extending around the inner edge of the center bushing.
- the outer wall may include, or form part of, an outer circular wall extending around the outer edge of the center bushing.
- the pockets may include, or take the form of, curved rib pockets.
- the center bushing surface may include an inner wall, an outer wall and a plurality of curved rib walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent curved rib walls connecting the inner wall portion and the corresponding outer wall portion.
- the pockets may include, or take the form of, extruded circle or circular pockets, e.g., which are formed as raised cylindrical protrusions having an outer cylindrical wall and a top surface.
- the pockets may include, or take the form of, full length rib pockets.
- the center bushing surface may include an inner wall, an outer wall and a plurality of full length rib walls all extending from the center bushing surface, each radially-formed rib pocket having by a combination of an inner wall portion, a corresponding outer wall portion and adjacent full length rib walls connecting the inner wall portion and the corresponding outer wall portion.
- the different stages may have an area/location of higher pressure and a corresponding area/location of lower pressure; and the pockets may be configured to increase the axial forces in the area/location of higher pressure.
- a center bushing side may include a high pressure side configured with the pockets facing the area/location of higher pressure.
- the multi-stage pump may include a stationary element configured with an aperture; and the center bushing may include an outer circumferential rim configured with a pin to couple into the aperture of the stationary element to prevent rotation of the center bushing.
- the stationary element may be configured with a circumferential surface having an inner diameter; and the outer circumferential rim may include an outer diameter that substantially corresponds in dimension to the inner diameter of the circumferential surface of the stationary element in order to substantially reduce or prevent leakage between the different stages.
- the different stages may include:
- first stage configured with an area/location of lower pressure
- second stage configured with a corresponding area/location of high pressure
- the present invention may take the form of a multi-stage device featuring a device having different stages configured to provide a fluid; and a center bushing configured between the different stages, having a center bushing side configured with pockets to balance axial forces between the different stages of the multistage device.
- the multi-stage device may include, or take the form of, a multi-stage pump, fan, blower or compressor.
- the pockets may include, or be configured as, radially-formed rib pockets, or curved rib pockets, or extruded circle or circular pockets, or full length rib pockets.
- advantages of the present invention may include the following:
- the new and unique center bushing helps to balance the uneven axial forces generated within the multi-stage pump, by allowing the higher pressures to flow to a location of lower pressure. Therefore, the axial thrust may be reduced and brought down to a level that can be handled by the bearing system.
- Figure 1 shows a diagram of a multistage pump, which is known in the art.
- Figure 2 shows a diagram of a multi-stage pump having a center bushing, according to some embodiments of the present invention.
- Figure 3 includes Figs. 3A and 3B, which shows different perspective views of a center bushing having radially-formed rib pockets, according to some
- Figure 4A shows a diagram of a center bushing having curved rib pockets, according to some embodiments of the present invention.
- Figure 4B shows a diagram of a center bushing having extruded circular rib pockets, according to some embodiments of the present invention.
- Figure 4C shows a diagram of a center bushing having full length rib pockets, according to some embodiments of the present invention.
- the present invention may take the form of a multi-stage pump generally indicated as 10, featuring:
- a pump having different stages, e.g., like stage pump 1 and stage pump 2, configured to pump a fluid from a pump suction PS and to a pump discharge PD; and
- a center bushing CB configured between the different stages, having a center bushing side labeled as CBS1 , CBS2, CBS3, CBS4 (see Figs. 3 and 4A, 4B, 4C) configured with pockets labeled as PKT, CRP, ECP, FLRP (see Figs. 3 and 4A, 4B, 4C) to balance axial forces between the different stages (e.g., stage 1 and stage 2) of the multistage pump 10.
- the different stages may have an area/location of higher pressure as shown and indicated in Figure 2 and a corresponding area/location of lower pressure as shown and indicated in Figure 2; and the pockets (see Figs. 3 and 4A, 4B, 4C) may be configured to increase the axial forces in the area/location of higher pressure.
- the center bushing side CBS1 may include a high pressure side configured with the pockets (e.g., such as PKT (Fig. 3), CRP (Fig. 4A), ECP (Fig. 4B),
- a high pressure side configured with the pockets (e.g., such as PKT (Fig. 3), CRP (Fig. 4A), ECP (Fig. 4B),
- the different stages may include:
- stage 1 configured with an area/location of lower pressure
- stage 2 configured with a corresponding area/location of high pressure
- the center bushing side CBS1 that includes a high pressure side configured with the pockets (e.g., such as PKT (Fig. 3), CRP (Fig. 4A), ECP (Fig. 4B), FLRP(Fig. 4C)) facing the corresponding area/location of higher pressure.
- pockets e.g., such as PKT (Fig. 3), CRP (Fig. 4A), ECP (Fig. 4B), FLRP(Fig. 4C) facing the corresponding area/location of higher pressure.
- FIG. 3 Radially-formed rib pockets (PKT)
- the pockets may be configured as radially-formed rib pockets.
- Figures 3A, 3B show the center bushing side CBS1 of the center bushing CB1 , which may include a center bushing surface cbs' having an inner wall IW, an outer wall OW and a plurality of radial walls RW, all extending outwardly from the center bushing surface cbs', as shown.
- each radially-formed rib pocket PKT may be formed by a combination of an inner wall portion/section of the inner wall IW, a corresponding outer wall portion/section of the outer wall OW, and adjacent radial walls RW1 , RW2 connecting the inner wall portion and the corresponding outer wall portion.
- the inner wall IW may include, or form part of, an inner circular wall extending around the inner edge of the center bushing, e.g., consistent with that shown in Figures 3A and 3B.
- the outer wall OW may include, or form part of, an outer circular wall extending around the outer edge of the center bushing, e.g., consistent with that shown in Figures 3A and 3B.
- the center bushing CB1 is shown configured with twelve (12) radially-formed rib pockets PKTs.
- the scope of the invention is not intended to be limited to any particular number of radially-formed rib pockets.
- the scope of the invention is intended to include, and embodiments are envisioned using, a center bushing having more or less than twelve (12) radially-formed rib pockets, e.g., including thirteen (13) radially-formed rib pockets, or fourteen (14) radially-formed rib pockets, etc.; or alternatively eleven (1 1 ) radially-formed rib pockets, or ten (10) radially-formed rib pockets, etc.
- Figure 4A shows a center bushing CB2 having the pockets configured as curved rib pockets CRP.
- the center bushing surface may include the inner wall, the outer wall and a plurality of curved walls all extending from the center bushing surface.
- Each curved rib pocket may include a combination of the inner wall portion, the corresponding outer wall portion and adjacent curved walls connecting the inner wall portion and the corresponding outer wall portion.
- the center bushing CB2 is shown configured with twelve (12) curved rib pockets.
- the scope of the invention is not intended to be limited to any particular number of curved rib pockets.
- the scope of the invention is intended to include, and embodiments are envisioned using, a center bushing having more or less than twelve (12) curved rib pockets, e.g., including thirteen (13) curved rib pockets, or fourteen (14) curved rib pockets, etc. ; or alternatively eleven (1 1 ) curved rib pockets, or ten (10) curved rib pockets, etc.
- Figure 4B Extruded circle or circular pockets ECPs
- Figure 4B shows a center bushing CB3 having the pockets configured as extruded pockets in the form of extruded circular pockets ECPs.
- the center bushing CB3 is shown configured with thirty six (36) extruded circle or circular pockets, e.g., arranged in a pattern of twelve (12) pairs of extruded circle or circular pockets ECPs, each arranged equi-distant about the center bushing surface and separated by a respective single extruded circle or circular pocket arranged inbetween.
- the scope of the invention is not intended to be limited to any particular number of extruded circle or circular pockets.
- the scope of the invention is intended to include, and embodiments are envisioned using, a center bushing having more or less than twelve (36) extruded circle or circular pockets, e.g., including thirty seven (37) extruded circle or circular pockets, or thirty eight (38) extruded circle or circular pockets, etc.; or thirty five (35) extruded circle or circular pockets, or thirty four (34) extruded circle or circular pockets, etc.
- the scope of the invention is not intended to be limited to any particular pattern of extruded circle or circular pockets.
- a center bushing having other types or kinds of patterns, e.g., like a pattern of eighteen (18) pairs of extruded circle or circular pockets, each arranged equi-distant about the center bushing surface, or like a pattern of twelve (12) triplets of extruded circle or circular pockets, each arranged equi-distant about the center bushing surface, etc.
- the extruded pockets ECPs are shown as cylindrical protrusions; however, the scope of the invention is not intended to be limited to any particular geometric shape of the extruded pockets.
- the scope of the invention is intended to include, and embodiments are envisioned in which, the extruded pockets take the form of other geometric shapes such as extruded 3-sided or triangular pockets, extruded 4-sided or rectangular pockets, extruded 5-sided or pentagonal pockets, etc., as well as other extruded 1 -side pockets like oval pockets.
- Figure 4C Full length rib pockets FLRPs
- Figure 4C shows a center bushing CB4 having the pockets configured as full length rib pockets FLRPs.
- the center bushing CB4 is shown configured with six (6) full length rib pockets FLRPs.
- the scope of the invention is not intended to be limited to any particular number of full length rib pockets.
- the scope of the invention is intended to include, and embodiments are envisioned using, a center bushing having more or less than six (6) full length rib pockets, e.g., including seven (7) full length rib pockets, or eight (8) full length rib pockets, etc.; or alternatively five (5) full length rib pockets, or four (4) full length rib pockets, etc.
- the multi-stage pump 10 may include a stationary element, e.g., some part of the pump's casing C, configured with an aperture; and the center bushing CB may include an outer circumferential rim or wall OW (Fig. 2) configured with a pin P to couple into the aperture of the stationary element to prevent rotation of the center bushing CB.
- a stationary element e.g., some part of the pump's casing C, configured with an aperture
- the center bushing CB may include an outer circumferential rim or wall OW (Fig. 2) configured with a pin P to couple into the aperture of the stationary element to prevent rotation of the center bushing CB.
- the stationary element or part of the pump's casing C may be configured with a circumferential surface having an inner diameter; and the outer circumferential rim may include an outer diameter that substantially corresponds in dimension to the inner diameter of the circumferential surface of the stationary element in order to substantially reduce or prevent leakage between the different stages.
- the scope of the invention is not intended to be limited by any particular dimensions of the pockets PKT (Fig. 3), CRP (Fig. 4A), ECP (Fig. 4B)or FLRP (Fig. 4C), e.g., including the length, width, diameter, and/or depth of the same, which will depend on the particular application, as would be appreciate by one skilled in the art.
- the pockets PKT, CRP, ECP or FLRP may be configured with one combination of a given length, width, diameter, and/or depth; while for another type of multi-stage pump
- the pockets PKT, CRP, ECP or FLRP may be configured with another combination of a given length, width, diameter, and/or depth of the same.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES17763886T ES2892902T3 (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multistage pumps |
CN201780016119.XA CN108779777B (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in a multi-stage pump |
EP17763886.3A EP3426925B1 (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multi-stage pumps |
MX2018010839A MX2018010839A (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multi-stage pumps. |
CA3016603A CA3016603C (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multi-stage pumps |
AU2017229346A AU2017229346B2 (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multi-stage pumps |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662305305P | 2016-03-08 | 2016-03-08 | |
US62/305,305 | 2016-03-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2017155972A2 true WO2017155972A2 (en) | 2017-09-14 |
WO2017155972A3 WO2017155972A3 (en) | 2017-10-19 |
Family
ID=59789783
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2017/021123 WO2017155972A2 (en) | 2016-03-08 | 2017-03-07 | Center bushing to balance axial forces in multi-stage pumps |
Country Status (9)
Country | Link |
---|---|
US (1) | US10746189B2 (en) |
EP (1) | EP3426925B1 (en) |
CN (1) | CN108779777B (en) |
AU (1) | AU2017229346B2 (en) |
CA (1) | CA3016603C (en) |
ES (1) | ES2892902T3 (en) |
MX (1) | MX2018010839A (en) |
TW (1) | TWI720146B (en) |
WO (1) | WO2017155972A2 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10663025B2 (en) * | 2018-07-31 | 2020-05-26 | Bendix Spicer Foundation Brake Llc | Bushing assembly for a spring brake actuator of a vehicle air braking system |
USD1028017S1 (en) * | 2019-11-27 | 2024-05-21 | Sulzer Management Ag | Multistage pump |
CN113007126A (en) * | 2021-02-26 | 2021-06-22 | 英飞同仁风机股份有限公司 | Multi-stage centrifugal blower partition plate, preparation method thereof and multi-stage centrifugal blower |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5232342A (en) | 1990-07-07 | 1993-08-03 | David Brown Engineering Limited | High pressure multi-stage centrifugal pumps |
US20060204359A1 (en) | 2005-03-11 | 2006-09-14 | Baker Hughes Incorporated | Abrasion resistant pump thrust bearing |
US20150071799A1 (en) | 2013-09-10 | 2015-03-12 | Baker Hughes Incorporated | Self-Aligning and Vibration Damping Bearings in a Submersible Well Pump |
Family Cites Families (60)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB430949A (en) * | 1934-08-29 | 1935-06-27 | Worthington Pump & Mach Corp | Improvements in and relating to centrifugal pumps |
US2286522A (en) * | 1940-04-13 | 1942-06-16 | Worthington Pump & Mach Corp | Centrifugal compressor |
US2395793A (en) * | 1943-03-04 | 1946-02-26 | Stratford Dev Corp | Centrifugal pump |
US2361521A (en) * | 1943-11-01 | 1944-10-31 | W S Darley & Company | Centrifugal pump |
US2391811A (en) * | 1943-11-06 | 1945-12-25 | Waterous Co | Multistage centrifugal pump |
US2750893A (en) * | 1949-09-19 | 1956-06-19 | Waterous Co | Fire pump |
US2706452A (en) | 1952-02-01 | 1955-04-19 | Plessey Co Ltd | Gear pump |
US2820088A (en) | 1955-08-25 | 1958-01-14 | Sperry Rubber And Plastics Com | Rubber bushing |
US3017837A (en) | 1959-02-17 | 1962-01-23 | Thomas E Judd | Multi stage centrifugal pump |
US3149819A (en) | 1961-02-14 | 1964-09-22 | Bbc Brown Boveri & Cie | Device for protecting a bearing against heat |
US3289542A (en) | 1963-10-29 | 1966-12-06 | Lawrence Machine & Mfg Company | Hydraulic motor or pump |
US3643290A (en) | 1969-12-01 | 1972-02-22 | John D Milne | Bushing and bushing assembly |
US3764236A (en) * | 1971-07-15 | 1973-10-09 | Carter Co J C | Modular pump |
AU505880B2 (en) * | 1975-02-28 | 1979-12-06 | Vsesjuzny Niipkidugsv | Split casing pump |
IT1133295B (en) | 1980-05-08 | 1986-07-09 | Weber Spa | ELECTRICALLY OPERATED FUEL PUMP, SUITABLE FOR USE IN INJECTION SYSTEMS FOR INTERNAL COMBUSTION ENGINES WITH COMMAND IGNITION |
CH655357A5 (en) * | 1981-09-28 | 1986-04-15 | Sulzer Ag | Method and device for reducing the axial thrust in turbo machines |
FR2691513B1 (en) | 1992-05-20 | 1995-11-10 | Peugeot | DEVICE FOR FIXING AN ELEMENT ON A STRUCTURE, WITH AUTOMATIC GAME RECOVERY. |
US5320482A (en) * | 1992-09-21 | 1994-06-14 | The United States Of America As Represented By The Secretary Of The Navy | Method and apparatus for reducing axial thrust in centrifugal pumps |
DE4234739C1 (en) * | 1992-10-15 | 1993-11-25 | Gutehoffnungshuette Man | Gearbox multi-shaft turbo compressor with feedback stages |
US5366359A (en) | 1993-08-20 | 1994-11-22 | General Motors Corporation | Scroll compressor orbital scroll drive and anti-rotation assembly |
EP1170184B1 (en) | 1995-02-03 | 2012-12-05 | Nvb International A/S | Valve connector |
JP3566781B2 (en) * | 1995-04-26 | 2004-09-15 | 株式会社 日立インダストリイズ | Vertical shaft submersible pump device for liquefied gas tank |
US5765950A (en) * | 1996-11-29 | 1998-06-16 | Goulds Pumps, Incorporated | Thrust bearing assembly |
US6061870A (en) | 1998-01-07 | 2000-05-16 | The Burton Corporation | Bushing system |
NL1008522C2 (en) | 1998-03-06 | 1999-09-07 | Beele Eng Bv | Transit device. |
US6068444A (en) * | 1998-08-17 | 2000-05-30 | Camco International, Inc. | Submergible centrifugal pump having improved diffuser bushings |
KR20020024933A (en) * | 2000-09-27 | 2002-04-03 | 구자홍 | Turbine compressor structure with Impeller |
DE10314979B3 (en) | 2003-04-02 | 2004-12-02 | Robert Bosch Gmbh | piston pump |
GB0401188D0 (en) * | 2004-01-21 | 2004-02-25 | Weir Pumps Ltd | Pump casing |
US7704009B2 (en) | 2005-03-25 | 2010-04-27 | Boote Carey J | Axial spacer for a rotational assembly |
US7354240B2 (en) | 2005-12-16 | 2008-04-08 | Korea Aerospace Research Institute | Centrifugal turbo machine with axial thrust control member |
US7670110B2 (en) * | 2006-07-13 | 2010-03-02 | United Technologies Corporation | Sideload vanes for fluid pump |
US20100021263A1 (en) | 2006-12-05 | 2010-01-28 | Illinois Tool Works Inc. | Bushing assembly |
US7731476B2 (en) * | 2007-01-30 | 2010-06-08 | Technology Commercialization Corp. | Method and device for reducing axial thrust and radial oscillations and rotary machines using same |
US20090004032A1 (en) * | 2007-03-29 | 2009-01-01 | Ebara International Corporation | Deswirl mechanisms and roller bearings in an axial thrust equalization mechanism for liquid cryogenic turbomachinery |
US20090062020A1 (en) | 2007-08-30 | 2009-03-05 | Edwards Stanley W | Multi-ribbed keyless coupling |
DE102009005386A1 (en) | 2009-01-21 | 2010-07-22 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Charging device for an internal combustion engine |
CN201401336Y (en) * | 2009-05-13 | 2010-02-10 | 丹东克隆集团有限责任公司 | Axial-thrust balancing centrifugal pump |
US20110072612A1 (en) | 2009-05-15 | 2011-03-31 | Boote Carey J | Axial spacer for a rotational assembly |
US8282340B2 (en) * | 2009-06-29 | 2012-10-09 | Korea Aerospace Research Institute | Turbo-machine having bellows unit for automatic axial thrust control |
DE102009029069A1 (en) | 2009-09-01 | 2011-03-03 | Robert Bosch Gmbh | Two-stage centrifugal pump |
FR2960923B1 (en) * | 2010-06-08 | 2013-12-20 | Snecma | AXIAL PUSH CONTROL BY GUIDING AIR FROM A CENTRIFUGAL COMPRESSOR |
CN101865138A (en) * | 2010-07-06 | 2010-10-20 | 浙江工业大学 | A New Type of Multistage Centrifugal Pump |
CN202273872U (en) * | 2011-10-23 | 2012-06-13 | 浙江丰球泵业股份有限公司 | Top outlet type barrel multilevel fire water pump |
CN103362949A (en) * | 2012-04-02 | 2013-10-23 | 珠海格力电器股份有限公司 | Dynamic pressure bearing, high-speed fluid power machine and high-speed centrifugal compressor |
CN103362854B (en) * | 2012-04-02 | 2016-06-08 | 珠海格力电器股份有限公司 | Centrifugal compressor |
CN202545341U (en) * | 2012-04-18 | 2012-11-21 | 浙江同泰泵业有限公司 | Axial force balancing structure of horizontal multi-stage pump |
RU2014148095A (en) | 2012-05-16 | 2016-06-27 | Боргварнер Инк. | OIL SEAL FOR OIL BREAKER RING AND TURBOCHARGER CONTAINING SUCH OIL SEAL |
PT2867538T (en) * | 2012-06-27 | 2019-04-01 | Flowserve Man Co | Anti-swirl device |
US9963998B2 (en) | 2013-06-18 | 2018-05-08 | Honeywell International Inc. | Assembly with bearings and spacer |
CN203412802U (en) * | 2013-06-27 | 2014-01-29 | 上海创科泵业制造有限公司 | Graphite bearing capable of reducing axial load |
US9334865B2 (en) | 2013-09-10 | 2016-05-10 | Baker Hughes Incorporated | Self-aligning and vibration damping bearings in a submersible well pump |
CA2874009C (en) | 2013-12-10 | 2016-11-29 | Baker Hughes Incorporated | Spherical sleeve and bushing bearing for centrifugal pump stage |
WO2015094249A1 (en) * | 2013-12-18 | 2015-06-25 | Ge Oil & Gas Esp, Inc. | Multistage centrifugal pump with integral abrasion-resistant axial thrust bearings |
CN203685655U (en) * | 2013-12-19 | 2014-07-02 | 大连深蓝泵业有限公司 | Rotating shaft support device of multistage centrifugal pump |
WO2015111169A1 (en) * | 2014-01-23 | 2015-07-30 | 三菱重工コンプレッサ株式会社 | Centrifugal compressor |
US9651091B2 (en) * | 2014-04-01 | 2017-05-16 | Hamilton Sundstrand Corporation | Thrust plate assembly |
US9784283B2 (en) * | 2014-06-06 | 2017-10-10 | Baker Hughes Incorporated | Diffuser vanes with pockets for submersible well pump |
CN204239309U (en) * | 2014-11-27 | 2015-04-01 | 台州凌霄泵业有限公司 | Double suction type centrifugal pump |
JP2017078356A (en) * | 2015-10-20 | 2017-04-27 | 株式会社豊田自動織機 | Centrifugal compressor |
-
2017
- 2017-03-07 AU AU2017229346A patent/AU2017229346B2/en active Active
- 2017-03-07 US US15/452,068 patent/US10746189B2/en active Active
- 2017-03-07 CA CA3016603A patent/CA3016603C/en active Active
- 2017-03-07 CN CN201780016119.XA patent/CN108779777B/en active Active
- 2017-03-07 MX MX2018010839A patent/MX2018010839A/en unknown
- 2017-03-07 ES ES17763886T patent/ES2892902T3/en active Active
- 2017-03-07 WO PCT/US2017/021123 patent/WO2017155972A2/en active Application Filing
- 2017-03-07 EP EP17763886.3A patent/EP3426925B1/en active Active
- 2017-03-08 TW TW106107517A patent/TWI720146B/en not_active IP Right Cessation
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5232342A (en) | 1990-07-07 | 1993-08-03 | David Brown Engineering Limited | High pressure multi-stage centrifugal pumps |
US20060204359A1 (en) | 2005-03-11 | 2006-09-14 | Baker Hughes Incorporated | Abrasion resistant pump thrust bearing |
US20150071799A1 (en) | 2013-09-10 | 2015-03-12 | Baker Hughes Incorporated | Self-Aligning and Vibration Damping Bearings in a Submersible Well Pump |
Also Published As
Publication number | Publication date |
---|---|
ES2892902T3 (en) | 2022-02-07 |
CA3016603A1 (en) | 2017-09-14 |
WO2017155972A3 (en) | 2017-10-19 |
EP3426925A2 (en) | 2019-01-16 |
CA3016603C (en) | 2022-05-17 |
TWI720146B (en) | 2021-03-01 |
MX2018010839A (en) | 2019-02-07 |
EP3426925B1 (en) | 2021-09-08 |
US10746189B2 (en) | 2020-08-18 |
CN108779777A (en) | 2018-11-09 |
CN108779777B (en) | 2020-12-08 |
AU2017229346B2 (en) | 2020-05-21 |
EP3426925A4 (en) | 2019-05-15 |
US20170298948A1 (en) | 2017-10-19 |
AU2017229346A1 (en) | 2018-09-27 |
TW201740032A (en) | 2017-11-16 |
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