US3103892A - Pump or the like - Google Patents
Pump or the like Download PDFInfo
- Publication number
- US3103892A US3103892A US70476A US7047660A US3103892A US 3103892 A US3103892 A US 3103892A US 70476 A US70476 A US 70476A US 7047660 A US7047660 A US 7047660A US 3103892 A US3103892 A US 3103892A
- Authority
- US
- United States
- Prior art keywords
- elements
- diaphragms
- pumps
- diffuser
- vanes
- 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
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
- F04D1/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D1/06—Multi-stage pumps
- F04D1/063—Multi-stage pumps of the vertically split casing type
-
- 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
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
- F04D17/125—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors the casing being vertically split
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49229—Prime mover or fluid pump making
- Y10T29/49236—Fluid pump or compressor making
- Y10T29/49243—Centrifugal type
Definitions
- FIGURE 1 is an axial section showing the pertinent parts of a pump constructed in accordance with the invention
- FlGURE 2 is an elevation of a diffuser element located between the discharge of one impeller and the entrance to a subsequent one;
- FIGURE 3 is an elevation side of FIGURE 2;
- FIGURES 4 and 5 are diagrams illustrating the assemblies of interstage diaphragms provided in accordance with the invention.
- FIGURE 6 is a diagram illustrating the form taken by a standard casting from which interstage diaphragms may be readily produced by machining.
- the pump shown is of the barrel type, and except for the parts specially provided in accordance with the invention has a generally conventional structure and operates in conventional fashion.
- An outer housing 2 is provided having a generally cylindrical form and designed to withstand the pressures involved.
- This housing is provided with an inlet passage at 4 and a discharge passage at 6.
- the housing is provided at its left-hand end with a shoulder 7 against which the casing assembly abuts under the high discharge pressure.
- the housing is provided with looking at the right-hand a conventional closure '8, Whlh houses conventional packing and bearing arrangements which are not illustrated.
- the bearing assembly generally indicated at 10.
- the invention is concerned primarily with the barrel assembly within the huosing and details of the housing and otherstructures are not involved and are therefore not shown in detail. It need only be remarked that for'pumps of different lengths (i.e. different numbers of stages) different housing 2 will be provided, though the associated end closures, bearings, etc., may be standard for different size pumps. 7
- the casing which is located within the housing ismade up of stacked elements "comprising the end element 12, the duplicate interstage diaphragms 14, and the outlet element 16. Concentric stacked arrangement of these elements in maintained by interlocking 'rabbets as will be evident from FIGURE 1. Nested'in the interstage diaphragms 1d are diffuser elements 18 secured bybolts 19. A shaft 20 has mounted thereon in conventional fashion the various impellers 22 of the stages involved, these being provided with the usual vanes. For pumps of different capacities these impellers will, in general, be different in the sense of having wider or narrower passages between the vanes; but in any individual multistage pump the impellers will generally be identical in usual pumps.
- the invention provides simplification in the :matter of minimizing the variety of elements to be used by special forms and assemblies particularly of the interstage diaphragms and the diffuser assemblies or elements.
- This diffuser element .18 comprises a cast disc which is of small axial extent except at its peripheral portions. It comprises diffuser vanes on the side facing the discharge of one impeller, cross-over passages for the liquid being pumped, and return passages and guide vanes on its opposite side arranged to direct the flow to the inlet of the next subsequent stage impeller.
- the relatively thin central portion of this element is indicated at 21. Adjacent the periphery there are provided the diffuser vanes 23 which spiral outwardly from their inlet edges 25. On the opposite side of the disc there are the return vanes 27 which spiral inwardly from their inlet edges at 26 to their outlet edges at .23. As will be evident from FIGURE 3, in particular, cross-over passages 30 exist at the periphery of the element 18 to carry the liquid from one side to the other of the central portion 21. Closer to the shaft there are provided the redirecting vanes 36 to turn the inwardly spiraling flow substantially radially for entrance into the eye of the next stage impeller without substantial spin.
- FIGURES 4 and 5 showing the assembly arrangement of interstage diaphragms, two adjacent ones of which are illustrated.
- these diaphragms are arranged to provide a minimum of axial space for the diffuser elements, the space 40 having the typical dimension A (The space, as indicated, may involve both radial and conical wall portions; but the dimension ,A may be regarded as typical).
- a typical wall thickness dimension is indicated at B From the fact that these typical dimensions are taken between radial wall portions, it will be evident that the interstage dimension,i.e.
- the space of similar parts of the impellers and the other repetitive elements will be A +B
- the space 40 is here indicated as the maximum space that may be desired in the case of a larger capacity impeller with a correspondingly axially wider diffuser element.
- the space dimension A is now greater.
- the wall dimension B, for the interstage diaphragms is now such that A +B is equal to Ari-B The interstage spacing is thus constant.
- FIGURE 6 the outside outline of this indicates the shape of a casting 14A from which both the extreme size diaphragms 14 and 14' may be produced by simple turning.
- a diaphragm such as 14 of maximum wall thickness
- the shaded portion 42 may be removed.
- the diaphragm of minimum wall thickness the shaded portion 44 may be removed.
- machining may produce any diaphragm of intermediate wall thickness by partial removals of material at both the right and left. (The original casting may, of course, be provided with excess material such as indicated at 46 to provide for proper finish machining.)
- the amply sized casting 14A and a casting for the diffuser element having an ample dimension between the faces 32 and 34 will sufiice for the construction and assemblage of pumps having different size impellers and/or different numbers of stages.
- the diffuser elements will rest Within and may be secured in the cups formed within the interstage diaphragms, securing being achieved by bolts as indicated at 19.
- the stacking of the interstage diaphragms will then result in the establishment of standard spacing for the various repetitive elements, including the impellers, along the shaft. The result is a completely satisfactory construction from the standpoint of operation with greatly simplified aspects of production of parts and their stock piling to meet the demands of various orders for pumps.
- discs similar to the diffuser elements of the pumps will carry vanes on one or both sides to define diffusers (which may, of course, be vaneless) and nozzles as well as redirecting vanes, all to provide gas or liquid passages functioning conventionally but structurally having the advantages of the invention.
- a multistage pump or the like comprising a rotary shaft, axially spaced vaned rotors carried by the shaft, a housing for said shaft and rotors, said housing comprising coaxially stacked peripherally abutting interstage diaphragms, one for each rotor, each of integral, vaneless and cup-shaped form, i.e., having a radially directed portion through which said shaft extends centrally and an outer peripheral portion projecting therefrom at one side of said radially directed portion, and disc-shaped elements in the spaces within each of said respective cup-shaped diaphragms, each of said elements comprising a radial portion, diffuser vanes integral with said radial portion, extending axially from said radial portion in one direction and spiralling outwardly, return vanes integral with said radial portion, extending axially from said radial portion in the opposite direction and spiralling inwardly, and redirecting vanes integral with said radial portion extending axially from said radial
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US70476A US3103892A (en) | 1960-11-21 | 1960-11-21 | Pump or the like |
GB39343/61A GB999900A (en) | 1960-11-21 | 1961-11-02 | Improvements in or relating to the manufacture of pumps, compressors, turbines or the like |
CH1286261A CH391469A (fr) | 1960-11-21 | 1961-11-06 | Procédé de fabrication d'un stator d'une turbo-machine |
DK455861AA DK113825B (da) | 1960-11-21 | 1961-11-16 | Fremgangsmåde ved fremstilling af et statoraggregat til centrifugalpumper eller lignende strømningsmaskiner. |
DE19611403853 DE1403853A1 (de) | 1960-11-21 | 1961-11-18 | Rotierende Einrichtung zum Bewegen eines fluessigen oder gasfoermigen Mediums |
NL7008084A NL7008084A (OSRAM) | 1960-11-21 | 1970-06-03 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US70476A US3103892A (en) | 1960-11-21 | 1960-11-21 | Pump or the like |
Publications (1)
Publication Number | Publication Date |
---|---|
US3103892A true US3103892A (en) | 1963-09-17 |
Family
ID=22095520
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US70476A Expired - Lifetime US3103892A (en) | 1960-11-21 | 1960-11-21 | Pump or the like |
Country Status (6)
Country | Link |
---|---|
US (1) | US3103892A (OSRAM) |
CH (1) | CH391469A (OSRAM) |
DE (1) | DE1403853A1 (OSRAM) |
DK (1) | DK113825B (OSRAM) |
GB (1) | GB999900A (OSRAM) |
NL (1) | NL7008084A (OSRAM) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3288074A (en) * | 1964-11-02 | 1966-11-29 | Weber Ind Inc | Submersible pump |
US4299536A (en) * | 1979-08-09 | 1981-11-10 | Roy E. Roth Company | Multi-stage pumps |
US4536128A (en) * | 1982-08-31 | 1985-08-20 | Klein, Schanzlin & Becker Aktiengesellschaft | Barrel housing for centrifugal fluid machines |
US20120128477A1 (en) * | 2009-07-31 | 2012-05-24 | Man Diesel & Turbo Se | Radial Compressor and Method for Producing a Radial Compressor |
US20120156023A1 (en) * | 2009-07-31 | 2012-06-21 | Man Diesel & Turbo Se | Radial Compressor And Method For Producing A Radial Compressor |
US20120171014A1 (en) * | 2011-01-05 | 2012-07-05 | Hitachi Plant Technologies, Ltd. | Barrel-type multistage pump |
EP2469022A4 (en) * | 2009-08-19 | 2015-01-07 | Mitsubishi Heavy Ind Compressor Corp | RADIAL GAS DETENDER |
CN107762979A (zh) * | 2017-10-19 | 2018-03-06 | 江苏大学 | 一种紧凑型液化天然气潜液泵导叶结构 |
US20190136869A1 (en) * | 2017-11-09 | 2019-05-09 | Mitsubishi Heavy Industries Compressor Corporation | Rotary machine and diaphragm |
CN111207080A (zh) * | 2020-01-22 | 2020-05-29 | 陈科 | 一种带轴开中分便拆结构的化工泵 |
CN112761959A (zh) * | 2021-02-06 | 2021-05-07 | 江苏大学 | 一种多级离心增压泵 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2516987B1 (fr) * | 1981-11-23 | 1986-08-14 | Peugeot | Pompe rotative, notamment pour liquide de refroidissement d'un moteur a combustion interne |
DE102009029069A1 (de) * | 2009-09-01 | 2011-03-03 | Robert Bosch Gmbh | Zweistufige Kreiselpumpe |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL77715C (OSRAM) * | ||||
AT62273B (de) * | 1912-12-09 | 1913-11-25 | Ernst Vogel | Schleuderpumpe. |
GB191517283A (en) * | 1915-12-09 | 1916-07-06 | Hans Rufener | Improvements in Turbine Pumps. |
CH221387A (de) * | 1940-12-30 | 1942-05-31 | Diebold Geb | Mehrstufige Zentrifugalpumpe. |
US2620553A (en) * | 1949-04-15 | 1952-12-09 | Bendix Aviat Corp | Method of manufacturing and assembling hydraulic pumps |
US2786261A (en) * | 1952-10-28 | 1957-03-26 | Garrett Corp | Method of forming passage structure |
GB785419A (en) * | 1955-03-22 | 1957-10-30 | Sulzer Ag | Radial flow compressors |
GB826569A (en) * | 1955-01-27 | 1960-01-13 | Alfred Johann Buchi | Methods for production of centrifugal compressors and compressors produced thereby |
US2954739A (en) * | 1956-01-03 | 1960-10-04 | Tait Mfg Co The | Pumps |
-
1960
- 1960-11-21 US US70476A patent/US3103892A/en not_active Expired - Lifetime
-
1961
- 1961-11-02 GB GB39343/61A patent/GB999900A/en not_active Expired
- 1961-11-06 CH CH1286261A patent/CH391469A/fr unknown
- 1961-11-16 DK DK455861AA patent/DK113825B/da unknown
- 1961-11-18 DE DE19611403853 patent/DE1403853A1/de active Pending
-
1970
- 1970-06-03 NL NL7008084A patent/NL7008084A/xx unknown
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL77715C (OSRAM) * | ||||
AT62273B (de) * | 1912-12-09 | 1913-11-25 | Ernst Vogel | Schleuderpumpe. |
GB191517283A (en) * | 1915-12-09 | 1916-07-06 | Hans Rufener | Improvements in Turbine Pumps. |
CH221387A (de) * | 1940-12-30 | 1942-05-31 | Diebold Geb | Mehrstufige Zentrifugalpumpe. |
US2620553A (en) * | 1949-04-15 | 1952-12-09 | Bendix Aviat Corp | Method of manufacturing and assembling hydraulic pumps |
US2786261A (en) * | 1952-10-28 | 1957-03-26 | Garrett Corp | Method of forming passage structure |
GB826569A (en) * | 1955-01-27 | 1960-01-13 | Alfred Johann Buchi | Methods for production of centrifugal compressors and compressors produced thereby |
GB785419A (en) * | 1955-03-22 | 1957-10-30 | Sulzer Ag | Radial flow compressors |
US2954739A (en) * | 1956-01-03 | 1960-10-04 | Tait Mfg Co The | Pumps |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3288074A (en) * | 1964-11-02 | 1966-11-29 | Weber Ind Inc | Submersible pump |
US4299536A (en) * | 1979-08-09 | 1981-11-10 | Roy E. Roth Company | Multi-stage pumps |
US4536128A (en) * | 1982-08-31 | 1985-08-20 | Klein, Schanzlin & Becker Aktiengesellschaft | Barrel housing for centrifugal fluid machines |
US9360022B2 (en) * | 2009-07-31 | 2016-06-07 | Man Diesel & Turbo Se | Radial compressor and method for producing a radial compressor |
US20120128477A1 (en) * | 2009-07-31 | 2012-05-24 | Man Diesel & Turbo Se | Radial Compressor and Method for Producing a Radial Compressor |
US20120156023A1 (en) * | 2009-07-31 | 2012-06-21 | Man Diesel & Turbo Se | Radial Compressor And Method For Producing A Radial Compressor |
US9488189B2 (en) * | 2009-07-31 | 2016-11-08 | Man Diesel & Turbo Se | Radial compressor and method for producing a radial compressor |
EP2469022A4 (en) * | 2009-08-19 | 2015-01-07 | Mitsubishi Heavy Ind Compressor Corp | RADIAL GAS DETENDER |
US8985945B2 (en) | 2009-08-19 | 2015-03-24 | Mitsubishi Heavy Industries Compressor Corporation | Radial gas expander |
US9249804B2 (en) * | 2011-01-05 | 2016-02-02 | Hitachi, Ltd. | Barrel-type multistage pump |
US20120171014A1 (en) * | 2011-01-05 | 2012-07-05 | Hitachi Plant Technologies, Ltd. | Barrel-type multistage pump |
US9863427B2 (en) | 2011-01-05 | 2018-01-09 | Hitachi, Ltd. | Barrel-type multistage pump |
CN107762979A (zh) * | 2017-10-19 | 2018-03-06 | 江苏大学 | 一种紧凑型液化天然气潜液泵导叶结构 |
US20190136869A1 (en) * | 2017-11-09 | 2019-05-09 | Mitsubishi Heavy Industries Compressor Corporation | Rotary machine and diaphragm |
US10876544B2 (en) * | 2017-11-09 | 2020-12-29 | Mitsubishi Heavy Industries Compressor Corporation | Rotary machine and diaphragm |
CN111207080A (zh) * | 2020-01-22 | 2020-05-29 | 陈科 | 一种带轴开中分便拆结构的化工泵 |
CN111207080B (zh) * | 2020-01-22 | 2020-12-15 | 乐清市芮易经济信息咨询有限公司 | 一种带轴开中分便拆结构的化工泵 |
CN112761959A (zh) * | 2021-02-06 | 2021-05-07 | 江苏大学 | 一种多级离心增压泵 |
CN112761959B (zh) * | 2021-02-06 | 2022-04-15 | 江苏大学 | 一种多级离心增压泵 |
Also Published As
Publication number | Publication date |
---|---|
DE1403853A1 (de) | 1968-10-24 |
CH391469A (fr) | 1965-04-30 |
GB999900A (en) | 1965-07-28 |
NL7008084A (OSRAM) | 1970-10-26 |
DK113825B (da) | 1969-04-28 |
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