GB999900A - Improvements in or relating to the manufacture of pumps, compressors, turbines or the like - Google Patents
Improvements in or relating to the manufacture of pumps, compressors, turbines or the likeInfo
- Publication number
- GB999900A GB999900A GB39343/61A GB3934361A GB999900A GB 999900 A GB999900 A GB 999900A GB 39343/61 A GB39343/61 A GB 39343/61A GB 3934361 A GB3934361 A GB 3934361A GB 999900 A GB999900 A GB 999900A
- Authority
- GB
- United Kingdom
- Prior art keywords
- machined
- diaphragms
- annular portion
- dimensions
- passages
- 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
Links
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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
999,900. Centrifugal pumps and compressors; turbines. DE LAVAL TURBINE Inc. Nov. 2, 1961 [Nov. 21, 1960], No. 39343/61. Headings F1C and FIT. In a method of manufacturing any one of a number of similar stator assemblies of identical length for a pump, compressor, turbine, etc. within a determined range of dimensions and machine capacities employing a single series of identical diaphragm blanks, each blank having a radial annular portion and a cylindrical portion which extends axially of the outer periphery of the annular portion, the annular portion is formed of a thickness which is not less than the maximum thickness and materially in excess of the normal machining allowance at the minimum thickness within the determined range of dimensions and the cylindrical portion is formed with an axial width in excess of the required finished width by an amount at least equal to the difference between the maximum and minimum thickness of the annular portion within the determined range of dimensions, either or both of the opposed radial faces of the blank being machined to reduce the axial thickness of the annular portion to the required dimension and to reduce the cylindrical portion to the required finished axial width such that a number of such finished machined diaphragms, when assembled in axially stacked relationship with end diaphragms, provide a stator assembly of the required dimensions for a particular machine capacity. In the multi-stage pump shown in Fig. 1, diaphragms 12, 14, 16, formed with interlocking rabbets, are assembled into an outer casing barrel 2 against a shoulder 7 and held together by tie members 24. During operation, the discharge pressure holds the assembly against the shoulder 7. Diffuser elements 18, Figs. 1 and 2, are nested within the diaphragms 12, 14 and secured to them by bolts 19. Diffuser vanes 23 spiral outwardly from their inlet edges 25, and return vanes 27 on the opposite side of each element 18 spiral inwardly from their inlet edges 26 to their outlet edges 28. Helical cross-over passages 30 lead 'the fluid from the diffuser passages to the return passages. Whirl-removing vanes 36 lead the fluid to the impeller eye of the next stage. Fig. 6 shows how a diaphragm casting 14A of stock size can be machined to suit pumps of different duties, i.e. having different sizes of impellers or numbers of stages, or both. For a low-capacity pump, the shaded portion 42 can be machined away to provide an axial dimension A 1 . For a highcapacity pump, the shaded portion 44 can be machined away instead to provide a larger axial dimension A 2 . For intermediate sizes, material is removed from both ends of the casting. Similarly, the diffuser elements 18 can be machined from stock castings of ample peripheral width to provide the required finished widths of the passages on both sides of the element. For pumps of different lengths, different barrels 2 are provided. In the case of compressors, the impellers are usually of different sizes in successive stages, necessitating correspondingly different amounts of machining of the diaphragms and diffuser elements. The invention is also applicable to turbines for gas or liquid.
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 |
---|---|
GB999900A true GB999900A (en) | 1965-07-28 |
Family
ID=22095520
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB39343/61A Expired GB999900A (en) | 1960-11-21 | 1961-11-02 | Improvements in or relating to the manufacture of pumps, compressors, turbines or the like |
Country Status (6)
Country | Link |
---|---|
US (1) | US3103892A (en) |
CH (1) | CH391469A (en) |
DE (1) | DE1403853A1 (en) |
DK (1) | DK113825B (en) |
GB (1) | GB999900A (en) |
NL (1) | NL7008084A (en) |
Families Citing this family (13)
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 |
FR2516987B1 (en) * | 1981-11-23 | 1986-08-14 | Peugeot | ROTARY PUMP, IN PARTICULAR FOR COOLING LIQUID OF AN INTERNAL COMBUSTION ENGINE |
DE3232326C2 (en) * | 1982-08-31 | 1985-10-03 | Klein, Schanzlin & Becker Ag, 6710 Frankenthal | Pot housing for centrifugal pumps |
DE102009035573A1 (en) * | 2009-07-31 | 2011-02-10 | Man Diesel & Turbo Se | Radial compressor and method of manufacturing a radial compressor |
DE102009035575A1 (en) * | 2009-07-31 | 2011-03-03 | Man Diesel & Turbo Se | Radial compressor and method of manufacturing a radial compressor |
JP4927129B2 (en) * | 2009-08-19 | 2012-05-09 | 三菱重工コンプレッサ株式会社 | Radial gas expander |
DE102009029069A1 (en) * | 2009-09-01 | 2011-03-03 | Robert Bosch Gmbh | Two-stage centrifugal pump |
JP5649055B2 (en) | 2011-01-05 | 2015-01-07 | 株式会社日立製作所 | Barrel type multistage pump |
CN107762979A (en) * | 2017-10-19 | 2018-03-06 | 江苏大学 | A kind of compact liquefied natural gas immersed pump guide vane structure |
JP6963471B2 (en) * | 2017-11-09 | 2021-11-10 | 三菱重工コンプレッサ株式会社 | Rotating machine |
CN112392730A (en) * | 2020-01-22 | 2021-02-23 | 陈科 | Chemical pump with shaft-split middle-opening conveniently-disassembled structure |
CN112761959B (en) * | 2021-02-06 | 2022-04-15 | 江苏大学 | Multistage centrifugal booster pump |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL77715C (en) * | ||||
AT62273B (en) * | 1912-12-09 | 1913-11-25 | Ernst Vogel | Centrifugal pump. |
GB191517283A (en) * | 1915-12-09 | 1916-07-06 | Hans Rufener | Improvements in Turbine Pumps. |
CH221387A (en) * | 1940-12-30 | 1942-05-31 | Diebold Geb | Multi-stage centrifugal pump. |
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 |
-
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/en unknown
- 1961-11-16 DK DK455861AA patent/DK113825B/en unknown
- 1961-11-18 DE DE19611403853 patent/DE1403853A1/en active Pending
-
1970
- 1970-06-03 NL NL7008084A patent/NL7008084A/xx unknown
Also Published As
Publication number | Publication date |
---|---|
NL7008084A (en) | 1970-10-26 |
CH391469A (en) | 1965-04-30 |
DK113825B (en) | 1969-04-28 |
US3103892A (en) | 1963-09-17 |
DE1403853A1 (en) | 1968-10-24 |
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