GB537720A - Improvements in and relating to centrifugal pumps - Google Patents
Improvements in and relating to centrifugal pumpsInfo
- Publication number
- GB537720A GB537720A GB366840A GB366840A GB537720A GB 537720 A GB537720 A GB 537720A GB 366840 A GB366840 A GB 366840A GB 366840 A GB366840 A GB 366840A GB 537720 A GB537720 A GB 537720A
- Authority
- GB
- United Kingdom
- Prior art keywords
- impeller
- passages
- blades
- centre
- periphery
- 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
- F04D1/08—Multi-stage pumps the stages being situated concentrically
Abstract
537,720. Centrifugal pumps. UMPLEBY, F. Feb. 28, 1940, No. 3668. [Class 110 (i)) A centrifugal pump comprises several sets of vanes F, F1, F<2> on the impeller, separated by sets of fixed vanes H, L on the casing, the fluid passing from the centre of the impeller to its periphery. A propeller B in the inlet eye gives an initial whirl to the entering fluid. The adjacent faces of the blades are approximately parallel, while the other two faces of the passages are convergent, so that the passages get narrower from the centre to the periphery, as shown in Fig. 2. Small openings R are formed in the blades to reduce turbulence. Several pumping units as above may be arranged in series.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB366840A GB537720A (en) | 1940-02-28 | 1940-02-28 | Improvements in and relating to centrifugal pumps |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB366840A GB537720A (en) | 1940-02-28 | 1940-02-28 | Improvements in and relating to centrifugal pumps |
Publications (1)
Publication Number | Publication Date |
---|---|
GB537720A true GB537720A (en) | 1941-07-03 |
Family
ID=9762683
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB366840A Expired GB537720A (en) | 1940-02-28 | 1940-02-28 | Improvements in and relating to centrifugal pumps |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB537720A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2853227A (en) * | 1948-05-29 | 1958-09-23 | Melville W Beardsley | Supersonic compressor |
DE1076145B (en) * | 1953-08-25 | 1960-02-25 | Siemens Ag | High pressure turbine with radial blading of the constant pressure control stage |
-
1940
- 1940-02-28 GB GB366840A patent/GB537720A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2853227A (en) * | 1948-05-29 | 1958-09-23 | Melville W Beardsley | Supersonic compressor |
DE1076145B (en) * | 1953-08-25 | 1960-02-25 | Siemens Ag | High pressure turbine with radial blading of the constant pressure control stage |
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