GB537720A - Improvements in and relating to centrifugal pumps - Google Patents

Improvements in and relating to centrifugal pumps

Info

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
Application number
GB366840A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB366840A priority Critical patent/GB537720A/en
Publication of GB537720A publication Critical patent/GB537720A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/06Multi-stage pumps
    • F04D1/08Multi-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.
GB366840A 1940-02-28 1940-02-28 Improvements in and relating to centrifugal pumps Expired GB537720A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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