GB512098A - An impeller for centrifugal pumps especially aero-engine super-chargers - Google Patents
An impeller for centrifugal pumps especially aero-engine super-chargersInfo
- Publication number
- GB512098A GB512098A GB30037/38A GB3003738A GB512098A GB 512098 A GB512098 A GB 512098A GB 30037/38 A GB30037/38 A GB 30037/38A GB 3003738 A GB3003738 A GB 3003738A GB 512098 A GB512098 A GB 512098A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vane
- passage
- impeller
- centrifugal pumps
- initial
- 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
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
512,098. Centrifugal pumps. MASCHINENFABRIK AUGSBURG-NURNBURG AKT.- GES. Oct. 17, 1938, No. 30037. Convention date, Oct. 19, 1937. Drawings to Specification. [Class 110 (i)] In a centrifugal pump with an impeller having radial vanes projecting from a central boss and each lying in a plane at right angles to the direction of rotation, the shape of each vane is such that the initial and final values of passage depth plotted above the centre-line of flow encloses an angle with the horizontal of 19 degrees or more. When the initial depth of the passage is constant for a certain distance from the inlet, the initial value is taken at the commencement of the contraction and the angle is then 22 degrees or more. The outlet area of passage is less than 65 times the inlet area. Each vane may have the end of its leading edge arched in the direction of flow, the back of the vane remaining rectilinear. Specification 279,426, [Class 110 (i)], is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE512098X | 1937-10-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB512098A true GB512098A (en) | 1939-08-29 |
Family
ID=6548021
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30037/38A Expired GB512098A (en) | 1937-10-19 | 1938-10-17 | An impeller for centrifugal pumps especially aero-engine super-chargers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB512098A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2819012A (en) * | 1950-12-22 | 1958-01-07 | Gen Motors Corp | Centrifugal compressor |
US4543041A (en) * | 1981-08-07 | 1985-09-24 | Holset Engineering Company Limited | Impellor for centrifugal compressor |
US4752187A (en) * | 1981-12-01 | 1988-06-21 | Klein, Schanzlin & Becker Aktiengesellschaft | Radial impeller for fluid flow machines |
-
1938
- 1938-10-17 GB GB30037/38A patent/GB512098A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2819012A (en) * | 1950-12-22 | 1958-01-07 | Gen Motors Corp | Centrifugal compressor |
US4543041A (en) * | 1981-08-07 | 1985-09-24 | Holset Engineering Company Limited | Impellor for centrifugal compressor |
US4752187A (en) * | 1981-12-01 | 1988-06-21 | Klein, Schanzlin & Becker Aktiengesellschaft | Radial impeller for fluid flow machines |
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