GB190816592A - Improvements relating to Fans, Pumps, Propellers, and the like. - Google Patents
Improvements relating to Fans, Pumps, Propellers, and the like.Info
- Publication number
- GB190816592A GB190816592A GB190816592DA GB190816592A GB 190816592 A GB190816592 A GB 190816592A GB 190816592D A GB190816592D A GB 190816592DA GB 190816592 A GB190816592 A GB 190816592A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blades
- inlet
- impeller
- edges
- hub
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
16,592. Vojacek, L. Aug. 6. Centrifugal pumps.-Centrifugal impellers for use as pumps &c , are formed with blades the inlet edges of which extend from the hub almost to the periphery, and are set to receive the axially-entering fluid without shock. The blades are of U of half- U section according as the impeller is of the double or single inlet type, and the peripheral edges may overap and be united to form a ring. The blades may be secured to a conical boss, and may be formed with straight backs inclined at any angle to the shaft, or with curved backs concave or convex towards the direction of rotation. Fig. 2 shows a blade of a double-inlet impeller, Figs. 3 and 3<a> being cylindrical sections on the lines b-b and b<a>-b<a> respectively. The inlet edges extending from the hub 2 to the periphery 22 are set at every point so that the fluid enters without shock, the factors considered being the axial entering velocity of the fluid and the linear velocity of the rotating point. It is stated that with this type of impeller the ratio of the axial inlet velocity to the speed of the shaft is constant. The impeller is narrowed towards the periphery to cause the fluid to fill the spaces between successive blades. The impeller may be cast in one piece. Figs. 7 and 8 show a double-inlet impeller the blades of which may be developed into a plane and may be made from sheet metal. The edges 14 of one blade overlap the preceding blade and are secured to it, thus forming two peripheral rings. In single -inlet impellers, one edge of each blade is secured to the disk on the shaft. Fig. 21 shows a modification in which the blades are secured to a conical hub 19, and are surrounded by an outer ring 21 which may or may not be of the same conicity. The edges of the blades touching the hub 19 need not lie in axial planes; in this case, if the edges are straight, the hub will be no longer conical. The parts may be connected by riveting, soldering, or welding, and the impellers may be used with suitable casings and diffusers.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB190816592T | 1908-08-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190816592A true GB190816592A (en) | 1909-08-05 |
Family
ID=32552791
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190816592D Expired GB190816592A (en) | 1908-08-06 | 1908-08-06 | Improvements relating to Fans, Pumps, Propellers, and the like. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190816592A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2910224A (en) * | 1953-11-17 | 1959-10-27 | Coleman Co | Blower structure and method of fabrication |
US3147911A (en) * | 1960-10-24 | 1964-09-08 | Francis H Clute & Son Inc | Conical impeller suction fan |
US4305698A (en) * | 1978-10-12 | 1981-12-15 | Nissan Motor Co., Ltd. | Radial-flow turbine wheel |
US5316443A (en) * | 1991-10-04 | 1994-05-31 | Chemineer, Inc. | Reversible mixing impeller |
US5791780A (en) * | 1997-04-30 | 1998-08-11 | Chemineer, Inc. | Impeller assembly with asymmetric concave blades |
WO2013075236A1 (en) | 2011-11-24 | 2013-05-30 | Li Wang | Mixing impeller having channel-shaped vanes |
-
1908
- 1908-08-06 GB GB190816592D patent/GB190816592A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2910224A (en) * | 1953-11-17 | 1959-10-27 | Coleman Co | Blower structure and method of fabrication |
US3147911A (en) * | 1960-10-24 | 1964-09-08 | Francis H Clute & Son Inc | Conical impeller suction fan |
US4305698A (en) * | 1978-10-12 | 1981-12-15 | Nissan Motor Co., Ltd. | Radial-flow turbine wheel |
US5316443A (en) * | 1991-10-04 | 1994-05-31 | Chemineer, Inc. | Reversible mixing impeller |
US5791780A (en) * | 1997-04-30 | 1998-08-11 | Chemineer, Inc. | Impeller assembly with asymmetric concave blades |
WO2013075236A1 (en) | 2011-11-24 | 2013-05-30 | Li Wang | Mixing impeller having channel-shaped vanes |
EP2782664A4 (en) * | 2011-11-24 | 2015-07-15 | Li Wang | Mixing impeller having channel-shaped vanes |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3275223A (en) | Fluid moving means | |
US2419669A (en) | Diffuser for centrifugal compressors | |
US3444817A (en) | Fluid pump | |
US2727680A (en) | Centrifugal fan | |
DK145512B (en) | AXIAL BLOWER OR PUMP | |
US4820115A (en) | Open impeller for centrifugal compressors | |
US3394876A (en) | Drum motor blade construction | |
US2399852A (en) | Centrifugal compressor | |
US2398203A (en) | Centrifugal compressor entry vane | |
US820399A (en) | Inlet-opening or eye of centrifugal fans or pumps. | |
US3169694A (en) | Propeller fans and the like | |
US1614091A (en) | Fan and fan blower | |
GB190816592A (en) | Improvements relating to Fans, Pumps, Propellers, and the like. | |
US2362514A (en) | Centrifugal compressor | |
US1887417A (en) | Rotary pump and fan | |
US2965287A (en) | Radial flow compressor | |
US2395704A (en) | Rotor | |
US1138083A (en) | Rotary fan. | |
US2240653A (en) | Fan | |
US3278115A (en) | Control of inlet flow to centrifugal fluid movers | |
US1199374A (en) | Conical-flow fan. | |
KR20170116754A (en) | High pressure centrifugal impeller | |
US2129808A (en) | Blower | |
US995562A (en) | Propelling-wheel. | |
US779473A (en) | Propeller. |