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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
Application number
Inventor
Ladislav Vojacek
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
Application granted granted Critical
Publication of GB190816592A publication Critical patent/GB190816592A/en
Expired legal-status Critical Current

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  • 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.
GB190816592D 1908-08-06 1908-08-06 Improvements relating to Fans, Pumps, Propellers, and the like. Expired GB190816592A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (7)

* Cited by examiner, † Cited by third party
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

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