US2247813A - Centrifugal impeller - Google Patents
Centrifugal impeller Download PDFInfo
- Publication number
- US2247813A US2247813A US352428A US35242840A US2247813A US 2247813 A US2247813 A US 2247813A US 352428 A US352428 A US 352428A US 35242840 A US35242840 A US 35242840A US 2247813 A US2247813 A US 2247813A
- Authority
- US
- United States
- Prior art keywords
- blades
- band
- shroud band
- impeller
- disk
- 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 - Lifetime
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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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/49329—Centrifugal blower or fan
Definitions
- the present invention relates to centrifugal impellers for compressors, blowers, pumps and the like. More specifically the invention relates to the type of impellers which include an impeller disk and a plurality of circumferentially spaced, substantially radially directed blades or vanes secured to or integrally formed with the disk and a shroud band or ring attached to the blades opposite the disk.
- the shroud band or rim during operation is subject to considerable centrifugal forces. This requires a firm connection between the shroud band and the impeller blades.
- One object of my invention is to provide an improved construction and arrangement of centrifugal impellers whereby the impeller shroud band is firmly attached to the impeller blades.
- FIG. 1 illustrates a top view of an impeller embodying my invention
- Fig. 2 is a front view partly in section taken along lines 2-2 of Fig. 1
- Figs. 3 and 4 are perspective views showing a shroud band in two successive stages of manufacture
- Figs. 5 and 6 are exploded, perspective Views of the impeller.
- An impeller according to my invention as shown in Figs. 1 and 2, comprises a disk Ill having a central portion with a bore forming a hub I II for attachment to an impeller shaft, not shown.
- a plurality of circumferentially, uniformly spaced blades I2 are secured, in the present instance integrally formed with the disk III.
- a shroud band I3 is attached to the edges of the blades opposite the disk ID.
- the band I3 has an inner cylindrical portion I4 and an outer substantially comically-shaped portion I5 the thickness of which decreases radially in outward direction.
- connection between the band I3 and the edges of the blades I2 is accomplished by two rows of dovetailed projections I 6 and Il integrally formed on the shroud band I3 and located in corresponding dovetailed recesses I8 and I9 respectively of the blades I2.
- Each blade has an outer edge 20 forming two radially spaced dovetailed recesses I8, I9 for receiving two dovetailed projections I6, ll of the shroud band I3.
- These means in the present instance are in the form of two locking members or plates 2
- , 22 have end faces 24 engaging ad acent faces of a pair of impeller blades I2, thereby preventing circumferential relative movement between the blades and the shroud band.
- the dovetailed projections I6, I! in the shroud band are formed by producing a shroud band'and machined thereon two annular undercut projections 25 and 26, as shown in Fig. 3. Intermediate portions of the annular projections 25, 26 are then removed or cut away, thus leaving two rows of dovetailed projections I6, II, as shown in Fig. 4.
- the latter is assembled with the blades by rotating it so that the projections I6, Il enter and fill the recesses I8, l9 respectively.
- the locking plates 22 are attached to the shroud band securely to lock the latter to the blades and to prevent relative movement between them.
- Centrifugal impeller comprising a disk with a plurality of circumferentially spaced substantially radially directed blades each having an edge engaging the disk, a shroud band engaging the other edges of the blades, dovetailed connecting means formed on the other edges of the blades and the shroud band rigidly to secure the band to the blades, and locking plate means fastened to the shroud band and engaging adjacent faces of a pair of blades to prevent relative circumferential movement between the blades and the band.
- Centrifugal impeller comprising a disk with a plurality of circumferentially spaced blades each having an edge secured to the disk, a shroud band engaging the other edges of the blades, dovetailed connecting means formed on the other edges of the blades and the shroud band rigidly to secure the band to the blades, and locking means fastened to the shroud band and engaging adjacent faces of a pair of blades to prevent relative circumferential movement between the blades and the band.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
RRHurrso CENTRIFUGAL IMPELLER July 1, 1941.
Filed Aug. 13, 1940 Inventor. \QObeTt. F2. Hu'ltson, b 6.2
tor'hey- Patented July I, 1941 CENTRIFUGAL IMPELLER Robert R. Huitson, Rugby, England, assignor to General Electric Company, a corporation of New Yo k Application August 13, 1940, Serial No. 352,428 In Great Britain August 11, 1939 2 Claims.
The present invention relates to centrifugal impellers for compressors, blowers, pumps and the like. More specifically the invention relates to the type of impellers which include an impeller disk and a plurality of circumferentially spaced, substantially radially directed blades or vanes secured to or integrally formed with the disk and a shroud band or ring attached to the blades opposite the disk. The shroud band or rim during operation is subject to considerable centrifugal forces. This requires a firm connection between the shroud band and the impeller blades.
One object of my invention is to provide an improved construction and arrangement of centrifugal impellers whereby the impeller shroud band is firmly attached to the impeller blades.
For a consideration of what I believe to be novel and my invention, attention is directed to the following description and the claims appended thereto in connection with the accompanying drawing.
In the drawing Fig. 1 illustrates a top view of an impeller embodying my invention; Fig. 2 is a front view partly in section taken along lines 2-2 of Fig. 1; Figs. 3 and 4 are perspective views showing a shroud band in two successive stages of manufacture; and Figs. 5 and 6 are exploded, perspective Views of the impeller.
An impeller according to my invention, as shown in Figs. 1 and 2, comprises a disk Ill having a central portion with a bore forming a hub I II for attachment to an impeller shaft, not shown. A plurality of circumferentially, uniformly spaced blades I2 are secured, in the present instance integrally formed with the disk III. A shroud band I3 is attached to the edges of the blades opposite the disk ID. The band I3 has an inner cylindrical portion I4 and an outer substantially comically-shaped portion I5 the thickness of which decreases radially in outward direction. The connection between the band I3 and the edges of the blades I2 is accomplished by two rows of dovetailed projections I 6 and Il integrally formed on the shroud band I3 and located in corresponding dovetailed recesses I8 and I9 respectively of the blades I2. Each blade has an outer edge 20 forming two radially spaced dovetailed recesses I8, I9 for receiving two dovetailed projections I6, ll of the shroud band I3. In order to retain the dovetailed projections within the recesses, that is, to prevent relative circumferential movement between the blades and the shroud band, means ar provided to preclude relative rotational movement between the shroud band and the impeller blades. These means in the present instance are in the form of two locking members or plates 2| and 22 arranged on diametrically opposite sides of the shroud band and fastened thereto by means of rivets 23. The plates 2|, 22 have end faces 24 engaging ad acent faces of a pair of impeller blades I2, thereby preventing circumferential relative movement between the blades and the shroud band.
During the manufacturing process two radially spaced rows of dovetailed recesses are machined into the edges 20 of the blades after the latter have been secured to or integrally formed on the disk Ill. The dovetailed projections I6, I! in the shroud band are formed by producing a shroud band'and machined thereon two annular undercut projections 25 and 26, as shown in Fig. 3. Intermediate portions of the annular projections 25, 26 are then removed or cut away, thus leaving two rows of dovetailed projections I6, II, as shown in Fig. 4. After completion of the blades and the shroud band the latter is assembled with the blades by rotating it so that the projections I6, Il enter and fill the recesses I8, l9 respectively. Finally, the locking plates 22 are attached to the shroud band securely to lock the latter to the blades and to prevent relative movement between them.
Having described the method of operation of my invention, together with the apparatus which I now consider to represent the best embodiment thereof, I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
What I claim as new and desire to secure by Letters Patent in the United States is:
1. Centrifugal impeller comprising a disk with a plurality of circumferentially spaced substantially radially directed blades each having an edge engaging the disk, a shroud band engaging the other edges of the blades, dovetailed connecting means formed on the other edges of the blades and the shroud band rigidly to secure the band to the blades, and locking plate means fastened to the shroud band and engaging adjacent faces of a pair of blades to prevent relative circumferential movement between the blades and the band.
2. Centrifugal impeller comprising a disk with a plurality of circumferentially spaced blades each having an edge secured to the disk, a shroud band engaging the other edges of the blades, dovetailed connecting means formed on the other edges of the blades and the shroud band rigidly to secure the band to the blades, and locking means fastened to the shroud band and engaging adjacent faces of a pair of blades to prevent relative circumferential movement between the blades and the band.
ROBERT R. HUITSON.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2247813X | 1939-08-11 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2247813A true US2247813A (en) | 1941-07-01 |
Family
ID=10902187
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US352428A Expired - Lifetime US2247813A (en) | 1939-08-11 | 1940-08-13 | Centrifugal impeller |
Country Status (1)
Country | Link |
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US (1) | US2247813A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2543633A (en) * | 1945-12-06 | 1951-02-27 | Hanna Coal & Ore Corp | Rotary pump |
US2641190A (en) * | 1949-11-22 | 1953-06-09 | Bendix Aviat Corp | Balanced impeller for centrifugal pumps |
US2652191A (en) * | 1942-02-21 | 1953-09-15 | Buchi Alfred | Rotor for compressing machines such as centrifugal blowers and pumps |
US2696171A (en) * | 1950-06-21 | 1954-12-07 | Borg Warner | Hydrodynamic coupling |
US2764096A (en) * | 1952-12-15 | 1956-09-25 | Continental Motors Corp | Water pump for internal combustion engine |
US2816509A (en) * | 1953-05-12 | 1957-12-17 | Dempster Mill Mfg Company | Submersible pumps |
US2921532A (en) * | 1956-02-17 | 1960-01-19 | Tokheim Corp | Submerged motor pump |
US3159106A (en) * | 1962-03-21 | 1964-12-01 | Allis Chalmers Mfg Co | Impeller and method of making same |
US3225422A (en) * | 1962-03-09 | 1965-12-28 | Ametek Inc | Method of fabricating centrifugal fan impellers |
US4647271A (en) * | 1984-06-08 | 1987-03-03 | Hitachi, Ltd. | Impeller of centrifugal blower |
US20110182736A1 (en) * | 2010-01-25 | 2011-07-28 | Larry David Wydra | Impeller Assembly |
US20180142691A1 (en) * | 2016-11-23 | 2018-05-24 | Eddy Pump Corporation | Eddy Pump Impeller |
WO2019020321A1 (en) * | 2017-07-28 | 2019-01-31 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Impeller division of a two-piece fan impeller |
US10883508B2 (en) | 2018-10-31 | 2021-01-05 | Eddy Pump Corporation | Eddy pump |
-
1940
- 1940-08-13 US US352428A patent/US2247813A/en not_active Expired - Lifetime
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2652191A (en) * | 1942-02-21 | 1953-09-15 | Buchi Alfred | Rotor for compressing machines such as centrifugal blowers and pumps |
US2543633A (en) * | 1945-12-06 | 1951-02-27 | Hanna Coal & Ore Corp | Rotary pump |
US2641190A (en) * | 1949-11-22 | 1953-06-09 | Bendix Aviat Corp | Balanced impeller for centrifugal pumps |
US2696171A (en) * | 1950-06-21 | 1954-12-07 | Borg Warner | Hydrodynamic coupling |
US2764096A (en) * | 1952-12-15 | 1956-09-25 | Continental Motors Corp | Water pump for internal combustion engine |
US2816509A (en) * | 1953-05-12 | 1957-12-17 | Dempster Mill Mfg Company | Submersible pumps |
US2921532A (en) * | 1956-02-17 | 1960-01-19 | Tokheim Corp | Submerged motor pump |
US3225422A (en) * | 1962-03-09 | 1965-12-28 | Ametek Inc | Method of fabricating centrifugal fan impellers |
US3159106A (en) * | 1962-03-21 | 1964-12-01 | Allis Chalmers Mfg Co | Impeller and method of making same |
US4647271A (en) * | 1984-06-08 | 1987-03-03 | Hitachi, Ltd. | Impeller of centrifugal blower |
US20110182736A1 (en) * | 2010-01-25 | 2011-07-28 | Larry David Wydra | Impeller Assembly |
US20180142691A1 (en) * | 2016-11-23 | 2018-05-24 | Eddy Pump Corporation | Eddy Pump Impeller |
US10480524B2 (en) * | 2016-11-23 | 2019-11-19 | Eddy Pump Corporation | Eddy pump impeller |
US11319969B2 (en) | 2016-11-23 | 2022-05-03 | Eddy Pump Corporation | Eddy pump impeller |
WO2019020321A1 (en) * | 2017-07-28 | 2019-01-31 | Ebm-Papst Mulfingen Gmbh & Co. Kg | Impeller division of a two-piece fan impeller |
US10883508B2 (en) | 2018-10-31 | 2021-01-05 | Eddy Pump Corporation | Eddy pump |
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