US2727679A - Fluid compressors - Google Patents
Fluid compressors Download PDFInfo
- Publication number
- US2727679A US2727679A US404919A US40491954A US2727679A US 2727679 A US2727679 A US 2727679A US 404919 A US404919 A US 404919A US 40491954 A US40491954 A US 40491954A US 2727679 A US2727679 A US 2727679A
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- Prior art keywords
- buckets
- rib
- ribs
- fluid
- 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.)
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Links
- 239000012530 fluid Substances 0.000 title description 16
- 241001630695 Plectorhinchus picus Species 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
Images
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
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/022—Multi-stage pumps with concentric rows of vanes
Definitions
- This invention relates to fluid compressors and more particularly to a one-wheel or single rotor, three-stage compressor for use to compress a fluid for any purpose.
- One object is to provide eflicient turbine and compressor apparatus of compact structure and simple mechanical assembly that is powerful in operation, durable in use and inexpensive to manufacture.
- a further object is to provide a multi-stage turbine and compressor of good aerodynamic efiiciency.
- Fig. 1 is a view in rear elevation of a turbine and compressor apparatus according to the invention.
- Fig. 2 is an approximately central vertical sectiona view through Fig. 1 on the line 22.
- Fig. 3 is a vertical sectional view through Fig. 2 on the line 33, with the bearing plate removed.
- Fig. 4 is a view partly in section and partly diagrammatic showing particularly the paths of travel of the fluid.
- Fig. 5 is a view of a modified form, and,
- Fig. 6 is a view partly in section and partly diagrammatic, of same.
- the instant turbine and compressor of centripetal type, includes a supporting stand or frame 1 that carries the apparatus proper which consists of a circular bearing plate or stator 2 having the central hub 3, the stator having the plate 4 secured thereto by bolts or rivets 5, defining a housing.
- a supporting stand or frame 1 that carries the apparatus proper which consists of a circular bearing plate or stator 2 having the central hub 3, the stator having the plate 4 secured thereto by bolts or rivets 5, defining a housing.
- Operatively arranged upon said stator 2 is the outer annular rib 6, the intermediate annular rib 7 and the inner annular rib 3, said ribs being concentric and spaced equal distances from each other consecutively, a hub 9 spaced from the inner rib 8 being aligned with the stator hub 3 and keyed to the rotary shaft 10 driven by a suitable motor (not shown).
- the contour of the housing includes a bearing 12 for the inner end of the shaft 10, said housing also having recessed inwardly disposed portions 13, 13a and 14, 14a; the portions 13, 14 being in fluid-tight relation with the ribs 7 and 8 respectively and the portions 13a, 14a in like relation with the hub 9, the ribs 6, 7, 8 with hub 9, stator 2, and vanes 11 defining buckets 15, the latter arranged between the hub 9 and rib 8 and between the several ribs.
- the vanes 11 are radially arranged so that the buckets 15 between the ribs 6 and 7 forming the first stage are larger than those between the ribs 7 and 8 forming the second stage, which buckets, in turn, are larger than the buckets between the ribs 8 and hub 9, which buckets comprise the third stage, the intake desirably located at the top portion of the housing and receiving fluid under pressure from a source.
- a conduit 17 communicating with the first and second stage buckets between ribs 7 and 8 that form the second stage, the conduit tapering somewhat from its point of communication with the first stage buckets 15, toward buckets 15 of the second stage between ribs 8 and hub 9.
- the fluid path is denoted by arrows in Figs. 2, 3 and 4.
- a discharge conduit 18 communicating with the buckets of the third stage between ribs 8 and hub 9, the conduit 18 tapering as it recedes from the second stage, the fluid from the third stage passing therefrom through the discharge outlet 19.
- a turbine and compressor of the centrifugal type which includes a supporting stand 20 to which a circular plate or stator similar to the stator 2 of Figs. 1 and 2 is secured by bolts or rivets 5 that also secure the stator to the plate 4.
- plate 4a and stator 2 Defined by plate 4a and stator 2 is a housing within which is the outer annular rib 21, the intermediate annular rib 22 and the inner annular rib 23, said ribs operatively arranged upon said stator, said ribs being concentric and spaced equal distances from each other consecutively, a hub 24 spaced from the inner rib 23 being aligned with the stator hub and keyed to the rotary shaft 25 driven by the motor (not shown), the shaft 25 being that receiving the stator.
- the contour of the housing includes a bearing for the inner end of rotary shaft 25, said housing also having recessed inwardly disposed portions 27 that in conjunction with ribs 21, 22, 23 define fluid passageways.
- the plate 4a is here formed with an intake 33 receiving fluid under pressure from a source, the fluid following the path denoted by the arrows, Fig. 6, filling the buckets 29, which are the first stage buckets, and actuating thethe intake point.
- the buckets in the largest and outermost circle rotate at greatest velocity.
- a housing including a stator, a rotary drive shaft mounted in said housing, a hub keyed to said shaft, spaced annular concentric ribs arranged about said shaft, vanes connecting said hub to the innermost rib, vanes connecting said innermost rib to the adjacent rib, vanes connecting said last rib to the outermost rib, the spaces between vanes of each group being progressively smaller from said hub to said outermost rib defining buckets, a fluid intake communicating with the innermost buckets, a conduit connecting the said innermost buckets to adjacent buckets, a conduit connecting said last named adjacent buckets to the outermost buckets, and an outlet for said outermost buckets, all of said conduits disposed in a plane common to that of said outlet, said inlet disposed in a plane at right angles to the aforesaid plane, each of said conduits tapered from its innermost extremity to its outermost to lessen fluid back pressure.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Dec. 20, 1955 D. PICA 2,727,679
FLUID COMPRESSORS I Filed Jan. 19, 1954 2 Sheets-Sheet l IN VEN TOR.
K 0 BY fmzzeZ 1 20a. a p: I O E 1 KW United States Patent 1 2,727,679 FLUID COMPRESSORS Daniel Pica, Chicago, Ill., assignor of one-half to Frank Kemptner, Silver Lake, Wis. Application January 19, 1954, Serial No. 404,919 1 Claim. (Cl. 230-124) This invention relates to fluid compressors and more particularly to a one-wheel or single rotor, three-stage compressor for use to compress a fluid for any purpose. One object is to provide eflicient turbine and compressor apparatus of compact structure and simple mechanical assembly that is powerful in operation, durable in use and inexpensive to manufacture.
A further object is to provide a multi-stage turbine and compressor of good aerodynamic efiiciency. With the foregoingand other objects in view the invention will be understood from the following specification, defined in the claim and illustrated in the accompanying drawing forming part of this disclosure. 1
In the drawing:
Fig. 1 is a view in rear elevation of a turbine and compressor apparatus according to the invention.
Fig. 2 is an approximately central vertical sectiona view through Fig. 1 on the line 22.
Fig. 3 is a vertical sectional view through Fig. 2 on the line 33, with the bearing plate removed.
Fig. 4 is a view partly in section and partly diagrammatic showing particularly the paths of travel of the fluid.
Fig. 5 is a view of a modified form, and,
Fig. 6 is a view partly in section and partly diagrammatic, of same.
Referring now to Figs. 1 through 4, the instant turbine and compressor, of centripetal type, includes a supporting stand or frame 1 that carries the apparatus proper which consists of a circular bearing plate or stator 2 having the central hub 3, the stator having the plate 4 secured thereto by bolts or rivets 5, defining a housing. Operatively arranged upon said stator 2 is the outer annular rib 6, the intermediate annular rib 7 and the inner annular rib 3, said ribs being concentric and spaced equal distances from each other consecutively, a hub 9 spaced from the inner rib 8 being aligned with the stator hub 3 and keyed to the rotary shaft 10 driven by a suitable motor (not shown).
Connecting the annular ribs to each other and to the hub9 are the vanes 11 of the same depth as said ribs. The contour of the housing includes a bearing 12 for the inner end of the shaft 10, said housing also having recessed inwardly disposed portions 13, 13a and 14, 14a; the portions 13, 14 being in fluid-tight relation with the ribs 7 and 8 respectively and the portions 13a, 14a in like relation with the hub 9, the ribs 6, 7, 8 with hub 9, stator 2, and vanes 11 defining buckets 15, the latter arranged between the hub 9 and rib 8 and between the several ribs.
The vanes 11 are radially arranged so that the buckets 15 between the ribs 6 and 7 forming the first stage are larger than those between the ribs 7 and 8 forming the second stage, which buckets, in turn, are larger than the buckets between the ribs 8 and hub 9, which buckets comprise the third stage, the intake desirably located at the top portion of the housing and receiving fluid under pressure from a source.
At a point 180 degrees from the intake conduit a conduit 17 communicating with the first and second stage buckets between ribs 7 and 8 that form the second stage, the conduit tapering somewhat from its point of communication with the first stage buckets 15, toward buckets 15 of the second stage between ribs 8 and hub 9. The fluid path is denoted by arrows in Figs. 2, 3 and 4. At a point 180 2,727,679 Patented Dec. 20, 1955 degrees removed from the point of fluid entry to the second stage that stage is provided with a discharge conduit 18 communicating with the buckets of the third stage between ribs 8 and hub 9, the conduit 18 tapering as it recedes from the second stage, the fluid from the third stage passing therefrom through the discharge outlet 19.
Referring now to Figs. 5 and 6 a turbine and compressor of the centrifugal type is shown which includes a supporting stand 20 to which a circular plate or stator similar to the stator 2 of Figs. 1 and 2 is secured by bolts or rivets 5 that also secure the stator to the plate 4. Defined by plate 4a and stator 2 is a housing within which is the outer annular rib 21, the intermediate annular rib 22 and the inner annular rib 23, said ribs operatively arranged upon said stator, said ribs being concentric and spaced equal distances from each other consecutively, a hub 24 spaced from the inner rib 23 being aligned with the stator hub and keyed to the rotary shaft 25 driven by the motor (not shown), the shaft 25 being that receiving the stator.
The contour of the housing includes a bearing for the inner end of rotary shaft 25, said housing also having recessed inwardly disposed portions 27 that in conjunction with ribs 21, 22, 23 define fluid passageways.
Connecting the hub 24 to the rib 23 are the radial vanes 28 defining large buckets 29 while connecting rib 23 with rib 22 are the vanes 30, in number twice that of the vanes 28 defining buckets 31 which therefore are materially smaller than the buckets 29, and connecting the rib 22 to the rib 21 are the vanes 32, in number twice that of the vanes 30, defining buckets 33a substantially smaller than the buckets 31.
The plate 4a is here formed with an intake 33 receiving fluid under pressure from a source, the fluid following the path denoted by the arrows, Fig. 6, filling the buckets 29, which are the first stage buckets, and actuating thethe intake point. In operation, the buckets in the largest and outermost circle rotate at greatest velocity.
What is claimed is:
In a fluid compressor, a housing including a stator, a rotary drive shaft mounted in said housing, a hub keyed to said shaft, spaced annular concentric ribs arranged about said shaft, vanes connecting said hub to the innermost rib, vanes connecting said innermost rib to the adjacent rib, vanes connecting said last rib to the outermost rib, the spaces between vanes of each group being progressively smaller from said hub to said outermost rib defining buckets, a fluid intake communicating with the innermost buckets, a conduit connecting the said innermost buckets to adjacent buckets, a conduit connecting said last named adjacent buckets to the outermost buckets, and an outlet for said outermost buckets, all of said conduits disposed in a plane common to that of said outlet, said inlet disposed in a plane at right angles to the aforesaid plane, each of said conduits tapered from its innermost extremity to its outermost to lessen fluid back pressure.
References Cited in the file of this patent UNITED STATES PATENTS 823,641 Senior June 19, 1906 945,742 Boeckel et a1 Jan. 11, 1910 986,016 Laufer Mar. 7, 1911 1,054,134 Moore Feb. 25, 1913 1,238,457 Thomson Aug. 28, 1917
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US404919A US2727679A (en) | 1954-01-19 | 1954-01-19 | Fluid compressors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US404919A US2727679A (en) | 1954-01-19 | 1954-01-19 | Fluid compressors |
Publications (1)
Publication Number | Publication Date |
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US2727679A true US2727679A (en) | 1955-12-20 |
Family
ID=23601572
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US404919A Expired - Lifetime US2727679A (en) | 1954-01-19 | 1954-01-19 | Fluid compressors |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2949224A (en) * | 1955-08-19 | 1960-08-16 | American Mach & Foundry | Supersonic centripetal compressor |
US3139232A (en) * | 1959-08-24 | 1964-06-30 | Orville N Peterson | Refrigeration pump |
FR3015589A1 (en) * | 2013-12-23 | 2015-06-26 | Snecma | AXIAL DOUBLE COMPRESSOR TURBOMACHINE |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US823641A (en) * | 1905-04-04 | 1906-06-19 | Alfred Senior Irvine | Steam-turbine. |
US945742A (en) * | 1908-12-04 | 1910-01-11 | Alexander Boeckel | Turbine. |
US986016A (en) * | 1910-05-31 | 1911-03-07 | Christopher F Laufer | Steam-engine. |
US1054134A (en) * | 1912-12-17 | 1913-02-25 | Kerr Turbine Company | Turbine. |
US1238457A (en) * | 1916-04-15 | 1917-08-28 | Alexander Thomson | Multiple-expansion rotary steam-engine, water-wheel, and gasolene-engine muffler. |
-
1954
- 1954-01-19 US US404919A patent/US2727679A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US823641A (en) * | 1905-04-04 | 1906-06-19 | Alfred Senior Irvine | Steam-turbine. |
US945742A (en) * | 1908-12-04 | 1910-01-11 | Alexander Boeckel | Turbine. |
US986016A (en) * | 1910-05-31 | 1911-03-07 | Christopher F Laufer | Steam-engine. |
US1054134A (en) * | 1912-12-17 | 1913-02-25 | Kerr Turbine Company | Turbine. |
US1238457A (en) * | 1916-04-15 | 1917-08-28 | Alexander Thomson | Multiple-expansion rotary steam-engine, water-wheel, and gasolene-engine muffler. |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2949224A (en) * | 1955-08-19 | 1960-08-16 | American Mach & Foundry | Supersonic centripetal compressor |
US3139232A (en) * | 1959-08-24 | 1964-06-30 | Orville N Peterson | Refrigeration pump |
FR3015589A1 (en) * | 2013-12-23 | 2015-06-26 | Snecma | AXIAL DOUBLE COMPRESSOR TURBOMACHINE |
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