US3169487A - High pressure vane pump - Google Patents
High pressure vane pump Download PDFInfo
- Publication number
- US3169487A US3169487A US202717A US20271762A US3169487A US 3169487 A US3169487 A US 3169487A US 202717 A US202717 A US 202717A US 20271762 A US20271762 A US 20271762A US 3169487 A US3169487 A US 3169487A
- Authority
- US
- United States
- Prior art keywords
- cylinder
- vanes
- ports
- rotor
- high pressure
- 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
Links
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 239000012530 fluid Substances 0.000 description 2
- 208000025814 Inflammatory myopathy with abundant macrophages Diseases 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- JTJMJGYZQZDUJJ-UHFFFAOYSA-N phencyclidine Chemical compound C1CCCCN1C1(C=2C=CC=CC=2)CCCCC1 JTJMJGYZQZDUJJ-UHFFFAOYSA-N 0.000 description 1
- 230000010349 pulsation Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000007789 sealing Methods 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
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/02—Rotary-piston machines or pumps of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
- F04C2/063—Rotary-piston machines or pumps of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them
- F04C2/077—Rotary-piston machines or pumps of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents with coaxially-mounted members having continuously-changing circumferential spacing between them having toothed-gearing type drive
Definitions
- FIG l2 FIG I3 INVENTOR AM NAMIKAWA W lira-U I Bmjnn's Atromqs United States Patent ice 3,169,487 I HIGH PRESSURE VANE PUMP m. TakashiNamikawa, Knre City,"Japan, assignor to Yehan Numata, Yokohama, Japan 7 Filed June 15, 1962, Ser. No. 202,717 Claimspriority, application Japan, Nov. 29, 1961,
- a concentric rotor is intermittently rotated.
- the cylinder and rotor are provided with overlapping vanes, and these define the end walls of'ch'arnbers which expand and contract due to the difference between the movements of the cylinder and rotor. During expansion, thesechambers register with the inlet ports of the valve plate, and during compression withthe outlet ports.
- the pump thus has over reciprocating pumps the advantage that it may be directly drivenfrom a rotating shaft, yet its mechanism is simplerthan that of centrifugal pumps.
- FIG. 1 is an end view of my new pump
- FIG. 2 is an axial section taken through the entire pump, except for the valve plate, which is sectioned along the line IIII of FIG. 1;
- FIG. 3 is a schematic cross-section through the pump cylinder and rotor
- FIGS. 4, 6, 8, 10 and 12 schematically show various positions assumed by the vanes relative to the ports
- FIGS. 5, 7, 9, l1 and 13 show the positions of the members of the Geneva movement when the vanes occupy the positions shown in FIGS. 4, 6, 8, 10 and 12, respectively;
- FIG. 14 is a graph showing the angular positions of the cylinder and rotor as a function of time.
- the pump comprises a stationary casing 1 closed at one end by the valve plate 2.
- a cylinder 3 is carried by bearings 16 and 20, located in the casing 1 and valve plate 2 respectively.
- the rotor 4 carried by the shaft 5.
- the inner Wall of the cylinder is provided with inwardly projecting vanes 7, and the rotor carries peripherally radiating vanes 6. These vanes overlap to form with the cylinder walls a plurality of expansible chambers. The volume of these chambers is varied by rotating the cylinder 3 at a constant speed, while driving the rotor 4 intermittently at an angular speed twice that of the cylinder.
- each exhaust port b is connected through the outlet 14 and passage d to a safety valve 8, which is connected through the passage e to the inlet 13 and thus to the suction ports 0.
- valve member 3 When the delivery pressure exceeds a prescribed limit, the valve member 3 is forced open against the resistance of'the spring 9, and oil passes through the passage e and suction port c, and thence back into the cylinder 3.
- the pressure required to open the valve 8 may be adjusted by turning the threaded. plug 33 so as to increase or relieve the compression of the spring 9.
- the valve 10 controls the passage 1 between the oil reservoir 19 and the inlet 13. This valve, which is biased shut by the spring 11, automatically opens when the suction pressure falls too low, and the pressure differential required to actuate it may be regulated by turning the threaded plug 12.
- the cylinder 3 is formed in two parts to permit insertion of the rotor 4, and these two parts are held together by bolts 30.
- the shaft 5 rotates in the cylinder, leakage therefrom being prevented by the sealing rings 31 and 32.
- One end of the shaft projects beyond the cylinder jinto bearing 28 in journal box 29.
- Both rotor shaft 5 and cylinder 3 are driven from a drive shaft 25 carried in bearings 26 and 27.
- the cylinder is driven through reduction gearing 21, 22, and the rotor shaft 5 through Geneva gearing 23, 24, so that it rotates intermittently, turning during only half the time that the cylinder turns, but at twice the speed. While Geneva gearing is shown to produce this relationship, it will be appreciated that any other means which produces the same efiect may be used.
- the Geneva gear 24 is keyed to the rotor shaft 5 by the key 18.
- FIGS. 4, 6, 8, l0 and 12 show successive positions of the vanes relative to the valve plate and the apertures therein.
- FIGS. 5, 7, 9, l1 and 13 show the positions of the driving member 23 and driven member 24 corresponding to each of these vane positions.
- each of the cylinder vanes 7 has been assigned one of the reference characters V1, V2, V3, V4 and each of the rotor vanes 6 one of the reference'characters V1, V2, V3, V4.
- the angle 0, through which a representative vane (V1 and V1) from each group turns, is plotted as a function of time intervals 11, t2, etc., on FIG. 14.
- V2 and V3,-V3 and V4, V4 and V1 draw in the oil' connected to outlet means and the remainder being connected to inlet means
- said 'valve' plate ports being posimounted within said casing and carrying a plurality of vanes projecting radially inward from its circumferential wall, an independently rotatable rotor coaxially mounted I to turn within said cylinder and provided with a pluralityof' vanes which project radially outward between the vanes carried by the cylinder, a transverse wall closing one end of said cylinder and pierced by a ring of spaced ports, with two'of said ports disposed between each pair of cylinder-carried vanes, a valve plate forming one end of said casing and positioned adjacent said transverse wall, resilient means biassing said transverse cylinder wall against said valve plate, said valve plate being likewise provided with a ring of spaced ports, alternate ports being tioned to successively register, with said cylinder ports during each revolution of said cylinder, means for rotating one of
- valve plate those of said valve plate ports con'n'ectedtdan outlet beingalso connected to one side of said pressure responsive safety valve and those connected to an inlet being also connected tothe other side of said safety valve, so that an excessive outlet pressure is relieved by passage of fluid from said outlet connected ports to said inlet connected ports through said safety valve, and means accessable from outside said casing for adjusting the loading of said pressure respon sive valve.
Description
HIGH PRESSURE VANE PUMP 5 Sheets-Sheet 1 Filed June 15, 1962 FIG.
INVENTDR TAK ASl NAMl KAWA @WLMM Arroanevs Feb. 16, 1965 TAKASHI NAMIKAWA 3,169,487
HIGH PRESSURE VANE PUMP Filed June 15, 1962 5 Sheets-Sheet 2 F I G 2 Iuvem-oa TAKM NANUKAWA E, MWLAMM{ 'KWAM Feb. 16, 1965 TAKASHI NAMlKAWA 3,169,487
HIGH PRESSURE VANE PUMP Filed June 15, 1962 5 Sheets-Sheet 3 INVENTOR TAKAH NAN KAWA baroauei s Feb. 16, 1965 TAKASHI NAMIKAWA 3,159,487
HIGH PRESSURE VANE PUMP Filed June 15, 1962 5 Sheets-Sheet 4 Imam-cm TAKASI NAMIKAWA AAWummpw m ATTORNE1$ Feb. 16, 1965 TAKASHI NAMIKAWA 3,169,487
HIGH PRESSURE VANE PUMP Filed June 15, 1962 5 Sheets-Sheet 5 FIG.I|
FIG l2 FIG I3 INVENTOR AM NAMIKAWA W lira-U I Bmjnn's Atromqs United States Patent ice 3,169,487 I HIGH PRESSURE VANE PUMP m. TakashiNamikawa, Knre City,"Japan, assignor to Yehan Numata, Yokohama, Japan 7 Filed June 15, 1962, Ser. No. 202,717 Claimspriority, application Japan, Nov. 29, 1961,
1 Claim; (Cl.103 1 29) My invention relates to a high pressure vane pump comprisinga valve plate and an intermittently driven rotor. I
and a concentric rotor is intermittently rotated. The cylinder and rotor are provided with overlapping vanes, and these define the end walls of'ch'arnbers which expand and contract due to the difference between the movements of the cylinder and rotor. During expansion, thesechambers register with the inlet ports of the valve plate, and during compression withthe outlet ports.
The pump thus has over reciprocating pumps the advantage that it may be directly drivenfrom a rotating shaft, yet its mechanism is simplerthan that of centrifugal pumps.
Since some chambers are in the compression stage In this pump the pump cylinder is continuously rotated while others are expanding there is a-relatively even flow ii of fluid, a decreased pulsation of oil pressure, and excel- Other objects and advantages'of the invention are in part obvious and will in part be set forth in the course of the following description of a preferred embodiment of the invention. This embodiment is described in conjunction With the annexed drawings, in which:
FIG. 1 is an end view of my new pump;
FIG. 2 is an axial section taken through the entire pump, except for the valve plate, which is sectioned along the line IIII of FIG. 1;
FIG. 3 is a schematic cross-section through the pump cylinder and rotor;
FIGS. 4, 6, 8, 10 and 12 schematically show various positions assumed by the vanes relative to the ports;
FIGS. 5, 7, 9, l1 and 13 show the positions of the members of the Geneva movement when the vanes occupy the positions shown in FIGS. 4, 6, 8, 10 and 12, respectively;
FIG. 14 is a graph showing the angular positions of the cylinder and rotor as a function of time.
Like reference characters denote like parts throughout the several views, except that in FIGS. 4, 6, 8, l0 and 12 the characters V1, V2, V3 and V4 are used .to identify individual vanes identified as a class by the reference numeral 7 in FIGS. 13, and reference characters V1, V2, V3 and V4 are used to identify individual vanes identified as a class by reference numeral 6 in FIGS. 1-3.
Referring now to FIG. 2, it will be seen that the pump comprises a stationary casing 1 closed at one end by the valve plate 2. A cylinder 3 is carried by bearings 16 and 20, located in the casing 1 and valve plate 2 respectively. Within this cylinder is mounted the rotor 4, carried by the shaft 5. As best seen in FIG. 3, the inner Wall of the cylinder is provided with inwardly projecting vanes 7, and the rotor carries peripherally radiating vanes 6. These vanes overlap to form with the cylinder walls a plurality of expansible chambers. The volume of these chambers is varied by rotating the cylinder 3 at a constant speed, while driving the rotor 4 intermittently at an angular speed twice that of the cylinder.
The,cylinder 3 is biased against the valve plate 2 by the spring 17 which is compressed between the bearing 16 and thrust bearing 15. Between the cylinder 3 and casing 1 is an oil reservoir 19. The valve plate 2 is provided with four exhaust ports b and four suction ports 0. As best seen in FIG. 2, each exhaust port b is connected through the outlet 14 and passage d to a safety valve 8, which is connected through the passage e to the inlet 13 and thus to the suction ports 0.
When the delivery pressure exceeds a prescribed limit, the valve member 3 is forced open against the resistance of'the spring 9, and oil passes through the passage e and suction port c, and thence back into the cylinder 3. The pressure required to open the valve 8 may be adjusted by turning the threaded. plug 33 so as to increase or relieve the compression of the spring 9.
The valve 10 controls the passage 1 between the oil reservoir 19 and the inlet 13. This valve, which is biased shut by the spring 11, automatically opens when the suction pressure falls too low, and the pressure differential required to actuate it may be regulated by turning the threaded plug 12. a
The cylinder 3 is formed in two parts to permit insertion of the rotor 4, and these two parts are held together by bolts 30. The shaft 5 rotates in the cylinder, leakage therefrom being prevented by the sealing rings 31 and 32. One end of the shaft projects beyond the cylinder jinto bearing 28 in journal box 29. Both rotor shaft 5 and cylinder 3 are driven from a drive shaft 25 carried in bearings 26 and 27. The cylinder is driven through reduction gearing 21, 22, and the rotor shaft 5 through Geneva gearing 23, 24, so that it rotates intermittently, turning during only half the time that the cylinder turns, but at twice the speed. While Geneva gearing is shown to produce this relationship, it will be appreciated that any other means which produces the same efiect may be used. The Geneva gear 24 is keyed to the rotor shaft 5 by the key 18.
The operation of the pump will now be explained with reference to FIGS. 4-14. FIGS. 4, 6, 8, l0 and 12 show successive positions of the vanes relative to the valve plate and the apertures therein. FIGS. 5, 7, 9, l1 and 13 show the positions of the driving member 23 and driven member 24 corresponding to each of these vane positions. For convenience, each of the cylinder vanes 7 has been assigned one of the reference characters V1, V2, V3, V4 and each of the rotor vanes 6 one of the reference'characters V1, V2, V3, V4. The angle 0, through which a representative vane (V1 and V1) from each group turns, is plotted as a function of time intervals 11, t2, etc., on FIG. 14.
From these it will be seen, that proceeding from the position at t1, shown in FIGS. 4-5, the cam 23 swings through half a revolution without affecting the position of the gear 24. During this time, the cylinder 3 is nevertheless being constantly driven, so that its vane V1 advances from the position shown in FIG. 4 to that shown in FIG. 6, while the rotor vane V1 remains stationary and thus occupies the same position on both figures. During this time oil is drawn in through the ports 0 and a into the chambers formed between vanes V1 and V1, V2 andV2, V3 and V3, V4 and V4, but simultaneously expelled from the chambers between V1 and V2, V2 and V3, V3 and V4, V4 and V1, through the ports b and a.
Next when the cam 23 turns from the position of FIGS. 6 and 7 in the direction of the arrow into the t3 position shown in FIGS. 8 and 9, oil is drawn into the chambers between vanes V1 and V2, V2 and V3, V3 and V4, V4 and V1, while it is being expelled from between V1 and V1, V2 and V2, V3 and V3, V4 and V4.
* Patented Feb. 1s, was
Further, while the cam23 turns 90 from the t3 position of FIGS. 8 and 9 in the direction of the arrow, into the t4 position of FIGS. 10 and 11, oil is drawn into the:
chambers between vanes V1 and V1, V2 and V2, V3 and V3, V4 and V4, while simultaneously expelled from those between V1 and V2',.V2 and V3, V3 and V4, V4 and 1.
Finally, when the cam turns another 90 from the t4 7 position of FIGS. 10 and 11 to the t position of FIGS.
12 and 13, the chambers between the vanes 1 and V2,
V2 and V3,-V3 and V4, V4 and V1 draw in the oil' connected to outlet means and the remainder being connected to inlet means, said 'valve' plate ports being posimounted within said casing and carrying a plurality of vanes projecting radially inward from its circumferential wall, an independently rotatable rotor coaxially mounted I to turn within said cylinder and provided with a pluralityof' vanes which project radially outward between the vanes carried by the cylinder, a transverse wall closing one end of said cylinder and pierced by a ring of spaced ports, with two'of said ports disposed between each pair of cylinder-carried vanes, a valve plate forming one end of said casing and positioned adjacent said transverse wall, resilient means biassing said transverse cylinder wall against said valve plate, said valve plate being likewise provided with a ring of spaced ports, alternate ports being tioned to successively register, with said cylinder ports during each revolution of said cylinder, means for rotating one of said cylinder and rotor at a constant first speed, means for driving the other intermittently at twice said speed for half of each cycle, a pressure responsive safety valve mounted in said valve. plate, those of said valve plate ports con'n'ectedtdan outlet beingalso connected to one side of said pressure responsive safety valve and those connected to an inlet being also connected tothe other side of said safety valve, so that an excessive outlet pressure is relieved by passage of fluid from said outlet connected ports to said inlet connected ports through said safety valve, and means accessable from outside said casing for adjusting the loading of said pressure respon sive valve.
- References Cited by the Examiner.
UNITED STATES PATENTS 2,211,292 8/40 Ryerson 123--11 2,833,225 5/58, Sherman 103--161 X 2,948,221 8/60 Carver 103-203 x 3,023,706 3/62 De Fezzy at al. 103-26 X FOREIGN PATENTS 758,187 10/56 Great Britain.
34,035 12/12 Sweden.
JOSEPH H. BRANSON, IR., Primary Examiner.
LAURENCE V. EFNER, Examiner.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP4237961 | 1961-11-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3169487A true US3169487A (en) | 1965-02-16 |
Family
ID=12634403
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US202717A Expired - Lifetime US3169487A (en) | 1961-11-29 | 1962-06-15 | High pressure vane pump |
Country Status (2)
Country | Link |
---|---|
US (1) | US3169487A (en) |
CH (1) | CH386253A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981638A (en) * | 1974-03-25 | 1976-09-21 | David Godfrey Williams | Rotary piston machine |
US4169697A (en) * | 1976-09-01 | 1979-10-02 | Doundoulakis George J | Angular compression expansion cylinder with radial pistons |
EP0279967A1 (en) * | 1986-01-06 | 1988-08-31 | Richard S. Stadden | Rotary piston machine utilizing dual action Geneva cam |
US5366356A (en) * | 1992-05-05 | 1994-11-22 | Savgal Compressors Ltd. | Rotary-vane machine |
US20070062482A1 (en) * | 2003-11-21 | 2007-03-22 | Anatoly Arov | Orbital engine/pump with multiple toroidal cylinders |
US20070297928A1 (en) * | 2006-06-25 | 2007-12-27 | Leonid Volftsun | Rotary vane machiine |
US20090038581A1 (en) * | 2006-02-22 | 2009-02-12 | Herbert Huettlin | Oscillating Piston Engine |
US11952899B1 (en) * | 2022-12-05 | 2024-04-09 | Herbert Dym | Bidirectional rotary hydraulic motor and pump |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0083892A3 (en) * | 1982-01-08 | 1984-08-08 | Robert Marcel Pierart | Rotary machine with pistons having a non-uniform rotational speed |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2211292A (en) * | 1938-11-07 | 1940-08-13 | Gerald E Ryerson | Split cycle internal combustion engine |
GB758187A (en) * | 1952-10-09 | 1956-10-03 | Parkwood Engineering Company L | Improvements in and relating to rotary internal combustion engines, pumps or compressors |
US2833225A (en) * | 1954-08-25 | 1958-05-06 | Motor Products Corp | Hydraulic pump structure |
US2948221A (en) * | 1956-05-29 | 1960-08-09 | Kontak Mfg Co Ltd | Pumps for liquids |
US3023706A (en) * | 1960-03-24 | 1962-03-06 | Gen Motors Corp | Gear pump and relief valve |
-
1962
- 1962-06-15 US US202717A patent/US3169487A/en not_active Expired - Lifetime
- 1962-07-13 CH CH843662A patent/CH386253A/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2211292A (en) * | 1938-11-07 | 1940-08-13 | Gerald E Ryerson | Split cycle internal combustion engine |
GB758187A (en) * | 1952-10-09 | 1956-10-03 | Parkwood Engineering Company L | Improvements in and relating to rotary internal combustion engines, pumps or compressors |
US2833225A (en) * | 1954-08-25 | 1958-05-06 | Motor Products Corp | Hydraulic pump structure |
US2948221A (en) * | 1956-05-29 | 1960-08-09 | Kontak Mfg Co Ltd | Pumps for liquids |
US3023706A (en) * | 1960-03-24 | 1962-03-06 | Gen Motors Corp | Gear pump and relief valve |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3981638A (en) * | 1974-03-25 | 1976-09-21 | David Godfrey Williams | Rotary piston machine |
US4169697A (en) * | 1976-09-01 | 1979-10-02 | Doundoulakis George J | Angular compression expansion cylinder with radial pistons |
EP0279967A1 (en) * | 1986-01-06 | 1988-08-31 | Richard S. Stadden | Rotary piston machine utilizing dual action Geneva cam |
US5366356A (en) * | 1992-05-05 | 1994-11-22 | Savgal Compressors Ltd. | Rotary-vane machine |
US20070062482A1 (en) * | 2003-11-21 | 2007-03-22 | Anatoly Arov | Orbital engine/pump with multiple toroidal cylinders |
US7631632B2 (en) * | 2003-11-21 | 2009-12-15 | Anatoly Arov | Orbital engine/pump with multiple toroidal cylinders |
US20090038581A1 (en) * | 2006-02-22 | 2009-02-12 | Herbert Huettlin | Oscillating Piston Engine |
US7866284B2 (en) * | 2006-02-22 | 2011-01-11 | Herbert Huettlin | Oscillating piston engine |
US20070297928A1 (en) * | 2006-06-25 | 2007-12-27 | Leonid Volftsun | Rotary vane machiine |
US7828532B2 (en) * | 2006-06-25 | 2010-11-09 | Leonid Volftsun | Rotary vane machine |
US11952899B1 (en) * | 2022-12-05 | 2024-04-09 | Herbert Dym | Bidirectional rotary hydraulic motor and pump |
Also Published As
Publication number | Publication date |
---|---|
CH386253A (en) | 1964-12-31 |
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