US3211104A - Pumps - Google Patents

Pumps Download PDF

Info

Publication number
US3211104A
US3211104A US303198A US30319863A US3211104A US 3211104 A US3211104 A US 3211104A US 303198 A US303198 A US 303198A US 30319863 A US30319863 A US 30319863A US 3211104 A US3211104 A US 3211104A
Authority
US
United States
Prior art keywords
vane
vanes
pressure
chamber
rotor
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
Application number
US303198A
Inventor
Oscar E Rosaen
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
Priority to US303198A priority Critical patent/US3211104A/en
Application granted granted Critical
Publication of US3211104A publication Critical patent/US3211104A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C2/3446Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along more than one line or surface
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders

Definitions

  • the present invention relates to rotary vane type fluid pumps and more particularly to an improvement in pressure balancing of the vanes of such pumps as those I have disclosed in my copending application Ser. No. 765,605, filed Oct. 6, 1958 now Patent No. 3,000,324 issued Sept. 19, 1961 and Ser. No. 765,606, also filed Oct. 6, 1958.
  • the present invention eliminates the need for such sealing vanes by providing a means of utilizing the differential in pressures in the area between the inlet and the outlet to tip the vane element and produce a sealing engagement between portions of the vane element and the walls of the slot. In this way pressure beneath the vane is sealed in and prevented from escaping.
  • One object then of the present invention is to maintain pressure balancing of the vane elements in all areas of the pumping cycle without the necessity of using sealing means.
  • Another object of the invention is to improve rotary vane pumps by providing vane elements which are ballanced by fluid pressures as nearly as possible in all directions to provide silent operation and elimination of pressure surges.
  • a further object of the invention is to simplify manufacture, handling and assembly of rotary vane pumps by providing passages for fluid pressure operative to maintain pressure balancing on the vanes at all times.
  • Yet another object of the invention is to improve rotary vane pump operation by providing pressure balanced vanes which in themselves act, during travel from the outlet areas to the inlet areas of the pumping chamber, to provide a sealing engagement with the sides of the slot to maintain a separation of the fluid pressures acting on the vane elements during such periods of travel.
  • FIG. 1 is a longitudinal cross-sectional view of a preferred rotary vane pump embodying the invention and as taken substantially on the line 11 of FIG. 2.
  • FIG. 2 is a cross sectional view of the pump taken substantially on the line 22 of FIG. 1.
  • FIG. 3 is a cross-sectional view of the pump taken substantially on the line 2-2 of FIG. 1.
  • FIG. 4 is a cross-sectional view of a cheek plate portion of the pump on a plane normal to the plane of the cross-section of FIG. 1.
  • FIG. 5 is an axial elevational view of the rotor and cam components of the pump.
  • FIG. 6 is a side elevational View of the cam component shown in FIG. 5.
  • FIG. 7 is an elevational plan view of'a vane embodied in the pump rotor.
  • FIG. 8 is an end elevational view of said vane.
  • FIG. 9 is a cross-sectional view taken substantially on line 9-9 of FIG. 7.
  • FIG. 10 is an enlarged fragmentary elevational view of structure shown in FIG. 5, and
  • FIG. 11 is a view similar to FIG. 10 but illustrating another preferred construction of the pump of the present invention.
  • the preferred pump 10 comprises a housing structure 11 provided with an end plate 12 enclosing a substantially cylindrical pumping chamber 13.
  • An inner cheek plate 14 and an outer cheek plate 15 are disposed in the chamber 13 with an annular cam ring 16 disposed between them and having a cam surface 16A forming the peripheral surface of a rotor chamber 16B.
  • a rotor 17 is rotatably carried in the chamber 16B and is keyed to a drive shaft 18 supported by a bearing 18A at one end of the housing 11 and a bushing 18B mounted in the outer cheek plate 15.
  • the housing 11 has a fluid inlet 19 connected with similar and diametrically opposite inlet grooves 20 in the sides of the chamber 13 to form passages extending axially between the wall of the chamber 13 and the outer surfaces of the cam ring 16.
  • the grooves 20 admit fluid to intake openings 21 in the cam ring 16, fluid thence entering the rotor chamber 16B at what is for purposes of discussion herein called the inlet areas of the chamber 16B.
  • the openings 21 are elongated as at grooves 21A shown in FIGS. 2 and 5 to provide inlet areas greater in annular length than the space between two adjacent rotor vanes.
  • Fluid will be impelled annularly around the spaces of the rotor chamber 16B between the cam surfaces 16A and the rotor 17 to an outlet area in the location of cam surface slopes 22.
  • a pair of diametrically opposite axially extending discharge openings 23 are provided in the cam ring 16 and are connected by grooves 23A with the outlet areas of the rotor chamber 16B.
  • the grooves 23A like the grooves 21A, are greater in annular length than the space between adjacent rotor vanes. Fluid from the discharge openings 23 is forced under pressure out through passages 24 provided in the inner cheek plate 14, through discharge passages 25 and 26 in the housing 11 to a pressure fluid outlet 27.
  • the ressure flow is produced by means of a plurality of axially elongated rotor vanes 30 radially slidably carried in a plurality of equally annularly spaced slots 31 provided around the periphery of the rotor 17.
  • Each slot 31 communicates at its inner end with axially bored holes 32 as shown.
  • the outer edges of the vanes 30 are quided along the cam surfaces 16A, the vanes 30 retracting in the slots 31 as they follow the cam slopes 22. Fluid is thus impelled from the inlet to the outlet areas.
  • Each vane 30, as shown in FIGS. 7, 8 and 9, is provided on its forward face with a radialy extending groove 33 and the forward outer edge is beveled as at 34 to provide substantially line contact between the vanes 30 and the cam surface 16A, the vanes thereby being readily held outward by the pressure under the vanes as will be described, the outer end 33A of the groove 33 being spaced slightly from the bevel 34.
  • the forward outer edges of the slots 31 are beveled as at 31A.
  • the vanes 30 When the vanes 30 are extended during travel from the inlet to the outlet areas of the chamber 163, the outer ends 33A of the grooves 33 are radially outward of the slot bevel 31A, the fluid presure is transmitted to the inner ends of the slots at the holes 32, so that both ends of the vanes 30 are subjected to substantially equal pressures.
  • pressure on the forward face is substantially balanced against the pressure on the rearward face, in the same fashion as that described in my prior patents.
  • the pressure As pressure rises in the chamber 16B ahead of each vane, the pressure also rises equally underneath the vanes 32, providing for extremely silent operation with practically no pressure surges.
  • the slot bevel 31A provides a fulcrum at 37B which permits the vanes 30 to tip.
  • a pressure differential is produced across the extended end of the vane element 30.
  • the pressures between the faces of the vane element and the sides of the slot 31 as well as the pressure beneath the vane element 30 will vary but will be somewhat intermediate the suction pressure on the forward face of the extended portion of the vane element 30 and the high outlet pressure on the rearward face of the extended portion of the vane element 30.
  • the vane element 30 will be caused to tip forward as illustrated in FIG. 10 and cause a substantially tight line contact between the rearward faces of the vanes and the inner edge of the slots 31 at the point 37 shown in FIGS. 5 and 10, and also between the forward faces of the vanes 30 and the outer edge of the slots 31 at the point 37B, preventing leakage of pressure past the vanes 30.
  • the slot bevel 31A performs the dual function of promoting tipping of the vane element 30 by exposing a greater portion of the vane element to the pressure differential which produces the tipping and by providing the fulcrum point 37B upon which the vane element 30 can tip as well as providing the closing point of the groove 33 below the halfway point of balance between the inner and outer ends of the slot 31.
  • the beveled face 34 of the vane elements 30 provide substantially line contact between the vanes 30 and the cam surface 16A.
  • a port 35 is provided in the inner cheek plate 14 in a position to register momentarily with the holes 32 at the inner ends of the slots 31 as they successively pass from the outlet areas.
  • the ports 35 are openly connected with the outlet passages 24 by means of passages 36.
  • FIG. 11 is a view similar to FIG. 10 but illustrates a preferred modification of the present invention.
  • the beveled face 34 of the vane element 30 is angled such that when the vane element 30 is in the retracted position, the edge of the bevel 34 and the leading face of the vane element is disposed above the line 37B. In this way the edge of the slot bevel 31A acts as the fulcrum upon which the vane element 30 is tipped.
  • the fulcrum upon which the vane element 130 will tip becomes the edge 137B formed by the bevel 134 and the leading face of the vane element 130.
  • the vane 130 is provided with a recessed portion 137C on the lower portion of the rearward face as shown in FIG. 11 so that a fulcrum point 137 is also provided on the rearward face of the vane 130.
  • the moment at point 137B will equal the moment at point 137 less the unbalancing force on the forward side of the vane between the fulcrum points 137B and 137, or:
  • a rotary vane pump comprising (a) a housing provided with a chamber having a peripheral wall,
  • vanes radially slidable in said slots and having outer ends guided in radial extension and retraction by said peripheral wall during rotation of said rotor
  • (e) means providing a fulcrum line between the forward facing portion of said vanes and the adjacent face of said slot and a sealing line between the rearward facing portion of said vanes and the adjacent face of said slot, said fulcrum and sealing lines being at all times at fixed relative positions, whereby when pressure on the rearwardly facing side of said vane is greater than the pressure on the forwardly facing side thereof, said vane will be caused to tip on said fulcrum to produce sealing line contact at the fulcrum line and the sealing line with the faces of said slot.
  • a rotary vane pump comprising,
  • each vane means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the rearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof
  • said means comprising said slot having a radially outward rearwardly facing face portion beveled at an angle with respect to the radially inward portion to provide a fulcrum adjacent the forwardly facing side of said vane on which said vane is caused to tilt, and
  • a rotary pump comprising,
  • vanes radially slidable in said slots and having outer ends guided in radial extensions and retraction by said peripheral wall during rotation of said rotor
  • each vane means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the trearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof,
  • said means comprising said vane having a radially outward face portion beveled at an angle with respect to the radially inward portion to provide a fulcrum adjacent the rearwardly facing face of said slot on which said vane is caused to tilt, and
  • said vane having a shoulder providing an edge adjacent the opposite face of said slot with said line sealing contact being obtained at said edge.
  • a rotary vane pump comprising,
  • vanes radially slidable in said slots and having outer ends guided in radial extension and retraction by said peripheral wall during rotation of said rotor
  • each vane means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the rearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)

Description

0. E. ROSAEN Oct. 12, 1965 PUMPS 4 Sheets-Sheet 1 Filed Aug. 2, 1963 INVENTOR. OSCAR EROSAEN ATTO R NEYS 0. E. ROSAEN Oct. 12, I965 PUMPS 4 Sheets-Sheet 2 Filed Aug. 2, 1963 INVENTOR. OSCAR E.ROSAEN v ATTORNEYS Oct. 12, 1965 o. E. ROSAEN 3,211,104
PUMPS Filed Aug. 2, 1963 4 Sheets-Sheet 5 as. H61
4 A- I; I
34 33 INVENTOR.
OSCAR E.ROSAEN 33A 3 33 BYv A I Fl 6.9. 30
ATTORNEYS 0. E. ROSAEN Oct. 12, 1965 PUMPS 4 Sheets-Sheet 4 Filed Aug. 2, 1963 w e H iGB INVENTOR. O$AR E. ROSAEN ATTORNEYS United States Patent f 3,211,104 PUMPS Oscar E. Rosaen, Grosse Pointe, Mich. Filed Aug. 2, 1963, Ser. No. 303,198 Claims. (Cl. 103-136) The present application is a continuation-in-part of my copending application Ser. No. 90,294, filed Feb. 20, 1961, now abandoned.
The present invention relates to rotary vane type fluid pumps and more particularly to an improvement in pressure balancing of the vanes of such pumps as those I have disclosed in my copending application Ser. No. 765,605, filed Oct. 6, 1958 now Patent No. 3,000,324 issued Sept. 19, 1961 and Ser. No. 765,606, also filed Oct. 6, 1958.
US. Patents Nos. 2,612,114 and 2,612,115 issued to W. Ernst on Sept. 30, 1952 disclose and claim vane type pumps in which pressure balancing of the vanes is achieved by providing an axial bore beneath each vane element and by providing means for regulating the pressure in the axial bores to maintain contact between the ends of the vane element and the cam surface. It has been found that in pumps of the type disclosed in the aforementioned Ernst patents that as the vanes travel through the area between the outlet and the inlet of the pump the inlet suction pressure on the forward face of the vane element and the high outlet pressure on the rearward face of the element causes the element to move against the forward face of the vane slot. The fluid on the rearward side of the vane element then escapes beneath the vane element and because a sealing fit cannot be produced between the vane slot and the forward face of the vane element, fluid beneath the vane element will escape to the suction side of the vane element.
To overcome this problem many other types of pumps have been provided in which slipper elements or the like are provided to replace the vane elements. Such pumps are disclosed in US. Patents Nos. 3,009,420 and 3,009,421, issued to W. T. Livermore et al. on Nov. 21, 1961. Such pump utilize a portion of the pressure beneath the slipper elements to force the depending legs of the elements against the sides of the slots. In this way a seal is produced and the fluid beneath the element is prevented from escaping. Such pumps have the disadvantages that the slipper elements are difficult and expensive to manufacture and high pressures must be maintained beneath the element to insure the necessary contact between the end portions of the element and the cam ring because of the resistance to outward movement of the element produced by the sealing contact between the legs of the element and the sides of the slot.
In the pumps disclosed in my first mentioned copending applications the effectiveness of pressure balancing of the vanes is insured by using vane-like sealing elements positioned intermediate the pumping vanes. The sealing vanes contact the cam ring during travel through the critical area from the outlet or discharge port to the inlet area of the chamber and thus seal the rearward face of the pumping vanes from the high outlet pressure. Although the sealing vanes effectively eliminate the problem in this area of the pumping cycle, they are rather small and hence diflicult to manufacture and handle and constitute an added expense in the manufacture of vane type pumps.
The present invention eliminates the need for such sealing vanes by providing a means of utilizing the differential in pressures in the area between the inlet and the outlet to tip the vane element and produce a sealing engagement between portions of the vane element and the walls of the slot. In this way pressure beneath the vane is sealed in and prevented from escaping.
3,211,104 Pateiited Oct. 12, 1965 One object then of the present invention is to maintain pressure balancing of the vane elements in all areas of the pumping cycle without the necessity of using sealing means.
Another object of the invention is to improve rotary vane pumps by providing vane elements which are ballanced by fluid pressures as nearly as possible in all directions to provide silent operation and elimination of pressure surges.
A further object of the invention is to simplify manufacture, handling and assembly of rotary vane pumps by providing passages for fluid pressure operative to maintain pressure balancing on the vanes at all times.
Yet another object of the invention is to improve rotary vane pump operation by providing pressure balanced vanes which in themselves act, during travel from the outlet areas to the inlet areas of the pumping chamber, to provide a sealing engagement with the sides of the slot to maintain a separation of the fluid pressures acting on the vane elements during such periods of travel.
For a more complete understanding of the present invention, reference may be had to the accompanying drawings in which like reference characters refer to like parts throughout the several views and in which FIG. 1 is a longitudinal cross-sectional view of a preferred rotary vane pump embodying the invention and as taken substantially on the line 11 of FIG. 2.
FIG. 2 is a cross sectional view of the pump taken substantially on the line 22 of FIG. 1.
FIG. 3 is a cross-sectional view of the pump taken substantially on the line 2-2 of FIG. 1.
FIG. 4 is a cross-sectional view of a cheek plate portion of the pump on a plane normal to the plane of the cross-section of FIG. 1.
FIG. 5 is an axial elevational view of the rotor and cam components of the pump.
FIG. 6 is a side elevational View of the cam component shown in FIG. 5.
FIG. 7 is an elevational plan view of'a vane embodied in the pump rotor.
FIG. 8 is an end elevational view of said vane.
FIG. 9 is a cross-sectional view taken substantially on line 9-9 of FIG. 7.
FIG. 10 is an enlarged fragmentary elevational view of structure shown in FIG. 5, and
FIG. 11 is a view similar to FIG. 10 but illustrating another preferred construction of the pump of the present invention.
Description The preferred pump 10 comprises a housing structure 11 provided with an end plate 12 enclosing a substantially cylindrical pumping chamber 13. An inner cheek plate 14 and an outer cheek plate 15 are disposed in the chamber 13 with an annular cam ring 16 disposed between them and having a cam surface 16A forming the peripheral surface of a rotor chamber 16B. A rotor 17 is rotatably carried in the chamber 16B and is keyed to a drive shaft 18 supported by a bearing 18A at one end of the housing 11 and a bushing 18B mounted in the outer cheek plate 15.
The housing 11 has a fluid inlet 19 connected with similar and diametrically opposite inlet grooves 20 in the sides of the chamber 13 to form passages extending axially between the wall of the chamber 13 and the outer surfaces of the cam ring 16.
The grooves 20 admit fluid to intake openings 21 in the cam ring 16, fluid thence entering the rotor chamber 16B at what is for purposes of discussion herein called the inlet areas of the chamber 16B. The openings 21 are elongated as at grooves 21A shown in FIGS. 2 and 5 to provide inlet areas greater in annular length than the space between two adjacent rotor vanes.
Fluid will be impelled annularly around the spaces of the rotor chamber 16B between the cam surfaces 16A and the rotor 17 to an outlet area in the location of cam surface slopes 22. A pair of diametrically opposite axially extending discharge openings 23 are provided in the cam ring 16 and are connected by grooves 23A with the outlet areas of the rotor chamber 16B. The grooves 23A, like the grooves 21A, are greater in annular length than the space between adjacent rotor vanes. Fluid from the discharge openings 23 is forced under pressure out through passages 24 provided in the inner cheek plate 14, through discharge passages 25 and 26 in the housing 11 to a pressure fluid outlet 27.
The ressure flow is produced by means of a plurality of axially elongated rotor vanes 30 radially slidably carried in a plurality of equally annularly spaced slots 31 provided around the periphery of the rotor 17.
Each slot 31 communicates at its inner end with axially bored holes 32 as shown. In operation, as the rotor 17 turns, the outer edges of the vanes 30 are quided along the cam surfaces 16A, the vanes 30 retracting in the slots 31 as they follow the cam slopes 22. Fluid is thus impelled from the inlet to the outlet areas.
Each vane 30, as shown in FIGS. 7, 8 and 9, is provided on its forward face with a radialy extending groove 33 and the forward outer edge is beveled as at 34 to provide substantially line contact between the vanes 30 and the cam surface 16A, the vanes thereby being readily held outward by the pressure under the vanes as will be described, the outer end 33A of the groove 33 being spaced slightly from the bevel 34.
As shown in FIGS. 2 and 5, the forward outer edges of the slots 31 are beveled as at 31A. When the vanes 30 are extended during travel from the inlet to the outlet areas of the chamber 163, the outer ends 33A of the grooves 33 are radially outward of the slot bevel 31A, the fluid presure is transmitted to the inner ends of the slots at the holes 32, so that both ends of the vanes 30 are subjected to substantially equal pressures. Moreover, as the vanes move from the inlet to the outlet areas, pressure on the forward face is substantially balanced against the pressure on the rearward face, in the same fashion as that described in my prior patents. Thus, as pressure rises in the chamber 16B ahead of each vane, the pressure also rises equally underneath the vanes 32, providing for extremely silent operation with practically no pressure surges.
A difference occurs, however, as each vane 30 is re- I tracted by the cam slope 22. Then the groove 33 is closed off by the slot 31, so that, as the vanes move from the outlet area to the inlet area, communication between the holes 32 and suction side of the vane 30 is substantially closed. Without more, however, the high pressure on the outlet side of the vane element 30 and the suction pressure on the inlet side of the vane element 30 would coact to press the vane element 30 against the forward face of the slot 31. Outlet pressure would then enter the hole 32 and escape between the leading face of the vane element 30 and the wall of the slot 31 to the suction side of the element 30. To prevent this, the slots 31 are beveled as at 31A. As can best be seen in FIG. the slot bevel 31A provides a fulcrum at 37B which permits the vanes 30 to tip. As the vane element 30 enters the area between the outlet and the inlet a pressure differential is produced across the extended end of the vane element 30. The pressures between the faces of the vane element and the sides of the slot 31 as well as the pressure beneath the vane element 30 will vary but will be somewhat intermediate the suction pressure on the forward face of the extended portion of the vane element 30 and the high outlet pressure on the rearward face of the extended portion of the vane element 30. For this reason the vane element 30 will be caused to tip forward as illustrated in FIG. 10 and cause a substantially tight line contact between the rearward faces of the vanes and the inner edge of the slots 31 at the point 37 shown in FIGS. 5 and 10, and also between the forward faces of the vanes 30 and the outer edge of the slots 31 at the point 37B, preventing leakage of pressure past the vanes 30.
It is apparent that without the slot bevel 31A not enough of the surface of the vane elements 30 would be exposed to the suction pressure and outlet presure to produce the tipping required to effectively seal the holes 32. The slot bevel 31A performs the dual function of promoting tipping of the vane element 30 by exposing a greater portion of the vane element to the pressure differential which produces the tipping and by providing the fulcrum point 37B upon which the vane element 30 can tip as well as providing the closing point of the groove 33 below the halfway point of balance between the inner and outer ends of the slot 31. In the embodiment illus trated in FIGS. 1-10 the beveled face 34 of the vane elements 30 provide substantially line contact between the vanes 30 and the cam surface 16A.
In order to equalize the pressure on the outer ends of the vanes 30 with the pressure sealed behind the vanes 30 as the grooves are closed off on retraction and the vanes tip as described above, a port 35 is provided in the inner cheek plate 14 in a position to register momentarily with the holes 32 at the inner ends of the slots 31 as they successively pass from the outlet areas. The ports 35 are openly connected with the outlet passages 24 by means of passages 36.
As the vanes 30 reach the inlet areas, and begin to extend the holes 32 move into registry, with elongated slots 38 provided in both inner and outer cheek plates 14 and 15. These slots communicate with the housing inlet grooves 20 via radially extending passages 39. This admits substantially atmospheric pressure to the inner ends of the vanes 30, the outer ends thereof being subjected to the less than atmospheric pressure at the inlet areas of the chamber 16B, causing the vanes 30 to extend.
FIG. 11 is a view similar to FIG. 10 but illustrates a preferred modification of the present invention. In FIG. 10, it will be noted the beveled face 34 of the vane element 30 is angled such that when the vane element 30 is in the retracted position, the edge of the bevel 34 and the leading face of the vane element is disposed above the line 37B. In this way the edge of the slot bevel 31A acts as the fulcrum upon which the vane element 30 is tipped. By extending the length of the bevel 134 of the vane element as shown in FIG. 11, the fulcrum upon which the vane element 130 will tip becomes the edge 137B formed by the bevel 134 and the leading face of the vane element 130.
The vane 130 is provided with a recessed portion 137C on the lower portion of the rearward face as shown in FIG. 11 so that a fulcrum point 137 is also provided on the rearward face of the vane 130.
It is possible in either of the modifications described above to regulate the pressure permitted in the hole 32 before the vane elements 30 or 130 tips by changing the position of the fulcrum 37B, 137B, 137. In this way, the force with which the vane 30 or 130 engages the cam surface 16A can be regulated. The embodiment illustrated in FIG. 11 has the added advantage that this can be readily accomplished. All that is necessary is to replace the vane elements 130 with new vanes having the desired fulcrum point.
For example, if the dimensions shown in FIG. 11 are used, and the pump is operating at 1000 p.s.i., then the moment at point 137B will equal the moment at point 137 less the unbalancing force on the forward side of the vane between the fulcrum points 137B and 137, or:
6-1000-3 equals 8-l0OO-4(84 P) P equals 437 Where P is the pressure in p.s.i. under the vane. The
force under the vane, which is one inch wide, urging it against the cam ring will thus be 51 lbs. since 3 mm. equals 0.117 in. and
0.117 437 1" equals 51 Therefore, it is clear that choosing the positions of the fulcrums actualy makes-the vane itself regulate the effective pressure under the vane to whatever value is desired.
It is also apparent that although I have described but two modifications of my invention, many changes can be made without departing from the spirit of the invention as expressed by the scope of the appended claims.
I claim:
1. A rotary vane pump comprising (a) a housing provided with a chamber having a peripheral wall,
(b) annularly spaced inlet and outlet ports connected respectively with suction and pressure portions of said chamber,
() a rotor rotatable in said chamber and having annularly spaced radially extending slots,
(d) vanes radially slidable in said slots and having outer ends guided in radial extension and retraction by said peripheral wall during rotation of said rotor,
(e) means providing a fulcrum line between the forward facing portion of said vanes and the adjacent face of said slot and a sealing line between the rearward facing portion of said vanes and the adjacent face of said slot, said fulcrum and sealing lines being at all times at fixed relative positions, whereby when pressure on the rearwardly facing side of said vane is greater than the pressure on the forwardly facing side thereof, said vane will be caused to tip on said fulcrum to produce sealing line contact at the fulcrum line and the sealing line with the faces of said slot.
2. A rotary vane pump comprising,
(a) a housing provided with a chamber having a peripheral wall,
(b) annularly spaced inlet and outlet ports connected respectively with suction and pressure portions of said chamber,
(c) a rotor rotatable in said chamber and having spaced radial slots,
((1) vanes radially slidable in said slots and having outer ends guided in radial extension and retraction by said peripheral wall during rotation of said rotor,
(e) means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the rearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof,
(f) said means comprising said slot having a radially outward rearwardly facing face portion beveled at an angle with respect to the radially inward portion to provide a fulcrum adjacent the forwardly facing side of said vane on which said vane is caused to tilt, and
(g) said slot having a shoulder providing an edge adjacent the opposite side of said vane with said line sealing contact being obtained at said edge. 3. The pump as defined in claim 2 and in WhlCh the inner end of the beveled portion of said slot is located about midway between the inner and outer ends of the slot.
4. A rotary pump comprising,
(a) a housing provided with a chamber having a peripheral Wall,
(b) annularly spaced inlet and outlet ports connected respectively with suction and pressure portions of said chamber,
(c) a rotor rotatable in said chamber and having spaced radial slots,
(d) vanes radially slidable in said slots and having outer ends guided in radial extensions and retraction by said peripheral wall during rotation of said rotor,
(e) means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the trearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof,
(f) said means comprising said vane having a radially outward face portion beveled at an angle with respect to the radially inward portion to provide a fulcrum adjacent the rearwardly facing face of said slot on which said vane is caused to tilt, and
(g) said vane having a shoulder providing an edge adjacent the opposite face of said slot with said line sealing contact being obtained at said edge.
5. A rotary vane pump comprising,
(a) a housing provided with a chamber having a peripheral wall,
(b) annularly spaced inlet and outlet ports connected respectively with suction and pressure portions of said chamber,
(c) a rotor rotatable in said chamber and having spaced radial slots,
(d) vanes radially slidable in said slots and having outer ends guided in radial extension and retraction by said peripheral wall during rotation of said rotor,
(e) means causing each vane to tilt in its slot to make line sealing contact therewith when pressure on the rearwardly facing side of the vane is greater than the pressure on the forwardly facing side thereof,
(f) the inner end of said slots each having an enlarged portion defining an edge on the inner end of the forwardly facing face making line contact with the rearward face of the vane when it tilts, and
(g) said slot having a fulcrum on the opposite face making line contact with the forward face of the vane.
References Cited by the Examiner UNITED STATES PATENTS 2,371,081 3/45 Tucker et al. 103--136 2,435,279 2/48 I-Iubacker 103-136 3,008,424 11/61 Roth 103-136 3,076,415 2/63 Farron 103136 3,159,336 12/64 Paschke 230 FOREIGN PATENTS 30,312 10/59 Finland.
DONLEY J. STOCKING, Primary Examiner.
JOSEPH H. BRANSON, 111., Examiner.

Claims (1)

1. A ROTARY VANE PUMP COMPRISING (A) A HOUSING PROVIDED WITH A CHAMBER HAVING A PERIPHERAL WALL, (B) ANNULARLY SPACED INLET AND OUTLET PORTS CONNECTED RESPECTIVELY WITH SUCTION AND PRESSURE PORTIONS OF SAID CHAMBER, (C) A ROTOR ROTATABLE IN SAID CHAMBER AND HAVING ANNULARLY SPACED RADIALLY EXTENDING SLOTS, (D) VANES RADIALLY SLIDABLE IN SAID SLOTS AND HAVING OUTER ENDS GUIDED IN RADIAL EXTENSION OF SAID ROTOR, BY SAID PERIPHERAL WALL DURING ROTATION OF SAID ROTOR, (E) MEANS PROVIDING A FULCRUM LINE BETWEEN THE FORWARD FACING PORTION OF SAID VANES AND THE ADJACENT
US303198A 1963-08-02 1963-08-02 Pumps Expired - Lifetime US3211104A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US303198A US3211104A (en) 1963-08-02 1963-08-02 Pumps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US303198A US3211104A (en) 1963-08-02 1963-08-02 Pumps

Publications (1)

Publication Number Publication Date
US3211104A true US3211104A (en) 1965-10-12

Family

ID=23170962

Family Applications (1)

Application Number Title Priority Date Filing Date
US303198A Expired - Lifetime US3211104A (en) 1963-08-02 1963-08-02 Pumps

Country Status (1)

Country Link
US (1) US3211104A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3380392A (en) * 1966-05-12 1968-04-30 Owatonna Tool Co Low-pressure roller pump
FR2469581A1 (en) * 1979-11-13 1981-05-22 Seiko Seiki Kk Rotary compressor with seal strips slidable in rotor slots - has slots widened at outer ends to prevent jamming of deformed strip tips
DE3034411A1 (en) * 1980-09-12 1982-04-22 Daimler-Benz Ag, 7000 Stuttgart PISTON OF A WING PISTON PUMP FOR HYDRAULIC PRODUCTS
US4552512A (en) * 1983-08-22 1985-11-12 Permutare Corporation Standby water-powered basement sump pump
EP0173049A2 (en) * 1984-08-31 1986-03-05 Rineer Hydraulics, Inc. Improved vane slots for a fluid power converter
US4610614A (en) * 1984-02-01 1986-09-09 Toyoda Koki Kabushiki Kaisha Vane pump
US4746280A (en) * 1987-02-19 1988-05-24 Corken International Corporation Sliding vane pump
US5083909A (en) * 1990-11-29 1992-01-28 The United States Of America As Represented By The Secretary Of The Navy Seawater hydraulic vane type pump
DE102008002763A1 (en) * 2008-02-01 2009-08-06 Zf Lenksysteme Gmbh Sliding vane pump, particularly for power steering of commercial motor vehicles, has rotor that consists of radially moving wing guided in slot, where wing forms wing head which with contact edge glides along inner contour of cam ring
US20140271310A1 (en) * 2013-03-14 2014-09-18 Woodward, Inc. Clubhead Vane Pump With Balanced Vanes

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2371081A (en) * 1941-02-06 1945-03-06 Hydraulic Dev Corp Inc Vane pump
US2435279A (en) * 1943-10-25 1948-02-03 Borg Warner Pump, vane type
FI30312A (en) * 1955-12-30 1959-04-10 Rotary piston pump
US3008424A (en) * 1958-03-07 1961-11-14 Mechanisms Company Hydraulic wheel
US3076415A (en) * 1960-01-08 1963-02-05 Bendix Corp Reversible vane fluid power device such as a pump or motor
US3159336A (en) * 1961-05-13 1964-12-01 Nsu Motorenwerke Ag Non-jamming apex seal

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2371081A (en) * 1941-02-06 1945-03-06 Hydraulic Dev Corp Inc Vane pump
US2435279A (en) * 1943-10-25 1948-02-03 Borg Warner Pump, vane type
FI30312A (en) * 1955-12-30 1959-04-10 Rotary piston pump
US3008424A (en) * 1958-03-07 1961-11-14 Mechanisms Company Hydraulic wheel
US3076415A (en) * 1960-01-08 1963-02-05 Bendix Corp Reversible vane fluid power device such as a pump or motor
US3159336A (en) * 1961-05-13 1964-12-01 Nsu Motorenwerke Ag Non-jamming apex seal

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3380392A (en) * 1966-05-12 1968-04-30 Owatonna Tool Co Low-pressure roller pump
FR2469581A1 (en) * 1979-11-13 1981-05-22 Seiko Seiki Kk Rotary compressor with seal strips slidable in rotor slots - has slots widened at outer ends to prevent jamming of deformed strip tips
DE3034411A1 (en) * 1980-09-12 1982-04-22 Daimler-Benz Ag, 7000 Stuttgart PISTON OF A WING PISTON PUMP FOR HYDRAULIC PRODUCTS
US4552512A (en) * 1983-08-22 1985-11-12 Permutare Corporation Standby water-powered basement sump pump
US4610614A (en) * 1984-02-01 1986-09-09 Toyoda Koki Kabushiki Kaisha Vane pump
EP0173049A2 (en) * 1984-08-31 1986-03-05 Rineer Hydraulics, Inc. Improved vane slots for a fluid power converter
US4599058A (en) * 1984-08-31 1986-07-08 Rineer Hydraulics, Inc. Vane slots for a fluid power converter
EP0173049A3 (en) * 1984-08-31 1987-05-06 Rineer Hydraulics, Inc. Improved vane slots for a fluid power converter
US4746280A (en) * 1987-02-19 1988-05-24 Corken International Corporation Sliding vane pump
US5083909A (en) * 1990-11-29 1992-01-28 The United States Of America As Represented By The Secretary Of The Navy Seawater hydraulic vane type pump
DE102008002763A1 (en) * 2008-02-01 2009-08-06 Zf Lenksysteme Gmbh Sliding vane pump, particularly for power steering of commercial motor vehicles, has rotor that consists of radially moving wing guided in slot, where wing forms wing head which with contact edge glides along inner contour of cam ring
US20140271310A1 (en) * 2013-03-14 2014-09-18 Woodward, Inc. Clubhead Vane Pump With Balanced Vanes

Similar Documents

Publication Publication Date Title
US3311064A (en) Vane-type rotary pumps
US3102494A (en) Rotary vane hydraulic power unit
US3211104A (en) Pumps
US4505654A (en) Rotary vane device with two pressure chambers for each vane
US6050796A (en) Vane pump
GB1423545A (en) Vane pump having extended undervane suction ports
US3221665A (en) Hydraulic pump or motor with hydraulic pressure-responsive vane
GB1565969A (en) Sliding-vane type hydraulic rotary machine
US4286933A (en) Rotary vane pump with pairs of end inlet or outlet ports
GB1505762A (en) Axial piston machines
US2880677A (en) Variable volume vane pump
GB1500107A (en) Rotary sliding-vane liquid pump
US3014431A (en) Sliding vane pump
US6481992B2 (en) Vane pump
GB1251816A (en)
US2428181A (en) Rotary gear pump
US3000324A (en) Vane for rotary pumps
US3254606A (en) Constant delivery pump
US3254570A (en) Motor
US4021166A (en) Rotary vane compressor with increased outlet through-flow area
US3314368A (en) Rotary piston pump with retractable cam sealing elements
US2968252A (en) Engine
US3128708A (en) Pump
US2902942A (en) Rotary pumps
US2918873A (en) Rotary vane pump or motor