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EP0058456A1 - A rotating vane-pump or -motor - Google Patents

A rotating vane-pump or -motor Download PDF

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Publication number
EP0058456A1
EP0058456A1 EP82200165A EP82200165A EP0058456A1 EP 0058456 A1 EP0058456 A1 EP 0058456A1 EP 82200165 A EP82200165 A EP 82200165A EP 82200165 A EP82200165 A EP 82200165A EP 0058456 A1 EP0058456 A1 EP 0058456A1
Authority
EP
European Patent Office
Prior art keywords
rotor
casing
vanes
structure according
wall
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.)
Withdrawn
Application number
EP82200165A
Other languages
German (de)
French (fr)
Inventor
Abraham De Kok
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
Publication of EP0058456A1 publication Critical patent/EP0058456A1/en
Withdrawn legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • F01C21/0809—Construction of vanes or vane holders
    • F01C21/0818—Vane tracking; control therefor
    • F01C21/0827—Vane tracking; control therefor by mechanical means
    • F01C21/0836—Vane tracking; control therefor by mechanical means comprising guiding means, e.g. cams, rollers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00—Sealing arrangements in rotary-piston machines or engines
    • F01C19/08—Axially-movable sealings for working fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08—Rotary pistons
    • 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
    • F04C2240/00—Components
    • F04C2240/80—Other components
    • F04C2240/801—Wear plates

Definitions

  • This invention relates to a rotating vane-pump or -motor provided with a circular-cylindrical rotor with slots in which vanes are guided slidingly, which rotor is supported eccentrically in a casing with a circular-cylindrical interior, which is closed at both ends by internally substantially plane end faces.
  • the structure is improved acccrdinc to the invention in essence by making the movement of the vanes independentfromthe speed of rotation and by providing very good sliding seals between casing and rotor and between casing and vanes.
  • Fi g . 1 shows an exploded view of a simple embodiment of a rotating vane- pump or -motor.
  • the means for causing the rad movement of the vanes 10 include a cam or disc 12 on each si rigidly connected to the covers 3 of the casing 1.
  • the slidi seal between the end faces of the rotor 8 and the covers 3 is obtained by segmental plates 22 between the vanes 10, which ; plates are supported under pressure of springs 24 in annular chambers 23 in the ends of the rotor 8.
  • the vanes themselves are provided with slot shaped recesses along the sides directed to the inner wall of the casing, said recesses taking up resilient sealing strips 42.
  • Fig. 2 shows a partial axial section of such a structure according to the invention, in which in an open chamber 11 concentric with the rotor axis and in the ends thereof there is a separate and as such freely rotatable ring 14 between the ends of the vanes directed towards the axis, which ring provides for the control of the movement of the vanes.
  • Fig. 3 shows a similar view and section of part of the structure with a loose rotatable ring 14 as in Fig. 2, but here active in a recessed corner 18 at the ends of the sides of the vanes directed towards the axis, ring 14 being shown at a distance from its operative position in recessed parts 18
  • Fig. 4 shows a similar view and section as Figures 2 and 3, in which the vanes 10 have a recess 19 opening towards the adjacent cover of the casing and taking up the separate movablf control ring 14, which in this case controls movement of the vanes positively both outwardly and inwardly.
  • Fig. 5 shows an exploded view of the same part of a structure according to the invention in a further embodiment in which the casing cover 3 is provided with a circular hub 17 concentric with the axis of the rotor and having a separate and separately rotatable ring 14 which, in this case, is of greater axial length to engage both around this hub 17 and in the recesses 19 of the vanes 10.
  • Fig. 6 shows a diagrammatic end view of a rotor of a structure according to the invention in another embodiment in which the vanes 10 at their ends near the axis of the rotor have a widened part 20 giving a better contact with the controlmembers such as control ring 14.
  • the vanes have inner end faces perpendicular to their radial direction so as to compensate for differences in contact angle by the eccentric position of the rotor in the casing.
  • Fig. 7 shows an end view of a rotor of a structure according to the invention, having, as in Fig. 1, separate segments 22 between the vanes 10. These segments are made of particularly wear-resistant and/or self-lubricating material and are taken up in an annular chamber in the rotor between the vanes, while they are resiliently pressed against the casing covers by springs 24.
  • Fig. 8 shows from a direction inclined with respect to the axis the end of a rotor of a structure according to the invention with a chamber with a deeper portion 11 and a shallow portion 26 outwardly thereof.
  • a disc 25 of wear-resistant and/or self-lubricating sealing material has a central hole 28 and radial slots 27 for taking up the ends of the vanes.
  • Fig. 9 shows the end of a rotor with an end disc 29 embodied as a cap engaging and slidingly fitting around an end part 30 of the rotor with smaller diameter.
  • Fig. 10 shows an exploded view of an embodiment of the structure according to the invention with the rotor 8 having in a recessed annular part 34 at both ends an annular body ? of wear-resistant and/or self-lubricating material having radial slots 33 for taking up the ends of the vanes.
  • the end covers 3 of the casing have an annular recess part 35 for taking up the outer ends of the rings 32 axiall outside the slots 33 so as to have the rings 32 fitting but being easily rotatable therein.
  • Fig. 11 shows an axial section for the movable sealing between the rotor and the casing cover, the rotor 8 having at its outer periphery a protruding annular part 37 engagi by a sliding fit in an annular chamber 38 of casing cover with interposition of wear-resistant material.
  • This material may be resilient to give a good sealing.
  • the annular chamber 38 may engage around the protruding part 37 with some clearance and this chamber 38 may be filled by grease of sufficiently high viscosity.
  • Fig. 12 shows diagrammatically a vane 10 for a structure according to the invention in front and end view, the vane having a slot shaped recess in which three separate sealing strips are mounted with a sliding fit. These strips may be maintained in sealing contact with the cylinder wall and the casing covers under a resilient pressure.
  • Fig. 13 shows this vane 10 of Fig. 12 in section parallel to its side faces and through the slot taking up the sealing strips.
  • the slot is indicated by 47, the side sealing strips by 42 and the outer sealing strip by 48.
  • a spring 51 embodied as a resilient wire of leafspring is positioned in the bottom of the slot 47 to urge the sealing strips 42 and 48 outwardly. The ends of this spring are bent outwardly as at 52.
  • Fig. 14 shows in perspective an embodiment of the sealing strips indicated by 49 giving a better and uninterrupted sealing around three sides of the vane
  • Fig. 15 shows such a sealing strip embodiment in position on the vane 10 in a peripheral slot 47 thereof as in Fig. 13.
  • the ends of the spring 51 are bent inwardly at 52 and are taken up in suitable small openings in the bottom of the recess 47.
  • Fig. 16 shows an embodiment of a pump according to the invention with an end cover removed and seen axially from one end.
  • the fluid enters through inlet 7 and leaves the design through outlet 6. It is always necessary to have a sufficient running clearance between the rotor and the casing, the vanes providing for the sealing between inlet 7 and outlet 6, with their different pressures.
  • the invention provides between the outlet 6 and the inlet 7 for a bypass opening 53 in the pumpcasing; said bypass opening 53 is positioned such that between the outlet 6 and opening 53 and between opening 53 and inlet 7 there is at any time at least one vane.
  • the bypass opening 54 between inlet 7 and the outlet 6, being separated from each at any time by at least one vane.
  • the bypass openings53 and 54 are interconnected by a pipe, hose or the like 55.
  • Said bypass duct 55 thus forms a connection between the spaces with the smallest dead volume, as soon as this volume is separated from the outlet opening by at least one vane and still separated by at least one vane from the inlet opening and another space with lower pressure in the suction-sector of the pump which is also separated from the suction-opening and the outlet opening by at least one vane.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rotary Pumps (AREA)
  • Details And Applications Of Rotary Liquid Pumps (AREA)

Abstract

The invention discloses designmeasures to improve the (volumetric) efficiency of known rotating vane-type pumps or -motors.
A control-means (12,14) is disclosed which mechanically controls the radial inward and outward movements of each vane (10) in its slot (9) in the rotor (11) during its rotation along the cylindrical inner-running-surface (2) of the housing (1) of the machine, in addition to the normal centrifugal force acting on the vanes (10).
Additional springs urging the vanes outward and appropriate wear-resisting running- and sealing inlays (42) for the vanes sliding over the housing and the endcovers are resealed as well. So are sealingrings (22) or-plates between the rotor-end faces and the endcovers. All the above measures reducing blow-by and wear.

Description

  • This invention relates to a rotating vane-pump or -motor provided with a circular-cylindrical rotor with slots in which vanes are guided slidingly, which rotor is supported eccentrically in a casing with a circular-cylindrical interior, which is closed at both ends by internally substantially plane end faces.
  • Such rotating machines are known already a long time, not only as pumps but also as pneumatic motors. Both embodiments have found a wide field of application notwithstanding the often low efficiency as a result of internal leakage and the dependency on the speed of rotation for moving the vanes outwardly in the correct time intervals and angular regions.
  • It is an object of this invention to increase the efficiency of such structures considerably while maintaining the existing advantages. By such an improvement it is possible to apply a very much wider field of applications both as pumps and as motors, to increase the applicability and suitability of the structure and it is thereby also possible to choose a more compact structure for the same purpose and output, in which it is even possible to apply wider manufacturing tolerances of the composing parts and an easier assembly.
  • To obtain this object the structure is improved acccrdinc to the invention in essence by making the movement of the vanes independentfromthe speed of rotation and by providing very good sliding seals between casing and rotor and between casing and vanes.
  • The invention will now be explained further with referen to the enclosed drawings showing by way of example several possible embodiments, in which description features and advar tages of the invention will become apparent. Fig. 1 shows an exploded view of a simple embodiment of a rotating vane- pump or -motor. The means for causing the rad movement of the vanes 10 include a cam or disc 12 on each si rigidly connected to the covers 3 of the casing 1. The slidi seal between the end faces of the rotor 8 and the covers 3 is obtained by segmental plates 22 between the vanes 10, which ; plates are supported under pressure of springs 24 in annular chambers 23 in the ends of the rotor 8. The vanes themselves are provided with slot shaped recesses along the sides directed to the inner wall of the casing, said recesses taking up resilient sealing strips 42.
  • Fig. 2 shows a partial axial section of such a structure according to the invention, in which in an open chamber 11 concentric with the rotor axis and in the ends thereof there is a separate and as such freely rotatable ring 14 between the ends of the vanes directed towards the axis, which ring provides for the control of the movement of the vanes.
  • Fig. 3 shows a similar view and section of part of the structure with a loose rotatable ring 14 as in Fig. 2, but here active in a recessed corner 18 at the ends of the sides of the vanes directed towards the axis, ring 14 being shown at a distance from its operative position in recessed parts 18
  • Fig. 4 shows a similar view and section as Figures 2 and 3, in which the vanes 10 have a recess 19 opening towards the adjacent cover of the casing and taking up the separate movablf control ring 14, which in this case controls movement of the vanes positively both outwardly and inwardly.
  • Fig. 5 shows an exploded view of the same part of a structure according to the invention in a further embodiment in which the casing cover 3 is provided with a circular hub 17 concentric with the axis of the rotor and having a separate and separately rotatable ring 14 which, in this case, is of greater axial length to engage both around this hub 17 and in the recesses 19 of the vanes 10.
  • Fig. 6 shows a diagrammatic end view of a rotor of a structure according to the invention in another embodiment in which the vanes 10 at their ends near the axis of the rotor have a widened part 20 giving a better contact with the controlmembers such as control ring 14. The vanes have inner end faces perpendicular to their radial direction so as to compensate for differences in contact angle by the eccentric position of the rotor in the casing.
  • Fig. 7 shows an end view of a rotor of a structure according to the invention, having, as in Fig. 1, separate segments 22 between the vanes 10. These segments are made of particularly wear-resistant and/or self-lubricating material and are taken up in an annular chamber in the rotor between the vanes, while they are resiliently pressed against the casing covers by springs 24.
  • Fig. 8 shows from a direction inclined with respect to the axis the end of a rotor of a structure according to the invention with a chamber with a deeper portion 11 and a shallow portion 26 outwardly thereof. A disc 25 of wear-resistant and/or self-lubricating sealing material has a central hole 28 and radial slots 27 for taking up the ends of the vanes. There may be spring means not shown such as 24 in Fig. 1 and 7 to push this disc 25 towards the adjacent casing cover, and there may be a pin 31 on the rotor in shallow chamber portion 26 engaging a hole in the disc 25 to avoid that the entire force for rotating disc 25 with the rotor should be exerted by the vanes only.
  • Fig. 9 shows the end of a rotor with an end disc 29 embodied as a cap engaging and slidingly fitting around an end part 30 of the rotor with smaller diameter. There are spring: 24 for urging this cap against the inner end face of the casing and pins 31 engaging in holes in disc 29 to keep this disc in position.
  • Fig. 10 shows an exploded view of an embodiment of the structure according to the invention with the rotor 8 having in a recessed annular part 34 at both ends an annular body ? of wear-resistant and/or self-lubricating material having radial slots 33 for taking up the ends of the vanes. In thi: case, the end covers 3 of the casing have an annular recess part 35 for taking up the outer ends of the rings 32 axiall outside the slots 33 so as to have the rings 32 fitting but being easily rotatable therein.
  • Fig. 11 shows an axial section for the movable sealing between the rotor and the casing cover, the rotor 8 having at its outer periphery a protruding annular part 37 engagi by a sliding fit in an annular chamber 38 of casing cover with interposition of wear-resistant material. This material may be resilient to give a good sealing. Instead thereof the annular chamber 38 may engage around the protruding part 37 with some clearance and this chamber 38 may be filled by grease of sufficiently high viscosity. There may be sealing material in the remainder of this end face of the rotor and at the righthand end of the rotor as indicated by 21.
  • Fig. 12 shows diagrammatically a vane 10 for a structure according to the invention in front and end view, the vane having a slot shaped recess in which three separate sealing strips are mounted with a sliding fit. These strips may be maintained in sealing contact with the cylinder wall and the casing covers under a resilient pressure.
  • Fig. 13 shows this vane 10 of Fig. 12 in section parallel to its side faces and through the slot taking up the sealing strips. The slot is indicated by 47, the side sealing strips by 42 and the outer sealing strip by 48. A spring 51 embodied as a resilient wire of leafspring is positioned in the bottom of the slot 47 to urge the sealing strips 42 and 48 outwardly. The ends of this spring are bent outwardly as at 52.
  • Fig. 14 shows in perspective an embodiment of the sealing strips indicated by 49 giving a better and uninterrupted sealing around three sides of the vane; and
  • Fig. 15 shows such a sealing strip embodiment in position on the vane 10 in a peripheral slot 47 thereof as in Fig. 13. In this case, the ends of the spring 51 are bent inwardly at 52 and are taken up in suitable small openings in the bottom of the recess 47.
  • Fig. 16 shows an embodiment of a pump according to the invention with an end cover removed and seen axially from one end. The fluid enters through inlet 7 and leaves the design through outlet 6. It is always necessary to have a sufficient running clearance between the rotor and the casing, the vanes providing for the sealing between inlet 7 and outlet 6, with their different pressures.
  • Nevertheless it cannot be avoided that more than negligible fluid-volumes are moved along by said clearance-spaces from the outletsectorto the inletsector, causing appreciable volumetric losses.
  • According to the execution as shown in Fig. 16, the invention provides between the outlet 6 and the inlet 7 for a bypass opening 53 in the pumpcasing; said bypass opening 53 is positioned such that between the outlet 6 and opening 53 and between opening 53 and inlet 7 there is at any time at least one vane. The same is true for the bypass opening 54 between inlet 7 and the outlet 6, being separated from each at any time by at least one vane. The bypass openings53 and 54 are interconnected by a pipe, hose or the like 55. Said bypass duct 55 thus forms a connection between the spaces with the smallest dead volume, as soon as this volume is separated from the outlet opening by at least one vane and still separated by at least one vane from the inlet opening and another space with lower pressure in the suction-sector of the pump which is also separated from the suction-opening and the outlet opening by at least one vane. In doing so, with the machine working as compressor, "pumping around" compressed fluid and the compressed fluid-losses due to this, as well as still further increasing losses in case the backpressure at the outlet increases, are substantially avoided. Higher compression ratios in one stage become possible as well. Should this machine act as vacuumpump, then through said bypass fluid will be sucked out from the spaces with the smallest dead volume (generally filled with fluid at atmosferic pressure) by an inactive space with reduced pressure. As a result an appreciably lower vacuum can be attained

Claims (22)

1. A rotating vane-pump or -motor provided with a circular-cylindrical rotor(8)with slots (9) in which vanes 10 are guided slidingly, which rotor(8)is supported eccentricall in an internally circular-cylindrical casing(l)closed at both ends by covers(3)of mainly plane inner surface characterized in that at at least one of the axial ends of the rotor(8) within the outer periphery thereof there are control members (12, 14 or 17) keeping the vanes(10)constantly in contact with the cylinder wall(2)of the casing(l).
2. A structure according to claim 1, characterized in that on at least one of the casing covers(3)a disc or cam(12) is provided, concentrically with the cylindrical inner wall of the casing, the vanes (10) being guided slidingly by the periphery of this disc or cam(12)between it and the inner wall(2)of the casing(l).
3. A structure according to claim 2 characterized in that a preferably circular-cylindrical disc , annular cam or ring(14)is freely movable with the rotor(8).
4. A structure according to claim 1 characterized in that in at least one of the end walls of the rotor concentrically therewith a circular chamber(ll)is provided in which a separate disc or cam ring(14)is present, having a periphery axially parallel to the inner cylindrical wall(2)of the casing(l)and that all the vanes (10) have parts fitting slidingly between the periphery(16)of the disc or of the cam and the inner wall(2)of the casing (1).
5. A structure according to claim 4 characterized in that the cam ring (14)is rotatably supported about a circular hub (17) rigid to the casing cover (3).
6. A structure according to any of the preceding claims characterized in that in an endwall of the rotor(8)concentric cally therewith a circular chamber (11) is recessed in which a separate circular disc with a periphery axially parallel to the internal cylinder wall(2)of the casing (1) is provided and that the vanes(10)have parts making a sliding fit between the periphery of the disc and the inner wall(2)of the casing(l), the rotor shaft(5)being supported rotatably only in the casing cover (3) at the other end of the rotor.
7. A structure according to any of the preceding claims characterized in that the vanes(10)slide in contact with the cam rings(14)or the discs (12) with the side of a recess(18), which is directed towards the rotor axis(5), said recess being provided in the vanes 10 inside of the outer periphery of the rotor (8).
8. A structure according to any of claims 3 to 5, characterized in that the vanes(10)at their ends directed towards the rotor axis(5)have inside the outer periphery of the rotor at the ends directed to the casing covers(3)a recess(19)at least partially surrounding the cam ring (14).
9. A structure according to any of the preceding claims characterized in that parts(20)of the vanes(10)directed towards and guided by the control or cam means(12, 14 or 17)are wider than the thickness of the remainder of the vane bodies.
10. A structure according to any of the preceding claims characterized in that between the ends of the rotor(8) and the casing covers(3)inside the outer periphery of the rotor (8) sealing rings(21)of wear-resistant and/or self-lubricating material are present between the vanes.
11. A structure according to claim 10 characterized in that sealing between the ends of the rotor(8)and the casing covers (3) is obtained by wedgeshaped segmental plates (22) of wear-resistant and/or self-lubricating material between the vanes (10), the ends of the segments (22) resting against the vanes(10), which segments(22)are supported in an annular chamber(23)provided concentrically in the end wall of the rotor (8), there being resilient means(24)to urge the segments (22) into contact with the adjacent casing cover (3).
12.A structure according to claim 10, characterized in that the sealing between the ends of the rotor(8)and the casing covers(3)is obtained by a circular disc(25)of wear-resistant and/or self-lubricating material taken up in a circular chamber(26)being provided concentrically in the end wall of the rotor(8), the disc being interrupted by slots (27) forming elongations of the slots(9)for the vanes in the rotor body(8)and having a central circular opening (28) for passage of the rotor axis(5), the disc (25) being urged outwardly against the adjacent casing cover (3) by resilient means (241
13. A structure according to claim 10 characterized in that the sealing between the ends of the rotor(8)and the casing covers (3) is obtained by a cap-shaped member (29) engaging with a sliding fit around and over one end (30) of the rotor (8), which end (30) has a smaller diameter than the rotor body so that the outer diameters of the cap-shaped member(29) and the rotor body are equal, said cap(29)being urged by resilient means (24) away from the rotor body, there being one or more guide means(31)to prevent rotation of the cap-shaped member (29) with respect to the rotor (8).
14. A structure according to claim 10 characterized in that the sealing between the ends of the rotor(8)and the : casing covers (3) is obtained by an annular member(32) of wear-resistant and/or self-lubricating sealing material, provided at the side of the rotor with corresponding recesses(33) for allowing passage of the vanes (10), said member (32) being in part taken up in an annular chamber (34) being concentrically provided in the end wall of the rotor (8) and said member(32) being at its other side rotatably taken up in a corresponding annular chamber (35)in the casing cover (3).
15. A structure according to claim 10 characterized in that the rotor (8)at at least one end has a protruding annular part protruding axially outside the vanes (10)and rotatably taken up in a chamber (37)in the casing cover(3), there being between the end wall of the rotor(8)and the chamber (37)in the casing cover(3)resilient sealing means(38) or grease of high viscosity.
16. A structure according to claim 10, characterized in that the vanes(10)at their sides directed towards the casing covers(3)have a slot-shaped recess(41)over their entire length, in which a strip(42)of wear-resisting and/or self-lubricating sealing material is taken up with a sliding fit, there being resilient means(43)to urge the strip (42) outwardly against the adjacent casing cover(3)
17. A structure according to claim 10 characterized in that the vanes(10)at their side directed towards the inner wall(2)of the casing (l)are provided over their entire length with a slot-shaped recess(44)in which a strip(45)of wear-resisting and/or self-lubricating sealing material is taken up, there being resilient means(46)to urge the strip (45)outwardly towards the inner wall(2)of the casing (1).
18. A structure according to claims 16 and 17 characterized in that the slot-shaped recess(41)at the sides of the vanes directed towards the casing covers(3)and the recess(44)at the side of the vanes directed to the inner wall(2)of the casing(l) together constitute a continuous slot-shaped recess(47), a strip (48)of wear-resistant and/or self-lubricating material being taken up with a sliding fit between the sealing strips(42) adjacent the casing covers (3).
19. A structure according to claim 18, characterized in that in the continuous slot-shaped recess(47)in the vanes(10) two sealing strips(49)in the shape of a carpenters square are taken up having their adjacent ends near the inner wall of the casing(2)in mutually overlapping relationship with local thinner strip parts (50).
20. A structure according to claims 18 and 19 characterized in that the sealing strips (42) and(48) or(49)at the three sides of the vanes are under an outwardly directed resilient pressure by a single U-shaped spring (51) of resilient wire or leaf material having an outwardly directed curve in the sides directed towards the casing covers (3) and having two outwardly directed curves in the part directed towards the inner wall(2) of the casing.
21. A structure according to claim 18 characterized in that the U-shaped spring (51) has hooked ends (52), which hooks engage behind the ends of the strips (42) directed towards the rotor axis (5).
22. A structure according to any of the preceeding claims applied as pump, characterized in that in the circular-cylindrical casing (1) between inlet and outlet there are openings (53) and (54) mutually connected by a closed passage (55) and positioned so that between the in- and outlet openings and these openings (53) and (54) there is always at least one vane.
EP82200165A 1981-02-13 1982-02-11 A rotating vane-pump or -motor Withdrawn EP0058456A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NL8100705 1981-02-13
NL8100705A NL8100705A (en) 1981-02-13 1981-02-13 ROTARY SHOT PUMP OR MOTOR.

Publications (1)

Publication Number Publication Date
EP0058456A1 true EP0058456A1 (en) 1982-08-25

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EP82200165A Withdrawn EP0058456A1 (en) 1981-02-13 1982-02-11 A rotating vane-pump or -motor

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NL (1) NL8100705A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0152395A1 (en) * 1984-02-15 1985-08-21 Jean-Marie Hublet Rotary vane machine
DE4036251A1 (en) * 1990-11-14 1992-05-21 Bosch Gmbh Robert Cellular pump or compressor - is for vehicle air conditioning and has mechanical pressure device to hold vanes in position
FR2692009A1 (en) * 1992-06-05 1993-12-10 Gilardini Spa Rotary vacuum pump of the pallet type.
FR2748068A1 (en) * 1996-04-26 1997-10-31 Magneti Marelli Spa ROTARY VANE PUMP
EP0838594A1 (en) * 1996-10-22 1998-04-29 Zexel Corporation Vane Compressor
WO2000055478A1 (en) * 1999-07-21 2000-09-21 Kolosovsky Vladimir Mikhailovi Volumetric-expansion rotor machine
GB2448078A (en) * 2007-03-28 2008-10-01 Goodrich Pump & Engine Control Vane pump with axial vane and rotor seals, radial and axial ports and discharge pressure biased vanes.
CN101930012B (en) * 2009-06-26 2011-12-14 鸿富锦精密工业（深圳）有限公司 Sensing device
ITMI20111828A1 (en) * 2011-10-07 2013-04-08 Augusto Mariani INTERNAL COMBUSTION ENGINE, ROTARY, HIGH PERFORMANCE.
CN106401948A (en) * 2016-12-15 2017-02-15 盐城工学院 Self residue removing servo vane pump
CN106438350A (en) * 2016-11-25 2017-02-22 盐城工学院 Deslagging base used for vane pump
WO2022159479A1 (en) * 2021-01-22 2022-07-28 Conmed Corporation Vane compressor for surgical gas delivery system with gas sealed insufflation and recirculation

Citations (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR498952A (en) * 1919-05-03 1920-01-28 Edmond Gustave Henry Improvements to rotary vane pumps
GB135834A (en) * 1918-11-23 1920-07-15 Hugo Lars Reinhold Swartling Improvement in Tightening Means for Rotary Compressors, Hydraulic Generators and Motors, and the like.
FR22604E (en) * 1919-10-06 1921-08-04 Emile Louis Mallard Rotary pump
GB278382A (en) * 1926-09-30 1927-12-22 Swiss Locomotive & Machine Works Improvements connected with the pistons of rotary compressors
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GB135834A (en) * 1918-11-23 1920-07-15 Hugo Lars Reinhold Swartling Improvement in Tightening Means for Rotary Compressors, Hydraulic Generators and Motors, and the like.
FR498952A (en) * 1919-05-03 1920-01-28 Edmond Gustave Henry Improvements to rotary vane pumps
FR22604E (en) * 1919-10-06 1921-08-04 Emile Louis Mallard Rotary pump
GB278382A (en) * 1926-09-30 1927-12-22 Swiss Locomotive & Machine Works Improvements connected with the pistons of rotary compressors
DE596625C (en) * 1931-10-17 1934-05-07 Dimitri Nicolas Hapkins Rotary piston internal combustion engine
US2311162A (en) * 1940-05-20 1943-02-16 Bois Virgil L Du Fluid pump or motor
US2672282A (en) * 1951-07-27 1954-03-16 Novas Camilo Vazquez Rotary vacuum and compression pump
GB908722A (en) * 1958-10-13 1962-10-24 American Thermocatalytic Corp Improvements in or relating to vane pumps
US3256831A (en) * 1959-09-11 1966-06-21 Eickmann Karl Rotary pump and fluid motor and sealing means therefor
US3167022A (en) * 1963-07-18 1965-01-26 Scognamillo Frank Rotary machine with blade centering rings
US3167023A (en) * 1963-08-15 1965-01-26 Scognamillo Frank Rotary machine with rings holding blades centered longitudinally and radially in the operating chamber
DE1811439A1 (en) * 1967-12-01 1969-07-03 Magnus Boeschen engine
FR2126668A5 (en) * 1971-02-11 1972-10-06 Peters Ag Claudius Multicell compressor wear edge - of PTFE
FR2370185A1 (en) * 1976-11-09 1978-06-02 Nippon Piston Ring Co Ltd ROTARY VANE PUMP OR COMPRESSOR
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0152395A1 (en) * 1984-02-15 1985-08-21 Jean-Marie Hublet Rotary vane machine
WO1985003736A1 (en) * 1984-02-15 1985-08-29 Hublet Jean Marie Palette rotary machine
DE4036251A1 (en) * 1990-11-14 1992-05-21 Bosch Gmbh Robert Cellular pump or compressor - is for vehicle air conditioning and has mechanical pressure device to hold vanes in position
FR2692009A1 (en) * 1992-06-05 1993-12-10 Gilardini Spa Rotary vacuum pump of the pallet type.
FR2748068A1 (en) * 1996-04-26 1997-10-31 Magneti Marelli Spa ROTARY VANE PUMP
EP0838594A1 (en) * 1996-10-22 1998-04-29 Zexel Corporation Vane Compressor
WO2000055478A1 (en) * 1999-07-21 2000-09-21 Kolosovsky Vladimir Mikhailovi Volumetric-expansion rotor machine
US8011909B2 (en) * 2007-03-28 2011-09-06 Goodrich Pump & Engine Control Systems, Inc. Balanced variable displacement vane pump with floating face seals and biased vane seals
GB2448078A (en) * 2007-03-28 2008-10-01 Goodrich Pump & Engine Control Vane pump with axial vane and rotor seals, radial and axial ports and discharge pressure biased vanes.
DE102008016212B4 (en) * 2007-03-28 2016-05-12 Triumph Engine Control Systems, Llc Balanced vane pump of variable capacity / displacement with floating face seals and prestressed leaf seals
CN101930012B (en) * 2009-06-26 2011-12-14 鸿富锦精密工业（深圳）有限公司 Sensing device
ITMI20111828A1 (en) * 2011-10-07 2013-04-08 Augusto Mariani INTERNAL COMBUSTION ENGINE, ROTARY, HIGH PERFORMANCE.
WO2013050852A3 (en) * 2011-10-07 2013-11-07 Mariani Augusto Rotary inner combustion engine with a half - cylinder shaped cavity in the rotor
CN106438350A (en) * 2016-11-25 2017-02-22 盐城工学院 Deslagging base used for vane pump
CN106438350B (en) * 2016-11-25 2018-04-06 盐城工学院 A kind of slagging-off base for vane pump
CN106401948A (en) * 2016-12-15 2017-02-15 盐城工学院 Self residue removing servo vane pump
CN106401948B (en) * 2016-12-15 2018-04-10 盐城工学院 A kind of slagging-off servo vane pump certainly
WO2022159479A1 (en) * 2021-01-22 2022-07-28 Conmed Corporation Vane compressor for surgical gas delivery system with gas sealed insufflation and recirculation

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