EP2504579A2 - Vane pump - Google Patents
Vane pumpInfo
- Publication number
- EP2504579A2 EP2504579A2 EP10781521A EP10781521A EP2504579A2 EP 2504579 A2 EP2504579 A2 EP 2504579A2 EP 10781521 A EP10781521 A EP 10781521A EP 10781521 A EP10781521 A EP 10781521A EP 2504579 A2 EP2504579 A2 EP 2504579A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- vane pump
- driver
- motor shaft
- pump
- 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- Withdrawn
Links
Classifications
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- 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
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0057—Driving elements, brakes, couplings, transmission specially adapted for machines or pumps
- F04C15/0061—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
- F04C15/0073—Couplings between rotors and input or output shafts acting by interengaging or mating parts, i.e. positive coupling of rotor and shaft
-
- 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
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0057—Driving elements, brakes, couplings, transmission specially adapted for machines or pumps
- F04C15/008—Prime movers
-
- 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
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/344—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F04C18/3446—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, 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 group F04C18/08 or F04C18/22 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
-
- 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
- F04C2/30—Rotary-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
- F04C2/34—Rotary-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
- F04C2/344—Rotary-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
- F04C2/3446—Rotary-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
-
- 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
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0042—Driving elements, brakes, couplings, transmissions specially adapted for pumps
- F04C29/005—Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
- F04C29/0071—Couplings between rotors and input or output shafts acting by interengaging or mating parts, i.e. positive coupling of rotor and shaft
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/08—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key
- F16D1/0876—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with axial keys and no other radial clamping
-
- 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
- F04C2240/20—Rotors
Definitions
- the present invention relates to a vane pump comprising an electric drive unit having an electric motor and a motor shaft, a pump chamber adjoining the electric drive unit, and a rotor having a number of sliders disposed within the pump chamber concentric with the motor shaft the motor shaft via a rotatably connected to the motor shaft driver associated with the rotor is engaged and the driver has at least one driver pin which engages in a corresponding thereto Rotorausneh- mung.
- Vane pumps of the type mentioned which are often referred to as rotary vane pumps, are already known from the prior art in various embodiments. Examples of vane pump are provided by DE 100 24 699 A1, DE 199 36 644 B4, DE 10 2006 058 977 A1, DE 10 2006 058 978 A1, DE 10 2006 058 979 A1 and DE 10 2006 058 980 A1.
- a vane pump according to the invention is characterized in that the at least one rotor recess is oval and that the driving pin is contoured such that two first slightly curved contour sections each form a contact region, each with an elongated surface portion of the rotor recess. It has been shown that due to the oval shape of the at least one rotor recess and the corresponding configuration of the driving pin, the surface pressure can be reduced, so that the life of the rotor compared to the known from the prior art solutions in which the driving pins are cylindrical and have a circular cross-section, can be increased. The reduction of the surface pressure is in particular due to the particular contour of the driving pin, which has increased radii in the contact region with the contact surfaces of the rotor recesses. The driving pins no longer work deeply into the material due to the reduced surface pressure, so that the service life of the driving pins and / or the rotor can be increased.
- the first contour sections of the driver have a larger radius of curvature than two second contour sections adjoining two mutually opposite, sectionally substantially semicircular surface sections of the rotor recess.
- the rotor comprises two rotor recesses and that the driver has two corresponding driving pins which are in engagement with the rotor recesses.
- the two rotor recesses can be formed offset by 180 ° within the rotor.
- the driving pins are in this embodiment also offset by 180 ° formed on the driver.
- each driver pin extends orthogonal to a transverse center plane of the rotor.
- each driver pin are formed mirror-symmetrically with respect to two central axes, which intersect at a central point and are oriented orthogonal to one another.
- each of the rotor recesses is formed as a slot.
- the driver is formed in sections annular and extends around the motor shaft.
- FIG. 1 shows a longitudinal section through a vane pump according to a preferred embodiment of the present invention.
- Fig. 2 shows a section through the vane pump along the line D-D according to
- Fig. 3 is an enlarged detail view of the longitudinal section of FIG. 1, the
- Fig. 4 is a plan view of the rotor of the vane pump
- FIG. 5 is an enlarged view of Fig. 4th
- the basic structural design and the basic operating principle of a vane pump 1, which is constructed according to a preferred embodiment of the present invention, are known from the prior art and will be explained in more detail below.
- the vane pump 1 comprises an electric drive unit, which is accommodated in a housing of the vane pump 1 and has an electric motor with a motor shaft 6.
- the vane pump 1 (rotary vane pump) can be designed in particular as a vacuum pump for generating a vacuum, which operates on the so-called displacement principle.
- Via a fluid inlet channel 15, which in the present case is designed as a fluid inlet nozzle air or another fluid medium is sucked in during operation of the vane pump 1 and flows into a pump chamber 2 of the vane pump 1 and is compressed there.
- the pump chamber 2 comprises a base plate 4 (motor side), a pump ring 3 and an axially offset to the base plate 4 cover plate 5, which are interconnected.
- the pump ring 3 has an elliptical in this embodiment nenkontur (in particular in Fig. 3 to recognize) with a correspondingly shaped inner wall 30.
- the possibility that the pump ring 3 is annular and has a circular inner contour.
- a cylindrical rotor 7 is arranged, which is in operative connection with the motor shaft 6 of the drive unit, which extends through a central opening of the base plate 4.
- the rotor 7 is driven during operation of the vane pump 1 by the motor shaft 6 of the electric motor and thereby set in rotation.
- the rotor 7 is rotatably connected to the motor shaft 6 via a correspondingly shaped driver 9, on the structural design will be discussed in more detail below.
- the driver 9 is in turn rotatably mounted on the motor shaft 6 of the electric motor.
- the rotor 7 has a number of guide slots 70, which are each suitable for receiving a slider 8.
- the rotor 7 distributed in the circumferential direction a total of eight guide slots 70 which extend from the outer periphery rotors inwardly.
- each one of the slide 8 is slidably disposed.
- the rotor 7 is driven during operation of the vane pump 1 by the motor shaft 6 of the electric motor and thereby set in rotation.
- the slides 8, depending on their rotational position form differently sized working cells with the inner wall 30 of the pump ring 3, the outer wall 71 of the rotor 7 and possibly adjacent slides 8.
- the mounting plate 1 1 may alternatively be part of the housing.
- a sealing ring 13 is provided, which is arranged during assembly on the mounting plate 1 1.
- the sealing ring 13 is suitable for sealing a muffler cap 14 which terminates the vane pump 1 at the end.
- the muffler cap 14 is screwed by means of suitable fastening screws 12 with the mounting plate 1 1.
- the fluid flows through the fluid inlet channel 15 and from there through corresponding fluid outlet openings of the mounting plate 1 1 and then by two 180 ° offset from each other (and thus opposite each other) arranged fluid inlet openings 40 which formed in the base plate 4 are in the pump chamber 2 a.
- the slides 8 of the rotating rotor 7 compress the fluid and drive it to two fluid outlet openings not shown here, which are preferably provided offset by 180 ° in the cover plate 5 of the pump chamber 2 and preferably to the fluid inlet openings 40 of the base plate 4 by about 90 ° offset and formed as elongated shaped openings
- the damping volume of the muffler means 10 is presently defined spatially substantially by the surface of the cover plate 5 and the muffler cap 14, which include the damping volume.
- the fluid flows after passing through the pump chamber 2 through the two fluid outlet openings of the cover plate 5 in the muffler volume of the muffler means 10. From there, the fluid flows to a fluid outlet 19 (see Fig. 3) and flows through this out of the vane pump 1 out.
- a pre-silencer means may be housed within the damping volume.
- the rotor 8 by means of the driver 9 rotatably connected to the motor shaft 6 of the electric motor whose free end extends through a central opening of the rotor 7, respectively.
- the rotor 7 has two rotor recesses 72, which are offset by 180 ° with respect to one another and which are in the present case oval-shaped and designed as elongated holes.
- the driver 9 is annular and extends around the motor shaft around and is rotatably connected to the motor shaft 6.
- the driver 9 has two Mit supportivezap- fer 90 corresponding with the two rotor recesses 72, which are also arranged offset by 180 ° to each other and Ortho extend gonal to a transverse center plane of the rotor 7.
- the two driver tap 90 are shaped so that they can engage in the two RotorausEnglishept 72 of the rotor 7, and thus therefore serve to transmit the torque from the motor shaft 6 to the rotor 7 of the vane pump. 1
- the driver 9 is designed so that caused by the driving pin 90 surface pressure in the slot-like recesses 72 of the rotor 3 can be minimized.
- the two driving pins 90 have an oval cross section, which is adapted to the shape of the oval rotor recesses 72, in which the driving pins 90 can engage.
- the cross section of the two driving pins 90 is mirror-symmetrical with respect to two central axes, which intersect in the middle and are oriented orthogonal to each other.
- the outer contour of the driving pins 90 has four contour sections 91, 92, 93, 94 with two different radii of curvature R1 and R2.
- the two first contour portions 91, 92, which bear against the straight surface portions 721 of the slot-like recesses 72 of the rotor 7 are slightly curved and have a radius of curvature R1, which is chosen so large that the surface pressure in the RotorausEnglishept 72 can be minimized ,
- the radii of the two second contour sections 93, 94 which are opposite to the curved, substantially semicircular in cross-section surface portions 720 of the slot-shaped recesses 72 and do not touch, have a radius R2 ⁇ R1.
- the two second contour portions 93, 94 are thus substantially more curved than the first two contour portions 91, 92.
- the radii of curvature R1 of the two first contour portions 91, 92 are thus greater than the radii of curvature R2 of the two second contour portions 93, 94.
- the in this way designed first contour portions 91, 92 respectively form the contact areas of the driving pin 90 with the straight surface portions 721 of the slots designed as slots 72.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Rotary Pumps (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
The invention relates to a vane pump (1) comprising an electrical drive unit having an electric motor and a motor shaft (6), a pump chamber (2) connecting to the electrical drive unit, a rotor (7) having a quantity of sliders (8) and disposed concentrically to the motor shaft (6) within the pump chamber (2), wherein the motor shaft (6) engages with the rotor (7) by means of a pusher dog (9) rotationally fixed to the motor shaft (6) and the pusher dog (9) comprises at least one tappet (90) engaging in a corresponding rotor recess (72), wherein the at least one rotor recess (72) is oval in shape and the tappet (90) is contoured such that two first slightly curved contour segments (91, 92) each form a contact region with one elongated surface segment (721) of the rotor recess (72).
Description
Flügelzellenpumpe Vane pump
Die vorliegende Erfindung betrifft eine Flügelzellenpumpe, umfassend eine elektrische Antriebseinheit mit einem Elektromotor und einer Motorwelle, eine Pumpenkammer, die sich an die elektrische Antriebseinheit anschließt, und einen Rotor mit einer Anzahl von Schiebern, der innerhalb der Pumpenkammer konzentrisch zu der Motorwelle angeordnet ist, wobei die Motorwelle über einen drehfest mit der Motorwelle verbundenen Mitnehmer mit dem Rotor in Eingriff steht und der Mitnehmer zumindest einen Mitnehmerzapfen aufweist, der in eine damit korrespondierende Rotorausneh- mung eingreift. The present invention relates to a vane pump comprising an electric drive unit having an electric motor and a motor shaft, a pump chamber adjoining the electric drive unit, and a rotor having a number of sliders disposed within the pump chamber concentric with the motor shaft the motor shaft via a rotatably connected to the motor shaft driver associated with the rotor is engaged and the driver has at least one driver pin which engages in a corresponding thereto Rotorausneh- mung.
Flügelzellenpumpen der eingangs genannten Art, die häufig auch als Drehschieberpumpen bezeichnet werden, sind aus dem Stand der Technik in verschiedenen Ausführungsformen bereits bekannt. Beispiele für Flügelzellenpumpe liefern die DE 100 24 699 A1 , die DE 199 36 644 B4, die DE 10 2006 058 977 A1 , die DE 10 2006 058 978 A1 , die DE 10 2006 058 979 A1 sowie die DE 10 2006 058 980 A1. Vane pumps of the type mentioned, which are often referred to as rotary vane pumps, are already known from the prior art in various embodiments. Examples of vane pump are provided by DE 100 24 699 A1, DE 199 36 644 B4, DE 10 2006 058 977 A1, DE 10 2006 058 978 A1, DE 10 2006 058 979 A1 and DE 10 2006 058 980 A1.
Aus dem Stand der Technik ist es bekannt, die drehfeste Anbindung des Rotors an die Antriebswelle mit Hilfe eines Mitnehmers zu realisieren, der ein oder mehrere zylindrisch geformte Mitnehmerzapfen mit einem kreisförmigen Querschnitt aufweist. Der/Die Mitnehmerzapfen steht/stehen dabei mit entsprechend geformten Ausnehmungen des Rotors in Eingriff. From the prior art it is known to realize the non-rotatable connection of the rotor to the drive shaft by means of a driver having one or more cylindrically shaped driving pins with a circular cross-section. The / the driving pin is / are doing with correspondingly shaped recesses of the rotor in engagement.
Es hat sich gezeigt, dass auf Grund der zylindrischen Mitnehmerzapfengeometrie die Flächenpressung mit den Berührungsflächen der Rotorausnehmungen sehr hoch ist. Die Mitnehmerzapfen können sich dabei tief in das Material hineinarbeiten, so dass sich die Lebensdauer der Mitnehmerzapfen und/oder des Rotors erheblich verringern kann. It has been shown that due to the cylindrical driving pin geometry, the surface pressure with the contact surfaces of the rotor recesses is very high. The driving pins can thereby work deep into the material, so that the service life of the driving pins and / or the rotor can be significantly reduced.
Hier setzt die vorliegende Erfindung an und macht es sich zur Aufgabe, eine Flügelzellenpumpe der eingangs genannten Art zur Verfügung zu stellen, bei der der Ver-
schleiß des Rotors verringert werden kann und damit die Lebensdauer des Rotors erhöht werden kann. This is where the present invention sets out and makes it its task to provide a vane pump of the type mentioned at the outset, in which the Wear of the rotor can be reduced and thus the life of the rotor can be increased.
Die Lösung dieser Aufgabe liefert eine Flügelzellenpumpe der eingangs genannten Art mit den Merkmalen des kennzeichnenden Teils des Anspruchs 1. Die Unteransprüche betreffen vorteilhafte Weiterbildungen der Erfindung. The solution to this problem provides a vane pump of the type mentioned above with the features of the characterizing part of claim 1. The dependent claims relate to advantageous developments of the invention.
Eine erfindungsgemäße Flügelzellenpumpe zeichnet sich dadurch aus, dass die mindestens eine Rotorausnehmung oval ausgebildet ist und dass der Mitnehmerzapfen derart konturiert ist, dass zwei erste schwach gekrümmte Konturabschnitte jeweils einen Berührungsbereich mit jeweils einem länglichen Flächenabschnitt der Rotor- ausnehmung bilden. Es hat sich gezeigt, dass auf Grund der ovalen Gestaltung der mindestens einen Rotorausnehmung und der damit korrespondierenden Ausgestaltung des Mitnehmerzapfens die Flächenpressung verringert werden kann, so dass die Lebensdauer des Rotors im Vergleich zu den aus dem Stand der Technik bekannten Lösungen, bei denen die Mitnehmerzapfen zylindrisch ausgebildet sind und einen kreisrunden Querschnitt aufweisen, erhöht werden kann. Die Minderung der Flächenpressung ist dabei insbesondere durch die besondere Kontur des Mitnehmerzapfens bedingt, welcher im Berührungsbereich mit den Berührungsflächen der Rotorausnehmungen vergrößerte Radien aufweist. Die Mitnehmerzapfen arbeiten sich auf Grund der verminderten Flächenpressung nicht mehr tief in das Material hinein, so dass die Lebensdauer der Mitnehmerzapfen und/oder des Rotors vergrößert werden kann. A vane pump according to the invention is characterized in that the at least one rotor recess is oval and that the driving pin is contoured such that two first slightly curved contour sections each form a contact region, each with an elongated surface portion of the rotor recess. It has been shown that due to the oval shape of the at least one rotor recess and the corresponding configuration of the driving pin, the surface pressure can be reduced, so that the life of the rotor compared to the known from the prior art solutions in which the driving pins are cylindrical and have a circular cross-section, can be increased. The reduction of the surface pressure is in particular due to the particular contour of the driving pin, which has increased radii in the contact region with the contact surfaces of the rotor recesses. The driving pins no longer work deeply into the material due to the reduced surface pressure, so that the service life of the driving pins and / or the rotor can be increased.
In einer besonders vorteilhaften Ausführungsform wird vorgeschlagen, dass die ersten Konturabschnitte des Mitnehmers einen größeren Krümmungsradius aufweisen als zwei zweite Konturabschnitte, die an zwei einander gegenüberliegende, abschnittsweise im Wesentlichen halbkreisförmige Flächenabschnitte der Rotorausnehmung angrenzen. In a particularly advantageous embodiment, it is proposed that the first contour sections of the driver have a larger radius of curvature than two second contour sections adjoining two mutually opposite, sectionally substantially semicircular surface sections of the rotor recess.
Um insbesondere bei sehr leistungsstarken Flügelzellenpumpen die Anbindung des Rotors an die Motorwelle zu verbessern, ist in einer besonders vorteilhaften Ausführungsform vorgesehen, dass der Rotor zwei Rotorausnehmungen umfasst und dass
der Mitnehmer zwei damit korrespondierende Mitnehmerzapfen aufweist, die mit den Rotorausnehmungen in Eingriff stehen. Vorzugsweise können die beiden Rotoraus- nehmungen um 180° versetzt innerhalb des Rotors ausgebildet sein. Die Mitnehmerzapfen sind in dieser Ausführungsform ebenfalls um 180° versetzt an dem Mitnehmer ausgebildet. In order to improve the connection of the rotor to the motor shaft, in particular in the case of very powerful vane pumps, it is provided in a particularly advantageous embodiment that the rotor comprises two rotor recesses and that the driver has two corresponding driving pins which are in engagement with the rotor recesses. Preferably, the two rotor recesses can be formed offset by 180 ° within the rotor. The driving pins are in this embodiment also offset by 180 ° formed on the driver.
Um die Montage des Rotors an dem Mitnehmer zu vereinfachen, ist in einer besonders vorteilhaften Ausführungsform vorgesehen, dass sich jeder Mitnehmerzapfen orthogonal zu einer Quermittelebene des Rotors erstreckt. In order to simplify the mounting of the rotor on the driver, it is provided in a particularly advantageous embodiment that each driver pin extends orthogonal to a transverse center plane of the rotor.
In einer besonders vorteilhaften Ausführungsform besteht die Möglichkeit, dass der Querschnitt jedes Mitnehmerzapfens spiegelsymmetrisch in Bezug auf zwei Mittelachsen ausgebildet sind, die sich in einem Mittelpunkt schneiden und orthogonal zueinander orientiert sind. In a particularly advantageous embodiment, there is the possibility that the cross section of each driver pin are formed mirror-symmetrically with respect to two central axes, which intersect at a central point and are oriented orthogonal to one another.
Um die Herstellung der Rotorausnehmungen zu vereinfachen, ist einer besonders vorteilhaften Ausführungsform vorgesehen, dass jede der Rotorausnehmungen als Langloch ausgebildet ist. In order to simplify the production of the rotor recesses, a particularly advantageous embodiment is provided that each of the rotor recesses is formed as a slot.
Um die Montage des Mitnehmers zu erleichtern, ist in einer besonders vorteilhaften Ausführungsform vorgesehen, dass der Mitnehmer abschnittsweise ringförmig ausgebildet ist und sich um die Motorwelle erstreckt.
In order to facilitate the mounting of the driver, it is provided in a particularly advantageous embodiment that the driver is formed in sections annular and extends around the motor shaft.
Anhand der beigefügten Zeichnungen wird die Erfindung nachfolgend näher erläutert. Dabei zeigt: Reference to the accompanying drawings, the invention is explained in more detail below. Showing:
Fig. 1 einen Längsschnitt durch eine Flügelzellenpumpe gemäß einem bevorzugten Ausführungsbeispiel der vorliegenden Erfindung; 1 shows a longitudinal section through a vane pump according to a preferred embodiment of the present invention.
Fig. 2 einen Schnitt durch die Flügelzellenpumpe entlang der Linie D-D gemäß Fig. 2 shows a section through the vane pump along the line D-D according to
Fig. 1 ; Fig. 1;
Fig. 3 eine vergrößerte Detailansicht des Längsschnitts gemäß Fig. 1 , die den Fig. 3 is an enlarged detail view of the longitudinal section of FIG. 1, the
Bereich zeigt, in der die Drehmomentübertragung erfolgt; Area shows, in which the torque transmission takes place;
Fig. 4 eine Draufsicht auf den Rotor der Flügelzellenpumpe; Fig. 4 is a plan view of the rotor of the vane pump;
Fig. 5 eine vergrößerte Darstellung von Fig. 4. 5 is an enlarged view of Fig. 4th
Der grundlegende konstruktive Aufbau sowie das grundlegende Funktionsprinzip einer Flügelzellenpumpe 1 , die gemäß einem bevorzugten Ausführungsbeispiel der vorliegenden Erfindung aufgebaut ist, sind aus dem Stand der Technik bekannt und sollen nachfolgend näher erläutert werden. Die Flügelzellenpumpe 1 umfasst eine elektrische Antriebseinheit, die in einem Gehäuse der Flügelzellenpumpe 1 untergebracht ist und einen Elektromotor mit einer Motorwelle 6 aufweist. Die Flügelzellenpumpe 1 (Drehschieberpumpe) kann insbesondere als Unterdruckpumpe zur Erzeugung eines Vakuums ausgebildet sein, die nach dem so genannten Verdrängerprinzip arbeitet. Über einen Fluideinlasskanal 15, der vorliegend als Fluideinlassstutzen ausgebildet ist, wird während des Betriebs der Flügelzellenpumpe 1 Luft oder ein anderes Fluid- medium angesaugt und strömt in eine Pumpenkammer 2 der Flügelzellenpumpe 1 ein und wird dort verdichtet. The basic structural design and the basic operating principle of a vane pump 1, which is constructed according to a preferred embodiment of the present invention, are known from the prior art and will be explained in more detail below. The vane pump 1 comprises an electric drive unit, which is accommodated in a housing of the vane pump 1 and has an electric motor with a motor shaft 6. The vane pump 1 (rotary vane pump) can be designed in particular as a vacuum pump for generating a vacuum, which operates on the so-called displacement principle. Via a fluid inlet channel 15, which in the present case is designed as a fluid inlet nozzle, air or another fluid medium is sucked in during operation of the vane pump 1 and flows into a pump chamber 2 of the vane pump 1 and is compressed there.
Die Pumpenkammer 2 umfasst eine Grundplatte 4 (motorseitig), einen Pumpenring 3 sowie eine axial zur Grundplatte 4 versetzte Abdeckplatte 5, die miteinander verbunden sind. Der Pumpenring 3 weist in diesem Ausführungsbeispiel eine elliptische In-
nenkontur (insbesondere in Fig. 3 zu erkennen) mit einer entsprechend geformten Innenwand 30 auf. Es besteht in einer alternativen Ausführungsform auch die Möglichkeit, dass der Pumpenring 3 kreisringförmig ausgebildet ist und eine kreisförmige Innenkontur aufweist. The pump chamber 2 comprises a base plate 4 (motor side), a pump ring 3 and an axially offset to the base plate 4 cover plate 5, which are interconnected. The pump ring 3 has an elliptical in this embodiment nenkontur (in particular in Fig. 3 to recognize) with a correspondingly shaped inner wall 30. There is an alternative embodiment, the possibility that the pump ring 3 is annular and has a circular inner contour.
Im Inneren der Pumpenkammer 2 ist ein zylindrischer Rotor 7 angeordnet, der mit der Motorwelle 6 der Antriebseinheit, die sich durch eine zentrale Öffnung der Grundplatte 4 erstreckt, in Wirkverbindung steht. Der Rotor 7 wird während des Betriebs der Flügelzellenpumpe 1 von der Motorwelle 6 des Elektromotors angetrieben und dadurch in Rotation versetzt. Zu diesem Zweck ist der Rotor 7 über einen entsprechend geformten Mitnehmer 9, auf dessen konstruktive Gestaltung weiter unten noch näher eingegangen werden wird, drehfest mit der Motorwelle 6 verbunden. Der Mitnehmer 9 ist seinerseits drehfest an der Motorwelle 6 des Elektromotors angebracht. Inside the pump chamber 2, a cylindrical rotor 7 is arranged, which is in operative connection with the motor shaft 6 of the drive unit, which extends through a central opening of the base plate 4. The rotor 7 is driven during operation of the vane pump 1 by the motor shaft 6 of the electric motor and thereby set in rotation. For this purpose, the rotor 7 is rotatably connected to the motor shaft 6 via a correspondingly shaped driver 9, on the structural design will be discussed in more detail below. The driver 9 is in turn rotatably mounted on the motor shaft 6 of the electric motor.
Der Rotor 7 weist eine Anzahl von Führungsschlitzen 70 auf, die jeweils zur Aufnahme eines Schiebers 8 geeignet sind. In diesem Ausführungsbeispiel weist der Rotor 7 in Umfangsrichtung verteilt insgesamt acht Führungsschlitze 70 auf, die sich von dessen Außenumfang rotore inwärts erstrecken. In jedem der Führungsschlitze 70 ist jeweils einer der Schieber 8 verschiebbar angeordnet. Der Rotor 7 wird während des Betriebs der Flügelzellenpumpe 1 von der Motorwelle 6 des Elektromotors angetrieben und dadurch in Rotation versetzt. Wie in Fig. 3 zu erkennen, bilden die Schieber 8 abhängig von ihrer Drehlage unterschiedlich große Arbeitszellen mit der Innenwand 30 des Pumpenrings 3, der Außenwand 71 des Rotors 7 und gegebenenfalls benachbarten Schiebern 8 aus. The rotor 7 has a number of guide slots 70, which are each suitable for receiving a slider 8. In this embodiment, the rotor 7 distributed in the circumferential direction a total of eight guide slots 70 which extend from the outer periphery rotors inwardly. In each of the guide slots 70 each one of the slide 8 is slidably disposed. The rotor 7 is driven during operation of the vane pump 1 by the motor shaft 6 of the electric motor and thereby set in rotation. As can be seen in FIG. 3, the slides 8, depending on their rotational position, form differently sized working cells with the inner wall 30 of the pump ring 3, the outer wall 71 of the rotor 7 and possibly adjacent slides 8.
Ferner weist die Flügelzellenpumpe 1 eine Montageplatte 1 1 auf, an der ein hier nicht explizit dargestelltes Gehäuse, in dem der Elektromotor untergebracht ist, befestigt ist. Die Montageplatte 1 1 kann alternativ auch ein Teil des Gehäuses sein. Ferner ist ein Dichtring 13 vorgesehen, der bei der Montage auf der Montageplatte 1 1 angeordnet wird. Der Dichtring 13 ist zur Abdichtung einer Schalldämpferkappe 14 geeignet, welche die Flügelzellenpumpe 1 endseitig abschließt. Die Schalldämpferkappe 14 ist mit Hilfe geeigneter Befestigungsschrauben 12 mit der Montageplatte 1 1 verschraubt.
Während des Betriebs der Flügelzellenpumpe 1 strömt das Fluid durch den Fluidein- lasskanal 15 und von dort durch entsprechende Fluidaustrittsöffnungen der Montageplatte 1 1 und anschließend durch zwei um 180° zueinander versetzt (und damit einander gegenüberliegend) angeordnete Fluideintrittsöffnungen 40, die in der Grundplatte 4 ausgebildet sind, in die Pumpenkammer 2 ein. Die Schieber 8 des sich drehenden Rotors 7 komprimieren das Fluid und treiben es zu zwei hier nicht explizit dargestellten Fluidaustrittsöffnungen, die vorzugsweise um 180° zueinander versetzt in der Abdeckplatte 5 der Pumpenkammer 2 vorgesehen sind und die vorzugsweise gegenüber den Fluideintrittsöffnungen 40 der Grundplatte 4 um etwa 90° versetzt angeordnet und als länglich geformte Öffnungen ausgebildet sind Further, the vane pump 1, a mounting plate 1 1, at which a not explicitly shown here housing, in which the electric motor is housed, is attached. The mounting plate 1 1 may alternatively be part of the housing. Furthermore, a sealing ring 13 is provided, which is arranged during assembly on the mounting plate 1 1. The sealing ring 13 is suitable for sealing a muffler cap 14 which terminates the vane pump 1 at the end. The muffler cap 14 is screwed by means of suitable fastening screws 12 with the mounting plate 1 1. During operation of the vane pump 1, the fluid flows through the fluid inlet channel 15 and from there through corresponding fluid outlet openings of the mounting plate 1 1 and then by two 180 ° offset from each other (and thus opposite each other) arranged fluid inlet openings 40 which formed in the base plate 4 are in the pump chamber 2 a. The slides 8 of the rotating rotor 7 compress the fluid and drive it to two fluid outlet openings not shown here, which are preferably provided offset by 180 ° in the cover plate 5 of the pump chamber 2 and preferably to the fluid inlet openings 40 of the base plate 4 by about 90 ° offset and formed as elongated shaped openings
Das Dämpfungsvolumen des Schalldämpfermittels 10 wird vorliegend im Wesentlichen durch die Oberfläche der Abdeckplatte 5 und die Schalldämpferkappe 14 räumlich definiert, die das Dämpfungsvolumen einschließen. Das Fluid strömt nach dem Hindurchtritt durch die Pumpenkammer 2 durch die beiden Fluidaustrittsöffnungen der Abdeckplatte 5 in das Schalldämpfervolumen des Schalldämpfermittels 10. Von dort strömt das Fluid zu einem Fluidauslassbereich 19 (siehe Fig. 3) und strömt durch diesen aus der Flügelzellenpumpe 1 heraus. Gegebenenfalls kann innerhalb des Dämpfungsvolumens noch ein Vorschalldämpfermittel untergebracht sein. The damping volume of the muffler means 10 is presently defined spatially substantially by the surface of the cover plate 5 and the muffler cap 14, which include the damping volume. The fluid flows after passing through the pump chamber 2 through the two fluid outlet openings of the cover plate 5 in the muffler volume of the muffler means 10. From there, the fluid flows to a fluid outlet 19 (see Fig. 3) and flows through this out of the vane pump 1 out. Optionally, a pre-silencer means may be housed within the damping volume.
Unter weiterer Bezugnahme auf Fig. 3 bis 5 soll nachfolgend der konstruktive Aufbau des Mitnehmers 9 näher erläutert werden, der bei der vorstehend beschriebenen Flügelzellenpumpe 1 verwendet wird. Wie oben bereits kurz erläutert, ist der Rotor 8 mit Hilfe des Mitnehmers 9 drehfest mit der Motorwelle 6 des Elektromotors, deren freies Ende sich durch eine zentrale Öffnung des Rotors 7 erstreckt, verbunden. Der Rotor 7 weist in diesem Ausführungsbeispiel zwei um 180° versetzt zueinander angeordnete Rotorausnehmungen 72 auf, die vorliegend oval geformt sind und als Langlöcher ausgebildet sind. Der Mitnehmer 9 ist ringförmig ausgebildet und erstreckt sich um die Motorwelle herum und ist drehfest mit der Motorwelle 6 verbunden. Der Mitnehmer 9 weist zwei mit den beiden Rotorausnehmungen 72 korrespondierende Mitnehmerzap- fer 90 auf, die ebenfalls um 180° zueinander versetzt angeordnet sind und sich Ortho-
gonal zu einer Quermittelebene des Rotor 7 erstrecken. Die beiden Mitnehmerzapfer 90 sind so geformt, dass sie in die beiden Rotorausnehmungen 72 des Rotors 7 eingreifen können, und dienen mithin also der Übertragung des Drehmoments von der Motorwelle 6 zum Rotor 7 der Flügelzellenpumpe 1 . With further reference to Figs. 3 to 5 will be explained in more detail below the structural design of the driver 9, which is used in the vane pump 1 described above. As already explained briefly above, the rotor 8 by means of the driver 9 rotatably connected to the motor shaft 6 of the electric motor whose free end extends through a central opening of the rotor 7, respectively. In this exemplary embodiment, the rotor 7 has two rotor recesses 72, which are offset by 180 ° with respect to one another and which are in the present case oval-shaped and designed as elongated holes. The driver 9 is annular and extends around the motor shaft around and is rotatably connected to the motor shaft 6. The driver 9 has two Mitnehmerzap- fer 90 corresponding with the two rotor recesses 72, which are also arranged offset by 180 ° to each other and Ortho extend gonal to a transverse center plane of the rotor 7. The two driver tap 90 are shaped so that they can engage in the two Rotorausnehmungen 72 of the rotor 7, and thus therefore serve to transmit the torque from the motor shaft 6 to the rotor 7 of the vane pump. 1
Der Mitnehmer 9 ist so ausgeführt, dass die von den Mitnehmerzapfen 90 hervorgerufene Flächenpressung in den langlochartig ausgeführten Ausnehmungen 72 des Rotors 3 minimiert werden kann. Dieses wird dadurch erreicht, dass die beiden Mitnehmerzapfen 90 einen ovalen Querschnitt aufweisen, der an die Form der ovalen Rotor- ausnehmungen 72, in die die Mitnehmerzapfen 90 eingreifen können, angepasst ist. Wie in der vergrößerten Darstellung in Fig. 5 zu erkennen, ist der Querschnitt der beiden Mitnehmerzapfen 90 spiegelsymmetrisch in Bezug auf zwei Mittelachsen, die sich in der Mitte schneiden und orthogonal zueinander orientiert sind. Die äußere Kontur der Mitnehmerzapfen 90 weist vorliegend vier Konturabschnitte 91 , 92, 93, 94 mit zwei unterschiedlichen Krümmungsradien R1 und R2 auf. Die beiden ersten Konturabschnitte 91 , 92, die an den geraden Flächenabschnitten 721 der langlochartig ausgebildeten Ausnehmungen 72 des Rotors 7 anliegen, sind schwach gekrümmt und weisen einen Krümmungsradius R1 auf, der so groß gewählt ist, dass die Flächenpressung in den Rotorausnehmungen 72 minimiert werden kann. The driver 9 is designed so that caused by the driving pin 90 surface pressure in the slot-like recesses 72 of the rotor 3 can be minimized. This is achieved in that the two driving pins 90 have an oval cross section, which is adapted to the shape of the oval rotor recesses 72, in which the driving pins 90 can engage. As can be seen in the enlarged illustration in Fig. 5, the cross section of the two driving pins 90 is mirror-symmetrical with respect to two central axes, which intersect in the middle and are oriented orthogonal to each other. In the present case, the outer contour of the driving pins 90 has four contour sections 91, 92, 93, 94 with two different radii of curvature R1 and R2. The two first contour portions 91, 92, which bear against the straight surface portions 721 of the slot-like recesses 72 of the rotor 7 are slightly curved and have a radius of curvature R1, which is chosen so large that the surface pressure in the Rotorausnehmungen 72 can be minimized ,
Die Radien der beiden zweiten Konturabschnitte 93, 94, die den gekrümmten, im Querschnitt im Wesentlichen halbkreisförmigen Flächenabschnitten 720 der langloch- förmigen Ausnehmungen 72 gegenüberliegen und diese nicht berühren, weisen einen Radius R2 < R1 auf. Die beiden zweiten Konturabschnitte 93, 94 sind somit wesentlich stärker gekrümmt als die beiden ersten Konturabschnitte 91 , 92. Die Krümmungsradien R1 der beiden ersten Konturabschnitte 91 , 92 sind also größer als die Krümmungsradien R2 der beiden zweiten Konturabschnitte 93, 94. Die auf diese Weise gestalteten ersten Konturabschnitte 91 , 92 bilden jeweils die Berührungsbereiche der Mitnehmerzapfen 90 mit den geraden Flächenabschnitten 721 der als Langlöcher ausgeführten Ausnehmungen 72. Es hat sich gezeigt, dass auf Grund der großen Radien R1 und der schwachen Krümmung der beiden ersten Konturabschnitte 91 , 92 die Flächenpressung in den Ausnehmungen 72 im Vergleich zu zylindrisch ausgeführten
Mitnehmern mit einem kreisrunden Querschnitt wesentlich verringert werden kann. Die Mitnehmerzapfen 90 arbeiten sich auf Grund der verminderten Flächenpressung nicht mehr tief in das Material hinein, so dass die Lebensdauer der Mitnehmerzapfen 90 und/oder des Rotors 7 vergrößert werden kann.
The radii of the two second contour sections 93, 94, which are opposite to the curved, substantially semicircular in cross-section surface portions 720 of the slot-shaped recesses 72 and do not touch, have a radius R2 <R1. The two second contour portions 93, 94 are thus substantially more curved than the first two contour portions 91, 92. The radii of curvature R1 of the two first contour portions 91, 92 are thus greater than the radii of curvature R2 of the two second contour portions 93, 94. The in this way designed first contour portions 91, 92 respectively form the contact areas of the driving pin 90 with the straight surface portions 721 of the slots designed as slots 72. It has been shown that due to the large radii R1 and the weak curvature of the first two contour portions 91, 92, the surface pressure in the recesses 72 compared to cylindrically executed Drivers with a circular cross-section can be substantially reduced. Due to the reduced surface pressure, the driving pins 90 no longer work deeply into the material, so that the service life of the driving pins 90 and / or of the rotor 7 can be increased.
Bezugszeichenliste LIST OF REFERENCE NUMBERS
1 Flügelzellenpumpe 1 vane pump
2 Pumpenkammer 2 pump chamber
3 Pumpenring 3 pump ring
4 Grundplatte 4 base plate
5 Abd eckplatte 5 cover plate
6 Motorwelle 6 motor shaft
7 Rotor 7 rotor
8 Schieber 8 slides
9 Mitnehmer 9 drivers
1 1 Montageplatte 1 1 mounting plate
12 Befestigungsschraube 12 fixing screw
13 Dichtring 13 sealing ring
14 Schalldämpferkappe 14 silencer cap
15 Fluideinlasskanal 15 fluid inlet channel
19 Fluidauslassbereich 19 fluid outlet area
30 Innenwand 30 inner wall
70 Führungsschlitz 70 guide slot
71 Außenwand 71 outer wall
72 Rotorausnehmung 72 rotor recess
90 Mitnehmerzapfen 90 driving pin
91 Konturabschnitt 91 contour section
92 Konturabschnitt 92 contour section
93 Konturabschnitt 93 contour section
94 Konturabschnitt 94 contour section
720 halbkreisförmiger Abschnitt 720 semicircular section
721 gerader Abschnitt
721 straight section
Claims
1. Flügelzellenpumpe (1 ), umfassend 1. vane pump (1) comprising
- eine elektrische Antriebseinheit mit einem Elektromotor und einer Motorwelle (6), an electric drive unit with an electric motor and a motor shaft (6),
- eine Pumpenkammer (2), die sich an die elektrische Antriebseinheit anschließt, a pump chamber (2) adjoining the electric drive unit,
- einen Rotor (7) mit einer Anzahl von Schiebern (8), der innerhalb der Pumpenkammer (2) konzentrisch zu der Motorwelle (6) angeordnet ist, a rotor (7) with a number of slides (8) arranged inside the pump chamber (2) concentric with the motor shaft (6),
wobei die Motorwelle (6) über einen drehfest mit der Motorwelle (6) verbundenen Mitnehmer (9) mit dem Rotor (7) in Eingriff steht und der Mitnehmer (9) zumindest einen Mitnehmerzapfen (90) aufweist, der in eine damit korrespondierende Rotorausnehmung (72) eingreift, dadurch gekennzeichnet, dass die mindestens eine Rotorausnehmung (72) oval ausgebildet ist und dass der Mitnehmerzapfen (90) derart konturiert ist, dass zwei erste schwach gekrümmte Konturabschnitte (91 , 92) jeweils einen Berührungsbereich mit jeweils einem länglichen Flächenabschnitt (721 ) der Rotorausnehmung (72) bilden. wherein the motor shaft (6) via a rotatably connected to the motor shaft (6) driver (9) with the rotor (7) is engaged and the driver (9) has at least one driving pin (90) in a corresponding thereto Rotorausnehmung ( 72), characterized in that the at least one rotor recess (72) is oval and in that the driving pin (90) is contoured such that two first slightly curved contour sections (91, 92) each have a contact area, each with an elongated surface section (721 ) form the rotor recess (72).
2. Flügelzellenpumpe (1 ) nach Anspruch 1 , dadurch gekennzeichnet, dass die ersten Konturabschnitte (91 , 92) des Mitnehmers (90) einen größeren Krümmungsradius aufweisen als zwei zweite Konturabschnitte (93, 94), die an zwei einander gegenüberliegende, abschnittsweise im Wesentlichen halbkreisförmige Flächenabschnitte (720) der Rotorausnehmung (72) angrenzen. 2. vane pump (1) according to claim 1, characterized in that the first contour portions (91, 92) of the driver (90) have a larger radius of curvature than two second contour portions (93, 94), the two opposite, partially substantially semicircular surface portions (720) of the rotor recess (72) are adjacent.
3. Flügelzellenpumpe (1 ) nach Anspruch 1 oder 2, dadurch gekennzeichnet, dass der Rotor (7) zwei Rotorausnehmungen (72) umfasst und dass der Mitnehmer (9) zwei damit korrespondierende Mitnehmerzapfen (90) aufweist, die mit den Rotorausnehmungen (72) in Eingriff stehen. 3. vane pump (1) according to claim 1 or 2, characterized in that the rotor (7) comprises two rotor recesses (72) and that the driver (9) has two corresponding driver pin (90), which with the Rotorausnehmungen (72) engage.
4. Flügelzellenpumpe (1 ) nach Anspruch 3, dadurch gekennzeichnet, dass die beiden Rotorausnehmungen (72) um 180° versetzt innerhalb des Rotors (7) ausgebildet sind. 4. vane pump (1) according to claim 3, characterized in that the two rotor recesses (72) offset by 180 ° within the rotor (7) are formed.
5. Flügelzellenpumpe (1 ) nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, dass sich jeder Mitnehmerzapfen (90) orthogonal zu einer Quermittelebene des Rotors (7) erstreckt. 5. vane pump (1) according to one of claims 1 to 4, characterized in that each driver pin (90) extends orthogonal to a transverse center plane of the rotor (7).
6. Flügelzellenpumpe (1 ) nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, dass der Querschnitt jedes Mitnehmerzapfens (90) spiegelsymmetrisch in Bezug auf zwei Mittelachsen ausgebildet ist, die sich in einem Mittelpunkt schneiden und orthogonal zueinander orientiert sind. 6. vane pump (1) according to one of claims 1 to 5, characterized in that the cross section of each driver pin (90) is formed mirror-symmetrically with respect to two central axes which intersect at a center and are oriented orthogonal to each other.
7. Flügelzellenpumpe (1 ) nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, dass jede der Rotorausnehmungen (72) als Langloch ausgebildet ist. 7. vane pump (1) according to one of claims 1 to 6, characterized in that each of the rotor recesses (72) is formed as a slot.
8. Flügelzellenpumpe (1 ) nach einem der Ansprüche 1 bis 7, dadurch gekennzeichnet, dass der Mitnehmer (9) abschnittsweise ringförmig ausgebildet ist und sich um die Motorwelle (6) erstreckt. 8. vane pump (1) according to one of claims 1 to 7, characterized in that the driver (9) is partially annular and extends around the motor shaft (6).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102009055945.0A DE102009055945B4 (en) | 2009-11-26 | 2009-11-26 | Vane pump |
| PCT/EP2010/068197 WO2011064290A2 (en) | 2009-11-26 | 2010-11-25 | Vane pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP2504579A2 true EP2504579A2 (en) | 2012-10-03 |
Family
ID=43927116
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP10781521A Withdrawn EP2504579A2 (en) | 2009-11-26 | 2010-11-25 | Vane pump |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US9212660B2 (en) |
| EP (1) | EP2504579A2 (en) |
| CN (1) | CN102782327A (en) |
| DE (1) | DE102009055945B4 (en) |
| WO (1) | WO2011064290A2 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102878080A (en) * | 2012-10-30 | 2013-01-16 | 东风汽车公司 | Electric vacuum pump |
| JP6350294B2 (en) * | 2015-01-15 | 2018-07-04 | 株式会社デンソー | Fuel pump |
| JP6528521B2 (en) * | 2015-04-14 | 2019-06-12 | 株式会社デンソー | Fluid pump |
| EP3314125B1 (en) | 2015-06-24 | 2019-03-13 | Pierburg Pump Technology GmbH | Mechanical automotive vacuum pump |
| DE102019124262A1 (en) | 2019-09-10 | 2021-03-11 | HELLA GmbH & Co. KGaA | Vane pump |
| US12018680B2 (en) * | 2022-04-12 | 2024-06-25 | Phinia Delphi Luxembourg Sarl | Fluid pump with thrust bearing driver |
| CN115977946B (en) * | 2023-02-24 | 2026-02-06 | 河北恒盛泵业股份有限公司 | Vane type rotor pump with variable displacement |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2619094A1 (en) * | 1976-05-03 | 1977-12-01 | Bosch Gmbh Robert | FUEL SUPPLY UNIT |
| US4464142A (en) * | 1983-02-03 | 1984-08-07 | General Motors Corporation | Ignition distributor shaft coupler |
| JPH0531279Y2 (en) * | 1988-05-25 | 1993-08-11 | ||
| DE3930734A1 (en) * | 1989-09-14 | 1991-03-28 | Vdo Schindling | Vaned rotor pump for vehicle door locking mechanism - has spindle with vertical ends housed in deep part of recess in rotor |
| US5145348A (en) * | 1991-05-15 | 1992-09-08 | Eaton Corporation | Gerotor pump having an improved drive mechanism |
| CN2196211Y (en) * | 1994-04-07 | 1995-05-03 | 石油大学(华东) | Transmission mechanismf or reducing gear box |
| JP3264616B2 (en) * | 1996-03-13 | 2002-03-11 | 株式会社山田製作所 | Elastic joints in steering devices |
| US5692856A (en) * | 1996-03-14 | 1997-12-02 | Robert D. Newman, Sr. | Lock assembly for extension handle |
| US6099261A (en) * | 1998-06-08 | 2000-08-08 | Worden; Gary | Roller vane stage for a fuel pump |
| DE19936644B4 (en) | 1999-08-04 | 2004-04-01 | Hella Kg Hueck & Co. | Electric air pump for motor vehicles |
| DE10024669B4 (en) * | 2000-05-18 | 2005-10-13 | Hella Kgaa Hueck & Co. | pump |
| DE10024699A1 (en) | 2000-05-18 | 2001-11-29 | Bosch Gmbh Robert | Plasma etching system |
| JP2004332754A (en) * | 2003-04-30 | 2004-11-25 | Mitsubishi Materials Corp | Shaft member, rotating member and rotation transmitting member |
| DE502004005440D1 (en) * | 2003-05-26 | 2007-12-20 | Ixetic Hueckeswagen Gmbh | WING CELL PUMP WITH DEEP BENT STEEL PLUG |
| WO2006075363A1 (en) * | 2005-01-12 | 2006-07-20 | Mitsubishi Materials Pmg Corporation | Inner rotor for internal gear pump |
| CN2869444Y (en) * | 2005-09-20 | 2007-02-14 | 于海鹰 | Torque transfer mechanism with secondary curve lineshape |
| CN100532845C (en) | 2005-12-21 | 2009-08-26 | 比亚迪股份有限公司 | Micro air pump |
| DE102006058977B4 (en) | 2006-12-14 | 2016-03-31 | Hella Kgaa Hueck & Co. | Vane pump |
| DE102006058980B4 (en) | 2006-12-14 | 2016-08-04 | Hella Kgaa Hueck & Co. | Vane pump |
| DE102006058979A1 (en) | 2006-12-14 | 2008-06-19 | Hella Kgaa Hueck & Co. | Vane pump, for a motor vehicle, has guide slits at the rotor extending inwards from the circumference to take sliding impellers |
| DE102006058978A1 (en) | 2006-12-14 | 2008-06-19 | Hella Kgaa Hueck & Co. | Vane pump, for motor vehicles, has a structured base plate and/or cover plate at the pump chamber to prevent snagging by the rotor impellers |
-
2009
- 2009-11-26 DE DE102009055945.0A patent/DE102009055945B4/en active Active
-
2010
- 2010-11-25 CN CN2010800537064A patent/CN102782327A/en active Pending
- 2010-11-25 WO PCT/EP2010/068197 patent/WO2011064290A2/en not_active Ceased
- 2010-11-25 EP EP10781521A patent/EP2504579A2/en not_active Withdrawn
-
2012
- 2012-05-24 US US13/479,997 patent/US9212660B2/en active Active
Non-Patent Citations (1)
| Title |
|---|
| See references of WO2011064290A2 * |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2011064290A3 (en) | 2012-05-03 |
| US20130052057A1 (en) | 2013-02-28 |
| WO2011064290A2 (en) | 2011-06-03 |
| DE102009055945A1 (en) | 2011-06-01 |
| US9212660B2 (en) | 2015-12-15 |
| CN102782327A (en) | 2012-11-14 |
| DE102009055945B4 (en) | 2018-10-04 |
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