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DE102008054009A1 - Vane pump for use as lubricant pump in internal combustion engine, has four flanks comprising only line contact with corresponding groove, where flanks of spring elements are pressable against rotation direction and against line contact - Google Patents

Vane pump for use as lubricant pump in internal combustion engine, has four flanks comprising only line contact with corresponding groove, where flanks of spring elements are pressable against rotation direction and against line contact Download PDF

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Publication number
DE102008054009A1
DE102008054009A1 DE102008054009A DE102008054009A DE102008054009A1 DE 102008054009 A1 DE102008054009 A1 DE 102008054009A1 DE 102008054009 A DE102008054009 A DE 102008054009A DE 102008054009 A DE102008054009 A DE 102008054009A DE 102008054009 A1 DE102008054009 A1 DE 102008054009A1
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Germany
Prior art keywords
rotation
flanks
rotor
line contact
cage
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Granted
Application number
DE102008054009A
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German (de)
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DE102008054009B4 (en
Inventor
Hussam-Eddin Saleh
Martin Korn
Martin Böhm
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Bayerische Motoren Werke AG
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Bayerische Motoren Werke AG
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Priority to DE200810054009 priority Critical patent/DE102008054009B4/en
Publication of DE102008054009A1 publication Critical patent/DE102008054009A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F04C2/3441Rotary-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 one line or continuous surface substantially parallel to the axis of rotation
    • F04C2/3442Rotary-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 one line or continuous surface substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C21/00Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
    • F01C21/08Rotary pistons
    • F01C21/0809Construction of vanes or vane holders
    • F01C21/0818Vane tracking; control therefor
    • F01C21/0827Vane tracking; control therefor by mechanical means
    • F01C21/0845Vane tracking; control therefor by mechanical means comprising elastic means, e.g. springs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/40Rotary-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 group F04C2/08 or F04C2/22 and having a hinged member
    • F04C2/46Rotary-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 group F04C2/08 or F04C2/22 and having a hinged member with vanes hinged to the outer member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C19/00Sealing arrangements in rotary-piston machines or engines
    • F01C19/02Radially-movable sealings for working fluids
    • F01C19/025Radial sealing elements specially adapted for intermeshing engagement type machines or engines, e.g. gear machines or engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/20Rotors

Landscapes

  • 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 pump (10) has a cage (2) and a rotor (5) that stay in effective connection with each other via four flanks (3). The flanks extend in a direction of rotation axes (8, 9) and guide grooves (11) corresponding to the flanks, where the rotation of fluid is conveyed from a fluid inlet (6) to a fluid outlet (7). The flanks have smaller thickness than the inner width of the grooves in an area that protrudes into the grooves. Each flank has only a line contact with the corresponding groove, where the flanks of spring elements (4) are pressable against a rotation direction and against the contact.

Description

Die Erfindung betrifft eine Flügelzellenpumpe mit den Merkmalen aus dem Oberbegriff des Patentanspruchs 1.The The invention relates to a vane pump with the features from the preamble of claim 1.

Sie geht von dem deutschen Gebrauchsmuster DE 295 14 202 U1 aus. Aus dieser Schrift ist eine als Pumpe oder Hydromotor einsetzbare, regelbare Pendelschiebermaschine bzw. Flügelzellenpumpe bekannt. Die Flügelzellenpumpe gemäß dem Stand der Technik weist ein Maschinengehäuse mit einem Fluidzufluss und einem weitgehend diametral zu dem Fluidzufluss angeordneten Fluidabfluss auf. In dem Maschinengehäuse ist ein, um eine erste Drehachse drehbar angeordneter, weitgehend rohrförmiger Käfig angeordnet. Im Innenraum des Käfigs ist wiederum ein um eine zweite, zur ersten Drehachse parallel angeordneten Drehachse drehbarer Rotor angeordnet. Der Käfig und der Rotor sind über acht schwenkbar gelagerte Flügel miteinander in Wirkverbindung, derart, dass bei einer Drehung des Rotors um seine Drehachse der rohrförmige Käfig über die Flügel ebenfalls mitgedreht wird. Hierzu sind die Flügel im rohrförmigen Käfig drehbar gelagert, während sie andernends in Nuten des Rotors geführt sind. Durch Verschieben der zwei Drehachsen zueinander kann die Fördermenge eines Förderfluids, z. B. ein Schmiermittel, welches vom Fluidzufluss zum Fluidabfluss gefördert wird, variiert werden.It is based on the German utility model DE 295 14 202 U1 out. From this document, a usable as a pump or hydraulic motor, adjustable pendulum pusher or vane pump is known. The vane pump according to the prior art has a machine housing with a fluid inlet and a fluid drain arranged substantially diametrically to the fluid inlet. In the machine housing a, about a first axis of rotation rotatably arranged, largely tubular cage is arranged. In the interior of the cage turn around a second, to the first axis of rotation arranged in parallel rotary axis rotatable rotor is arranged. The cage and the rotor are operatively connected to each other via eight pivotally mounted wings, such that upon rotation of the rotor about its axis of rotation, the tubular cage is likewise rotated over the wings. For this purpose, the wings are rotatably mounted in the tubular cage, while at the other end they are guided in grooves of the rotor. By moving the two axes of rotation to each other, the flow rate of a conveying fluid, for. As a lubricant, which is funded by the fluid inlet to the fluid drain, can be varied.

Nachteilig an der bekannten Konstruktion ist eine relativ hohe innere Reibung der Flügelzellenpumpe, bedingt durch Fertigungstoleranzen. Weiter weist die Flügelzellenpumpe einen hohen inneren Pumpwiderstand bei hoher Drehzahl auf sowie eine hohe Empfindlichkeit gegen Verschmutzung.adversely on the known construction is a relatively high internal friction the vane pump, due to manufacturing tolerances. Next, the vane pump has a high internal pumping resistance at high speed and high sensitivity to contamination.

Aufgabe der vorliegenden Erfindung ist es, die o. g. Nachteile zu vermeiden.task It is the object of the present invention that o. g. To avoid disadvantages.

Diese Aufgabe wird durch die Merkmale im kennzeichnenden Teil des Patentanspruchs 1 gelöst.These The object is achieved by the features in the characterizing part of the claim 1 solved.

Aufgrund der erfindungsgemäßen Ausgestaltung wird die innere Reibung durch Minimierung der reibenden Flächen und Gleitgeschwindigkeiten reduziert, da durch die erfindungsgemäße Ausgestaltung nur noch eine Linienberührung zwischen den Reibpartnern existiert. Gleichzeitig werden die inneren Pumpwiderstände durch eine Reduktion des Arbeitshubes der Flügel im Rotor reduziert. In vorteilhafter Weise ist keine Passung für die Flügel im Rotor notwendig, wodurch die erfindungsgemäße Flügelzellenpumpe weitgehend unempfindlich gegenüber Schmutz ist. Darüber hinaus werden in vorteilhafter Weise die Volumina der Nebenkammern (von den Nuten und den Flügeln gebildet) durch die Anordnung und die Form der Flügel reduziert, wodurch eine Drehungleichförmigkeit der Flügelzellenpumpe deutlich verringert wird. Darüber hinaus ist in vorteilhafter Weise der radiale Hub der Flügel durch die Überlagerung mit einer tangentialen Bewegung verringert. Dadurch kann der Rotor bei gleicher Baugröße der Flügelzellenpumpe wesentlich stabiler gestaltet werden.by virtue of the embodiment of the invention is the inner Reduces friction by minimizing rubbing surfaces and sliding speeds, because of the inventive design only there is still a line contact between the friction partners. At the same time, the internal pumping resistances are replaced by a Reduction of the working stroke of the blades in the rotor reduced. Advantageously, there is no fit for the wings necessary in the rotor, whereby the inventive Vane pump largely insensitive to dirt is. In addition, the volumes are advantageously the secondary chambers (formed by the grooves and the wings) reduced by the arrangement and shape of the wings, whereby a rotational nonuniformity of the vane pump is significantly reduced. In addition, it is advantageous the radial stroke of the wings due to the overlay reduced with a tangential movement. This allows the rotor with the same size of the vane pump be made much more stable.

Die Ausgestaltung gemäß Patentanspruch 2 ist eine besonders robuste und bevorzugte Ausführungsform.The Embodiment according to claim 2 is a particularly robust and preferred embodiment.

Mit der Ausgestaltung gemäß Patentanspruch 3 kann die Fördermenge der Flügelzellenpumpe variiert werden.With The embodiment according to claim 3 can the flow rate of the vane pump varies become.

Im Folgenden ist die erfindungsgemäße Flügelzellenpumpe anhand eines besonders bevorzugten Ausführungsbeispieles in zwei Figuren näher erläutert.in the The following is the vane pump according to the invention using a particularly preferred embodiment explained in two figures.

1 zeigt einen Schnitt durch eine erfindungsgemäß ausgestaltete Flügelzellenpumpe. 1 shows a section through an inventively designed vane pump.

2 zeigt eine Detailansicht aus 1. 2 shows a detailed view 1 ,

1 zeigt einen Schnitt durch eine erfindungsgemäß ausgestaltete Flügelzellenpumpe 10. In einem Maschinengehäuse 1 ist ein rohrförmiger, in dem Maschinengehäuse 1 um eine erste Drehachse 8 drehbar gelagerter Käfig 2 angeordnet. In einem nicht bezifferten Innenvolumen des Käfigs 2 ist ein um eine zweite Drehachse 9 drehbar angeordneter Rotor 5 angeordnet. Der Kä2 und der Rotor 5 sind in dem vorliegenden Ausführungsbeispiel beispielsweise über sechs Flügel 3, wobei nur ein Flügel beziffert ist, miteinander in Wirkverbindung. Hierfür sind die Flügel 3 parallel zu den Drehachsen 8, 9 schwenkbar in dem Käfig 2 angeordnet, während sie andernends in Nuten 11 in dem Rotor 5 gelagert sind. Im Bereich der schwenkbaren Lagerung im Rotor 5 werden die Flügel 3 von Federelementen 4 entgegen einer, mit einem Pfeil symbolisch dargestellten Drehrichtung des Rotors 5 gegen eine Seitenwand der Nut 11 gedrückt. Beim Betrieb der Flügelzellenpumpe 10 wird der drehbare Rotor 5 angetrieben, wodurch der Käfig 2 über die Flügel 3 mitgedreht wird. Hierbei wird ein Fluid von einem gestrichelt dargestellten Fluidzufluss 6 zu einem ebenfalls gestrichelt dargestellten Fluidabfluss 7 gefördert. Durch Veränderung des Abstandes der ersten Drehachse 8 zur zweiten Drehachse 9, weitgehend senkrecht zu einer Verbindungslinie vom Fluidzufluss 6 zum Fluidabfluss 7, ist eine Fluidfördermenge veränderbar. 1 shows a section through an inventively designed vane pump 10 , In a machine housing 1 is a tubular, in the machine housing 1 around a first axis of rotation 8th rotatably mounted cage 2 arranged. In an unnumbered interior volume of the cage 2 is a about a second axis of rotation 9 rotatably mounted rotor 5 arranged. The Ka 2 and the rotor 5 For example, in the present embodiment, there are six wings 3 , where only one wing is numbered, in operative connection with each other. For this are the wings 3 parallel to the axes of rotation 8th . 9 swiveling in the cage 2 while at the other end they are in grooves 11 in the rotor 5 are stored. In the area of the pivotable bearing in the rotor 5 become the wings 3 of spring elements 4 against a direction of rotation of the rotor symbolically represented by an arrow 5 against a side wall of the groove 11 pressed. When operating the vane pump 10 becomes the rotatable rotor 5 driven, causing the cage 2 over the wings 3 is turned. In this case, a fluid from a fluid flow shown in dashed lines 6 to a likewise shown in dashed lines fluid drain 7 promoted. By changing the distance of the first axis of rotation 8th to the second axis of rotation 9 , substantially perpendicular to a connecting line from the fluid inlet 6 to the fluid drain 7 , a fluid delivery rate is changeable.

Erfindungsgemäß weisen die Flügel 3 zumindest in dem Bereich, der in die Nuten 11 ragt, eine geringere Dicke auf als eine lichte Weite der Nuten 11 ist, wobei jeder Flügel 3 eine einzige Linienberührung mit der korrespondieren den Nut 11 aufweist und die Flügel 3 von Federelementen 4 entgegen einer Drehrichtung gegen die Linienberührung drückbar sind.According to the invention, the wings 3 at least in the area that is in the grooves 11 protrudes, a smaller thickness than a clear width of the grooves 11 is, each wing 3 a single line contact with the corresponding groove 11 has and the wings 3 of spring elements 4 against a direction of rotation against the line contact can be pressed.

Die erfindungsgemäße Flügelzellenpumpe 10 kann beispielsweise aus einem Kunststoff, wie ABS (Acrylbuthadienstyrol) oder einem Metall, beispielsweise einem Leichtmetall, wie Aluminium oder auch aus Verbundwerkstoffen gefertigt sein. Die erfindungsgemäße Flügelzellenpumpe 10 kann beispielsweise als Schmiermittelpumpe für eine Verbrennungskraftmaschine eingesetzt werden.The vane pump according to the invention 10 may for example be made of a plastic such as ABS (Acrylbuthadienstyrol) or a metal, such as a light metal, such as aluminum or composite materials. The vane pump according to the invention 10 For example, it can be used as a lubricant pump for an internal combustion engine.

Durch die erfindungsgemäße Ausgestaltung wird die innere Reibung durch Minimierung der reibenden Flächen (nur Linienberührung) und Gleitgeschwindigkeiten reduziert. Weiter werden die inneren Pumpwiderstände durch Reduktion des Arbeitshubes der Flügel 3 im Rotor 2 minimiert. Darüber hinaus ist in vorteilhafter Weise keine Passung der Flügel 3 im Rotor 2 notwendig, wodurch die erfindungsgemäße Flügelzellenpumpe 10 unempfindlich gegenüber Schmutz ist. Darüber hinaus werden die Volumina der Nebenkammern durch die Anordnung und die Form der Flügel 3 verkleinert, wodurch eine Verringerung der Drehungleichförmigkeit erzielt ist. Weiter wird der radiale Hub der Flügel 3 durch Überlagerung einer tangentialen Bewegung verringert. Dadurch kann der Rotor 2, bei gleicher Baugröße der Flügelzellenpumpe 10, stabiler gestaltet werden.The inventive design, the internal friction is reduced by minimizing the rubbing surfaces (only line contact) and sliding speeds. Further, the internal pumping resistance by reducing the working stroke of the wings 3 in the rotor 2 minimized. In addition, advantageously no fit of the wings 3 in the rotor 2 necessary, whereby the vane pump according to the invention 10 Insensitive to dirt. In addition, the volumes of the secondary chambers are determined by the arrangement and shape of the wings 3 reduced, whereby a reduction in rotational nonuniformity is achieved. Next is the radial stroke of the wings 3 reduced by superposition of a tangential movement. This allows the rotor 2 , with the same size of the vane pump 10 , be made more stable.

Das grundsätzliche Funktionsprinzip der erfindungsgemäßen Flügelzellenpumpe 10 mit einseitiger Flügelanlage mit Linienberührung entspricht dem bisher bekannten Stand der Technik. Die Neuerung liegt in der über einen weiteren Bereich eines Umlaufs einseitigen Anlage des Flügels 3 in einer Nut 11 im Rotor 2. Dabei gleitet bzw. rollt der Flügel 3 in der Nut 11 des Rotors 2 ab. Damit der Rotor 5 die Drehbewegung auf dem Käfig 2, über die darin drehbar verankerten Flügel 3 übertragen kann, ist eine aufeinander abgestimmte Form von Flügel 3 und Nut 11 im Rotor 5 erforderlich. Die Form der Flügel 3 und der Nuten 11 beeinflussen sich gegenseitig. Zusätzlich wird die Form der Flügel 3 und der Nuten 11 von der Exzentrizität (Rotor 5, Käfig 2) und dem Anstellwinkel des Flügels 3 im Käfig 2 beeinflusst. Damit eine kontinuierliche Kraftübertragung möglich ist, muss die Nut 11 so geformt sein, dass der Freiheitsgrad des Flügels 3 über einen Bereich einer Umdrehung (360° geteilt durch die Anzahl der Flügel) so weit eingeschränkt wird, dass über Formschluss die Kraft übertragen werden kann.The basic operating principle of the vane pump according to the invention 10 with one-sided wing system with line contact corresponds to the previously known prior art. The innovation lies in the over a wider range of a circulation one-sided investment of the wing 3 in a groove 11 in the rotor 2 , It slides or rolls the wing 3 in the groove 11 of the rotor 2 from. So that the rotor 5 the rotary motion on the cage 2 , about the wings rotatably anchored therein 3 is a coordinated shape of wings 3 and groove 11 in the rotor 5 required. The shape of the wings 3 and the grooves 11 influence each other. In addition, the shape of the wings 3 and the grooves 11 from the eccentricity (rotor 5 , Cage 2 ) and the angle of attack of the wing 3 in the cage 2 affected. For a continuous power transmission is possible, the groove 11 be shaped so that the degree of freedom of the wing 3 is limited over a range of one revolution (360 ° divided by the number of blades) so far that the force can be transmitted via positive engagement.

Denkbar ist aber auch eine kinematische Umkehrung, d. h. die Flügel 3 sind schwenkbar in der Nabe 5 gelagert und der Arbeitshubausgleich wird durch entsprechend geformte Nuten 11 im Käfig 2 gewährleistet.It is also conceivable, however, a kinematic reversal, ie the wings 3 are pivotable in the hub 5 stored and the working stroke compensation is by appropriately shaped grooves 11 in the cage 2 guaranteed.

2 zeigt eine Detailansicht eines Flügels 3 mit einem Federelement 4 aus 1. 2 shows a detail view of a grand piano 3 with a spring element 4 out 1 ,

Nochmals die Vorteile der erfindungsgemäßen Flügelzellenpumpe 10 in Stichworten:

  • – Verringerung der inneren Reibung, weniger Verschleiß;
  • – Innerer Pumpwiderstand wird reduziert;
  • – Unempfindlichkeit gegen Schmutz;
  • – Geringere Anfälligkeit gegen Kavitation;
  • – Geringere innere Verschäumung des Fluids.
Again the advantages of the vane pump according to the invention 10 in keywords:
  • - Reduction of internal friction, less wear;
  • - Internal pumping resistance is reduced;
  • - insensitivity to dirt;
  • - Less susceptibility to cavitation;
  • - Lower internal foaming of the fluid.

11
Maschinengehäusemachine housing
22
KäfigCage
33
Flügelwing
44
Federelementspring element
55
Rotorrotor
66
Fluidzuflussfluid inflow
77
Fluidabflussfluid outflow
88th
erste Drehachsefirst axis of rotation
99
zweite Drehachsesecond axis of rotation
1010
FlügelzellenpumpeVane pump
1111
Nutgroove

ZITATE ENTHALTEN IN DER BESCHREIBUNGQUOTES INCLUDE IN THE DESCRIPTION

Diese Liste der vom Anmelder aufgeführten Dokumente wurde automatisiert erzeugt und ist ausschließlich zur besseren Information des Lesers aufgenommen. Die Liste ist nicht Bestandteil der deutschen Patent- bzw. Gebrauchsmusteranmeldung. Das DPMA übernimmt keinerlei Haftung für etwaige Fehler oder Auslassungen.This list The documents listed by the applicant have been automated generated and is solely for better information recorded by the reader. The list is not part of the German Patent or utility model application. The DPMA takes over no liability for any errors or omissions.

Zitierte PatentliteraturCited patent literature

  • - DE 29514202 U1 [0002] - DE 29514202 U1 [0002]

Claims (3)

Flügelzellenpumpe (10) in einem Maschinengehäuse (1) mit einem Fluidzufluss (6) und einem weitgehend diametral zu dem Fluidzufluss (6) angeordneten Fluidabfluss (7) und mit einem, in dem Maschinengehäuse (1) um eine erste Drehachse (8) drehbar angeordneten, weitgehend rohrförmigen Käfig (2) und mit einem, in einem Innenraum des Käfigs (2) angeordneten, um eine zweite, zur ersten Drehachse (8) parallelen Drehachse (9) drehbaren Rotor (5), wobei der Käfig (2) und der Rotor (5) über zumindest vier, einerseits koaxial zu den Drehachsen (8, 9) schwenkbar gelagerte und andererseits in sich in Richtung der Drehachsen (8, 9) erstreckenden, zu den Flügeln (3) korrespondierenden Nuten (11) geführten Flügel (3) derart miteinander in Wirkverbindung stehen, dass bei einer Drehung des Rotors (5) der Käfig (2) mitdrehbar ist, wobei durch die Drehung ein Fluid vom Fluidzufluss (6) zum Fluidabfluss (7) förderbar ist, dadurch gekennzeichnet, dass die Flügel (3) zumindest in dem Bereich, der in die Nuten (11) ragt, eine geringere Dicke aufweisen als eine lichte Weite der Nuten (11) ist, wobei jeder Flügel (3) eine einzige Linienberührung mit der korrespondierenden Nut (11) aufweist und die Flügel (3) von Federelementen (4) entgegen einer Drehrichtung gegen die Linienberührung drückbar sind.Vane pump ( 10 ) in a machine housing ( 1 ) with a fluid inflow ( 6 ) and a largely diametrically to the fluid flow ( 6 ) arranged fluid outflow ( 7 ) and with one, in the machine housing ( 1 ) about a first axis of rotation ( 8th ) rotatably arranged, largely tubular cage ( 2 ) and with one, in an interior of the cage ( 2 ), to a second, to the first axis of rotation ( 8th ) parallel axis of rotation ( 9 ) rotatable rotor ( 5 ), with the cage ( 2 ) and the rotor ( 5 ) over at least four, on the one hand coaxial with the axes of rotation ( 8th . 9 ) pivotally mounted and on the other hand in the direction of the axes of rotation ( 8th . 9 ), to the wings ( 3 ) corresponding grooves ( 11 ) guided wings ( 3 ) are in operative connection with one another in such a way that upon rotation of the rotor ( 5 ) the cage ( 2 ) is rotatable, wherein the rotation of a fluid from the fluid inlet ( 6 ) to the fluid drain ( 7 ), characterized in that the wings ( 3 ) at least in the region that enters the grooves ( 11 ) protrudes, have a smaller thickness than a clear width of the grooves ( 11 ), each wing ( 3 ) a single line contact with the corresponding groove ( 11 ) and the wings ( 3 ) of spring elements ( 4 ) are pressed against a direction of rotation against the line contact. Flügelzellenpumpe nach Patentanspruch 1, dadurch gekennzeichnet, dass die Flügel (3) im Rotor (5) oder im Käfig (2) schwenkbar gelagert sind und die Federelemente (4) im Bereich der schwenkbaren Lagerungen angeordnet sind.Vane pump according to claim 1, characterized in that the wings ( 3 ) in the rotor ( 5 ) or in the cage ( 2 ) are pivotally mounted and the spring elements ( 4 ) are arranged in the region of the pivotable bearings. Flügelzellenpumpe nach Patentanspruch 1 oder 2, dadurch gekennzeichnet, dass die zweite Drehachse (9) des Rotors (5) zur ersten Drehachse (8) des Käfigs (2) weitgehend quer zu einer Verbindungslinie von dem Fluidzufluss (6) zu dem Fluidabfluss (7) parallel verschiebbar ist.Vane pump according to claim 1 or 2, characterized in that the second axis of rotation ( 9 ) of the rotor ( 5 ) to the first axis of rotation ( 8th ) of the cage ( 2 ) substantially transversely to a connecting line from the fluid inlet ( 6 ) to the fluid drain ( 7 ) is displaceable in parallel.
DE200810054009 2008-10-30 2008-10-30 Vane pump Active DE102008054009B4 (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012218972A1 (en) 2012-10-18 2014-04-24 Bayerische Motoren Werke Aktiengesellschaft Vane pump for use in machine housing, has external rotor and inner rotor that are connected over four wings and swingably supported in bearing axial stop for wings provided in region of swingable bearing
DE102014220766A1 (en) * 2014-10-14 2016-04-14 Continental Automotive Gmbh Pendulum slide machine
DE102019103974A1 (en) * 2019-02-18 2020-08-20 Angela Böckmann-Hannibal Liquid transfer pump
DE102019103970A1 (en) * 2019-02-18 2020-08-20 Angela Böckmann-Hannibal Rotor pump

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR980766A (en) * 1943-02-26 1951-05-17 Oscillating Allergies Pump
DE2460949A1 (en) * 1974-01-02 1975-07-10 Gustav Bernard Mielitz Combustion engine with rotating vane pistons - has piston to produce compressed air and combustion products driving second piston
US4435138A (en) * 1980-10-20 1984-03-06 Johnson Howard B Rotary vane machine with rotating end sealing plates
DE3431719A1 (en) * 1984-08-29 1986-03-13 SKF GmbH, 8720 Schweinfurt WING CELL PUMP
DE29514202U1 (en) 1995-09-05 1995-10-26 Bauer, Hans-Günter, 98678 Hirschendorf Pendulum slide machine
DE19545045A1 (en) * 1995-09-06 1997-03-13 Joma Polytec Kunststofftechnik Pump for liquids or gases with simple and effective construction
DE10352267A1 (en) * 2003-11-08 2005-06-16 Beez, Günther, Dipl.-Ing. Pendulum slide machine
DE102004051561A1 (en) * 2004-10-22 2006-05-04 Siemens Ag Vane pump
DE102006061326A1 (en) * 2006-12-22 2008-07-03 Beez, Günther, Dipl.-Ing. Adjusting device for use in e.g. lubricating oil pump in motor vehicle, has control pressure chambers separately controlled and subjected with pump- or main channel pressure and arranged at circumference of control slide valve

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR980766A (en) * 1943-02-26 1951-05-17 Oscillating Allergies Pump
DE2460949A1 (en) * 1974-01-02 1975-07-10 Gustav Bernard Mielitz Combustion engine with rotating vane pistons - has piston to produce compressed air and combustion products driving second piston
US4435138A (en) * 1980-10-20 1984-03-06 Johnson Howard B Rotary vane machine with rotating end sealing plates
DE3431719A1 (en) * 1984-08-29 1986-03-13 SKF GmbH, 8720 Schweinfurt WING CELL PUMP
DE29514202U1 (en) 1995-09-05 1995-10-26 Bauer, Hans-Günter, 98678 Hirschendorf Pendulum slide machine
DE19545045A1 (en) * 1995-09-06 1997-03-13 Joma Polytec Kunststofftechnik Pump for liquids or gases with simple and effective construction
DE10352267A1 (en) * 2003-11-08 2005-06-16 Beez, Günther, Dipl.-Ing. Pendulum slide machine
DE102004051561A1 (en) * 2004-10-22 2006-05-04 Siemens Ag Vane pump
DE102006061326A1 (en) * 2006-12-22 2008-07-03 Beez, Günther, Dipl.-Ing. Adjusting device for use in e.g. lubricating oil pump in motor vehicle, has control pressure chambers separately controlled and subjected with pump- or main channel pressure and arranged at circumference of control slide valve

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012218972A1 (en) 2012-10-18 2014-04-24 Bayerische Motoren Werke Aktiengesellschaft Vane pump for use in machine housing, has external rotor and inner rotor that are connected over four wings and swingably supported in bearing axial stop for wings provided in region of swingable bearing
DE102014220766A1 (en) * 2014-10-14 2016-04-14 Continental Automotive Gmbh Pendulum slide machine
DE102014220766B4 (en) * 2014-10-14 2017-11-02 Continental Automotive Gmbh Pendulum slide machine
DE102019103974A1 (en) * 2019-02-18 2020-08-20 Angela Böckmann-Hannibal Liquid transfer pump
DE102019103970A1 (en) * 2019-02-18 2020-08-20 Angela Böckmann-Hannibal Rotor pump

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