EP2486280B1 - Vane pump - Google Patents

Vane pump Download PDF

Info

Publication number
EP2486280B1
EP2486280B1 EP10752530.5A EP10752530A EP2486280B1 EP 2486280 B1 EP2486280 B1 EP 2486280B1 EP 10752530 A EP10752530 A EP 10752530A EP 2486280 B1 EP2486280 B1 EP 2486280B1
Authority
EP
European Patent Office
Prior art keywords
vane
vane pump
pressure
pump
consumer
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.)
Active
Application number
EP10752530.5A
Other languages
German (de)
French (fr)
Other versions
EP2486280A2 (en
EP2486280B8 (en
Inventor
Heiko Schulz-Andres
Christian Böhm
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.)
Magna Powertrain Bad Homburg GmbH
Original Assignee
ixetic Bad Homburg GmbH
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 ixetic Bad Homburg GmbH filed Critical ixetic Bad Homburg GmbH
Publication of EP2486280A2 publication Critical patent/EP2486280A2/en
Application granted granted Critical
Publication of EP2486280B1 publication Critical patent/EP2486280B1/en
Publication of EP2486280B8 publication Critical patent/EP2486280B8/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2/00Rotary-piston machines or pumps
    • F04C2/30Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F04C2/34Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members
    • F04C2/344Rotary-piston machines or pumps having the characteristics covered by two or more groups F04C2/02, F04C2/08, F04C2/22, F04C2/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in groups F04C2/08 or F04C2/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • 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
    • F01C21/0854Vane tracking; control therefor by fluid means
    • F01C21/0863Vane tracking; control therefor by fluid means the fluid being the working fluid
    • 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
    • F04C11/00Combinations of two or more machines or pumps, each being of rotary-piston or oscillating-piston type; Pumping installations
    • F04C11/001Combinations of two or more machines or pumps, each being of rotary-piston or oscillating-piston type; Pumping installations of similar working principle
    • 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
    • F04C15/00Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
    • F04C15/06Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
    • 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
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/30Rotary-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
    • F04C18/34Rotary-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
    • F04C18/344Rotary-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
    • 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
    • F04C2240/30Casings or housings
    • 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
    • F04C2240/80Other components

Definitions

  • the invention relates to a vane pump having a wing pump associated with a first consumer and an under wing pump including an under wing pressure area and a lower wing suction area connected to the wing pump.
  • German patent application DE 196 31 846 A1 is a generic vane pump with at least two each having a suction region and a pressure region having pump sections known.
  • German patent application DE 195 14 929 A1 is a vehicle device with a drive motor known to which at least two ancillaries are assigned, which are driven by a single electric motor.
  • the international publication WO 03/056180 A1 discloses a vane pump that can supply multiple consumers, but without using the underfloor pressure ranges as a supply to a separate consumer.
  • the German patent application DE 39 13 414 A1 discloses a multi-circuit control pump for pressure medium supply of several in the pressure level and demand quantity of different supply circuits.
  • the object of the invention is to change a vane pump with a wing pump, which is associated with a first consumer, and an underfloor pump, which includes an underfloor pressure region and a lower wing suction, which is connected to the wing pump to change so that with the vane pump different consumers with hydraulic medium volume flows can be supplied, which are different in size and / or have different pressures.
  • the object is solved in a vane pump with a wing pump associated with a first consumer and an underfloor pump including an underfloor pressure area and a lower wing suction area connected to the wing pump, wherein the underfloor pressure area is separated from the lower wing suction area and a second consumer
  • the underfloor pressure range is assigned to the second consumer. Due to the subdivision of the underfloor pump according to the invention can with the vane pump to simple Way different volume flows are provided at different pressure levels at the same time.
  • a preferred embodiment of the vane pump is characterized in that the lower wing suction and the lower wing pressure range can be acted upon with different pressures. This makes it possible for the vane pump to simultaneously provide different pressure levels for different consumers.
  • the lower wing suction area and the lower wing pressure area are also referred to as under wing areas.
  • the lower wing suction region comprises at least one lower wing groove section which is assigned to the first consumer via a pressure region of the wing pump.
  • hydraulic medium is pressurized and conveyed in the form of a hydraulic medium volume flow to the first consumer.
  • a further preferred exemplary embodiment of the vane pump is characterized in that the lower vane groove portion of the lower vane suction region is arranged radially inside and in the circumferential direction overlapping to a suction region of the vane pump.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that the lower-wing pressure region comprises at least one lower-wing groove section which is assigned to the second consumer.
  • the underfloor groove portion of the underfoil pressure range is preferably directly, for example via a corresponding hydraulic line or a corresponding hydraulic channel, with the second consumer in combination.
  • the underfoil pressure range is supplied during operation of the vane pump by entrainment of the hydraulic medium from the lower wing suction with hydraulic medium.
  • a further preferred exemplary embodiment of the vane pump is characterized in that the lower vane groove portion of the lower vane pressure region is arranged radially inside and in the circumferential direction overlapping one or the pressure region of the upper vane pump.
  • the vanes move radially inwardly during operation of the vane pump, thereby pressurizing the hydraulic medium in the underfloor groove portion of the underfloor pressure area by the incoming vanes.
  • the retraction of the wings in the pressure range is effected by the stroke contour of the vane pump.
  • the lower wing suction region and the lower wing pressure region each comprise two diametrically arranged lower blade groove sections.
  • the lower-wing groove portions of the lower-wing suction region are preferably arranged radially inward and circumferentially overlapping each with one of two suction regions of the vane-cell pump.
  • the underfloor groove sections of the underfoil pressure region are preferably arranged radially in each case and overlapping in the circumferential direction in each case to one of two pressure regions of the vane pump.
  • Another preferred embodiment of the vane pump is characterized in that the lower wing suction and the lower wing pressure range are separated by a seal.
  • the seal prevents unwanted pressure equalization between the two lower wing areas.
  • a further preferred embodiment of the vane pump is characterized in that the seal has in plan view substantially the shape of a figure eight, outside which the lower wing suction area and within which the lower wing pressure area is arranged.
  • the figure 8 is designed at its center so as to leave free a distance which establishes a connection between the two underfloor groove portions of the underfoil printing area.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that a check valve is arranged between the second consumer and the lower-wing pressure region assigned to it.
  • the check valve on the one hand prevents unwanted backflow of hydraulic medium.
  • the check valve allows a demand-dependent switching off of the second consumer associated Untereriel Kunststoff Kunststoffs.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that the underfloor pressure region can be connected to the lower-wing suction region via a switching valve device.
  • the switching valve device serves to shut off the underfloor pressure range. As a result, the power required to drive the vane pump can be reduced. For a discontinuous charging of the hydraulic accumulator, the underfloor pressure range can be switched on with the aid of the switching valve device as needed.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that the underfloor pressure region can be connected to the first consumer via a switching valve device.
  • This embodiment is particularly advantageous when the vane pump is electrically driven and has a higher starting speed than pumps driven directly by an internal combustion engine.
  • a further preferred embodiment of the vane pump is characterized in that the switching valve device is electromagnetically or hydraulically actuated.
  • the underfoil pressure range can be connected to the lower-wing suction region or to the first consumer when the pressure in the hydraulic accumulator is above a desired minimum pressure.
  • the pressure in the hydraulic accumulator is detected, for example, by means of a pressure sensor.
  • the pressure in the hydraulic accumulator can be used directly for sensing.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that an additional valve device is connected between the lower-wing suction region or the pressure region of the upper-wing pump and the consumer associated therewith.
  • the valve device can be designed as a switching valve or as a check valve.
  • the additional valve device is preferably used to separate the pressure output of the wing pump at standstill of the vane pump from the first consumer.
  • a further preferred embodiment of the vane pump is characterized in that the operating pressure in the lower wing pressure range is greater than in the lower wing suction. This ensures that the wings always rest against the stroke contour in the pressure area and in a separation area of the wing pump.
  • a further preferred exemplary embodiment of the vane-cell pump is characterized in that a hydraulic resistance is connected between the lower-wing regions or between the lower-wing pressure region and the first consumer.
  • the hydraulic resistance is designed, for example, as a hydraulic bottleneck or as a throttle.
  • FIG. 1 is a vane pump 1 very simplified schematically shown.
  • the structure and function of the vane pump 1 are, for example, in the German Offenlegungsschrift DE 196 31 846 A1 described.
  • switchable double-stroke vane pumps can be used.
  • the two pump floods resulting from the Doppelhubmaschine, separately conveyed from the pump and fed to different consumers.
  • the vane pump 1 which is shown in a highly simplified manner, is supplied with hydraulic fluid from a tank 2 to a vane pump area 4 and an underwing pump area 5.
  • the two vane pump areas 4, 5 represent a vane pump, which is operated by vanes of the vane pump 1.
  • the conveying effect of the underfloor pump is achieved by a lifting movement of the radially inner wing ends.
  • the vane pump 1 comprises the wing pump with two substantially crescent-shaped delivery spaces, which are traversed by the wings and are arranged in the radial direction between a rotor and a stroke contour.
  • the rotor and the stroke contour are limited in the axial direction on one side by a pressure plate, which is arranged for example in a housing of the vane pump 1.
  • the upper wing pump region 4 is connected to a first consumer 6 in connection.
  • the underwing pump area 5 communicates with a second consumer 7.
  • the second consumer 7 comprises a hydraulic accumulator 8.
  • the vane pump 1 is, preferably in a motor vehicle, used to supply a transmission with hydraulic medium, which can be acted upon by the vane pump 1 with different pressures.
  • the hydraulic accumulator 8 requires, for example, a hydraulic pressure of about 20 bar.
  • the underwing pump area 5 has a stroke volume of approximately one cubic centimeter.
  • the vane pump 1 is preferably driven by an electric motor.
  • the first consumer 6 is, for example, a wet clutch which requires a volume flow of up to 30 liters per minute for cooling at a pressure of 3 bar.
  • a volumetric flow ratio of 7 to 1 and a pressure ratio of 1 to 6 can be provided.
  • the two vane pump areas 4 and 5 can be operated simultaneously.
  • the underfloor pump the vane pump 1 is used with its underwing pump area 5 as an independent pump to charge the hydraulic accumulator 8.
  • a vane pump 11 is shown in various embodiments. The same or similar parts are provided with the same reference numerals.
  • the vane pump 11 is connected to a tank 12 with hydraulic medium, in particular oil.
  • a pressure plate 13 is shown, which represents an axial bearing surface for the rotor and / or the blades of the vane pump 1.
  • the pressure plate 13 comprises two suction regions 15, 16 and two pressure regions 17, 18 of the overflow pump.
  • the pressure plate 13 further comprises one of the underfloor pump with a lower wing suction region, which comprises two Untererielnutabête 21, 22.
  • the two Untererielnutabête 21, 22 are arranged radially inwardly and circumferentially overlapping the two suction regions 15, 16 of the wing pump.
  • dashed lines hydraulic lines or hydraulic channels are indicated, via which the two Untererielnutab mustarde 21, 22 are each connected to one of the pressure areas 17, 18 of the wing pump.
  • the pressure areas 17, 18 of the wing pump in turn are connected via hydraulic lines or hydraulic channels 23, 24 with a first consumer 26 in connection.
  • a second load 27 comprises a hydraulic accumulator 28 and is connected via hydraulic lines or hydraulic channels 29, 30 with Untererielnutabroughen 31, 32 of an underfloor pressure range of the underfloor pump in connection.
  • the two Untererielnutabroughe 31, 32 are each disposed radially inwardly and circumferentially overlapping the pressure areas 18, 17 of the wing pump.
  • the Untererielnutabroughe 21, 22 and 31, 32 have substantially the shape of circular arcs, which are arranged on a common circle.
  • the Untererielnutabitese 21, 22 of the lower wing suction are filled, for example, indicated by dashed lines channels or holes in the pressure plate 13 from the wing pump with hydraulic medium.
  • the wings are forcibly extended by the pressure in the two Untererielnutabêten 21, 22 in the suction regions 15, 16.
  • the wings are by design retracted by the interaction with the stroke contour, so that the hydraulic medium in the Untererielnutabêten 31, 32 is acted upon by the retracting wing with pressure.
  • This relatively high pressure is used to fill the hydraulic accumulator 28 with hydraulic medium.
  • the by the small size of the Untererielnutabête 31, 32 relatively small volume flow is sufficient for this purpose.
  • the first consumer 26 is supplied via the pressure regions 17, 18 of the wing pump with a significantly larger volume flow, which is, however, subjected to a significantly lower pressure.
  • the pressure plate 13 is shown in plan view on one side and folded 180 degrees in the bottom view on the other side.
  • the separation points between the Untererielnutabêten 21, 22 and 31, 32 are preferably in angular ranges of the stroke contour, where no significant change in volume of the delivery chambers of the vane pump 11 occurs.
  • FIG. 4 it can be seen that the two Untererielnutabitese 31, 32 are disposed within a substantially eight-shaped first seal 35.
  • the two Untererielnutabitese 21, 22 and extending through the pressure plate 13 through pressure regions 17, 18 of the wing pump are arranged outside of the eight-shaped first seal 35 and within a circular second seal 36.
  • the two seals 35, 36 serve to seal against a housing of the vane pump 11 or a control plate of a transmission.
  • the eight-shaped first seal 35 is designed in the illustrated embodiment so that the two Untererielnutabête 31, 32 communicate with each other. By appropriate modification of the first seal 35 or by using two circular seals, the two Untererielnutabête 31, 32 but also be sealed individually.
  • FIG. 4 illustrated pressure transfer has the advantage that an undesirable plate deflection can be compensated by the increased pressures in the Untererielnutabêten 31, 32 on the rotor side of the pressure plate 13 by the pressurization with the increased pressure on the sealing side to the housing or to a control plate of a transmission.
  • the gap heights should always be designed in a measure that is inversely proportional to the pressure. As a result, the towing capacity can be minimized.
  • the ratio of the two consumers 26, 27 supplied volume flows can be varied.
  • the pump volume of the underfloor pump results from the thickness of the wings and the length of the wing stroke.
  • the stroke volume of the underfloor pump can be varied in a simple manner. With a given geometry of the wing pump doubling the wing thickness leads to a significant change in the pump delivery volume.
  • the ratio of the width of the rotor group to the wing stroke the input power of the vane pump can also be influenced.
  • a branch 40 is provided between the hydraulic lines 29, 30 and the second load 27.
  • a check valve 41 is provided which prevents unwanted backflow of hydraulic fluid from the hydraulic accumulator 28 when the vane pump 11 is stationary.
  • the underfloor pump in particular the second consumer 27 associated underfloor pump area with the Untererielnutabêten 31, 32, can be switched off. This is particularly useful in the application of the vane pump 11 according to the invention, since the charging of the hydraulic accumulator 28 is preferably carried out discontinuously.
  • a hydraulic line or a hydraulic channel 42 goes out, which is connected via further hydraulic lines or hydraulic channels 43, 44 with the two Untererielnutabbalden 21, 22 of the lower wing suction.
  • a switching valve device 45 is arranged, which is designed as a 2/2-way valve with an open position and a blocking position. By a spring, the switching valve device 45 is biased in the illustrated blocking position.
  • the switching valve means 45 By switching the switching valve means 45 to the open position, the communication between the under-wing groove portions 31, 32 of the under-wing pressure portion with the under-wing groove portions 21, 22 of the lower-wing suction portion is released. Thereby, the driving power of the vane pump 1 can be reduced when there is no need to charge the hydraulic accumulator 28.
  • the connection of the two sub-vane pump areas via the switching valve 45 also provides the advantage that when starting the vane pump 1 immediately hydraulic medium under the wings in the suction areas 15, 16 is promoted to force an extension of these wings.
  • FIG. 6 an embodiment of the vane pump 11 is shown, in which the branch 40 via a hydraulic line 52 or a hydraulic channel and with the interposition of a switching valve device 55 directly to the pressure output of the wing pump or the first load 26 is connectable.
  • This arrangement is advantageous in electrically driven vane pumps 11, which typically have a higher starting speed than pumps driven directly by an internal combustion engine.
  • the operating pressure in the underfloor groove portions 31, 32 of the underfloor pressure region is always above the operating pressure in the underfloor groove portions 21, 22 of the lower wing suction region. This can ensure that the wings in the pressure areas 17, 18 and the separation areas in operation always rest against the stroke contour.
  • the throttle 48; 58 can also in the respective switching valve device 45; 55 be integrated.
  • FIG. 7 is indicated by a symbol 60 that the switching valve device 55 from FIG. 6 can be electrically or electromagnetically actuated.
  • the switching valve 55 is preferably always switched from its illustrated blocking position to its open position, not shown, when the pressure in the hydraulic accumulator 28 is above a minimum pressure.
  • the pressure in the hydraulic accumulator 28 is detected by means of a pressure sensor.
  • switching valve 45 may also be hydraulically actuated, as indicated by a control pressure line 64 and a symbol 65 on the switching valve device 45.
  • This in FIG. 6 shown switching valve 55, as well as the switching valve 45 in FIG. 8 , hydraulically operated.
  • hydraulic actuation of the pressure in the hydraulic accumulator 28 is used directly for sensing.
  • the switching valve 45 is closed and the underfloor pump conveys via the Untererielnutabête 31, 32 of the Untererieldruck Schemes via the check valve 41 in the hydraulic accumulator 28.
  • the switching valve 45 is opened and the underfloor pump promotes the Untererielnutabêten 31st , 32 lower wing pressure range over the Untererielnutabête 21, 22 of the lower wing suction and the pressure areas 17, 18 with the lower operating pressure of the wing pump.
  • FIG. 9 is a similar vane pump 71 as in FIG. 1 shown greatly simplified. Since only relatively small volume flows are supplied to the second consumer 7 with the lower pad pump region 5, in contrast to the upper pad pump region 4, both the check valve 40 and the switching valve device 45 can be made relatively small and integrated into the vane pump 71 in a simple manner. In addition, the throttle 48 in the vane pump 71, in particular in the switching valve 45, are integrated. This results in a compact unit that only needs to be connected with three connections to the tank 2 and the two consumers 6 and 7.
  • the output of the wing pump can be separated by a switching valve device 74 and a check valve 80 from the consumer 26.
  • a switching valve device 74 is designed as a 2/2-way valve, which by means of a spring in its illustrated blocking position is biased.
  • the operating pressure of the vane cell pump acting on the switching valve 74 via a control pressure line 75 ensures that the switching valve 74 opens and releases the connection between the vane pump 11 and the consumer 26.
  • the spring side of the switching valve 74 is connected to ambient pressure, so that at the switching valve 74 no throttle losses for keeping the switching valve 74 open.

Description

Die Erfindung betrifft eine Flügelzellenpumpe mit einer Oberflügelpumpe, die einem ersten Verbraucher zugeordnet ist, und einer Unterflügelpumpe, die einen Unterflügeldruckbereich und einen Unterflügelsaugbereich umfasst, der mit der Oberflügelpumpe verbunden ist.The invention relates to a vane pump having a wing pump associated with a first consumer and an under wing pump including an under wing pressure area and a lower wing suction area connected to the wing pump.

Aus der deutschen Offenlegungsschrift DE 196 31 846 A1 ist eine gattungsgemäße Flügelzellenpumpe mit mindestens zwei jeweils einen Saugbereich und einen Druckbereich aufweisenden Pumpenabschnitten bekannt. Aus der deutschen Offenlegungsschrift DE 195 14 929 A1 ist eine Fahrzeugeinrichtung mit einem Antriebsmotor bekannt, dem mindestens zwei Nebenaggregate zugeordnet sind, die durch einen einzigen Elektromotor antreibbar sind. Die internationale Veröffentlichung WO 03/056180 A1 offenbart eine Flügelzellenpumpe, die mehrere Verbraucher versorgen kann, jedoch ohne die Unterflügeldruckbereiche als Versorgung für einen getrennten Verbraucher zu verwenden. Die deutsche Offenlegungsschrift DE 39 13 414 A1 offenbart eine Mehrkreis-Regelpumpe zur Druckmittelversorgung mehrerer im Druckniveau und Bedarfsmenge unterschiedlicher Versorgungskreise.From the German patent application DE 196 31 846 A1 is a generic vane pump with at least two each having a suction region and a pressure region having pump sections known. From the German patent application DE 195 14 929 A1 is a vehicle device with a drive motor known to which at least two ancillaries are assigned, which are driven by a single electric motor. The international publication WO 03/056180 A1 discloses a vane pump that can supply multiple consumers, but without using the underfloor pressure ranges as a supply to a separate consumer. The German patent application DE 39 13 414 A1 discloses a multi-circuit control pump for pressure medium supply of several in the pressure level and demand quantity of different supply circuits.

Aufgabe der Erfindung ist es, eine Flügelzellenpumpe mit einer Oberflügelpumpe, die einem ersten Verbraucher zugeordnet ist, und einer Unterflügelpumpe, die einen Unterflügeldruckbereich und einen Unterflügelsaugbereich umfasst, der mit der Oberflügelpumpe verbunden ist, so zu verändern, dass mit der Flügelzellenpumpe unterschiedliche Verbraucher mit Hydraulikmediumvolumenströmen versorgt werden können, die unterschiedlich groß sind und/oder unterschiedliche Drücke aufweisen.The object of the invention is to change a vane pump with a wing pump, which is associated with a first consumer, and an underfloor pump, which includes an underfloor pressure region and a lower wing suction, which is connected to the wing pump to change so that with the vane pump different consumers with hydraulic medium volume flows can be supplied, which are different in size and / or have different pressures.

Die Aufgabe ist bei einer Flügelzellenpumpe mit einer Oberflügelpumpe, die einem ersten Verbraucher zugeordnet ist, und einer Unterflügelpumpe, die einen Unterflügeldruckbereich und einen Unterflügelsaugbereich umfasst, der mit der Oberflügelpumpe verbunden ist, dadurch gelöst, dass der Unterflügeldruckbereich von dem Unterflügelsaugbereich getrennt und einem zweiten Verbraucher zugeordnet ist.. Gemäß einem wesentlichen Aspekt der Erfindung wird der Unterflügeldruckbereich dem zweiten Verbraucher zugeordnet. Durch die erfindungsgemäße Unterteilung der Unterflügelpumpe können mit der Flügelzellenpumpe auf einfache Art und Weise unterschiedliche Volumenströme auf unterschiedlichen Druckniveaus zeitgleich bereitgestellt werden.The object is solved in a vane pump with a wing pump associated with a first consumer and an underfloor pump including an underfloor pressure area and a lower wing suction area connected to the wing pump, wherein the underfloor pressure area is separated from the lower wing suction area and a second consumer According to one essential aspect of the invention, the underfloor pressure range is assigned to the second consumer. Due to the subdivision of the underfloor pump according to the invention can with the vane pump to simple Way different volume flows are provided at different pressure levels at the same time.

Ein bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelsaugbereich und der Unterflügeldruckbereich mit unterschiedlichen Drücken beaufschlagbar sind. Dadurch ist es möglich, dass die Flügelzellenpumpe gleichzeitig unterschiedliche Druckniveaus für verschiedene Verbraucher bereitstellt. Der Unterflügelsaugbereich und der Unterflügeldruckbereich werden auch als Unterflügelbereiche bezeichnet.A preferred embodiment of the vane pump is characterized in that the lower wing suction and the lower wing pressure range can be acted upon with different pressures. This makes it possible for the vane pump to simultaneously provide different pressure levels for different consumers. The lower wing suction area and the lower wing pressure area are also referred to as under wing areas.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelsaugbereich mindestens einen Unterflügelnutabschnitt umfasst, der über einen Druckbereich der Oberflügelpumpe dem ersten Verbraucher zugeordnet ist. In dem Druckbereich der Oberflügelpumpe wird Hydraulikmedium mit Druck beaufschlagt und in Form eines Hydraulikmediumvolumenstroms zu dem ersten Verbraucher gefördert. Durch eine Verbindung zwischen dem Unterflügelnutabschnitt des Unterflügelsaugbereichs und dem Druckbereich der Oberflügelpumpe wird dieser Unterflügelnutabschnitt auf das gleiche Druckniveau wie der erste Verbraucher gebracht.Another preferred exemplary embodiment of the vane pump is characterized in that the lower wing suction region comprises at least one lower wing groove section which is assigned to the first consumer via a pressure region of the wing pump. In the pressure range of the wing pump, hydraulic medium is pressurized and conveyed in the form of a hydraulic medium volume flow to the first consumer. Through a connection between the lower wing groove portion of the lower wing suction area and the pressure area of the upper wing pump, this lower wing groove portion is brought to the same pressure level as the first consumer.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelnutabschnitt des Unterflügelsaugbereichs radial innerhalb und in Umfangsrichtung überlappend zu einem Saugbereich der Oberflügelpumpe angeordnet ist. Durch diese Anordnung und die Verbindung mit dem Druckbereich der Oberflügelpumpe wird sichergestellt, dass die Flügel der Flügelzellenpumpe sicher ausfahren, so dass sie radial außen an einer Hubkontur der Flügelzellenpumpe anliegen.A further preferred exemplary embodiment of the vane pump is characterized in that the lower vane groove portion of the lower vane suction region is arranged radially inside and in the circumferential direction overlapping to a suction region of the vane pump. By this arrangement and the connection with the pressure range of the wing pump ensures that the wings of the vane pump safely extend, so that they rest radially outward on a stroke contour of the vane pump.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügeldruckbereich mindestens einen Unterflügelnutabschnitt umfasst, der dem zweiten Verbraucher zugeordnet ist. Der Unterflügelnutabschnitt des Unterflügeldruckbereichs steht vorzugsweise direkt, zum Beispiel über eine entsprechende Hydraulikleitung oder einen entsprechenden Hydraulikkanal, mit dem zweiten Verbraucher in Verbindung. Der Unterflügeldruckbereich wird im Betrieb der Flügelzellenpumpe durch Mitnahme des Hydraulikmediums aus dem Unterflügelsaugbereich mit Hydraulikmedium versorgt.A further preferred exemplary embodiment of the vane-cell pump is characterized in that the lower-wing pressure region comprises at least one lower-wing groove section which is assigned to the second consumer. The underfloor groove portion of the underfoil pressure range is preferably directly, for example via a corresponding hydraulic line or a corresponding hydraulic channel, with the second consumer in combination. The underfoil pressure range is supplied during operation of the vane pump by entrainment of the hydraulic medium from the lower wing suction with hydraulic medium.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelnutabschnitt des Unterflügeldruckbereichs radial innerhalb und in Umfangsrichtung überlappend zu einem beziehungsweise dem Druckbereich der Oberflügelpumpe angeordnet ist. In dem Druckbereich der Oberflügelpumpe bewegen sich die Flügel im Betrieb der Flügelzellenpumpe radial nach innen, wodurch das Hydraulikmedium in dem Unterflügelnutabschnitt des Unterflügeldruckbereichs durch die einfahrenden Flügel mit Druck beaufschlagt wird. Das Einfahren der Flügel im Druckbereich wird durch die Hubkontur der Flügelzellenpumpe bewirkt.A further preferred exemplary embodiment of the vane pump is characterized in that the lower vane groove portion of the lower vane pressure region is arranged radially inside and in the circumferential direction overlapping one or the pressure region of the upper vane pump. In the pressure range of the wing pump, the vanes move radially inwardly during operation of the vane pump, thereby pressurizing the hydraulic medium in the underfloor groove portion of the underfloor pressure area by the incoming vanes. The retraction of the wings in the pressure range is effected by the stroke contour of the vane pump.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelsaugbereich und der Unterflügeldruckbereich jeweils zwei diametral angeordnete Unterflügelnutabschnitte umfasst. Die Unterflügelnutabschnitte des Unterflügelsaugbereichs sind vorzugsweise jeweils radial innerhalb und in Umfangsrichtung überlappend zu jeweils einem von zwei Saugbereichen der Flügelzellenpumpe angeordnet. Analog sind die Unterflügelnutabschnitte des Unterflügeldruckbereichs vorzugsweise jeweils radial innerhalb und in Umfangsrichtung überlappend zu jeweils einem von zwei Druckbereichen der Flügelzellenpumpe angeordnet.Another preferred exemplary embodiment of the vane pump is characterized in that the lower wing suction region and the lower wing pressure region each comprise two diametrically arranged lower blade groove sections. The lower-wing groove portions of the lower-wing suction region are preferably arranged radially inward and circumferentially overlapping each with one of two suction regions of the vane-cell pump. Analogously, the underfloor groove sections of the underfoil pressure region are preferably arranged radially in each case and overlapping in the circumferential direction in each case to one of two pressure regions of the vane pump.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügelsaugbereich und der Unterflügeldruckbereich durch eine Dichtung voneinander getrennt sind. Die Dichtung verhindert einen unerwünschten Druckausgleich zwischen den beiden Unterflügelbereichen.Another preferred embodiment of the vane pump is characterized in that the lower wing suction and the lower wing pressure range are separated by a seal. The seal prevents unwanted pressure equalization between the two lower wing areas.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass die Dichtung in der Draufsicht im Wesentlichen die Gestalt einer Acht aufweist, außerhalb welcher der Unterflügelsaugbereich und innerhalb welcher der Unterflügeldruckbereich angeordnet ist. Dabei ist die Acht, im Unterschied zu der normalen Schreibweise, in ihrer Mitte so gestaltet, dass ein Abstand freibleibt, der eine Verbindung zwischen den beiden Unterflügelnutabschnitte des Unterflügeldruckbereichs schafft.A further preferred embodiment of the vane pump is characterized in that the seal has in plan view substantially the shape of a figure eight, outside which the lower wing suction area and within which the lower wing pressure area is arranged. In this case, unlike the usual notation, the figure 8 is designed at its center so as to leave free a distance which establishes a connection between the two underfloor groove portions of the underfoil printing area.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass zwischen dem zweiten Verbraucher und dem diesem zugeordneten Unterflügeldruckbereich ein Rückschlagventil angeordnet ist. Das Rückschlagventil verhindert einerseits ein unerwünschtes Rückströmen von Hydraulikmedium. Darüber hinaus ermöglicht das Rückschlagventil ein bedarfsabhängiges Abschalten des dem zweiten Verbraucher zugeordneten Unterflügeldruckbereichs.A further preferred exemplary embodiment of the vane-cell pump is characterized in that a check valve is arranged between the second consumer and the lower-wing pressure region assigned to it. The check valve on the one hand prevents unwanted backflow of hydraulic medium. In addition, the check valve allows a demand-dependent switching off of the second consumer associated Unterflügeldruckbereichs.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügeldruckbereich über eine Schaltventileinrichtung mit dem Unterflügelsaugbereich verbindbar ist. Die Schaltventileinrichtung dient dazu, den Unterflügeldruckbereich abzuschalten. Dadurch kann die zum Antrieb der Flügelzellenpumpe benötigte Leistung reduziert werden. Zu einem diskontinuierlichen Aufladen des Hydraulikspeichers kann der Unterflügeldruckbereich mit Hilfe der Schaltventileinrichtung bedarfsabhängig eingeschaltet werden.A further preferred exemplary embodiment of the vane-cell pump is characterized in that the underfloor pressure region can be connected to the lower-wing suction region via a switching valve device. The switching valve device serves to shut off the underfloor pressure range. As a result, the power required to drive the vane pump can be reduced. For a discontinuous charging of the hydraulic accumulator, the underfloor pressure range can be switched on with the aid of the switching valve device as needed.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Unterflügeldruckbereich über eine Schaltventileinrichtung mit dem ersten Verbraucher verbindbar ist. Diese Ausführung ist besonders vorteilhaft, wenn die Flügelzellenpumpe elektrisch angetrieben ist und eine höhere Startdrehzahl aufweist als Pumpen, die direkt von einem Verbrennungsmotor angetrieben werden.A further preferred exemplary embodiment of the vane-cell pump is characterized in that the underfloor pressure region can be connected to the first consumer via a switching valve device. This embodiment is particularly advantageous when the vane pump is electrically driven and has a higher starting speed than pumps driven directly by an internal combustion engine.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass die Schaltventileinrichtung elektromagnetisch oder hydraulisch betätigbar ist. Über die elektromagnetische Betätigung der Schaltventileinrichtung kann der Unterflügeldruckbereich zum Beispiel immer dann mit dem Unterflügelsaugbereich oder mit dem ersten Verbraucher verbunden werden, wenn der Druck im Hydraulikspeicher oberhalb eines gewünschten Mindestdrucks liegt. Dabei wird der Druck in dem Hydraulikspeicher zum Beispiel mit Hilfe eines Drucksensors erfasst. Bei der hydraulischen Betätigung der Schaltventileinrichtung kann der Druck im Hydraulikspeicher direkt zur Sensierung genutzt werden.A further preferred embodiment of the vane pump is characterized in that the switching valve device is electromagnetically or hydraulically actuated. For example, via the electromagnetic actuation of the switching valve device, the underfoil pressure range can be connected to the lower-wing suction region or to the first consumer when the pressure in the hydraulic accumulator is above a desired minimum pressure. In this case, the pressure in the hydraulic accumulator is detected, for example, by means of a pressure sensor. In the hydraulic actuation of the switching valve device, the pressure in the hydraulic accumulator can be used directly for sensing.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass eine zusätzliche Ventileinrichtung zwischen den Unterflügelsaugbereich beziehungsweise den Druckbereich der Oberflügelpumpe und den diesem zugeordneten Verbraucher geschaltet ist. Die Ventileinrichtung kann als Schaltventil oder als Rückschlagventil ausgeführt sein. Die zusätzliche Ventileinrichtung dient vorzugsweise dazu, den Druckausgang der Oberflügelpumpe im Stillstand der Flügelzellenpumpe von dem ersten Verbraucher zu trennen.A further preferred exemplary embodiment of the vane-cell pump is characterized in that an additional valve device is connected between the lower-wing suction region or the pressure region of the upper-wing pump and the consumer associated therewith. The valve device can be designed as a switching valve or as a check valve. The additional valve device is preferably used to separate the pressure output of the wing pump at standstill of the vane pump from the first consumer.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass der Betriebsdruck in dem Unterflügeldruckbereich größer als in dem Unterflügelsaugbereich ist. Dadurch wird sichergestellt, dass die Flügel im Druckbereich und in einem Trennbereich der Oberflügelpumpe immer an der Hubkontur anliegen.A further preferred embodiment of the vane pump is characterized in that the operating pressure in the lower wing pressure range is greater than in the lower wing suction. This ensures that the wings always rest against the stroke contour in the pressure area and in a separation area of the wing pump.

Ein weiteres bevorzugtes Ausführungsbeispiel der Flügelzellenpumpe ist dadurch gekennzeichnet, dass ein hydraulischer Widerstand zwischen die Unterflügelbereiche beziehungsweise zwischen den Unterflügeldruckbereich und den ersten Verbraucher,geschaltet ist. Der hydraulische Widerstand ist zum Beispiel als hydraulische Engstelle oder als Drossel ausgeführt.A further preferred exemplary embodiment of the vane-cell pump is characterized in that a hydraulic resistance is connected between the lower-wing regions or between the lower-wing pressure region and the first consumer. The hydraulic resistance is designed, for example, as a hydraulic bottleneck or as a throttle.

Weitere Vorteile, Merkmale und Einzelheiten der Erfindung ergeben sich aus der nachfolgenden Beschreibung, in der unter Bezugnahme auf die Zeichnung verschiedene Ausführungsbeispiele im Einzelnen beschrieben sind. Es zeigen:

Figur 1
eine stark vereinfachte Darstellung einer erfindungsgemäßen Flügelzellenpumpe;
Figur 2
ein Ausführungsbeispiel der erfindungsgemäßen Flügelzellenpumpe, die zwei unterschiedliche Verbraucher mit unterschiedlichen Hydraulikmediumvolumenströmen versorgt, die unterschiedliche Drücke aufweisen;
Figur 3
eine Druckplatte der Flügelzellenpumpe aus Figur 2 in der Draufsicht;
Figur 4
die Druckplatte aus Figur 3 in der Untersicht;
Figur 5
ein ähnliches Ausführungsbeispiel wie in Figur 2 mit einer möglichen Verbindung zwischen verschiedenen Unterflügelbereichen;
Figur 6
ein ähnliches Ausführungsbeispiel wie in Figur 2 mit einer möglichen Verbindung zwischen einem der Unterflügelbereiche und einem diesem nicht zugeordneten Verbraucher;
Figur 7
eine Variante eines Schaltventils aus Figur 6;
Figur 8
ein ähnliches Ausführungsbeispiel wie in Figur 5 mit einem anderen Schaltventil;
Figur 9
eine ähnliche Darstellung wie in Figur 1 mit in die Flügelzellenpumpe integrierten Ventilen;
Figur 10
ein ähnliches Ausführungsbeispiel wie in Figur 6 mit einer zusätzlichen Schaltventileinrichtung und
Figur 11
ein ähnliches Ausführungsbeispiel wie in Figur 10 mit einem Rückschlagventil.
Further advantages, features and details of the invention will become apparent from the following description in which, with reference to the drawings, various embodiments are described in detail. Show it:
FIG. 1
a greatly simplified representation of a vane pump according to the invention;
FIG. 2
an embodiment of the vane pump according to the invention, which supplies two different consumers with different hydraulic medium flow rates having different pressures;
FIG. 3
a pressure plate of the vane pump FIG. 2 in the plan view;
FIG. 4
the pressure plate off FIG. 3 in the lower view;
FIG. 5
a similar embodiment as in FIG. 2 with a possible connection between different sub-wing areas;
FIG. 6
a similar embodiment as in FIG. 2 with a possible connection between one of the underflying areas and a consumer not assigned to it;
FIG. 7
a variant of a switching valve FIG. 6 ;
FIG. 8
a similar embodiment as in FIG. 5 with another switching valve;
FIG. 9
a similar representation as in FIG. 1 with valves integrated into the vane pump;
FIG. 10
a similar embodiment as in FIG. 6 with an additional switching valve device and
FIG. 11
a similar embodiment as in FIG. 10 with a check valve.

In Figur 1 ist eine Flügelzellenpumpe 1 stark vereinfacht schematisch dargestellt. Der Aufbau und die Funktion der Flügelzellenpumpe 1 sind zum Beispiel in der deutschen Offenlegungsschrift DE 196 31 846 A1 beschrieben.In FIG. 1 is a vane pump 1 very simplified schematically shown. The structure and function of the vane pump 1 are, for example, in the German Offenlegungsschrift DE 196 31 846 A1 described.

Um den hydraulischen Bedarf von zwei unterschiedlichen Volumenströmen auf unterschiedlichen Druckniveaus, beispielsweise in einer hydraulischen Getriebesteuerung, zeitgleich decken zu können, können schaltbare doppelhubige Flügelzellenpumpen eingesetzt werden. Hierbei werden die zwei Pumpenfluten, die sich aus der Doppelhubigkeit ergeben, getrennt voneinander aus der Pumpe gefördert und unterschiedlichen Verbrauchern zugeführt.In order to cover the hydraulic demand of two different volume flows at different pressure levels, for example in a hydraulic transmission control, at the same time, switchable double-stroke vane pumps can be used. Here, the two pump floods resulting from the Doppelhubigkeit, separately conveyed from the pump and fed to different consumers.

Es ist auch möglich, zwei oder mehr separate Pumpen zu verwenden, um unterschiedliche Verbraucher mit unterschiedlichen Volumenströmen und/oder Drücken zu versorgen. In der deutschen Offenlegungsschrift DE 195 14 929 A1 wird vorgeschlagen, zwei Pumpen durch einen einzigen Elektromotor anzutreiben.It is also possible to use two or more separate pumps to supply different consumers with different flow rates and / or pressures. In the German patent application DE 195 14 929 A1 It is proposed to drive two pumps by a single electric motor.

Durch die in Figur 1 stark vereinfacht dargestellte Flügelzellenpumpe 1 wird Hydraulikmedium aus einem Tank 2 einem Oberflügelpumpenbereich 4 und einem Unterflügelpumpenbereich 5 zugeführt. Die beiden Flügelpumpenbereiche 4, 5 stellen eine Flügelpumpe dar, die durch Flügel der Flügelzellenpumpe 1 betrieben wird. Die Förderwirkung der Unterflügelpumpe wird durch eine Hubbewegung der radial inneren Flügelenden erzielt.By the in FIG. 1 The vane pump 1, which is shown in a highly simplified manner, is supplied with hydraulic fluid from a tank 2 to a vane pump area 4 and an underwing pump area 5. The two vane pump areas 4, 5 represent a vane pump, which is operated by vanes of the vane pump 1. The conveying effect of the underfloor pump is achieved by a lifting movement of the radially inner wing ends.

Die Flügelzellenpumpe 1 umfasst die Oberflügelpumpe mit zwei im Wesentlichen sichelförmigen Förderräumen, die von den Flügeln durchlaufen werden und in radialer Richtung zwischen einem Rotor und einer Hubkontur angeordnet sind. Der Rotor und die Hubkontur werden in axialer Richtung auf einer Seite von einer Druckplatte begrenzt, die beispielsweise in einem Gehäuse der Flügelzellenpumpe 1 angeordnet ist.The vane pump 1 comprises the wing pump with two substantially crescent-shaped delivery spaces, which are traversed by the wings and are arranged in the radial direction between a rotor and a stroke contour. The rotor and the stroke contour are limited in the axial direction on one side by a pressure plate, which is arranged for example in a housing of the vane pump 1.

Der Oberflügelpumpenbereich 4 steht mit einem ersten Verbraucher 6 in Verbindung. Der Unterflügelpumpenbereich 5 steht mit einem zweiten Verbraucher 7 in Verbindung. Der zweite Verbraucher 7 umfasst einen Hydraulikspeicher 8. Die Flügelzellenpumpe 1 wird, vorzugsweise in einem Kraftfahrzeug, zur Versorgung eines Getriebes mit Hydraulikmedium eingesetzt, das durch die Flügelzellenpumpe 1 mit unterschiedlichen Drücken beaufschlagbar ist. Der Hydraulikspeicher 8 benötigt zum Beispiel einen Hydraulikdruck von circa 20 bar. Der Unterflügelpumpenbereich 5 hat ein Hubvolumen von circa einem Kubikzentimeter. Die Flügelzellenpumpe 1 ist vorzugsweise durch einen Elektromotor angetrieben.The upper wing pump region 4 is connected to a first consumer 6 in connection. The underwing pump area 5 communicates with a second consumer 7. The second consumer 7 comprises a hydraulic accumulator 8. The vane pump 1 is, preferably in a motor vehicle, used to supply a transmission with hydraulic medium, which can be acted upon by the vane pump 1 with different pressures. The hydraulic accumulator 8 requires, for example, a hydraulic pressure of about 20 bar. The underwing pump area 5 has a stroke volume of approximately one cubic centimeter. The vane pump 1 is preferably driven by an electric motor.

Bei dem ersten Verbraucher 6 handelt es sich zum Beispiel um eine Nasskupplung, die zur Kühlung einen Volumenstrom von bis zu 30 Litern pro Minute bei einem Druck von 3 bar benötigt. Durch die Ausnutzung der Oberflügelpumpe und der Unterflügelpumpe der Flügelzellenpumpe 1 kann ein Volumenstromverhältnis von 7 zu 1 und ein Druckverhältnis von 1 zu 6 bereitgestellt werden. Dabei können die beiden Flügelpumpenbereiche 4 und 5 gleichzeitig betrieben werden. Darüber hinaus ist es möglich, den Unterflügelpumpenbereich 5 abzuschalten, um bei tiefen Temperaturen den zum Antrieb benötigten Drehmomentbedarf so gering wie möglich zu halten. Gemäß einem wesentlichen Aspekt der Erfindung wird die Unterflügelpumpe der Flügelzellenpumpe 1 mit ihrem Unterflügelpumpenbereich 5 als eigenständige Pumpe genutzt, um den Hydraulikspeicher 8 aufzuladen.The first consumer 6 is, for example, a wet clutch which requires a volume flow of up to 30 liters per minute for cooling at a pressure of 3 bar. By utilizing the underfloor pump and the underfloor pump of the vane pump 1, a volumetric flow ratio of 7 to 1 and a pressure ratio of 1 to 6 can be provided. The two vane pump areas 4 and 5 can be operated simultaneously. Moreover, it is possible to switch off the underfloor pump area 5 in order to keep the torque requirement required for the drive as low as possible at low temperatures. According to an essential aspect of the invention, the underfloor pump the vane pump 1 is used with its underwing pump area 5 as an independent pump to charge the hydraulic accumulator 8.

In den Figuren 2 bis 8 und 10 bis 11 ist eine Flügelzellenpumpe 11 in verschiedenen Ausführungsbeispielen dargestellt. Gleiche oder ähnliche Teile sind mit gleichen Bezugszeichen versehen. Die Flügelzellenpumpe 11 ist an einen Tank 12 mit Hydraulikmedium, insbesondere Öl, angeschlossen. Zum besseren Verständnis der Erfindung ist von der Flügelzellenpumpe 11 hauptsächlich eine Druckplatte 13 dargestellt, die eine axiale Anlagefläche für den Rotor und/oder die Flügel der Flügelzellenpumpe 1 darstellt.In the FIGS. 2 to 8 and 10 to 11 a vane pump 11 is shown in various embodiments. The same or similar parts are provided with the same reference numerals. The vane pump 11 is connected to a tank 12 with hydraulic medium, in particular oil. For a better understanding of the invention of the vane pump 11 mainly a pressure plate 13 is shown, which represents an axial bearing surface for the rotor and / or the blades of the vane pump 1.

Die Druckplatte 13 umfasst zwei Saugbereiche 15, 16 und zwei Druckbereiche 17, 18 der O-berflügelpumpe. Die Druckplatte 13 umfasst des Weiteren eine der Unterflügelpumpe mit einem Unterflügelsaugbereich, der zwei Unterflügelnutabschnitte 21, 22 umfasst. Die beiden Unterflügelnutabschnitte 21, 22 sind radial innerhalb und in Umfangsrichtung überlappend zu den beiden Saugbereichen 15, 16 der Oberflügelpumpe angeordnet. Durch gestrichelte Linien sind Hydraulikleitungen oder Hydraulikkanäle angedeutet, über welche die beiden Unterflügelnutabschnitte 21, 22 mit jeweils einem der Druckbereiche 17, 18 der Oberflügelpumpe verbunden sind. Die Druckbereiche 17, 18 der Oberflügelpumpe wiederum stehen über Hydraulikleitungen oder Hydraulikkanäle 23, 24 mit einem ersten Verbraucher 26 in Verbindung.The pressure plate 13 comprises two suction regions 15, 16 and two pressure regions 17, 18 of the overflow pump. The pressure plate 13 further comprises one of the underfloor pump with a lower wing suction region, which comprises two Unterflügelnutabschnitte 21, 22. The two Unterflügelnutabschnitte 21, 22 are arranged radially inwardly and circumferentially overlapping the two suction regions 15, 16 of the wing pump. By dashed lines hydraulic lines or hydraulic channels are indicated, via which the two Unterflügelnutabschnitte 21, 22 are each connected to one of the pressure areas 17, 18 of the wing pump. The pressure areas 17, 18 of the wing pump in turn are connected via hydraulic lines or hydraulic channels 23, 24 with a first consumer 26 in connection.

Ein zweiter Verbraucher 27 umfasst einen Hydraulikspeicher 28 und steht über Hydraulikleitungen oder Hydraulikkanäle 29, 30 mit Unterflügelnutabschnitten 31, 32 eines Unterflügeldruckbereichs der Unterflügelpumpe in Verbindung. Die beiden Unterflügelnutabschnitte 31, 32 sind jeweils radial innerhalb und in Umfangsrichtung überlappend zu den Druckbereichen 18, 17 der Oberflügelpumpe angeordnet. Die Unterflügelnutabschnitte 21, 22 und 31, 32 haben im Wesentlichen die Gestalt von Kreisbögen, die auf einem gemeinsamen Kreis angeordnet sind.A second load 27 comprises a hydraulic accumulator 28 and is connected via hydraulic lines or hydraulic channels 29, 30 with Unterflügelnutabschnitten 31, 32 of an underfloor pressure range of the underfloor pump in connection. The two Unterflügelnutabschnitte 31, 32 are each disposed radially inwardly and circumferentially overlapping the pressure areas 18, 17 of the wing pump. The Unterflügelnutabschnitte 21, 22 and 31, 32 have substantially the shape of circular arcs, which are arranged on a common circle.

Die Unterflügelnutabschnitte 21, 22 des Unterflügelsaugbereichs werden zum Beispiel über gestrichelt angedeutete Kanäle oder Bohrungen in der Druckplatte 13 aus der Oberflügelpumpe mit Hydraulikmedium gefüllt. Im Betrieb der Flügelzellenpumpe 1 werden die Flügel durch den Druck in den beiden Unterflügelnutabschnitten 21, 22 in den Saugbereichen 15, 16 zwangsweise ausgefahren. In den Unterflügelnutabschnitten 31, 32 werden die Flügel konstruktionsbedingt durch das Zusammenwirken mit der Hubkontur eingefahren, so dass das Hydraulikmedium in den Unterflügelnutabschnitten 31, 32 durch die einfahrenden Flügel mit Druck beaufschlagt wird. Dieser relativ hohe Druck wird genutzt, um den Hydraulikspeicher 28 mit Hydraulikmedium zu füllen. Der durch die geringe Größe der Unterflügelnutabschnitte 31, 32 relativ kleine Volumenstrom reicht zu diesem Zweck aus. Der erste Verbraucher 26 wird über die Druckbereiche 17, 18 der Oberflügelpumpe mit einem deutlich größeren Volumenstrom versorgt, der allerdings mit einem deutlich geringeren Druck beaufschlagt ist.The Unterflügelnutabschnitte 21, 22 of the lower wing suction are filled, for example, indicated by dashed lines channels or holes in the pressure plate 13 from the wing pump with hydraulic medium. In operation of the vane pump 1, the wings are forcibly extended by the pressure in the two Unterflügelnutabschnitten 21, 22 in the suction regions 15, 16. In the Unterflügelnutabschnitten 31, 32, the wings are by design retracted by the interaction with the stroke contour, so that the hydraulic medium in the Unterflügelnutabschnitten 31, 32 is acted upon by the retracting wing with pressure. This relatively high pressure is used to fill the hydraulic accumulator 28 with hydraulic medium. The by the small size of the Unterflügelnutabschnitte 31, 32 relatively small volume flow is sufficient for this purpose. The first consumer 26 is supplied via the pressure regions 17, 18 of the wing pump with a significantly larger volume flow, which is, however, subjected to a significantly lower pressure.

In den Figuren 3 und 4 ist die Druckplatte 13 in der Draufsicht auf eine Seite und um 180 Grad umgeklappt in der Untersicht auf die andere Seite dargestellt. Die Trennstellen zwischen den Unterflügelnutabschnitten 21, 22 und 31, 32 liegen vorzugsweise in Winkelbereichen der Hubkontur, an denen keinen wesentliche Volumenänderung der Förderkammern der Flügelzellenpumpe 11 auftritt.In the FIGS. 3 and 4 the pressure plate 13 is shown in plan view on one side and folded 180 degrees in the bottom view on the other side. The separation points between the Unterflügelnutabschnitten 21, 22 and 31, 32 are preferably in angular ranges of the stroke contour, where no significant change in volume of the delivery chambers of the vane pump 11 occurs.

In Figur 4 sieht man, dass die beiden Unterflügelnutabschnitte 31, 32 innerhalb einer im Wesentlichen Acht-förmigen ersten Dichtung 35 angeordnet sind. Die beiden Unterflügelnutabschnitte 21, 22 und die sich durch die Druckplatte 13 hindurch erstreckenden Druckbereiche 17, 18 der Oberflügelpumpe sind außerhalb der Acht-förmigen ersten Dichtung 35 und innerhalb einer kreisförmigen zweiten Dichtung 36 angeordnet. Die beiden Dichtungen 35, 36 dienen zur Abdichtung gegenüber einem Gehäuse der Flügelzellenpumpe 11 oder einer Steuerplatte eines Getriebes.In FIG. 4 it can be seen that the two Unterflügelnutabschnitte 31, 32 are disposed within a substantially eight-shaped first seal 35. The two Unterflügelnutabschnitte 21, 22 and extending through the pressure plate 13 through pressure regions 17, 18 of the wing pump are arranged outside of the eight-shaped first seal 35 and within a circular second seal 36. The two seals 35, 36 serve to seal against a housing of the vane pump 11 or a control plate of a transmission.

Die Acht-förmige erste Dichtung 35 ist im dargestellten Ausführungsbeispiel so ausgeführt, dass die beiden Unterflügelnutabschnitte 31, 32 miteinander in Verbindung stehen. Durch entsprechende Änderung der ersten Dichtung 35 oder durch Verwendung von zwei kreisförmigen Dichtungen können die beiden Unterflügelnutabschnitte 31, 32 aber auch einzeln abgedichtet werden. Die in Figur 4 dargestellte Druckübergabe hat den Vorteil, dass eine unerwünschte Plattendurchbiegung durch die erhöhten Drücke in den Unterflügelnutabschnitten 31, 32 auf der Rotorseite der Druckplatte 13 durch die Druckbeaufschlagung mit dem erhöhten Druck auf der Dichtseite zum Gehäuse beziehungsweise zu einer Steuerplatte eines Getriebes kompensiert werden kann.The eight-shaped first seal 35 is designed in the illustrated embodiment so that the two Unterflügelnutabschnitte 31, 32 communicate with each other. By appropriate modification of the first seal 35 or by using two circular seals, the two Unterflügelnutabschnitte 31, 32 but also be sealed individually. In the FIG. 4 illustrated pressure transfer has the advantage that an undesirable plate deflection can be compensated by the increased pressures in the Unterflügelnutabschnitten 31, 32 on the rotor side of the pressure plate 13 by the pressurization with the increased pressure on the sealing side to the housing or to a control plate of a transmission.

Durch die erfindungsgemäße Gestaltung der druckbeaufschlagten Flächen sowie der Dicke der Druckplatte 13 kann eine zusätzliche Kompensation erzielt werden. Dabei sollten die Spalthöhen immer in einem umgekehrt proportional zum Druck entsprechenden Maß konzipiert werden. Dadurch kann die Schleppleistung minimiert werden. Durch die erfindungsgemäße Anordnung der beiden Dichtungen 35, 36 ist es möglich, die Flügelzellenpumpe 11 ohne Gehäuse als Einschubbauteil in eine Steuerungsplatte eines Getriebes zu integrieren.The inventive design of the pressurized surfaces and the thickness of the pressure plate 13, an additional compensation can be achieved. The gap heights should always be designed in a measure that is inversely proportional to the pressure. As a result, the towing capacity can be minimized. The inventive arrangement of the two seals 35, 36, it is possible to integrate the vane pump 11 without housing as a plug-in component in a control plate of a transmission.

Durch eine geeignete Wahl der Flügelgeometrie kann das Verhältnis der den beiden Verbrauchern 26, 27 zugeführten Volumenströme variiert werden. Das Pumpenvolumen der Unterflügelpumpe ergibt sich aus der Dicke der Flügel und der Länge des Flügelhubs. Durch eine Variation der Flügeldicke kann auf einfache Art und Weise das Hubvolumen der Unterflügelpumpe variiert werden. Bei einer vorgegebenen Geometrie der Oberflügelpumpe führt eine Verdopplung der Flügeldicke zu einer deutlichen Veränderung des Pumpenfördervolumens. Durch eine geeignete Wahl des Verhältnisses der Breite der Rotorgruppe zum Flügelhub kann die Eingangsleistung der Flügelzellenpumpe ebenfalls beeinflusst werden.By a suitable choice of the blade geometry, the ratio of the two consumers 26, 27 supplied volume flows can be varied. The pump volume of the underfloor pump results from the thickness of the wings and the length of the wing stroke. By varying the wing thickness, the stroke volume of the underfloor pump can be varied in a simple manner. With a given geometry of the wing pump doubling the wing thickness leads to a significant change in the pump delivery volume. By a suitable choice of the ratio of the width of the rotor group to the wing stroke, the input power of the vane pump can also be influenced.

Bei dem in Figur 5 dargestellten Ausführungsbeispiel ist zwischen den Hydraulikleitungen 29, 30 und dem zweiten Verbraucher 27 eine Verzweigung 40 vorgesehen. Zwischen der Verzweigung 40 und dem zweiten Verbraucher 27 ist ein Rückschlagventil 41 vorgesehen, das ein unerwünschtes Zurückströmen von Hydraulikmedium aus dem Hydraulikspeicher 28 verhindert, wenn die Flügelzellenpumpe 11 stillsteht. Durch das Rückschlagventil 41 wird des Weiteren ermöglicht, dass die Unterflügelpumpe, insbesondere der dem zweiten Verbraucher 27 zugeordnete Unterflügelpumpenbereich mit den Unterflügelnutabschnitten 31, 32, abgeschaltet werden kann. Das ist bei der erfindungsgemäßen Anwendung der Flügelzellenpumpe 11 besonders hilfreich, da die Aufladung des Hydraulikspeichers 28 vorzugsweise diskontinuierlich erfolgt.At the in FIG. 5 illustrated embodiment, a branch 40 is provided between the hydraulic lines 29, 30 and the second load 27. Between the branch 40 and the second consumer 27, a check valve 41 is provided which prevents unwanted backflow of hydraulic fluid from the hydraulic accumulator 28 when the vane pump 11 is stationary. By the check valve 41 is further made possible that the underfloor pump, in particular the second consumer 27 associated underfloor pump area with the Unterflügelnutabschnitten 31, 32, can be switched off. This is particularly useful in the application of the vane pump 11 according to the invention, since the charging of the hydraulic accumulator 28 is preferably carried out discontinuously.

Von der Verzweigung 40 geht eine Hydraulikleitung oder ein Hydraulikkanal 42 aus, der über weitere Hydraulikleitungen oder Hydraulikkanäle 43, 44 mit den beiden Unterflügelnutabschnitten 21, 22 des Unterflügelsaugbereichs verbunden ist. In der Hydraulikleitung 42 ist eine Schaltventileinrichtung 45 angeordnet, die als 2/2-Wegeventil mit einer Öffnungsstellung und einer Sperrstellung ausgeführt ist. Durch eine Feder ist die Schaltventileinrichtung 45 in die dargestellte Sperrstellung vorgespannt.From the branch 40 is a hydraulic line or a hydraulic channel 42 goes out, which is connected via further hydraulic lines or hydraulic channels 43, 44 with the two Unterflügelnutabschnitten 21, 22 of the lower wing suction. In the hydraulic line 42, a switching valve device 45 is arranged, which is designed as a 2/2-way valve with an open position and a blocking position. By a spring, the switching valve device 45 is biased in the illustrated blocking position.

In der Sperrstellung ist die Verbindung zwischen den Unterflügelnutabschnitten 31, 32 des zweiten Unterflügelpumpenbereichs und den Unterflügelnutabschnitten 21, 22 des Unterflügelsaugbereichs unterbrochen, so dass der Hydraulikspeicher 8 über die beiden Unterflügelnutabschnitte 31, 32 des Unterflügeldruckbereichs aufgeladen wird.In the locked position, communication between the under-wing groove portions 31, 32 of the second under-wing pump portion and the lower-wing groove portions 21, 22 of the lower-wing suction portion is interrupted, so that the hydraulic accumulator 8 is charged via the two under-wing groove portions 31, 32 of the under-wing pressure portion.

Durch Umschalten der Schaltventileinrichtung 45 in die Öffnungsstellung wird die Verbindung zwischen den Unterflügelnutabschnitten 31, 32 des Unterflügeldruckbereichs mit den Unterflügelnutabschnitten 21, 22 des Unterflügelsaugbereichs freigegeben. Dadurch kann die Antriebsleistung der Flügelzellenpumpe 1 reduziert werden, wenn kein Bedarf vorhanden ist, den Hydraulikspeicher 28 aufzuladen. Die Verbindung der beiden Unterflügelpumpenbereiche über das Schaltventil 45 liefert darüber hinaus den Vorteil, dass beim Starten der Flügelzellenpumpe 1 sofort Hydraulikmedium unter die Flügel in den Saugbereichen 15, 16 gefördert wird, um ein Ausfahren dieser Flügel zu erzwingen.By switching the switching valve means 45 to the open position, the communication between the under-wing groove portions 31, 32 of the under-wing pressure portion with the under-wing groove portions 21, 22 of the lower-wing suction portion is released. Thereby, the driving power of the vane pump 1 can be reduced when there is no need to charge the hydraulic accumulator 28. The connection of the two sub-vane pump areas via the switching valve 45 also provides the advantage that when starting the vane pump 1 immediately hydraulic medium under the wings in the suction areas 15, 16 is promoted to force an extension of these wings.

In Figur 6 ist ein Ausführungsbeispiel der Flügelzellenpumpe 11 dargestellt, bei dem die Verzweigung 40 über eine Hydraulikleitung 52 oder einen Hydraulikkanal und unter Zwischenschaltung einer Schaltventileinrichtung 55 direkt mit dem Druckausgang der Oberflügelpumpe beziehungsweise dem ersten Verbraucher 26 verbindbar ist. Diese Anordnung ist bei elektrisch angetriebenen Flügelzellenpumpen 11 vorteilhaft, die in der Regel eine höhere Startdrehzahl als Pumpen haben, die direkt von einem Verbrennungsmotor angetrieben werden.In FIG. 6 an embodiment of the vane pump 11 is shown, in which the branch 40 via a hydraulic line 52 or a hydraulic channel and with the interposition of a switching valve device 55 directly to the pressure output of the wing pump or the first load 26 is connectable. This arrangement is advantageous in electrically driven vane pumps 11, which typically have a higher starting speed than pumps driven directly by an internal combustion engine.

Gemäß einem weiteren Aspekt der Erfindung liegt der Betriebsdruck in den Unterflügelnutabschnitten 31, 32 des Unterflügeldruckbereichs immer oberhalb des Betriebsdrucks in den Unterflügelnutabschnitten 21, 22 des Unterflügelsaugbereichs. Dadurch kann sichergestellt werden, dass die Flügel in den Druckbereichen 17, 18 und den Trennbereichen im Betrieb immer an der Hubkontur anliegen. Um eine für den Pumpenbetrieb notwendige, ausreichende Differenz der Betriebsdrücke zu erreichen, ist in den Hydraulikleitungen 42; 52 der in den Figuren 5 und 6 dargestellten Ausführungsbeispiele jeweils gestrichelt eine Drossel 48; 58 angedeutet, die der jeweiligen Schaltventileinrichtung 45; 55 nachgeschaltet ist. Die Drossel 48; 58 kann auch in die jeweilige Schaltventileinrichtung 45; 55 integriert sein.According to another aspect of the invention, the operating pressure in the underfloor groove portions 31, 32 of the underfloor pressure region is always above the operating pressure in the underfloor groove portions 21, 22 of the lower wing suction region. This can ensure that the wings in the pressure areas 17, 18 and the separation areas in operation always rest against the stroke contour. In order to achieve a necessary difference in the operating pressures necessary for pump operation, in the hydraulic lines 42; 52 of the in the Figures 5 and 6 illustrated embodiments each dashed a throttle 48; 58 indicated that the respective switching valve device 45; 55 is connected downstream. The throttle 48; 58 can also in the respective switching valve device 45; 55 be integrated.

In Figur 7 ist durch ein Symbol 60 angedeutet, dass die Schaltventileinrichtung 55 aus Figur 6 elektrisch beziehungsweise elektromagnetisch betätigbar sein kann. Durch die elektrische beziehungsweise elektromagnetische Betätigung wird das Schaltventil 55 vorzugsweise immer dann aus seiner dargestellten Sperrstellung in seine nicht dargestellte Öffnungsstellung geschaltet, wenn der Druck im Hydraulikspeicher 28 oberhalb eines Mindestdrucks liegt. Zu diesem Zweck wird der Druck im Hydraulikspeicher 28 mit Hilfe eines Drucksensors erfasst.In FIG. 7 is indicated by a symbol 60 that the switching valve device 55 from FIG. 6 can be electrically or electromagnetically actuated. By the electrical respectively electromagnetic actuation, the switching valve 55 is preferably always switched from its illustrated blocking position to its open position, not shown, when the pressure in the hydraulic accumulator 28 is above a minimum pressure. For this purpose, the pressure in the hydraulic accumulator 28 is detected by means of a pressure sensor.

In Figur 8 ist angedeutet, dass das in Figur 5 gezeigt Schaltventil 45 auch hydraulisch betätigbar sein kann, wie durch eine Steuerdruckleitung 64 und ein Symbol 65 an der Schaltventileinrichtung 45 angedeutet ist. Das in Figur 6 dargestellte Schaltventil 55 kann, genauso wie das Schaltventil 45 in Figur 8, hydraulisch betätigt werden. Bei der in Figur 8 dargestellten hydraulischen Betätigung wird der Druck im Hydraulikspeicher 28 direkt zur Sensierung genutzt.In FIG. 8 is hinted that in FIG. 5 shown switching valve 45 may also be hydraulically actuated, as indicated by a control pressure line 64 and a symbol 65 on the switching valve device 45. This in FIG. 6 shown switching valve 55, as well as the switching valve 45 in FIG. 8 , hydraulically operated. At the in FIG. 8 shown hydraulic actuation of the pressure in the hydraulic accumulator 28 is used directly for sensing.

Bei einem unteren Schaltpunkt am Hydraulikspeicher 28 wird das Schaltventil 45 geschlossen und die Unterflügelpumpe fördert über die Unterflügelnutabschnitte 31, 32 des Unterflügeldruckbereichs über das Rückschlagventil 41 in den Hydraulikspeicher 28. Bei einem oberen Schaltpunkt wird das Schaltventil 45 geöffnet und die Unterflügelpumpe fördert mit den Unterflügelnutabschnitten 31, 32 Unterflügeldruckbereichs über die Unterflügelnutabschnitte 21, 22 des Unterflügelsaugbereichs und die Druckbereiche 17, 18 mit dem niedrigeren Betriebsdruck der Oberflügelpumpe.At a lower switching point on the hydraulic accumulator 28, the switching valve 45 is closed and the underfloor pump conveys via the Unterflügelnutabschnitte 31, 32 of the Unterflügeldruckbereichs via the check valve 41 in the hydraulic accumulator 28. At an upper switching point, the switching valve 45 is opened and the underfloor pump promotes the Unterflügelnutabschnitten 31st , 32 lower wing pressure range over the Unterflügelnutabschnitte 21, 22 of the lower wing suction and the pressure areas 17, 18 with the lower operating pressure of the wing pump.

In Figur 9 ist eine ähnliche Flügelzellenpumpe 71 wie in Figur 1 stark vereinfacht dargestellt. Da mit dem Unterflügelpumpenbereich 5 im Gegensatz zu dem Oberflügelpumpenbereich 4 nur relativ geringe Volumenströme zu dem zweiten Verbraucher 7 geliefert werden, können sowohl das Rückschlagventil 40 als auch die Schaltventileinrichtung 45 relativ klein ausgeführt und auf einfache Art und Weise in die Flügelzellenpumpe 71 integriert werden. Darüber hinaus kann die Drossel 48 in die Flügelzellenpumpe 71, insbesondere in das Schaltventil 45, integriert werden. Hierdurch ergibt sich eine kompakte Baueinheit, die nur noch mit drei Anschlüssen an den Tank 2 und die beiden Verbraucher 6 und 7 angeschlossen werden muss.In FIG. 9 is a similar vane pump 71 as in FIG. 1 shown greatly simplified. Since only relatively small volume flows are supplied to the second consumer 7 with the lower pad pump region 5, in contrast to the upper pad pump region 4, both the check valve 40 and the switching valve device 45 can be made relatively small and integrated into the vane pump 71 in a simple manner. In addition, the throttle 48 in the vane pump 71, in particular in the switching valve 45, are integrated. This results in a compact unit that only needs to be connected with three connections to the tank 2 and the two consumers 6 and 7.

In den Figuren 10 und 11 ist gezeigt, dass der Ausgang der Oberflügelpumpe durch eine Schaltventileinrichtung 74 beziehungsweise ein Rückschlagventil 80 von dem Verbraucher 26 getrennt werden kann. Dadurch kann ein unerwünschtes Rückströmen von Hydraulikmedium von dem Verbraucher 26 vermieden werden. Das in Figur 10 dargestellte Schaltventil 74 ist als 2/2-Wegeventil ausgeführt, das mit Hilfe einer Feder in seine dargestellte Sperrstellung vorgespannt ist. Im Betrieb der Flügelzellenpumpe 11 sorgt der über eine Steuerdruckleitung 75 auf das Schaltventil 74 wirkende Betriebsdruck der Oberflügelzellenpumpe dafür, dass das Schaltventil 74 öffnet und die Verbindung zwischen der Flügelzellenpumpe 11 und dem Verbraucher 26 freigibt. Die Federseite des Schaltventils 74 ist mit Umgebungsdruck verbunden, so dass an dem Schaltventil 74 keine Drosselverluste zum Offenhalten des Schaltventils 74 entstehen.In the Figures 10 and 11 It is shown that the output of the wing pump can be separated by a switching valve device 74 and a check valve 80 from the consumer 26. As a result, an undesired backflow of hydraulic medium from the consumer 26 can be avoided. This in FIG. 10 illustrated switching valve 74 is designed as a 2/2-way valve, which by means of a spring in its illustrated blocking position is biased. During operation of the vane pump 11, the operating pressure of the vane cell pump acting on the switching valve 74 via a control pressure line 75 ensures that the switching valve 74 opens and releases the connection between the vane pump 11 and the consumer 26. The spring side of the switching valve 74 is connected to ambient pressure, so that at the switching valve 74 no throttle losses for keeping the switching valve 74 open.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

11
FlügelzellenpumpeVane pump
22
Tanktank
44
OberflügelpumpenbereichUpper wing pump area
55
UnterflügelpumpenbereichUnderwing pump area
66
erster Verbraucherfirst consumer
77
zweiter Verbrauchersecond consumer
88th
Hydraulikspeicherhydraulic accumulator
1111
FlügelzellenpumpeVane pump
1212
Tanktank
1313
Druckplatteprinting plate
1515
Saugbereichsuction area
1616
Saugbereichsuction area
1717
Druckbereichpressure range
1818
Druckbereichpressure range
2121
UnterflügelnutabschnittUnterflügelnutabschnitt
2222
UnterflügelnutabschnittUnterflügelnutabschnitt
2323
Hydraulikleitunghydraulic line
2424
Hydraulikleitunghydraulic line
2626
erster Verbraucherfirst consumer
2727
zweiter Verbrauchersecond consumer
2828
Hydraulikspeicherhydraulic accumulator
2929
Hydraulikleitunghydraulic line
3030
Hydraulikleitunghydraulic line
3131
UnterflügelnutabschnittUnterflügelnutabschnitt
3232
UnterflügelnutabschnittUnterflügelnutabschnitt
3535
erste Dichtungfirst seal
3636
zweite Dichtungsecond seal
4040
Verzweigungbranch
4141
Rückschlagventilcheck valve
4242
Hydraulikleitunghydraulic line
4343
Hydraulikleitunghydraulic line
4444
Hydraulikleitunghydraulic line
4545
SchaltventileinrichtungValving means
4848
Drosselthrottle
5252
Hydraulikleitunghydraulic line
5555
SchaltventileinrichtungValving means
5858
Drosselthrottle
6060
Symbolsymbol
6464
Steuerleitungcontrol line
6565
Symbolsymbol
7171
FlügelzellenpumpeVane pump
7474
zusätzliche Schaltventileinrichtungadditional switching valve device
7575
Steuerleitungcontrol line
8080
Rückschlagventilcheck valve

Claims (16)

  1. Vane pump with an upper vane pump assigned to a first consumer (6; 26) and a lower vane pump comprising a lower vane pressure area and a lower vane suction area which is connected to the upper vane pump, characterised in that the lower vane pressure area is separated from the lower vane suction area and is assigned to a second consumer (7; 27).
  2. Vane pump according to claim 1, characterised in that the sub-divided lower vane areas can be subjected to different pressures.
  3. Vane pump according to one of the preceding claims, characterised in that the lower vane suction area comprises at least one lower vane groove section (21, 22) which is assigned via a pressure area (17, 18) of the upper vane pump to the first consumer (6; 26).
  4. Vane pump according to claim 3, characterised in that the lower vane groove section (21, 22) of the lower vane suction area is arranged radially within and overlapping in the circumferential direction with respect to a suction area (15, 16) of the upper vane pump.
  5. Vane pump according to claim 3 or 4, characterised in that the lower vane pressure area comprises at least one lower vane groove section (31, 32) which is assigned to the second consumer (7; 27).
  6. Vane pump according to claim 5, characterised in that the lower vane groove section (31, 32) of the lower vane pressure area is arranged radially within and overlapping in the circumferential direction with respect to the pressure area (17, 18) of the upper vane pump.
  7. Vane pump according to claim 5 or 6, characterised in that the lower vane suction area and the lower vane pressure area each have two diametrically arranged lower vane groove sections (21, 22; 31, 32).
  8. Vane pump according to one of the preceding claims, characterised in that the lower vane suction area and the lower vane pressure area are separated from each other by a seal (35).
  9. Vane pump according to claim 8, characterised in that the seal (35) has in the top view essentially the form of a figure eight, outside of which the lower vane suction area and within which the lower vane pressure area are arranged.
  10. Vane pump according to one of the preceding claims, characterised in that a non-return valve (41) is arranged between the second consumer (7; 27) and the lower vane pressure area assigned thereto.
  11. Vane pump according to one of the preceding claims, characterised in that the lower vane pressure area can be connected via a switching valve means (45) to the lower vane suction area.
  12. Vane pump according to one of the claims 1 to 10, characterised in that the lower vane pressure area can be connected via a switching valve means (55) to the first consumer (6; 26).
  13. Vane pump according to claim 11 or 12, characterised in that the switching valve means (45; 55) can be electro-magnetically or hydraulically activated.
  14. Vane pump according to one of the preceding claims, characterised in that an additional valve means (74) is provided between the lower vane suction area or the pressure area (17, 18) of the upper vane pump and the consumer (6; 26) assigned thereto.
  15. Vane pump according to one of the preceding claims, characterised in that the operating pressure in the lower vane pressure area is greater than in the lower vane suction area.
  16. Vane pump according to one of the preceding claims, characterised in that a hydraulic resistor (48; 58) is provided between the lower vane areas or between the lower vane pressure area and the first consumer (6; 26).
EP10752530.5A 2009-10-07 2010-09-09 Vane pump Active EP2486280B8 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009049532 2009-10-07
PCT/EP2010/005540 WO2011042105A2 (en) 2009-10-07 2010-09-09 Vane pump

Publications (3)

Publication Number Publication Date
EP2486280A2 EP2486280A2 (en) 2012-08-15
EP2486280B1 true EP2486280B1 (en) 2014-05-21
EP2486280B8 EP2486280B8 (en) 2014-07-09

Family

ID=43857203

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10752530.5A Active EP2486280B8 (en) 2009-10-07 2010-09-09 Vane pump

Country Status (8)

Country Link
US (1) US9217431B2 (en)
EP (1) EP2486280B8 (en)
JP (1) JP5671046B2 (en)
KR (1) KR20120089664A (en)
CN (1) CN103003572B (en)
DE (1) DE112010003973A5 (en)
ES (1) ES2484373T3 (en)
WO (1) WO2011042105A2 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105579706B (en) * 2013-09-24 2018-02-09 爱信精机株式会社 Oil pump
JP6123606B2 (en) * 2013-09-24 2017-05-10 アイシン精機株式会社 Oil pump
DE102017223530A1 (en) 2017-12-21 2019-06-27 Zf Friedrichshafen Ag Vane pump
DE102018200225B3 (en) * 2018-01-09 2019-03-07 Magna Powertrain Bad Homburg GmbH Pump assembly for a vehicle, and control for a pump assembly and method
DE102018126550B4 (en) * 2018-10-24 2024-02-29 Valeo Powertrain Gmbh Hydraulic transmission actuator
DE102020105173A1 (en) * 2020-02-27 2021-09-02 Fte Automotive Gmbh Pump unit for a drive train of a motor vehicle
DE102020105172A1 (en) * 2020-02-27 2021-09-02 Fte Automotive Gmbh Rotary vane pump
DE102020127070A1 (en) * 2020-10-14 2022-04-14 Fte Automotive Gmbh Pump unit for clutch actuation

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2993445A (en) 1955-07-23 1961-07-25 Teves Kg Alfred Pump, in particular for control systems
US3953153A (en) * 1974-05-17 1976-04-27 Sundstrand Corporation Multiple displacement pump system and method
JPS56110590A (en) * 1980-02-04 1981-09-01 Nippon Denso Co Ltd Rotary compressor
US4633767A (en) 1985-08-02 1987-01-06 Trailer Marine Transport Corporation Modular ventilation system for vehicles
JPH01134790U (en) * 1988-03-04 1989-09-14
DE3913414A1 (en) * 1989-04-24 1990-10-25 Walter Schopf Variable-delivery rotary-vane pump - has compression zone in sections supplying separate hydraulic circuits
JPH03118286A (en) 1989-09-29 1991-05-20 Suzuki Motor Corp Article storage device of motorcycle
JPH03118286U (en) * 1990-03-20 1991-12-06
DE19514929A1 (en) 1994-05-09 1995-11-16 Luk Fahrzeug Hydraulik Vehicle equipment with a drive motor and at least two ancillary units
DE19631846A1 (en) 1995-08-14 1997-02-20 Luk Fahrzeug Hydraulik Centrifugal flywheel pump with two section
US5692761A (en) 1996-07-15 1997-12-02 Republic Tool & Mfg. Corp. Utility cart
US6352415B1 (en) * 1999-08-27 2002-03-05 Bosch Braking Systems Co., Ltd. variable capacity hydraulic pump
JP3942806B2 (en) * 1999-08-27 2007-07-11 ユニシア ジェーケーシー ステアリングシステム株式会社 Variable displacement pump
DE10020162C2 (en) * 2000-04-25 2002-04-25 Hennecke Gmbh Method and device for producing a flowable reaction mixture that forms a solid or foam
AU2002363838A1 (en) * 2001-12-27 2003-07-15 Luk Fahrzeug-Hydraulik Gmbh And Co. Kg Pump
DE102005014654B4 (en) * 2005-03-31 2014-03-06 Gkn Driveline International Gmbh Motor vehicle hydraulic pump
GB0520153D0 (en) 2005-10-04 2005-11-09 Ellis Brian An inflatable structure and mobile power supply unit

Also Published As

Publication number Publication date
CN103003572A (en) 2013-03-27
ES2484373T3 (en) 2014-08-11
DE112010003973A5 (en) 2013-01-10
WO2011042105A2 (en) 2011-04-14
JP2013510975A (en) 2013-03-28
EP2486280A2 (en) 2012-08-15
KR20120089664A (en) 2012-08-13
EP2486280B8 (en) 2014-07-09
US9217431B2 (en) 2015-12-22
CN103003572B (en) 2016-06-29
WO2011042105A3 (en) 2013-03-21
US20120275945A1 (en) 2012-11-01
JP5671046B2 (en) 2015-02-18

Similar Documents

Publication Publication Date Title
EP2486280B1 (en) Vane pump
EP2952365B1 (en) Rotary feed-through for a motor vehicle wheel
EP2796674B1 (en) Central valve for a pivotable motor adjuster
EP2337928B1 (en) Pump, particularly vane-type pump
DE3142604A1 (en) OIL PUMP UNIT
DE102014109097A1 (en) hydraulic valve
DE102013104051A1 (en) Central valve for a Schwenkmotorversteller
WO2015062752A1 (en) Coolant pump with a hydraulically adjustable valve slide, with an integrated secondary pump and an electromagnetic valve for generating and controlling the regulating pressure
EP1461533B1 (en) Pump
WO2008135420A1 (en) Camshaft adjuster for an internal combustion engine with improved design of the pressure chambers
EP1903238B1 (en) Hydraulic system
DE102012001462A1 (en) Internal gear pump comprises control bevel, which is provided in area of sealing segment side facing hollow wheel, and is extended out in peripheral direction of hollow wheel and broadens opening area of control groove
DE102012214107A1 (en) Pressure control device for hydraulic conductor of hydraulic system for operating clutch in motor vehicle, has sleeve part concentrically surrounding diaphragm body, where sleeve part and diaphragm body are made of steel material
DE102013104031A1 (en) Central valve for a Schwenkmotorversteller
DE102012001369A1 (en) Adjustable hydraulic pump
DE102012202904A1 (en) Pump assembly for producing variable volumetric flow in pressure system of automatic transmission used in motor car, has control unit through which position of control slide is actively changed based on control signal
EP3530892B1 (en) Hydraulic valve for a pivoting engine adjuster of a camshaft
DE102019101115A1 (en) Hydraulic valve for a Schwenkmotorversteller a camshaft
DE102009038377A1 (en) Hydraulic arrangement for controlling clutches of adjustable torque distributor device in motor vehicle, has common supply connected with high pressure circuit behind branch to low pressure circuit by valve closed against pumping direction
DE102014209865B4 (en) Camshaft adjuster with additional switchable short-circuit device
DE102012016683A1 (en) Lubricant pump device for motor vehicle, has electrically and/or electronically controlled actuator for controlling lubricant pressure to form additional force on pilot valve, where lubricant pressure is generated by pump unit
EP2292480B1 (en) Retarder system for a motor vehicle
DE102012213985A1 (en) pump means
DE2952101A1 (en) Rotary pump for vehicle engine - has outer cam track-operated radial pistons and valve in inlet line shut=off for zero output
EP3530891B1 (en) Hydraulic valve for a pivoting engine adjuster of a camshaft

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20120330

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

RIN1 Information on inventor provided before grant (corrected)

Inventor name: SCHULZ-ANDRES, HEIKO

Inventor name: BOEHM, CHRISTIAN

DAX Request for extension of the european patent (deleted)
R17D Deferred search report published (corrected)

Effective date: 20130321

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

INTG Intention to grant announced

Effective date: 20131210

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

RAP2 Party data changed (patent owner data changed or rights of a patent transferred)

Owner name: MAGNA POWERTRAIN BAD HOMBURG GMBH

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 669743

Country of ref document: AT

Kind code of ref document: T

Effective date: 20140615

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

Free format text: LANGUAGE OF EP DOCUMENT: GERMAN

REG Reference to a national code

Ref country code: DE

Ref legal event code: R096

Ref document number: 502010007041

Country of ref document: DE

Effective date: 20140710

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2484373

Country of ref document: ES

Kind code of ref document: T3

Effective date: 20140811

REG Reference to a national code

Ref country code: AT

Ref legal event code: HC

Ref document number: 669743

Country of ref document: AT

Kind code of ref document: T

Owner name: MAGNA POWERTRAIN BAD HOMBURG GMBH, DE

Effective date: 20140701

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20140521

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: LT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140822

Ref country code: IS

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140921

Ref country code: NO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140821

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: LV

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: PL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: HR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140922

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502010007041

Country of ref document: DE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20150224

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140909

Ref country code: MC

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 502010007041

Country of ref document: DE

Effective date: 20150224

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140930

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140909

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SM

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO

Effective date: 20100909

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20160920

Year of fee payment: 7

REG Reference to a national code

Ref country code: AT

Ref legal event code: MM01

Ref document number: 669743

Country of ref document: AT

Kind code of ref document: T

Effective date: 20150909

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20160921

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20160916

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20150909

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20160922

Year of fee payment: 7

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20170909

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20180531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170909

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170909

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20171002

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20181019

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20140521

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170910

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502010007041

Country of ref document: DE

Representative=s name: HOFFMANN - EITLE PATENT- UND RECHTSANWAELTE PA, DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 502010007041

Country of ref document: DE

Representative=s name: HOFFMANN - EITLE PATENT- UND RECHTSANWAELTE PA, DE

Ref country code: DE

Ref legal event code: R081

Ref document number: 502010007041

Country of ref document: DE

Owner name: HANON SYSTEMS EFP DEUTSCHLAND GMBH, DE

Free format text: FORMER OWNER: MAGNA POWERTRAIN BAD HOMBURG GMBH, 61352 BAD HOMBURG, DE

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230613

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20230920

Year of fee payment: 14