EP2151542A2 - Rotating piston pump with pockets for lubricant - Google Patents
Rotating piston pump with pockets for lubricant Download PDFInfo
- Publication number
- EP2151542A2 EP2151542A2 EP09166834A EP09166834A EP2151542A2 EP 2151542 A2 EP2151542 A2 EP 2151542A2 EP 09166834 A EP09166834 A EP 09166834A EP 09166834 A EP09166834 A EP 09166834A EP 2151542 A2 EP2151542 A2 EP 2151542A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- sliding surface
- piston pump
- pockets
- 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.)
- Granted
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/344—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F04C18/3441—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the inner and outer member being in contact along one line or continuous surface substantially parallel to the axis of rotation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/02—Lubrication; Lubricant separation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
- F04C2240/54—Hydrostatic or hydrodynamic bearing assemblies specially adapted for rotary positive displacement pumps or compressors
Definitions
- the invention relates to rotary piston pumps and is directed in particular to vacuum pumps.
- the drive of the pump which is permanent during operation of the internal combustion engine, must continue to pay attention to a reduction in the drive power required for the pump against the background of the CO 2 problem and the constant compulsion to reduce fuel consumption.
- a starting point for improving the efficiency is the reduction of the friction power at the end face of the pump rotor.
- Lubricant is supplied to the two bearing gaps on the end faces of a rotor of a vacuum pump.
- the rotor is rotatable about an axis of rotation between two side plates facing its end faces.
- the side plates are axially movable and are acted upon in the direction of the respective facing end face of the rotor with a pneumatic pressure to seal the delivery chamber of the pump.
- the rotor has at both end faces in each case a peripheral Gleitdicht Structure surrounding the rotation axis. Radially within this annular sliding surface, the end face of the rotor is axially withdrawn a bit.
- the two peripheral sliding surfaces provide in cooperation with the axially movable side plates for the tightness of the delivery chamber, while the recessed, central region through the respective side plate through lubricant is supplied.
- the side plates are for this purpose of open porosity and saturated with the lubricant.
- the friction between the side plates and the peripheral sliding surfaces of the rotor should still be considerable due to mixed friction.
- the execution of the side plates with the porosity required for the lubrication with sufficient stability and wear resistance will also not be unproblematic.
- the DE 33 25 261 A1 known vacuum pump is used as a sealing and lubricating oil centrally supplied to one end face of the rotor and guided via two radially branching off from the central feed throttle channels in a reclaimed at the end face of the rotor annulus.
- the two narrow throttle passages each extend radially beyond an inner sliding sealing surface of the rotor to open into the recessed annular space which extends in the face of the rotor about an inner sliding surface and is circumferentially enclosed by a peripheral sliding surface sealing the housing cover.
- the friction in the sliding bearing clearance between the sliding surface of the housing cover and the two sliding surfaces of the rotor, the inner sliding surface and the peripheral sliding surface should be considerable.
- the JP 2000-337267 A discloses a lubrication of the frontal bearing gaps for a hydraulic pump.
- the working fluid also serves as a lubricant.
- An improvement in the lubricating effect is achieved in that formed in the front side of the conveying chamber bounding chamber walls, between the formed in these chamber walls inlet and outlet openings for the working and lubricating medium each have many small, circular depressions and about the axis of rotation of the rotor on a Circle are evenly distributed.
- the depressions act as lubrication pockets, but you will not learn more about the mode of action and the shape of the wells.
- the JP 10-068393 A teaches to improve the lubrication of a vacuum pump, to form in a forming with the chamber wall, the sliding bearing gap sliding surface of the rotor a plurality of pockets which are seen in the plan view of the end face of the rotor are each completely within the sliding surface, thus beerbstandet in the circumferential direction of each other and both radially be limited inwardly and outwardly from the sliding surface.
- the pockets each have the shape of a slender, curved around the axis of rotation part ring.
- this solution also requires a thick lubricant film, associated with corresponding leakage losses and with regard to the efficiency of the pump.
- the subject of the invention is a rotary piston pump comprising a housing with a delivery chamber and at least one rotor rotatable about a rotation axis in the delivery chamber.
- the rotor has on its two end faces sliding surfaces which each form a sliding pair with axially facing sliding surfaces of the chamber.
- the end-side chamber walls which form said sliding surfaces of the chamber are preferably not movable, but stationary in the housing.
- at least one of the sliding surfaces i. in at least one of the front-side sliding surfaces of the rotor or in at least one of the front-side sliding surfaces of the chamber, at least one pocket for lubricant is formed.
- the pocket is bounded circumferentially with respect to the axis of rotation and radially outward by the sliding surface containing the pocket.
- the pocket is shaped so that, when the rotor is rotating, a hydrodynamic lubricating film builds up in the gap of the bearing bearing the pocket.
- the hydrodynamic lubricant film is viable and the rotor begins to slide on the lubricant.
- the rotor slides in the fully supporting area, and there is only liquid friction. In this way, the sliding surfaces of the sliding pair are separated and solid friction avoided, while the axial thickness of the axially limited by the sliding surfaces gap can still be kept low.
- the pocket is shaped so that the hydrodynamic lubricant film builds up at the speeds typical for the operation of the rotary piston pump, in which the rotary piston pump is predominantly operated.
- the bag has for this purpose a sufficient volume and a suitable shape, in particular, it has a care for the lubricating film construction depth profile.
- the pocket is preferably shaped such that the hydrodynamic lubricating film sets in the sliding gap immediately after the trailing end of the pocket in the direction of rotation of the rotor.
- the same or the axially opposite sliding surface can or may contain one or more further pocket (s) that do not meet this condition, as long as in the gap of the sliding surfaces as a whole from the transition speed prevails the hydrodynamic lubrication state. If, as preferred, several pockets according to the invention are provided, it is sufficient if these pockets bring about the construction of the hydrodynamic shear film only in combination.
- the pocket flattens in the circumferential direction, in the direction of its trailing end, thus tapering, preferably over its entire radially measured width. If the taper extends only over part of the radial pocket width, this tapered width region is preferably arranged radially in the middle region of the sliding surface.
- the pocket forms a wedge in the gap of the sliding surfaces at the trailing end.
- the pocket may have a variable inclination in the course of the rise to the sliding surface containing it, in particular an inclination which decreases towards the trailing end, so that the bottom of the pocket in the region of the wedge towards the opposite Sliding surface of the sliding couple bulges around.
- the inclination is constant over at least one larger, preferably the predominant part of the wedge.
- the pocket bottom may include in the rise one or more curved section (s) in combination with one or more straight section (s). It may also have one or more stages in the wedge-shaped gap, but a continuous course is preferred. It can with respect to the axially opposite sliding surface from the outlet in the sliding surface in the circumferential direction may even have one or more concave sections, as long as the hydrodynamic lubricant film is still built up.
- the wedge preferably extends over at least a quarter, more preferably over at least half of the pocket depth, the reference depth being the maximum depth of the pocket.
- the bag may be perpendicular to the bottom of the bag, i. in the axial direction, or increase with increasing inclination and only from half the pocket depth or already before tapering gradually.
- the taper can already be used immediately in the pocket bottom, i. From the pocket bottom flatten out directly with an inclination to the sliding surface containing them.
- the inclination to the sliding surface should be at most in the trailing end region of the wedge at most 45 °, more preferably at most 30 °, both in the case of a constant and in the case of a variable inclination.
- the mentioned angle values should not be exceeded.
- Lower angles of inclination are advantageous in view of the shear forces acting on the structure of the hydrodynamic lubricant film in the lubricant, in particular in the outlet of the wedge.
- an inclination directly at the end of the wedge of at most 15 ° is particularly preferred, it also corresponds to preferred embodiments, when the inclination decreases continuously, at least at the end of the wedge, the wedge can expire in particular tangentially into the sliding surface.
- the wedge length measured in the circumferential direction it is advantageous if the wedge extends over at least half the pocket length, wherein the advantage of this geometry feature increases with decreasing pocket length.
- the bag expires at its trailing end in the sliding surface flat, with less inclination than at its leading end.
- At the leading end of the bag can steeply, in particular vertically, rise to the sliding surface, with a chamfer at the transition to the sliding surface as belonging to the steep wall, since chamfers serve only the deburring, but do not cause hydrodynamic film structure.
- the invention also relates to embodiments in which the bag also terminates wedge-shaped at the leading end. The geometric asymmetry with a pronounced wedge at the trailing end to produce the hydrodynamic lubricating film and at the leading end steep or at least significantly steeper to the Sliding surface rising pocket is preferred, however, as this minimizes the area ratio of the pocket relative to the sliding surface.
- a connection can additionally be provided between the pocket and the radially outer edge of the sliding surface or pocket and a circumferential surface radially adjoining the sliding surface, either in the form of a connecting channel lying below the sliding surface or open on the sliding surface.
- such an optional connection channel is designed so that it provides the flow of lubricant from the bag considerable resistance to flow, which is several times greater than in the case of a pocket which passes through the sliding surface radially with its full pocket cross-section.
- a radial boundary of the pocket by the sliding surface is thus also seen when a narrow in the circumferential direction or in the depth direction of the pocket flat connecting channel has a flow cross-section which is smaller by a multiple than a largest pocket cross-section.
- An optional connection channel can be used to selectively use lubricant on the bag radially outward into the chamber and there for lubrication, for example, the tip of a wing of a vane pump.
- the optional connecting channel is dimensioned such that, in spite of the drainage of lubricant facilitated by it, the hydrodynamic lubricating film forms.
- the trailing end of the pocket can, seen in plan view of the sliding surface, run straight over its entire radial width and run at least essentially radially, ie pass over the pocket into the sliding surface via a radial edge line.
- the pocket may also be undercut in plan view of the sliding surface, so that it has a circumferentially extending extension at the trailing end which is bounded radially inwards, in the direction of the axis of rotation of the rotor, by the sliding surface.
- the undercut counteracts a flow of the lubricant radially inwardly, in particular in preferred embodiments, in which the pocket radially inward, ie in the direction of the axis of rotation, on an inner peripheral surface opens, so that the sliding surface passes radially in the direction of the axis of rotation.
- the sliding surface is in such embodiments extends annularly around the axis of rotation. A radially inwardly passing through the sliding surface has the advantage that such a pocket can be supplied with lubricant from the central region within the annular sliding surface.
- further pockets in the manner according to the invention are formed in the sliding surface containing the pocket.
- the pockets are circumferentially spaced from each other about the axis of rotation, preferably a portion of the sliding surface remains between them, and are bounded radially outward by the sliding surface containing them.
- the pockets are advantageously arranged distributed around the axis of rotation at least substantially uniformly.
- the angular distances of respectively adjacent pockets are substantially the same in such embodiments.
- a rotary vane pump with a single vane, which passes radially through the rotor is regarded as a uniform angle division, an arrangement in which the pockets are distributed symmetrically with respect to the wing.
- the pockets are seen in plan view of the sliding surface and in cross section preferably equal to each other, but may in principle also differ from each other. You can also deviate from each other in the depth profile, but more preferably they are equal to each other in the depth profile.
- the depth profile is the course of the axial depth in the circumferential direction on a cylindrical surface which cuts the pocket about the axis of rotation.
- this pocket may in particular be arranged so that it counteracts a light tilting position of the rotor axis which is present in some applications in pump operation.
- the pocket is arranged in one of the end-side sliding surfaces of the chamber, ie stationary with respect to the chamber. The tilting position of the rotor, if present during operation, is known in advance, so that the bag can be arranged accordingly.
- pockets of the type according to the invention are formed in the respective sliding surface of the chamber in the circumferential direction, these pockets are arranged so as to at least partially compensate the tilting position, for example by providing the pockets in the circumferential direction only in half of the sliding surface, in the the gap between the sliding surfaces is smaller due to the tilted position than in the other hemisphere.
- pockets can also be distributed over the entire circumference, with the ratio of pocket area to remaining sliding area being greater than in the other hemisphere of the relevant sliding area in order to compensate for a tilted position in the corresponding hemisphere.
- the pocket or preferably a plurality of pockets may or may not be formed in one of the sliding surfaces of the rotor or one of the chamber sides of the rotor facing side.
- the word "or” is always understood in the usual logical sense as an “inclusive or”, ie includes both the meaning of "either ... or” as well as the meaning of "and”, as far as the specific context is not exclusively only one limited meaning.
- a single or multiple pockets may or may therefore be provided, for example, only in one or only in both frontal sliding surfaces of the rotor, these two embodiments are particularly preferred, or only in one of the two sliding pairings co-forming sliding surfaces of the chamber or only in both frontal sliding surfaces the chamber.
- a single pocket or pockets may also be formed in one or both of the sliding surface (s) of the rotor and additionally in one or both facing sliding surfaces of the chamber, including, for example, the case where a single pocket or a plurality of pockets only on one of the two end faces of the rotor and a single or more pockets is formed only in that sliding surface of the chamber or are, which forms a sliding pair on the opposite end face of the rotor with the local Rotorgleit
- the invention also includes the case that the rotor on one or both ends has a single or more pockets and the chamber is also provided on the same face also with a single or more pockets of the type according to the invention, which associated with the same sliding pair Bags of the rotor and the chamber are radially offset from each other so that they do not overlap during rotation of the rotor.
- vane pumps having a single or multiple vanes (s) slidably guided by the rotor, and also swing vane pumps.
- single-wing designs are preferred, ie Versions in which the rotor with the wing divides the delivery chamber into only two cells.
- the rotary piston pump can be designed with a variable or constant delivery volume. It can be multi-stroke, but is preferably one-stroke.
- a plurality of rotors, for example two rotors, may be arranged in the delivery chamber, with a pair of bearings preferably being formed in accordance with the invention in each case on both rotors at at least one axial end side.
- the bag is advantageously formed in shaping on the rotor in a peripheral region of the sliding surface, which is not penetrated by a wing, a sliding or swing wing.
- the sliding surface with the at least one pocket according to the invention is not interrupted in the circumferential direction, but extends completely circumferentially around the axis of rotation, this consideration plays no role.
- the plurality of pockets are advantageously arranged in the rotor around the axis of rotation in such a number that at least one of the pockets is arranged in the angular region of each cell of the cell pump.
- per cell which forms the rotor with its one-piece or divided wing, preferably at least two of the pockets according to the invention are arranged.
- the rotary piston pump preferably requires a gaseous working fluid while the lubricant is preferably liquid.
- the invention is directed to a vacuum pump which is installed in a motor vehicle or intended for installation in a motor vehicle.
- the pump can generate the vacuum required for a brake booster. It is preferably powered by the engine, which is preferably an internal combustion engine.
- the engine which is preferably an internal combustion engine.
- the rotor on the circumference of a rotor bearing portion provided with a floating sliding bearing and thus axially fixed, but is movable either within the axial tolerance or a deliberately provided axial play between the end faces of the delivery chamber.
- the pressure of the crankcase of the engine which generally corresponds approximately to the atmospheric pressure, while at the opposite, opposite projection surface of the rotor in the a relatively high negative pressure acts on a large number of operating states of the pump, so that the rotor is pressed against the relevant sliding surface of the chamber. It arises according to the pressure gradient, a considerable axial thrust, which leads to a large friction in the case of planning in the prior art frontal geometry of the rotor, countermeasures are not taken according to the invention.
- the mixed friction states in the axial thrust bearing of the rotor due to unfavorable tribological conditions entail the risk of wear, which in many cases must be prevented by a coating of the chamber wall which causes costs.
- inventive design can be dispensed with a coating only for the purpose of Reibverschl fashionminderung, even if a coating as an additional measure should not be excluded categorically.
- the invention is not limited to the field of vacuum pumps.
- the medium to be conveyed may also be a liquid and in such embodiments also simultaneously form the lubricant.
- Preferred examples of liquid pumps are lubricating oil pumps for supplying an internal combustion engine of a vehicle or another unit of a vehicle with lubricant or hydraulic fluid. Such a pump is preferably driven by the engine of the vehicle.
- the sliding pairing with the at least one pocket according to the invention is preferably designed such that the transition rotational speed for the construction of the hydrodynamic lubricating film is already in idling operation of the drive motor is exceeded.
- the pump may be mounted in a vehicle or provided for use in a vehicle, and the drive motor may in particular be the drive motor of the vehicle.
- an axially flying bearing of the rotor is realized.
- an axial sliding bearing gap is formed between the sliding pair of axially facing sliding surfaces by the rotor when the transition speed of the opposite sliding surface of the chamber of the hydrodynamic lubricating film worn lifts off.
- the pairing on the opposite end face of the rotor is also formed so that there forms a hydrodynamic lubricating film, wherein the lubricant film thicknesses of the two lubricating films adjust the axial balance of forces accordingly.
- Axial flying or floating bearing allows for this adjustment.
- a single or more preferred pocket (s) according to the invention is expediently provided in the case of the sliding pair which has to absorb the axial thrust whose axial sliding surfaces therefore press against each other axially examined.
- the rotor can be reduced by means of a forming tool to the bag (s) by forming the rotor tool, i. be produced without additional processing and thus virtually cost-neutral.
- a subsequent machining process for example a grinding process
- the end face of the rotor is thus produced without additional manufacturing effort a suitable wedge gap geometry which is effective in tribological interaction with the preferably plane chamber wall.
- the inventive lubricating pocket (s) can be dispensed with an additional anti-wear coating one of the sliding bearing gap forming sliding surfaces.
- the rotor can be molded in particular by pressing and sintering as a sintered part made of metal or plastic or by injection molding of plastic as an injection molded part.
- FIG. 1 shows a rotary piston pump in a longitudinal section. It is a vacuum pump, for example for generating a negative pressure for a brake booster of a motor vehicle.
- the pump is driven by the combustion engine of the vehicle. It comprises a housing 1 with a housing structure 2 and a cover 3, which is detachably connected to the housing structure 2.
- FIG. 2 shows the pump in a plan view from the side of the lid 3 ago, with the lid 3 is removed.
- the housing 1 forms a delivery chamber 4 with an inlet 5 and an outlet 6 for the fluid to be delivered, in the exemplary embodiment air.
- the inlet 5 and the outlet 6 open at an inner circumferential surface 14 of the housing 1, in the embodiment of the housing structure 2, in the chamber 4.
- the inlet 5 is provided with a valve which allows a flow only in the chamber 4.
- the inlet 5 merges with an additional outlet 7.
- the outlet 6 is closed by a lamella valve 8 and the outlet 7 by a lamella valve 9, so that fluid through the outlet 6 and also through the outlet 7 only out of the chamber, but not in the chamber can flow in.
- the additional outlet 7 acquires significance only in the case of a temporary reversal of the direction of rotation V.
- a rotor 10 is rotatably disposed about a rotation axis R in the chamber 4.
- the rotor 10 is slidably mounted for rotation axially axially rotatable outside the chamber 4 along a rotor bearing section 11, for which purpose the bearing section 11 and by way of example the housing structure 2 form an axially relative to each other Oleitlagercruung.
- the rotor 10 has at the end facing away from the delivery chamber 4 a connection for a rotation secured connection directly with a camshaft or a drive wheel, via which it is in the mounted state of the internal combustion engine, for example, driven by the camshaft.
- the pump is designed as a single-vane vane pump.
- a wing 13 passes through the rotor 10 in the radial direction and is guided by the rotor 10 in a rotor slot 12 radially reciprocating back and forth.
- the rotor 10 and the wing 13 divide the delivery chamber 4 into two delivery cells, one of which is connected to the inlet 5 and the other to the outlet 6.
- the rotor 10 is arranged eccentrically in the chamber 4, so that it fluidly separates the two conveyor cells and in particular the inlet 5 and the outlet 6 with its outer circumferential surface.
- FIG. 2 take the rotor 10 and the wing 13 just a symmetry position, in which the two conveyor cells are the same size. If the rotor 10 rotates in the direction of rotation V, the in FIG.
- the rotor 10 has a sliding surface 15 on an end face remote from the drive side and a sliding surface 17 on the other end side facing the drive side.
- the sliding surfaces 15 and 17 form with axially opposite sliding surfaces 16 and 18 of the housing 1 each have a sliding pair.
- the frontal sliding surfaces of the wing 13 are not provided with their own reference numerals, but form with the axially facing chamber walls each have a further pair of bearings.
- the housing-side sliding surface 16 on the end face of the rotor 10 facing away from the drive side is formed by the cover 3, while the housing structure 2 forms the counter-sliding surface 18 for the rotor sliding surface 17.
- a lubricating oil or other suitable lubricant is supplied.
- the lubricant can be conducted into a central cavity passing axially through the rotor 10 and from there spreading over the sealing gaps 15 and 16 on the one hand and the sliding surfaces 17 and 18 on the other hand.
- a lubricant channel lead in particular through the bearing section 11.
- the lubricant passes through the centrifugal force acting on the rotating rotor 10 through the axial sliding gap of the sliding pair of sliding surfaces 17 and 18 in the chamber 4 and thereby ensures adequate lubrication of the sliding pair 17 and 18.
- the lubricant passes through the central cavity of the Rotor 10 at the other end face and there also distributed supported by the centrifugal force radially outwards and provides for the lubrication of the sliding surfaces formed by the sliding surfaces 15 and 16 and also the sliding pairings formed with the wing 13.
- the rotor 10 is provided in the side facing away from its drive side sliding surface 15 with pockets 20 in which the lubricant collects.
- the pockets 20 may also be referred to as lubrication pockets.
- a total of four pockets 20 are formed, in each case two pockets 20 on both sides of the wing 13.
- the wing 13 divides the sliding surface 15 in two Gleit vomhemissphDC, by way of example and preferably the same further as also preferably shaped as circular ring segments.
- the pockets 20 are uniformly distributed in the two hemispheres in the sense of a uniform distribution over the circumference of the lubricant.
- the sliding surface 15 separates the pockets 20 in the circumferential direction from each other and limits them radially outward, so forms radially outward of the two slots 12 a circumferential sliding pair with the axially opposite sliding surface 16.
- the pockets 20 are radially inwardly in the direction of the axis of rotation R. open, so open at an inner peripheral surface of the rotor 10.
- the lubricant passes from the central cavity of the rotor 10 into the cavity opening into the pockets 20, accumulates in it and is supported in the operation of the pump by the centrifugal force radially outward to to lubricate the sliding pair of the sliding surfaces 15 and 16 and at the same time to seal the axial sliding gap formed between the sliding surfaces 15 and 16 and thus contribute to the fluidic separation of the delivery cells.
- the sliding pair of sliding surfaces 17 and 18 also pockets, preferably inventive pockets, these may open radially into the said distribution groove and be supplied via this with the lubricant.
- the pockets 20 pass respectively at their leading in the direction of rotation V end 23 along a curved in plan view of the sliding surface 15 Taschenö Stammsrand in the sliding surface 15, while they pass at their trailing end 24 each along a straight radial opening edge in the sliding surface 15.
- the leading edge drops from a tangent to the edge with everywhere continuous curvature against the direction of rotation V in the direction of the trailing end 24 from. This smoothes the flow of the lubricant into the respective pocket 20, counteracts recirculation and the formation of dirt traps.
- the circumferentially measured length L in each of the pockets 20 continuously decreases in the radial direction from inside to outside.
- the pockets 20 are each shaped so that a hydrodynamic lubricant film builds up between the sliding surfaces 15 and 16 during operation of the pump as soon as the transition speed required for this purpose is exceeded.
- the pockets 20 are shaped and arranged to exceed the transition speed in the wear-related operating conditions of the pump. Is the pump for a drive by a Internal combustion engine of a vehicle provided or mounted in the vehicle so, the design is preferably such that the transition speed is below the speed that reaches the rotor 10 when the engine is idling.
- the pockets 20 each flat in the direction of their trailing end 24 continuously, so that they form with the axially opposite sliding surface 16 to a trailing end 24 tapered wedge gap.
- the lubricant is due to the force acting in the lubricant upon rotation of the rotor 10 thrust forces at the trailing end 24 of each of the pockets 20 between the sliding surfaces 15 and 16 and forms there when the transition speed is exceeded, a bearing lubricating film, the sliding surfaces 15 and 16 separated from each other and in the axial sliding gap ensures pure fluid friction. Due to the inventive design of the sliding pair 15 and 16 with the pockets 20, a rotor 10 axially supporting axial plain bearing is created in combination with the axially flying or floating slide bearing of the rotor 10.
- the sliding mating 15 and 16 with the pockets 20 is preferably further designed so that this thrust bearing also carries full and works at the transition speed is exceeded only in the field of fluid friction when it takes a stemming from the drive side at 11 axial force, an axial thrust must, as is the case in particular in preferred installation situations in which the vacuum pump is arranged on the housing or in a modification in the housing of an internal combustion engine of a motor vehicle.
- FIG. 3 shows a plan view of the end face of a rotor 10, in the sliding surface 15 pockets 21 are formed according to a second embodiment.
- the rotor 10 corresponds to the rotor 10 of Figures 1 and 2 and can replace it in the pump.
- the pockets 21 are rectangular in the radial plane shown. They each pass both at the leading end 23 and at the trailing end 24 along a straight, approximately radially pointing opening edge into the sliding surface 15.
- the two opening edges extend parallel to each other.
- the circumferentially extending radially outer opening edge interconnecting the opening edges at the leading end 23 and trailing end 24 is an arc portion on a circle about the axis of rotation R, but could be simply straight, for example.
- the pockets 21 are open at their radially inner side as in the first embodiment, thus open with their full pocket cross section on the inner circumferential surface of the rotor 10 in the central Cavity.
- FIG. 3 are the dimensions of the opening edge, along which the respective pocket 21 merges into the sliding surface 15, registered.
- the length measured in the circumferential direction is L and the width measured in the radial direction is designated B.
- the length L is constant over the entire width B.
- FIG. 4 is the sliding pair formed by the sliding surfaces 15 and 16 of the second embodiment in the in FIG. 3 registered section AA shown (without break edges).
- FIG. 4 is the settlement of the circular cylindrical section AA.
- the shape of the cross section of the pockets 21 can be seen.
- FIG. 5 shows one of the pockets 21 in an enlarged view. D denotes the same pocket depth for all pockets 21, which is measured in the axial direction between the lowest point of the respective pocket 21, the pocket bottom, and the plane sliding surface 15 which extends radially to the axis of rotation R.
- the pockets 21 rise from the bottom of the bag with the same constant inclination ⁇ in each case in the direction of the trailing end 24 of the respective pocket 21.
- the inclination ⁇ is less than 30 °, in the embodiment, it is about 15 °.
- the pockets 21 rise from the bottom of the bag into the sliding surface 15 steeply, in the embodiment as preferred with an inclination angle ⁇ of about 90 ° to the sliding surface 15.
- the opening edge at the leading end 23 may be chamfered, with such a chamfer than for steeply rising pocket wall is expected.
- the pockets 21 and the axially opposed sliding surface 16 define a substantially triangular wedge-shaped gap which tapers towards the trailing end of each pocket 21.
- a modification to the first embodiment is thus that the pockets 21 have a different course at the leading end by being straight there and not, as is preferred, continuously falling against the direction of rotation V. Further, in the sliding surface 15, a larger number of the pockets 21 are formed as in the first embodiment. As in the first embodiment, the pockets 21 on both sides of an extending through the slot 12, imaginary dividing plane symmetrical and arranged distributed uniformly in the two hemispheres of the sliding surface 15 in the circumferential direction.
- FIG. 6 shows an end view of a rotor 10, which has in the illustrated sliding surface 15 pockets 22 of a third embodiment, but otherwise the first and second Embodiment corresponds.
- the pockets 22 have an undercut with respect to the radial direction, so that over a part of their circumferentially measured length L, which is correspondingly variable in the third embodiment, a web is obtained, which is part of the sliding surface 15, and one through the Undercut obtained projection 25 in each of the pockets 22 radially bounded in the direction of the axis of rotation R.
- Each of the pockets 22 is extended by its extension 25 in the circumferential direction, namely as preferred against the direction of rotation V, ie at the trailing end.
- the extensions 25 are each formed in the region of the radial center of the sliding surface 15.
- the pockets 22 thus extend radially outward from their mouth into the central cavity of the rotor 10, first over a width region of shorter length L, and progressing radially outward into an outer region elongated by the extension 25, but as in the other embodiments bounded radially on the outside by a remaining there peripheral strip of the sliding surface 15 without interruption.
- FIG. 7 shows the sliding pair of the sliding surfaces 15 and 16 in the development of Kxeiszylinderroughs BB of FIG. 6 (without break lines).
- the pockets 22 form with the opposite sliding surface 16 each at the trailing end of a wedge gap by the pockets 22 rise from the respective pocket bottom with a constant inclination ⁇ to the trailing end 24 to the axial height of the sliding surface 15.
- the wedge gap is the same as the first and second embodiments.
- the pockets 22 at the leading end 23 are modified relative to the second exemplary embodiment in that they rise there from the pocket bottom with a pronounced curvature into the chamber wall which is then again orthogonal to the sliding surface 15.
- a chamfering advantageously present at the leading edge of the opening is again neglected, since it plays no role in terms of flow technology.
- the wedge-shaped gap can, as shown by way of example, extend at the trailing end over the entire width B of the pockets 22 or, in a modification, only over the radial width of the respective extension 25. However, an extent over the entire radial width B is preferred.
- the pockets 22 are seen in the radial plane at the leading end 23 are each continuously curved and fall as in the first embodiment in the direction of the trailing end 24 from a set to the opening edge of the front end 23 tangent. As in the first embodiment, the formation of dirt traps and recirculations are thereby prevented at the leading end.
- nachzutragen still be that in the region of the circumferentially elongated extension 25 is a larger pocket length L than in the radially inner and narrower pocket area is available to form the wedge-shaped gap.
- the pockets 22 can accordingly increase in the region of the respective extension 25 with a smaller inclination ⁇ in the direction of the trailing end 24, since the increase can be distributed over a greater length.
- FIGS. 8 to 11 each show a development of a circular cylindrical sectional area in the manner of the sectional views of FIGS. 4 and 7 (each without break line). Shown are pockets that are modified with respect to their cross-section, ie their axial depth profile, compared to the second and the third embodiment.
- the pockets are designated 26. They each rise from the pocket bottom in the direction of the trailing end 24 with a variable inclination ⁇ up to the sliding surface 15.
- the leading ends 23 each correspond to the second embodiment, the local inclination ⁇ is again about 90 °, with a chamfer is neglected.
- the wedge-gap-inducing rejuvenation sets like in the second embodiment, directly at the steep pocket wall of the leading end 23, thus extending over at least substantially the entire length L of the respective pocket 26.
- the inclination ⁇ decreases continuously in the direction of the trailing end 24, so that the bottom of the Pockets 26 in each case continuously bulges around in the direction of the opposite sliding surface 16, in relation to the sliding surface 16 is thus formed round convex.
- the inclination ⁇ is in the bag base between 40 and 60 °, but could well be up to 90 ° or less than 30 °. At the bottom of the bag could also be as in the third embodiment, a pronounced Kehlung be present.
- the inclination ⁇ is at the trailing end 24 at the transition into the sliding surface 15 less than 15 °, in particular, the bottom of the pocket 26 can pass tangentially into the sliding surface 15, so the inclination ⁇ continuously decrease to the value "zero".
- FIG. 9 shows pockets 27 of a fifth embodiment which differ substantially from the pockets of the other embodiments in that a wedge-shaped gap is also formed at the leading end 23 of each pocket 27.
- the pockets 27 are symmetrical in the cross section shown with respect to the direction of rotation V and the opposite direction, ie the pockets 27 each rise from the pocket bottom in and against the direction of rotation V with the same inclination to the sliding surface 15.
- the course of the inclination ⁇ thus corresponds to the course of the inclination ⁇ .
- consistency is assumed for the inclinations ⁇ and ⁇ .
- An advantage of forming a wedge gap with both the leading end 23 and the trailing end 24 is that the rotor 10 is rotationally invariant with respect to the formation of the hydrodynamic lubricating film, which may be advantageous for certain applications.
- FIG. 10 shows pockets 28 of a sixth embodiment.
- the wedge-shaped gap at the trailing end 24 only extends over approximately half the total length of each pocket 28 and only over one to two quarters of the pocket depth D. Seen in cross-section in this way in the region of the leading end 23 a pronounced Collection space for the lubricant and in the region of the trailing end 24 a smaller wedge gap than in the previous examples obtained.
- FIG. 11 shows pockets 29 of a seventh embodiment.
- the wedge gap is even flatter than in the pockets 28 of the sixth embodiment and also slightly longer.
- the inclination ⁇ is correspondingly lower and in the wedge gap is less than 10 ° everywhere.
- the wedge-shaped gap therefore extends over slightly more than half the length L and between one-sixth and one-fourth of the pocket depth D of the respective pocket 29.
- the pockets 29 are also modified relative to the pockets 28 in the region of the leading end 23, where they have a pronounced Have Kehlung, which has approximately the shape of a semicircle, for example.
- the bottom of the bag is formed by the trough-shaped groove and the subsequent wedge gap in the direction of the trailing end 24.
- the chamber wall immediately at the leading end 23 corresponds to the third embodiment ( FIG. 7 ).
- the pockets 20, 21 and 22 of the first, second and third embodiments may optionally have any of the different depth profiles, that is, each of the depth profiles may be combined with each of the pocket contour related to the radial direction and the circumferential direction.
- wedge gaps at the leading end 23 and at the trailing end 24, as exemplified in FIG. 9 are also obtained with a variable inclination ⁇ and ⁇ , for example in the manner of the wedge gap of FIG. 8
- the wedge column of the FIGS. 10 and 11 in the direction of the trailing end 24 a variable inclination ⁇ , for example, congruent to the embodiment of FIG. 8 exhibit.
- the pockets 28 and 29 may also run out to the leading end 23 in a wedge-shaped gap, but a particularly large proportion of the sliding surface 15 would be claimed by the thus shaped pocket 28 or 29 by such a geometry in relation to the length of the respective wedge gap.
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Abstract
Description
Die Erfindung betrifft Rotationskolbenpumpen und ist insbesondere auf Vakuumpumpen gerichtet.The invention relates to rotary piston pumps and is directed in particular to vacuum pumps.
Personenkraftwagen und auch leichte Nutzfahrzeuge werden seit langem mit pneumatischem Bremskraftverstärker ausgerüstet. Wurden die für die Bremskraftverstärker erforderlichen Unterdrücke bei Pkw-Ottomotoren früher noch durch die hinter den Drosselklappen des Ansaugsystems wirkenden Saugrohrunterdrücke aufgebracht, so reichen diese Saugrohrunterdrücke bei Dieselmotoren und auch modernen Ottomotoren mit Benzin-Direkteinspritzung wegen abweichender Lastregelkonzepte nicht mehr aus. Bei diesen Motorkonzepten kommen daher separate, vom Verbrennungsmotor angetriebene Vakuumpumpen zum Einsatz. Die üblicherweise in Drehschieberbauart ausgebildeten Pumpen werden mechanisch in der überwiegenden Zahl der Anwendungsfälle von der Nockenwelle des Motors angetrieben und sind in der Regel an der Stirnseite des Zylinderkopfs angeflanscht. In den letzten Jahren haben sich im Hinblick auf die Wirkungsgrade Pumpen mit nur einem Drehschieberflügel gegenüber Flügelzellenpumpen mit mehreren Flügeln durchgesetzt. Trotz der vergleichsweise guten Wirkungsgrade der einflügeligen Vakuumpumpen bedingt der bei Betrieb des Verbrennungsmotors permanente Antrieb der Pumpe, das vor dem Hintergrund der CO2-Problematik und dem ständigen Zwang zur Reduzierung des Kraftstoffverbrauchs einer Verringerung der für die Pumpe erforderlichen Antriebsleistung weiterhin Beachtung geschenkt werden muss. Ein Ansatzpunkt, den Wirkungsgrad zu verbessern, ist die Verringerung der Reibleistung an der Stirnseite des Pumpenrotors.Passenger cars and light commercial vehicles have long been equipped with pneumatic brake booster. Were the necessary for the brake booster negative pressure in passenger car gasoline engines formerly applied by acting behind the throttle of the intake manifold vacuum, so these Saugrohrunterdrücke sufficient for diesel engines and modern gasoline engines with gasoline direct injection because of different load control concepts no longer. These engine concepts therefore use separate vacuum pumps driven by the combustion engine. The pumps, which are usually designed in rotary vane type, are mechanically driven by the camshaft of the engine in the majority of applications and are usually flange-mounted on the front side of the cylinder head. In recent years, in terms of efficiencies, pumps with only one rotary vane have prevailed over multi-vane vane pumps. Despite the comparatively good efficiencies of the single-leaf vacuum pumps, the drive of the pump, which is permanent during operation of the internal combustion engine, must continue to pay attention to a reduction in the drive power required for the pump against the background of the CO 2 problem and the constant compulsion to reduce fuel consumption. A starting point for improving the efficiency is the reduction of the friction power at the end face of the pump rotor.
Nach der
In einer aus der
Die
Die
Es ist eine Aufgabe der Erfindung, die Reibleistung der stirnseitigen tribologischen Paarung zwischen Kammerwand und Rotor einer Rotationskolbenpumpe mit geringem technischen Aufwand bei möglichst geringer Leckage zu mindern.It is an object of the invention to reduce the friction of the front tribological pairing between chamber wall and rotor of a rotary piston pump with little technical effort at the lowest possible leakage.
Die Erfindung hat eine Rotationskolbenpumpe zum Gegenstand, die ein Gehäuse mit einer Förderkammer und wenigstens einen in der Förderkammer um eine Rotationsachse drehbaren Rotor umfasst. Der Rotor weist an seinen beiden Stirnseiten Gleitflächen auf, die mit axial zugewandten Gleitflächen der Kammer jeweils eine Gleitpaarung bilden. Die stirnseitigen Kammerwände, die besagte Gleitflächen der Kammer bilden, sind vorzugsweise nicht beweglich, sondern im Gehäuse stationär. In wenigstens einer der Gleitflächen, d.h. in wenigstens einer der stirnseitigen Gleitflächen des Rotors oder in wenigstens einer der stirnseitigen Gleitflächen der Kammer, ist wenigstens eine Tasche für Schmiermittel geformt. Die Tasche wird bezüglich der Rotationsachse in Umfangsrichtung und radial außen von der die Tasche enthaltenden Gleitfläche begrenzt.The subject of the invention is a rotary piston pump comprising a housing with a delivery chamber and at least one rotor rotatable about a rotation axis in the delivery chamber. The rotor has on its two end faces sliding surfaces which each form a sliding pair with axially facing sliding surfaces of the chamber. The end-side chamber walls which form said sliding surfaces of the chamber are preferably not movable, but stationary in the housing. In at least one of the sliding surfaces, i. in at least one of the front-side sliding surfaces of the rotor or in at least one of the front-side sliding surfaces of the chamber, at least one pocket for lubricant is formed. The pocket is bounded circumferentially with respect to the axis of rotation and radially outward by the sliding surface containing the pocket.
Nach der Erfindung ist die Tasche so geformt, dass sich bei drehendem Rotor im Spalt der die Tasche aufweisenden Gleitpaarung ein hydrodynamischer Schmierfilm aufbaut. Sobald der Rotor die Übergangsdrehzahl der Gleitpaarung erreicht, ist der hydrodynamische Schmierfilm tragfähig und der Rotor beginnt auf dem Schmiermittel zu gleiten. Bei Überschreiten der Übergangsdrehzahl gleitet der Rotor im voll tragenden Bereich, und es herrscht nur noch Flüssigkeitsreibung. Auf diese Weise werden die Gleitflächen der Gleitpaarung voneinander getrennt und Festkörperreibung vermieden, während die axiale Dicke des von den Gleitflächen axial begrenzten Spalts dennoch gering gehalten werden kann. Die Tasche ist so geformt, dass sich der hydrodynamische Schmierfilm bei den für den Betrieb der Rotationskolbenpumpe typischen Drehzahlen, bei denen die Rotationskolbenpumpe überwiegend betrieben wird, aufbaut. Die Tasche hat hierfür ein ausreichendes Volumen und eine geeignete Form, insbesondere weist sie ein für den Schmierfilmaufbau sorgendes Tiefenprofil auf. Vorzugsweise ist die Tasche so geformt, dass sich im Gleitspalt unmittelbar im Anschluss an das in Drehrichtung des Rotors nachlaufende Ende der Tasche der hydrodynamische Schmierfilm einstellt. Die gleiche oder die axial gegenüberliegende Gleitfläche kann oder können eine oder mehrere weitere Tasche(n) enthalten, die diese Bedingung nicht erfüllen, solange im Spalt der Gleitflächen insgesamt ab der Übergangsdrehzahl der hydrodynamische Schmierungszustand herrscht. Falls wie bevorzugt mehrere erfindungsgemäße Taschen vorgesehen sind, genügt es, wenn diese Taschen erst im Verbund den Aufbau des hydrodynamischen Schierfilms bewirken.According to the invention, the pocket is shaped so that, when the rotor is rotating, a hydrodynamic lubricating film builds up in the gap of the bearing bearing the pocket. Once the rotor reaches the transition speed of the mating pair, the hydrodynamic lubricant film is viable and the rotor begins to slide on the lubricant. When crossing the Transitional speed, the rotor slides in the fully supporting area, and there is only liquid friction. In this way, the sliding surfaces of the sliding pair are separated and solid friction avoided, while the axial thickness of the axially limited by the sliding surfaces gap can still be kept low. The pocket is shaped so that the hydrodynamic lubricant film builds up at the speeds typical for the operation of the rotary piston pump, in which the rotary piston pump is predominantly operated. The bag has for this purpose a sufficient volume and a suitable shape, in particular, it has a care for the lubricating film construction depth profile. The pocket is preferably shaped such that the hydrodynamic lubricating film sets in the sliding gap immediately after the trailing end of the pocket in the direction of rotation of the rotor. The same or the axially opposite sliding surface can or may contain one or more further pocket (s) that do not meet this condition, as long as in the gap of the sliding surfaces as a whole from the transition speed prevails the hydrodynamic lubrication state. If, as preferred, several pockets according to the invention are provided, it is sufficient if these pockets bring about the construction of the hydrodynamic shear film only in combination.
Die Tasche flacht in Umfangsrichtung, in Richtung ihres nachlaufenden Endes ab, verjüngt sich also, vorzugsweise über ihre gesamte radial gemessene Breite. Falls sich die Verjüngung nur über einen Teil der radialen Taschenbreite erstreckt, ist dieser verjüngte Breitenbereich vorzugsweise radial im mittleren Bereich der Gleitfläche angeordnet. Die Tasche bildet im Spalt der Gleitflächen am nachlaufenden Ende einen Keil. Im verjüngten Bereich kann die Tasche im Verlauf des Anstiegs auf die sie enthaltende Gleitfläche eine variable Neigung aufweisen, insbesondere eine Neigung, die sich in Richtung auf das nachlaufende Ende verringert, so dass sich der Boden der Tasche im Bereich des Keils in Richtung auf die gegenüberliegende Gleitfläche der Gleitpaarung rund wölbt. In ebenfalls bevorzugten Ausführungen ist die Neigung über zumindest einen größeren, vorzugsweise den überwiegenden Teil des Keils konstant. Der Taschenboden kann in dem Anstieg ein oder mehrere gekrümmte(s) Teilstück(e) in Kombination mit einem oder mehreren geraden Teilstück(en) aufweisen. Er kann im Keilspalt auch eine oder mehrere Stufe(n) aufweisen, ein kontinuierlicher Verlauf wird allerdings bevorzugt. Er kann in Bezug auf die axial gegenüberliegende Gleitfläche vom Auslauf in die Gleitfläche in Umfangsrichtung beabstandet sogar einen oder mehrere konkave Abschnitte aufweisen, solange dennoch der hydrodynamische Schmierfilm aufgebaut wird.The pocket flattens in the circumferential direction, in the direction of its trailing end, thus tapering, preferably over its entire radially measured width. If the taper extends only over part of the radial pocket width, this tapered width region is preferably arranged radially in the middle region of the sliding surface. The pocket forms a wedge in the gap of the sliding surfaces at the trailing end. In the tapered region, the pocket may have a variable inclination in the course of the rise to the sliding surface containing it, in particular an inclination which decreases towards the trailing end, so that the bottom of the pocket in the region of the wedge towards the opposite Sliding surface of the sliding couple bulges around. In likewise preferred embodiments, the inclination is constant over at least one larger, preferably the predominant part of the wedge. The pocket bottom may include in the rise one or more curved section (s) in combination with one or more straight section (s). It may also have one or more stages in the wedge-shaped gap, but a continuous course is preferred. It can with respect to the axially opposite sliding surface from the outlet in the sliding surface in the circumferential direction may even have one or more concave sections, as long as the hydrodynamic lubricant film is still built up.
Der Keil erstreckt sich vorzugsweise über wenigstens ein Viertel, noch bevorzugter über wenigstens die Hälfte der Taschentiefe, wobei als Bezugstiefe die maximale Tiefe der Tasche dient. So kann die Tasche vom Taschengrund aus beispielsweise senkrecht, d.h. in axialer Richtung, oder mit zunehmender Neigung ansteigen und erst ab der Hälfte der Taschentiefe oder bereits vorher sich allmählich verjüngen. Die Verjüngung kann insbesondere bereits unmittelbar im Taschengrund einsetzen, d.h. vom Taschengrund aus unmittelbar mit einer Neigung zu der sie enthaltenden Gleitfläche hin abflachen. Die Neigung zur Gleitfläche sollte zumindest im nachlaufenden Endbereich des Keils höchstens 45°, bevorzugter höchstens 30°, betragen, sowohl im Falle einer konstanten als auch im Falle einer variablen Neigung. Zumindest am nachlaufenden Ende des Keils, beim Auslaufen in die Gleitfläche, sollten die genannten Winkelwerte nicht überstiegen werden. Geringere Neigungswinkel sind im Hinblick auf die für den Aufbau des hydrodynamischen Schmierfilms im Schmiermittel wirkenden Scherkräfte insbesondere im Auslauf des Keils von Vorteil. So wird eine Neigung unmittelbar am Ende des Keils von höchstens 15° besonders bevorzugt, ebenso entspricht es bevorzugten Ausführungen, wenn die Neigung zumindest am Ende des Keils kontinuierlich abnimmt, wobei der Keil insbesondere tangential in die Gleitfläche auslaufen kann. Hinsichtlich der in Umfangsrichtung gemessenen Keillänge ist es von Vorteil, wenn sich der Keil über wenigstens die halbe Taschenlänge erstreckt, wobei der Vorteil dieses Geometriemerkmals mit abnehmender Taschenlänge zunimmt.The wedge preferably extends over at least a quarter, more preferably over at least half of the pocket depth, the reference depth being the maximum depth of the pocket. For example, the bag may be perpendicular to the bottom of the bag, i. in the axial direction, or increase with increasing inclination and only from half the pocket depth or already before tapering gradually. In particular, the taper can already be used immediately in the pocket bottom, i. From the pocket bottom flatten out directly with an inclination to the sliding surface containing them. The inclination to the sliding surface should be at most in the trailing end region of the wedge at most 45 °, more preferably at most 30 °, both in the case of a constant and in the case of a variable inclination. At least at the trailing end of the wedge, when leaving the sliding surface, the mentioned angle values should not be exceeded. Lower angles of inclination are advantageous in view of the shear forces acting on the structure of the hydrodynamic lubricant film in the lubricant, in particular in the outlet of the wedge. Thus, an inclination directly at the end of the wedge of at most 15 ° is particularly preferred, it also corresponds to preferred embodiments, when the inclination decreases continuously, at least at the end of the wedge, the wedge can expire in particular tangentially into the sliding surface. With regard to the wedge length measured in the circumferential direction, it is advantageous if the wedge extends over at least half the pocket length, wherein the advantage of this geometry feature increases with decreasing pocket length.
Vorteilhaft ist, wenn die Tasche an ihrem nachlaufenden Ende in die Gleitfläche flacher, mit geringerer Neigung als an ihrem vorlaufenden Ende ausläuft. Am vorlaufenden Ende kann die Tasche steil, insbesondere senkrecht, bis in die Gleitfläche ansteigen, wobei eine Anfasung beim Übergang in die Gleitfläche als zur steilen Wand gehörig angesehen wird, da Anfasungen nur der Entgratung dienen, aber keinen hydrodynamischen Schmierfilmaufbau bewirken. Die Erfindung betrifft aber auch Ausführungen, in denen die Tasche auch am vorlaufenden Ende keilförmig ausläuft. Die geometrische Asymmetrie mit einem ausgeprägten Keil am nachlaufenden Ende zur Erzeugung des hydrodynamischen Schmierfilms und einer am vorlaufenden Ende steil oder zumindest deutlich steiler bis in die Gleitfläche ansteigenden Tasche wird jedoch bevorzugt, da hierdurch der Flächenanteil der Tasche im Verhältnis zur Gleitfläche minimiert wird.It is advantageous if the bag expires at its trailing end in the sliding surface flat, with less inclination than at its leading end. At the leading end of the bag can steeply, in particular vertically, rise to the sliding surface, with a chamfer at the transition to the sliding surface as belonging to the steep wall, since chamfers serve only the deburring, but do not cause hydrodynamic film structure. However, the invention also relates to embodiments in which the bag also terminates wedge-shaped at the leading end. The geometric asymmetry with a pronounced wedge at the trailing end to produce the hydrodynamic lubricating film and at the leading end steep or at least significantly steeper to the Sliding surface rising pocket is preferred, however, as this minimizes the area ratio of the pocket relative to the sliding surface.
Vorzugsweise besteht eine fluidische Verbindung zwischen der Tasche und einem radial äußeren Rand der sie enthaltenden Gleitfläche nur über den axialen Spalt zwischen den einander zugewandten Gleitflächen, so dass Schmiermittel nur über die die Gleitpaarung bildenden Gleitflächen aus der Tasche nach radial außen dringen kann. Alternativ kann aber auch zwischen der Tasche und dem radial äußeren Rand der sie enthaltenden Gleitfläche oder der Tasche und einer radial außen an die Gleitfläche grenzenden Umfangsfläche, eine Verbindung zusätzlich vorgesehen sein, entweder in Form eines unter der Gleitfläche liegenden oder an der Gleitfläche offenen Verbindungskanals. Solch ein optionaler Verbindungskanal ist jedoch so gestaltet, dass er dem Abfluss des Schmiermittels aus der Tasche einen erheblichen Strömungswiderstand entgegenstellt, der um ein Mehrfaches größer ist als im Falle einer Tasche, die die Gleitfläche radial mit ihrem vollen Taschenquerschnitt durchsetzt. Eine radiale Begrenzung der Tasche durch die Gleitfläche wird somit auch dann gesehen, wenn ein in Umfangsrichtung schmaler oder in Tiefenrichtung der Tasche flacher Verbindungskanal einen Strömungsquerschnitt aufweist, der um ein Mehrfaches kleiner ist als ein größter Taschenquerschnitt. Ein optionaler Verbindungskanal kann dazu genutzt werden, über die Tasche gezielt Schmiermittel nach radial außen in die Kammer und dort zur Schmierung beispielsweise der Spitze eines Flügels einer Flügelzellenpumpe zu nutzen. Der optionale Verbindungskanal ist aber in jedem Fall so bemessen, dass sich trotz des durch ihn erleichterten Abflusses von Schmiermittel der hydrodynamische Schmierfilm bildet.Preferably, there is a fluidic connection between the pocket and a radially outer edge of the sliding surface containing them only over the axial gap between the sliding surfaces facing each other, so that lubricant can penetrate only radially outward from the pocket via the sliding surfaces forming sliding surfaces. Alternatively, however, a connection can additionally be provided between the pocket and the radially outer edge of the sliding surface or pocket and a circumferential surface radially adjoining the sliding surface, either in the form of a connecting channel lying below the sliding surface or open on the sliding surface. However, such an optional connection channel is designed so that it provides the flow of lubricant from the bag considerable resistance to flow, which is several times greater than in the case of a pocket which passes through the sliding surface radially with its full pocket cross-section. A radial boundary of the pocket by the sliding surface is thus also seen when a narrow in the circumferential direction or in the depth direction of the pocket flat connecting channel has a flow cross-section which is smaller by a multiple than a largest pocket cross-section. An optional connection channel can be used to selectively use lubricant on the bag radially outward into the chamber and there for lubrication, for example, the tip of a wing of a vane pump. In any case, the optional connecting channel is dimensioned such that, in spite of the drainage of lubricant facilitated by it, the hydrodynamic lubricating film forms.
Das nachlaufende Ende der Tasche kann in der Draufsicht auf die Gleitfläche gesehen über seine gesamte radiale Breite gerade und zumindest im Wesentlichen radial verlaufen, die Tasche also über eine radiale Randlinie in die Gleitfläche übergehen. Die Tasche kann in der Draufsicht auf die Gleitfläche gesehen stattdessen aber auch hinterschnitten sein, so dass sie am nachlaufenden Ende einen sich in Umfangsrichtung erstreckenden Fortsatz aufweist, der nach radial innen, in Richtung auf die Rotationsachse des Rotors, von der Gleitfläche begrenzt wird. Durch den Hinterschnitt wird einem Abströmen des Schmiermittels nach radial einwärts entgegengewirkt, insbesondere in bevorzugten Ausführungen, in denen die Tasche nach radial innen, d. h. in Richtung auf die Rotationsachse, an einer inneren Umfangsfläche mündet, die Gleitfläche radial in Richtung auf die Rotationsachse also durchsetzt. Die Gleitfläche ist in derartigen Ausführungen ringförmig um die Rotationsachse erstreckt. Eine die Gleitfläche nach radial innen durchsetzende Tasche hat den Vorteil, dass solch eine Tasche aus dem zentralen Bereich innerhalb der ringförmigen Gleitfläche mit Schmiermittel versorgt werden kann.The trailing end of the pocket can, seen in plan view of the sliding surface, run straight over its entire radial width and run at least essentially radially, ie pass over the pocket into the sliding surface via a radial edge line. Instead, the pocket may also be undercut in plan view of the sliding surface, so that it has a circumferentially extending extension at the trailing end which is bounded radially inwards, in the direction of the axis of rotation of the rotor, by the sliding surface. The undercut counteracts a flow of the lubricant radially inwardly, in particular in preferred embodiments, in which the pocket radially inward, ie in the direction of the axis of rotation, on an inner peripheral surface opens, so that the sliding surface passes radially in the direction of the axis of rotation. The sliding surface is in such embodiments extends annularly around the axis of rotation. A radially inwardly passing through the sliding surface has the advantage that such a pocket can be supplied with lubricant from the central region within the annular sliding surface.
In bevorzugten Ausführungen sind in der die Tasche enthaltenden Gleitfläche weitere Taschen in der erfindungsgemäßen Art geformt. Die Taschen sind um die Rotationsachse in Umfangsrichtung voneinander beabstandet, vorzugsweise verbleibt zwischen ihnen jeweils ein Bereich der Gleitfläche, und werden radial außen von der sie enthaltenden Gleitfläche begrenzt. Die Taschen sind um die Rotationsachse vorteilhafterweise zumindest im Wesentlichen gleichmäßig verteilt angeordnet. Die Winkelabstände jeweils nächstbenachbarter Taschen sind in derartigen Ausführungen im Wesentlichen gleich. Im Falle einer Drehschieberpumpe mit einem einzigen Flügel, der den Rotor radial durchsetzt, wird als gleichmäßige Winkelteilung auch eine Anordnung angesehen, in der die Taschen symmetrisch in Bezug auf den Flügel verteilt sind. Die Taschen sind in der Draufsicht auf die Gleitfläche gesehen und im Querschnitt vorzugsweise untereinander gleich, können grundsätzlich aber auch voneinander abweichen. Sie können auch im Tiefenprofil voneinander abweichen, bevorzugter sind sie jedoch auch im Tiefenprofil untereinander gleich. Das Tiefenprofil ist der Verlauf der axialen Tiefe in Umfangsrichtung auf einer die Tasche schneidenden Zylinderfläche um die Rotationsachse.In preferred embodiments, further pockets in the manner according to the invention are formed in the sliding surface containing the pocket. The pockets are circumferentially spaced from each other about the axis of rotation, preferably a portion of the sliding surface remains between them, and are bounded radially outward by the sliding surface containing them. The pockets are advantageously arranged distributed around the axis of rotation at least substantially uniformly. The angular distances of respectively adjacent pockets are substantially the same in such embodiments. In the case of a rotary vane pump with a single vane, which passes radially through the rotor, is regarded as a uniform angle division, an arrangement in which the pockets are distributed symmetrically with respect to the wing. The pockets are seen in plan view of the sliding surface and in cross section preferably equal to each other, but may in principle also differ from each other. You can also deviate from each other in the depth profile, but more preferably they are equal to each other in the depth profile. The depth profile is the course of the axial depth in the circumferential direction on a cylindrical surface which cuts the pocket about the axis of rotation.
In Ausführungen mit nur einer einzigen Tasche kann diese Tasche insbesondere so angeordnet sein, dass sie einer in manchen Verwendungen im Pumpenbetrieb vorhandenen leichten Kippstellung der Rotorachse entgegenwirkt. In solch einer Zusatzfunktion ist die Tasche in einer der stirnseitigen Gleitflächen der Kammer angeordnet, also in Bezug auf die Kammer stationär. Die Kippstellung des Rotors, falls im Betrieb vorhanden, ist im Vorhinein bekannt, so dass die Tasche entsprechend angeordnet werden kann. Falls in der betreffenden Gleitfläche der Kammer in Umfangsrichtung voneinander beabstandet mehrere Taschen der erfindungsgemäßen Art geformt sind, sind diese Taschen so angeordnet, dass sie die Kippstellung zusammenwirkend zumindest teilweise kompensieren, beispielsweise indem die Taschen in Umfangsrichtung gesehen nur in der Hälfte der Gleitfläche vorgesehen sind, in der der Spalt zwischen den Gleitflächen aufgrund der Kippstellung kleiner als in der anderen Hemisphäre ist. Andererseits können Taschen aber auch über den gesamten Umfang verteilt angeordnet sein, wobei zur Kompensation einer Kippstellung in der entsprechenden Hemisphäre das Verhältnis von Taschenfläche zu verbleibender Gleitfläche größer als in der anderen Hemisphäre der betreffenden Gleitfläche ist.In embodiments with only a single pocket, this pocket may in particular be arranged so that it counteracts a light tilting position of the rotor axis which is present in some applications in pump operation. In such an additional function, the pocket is arranged in one of the end-side sliding surfaces of the chamber, ie stationary with respect to the chamber. The tilting position of the rotor, if present during operation, is known in advance, so that the bag can be arranged accordingly. If a plurality of pockets of the type according to the invention are formed in the respective sliding surface of the chamber in the circumferential direction, these pockets are arranged so as to at least partially compensate the tilting position, for example by providing the pockets in the circumferential direction only in half of the sliding surface, in the the gap between the sliding surfaces is smaller due to the tilted position than in the other hemisphere. On the other hand, however, pockets can also be distributed over the entire circumference, with the ratio of pocket area to remaining sliding area being greater than in the other hemisphere of the relevant sliding area in order to compensate for a tilted position in the corresponding hemisphere.
Die Tasche oder die bevorzugt mehreren Taschen kann oder können wie erwähnt in einer der Gleitflächen des Rotors oder einer der Rotorstimseite axial zugewandten Kammerwand geformt sein. Das Wort "oder" wird stets im üblichen logischen Sinn als ein "inklusiv oder" verstanden, umfasst also sowohl die Bedeutung von "entweder ... oder" als auch die Bedeutung von "und", soweit der jeweils konkrete Zusammenhang nicht ausschließlich nur eine eingeschränkte Bedeutung zulässt. Eine einzige oder mehrere Taschen kann oder können daher beispielsweise nur in einer oder nur in beiden stirnseitigen Gleitflächen des Rotors vorgesehen sein, wobei diese beiden Ausführungen besonders bevorzugt werden, oder nur in einer der die beiden Gleitpaarungen mitbildenden Gleitflächen der Kammer oder nur in beiden stirnseitigen Gleitflächen der Kammer. In weiteren Ausführungsformen kann eine einzige Tasche oder können mehrere Taschen auch in einer oder in beiden Gleitfläche(n) des Rotors und zusätzlich in einer oder in beiden zugewandten Gleitfläche(n) der Kammer geformt sein, was beispielsweise auch den Fall einschließt, dass eine einzige oder mehrere Taschen nur an einer der beiden Stirnseiten des Rotors und eine einzige oder mehrere Taschen nur in derjenigen Gleitfläche der Kammer geformt ist oder sind, die eine Gleitpaarung an der gegenüberliegenden Stirnseite des Rotors mit der dortigen Rotorgleitfläche bildet. Zur Erfindung gehört ferner auch der Fall, dass der Rotor an einer oder an beiden Stirnseiten eine einzige oder mehrere Taschen aufweist und die Kammer zusätzlich an der gleichen Stirnseite ebenfalls mit einer einzigen oder mehreren Taschen der erfindungsgemäßen Art versehen ist, wobei die der gleichen Gleitpaarung zugeordneten Taschen des Rotors und der Kammer radial zueinander so versetzt sind, dass sie bei Rotation des Rotors nicht in Überdeckung gelangen.As mentioned, the pocket or preferably a plurality of pockets may or may not be formed in one of the sliding surfaces of the rotor or one of the chamber sides of the rotor facing side. The word "or" is always understood in the usual logical sense as an "inclusive or", ie includes both the meaning of "either ... or" as well as the meaning of "and", as far as the specific context is not exclusively only one limited meaning. A single or multiple pockets may or may therefore be provided, for example, only in one or only in both frontal sliding surfaces of the rotor, these two embodiments are particularly preferred, or only in one of the two sliding pairings co-forming sliding surfaces of the chamber or only in both frontal sliding surfaces the chamber. In further embodiments, a single pocket or pockets may also be formed in one or both of the sliding surface (s) of the rotor and additionally in one or both facing sliding surfaces of the chamber, including, for example, the case where a single pocket or a plurality of pockets only on one of the two end faces of the rotor and a single or more pockets is formed only in that sliding surface of the chamber or are, which forms a sliding pair on the opposite end face of the rotor with the local Rotorgleitfläche. The invention also includes the case that the rotor on one or both ends has a single or more pockets and the chamber is also provided on the same face also with a single or more pockets of the type according to the invention, which associated with the same sliding pair Bags of the rotor and the chamber are radially offset from each other so that they do not overlap during rotation of the rotor.
Eine bevorzugte Bauart sind Flügelzellenpumpen mit einem einzigen oder mehreren verschiebbar vom Rotor geführten Flügel(n), und auch Schwenkflügelpumpen. Unter den Drehschiebermaschinen werden wiederum einflügelige Ausführungen bevorzugt, also Ausführungen in denen der Rotor mit dem Flügel die Förderkammer in nur zwei Zellen unterteilt. Die Rotationskolbenpumpe kann mit variablem oder konstantem Fördervolumen ausgeführt sein. Sie kann mehrhubig sein, ist aber bevorzugt einhubig. In der Förderkammer können mehrere Rotoren, beispielsweise zwei Rotoren, angeordnet sein, wobei vorzugsweise bei beiden Rotoren an jeweils wenigstens einer axialen Stirnseite eine Gleitpaarung in erfindungsgemäßer Weise gebildet wird. In den Ausführungen als Drehschieber-, Schwenkflügel oder gegebenenfalls auch Pendelschieberpumpe ist die Tasche bei Formung am Rotor vorteilhafterweise in einem Umfangsbereich der Gleitfläche geformt, der nicht von einem Flügel, einem Schiebe- oder Schwenkflügel, durchsetzt wird. In Ausführungen, in denen die Gleitfläche mit der wenigstens einen erfindungsgemäßen Tasche in Umfangsrichtung nicht durchbrochen ist, sondern sich um die Rotationsachse vollständig umlaufend erstreckt, spielt diese Überlegung keine Rolle. Sind in der betreffenden Gleitfläche wie bevorzugt mehrere Taschen erfindungsgemäß geformt und angeordnet, so sind die mehreren Taschen bei Anordnung im Rotor um die Rotationsachse vorteilhafterweise so und in solcher Zahl angeordnet, dass im Winkelbereich jeder Zelle der Zellenpumpe jeweils wenigstens eine der Taschen angeordnet ist. In einflügeligen Ausführungen sind pro Zelle, die der Rotor mit seinem einstückigen oder geteilten Flügel bildet, vorzugsweise je wenigstens zwei der erfindungsgemäßen Taschen angeordnet.One preferred type is vane pumps having a single or multiple vanes (s) slidably guided by the rotor, and also swing vane pumps. Among the rotary vane machines in turn single-wing designs are preferred, ie Versions in which the rotor with the wing divides the delivery chamber into only two cells. The rotary piston pump can be designed with a variable or constant delivery volume. It can be multi-stroke, but is preferably one-stroke. A plurality of rotors, for example two rotors, may be arranged in the delivery chamber, with a pair of bearings preferably being formed in accordance with the invention in each case on both rotors at at least one axial end side. In the embodiments as a rotary valve, swing or possibly also pendulum slide pump, the bag is advantageously formed in shaping on the rotor in a peripheral region of the sliding surface, which is not penetrated by a wing, a sliding or swing wing. In embodiments in which the sliding surface with the at least one pocket according to the invention is not interrupted in the circumferential direction, but extends completely circumferentially around the axis of rotation, this consideration plays no role. If several pockets are shaped and arranged according to the invention in the relevant sliding surface, the plurality of pockets are advantageously arranged in the rotor around the axis of rotation in such a number that at least one of the pockets is arranged in the angular region of each cell of the cell pump. In single-leaf embodiments, per cell, which forms the rotor with its one-piece or divided wing, preferably at least two of the pockets according to the invention are arranged.
Die Rotationskolbenpumpe fordert vorzugsweise ein gasförmiges Arbeitsfluid, während das Schmiermittel vorzugsweise flüssig ist. Insbesondere ist die Erfindung auf eine Vakuumpumpe gerichtet, die in einem Kraftfahrzeug eingebaut oder für den Einbau in einem Kraftfahrzeug vorgesehen ist. Die Pumpe kann den für einen Bremskraftverstärker erforderlichen Unterdruck erzeugen. Sie wird vorzugsweise vom Motor angetrieben, bei dem es sich vorzugsweise um einen Verbrennungsmotor handelt. Für solche Vakuumpumpen ist es üblich, dass der Rotor am Umfang eines Rotorlagerabschnitts mit einer fliegenden Gleitlagerung versehen und somit axial nicht fixiert, sondern entweder innerhalb der axialen Toleranz oder eines bewusst vorgesehenen axialen Spiels zwischen den stirnseitigen Gleitflächen der Förderkammer beweglich ist. Antriebsseitig wirkt dabei auf der dem Durchmesser des Lagerabschnitts entsprechenden Projektionsfläche des Rotors der Druck des Kurbelgehäuses des Motors, der in der Regel etwa dem Atmosphärendruck entspricht, während an der abgewandten, gegenüberliegenden Projektionsfläche des Rotors in der überwiegenden Zahl der Betriebszustände der Pumpe ein vergleichsweise hoher Unterdruck wirkt, so dass der Rotor gegen die betreffende Gleitfläche der Kammer gedrückt wird. Es entsteht entsprechend dem Druckgefälle ein beachtlicher Axialschub, der wegen der im Falle einer im Stand der Technik planen stirnseitigen Geometrie des Rotors zu einer großen Reibleistung führt, werden nicht erfindungsgemäß Gegenmaßnahmen ergriffen. Die durch ungünstige tribologische Verhältnisse bedingten Mischreibungszustände im dortigen Axialgleitlager des Rotors bergen die Gefahr von Verschleiß, dem in vielen Fällen durch eine kostenverursachende Beschichtung der Kammerwand vorgebeugt werden muss. Bei erfindungsgemäßer Gestaltung kann auf eine Beschichtung nur zum Zwecke der Reibverschleißminderung verzichtet werden, auch wenn ein Beschichten als zusätzliche Maßnahme nicht kategorisch ausgeschlossen werden soll.The rotary piston pump preferably requires a gaseous working fluid while the lubricant is preferably liquid. In particular, the invention is directed to a vacuum pump which is installed in a motor vehicle or intended for installation in a motor vehicle. The pump can generate the vacuum required for a brake booster. It is preferably powered by the engine, which is preferably an internal combustion engine. For such vacuum pumps, it is usual that the rotor on the circumference of a rotor bearing portion provided with a floating sliding bearing and thus axially fixed, but is movable either within the axial tolerance or a deliberately provided axial play between the end faces of the delivery chamber. On the drive side acts on the corresponding diameter of the bearing portion projection surface of the rotor, the pressure of the crankcase of the engine, which generally corresponds approximately to the atmospheric pressure, while at the opposite, opposite projection surface of the rotor in the a relatively high negative pressure acts on a large number of operating states of the pump, so that the rotor is pressed against the relevant sliding surface of the chamber. It arises according to the pressure gradient, a considerable axial thrust, which leads to a large friction in the case of planning in the prior art frontal geometry of the rotor, countermeasures are not taken according to the invention. The mixed friction states in the axial thrust bearing of the rotor due to unfavorable tribological conditions entail the risk of wear, which in many cases must be prevented by a coating of the chamber wall which causes costs. In the inventive design can be dispensed with a coating only for the purpose of Reibverschleißminderung, even if a coating as an additional measure should not be excluded categorically.
Grundsätzlich ist die Erfindung auf das Gebiet der Vakuumpumpen nicht beschränkt. Das zu fördernde Medium kann auch eine Flüssigkeit sein und in derartigen Ausführungen auch gleichzeitig das Schmiermittel bilden. Bevorzugte Beispiele für Flüssigkeitspumpen sind Schmierölpumpen für die Versorgung eines Verbrennungsmotors eines Fahrzeugs oder eines anderen Aggregats eines Fahrzeugs mit Schmiermittel oder Hydraulikflüssigkeit. Auch eine solche Pumpe wird bevorzugt vom Motor des Fahrzeugs angetrieben.Basically, the invention is not limited to the field of vacuum pumps. The medium to be conveyed may also be a liquid and in such embodiments also simultaneously form the lubricant. Preferred examples of liquid pumps are lubricating oil pumps for supplying an internal combustion engine of a vehicle or another unit of a vehicle with lubricant or hydraulic fluid. Such a pump is preferably driven by the engine of the vehicle.
Wird die Rotationskolbenpumpe in Abhängigkeit von der Drehzahl eines Antriebsmotors, vorzugsweise Verbrennungsmotors, drehangetrieben, beispielsweise wie bevorzugt über eine mechanische Kopplung, so ist die Gleitpaarung mit der wenigstens einen erfindungsgemäßen Tasche vorzugsweise so gestaltet, dass die Übergangsdrehzahl für den Aufbau des hydrodynamischen Schmierfilm bereits im Leerlaufbetrieb des Antriebsmotors überschritten wird. Die Pumpe kann wie bereits erwähnt in einem Fahrzeug montiert oder für eine Verwendung in einem Fahrzeug vorgesehen sein, und bei dem Antriebsmotor kann es sich insbesondere um den Antriebsmotor des Fahrzeugs handeln.If the rotary piston pump is rotationally driven as a function of the rotational speed of a drive motor, preferably an internal combustion engine, for example as preferably via a mechanical coupling, the sliding pairing with the at least one pocket according to the invention is preferably designed such that the transition rotational speed for the construction of the hydrodynamic lubricating film is already in idling operation of the drive motor is exceeded. As already mentioned, the pump may be mounted in a vehicle or provided for use in a vehicle, and the drive motor may in particular be the drive motor of the vehicle.
In bevorzugten Ausführungen ist eine axial fliegende Lagerung des Rotors verwirklicht. Durch die Erfindung wird zwischen der Gleitpaarung der axial einander zugewandten Gleitflächen ein axialer Gleitlagerspalt gebildet, indem der Rotor bei Überschreiten der Übergangsdrehzahl von der gegenüberliegenden Gleitfläche der Kammer von dem hydrodynamischen Schmierfilm getragen abhebt. Vorteilhafterweise ist die Gleitpaarung an der gegenüberliegenden Stirnseite des Rotors ebenfalls so gebildet, dass sich dort ein hydrodynamischer Schmierfilm bildet, wobei sich die Schmierfilmdicken der beiden Schmierfilme dem axialen Kräftegleichgewicht entsprechend einstellen. Die axial fliegende oder schwimmende Lagerung lässt dieses Einstellen zu. Falls im Betrieb der Pumpe ein Achsschub in eine bestimmte Richtung wie beispielhaft vorstehend geschildert auftritt, ist eine einzige oder bevorzugter sind mehrere erfindungsgemäße Tasche(n) zweckmäßigerweise bei der Gleitpaarung vorgesehen, die den Achsschub aufnehmen muss, deren Gleitflächen also der Achsschub axial gegeneinander zu drücken sucht.In preferred embodiments, an axially flying bearing of the rotor is realized. By the invention, an axial sliding bearing gap is formed between the sliding pair of axially facing sliding surfaces by the rotor when the transition speed of the opposite sliding surface of the chamber of the hydrodynamic lubricating film worn lifts off. Advantageously, the pairing on the opposite end face of the rotor is also formed so that there forms a hydrodynamic lubricating film, wherein the lubricant film thicknesses of the two lubricating films adjust the axial balance of forces accordingly. Axial flying or floating bearing allows for this adjustment. If, during operation of the pump, an axial thrust occurs in a certain direction as exemplarily described above, a single or more preferred pocket (s) according to the invention is expediently provided in the case of the sliding pair which has to absorb the axial thrust whose axial sliding surfaces therefore press against each other axially examined.
Da die erfindungsgemäß geformte(n) Tasche(n) in Tiefenrichtung vorzugsweise ohne Hinterschnitt geformt wird oder werden, kann der Rotor mittels eines Formwerkzeugs mit der oder den Tasche(n) im Wege einer Urformung des Rotors Werkzeug fallend, d.h. ohne zusätzliche Bearbeitung und damit praktisch kostenneutral erzeugt werden. Durch eine dem Prozess der Urformung folgende spanende Bearbeitung, beispielsweise ein Schleifprozess, der Stirnfläche des Rotors wird ohne zusätzlichen Herstellungsaufwand somit eine geeignete, im tribologischen Zusammenspiel mit der bevorzugt planen Kammerwand wirksame Keilspaltgeometrie erzeugt. Gleichzeitig ergeben sich Kostenreduzierungspotentiale, da wegen der erfindungsgemäßen Schmiertasche(n) auf eine zusätzliche Antiverschleißbeschichtung einer der den Gleitlagerspalt bildenden Gleitflächen verzichtet werden kann. Der Rotor kann insbesondere durch Pressen und Sintern als Sinterteil aus Metall oder Kunststoff oder im Spritzguss aus Kunststoff als Spritzgussteil geformt werden.Since the bag (s) formed in accordance with the invention are preferably formed without undercut in the depth direction, the rotor can be reduced by means of a forming tool to the bag (s) by forming the rotor tool, i. be produced without additional processing and thus virtually cost-neutral. By means of a subsequent machining process, for example a grinding process, the end face of the rotor is thus produced without additional manufacturing effort a suitable wedge gap geometry which is effective in tribological interaction with the preferably plane chamber wall. At the same time there are cost reduction potentials, because of the inventive lubricating pocket (s) can be dispensed with an additional anti-wear coating one of the sliding bearing gap forming sliding surfaces. The rotor can be molded in particular by pressing and sintering as a sintered part made of metal or plastic or by injection molding of plastic as an injection molded part.
Vorteilhafte Merkmale werden auch in den Unteransprüchen und deren Kombinationen beschrieben.Advantageous features are also described in the subclaims and their combinations.
Ausführungsbeispiele der Erfindung werden nachfolgend anhand von Figuren erläutert. An den Ausführungsbeispielen offenbar werdende Merkmale bilden je einzeln und in jeder Merkmalskombination die Gegenstände der Ansprüche und auch die vorstehend diskutierten Ausgestaltungen vorteilhaft weiter. Es zeigen:
- Figur 1
- eine erfindungsgemäße Rotationskolbenpumpe in einem Längsschnitt,
Figur 2- die Rotationskolbenpumpe in einer zum Längsschnitt der
Figur 1 orthogonalen Draufsicht und mit einem Rotor, der Schmiertaschen eines ersten Ausführungsbeispiels aufweist, Figur 3- eine Draufsicht auf eine Stirnfläche eines Rotors mit Schmiertaschen eines zweiten Ausführungsbeispiels,
Figur 4- den in Umfangsrichtung um eine Rotationsachse des Rotors erstreckten Schnitt
A-A der Figur 3 , - Figur 5
- ein
Detail der Figur 4 , Figur 6- eine Draufsicht auf eine Stirnfläche eines Rotors mit Schmiertaschen eines dritten Ausführungsbeispiels,
- Figur 7
- den in Umfangsrichtung um eine Rotationsachse des Rotors erstreckten Schnitt
B-B der Figur 6 , - Figur 8
- Schmiertaschen eines vierten Ausführungsbeispiels,
Figur 9- Schmiertaschen eines fünften Ausführungsbeispiels,
Figur 10- Schmiertaschen eines sechsten Ausführungsbeispiels und
- Figur 11
- Schmiertaschen eines siebten Ausführungsbeispiels.
- FIG. 1
- a rotary piston pump according to the invention in a longitudinal section,
- FIG. 2
- the rotary piston pump in a longitudinal section of the
FIG. 1 orthogonal plan view and with a rotor having lubrication pockets of a first embodiment, - FIG. 3
- a plan view of an end face of a rotor with lubrication pockets of a second embodiment,
- FIG. 4
- the circumferentially about an axis of rotation of the rotor extending section AA of the
FIG. 3 . - FIG. 5
- a detail of
FIG. 4 . - FIG. 6
- a plan view of an end face of a rotor with lubricating pockets of a third embodiment,
- FIG. 7
- the circumferentially about an axis of rotation of the rotor extending section BB of
FIG. 6 . - FIG. 8
- Lubrication pockets of a fourth embodiment,
- FIG. 9
- Lubrication pockets of a fifth embodiment,
- FIG. 10
- Lubrication pockets of a sixth embodiment and
- FIG. 11
- Lubrication pockets of a seventh embodiment.
Ein Rotor 10 ist um eine Rotationsachse R in der Kammer 4 drehbar angeordnet. Der Rotor 10 ist außerhalb der Kammer 4 längs eines Rotorlagerabschnitts 11 axial fliegend drehbar gleitgelagert, wofür der Lagerabschnitt 11 und beispielhaft die Gehäusestruktur 2 eine axial relativ zueinander bewegliche Oleitlagerpaarung bilden. Der Rotor 10 weist an dem von der Förderkammer 4 abgewandten Ende einen Anschluss für eine verdrehgesicherte Verbindung unmittelbar mit einer Nockenwelle oder einem Antriebsrad auf, über das er im montierten Zustand vom Verbrennungsmotor her, beispielsweise von der Nockenwelle angetrieben wird.A
Die Pumpe ist als einflügelige Flügelzellenpumpe ausgeführt. Ein Flügel 13 durchsetzt den Rotor 10 in radialer Richtung und wird von dem Rotor 10 in einem Rotorschlitz 12 radial linear hin und her beweglich geführt. Der Rotor 10 und der Flügel 13 unterteilen die Förderkammer 4 in zwei Förderzellen, von denen die eine mit dem Einlass 5 und die andere mit dem Auslass 6 verbunden ist. Der Rotor 10 ist in der Kammer 4 exzentrisch angeordnet, so dass er mit seiner äußeren Umfangsfläche die beiden Förderzellen und insbesondere den Einlass 5 und den Auslass 6 fluidisch voneinander trennt. In
Für die axiale Abdichtung der Förderzellen weist der Rotor 10 an einer von der Antriebsseite abgewandten Stirnseite eine Gleitfläche 15 und an der anderen, der Antriebsseite zugewandten Stirnseite eine Gleitfläche 17 auf. Die Gleitflächen 15 und 17 bilden mit axial gegenüberliegenden Gleitflächen 16 und 18 des Gehäuses 1 jeweils eine Gleitpaarung. Die stirnseitigen Gleitflächen des Flügels 13 sind nicht mit eigenen Bezugszeichen versehen, bilden aber mit den axial zugewandten Kammerwänden jeweils eine weitere Gleitpaarung. Die gehäuseseitige Gleitfläche 16 an der von der Antriebsseite abgewandten Stirnseite des Rotors 10 wird von dem Deckel 3 gebildet, während die Gehäusestruktur 2 die Gegengleitfläche 18 für die Rotorgleitfläche 17 bildet. Um Reibverschleiß der Gleitpaarungen zu mindern und die Abdichtung der Förderzellen zu verbessern, wird den Gleitpaarungen ein Schmieröl oder anderes geeignetes Schmiermittel zugeführt.For the axial sealing of the delivery cells, the
Das Schmiermittel kann insbesondere wie im Ausführungsbeispiel in einen den Rotor 10 axial durchsetzenden zentralen Hohlraum geleitet werden und sich von dort aus über die von den Gleitflächen 15 und 16 einerseits und den Gleitflächen 17 und 18 andererseits axial begrenzten Dichtspalte verteilen. So kann ein Schmiermittelkanal insbesondere durch den Lagerabschnitt 11 führen. An der dem Lagerabschnitt 11 zugewandten Stirnseite kann im Rotor 10 beispielsweise in Umfangsrichtung erstreckte Verteilernut vorgesehen sein, in die der Schmiermittelkanal mündet. Das Schmiermittel gelangt unterstützt von der bei drehendem Rotor 10 wirkenden Zentrifugalkraft durch den axialen Gleitspalt der Gleitpaarung der Gleitflächen 17 und 18 in die Kammer 4 und sorgt dabei für eine ausreichende Schmierung der Gleitpaarung 17 und 18. Das Schmiermittel gelangt des Weiteren durch den zentralen Hohlraum des Rotors 10 an dessen andere Stirnseite und verteilt sich dort ebenfalls unterstützt durch die Zentrifugalkraft nach radial außen und sorgt für die Schmierung der von den Gleitflächen 15 und 16 gebildeten Gleitpaarung sowie ferner der mit dem Flügel 13 gebildeten Gleitpaarungen.In particular, as in the exemplary embodiment, the lubricant can be conducted into a central cavity passing axially through the
Der Rotor 10 ist in der von seiner Antriebsseite abgewandten Gleitfläche 15 mit Taschen 20 versehen, in denen sich das Schmiermittel sammelt. Die Taschen 20 können auch als Schmiertaschen bezeichnet werden. In der Gleitfläche 15 sind insgesamt vier Taschen 20 geformt, jeweils zwei Taschen 20 zu beiden Seiten des Flügels 13. Der Flügel 13 unterteilt die Gleitfläche 15 in zwei Gleitflächenhemissphären, die beispielhaft wie bevorzugt gleich und ferner wie ebenfalls bevorzugt als Kreisringsegmente geformt sind. Die Taschen 20 sind in den beiden Hemissphären im Sinne einer über den Umfang gleichmäßigen Verteilung des Schmiermittels gleichmäßig verteilt angeordnet. Die Gleitfläche 15 separiert die Taschen 20 in Umfangsrichtung voneinander und begrenzt sie nach radial außen, bildet also von den beiden Schlitzen 12 abgesehen radial außen eine umlaufende Gleitpaarung mit der axial gegenüberliegenden Gleitfläche 16. Die Taschen 20 sind jedoch radial einwärts in Richtung auf die Rotationsachse R offen, münden also an einer inneren Umfangsfläche des Rotors 10. Das Schmiermittel gelangt aus dem zentralen Hohlraum des Rotors 10 in die in den Hohlraum mündenden Taschen 20, sammelt sich darin und wird im Betrieb der Pumpe von der Fliehkraft unterstützt nach radial außen gedrängt, um die Gleitpaarung der Gleitflächen 15 und 16 zu schmieren und gleichzeitig auch den zwischen den Gleitflächen 15 und 16 gebildeten axialen Gleitspalt abzudichten und so zur fluidischen Trennung der Förderzellen beizutragen. Falls die Gleitpaarung der Gleitflächen 17 und 18 ebenfalls Taschen, vorzugsweise erfindungsgemäße Taschen, aufweist, können diese radial innen in die genannte Verteilernut münden und über diese mit dem Schmiermittel versorgt werden.The
Die Taschen 20 gehen jeweils an ihrem in Drehrichtung V vorlaufenden Ende 23 entlang eines in der Draufsicht auf die Gleitfläche 15 gebogenen Taschenöffnungsrands in die Gleitfläche 15 über, während sie an ihrem nachlaufenden Ende 24 jeweils längs eines geraden radialen Öffnungsrands in die Gleitfläche 15 übergehen. Der vorlaufende Rand fällt von einer an den Rand gelegten Tangente mit überall kontinuierlicher Krümmung gegen die Drehrichtung V in Richtung auf das nachlaufende Ende 24 ab. Dies vergleichmäßigt den Fluss des Schmiermittels in die jeweilige Tasche 20, wirkt einer Rezirkulation und der Bildung von Schmutzecken entgegen. Die in Umfangsrichtung gemessene Länge L verringert sich im Ergebnis bei jeder der Taschen 20 in radialer Richtung von innen nach außen kontinuierlich.The
Insbesondere sind die Taschen 20 jeweils so geformt, dass sich im Betrieb der Pumpe zwischen den Gleitflächen 15 und 16 ein hydrodynamischer Schmierfilm aufbaut, sobald die hierfür erforderliche Übergangsdrehzahl überschritten wird. Die Taschen 20 sind so geformt und angeordnet, dass die Übergangsdrehzahl in den für Verschleiß maßgeblichen Betriebszuständen der Pumpe überschritten wird. Ist die Pumpe für einen Antrieb durch einen Verbrennungsmotor eines Fahrzeugs vorgesehen oder im Fahrzeug so montiert, ist die Gestaltung vorzugsweise so, dass die Übergangsdrehzahl unter der Drehzahl liegt, die der Rotor 10 im Leerlauf des Motors erreicht. Die Taschen 20 flachen jeweils in Richtung auf ihr nachlaufendes Ende 24 kontinuierlich ab, so dass sie mit der axial gegenüberliegenden Gleitfläche 16 einen sich zum nachlaufenden Ende 24 verjüngenden Keilspalt bilden. Das Schmiermittel wird aufgrund der bei Drehung des Rotors 10 im Schmiermittel wirkenden Schubkräfte am nachlaufenden Ende 24 jeder der Taschen 20 zwischen die Gleitflächen 15 und 16 gefördert und bildet dort bei Überschreiten der Übergangsdrehzahl einen tragenden Schmierfilm, der die Gleitflächen 15 und 16 voneinander separiert und im axialen Gleitspalt für reine Flüssigkeitsreibung sorgt. Durch die erfindungsgemäße Gestaltung der Gleitpaarung 15 und 16 mit den Taschen 20 wird in Kombination mit der axial fliegenden bzw. schwimmenden Gleitlagerung des Rotors 10 ein den Rotor 10 axial tragendes Axialgleitlager geschaffen. Die Gleitpaarung 15 und 16 mit den Taschen 20 ist vorzugsweise ferner so gestaltet, dass dieses Axialgleitlager auch dann voll trägt und bei Überschreiten der Übergangsdrehzahl nur im Bereich der Flüssigkeitsreibung arbeitet, wenn es eine von der Antriebsseite bei 11 herrührende axiale Kraft, einen Achsschub, aufnehmen muss, wie dies insbesondere in bevorzugten Einbausituationen der Fall ist, in denen die Vakuumpumpe am Gehäuse oder in einer Modifikation im Gehäuse eines Verbrennungsmotors eines Kraftfahrzeugs angeordnet ist.In particular, the
In
Eine Modifikation zum ersten Ausführungsbeispiel besteht somit darin, dass die Taschen 21 am vorlaufenden Ende einen anderen Verlauf aufweisen, indem sie dort gerade sind und nicht, wie bevorzugt, gegen die Drehrichtung V kontinuierlich abfallen. Ferner ist in der Gleitfläche 15 eine größere Anzahl der Taschen 21 als im ersten Ausführungsbeispiel geformt. Wie im ersten Ausführungsbeispiel sind die Taschen 21 beidseits einer durch den Schlitz 12 verlaufenden, gedachten Teilungsebene symmetrisch und in den beiden Hemisphären der Gleitfläche 15 jeweils in Umfangsrichtung gleichmäßig verteilt angeordnet.A modification to the first embodiment is thus that the
Aufgrund des Hinterschnitts wird, wie bereits erwähnt, im Bereich des dadurch erhaltenen Fortsatzes 25 radial innen ein Steg erhalten, der vorzugsweise einen Teil der Gleitfläche 15 bildet. Insbesondere durch solch einen verbleibenden Gleitflächensteg wird einem Abströmen des Schmiermittels in den zentralen Hohlraum des Rotors 10 entgegengewirkt. Obgleich bevorzugt im Bereich des genannten Stegs die Gleitfläche 15 verbleibt, wird diese vorteilhafte Wirkung zwar in abgeschwächter Form, aber grundsätzlich auch dann erreicht, wenn der durch den Hinterschnitt erhaltene Steg axial nicht bis ganz zur Gleitfläche 15 reicht, aber immer noch nach radial einwärts einen verengten Strömungsquerschnitt darstellt, der das Abströmen in den zentralen Hohlraum am nachlaufenden Ende 24 drosselt. Der Hinterschnitt kann bevorzugt, wie in
Die Taschen 22 sind in der Radialebene gesehen am vorlaufenden Ende 23 jeweils kontinuierlich gekrümmt und fallen wie im ersten Ausführungsbeispiel in Richtung auf das nachlaufende Ende 24 von einer an den Öffnungsrand des vorderen Endes 23 gelegten Tangente ab. Wie im ersten Ausführungsbeispiel werden hierdurch am vorlaufenden Ende die Ausbildung von Schmutzecken und Rezirkulationen verhindert. Zum Hinterschnitt ist noch nachzutragen, dass im Bereich des in Umfangsrichtung verlängerten Fortsatzes 25 eine größere Taschenlänge L als im radial inneren und schmaleren Taschenbereich zur Verfügung steht, um den Keilspalt zu bilden. Die Taschen 22 können dementsprechend im Bereich des jeweiligen Fortsatzes 25 mit einer geringeren Neigung α in Richtung auf das nachlaufende Ende 24 ansteigen, da der Anstieg über eine größere Länge verteilt werden kann.The
Die
In dem in
Die Taschen 20, 21 und 22 des ersten, zweiten und dritten Ausführungsbeispiels können wahlweise jedes der unterschiedlichen Tiefenprofile aufweisen, d. h. jedes der Tiefenprofile kann mit jeder der auf die radiale Richtung und die Umfangsrichtung bezogenen Taschenkontur kombiniert werden. Ferner können Keilspalte am vorlaufenden Ende 23 und am nachlaufenden Ende 24, wie sie beispielhaft in
- 11
- Gehäusecasing
- 22
- Gehäusestrukturhousing structure
- 33
- Deckelcover
- 44
- Kammerchamber
- 55
- Einlassinlet
- 66
- Auslassoutlet
- 77
- Auslassoutlet
- 88th
- VentilValve
- 99
- VentilValve
- 1010
- Rotorrotor
- 1111
- Lagerabschnittbearing section
- 1212
- Schlitzslot
- 1313
- Flügelwing
- 1414
- Umfangsflächeperipheral surface
- 1515
- Gleitfläche RotorSliding surface rotor
- 1616
- Gleitfläche DeckelSliding surface cover
- 1717
- Gleitfläche RotorSliding surface rotor
- 1818
- Gleitfläche GehäusestrukturSliding surface housing structure
- 1919
- --
- 2020
- Taschebag
- 2121
- Taschebag
- 2222
- Taschebag
- 2323
- vorlaufendes Endeleading end
- 2424
- nachlaufendes Endetrailing end
- 2525
- Fortsatzextension
- 2626
- Taschebag
- 2727
- Taschebag
- 2828
- Taschebag
- 2929
- Taschebag
- αα
- NeigungTilt
- ββ
- NeigungTilt
- BB
- Breitewidth
- DD
- Tiefedepth
- LL
- Längelength
- RR
- Rotationsachseaxis of rotation
- VV
- Drehrichtungdirection of rotation
Claims (19)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE200810036273 DE102008036273B4 (en) | 2008-08-04 | 2008-08-04 | Rotary piston pump with pockets for lubricant |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2151542A2 true EP2151542A2 (en) | 2010-02-10 |
EP2151542A3 EP2151542A3 (en) | 2011-12-14 |
EP2151542B1 EP2151542B1 (en) | 2015-07-08 |
Family
ID=41382083
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09166834.3A Not-in-force EP2151542B1 (en) | 2008-08-04 | 2009-07-30 | Rotating piston pump with pockets for lubricant |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP2151542B1 (en) |
DE (1) | DE102008036273B4 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011131598A3 (en) * | 2010-04-22 | 2013-01-31 | Robert Bosch Gmbh | Vane cell pump |
WO2017163770A1 (en) * | 2016-03-24 | 2017-09-28 | 大豊工業株式会社 | Vane pump |
WO2018068806A1 (en) * | 2016-10-10 | 2018-04-19 | Wabco Europe Bvba | Rotary vacuum pump with a rotor end groove |
Families Citing this family (6)
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DE102011018394A1 (en) | 2011-04-21 | 2012-10-25 | Daimler Ag | Displacement pump e.g. oil pump, for supplying oil to lubricate internal combustion engine of motor car, has rotor comprising recess inserted into chamber wall and retaining part of operating medium in chamber in standstill state of pump |
DE102014102643A1 (en) | 2014-02-27 | 2015-08-27 | Schwäbische Hüttenwerke Automotive GmbH | Rotary pump with plastic composite structure |
DE202014106121U1 (en) | 2014-12-17 | 2015-01-15 | Schwäbische Hüttenwerke Automotive GmbH | Rotary pump with compact positioning structure for adjusting the delivery volume |
DE102017101142A1 (en) | 2017-01-20 | 2018-07-26 | Otto Altmann | Heat exchanger or heat exchanger assembly for a cooling device and a cooling device with such a heat exchanger |
DE102017128787A1 (en) | 2017-12-04 | 2019-06-06 | Schwäbische Hüttenwerke Automotive GmbH | rotary pump |
DE102022113977A1 (en) | 2022-06-02 | 2023-12-07 | Zf Cv Systems Europe Bv | Pneumatic valve and compressor |
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DE3301098A1 (en) | 1983-01-14 | 1984-07-19 | Knorr-Bremse GmbH, 8000 München | ROTATIONAL COMPRESSOR |
DE3325261A1 (en) | 1983-07-13 | 1985-01-24 | Robert Bosch Gmbh, 7000 Stuttgart | Vacuum pump |
JPH1068393A (en) | 1996-08-28 | 1998-03-10 | Mikuni Corp | Vacuum pump |
JP2000337267A (en) | 1999-05-24 | 2000-12-05 | Showa Corp | Variable displacement vane pump |
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GB2012874A (en) * | 1977-12-07 | 1979-08-01 | Seiko Instr & Electronics | Rotary Positive-displacement Fluid-machines |
JPS56106088A (en) * | 1980-01-29 | 1981-08-24 | Matsushita Electric Ind Co Ltd | Rotary type fluid equipment |
DE3014519A1 (en) * | 1980-04-16 | 1981-10-22 | Skf Kugellagerfabriken Gmbh, 8720 Schweinfurt | TURNING PISTON, IN PARTICULAR CELL PUMP |
JPH04279792A (en) * | 1991-03-08 | 1992-10-05 | Toshiba Corp | Fluid compressor |
-
2008
- 2008-08-04 DE DE200810036273 patent/DE102008036273B4/en not_active Expired - Fee Related
-
2009
- 2009-07-30 EP EP09166834.3A patent/EP2151542B1/en not_active Not-in-force
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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DE3301098A1 (en) | 1983-01-14 | 1984-07-19 | Knorr-Bremse GmbH, 8000 München | ROTATIONAL COMPRESSOR |
DE3325261A1 (en) | 1983-07-13 | 1985-01-24 | Robert Bosch Gmbh, 7000 Stuttgart | Vacuum pump |
JPH1068393A (en) | 1996-08-28 | 1998-03-10 | Mikuni Corp | Vacuum pump |
JP2000337267A (en) | 1999-05-24 | 2000-12-05 | Showa Corp | Variable displacement vane pump |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2011131598A3 (en) * | 2010-04-22 | 2013-01-31 | Robert Bosch Gmbh | Vane cell pump |
CN103038452A (en) * | 2010-04-22 | 2013-04-10 | 罗伯特·博世有限公司 | Vane cell pump |
WO2017163770A1 (en) * | 2016-03-24 | 2017-09-28 | 大豊工業株式会社 | Vane pump |
JP2017172472A (en) * | 2016-03-24 | 2017-09-28 | 大豊工業株式会社 | Vane pump |
CN109072915A (en) * | 2016-03-24 | 2018-12-21 | 大丰工业株式会社 | Impeller pump |
US20190101117A1 (en) * | 2016-03-24 | 2019-04-04 | Taiho Kogyo Co., Ltd. | Vane pump |
CN109072915B (en) * | 2016-03-24 | 2020-07-07 | 大丰工业株式会社 | Vane pump |
US11035363B2 (en) | 2016-03-24 | 2021-06-15 | Taiho Kogyo Co., Ltd. | Vane pump |
WO2018068806A1 (en) * | 2016-10-10 | 2018-04-19 | Wabco Europe Bvba | Rotary vacuum pump with a rotor end groove |
CN109563740A (en) * | 2016-10-10 | 2019-04-02 | 威伯科欧洲有限责任公司 | Rotary vacuum pump with rotor-end groove |
CN109563740B (en) * | 2016-10-10 | 2021-07-27 | 威伯科欧洲有限责任公司 | Rotary vacuum pump with rotor end grooves |
US11168691B2 (en) | 2016-10-10 | 2021-11-09 | Zf Cv Systems Europe Bv | Rotary vacuum pump with a rotor end groove |
Also Published As
Publication number | Publication date |
---|---|
EP2151542A3 (en) | 2011-12-14 |
DE102008036273B4 (en) | 2013-09-26 |
EP2151542B1 (en) | 2015-07-08 |
DE102008036273A1 (en) | 2010-02-11 |
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