EP3507495B1 - Screw-type vacuum pump - Google Patents

Screw-type vacuum pump Download PDF

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Publication number
EP3507495B1
EP3507495B1 EP17751761.2A EP17751761A EP3507495B1 EP 3507495 B1 EP3507495 B1 EP 3507495B1 EP 17751761 A EP17751761 A EP 17751761A EP 3507495 B1 EP3507495 B1 EP 3507495B1
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EP
European Patent Office
Prior art keywords
screw
pressure
vacuum pump
type vacuum
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP17751761.2A
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German (de)
French (fr)
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EP3507495A1 (en
Inventor
Thomas Dreifert
Dirk Schiller
Wolfgang Giebmanns
Roland Müller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Leybold GmbH
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Leybold GmbH
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Publication of EP3507495A1 publication Critical patent/EP3507495A1/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/082Details specially related to intermeshing engagement type pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C25/00Adaptations of pumps for special use of pumps for elastic fluids
    • F04C25/02Adaptations of pumps for special use of pumps for elastic fluids for producing high vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/082Details specially related to intermeshing engagement type pumps
    • F04C18/084Toothed wheels
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/08Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F04C18/12Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
    • F04C18/14Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
    • F04C18/16Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/04Heating; Cooling; Heat insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2220/00Application
    • F04C2220/10Vacuum
    • F04C2220/12Dry running
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C2240/00Components
    • F04C2240/20Rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/02Light metals
    • F05C2201/021Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/90Alloys not otherwise provided for
    • F05C2201/903Aluminium alloy, e.g. AlCuMgPb F34,37

Definitions

  • the invention relates to a screw vacuum pump.
  • Screw vacuum pumps have a pumping chamber in a housing, in which two screw rotors are arranged. Each screw rotor has at least one displacement element with a helical recess. As a result, a large number of turns are formed.
  • known screw vacuum pumps In order to be able to achieve low pressures or a high vacuum of in particular less than 200 mbar (absolute pressure) with a low specific power consumption with the aid of screw vacuum pumps, known screw vacuum pumps have a high internal compression. The internal compression defines the reduction of the delivery volume from the inlet to the outlet of the pump. Low outlet pressures are achieved, in particular, in that a gap with a small height is formed between an outside of the at least one displacement element and an inside of the scooping chamber.
  • EP 1 242 743 known to provide internal rotor cooling. With the help of the rotor internal cooling, an effective cooling of the rotor and thus of the at least one displacement element connected to the rotor or integrally formed therewith is ensured, so that small gap heights can be realized. Such an internal rotor cooling is structurally very complex and therefore expensive.
  • the object of the invention is to provide a screw vacuum pump with which a high vacuum of in particular less than 200 mbar and particularly preferably less than 10 mbar can be achieved, it being possible to dispense with internal rotor cooling.
  • the screw vacuum pump according to the invention has a housing which forms a scooping space in which the two screw rotors are arranged.
  • the housing and the rotors are made of aluminum or an aluminum alloy. Particularly preferred is the aluminum alloy for the housing AISi7Mg or AlMg0.75Si.
  • the coefficient of expansion of the material of the screw rotors is less than the coefficient of expansion of the material of the housing. It is particularly preferred that the expansion coefficient of the screw rotors is less than 22 * 10 -6 1 / K, particularly preferably less than 20 * 10 -6 1 / K.
  • the two screw rotors arranged in the scoop have at least one displacement element which has a helical recess.
  • the helical recesses form several turns.
  • this is at least one displacement element made of aluminum or an aluminum alloy. It is preferred to produce at least one displacement element made of AISi9Mg or AlSi17Cu4Mg. It is particularly preferred that the aluminum or the aluminum alloy has a low expansion coefficient of in particular less than 22 * 10 -6 1 / K, in particular less than 20 * 10 -6 1 / K.
  • the screw rotors and in particular the at least one displacement element per screw rotor have a lower expansion coefficient than the housing. It is particularly preferred here that the expansion coefficient of the housing is at least 5%, particularly preferably at least 10% larger than that of the screw rotors or of the at least one displacement element. It is particularly preferred that the alloy of the rotor has a high silicon content of preferably at least 9%, particularly preferably of more than 15%, in order to realize a low coefficient of thermal expansion.
  • the screw rotors and the at least one displacement element provided are designed such that at least 6, in particular at least 8 and particularly preferably at least 10 windings are provided between an area in which 5% to 20% of the outlet pressure prevails and the pressure-side rotor end.
  • the rotor end on the pressure side is the area of the pump outlet.
  • the high number of turns in this area according to the invention can be provided in a preferred embodiment in the case of a single pressure-side displacement element provided per rotor. However, it is also possible to provide a corresponding number of turns in this area on the pressure side, for example on two displacement elements.
  • the large number of turns means that a large surface is available for heat exchange with the housing.
  • the at least 6, in particular at least 8 and particularly preferably at least 10 windings are provided in a pressure-side displacement element.
  • the pressure ratio caused by the pressure-side displacement element is less than 20, in particular less than 10, and particularly preferably less than 5.
  • the last 6, in particular last 8 and particularly preferably last 10 windings in accordance with the invention result in a compression of 50 mbar to 1,000 mbar at a pressure ratio of 20.
  • a compression of 100 mbar occurs at a pressure ratio of 10 1,000 mbar and at a pressure ratio of 5 a compression from 200 mbar to 1,000 mbar.
  • the distance between an area in which 5% - 20% of the outlet pressure prevails, up to the last turn in the conveying direction, i.e. essentially up to the pump outlet is preferably at least 20% to 30% of the rotor length. This in turn has the advantage that in a relatively large area there is only a relatively low compression. This in turn causes a relatively small increase in temperature due to the low compression.
  • the pressure-side displacement element has at least 6, in particular at least 8 and particularly preferably at least 10 turns has an average working pressure of more than 50 mbar.
  • end pressure ie when the inlet is closed
  • a (time-averaged) pressure of 50 mbar is reached at this point of the pump.
  • a cold gap between the surface of the at least one displacement element and the inside of the scooping space in particular in the pressure-side area a height of 0.05 mm - 0.3 mm and in particular 0.1 mm - 0.2 mm.
  • Such a relatively large gap height can be provided on the basis of the configuration according to the invention described above, in particular 6, preferably 8 and particularly preferably 10 last windings.
  • Each displacement element has at least one helical recess which has the same contour over its entire length.
  • the contours are preferably different for each displacement element.
  • the individual displacement element thus has a constant contour and preferably a constant slope. This considerably simplifies the production, so that the production costs can be greatly reduced.
  • the contour of the displacement element on the suction side is preferably asymmetrical. Due to the asymmetrical design of the contour or profile, the flanks can be designed in such a way that the leakage areas, the so-called blowholes, in particular completely disappear or at least have a small cross section.
  • a particularly suitable asymmetrical profile is the so-called "Quimby profile”. Such a profile is relatively difficult to manufacture, has the advantage, however, that there is no continuous blow hole. A short circuit only exists between two neighboring chambers. Since it is an asymmetrical profile with different profile flanks, at least two work steps are required for the production, since the two flanks have to be produced in different work steps due to their asymmetry.
  • the pressure-side displacement element in particular the last displacement element in the pumping direction, is preferably provided with a symmetrical contour.
  • the symmetrical contour has the particular advantage that production is easier.
  • both flanks with a symmetrical contour can be produced in one work step by a rotating end mill or by a rotating side milling cutter.
  • Such symmetrical profiles have blowholes, they are continuous, i.e. not only provided between two adjacent chambers. The size of the blow hole decreases as the slope decreases.
  • such symmetrical profiles can be provided in particular in the case of the pressure-side displacement element, since in a preferred embodiment this has a smaller slope than the suction-side displacement element and preferably also as the displacement element arranged between the suction-side and the pressure-side displacement element.
  • the tightness of such symmetrical profiles is somewhat lower, they have the advantage that the manufacture is significantly easier.
  • a particularly suitable symmetrical profile is the so-called "cycloid profile".
  • the provision of at least two such displacement elements means that the corresponding screw vacuum pump can generate low inlet pressures with low power consumption.
  • the thermal load is also low.
  • the arrangement of at least two displacement elements designed according to the invention with constant pitch and constant Contour in a vacuum pump leads to essentially the same results as with a vacuum pump with a displacement element with changing pitch. With high built-in volume ratios, three or four displacement elements can be provided for each rotor.
  • a pressure-side, that is to say in particular the last, displacement element has a large number of turns. Due to the large number of turns, a larger gap between the screw rotor and the housing can be accepted while maintaining the same performance.
  • the gap can have a cold gap width of 0.05-0.3 mm.
  • a large number of outlet windings or number of windings in the pressure-side displacement element can be produced inexpensively, since, according to the invention, this displacement element has a constant pitch and preferably also a symmetrical contour. This enables simple and inexpensive production, so that the provision of a larger number of turns is acceptable.
  • This pressure-side or last displacement element preferably has more than 6, in particular more than 8 and particularly preferably more than 10 turns.
  • the use of symmetrical profiles has the advantage that both flanks of the profile can be cut simultaneously with one milling cutter.
  • the milling cutter is additionally supported by the opposite flank, so that deformation or bending of the milling cutter during the milling process and inaccuracies caused thereby are avoided.
  • the displacement elements and the rotor shaft are formed in one piece.
  • the change in pitch between adjacent displacement elements is discontinuous or erratic.
  • the two displacement elements are in the longitudinal direction arranged at a distance from each other so that a circumferential cylindrical ring-shaped chamber is formed between two displacement elements, which serves as a tool outlet. This is particularly advantageous in the case of rotors formed in one piece, since the tool producing the helical line can be led out in a simple manner in this area. If the displacement elements are manufactured independently of one another and then mounted on a shaft, the provision of a tool outlet, in particular of such a ring-cylindrical region, is not necessary.
  • no tool outlet is provided between two adjacent displacement elements on the change of pitch.
  • both flanks have a defect or recess in order to be able to lead the tool out.
  • Such a flaw has no significant influence on the compression performance of the pump, since it is a flaw or recess that is very local.
  • the vacuum pump screw rotor according to the invention has, in particular, a plurality of displacement elements. These can each have the same or different diameters. It is preferred here that the pressure-side displacement element has a smaller diameter than the suction-side displacement element.
  • displacement elements produced independently of the rotor shaft, these are mounted on the shaft by press fits, for example.
  • elements such as dowel pins for fixing the angular position of the displacement elements to one another.
  • the screw rotor In particular in the one-piece configuration of the screw rotor, but also in the case of a multi-piece configuration, it is preferred to produce it from aluminum or from an aluminum alloy. Particularly preferred is to manufacture the rotor from aluminum or an aluminum alloy, in particular AlSi9Mg or AlMg0.7Si.
  • the alloy preferably has a high silicon content of preferably more than 9%, in particular more than 15%, in order to reduce the coefficient of expansion.
  • the aluminum used for the rotors has a low coefficient of expansion. It is preferred if the material has an expansion coefficient of less than 22 * 10 -6 1 / K, in particular less than 20 * 10 -6 1 / K.
  • the surface of the displacement elements is coated, a coating against wear and / or corrosion being provided in particular. It is preferred to provide an anodic or other suitable coating depending on the area of application.
  • the screw rotor is made in one piece, in particular from aluminum or an aluminum alloy.
  • the screw rotor can also have a rotor shaft which carries the at least one displacement element. This has the advantage, in particular when providing a plurality of displacement elements, that these can be produced independently of one another and are subsequently connected to the rotor shaft in particular by being pressed on or shrunk on. It is possible to provide feather keys or the like to define the angular position of the individual displacement elements.
  • the rotor shaft can be made of steel and carry the at least one displacement element made of aluminum or an aluminum alloy.
  • the screw rotors have no internal rotor cooling.
  • the screw rotors have no channels through which liquid coolant flows.
  • the screw rotors can have bores or channels, for example for reducing weight, for balancing or the like. It is particularly preferred that the screw rotors are solid.
  • the pressure-side displacement elements i.e. in particular in the area of the last 6, preferably last 8 and particularly preferably last 10 windings, there is a small temperature difference between the displacement elements and the housing.
  • this temperature difference is preferably less than 50 K and in particular less than 20 K. Normal operation means the entire intake pressure range from the final pressure to an open inlet (atmospheric intake).
  • the housing in the area of the pressure-side displacement elements ie in particular in the area of the last 6, in particular last 8 and particularly preferably last 10 turns, has an average heat flow density which is less than 20,000 W / m 2 , preferably less than 15,000 W / m 2 and in particular less than 10,000 W / m 2 .
  • the average heat flow density is the ratio of the compression performance to the wall area of the outlet area.
  • the in the 1 and 2 Screw rotors shown can in a screw vacuum pump according to the invention, as in Fig. 5 shown, used.
  • the rotor has two displacement elements 10, 12.
  • a first displacement-side displacement element 10 has a large pitch of approximately 50-150 mm / revolution. The slope is constant over the entire displacement element 10. The contour of the helical recess is also constant.
  • the second pressure-side displacement element 12 again has a constant slope and a constant contour of the recess over its length. The slope of the pressure-side displacement element 12 is preferably in the range of 10-30 mm / revolution.
  • An annular cylindrical recess 14 is provided between the two displacement elements. This serves to ensure that due to the one-piece design of the in Fig. 1 shown screw rotor a tool outlet is realized.
  • the one-piece screw rotor has two bearing seats 16 and one shaft end 18.
  • a gearwheel for driving is connected to the shaft end 18, for example.
  • the two displacement elements 10, 12 manufactured separately and then fixed on a rotor shaft 20, for example by pressing.
  • the cylindrical distance 14 between two adjacent displacement elements 10, 12 is not required as a tool outlet.
  • the bearing seats 16 and the shaft ends 18 can be an integral part of the shaft 20.
  • the continuous shaft 20 can also be made of another material that differs from the displacement elements 10, 12.
  • Fig. 3 shows a schematic sectional view of an asymmetrical profile (eg a Quimby profile).
  • the asymmetrical profile shown is a so-called "Quimby profile”.
  • the sectional view shows two screw rotors which mesh with one another and whose longitudinal direction is perpendicular to the plane of the drawing. The opposite rotation of the rotors is indicated by the two arrows 15.
  • the profiles of the flanks 19 and 21 are designed differently for each rotor.
  • the mutually opposite flanks 19, 21 must therefore be produced independently of one another.
  • the production which is therefore somewhat more complex and difficult, has the advantage, however, that there is no continuous blow hole, but only a short circuit between two adjacent chambers.
  • Such an asymmetrical profile is preferably provided in the suction-side displacement element 10.
  • FIG. 4 The schematic sectional view in Fig. 4 again shows a cross section of two displacement elements or two screw rotors, which in turn rotate in opposite directions (arrows 15). Relative to the axis of symmetry 17, the flanks 23 are formed symmetrically for each displacement element.
  • the illustrated preferred embodiment of a symmetrically designed contour is a cycloid profile.
  • a symmetrical profile, as in Fig. 4 is preferably provided in the pressure-side displacement elements 12.
  • displacement elements are provided. If necessary, these can also have different head diameters and corresponding foot diameters. It is preferred here that a displacement element with a larger head diameter at the inlet, i.e. is arranged on the suction side in order to achieve a greater pumping speed in this area and / or to increase the built-in volume ratio. Combinations of the above-described embodiments are also possible. For example, one or more displacement elements can be produced in one piece with the shaft or an additional displacement element can be produced independently of the shaft and then mounted on the shaft.
  • FIG. 5 Shown schematic view of a preferred embodiment of a screw vacuum pump according to the invention are two screw rotors, as in Fig. 1 shown, arranged in a housing 26.
  • the vacuum pump housing 26 has an inlet 28 through which gas is drawn in in the direction of an arrow 30.
  • the inlet 28 is connected, for example, to a chamber to be evacuated.
  • the pump housing 26 has an outlet 32 on the pressure side, through which the gas is expelled in the direction of an arrow 38.
  • the screw vacuum pump according to the invention preferably pumps directly against the atmosphere, so that no forevacuum pump is connected to the outlet 32, although this is also possible.
  • the two pressure-side displacement elements 12 have 10 turns per screw rotor.
  • there is an area 40 i.e. in a region of the first turn of the pressure-side displacement element 12 in the conveying direction, a pressure of 5% - 20% of the pressure prevailing at the outlet 32.
  • a gap is formed between the surfaces 42 of the two pressure-side displacement elements 12 and an inner surface 44 of a scooping space 46 formed by the pump housing 26, the height of which is preferably in the range from 0.05 mm to 0.3 mm and in particular in the range from 0.1 mm - 0.2 mm.
  • the vacuum pump housing 26 is closed in the illustrated embodiment with two housing covers 47.
  • the in Fig. 4 left housing cover 47 has two bearing receptacles, in each of which a ball bearing 48 is arranged for mounting the two rotor shafts.
  • a ball bearing 48 is arranged for mounting the two rotor shafts.
  • the pins 50 of the two screw rotor shafts protrude through the covers 47.
  • a gear wheel 52 is arranged on each of the two shaft journals 50.
  • the two gear wheels 52 mesh with one another in order to synchronize the two screw rotors with one another.
  • two bearings 48 arranged for storing the screw rotors.
  • Housing material AlSi7Mg (cast, expansion coefficient 22 ⁇ 10 -6 K -1 or AlMg0.7Si (extrusion, expansion coefficient 23 ⁇ 10 -6 K -1 )
  • Material rotor AlSi9Mg (cast iron, coefficient of expansion 21 ⁇ 10 -6 K -1 ) or AlSi17Cu4Mg (cast iron, coefficient of expansion 18 ⁇ 10 -6 K -1 )
  • Silicon content rotor at least 9%, particularly preferably more than 15%
  • Coefficient of thermal expansion Housing / rotor at least 5% larger, particularly preferably 10% larger
  • Intermediate pressure between the suction-side and the pressure-side displacement element :

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Rotary Pumps (AREA)

Description

Die Erfindung betrifft eine Schraubenvakuumpumpe.The invention relates to a screw vacuum pump.

Schraubenvakuumpumpen weisen in einem Gehäuse einen Schöpfraum auf, in dem zwei Schraubenrotoren angeordnet sind. Jeder Schraubenrotor weist mindestens ein Verdrängungselement mit schraubenlinienförmiger Ausnehmung auf. Hierdurch ist eine Vielzahl von Windungen ausgebildet. Um mit Hilfe von Schraubenvakuumpumpen niedrige Drücke bzw. ein hohes Vakuum von insbesondere weniger als 200 mbar (Absolutdruck) bei niedriger spezifischer Leistungsaufnahme erzielen zu können, weisen bekannte Schraubenvakuumpumpen eine hohe innere Verdichtung auf. Die innere Verdichtung definiert die Reduktion des Fördervorlumens vom Einlass zum Auslass der Pumpe. Niedrige Ausgangsdrücke werden insbesondere dadurch erzielt, dass zwischen einer Außenseite des mindestens einen Verdrängungselements und einer Innenseite des Schöpfraums ein Spalt mit geringer Höhe ausgebildet ist. Um derartige geringe Spalte realisieren zu können, muss eine zuverlässige Kühlung der Schraubenrotoren gewährleistet sein. Nur hierdurch kann verhindert werden, dass insbesondere im druckseitigen Bereich der Schraubenvakuumpumpe, in dem hohe Druckdifferenzen auftreten, die Temperatur des Rotors und damit des mindestens einen Verdrängungselements des Rotors derart steigt, dass aufgrund der durch die Temperatur hervorgerufene Ausdehnung des Verdrängungselements ein Berühren zwischen der Außenseite des Verdrängungselements und der Innenseite des Schöpfraums auftritt.Screw vacuum pumps have a pumping chamber in a housing, in which two screw rotors are arranged. Each screw rotor has at least one displacement element with a helical recess. As a result, a large number of turns are formed. In order to be able to achieve low pressures or a high vacuum of in particular less than 200 mbar (absolute pressure) with a low specific power consumption with the aid of screw vacuum pumps, known screw vacuum pumps have a high internal compression. The internal compression defines the reduction of the delivery volume from the inlet to the outlet of the pump. Low outlet pressures are achieved, in particular, in that a gap with a small height is formed between an outside of the at least one displacement element and an inside of the scooping chamber. In order to be able to realize such small gaps, reliable cooling of the screw rotors must be guaranteed. This is the only way to prevent the temperature of the rotor and thus of the at least one displacement element of the rotor, in particular in the pressure-side area of the screw vacuum pump, in which high pressure differences occur, from increasing in such a way that due to the expansion of the displacement element caused by the temperature a contact occurs between the outside of the displacement element and the inside of the scoop.

Hierzu ist es aus EP 1 242 743 bekannt, eine Rotorinnenkühlung vorzusehen. Mit Hilfe der Rotorinnenkühlung ist eine effektive Kühlung des Rotors und somit des mit dem Rotor verbundenen oder einstückig mit diesem ausgebildeten mindestens einen Verdrängungselements gewährleistet, so dass geringe Spalthöhen realisiert werden können. Eine derartige Rotorinnenkühlung ist konstruktiv sehr aufwändig und daher kostenintensiv.For this it is over EP 1 242 743 known to provide internal rotor cooling. With the help of the rotor internal cooling, an effective cooling of the rotor and thus of the at least one displacement element connected to the rotor or integrally formed therewith is ensured, so that small gap heights can be realized. Such an internal rotor cooling is structurally very complex and therefore expensive.

Der nächstliegende Stand der Technik in Form von DE 10 2010 019 402 beschreibt eine Rotorschraubenvakuumpumpe ohne Rotorinnenkühlung mit nur jeweils einem Verdrängungselement je Rotor, das eine sich verändernde Steigung aufweist.The closest prior art in the form of DE 10 2010 019 402 describes a rotor screw vacuum pump without internal rotor cooling with only one displacement element per rotor, which has a changing pitch.

Aufgabe der Erfindung ist es, eine Schraubenvakuumpumpe zu schaffen, mit der ein hohes Vakuum von insbesondere weniger als 200 mbar und besonders bevorzugt weniger als 10 mbar erzielt werden kann, wobei auf eine Rotorinnenkühlung verzichtet werden kann.The object of the invention is to provide a screw vacuum pump with which a high vacuum of in particular less than 200 mbar and particularly preferably less than 10 mbar can be achieved, it being possible to dispense with internal rotor cooling.

Die Lösung der Aufgabe erfolgt erfindungsgemäß durch eine Schraubenvakuumpumpe gemäß Anspruch 1.The object is achieved according to the invention by a screw vacuum pump according to claim 1.

Die erfindungsgemäße Schraubenvakuumpumpe weist ein Gehäuse auf, das einen Schöpfraum ausbildet, in dem die beiden Schraubenrotoren angeordnet sind. Erfindungsgemäß sind das Gehäuse und die Rotoren aus Aluminium oder einer Aluminiumlegierung hergestellt. Besonders bevorzugt ist hierbei als Aluminiumlegierung für das Gehäuse AISi7Mg oder AlMg0,75Si. Insbesondere ist der Ausdehnungskoeffizient des Materials der Schraubenrotoren geringer als der Ausdehnungskoeffizient des Materials des Gehäuses. Besonders bevorzugt ist es, dass der Ausdehnungskoeffizient der Schraubenrotoren kleiner ist als 22*10-61/K, besonders bevorzugt kleiner als 20*10-61/K.The screw vacuum pump according to the invention has a housing which forms a scooping space in which the two screw rotors are arranged. According to the invention, the housing and the rotors are made of aluminum or an aluminum alloy. Particularly preferred is the aluminum alloy for the housing AISi7Mg or AlMg0.75Si. In particular, the coefficient of expansion of the material of the screw rotors is less than the coefficient of expansion of the material of the housing. It is particularly preferred that the expansion coefficient of the screw rotors is less than 22 * 10 -6 1 / K, particularly preferably less than 20 * 10 -6 1 / K.

Die beiden in dem Schöpfraum angeordneten Schraubenrotoren weisen mindestens ein Verdrängungselement auf, das eine schraubenlinienförmige Ausnehmung aufweist. Die schraubenlinienförmigen Ausnehmungen bilden mehrere Windungen aus. Erfindungsgemäß ist das mindestens eine Verdrängungselement aus Aluminium oder einer Aluminiumlegierung hergestellt. Bevorzugt ist es mindestens ein Verdrängungselement aus AISi9Mg oder AlSi17Cu4Mg herzustellen. Besonders bevorzugt ist es, dass das Aluminium bzw. die Aluminiumlegierung einen geringen Ausdehnungskoeffizienten von insbesondere weniger als 22*10-61/K, insbesondere weniger als 20*10-61/K aufweist.The two screw rotors arranged in the scoop have at least one displacement element which has a helical recess. The helical recesses form several turns. According to the invention, this is at least one displacement element made of aluminum or an aluminum alloy. It is preferred to produce at least one displacement element made of AISi9Mg or AlSi17Cu4Mg. It is particularly preferred that the aluminum or the aluminum alloy has a low expansion coefficient of in particular less than 22 * 10 -6 1 / K, in particular less than 20 * 10 -6 1 / K.

Besonders bevorzugt ist es, dass die Schraubenrotoren und insbesondere das mindestens eine Verdrängungselement je Schraubenrotor einen geringeren Ausdehnungskoeffizienten als das Gehäuse aufweist. Bevorzugt ist hierbei insbesondere, dass der Ausdehnungskoeffizient des Gehäuses mindestens 5%, besonders bevorzugt mindestens 10% größer ist als derjenige der Schraubenrotoren bzw. des mindestens einen Verdrängungselements. Besonders bevorzugt ist es, dass die Legierung des Rotors einen hohen Silicium-Anteil von vorzugsweise mindestens 9%, besonders bevorzugt von mehr als 15% aufweist, um einen geringen Wärme-Ausdehnungskoeffizienten zu realisieren.It is particularly preferred that the screw rotors and in particular the at least one displacement element per screw rotor have a lower expansion coefficient than the housing. It is particularly preferred here that the expansion coefficient of the housing is at least 5%, particularly preferably at least 10% larger than that of the screw rotors or of the at least one displacement element. It is particularly preferred that the alloy of the rotor has a high silicon content of preferably at least 9%, particularly preferably of more than 15%, in order to realize a low coefficient of thermal expansion.

Erfindungsgemäß sind die Schraubenrotoren und das mindestens eine vorgesehene Verdrängungselement derart ausgebildet, dass zwischen einem Bereich, in dem 5% - 20 % des Auslassdrucks herrschen, und dem druckseitigen Rotorende mindestens 6, insbesondere mindestens 8 und besonders bevorzugt mindestens 10 Windungen vorgesehen sind. Das druckseitige Rotorende ist hierbei der Bereich des Pumpenauslasses. Die erfindungsgemäß hohe Anzahl an Windungen in diesem Bereich kann hierbei in bevorzugter Ausführungsform bei einem einzigen je Rotor vorgesehenen druckseitigen Verdrängungselement vorgesehen sein. Möglich ist es jedoch auch, eine entsprechende Anzahl an Windungen in diesem druckseitigen Bereich, beispielsweise an zwei Verdrängungselementen vorzusehen. Durch Vorsehen einer erfindungsgemäß hohen Windungsanzahl in einem Bereich, in dem erfindungsgemäß sodann nur noch eine relativ geringe Kompression des zu fördernden Mediums je Windung erfolgt, ist es möglich, auf eine Rotorinnenkühlung zu verzichten. Dies liegt insbesondere darin begründet, dass aufgrund der verhältnismäßig geringen Kompression in diesem Bereich die durch die Kompression hervorgerufene Temperaturerhöhung des Verdrängungselements geringer ist. Des Weiteren erfolgt ebenfalls aufgrund der relativ hohen Dichte des Mediums in diesem Bereich durch das geförderte Medium selbst eine gute Wärmeabfuhr von dem Verdrängungselement in das Pumpengehäuse.According to the invention, the screw rotors and the at least one displacement element provided are designed such that at least 6, in particular at least 8 and particularly preferably at least 10 windings are provided between an area in which 5% to 20% of the outlet pressure prevails and the pressure-side rotor end. The rotor end on the pressure side is the area of the pump outlet. The high number of turns in this area according to the invention can be provided in a preferred embodiment in the case of a single pressure-side displacement element provided per rotor. However, it is also possible to provide a corresponding number of turns in this area on the pressure side, for example on two displacement elements. By providing a high number of turns according to the invention in a region in which according to the invention there is then only a relatively low compression of the medium to be conveyed per turn, it is possible to dispense with internal rotor cooling. This is due in particular to the fact that, due to the relatively low compression in this area, the temperature increase caused by the compression of the displacement element is lower. Furthermore, due to the relatively high density of the medium in this area, the conveyed medium itself also provides good heat dissipation from the displacement element into the pump housing.

Außerdem steht durch die hohe Zahl an Windungen eine große Oberfläche für den Wärmetausch zum Gehäuse zur Verfügung.In addition, the large number of turns means that a large surface is available for heat exchange with the housing.

Erfindungsgemäß sind die mindestens 6, insbesondere mindestens 8 und besonders bevorzugt mindestens 10 Windungen in einem druckseitigen Verdrängungselement vorgesehen. Hierbei ist es besonders bevorzugt, dass das durch das druckseitige Verdrängungselement hervorgerufene Druckverhältnis (= Austrittsdruck / Zwischendruck vor dem druckseitigen Verdrängungselement) weniger als 20, insbesondere weniger als 10, und besonders bevorzugt weniger als 5 ist. Bei einer Verdichtung auf Atmosphärendruck am Pumpenauslass erfolgt somit durch die erfindungsgemäß letzten 6, insbesondere letzten 8 und besonders bevorzugt letzten 10 Windungen eine Verdichtung von 50mbar auf 1.000 mbar bei einem Druckverhältnis von 20. Insofern erfolgt bei einem Druckverhältnis von 10 eine Verdichtung von 100 mbar auf 1.000 mbar und bei einem Druckverhältnis von 5 eine Verdichtung von 200 mbar auf 1.000 mbar.According to the invention, the at least 6, in particular at least 8 and particularly preferably at least 10 windings are provided in a pressure-side displacement element. It is particularly preferred here that the pressure ratio caused by the pressure-side displacement element (= outlet pressure / intermediate pressure in front of the pressure-side displacement element) is less than 20, in particular less than 10, and particularly preferably less than 5. When compressing to atmospheric pressure at the pump outlet, the last 6, in particular last 8 and particularly preferably last 10 windings in accordance with the invention result in a compression of 50 mbar to 1,000 mbar at a pressure ratio of 20. In this respect, a compression of 100 mbar occurs at a pressure ratio of 10 1,000 mbar and at a pressure ratio of 5 a compression from 200 mbar to 1,000 mbar.

Der Abstand zwischen einem Bereich, in dem 5% - 20% des Auslassdrucks herrschen, bis zur letzten Windung in Förderrichtung, d.h. im Wesentlichen bis zum Pumpenauslass beträgt vorzugsweise mindestens 20 % - 30 % der Rotorlänge. Dies hat wiederum den Vorteil, dass in einem relativ großen Bereich nur noch eine relativ geringe Kompression erfolgt. Dies bewirkt wiederum eine verhältnismäßig geringe Temperaturerhöhung aufgrund der geringen Kompression.The distance between an area in which 5% - 20% of the outlet pressure prevails, up to the last turn in the conveying direction, i.e. essentially up to the pump outlet is preferably at least 20% to 30% of the rotor length. This in turn has the advantage that in a relatively large area there is only a relatively low compression. This in turn causes a relatively small increase in temperature due to the low compression.

Des Weiteren ist es zur erfindungsgemäßen Ausgestaltung von Schraubenrotoren ohne Innenkühlung bevorzugt, dass das druckseitige Verdrängungselement an mindestens 6, insbesondere mindestens 8 und besonders bevorzugt mindestens 10 Windungen einen mittleren Arbeitsdruck von mehr als 50 mbar aufweist. Bei Enddruckbetrieb der Pumpe, d.h. bei geschlossenem Einlass wird an dieser Stelle der Pumpe ein (zeitlich gemittelter) Druck von 50 mbar erreicht.Furthermore, for the inventive design of screw rotors without internal cooling, it is preferred that the pressure-side displacement element has at least 6, in particular at least 8 and particularly preferably at least 10 turns has an average working pressure of more than 50 mbar. When the pump is operating at end pressure, ie when the inlet is closed, a (time-averaged) pressure of 50 mbar is reached at this point of the pump.

Erfindungsgemäß ist es somit möglich, auch bei Rotoren ohne Rotorinnenkühlung und bei einem Gehäuse aus Aluminium oder aus einer Aluminiumlegierung sowie mindestens einem Verdrängungselement aus Aluminium oder Aluminiumlegierung zwischen der Oberfläche des mindestens einen Verdrängungselements und der Innenseite des Schöpfraums insbesondere im druckseitigen Bereich einen Kalt-Spalt mit einer Höhe von 0,05 mm - 0,3 mm und insbesondere 0,1 mm - 0,2 mm vorzusehen. Eine derart verhältnismäßig große Spalthöhe kann aufgrund der erfindungsgemäßen, vorstehend beschriebenen Ausgestaltung der insbesondere 6, vorzugsweise 8 und besonders bevorzugt 10 letzten Windungen, vorgesehen werden.According to the invention, it is therefore possible, even in the case of rotors without internal rotor cooling and in a housing made of aluminum or an aluminum alloy and at least one displacement element made of aluminum or aluminum alloy, to have a cold gap between the surface of the at least one displacement element and the inside of the scooping space, in particular in the pressure-side area a height of 0.05 mm - 0.3 mm and in particular 0.1 mm - 0.2 mm. Such a relatively large gap height can be provided on the basis of the configuration according to the invention described above, in particular 6, preferably 8 and particularly preferably 10 last windings.

Jedes Verdrängungselement weist mindestens eine schraubenlinienförmige Ausnehmung auf, die über ihre gesamte Länge dieselbe Kontur aufweist. Die Konturen sind vorzugsweise je Verdrängungselement unterschiedlich. Das einzelne Verdrängungselement weist somit eine gleichbleibende Kontur auf und vorzugsweise eine konstante Steigung. Dies vereinfacht die Herstellung erheblich, so dass die Herstellungskosten stark gesenkt werden können.Each displacement element has at least one helical recess which has the same contour over its entire length. The contours are preferably different for each displacement element. The individual displacement element thus has a constant contour and preferably a constant slope. This considerably simplifies the production, so that the production costs can be greatly reduced.

Zur weiteren Verbesserung der Saugleistung ist die Kontur des saugseitigen Verdrängungselements, das heißt insbesondere des in Pumprichtung ersten Verdrängungselements vorzugsweise asymmetrisch ausgebildet. Durch die asymmetrische Ausbildung der Kontur bzw. des Profils können die Flanken derart ausgestaltet werden, dass die Leckageflächen, die sogenannten Blaslöcher insbesondere vollständig verschwinden oder zumindest einen geringen Querschnitt aufweisen. Ein besonders geeignetes asymmetrisches Profil ist das sogenannte "Quimby-Profil". Ein derartiges Profil ist zwar relativ schwierig herzustellen, weist jedoch den Vorteil auf, dass kein durchgehendes Blasloch vorhanden ist. Ein Kurzschluss ist nur zwischen zwei benachbarten Kammern gegeben. Da es sich um ein asymmetrisches Profil mit unterschiedlichen Profilflanken handelt, sind für die Herstellung zumindest zwei Arbeitsschritte erforderlich, da die beiden Flanken aufgrund ihrer Asymmetrie in unterschiedlichen Arbeitsschritten hergestellt werden müssen.In order to further improve the suction power, the contour of the displacement element on the suction side, that is to say in particular of the first displacement element in the pumping direction, is preferably asymmetrical. Due to the asymmetrical design of the contour or profile, the flanks can be designed in such a way that the leakage areas, the so-called blowholes, in particular completely disappear or at least have a small cross section. A particularly suitable asymmetrical profile is the so-called "Quimby profile". Such a profile is relatively difficult to manufacture, has the advantage, however, that there is no continuous blow hole. A short circuit only exists between two neighboring chambers. Since it is an asymmetrical profile with different profile flanks, at least two work steps are required for the production, since the two flanks have to be produced in different work steps due to their asymmetry.

Das druckseitige Verdrängungselement, insbesondere das in Pumprichtung letzte Verdrängungselement, ist vorzugsweise mit einer symmetrischen Kontur versehen. Die symmetrische Kontur hat insbesondere den Vorteil, dass die Herstellung einfacher ist. Insbesondere können beide Flanken mit symmetrischer Kontur durch einen rotierenden Fingerfräser oder durch einen rotierenden Scheibenfräser in einem Arbeitsschritt hergestellt werden. Derartige symmetrische Profile weisen zwar Blaslöcher auf, diese sind jedoch durchgehend, d.h. nicht nur zwischen zwei benachbarten Kammern vorgesehen. Die Größe des Blaslochs verringert sich bei Verringerung der Steigung. Insofern können derartige symmetrische Profile insbesondere bei dem druckseitigen Verdrängungselement vorgesehen werden, da diese in bevorzugter Ausführungsform eine kleinere Steigung als das saugseitige Verdrängungselement und vorzugsweise auch als das zwischen dem saugseitigen und dem druckseitigen Verdrängungselement angeordnete Verdrängungselemente aufweist. Wenngleich die Dichtigkeit derartiger symmetrischer Profile etwas geringer ist, weisen diese den Vorteil auf, dass die Herstellung deutlich einfacher ist. Insbesondere ist es möglich, das symmetrische Profil in einem einzigen Arbeitsschritt und vorzugsweise mit einem einfachen Fingerfräser oder Scheibenfräser herzustellen. Dies reduziert die Kosten erheblich. Ein besonders geeignetes symmetrisches Profil ist das sogenannte "Zykloiden-Profil".The pressure-side displacement element, in particular the last displacement element in the pumping direction, is preferably provided with a symmetrical contour. The symmetrical contour has the particular advantage that production is easier. In particular, both flanks with a symmetrical contour can be produced in one work step by a rotating end mill or by a rotating side milling cutter. Although such symmetrical profiles have blowholes, they are continuous, i.e. not only provided between two adjacent chambers. The size of the blow hole decreases as the slope decreases. In this respect, such symmetrical profiles can be provided in particular in the case of the pressure-side displacement element, since in a preferred embodiment this has a smaller slope than the suction-side displacement element and preferably also as the displacement element arranged between the suction-side and the pressure-side displacement element. Although the tightness of such symmetrical profiles is somewhat lower, they have the advantage that the manufacture is significantly easier. In particular, it is possible to produce the symmetrical profile in a single work step and preferably with a simple end mill or side milling cutter. This significantly reduces costs. A particularly suitable symmetrical profile is the so-called "cycloid profile".

Das Vorsehen mindestens zweier derartiger Verdrängungselemente führt dazu, dass die entsprechende Schraubenvakuumpumpe bei geringer Leistungsaufnahme niedrige Einlassdrücke erzeugen kann. Auch ist die thermische Belastung gering. Das Anordnen von mindestens zwei erfindungsgemäß ausgestalteten Verdrängungselementen mit konstanter Steigung und gleichbleibender Kontur in einer Vakuumpumpe führt zu im Wesentlichen gleichen Ergebnissen, wie bei einer Vakuumpumpe mit einem Verdrängungselement mit sich ändernder Steigung. Bei hohen eingebauten Volumenverhältnissen können je Rotor drei oder vier Vedrängungselemente vorgesehen werden.The provision of at least two such displacement elements means that the corresponding screw vacuum pump can generate low inlet pressures with low power consumption. The thermal load is also low. The arrangement of at least two displacement elements designed according to the invention with constant pitch and constant Contour in a vacuum pump leads to essentially the same results as with a vacuum pump with a displacement element with changing pitch. With high built-in volume ratios, three or four displacement elements can be provided for each rotor.

Zur Verringerung des erzielbaren Einlassdrucks und/oder zur Verringerung der Leistungsaufnahme und/oder der thermischen Belastung weist bei einer besonders bevorzugten Ausführungsform ein druckseitiges, das heißt insbesondere in Pumprichtung letztes Verdrängungselement eine große Anzahl an Windungen auf. Durch eine hohe Anzahl an Windungen kann ein größerer Spalt zwischen dem Schraubenrotor und dem Gehäuse akzeptiert werden bei gleichbleibender Performance. Der Spalt kann hierbei eine Kalt-Spaltweite von 0,05 - 0,3 mm aufweisen. Eine große Anzahl an Auslasswindungen bzw. Anzahl an Windungen bei dem druckseitigen Verdrängungselement ist kostengünstig herstellbar, da erfindungsgemäß dieses Verdrängungselement eine konstante Steigung und vorzugsweise auch eine symmetrische Kontur aufweist. Hierdurch ist eine einfache und kostengünstige Herstellung möglich, so dass das Vorsehen einer größeren Anzahl an Windungen akzeptabel ist. Vorzugsweise weist dieses druckseitige bzw. letzte Verdrängungselement mehr als 6, insbesondere mehr als 8 und besonders bevorzugt mehr als 10 Windungen auf. Das Verwenden symmetrischer Profile hat in besonders bevorzugter Ausführungsform den Vorteil, dass beide Flanken des Profils mit einem Fräser gleichzeitig geschnitten werden können. Hierbei erfolgt zusätzlich ein Abstützen des Fräsers durch die jeweils gegenüberliegende Flanke, so dass ein Verformen bzw. Verbiegen des Fräsers während des Fräsvorgangs und hierdurch hervorgerufene Ungenauigkeiten vermieden sind.In order to reduce the achievable inlet pressure and / or to reduce the power consumption and / or the thermal load, in a particularly preferred embodiment a pressure-side, that is to say in particular the last, displacement element has a large number of turns. Due to the large number of turns, a larger gap between the screw rotor and the housing can be accepted while maintaining the same performance. The gap can have a cold gap width of 0.05-0.3 mm. A large number of outlet windings or number of windings in the pressure-side displacement element can be produced inexpensively, since, according to the invention, this displacement element has a constant pitch and preferably also a symmetrical contour. This enables simple and inexpensive production, so that the provision of a larger number of turns is acceptable. This pressure-side or last displacement element preferably has more than 6, in particular more than 8 and particularly preferably more than 10 turns. In a particularly preferred embodiment, the use of symmetrical profiles has the advantage that both flanks of the profile can be cut simultaneously with one milling cutter. Here, the milling cutter is additionally supported by the opposite flank, so that deformation or bending of the milling cutter during the milling process and inaccuracies caused thereby are avoided.

Zur weiteren Reduzierung der Herstellungskosten ist es besonders bevorzugt, die Verdrängungselemente und die Rotorwelle einstückig auszubilden.To further reduce the manufacturing costs, it is particularly preferred to form the displacement elements and the rotor shaft in one piece.

Bei einer weiteren bevorzugten Ausführungsform ist der Steigungswechsel zwischen benachbarten Verdrängungselementen unstetig bzw. sprunghaft ausgebildet. Gegebenenfalls sind die beiden Verdrängungselemente in Längsrichtung in einem Abstand zueinander angeordnet, so dass zwischen zwei Verdrängungselementen eine umlaufende zylinderringförmige Kammer ausgebildet ist, die als Werkzeugauslauf dient. Dies ist insbesondere bei einstückig ausgebildeten Rotoren vorteilhaft, da das die Schraubenlinie herstellende Werkzeug in diesem Bereich auf einfache Weise herausgeführt werden kann. Sofern die Verdrängungselemente unabhängig voneinander hergestellt und sodann auf einer Welle montiert werden, ist das Vorsehen eines Werkzeugauslaufs, insbesondere eines derartigen ringzylindrischen Bereichs nicht erforderlich.In a further preferred embodiment, the change in pitch between adjacent displacement elements is discontinuous or erratic. If necessary, the two displacement elements are in the longitudinal direction arranged at a distance from each other so that a circumferential cylindrical ring-shaped chamber is formed between two displacement elements, which serves as a tool outlet. This is particularly advantageous in the case of rotors formed in one piece, since the tool producing the helical line can be led out in a simple manner in this area. If the displacement elements are manufactured independently of one another and then mounted on a shaft, the provision of a tool outlet, in particular of such a ring-cylindrical region, is not necessary.

Bei einer bevorzugten Weiterbildung der Erfindung ist zwischen zwei benachbarten Verdrängungselementen am Steigungswechsel kein Werkzeugauslauf vorgesehen. In dem Bereich des Steigungswechsels weisen vorzugsweise beide Flanken eine Fehlstelle bzw. Ausnehmung auf, um das Werkzeug herausführen zu können. Eine derartige Fehlstelle hat keinen nennenswerten Einfluss auf die Verdichtungsleistung der Pumpe, da es sich um eine örtlich stark begrenzte Fehlstelle bzw. Ausnehmung handelt.In a preferred development of the invention, no tool outlet is provided between two adjacent displacement elements on the change of pitch. In the area of the change of pitch, preferably both flanks have a defect or recess in order to be able to lead the tool out. Such a flaw has no significant influence on the compression performance of the pump, since it is a flaw or recess that is very local.

Der erfindungsgemäße Vakuumpumpen-Schraubenrotor weist insbesondere mehrere Verdrängungselemente auf. Diese können jeweils den gleichen oder unterschiedliche Durchmesser aufweisen. Bevorzugt ist es hierbei, dass das druckseitige Verdrängungselement einen kleineren Durchmesser als das saugseitige Verdrängungselement aufweist.The vacuum pump screw rotor according to the invention has, in particular, a plurality of displacement elements. These can each have the same or different diameters. It is preferred here that the pressure-side displacement element has a smaller diameter than the suction-side displacement element.

Bei unabhängig von der Rotorwelle hergestellten Verdrängungselementen werden diese beispielsweise durch Presspassungen auf der Welle montiert. Hierbei ist es bevorzugt, Elemente wie Passstifte zur Festlegung der Winkelposition der Verdrängungselemente zueinander vorzusehen.In the case of displacement elements produced independently of the rotor shaft, these are mounted on the shaft by press fits, for example. Here, it is preferred to provide elements such as dowel pins for fixing the angular position of the displacement elements to one another.

Insbesondere bei der einstückigen Ausgestaltung des Schraubenrotors aber auch bei einer mehrstückigen Ausgestaltung ist es bevorzugt, diesen aus Aluminium oder aus einer Aluminiumlegierung herzustellen. Besonders bevorzugt ist es, den Rotor aus Aluminium oder einer Aluminium-Legierung insbesondere AlSi9Mg oder AlMg0,7Si herzustellen. Die Legierung hat vorzugsweise einen hohen Silicium-Anteil von vorzugsweise mehr als 9%, insbesondere mehr als 15 %, um den Ausdehnungskoeffizienten zu verringern.In particular in the one-piece configuration of the screw rotor, but also in the case of a multi-piece configuration, it is preferred to produce it from aluminum or from an aluminum alloy. Particularly preferred is to manufacture the rotor from aluminum or an aluminum alloy, in particular AlSi9Mg or AlMg0.7Si. The alloy preferably has a high silicon content of preferably more than 9%, in particular more than 15%, in order to reduce the coefficient of expansion.

Das für die Rotoren verwendete Aluminium weist in einer weiteren bevorzugten Weiterbildung der Erfindung einen geringen Ausdehnungskoeffizienten auf. Bevorzugt ist es, wenn das Material einen Ausdehnungskoeffizienten von weniger als 22*10-61/K, insbesondere von weniger als 20*10-61/K, aufweist. In einer weiter bevorzugten Ausführungsform ist die Oberfläche der Verdrängungselemente beschichtet, wobei insbesondere eine Beschichtung gegen Verschleiß und/oder Korrosion vorgesehen ist. Hierbei ist es bevorzugt eine anodische oder eine andere geeignete Beschichtung je nach Anwendungsgebiet vorzusehen.In a further preferred development of the invention, the aluminum used for the rotors has a low coefficient of expansion. It is preferred if the material has an expansion coefficient of less than 22 * 10 -6 1 / K, in particular less than 20 * 10 -6 1 / K. In a further preferred embodiment, the surface of the displacement elements is coated, a coating against wear and / or corrosion being provided in particular. It is preferred to provide an anodic or other suitable coating depending on the area of application.

Besonders bevorzugt ist es, dass der Schraubenrotor einstückig, insbesondere aus Aluminium oder einer Aluminiumlegierung hergestellt ist. Der Schraubenrotor kann auch eine Rotorwelle aufweisen, die das mindestens eine Verdrängungselement trägt. Dies hat insbesondere beim Vorsehen mehrerer Verdrängungselemente den Vorteil, dass diese unabhängig voneinander hergestellt werden können und anschließend insbesondere durch Aufpressen oder Aufschrumpfen mit der Rotorwelle verbunden werden. Hierbei ist es möglich, zur Definition der Winkellage der einzelnen Verdrängungselemente Passfedern oder dergleichen vorzusehen. Die Rotorwelle kann aus Stahl hergestellt sein und das mindestens eine aus Aluminium oder einer Aluminiumlegierung hergestellte Verdrängungselement tragen.It is particularly preferred that the screw rotor is made in one piece, in particular from aluminum or an aluminum alloy. The screw rotor can also have a rotor shaft which carries the at least one displacement element. This has the advantage, in particular when providing a plurality of displacement elements, that these can be produced independently of one another and are subsequently connected to the rotor shaft in particular by being pressed on or shrunk on. It is possible to provide feather keys or the like to define the angular position of the individual displacement elements. The rotor shaft can be made of steel and carry the at least one displacement element made of aluminum or an aluminum alloy.

Bei dem bevorzugten Vorsehen von mehreren Verdrängungselementen je Schraubenrotor ist es möglich, die Verdrängungselemente einstückig auszubilden.In the preferred provision of a plurality of displacement elements per screw rotor, it is possible to form the displacement elements in one piece.

Erfindungsgemäß bevorzugt ist es, dass die Schraubenrotoren keine Rotorinnenkühlung aufweisen. Insofern ist es besonders bevorzugt, dass die Schraubenrotoren keine von insbesondere flüssigem Kühlmittel durchströmten Kanäle aufweisen. Die Schraubenrotoren können jedoch Bohrungen oder Kanäle, beispielsweise zur Gewichtsreduzierung, zum Wuchten oder dgl. aufweisen. Bevorzugt ist es insbesondere, dass die Schraubenrotoren massiv ausgebildet sind.It is preferred according to the invention that the screw rotors have no internal rotor cooling. In this respect, it is particularly preferred that the screw rotors have no channels through which liquid coolant flows. However, the screw rotors can have bores or channels, for example for reducing weight, for balancing or the like. It is particularly preferred that the screw rotors are solid.

Des Weiteren ist es bevorzugt, dass im Bereich der druckseitigen Verdrängungselemente, d.h. insbesondere im Bereich der letzten 6, bevorzugt letzten 8 und besonders bevorzugt letzten 10 Windungen zwischen den Verdrängungselementen und dem Gehäuse ein geringer Temperaturunterschied herrscht. In Normalbetrieb ist dieser Temperaturunterschied vorzugsweise kleiner als 50 K und insbesondere kleiner als 20 K. Unter Normalbetrieb wird der gesamte Ansaugdruckbereich vom Enddruck bis hin zu einem offenen Einlass (atmosphärisches Ansaugen) verstanden.Furthermore, it is preferred that in the area of the pressure-side displacement elements, i.e. in particular in the area of the last 6, preferably last 8 and particularly preferably last 10 windings, there is a small temperature difference between the displacement elements and the housing. In normal operation, this temperature difference is preferably less than 50 K and in particular less than 20 K. Normal operation means the entire intake pressure range from the final pressure to an open inlet (atmospheric intake).

Des Weiteren ist es bevorzugt, dass das Gehäuse im Bereich der druckseitigen Verdrängungselemente, d.h. insbesondere im Bereich der letzten 6, insbesondere letzten 8 und besonders bevorzugt letzten 10 Windungen eine mittlere Wärmestromdichte aufweist, die kleiner als 20.000 W/m2, vorzugsweise kleiner als 15.000 W/m2 und insbesondere kleiner als 10.000 W/m2 ist. Die mittlere Wärmestromdichte ist das Verhältnis aus Verdichtungsleistung zur Wandfläche des Auslassbereichs.Furthermore, it is preferred that the housing in the area of the pressure-side displacement elements, ie in particular in the area of the last 6, in particular last 8 and particularly preferably last 10 turns, has an average heat flow density which is less than 20,000 W / m 2 , preferably less than 15,000 W / m 2 and in particular less than 10,000 W / m 2 . The average heat flow density is the ratio of the compression performance to the wall area of the outlet area.

Nachfolgend wird die Erfindung anhand einer bevorzugten Ausführungsform unter Bezugnahme auf die anliegenden Zeichnungen näher erläutert.The invention is explained in more detail below on the basis of a preferred embodiment with reference to the attached drawings.

Es zeigen:

Fig. 1
eine schematische Draufsicht einer ersten bevorzugten Ausführungsform eines Schraubenrotors der erfindungsgemäßen Schraubenvakuumpumpe,
Fig. 2
eine schematische Draufsicht einer zweiten bevorzugten Ausführungsform eines Schraubenrotors der erfindungsgemäßen Schraubenvakuumpumpe,
Fig. 3
eine schematische Schnittansicht von Verdrängungselementen mit asymmetrischem Profil,
Fig. 4
eine schematische Schnittansicht von Verdrängungselementen mit symmetrischem Profil, und
Fig. 5
eine schematische Schnittansicht einer Schraubenvakuumpumpe.
Show it:
Fig. 1
2 shows a schematic top view of a first preferred embodiment of a screw rotor of the screw vacuum pump according to the invention,
Fig. 2
1 shows a schematic top view of a second preferred embodiment of a screw rotor of the screw vacuum pump according to the invention,
Fig. 3
1 shows a schematic sectional view of displacement elements with an asymmetrical profile,
Fig. 4
is a schematic sectional view of displacement elements with a symmetrical profile, and
Fig. 5
is a schematic sectional view of a screw vacuum pump.

Die in den Fig. 1 und 2 dargestellten Schraubenrotoren können in einer erfindungsgemäßen Schraubenvakuumpumpe, wie in Fig. 5 dargestellt, eingesetzt werden.The in the 1 and 2 Screw rotors shown can in a screw vacuum pump according to the invention, as in Fig. 5 shown, used.

Bei der ersten bevorzugten Ausführungsform des Vakuumpumpen-Schraubenrotors weist der Rotor zwei Verdrängungselemente 10, 12 auf. Ein erstes saugseitiges Verdrängungselement 10 weist eine große Steigung von ca. 50 - 150 mm/Umdrehung auf. Die Steigung ist über das gesamte Verdrängungselement 10 konstant. Auch die Kontur der schraubenlinienförmigen Ausnehmung ist konstant. Das zweite druckseitige Verdrängungselement 12 weist über seine Länge wiederum eine konstante Steigung und eine konstante Kontur der Ausnehmung auf. Die Steigung des druckseitigen Verdrängungselements 12 liegt vorzugsweise im Bereich von 10 - 30 mm/Umdrehung. Zwischen den beiden Verdrängungselementen ist eine ringzylindrische Ausnehmung 14 vorgesehen. Diese dient dazu, das aufgrund der einstückigen Ausgestaltung des in Fig. 1 dargestellten Schraubenrotors ein Werkzeugauslauf realisiert ist.In the first preferred embodiment of the vacuum pump screw rotor, the rotor has two displacement elements 10, 12. A first displacement-side displacement element 10 has a large pitch of approximately 50-150 mm / revolution. The slope is constant over the entire displacement element 10. The contour of the helical recess is also constant. The second pressure-side displacement element 12 again has a constant slope and a constant contour of the recess over its length. The slope of the pressure-side displacement element 12 is preferably in the range of 10-30 mm / revolution. An annular cylindrical recess 14 is provided between the two displacement elements. This serves to ensure that due to the one-piece design of the in Fig. 1 shown screw rotor a tool outlet is realized.

Ferner weist der einstückig ausgebildete Schraubenrotor zwei Lagersitze 16 und ein Wellenende 18 auf. Mit dem Wellenende 18 wird beispielsweise ein Zahnrad zum Antrieb verbunden.Furthermore, the one-piece screw rotor has two bearing seats 16 and one shaft end 18. A gearwheel for driving is connected to the shaft end 18, for example.

Bei der in Fig. 2 dargestellten zweiten bevorzugten Ausführungsform sind die beiden Verdrängungselemente 10, 12 gesondert hergestellt und sodann auf einer Rotorwelle 20 beispielsweise durch Aufpressen fixiert. Diese Herstellung ist zwar etwas aufwendiger, jedoch ist der zylindrische Abstand 14 zwischen zwei benachbarten Verdrängungselementen 10, 12 als Werkzeugauslauf nicht erforderlich. Die Lagersitze 16 und die Wellenenden 18 können integraler Bestandteil der Welle 20 sein. Die durchgehende Welle 20 kann auch aus einem anderen sich von den Verdrängungselementen 10, 12 unterscheidenden Werkstoff hergestellt sein.At the in Fig. 2 Second preferred embodiment shown are the two displacement elements 10, 12 manufactured separately and then fixed on a rotor shaft 20, for example by pressing. Although this production is somewhat more complex, the cylindrical distance 14 between two adjacent displacement elements 10, 12 is not required as a tool outlet. The bearing seats 16 and the shaft ends 18 can be an integral part of the shaft 20. The continuous shaft 20 can also be made of another material that differs from the displacement elements 10, 12.

Fig. 3 zeigt eine schematische Schnittansicht eines asymmetrischen Profils (z.B. ein Quimby-Profil). Bei dem dargestellten asymmetrischen Profil handelt es sich um ein sogenanntes "Quimby-Profil". Die Schnittansicht zeigt zwei Schraubenrotoren, die miteinander kämmen und deren Längsrichtung senkrecht zur Zeichenebene ist. Die gegenläufige Drehung der Rotoren ist durch die beiden Pfeile 15 angedeutet. Bezogen auf eine senkrecht zur Längsachse der Verdrängungselemente verlaufenden Ebene 17 sind die Profile der Flanken 19 und 21 je Rotor unterschiedlich ausgestaltet. Die einander gegenüberliegenden Flanken 19, 21 müssen somit unabhängig voneinander hergestellt werden. Die daher zwar etwas aufwändigere und schwierigere Herstellung hat jedoch den Vorteil, dass kein durchgehendes Blasloch vorhanden ist, sondern lediglich zwischen zwei benachbarten Kammern ein Kurzschluss besteht. Fig. 3 shows a schematic sectional view of an asymmetrical profile (eg a Quimby profile). The asymmetrical profile shown is a so-called "Quimby profile". The sectional view shows two screw rotors which mesh with one another and whose longitudinal direction is perpendicular to the plane of the drawing. The opposite rotation of the rotors is indicated by the two arrows 15. In relation to a plane 17 running perpendicular to the longitudinal axis of the displacement elements, the profiles of the flanks 19 and 21 are designed differently for each rotor. The mutually opposite flanks 19, 21 must therefore be produced independently of one another. The production, which is therefore somewhat more complex and difficult, has the advantage, however, that there is no continuous blow hole, but only a short circuit between two adjacent chambers.

Ein derartiges asymmetrisches Profil ist vorzugsweise bei dem saugseitigen Verdrängungselement 10 vorgesehen.Such an asymmetrical profile is preferably provided in the suction-side displacement element 10.

Die schematische Schnittansicht in Fig. 4 zeigt wiederum einen Querschnitt zweier Verdrängungselemente bzw. zweier Schraubenrotoren, die wiederum gegenläufig rotieren (Pfeile 15). Bezogen auf die Symmetrieachse 17 sind die Flanken 23 je Verdrängungselement symmetrisch ausgebildet. Bei dem in Fig. 4 dargestellten bevorzugten Ausführungsbeispiel einer symmetrisch ausgestalteten Kontur handelt es sich um ein Zykloiden-Profil.The schematic sectional view in Fig. 4 again shows a cross section of two displacement elements or two screw rotors, which in turn rotate in opposite directions (arrows 15). Relative to the axis of symmetry 17, the flanks 23 are formed symmetrically for each displacement element. At the in Fig. 4 The illustrated preferred embodiment of a symmetrically designed contour is a cycloid profile.

Ein symmetrisches Profil, wie in Fig. 4 dargestellt, ist vorzugsweise bei den druckseitigen Verdrängungselementen 12 vorgesehen.A symmetrical profile, as in Fig. 4 is preferably provided in the pressure-side displacement elements 12.

Ferner ist es möglich, dass mehr als zwei Verdrängungselemente vorgesehen sind. Diese können ggf. auch unterschiedliche Kopfdurchmesser und entsprechende Fußdurchmesser aufweisen. Hierbei ist es bevorzugt, dass ein Verdrängungselement mit größerem Kopfdurchmesser am Einlass, d.h. saugseitig angeordnet ist, um in diesem Bereich ein größeres Saugvermögen zu realisieren und/ oder das eingebaute Volumenverhältnis zu vergrößern. Ferner sind Kombinationen der vorstehend beschriebenen Ausführungsformen möglich. Beispielsweise können ein oder mehrere Verdrängungselemente einstückig mit der Welle oder ein zusätzliches Verdrängungselement unabhängig von der Welle hergestellt und sodann auf der Welle montiert werden.It is also possible that more than two displacement elements are provided. If necessary, these can also have different head diameters and corresponding foot diameters. It is preferred here that a displacement element with a larger head diameter at the inlet, i.e. is arranged on the suction side in order to achieve a greater pumping speed in this area and / or to increase the built-in volume ratio. Combinations of the above-described embodiments are also possible. For example, one or more displacement elements can be produced in one piece with the shaft or an additional displacement element can be produced independently of the shaft and then mounted on the shaft.

In der in Fig. 5 dargestellten schematischen Ansicht einer erfindungsgemäßen bevorzugten Ausführungsform einer Schraubenvakuumpumpe sind zwei Schraubenrotoren, wie in Fig. 1 dargestellt, in einem Gehäuse 26 angeordnet. Das Vakuumpumpen-Gehäuse 26 weist einen Einlass 28 auf, durch den Gas in Richtung eines Pfeils 30 eingesaugt wird. Der Einlass 28 ist beispielsweise mit einer zu evakuierenden Kammer verbunden. Ferner weist das Pumpengehäuse 26 einen druckseitigen Auslass 32 auf, durch den das Gas in Richtung eines Pfeils 38 ausgestoßen wird. Vorzugsweise pumpt die erfindungsgemäße Schraubenvakuumpumpe unmittelbar gegen Atmosphäre, so dass mit dem Auslass 32 keine Vorvakuumpumpe mehr verbunden ist, wobei dies auch möglich ist.In the in Fig. 5 Shown schematic view of a preferred embodiment of a screw vacuum pump according to the invention are two screw rotors, as in Fig. 1 shown, arranged in a housing 26. The vacuum pump housing 26 has an inlet 28 through which gas is drawn in in the direction of an arrow 30. The inlet 28 is connected, for example, to a chamber to be evacuated. Furthermore, the pump housing 26 has an outlet 32 on the pressure side, through which the gas is expelled in the direction of an arrow 38. The screw vacuum pump according to the invention preferably pumps directly against the atmosphere, so that no forevacuum pump is connected to the outlet 32, although this is also possible.

In dem dargestellten Ausführungsbeispiel weisen die beiden druckseitigen Verdrängungselemente 12 je Schraubenrotor 10 Windungen auf. Insbesondere herrscht in einem Bereich 40, d.h. in einem Bereich der in Förderrichtung ersten Windung des druckseitigen Verdrängungselements 12 ein Druck von 5% - 20 % des am Auslass 32 herrschenden Drucks.In the exemplary embodiment shown, the two pressure-side displacement elements 12 have 10 turns per screw rotor. In particular, there is an area 40, i.e. in a region of the first turn of the pressure-side displacement element 12 in the conveying direction, a pressure of 5% - 20% of the pressure prevailing at the outlet 32.

Zwischen den Oberflächen 42 der beiden druckseitigen Verdrängungselemente 12 und einer Innenfläche 44 eines durch das Pumpengehäuse 26 ausgebildeten Schöpfraums 46 ist ein Spalt ausgebildet, dessen Höhe vorzugsweise im Bereich von 0,05 mm - 0, 3 mm und insbesondere im Bereich von 0,1 mm - 0,2 mm liegt.A gap is formed between the surfaces 42 of the two pressure-side displacement elements 12 and an inner surface 44 of a scooping space 46 formed by the pump housing 26, the height of which is preferably in the range from 0.05 mm to 0.3 mm and in particular in the range from 0.1 mm - 0.2 mm.

Das Vakuumpumpengehäuse 26 ist im dargestellten Ausführungsbeispiel mit zwei Gehäusedeckeln 47 verschlossen. Der in Fig. 4 linke Gehäusedeckel 47 weist zwei Lageraufnahmen auf, in denen jeweils ein Kugellager 48 zur Lagerung der beiden Rotorwellen angeordnet ist. Auf der in Fig. 4 rechten Seite ragen die Zapfen 50 der beiden Schraubenrotorwellen durch die Deckel 47 hindurch. Auf der Außenseite ist auf den beiden Wellenzapfen 50 jeweils ein Zahnrad 52 angeordnet. Die beiden Zahnräder 52 kämmen im dargestellten Ausführungsbeispiel miteinander, um die beiden Schraubenrotoren miteinander zu synchronisieren. Ferner sind auch in dem in Fig. 4 rechten Deckel 47 zwei Lager 48 zur Lagerung der Schraubenrotoren angeordnet.The vacuum pump housing 26 is closed in the illustrated embodiment with two housing covers 47. The in Fig. 4 left housing cover 47 has two bearing receptacles, in each of which a ball bearing 48 is arranged for mounting the two rotor shafts. On the in Fig. 4 on the right side, the pins 50 of the two screw rotor shafts protrude through the covers 47. On the outside, a gear wheel 52 is arranged on each of the two shaft journals 50. In the exemplary embodiment shown, the two gear wheels 52 mesh with one another in order to synchronize the two screw rotors with one another. Furthermore, in the in Fig. 4 right cover 47 two bearings 48 arranged for storing the screw rotors.

Bei der in Fig. 5 unteren Welle handelt es sich um die Antriebswelle, die mit einem nicht dargestellten Antriebsmotor verbunden ist.At the in Fig. 5 lower shaft is the drive shaft, which is connected to a drive motor, not shown.

Besonders gute Ergebnisse gemäß der Erfindung konnten bei nachfolgender Ausgestaltung erzielt werden, die daher besonders bevorzugt ist: Werkstoff Gehäuse AlSi7Mg (Guss, Ausdehnungskoeffizient 2210-6K-1 oder AlMg0,7Si (Strangpress, Ausdehnungskoeffizient 2310-6 K-1) Werkstoff Rotor AlSi9Mg (Guss, Ausdehnungskoeffizient 2110-6 K-1) oder AlSi17Cu4Mg (Guss, Ausdehnungskoeffizient 1810-6K-1) Siliciumanteil Rotor mindestens 9%, besonders bevorzugt mehr als 15% Wärmeausdehnungskoeffizient Gehäuse/Rotor mindestens 5% größer, besonders bevorzugt 10% größer Zwischendruck zwischen dem saugseitigen und dem druckseitigen Ver-drängungselement: Particularly good results according to the invention could be achieved with the following configuration, which is therefore particularly preferred: Housing material AlSi7Mg (cast, expansion coefficient 22 10 -6 K -1 or AlMg0.7Si (extrusion, expansion coefficient 23 10 -6 K -1 ) Material rotor AlSi9Mg (cast iron, coefficient of expansion 21 10 -6 K -1 ) or AlSi17Cu4Mg (cast iron, coefficient of expansion 18 10 -6 K -1 ) Silicon content rotor at least 9%, particularly preferably more than 15% Coefficient of thermal expansion Housing / rotor at least 5% larger, particularly preferably 10% larger Intermediate pressure between the suction-side and the pressure-side displacement element:

DruckverhältnisPressure ratio Auslassdruck/Zwischend ruckOutlet pressure / intermediate pressure

Besonders bevorzugt weniger als: 1000 mbar 200 mbar = 5

Figure imgb0001
Zwischendruck = 20% Auslassdruck Particularly preferably less than: 1000 mbar 200 mbar = 5
Figure imgb0001
Intermediate pressure = 20% outlet pressure

Insbesondere weniger als 1000 mbar 100 mbar = 10

Figure imgb0002
Zwischendruck = 10% Auslassdruck weniger als 1000 mbar 50 mbar = 20
Figure imgb0003
Zwischendruck = 5% Auslassdruck
Kaltspalt Höhe 0,05 mm - 0,3 mm Besonders bevorzugt 0,1 mm - 0,2 mm In particular less than 1000 mbar 100 mbar = 10
Figure imgb0002
Intermediate pressure = 10% outlet pressure
less than 1000 mbar 50 mbar = 20
Figure imgb0003
Intermediate pressure = 5% outlet pressure
Cold gap height 0.05 mm - 0.3 mm Particularly preferably 0.1 mm - 0.2 mm

Claims (15)

  1. A screw-type vacuum pump, comprising
    a housing (26) defining a suction chamber, wherein the housing (26) is made of aluminum or an aluminum alloy,
    two screw rotors arranged in said suction chamber (46), each comprising at least one displacer element (10, 12) having a helical recess for forming several windings, wherein the at least one displacer element (10, 12) is made of aluminum or an aluminum alloy,
    characterized in that
    in case of a prevailing suction pressure of less than 200 mbar (absolute pressure) between the region in which 5% to 20% of the outlet pressure prevail and a pressure-side rotor end (pump outlet) at least six, particularly at least eight and with particular preference at least ten windings are provided, and
    that the one displacer element is formed as a pressure-side displacer element (12) and at least one further displacer element (10) is provided per screw rotor, wherein the recesses of the displacer elements (10, 12) each have the same contour along the entire length.
  2. The screw-type vacuum pump of claim 1, characterized in that the pressure-side displacer element (12) effects a pressure ratio of less than 20, particularly less than 10 and with particular preference less than 5.
  3. The screw-type vacuum pump of claim 1 or 2, characterized in that the pressure-side displacer element (12) at a minimum of 6, particularly at a minimum of 8 and with particular preference at a minimum of 10 windings has an average working pressure of more than 50 mbar.
  4. The screw-type vacuum pump of claim 1 to 3, characterized in that between a surface (42) of the displacer element (12) and an inner surface (44) of the suction chamber (46) a gap is formed having a height in the range from 0.05 mm to 0.3 mm, particularly from 0.05 mm to 0.2 mm.
  5. The screw-type vacuum pump of one of claim 1 to 4, characterized in that the pressure-side displacer elements (12) comprise a constant pitch and/or a uniform symmetric contour along their entire length.
  6. The screw-type vacuum pump of one of claim 1 to 5, characterized in that the recesses of the pressure-side displacer elements (12) comprise a uniform symmetric contour along their entire length.
  7. The screw-type vacuum pump of one of claim 1 to 6, characterized in that each screw rotor comprises a rotor shaft carrying the at least two displacer elements (10, 12).
  8. The screw-type vacuum pump of one of claim 1 to 7, characterized in that a screw rotor made of aluminum or an aluminum alloy has a low expansion coefficient of and particularly of less than 22*10-61/K and with particular preference of less than 20*10-61/K.
  9. The screw-type vacuum pump of one of claim 1 to 8, characterized in that the screw rotor and particularly the at least one displacer element (10, 12) comprise a lower expansion coefficient per screw rotor than the housing (26), wherein the expansion coefficient of the housing (26) is particularly at least larger than the expansion coefficient of the screw rotors and of the at least one displacer element (10, 12), respectively.
  10. The screw-type vacuum pump of one of claim 1 to 9, characterized in that the screw rotors do not comprise a rotor internal cooling.
  11. The screw-type vacuum pump of one of claim 1 to 10, characterized in that the screw rotors do not comprise channels with particularly liquid coolant flowing through them.
  12. The screw-type vacuum pump of one of claim 1 to 11, characterized in that the screw rotors are configured to be solid.
  13. The screw-type vacuum pump of one of claim 1 to 12, characterized in that in normal operation a temperature difference in the region of the pressure-side displacer elements (12) between said displacer elements and the housing (26) is smaller than 50 K and particularly smaller than 20 K.
  14. The screw-type vacuum pump of one of claim 1 to 13, characterized in that in the region of the pressure-side displacer elements (12) the average heat flux density is less than 20000 W/m2, preferably less than 15000 W/m2 and particularly less than 10000 W/m2.
  15. The screw-type vacuum pump of one of claim 1 to 14, characterized in that the distance from the region in which 5% to 20% of the outlet pressure prevail to the last winding of the pressure-side displacer element (12) is at least 20% to 30% of the rotor length.
EP17751761.2A 2016-08-30 2017-08-14 Screw-type vacuum pump Active EP3507495B1 (en)

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EP3507495A1 (en) 2019-07-10
CN109642573B (en) 2020-09-29

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