EP3133290B1 - Vacuum pump - Google Patents

Vacuum pump Download PDF

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Publication number
EP3133290B1
EP3133290B1 EP15181767.3A EP15181767A EP3133290B1 EP 3133290 B1 EP3133290 B1 EP 3133290B1 EP 15181767 A EP15181767 A EP 15181767A EP 3133290 B1 EP3133290 B1 EP 3133290B1
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EP
European Patent Office
Prior art keywords
rotor
stator
section
blades
vacuum pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP15181767.3A
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German (de)
French (fr)
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EP3133290A1 (en
Inventor
Florian Bader
Jan Hofmann
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Pfeiffer Vacuum GmbH
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Pfeiffer Vacuum GmbH
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Priority to EP15181767.3A priority Critical patent/EP3133290B1/en
Publication of EP3133290A1 publication Critical patent/EP3133290A1/en
Application granted granted Critical
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/042Turbomolecular vacuum pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/048Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps comprising magnetic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/059Roller bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/50Building or constructing in particular ways
    • F05D2230/53Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction

Definitions

  • the present invention relates to a vacuum pump, in particular a turbo molecular pump, with at least one rotor which has a rotor shaft and a plurality of rotor sections arranged on the rotor shaft, axially spaced along the rotor shaft, each comprising a plurality of rotor blades distributed in the circumferential direction, and at least one of the rotor associated stator, which has a plurality of stator sections each with a plurality of stator blades distributed in the circumferential direction, wherein a respective stator section is arranged in the axial direction between a first and a second rotor section and adjacent to these two rotor sections, and wherein between the first rotor section and a a first axial distance is provided for each stator section and a second axial distance is provided between the respective stator section and the second rotor section.
  • a plurality of rotor sections and a plurality of stator sections are provided, which are arranged alternately in the axial direction, a respective stator section being located centrally between two respectively adjacent rotor sections.
  • the rotor sections can each either be designed in one piece with the rotor shaft or be provided in the form of a separately manufactured rotor disk that is connected to the rotor shaft in a rotationally fixed manner.
  • a vacuum pump of the type mentioned in which the rotor can be adjusted in the axial direction via electromagnetic control means so that the axial distance of a respective rotor section to the stator section on one side is smaller than the axial distance of the respective Rotor section to the stator section on the other hand to adjust the distance on the one hand to a desired value. It remains open in which direction the rotor should be adjusted.
  • stator sections are each arranged between two adjacent rotor sections. The stator sections are each fixed directly to the pump housing or integrated in it.
  • stator sections are separated from one another by spacer rings and are each arranged between two rotor sections, from which they are at least substantially the same distance apart.
  • the object is achieved by a vacuum pump according to claim 1, and in particular in that the second axial distance is different from the first axial distance, the first rotor section being arranged in front of a respective stator section in the pumping direction and the second rotor section being arranged after the respective rotor section in the pumping direction is arranged, the first axial distance is smaller than the second distance and less than 0.7 times the second axial distance, and the two different distances of a respective stator section to the two adjacent rotor sections are defined by corresponding spacer rings between the individual stator sections .
  • the invention allows the arrangement of the rotor and stator sections to be adapted to the movement of the molecules to be conveyed, so that the pumping effect is improved.
  • the mode of operation of the invention is described below in particular with reference to FIG Fig. 2 explained in more detail.
  • the invention allows an existing construction of a vacuum pump to be improved by merely changing the position of the stator sections relative to the rotor sections. This can be achieved in a particularly simple way, e.g. by changing spacer rings between individual stator sections.
  • the invention thus improves the performance of a vacuum pump using particularly simple means, without the need to change the overall construction of the vacuum pump.
  • a respective stator section is arranged between two rotor sections adjacent to it.
  • a respective stator section and each of the two rotor sections adjacent to it are arranged directly one after the other in the respective axial direction.
  • No further stator or rotor sections are arranged between a respective stator section and a respective adjacent rotor section.
  • the respective stator section has an adjacent rotor section in both axial directions.
  • the first rotor section is arranged in front of a respective stator section in the pumping direction, while the second rotor section is arranged after the stator section in the pumping direction.
  • the first axial distance is smaller than that second axial distance.
  • the first axial distance in the pumping direction is smaller than the second axial distance in the pumping direction.
  • the first axial distance can be made as small as possible. A certain minimum distance greater than zero is maintained between a respective stator section and an adjacent rotor section.
  • the second axial distance can become relatively large by reducing the first axial distance, it has been shown that the second axial distance does not have such a strong influence on the pump output, so that the pump output is improved overall when the first axial distance is reduced.
  • the first axial distance is less than 0.7 times the second axial distance.
  • a particularly good pump performance has resulted.
  • Even better pump capacities can result if, according to one embodiment, the first axial distance is less than or equal to half the second axial distance.
  • the rotor shaft is mounted on the inlet side, in particular in a high vacuum area, by a lubrication-free bearing, in particular a magnetic bearing.
  • a lubrication-free bearing in particular a magnetic bearing.
  • the rotor shaft can alternatively or additionally on the outlet side, in particular in a medium or low vacuum range, by a lubricated bearing, in particular a roller bearing such as a ball bearing. This allows inexpensive storage with relatively little play, while the contamination problem on the outlet side is eliminated.
  • At least one rotor section is formed in one piece with the rotor shaft.
  • all rotor sections are designed in one piece with the rotor shaft.
  • a rotor configured in this way is also referred to as a full rotor.
  • at least one rotor section can be formed by a rotor disk produced separately from the rotor shaft and fastened to the rotor shaft.
  • all rotor sections can be formed by separately produced rotor disks. This is also referred to as a disk rotor.
  • At least one stator section is designed as a stator disk made from sheet metal.
  • the production of the stator disk and thus also that of the vacuum pump is technically simplified and more cost-effective.
  • the stator disk is stamped from sheet metal, which further simplifies the manufacturing process.
  • the rotor blades and the stator blades can each be inclined to a plane running at least essentially perpendicular to an axis of rotation, the rotor blades having an angle of attack and the stator blades having an angle of attack and the sum of the angle of attack of the stator blades and the angle of attack of the rotor blades at least substantially 90 ° is.
  • a respective stator blade in particular with a radially outer area, can be aligned at least substantially perpendicular to a respective rotor blade, in particular to its radially outer area.
  • the molecules to be conveyed move away primarily perpendicularly from a respective blade surface of the rotor in the direction of the stator section, as shown below with reference to FIG Fig. 2 explained in more detail. So if the stator blades are parallel to If the molecules are aligned in this direction of movement, they offer minimal resistance to the molecules and the pump performance is optimized.
  • the angle of incidence of the rotor blades is at least substantially 45 °, as a result of which the performance of the pump can be further improved.
  • An exemplary vacuum pump designed as a turbo molecular pump (not shown), which can be further developed by the invention and also by at least one of the embodiments disclosed here, comprises an inlet surrounded by an inlet flange and several pump stages for conveying the gas present at the inlet to an outlet .
  • the turbo molecular pump can have a side tap.
  • the turbomolecular pump comprises a stator with a static housing and a rotor, which is arranged in the housing and has a rotor shaft which is rotatably mounted about an axis of rotation.
  • the turbomolecular pump comprises several turbomolecular pump stages connected in series with one another for effective pumping, with several rotor sections connected to the rotor shaft, designed as turbomolecular rotor disks and with several stator sections arranged in the axial direction between the rotor disks and fixed in the housing, designed as turbomolecular stator disks, which are formed by spacer rings in one desired axial distance from each other are kept.
  • the rotor disks and stator disks provide an axial pumping action directed in the pumping direction in a pumping area.
  • the turbomolecular pump also comprises three Holweck pump stages which are arranged one inside the other in the radial direction and are connected in series with one another for effective pumping.
  • the rotor-side part of the Holweck pump stages comprises two cylinder-jacket-shaped Holweck rotor sleeves fastened to the rotor shaft and carried by the latter, which are oriented coaxially to the axis of rotation and are nested in one another.
  • two cylinder jacket-shaped Holweck stator sleeves are provided, which are also oriented coaxially to the axis of rotation and nested one inside the other.
  • the active pumping surfaces of the Holweck pump stages are each formed by the radial jacket surfaces lying opposite one another with the formation of a narrow radial Holweck gap, namely a Holweck rotor sleeve and a Holweck stator sleeve.
  • One of the active pumping surfaces is smooth, in the present case, for example, that of the Holweck rotor sleeve, the opposite, active pumping surface of the respective Holweck stator sleeve having a structure with grooves running helically around the axis of rotation in the axial direction, in which the rotation of the rotor, the gas is propelled and thereby pumped.
  • the rotatable mounting of the rotor shaft is brought about by a roller bearing in the area of the outlet and a permanent magnetic bearing in the area of the inlet.
  • the permanent magnetic bearing comprises a rotor-side bearing half and a stator-side bearing half, each of which comprises a ring stack of several permanent magnetic rings stacked on top of one another in the axial direction, the magnetic rings being opposite one another to form a radial bearing gap.
  • an emergency or safety bearing is provided, which is designed as an unlubricated roller bearing and runs empty during normal operation of the vacuum pump without contact and only comes into engagement with an excessive radial deflection of the rotor relative to the stator to create a radial stop for the rotor to form, which prevents a collision of the rotor-side structures with the stator-side structures.
  • a conical injection nut with an outer diameter that increases towards the roller bearing is provided on the rotor shaft, which is in sliding contact with a scraper of a plurality of absorbent disks soaked with an operating medium such as a lubricant.
  • an operating medium such as a lubricant.
  • the operating medium is transferred from the operating medium storage via the scraper to the rotating injection nut by capillary action and, as a result of the centrifugal force, is conveyed along the injection nut in the direction of the increasing outer diameter of the injection nut to the roller bearing, where it has a lubricating function, for example.
  • the turbo molecular pump comprises a drive motor for rotatingly driving the rotor, the rotor of which is formed by the rotor shaft.
  • a control unit controls the drive motor.
  • Fig. 1 shows a rotor shaft 14 of a rotor of a turbomolecular pump according to the invention, shown here only partially, with two rotor sections designed as rotor disks 16 being connected to the rotor shaft 14 in a rotationally fixed manner.
  • the respective rotor disk 16 has a plurality of rotor blades (not shown) which are arranged spaced apart in the circumferential direction.
  • stator section designed as a stator disk 22, which is not connected to the rotor shaft 14, but statically to a housing of the turbo molecular pump, not shown.
  • the stator disk 22 has a plurality of stator blades, likewise not shown, which are arranged spaced apart in the circumferential direction.
  • first axial distance A1 between the upper rotor disk 16 and the stator disk 22, and there is a second axial distance A2 between the stator disk 22 and the lower rotor disk 16.
  • the first axial distance A1 is smaller than the second axial distance A2.
  • the axial distance A1 is approximately 0.4 times the second axial distance A2. According to the invention, this distance ratio must be less than 0.7.
  • stator section is here arranged outside an axial center between the first rotor section, here the upper rotor disk 16, and the second rotor section, here the lower rotor disk 16.
  • stator section is arranged closer to one of the adjacent rotor sections, namely closer to the upper rotor disk 16, than to the respective other rotor section, viewed in the axial direction, that is, along the rotor shaft 14.
  • a pumping direction P describes a desired direction of movement of the gas molecules to be conveyed during a pumping process.
  • the intermediate space immediately following the upper rotor disk 16 in the pumping direction P, which is assigned to the first axial distance A1 is smaller than the second intermediate space in the pumping direction, which immediately follows the stator disk 22 and the second axial distance A2 is assigned. It may be desirable to make the first axial distance A1 as small as possible in order to further improve the pumping capacity of the turbo molecular pump.
  • rotor blades 18 and stator blades 24 are shown in simplified form, namely as a simplified developed view in the radial direction, ie in the direction of the rotor shaft 14 shown here only as a dashed line is arranged in front of a stator disk including the stator blades 24, also not shown in detail.
  • the rotor blades 18 move in at high speed during pumping Fig. 2 to the right (direction of rotation) while the stator blades 24 are fixed, ie not moving.
  • the rotor blades 18 and the stator blades 24 are arranged obliquely at a respective angle of attack of 45 °, the stator blades 24 being oriented obliquely opposite to the rotor blades 18.
  • the angle of attack is measured here in each case starting from a plane running perpendicular to the rotor shaft 14.
  • a molecule to be conveyed which gets into the axial area of the rotor blades 18, is to a certain extent captured by the obliquely downwardly directed surface of a rotor blade 18 moving rapidly to the right, the molecule being adsorbed on the surface. The molecule then desorbs from the surface, moving away from the rotor blade. The molecule adopts a preferred direction which is perpendicular to the surface from which the molecule was previously desorbed. In Fig.
  • stator blades 24 are also aligned perpendicular to the obliquely downwardly directed surfaces of the rotor blades 18, so that a molecule which moves in the preferred direction can pass parallel to the stator blades 24 and thus almost unhindered through the axially following stator disk 22, with only the - relatively small - thickness of the stator blades 24 opposing this movement.
  • the axial distance between the stator disk and the rotor disk following in the pumping direction has less of an influence on the pumping power. This is because here the molecule to be conveyed can be actively captured by the rotor disk, essentially regardless of its direction of movement, and thus transported further.
  • the pumping performance of the turbo molecular pump is therefore improved by the invention, in particular in the molecular working range.

Description

Die vorliegende Erfindung betrifft eine Vakuumpumpe, insbesondere Turbomolekularpumpe, mit wenigstens einem Rotor, der eine Rotorwelle und mehrere an der Rotorwelle angeordnete, axial längs der Rotorwelle beabstandete Rotorabschnitte aufweist, welche jeweils eine Mehrzahl von in Umfangsrichtung verteilt angeordneten Rotorschaufeln umfassen, und wenigstens einem dem Rotor zugeordneten Stator, der mehrere Statorabschnitte mit jeweils einer Mehrzahl von in Umfangsrichtung verteilt angeordneten Statorschaufeln aufweist, wobei ein jeweiliger Statorabschnitt in axialer Richtung zwischen einem ersten und einem zweiten Rotorabschnitt und zu diesen beiden Rotorabschnitten jeweils benachbart angeordnet ist, und wobei zwischen dem ersten Rotorabschnitt und einem jeweiligen Statorabschnitt ein erster axialer Abstand vorgesehen ist und zwischen dem jeweiligen Statorabschnitt und dem zweiten Rotorabschnitt ein zweiter axialer Abstand vorgesehen ist.The present invention relates to a vacuum pump, in particular a turbo molecular pump, with at least one rotor which has a rotor shaft and a plurality of rotor sections arranged on the rotor shaft, axially spaced along the rotor shaft, each comprising a plurality of rotor blades distributed in the circumferential direction, and at least one of the rotor associated stator, which has a plurality of stator sections each with a plurality of stator blades distributed in the circumferential direction, wherein a respective stator section is arranged in the axial direction between a first and a second rotor section and adjacent to these two rotor sections, and wherein between the first rotor section and a a first axial distance is provided for each stator section and a second axial distance is provided between the respective stator section and the second rotor section.

Typischerweise sind eine Vielzahl von Rotorabschnitten und eine Vielzahl von Statorabschnitten vorgesehen, die in axialer Richtung abwechselnd angeordnet sind, wobei ein jeweiliger Statorabschnitt sich mittig zwischen zwei jeweils benachbarten Rotorabschnitten befindet. Die Rotorabschnitte können jeweils entweder einstückig mit der Rotorwelle ausgebildet oder in Form einer separat hergestellten und drehfest mit der Rotorwelle verbundenen Rotorscheibe vorgesehen sein.Typically, a plurality of rotor sections and a plurality of stator sections are provided, which are arranged alternately in the axial direction, a respective stator section being located centrally between two respectively adjacent rotor sections. The rotor sections can each either be designed in one piece with the rotor shaft or be provided in the form of a separately manufactured rotor disk that is connected to the rotor shaft in a rotationally fixed manner.

In der JP 2000 257586 A ist eine Vakuumpumpe der eingangs genannten Art beschrieben, bei der der Rotor über elektromagnetische Steuermittel in axialer Richtung so verstellbar ist, dass der axiale Abstand eines jeweiligen Rotorabschnitts zu dem Statorabschnitt auf einer Seite kleiner ist als der axiale Abstand des jeweiligen Rotorabschnitts zu dem Statorabschnitt auf der anderen Seite, um den Abstand auf der einen Seite auf einen gewünschten Wert einzustellen. Es bleibt offen, in welcher Richtung der Rotor verstellt werden soll. Zudem sind nicht alle Statorabschnitte jeweils zwischen zwei benachbarten Rotorabschnitten angeordnet. Die Statorabschnitte sind jeweils unmittelbar am Pumpengehäuse festgelegt bzw. in diesem integriert.In the JP 2000 257586 A a vacuum pump of the type mentioned is described in which the rotor can be adjusted in the axial direction via electromagnetic control means so that the axial distance of a respective rotor section to the stator section on one side is smaller than the axial distance of the respective Rotor section to the stator section on the other hand to adjust the distance on the one hand to a desired value. It remains open in which direction the rotor should be adjusted. In addition, not all stator sections are each arranged between two adjacent rotor sections. The stator sections are each fixed directly to the pump housing or integrated in it.

Bei einer aus der EP 2 757 266 A1 bekannten Vakuumpumpe der eingangs genannten Art sind die Statorabschnitte über Distanzringe voneinander getrennt und jeweils zwischen zwei Rotorabschnitten angeordnet, von denen sie einen zumindest im Wesentlichen gleichen Abstand aufweisen.With one of the EP 2 757 266 A1 Known vacuum pumps of the type mentioned at the beginning, the stator sections are separated from one another by spacer rings and are each arranged between two rotor sections, from which they are at least substantially the same distance apart.

Es ist eine Aufgabe der Erfindung, die Leistung einer derartigen Vakuumpumpe zu verbessern.It is an object of the invention to improve the performance of such a vacuum pump.

Die Aufgabe wird durch eine Vakuumpumpe gemäß Anspruch 1 gelöst, und insbesondere dadurch, dass der zweite axiale Abstand von dem ersten axialen Abstand verschieden ist, wobei der erste Rotorabschnitt in Pumprichtung vor einem jeweiligen Statorabschnitt angeordnet ist und der zweite Rotorabschnitt in Pumprichtung nach dem jeweiligen Rotorabschnitt angeordnet ist, der erste axiale Abstand kleiner ist als der zweite Abstand und weniger als das 0,7-fache des zweiten axialen Abstands beträgt, und die beiden verschiedenen Abstände eines jeweiligen Statorabschnitts zu den beiden benachbarten Rotorabschnitten durch entsprechende Distanzringe zwischen den einzelnen Statorabschnitten definiert sind.The object is achieved by a vacuum pump according to claim 1, and in particular in that the second axial distance is different from the first axial distance, the first rotor section being arranged in front of a respective stator section in the pumping direction and the second rotor section being arranged after the respective rotor section in the pumping direction is arranged, the first axial distance is smaller than the second distance and less than 0.7 times the second axial distance, and the two different distances of a respective stator section to the two adjacent rotor sections are defined by corresponding spacer rings between the individual stator sections .

Durch die Erfindung lässt sich die Anordnung der Rotor- und Statorabschnitte an die Bewegung der zu fördernden Moleküle anpassen, sodass die Pumpwirkung verbessert wird. Die Wirkungsweise der Erfindung wird nachstehend insbesondere anhand von Fig. 2 näher erläutert.The invention allows the arrangement of the rotor and stator sections to be adapted to the movement of the molecules to be conveyed, so that the pumping effect is improved. The mode of operation of the invention is described below in particular with reference to FIG Fig. 2 explained in more detail.

Außerdem erlaubt die Erfindung, dass eine bestehende Konstruktion einer Vakuumpumpe dadurch verbessert werden kann, dass lediglich die Lage der Statorabschnitte relativ zu den Rotorabschnitten verändert wird. Dies kann z.B. durch veränderte Distanzringe zwischen einzelnen Statorabschnitten in besonders einfacher Weise realisiert werden. Die Erfindung verbessert also die Leistung einer Vakuumpumpe unter Einsatz besonders einfacher Mittel, ohne dass die Gesamtkonstruktion der Vakuumpumpe verändert werden muss.In addition, the invention allows an existing construction of a vacuum pump to be improved by merely changing the position of the stator sections relative to the rotor sections. This can be achieved in a particularly simple way, e.g. by changing spacer rings between individual stator sections. The invention thus improves the performance of a vacuum pump using particularly simple means, without the need to change the overall construction of the vacuum pump.

Ein jeweiliger Statorabschnitt ist zwischen zwei ihm benachbarten Rotorabschnitten angeordnet. Mit anderen Worten sind ein jeweiliger Statorabschnitt und jeder der beiden ihm benachbarten Rotorabschnitte in der jeweiligen axialen Richtung unmittelbar aufeinanderfolgend angeordnet. Zwischen einem jeweiligen Statorabschnitt und einem jeweiligen benachbarten Rotorabschnitt sind keine weiteren Stator- oder Rotorabschnitte angeordnet. Der jeweilige Statorabschnitt weist in beiden axialen Richtungen jeweils einen benachbarten Rotorabschnitt auf.A respective stator section is arranged between two rotor sections adjacent to it. In other words, a respective stator section and each of the two rotor sections adjacent to it are arranged directly one after the other in the respective axial direction. No further stator or rotor sections are arranged between a respective stator section and a respective adjacent rotor section. The respective stator section has an adjacent rotor section in both axial directions.

Im Stand der Technik wird davon ausgegangen, dass eine optimale Leistung der Vakuumpumpe erzielt wird, wenn der Statorabschnitt genau in der Mitte zwischen zwei benachbarten Rotorabschnitten angeordnet ist. Erfindungsgemäß wurde jedoch erkannt, dass der erste axiale Abstand und der zweite axiale Abstand einen unterschiedlichen Einfluss auf die Pumpwirkung haben können, sodass sich die Pumpwirkung durch unterschiedliche Wahl der beiden Abstände vorteilhaft beeinflussen lässt.In the prior art, it is assumed that optimum performance of the vacuum pump is achieved when the stator section is arranged exactly in the middle between two adjacent rotor sections. According to the invention, however, it was recognized that the first axial distance and the second axial distance can have a different influence on the pumping action, so that the pumping action can advantageously be influenced by different choices of the two distances.

Der erste Rotorabschnitt ist dabei in Pumprichtung vor einem jeweiligen Statorabschnitt angeordnet, während der zweite Rotorabschnitt in Pumprichtung nach dem Statorabschnitt angeordnet ist. Dabei ist der erste axiale Abstand kleiner als der zweite axiale Abstand. Mit anderen Worten ist also der in Pumprichtung erste axiale Abstand kleiner als der in Pumprichtung zweite axiale Abstand. Dabei kann der erste axiale Abstand möglichst klein ausgeführt sein. Dabei wird zwischen einem jeweiligen Statorabschnitt und einem benachbarten Rotorabschnitt ein gewisser Mindestabstand größer Null eingehalten. Obwohl durch Verkleinern des ersten axialen Abstands der zweite axiale Abstand relativ groß werden kann, hat sich gezeigt, dass der zweite axiale Abstand keinen so starken Einfluss auf die Pumpleistung ausübt, sodass insgesamt die Pumpleistung verbessert wird, wenn der erste axiale Abstand verkleinert wird.The first rotor section is arranged in front of a respective stator section in the pumping direction, while the second rotor section is arranged after the stator section in the pumping direction. The first axial distance is smaller than that second axial distance. In other words, the first axial distance in the pumping direction is smaller than the second axial distance in the pumping direction. The first axial distance can be made as small as possible. A certain minimum distance greater than zero is maintained between a respective stator section and an adjacent rotor section. Although the second axial distance can become relatively large by reducing the first axial distance, it has been shown that the second axial distance does not have such a strong influence on the pump output, so that the pump output is improved overall when the first axial distance is reduced.

Erfindungsgemäß beträgt der erste axiale Abstand weniger als das 0,7-fache des zweiten axialen Abstands. Bei dieser Ausgestaltung hat sich eine besonders gute Pumpleistung ergeben. Noch bessere Pumpleistungen können sich ergeben, wenn gemäß einer Ausführungsform der erste axiale Abstand kleiner als die oder gleich der Hälfte des zweiten axialen Abstands ist.According to the invention, the first axial distance is less than 0.7 times the second axial distance. In this embodiment, a particularly good pump performance has resulted. Even better pump capacities can result if, according to one embodiment, the first axial distance is less than or equal to half the second axial distance.

Bei einer weiteren Ausführungsform ist die Rotorwelle einlassseitig, insbesondere in einem Hochvakuumbereich, durch ein schmierungsfreies Lager, insbesondere ein Magnetlager, gelagert. Dadurch lässt sich die einlassseitige Lagerung nicht nur wartungsfrei ausführen, sondern eine Kontamination des Vakuums durch die Lagerung wird außerdem aufgrund fehlender Schmierstoffe verhindert.In a further embodiment, the rotor shaft is mounted on the inlet side, in particular in a high vacuum area, by a lubrication-free bearing, in particular a magnetic bearing. As a result, the storage on the inlet side can not only be carried out maintenance-free, but contamination of the vacuum by the storage is also prevented due to the lack of lubricants.

Die Rotorwelle kann alternativ oder zusätzlich auslassseitig, insbesondere in einem Mittel- oder Niedrigvakuumbereich, durch ein geschmiertes Lager, insbesondere ein Wälzlager wie z.B. ein Kugellager, gelagert sein. Dies erlaubt eine kostengünstige und mit relativ wenig Spiel behaftete Lagerung, während die Kontaminationsproblematik an der Auslassseite entfällt.The rotor shaft can alternatively or additionally on the outlet side, in particular in a medium or low vacuum range, by a lubricated bearing, in particular a roller bearing such as a ball bearing. This allows inexpensive storage with relatively little play, while the contamination problem on the outlet side is eliminated.

Bei einer Ausführungsform ist zumindest ein Rotorabschnitt mit der Rotorwelle einstückig ausgebildet ist. Insbesondere sind dabei alle Rotorabschnitte mit der Rotorwelle einstückig ausgebildet. Ein derart ausgestalteter Rotor wird auch als Vollrotor bezeichnet. Im Gegensatz dazu kann zumindest ein Rotorabschnitt durch eine separat von der Rotorwelle hergestellte und an der Rotorwelle befestigte Rotorscheibe gebildet sein. Insbesondere können alle Rotorabschnitte durch separat hergestellte Rotorscheiben gebildet sein. Man spricht hierbei auch von einem Scheibenrotor.In one embodiment, at least one rotor section is formed in one piece with the rotor shaft. In particular, all rotor sections are designed in one piece with the rotor shaft. A rotor configured in this way is also referred to as a full rotor. In contrast to this, at least one rotor section can be formed by a rotor disk produced separately from the rotor shaft and fastened to the rotor shaft. In particular, all rotor sections can be formed by separately produced rotor disks. This is also referred to as a disk rotor.

Bei einer weiteren Ausführungsform ist zumindest ein Statorabschnitt als aus Blech hergestellte Statorscheibe ausgeführt. Dadurch wird die Herstellung der Statorscheibe und damit auch jene der Vakuumpumpe technisch vereinfacht und kostengünstiger. Insbesondere ist die Statorscheibe aus Blech gestanzt, was den Herstellungsvorgang weiter vereinfacht.In a further embodiment, at least one stator section is designed as a stator disk made from sheet metal. As a result, the production of the stator disk and thus also that of the vacuum pump is technically simplified and more cost-effective. In particular, the stator disk is stamped from sheet metal, which further simplifies the manufacturing process.

Die Rotorschaufeln und die Statorschaufeln können jeweils zu einer zumindest im Wesentlichen senkrecht zu einer Rotationsachse verlaufenden Ebene schräg gestellt sein, wobei die Rotorschaufeln einen Anstellwinkel und die Statorschaufeln einen Anstellwinkel aufweisen und die Summe aus dem Anstellwinkel der Statorschaufeln und dem Anstellwinkel der Rotorschaufeln zumindest im Wesentlichen 90° beträgt. Mit anderen Worten kann eine jeweilige Statorschaufel, insbesondere mit einem radial äußeren Bereich, zumindest im Wesentlichen senkrecht zu einer jeweiligen Rotorschaufel, insbesondere zu deren radial äußerem Bereich, ausgerichtet sein. Die zu fördernden Moleküle entfernen sich vornehmlich senkrecht von einer jeweiligen Schaufelfläche des Rotors in Richtung des Statorabschnitts, wie unten anhand von Fig. 2 näher erläutert. Wenn also die Statorschaufeln parallel zu dieser Bewegungsrichtung der Moleküle ausgerichtet sind, setzen sie den Molekülen einen minimalen Widerstand entgegen und die Pumpleistung wird optimiert.The rotor blades and the stator blades can each be inclined to a plane running at least essentially perpendicular to an axis of rotation, the rotor blades having an angle of attack and the stator blades having an angle of attack and the sum of the angle of attack of the stator blades and the angle of attack of the rotor blades at least substantially 90 ° is. In other words, a respective stator blade, in particular with a radially outer area, can be aligned at least substantially perpendicular to a respective rotor blade, in particular to its radially outer area. The molecules to be conveyed move away primarily perpendicularly from a respective blade surface of the rotor in the direction of the stator section, as shown below with reference to FIG Fig. 2 explained in more detail. So if the stator blades are parallel to If the molecules are aligned in this direction of movement, they offer minimal resistance to the molecules and the pump performance is optimized.

Bei einer Ausführungsform der Erfindung beträgt der Anstellwinkel der Rotorschaufeln zumindest im Wesentlichen 45°, wodurch die Leistung der Pumpe weiter verbessert werden kann.In one embodiment of the invention, the angle of incidence of the rotor blades is at least substantially 45 °, as a result of which the performance of the pump can be further improved.

Weitere Ausführungsformen der Erfindung sind in den abhängigen Ansprüchen, der Beschreibung und den Figuren angegeben.Further embodiments of the invention are specified in the dependent claims, the description and the figures.

Die Erfindung wird nachfolgend lediglich beispielhaft unter Bezugnahme auf die schematische Zeichnung erläutert.

Fig. 1
zeigt eine erfindungsgemäße Anordnung zweier Rotorscheiben mit einer dazwischenliegenden Statorscheibe, und
Fig. 2
zeigt Rotor- und Statorschaufeln zur Veranschaulichung der Wirkungsweise der Erfindung.
The invention is explained below by way of example only with reference to the schematic drawing.
Fig. 1
shows an arrangement according to the invention of two rotor disks with a stator disk in between, and
Fig. 2
shows rotor and stator blades to illustrate the mode of operation of the invention.

Eine beispielhafte, als Turbomolekularpumpe ausgebildete Vakuumpumpe (nicht gezeigt), welche durch die Erfindung und auch durch zumindest eine der hier offenbarten Ausführungsformen weitergebildet werden kann, umfasst einen von einem Einlassflansch umgebenen Einlass sowie mehrere Pumpstufen zur Förderung des an dem Einlass anstehenden Gases zu einem Auslass. Die Turbomolekularpumpe kann eine seitliche Anzapfung aufweisen. Die Turbomolekularpumpe umfasst einen Stator mit einem statischen Gehäuse und einen in dem Gehäuse angeordneten Rotor mit einer um eine Rotationsachse drehbar gelagerten Rotorwelle.An exemplary vacuum pump designed as a turbo molecular pump (not shown), which can be further developed by the invention and also by at least one of the embodiments disclosed here, comprises an inlet surrounded by an inlet flange and several pump stages for conveying the gas present at the inlet to an outlet . The turbo molecular pump can have a side tap. The turbomolecular pump comprises a stator with a static housing and a rotor, which is arranged in the housing and has a rotor shaft which is rotatably mounted about an axis of rotation.

Die Turbomolekularpumpe umfasst mehrere pumpwirksam miteinander in Serie geschaltete turbomolekulare Pumpstufen mit mehreren mit der Rotorwelle verbundenen, als turbomolekulare Rotorscheiben ausgebildeten Rotorabschnitten und mit mehreren in axialer Richtung zwischen den Rotorscheiben angeordneten und in dem Gehäuse festgelegten, als turbomolekulare Statorscheiben ausgebildeten Statorabschnitten, die durch Distanzringe in einem gewünschten axialen Abstand zueinander gehalten sind. Die Rotorscheiben und Statorscheiben stellen in einem Schöpfbereich eine in Pumprichtung gerichtete axiale Pumpwirkung bereit.The turbomolecular pump comprises several turbomolecular pump stages connected in series with one another for effective pumping, with several rotor sections connected to the rotor shaft, designed as turbomolecular rotor disks and with several stator sections arranged in the axial direction between the rotor disks and fixed in the housing, designed as turbomolecular stator disks, which are formed by spacer rings in one desired axial distance from each other are kept. The rotor disks and stator disks provide an axial pumping action directed in the pumping direction in a pumping area.

Die Turbomolekularpumpe umfasst zudem drei in radialer Richtung ineinander angeordnete und pumpwirksam miteinander in Serie geschaltete Holweck-Pumpstufen. Der rotorseitige Teil der Holweck-Pumpstufen umfasst zwei an der Rotorwelle befestigte und von dieser getragene zylindermantelförmige Holweck-Rotorhülsen, die koaxial zu der Rotationsachse orientiert und ineinander geschachtelt sind. Ferner sind zwei zylindermantelförmige Holweck-Statorhülsen vorgesehen, die ebenfalls koaxial zu der Rotationsachse orientiert und ineinander geschachtelt sind. Die pumpaktiven Oberflächen der Holweck-Pumpstufen sind jeweils durch die einander unter Ausbildung eines engen radialen Holweck-Spalts gegenüberliegenden radialen Mantelflächen, nämlich jeweils einer Holweck-Rotorhülse und einer Holweck-Statorhülse, gebildet. Dabei ist jeweils eine der pumpaktiven Oberflächen glatt ausgebildet, im vorliegenden Fall beispielsweise die der Holweck-Rotorhülse, wobei die gegenüberliegende pumpaktive Oberfläche der jeweiligen Holweck-Statorhülse eine Strukturierung mit schraubenlinienförmig um die Rotationsachse herum in axialer Richtung verlaufenden Nuten aufweist, in denen durch die Rotation des Rotors das Gas vorangetrieben und dadurch gepumpt wird.The turbomolecular pump also comprises three Holweck pump stages which are arranged one inside the other in the radial direction and are connected in series with one another for effective pumping. The rotor-side part of the Holweck pump stages comprises two cylinder-jacket-shaped Holweck rotor sleeves fastened to the rotor shaft and carried by the latter, which are oriented coaxially to the axis of rotation and are nested in one another. Furthermore, two cylinder jacket-shaped Holweck stator sleeves are provided, which are also oriented coaxially to the axis of rotation and nested one inside the other. The active pumping surfaces of the Holweck pump stages are each formed by the radial jacket surfaces lying opposite one another with the formation of a narrow radial Holweck gap, namely a Holweck rotor sleeve and a Holweck stator sleeve. One of the active pumping surfaces is smooth, in the present case, for example, that of the Holweck rotor sleeve, the opposite, active pumping surface of the respective Holweck stator sleeve having a structure with grooves running helically around the axis of rotation in the axial direction, in which the rotation of the rotor, the gas is propelled and thereby pumped.

Die drehbare Lagerung der Rotorwelle wird durch ein Wälzlager im Bereich des Auslasses und ein Permanentmagnetlager im Bereich des Einlasses bewirkt.The rotatable mounting of the rotor shaft is brought about by a roller bearing in the area of the outlet and a permanent magnetic bearing in the area of the inlet.

Das Permanentmagnetlager umfasst eine rotorseitige Lagerhälfte und eine statorseitige Lagerhälfte, die jeweils einen Ringstapel aus mehreren in axialer Richtung aufeinander gestapelten permanentmagnetischen Ringen umfassen, wobei die Magnetringe unter Ausbildung eines radialen Lagerspalts einander gegenüberliegen.The permanent magnetic bearing comprises a rotor-side bearing half and a stator-side bearing half, each of which comprises a ring stack of several permanent magnetic rings stacked on top of one another in the axial direction, the magnetic rings being opposite one another to form a radial bearing gap.

Innerhalb des Permanentmagnetlagers ist ein Not- oder Fanglager vorgesehen, das als ungeschmiertes Wälzlager ausgebildet ist und im normalen Betrieb der Vakuumpumpe ohne Berührung leer läuft und erst bei einer übermäßigen radialen Auslenkung des Rotors gegenüber dem Stator in Eingriff gelangt, um einen radialen Anschlag für den Rotor zu bilden, der eine Kollision der rotorseitigen Strukturen mit den statorseitigen Strukturen verhindert.Inside the permanent magnetic bearing, an emergency or safety bearing is provided, which is designed as an unlubricated roller bearing and runs empty during normal operation of the vacuum pump without contact and only comes into engagement with an excessive radial deflection of the rotor relative to the stator to create a radial stop for the rotor to form, which prevents a collision of the rotor-side structures with the stator-side structures.

Im Bereich des Wälzlagers ist an der Rotorwelle eine konische Spritzmutter mit einem zu dem Wälzlager hin zunehmenden Außendurchmesser vorgesehen, die mit einem Abstreifer eines mehrere mit einem Betriebsmittel, wie z.B. einem Schmiermittel, getränkte saugfähige Scheiben umfassenden Betriebsmittelspeichers in gleitendem Kontakt steht. Im Betrieb wird das Betriebsmittel durch kapillare Wirkung von dem Betriebsmittelspeicher über den Abstreifer auf die rotierende Spritzmutter übertragen und infolge der Zentrifugalkraft entlang der Spritzmutter in Richtung des größer werdenden Außendurchmessers der Spritzmutter zu dem Wälzlager hin gefördert, wo es z.B. eine schmierende Funktion erfüllt.In the area of the roller bearing, a conical injection nut with an outer diameter that increases towards the roller bearing is provided on the rotor shaft, which is in sliding contact with a scraper of a plurality of absorbent disks soaked with an operating medium such as a lubricant. During operation, the operating medium is transferred from the operating medium storage via the scraper to the rotating injection nut by capillary action and, as a result of the centrifugal force, is conveyed along the injection nut in the direction of the increasing outer diameter of the injection nut to the roller bearing, where it has a lubricating function, for example.

Die Turbomolekularpumpe umfasst einen Antriebsmotor zum drehenden Antreiben des Rotors, dessen Läufer durch die Rotorwelle gebildet ist. Eine Steuereinheit steuert den Antriebsmotor an.The turbo molecular pump comprises a drive motor for rotatingly driving the rotor, the rotor of which is formed by the rotor shaft. A control unit controls the drive motor.

Fig. 1 zeigt eine Rotorwelle 14 eines hier nur teilweise dargestellten Rotors einer erfindungsgemäßen Turbomolekularpumpe, wobei mit der Rotorwelle 14 zwei als Rotorscheiben 16 ausgebildete Rotorabschnitte drehfest verbunden sind. Eine jeweilige Rotorscheibe 16 weist eine Mehrzahl von in Umfangsrichtung beabstandet angeordneten, nicht dargestellten Rotorschaufeln auf. Fig. 1 shows a rotor shaft 14 of a rotor of a turbomolecular pump according to the invention, shown here only partially, with two rotor sections designed as rotor disks 16 being connected to the rotor shaft 14 in a rotationally fixed manner. A The respective rotor disk 16 has a plurality of rotor blades (not shown) which are arranged spaced apart in the circumferential direction.

Zwischen den Rotorscheiben 16 ist ein als Statorscheibe 22 ausgebildeter Statorabschnitt angeordnet, welcher nicht mit der Rotorwelle 14, sondern statisch mit einem nicht dargestellten Gehäuse der Turbomolekularpumpe verbunden ist. Die Statorscheibe 22 weist eine Mehrzahl von in Umfangsrichtung beabstandet angeordneten, ebenfalls nicht dargestellten Statorschaufeln auf.Arranged between the rotor disks 16 is a stator section designed as a stator disk 22, which is not connected to the rotor shaft 14, but statically to a housing of the turbo molecular pump, not shown. The stator disk 22 has a plurality of stator blades, likewise not shown, which are arranged spaced apart in the circumferential direction.

Zwischen der oberen Rotorscheibe 16 und der Statorscheibe 22 besteht ein erster axialer Abstand A1 und zwischen der Statorscheibe 22 und der unteren Rotorscheibe 16 besteht ein zweiter axialer Abstand A2. Der erste axiale Abstand A1 ist kleiner als der zweite axiale Abstand A2. Hierbei beträgt der axiale Abstand A1 etwa das 0,4-fache des zweiten axialen Abstands A2. Dieses Abstandsverhältnis muss erfindungsgemäß kleiner als 0,7 sein.There is a first axial distance A1 between the upper rotor disk 16 and the stator disk 22, and there is a second axial distance A2 between the stator disk 22 and the lower rotor disk 16. The first axial distance A1 is smaller than the second axial distance A2. Here, the axial distance A1 is approximately 0.4 times the second axial distance A2. According to the invention, this distance ratio must be less than 0.7.

Der Statorabschnitt ist hier also, mit anderen Worten, außerhalb einer axialen Mitte zwischen dem ersten Rotorabschnitt, hier der oberen Rotorscheibe 16, und dem zweiten Rotorabschnitt, hier der unteren Rotorscheibe 16, angeordnet. Wiederum mit anderen Worten ist der Statorabschnitt in axialer Richtung, also längs der Rotorwelle 14, betrachtet näher an einem der benachbarten Rotorabschnitte, nämlich näher an der oberen Rotorscheibe 16, als an dem jeweils anderen Rotorabschnitt angeordnet.In other words, the stator section is here arranged outside an axial center between the first rotor section, here the upper rotor disk 16, and the second rotor section, here the lower rotor disk 16. Again, in other words, the stator section is arranged closer to one of the adjacent rotor sections, namely closer to the upper rotor disk 16, than to the respective other rotor section, viewed in the axial direction, that is, along the rotor shaft 14.

Eine Pumprichtung P beschreibt eine erwünschte Bewegungsrichtung von zu fördernden Gasmolekülen während eines Pumpvorgangs. Der in Pumprichtung P unmittelbar auf die obere Rotorscheibe 16 folgende Zwischenraum, welcher dem ersten axialen Abstand A1 zugeordnet ist, ist kleiner als der in Pumprichtung zweite Zwischenraum, welcher unmittelbar auf die Statorscheibe 22 folgt und dem zweiten axialen Abstand A2 zugeordnet ist. Dabei kann es wünschenswert sein, den ersten axialen Abstand A1 möglichst gering auszuführen, um die Pumpleistung der Turbomolekularpumpe weiter zu verbessern.A pumping direction P describes a desired direction of movement of the gas molecules to be conveyed during a pumping process. The intermediate space immediately following the upper rotor disk 16 in the pumping direction P, which is assigned to the first axial distance A1, is smaller than the second intermediate space in the pumping direction, which immediately follows the stator disk 22 and the second axial distance A2 is assigned. It may be desirable to make the first axial distance A1 as small as possible in order to further improve the pumping capacity of the turbo molecular pump.

Die Wirkungsweise der Erfindung soll nun anhand von Fig. 2 und eines vereinfachten physikalischen Modells genauer veranschaulicht werden.The mode of operation of the invention will now be based on Fig. 2 and a simplified physical model can be illustrated in more detail.

In Fig. 2 sind dazu Rotorschaufeln 18 und Statorschaufeln 24 vereinfacht dargestellt, und zwar als vereinfachte abgewickelte Ansicht in radialer Richtung, d.h. in Richtung auf die hier nur als gestrichelte Linie dargestellte Rotorwelle 14. Die Rotorschaufeln 18 sind Teil einer nicht näher dargestellten Rotorscheibe, welche in Pumprichtung P unmittelbar vor einer die Statorschaufeln 24 umfassenden, ebenfalls nicht näher dargestellten Statorscheibe angeordnet ist.In Fig. 2 rotor blades 18 and stator blades 24 are shown in simplified form, namely as a simplified developed view in the radial direction, ie in the direction of the rotor shaft 14 shown here only as a dashed line is arranged in front of a stator disk including the stator blades 24, also not shown in detail.

Die Rotorschaufeln 18 bewegen sich während des Pumpvorgangs mit hoher Geschwindigkeit in Fig. 2 nach rechts (Rotationsrichtung), während die Statorschaufeln 24 fest sind, d.h. sich nicht bewegen. Die Rotorschaufeln 18 sowie die Statorschaufeln 24 sind schräg unter einem jeweiligen Anstellwinkel von 45°angeordnet, wobei die Statorschaufeln 24 zu den Rotorschaufeln 18 entgegengesetzt schräg ausgerichtet sind. Der Anstellwinkel wird hierbei jeweils ausgehend von einer senkrecht zur Rotorwelle 14 verlaufenden Ebene gemessen.The rotor blades 18 move in at high speed during pumping Fig. 2 to the right (direction of rotation) while the stator blades 24 are fixed, ie not moving. The rotor blades 18 and the stator blades 24 are arranged obliquely at a respective angle of attack of 45 °, the stator blades 24 being oriented obliquely opposite to the rotor blades 18. The angle of attack is measured here in each case starting from a plane running perpendicular to the rotor shaft 14.

Ein zu förderndes Molekül, welches in den axialen Bereich der Rotorschaufeln 18 gerät, wird durch die schräg nach unten gerichtete Fläche einer sich schnell nach rechts bewegenden Rotorschaufel 18 gewissermaßen eingefangen, wobei das Molekül an der Fläche adsorbiert. Anschließend desorbiert das Molekül von der Fläche, wobei es sich von der Rotorschaufel entfernt. Dabei nimmt das Molekül eine Vorzugsrichtung an, welche senkrecht zu der Fläche steht, von welcher das Molekül zuvor desorbiert ist. In Fig. 2 sind auch die Statorschaufeln 24 senkrecht zu den schräg nach unten gerichteten Flächen der Rotorschaufeln 18 ausgerichtet, so dass ein Molekül, welches sich in der Vorzugsrichtung bewegt, parallel zu den Statorschaufeln 24 und somit nahezu ungehindert durch die axial nachfolgende Statorscheibe 22 hindurchtreten kann, wobei lediglich die - relativ geringe - Dicke der Statorschaufeln 24 dieser Bewegung entgegensteht.A molecule to be conveyed, which gets into the axial area of the rotor blades 18, is to a certain extent captured by the obliquely downwardly directed surface of a rotor blade 18 moving rapidly to the right, the molecule being adsorbed on the surface. The molecule then desorbs from the surface, moving away from the rotor blade. The molecule adopts a preferred direction which is perpendicular to the surface from which the molecule was previously desorbed. In Fig. 2 the stator blades 24 are also aligned perpendicular to the obliquely downwardly directed surfaces of the rotor blades 18, so that a molecule which moves in the preferred direction can pass parallel to the stator blades 24 and thus almost unhindered through the axially following stator disk 22, with only the - relatively small - thickness of the stator blades 24 opposing this movement.

Je weiter allerdings die Strecke ist, welche das Molekül nach der Desorption von der Rotorschaufel 18 beim Eintreten in den axialen Bereich der nachfolgenden Statorscheibe 22 bereits zurückgelegt hat, desto wahrscheinlicher weicht seine Bewegungsrichtung von der oben erwähnten Vorzugsrichtung ab. Dies wird zum Beispiel durch Stöße mit der Gehäusewand, der Rotorwelle oder anderen Molekülen begründet und kann auch als "Verwischen" bezeichnet werden. Erfindungsgemäß wurde erkannt, dass die Durchtrittswahrscheinlichkeit für ein jeweiliges zu förderndes Molekül steigt, wenn die Statorscheibe möglichst nahe an der Rotorscheibe angeordnet ist und dadurch mit hoher Wahrscheinlichkeit das Molekül nicht bereits eine von der Vorzugsrichtung abweichende Bewegungsrichtung aufweist, wenn es die Statorscheibe erreicht. Dagegen nimmt der axiale Abstand der Statorscheibe zur in Pumprichtung nachfolgenden Rotorscheibe weniger Einfluss auf die Pumpleistung. Denn hier kann das zu fördernde Molekül im Wesentlichen unabhängig von seiner Bewegungsrichtung durch die Rotorscheibe aktiv eingefangen und dadurch weitertransportiert werden. Die Pumpleistung der Turbomolekularpumpe wird also insbesondere im molekularen Arbeitsbereich durch die Erfindung verbessert.However, the further the distance that the molecule has already covered after desorption from the rotor blade 18 when entering the axial area of the following stator disk 22, the more likely its direction of movement will deviate from the preferred direction mentioned above. This is due, for example, to impacts with the housing wall, the rotor shaft or other molecules and can also be referred to as "blurring". According to the invention, it was recognized that the passage probability for a respective molecule to be conveyed increases if the stator disk is arranged as close as possible to the rotor disk and, as a result, there is a high probability that the molecule does not already have a direction of movement deviating from the preferred direction when it reaches the stator disk. In contrast, the axial distance between the stator disk and the rotor disk following in the pumping direction has less of an influence on the pumping power. This is because here the molecule to be conveyed can be actively captured by the rotor disk, essentially regardless of its direction of movement, and thus transported further. The pumping performance of the turbo molecular pump is therefore improved by the invention, in particular in the molecular working range.

BezugszeichenlisteList of reference symbols

1414th
RotorwelleRotor shaft
1616
RotorscheibeRotor disk
1818th
RotorschaufelRotor blade
2222nd
StatorscheibeStator disc
2424
StatorschaufelStator blade
PP.
PumprichtungPumping direction

Claims (9)

  1. A vacuum pump, in particular a turbomolecular pump, comprising
    at least one rotor which has a rotor shaft (14) and a plurality of rotor sections (16) which are arranged at the rotor shaft (14), which are axially spaced apart along the rotor shaft (14) and which each comprise a plurality of rotor blades (18) arranged distributed in the peripheral direction; and
    at least one stator which is associated with the rotor and which has a plurality of stator sections (22) which each have a plurality of stator blades (24) arranged distributed in the peripheral direction,
    wherein a respective stator section (22) is arranged in the axial direction between a first and a second rotor section (16) and is in each case arranged adjacent to these two rotor sections (16),
    wherein a first axial spacing (A1) is provided between the first rotor section (16) and a respective stator section (22) and a second axial spacing (A2) is provided between the respective stator section (22) and the second rotor section (16),
    wherein the second axial spacing (A2) is different from the first axial spacing (A1),
    wherein the first rotor section (16) is arranged before a respective stator section (22) in the pump direction (P) and the second rotor section (16) is arranged after the respective stator section (22) in the pump direction (P), wherein the first axial spacing (A1) is smaller than the second axial spacing (A2), characterized in that the first axial spacing (A1) amounts to less than 0.7 times the second axial spacing (A2);
    and in that the two different spacings (A1, A2) of a respective stator section (22) from the two adjacent rotor sections (16) are defined by corresponding spacer rings between the individual stator sections (22).
  2. A vacuum pump in accordance with claim 1,
    characterized in that
    the first axial spacing (A1) is smaller than half the second axial spacing (A2).
  3. A vacuum pump in accordance with claim 1 or claim 2,
    characterized in that
    the rotor shaft (14) is supported at the inlet side by a lubrication-free bearing, in particular a magnetic bearing.
  4. A vacuum pump in accordance with any one of the preceding claims,
    characterized in that
    the rotor shaft (14) is supported at the outlet side by a lubricated bearing, in particular a roller element bearing.
  5. A vacuum pump in accordance with any one of the preceding claims,
    characterized in that
    at least one rotor section (16) is formed in one piece with the rotor shaft (14).
  6. A vacuum pump in accordance with any one of the preceding claims,
    characterized in that
    at least one stator section (22) is designed as a stator disk produced from sheet metal.
  7. A vacuum pump in accordance with claim 6,
    characterized in that
    the stator disk is stamped from sheet metal.
  8. A vacuum pump in accordance with any one of the preceding claims,
    characterized in that
    the rotor blades (18) and the stator blades (24) are each inclined with respect to a plane extending at least substantially perpendicular to an axis of rotation (R), with the rotor blades (18) having a blade angle and the stator blades (24) having a blade angle and the sum of the blade angle of the stator blades (24) and the blade angle of the rotor blades (18) amounting to at least substantially 90°.
  9. A vacuum pump in accordance with claim 8,
    characterized in that
    the blade angle of the rotor blades (18) amounts to at least substantially 45°.
EP15181767.3A 2015-08-20 2015-08-20 Vacuum pump Active EP3133290B1 (en)

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DE29516599U1 (en) * 1995-10-20 1995-12-07 Leybold Ag Friction vacuum pump with intermediate inlet
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