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EP3032106B1 - Vacuum pump - Google Patents

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Publication number
EP3032106B1
EP3032106B1 EP15177253.0A EP15177253A EP3032106B1 EP 3032106 B1 EP3032106 B1 EP 3032106B1 EP 15177253 A EP15177253 A EP 15177253A EP 3032106 B1 EP3032106 B1 EP 3032106B1
Authority
EP
European Patent Office
Prior art keywords
rotor
stator
pump
vacuum pump
pure
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
EP15177253.0A
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German (de)
French (fr)
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EP3032106A1 (en
Inventor
Jan Hofmann
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.)
Pfeiffer Vacuum GmbH
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Pfeiffer Vacuum GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from DE102014118083.6A external-priority patent/DE102014118083A1/en
Application filed by Pfeiffer Vacuum GmbH filed Critical Pfeiffer Vacuum GmbH
Priority to EP15177253.0A priority Critical patent/EP3032106B1/en
Priority to JP2015238692A priority patent/JP6138897B2/en
Publication of EP3032106A1 publication Critical patent/EP3032106A1/en
Application granted granted Critical
Publication of EP3032106B1 publication Critical patent/EP3032106B1/en
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Classifications

    • 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
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers

Definitions

  • the present invention relates to a vacuum pump, in particular a turbomolecular pump.
  • An exemplary turbomolecular vacuum pump comprises a rotor with a rotor shaft on which a plurality of rotor disks are arranged axially offset. Each rotor disk has a plurality of rotor blades arranged distributed in the circumferential direction.
  • the exemplary turbomolecular pump comprises a stator with a plurality of stator disks, each of which comprises a plurality of stator blades arranged distributed in the circumferential direction.
  • the rotor disks and the stator disks are arranged alternately in the axial direction.
  • the exemplary turbomolecular pump has certain vacuum performance values, such as Pumping speed and compression ratio, which are set at a target speed of the rotor.
  • vacuum performance values such as Pumping speed and compression ratio
  • customer requirements regarding vacuum performance values can vary widely. In practice, therefore, many different vacuum pump models are kept available for different requirements, or a vacuum pump is complexly adapted to special requirements or even specifically developed accordingly.
  • WO 2005/033521 A1 a vacuum pump which has a second inlet or a lateral tap in the area of a helical element of a rotor.
  • a vacuum pump according to claim 1 and claim 5, and in particular in that at least one pure rotor area is provided in an axial area of the rotor, into which no lateral tap opens, in which at least two rotor sections follow one another without an intermediate stator section, or at least a pure stator area is provided, in which at least two stator sections follow one another without an intermediate rotor section.
  • an axial distance is provided between the two rotor sections of the pure rotor area or between the two stator sections of the pure stator area.
  • one or more rotor sections and / or stator sections are therefore missing compared to the usual structure of a vacuum pump, in which the rotor and stator sections are arranged alternately in the axial direction.
  • stator or rotor sections are deliberately omitted.
  • the rotor and stator sections are, in particular, so-called rotor or stator disks, each of which has a plurality of rotor or stator blades arranged distributed in the circumferential direction and have a disk shape insofar as they have a height measured in the axial direction, which is smaller and in particular much smaller than their diameter.
  • the rotor and stator sections are in particular stacked one above the other, alternately in the prior art, ie on a stator disk follows a rotor disc and vice versa.
  • turbomolecular pump with alternately arranged rotor and stator sections is assumed, as is known per se in the prior art.
  • This turbomolecular pump has certain vacuum performance values. If there are now demands on the turbomolecular pump which differ from the vacuum performance values of the pump, for example lower, only one or more rotor and / or stator sections are removed or omitted during assembly. As a result, the performance values of the pump that are possible within the framework of the construction of the turbomolecular pump are changed, e.g. reduced. However, this allows the requirements to be met in a very simple manner, while the pump does not have to be changed in construction.
  • stator section in the vacuum pump also fulfills structural tasks in addition to its vacuum function
  • stator section can be replaced by a replacement piece for the structural tasks, such as a spacer, in the pure rotor area.
  • a replacement piece for the structural tasks such as a spacer
  • the invention is An axial distance is therefore provided between the two rotor sections of the pure rotor area.
  • the vacuum pump has at least one side tap.
  • the side tap is different from an inlet and an outlet of the vacuum pump.
  • the invention can be used in a targeted manner in order to individually set the vacuum performance values of pump areas in front of and behind the tap.
  • the achievable pressure in a chamber connected to the side tap in which e.g. a larger amount of residual gas is permitted or desired, can be set specifically.
  • a complex design change of the vacuum pump is not necessary.
  • the lateral tap can be provided in at least one area of the rotor.
  • the lateral tap can be arranged between an inlet and an outlet of the vacuum pump.
  • the pure rotor region can be arranged in the axial direction directly in front of or behind the side tap or close to a side tap.
  • the vacuum pump can also have no side tap.
  • a stator section is arranged in the axial direction between the first rotor section in the pumping direction and the second rotor section in the pumping direction.
  • the rotor sections are each formed by a rotor disk which is produced separately from the rotor shaft and is fastened to the rotor shaft.
  • it can be a disk rotor.
  • a full rotor can be provided, in which the rotor sections are connected in one piece to the rotor shaft.
  • the vacuum pump shown as a turbomolecular pump 10 comprises an inlet 30 surrounded by an inlet flange 31 and a plurality of pump stages for conveying the gas present at the inlet 30 to an outlet.
  • the outlet is in Fig. 1 not shown (see, for example, the outlet 32 of Fig. 2 pump shown).
  • the turbomolecular pump 10 has no lateral tapping.
  • the turbomolecular pump 10 comprises a stator with a static housing 36 and a rotor 12 arranged in the housing 36 with a rotor shaft 14 which is rotatably mounted about an axis of rotation R.
  • the turbomolecular pump 10 comprises a plurality of turbomolecular pump stages, which are connected to one another in series with effective pumping, with a plurality of rotor sections connected to the rotor shaft 14, designed as turbomolecular rotor disks 16, and with a plurality of stator sections arranged in the axial direction between the rotor disks 16 and fixed in the housing 36 and designed as a turbomolecular stator disks 22 by spacer rings 40 in a desired axial distance from each other.
  • the rotor disks 16 and stator disks 22 provide an axial pumping action directed in the pumping direction P in a scoop area.
  • the turbomolecular pump 10 also comprises three Holweck pump stages which are arranged one inside the other in the radial direction and have a pumping effect and are connected in series with one another.
  • the rotor-side part of the Holweck pump stages comprises two Holweck rotor sleeves 46, 48 fastened to and supported by the rotor shaft 14, which are oriented coaxially to the axis of rotation R and nested one inside the other.
  • two cylindrical jacket-shaped Holweck stator sleeves 50, 52 are provided, which are also oriented coaxially to the axis of rotation R and are nested one inside the other.
  • the pump-active surfaces of the Holweck pump stages are each formed by the radial lateral surfaces opposite one another with the formation of a narrow radial Holweck gap, namely a Holweck rotor sleeve 46, 48 and a Holweck stator sleeve 50, 52, respectively.
  • one of the pump-active surfaces is smooth, in the present case, for example, that of the Holweck rotor sleeve 46 or 48, the opposite pump-active surface of the respective Holweck stator sleeve 50 or 52 being structured with a helix around the axis of rotation R in the axial direction has extending grooves in which the gas is propelled by the rotation of the rotor 12 and thereby pumped.
  • the rotatable mounting of the rotor shaft 14 is effected by a roller bearing 54 in the area of the outlet and a permanent magnet bearing 56 in the area of the inlet 30.
  • the permanent magnet bearing 56 comprises a rotor-side bearing half 60 and a stator-side bearing half 58, each of which comprises an annular stack of a plurality of permanent magnetic rings stacked on one another in the axial direction, wherein the magnetic rings face each other, forming a radial bearing gap.
  • an emergency or catch bearing 62 is provided, which is designed as an unlubricated roller bearing and runs empty without contact during normal operation of the vacuum pump and only comes into engagement with an radial radial deflection of the rotor 12 with respect to the stator in order to make a radial stop to form for the rotor 12, which prevents a collision of the rotor-side structures with the stator-side structures.
  • a conical injection nut 64 with an external diameter increasing towards the roller bearing 54 is provided on the rotor shaft 14, which is connected to one scraper by a plurality of devices, such as a lubricant, impregnated absorbent discs 66 comprising operating fluid storage is in sliding contact.
  • the operating medium is transferred by capillary action from the operating medium storage via the wiper to the rotating injection nut 64 and, as a result of the centrifugal force along the injection nut 64, is conveyed in the direction of the increasing outer diameter of the injection nut 64 to the roller bearing 54, where it is e.g. fulfills a lubricating function.
  • the turbomolecular pump 10 comprises a drive motor 68 for rotatingly driving the rotor, the rotor of which is formed by the rotor shaft 14.
  • a control unit (not shown) controls the drive motor 68.
  • the turbomolecular group 10 of the Fig. 1 comprises a pure rotor region 28 and a pure stator region 29.
  • two rotor disks 16 follow one another without an interposed stator disk 22.
  • a stator disk 22 is therefore missing between the rotor disks 16.
  • a rotor disk 16 between the stator disks 22 is accordingly missing here.
  • the two rotor disks 16 in the pure rotor area 28 and the two stator disks 22 in the pure stator area 29 are each arranged at an axial distance from one another.
  • a respective stator disk 22 is designed in the form of two half rings which can be placed between the rotor disks 16 from the side, that is to say in the radial direction.
  • the stator disks 22 are placed on the spacer rings 40 and carried by them. Individual stator disks 22 can thereby be removed or omitted particularly easily in order to adapt the turbomolecular pump 10 in terms of its vacuum performance values to specific requirements.
  • FIG. 2 A further turbomolecular pump 10 is shown which, however, has a lateral tap 26.
  • the side tap 26 is provided for connecting an additional vacuum chamber, not shown, in which a vacuum of a different quality is to be set than is the case in a chamber connected to the inlet 30.
  • the lateral tap 26 defines a tap region 34 of the rotor 12, into which the lateral tap 26 opens.
  • No stator disks 22 are arranged in the tapping area 34.
  • a large axial distance is provided between the rotor disks 16, which delimit the tapping area, which essentially corresponds to the axial extent of the tapping area 34.
  • the tapping area 34 is therefore kept free of pump-active elements.
  • a pure rotor area 28 is provided in an axial area of the rotor 12, into which no lateral tapping opens.
  • the pure rotor area 28 here comprises three successive rotor disks 16 without stator disks 22 lying between them.
  • the pure rotor area 28 is arranged directly in front of the tapping area 34 in the pumping direction P.
  • a stator disk 22 is arranged in the pumping direction P between the first rotor disk 16 and the second rotor disk 16.
  • the turbomolecular pump 10 has rotor disks 16 and stator disks 22 arranged alternately in the axial direction.
  • FIG. 3 Another turbomolecular pump 10 is shown with a side tap. However, the side tap is not visible in the view shown.
  • the lateral tap defines a tap area 34, in which no stator disks 22 are arranged.
  • a pure rotor area 28 is provided, in which no stator disks 22 are likewise arranged.
  • a stator disk 22 is arranged between the first pair of rotor disks 16 in the pumping direction.
  • rotor disks 16 and stator disks 22 are provided in the alternating arrangement known per se.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Non-Positive Displacement Air Blowers (AREA)

Description

Die vorliegende Erfindung betrifft eine Vakuumpumpe, insbesondere Turbomolekularpumpe.The present invention relates to a vacuum pump, in particular a turbomolecular pump.

Eine beispielhafte Turbomolekular-Vakuumpumpe umfasst einen Rotor mit einer Rotorwelle, auf der mehrere Rotorscheiben axial versetzt angeordnet sind. Eine jeweilige Rotorscheibe weist eine Mehrzahl von in Umfangsrichtung verteilt angeordneten Rotorschaufeln auf. Daneben umfasst die beispielhafte Turbomolekularpumpe einen Stator mit einer Mehrzahl von Statorscheiben, welche jeweils eine Mehrzahl von in Umfangsrichtung verteilt angeordneten Statorschaufeln umfassen. Bei dieser beispielhaften Turbomolekular-Vakuumpumpe sind in axialer Richtung die Rotorscheiben und die Statorscheiben abwechselnd angeordnet.An exemplary turbomolecular vacuum pump comprises a rotor with a rotor shaft on which a plurality of rotor disks are arranged axially offset. Each rotor disk has a plurality of rotor blades arranged distributed in the circumferential direction. In addition, the exemplary turbomolecular pump comprises a stator with a plurality of stator disks, each of which comprises a plurality of stator blades arranged distributed in the circumferential direction. In this exemplary turbomolecular vacuum pump, the rotor disks and the stator disks are arranged alternately in the axial direction.

Die beispielhafte Turbomolekularpumpe besitzt bestimmte vakuumtechnische Leistungswerte, wie z.B. Saugvermögen und Kompressionsverhältnis, welche sich bei einer Solldrehzahl des Rotors einstellen. Kundenanforderungen bezüglich der vakuumtechnischen Leistungswerte können jedoch höchst unterschiedlich sein. In der Praxis werden daher für unterschiedliche Anforderungen viele verschiedene Vakuumpumpenmodelle vorgehalten oder eine Vakuumpumpe wird aufwändig konstruktiv an besondere Anforderungen angepasst oder sogar gezielt entsprechend entwickelt.The exemplary turbomolecular pump has certain vacuum performance values, such as Pumping speed and compression ratio, which are set at a target speed of the rotor. However, customer requirements regarding vacuum performance values can vary widely. In practice, therefore, many different vacuum pump models are kept available for different requirements, or a vacuum pump is complexly adapted to special requirements or even specifically developed accordingly.

Aus der EP 1 850 011 A2 ist eine Vakuumpumpe gemäß dem Oberbegriff des Anspruchs 1 bekannt.From the EP 1 850 011 A2 a vacuum pump according to the preamble of claim 1 is known.

Ferner beschreibt die WO 2005/033521 A1 eine Vakuumpumpe, die im Bereich eines helikalen Elements eines Rotors einen zweiten Einlass bzw. eine seitliche Anzapfung aufweist.Furthermore describes the WO 2005/033521 A1 a vacuum pump which has a second inlet or a lateral tap in the area of a helical element of a rotor.

Es ist eine Aufgabe der Erfindung, unterschiedliche Anforderungen an eine Vakuumpumpe auf einfachem Wege zu erfüllen.It is an object of the invention to easily meet different requirements for a vacuum pump.

Diese Aufgabe wird durch eine Vakuumpumpe gemäß Anspruch 1 und Anspruch 5 gelöst, und insbesondere dadurch, dass in einem axialen Bereich des Rotors, in den keine seitliche Anzapfung mündet, zumindest ein reiner Rotorbereich vorgesehen ist, in welchem wenigstens zwei Rotorabschnitte ohne dazwischenliegenden Statorabschnitt aufeinanderfolgen, oder zumindest ein reiner Statorbereich vorgesehen ist, in welchem wenigstens zwei Statorabschnitte ohne dazwischenliegenden Rotorabschnitt aufeinanderfolgen. Erfindungsgemäß ist zwischen den zwei Rotorabschnitten des reinen Rotorbereichs oder zwischen den zwei Statorabschnitten des reinen Statorbereichs ein axialer Abstand vorgesehen.This object is achieved by a vacuum pump according to claim 1 and claim 5, and in particular in that at least one pure rotor area is provided in an axial area of the rotor, into which no lateral tap opens, in which at least two rotor sections follow one another without an intermediate stator section, or at least a pure stator area is provided, in which at least two stator sections follow one another without an intermediate rotor section. According to the invention, an axial distance is provided between the two rotor sections of the pure rotor area or between the two stator sections of the pure stator area.

Jeweils einzelne oder mehrere Rotorabschnitte und/oder Statorabschnitte fehlen also gegenüber dem gewöhnlichen Aufbau einer Vakuumpumpe, bei dem Rotor- und Statorabschnitte in axialer Richtung abwechselnd angeordnet sind.In each case, one or more rotor sections and / or stator sections are therefore missing compared to the usual structure of a vacuum pump, in which the rotor and stator sections are arranged alternately in the axial direction.

Mit anderen Worten können also erfindungsgemäß z.B. gegenüber einem nicht erfindungsgemäßen Pumpenaufbau jeweils ein oder mehrere Stator- bzw. Rotorabschnitte gezielt weggelassen werden.In other words, according to the invention, e.g. compared to a pump structure not according to the invention, one or more stator or rotor sections are deliberately omitted.

Bei den Rotor- und Statorabschnitten handelt es sich insbesondere um so genannte Rotor- bzw. Statorscheiben, die jeweils eine Mehrzahl von in Umfangsrichtung verteilt angeordneten Rotor- bzw. Statorschaufeln aufweisen und insofern eine Scheibenform aufweisen, als sie eine in axialer Richtung gemessene Höhe aufweisen, die kleiner und insbesondere wesentlich kleiner ist als deren Durchmesser. Die Rotor- und Statorabschnitte sind insbesondere stapelartig übereinander angeordnet, im Stand der Technik abwechselnd, d.h. auf eine Statorscheibe folgt eine Rotorscheibe und umgekehrt. In einer erfindungsgemäßen Ausführungsform dagegen kann also vorgesehen sein, dass in einem reinen Rotorbereich wenigstens zwei Rotorscheiben ohne dazwischenliegende Statorscheibe aufeinanderfolgen, während bei einem reinen Statorbereich wenigstens zwei Statorscheiben ohne dazwischenliegende Rotorscheibe aufeinanderfolgen.The rotor and stator sections are, in particular, so-called rotor or stator disks, each of which has a plurality of rotor or stator blades arranged distributed in the circumferential direction and have a disk shape insofar as they have a height measured in the axial direction, which is smaller and in particular much smaller than their diameter. The rotor and stator sections are in particular stacked one above the other, alternately in the prior art, ie on a stator disk follows a rotor disc and vice versa. In contrast, in an embodiment according to the invention it can be provided that in a pure rotor area at least two rotor disks follow one another without an interposed stator disk, while in a pure stator area at least two stator disks follow one another without an interposed rotor disk.

Zur weiteren Verdeutlichung wird von einer beispielhaften Turbomolekularpumpe mit abwechselnd angeordneten Rotor- und Statorabschnitten ausgegangen, wie sie für sich im Stand der Technik bekannt ist. Diese Turbomolekularpumpe besitzt bestimmte vakuumtechnische Leistungswerte. Stellen sich nun Anforderungen an die Turbomolekularpumpe, welche von den vakuumtechnischen Leistungswerten der Pumpe abweichen, beispielsweise geringer sind, werden lediglich einzelne oder mehrere Rotor- und/oder Statorabschnitte entfernt oder bei der Montage weggelassen. Dadurch werden die im Rahmen der Konstruktion der Turbomolekularpumpe möglichen Leistungswerte der Pumpe zwar verändert, z.B. verringert. Allerdings lassen sich dadurch auf sehr einfache Weise die Anforderungen erfüllen, während die Pumpe nicht konstruktiv verändert werden muss. Dies ermöglicht es, mit einem einzigen Pumpenmodell nicht nur eine bestimmte Leistungscharakteristik anzubieten, sondern auch eine Vielzahl unterschiedlicher Leistungscharakteristika mit demselben Pumpenmodell zu verwirklichen. In der Folge müssen weniger unterschiedliche Pumpenmodelle vorgehalten werden und weniger konstruktive Anpassungen der Pumpen an Kundenanforderungen durchgeführt werden, während unterschiedlichste Kundenanforderungen dennoch bedient werden können.For further clarification, an exemplary turbomolecular pump with alternately arranged rotor and stator sections is assumed, as is known per se in the prior art. This turbomolecular pump has certain vacuum performance values. If there are now demands on the turbomolecular pump which differ from the vacuum performance values of the pump, for example lower, only one or more rotor and / or stator sections are removed or omitted during assembly. As a result, the performance values of the pump that are possible within the framework of the construction of the turbomolecular pump are changed, e.g. reduced. However, this allows the requirements to be met in a very simple manner, while the pump does not have to be changed in construction. This makes it possible not only to offer a specific performance characteristic with a single pump model, but also to implement a large number of different performance characteristics with the same pump model. As a result, fewer different pump models have to be kept in stock and fewer design adaptations of the pumps to customer requirements have to be carried out, while a wide variety of customer requirements can still be served.

Sofern ein Statorabschnitt in der Vakuumpumpe neben seiner vakuumtechnischen Funktion auch strukturelle Aufgaben erfüllt, kann der Statorabschnitt durch ein Ersatzstück für die strukturellen Aufgaben, wie z.B. ein Abstandsstück, in dem reinen Rotorbereich ersetzt werden. Generell und insbesondere unabhängig von dem Vorhandensein oder Nichtvorhandensein eines Ersatzstücks ist erfindungsgemäß zwischen den zwei Rotorabschnitten des reinen Rotorbereichs also ein axialer Abstand vorgesehen.If a stator section in the vacuum pump also fulfills structural tasks in addition to its vacuum function, the stator section can be replaced by a replacement piece for the structural tasks, such as a spacer, in the pure rotor area. In general, and in particular regardless of the presence or absence of a replacement part, the invention is An axial distance is therefore provided between the two rotor sections of the pure rotor area.

Es versteht sich, dass die vorstehende wie auch die folgenden Weiterbildungen, welche lediglich für einen oder mehrere reine Rotorbereiche beschrieben sind, entsprechend für reine Statorbereiche anwendbar sind. Hierdurch wird die Variationsvielfalt weiter verbessert.It goes without saying that the above and the following further developments, which are only described for one or more pure rotor areas, can be used correspondingly for pure stator areas. This further improves the variety.

Die Vakuumpumpe weist bei einer Ausführungsform zumindest eine seitliche Anzapfung auf. Die seitliche Anzapfung ist von einem Einlass und einem Auslass der Vakuumpumpe verschieden. Die Erfindung kann bei dieser Ausführungsform gezielt eingesetzt werden, um die vakuumtechnischen Leistungswerte von Pumpenbereichen vor und hinter der Anzapfung individuell einzustellen. Insbesondere kann dadurch der erreichbare Druck in einer an die seitliche Anzapfung angeschlossenen Kammer, in welcher z.B. eine größere Restgasmenge zulässig oder erwünscht ist, gezielt eingestellt werden. Eine aufwändige konstruktive Änderung der Vakuumpumpe ist dabei nicht notwendig.In one embodiment, the vacuum pump has at least one side tap. The side tap is different from an inlet and an outlet of the vacuum pump. In this embodiment, the invention can be used in a targeted manner in order to individually set the vacuum performance values of pump areas in front of and behind the tap. In particular, the achievable pressure in a chamber connected to the side tap, in which e.g. a larger amount of residual gas is permitted or desired, can be set specifically. A complex design change of the vacuum pump is not necessary.

Die seitliche Anzapfung kann in zumindest einem Bereich des Rotors vorgesehen sein. Alternativ oder zusätzlich kann die seitliche Anzapfung zwischen einem Einlass und einem Auslass der Vakuumpumpe angeordnet sein. Alternativ oder zusätzlich kann der reine Rotorbereich in axialer Richtung unmittelbar vor oder hinter der seitlichen Anzapfung oder nahe einer seitlichen Anzapfung angeordnet sein. Alternativ kann die Vakuumpumpe aber auch keine seitliche Anzapfung aufweisen.The lateral tap can be provided in at least one area of the rotor. Alternatively or additionally, the lateral tap can be arranged between an inlet and an outlet of the vacuum pump. As an alternative or in addition, the pure rotor region can be arranged in the axial direction directly in front of or behind the side tap or close to a side tap. Alternatively, the vacuum pump can also have no side tap.

Bei einer Ausführungsform ist in axialer Richtung zwischen dem in Pumprichtung ersten und dem in Pumprichtung zweiten Rotorabschnitt ein Statorabschnitt angeordnet. Dadurch werden weiterhin gute vakuumtechnische Leistungswerte erreicht, während die Pumpe an unterschiedliche Anforderungen angepasst werden kann.In one embodiment, a stator section is arranged in the axial direction between the first rotor section in the pumping direction and the second rotor section in the pumping direction. As a result, good vacuum performance values are still achieved, while the pump can be adapted to different requirements.

Bei einer weiteren Ausführungsform sind die Rotorabschnitte jeweils durch eine separat von der Rotorwelle hergestellte und an der Rotorwelle befestigte Rotorscheibe gebildet. Mit anderen Worten kann es sich also um einen Scheibenrotor handeln. Alternativ kann ein Vollrotor vorgesehen sein, bei dem die Rotorabschnitte einstückig mit der Rotorwelle verbunden sind.In a further embodiment, the rotor sections are each formed by a rotor disk which is produced separately from the rotor shaft and is fastened to the rotor shaft. In other words, it can be a disk rotor. Alternatively, a full rotor can be provided, in which the rotor sections are connected in one piece to the rotor shaft.

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

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

Fig. 1
zeigt eine Turbomolekularpumpe mit einem reinen Rotorbereich und einem reinen Statorbereich.
Fig. 2
zeigt eine Turbomolekularpumpe mit einer seitlichen Anzapfung und einem reinen Rotorbereich.
Fig. 3
zeigt eine weitere Turbomolekularpumpe mit einer seitlichen Anzapfung und einem reinen Rotorbereich.
The invention is explained below by way of example only with reference to the drawing.
Fig. 1
shows a turbomolecular pump with a pure rotor area and a pure stator area.
Fig. 2
shows a turbomolecular pump with a side tap and a pure rotor area.
Fig. 3
shows another turbomolecular pump with a side tap and a pure rotor area.

Die in Fig. 1 gezeigte, als Turbomolekularpumpe 10 ausgebildete Vakuumpumpe umfasst einen von einem Einlassflansch 31 umgebenen Einlass 30 sowie mehrere Pumpstufen zur Förderung des an dem Einlass 30 anstehenden Gases zu einem Auslass. Der Auslass ist in Fig. 1 nicht dargestellt (vgl. aber z.B. den Auslass 32 der in Fig. 2 dargestellten Pumpe). Die Turbomolekularpumpe 10 weist keine seitliche Anzapfung auf. Die Turbomolekularpumpe 10 umfasst einen Stator mit einem statischen Gehäuse 36 und einen in dem Gehäuse 36 angeordneten Rotor 12 mit einer um eine Rotationsachse R drehbar gelagerten Rotorwelle 14.In the Fig. 1 The vacuum pump shown as a turbomolecular pump 10 comprises an inlet 30 surrounded by an inlet flange 31 and a plurality of pump stages for conveying the gas present at the inlet 30 to an outlet. The outlet is in Fig. 1 not shown (see, for example, the outlet 32 of Fig. 2 pump shown). The turbomolecular pump 10 has no lateral tapping. The turbomolecular pump 10 comprises a stator with a static housing 36 and a rotor 12 arranged in the housing 36 with a rotor shaft 14 which is rotatably mounted about an axis of rotation R.

Die Turbomolekularpumpe 10 umfasst mehrere pumpwirksam miteinander in Serie geschaltete turbomolekulare Pumpstufen mit mehreren mit der Rotorwelle 14 verbundenen, als turbomolekulare Rotorscheiben 16 ausgebildeten Rotorabschnitten und mit mehreren in axialer Richtung zwischen den Rotorscheiben 16 angeordneten und in dem Gehäuse 36 festgelegten, als turbomolekulare Statorscheiben 22 ausgebildeten Statorabschnitten, die durch Distanzringe 40 in einem gewünschten axialen Abstand zueinander gehalten sind. Die Rotorscheiben 16 und Statorscheiben 22 stellen in einem Schöpfbereich eine in Pumprichtung P gerichtete axiale Pumpwirkung bereit.The turbomolecular pump 10 comprises a plurality of turbomolecular pump stages, which are connected to one another in series with effective pumping, with a plurality of rotor sections connected to the rotor shaft 14, designed as turbomolecular rotor disks 16, and with a plurality of stator sections arranged in the axial direction between the rotor disks 16 and fixed in the housing 36 and designed as a turbomolecular stator disks 22 by spacer rings 40 in a desired axial distance from each other. The rotor disks 16 and stator disks 22 provide an axial pumping action directed in the pumping direction P in a scoop area.

Die Turbomolekularpumpe 10 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 14 befestigte und von dieser getragene zylindermantelförmige Holweck-Rotorhülsen 46, 48, die koaxial zu der Rotationsachse R orientiert und ineinander geschachtelt sind. Ferner sind zwei zylindermantelförmige Holweck-Statorhülsen 50, 52 vorgesehen, die ebenfalls koaxial zu der Rotationsachse R 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 46, 48 und einer Holweck-Statorhülse 50, 52, gebildet. Dabei ist jeweils eine der pumpaktiven Oberflächen glatt ausgebildet, im vorliegenden Fall beispielsweise die der Holweck-Rotorhülse 46 bzw. 48, wobei die gegenüberliegende pumpaktive Oberfläche der jeweiligen Holweck-Statorhülse 50 bzw. 52 eine Strukturierung mit schraubenlinienförmig um die Rotationsachse R herum in axialer Richtung verlaufenden Nuten aufweist, in denen durch die Rotation des Rotors 12 das Gas vorangetrieben und dadurch gepumpt wird.The turbomolecular pump 10 also comprises three Holweck pump stages which are arranged one inside the other in the radial direction and have a pumping effect and are connected in series with one another. The rotor-side part of the Holweck pump stages comprises two Holweck rotor sleeves 46, 48 fastened to and supported by the rotor shaft 14, which are oriented coaxially to the axis of rotation R and nested one inside the other. Furthermore, two cylindrical jacket-shaped Holweck stator sleeves 50, 52 are provided, which are also oriented coaxially to the axis of rotation R and are nested one inside the other. The pump-active surfaces of the Holweck pump stages are each formed by the radial lateral surfaces opposite one another with the formation of a narrow radial Holweck gap, namely a Holweck rotor sleeve 46, 48 and a Holweck stator sleeve 50, 52, respectively. In each case, one of the pump-active surfaces is smooth, in the present case, for example, that of the Holweck rotor sleeve 46 or 48, the opposite pump-active surface of the respective Holweck stator sleeve 50 or 52 being structured with a helix around the axis of rotation R in the axial direction has extending grooves in which the gas is propelled by the rotation of the rotor 12 and thereby pumped.

Die drehbare Lagerung der Rotorwelle 14 wird durch ein Wälzlager 54 im Bereich des Auslasses und ein Permanentmagnetlager 56 im Bereich des Einlasses 30 bewirkt.The rotatable mounting of the rotor shaft 14 is effected by a roller bearing 54 in the area of the outlet and a permanent magnet bearing 56 in the area of the inlet 30.

Das Permanentmagnetlager 56 umfasst eine rotorseitige Lagerhälfte 60 und eine statorseitige Lagerhälfte 58, 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 magnet bearing 56 comprises a rotor-side bearing half 60 and a stator-side bearing half 58, each of which comprises an annular stack of a plurality of permanent magnetic rings stacked on one another in the axial direction, wherein the magnetic rings face each other, forming a radial bearing gap.

Innerhalb des Permanentmagnetlagers 56 ist ein Not- oder Fanglager 62 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 12 gegenüber dem Stator in Eingriff gelangt, um einen radialen Anschlag für den Rotor 12 zu bilden, der eine Kollision der rotorseitigen Strukturen mit den statorseitigen Strukturen verhindert.Within the permanent magnet bearing 56, an emergency or catch bearing 62 is provided, which is designed as an unlubricated roller bearing and runs empty without contact during normal operation of the vacuum pump and only comes into engagement with an radial radial deflection of the rotor 12 with respect to the stator in order to make a radial stop to form for the rotor 12, which prevents a collision of the rotor-side structures with the stator-side structures.

Im Bereich des Wälzlagers 54 ist an der Rotorwelle 14 eine konische Spritzmutter 64 mit einem zu dem Wälzlager 54 hin zunehmenden Außendurchmesser vorgesehen, die mit einem Abstreifer eines mehrere mit einem Betriebsmittel, wie z.B. einem Schmiermittel, getränkte saugfähige Scheiben 66 umfassenden Betriebsmittelspeichers in gleitendem Kontakt steht. Im Betrieb wird das Betriebsmittel durch kapillare Wirkung von dem Betriebsmittelspeicher über den Abstreifer auf die rotierende Spritzmutter 64 übertragen und infolge der Zentrifugalkraft entlang der Spritzmutter 64 in Richtung des größer werdenden Außendurchmessers der Spritzmutter 64 zu dem Wälzlager 54 hin gefördert, wo es z.B. eine schmierende Funktion erfüllt.In the area of the roller bearing 54, a conical injection nut 64 with an external diameter increasing towards the roller bearing 54 is provided on the rotor shaft 14, which is connected to one scraper by a plurality of devices, such as a lubricant, impregnated absorbent discs 66 comprising operating fluid storage is in sliding contact. In operation, the operating medium is transferred by capillary action from the operating medium storage via the wiper to the rotating injection nut 64 and, as a result of the centrifugal force along the injection nut 64, is conveyed in the direction of the increasing outer diameter of the injection nut 64 to the roller bearing 54, where it is e.g. fulfills a lubricating function.

Die Turbomolekularpumpe 10 umfasst einen Antriebsmotor 68 zum drehenden Antreiben des Rotors, dessen Läufer durch die Rotorwelle 14 gebildet ist. Eine nicht dargestellte Steuereinheit steuert den Antriebsmotor 68 an.The turbomolecular pump 10 comprises a drive motor 68 for rotatingly driving the rotor, the rotor of which is formed by the rotor shaft 14. A control unit (not shown) controls the drive motor 68.

Die Turbomolekulargruppe 10 der Fig. 1 umfasst einen reinen Rotorbereich 28 und einen reinen Statorbereich 29. In dem reinen Rotorbereich 28 folgen zwei Rotorscheiben 16 ohne dazwischenliegende Statorscheibe 22 aufeinander. Zwischen den Rotorscheiben 16 fehlt also eine Statorscheibe 22. Im reinen Statorbereich 29 folgen zwei Statorscheiben 22 ohne dazwischenliegende Rotorscheibe 16 aufeinander. Hier fehlt also entsprechend eine Rotorscheibe 16 zwischen den Statorscheiben 22. Die beiden Rotorscheiben 16 im reinen Rotorbereich 28 und die beiden Statorscheiben 22 im reinen Statorbereich 29 sind jeweils mit einem axialen Abstand voneinander angeordnet.The turbomolecular group 10 of the Fig. 1 comprises a pure rotor region 28 and a pure stator region 29. In the pure rotor region 28, two rotor disks 16 follow one another without an interposed stator disk 22. A stator disk 22 is therefore missing between the rotor disks 16. Two stator disks 22 without a rotor disk in between follow in the pure stator area 29 16 on top of each other. A rotor disk 16 between the stator disks 22 is accordingly missing here. The two rotor disks 16 in the pure rotor area 28 and the two stator disks 22 in the pure stator area 29 are each arranged at an axial distance from one another.

Eine jeweilige Statorscheibe 22 ist in Form von zwei Halbringen ausgeführt, die von der Seite, also in radialer Richtung, zwischen die Rotorscheiben 16 gelegt werden können. Dabei werden die Statorscheiben 22 auf die Distanzringe 40 aufgelegt und durch diese getragen. Einzelne Statorscheiben 22 lassen sich dadurch besonders einfach entfernen oder weglassen, um die Turbomolekularpumpe 10 in ihren vakuumtechnischen Leistungswerten an bestimmte Anforderungen anzupassen.A respective stator disk 22 is designed in the form of two half rings which can be placed between the rotor disks 16 from the side, that is to say in the radial direction. The stator disks 22 are placed on the spacer rings 40 and carried by them. Individual stator disks 22 can thereby be removed or omitted particularly easily in order to adapt the turbomolecular pump 10 in terms of its vacuum performance values to specific requirements.

In Fig. 2 ist eine weitere Turbomolekularpumpe 10 gezeigt, die jedoch eine seitliche Anzapfung 26 aufweist. Die seitliche Anzapfung 26 ist zum Anschluss einer zusätzlichen, nicht gezeigten Vakuumkammer vorgesehen, in der ein Vakuum von einer anderen Qualität eingestellt werden soll, als es in einer am Einlass 30 angeschlossenen Kammer der Fall ist. Die seitliche Anzapfung 26 definiert einen Anzapfungsbereich 34 des Rotors 12, in den die seitliche Anzapfung 26 mündet. In dem Anzapfungsbereich 34 sind keine Statorscheiben 22 angeordnet. Zwischen den Rotorscheiben 16, welche den Anzapfungsbereich begrenzen, ist ein großer axialer Abstand vorgesehen, der im Wesentlichen der axialen Erstreckung des Anzapfungsbereichs 34 entspricht. Der Anzapfungsbereich 34 ist also von pumpaktiven Elementen freigehalten.In Fig. 2 A further turbomolecular pump 10 is shown which, however, has a lateral tap 26. The side tap 26 is provided for connecting an additional vacuum chamber, not shown, in which a vacuum of a different quality is to be set than is the case in a chamber connected to the inlet 30. The lateral tap 26 defines a tap region 34 of the rotor 12, into which the lateral tap 26 opens. No stator disks 22 are arranged in the tapping area 34. A large axial distance is provided between the rotor disks 16, which delimit the tapping area, which essentially corresponds to the axial extent of the tapping area 34. The tapping area 34 is therefore kept free of pump-active elements.

Über die seitliche Anzapfung 26 in die Pumpe gelangendes Gas wird in Pumprichtung P - in Fig. 2 also nach unten - weitergepumpt und gelangt schließlich zu einem Auslass 32.Gas entering the pump via the side tap 26 becomes P - in in the pumping direction Fig. 2 So down - pumped on and finally arrives at an outlet 32.

Außerhalb des Anzapfungsbereichs 34 ist ein reiner Rotorbereich 28 in einem axialen Bereich des Rotors 12 vorgesehen, in den keine seitliche Anzapfung mündet. Der reine Rotorbereich 28 umfasst hier drei aufeinanderfolgende Rotorscheiben 16 ohne dazwischenliegende Statorscheiben 22. Der reine Rotorbereich 28 ist in Pumprichtung P unmittelbar vor dem Anzapfungsbereich 34 angeordnet. Außerdem ist in Pumprichtung P zwischen der ersten Rotorscheibe 16 und der zweiten Rotorscheibe 16 eine Statorscheibe 22 angeordnet. In Pumprichtung P unmittelbar hinter dem Anzapfungsbereich 34 weist die Turbomolekularpumpe 10 in axialer Richtung abwechselnd angeordnete Rotorscheiben 16 und Statorscheiben 22 auf.Outside the tapping area 34, a pure rotor area 28 is provided in an axial area of the rotor 12, into which no lateral tapping opens. The pure rotor area 28 here comprises three successive rotor disks 16 without stator disks 22 lying between them. The pure rotor area 28 is arranged directly in front of the tapping area 34 in the pumping direction P. In addition, a stator disk 22 is arranged in the pumping direction P between the first rotor disk 16 and the second rotor disk 16. In the pump direction P directly behind the tapping area 34, the turbomolecular pump 10 has rotor disks 16 and stator disks 22 arranged alternately in the axial direction.

In Fig. 3 ist eine weitere Turbomolekularpumpe 10 mit einer seitlichen Anzapfung gezeigt. Die seitliche Anzapfung ist jedoch in der dargestellten Ansicht nicht sichtbar. Die seitliche Anzapfung definiert einen Anzapfungsbereich 34, in welchem keine Statorscheiben 22 angeordnet sind. In Pumprichtung unmittelbar vor dem Anzapfungsbereich 34 ist ein reiner Rotorbereich 28 vorgesehen, in dem ebenfalls keine Statorscheiben 22 angeordnet sind. Zwischen dem in Pumprichtung ersten Paar von Rotorscheiben 16 ist dagegen eine Statorscheibe 22 angeordnet. Unmittelbar hinter dem Anzapfungsbereich 34 sind Rotorscheiben 16 und Statorscheiben 22 in der an sich bekannten alternierenden Anordnung vorgesehen.In Fig. 3 Another turbomolecular pump 10 is shown with a side tap. However, the side tap is not visible in the view shown. The lateral tap defines a tap area 34, in which no stator disks 22 are arranged. In the pumping direction, directly before the tapping area 34, a pure rotor area 28 is provided, in which no stator disks 22 are likewise arranged. In contrast, a stator disk 22 is arranged between the first pair of rotor disks 16 in the pumping direction. Immediately behind the tapping area 34, rotor disks 16 and stator disks 22 are provided in the alternating arrangement known per se.

BezugszeichenlisteLIST OF REFERENCE NUMBERS

1010
TurbomolekularpumpeTurbo molecular pump
1212
Rotorrotor
1414
Rotorwellerotor shaft
1616
Rotorscheiberotor disc
1818
Rotorschaufelrotor blade
2222
Statorscheibestator
2424
Statorschaufelstator
2626
seitliche Anzapfungside tap
2828
reiner Rotorbereichpure rotor area
2929
reiner Statorbereichpure stator area
3030
Einlassinlet
3131
Einlassflanschinlet flange
3232
Auslassoutlet
3434
Anzapfungsbereichtapping range
3636
Gehäusecasing
4040
Distanzringspacer
4646
Holweck-RotorhülseHolweck rotor sleeve
4848
Holweck-RotorhülseHolweck rotor sleeve
5050
Holweck-StatorhülseHolweck stator
5252
Holweck-StatorhülseHolweck stator
5454
Wälzlagerroller bearing
5656
PermanentmagnetlagerPermanent magnetic bearings
5858
statorseitige Permanentmagnetlagerhälftepermanent magnet bearing half on the stator side
6060
rotorseitige Permanentmagnetlagerhälfterotor-side permanent magnet bearing half
6262
Fanglagersafety bearing
6464
Spritzmutterspray mother
6666
saugfähige Scheibeabsorbent disc
6868
Antriebsmotordrive motor
PP
Pumprichtungpumping direction
RR
Rotationsachseaxis of rotation

Claims (9)

  1. A vacuum pump (10), in particular a turbomolecular pump, comprising
    at least one rotor (12) which has a rotor shaft (14) and at least one rotor section (16) which is arranged at the rotor shaft (14) and which comprises a plurality of rotor blades (18) arranged distributed in the peripheral direction; and
    at least one stator which is associated with the rotor (12) and which has at least one stator section (22) which follows a rotor section (16) in the axial direction and which comprises a plurality of stator blades (24) arranged distributed in the peripheral direction,
    wherein at least one pure rotor region (28), in which at least two rotor sections (16) follow one another without a stator section (22) disposed therebetween, is provided in an axial region of the rotor (12) into which no lateral tap (26) opens,
    characterized in that
    an axial spacing is provided between the two rotor sections (16) of the pure rotor region (28).
  2. A vacuum pump (10) in accordance with claim 1,
    characterized in that
    at least one pure stator region (29) is provided in which at least two stator sections (22) follow one another without a rotor section (16) disposed therebetween; and in that an axial spacing is provided between the two stator sections (22) of the pure stator region (29).
  3. A vacuum pump (10) in accordance with claim 1 or claim 2,
    characterized in that
    the rotor sections (16) are each formed by a rotor disk manufactured separately from the rotor shaft (14) and fastened to the rotor shaft (14).
  4. A vacuum pump (10) in accordance with at least one of the preceding claims,
    characterized in that
    the pure rotor region (28) is arranged directly in front of or behind a lateral tap (26) or near a lateral tap (26) in the axial direction.
  5. A vacuum pump (10), in particular a turbomolecular pump, comprising
    at least one rotor (12) which has a rotor shaft (14) and at least one rotor section (16) which is arranged at the rotor shaft (14) and which comprises a plurality of rotor blades (18) arranged distributed in the peripheral direction; and
    at least one stator which is associated with the rotor (12) and which has at least one stator section (22) which follows a rotor section (16) in the axial direction and which comprises a plurality of stator blades (24) arranged distributed in the peripheral direction,
    wherein at least one pure stator region (29), in which at least two stator sections (22) follow one another without a rotor section (16) disposed therebetween, is provided in an axial region of the rotor (12) into which no lateral tap (26) opens,
    characterized in that
    an axial spacing is provided between the two stator sections (22) of the pure stator region (29).
  6. A vacuum pump (10) in accordance with at least one of the preceding claims,
    characterized in that
    a lateral tap (26) is provided in at least one region of the rotor.
  7. A vacuum pump (10) in accordance with at least one of the preceding claims,
    characterized in that
    a lateral tap (26) is arranged between an inlet (30) and an outlet (32) of the vacuum pump (10).
  8. A vacuum pump (10) in accordance with at least one of the claims 1 to 5,
    characterized in that
    the vacuum pump (10) does not have a lateral tap.
  9. A vacuum pump (10) in accordance with at least one of the preceding claims,
    characterized in that
    a stator section (22) is arranged in the axial direction between the rotor section (16) which is the first rotor section in the pump direction (P) and the rotor section (16) which is the second rotor section in the pump direction (P).
EP15177253.0A 2014-12-08 2015-07-17 Vacuum pump Active EP3032106B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP15177253.0A EP3032106B1 (en) 2014-12-08 2015-07-17 Vacuum pump
JP2015238692A JP6138897B2 (en) 2014-12-08 2015-12-07 Vacuum pump

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014118083.6A DE102014118083A1 (en) 2014-12-08 2014-12-08 TURBO MOLECULAR PUMP
EP15177253.0A EP3032106B1 (en) 2014-12-08 2015-07-17 Vacuum pump

Publications (2)

Publication Number Publication Date
EP3032106A1 EP3032106A1 (en) 2016-06-15
EP3032106B1 true EP3032106B1 (en) 2020-02-12

Family

ID=57003097

Family Applications (1)

Application Number Title Priority Date Filing Date
EP15177253.0A Active EP3032106B1 (en) 2014-12-08 2015-07-17 Vacuum pump

Country Status (2)

Country Link
EP (1) EP3032106B1 (en)
JP (1) JP6138897B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4293232A1 (en) * 2023-10-17 2023-12-20 Pfeiffer Vacuum Technology AG Pump

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1071275B (en) * 1959-12-17
JPH03237295A (en) * 1990-02-09 1991-10-23 Shimadzu Corp Turbo-molecular pump
JPH09303288A (en) * 1996-05-16 1997-11-25 Daikin Ind Ltd Turbo molecular pump wings
DE10052637B4 (en) * 2000-10-24 2021-03-11 Pfeiffer Vacuum Gmbh 02/16/2001 Discs for a turbo molecular pump
GB0322883D0 (en) * 2003-09-30 2003-10-29 Boc Group Plc Vacuum pump
GB0409139D0 (en) * 2003-09-30 2004-05-26 Boc Group Plc Vacuum pump
DE102006020081A1 (en) * 2006-04-29 2007-10-31 Pfeiffer Vacuum Gmbh Rotor or stator disk for a molecular pump
GB2440947A (en) * 2006-08-16 2008-02-20 Boc Group Plc A stator blade made of at least two stacked sheets

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Also Published As

Publication number Publication date
JP2016109137A (en) 2016-06-20
EP3032106A1 (en) 2016-06-15
JP6138897B2 (en) 2017-05-31

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