EP2565463B1 - Vacuum pump - Google Patents

Vacuum pump Download PDF

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Publication number
EP2565463B1
EP2565463B1 EP12180536.0A EP12180536A EP2565463B1 EP 2565463 B1 EP2565463 B1 EP 2565463B1 EP 12180536 A EP12180536 A EP 12180536A EP 2565463 B1 EP2565463 B1 EP 2565463B1
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EP
European Patent Office
Prior art keywords
groove
vacuum pump
sleeve
layer
fibre
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EP12180536.0A
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German (de)
French (fr)
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EP2565463A2 (en
EP2565463A3 (en
Inventor
Armin Conrad
Jörg Stanzel
Aleksandr Shirinov
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Pfeiffer Vacuum GmbH
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Pfeiffer Vacuum GmbH
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Priority to JP2012193204A priority Critical patent/JP5468117B2/en
Publication of EP2565463A2 publication Critical patent/EP2565463A2/en
Publication of EP2565463A3 publication Critical patent/EP2565463A3/en
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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
    • F04D19/044Holweck-type 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
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2253/00Other material characteristics; Treatment of material
    • F05C2253/04Composite, e.g. fibre-reinforced
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6034Orientation of fibres, weaving, ply angle

Definitions

  • the invention relates to a vacuum pump with a rotor according to the preamble of claim 1, a method for manufacturing a rotor according to the preamble of claim 10 and a section for a rotor according to the preamble of claim 15.
  • Vacuum pumps exploit various physical effects to produce pressure differentials.
  • One such effect is the momentum transfer to gas molecules by a rapidly moving component.
  • a special embodiment provides a rotating sleeve, which cooperates with a stationary, coaxially arranged stator sleeve. If this stator sleeve provided with thread-like channels and the pumping stage used in the molecular pressure range, is generally spoken of a Holweckcut.
  • the vacuum capability of a Holweck stage depends, among other things, on the speed of the sleeve and the shape of the channels.
  • An improvement of the vacuum technical efficiency is in the DE 196 32 375 presented in which a plurality of coaxial with each other and in the gas stream parallel to each other, rotating sleeves are used.
  • the technical problem underlying the invention is to further increase the performance of a vacuum pump of the type described.
  • the vacuum pump according to the invention with a rotor which at least a portion of a fiber composite material with at least one fiber direction, is characterized in that the section at least one helical arranged groove and fibers of the fiber composite material are aligned such that at least a portion of the fibers is aligned with the fiber direction parallel to the groove.
  • the section has at least one helically arranged groove and the fiber direction is aligned parallel to the groove, so that the section resists the action of centrifugal forces during operation of the vacuum pump.
  • a groove on a section of a rotor improves performance with respect to vacuum data, for example, increases compression.
  • a high strength of the section is achieved. Due to the orientation, long fiber lengths in the rotor are also possible adjacent to the groove, which also results in high strength at these points.
  • a high strength brings a long life with it, also allows a fast rotation of the rotor and thus an improvement in the performance of the vacuum generation.
  • the low expansion of fiber composite materials under applied centrifugal forces allows close Column between section and associated stator, which also brings an improvement in performance.
  • the section comprises a sleeve.
  • the portion having at least one helically arranged groove is formed as a sleeve.
  • This sleeve-like construction is used in particular Holweckpumpplantn.
  • a further advantageous embodiment of the invention provides that on an inner side of the sleeve, an inner groove and on an outer side of the sleeve, an outer groove are provided.
  • This structure is achieved in that a further inner layer is disposed on an inner circumferential surface of the sleeve. By this additional layer, the stability of the sleeve is significantly increased.
  • a further advantageous embodiment of the invention provides that the groove extends completely over an axial extent of the section.
  • a wrap angle of the groove is more than 360 °.
  • the section comprises at least a first and a second layer, wherein the groove is arranged in one of the layers.
  • the groove is arranged in a layer which reinforces the sleeve.
  • the groove is not taken from the material of the sleeve, so that the stability of the sleeve is increased by the further layer.
  • the groove in the layer ensures that the pumping power is also improved.
  • a further advantageous embodiment of the invention provides that the first layer comprises a first matrix and the second layer comprises a second matrix.
  • the fibers of the fiber composite material are arranged in the matrix. The fibers are thus in a first fiber direction.
  • the fibers forming the sleeve are substantially parallel to a terminal edge. This ensures that centrifugal forces occurring during rapid rotation thus generate forces acting essentially along the grain direction, so that the sleeve can withstand them very well.
  • the second layer advantageously has a second matrix. This makes it possible to allow the fibers forming a projection on the sleeve to extend at an acute angle to the terminal edge. As a result, the stability of the sleeve, that is the section is significantly increased.
  • the groove has a first groove portion and a second groove portion with mutually different geometries.
  • This embodiment is advantageous in pumps with a gas inlet and two gas outlets.
  • the conveying direction of the grooves is formed opposite and directed away from the gas inlet, it is advantageous to provide two groove sections, which have an opposite direction of rotation. This means that the groove sections have different geometries from each other.
  • a groove running around the rotor is provided between the first and the second groove portion. Where the grooves of the opposing groove portions collide, the groove encircling the rotor is provided to ensure that the gas impinging from the gas inlet on the circumferential groove is conveyed in the direction of the two spirally formed grooves.
  • the invention further relates to a method for manufacturing a rotor of a vacuum pump, which comprises a sleeve in which the sleeve is wound from a fiber material having a fiber direction and the fiber material is embedded in a plastic matrix to form a fiber composite, which is characterized in that the fiber direction is wound at an angle to a terminal edge of the sleeve and a groove aligned with the fiber direction is formed. Ideally, the groove is formed parallel to the fiber direction.
  • This design ensures that the section resists the action of centrifugal forces during operation of the vacuum pump.
  • An advantageous embodiment of the method provides that the shaping of the groove comprises a milling along the fiber direction. This way of making the groove is relatively easy.
  • the shaping of the groove takes place by winding the fiber material onto a negative mold. This ensures that the fiber material is not damaged on the one hand by a milling operation, on the other hand, this is a material-saving way of production, since the grooves are formed by the winding and thus later no material must be removed.
  • a particularly preferred embodiment of the method according to the invention provides that a first layer with a first fiber direction and a second layer with a second fiber direction are wound and the groove is formed in at least one of the layers.
  • This embodiment has the advantage that the sleeve is very stable, since on the one hand the different layers are formed and on the other hand, the fiber directions differ from each other.
  • the deviation means that, in the ideal case, an acute angle is included between the fiber direction of the first layer and the fiber direction of the second layer.
  • a further advantageous embodiment of the invention provides that the groove is formed with a first groove portion and a second groove portion with mutually different geometries.
  • This embodiment is particularly advantageous in dual-flow pumps having a gas inlet and two gas outlets. In these pumps, it is necessary that the grooves of the two sections are arranged in opposite directions to each other.
  • a section for a rotor of a vacuum pump which comprises a fiber composite with a fiber direction, which is characterized in that the section has a groove and fibers of the fiber composite are aligned such that at least a portion of the fibers is aligned with the fiber direction parallel to the groove. This ensures that the section resists the action of centrifugal forces during operation of the vacuum pump.
  • a longitudinal section through a vacuum pump shows Fig. 1 ,
  • a housing 2 has an inlet 4 through which gas enters the vacuum pump. This is ejected after compression by the pump-active elements through an outlet. 6
  • a rotor 12 which is rotatably supported by a permanent magnet bearing 8 and a rolling bearing 10.
  • Alternative bearings include active magnetic bearings and gas bearings.
  • a drive 18 rotates it about an axis of rotation 310, whereby the speed is measured according to the pumping principles used and in the case of molecular pumping it is several tens of thousands of revolutions per minute.
  • a turbomolecular pump section 14 may be provided, a molecular pumping section 16 is provided, the latter downstream of the gas stream and compressed to higher pressures.
  • Part of the rotor 12 is a section 22 belonging to the molecular pumping section 16 which comprises a hub 20 and a sleeve 24 fastened to the hub 20. Furthermore, the section 22 comprises at least one web 28 extending in a helical manner on the outer surface of the sleeve. Between the webs 28 of adjacent turns there remains at least one helical groove 30 with a groove depth T, wherein between web 28 and a terminal edge 26 of the sleeve 24 is an acute angle 312. This groove 30 or plurality of grooves 30 together with a stator 40 generates a pumping action.
  • the stator 40 may have a smooth inner circumferential surface 42 or have on this helical grooves.
  • Fig. 2 is the structure of the section in the area of the dashed box off Fig. 1 shown in a partially sectioned, perspective partial view.
  • a first layer 50 comprises a fiber composite having fibers 60 embedded in a first matrix 62.
  • the fibers 60 lie in a first fiber direction 314.
  • This layer 50 forms the sleeve 24, therefore, the fibers lie substantially parallel to the end edge 26. With fast rotation occurring centrifugal forces thus substantially along the fiber direction 314 acting forces, so that the sleeve 24th can resist this very well.
  • a second layer 52 is bonded to the first layer 50 and includes a fiber composite having fibers 60 embedded in a second matrix 64.
  • the fibers 60 of this layer 52 are mostly oriented in the angle 312 to the end edge 26, which also web 28 and end edge 26 together.
  • a fiber direction 316 is aligned with the groove 30 such that the portion resists the action of centrifugal forces during operation of the vacuum pump.
  • the web 28 loading centrifugal forces mainly have a force component along the fiber direction 316 of the second layer 52.
  • a high stability is achieved when the wrap angle is more than 360 °. It is advantageous to carry out the winding over the entire axial length of the web 28.
  • the fiber composite material can be a carbon fiber composite, CFRP, since it can counteract the occurring forces sufficiently well.
  • CFRP carbon fiber composite
  • the temperature expansion and chemical resistance are also advantageous when used in vacuum pumps.
  • the groove depth T can correspond to a complete layer thickness S. A higher strength is achieved if it is slightly lower, ie T ⁇ S applies.
  • the portion shown there has three layers 50, 52 and 54.
  • Layer 50 is the middle of the three layers and forms a supporting sleeve.
  • the layer 52 is provided, the helical groove 30 and web 28, as shown Fig. 2 described, owns.
  • the third layer 54 is arranged on an inner circumferential surface of the layer 50.
  • This layer 54 is constructed in terms of fiber layer and matrix according to the aspects of the second layer 52. It has a first inner groove 32 and a second inner groove 36 which have a different pitch. This is accomplished by having a first land 34 forming a first angle 320 with the end edge 26 and a second land 38 forming a second angle 322 with the end edge 26, where first and second angles 320, 322 are different.
  • the sense of rotation of the helical grooves in the layers 52 and 54 may be the same or opposite.
  • the section of the rotor 12 is made after Fig. 1 and Fig. 2 and the outer layer 52 of the section Fig. 3 by first forming the first layer 50. This is created by winding fibers in such a way that they are mostly in the circumferential direction. These are embedded in a matrix.
  • the second and outer layers 52 are now formed by winding fibers at an angle 320, 322 to the final edge 26 of the first layer 50 on the first layer 50 and then also embedded in a matrix. It is now possible to leave free space between fibers, that is to wind only the webs 28 in the second layer 52.
  • a groove 30 is pierced such that the angle 320, 322 corresponds to the end edge 26 substantially at the angle in which the fibers of the second layer 52 on the first layer 50 were wound.
  • An advantage of this method is that the groove depth can be easily varied. For example, a deeper groove may be formed at one axial end of the portion than at the opposite axial end of the portion. This is desirable in terms of vacuum performance when the less deep groove end operates at the higher pressure range. In the area of the less deep groove, the second layer 52 is not completely removed and at the deepest point of the groove, the groove depth reaches at most the value of the layer thickness S. In this way, particularly high resistance to centrifugal forces is maintained.
  • a negative mold 70 has a cylindrical portion, on the lateral surface of a helical shape groove 72 is introduced. Ribbon-like fiber material 74 is now wound in this molding groove 72, so that the molding groove 72 is gradually filled up.
  • Fig. 5 shows a half-filled state in cross section.
  • the third layer 54 is finished.
  • fibers 76 are wound around the outer surface itself, cf. Fig. 6 , and so made the layer 50.
  • the molding groove 72 may be formed as a multi-thread helix.
  • the female mold 70 is removed by unscrewing from the sleeve 24 produced.
  • the vacuum technical efficiency of the arrangement is based on the Fig. 9 be occupied. In it, the pressure ratio between the inlet and outlet in the absence of gas flow, the so-called idle compression over represented the discharge pressure.
  • the curve 300 shows a conventional arrangement in which only one stator has a helical groove, as used for example in so-called Holweckpump processn.
  • the curve 302 shows an arrangement with a groove on the rotor. The idle compression is significantly increased.
  • a double-flow vacuum pump is shown in section. It has a housing 202 which is equipped with a gas inlet 204 and two gas outlets 206. The gas outlets 206 may be combined by an inner channel provided in the housing 202.
  • a rotor 212 is rotatably mounted in bearings 208 and 210 and is driven by a drive 218.
  • the rotor 212 has a section with a sleeve 224, on the outer circumferential surface of which are formed two grooves 230a and 230b according to the above-described method.
  • the conveying direction of the grooves 230a, 230b is opposite and directed away from the gas inlet 204, as the arrows in FIG Fig. 7 clarify.
  • the grooves 230a, 230b have an opposite direction of rotation.
  • the grooves on the portion cooperate with stator-side grooves 242a and 242b, which are also helically designed in opposite directions of rotation.
  • the grooves 230a, 230b of the sleeve 224 are arranged opposite the stator-side grooves 242a, 242b.
  • a portion 222 has a helical groove having a first groove portion 250 and a second groove portion 254.
  • the geometries, in particular the cross sections, of the groove sections 250, 254 are different.
  • the first groove portion 250 has a semicircular cross section and the second groove portion 254 has a triangular cross section.
  • a circumferential groove 260 is provided between the groove portions 250, 254.
  • the cross sections allow adaptation to the pressure region in which the respective groove section is to act preferentially.
  • the geometries may differ with respect to the pitch of the helix.
  • the circumferential groove portion may be provided at the transition point between different flow areas.

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Description

Die Erfindung betrifft eine Vakuumpumpe mit einem Rotor nach dem Oberbegriff von Anspruch 1, ein Verfahren zum Herstellen eines Rotors nach dem Oberbegriff von Anspruch 10 und einen Abschnitt für einen Rotor nach dem Oberbegriff von Anspruch 15.The invention relates to a vacuum pump with a rotor according to the preamble of claim 1, a method for manufacturing a rotor according to the preamble of claim 10 and a section for a rotor according to the preamble of claim 15.

In Vakuumpumpen werden verschiedene physikalische Effekte zur Erzeugung von Druckunterschieden ausgenutzt. Ein solcher Effekt ist der Impulsübertrag auf Gasmoleküle durch ein schnell bewegtes Bauteil. Eine spezielle Ausprägung sieht eine rotierende Hülse vor, welche mit einer feststehenden, koaxial angeordneten Statorhülse zusammenwirkt. Wird diese Statorhülse mit gewindeartig gestalteten Kanälen versehen und die Pumpstufe im molekularen Druckbereich eingesetzt, wird im Allgemeinen von einer Holweckstufe gesprochen.Vacuum pumps exploit various physical effects to produce pressure differentials. One such effect is the momentum transfer to gas molecules by a rapidly moving component. A special embodiment provides a rotating sleeve, which cooperates with a stationary, coaxially arranged stator sleeve. If this stator sleeve provided with thread-like channels and the pumping stage used in the molecular pressure range, is generally spoken of a Holweckstufe.

Die vakuumtechnische Leistungsfähigkeit einer Holweckstufe hängt unter anderem von der Drehzahl der Hülse und der Form der Kanäle ab. Eine Verbesserung der vakuumtechnischen Leistungsfähigkeit ist in der DE 196 32 375 vorgestellt, in der mehrere koaxial zueinander und im Gasstrom parallel zueinander angeordnete, rotierende Hülsen benutzt werden.The vacuum capability of a Holweck stage depends, among other things, on the speed of the sleeve and the shape of the channels. An improvement of the vacuum technical efficiency is in the DE 196 32 375 presented in which a plurality of coaxial with each other and in the gas stream parallel to each other, rotating sleeves are used.

Eine andere Möglichkeit zur Steigerung der Leistungsfähigkeit betrifft die Drehzahl. Mit steigender Drehzahl steigt die Belastung der Hülse durch Trägheitskräfte. Um eine geringe Verformung der Hülse zu erreichen, durch die vakuumtechnisch vorteilhafte enge Spalte ermöglicht werden, stellt die EP 1 408 237 A1 eine Hülse aus kohlenstofffaserverstärktem Material vor. Ähnliche Vorrichtungen sind bekannt aus GB 2 420 379 A und US 6 419 444 B1 .Another way to increase performance is speed. As the speed increases, the load on the sleeve increases due to inertial forces. In order to achieve a small deformation of the sleeve, are made possible by the vacuum technically advantageous narrow column, provides EP 1 408 237 A1 a sleeve of carbon fiber reinforced material. Similar devices are known from GB 2 420 379 A and US Pat. No. 6,419,444 B1 ,

Das der Erfindung zugrunde liegende technische Problem besteht darin, die Leistungsfähigkeit einer Vakuumpumpe der beschriebenen Art weiter zu erhöhen.The technical problem underlying the invention is to further increase the performance of a vacuum pump of the type described.

Dieses technische Problem wird durch einen Abschnitt mit den Merkmalen des Anspruches 1, eine Vakuumpumpe mit den Merkmalen des Anspruches 2 und einem Verfahren mit den Merkmalen des Anspruches 11 gelöst. Die abhängigen Ansprüche 3 bis 10 sowie 12 bis 15 geben vorteilhafte Weiterbildungen der Erfindung an.This technical problem is solved by a section having the features of claim 1, a vacuum pump having the features of claim 2 and a method having the features of claim 11. The dependent claims 3 to 10 and 12 to 15 indicate advantageous developments of the invention.

Die erfindungsgemäße Vakuumpumpe mit einem Rotor, welcher wenigstens einen Abschnitt aus einem Faserverbundstoff mit wenigstens einer Faserrichtung umfasst, zeichnet sich dadurch aus, dass der Abschnitt wenigstens eine schraubenlinienartig angeordnete Nut aufweist und Fasern des Faserverbundwerkstoffes derart ausgerichtet sind, dass wenigstens ein Teil der Fasern mit der Faserrichtung parallel zu der Nut ausgerichtet ist.The vacuum pump according to the invention with a rotor, which at least a portion of a fiber composite material with at least one fiber direction, is characterized in that the section at least one helical arranged groove and fibers of the fiber composite material are aligned such that at least a portion of the fibers is aligned with the fiber direction parallel to the groove.

Fertigungsbedingt liegen nicht alle Fasern exakt parallel mit einer Faserrichtung, die parallel zu der Nut ausgerichtet ist. Dadurch, dass wenigstens ein Teil der Fasern mit der Faserrichtung derart ausgerichtet ist, dass die Faserrichtung im Wesentlichen parallel zur Nut ausgerichtet ist, erhält man die geforderte Stabilität.For manufacturing reasons, not all fibers lie exactly parallel with a fiber direction which is aligned parallel to the groove. Characterized in that at least a part of the fibers is aligned with the fiber direction such that the fiber direction is aligned substantially parallel to the groove, one obtains the required stability.

Das bedeutet, dass die Faserrichtung im Wesentlichen parallel zu der Nut ausgerichtet ist.This means that the fiber direction is aligned substantially parallel to the groove.

Vorteilhaft weist der Abschnitt wenigstens eine schraubenlinienartig angeordnete Nut auf und die Faserrichtung ist parallel zu der Nut ausgerichtet, so dass der Abschnitt dem Einwirken von Fliehkräften bei Betrieb der Vakuumpumpe widersteht.Advantageously, the section has at least one helically arranged groove and the fiber direction is aligned parallel to the groove, so that the section resists the action of centrifugal forces during operation of the vacuum pump.

Es wurde festgestellt, dass eine Nut auf einem Abschnitt eines Rotors die Leistungsfähigkeit in Bezug auf die Vakuumdaten verbessert, beispielsweise erhöht sie die Kompression. Durch Ausrichtung von Nut und Faserlage aneinander wird eine hohe Festigkeit des Abschnittes erreicht. Aufgrund der Ausrichtung sind lange Faserlängen im Rotor auch an die Nut angrenzend möglich, womit auch an diesen Stellen eine hohe Festigkeit erreicht wird. Eine hohe Festigkeit bringt eine lange Lebensdauer mit sich, außerdem erlaubt sie eine schnelle Rotation des Rotors und damit eine Verbesserung der Leistungsfähigkeit bei der Vakuumerzeugung. Die geringe Ausdehnung von Faserverbundmaterialien unter einwirkenden Fliehkräften ermöglicht enge Spalte zwischen Abschnitt und zugeordnetem Stator, was ebenfalls eine Verbesserung der Leistungsfähigkeit mit sich bringt.It has been found that a groove on a section of a rotor improves performance with respect to vacuum data, for example, increases compression. By aligning the groove and fiber layer together a high strength of the section is achieved. Due to the orientation, long fiber lengths in the rotor are also possible adjacent to the groove, which also results in high strength at these points. A high strength brings a long life with it, also allows a fast rotation of the rotor and thus an improvement in the performance of the vacuum generation. The low expansion of fiber composite materials under applied centrifugal forces allows close Column between section and associated stator, which also brings an improvement in performance.

Gemäß einer besonders bevorzugten Ausführungsform der Erfindung umfasst der Abschnitt eine Hülse. Das bedeutet, dass der Abschnitt, der wenigstens eine schraubenlinienartig angeordnet Nut aufweist, als Hülse ausgebildet ist. Dieser hülsenartige Aufbau wird insbesondere in Holweckpumpstufen verwendet.According to a particularly preferred embodiment of the invention, the section comprises a sleeve. This means that the portion having at least one helically arranged groove is formed as a sleeve. This sleeve-like construction is used in particular Holweckpumpstufen.

Eine weitere vorteilhafte Ausführungsform der Erfindung sieht vor, dass auf einer Innenseite der Hülse eine innere Nut und auf einer Außenseite der Hülse eine äußere Nut vorgesehen sind. Dieser Aufbau wird dadurch erreicht, dass eine weitere innere Schicht auf einer inneren Mantelfläche der Hülse angeordnet wird. Durch diese weitere Schicht wird die Stabilität der Hülse deutlich erhöht.A further advantageous embodiment of the invention provides that on an inner side of the sleeve, an inner groove and on an outer side of the sleeve, an outer groove are provided. This structure is achieved in that a further inner layer is disposed on an inner circumferential surface of the sleeve. By this additional layer, the stability of the sleeve is significantly increased.

Eine weitere vorteilhafte Ausführungsform der Erfindung sieht vor, dass sich die Nut vollständig über eine axiale Ausdehnung des Abschnittes erstreckt.A further advantageous embodiment of the invention provides that the groove extends completely over an axial extent of the section.

Hierdurch wird die Erhöhung der Pumpleistung am besten erzielt.This is the best way to increase the pumping capacity.

Gemäß einer weiteren besonders bevorzugten Ausführungsform der Erfindung beträgt ein Umschlingungswinkel der Nut mehr als 360°. Hierdurch wird eine sehr hohe Stabilität der Hülse erreicht.According to a further particularly preferred embodiment of the invention, a wrap angle of the groove is more than 360 °. As a result, a very high stability of the sleeve is achieved.

Gemäß einer weiteren vorteilhaften Ausführungsform der Erfindung ist vorgesehen, dass der Abschnitt wenigstens eine erste und eine zweite Schicht umfasst, wobei die Nut in einer der Schichten angeordnet ist. Durch diesen Aufbau wird erreicht, dass die Nut in einer Schicht, die die Hülse verstärkt, angeordnet ist. Die Nut wird nicht aus dem Material der Hülse genommen, so dass die Stabilität der Hülse durch die weitere Schicht erhöht wird. Die Nut in der Schicht gewährleistet, dass die Pumpleistung ebenfalls verbessert wird.According to a further advantageous embodiment of the invention, it is provided that the section comprises at least a first and a second layer, wherein the groove is arranged in one of the layers. By this construction it is achieved that the groove is arranged in a layer which reinforces the sleeve. The groove is not taken from the material of the sleeve, so that the stability of the sleeve is increased by the further layer. The groove in the layer ensures that the pumping power is also improved.

Eine weitere vorteilhafte Ausführungsform der Erfindung sieht vor, dass die erste Schicht eine erste Matrix und die zweite Schicht eine zweite Matrix umfasst. In der Matrix sind die Fasern des Faserverbundwerkstoffes angeordnet. Die Fasern liegen damit in einer ersten Faserrichtung. Die Fasern, die die Hülse bilden, liegen im Wesentlichen parallel zu einer Abschlusskante. Hierdurch ist gewährleistet, dass bei schneller Drehung auftretende Fliehkräfte so im Wesentlichen entlang der Faserrichtung wirkende Kräfte erzeugen, so dass die Hülse diesen sehr gut widerstehen kann.A further advantageous embodiment of the invention provides that the first layer comprises a first matrix and the second layer comprises a second matrix. The fibers of the fiber composite material are arranged in the matrix. The fibers are thus in a first fiber direction. The fibers forming the sleeve are substantially parallel to a terminal edge. This ensures that centrifugal forces occurring during rapid rotation thus generate forces acting essentially along the grain direction, so that the sleeve can withstand them very well.

Die zweite Schicht weist vorteilhaft eine zweite Matrix auf. Hierdurch besteht die Möglichkeit, die Fasern, die einen Vorsprung auf der Hülse bilden, in einem spitzen Winkel zu der Abschlusskante verlaufen zu lassen. Hierdurch wird die Stabilität der Hülse, das heißt des Abschnittes deutlich erhöht.The second layer advantageously has a second matrix. This makes it possible to allow the fibers forming a projection on the sleeve to extend at an acute angle to the terminal edge. As a result, the stability of the sleeve, that is the section is significantly increased.

Vorteilhaft weist die Nut einen ersten Nutabschnitt und einen zweiten Nutabschnitt mit voneinander verschiedenen Geometrien auf. Diese Ausführungsform ist vorteilhaft bei Pumpen mit einem Gaseinlass und zwei Gasauslässen. Da bei dieser Ausführungsform die Förderrichtung der Nuten entgegengesetzt ausgebildet und von dem Gaseinlass weggerichtet ist, ist es vorteilhaft, zwei Nutabschnitte vorzusehen, die einen entgegengesetzten Drehsinn aufweisen. Das bedeutet, dass die Nutabschnitte voneinander verschiedene Geometrien aufweisen.Advantageously, the groove has a first groove portion and a second groove portion with mutually different geometries. This embodiment is advantageous in pumps with a gas inlet and two gas outlets. In this embodiment, since the conveying direction of the grooves is formed opposite and directed away from the gas inlet, it is advantageous to provide two groove sections, which have an opposite direction of rotation. This means that the groove sections have different geometries from each other.

Gemäß einer weiteren vorteilhaften Ausführungsform der Erfindung ist zwischen dem ersten und dem zweiten Nutabschnitt eine um den Rotor umlaufende Nut vorgesehen. Dort, wo die Nuten der gegenläufigen Nutabschnitte zusammenstoßen, ist die den Rotor umlaufende Nut vorgesehen, um zu gewährleisten, dass das von dem Gaseinlass auf die umlaufende Nut treffende Gas in Richtung der beiden spiralförmig ausgebildeten Nuten gefördert wird.According to a further advantageous embodiment of the invention, a groove running around the rotor is provided between the first and the second groove portion. Where the grooves of the opposing groove portions collide, the groove encircling the rotor is provided to ensure that the gas impinging from the gas inlet on the circumferential groove is conveyed in the direction of the two spirally formed grooves.

Die Erfindung betrifft weiterhin ein Verfahren zum Herstellen eines Rotors einer Vakuumpumpe, welcher eine Hülse umfasst, in welchem die Hülse aus einem Faserwerkstoff mit einer Faserrichtung gewickelt und der Faserwerkstoff zur Bildung eines Faserverbundwerkstoffes in einer Kunststoffmatrix eingebettet wird, das sich dadurch auszeichnet, dass die Faserrichtung in einem Winkel zu einer Abschlusskante der Hülse gewickelt und eine an der Faserrichtung ausgerichtet Nut geformt wird. Im Idealfall ist die Nut parallel zur Faserrichtung ausgebildet.The invention further relates to a method for manufacturing a rotor of a vacuum pump, which comprises a sleeve in which the sleeve is wound from a fiber material having a fiber direction and the fiber material is embedded in a plastic matrix to form a fiber composite, which is characterized in that the fiber direction is wound at an angle to a terminal edge of the sleeve and a groove aligned with the fiber direction is formed. Ideally, the groove is formed parallel to the fiber direction.

Durch diese Ausbildung ist gewährleistet, dass der Abschnitt dem Einwirken von Fliehkräften bei Betrieb der Vakuumpumpe widersteht.This design ensures that the section resists the action of centrifugal forces during operation of the vacuum pump.

Eine vorteilhafte Ausführungsform des Verfahrens sieht vor, dass das Formen der Nut ein Fräsen entlang der Faserrichtung umfasst. Diese Art der Herstellung der Nut ist relativ einfach.An advantageous embodiment of the method provides that the shaping of the groove comprises a milling along the fiber direction. This way of making the groove is relatively easy.

Gemäß einem alternativen Verfahren ist vorgesehen, dass das Formen der Nut durch das Wickeln des Faserwerkstoffes auf eine Negativform erfolgt. Hierdurch ist gewährleistet, dass der Faserwerkstoff zum einen durch einen Fräsvorgang nicht beschädigt wird, zum anderen ist dies eine Material sparende Art der Herstellung, da durch das Wickeln die Nuten ausgebildet werden und damit später kein Material entfernt werden muss.According to an alternative method, it is provided that the shaping of the groove takes place by winding the fiber material onto a negative mold. This ensures that the fiber material is not damaged on the one hand by a milling operation, on the other hand, this is a material-saving way of production, since the grooves are formed by the winding and thus later no material must be removed.

Eine besonders bevorzugte Ausführungsform des erfindungsgemäßen Verfahrens sieht vor, dass eine erste Schicht mit einer ersten Faserrichtung und eine zweite Schicht mit einer zweiten Faserrichtung gewickelt werden und die Nut in wenigstens einer der Schichten geformt wird. Diese Ausführungsform weist den Vorteil auf, dass die Hülse sehr stabil wird, da zum einen die verschiedenen Schichten geformt werden und zum anderen die Faserrichtungen voneinander abweichen. Die Abweichung bedeutet, dass im Idealfalle zwischen der Faserrichtung der ersten Schicht und der Faserrichtung der zweiten Schicht ein spitzer Winkel eingeschlossen wird.A particularly preferred embodiment of the method according to the invention provides that a first layer with a first fiber direction and a second layer with a second fiber direction are wound and the groove is formed in at least one of the layers. This embodiment has the advantage that the sleeve is very stable, since on the one hand the different layers are formed and on the other hand, the fiber directions differ from each other. The deviation means that, in the ideal case, an acute angle is included between the fiber direction of the first layer and the fiber direction of the second layer.

Eine weitere vorteilhafte Ausführungsform der Erfindung sieht vor, dass die Nut mit einem ersten Nutabschnitt und einem zweiten Nutabschnitt mit voneinander verschiedenen Geometrien geformt wird. Diese Ausführungsform ist besonders vorteilhaft bei zweiflutigen Pumpen, die einen Gaseinlass und zwei Gasauslässe aufweisen. Bei diesen Pumpen ist es erforderlich, dass die Nuten der beiden Abschnitte gegenläufig zueinander angeordnet sind.A further advantageous embodiment of the invention provides that the groove is formed with a first groove portion and a second groove portion with mutually different geometries. This embodiment is particularly advantageous in dual-flow pumps having a gas inlet and two gas outlets. In these pumps, it is necessary that the grooves of the two sections are arranged in opposite directions to each other.

Gemäß der Erfindung ist weiterhin ein Abschnitt für einen Rotor einer Vakuumpumpe unter Schutz gestellt, welcher einen Faserverbundstoff mit einer Faserrichtung umfasst, der sich dadurch auszeichnet, dass der Abschnitt eine Nut aufweist und Fasern des Faserverbundstoffes derart ausgerichtet sind, dass wenigstens ein Teil der Fasern mit der Faserrichtung parallel zu der Nut ausgerichtet ist. Hierdurch ist gewährleistet, dass der Abschnitt dem Einwirken von Fliehkräften bei Betrieb der Vakuumpumpe widersteht.According to the invention, furthermore, a section for a rotor of a vacuum pump is provided, which comprises a fiber composite with a fiber direction, which is characterized in that the section has a groove and fibers of the fiber composite are aligned such that at least a portion of the fibers is aligned with the fiber direction parallel to the groove. This ensures that the section resists the action of centrifugal forces during operation of the vacuum pump.

Anhand eines Ausführungsbeispieles und seiner Weiterbildungen soll die Erfindung näher erläutert und die Darstellung ihrer Vorteile vertieft werden. Es zeigen:

Fig. 1
einen Längsschnitt durch eine Vakuumpumpe mit einem Rotor, welcher eine Hülse aufweist;
Fig. 2
einen Schnitt durch einen Teil der Hülse zur Verdeutlichung der Lage von Nut und Faserrichtung;
Fig. 3
einen Schnitt durch eine Hülse mit innerer, äußerer und Umfangsnut;
Fig. 4
eine Seitenansicht auf eine Negativform;
Fig. 5
einen Querschnitt durch die Negativform zur Herstellung einer Hülse mit innerer Nut und Wickeln der Nutstege;
Fig. 6
einen Querschnitt durch die Negativform und Wickeln der mittleren Schicht;
Fig. 7
einen Längsschnitt durch eine doppelflutige Vakuumpumpe gemäß zweitem Beispiel;
Fig. 8
einen Rotor in Seitenansicht in einer Weiterbildung;
Fig. 9
einen Verlauf von Kompression über Ausstoßdruck zur Darstellung eines erreichten Vorteiles.
Reference to an embodiment and its developments, the invention will be explained in more detail and the representation of its benefits to be deepened. Show it:
Fig. 1
a longitudinal section through a vacuum pump with a rotor having a sleeve;
Fig. 2
a section through a part of the sleeve to illustrate the position of the groove and fiber direction;
Fig. 3
a section through a sleeve with inner, outer and circumferential groove;
Fig. 4
a side view of a negative mold;
Fig. 5
a cross section through the female mold for producing a sleeve with an inner groove and winding the Nutstege;
Fig. 6
a cross section through the negative mold and winding the middle layer;
Fig. 7
a longitudinal section through a double-suction vacuum pump according to the second example;
Fig. 8
a rotor in side view in a development;
Fig. 9
a course of compression over ejection pressure to represent an advantage achieved.

Einen Längsschnitt durch eine Vakuumpumpe zeigt Fig. 1. Ein Gehäuse 2 weist einen Einlass 4 auf, durch den Gas in die Vakuumpumpe gelangt. Ausgestoßen wird dieses nach Verdichten durch die pumpaktiven Elemente durch einen Auslass 6.A longitudinal section through a vacuum pump shows Fig. 1 , A housing 2 has an inlet 4 through which gas enters the vacuum pump. This is ejected after compression by the pump-active elements through an outlet. 6

Im Gehäuse 2 befindet sich ein Rotor 12, der von einem Permanentmagnetlager 8 und einem Wälzlager 10 drehbar unterstützt wird. Alternative Lagerungen umfassen aktive Magnetlager und Gaslager. Ein Antrieb 18 versetzt ihn in Drehung um eine Drehachse 310, wobei sich die Drehzahl nach den verwendeten Pumpprinzipien bemisst und im Falle molekularen Pumpens bei einigen zehntausend Umdrehungen pro Minute liegt. Ein turbomolekularer Pumpabschnitt 14 kann vorgesehen sein, ein molekularer Pumpabschnitt 16 ist vorgesehen, wobei letzterer im Gasstrom nachgelagert ist und zu höheren Drücken hin verdichtet.In the housing 2 is a rotor 12 which is rotatably supported by a permanent magnet bearing 8 and a rolling bearing 10. Alternative bearings include active magnetic bearings and gas bearings. A drive 18 rotates it about an axis of rotation 310, whereby the speed is measured according to the pumping principles used and in the case of molecular pumping it is several tens of thousands of revolutions per minute. A turbomolecular pump section 14 may be provided, a molecular pumping section 16 is provided, the latter downstream of the gas stream and compressed to higher pressures.

Teil des Rotors 12 ist ein zum Molekularpumpabschnitt 16 gehörender Abschnitt 22, der eine Nabe 20 und eine an der Nabe 20 befestigte Hülse 24 umfasst. Weiterhin umfasst der Abschnitt 22 wenigstens einen schraubenlinienartig auf der äußeren Mantelfläche der Hülse verlaufenden Steg 28. Zwischen den Stegen 28 benachbarter Windungen verbleibt wenigstens eine schraubenlinienartig verlaufende Nut 30 mit einer Nuttiefe T, wobei zwischen Steg 28 und einer Abschlusskante 26 der Hülse 24 ein spitzer Winkel 312 besteht. Diese Nut 30 oder Mehrzahl an Nuten 30 erzeugt zusammen mit einem Stator 40 eine Pumpwirkung. Der Stator 40 kann eine glatte innere Mantelfläche 42 haben oder auf dieser schraubenlinienartig verlaufende Nuten besitzen.Part of the rotor 12 is a section 22 belonging to the molecular pumping section 16 which comprises a hub 20 and a sleeve 24 fastened to the hub 20. Furthermore, the section 22 comprises at least one web 28 extending in a helical manner on the outer surface of the sleeve. Between the webs 28 of adjacent turns there remains at least one helical groove 30 with a groove depth T, wherein between web 28 and a terminal edge 26 of the sleeve 24 is an acute angle 312. This groove 30 or plurality of grooves 30 together with a stator 40 generates a pumping action. The stator 40 may have a smooth inner circumferential surface 42 or have on this helical grooves.

In Fig. 2 ist der Aufbau des Abschnittes im Bereich des gestrichelten Kastens aus Fig. 1 in einer teilgeschnittenen, perspektivischen Teilansicht dargestellt.In Fig. 2 is the structure of the section in the area of the dashed box off Fig. 1 shown in a partially sectioned, perspective partial view.

Eine erste Schicht 50 umfasst einen Faserverbundwerkstoff mit Fasern 60, die in einer ersten Matrix 62 eingebettet sind. Die Fasern 60 liegen in einer ersten Faserrichtung 314. Diese Schicht 50 bildet die Hülse 24, daher liegen die Fasern im Wesentlichen parallel zur Abschlusskante 26. Bei schneller Drehung auftretende Fliehkräfte erzeugen so im Wesentlichen entlang der Faserrichtung 314 wirkende Kräfte, so dass die Hülse 24 diesen sehr gut widerstehen kann.A first layer 50 comprises a fiber composite having fibers 60 embedded in a first matrix 62. The fibers 60 lie in a first fiber direction 314. This layer 50 forms the sleeve 24, therefore, the fibers lie substantially parallel to the end edge 26. With fast rotation occurring centrifugal forces thus substantially along the fiber direction 314 acting forces, so that the sleeve 24th can resist this very well.

Eine zweite Schicht 52 ist mit der ersten Schicht 50 verbunden und umfasst einen Faserverbundwerkstoff mit Fasern 60, die in eine zweite Matrix 64 eingebettet sind. Die Fasern 60 dieser Schicht 52 sind mehrheitlich in dem Winkel 312 zur Abschlusskante 26 orientiert, den auch Steg 28 und Abschlusskante 26 miteinander bilden. Auf diese Weise ist eine Faserrichtung 316 derart an der Nut 30 ausgerichtet, dass der Abschnitt dem Einwirken von Fliehkräften bei Betrieb der Vakuumpumpe widersteht. Den Steg 28 belastende Fliehkräfte besitzen hauptsächlich eine Kraftkomponente entlang der Faserrichtung 316 der zweiten Schicht 52. Eine hohe Stabilität wird erreicht, wenn der Umschlingungswinkel mehr als 360° beträgt. Vorteilhaft ist es, die Wicklung über die gesamte axiale Länge des Steges 28 auszuführen.A second layer 52 is bonded to the first layer 50 and includes a fiber composite having fibers 60 embedded in a second matrix 64. The fibers 60 of this layer 52 are mostly oriented in the angle 312 to the end edge 26, which also web 28 and end edge 26 together. In this way, a fiber direction 316 is aligned with the groove 30 such that the portion resists the action of centrifugal forces during operation of the vacuum pump. The web 28 loading centrifugal forces mainly have a force component along the fiber direction 316 of the second layer 52. A high stability is achieved when the wrap angle is more than 360 °. It is advantageous to carry out the winding over the entire axial length of the web 28.

Der Faserverbundwerkstoff kann ein Kohlenstofffaserverbund, CFK, sein, da dieser hinreichend gut den auftretenden Kräften begegnen kann. Die Temperaturausdehnung und chemische Beständigkeit sind ebenfalls vorteilhaft beim Einsatz in Vakuumpumpen.The fiber composite material can be a carbon fiber composite, CFRP, since it can counteract the occurring forces sufficiently well. The temperature expansion and chemical resistance are also advantageous when used in vacuum pumps.

Die Nuttiefe T kann einer kompletten Schichtstärke S entsprechen. Eine höhere Festigkeit wird erreicht, wenn sie geringfügig geringer ist, also T < S gilt.The groove depth T can correspond to a complete layer thickness S. A higher strength is achieved if it is slightly lower, ie T <S applies.

Eine Weiterbildung des Abschnittes ist in einem Schnitt in Fig. 3 dargestellt.A development of the section is in a cut in Fig. 3 shown.

Der dort gezeigte Abschnitt besitzt drei Schichten 50, 52 und 54. Schicht 50 ist die mittlere der drei Schichten und bildet eine tragende Hülse. Auf der äußeren Oberfläche ist die Schicht 52 vorgesehen, die schraubenlinienartige Nut 30 und Steg 28, wie anhand Fig. 2 beschrieben, besitzt.The portion shown there has three layers 50, 52 and 54. Layer 50 is the middle of the three layers and forms a supporting sleeve. On the outer surface, the layer 52 is provided, the helical groove 30 and web 28, as shown Fig. 2 described, owns.

Auf einer inneren Mantelfläche der Schicht 50 ist die dritte Schicht 54 angeordnet. Diese Schicht 54 ist in Bezug auf Faserlage und Matrix nach den Gesichtspunkten der zweiten Schicht 52 aufgebaut. Sie weist eine erste innere Nut 32 und eine zweite innere Nut 36 auf, die eine unterschiedliche Steigung besitzen. Dies wird erreicht, indem ein erster Steg 34 einen ersten Winkel 320 mit der Abschlusskante 26 und ein zweiter Steg 38 einen zweiten Winkel 322 mit der Abschlusskante 26 bildet, wobei erster und zweiter Winkel 320, 322 verschieden voneinander sind. Die Drehsinne der schraubenlinienartigen Nuten in den Schichten 52 und 54 können gleich oder gegensinnig sein.On an inner circumferential surface of the layer 50, the third layer 54 is arranged. This layer 54 is constructed in terms of fiber layer and matrix according to the aspects of the second layer 52. It has a first inner groove 32 and a second inner groove 36 which have a different pitch. This is accomplished by having a first land 34 forming a first angle 320 with the end edge 26 and a second land 38 forming a second angle 322 with the end edge 26, where first and second angles 320, 322 are different. The sense of rotation of the helical grooves in the layers 52 and 54 may be the same or opposite.

Hergestellt wird der Abschnitt des Rotors 12 nach Fig. 1 und Fig. 2 und die äußere Schicht 52 des Abschnittes nach Fig. 3, indem zunächst die erste Schicht 50 gebildet wird. Diese entsteht durch Wickeln von Fasern derart, dass diese mehrheitlich in Umfangsrichtung liegen. Diese werden in eine Matrix eingebettet. Die zweite und äußere Schicht 52 wird nun gebildet, indem Fasern in einem Winkel 320, 322 zur Abschlusskante 26 der ersten Schicht 50 auf die erste Schicht 50 gewickelt werden und dann ebenfalls in eine Matrix eingebettet werden. Es ist nun möglich, zwischen Fasern Freiraum zu lassen, das heißt, nur die Stege 28 in der zweiten Schicht 52 zu wickeln. Vorteilhafter ist es, eine durchgängige zweite Schicht 52 zu schaffen, in die nach Aushärten eine Nut 30 derart eingestochen wird, dass der Winkel 320, 322 zur Abschlusskante 26 im Wesentlichen dem Winkel entspricht, in dem die Fasern der zweiten Schicht 52 auf die erste Schicht 50 gewickelt wurden. Ein Vorteil an diesem Verfahren ist, dass die Nuttiefe leicht variiert werden kann. Beispielsweise kann an einem axialen Ende des Abschnittes eine tiefere Nut als am gegenüberliegenden axialen Ende des Abschnittes geformt werden. Dies ist im Hinblick auf die vakuumtechnische Leistungsfähigkeit wünschenswert, wenn das weniger tiefe Nutende im höheren Druckbereich arbeitet. Im Bereich der weniger tiefen Nut ist die zweite Schicht 52 nicht vollständig weggenommen und an der tiefsten Stelle der Nut erreicht die Nuttiefe maximal den Wert der Schichtdicke S. Hierdurch wird besonders hohe Widerstandsfähigkeit gegen Fliehkräfte aufrecht erhalten.The section of the rotor 12 is made after Fig. 1 and Fig. 2 and the outer layer 52 of the section Fig. 3 by first forming the first layer 50. This is created by winding fibers in such a way that they are mostly in the circumferential direction. These are embedded in a matrix. The second and outer layers 52 are now formed by winding fibers at an angle 320, 322 to the final edge 26 of the first layer 50 on the first layer 50 and then also embedded in a matrix. It is now possible to leave free space between fibers, that is to wind only the webs 28 in the second layer 52. It is more advantageous to provide a continuous second layer 52 in which, after curing, a groove 30 is pierced such that the angle 320, 322 corresponds to the end edge 26 substantially at the angle in which the fibers of the second layer 52 on the first layer 50 were wound. An advantage of this method is that the groove depth can be easily varied. For example, a deeper groove may be formed at one axial end of the portion than at the opposite axial end of the portion. This is desirable in terms of vacuum performance when the less deep groove end operates at the higher pressure range. In the area of the less deep groove, the second layer 52 is not completely removed and at the deepest point of the groove, the groove depth reaches at most the value of the layer thickness S. In this way, particularly high resistance to centrifugal forces is maintained.

Es können sich Nuttiefe T oder Nutbreite oder beide über die Länge der Nut 30 ändern, wodurch vorteilhaft die Geometrie der Nut 30 an den Arbeitsdruckbereich angepasst wird und die Leistungsfähigkeit der Pumpe verbessert werden kann.It can groove depth T or groove width or both change over the length of the groove 30, thereby advantageously adapted to the geometry of the groove 30 to the working pressure range and the performance of the pump can be improved.

Die Herstellung der Nuten auf der inneren Mantelfläche der Hülse soll anhand der Fig. 4 bis 6 näher erläutert werden.The preparation of the grooves on the inner circumferential surface of the sleeve is based on the 4 to 6 be explained in more detail.

Eine Negativform 70 besitzt einen zylindrischen Abschnitt, auf dessen Mantelfläche eine schraubenlinienartige Formnut 72 eingebracht ist. In diese Formnut 72 wird nun bandartiges Fasermaterial 74 gewickelt, so dass die Formnut 72 nach und nach aufgefüllt wird. Fig. 5 zeigt einen halbgefüllten Zustand im Querschnitt. Ist die Formnut 72 gefüllt und die Matrix geschaffen, ist das Herstellen der dritten Schicht 54 beendet. Nun werden Fasern 76 um die Mantelfläche selbst gewickelt, vergleiche Fig. 6, und so die Schicht 50 hergestellt.A negative mold 70 has a cylindrical portion, on the lateral surface of a helical shape groove 72 is introduced. Ribbon-like fiber material 74 is now wound in this molding groove 72, so that the molding groove 72 is gradually filled up. Fig. 5 shows a half-filled state in cross section. When the forming groove 72 is filled and the matrix is created, the third layer 54 is finished. Now, fibers 76 are wound around the outer surface itself, cf. Fig. 6 , and so made the layer 50.

Die Formnut 72 kann als mehrgängige Schraubenlinie geformt sein.The molding groove 72 may be formed as a multi-thread helix.

Werden nur die Formnuten 72 gefüllt und anschließend die Mantelfläche gewickelt, entsteht eine Hülse 24, die lediglich innen eine Nut aufweist. Dies schafft ein sehr stabiles Gebilde.If only the mold grooves 72 are filled and then the jacket surface is wound, a sleeve 24 is created which has a groove only on the inside. This creates a very stable structure.

Nach dem abgeschlossenen Wickelvorgang wird die Negativform 70 durch Herausdrehen aus der hergestellten Hülse 24 entfernt.After the completed winding process, the female mold 70 is removed by unscrewing from the sleeve 24 produced.

Die vakuumtechnische Leistungsfähigkeit der Anordnung soll anhand der Fig. 9 belegt werden. In ihr ist das Druckverhältnis zwischen Einlass und Auslass bei nicht vorhandenem Gasdurchsatz, die so genannte Leerlaufkompression, über dem Ausstoßdruck dargestellt. Die Kurve 300 zeigt eine übliche Anordnung, in der lediglich ein Stator eine schraubenlinienartige Nut aufweist, wie sie beispielsweise in so genannten Holweckpumpstufen verwendet wird. Die Kurve 302 zeigt eine Anordnung mit einer Nut auf dem Rotor. Die Leerlaufkompression ist deutlich erhöht.The vacuum technical efficiency of the arrangement is based on the Fig. 9 be occupied. In it, the pressure ratio between the inlet and outlet in the absence of gas flow, the so-called idle compression over represented the discharge pressure. The curve 300 shows a conventional arrangement in which only one stator has a helical groove, as used for example in so-called Holweckpumpstufen. The curve 302 shows an arrangement with a groove on the rotor. The idle compression is significantly increased.

Die Verwendung der Erfindung ist nicht auf den bisher gezeigten Fall beschränkt.The use of the invention is not limited to the case shown so far.

In Fig. 7 ist eine zweiflutige Vakuumpumpe im Schnitt gezeigt. Sie besitzt ein Gehäuse 202, welches mit einem Gaseinlass 204 und zwei Gasauslässen 206 ausgerüstet ist. Die Gasauslässe 206 können durch einen im Gehäuse 202 vorgesehenen inneren Kanal zusammengefasst sein. Ein Rotor 212 ist in Lagern 208 und 210 drehbar gelagert und wird von einem Antrieb 218 angetrieben. Der Rotor 212 weist einen Abschnitt mit einer Hülse 224 auf, auf deren äußeren Mantelfläche zwei Nuten 230a und 230b nach oben beschriebenem Verfahren geformt sind. Die Förderrichtung der Nuten 230a, 230b ist entgegengesetzt und von dem Gaseinlass 204 weggerichtet, wie die Pfeile in Fig. 7 verdeutlichen. Die Nuten 230a, 230b weisen einen entgegengesetzten Drehsinn auf. Die Nuten auf dem Abschnitt wirken mit statorseitigen Nuten 242a und 242b zusammen, die ebenfalls schraubenlinienartig mit entgegengesetztem Drehsinn gestaltet sind. Die Nuten 230a, 230b der Hülse 224 sind den statorseitigen Nuten 242a, 242b gegenüberliegend angeordnet.In Fig. 7 a double-flow vacuum pump is shown in section. It has a housing 202 which is equipped with a gas inlet 204 and two gas outlets 206. The gas outlets 206 may be combined by an inner channel provided in the housing 202. A rotor 212 is rotatably mounted in bearings 208 and 210 and is driven by a drive 218. The rotor 212 has a section with a sleeve 224, on the outer circumferential surface of which are formed two grooves 230a and 230b according to the above-described method. The conveying direction of the grooves 230a, 230b is opposite and directed away from the gas inlet 204, as the arrows in FIG Fig. 7 clarify. The grooves 230a, 230b have an opposite direction of rotation. The grooves on the portion cooperate with stator-side grooves 242a and 242b, which are also helically designed in opposite directions of rotation. The grooves 230a, 230b of the sleeve 224 are arranged opposite the stator-side grooves 242a, 242b.

Einen anderen Gestaltungsgesichtspunkt zeigt Fig. 8 auf. Ein Abschnitt 222' besitzt eine schraubenlinienartige Nut, die einen ersten Nutabschnitt 250 und einen zweiten Nutabschnitt 254 aufweist. Die Geometrien, insbesondere die Querschnitte, der Nutabschnitte 250, 254 sind unterschiedlich. So weist der erste Nutabschnitt 250 einen halbkreisförmigen Querschnitt und der zweite Nutabschnitt 254 einen dreieckigen Querschnitt auf. Zwischen den Nutabschnitten 250, 254 ist eine umlaufende Nut 260 vorgesehen. Die Querschnitte erlauben eine Anpassung an den Druckbereich, in dem der jeweilige Nutabschnitt bevorzugt wirken soll. Alternativ oder zusätzlich können die Geometrien in Bezug auf die Steigung der Schraubenlinie voneinander abweichen. Der umlaufende Nutabschnitt kann am Übergangspunkt zwischen unterschiedlichen Strömungsbereichen vorgesehen sein.Shows another design point of view Fig. 8 on. A portion 222 'has a helical groove having a first groove portion 250 and a second groove portion 254. The geometries, in particular the cross sections, of the groove sections 250, 254 are different. Thus, the first groove portion 250 has a semicircular cross section and the second groove portion 254 has a triangular cross section. Between the groove portions 250, 254, a circumferential groove 260 is provided. The cross sections allow adaptation to the pressure region in which the respective groove section is to act preferentially. Alternatively or additionally, the geometries may differ with respect to the pitch of the helix. The circumferential groove portion may be provided at the transition point between different flow areas.

Bezugszahlenreference numerals

22
Gehäusecasing
44
Einlassinlet
66
Auslassoutlet
88th
PermanentmagnetlagerPermanent magnetic bearings
1010
WälzlagerRolling
1212
Rotorrotor
1414
turbomolekularer Pumpabschnittturbomolecular pump section
1616
molekularer Pumpabschnittmolecular pump section
1818
Antriebdrive
2020
Nabehub
2222
Abschnitt des molekularen Pumpabschnittes 16Section of the molecular pumping section 16
2424
Hülseshell
2626
Abschlusskanteterminal edge
2828
Stegweb
3030
Nutgroove
3232
eine innere Nutan inner groove
3434
erster Stegfirst jetty
3636
zweite innere Nutsecond inner groove
3838
zweiter Stegsecond bridge
4040
Statorstator
4242
Mantelfläche des Stators 40Lateral surface of the stator 40
5050
erste Schichtfirst shift
5252
zweite Schicht, mittlere Schichtsecond layer, middle layer
5454
dritte Schichtthird layer
6060
Fasernfibers
6262
Matrixmatrix
6464
zweite Matrixsecond matrix
7070
Negativformnegative form
7272
Formnutforming groove
7474
bandartiges Fasermaterialband-like fiber material
7676
bandartiges Fasermaterialband-like fiber material
202202
Gehäusecasing
204204
Gaseinlassgas inlet
206206
Gasauslässegas outlets
208208
Lagerwarehouse
210210
Lagerwarehouse
212212
Rotorrotor
218218
Antriebdrive
222'222 '
Abschnittsection
224224
Hülseshell
230a230a
Nutengroove
230b230b
Nutengroove
242a242a
statorseitige Nutenstator-side grooves
242b242b
statorseitige Nutenstator-side grooves
250250
Nutabschnittgroove
254254
zweiter Nutabschnittsecond groove section
260260
Nutgroove
300300
KurveCurve
302302
KurveCurve
310310
Drehachseaxis of rotation
312312
Winkelcorner
314314
Faserrichtungthe grain
316316
Faserrichtungthe grain
320320
erster Winkelfirst angle
322322
zweiter Winkelsecond angle
SS
Schichtstärkelayer thickness
TT
Nuttiefegroove depth

Claims (15)

  1. Part (22; 224; 222') for a rotor (12; 212) of a vacuum pump, which comprises a fibre composite material with a fibre direction (314, 316), characterised in that the part (22; 224; 222') has a groove (30; 32, 36; 230a; 230b; 250, 254) and fibres (60) of the fibre composite material are oriented such that at least a part of the fibres (60) is aligned with the fibre direction (314, 316) parallel to the groove (30; 32, 36; 230a; 230b; 250, 254), so that the part resists the influence of centrifugal forces during operation of the vacuum pump.
  2. Vacuum pump with a rotor (12; 212), which comprises at least one part (22; 224; 222') according to the preamble of claim 1, made of a fibre composite material with at least one fibre direction (314, 316), characterised in that the part (22; 224; 222') comprises at least one helically arranged groove (30; 32, 36; 230a, 230b) and fibres (60) of the fibre composite material are oriented such that at least a part of the fibres (60) is aligned with the fibre direction (314, 316) parallel to the groove (30; 32, 36; 230a, 230b).
  3. Vacuum pump according to claim 2, characterised in that the part (22; 224; 222') comprises a sleeve (24; 224).
  4. Vacuum pump according to claim 3, characterised in that provided on an interior side of the sleeve (24; 224) is an inner groove (32, 36) and provided on an exterior side of the sleeve (24; 224) is an outer groove (30).
  5. Vacuum pump according to one of the preceding claims, characterised in that the groove (30; 230a; 230b) extends completely over an axial extent of the at least one part (22; 224; 222').
  6. Vacuum pump according to one of the preceding claims, characterised in that a wrap angle of the groove (30; 32, 36; 230a; 230b) is more than 360°.
  7. Vacuum pump according to one of the preceding claims, characterised in that the part (22; 224; 222') comprises at least one first and one second layer (50, 52), wherein the groove (30; 32, 36; 230a; 230b) is arranged in one of the layers (50, 52).
  8. Vacuum pump according to claim 7, characterised in that the first layer (50) comprises a first matrix (62) and the second layer (52) comprises a second matrix (64).
  9. Vacuum pump according to one of the preceding claims, characterised in that the groove comprises a first groove portion (250) and a second groove portion (254) with mutually different geometries.
  10. Vacuum pump according to claim 9, characterised in that a groove (260) encircling the rotor (12) is provided between the first and the second groove portion (250, 254).
  11. Method for producing a rotor (12; 212) of a vacuum pump, which comprises a sleeve (24; 224; 222'), in which the sleeve (24; 224; 222') is wound from a fibre material with a fibre direction (314, 316) and the fibre material is embedded in a plastics matrix to form a fibre composite material, characterised in that the fibre direction (314, 316) is wound at an angle (312) to a termination edge (26) of the sleeve and a groove (30; 32, 36; 230a; 230b; 250, 254) is formed aligned to the fibre direction.
  12. Method according to claim 11, characterised in that the formation of the groove (30; 32, 36; 230a; 230b; 250, 254) comprises a milling along the fibre direction (314, 316).
  13. Method according to claim 11 or 12, characterised in that the formation of the groove (30; 32, 36; 230a; 230b; 250, 254) comprises the winding of the fibre material onto a negative mould (70).
  14. Method according to one of the claims 11 to 13, characterised in that a first layer (50) is wound with a first fibre direction (314) and a second layer (52) is wound with a second fibre direction (316) and the groove is formed in at least one of the layers.
  15. Method according to one of the claims 11 to 14, characterised in that the groove is formed with a first groove portion (250) and a second groove portion (254) with mutually different geometries.
EP12180536.0A 2011-09-05 2012-08-15 Vacuum pump Active EP2565463B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2012193204A JP5468117B2 (en) 2011-09-05 2012-09-03 Vacuum pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102011112691A DE102011112691A1 (en) 2011-09-05 2011-09-05 vacuum pump

Publications (3)

Publication Number Publication Date
EP2565463A2 EP2565463A2 (en) 2013-03-06
EP2565463A3 EP2565463A3 (en) 2015-10-14
EP2565463B1 true EP2565463B1 (en) 2019-01-23

Family

ID=46963388

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12180536.0A Active EP2565463B1 (en) 2011-09-05 2012-08-15 Vacuum pump

Country Status (3)

Country Link
EP (1) EP2565463B1 (en)
JP (1) JP5468117B2 (en)
DE (1) DE102011112691A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
TWI586893B (en) * 2011-11-30 2017-06-11 Edwards Japan Ltd Vacuum pump
DE202013009660U1 (en) * 2013-10-31 2015-02-03 Oerlikon Leybold Vacuum Gmbh Bearing holding element for a bearing element of a rotor shaft of a vacuum pump and vacuum pump
DE102013114290A1 (en) 2013-12-18 2015-06-18 Pfeiffer Vacuum Gmbh vacuum pump
JP2016166594A (en) * 2015-03-10 2016-09-15 株式会社島津製作所 Vacuum pump
CN106015034A (en) * 2016-07-11 2016-10-12 中国工程物理研究院机械制造工艺研究所 High-pressure ratio compound molecular pump

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19632375A1 (en) 1996-08-10 1998-02-19 Pfeiffer Vacuum Gmbh Gas friction pump
JP2000337289A (en) * 1999-05-24 2000-12-05 Seiko Seiki Co Ltd Thread groove type vacuum pump, composite vacuum pump and vacuum pump system
FR2845737B1 (en) 2002-10-11 2005-01-14 Cit Alcatel TURBOMOLECULAR PUMP WITH COMPOSITE SKIRT
GB0229356D0 (en) * 2002-12-17 2003-01-22 Boc Group Plc Vacuum pumping arrangement
GB2420379A (en) * 2004-11-18 2006-05-24 Boc Group Plc Vacuum pump having a motor combined with an impeller
DE102005008643A1 (en) * 2005-02-25 2006-08-31 Leybold Vacuum Gmbh Holweck vacuum pump has shoulders on rotor side of vanes of vane disc to support supporting ring
GB0503946D0 (en) * 2005-02-25 2005-04-06 Boc Group Plc Vacuum pump
JP2009108752A (en) * 2007-10-30 2009-05-21 Edwards Kk Vacuum pump

Non-Patent Citations (1)

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

Also Published As

Publication number Publication date
EP2565463A2 (en) 2013-03-06
EP2565463A3 (en) 2015-10-14
JP5468117B2 (en) 2014-04-09
DE102011112691A1 (en) 2013-03-07
JP2013053627A (en) 2013-03-21

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