EP1443214A1 - Turbomolecular pump stator - Google Patents

Turbomolecular pump stator Download PDF

Info

Publication number
EP1443214A1
EP1443214A1 EP04290163A EP04290163A EP1443214A1 EP 1443214 A1 EP1443214 A1 EP 1443214A1 EP 04290163 A EP04290163 A EP 04290163A EP 04290163 A EP04290163 A EP 04290163A EP 1443214 A1 EP1443214 A1 EP 1443214A1
Authority
EP
European Patent Office
Prior art keywords
stator
fins
sectors
sector
turbomolecular pump
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP04290163A
Other languages
German (de)
French (fr)
Other versions
EP1443214B1 (en
Inventor
Laurent Maniglier
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.)
Alcatel Lucent SAS
Original Assignee
Alcatel CIT SA
Alcatel SA
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
Application filed by Alcatel CIT SA, Alcatel SA filed Critical Alcatel CIT SA
Publication of EP1443214A1 publication Critical patent/EP1443214A1/en
Application granted granted Critical
Publication of EP1443214B1 publication Critical patent/EP1443214B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • F04D29/40Casings; 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
    • 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/64Mounting; Assembling; Disassembling of axial pumps
    • F04D29/644Mounting; Assembling; Disassembling of axial pumps especially adapted for elastic fluid pumps

Definitions

  • the present invention relates to pumps turbomolecular, suitable for pumping gases and creating a vacuum pushed into an empty enclosure.
  • Turbomolecular pumps usually have a stator multistage device with fins engaged between fins of a multi-stage central rotor.
  • a multistage turbomolecular pump rotor includes a axial series of rotor stages each consisting of a crown central from which depart, in a substantially radial direction, rotor fins regularly distributed around the periphery of the central crown.
  • the assembly is rotatably mounted along an axis of rotation, and is driven by motor means.
  • the multistage stator is composed of an axial series of annular stators each forming a stator stage, each stage stator being formed of an annular rim from which depart, in substantially radial direction, inclined fins.
  • stator stage inclined fins come engage between the inclined fins of two rotor stages successive.
  • turbomolecular pumps include means for mounting and dismounting radial elements stator around the rotor.
  • stator After having produced a multi-stage monobloc rotor, we realizes the stator by gradually assembling around the rotor elements or sub-assemblies intended to constitute the stator.
  • a first known pump stator structure turbomolecular is illustrated in figure 1.
  • a rotor monobloc not shown in the figure, we just adapt gradually a plurality of fin stator sectors, on the one hand to form annular stator stages, on the other hand to form the plurality of staggered annular stator stages axially to make the successive stages of the stator.
  • annular spacer 5 is axially engaged, by movement according to arrow 6, the spacer 5 coming to bear on the periphery of the two stator sectors 1 and 3.
  • the spacer 5 has the dimension necessary to separate two successive stator stages according to the spacing of two corresponding successive rotor stages.
  • stator sectors 7 and 8 we position the two in a similar way following stator sectors 7 and 8, then an annular spacer 9, then two stator sectors 10 and 11 and a spacer annular 12, and so on depending on the number of stages of the stator.
  • Figure 2 illustrates a second known pump structure turbomolecular, with different means to solve the problem of the nesting of the stator fins in the fins of the rotor.
  • the rotor 13 has been illustrated, rotatably mounted around its axis of rotation I-I as illustrated by arrow 14, and comprising a series of rotor stages each having inclined fins.
  • rotor stages successive identified by the reference numerals 13a, 13b, 13c, 13d, 13e, 13f, 13g, 13h and 13i.
  • the stator 15 is formed of the assembly of two half-stators 15a and 15b, each half-stator 15a and 15b consisting of a half-shell 16a or 16b in the form of half cylinder from which radially inward stator fins such as fins 17a and 17b, arranged in a series of stator stages overlapping with the fins of the rotor stages 13a-13i.
  • two monoblock half-stators 15a and 15b allows for insertable pumps, intended to be housed directly into a customer's pre-defined housing or system.
  • each half-stator 15a or 15b monobloc is machined in a metal block to constitute the fins 17a or 17b. Because of the configuration and the convergent radial orientation of the fins, protruding from the concave inner face of the peripheral half-shell 16a or 16b, it is not possible to machine fins 17a or 17b whose radial length exceeds a maximum length determined by the possibility of passage of the milling tools of the fins.
  • this known pump structure turbomolecular limits the maximum flow rate of the pump turbomolecular, the flow limit being determined by the radial length of the fins.
  • the problem proposed by the present invention is to design a new turbomolecular pump structure which can be carried out at lower cost, avoiding the assembly of too much large number of parts or the production of complex parts, and which allows for insertable turbomolecular pumps whose flow is greater than that obtained by the structure of the figure 2.
  • Another problem is also to avoid having to make component parts whose dimensions are very precise because it increases the production cost of the pump turbomolecular.
  • stator sectors to fins constitute individual elements which can be easily manufactured by machining metal parts, and the ease of machining makes it possible to produce stators with fins have a radial dimension greater than that which can be achieved in a structure of figure 2.
  • turbomolecular pump structure can be realized with less tight tolerances than the structural parts of the FIG. 1, because the peripheral shell sector achieves by itself, with the retaining means, a multi-stage spacer which individually positions the stator sectors with fins, so there is not a stack of multiple pieces put them one after the other.
  • the sectors of stator with fins include a single row of fins, each constituting a single-stage stator sector.
  • fin stator sectors comprising two or more rows of fins, each constituting a sector multi-stage finned partial stator, insofar as the machining of the fins allows this.
  • the stator sectors with fins can thus include at least one annular row of fins integral with a rim in crown sector shape.
  • the rim can connect the outer ends of the fins, and it's the rim that forms then the peripheral edge of the finned stator sector and which attaches to the concave inner face of the peripheral shell sector corresponding to form the multistage stator sector.
  • the rim connects the inner ends of the fins.
  • this structure achieves better performance efficiency empty, and the realization is facilitated by the fact that the machining of fins is made from outside the rim in the sector of crown, on fins in divergent radial orientations. This are then the outer ends of the fins which form the peripheral edge of the stator sector with fins and which are fixed to the concave inner face of the peripheral hull sector corresponding to form the multistage stator sector.
  • the means of restraint of the stator sectors with fins on the concave inner face of the peripheral shell sector can be of different kinds.
  • the concave inner face of the hull sector peripheral comprises a plurality of annular grooves, and the finned stator sectors each have at least one edge peripheral which is radially embedded in force in one annular grooves in the peripheral hull sector.
  • the edge (s) devices of the finned stator sectors are constituted by the outer ends of the fins of said stator sectors which are radially embedded in force in the grooves corresponding annulars of the peripheral hull sector.
  • stator sectors have a rim which connects the outer ends of the fins
  • edge (s) devices of the finned stator sectors are constituted by the rims themselves which fit into the grooves annulars of the peripheral hull sector.
  • the turbomolecular pump according to the invention comprises a multistage rotor 18, comprising a series rotor stages axially offset from each other and identified by the reference numbers 18a, 18b, 18c, 18d, 18th, 18f, 18g, 18h, 18i and 18d.
  • Each stage of the rotor 18 is formed of a inner crown such as crown 19 from which depart inclined fins such as the fin 18a oriented in substantially radial outward direction.
  • the rotor 18 is rotatably mounted around an axis of rotation I-I as indicated by arrow 20.
  • the stator is formed from the assembly of two sub-assemblies 21 and 22 each forming a multistage stator sector, which are reported radially around the rotor 18 as indicated by the respective arrows 23 and 23a.
  • Each sub-assembly 21 or 22 is formed from the assembly a respective peripheral hull sector 24 or 25 and a axial row of stator sectors with fins 26 or 27.
  • a first axial row of stator sectors to fins 26 formed by the stator sectors with fins 26a, 26b, 26c, 26d, 26e, 26f, 26g, 26h, 26i and 26j aligned parallel to the axis of rotation I-I.
  • a second row axial of finned stator sectors formed by the sectors of stator with fins 27a, 27b, 27c, 27d, 27e, 27f, 27g, 27h, 27i and 27j aligned parallel to the axis of rotation I-I.
  • the sectors stator with fins are of the inner rim type, as see better in Figure 5.
  • the sector stator of fins 26a includes an annular row of fins 126a integral with a rim 226a itself in the form of a sector of crowned. Rim 226a connects the inner ends of the fins of the annular row of fins 126a. The edge device 326a of the finned stator sector 26a is then formed by the outer ends of the row fins fin ring 126a.
  • the invention can also be applied to a second mode of realization of stator sector with fins illustrated in the figure 6.
  • Rim 226a connects the outer ends of the fins of the annular row of fins 126a.
  • the edge device 326a of the finned stator sector 26a is then constituted by the rim 226a itself.
  • each peripheral shell sector 24 or 25 comprises a plurality of annular grooves.
  • annular grooves 24a, 24b, 24c, 24d, 24e, 24f, 24g, 24h, 24i and 24d we can thus distinguish the annular grooves 24a, 24b, 24c, 24d, 24e, 24f, 24g, 24h, 24i and 24d.
  • Each annular groove 24a-24j is arranged and shaped to receive the peripheral edge of one of the stator sectors 26a-26j, and to thereby hold said positions individually stator sectors 26a-26j.
  • peripheral shell sector 25 which receives and retains the finned stator sectors 27a-27j.
  • the hull sectors peripheral such as the peripheral shell sector 25 can if necessary, include holes such as hole 29, to favor the degassing of the space located on the periphery of the sectors peripheral hulls 24 and 25.
  • the stator is made by assembling two half-stators multistage 21 and 22 each consisting of a 180 ° sector.
  • each peripheral shell sector 24 or 25 is a half-cylinder
  • each fin stator sector 26a-26j and 27a-27j is a half ring.
  • stator is a radial assembly of a single stage of multi-stage sectors of stator 21 and 22.
  • each peripheral shell sector 24 or 25 covers the entire length of the stator of the turbomolecular pump.
  • the stator can be an assembly of several stages of multistage stator sectors.
  • a first stator stage as illustrated on the FIG. 3, to which a second coaxial stage of stator with similar structure, possibly with structures different fins and different diameters.
  • the stator is then an assembly of several floors of multi-level sectors of stator.
  • a pump can be produced. insertable turbomolecular, i.e. adapted to be inserted in a housing or customer system such as a vacuum enclosure.
  • the pump is then installed as close as possible to the application and optimizes pumping performance.
  • the sectors of shell 24 and 25 allow the pump elements to be enclosed turbomolecular, to form a possibly held whole by means of temporary assembly, which can be removed during the introduction of the pump into the customer's system.
  • the hull sectors 24 and 25 must preferably fit with little play in the housing or the system of the customer, to ensure between hull sectors 24 and 25 and the housing or customer system a good contact that promotes heat exchanges.
  • the turbomolecular pump structure according to the invention authorizes all possible fin geometries in terms inclination, inside diameter, outside diameter, floor height and thickness.
  • This system also simplifies the stacking of spacers and stators, and to get rid of the chain of ratings of these different elements.
  • this structure improves the heat exchange between the rotor and the environment, via hull areas, promoting thermal contact between the stator fins and hull sectors, then between the hull sectors and the peripheral casing or shell of the pump, and reducing the number of transmission discontinuities thermal thanks to the monobloc character of the hull sectors multistage.
  • This structure makes it possible to offer an insertable version for higher flow rate vacuum pumps.

Abstract

The pump has a stator including blade sectors (26a-26j) arranged around a rotor (18), where the blade sectors are divided into axial lines. The blade sectors are connected and integrated with a concave internal face of corresponding peripheral structure (24,25) of the stator to form a multi-stage sector. The internal face has retaining units (24a-24j) for retaining individually each sector blade in a position.

Description

La présente invention concerne les pompes turbomoléculaires, adaptées pour pomper des gaz et créer un vide poussé dans une enceinte à vide.The present invention relates to pumps turbomolecular, suitable for pumping gases and creating a vacuum pushed into an empty enclosure.

Les pompes turbomoléculaires ont généralement un stator périphérique multiétagé à ailettes engagées entre des ailettes d'un rotor central multiétagé.Turbomolecular pumps usually have a stator multistage device with fins engaged between fins of a multi-stage central rotor.

Un rotor multiétagé de pompe turbomoléculaire comprend une série axiale d'étages rotors constitués chacun d'une couronne centrale de laquelle partent, en direction sensiblement radiale, des ailettes de rotor réparties régulièrement en périphérie de la couronne centrale. L'ensemble est monté rotatif selon un axe de rotation, et est entraíné par des moyens moteurs.A multistage turbomolecular pump rotor includes a axial series of rotor stages each consisting of a crown central from which depart, in a substantially radial direction, rotor fins regularly distributed around the periphery of the central crown. The assembly is rotatably mounted along an axis of rotation, and is driven by motor means.

Le stator multiétagé est composé d'une série axiale de stators annulaires formant chacun un étage stator, chaque étage stator étant formé d'une jante annulaire de laquelle partent, en direction sensiblement radiale, des ailettes inclinées.The multistage stator is composed of an axial series of annular stators each forming a stator stage, each stage stator being formed of an annular rim from which depart, in substantially radial direction, inclined fins.

Les ailettes inclinées d'un étage stator viennent s'engager entre les ailettes inclinées de deux étages rotors successifs.The stator stage inclined fins come engage between the inclined fins of two rotor stages successive.

On comprend donc que la présence des ailettes imbriquées les unes dans les autres empêche tout mouvement axial du rotor par rapport au stator, soit pour le montage de la pompe turbomoléculaire, soit pour son démontage.We therefore understand that the presence of nested fins one inside the other prevents any axial movement of the rotor by report to the stator, either for mounting the pump turbomolecular, either for its disassembly.

Par conséquent, les pompes turbomoléculaires comprennent des moyens permettant le montage et le démontage radial d'éléments du stator autour du rotor.Therefore, turbomolecular pumps include means for mounting and dismounting radial elements stator around the rotor.

Après avoir réalisé un rotor monobloc multiétagé, on réalise le stator en assemblant progressivement autour du rotor des éléments ou sous-ensembles destinés à constituer le stator.After having produced a multi-stage monobloc rotor, we realizes the stator by gradually assembling around the rotor elements or sub-assemblies intended to constitute the stator.

Une première structure connue de stator de pompe turbomoléculaire est illustrée sur la figure 1. Autour d'un rotor monobloc, non représenté sur la figure, on vient adapter progressivement une pluralité de secteurs de stator à ailettes, d'une part pour former des étages stators annulaires, d'autre part pour former la pluralité d'étages stators annulaires décalés axialement pour réaliser les étages successifs du stator. A first known pump stator structure turbomolecular is illustrated in figure 1. Around a rotor monobloc, not shown in the figure, we just adapt gradually a plurality of fin stator sectors, on the one hand to form annular stator stages, on the other hand to form the plurality of staggered annular stator stages axially to make the successive stages of the stator.

Si l'on considère un rotor orienté avec son axe de rotation vertical, on vient positionner un premier secteur de stator à ailettes 1 entre deux étages rotors successifs à ailettes, par déplacement radial illustré par la flèche 2, et l'on engage un deuxième secteur de stator 3 par déplacement radial opposé selon la flèche 4 pour l'engager entre les mêmes deux étages rotors à ailettes, les deux secteurs de stator 1 et 3 formant un étage stator annulaire.If we consider a rotor oriented with its axis of vertical rotation, we just position a first sector of stator with fins 1 between two successive stages rotor with fins, by radial displacement illustrated by arrow 2, and a second stator sector 3 by opposite radial displacement according to the arrow 4 to engage it between the same two stages rotors to fins, the two stator sectors 1 and 3 forming a stage ring stator.

Ensuite, on engage axialement une entretoise annulaire 5, par mouvement selon la flèche 6, l'entretoise 5 venant en appui sur la périphérie des deux secteurs de stator 1 et 3. L'entretoise 5 a la dimension nécessaire pour écarter deux étages stators successifs selon l'écartement de deux étages rotors successifs correspondants.Then, an annular spacer 5 is axially engaged, by movement according to arrow 6, the spacer 5 coming to bear on the periphery of the two stator sectors 1 and 3. The spacer 5 has the dimension necessary to separate two successive stator stages according to the spacing of two corresponding successive rotor stages.

On positionne ensuite de manière similaire les deux secteurs de stator suivants 7 et 8, puis une entretoise annulaire 9, puis deux secteurs de stator 10 et 11 et une entretoise annulaire 12, et ainsi de suite en fonction du nombre d'étages du stator.Then we position the two in a similar way following stator sectors 7 and 8, then an annular spacer 9, then two stator sectors 10 and 11 and a spacer annular 12, and so on depending on the number of stages of the stator.

On comprend que le montage d'une telle structure est fastidieux, et qu'il nécessite de prévoir des composants dont les dimensions sont déterminées de façon suffisamment précise pour que le cumul des tolérances éventuelles de dimension des composants soit inférieur à la tolérance dimensionnelle axiale du rotor, afin d'éviter le contact entre les ailettes du rotor et les ailettes du stator en cours de fonctionnement de la pompe. Il en résulte un coût de réalisation relativement élevé que l'on pourrait trouver avantage à réduire.We understand that the mounting of such a structure is tedious, and it requires the provision of components whose dimensions are determined with sufficient precision that the cumulation of any dimensional tolerances of the components is less than the axial dimensional tolerance of the rotor, so avoid contact between the rotor fins and the fins of the stator during pump operation. This results in a relatively high cost of realization that one could find advantage to reduce.

La figure 2 illustre une seconde structure connue de pompe turbomoléculaire, comportant des moyens différents pour résoudre le problème de l'imbrication des ailettes du stator dans les ailettes du rotor.Figure 2 illustrates a second known pump structure turbomolecular, with different means to solve the problem of the nesting of the stator fins in the fins of the rotor.

Dans cette structure connue, on a illustré le rotor 13, monté rotatif autour de son axe de rotation I-I comme illustré par la flèche 14, et comportant une série d'étages rotors ayant chacun des ailettes inclinées. On distingue ainsi les étages rotors successifs repérés par les références numériques 13a, 13b, 13c, 13d, 13e, 13f, 13g, 13h et 13i. Le stator 15 est formé de l'assemblage de deux demi-stators 15a et 15b, chaque demi-stator 15a et 15b étant constitué d'une demi-coque 16a ou 16b en forme de demi-cylindre et de laquelle partent radialement vers l'intérieur des ailettes de stator telles que les ailettes 17a et 17b, agencées en une série d'étages stators s'imbriquant avec les ailettes des étages rotors 13a-13i.In this known structure, the rotor 13 has been illustrated, rotatably mounted around its axis of rotation I-I as illustrated by arrow 14, and comprising a series of rotor stages each having inclined fins. We thus distinguish the rotor stages successive identified by the reference numerals 13a, 13b, 13c, 13d, 13e, 13f, 13g, 13h and 13i. The stator 15 is formed of the assembly of two half-stators 15a and 15b, each half-stator 15a and 15b consisting of a half-shell 16a or 16b in the form of half cylinder from which radially inward stator fins such as fins 17a and 17b, arranged in a series of stator stages overlapping with the fins of the rotor stages 13a-13i.

La présence des deux demi-stators 15a et 15b monoblocs permet de réaliser des pompes insérables, destinées à se loger directement dans un carter ou un système prédéfini du client.The presence of two monoblock half-stators 15a and 15b allows for insertable pumps, intended to be housed directly into a customer's pre-defined housing or system.

Dans cette structure, chaque demi-stator 15a ou 15b monobloc est usiné dans un bloc de métal pour constituer les ailettes 17a ou 17b. A cause de la configuration et de l'orientation radiale convergente des ailettes, dépassant de la face intérieure concave de la demi-coque périphérique 16a ou 16b, il n'est pas possible d'usiner des ailettes 17a ou 17b dont la longueur radiale excède une longueur maximale déterminée par les possibilités de passage des outils de fraisage des ailettes.In this structure, each half-stator 15a or 15b monobloc is machined in a metal block to constitute the fins 17a or 17b. Because of the configuration and the convergent radial orientation of the fins, protruding from the concave inner face of the peripheral half-shell 16a or 16b, it is not possible to machine fins 17a or 17b whose radial length exceeds a maximum length determined by the possibility of passage of the milling tools of the fins.

Il en résulte que cette structure connue de pompe turbomoléculaire limite le débit maximal de la pompe turbomoléculaire, la limite de débit étant déterminée par la longueur radiale des ailettes.As a result, this known pump structure turbomolecular limits the maximum flow rate of the pump turbomolecular, the flow limit being determined by the radial length of the fins.

En outre, la réalisation des demi-stators 15a et 15b par usinage est relativement complexe et onéreuse, de sorte que l'intérêt de cette structure de pompe est limité.In addition, the production of the half-stators 15a and 15b by machining is relatively complex and expensive, so that the advantage of this pump structure is limited.

Le problème proposé par la présente invention est de concevoir une nouvelle structure de pompe turbomoléculaire qui puisse être réalisée à moindre coût, évitant l'assemblage d'un trop grand nombre de pièces ou la réalisation de pièces complexes, et qui permette de réaliser des pompes turbomoléculaires insérables dont le débit est supérieur à celui obtenu par la structure de la figure 2.The problem proposed by the present invention is to design a new turbomolecular pump structure which can be carried out at lower cost, avoiding the assembly of too much large number of parts or the production of complex parts, and which allows for insertable turbomolecular pumps whose flow is greater than that obtained by the structure of the figure 2.

Un autre problème est également d'éviter d'avoir à réaliser des pièces constitutives dont les dimensions sont très précises, car cela augmente le coût de production de la pompe turbomoléculaire.Another problem is also to avoid having to make component parts whose dimensions are very precise because it increases the production cost of the pump turbomolecular.

Pour atteindre ces buts ainsi que d'autres, l'invention propose une pompe turbomoléculaire ayant un stator périphérique multiétagé à ailettes engagées entre des ailettes d'un rotor central multiétagé, dans laquelle :

  • le stator comporte plusieurs secteurs de stator à ailettes assemblés autour du rotor,
  • les secteurs de stator à ailettes sont répartis en plusieurs rangées axiales de secteurs annulaires de stator à ailettes,
  • chaque rangée axiale de secteurs de stator à ailettes est solidaire d'un secteur de coque périphérique et forme ainsi un secteur multiétagé de stator,
  • les secteurs de stator à ailettes constituent chacun un élément individuel,
  • les secteurs de stator à ailettes d'une même rangée axiale de secteurs de stator à ailettes sont rapportés et solidarisés à la face interne concave du secteur de coque périphérique correspondant, pour former le secteur multiétagé de stator,
  • la face interne concave du secteur de coque périphérique comprend des moyens de retenue pour retenir individuellement en position les secteurs de stator à ailettes.
To achieve these and other aims, the invention provides a turbomolecular pump having a multi-stage peripheral stator with fins engaged between fins of a central multi-stage rotor, in which:
  • the stator comprises several stator sectors with fins assembled around the rotor,
  • the stator sectors with fins are divided into several axial rows of annular sectors with stator fins,
  • each axial row of stator sectors with fins is integral with a peripheral shell sector and thus forms a multistage stator sector,
  • the stator sectors with fins each constitute an individual element,
  • the stator sectors with fins of the same axial row of stator sectors with fins are attached and secured to the concave internal face of the corresponding peripheral shell sector, to form the multistage stator sector,
  • the concave inner face of the peripheral shell sector includes retaining means for individually retaining the stator sectors with fins.

Dans une telle structure, les secteurs de stator à ailettes constituent des éléments individuels qui peuvent être aisément fabriqués par usinage de pièces métalliques, et la facilité d'usinage permet de réaliser des stators dont les ailettes ont une dimension radiale supérieure à celle qui peut être réalisée dans une structure de la figure 2.In such a structure, the stator sectors to fins constitute individual elements which can be easily manufactured by machining metal parts, and the ease of machining makes it possible to produce stators with fins have a radial dimension greater than that which can be achieved in a structure of figure 2.

Simultanément, le nombre de pièces à assembler lors du montage d'une pompe turbomoléculaire est réduit par rapport à la structure connue de la figure 1.Simultaneously, the number of parts to be assembled during the mounting of a turbomolecular pump is reduced compared to the known structure of figure 1.

Et simultanément, les pièces constitutives d'une telle structure de pompe turbomoléculaire peuvent être réalisées avec des tolérances moins strictes que les pièces de la structure de la figure 1, car le secteur de coque périphérique réalise par lui-même, avec les moyens de retenue, une entretoise multiétagée qui positionne individuellement les secteurs de stator à ailettes, de sorte qu'il n'y a pas un empilement de plusieurs pièces mises les unes à la suite des autres. And simultaneously, the constituent parts of such turbomolecular pump structure can be realized with less tight tolerances than the structural parts of the FIG. 1, because the peripheral shell sector achieves by itself, with the retaining means, a multi-stage spacer which individually positions the stator sectors with fins, so there is not a stack of multiple pieces put them one after the other.

Selon un mode de réalisation avantageux, les secteurs de stator à ailettes comprennent une seule rangée d'ailettes, constituant chacun un secteur de stator monoétagé.According to an advantageous embodiment, the sectors of stator with fins include a single row of fins, each constituting a single-stage stator sector.

On pourra toutefois, sans sortir du domaine de l'invention, imaginer des secteurs de stator à ailettes comprenant deux ou plusieurs rangées d'ailettes, constituant chacun un secteur de stator partiel à ailettes multiétagé, dans la mesure où l'usinage des ailettes le permet.We can, however, without leaving the domain of the invention, imagine fin stator sectors comprising two or more rows of fins, each constituting a sector multi-stage finned partial stator, insofar as the machining of the fins allows this.

Les secteurs de stator à ailettes peuvent ainsi comprendre au moins une rangée annulaire d'ailettes solidaires d'une jante en forme de secteur de couronne.The stator sectors with fins can thus include at least one annular row of fins integral with a rim in crown sector shape.

Selon une première possibilité, la jante peut relier les extrémités extérieures des ailettes, et c'est la jante qui forme alors le bord périphérique du secteur de stator à ailettes et qui se fixe à la face interne concave du secteur de coque périphérique correspondant pour former le secteur multiétagé de stator.According to a first possibility, the rim can connect the outer ends of the fins, and it's the rim that forms then the peripheral edge of the finned stator sector and which attaches to the concave inner face of the peripheral shell sector corresponding to form the multistage stator sector.

Toutefois, on pourra trouver avantage à prévoir que la jante relie les extrémités intérieures des ailettes. En effet, cette structure réalise une meilleure efficacité des performances vide, et la réalisation est facilitée par le fait que l'usinage des ailettes se fait depuis l'extérieur de la jante en secteur de couronne, sur des ailettes en orientations radiales divergentes. Ce sont alors les extrémités extérieures des ailettes qui forment le bord périphérique du secteur de stator à ailettes et qui se fixent à la face interne concave du secteur de coque périphérique correspondant pour former le secteur multiétagé de stator.However, it may be advantageous to provide that the rim connects the inner ends of the fins. Indeed, this structure achieves better performance efficiency empty, and the realization is facilitated by the fact that the machining of fins is made from outside the rim in the sector of crown, on fins in divergent radial orientations. This are then the outer ends of the fins which form the peripheral edge of the stator sector with fins and which are fixed to the concave inner face of the peripheral hull sector corresponding to form the multistage stator sector.

Les moyens de retenue des secteurs de stator à ailettes sur la face interne concave du secteur de coque périphérique peuvent être de différentes sortes. Selon un mode de réalisation avantageux, la face interne concave du secteur de coque périphérique comprend une pluralité de gorges annulaires, et les secteurs de stator à ailettes comportent chacun au moins un bord périphérique qui vient s'encastrer radialement en force dans l'une des gorges annulaires du secteur de coque périphérique.The means of restraint of the stator sectors with fins on the concave inner face of the peripheral shell sector can be of different kinds. According to one embodiment advantageous, the concave inner face of the hull sector peripheral comprises a plurality of annular grooves, and the finned stator sectors each have at least one edge peripheral which is radially embedded in force in one annular grooves in the peripheral hull sector.

Dans le cas où les secteurs de stator ont une jante qui relie les extrémités intérieures des ailettes, le ou les bords périphériques des secteurs de stator à ailettes sont constitués par les extrémités extérieures des ailettes desdits secteurs de stator qui viennent s'encastrer radialement en force dans les gorges annulaires correspondantes du secteur de coque périphérique.In the case where the stator sectors have a rim which connects the inner ends of the fins, the edge (s) devices of the finned stator sectors are constituted by the outer ends of the fins of said stator sectors which are radially embedded in force in the grooves corresponding annulars of the peripheral hull sector.

Dans le cas où les secteurs de stator ont une jante qui relie les extrémités extérieures des ailettes, le ou les bords périphériques des secteurs de stator à ailettes sont constitués par les jantes elles-mêmes qui viennent s'encastrer dans les gorges annulaires du secteur de coque périphérique.In the case where the stator sectors have a rim which connects the outer ends of the fins, the edge (s) devices of the finned stator sectors are constituted by the rims themselves which fit into the grooves annulars of the peripheral hull sector.

D'autres objets, caractéristiques et avantages de la présente invention ressortiront de la description suivante de modes de réalisation particuliers, faite en relation avec les figures jointes, parmi lesquelles:

  • la figure 1 est une vue éclatée en perspective illustrant une première structure de stator de pompe turbomoléculaire connue dans l'état de la technique ;
  • la figure 2 illustre en perspective une vue éclatée d'une seconde structure de pompe turbomoléculaire connue dans l'état de la technique ;
  • la figure 3 est une vue en perspective éclatée montrant la structure générale d'une pompe turbomoléculaire selon un mode de réalisation de la présente invention ;
  • la figure 4 est une vue en perspective illustrant le montage successif des secteurs de stator à ailettes sur les secteurs de coque périphérique correspondants selon l'invention ; et
  • les figures 5 et 6 illustrent deux modes de réalisation de secteurs de stator à ailettes selon l'invention.
Other objects, characteristics and advantages of the present invention will emerge from the following description of particular embodiments, given in relation to the attached figures, among which:
  • FIG. 1 is an exploded perspective view illustrating a first structure of a turbomolecular pump stator known in the state of the art;
  • FIG. 2 illustrates in perspective an exploded view of a second turbomolecular pump structure known in the state of the art;
  • FIG. 3 is an exploded perspective view showing the general structure of a turbomolecular pump according to an embodiment of the present invention;
  • Figure 4 is a perspective view illustrating the successive mounting of the stator sectors with fins on the corresponding peripheral shell sectors according to the invention; and
  • Figures 5 and 6 illustrate two embodiments of fin stator sectors according to the invention.

Les structures connues de pompes turbomoléculaires des figures 1 et 2 ont été décrites précédemment.The known structures of turbomolecular pumps of Figures 1 and 2 have been described previously.

On se réfère maintenant aux figures 3 et 4 illustrant la structure d'une pompe turbomoléculaire selon un mode de réalisation de la présente invention.We now refer to Figures 3 and 4 illustrating the structure of a turbomolecular pump according to one embodiment of the present invention.

Sur la figure 3, la pompe turbomoléculaire selon l'invention comprend un rotor 18 multiétagé, comportant une série d'étages rotors axialement décalés les uns par rapport aux autres et repérés par les références numériques 18a, 18b , 18c, 18d, 18e, 18f, 18g, 18h, 18i et 18j. Chaque étage du rotor 18 est formé d'une couronne intérieure telle que la couronne 19 de laquelle partent des ailettes inclinées telles que l'ailette 18a orientée en direction sensiblement radiale vers l'extérieur.In FIG. 3, the turbomolecular pump according to the invention comprises a multistage rotor 18, comprising a series rotor stages axially offset from each other and identified by the reference numbers 18a, 18b, 18c, 18d, 18th, 18f, 18g, 18h, 18i and 18d. Each stage of the rotor 18 is formed of a inner crown such as crown 19 from which depart inclined fins such as the fin 18a oriented in substantially radial outward direction.

Le rotor 18 est monté rotatif autour d'un axe de rotation I-I comme indiqué par la flèche 20.The rotor 18 is rotatably mounted around an axis of rotation I-I as indicated by arrow 20.

Le stator est formé de l'assemblage de deux sous-ensembles 21 et 22 formant chacun un secteur de stator multiétagé, qui sont rapportés radialement autour du rotor 18 comme indiqué par les flèches respectives 23 et 23a.The stator is formed from the assembly of two sub-assemblies 21 and 22 each forming a multistage stator sector, which are reported radially around the rotor 18 as indicated by the respective arrows 23 and 23a.

Chaque sous-ensemble 21 ou 22 est formé de l'assemblage d'un secteur de coque périphérique respectif 24 ou 25 et d'une rangée axiale de secteurs de stator à ailettes 26 ou 27.Each sub-assembly 21 or 22 is formed from the assembly a respective peripheral hull sector 24 or 25 and a axial row of stator sectors with fins 26 or 27.

On distingue ainsi, dans le mode de réalisation représenté, une première rangée axiale de secteurs de stator à ailettes 26 formée par les secteurs de stator à ailettes 26a ,26b, 26c, 26d, 26e, 26f, 26g, 26h, 26i et 26j alignés parallèlement à l'axe de rotation I-I. De même, on distingue une seconde rangée axiale de secteurs de stator à ailettes formée par les secteurs de stator à ailettes 27a ,27b, 27c, 27d, 27e, 27f, 27g, 27h, 27i et 27j alignés parallèlement à l'axe de rotation I-I.We thus distinguish, in the embodiment shown, a first axial row of stator sectors to fins 26 formed by the stator sectors with fins 26a, 26b, 26c, 26d, 26e, 26f, 26g, 26h, 26i and 26j aligned parallel to the axis of rotation I-I. Similarly, there is a second row axial of finned stator sectors formed by the sectors of stator with fins 27a, 27b, 27c, 27d, 27e, 27f, 27g, 27h, 27i and 27j aligned parallel to the axis of rotation I-I.

Dans le mode de réalisation de la figure 3, les secteurs de stator à ailettes sont du type à jante intérieure, comme on le voit mieux sur la figure 5. Dans ce mode de réalisation, le secteur de stator à ailettes 26a comprend une rangée annulaire d'ailettes 126a solidaires d'une jante 226a elle-même en forme de secteur de couronne. La jante 226a relie les extrémités intérieures des ailettes de la rangée annulaire d'ailettes 126a. Le bord périphérique 326a du secteur de stator à ailettes 26a est alors formé par les extrémités extérieures des ailettes de la rangée annulaire d'ailettes 126a.In the embodiment of Figure 3, the sectors stator with fins are of the inner rim type, as see better in Figure 5. In this embodiment, the sector stator of fins 26a includes an annular row of fins 126a integral with a rim 226a itself in the form of a sector of crowned. Rim 226a connects the inner ends of the fins of the annular row of fins 126a. The edge device 326a of the finned stator sector 26a is then formed by the outer ends of the row fins fin ring 126a.

L'invention peut également s'appliquer à un second mode de réalisation de secteur de stator à ailettes illustré sur la figure 6. Dans ce cas, on retrouve une jante 226a et une rangée annulaire d'ailettes 126a. La jante 226a relie les extrémités extérieures des ailettes de la rangée annulaire d'ailettes 126a. Le bord périphérique 326a du secteur de stator à ailettes 26a est alors constitué par la jante 226a elle-même. The invention can also be applied to a second mode of realization of stator sector with fins illustrated in the figure 6. In this case, there is a rim 226a and an annular row of fins 126a. Rim 226a connects the outer ends of the fins of the annular row of fins 126a. The edge device 326a of the finned stator sector 26a is then constituted by the rim 226a itself.

Comme on le voit en relation avec le secteur de coque périphérique 24 de la figure 3, la face interne concave de chaque secteur de coque périphérique 24 ou 25 comprend une pluralité de gorges annulaires. On distingue ainsi les gorges annulaires 24a ,24b, 24c, 24d, 24e, 24f, 24g, 24h, 24i et 24j.As seen in relation to the hull sector peripheral 24 of FIG. 3, the concave internal face of each peripheral shell sector 24 or 25 comprises a plurality of annular grooves. We can thus distinguish the annular grooves 24a, 24b, 24c, 24d, 24e, 24f, 24g, 24h, 24i and 24d.

Chaque gorge annulaire 24a-24j est disposée et conformée pour recevoir le bord périphérique de l'un des secteurs de stator 26a-26j, et pour tenir ainsi individuellement en position lesdits secteurs de stator 26a-26j.Each annular groove 24a-24j is arranged and shaped to receive the peripheral edge of one of the stator sectors 26a-26j, and to thereby hold said positions individually stator sectors 26a-26j.

Il en est de même du secteur de coque périphérique 25 qui reçoit et retient les secteurs de stator à ailettes 27a-27j.It is the same for the peripheral shell sector 25 which receives and retains the finned stator sectors 27a-27j.

Au montage, on commence par engager les secteurs de stator à ailettes 26a-26j et 27a-27j par engagement radial de leur bord périphérique (tel que le bord périphérique 326a du secteur de stator à ailettes 26a) dans les gorges annulaires correspondantes 24a-24j des secteurs de coque périphérique respectifs 24 et 25, comme illustré par exemple par les flèches 28 et 28a. On réalise ainsi les deux secteurs de stator multiétagés 21 et 22, que l'on peut ensuite assembler radialement sur le rotor 18 comme illustré par les flèches 23 et 23a de la figure 3.During assembly, we start by engaging the stator sectors with fins 26a-26j and 27a-27j by radial engagement of their edge peripheral (such as the peripheral edge 326a of the sector of stator with fins 26a) in the corresponding annular grooves 24a-24j of the respective peripheral shell sectors 24 and 25, as illustrated for example by arrows 28 and 28a. We realize thus the two multistage stator sectors 21 and 22, which are can then assemble radially on the rotor 18 as illustrated by arrows 23 and 23a in Figure 3.

On remarquera également que les secteurs de coque périphérique tels que le secteur de coque périphérique 25 peuvent si nécessaire comporter des trous tels que le trou 29, pour favoriser le dégazage de l'espace situé en périphérie des secteurs de coque périphériques 24 et 25.It will also be noted that the hull sectors peripheral such as the peripheral shell sector 25 can if necessary, include holes such as hole 29, to favor the degassing of the space located on the periphery of the sectors peripheral hulls 24 and 25.

Dans la réalisation illustrée sur les figures 3 et 4, le stator est réalisé par l'assemblage de deux demi-stators multiétagés 21 et 22 constitués chacun d'un secteur de 180°. Dans ce cas, chaque secteur de coque périphérique 24 ou 25 est un demi-cylindre, et chaque secteur de stator à ailettes 26a-26j et 27a-27j est un demi-anneau.In the embodiment illustrated in Figures 3 and 4, the stator is made by assembling two half-stators multistage 21 and 22 each consisting of a 180 ° sector. In in this case, each peripheral shell sector 24 or 25 is a half-cylinder, and each fin stator sector 26a-26j and 27a-27j is a half ring.

Selon l'invention, en fonction des conformations d'ailettes, on pourra trouver avantage à prévoir un stator réalisé par l'assemblage de trois secteurs multiétagés de stator de 120° chacun, ou de quatre secteurs multiétagés de stator de 90° chacun, ou encore de secteurs multiétagés de stator d'angles différents. According to the invention, depending on the conformations fins, we could find advantage in providing a stator made by the assembly of three multistage stator sectors of 120 ° each, or four multi-stage stator sectors of 90 ° each, or even multistage stator sectors with different angles.

Toutefois, la structure illustrée minimise le nombre de pièces à assembler, ce qui peut s'avérer avantageux.However, the structure illustrated minimizes the number of parts to be assembled, which can be advantageous.

Egalement, dans le mode de réalisation illustré sur les figures 3 et 4, le stator est un assemblage radial d'un seul étage de secteurs multiétagés de stator 21 et 22. Autrement dit, dans ce cas, chaque secteur de coque périphérique 24 ou 25 couvre toute la longueur du stator de la pompe turbomoléculaire.Also, in the embodiment illustrated on the Figures 3 and 4, the stator is a radial assembly of a single stage of multi-stage sectors of stator 21 and 22. In other words, in this case, each peripheral shell sector 24 or 25 covers the entire length of the stator of the turbomolecular pump.

En alternative, le stator peut être un assemblage de plusieurs étages de secteurs multiétagés de stator. On peut par exemple imaginer un premier étage de stator tel qu'illustré sur la figure 3, auquel on raccorde axialement un second étage coaxial de stator à structure similaire, avec éventuellement des structures d'ailettes différentes et des diamètres différents. Le stator est alors un assemblage de plusieurs étages de secteurs multiétagés de stator.Alternatively, the stator can be an assembly of several stages of multistage stator sectors. We can by example imagine a first stator stage as illustrated on the FIG. 3, to which a second coaxial stage of stator with similar structure, possibly with structures different fins and different diameters. The stator is then an assembly of several floors of multi-level sectors of stator.

Après avoir réalisé l'assemblage de la pompe turbomoléculaire telle qu'illustrée sur la figure 3, l'ensemble doit être inséré dans un carter, pour réaliser une pompe turbomoléculaire fonctionnellement complète. On peut alors prévoir un carter spécifique, avec des moyens de fixation à une enceinte à vide.After completing the pump assembly turbomolecular as illustrated in Figure 3, the assembly must be inserted into a housing, to make a pump functionally complete turbomolecular. We can then predict a specific casing, with means for fixing to an enclosure to empty.

Toutefois, selon l'invention, on peut réaliser une pompe turbomoléculaire insérable, c'est-à-dire adaptée pour être insérée dans un carter ou un système du client tel qu'une enceinte à vide. La pompe est alors installée au plus près de l'application et permet d'optimiser les performances de pompage. Les secteurs de coque 24 et 25 permettent d'enfermer les éléments de la pompe turbomoléculaire, pour constituer un ensemble éventuellement tenu par des moyens d'assemblage provisoire, que l'on peut ôter lors de l'introduction de la pompe dans le système du client.However, according to the invention, a pump can be produced. insertable turbomolecular, i.e. adapted to be inserted in a housing or customer system such as a vacuum enclosure. The pump is then installed as close as possible to the application and optimizes pumping performance. The sectors of shell 24 and 25 allow the pump elements to be enclosed turbomolecular, to form a possibly held whole by means of temporary assembly, which can be removed during the introduction of the pump into the customer's system.

Dans tous les cas, les secteurs de coque 24 et 25 doivent de préférence s'insérer à faible jeu dans le carter ou le système du client, pour assurer entre les secteurs de coque 24 et 25 et le carter ou système du client un bon contact qui favorise les échanges thermiques.In all cases, the hull sectors 24 and 25 must preferably fit with little play in the housing or the system of the customer, to ensure between hull sectors 24 and 25 and the housing or customer system a good contact that promotes heat exchanges.

La structure de pompe turbomoléculaire selon l'invention autorise toutes les géométries d'ailettes possibles en termes d'inclinaison, de diamètre intérieur, de diamètre extérieur, de hauteur d'étage et d'épaisseur.The turbomolecular pump structure according to the invention authorizes all possible fin geometries in terms inclination, inside diameter, outside diameter, floor height and thickness.

Ce système permet de simplifier également l'empilement des entretoises et des stators, et de s'affranchir de la chaíne de cotes de ces différents éléments.This system also simplifies the stacking of spacers and stators, and to get rid of the chain of ratings of these different elements.

En outre, cette structure améliore l'échange thermique entre le rotor et le milieu ambiant, par l'intermédiaire des secteurs de coque, en favorisant le contact thermique entre les ailettes du stator et les secteurs de coque, puis entre les secteurs de coque et le carter ou enveloppe périphérique de la pompe, et en réduisant le nombre des discontinuités de transmission thermique grâce au caractère monobloc des secteurs de coque multiétagés.In addition, this structure improves the heat exchange between the rotor and the environment, via hull areas, promoting thermal contact between the stator fins and hull sectors, then between the hull sectors and the peripheral casing or shell of the pump, and reducing the number of transmission discontinuities thermal thanks to the monobloc character of the hull sectors multistage.

Cette structure permet de proposer une version insérable pour des pompes à vide à plus grand débit.This structure makes it possible to offer an insertable version for higher flow rate vacuum pumps.

Le nombre de pièces précises est réduit par rapport à un assemblage classique. Le coût de production de la pompe est ainsi fortement diminué.The number of precise parts is reduced compared to a classic assembly. The production cost of the pump is thus greatly decreased.

La présente invention n'est pas limitée aux modes de réalisation qui ont été explicitement décrits, mais elle en inclut les diverses variantes et généralisations qui sont à la portée de l'homme du métier.The present invention is not limited to the modes of which have been explicitly described, but it includes the various variants and generalizations which are within the reach of the skilled person.

Claims (11)

Pompe turbomoléculaire ayant un stator périphérique multiétagé à ailettes engagées entre des ailettes d'un rotor central multiétagé (18), dans laquelle : le stator comporte plusieurs secteurs de stator à ailettes (26a-26j ; 27a-27j) assemblés autour du rotor (18), les secteurs de stator à ailettes (26a-26j ; 27a-27j) sont répartis en plusieurs rangées axiales de secteurs de stator à ailettes (26, 27), chaque rangée axiale de secteurs de stator à ailettes (26, 27) est solidaire d'un secteur de coque périphérique (24, 25) et forme ainsi un secteur multiétagé de stator, caractérisée en ce que : les secteurs de stator à ailettes (26a-26j ; 27a-27j) constituent chacun un élément individuel, les secteurs de stator à ailettes d'une même rangée axiale de secteurs de stator à ailettes (26, 27) sont rapportés et solidarisés à la face interne concave du secteur de coque périphérique correspondant (24, 25), pour former le secteur multiétagé de stator, la face interne concave du secteur de coque périphérique (24, 25) comprend des moyens de retenue (24a-24j) pour retenir individuellement en position les secteurs de stator à ailettes (26a-26j). Turbomolecular pump having a multi-stage peripheral stator with fins engaged between fins of a multi-stage central rotor (18), in which: the stator comprises several stator sectors with fins (26a-26j; 27a-27j) assembled around the rotor (18), the stator sectors with fins (26a-26j; 27a-27j) are distributed in several axial rows of stator sectors with fins (26, 27), each axial row of finned stator sectors (26, 27) is integral with a peripheral shell sector (24, 25) and thus forms a multistage stator sector, characterized in that : the stator sectors with fins (26a-26j; 27a-27j) each constitute an individual element, the finned stator sectors of the same axial row of finned stator sectors (26, 27) are attached and secured to the concave internal face of the corresponding peripheral shell sector (24, 25), to form the multistage sector of stator, the concave inner face of the peripheral shell sector (24, 25) comprises retaining means (24a-24j) for individually retaining the finned stator sectors (26a-26j) in position. Pompe turbomoléculaire selon la revendication 1, caractérisée en ce que les secteurs de stator à ailettes (26a-26j ; 27a-27j) comprennent une seule rangée d'ailettes, constituant chacun un secteur de stator monoétagé.Turbomolecular pump according to claim 1, characterized in that the finned stator sectors (26a-26j; 27a-27j) comprise a single row of fins, each constituting a single-stage stator sector. Pompe turbomoléculaire selon l'une des revendications 1 ou 2, caractérisée en ce que les secteurs de stator à ailettes (26a-26j ; 27a-27j) comprennent au moins une rangée annulaire d'ailettes (126a) solidaires d'une jante (226a).Turbomolecular pump according to one of claims 1 or 2, characterized in that the stator sectors with fins (26a-26j; 27a-27j) comprise at least one annular row of fins (126a) integral with a rim (226a ). Pompe turbomoléculaire selon la revendication 3, caractérisée en ce que la jante (226a) relie les extrémités intérieures des ailettes de la rangée annulaire d'ailettes (126a). Turbomolecular pump according to claim 3, characterized in that the rim (226a) connects the inner ends of the fins of the annular row of fins (126a). Pompe turbomoléculaire selon la revendication 3, caractérisée en ce que la jante (226a) relie les extrémités extérieures des ailettes de la rangée annulaire d'ailettes (126a).Turbomolecular pump according to claim 3, characterized in that the rim (226a) connects the outer ends of the fins of the annular row of fins (126a). Pompe turbomoléculaire selon l'une quelconque des revendications 1 à 5, caractérisée en ce que : la face interne concave du secteur de coque périphérique (24, 25) comprend une pluralité de gorges annulaires (24a-24j), les secteurs de stator à ailettes (26a-26j) comportent chacun au moins un bord périphérique (326a) qui vient s'encastrer radialement en force dans l'une des gorges annulaires (24a-24j) du secteur de coque périphérique (24). Turbomolecular pump according to any one of Claims 1 to 5, characterized in that : the concave internal face of the peripheral shell sector (24, 25) comprises a plurality of annular grooves (24a-24j), the finned stator sectors (26a-26j) each have at least one peripheral edge (326a) which is radially embedded in force in one of the annular grooves (24a-24j) of the peripheral shell sector (24). Pompe turbomoléculaire selon la revendication 6, caractérisée en ce que les bords périphériques (326a) des secteurs de stator à ailettes (26a-26j) sont constitués par les extrémités extérieures des ailettes desdits secteurs de stator (26a-26j).Turbomolecular pump according to claim 6, characterized in that the peripheral edges (326a) of the finned stator sectors (26a-26j) are constituted by the outer ends of the fins of said stator sectors (26a-26j). Pompe turbomoléculaire selon la revendication 6, caractérisée en ce que les bords périphériques (326a) des secteurs de stator à ailettes (26a-26j) sont constitués par des jantes (226a) qui relient les extrémités extérieures des ailettes desdits secteurs de stator à ailettes (26a-26j).Turbomolecular pump according to claim 6, characterized in that the peripheral edges (326a) of the fin stator sectors (26a-26j) are constituted by rims (226a) which connect the outer ends of the fins of said fin stator sectors ( 26a-26j). Pompe turbomoléculaire selon l'une quelconque des revendications 1 à 8, caractérisée en ce que le stator est un assemblage radial d'un seul étage de secteurs multiétagés de stator (21, 22).Turbomolecular pump according to any one of claims 1 to 8, characterized in that the stator is a radial assembly of a single stage of multistage stator sectors (21, 22). Pompe turbomoléculaire selon l'une quelconque des revendications 1 à 8, caractérisée en ce que le stator est un assemblage de plusieurs étages de secteurs multiétagés de stator.Turbomolecular pump according to any one of Claims 1 to 8, characterized in that the stator is an assembly of several stages of multistage sectors of the stator. Pompe turbomoléculaire selon l'une des revendications 9 ou 10, caractérisée en ce que les secteurs multiétagés de stator (21, 22) sont des secteurs de 180°.Turbomolecular pump according to one of claims 9 or 10, characterized in that the multistage stator sectors (21, 22) are sectors of 180 °.
EP04290163A 2003-02-03 2004-01-21 Turbomolecular pump stator Expired - Lifetime EP1443214B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0301223A FR2850714B1 (en) 2003-02-03 2003-02-03 TURBOMOLECULAR PUMP WITH STATOR MULTISTAGE SPACERS
FR0301223 2003-02-03

Publications (2)

Publication Number Publication Date
EP1443214A1 true EP1443214A1 (en) 2004-08-04
EP1443214B1 EP1443214B1 (en) 2010-03-31

Family

ID=32605991

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04290163A Expired - Lifetime EP1443214B1 (en) 2003-02-03 2004-01-21 Turbomolecular pump stator

Country Status (5)

Country Link
US (1) US7588417B2 (en)
EP (1) EP1443214B1 (en)
AT (1) ATE462886T1 (en)
DE (1) DE602004026235D1 (en)
FR (1) FR2850714B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005027097A1 (en) * 2005-06-11 2006-12-14 Pfeiffer Vacuum Gmbh Stator disk for turbomolecular pump
US9890795B2 (en) * 2015-05-06 2018-02-13 Asia Vital Components Co., Ltd. Cooling fan structure
GB2552793A (en) * 2016-08-08 2018-02-14 Edwards Ltd Vacuum pump
JP2021173257A (en) * 2020-04-28 2021-11-01 株式会社島津製作所 Turbomolecular pump and stator of turbomolecular pump
JP7396209B2 (en) * 2020-06-03 2023-12-12 株式会社島津製作所 Turbomolecular pumps, rotors and stators of turbomolecular pumps

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2218615A1 (en) * 1972-04-18 1973-10-31 Leybold Heraeus Gmbh & Co Kg TURBOMOLECULAR PUMP WITH ROTOR AND STATOR
EP0442556A1 (en) * 1990-02-16 1991-08-21 VARIAN S.p.A. A stator for a turbo-molecular pump
DE29717764U1 (en) * 1997-10-06 1997-11-20 Leybold Vakuum Gmbh Stator for a turbomolecular vacuum pump
US6412173B1 (en) * 1999-07-26 2002-07-02 Phoenix Analysis And Design Technologies, Inc. Miniature turbomolecular pump
EP1249613A1 (en) * 2001-03-15 2002-10-16 VARIAN S.p.A. Turbine pump with a stator stage integrated with a spacer ring

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6332752B2 (en) * 1997-06-27 2001-12-25 Ebara Corporation Turbo-molecular pump
JP2003269364A (en) * 2002-03-12 2003-09-25 Boc Edwards Technologies Ltd Vacuum pump

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2218615A1 (en) * 1972-04-18 1973-10-31 Leybold Heraeus Gmbh & Co Kg TURBOMOLECULAR PUMP WITH ROTOR AND STATOR
EP0442556A1 (en) * 1990-02-16 1991-08-21 VARIAN S.p.A. A stator for a turbo-molecular pump
DE29717764U1 (en) * 1997-10-06 1997-11-20 Leybold Vakuum Gmbh Stator for a turbomolecular vacuum pump
US6412173B1 (en) * 1999-07-26 2002-07-02 Phoenix Analysis And Design Technologies, Inc. Miniature turbomolecular pump
EP1249613A1 (en) * 2001-03-15 2002-10-16 VARIAN S.p.A. Turbine pump with a stator stage integrated with a spacer ring

Also Published As

Publication number Publication date
ATE462886T1 (en) 2010-04-15
DE602004026235D1 (en) 2010-05-12
EP1443214B1 (en) 2010-03-31
FR2850714A1 (en) 2004-08-06
US7588417B2 (en) 2009-09-15
US20040156715A1 (en) 2004-08-12
FR2850714B1 (en) 2005-04-29

Similar Documents

Publication Publication Date Title
EP0063993B1 (en) Bearing assembly, in particular for a turbo machine
EP3455927B1 (en) Electrical machine with a rotor having a cavity for the dynamic balancing of the rotor
FR2930590A1 (en) TURBOMACHINE HOUSING HAVING A DEVICE WHICH PREVENTS INSTABILITY IN CONTACT BETWEEN THE CARTER AND THE ROTOR
EP1808573B1 (en) Balancing mass and rotor disc, rotor and aircraft engine comprising such a mass
CH704640B1 (en) pivot member.
FR2887702A1 (en) ELEMENT FOR POSITIONING AND MAINTAINING AN ELECTRIC MOTOR STATOR IN A COMPRESSOR, COMPRESSOR AND MOUNTING METHOD
FR2859049A1 (en) Squirrel cage rotor for induction motor, has end rings with support holes circumferentially aligned in periphery part, and conducting units supported at support part of corresponding support holes
EP1443214B1 (en) Turbomolecular pump stator
CH665316A5 (en) ELECTRIC RETARDER.
EP2751821A1 (en) Cover for connecting energy storage assemblies
FR2617543A1 (en) TURBOMOLECULAR PUMP
FR2985870A1 (en) ROTOR, METHOD OF MANUFACTURE AND CORRESPONDING ELECTRIC MACHINE
FR2988128A1 (en) TURBINE ROTOR FOR A THERMOELECTRIC POWER PLANT
EP1532721A2 (en) Internal ventilating system for a rotating electrical machine such as a motor vehicle alternator
EP0263218B1 (en) Hydraulic mechanism with fluid distribution disk and counter disk
FR3135306A1 (en) Turbomolecular vacuum pump and assembly process
WO2020233936A1 (en) Stator for an axial flux electric machine and method for assembling such a stator
FR3012185A1 (en) AIR BLADE WHEEL FOR TRANSPORTING AND COMPRESSING AIR WITH AIR BEARING AND RADIAL COMPRESSOR EQUIPPED WITH SUCH WHEEL.
FR3002822A1 (en) ELECTRIC MACHINE WITH COUPLING FLANGE.
EP3107193B1 (en) Stacked-plate rotor
EP1319805A1 (en) Rotor or rotor element for turbocompressors
EP0344059B1 (en) Rotary gear apparatus for the circulation of a fluid
FR2561339A1 (en) Ventilator mounting for electrical machine
FR2732412A1 (en) Liquid or liquid-gas mixture pump with integral electric motor
EP4206494A1 (en) Gear wheel - gear assembly comprising such a gear wheel - method of manufacturing

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

17P Request for examination filed

Effective date: 20041216

AKX Designation fees paid

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: ALCATEL LUCENT

17Q First examination report despatched

Effective date: 20070807

GRAJ Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted

Free format text: ORIGINAL CODE: EPIDOSDIGR1

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 602004026235

Country of ref document: DE

Date of ref document: 20100512

Kind code of ref document: P

REG Reference to a national code

Ref country code: NL

Ref legal event code: VDEP

Effective date: 20100331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: SI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

REG Reference to a national code

Ref country code: IE

Ref legal event code: FD4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: ES

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100712

Ref country code: EE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: RO

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: CZ

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: PT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100802

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20110104

BERE Be: lapsed

Owner name: ALCATEL LUCENT

Effective date: 20110131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110131

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110131

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110131

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20120119

Year of fee payment: 9

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20130128

Year of fee payment: 10

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20110121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: TR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

Ref country code: BG

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100630

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: HU

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

Owner name: ADIXEN VACUUM PRODUCTS, FR

Effective date: 20131009

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20100331

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20140121

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20140121

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 12

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 13

REG Reference to a national code

Ref country code: FR

Ref legal event code: CD

Owner name: PFEIFFER VACCUUM, FR

Effective date: 20160118

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20160201

Year of fee payment: 13

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20160128

Year of fee payment: 13

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 602004026235

Country of ref document: DE

Representative=s name: FDST PATENTANWAELTE FREIER DOERR STAMMLER TSCH, DE

Ref country code: DE

Ref legal event code: R081

Ref document number: 602004026235

Country of ref document: DE

Owner name: ADIXEN VACUUM PRODUCTS, FR

Free format text: FORMER OWNER: ALCATEL LUCENT, PARIS, FR

Ref country code: DE

Ref legal event code: R081

Ref document number: 602004026235

Country of ref document: DE

Owner name: PFEIFFER VACUUM, FR

Free format text: FORMER OWNER: ALCATEL LUCENT, PARIS, FR

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 602004026235

Country of ref document: DE

Representative=s name: FDST PATENTANWAELTE FREIER DOERR STAMMLER TSCH, DE

Ref country code: DE

Ref legal event code: R081

Ref document number: 602004026235

Country of ref document: DE

Owner name: PFEIFFER VACUUM, FR

Free format text: FORMER OWNER: ADIXEN VACUUM PRODUCTS, ANNECY, FR

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 602004026235

Country of ref document: DE

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602004026235

Country of ref document: DE

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20170929

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170131

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20170801