[go: up one dir, main page]

EP3880969A1 - Motor as molecular drag stage - Google Patents

Motor as molecular drag stage

Info

Publication number
EP3880969A1
EP3880969A1 EP19804785.4A EP19804785A EP3880969A1 EP 3880969 A1 EP3880969 A1 EP 3880969A1 EP 19804785 A EP19804785 A EP 19804785A EP 3880969 A1 EP3880969 A1 EP 3880969A1
Authority
EP
European Patent Office
Prior art keywords
stage
molecular drag
gap
accordance
rotor shaft
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.)
Withdrawn
Application number
EP19804785.4A
Other languages
German (de)
French (fr)
Inventor
Alexander James PATEY
Richard Glyn Horler
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.)
Edwards Ltd
Original Assignee
Edwards Ltd
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 Edwards Ltd filed Critical Edwards Ltd
Publication of EP3880969A1 publication Critical patent/EP3880969A1/en
Withdrawn legal-status Critical Current

Links

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
    • F04D19/044Holweck-type pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/042Turbomolecular vacuum pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/046Combinations of two or more different types of pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
    • 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
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/5806Cooling the drive system

Definitions

  • the present invention relates to a molecular drag stage, preferably for a turbo- molecular pum p.
  • the present invention further relates to a turbomolecular pum p with such a m olecular drag stage.
  • turbom olecular vacuum pum ps com prise a housing form ing an inlet and an outlet. I n the housing a m otor is arranged in order to rotate a rotor shaft.
  • the turbomolecular vacuum pum p comprises a turbom olecular stage where veins are interacting with a stator in order to convey a gaseous medium from the inlet towards the outlet.
  • the turbomolecular stage is followed by a m olecular drag stage such as a Holweck stage.
  • Known m olecular drag stages com prise a rotating cylinder close to a stator with a narrow gap in between wherein either the stator or the cylinder has a threaded groove or a thread.
  • the present technical problem is solved by a m olecular drag stage in accordance to claim 1 as well as a turbomolecular pump in accordance to claim 1 1 .
  • a m olecular drag stage in accordance with the present invention comprises a housing with an inlet and an outlet.
  • a rotor shaft is rotatably supported within the housing.
  • the m olecular drag stage further com prises an electric motor within the housing, wherein the m otor is built by a m otor stator surrounding the rotor shaft in order to rotate the rotor shaft.
  • a small gap is defined between the outer side of the rotor shaft and the inner side of the m otor stator, such that the rotor shaft and the motor stator are contact-free and the rotor shaft is rotatable within the motor stator.
  • the outer side of the rotor shaft or the inner side of the m otor stator com prises a thread or a threaded groove in order to convey a gaseous m edium from the inlet to the outlet.
  • one of the outer side of the rotor shaft or the inner side of the m otor stator com prises a thread or a threaded groove while the opposite surface is sm ooth.
  • the motor itself of the molecular drag stage is adapted to actively convey the gaseous m edium towards the outlet.
  • a heat build-up in the m otor is pre vented and the efficiency of the molecular drag stage is enhanced by utilizing the motor itself as active elem ent for conveying the gaseous medium .
  • the in nerm ost side of the motor stator together with the outer side of the rotor shaft thus is building an additional molecular drag stage.
  • m olecules of the gaseous medium are conveyed by a molecular drag process.
  • At least one further pum p stage built as m olecular drag stage is im plem ented wherein the pum p stage comprises a rotor elem ent connected to the rotor shaft to interact with a non-rotating pump stator elem ent to convey the gaseous m edium from the inlet to the outlet.
  • the rotor elem ent m ay be built as cylindrical elem ent surrounded by or surrounding the pum p stator element.
  • either the rotor element or the pump stator element comprise a thread or threaded groove to build a m olecular drag stage.
  • a sm all gap is defined between the rotor element and the pum p stator for a contact-less rota tion of the rotor element, in order to convey a gaseous m edium from the inlet towards the outlet.
  • At least two and preferably four further pum p stages are imple mented wherein m ore preferably neighboring pum p stages share a com mon rotor element and convey the gaseous medium in opposite directions.
  • the outer surface of the rotor element may belong to a first pum p stage wherein the inner surface of the sam e rotor elem ent m ay belong to the neighboring pum p stage, in order to achieve a compact design of the molecular drag stage.
  • the gap between the outer side of the rotor shaft and the inner side of the m otor stator defines an entrance through which the gaseous medium enters into the gap and an exit through which the gaseous medium leaves the gap, wherein the entrance is in fluid com m unication with an exit of the last pum p stage and the exit of the gap is preferably in direct fluid com m unication with the outlet.
  • the gaseous m edium is first flowing to one or further pum p stages built by respective rotor elem ents and pum p stator elem ents, and after this the gaseous medium is conveyed through the gap formed by the electric motor towards the outlet.
  • the active gap of the electric m otor is utilized for conveying the gaseous m edium through the outlet.
  • a pressure is below 30m bar and more preferably below 10 2 m bar .
  • a pressure is equal to the pressure of the environment or below. More preferably the pressure at the exit is between l OOm bar and 0.02m bar.
  • the main flow of the gaseous m edium is directed through the gap.
  • the gap of the electric m otor is not utilized as bypass or the like.
  • no purge gas is conveyed through the gap.
  • the exit of the last pum p stage is connected with the outlet only via the gap.
  • gas leaving the last pum p stage can only reach the outlet if flowing through the active gap of the electric m otor.
  • the pump stages are built as Holweck stages.
  • the m otor stator is built as a lam inated stator core com prising a plurality of sheet elements.
  • the plurality of sheet elements is arranged within the m otor stator, or in other words, the m otor stator surrounds the plu rality of sheet elem ents connected to the rotor shaft.
  • the sheet elements of the motor stator are m ade of steel.
  • directly adjacent sheet elements of the m otor stator differ at their inner side from each other in at least one structural feature, such as a protrusion or indentation that is displaced from one sheet elem ent to the next, wherein along the length of the gap the thread or threaded groove is form ed by the sum of the individual displaced structural features.
  • the thread or threaded groove of the gap is built in a step-wise m anner.
  • the present invention relates to a vacuum pump com prising a m olecular drag stage as described above.
  • the m olecular pump is a turbomo- lecular pum p com prising a turbom olecular pum p stage.
  • the turbom olecular pump stage com prises veins connected to the rotor shaft interacting with stator veins in order to convey a gaseous m edium from the inlet towards the outlet.
  • the turbom olecular pump stage is arranged upstream of the molecular drag stage in accordance with the general flow of the gaseous m e dium within the vacuum pum p.
  • the vacuum pum p is able to produce a vacuum of 1 0 2 to 10 12 m bar.
  • Fig. 1 shows a schem atic drawing of a vacuum pum p in accordance with the present invention
  • Fig. 2 shows a detailed view of the m otor stator in accordance to the present invention.
  • the vacuum pump 10 of Fig. 1 is built as turbom olecular vacuum pum p com prising a turbomolecular pump stage 1 2 and a m olecular drag stage 14.
  • the vacuum pum p 10 comprises a housing 16, wherein in the housing 16 a rotor shaft 18 is rotatably supported by, for example, ball bearings 20. The rotor shaft 18 is rotated by an electric motor 22.
  • the rotor shaft 18 is connected with rotor elements built as veins 24, interacting with stator veins 26 in order to convey a gaseous m edium from an inlet 28 towards an outlet 30.
  • the gaseous m edium is conveyed through the turbom olecular pum p stage 12 and enters the molecular drag stage 14.
  • the rotor shaft 1 8 is connected to a rotor element 32 with a first cylinder 34 and a second cylinder 36.
  • a threaded first stator 38 is implem ented, wherein the thread of the first stator 38 faces the outer surface of the first cylinder 34 such that the gaseous medium is pum ped through the first pum p stage 40 from an entrance 42 of the m olecular drag stage 14 to a first turning point 44.
  • the inner surface of the first cylinder 34 is facing a second threaded pum p stator 46 form ing a second pum p stage 48, pum ping the gaseous m edium from the first turning point 44 to a second turning point 50.
  • the gaseous medium is pum ped through a third pum p stage 52 and a fourth pump stage 54, which are equal or sim ilarly built as the first pum p stage 40 or the second pum p stage 48.
  • the gas reaches a last turning point 56 which lies within the vacuum pum p 1 0.
  • the electric m otor 22 com prises a motor stator 58, wherein a gap 60 is defined between the motor stator 58 and the outer surface 62 of the rotor shaft 18.
  • the inner surface 64 of the m otor stator 58 comprises a thread 66, thereby actively pumping the gaseous m edium from the last turning point 56 form ing the entrance of the gap 60 towards the outlet 30.
  • the gaseous medium entering the m olecular drag stage 14 through the entrance 42 can only reach the outlet 30 through the gap 60.
  • the gaseous medium is actively pum ped in the gap 60 by the thread 66 in order to enhance the efficiency of the molecular drag stage 14, and to avoid frictional losses as well as heat-up within the electric motor 22.
  • the outer surface 62 of the rotor shaft 18 may com prise a thread or threaded groove.
  • the inner surface 64 of the motor stator 58 may be built as planar surface.
  • the motor stator 58 is built by a plurality of sheet elements 68 preferably m ade of steel.
  • the sheet elem ents 68 may comprise a structural feature 70 which can be built as protrusion or indentation.
  • Fig. 2 shows the structural fea ture 70 as protrusion .
  • the structural feature 70 is displaced from one sheet elem ent 68 to the next or neighboring by a small angular amount, thereby form ing the thread 66 in a step-wise m anner by the structural features 70.
  • the thread or threaded groove in the active gap 60 of the electric motor 22 is easy to m anufacture such that m anufacturing costs of the m otor stator 58 of the electric motor 22 can be reduced.

Landscapes

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

Abstract

A molecular drag stage (14), preferably for a turbomolecular pump (10), with a housing (16) comprising an inlet (28) and an outlet (30), a rotor shaft (18) rotatably supported within the housing (16), a electric motor (22) wherein the motor (22) is built by a motor stator (58) surrounding the rotor shaft (18) in order to rotate the rotor shaft (18). Thereby, a small gap (60) is defined be- tween the outer side (62) of the rotor shaft (18) and the inner side (64) of the motor stator (58). The outer side (62) of the rotor shaft (18) or the inner side (64) of the motor stator (58) comprises a thread (66) or a threaded groove in order to convey a gaseous medium from the inlet (28) to the outlet (30).

Description

MOTOR AS MOLECULAR DRAG STAGE
The present invention relates to a molecular drag stage, preferably for a turbo- molecular pum p. The present invention further relates to a turbomolecular pum p with such a m olecular drag stage.
Known turbom olecular vacuum pum ps com prise a housing form ing an inlet and an outlet. I n the housing a m otor is arranged in order to rotate a rotor shaft. The turbomolecular vacuum pum p comprises a turbom olecular stage where veins are interacting with a stator in order to convey a gaseous medium from the inlet towards the outlet. The turbomolecular stage is followed by a m olecular drag stage such as a Holweck stage. Known m olecular drag stages com prise a rotating cylinder close to a stator with a narrow gap in between wherein either the stator or the cylinder has a threaded groove or a thread.
I n order to enhance the efficiency of the m olecular drag stage, several stages are nested together, also to keep the dim ension of the casing sm all. Thereby, in subsequent molecular drag stages the gaseous m edium is pum ped in opposite directions. An even number of stages com plicates the design by leaving the gas within the pum p m echanism , requiring additional channels or drillings to facili tate gas movem ent to the exhaust. Thus, usually only an odd num ber of m olec ular drag stages is possible such that the last molecular drag stage ends towards the outlet of the vacuum pum p, thereby lim iting the freedom of the design of the vacuum pump.
However, concepts are known com prising an even num ber of m olecular drag stages wherein the gaseous m edium is flowing through the gap between a motor stator and the rotor shaft towards the outlet. However, this arrangement causes a heat build-up within the motor and leads to frictional losses rendering this arrangem ent inefficient. It is an object of the present invention to provide a molecular drag stage as well as a turbom olecular pump which is m ore efficient and provides a high degree of freedom in design.
The present technical problem is solved by a m olecular drag stage in accordance to claim 1 as well as a turbomolecular pump in accordance to claim 1 1 .
A m olecular drag stage in accordance with the present invention comprises a housing with an inlet and an outlet. A rotor shaft is rotatably supported within the housing. The m olecular drag stage further com prises an electric motor within the housing, wherein the m otor is built by a m otor stator surrounding the rotor shaft in order to rotate the rotor shaft. Thereby a small gap is defined between the outer side of the rotor shaft and the inner side of the m otor stator, such that the rotor shaft and the motor stator are contact-free and the rotor shaft is rotatable within the motor stator. Thereby the outer side of the rotor shaft or the inner side of the m otor stator com prises a thread or a threaded groove in order to convey a gaseous m edium from the inlet to the outlet. Thus, one of the outer side of the rotor shaft or the inner side of the m otor stator com prises a thread or a threaded groove while the opposite surface is sm ooth. Hence, the motor itself of the molecular drag stage is adapted to actively convey the gaseous m edium towards the outlet. A heat build-up in the m otor is pre vented and the efficiency of the molecular drag stage is enhanced by utilizing the motor itself as active elem ent for conveying the gaseous medium . The in nerm ost side of the motor stator together with the outer side of the rotor shaft thus is building an additional molecular drag stage. Thereby m olecules of the gaseous medium are conveyed by a molecular drag process.
Preferably, at least one further pum p stage built as m olecular drag stage is im plem ented wherein the pum p stage comprises a rotor elem ent connected to the rotor shaft to interact with a non-rotating pump stator elem ent to convey the gaseous m edium from the inlet to the outlet. Thereby the rotor elem ent m ay be built as cylindrical elem ent surrounded by or surrounding the pum p stator element. Thereby, either the rotor element or the pump stator element comprise a thread or threaded groove to build a m olecular drag stage. A sm all gap is defined between the rotor element and the pum p stator for a contact-less rota tion of the rotor element, in order to convey a gaseous m edium from the inlet towards the outlet.
Preferably, at least two and preferably four further pum p stages are imple mented wherein m ore preferably neighboring pum p stages share a com mon rotor element and convey the gaseous medium in opposite directions. Thus, the outer surface of the rotor element may belong to a first pum p stage wherein the inner surface of the sam e rotor elem ent m ay belong to the neighboring pum p stage, in order to achieve a compact design of the molecular drag stage.
Preferably, the gap between the outer side of the rotor shaft and the inner side of the m otor stator defines an entrance through which the gaseous medium enters into the gap and an exit through which the gaseous medium leaves the gap, wherein the entrance is in fluid com m unication with an exit of the last pum p stage and the exit of the gap is preferably in direct fluid com m unication with the outlet. Thus, in the molecular drag stage, the gaseous m edium is first flowing to one or further pum p stages built by respective rotor elem ents and pum p stator elem ents, and after this the gaseous medium is conveyed through the gap formed by the electric motor towards the outlet. Thus, it is possible to im plement an even number of pum p stages without disadvantages since the active gap of the electric m otor is utilized for conveying the gaseous m edium through the outlet.
Preferably, at the entrance of the gap a pressure is below 30m bar and more preferably below 10 2 m bar . At the exit of the gap preferably a pressure is equal to the pressure of the environment or below. More preferably the pressure at the exit is between l OOm bar and 0.02m bar.
Preferably, the main flow of the gaseous m edium is directed through the gap. Thus, the gap of the electric m otor is not utilized as bypass or the like. Preferably, no purge gas is conveyed through the gap.
Preferably, the exit of the last pum p stage is connected with the outlet only via the gap. Thus, gas leaving the last pum p stage can only reach the outlet if flowing through the active gap of the electric m otor.
Preferably, the pump stages are built as Holweck stages.
Preferably, the m otor stator is built as a lam inated stator core com prising a plurality of sheet elements. Thereby, the plurality of sheet elements is arranged within the m otor stator, or in other words, the m otor stator surrounds the plu rality of sheet elem ents connected to the rotor shaft. I n particular the sheet elements of the motor stator are m ade of steel.
Preferably, directly adjacent sheet elements of the m otor stator differ at their inner side from each other in at least one structural feature, such as a protrusion or indentation that is displaced from one sheet elem ent to the next, wherein along the length of the gap the thread or threaded groove is form ed by the sum of the individual displaced structural features. Thus, by the angular displace ment of the structural feature of directly neighboring sheet elem ents, the thread or threaded groove of the gap is built in a step-wise m anner. Thereby, the active gap of the electric motor is easy to m anufacture. Since the motor stator of the electric m otor usually com prises sheet elem ents in any way, these sheet ele ments can be utilized to build the thread or threaded groove in order to form the active gap of the electric m otor.
Further, the present invention relates to a vacuum pump com prising a m olecular drag stage as described above. Preferably, the m olecular pump is a turbomo- lecular pum p com prising a turbom olecular pum p stage. The turbom olecular pump stage com prises veins connected to the rotor shaft interacting with stator veins in order to convey a gaseous m edium from the inlet towards the outlet. Thereby, preferably the turbom olecular pump stage is arranged upstream of the molecular drag stage in accordance with the general flow of the gaseous m e dium within the vacuum pum p. Preferably, the vacuum pum p is able to produce a vacuum of 1 0 2 to 10 12 m bar.
I n the following, the invention is described with respect to a specific embodiment with reference to the accompanying drawings.
Fig. 1 shows a schem atic drawing of a vacuum pum p in accordance with the present invention, and
Fig. 2 shows a detailed view of the m otor stator in accordance to the present invention.
The vacuum pump 10 of Fig. 1 is built as turbom olecular vacuum pum p com prising a turbomolecular pump stage 1 2 and a m olecular drag stage 14. The vacuum pum p 10 comprises a housing 16, wherein in the housing 16 a rotor shaft 18 is rotatably supported by, for example, ball bearings 20. The rotor shaft 18 is rotated by an electric motor 22.
I n the turbom olecular pump stage 12, the rotor shaft 18 is connected with rotor elements built as veins 24, interacting with stator veins 26 in order to convey a gaseous m edium from an inlet 28 towards an outlet 30. The gaseous m edium is conveyed through the turbom olecular pum p stage 12 and enters the molecular drag stage 14. I n the molecular drag stage 14, the rotor shaft 1 8 is connected to a rotor element 32 with a first cylinder 34 and a second cylinder 36. Further, a threaded first stator 38 is implem ented, wherein the thread of the first stator 38 faces the outer surface of the first cylinder 34 such that the gaseous medium is pum ped through the first pum p stage 40 from an entrance 42 of the m olecular drag stage 14 to a first turning point 44. The inner surface of the first cylinder 34 is facing a second threaded pum p stator 46 form ing a second pum p stage 48, pum ping the gaseous m edium from the first turning point 44 to a second turning point 50. From the second turning point 50, the gaseous medium is pum ped through a third pum p stage 52 and a fourth pump stage 54, which are equal or sim ilarly built as the first pum p stage 40 or the second pum p stage 48. Thus, the gas reaches a last turning point 56 which lies within the vacuum pum p 1 0.
The electric m otor 22 com prises a motor stator 58, wherein a gap 60 is defined between the motor stator 58 and the outer surface 62 of the rotor shaft 18. Thereby the inner surface 64 of the m otor stator 58 comprises a thread 66, thereby actively pumping the gaseous m edium from the last turning point 56 form ing the entrance of the gap 60 towards the outlet 30. Thus, the gaseous medium entering the m olecular drag stage 14 through the entrance 42 can only reach the outlet 30 through the gap 60. Thereby the gaseous medium is actively pum ped in the gap 60 by the thread 66 in order to enhance the efficiency of the molecular drag stage 14, and to avoid frictional losses as well as heat-up within the electric motor 22. Alternatively, the outer surface 62 of the rotor shaft 18 may com prise a thread or threaded groove. I n this case, the inner surface 64 of the motor stator 58 may be built as planar surface.
The motor stator 58 is built by a plurality of sheet elements 68 preferably m ade of steel. Thereby, the sheet elem ents 68 may comprise a structural feature 70 which can be built as protrusion or indentation. Fig. 2 shows the structural fea ture 70 as protrusion . Thereby the structural feature 70 is displaced from one sheet elem ent 68 to the next or neighboring by a small angular amount, thereby form ing the thread 66 in a step-wise m anner by the structural features 70. Of course, one sheet elem ent 68 m ay com prise m ore than one structural feature 70. Thus, the thread or threaded groove in the active gap 60 of the electric motor 22 is easy to m anufacture such that m anufacturing costs of the m otor stator 58 of the electric motor 22 can be reduced.

Claims

CLAI MS
1. Molecular drag stage (14), preferably for a turbomolecular pump (10), with a housing (16) comprising an inlet (28) and an outlet (30), a rotor shaft (18) rotatably supported within the housing (16), a electric motor (22), wherein the motor (22) is built by a motor stator (58) surrounding the rotor shaft (18) in order to rotate the rotor shaft (18), wherein a small gap (60) is defined between the outer side (62) of the rotor shaft (18) and the inner side (64) of the motor stator (58), wherein the outer side (62) of the rotor shaft (18) or the inner side (64) of the motor stator (58) comprises a thread (66) or a threaded groove in order to convey a gaseous medium from the inlet (28) to the outlet (30).
2. Molecular drag stage in accordance with claim 1, characterized by at least one further pump stage (40), wherein the pump stage (40) comprises a rotor element (34) connected to the rotor shaft (18) to interact with a non rotating pump stator element (38) to convey the gaseous medium from the inlet (28) to the outlet (30).
3. Molecular drag stage in accordance with claim 2, characterized by at least two and preferably four further pump stages (40, 48, 52, 54), wherein more preferably neighboring pump stages share a common rotor element (34, 36) and convey the gaseous medium in opposite directions.
4. Molecular drag stage in accordance with claim 2 or 3, characterized in that the gap (60) defines an entrance through which the gaseous medium en ters into the gap (60) and an exit through which the gaseous medium leaves the gap (60), wherein the entrance is in fluid communication with an exit (56) of the last pum p stage (54) and the exit is preferably in direct fluid com m unication with the outlet (30) .
5. Molecular drag stage in accordance with any of claims 1 to 4, characterized in that the main flow of the gaseous medium is directed through the gap (60) .
6. Molecular drag stage in accordance with any of claims 1 to 5, characterized in that no purge gas is conveyed through the gap (60) .
7. Molecular drag stage in accordance with any of claims 2 to 6, characterized in that the exit (56) of the last pump stage (54) is connected with the outlet (30) only via the gap (60) .
8. Molecular drag stage in accordance with any of claims 2 to 7, characterized in that the pum p stages (40, 48, 52, 54) are built as Holweck stages.
9. Molecular drag stage in accordance with any of claims 1 to 8, characterized in that the m otor stator (58) is built as lam inated stator core com prising a plurality of sheet elements (68) wherein the sheet elem ents (68) are pref erably m ade of steel.
10. Molecular drag stage in accordance with claim 9, characterized in that di rectly adjacent sheet elements (68) differ at their inner side from each other such that at least one feature (70) is displaced from one sheet ele ment (68) to the next, wherein along the length of the gap (60) the thread (66) is formed by the sum of the individual displaced features (70) .
1 1 . Vacuum pump ( 10) , in particular a turbomolecular vacuum pum p, com prising a molecular drag stage ( 14) in accordance with any of claim s 1 to 1 0.
EP19804785.4A 2018-11-14 2019-11-07 Motor as molecular drag stage Withdrawn EP3880969A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1818600.7A GB2579028A (en) 2018-11-14 2018-11-14 Molecular drag stage
PCT/GB2019/053149 WO2020099834A1 (en) 2018-11-14 2019-11-07 Motor as molecular drag stage

Publications (1)

Publication Number Publication Date
EP3880969A1 true EP3880969A1 (en) 2021-09-22

Family

ID=64739600

Family Applications (1)

Application Number Title Priority Date Filing Date
EP19804785.4A Withdrawn EP3880969A1 (en) 2018-11-14 2019-11-07 Motor as molecular drag stage

Country Status (4)

Country Link
EP (1) EP3880969A1 (en)
GB (1) GB2579028A (en)
TW (1) TW202106979A (en)
WO (1) WO2020099834A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114076106B (en) * 2020-08-18 2024-03-12 佛山市顺德区美的洗涤电器制造有限公司 Motor assembly, fan and range hood
GB2607339A (en) * 2021-06-04 2022-12-07 Edwards Ltd Holweck drag pump

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL135263C (en) * 1900-01-01
US6179573B1 (en) * 1999-03-24 2001-01-30 Varian, Inc. Vacuum pump with inverted motor
ITTO20030421A1 (en) * 2003-06-05 2004-12-06 Varian Spa COMPACT VACUUM PUMP
DE102013214662A1 (en) * 2013-07-26 2015-01-29 Pfeiffer Vacuum Gmbh vacuum pump
DE102014118083A1 (en) * 2014-12-08 2016-06-09 Pfeiffer Vacuum Gmbh TURBO MOLECULAR PUMP
DE102014118881A1 (en) * 2014-12-17 2016-06-23 Pfeiffer Vacuum Gmbh vacuum pump

Also Published As

Publication number Publication date
TW202106979A (en) 2021-02-16
GB2579028A (en) 2020-06-10
WO2020099834A1 (en) 2020-05-22
GB201818600D0 (en) 2018-12-26

Similar Documents

Publication Publication Date Title
EP2491249B1 (en) Vacuum pump
EP2064449B1 (en) Molecular drag pumping mechanism
US8235678B2 (en) Multi-stage vacuum pumping arrangement
EP2481077B1 (en) Mass spectrometer system
WO2020099834A1 (en) Motor as molecular drag stage
US8740588B2 (en) Multiple inlet vacuum pumps
JP2636356B2 (en) Molecular pump
US9624938B2 (en) Integrated motor bearing and rotor
CN102016323A (en) Arrangement with an electric motor and a pump
EP3524822A1 (en) Vacuum pump, helical plate for vacuum pump, spacer, and rotating cylindrical body
JPS62255597A (en) Vacuum pump
WO1991004417A1 (en) Pump or compressor unit
EP2757266B1 (en) Rotary vacuum pump
CN105324578B (en) Vacuum pump
EP1851439B1 (en) Vacuum pump
US8393854B2 (en) Vacuum pump
JP7015106B2 (en) Vacuum pumps and rotating cylinders included in vacuum pumps
WO2021105656A1 (en) Pumping stage of a vacuum pump
JP2019023469A (en) Vacuum pump
JP2011027049A (en) Turbo-molecular pump
EP3497337B1 (en) Vacuum pump
US20100322799A1 (en) Turbomolecular pump
CN221442879U (en) Vacuum pump
CN114593074A (en) Vacuum pump with elastic spacer
JP2021017810A (en) Vacuum pump

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

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

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20210525

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20220104