EP2472120B1 - Vacuum pump and member used for vacuum pump - Google Patents

Vacuum pump and member used for vacuum pump Download PDF

Info

Publication number
EP2472120B1
EP2472120B1 EP10811581.7A EP10811581A EP2472120B1 EP 2472120 B1 EP2472120 B1 EP 2472120B1 EP 10811581 A EP10811581 A EP 10811581A EP 2472120 B1 EP2472120 B1 EP 2472120B1
Authority
EP
European Patent Office
Prior art keywords
vacuum pump
rotating body
exhaust passage
hole
gas exhaust
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
EP10811581.7A
Other languages
German (de)
French (fr)
Other versions
EP2472120A1 (en
EP2472120A4 (en
Inventor
Yoshinobu Ohtachi
Yasushi Maejima
Tsutomu Takaada
Tooru Miwata
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 Japan Ltd
Original Assignee
Edwards Japan 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 Japan Ltd filed Critical Edwards Japan Ltd
Publication of EP2472120A1 publication Critical patent/EP2472120A1/en
Publication of EP2472120A4 publication Critical patent/EP2472120A4/en
Application granted granted Critical
Publication of EP2472120B1 publication Critical patent/EP2472120B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F04D25/0693Details or arrangements of the wiring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0292Stop safety or alarm devices, e.g. stop-and-go control; Disposition of check-valves
    • 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
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/426Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps
    • F04D29/428Discharge tongues
    • 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
    • F04D29/522Casings; Connections of working fluid for axial pumps especially adapted for elastic fluid 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/601Mounting; Assembling; Disassembling specially adapted for elastic fluid pumps

Definitions

  • the present invention relates to a vacuum pump such as a turbomolecular pump performing gas evacuation from a vacuum container such as a process chamber used in a semiconductor fabrication apparatus. More particularly, the present invention relates to a technique for improving the evacuation performance that decreases depending on the arrangement positions of an outlet port and a connector, and for reducing the size of a vacuum pump.
  • a multiple-stage blade pump in which a rotary blade section and a cylindrical threaded section are combined is widely used as a large-flow-rate pump such as a turbomolecular pump.
  • FIG. 9 illustrates an example of such a multiple-stage blade pump.
  • This multiple-stage blade pump 200 is constituted by a tubular casing 20 having, formed in the upper portion thereof, an inlet port 10 for sucking in the gas from a chamber that is not shown in the figure, a plurality of rotary blades 32 that are provided at a rotating body 30 inside the casing 20, fixed blades 40 provided alternately with the rotary blades 32, a thread groove spacer 45 and a rotary blade cylindrical portion 50 constituting a spiral groove portion 80 where evacuation is performed by drag action, a disk-shaped base 70 covering the lower portion of the casing 20, an outlet port 90 for evacuating the gas evacuated from the upstream side where the inlet port is located to the outside on the downstream side, a connector 100 that is electrically connected to an externally located controller for controlling the pump, and a rear lid 110 that covers the bottom portion.
  • the rotating body 30 is contactless supported and position controlled by magnetic levitation implemented by radial bearings 34, 36 and a thrust bearing 38.
  • the rotating body 30 is rotatably driven at a high speed by a drive motor 60.
  • the rotating body 30 rotates at a high speed
  • the rotary blades 32 provided at the rotating body 30 simultaneously rotate at a high speed such that these rotary blades 32 interact with the alternately disposed stator blades 40, whereby evacuation is performed.
  • Turbomolecular pumps generally have a back pressure dependence, that is, the pump performance is affected by the pressure on the back pressure side (outlet port side). Accordingly, in a multiple-stage blade pump, a low pressure is maintained on the inlet port side and the back pressure is increased, thereby improving the pump performance, by enlarging the diameter of the spiral groove portion 80 and increasing the axial length of the spiral groove portion 80.
  • multiple-stage blade pumps should be designed with consideration for restrictive conditions relating to the installation thereof.
  • the length of the spiral groove portion 80 is increased, the axial length of the pump itself is also increased causing problems in installation.
  • Japanese Patent Application Publication No. 2008-163857 discloses a technique for preventing the reduction of the opening area of outlet port inside the pump and the degradation of exhaust performance caused by the extension of the spiral groove portion.
  • the exhaust performance is degraded because the reduction of the opening decreases the conductance and prevents the flow of gas into the outlet port.
  • a U-shaped groove for which the radial direction from the inner side serves as a depth direction is provided with respect to a cylindrical hole connecting the spiral groove portion with the outlet port provided in the base or thread groove spacer.
  • the reduction in the opening area of outlet port is thereby prevented.
  • the exhaust performance of the pump is improved.
  • the housing is manufactured by casting, since the concave groove exists on the inner side, the cast housing is difficult to remove from the mold, the mold structure becomes complex, and the casting cost rises significantly.
  • the spiral rotor is broken during rotation, the broken pieces thereof collide with the spiral stator and a force acts on the spiral stator or on the housing via the spiral stator.
  • stress concentration occurs in the corners of the formed groove, thereby creating weak points in terms of the pump strength and reducing the strength of the pump itself.
  • a dry etching apparatus which is one of semiconductor fabrication apparatuses
  • the pressure of process gas that has taken part in a reaction inside the chamber increases
  • the increase in temperature over the normal temperature results in a phase transition from a gaseous state to a solid state.
  • the solidified reaction products of the process gas are deposited on the spiral groove portion where the gas pressure rises, thereby degrading the exhaust performance of the pump.
  • the reaction products that have deposited on the interior portions of the pump should be removed periodically.
  • a cleaning agent or a removal tool is difficult to insert into the U-shaped groove and therefore the removal operation becomes difficult.
  • reaction products when the reaction products are removed, it is necessary to confirm visually that all of the reaction products have been removed. Since the process gas in the dry etching apparatus is typically highly corrosive, it is also necessary to verify visually after the removal whether corrosion is present on the gas flow channel surface of the housing or spiral stator and whether the surface film such as a plated film provided for corrosion protection has peeled off from the surface, and where such defects are present, they should be repaired. Where portions of the gas flow channel surface cannot be visually inspected, the residues of corrosion products or corrosion can remain unnoticed on such portions and the vacuum pump is restarted in the unrepaired state.
  • a turbomolecular pump has a connector serving to connect the pump to a controller for power supply to the motor or magnetic bearings or input/output of signals.
  • the pump structure is such that the hole for passing the connector wiring is completely isolated from the exhaust flow channel. Such a structure is used because if the exhaust flow channel and the hole are connected and gas flows to the connector, the exhaust performance is degraded or the connector is corroded. In some cases, it can result in accidents and cause significant problems for the pump.
  • the opening area of the hole for connector wiring should be reduced and the operation of passing the wiring from the motor or magnetic bearings to the connector becomes complex. Accordingly, the problem associated with the connector is similar to that relating to the outlet port. Namely, the increase in the spiral groove portion length requires the vacuum pump height to be increased.
  • JP2003278691 and JPS6413295U disclose solutions belonging to the technical background of the present invention.
  • Also described herein is a vacuum pump in which the operability of connector wiring that decreases when the spiral groove portion is extended or positioned further below inside the pump with the object of reducing the size of the vacuum pump can be improved.
  • the invention described in claim 2 provides the vacuum pump according to claim 1, wherein an inner corner portion of the opening edge portion has a rounded inner corner shape that reduces stress concentration.
  • the effect of reducing stress concentration can be obtained even when the rounding size of the rounded inner corner portion is 0.1 mm. Even greater effect can be obtained when the rounding size is further increased.
  • the invention described in claim 3 provides the vacuum pump according to any one of claims 1 to 2, further including a connector for connecting a controller that controls the rotation of the rotating body, wherein the housing or the base member has a nearly coaxial hole that is nearly coaxial with a rotation center axis of the rotating body, a conductor wire insertion hole into which a conductor wire that connects the connector and the motor is inserted, and a groove that combines the nearly coaxial hole with the conductor wire insertion hole.
  • the controller may be directly connected to the connector or may be connected by a cable.
  • the invention described in claim 4 provides the vacuum pump according to claim 3, wherein an edge of at least one from the nearly coaxial hole, the conductor wire insertion hole, and the groove has a rounded outer corner shape such that damage of the conductor wire caused by contact with the edge is reduced.
  • the invention described in claim 5 provides the vacuum pump according to any one of claims 3 or 4, wherein an outer circumferential end of the groove in the radial direction of the rotating body is positioned further toward the outer circumferential side than an inner circumferential end of the conductor wire insertion hole.
  • the decrease in exhaust performance of the vacuum pump occurring when the spiral groove portion of the pump is extended or positioned further below inside the pump can be prevented.
  • the degradation of wiring operability that decreases when the spiral groove portion is extended or positioned further below inside the pump can be reduced.
  • FIGS. 1 and 2 are vertical sectional views illustrating the configuration of the multiple-stage blade pump using the present invention.
  • FIG. 1 illustrates an example where an outlet port is provided in a thread groove spacer 45 serving as a stator.
  • FIG. 2 illustrates an example where an outlet port is provided in a base 70 serving as a base member.
  • the members identical to those in FIG. 9 that illustrates the conventional example will be assigned with same reference numerals.
  • the first embodiment relates to a technique for improving the exhaust performance of a vacuum pump that has decreased because a rotary blade cylindrical portion 50 serving as a rotating body or a thread groove spacer 45 covers the opening of a cylindrical hole 45a or 70a serving as a gas exhaust passage combining an outlet port 90 with a downstream space S of the rotary blade cylindrical portion 50 on the space S side.
  • a thread groove spacer 45 serving as a gas exhaust passage forming member in the configuration shown in FIG. 1 and the base 70 serving as a gas exhaust passage forming member in the configuration shown in FIG. 2 form the cylindrical hole 45a or 70a as shown in FIGS. 3B and 4B .
  • the opening edge portion 130 of the cylindrical hole 45a on the space S side in the thread groove spacer 45 is formed such that no blind portion exists at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side.
  • the opening edge portion 130 of the cylindrical hole 70a on the space S side in the base 70 is formed such that no blind portion exists at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side.
  • FIG. 5 is an explanatory drawing illustrating the blind portions in the case where the cylindrical hole 45a is formed as the gas exhaust passage in the thread groove spacer 45.
  • the opening edge portion 130 is formed such that no blind portion exists at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side.
  • the opening edge portion 130 is formed such that no blind portion exists at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side.
  • the field of view such as the cross-hatched portion in FIG. 5 is not blocked. Therefore, the entire opening edge portion 130 can be seen.
  • FIG. 6 shows the thread groove spacer 45 and FIG. 7 shows the base 70.
  • the inlet port is on the upper side and the pump bottom is on the lower side.
  • the C side of the center line C-C' is taken as the upper side and the C' side is taken as the lower side.
  • the C side of a straight line forming an angle ⁇ less than 90 degrees with the center line C-C' is taken as the oblique upper side and the C' side meeting such a requirement is taken as the oblique lower side.
  • the absence of an blind portion at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side means that any portion of the opening edge portion 130 is included in at least either of the visible portion of the opening edge portion 130 when it is viewed from the lower side or the visible portion of the opening edge portion 130 when it is viewed from the oblique lower side.
  • the absence of a blind portion at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side means that any portion of the opening edge portion 130 is included in at least either of the visible portion of the opening edge portion 130 when it is viewed from the upper side or the visible portion of the opening edge portion 130 when it is viewed from the oblique upper side.
  • the outer side of the outlet port 90 is connected by a pipe to an auxiliary pump having the usual suction power.
  • FIGS. 3A and 4A illustrate an example in which the conventional U-shaped groove is formed.
  • the inner corner portion of the opening edge portion 130 does not have the rounded inner corner shape such as shown in these figures.
  • Cylindrical shapes and cavities thereof are usually machined by turning, and when a groove is bored in the direction perpendicular to the center axial line of the cylinder in the inner wall of the cavity portion, the cutting cannot be performed to the necessary depth or the cutting process becomes complex and the production cost rises due to the restrictions such as a machinable range of the cutting tool (bite).
  • cutting may be performed so as to bore a hole that becomes coaxial with the cylindrical outer circumferential surface in the center axial line direction of the cylinder and therefore the machining in the turning process is facilitated.
  • the mold structure does not become complex and the cast article can be easily removed from the mold, thereby making it possible to reduce the casting cost.
  • the operation of removing the deposited reaction products, verifying the presence of corrosion on the thread groove spacer 45 or base 70, and repairing the corrosion are not complex. Therefore, the residual amount of reaction products and leak caused by poor repair of corrosion can be reduced.
  • the rotary blade cylindrical portion 50 can be moved further down or the vacuum pump height can be further reduced.
  • a structure is considered in which the inner corner portion of the opening edge portion 130 of the cylindrical hole 45a on the space S side is rounded as shown in FIG. 3B , and stress concentration is reduced.
  • a vacuum pump in particular a turbomolecular pump
  • the rotary blade 32 and the rotary blade cylindrical portion 50 rotate at a high speed during operation and a large centrifugal force acts thereupon.
  • the resistance to the centrifugal force decreases and the pump is fractured.
  • the rotary blade cylindrical portion 50 is fractured in high-speed rotation, the rotary blade cylindrical portion is often split into 3 to 4 sections and these split cylindrical sections collide with the thread groove spacer 45.
  • a force is applied to the thread groove spacer 45 and to the base 70 via the thread groove spacer 45.
  • the rotary blade 32 and rotary blade cylindrical portion 50 usually rotate as a speed equal to or higher than 10,000 rpm, and where they are fractured the rotation energy thereof is released. Therefore, the force acting upon the thread groove spacer 45 or base 70 becomes very strong. When such a force is received, large stresses are generated in the thread groove spacer 45 and base 70.
  • stress concentration occurs in the inner corner portions of the groove and cracks can initiate from the stress concentration zones.
  • the cracks can cause fracture and destruction of the thread groove spacer 45 or base 70 that can result in the gas leaking to the outside of the pump. This gas leak adversely affects the environment.
  • the stress concentration can be reduced.
  • the strength of the pump itself can be increased and the probability of gas leak can be reduced.
  • only one inner corner portion exists, by contrast with the conventional U-shaped groove having two inner corner portions and the number of stress concentration zones is small. Therefore, the probability of gas leak can be further reduced.
  • the inner corner portions of the conventional U-shaped groove may be also rounded as shown in FIGS. 3A and 4A .
  • FIG. 8 is the view of the base 70 taken from the rear lid 110.
  • a structure is obtained in which when the connector wiring hole 120 serving as a conductor wire insertion hole is drilled in the base 70 from the outer circumferential side, the drilling is performed to the outer circumferential side in the radial direction of the rotary blade cylindrical portion 50 and a groove 102 is provided from the bottom surface of the base 70 so as to combine the connector wiring hole 120 with the hole 101 that is nearly coaxial with the rotation center axial line of the rotary blade cylindrical portion 50.
  • the connector wiring hole 120 is drilled as far as the outer circumferential side of the rotary blade cylindrical portion 50, rather than linearly to the hole 101 in order to avoid interference of the connector wiring hole 120 with the rotary blade cylindrical portion 50 or with the space S for the gas flow channel located therebelow. Where the connector wiring hole 120 interferes and is combined with the space S for the gas flow channel, the gas flows into the connector wiring hole 120 and the connector is corroded.
  • the outer corners formed in the connector wiring hole 120 and groove 102 can have the rounded outer corner shape. In such a case, a structure can be obtained in which the connector 100 and the conductor wire connected to the motor or magnetic bearings are unlikely to be damaged.
  • the end o of the groove 102 on the outer circumferential side of the pump is located on the outside of the end i of the connector wiring hole 120 on the inner circumferential side of the pump. This is done so because by increasing the distance "L” between the two ends "o” and “I” it is possible to ensure a larger pass-through area from the groove 102 to the connector 100.
  • the rotary blade cylindrical portion 50 or the space S for the gas flow channel located therebelow can be disposed at a lower level. Since the wiring of the conductor wire to the connector 100 is also performed by the groove of the shape obtained by cutting the wall below the inner circumferential portion of the connector wiring hole 120, the wiring connection is facilitated. Consequently, the production time of the pump can be reduced.
  • the rotary blade cylindrical portion 50 and the space S for the gas flow channel located therebelow can be enlarged in length to reach the lower level or disposed at the lower level without interfering with the connector wiring hole 120.
  • the connector 100 can be provided at a height greater than that in the conventional pump. As a result, the vacuum pump can be reduced in height.
  • the machined shape of the base 70 can be simplified and the production cost thereof can be reduced, without changing significantly the structure of the conventional pump.

Landscapes

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

Description

  • The present invention relates to a vacuum pump such as a turbomolecular pump performing gas evacuation from a vacuum container such as a process chamber used in a semiconductor fabrication apparatus. More particularly, the present invention relates to a technique for improving the evacuation performance that decreases depending on the arrangement positions of an outlet port and a connector, and for reducing the size of a vacuum pump.
  • A multiple-stage blade pump in which a rotary blade section and a cylindrical threaded section are combined is widely used as a large-flow-rate pump such as a turbomolecular pump.
  • FIG. 9 illustrates an example of such a multiple-stage blade pump. This multiple-stage blade pump 200 is constituted by a tubular casing 20 having, formed in the upper portion thereof, an inlet port 10 for sucking in the gas from a chamber that is not shown in the figure, a plurality of rotary blades 32 that are provided at a rotating body 30 inside the casing 20, fixed blades 40 provided alternately with the rotary blades 32, a thread groove spacer 45 and a rotary blade cylindrical portion 50 constituting a spiral groove portion 80 where evacuation is performed by drag action, a disk-shaped base 70 covering the lower portion of the casing 20, an outlet port 90 for evacuating the gas evacuated from the upstream side where the inlet port is located to the outside on the downstream side, a connector 100 that is electrically connected to an externally located controller for controlling the pump, and a rear lid 110 that covers the bottom portion.
  • The rotating body 30 is contactless supported and position controlled by magnetic levitation implemented by radial bearings 34, 36 and a thrust bearing 38. The rotating body 30 is rotatably driven at a high speed by a drive motor 60. When the rotating body 30 rotates at a high speed, the rotary blades 32 provided at the rotating body 30 simultaneously rotate at a high speed such that these rotary blades 32 interact with the alternately disposed stator blades 40, whereby evacuation is performed.
  • Turbomolecular pumps generally have a back pressure dependence, that is, the pump performance is affected by the pressure on the back pressure side (outlet port side). Accordingly, in a multiple-stage blade pump, a low pressure is maintained on the inlet port side and the back pressure is increased, thereby improving the pump performance, by enlarging the diameter of the spiral groove portion 80 and increasing the axial length of the spiral groove portion 80.
  • However, multiple-stage blade pumps should be designed with consideration for restrictive conditions relating to the installation thereof. In particular, where the length of the spiral groove portion 80 is increased, the axial length of the pump itself is also increased causing problems in installation.
  • Japanese Patent Application Publication No. 2008-163857 discloses a technique for preventing the reduction of the opening area of outlet port inside the pump and the degradation of exhaust performance caused by the extension of the spiral groove portion. Thus, when the rotary section of the pump blocks a opening portion of the outlet port inside the pump, the exhaust performance is degraded because the reduction of the opening decreases the conductance and prevents the flow of gas into the outlet port.
  • Accordingly, with the aforementioned technique, a U-shaped groove for which the radial direction from the inner side serves as a depth direction is provided with respect to a cylindrical hole connecting the spiral groove portion with the outlet port provided in the base or thread groove spacer. The reduction in the opening area of outlet port is thereby prevented. As a result, the exhaust performance of the pump is improved.
  • However, where a U-shaped groove is provided from the inside with respect to the cylindrical hole leading to the outlet port according to the technique described in Japanese Patent Application Publication No. 2008-163857 , special cutting tools and settings are required during turning and the machining is difficult. Further, even if the machining is successful, significant time and efforts are required therefor and the production cost rises.
  • Further, where the housing is manufactured by casting, since the concave groove exists on the inner side, the cast housing is difficult to remove from the mold, the mold structure becomes complex, and the casting cost rises significantly.
  • In addition, where the spiral rotor is broken during rotation, the broken pieces thereof collide with the spiral stator and a force acts on the spiral stator or on the housing via the spiral stator. In this case, stress concentration occurs in the corners of the formed groove, thereby creating weak points in terms of the pump strength and reducing the strength of the pump itself.
  • Further, in a dry etching apparatus, which is one of semiconductor fabrication apparatuses, where the pressure of process gas that has taken part in a reaction inside the chamber increases, the increase in temperature over the normal temperature results in a phase transition from a gaseous state to a solid state. For this property, when a multiple-stage blade pump is used for evacuating a dry etching apparatus, the solidified reaction products of the process gas are deposited on the spiral groove portion where the gas pressure rises, thereby degrading the exhaust performance of the pump. For this reason, the reaction products that have deposited on the interior portions of the pump should be removed periodically. However, a cleaning agent or a removal tool is difficult to insert into the U-shaped groove and therefore the removal operation becomes difficult.
  • Furthermore, when the reaction products are removed, it is necessary to confirm visually that all of the reaction products have been removed. Since the process gas in the dry etching apparatus is typically highly corrosive, it is also necessary to verify visually after the removal whether corrosion is present on the gas flow channel surface of the housing or spiral stator and whether the surface film such as a plated film provided for corrosion protection has peeled off from the surface, and where such defects are present, they should be repaired. Where portions of the gas flow channel surface cannot be visually inspected, the residues of corrosion products or corrosion can remain unnoticed on such portions and the vacuum pump is restarted in the unrepaired state. Another problem is that when the corrosion advances, the strength of the spiral stator or housing decreases and the abovementioned rotor fracture occurs, the spiral stator and housing can be fractured and the gas can leak therethrough. With the U-shaped groove, such as that of the conventional technique, the portion that cannot be visually inspected can be reduced in size by decreasing the groove depth. However, the problem arising in this case is that because the groove is shallow, a sufficient opening area cannot be ensured.
  • Another problem is associated with a connector. A turbomolecular pump has a connector serving to connect the pump to a controller for power supply to the motor or magnetic bearings or input/output of signals. The pump structure is such that the hole for passing the connector wiring is completely isolated from the exhaust flow channel. Such a structure is used because if the exhaust flow channel and the hole are connected and gas flows to the connector, the exhaust performance is degraded or the connector is corroded. In some cases, it can result in accidents and cause significant problems for the pump.
  • Further, when the height position of the lower end of the spiral groove portion is below the height position of the hole for connector wiring, the opening area of the hole for connector wiring should be reduced and the operation of passing the wiring from the motor or magnetic bearings to the connector becomes complex. Accordingly, the problem associated with the connector is similar to that relating to the outlet port. Namely, the increase in the spiral groove portion length requires the vacuum pump height to be increased.
  • Such a problem relating to the connector is not taken into account in the above-described conventional technique. JP2003278691 and JPS6413295U disclose solutions belonging to the technical background of the present invention.
  • It is the first object of the present invention to provide a vacuum pump in which the decrease in exhaust performance occurring when the spiral groove portion is extended or positioned further below inside the pump with the object of reducing the size of the vacuum pump can be prevented.
  • Also described herein is a vacuum pump in which the operability of connector wiring that decreases when the spiral groove portion is extended or positioned further below inside the pump with the object of reducing the size of the vacuum pump can be improved.
  • The invention is defined by the appended independent claim 1.Preferred embodiments of the invention are defined by the appended dependent claims 2-5.
  • The invention described in claim 2 provides the vacuum pump according to claim 1, wherein an inner corner portion of the opening edge portion has a rounded inner corner shape that reduces stress concentration.
  • The effect of reducing stress concentration can be obtained even when the rounding size of the rounded inner corner portion is 0.1 mm. Even greater effect can be obtained when the rounding size is further increased.
  • The invention described in claim 3 provides the vacuum pump according to any one of claims 1 to 2, further including a connector for connecting a controller that controls the rotation of the rotating body, wherein the housing or the base member has a nearly coaxial hole that is nearly coaxial with a rotation center axis of the rotating body, a conductor wire insertion hole into which a conductor wire that connects the connector and the motor is inserted, and a groove that combines the nearly coaxial hole with the conductor wire insertion hole.
  • The controller may be directly connected to the connector or may be connected by a cable.
  • The invention described in claim 4 provides the vacuum pump according to claim 3, wherein an edge of at least one from the nearly coaxial hole, the conductor wire insertion hole, and the groove has a rounded outer corner shape such that damage of the conductor wire caused by contact with the edge is reduced.
  • The invention described in claim 5 provides the vacuum pump according to any one of claims 3 or 4, wherein an outer circumferential end of the groove in the radial direction of the rotating body is positioned further toward the outer circumferential side than an inner circumferential end of the conductor wire insertion hole.
  • In accordance with the present invention, the decrease in exhaust performance of the vacuum pump occurring when the spiral groove portion of the pump is extended or positioned further below inside the pump can be prevented.
  • Further, the degradation of wiring operability that decreases when the spiral groove portion is extended or positioned further below inside the pump can be reduced.
    • FIG. 1 is a vertical sectional view illustrating a multiple-stage blade pump in which an outlet port is provided in a thread groove spacer according to the first embodiment;
    • FIG. 2 is vertical sectional view illustrating a multiple-stage blade pump in which an outlet port is provided in a base according to the first embodiment;
    • FIG. 3 illustrates the first embodiment relating to the case in which the outlet port is provided in the thread groove spacer;
    • FIG. 4 illustrates the first embodiment relating to the case in which the outlet port is provided in the base;
    • FIG. 5 relates to an example in which a cylindrical hole is formed as a gas evacuation passage in the thread groove spacer and illustrates the blind portions;
    • FIG. 6 illustrates how the thread groove spacer is viewed directly from a lower side and an oblique lower side;
    • FIG. 7 illustrates how the base is viewed directly from an upper side and an oblique upper side;
    • FIG. 8 is the view of a vacuum pump base taken from the rear lid; and
    • FIG. 9 is a vertical sectional view illustrating an example of the conventional multiple-stage blade pump.
  • The preferred embodiment of the vacuum pump in accordance with the present invention will be explained below in greater detail with reference to FIGS. 1 to 8.
  • FIGS. 1 and 2 are vertical sectional views illustrating the configuration of the multiple-stage blade pump using the present invention.
  • FIG. 1 illustrates an example where an outlet port is provided in a thread groove spacer 45 serving as a stator. FIG. 2 illustrates an example where an outlet port is provided in a base 70 serving as a base member. In the explanation of FIGS. 1 to 8, the members identical to those in FIG. 9 that illustrates the conventional example will be assigned with same reference numerals.
  • The first embodiment relates to a technique for improving the exhaust performance of a vacuum pump that has decreased because a rotary blade cylindrical portion 50 serving as a rotating body or a thread groove spacer 45 covers the opening of a cylindrical hole 45a or 70a serving as a gas exhaust passage combining an outlet port 90 with a downstream space S of the rotary blade cylindrical portion 50 on the space S side.
  • In this embodiment, a thread groove spacer 45 serving as a gas exhaust passage forming member in the configuration shown in FIG. 1 and the base 70 serving as a gas exhaust passage forming member in the configuration shown in FIG. 2 form the cylindrical hole 45a or 70a as shown in FIGS. 3B and 4B. The opening edge portion 130 of the cylindrical hole 45a on the space S side in the thread groove spacer 45 is formed such that no blind portion exists at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side.
  • The opening edge portion 130 of the cylindrical hole 70a on the space S side in the base 70 is formed such that no blind portion exists at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side.
  • FIG. 5 is an explanatory drawing illustrating the blind portions in the case where the cylindrical hole 45a is formed as the gas exhaust passage in the thread groove spacer 45. In FIG. 5, because the cross-hatched portion exists, blind portions exist at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side. By contrast, in the present embodiment, in the cylindrical hole 45a formed by the thread groove spacer 45, the opening edge portion 130 is formed such that no blind portion exists at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side. When the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side, the field of view such as the cross-hatched portion in FIG. 5 is not blocked. Therefore, the entire opening edge portion 130 can be seen. In accordance with the present invention, no blind portion exists in such a state.
  • Meanwhile, in the cylindrical hole 70a formed by the base 70, the opening edge portion 130 is formed such that no blind portion exists at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side. When the base 70 is viewed from at least either of the upper side or the oblique upper side, the field of view such as the cross-hatched portion in FIG. 5 is not blocked. Therefore, the entire opening edge portion 130 can be seen.
  • The definition of the "upper side", "oblique upper side", "lower side", and "oblique lower side" will be explained below. FIG. 6 shows the thread groove spacer 45 and FIG. 7 shows the base 70. As shown in FIGS. 6 and 7, when these components are assembled in the multiple-stage blade pump, the inlet port is on the upper side and the pump bottom is on the lower side. Thus, the C side of the center line C-C' is taken as the upper side and the C' side is taken as the lower side. Further, the C side of a straight line forming an angle α less than 90 degrees with the center line C-C' is taken as the oblique upper side and the C' side meeting such a requirement is taken as the oblique lower side. The absence of an blind portion at the opening edge portion 130 when the thread groove spacer 45 is viewed from at least either of the lower side or the oblique lower side means that any portion of the opening edge portion 130 is included in at least either of the visible portion of the opening edge portion 130 when it is viewed from the lower side or the visible portion of the opening edge portion 130 when it is viewed from the oblique lower side. The absence of a blind portion at the opening edge portion 130 when the base 70 is viewed from at least either of the upper side or the oblique upper side means that any portion of the opening edge portion 130 is included in at least either of the visible portion of the opening edge portion 130 when it is viewed from the upper side or the visible portion of the opening edge portion 130 when it is viewed from the oblique upper side.
  • The outer side of the outlet port 90 is connected by a pipe to an auxiliary pump having the usual suction power.
  • In the above-described related art, a U-shaped groove is formed in the opening edge portion 130 of the cylindrical hole combining the outlet port 90 with the downstream space S of the rotary blade cylindrical portion 50, the groove being formed on the space S side of the cylindrical hole. FIGS. 3A and 4A illustrate an example in which the conventional U-shaped groove is formed. With the conventional technique, the inner corner portion of the opening edge portion 130 does not have the rounded inner corner shape such as shown in these figures.
  • Cylindrical shapes and cavities thereof are usually machined by turning, and when a groove is bored in the direction perpendicular to the center axial line of the cylinder in the inner wall of the cavity portion, the cutting cannot be performed to the necessary depth or the cutting process becomes complex and the production cost rises due to the restrictions such as a machinable range of the cutting tool (bite). However, with the shape of the opening edge portion 130 of the present embodiment, cutting may be performed so as to bore a hole that becomes coaxial with the cylindrical outer circumferential surface in the center axial line direction of the cylinder and therefore the machining in the turning process is facilitated.
  • Furthermore, when the thread groove spacer 45 or base 70 is cast, since no concave groove exists on the inner wall of the hollow portion, the mold structure does not become complex and the cast article can be easily removed from the mold, thereby making it possible to reduce the casting cost.
  • Further, with the present embodiment, the operation of removing the deposited reaction products, verifying the presence of corrosion on the thread groove spacer 45 or base 70, and repairing the corrosion are not complex. Therefore, the residual amount of reaction products and leak caused by poor repair of corrosion can be reduced.
  • Further, since the cross-hatched portions shown in FIGS. 3A and 4A do not exist, the rotary blade cylindrical portion 50 can be moved further down or the vacuum pump height can be further reduced.
  • As a variation example of the first embodiment, a structure is considered in which the inner corner portion of the opening edge portion 130 of the cylindrical hole 45a on the space S side is rounded as shown in FIG. 3B, and stress concentration is reduced. In a vacuum pump, in particular a turbomolecular pump, the rotary blade 32 and the rotary blade cylindrical portion 50 rotate at a high speed during operation and a large centrifugal force acts thereupon. Where the material strength decreases due to corrosion or temperature increase caused by friction with the gas or the like, the resistance to the centrifugal force decreases and the pump is fractured. Where the rotary blade cylindrical portion 50 is fractured in high-speed rotation, the rotary blade cylindrical portion is often split into 3 to 4 sections and these split cylindrical sections collide with the thread groove spacer 45. As a result a force is applied to the thread groove spacer 45 and to the base 70 via the thread groove spacer 45. The rotary blade 32 and rotary blade cylindrical portion 50 usually rotate as a speed equal to or higher than 10,000 rpm, and where they are fractured the rotation energy thereof is released. Therefore, the force acting upon the thread groove spacer 45 or base 70 becomes very strong. When such a force is received, large stresses are generated in the thread groove spacer 45 and base 70. In the case of the conventional U-shaped groove, stress concentration occurs in the inner corner portions of the groove and cracks can initiate from the stress concentration zones. The cracks can cause fracture and destruction of the thread groove spacer 45 or base 70 that can result in the gas leaking to the outside of the pump. This gas leak adversely affects the environment. When the inner corner portion of the opening edge portion 130 of the cylindrical hole 45a or 70a on the spacer S side is machined to a rounded shape, as in the present embodiment, the stress concentration can be reduced. As a result, the strength of the pump itself can be increased and the probability of gas leak can be reduced. Further, in the present embodiment, only one inner corner portion exists, by contrast with the conventional U-shaped groove having two inner corner portions and the number of stress concentration zones is small. Therefore, the probability of gas leak can be further reduced.
  • The inner corner portions of the conventional U-shaped groove may be also rounded as shown in FIGS. 3A and 4A.
  • FIG. 8 is the view of the base 70 taken from the rear lid 110. As shown in the figure, a structure is obtained in which when the connector wiring hole 120 serving as a conductor wire insertion hole is drilled in the base 70 from the outer circumferential side, the drilling is performed to the outer circumferential side in the radial direction of the rotary blade cylindrical portion 50 and a groove 102 is provided from the bottom surface of the base 70 so as to combine the connector wiring hole 120 with the hole 101 that is nearly coaxial with the rotation center axial line of the rotary blade cylindrical portion 50.
  • As shown in FIG. 8, the connector wiring hole 120 is drilled as far as the outer circumferential side of the rotary blade cylindrical portion 50, rather than linearly to the hole 101 in order to avoid interference of the connector wiring hole 120 with the rotary blade cylindrical portion 50 or with the space S for the gas flow channel located therebelow. Where the connector wiring hole 120 interferes and is combined with the space S for the gas flow channel, the gas flows into the connector wiring hole 120 and the connector is corroded.
  • Further, as shown in FIG. 8, the outer corners formed in the connector wiring hole 120 and groove 102 can have the rounded outer corner shape. In such a case, a structure can be obtained in which the connector 100 and the conductor wire connected to the motor or magnetic bearings are unlikely to be damaged.
  • Further, the end o of the groove 102 on the outer circumferential side of the pump is located on the outside of the end i of the connector wiring hole 120 on the inner circumferential side of the pump. This is done so because by increasing the distance "L" between the two ends "o" and "I" it is possible to ensure a larger pass-through area from the groove 102 to the connector 100.
  • Accordingly, where the depth of the groove 102 is reduced within a range in which the minimum pass-through area necessary for the wiring of the conductor wire can be ensured, the rotary blade cylindrical portion 50 or the space S for the gas flow channel located therebelow can be disposed at a lower level. Since the wiring of the conductor wire to the connector 100 is also performed by the groove of the shape obtained by cutting the wall below the inner circumferential portion of the connector wiring hole 120, the wiring connection is facilitated. Consequently, the production time of the pump can be reduced.
  • As a result, the rotary blade cylindrical portion 50 and the space S for the gas flow channel located therebelow can be enlarged in length to reach the lower level or disposed at the lower level without interfering with the connector wiring hole 120. In addition, the connector 100 can be provided at a height greater than that in the conventional pump. As a result, the vacuum pump can be reduced in height.
  • Further,
    the machined shape of the base 70 can be simplified and the production cost thereof can be reduced, without changing significantly the structure of the conventional pump.
  • 10
    Inlet port
    20
    Casing
    30
    Rotating body
    32
    Rotary blade
    34,
    36 Radial bearings
    38
    Thrust bearing
    40
    Fixed blade
    45
    Thread groove spacer
    45a
    Cylindrical hole
    50
    Rotary blade cylindrical portion
    60
    Drive motor
    70
    Base
    70a
    Cylindrical hole
    80
    Spiral groove portion
    90
    Outlet port
    100
    Connector
    110
    Rear lid
    120
    Connector wiring hole
    130
    Opening edge portion

Claims (5)

  1. A vacuum pump (200) comprising:
    an inlet port (10);
    a motor (60);
    a rotating body (30) rotatably driven by the motor, comprising a rotary blade cylindrical portion (50);
    a stator located facing the rotating body, comprising a thread groove spacer (45);
    an outlet port (90) for exhausting a gas that has been sucked in through the inlet port; and
    a gas exhaust passage (45a, 70a) connecting a downstream space of the rotating body to the outlet port and being formed in a flow channel of the gas, and
    the rotating body extending in an inner circumferential side of the gas exhaust passage in a radial direction of the rotating body, wherein the rotary blade cylindrical portion (50) or the thread groove spacer (45) covers the opening of a cylindrical hole (45a, 70) serving as the gas exhaust passage, wherein the thread groove spacer (45) serving as a gas exhaust passage forming member or a base member (70) serving as a gas exhaust passage forming member forms the cylindrical hole (45a, 70a),
    wherein no blind portion exists at an opening edge (130) of the gas exhaust passage in the downstream space side when the gas exhaust passage forming member that forms the gas exhaust passage is viewed from at least either of an upper side or an oblique upper side, or from at least either of a lower side or an oblique lower side.
  2. The vacuum pump according to claim 1, wherein an inner corner portion of the opening edge has a rounded inner corner shape that reduces stress concentration.
  3. The vacuum pump according to any one of claims 1 or 2, further comprising a connector for connecting a controller that controls the rotation of the rotating body, wherein
    a housing or the base member of the vacuum pump has a nearly coaxial hole that is nearly coaxial with a rotation center axis of the rotating body, a conductor wire insertion hole into which a conductor wire that connects the connector and the motor is inserted, and a groove that combines the nearly coaxial hole with the conductor wire insertion hole.
  4. The vacuum pump according to claim 3, wherein an edge of at least one from the nearly coaxial hole, the conductor wire insertion hole, and the groove has a rounded outer corner shape such that damage of the conductor wire caused by contact with the edge is reduced.
  5. The vacuum pump according to any one of claims 3 or 4, wherein
    an outer circumferential end of the groove in the radial direction of the rotating body is positioned further toward the outer circumferential side than an inner circumferential end of the conductor wire insertion hole.
EP10811581.7A 2009-08-28 2010-05-31 Vacuum pump and member used for vacuum pump Active EP2472120B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2009198274 2009-08-28
PCT/JP2010/059186 WO2011024528A1 (en) 2009-08-28 2010-05-31 Vacuum pump and member used for vacuum pump

Publications (3)

Publication Number Publication Date
EP2472120A1 EP2472120A1 (en) 2012-07-04
EP2472120A4 EP2472120A4 (en) 2017-08-02
EP2472120B1 true EP2472120B1 (en) 2022-11-30

Family

ID=43627641

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10811581.7A Active EP2472120B1 (en) 2009-08-28 2010-05-31 Vacuum pump and member used for vacuum pump

Country Status (6)

Country Link
US (1) US20120141254A1 (en)
EP (1) EP2472120B1 (en)
JP (2) JP5785494B2 (en)
KR (1) KR101784016B1 (en)
CN (1) CN102483069B (en)
WO (1) WO2011024528A1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6390098B2 (en) * 2013-12-25 2018-09-19 株式会社島津製作所 Vacuum pump
JP6906941B2 (en) * 2016-12-16 2021-07-21 エドワーズ株式会社 Vacuum pump and stator column used for it and its manufacturing method
JP6948147B2 (en) 2017-04-18 2021-10-13 エドワーズ株式会社 Vacuum pumps, magnetic bearings and shafts of vacuum pumps
JP7289627B2 (en) * 2018-10-31 2023-06-12 エドワーズ株式会社 Vacuum pumps, protection nets and contact parts
JP7456394B2 (en) * 2021-01-22 2024-03-27 株式会社島津製作所 Vacuum pump

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6413295U (en) * 1987-07-13 1989-01-24
JP2003278691A (en) * 2002-03-20 2003-10-02 Boc Edwards Technologies Ltd Vacuum pump

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE7121095U (en) * 1971-05-29 1972-11-23 Leybold-Heraeus Gmbh & Co Kg DEVICE FOR OIL SUPPLY TO THE BEARING POINTS OF A VERTICALLY ARRANGED SHAFT, PREFERABLY THE SHAFT OF A TURBOMOLECULAR PUMP
JP2650372B2 (en) * 1988-12-01 1997-09-03 トヨタ自動車株式会社 Method of joining ceramic member and metal member
JPH0414793U (en) * 1990-05-24 1992-02-06
JPH05272478A (en) * 1992-01-31 1993-10-19 Matsushita Electric Ind Co Ltd Vacuum pump
JP2585265Y2 (en) * 1993-03-19 1998-11-18 セイコー精機株式会社 Exhaust pump
JP3795979B2 (en) * 1996-03-21 2006-07-12 株式会社大阪真空機器製作所 Molecular pump
JP3038432B2 (en) * 1998-07-21 2000-05-08 セイコー精機株式会社 Vacuum pump and vacuum device
JP4104098B2 (en) * 1999-03-31 2008-06-18 エドワーズ株式会社 Vacuum pump
JP2001241393A (en) * 1999-12-21 2001-09-07 Seiko Seiki Co Ltd Vacuum pump
JP2002070787A (en) * 2000-08-25 2002-03-08 Kashiyama Kogyo Kk Vacuum pump
JP2002113607A (en) * 2000-10-04 2002-04-16 Mitsubishi Heavy Ind Ltd Centrifugal hole chamfering tool and chamfering method
JP2002276587A (en) * 2001-03-19 2002-09-25 Boc Edwards Technologies Ltd Turbo molecular drag pump
JP4156830B2 (en) * 2001-12-13 2008-09-24 エドワーズ株式会社 Vacuum pump
JP2003254286A (en) * 2002-03-04 2003-09-10 Boc Edwards Technologies Ltd Vacuum pump device
JP4147042B2 (en) * 2002-03-12 2008-09-10 エドワーズ株式会社 Vacuum pump
DE10224604B4 (en) * 2002-06-04 2014-01-30 Oerlikon Leybold Vacuum Gmbh evacuation device
EP2228539A3 (en) * 2003-08-08 2017-05-03 Edwards Japan Limited Vacuum pump
FR2859250B1 (en) * 2003-08-29 2005-11-11 Cit Alcatel VACUUM PUMP
JP2005194921A (en) * 2004-01-06 2005-07-21 Boc Edwards Kk Molecular pump
JP4594689B2 (en) * 2004-09-27 2010-12-08 エドワーズ株式会社 Vacuum pump
JP5194450B2 (en) * 2006-12-28 2013-05-08 株式会社島津製作所 Turbo molecular pump
DE202007012070U1 (en) * 2007-08-30 2009-01-08 Oerlikon Leybold Vacuum Gmbh Electric feedthrough of a vacuum pump
DE102007053980A1 (en) * 2007-11-13 2009-05-14 Pfeiffer Vacuum Gmbh vacuum pump

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6413295U (en) * 1987-07-13 1989-01-24
JP2003278691A (en) * 2002-03-20 2003-10-02 Boc Edwards Technologies Ltd Vacuum pump

Also Published As

Publication number Publication date
EP2472120A1 (en) 2012-07-04
KR101784016B1 (en) 2017-10-10
JP5689546B2 (en) 2015-03-25
CN102483069A (en) 2012-05-30
JP2014080981A (en) 2014-05-08
CN102483069B (en) 2016-09-07
KR20120061770A (en) 2012-06-13
EP2472120A4 (en) 2017-08-02
JP5785494B2 (en) 2015-09-30
JPWO2011024528A1 (en) 2013-01-24
US20120141254A1 (en) 2012-06-07
WO2011024528A1 (en) 2011-03-03

Similar Documents

Publication Publication Date Title
EP2472120B1 (en) Vacuum pump and member used for vacuum pump
EP1318309B1 (en) Vacuum pump
KR100568183B1 (en) Turbo compressor
EP0228040B1 (en) Vacuum pump
KR100730073B1 (en) Evacuating apparatus
US6503050B2 (en) Turbo-molecular pump having enhanced pumping capacity
TW201812178A (en) Stator, rotary shaft, dry vacuum pump and associated manufacturing processes
CN107208650B (en) Adapter and vacuum pump
EP3581801B1 (en) Vacuum pump and imbalance correction method
KR102167210B1 (en) Vacuum pump
JP5180709B2 (en) Screw compressor
JP3038432B2 (en) Vacuum pump and vacuum device
JP6017820B2 (en) Impeller and submersible pump
JP4872640B2 (en) Vacuum pump and manufacturing method
JP6758865B2 (en) Vacuum pump
JP5156649B2 (en) Vacuum pump
JP2009513861A (en) Pump equipment for semiconductor processing
JP3026217B1 (en) Vacuum pump
JP2009138641A (en) Compressor
WO2019180990A1 (en) Fixed member extraction method, fixed member machining method, rotary machine, and jig
JP2009275578A (en) Magnetic bearing type turbo-molecular pump and vacuum system
JP2541291Y2 (en) Vacuum pump
KR20240029264A (en) Passive air curtain spindle for dental drilling machine
KR20220105203A (en) centrifugal turbo compressor
JP2009150238A (en) Liquid-sealed vacuum pump, and method for performance adjusting of liquid-sealed vacuum pump

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

17P Request for examination filed

Effective date: 20120104

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 SE SI SK SM TR

DAX Request for extension of the european patent (deleted)
RIC1 Information provided on ipc code assigned before grant

Ipc: F04D 19/04 20060101AFI20170322BHEP

Ipc: F04D 29/52 20060101ALI20170322BHEP

RA4 Supplementary search report drawn up and despatched (corrected)

Effective date: 20170704

RIC1 Information provided on ipc code assigned before grant

Ipc: F04D 29/52 20060101ALI20170628BHEP

Ipc: F04D 19/04 20060101AFI20170628BHEP

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

17Q First examination report despatched

Effective date: 20180309

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTG Intention to grant announced

Effective date: 20220301

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

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

Free format text: STATUS: EXAMINATION IS IN PROGRESS

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

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

Free format text: STATUS: GRANT OF PATENT IS INTENDED

INTC Intention to grant announced (deleted)
INTG Intention to grant announced

Effective date: 20220712

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

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

Free format text: STATUS: THE PATENT HAS BEEN GRANTED

AK Designated contracting states

Kind code of ref document: B1

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 SE SI SK SM 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

REG Reference to a national code

Ref country code: DE

Ref legal event code: R082

Ref document number: 602010068601

Country of ref document: DE

Representative=s name: FLEUCHAUS & GALLO PARTNERSCHAFT MBB - PATENT- , DE

Ref country code: DE

Ref legal event code: R082

Ref document number: 602010068601

Country of ref document: DE

Representative=s name: FLEUCHAUS & GALLO PARTNERSCHAFT MBB PATENTANWA, DE

REG Reference to a national code

Ref country code: AT

Ref legal event code: REF

Ref document number: 1534896

Country of ref document: AT

Kind code of ref document: T

Effective date: 20221215

Ref country code: DE

Ref legal event code: R096

Ref document number: 602010068601

Country of ref document: DE

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: NL

Ref legal event code: FP

REG Reference to a national code

Ref country code: LT

Ref legal event code: MG9D

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 14

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

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: 20221130

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: 20230331

Ref country code: NO

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: 20230228

Ref country code: LT

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: 20221130

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: 20221130

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: 20221130

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK05

Ref document number: 1534896

Country of ref document: AT

Kind code of ref document: T

Effective date: 20221130

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

Ref country code: PL

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: 20221130

Ref country code: LV

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: 20221130

Ref country code: IS

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: 20230330

Ref country code: HR

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: 20221130

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: 20230301

P01 Opt-out of the competence of the unified patent court (upc) registered

Effective date: 20230503

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

Ref country code: SM

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: 20221130

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: 20221130

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: 20221130

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: 20221130

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: 20221130

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: 20221130

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

Ref country code: IT

Payment date: 20230412

Year of fee payment: 14

Ref country code: IE

Payment date: 20230412

Year of fee payment: 14

Ref country code: DE

Payment date: 20230404

Year of fee payment: 14

Ref country code: CH

Payment date: 20230602

Year of fee payment: 14

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: 20221130

Ref country code: AL

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: 20221130

REG Reference to a national code

Ref country code: DE

Ref legal event code: R097

Ref document number: 602010068601

Country of ref document: DE

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

Ref country code: BE

Payment date: 20230418

Year of fee payment: 14

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

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

Ref country code: GB

Payment date: 20230406

Year of fee payment: 14

26N No opposition filed

Effective date: 20230831

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

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: 20221130

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20221130

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 FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20221130

Ref country code: LU

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

Effective date: 20230531

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

Ref country code: NL

Payment date: 20240415

Year of fee payment: 15

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

Ref country code: FR

Payment date: 20240328

Year of fee payment: 15