US20130309076A1 - Rotating Body of Vacuum Pump, Fixed Member Disposed Opposite Rotating Body, and Vacuum Pump Provided with Rotating Body and Fixed Member - Google Patents
Rotating Body of Vacuum Pump, Fixed Member Disposed Opposite Rotating Body, and Vacuum Pump Provided with Rotating Body and Fixed Member Download PDFInfo
- Publication number
- US20130309076A1 US20130309076A1 US13/982,412 US201113982412A US2013309076A1 US 20130309076 A1 US20130309076 A1 US 20130309076A1 US 201113982412 A US201113982412 A US 201113982412A US 2013309076 A1 US2013309076 A1 US 2013309076A1
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- Prior art keywords
- rotating body
- rotor
- vacuum pump
- fixed member
- fiber
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
- F04D19/042—Turbomolecular vacuum pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
- F04D19/044—Holweck-type pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/30—Manufacture with deposition of material
- F05D2230/31—Layer deposition
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/95—Preventing corrosion
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/10—Metals, alloys or intermetallic compounds
- F05D2300/17—Alloys
- F05D2300/173—Aluminium alloys, e.g. AlCuMgPb
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
- F05D2300/2112—Aluminium oxides
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/40—Organic materials
- F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/611—Coating
Definitions
- the present invention relates to a rotating body of a vacuum pump that can be used, for example, for evacuating a process chamber or another sealed chamber in a semiconductor production device, a flat panel display production device, or a solar panel production device, and relates to a fixed member disposed opposite the rotating body, and to a vacuum pump provided with the rotating body and fixed member.
- a composite turbomolecular pump described in Japanese Patent Publication No. 3098139 is known as the conventional vacuum pump of this type.
- this composite turbomolecular pump is provided with a turbomolecular pump portion ( 2 ) as a vane exhaust portion that exhausts gas by interaction of rotating vanes ( 2 a ) and fixed vanes ( 2 b ), and a thread groove pump portion ( 3 ) that exhausts gas with a thread groove ( 7 a ).
- a rotor ( 4 a ) of the turbomolecular pump portion ( 2 ) is made from an aluminum alloy
- a rotor ( 6 ) of the thread groove pump portion ( 3 ) is made from a carbon fiber reinforced plastic (CFRP).
- CFRP carbon fiber reinforced plastic
- the rotor ( 6 ) of the thread groove pump portion ( 3 ) is formed from a lightweight fiber-reinforced plastic material having a high strength. Therefore, the circumferential speed of the rotor ( 6 ) can be increased and the exhaust performance of the thread groove pump portion ( 3 ) can be improved over those attained with the rotor in which the aforementioned portion is formed from an aluminum alloy by increasing the revolution speed of the rotor ( 6 ) or enlarging the diameter of the rotor ( 6 ).
- the strength of the CFRP material decreases and the rotor ( 6 ) becomes susceptible to brittle fracture due to thermal transformation of the CFRP material. For this reason, in a pump in which the exhaust performance is improved by increasing the circumferential speed of the rotor ( 6 ), it is difficult to improve the exhaust performance and increase the maximum flow rate at the same time.
- the heat accumulated in the rotor ( 6 ) is generally radiated by thermal conduction via the exhausted gas (first heat radiation route), thermal conduction via the bearing of the rotor ( 6 ) (second heat radiation route), and emission from the surface of the rotor ( 6 ) (third heat radiation route).
- first heat radiation route thermal conduction via the exhausted gas
- second heat radiation route thermal conduction via the bearing of the rotor ( 6 )
- emission from the surface of the rotor ( 6 ) third heat radiation route.
- a contactless bearing such as a magnetic bearing
- the thermal conductivity of the CFRP which is the structural material of the rotor ( 6 )
- the aluminum alloy which is the structural material of the rotor ( 4 a ) or rotating vanes ( 2 a ) of the turbomolecular pump portion ( 2 )
- a temperature distribution can easily occur therein.
- the present invention has been created to resolve the abovementioned problems and it is an object thereof to provide a rotating body of a vacuum pump that is advantageous for obtaining a highly reliable vacuum pump in which the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust can be increased at the same time, and also a fixed member facing the rotating body, and a vacuum pump provided with the rotating body and the fixed member.
- the present invention provides a rotating body of a vacuum pump that is entirely or partially constituted by a fiber-reinforced plastic and that exhausts gas by rotation, wherein the rotating body is provided with a corrosion-resistant layer on a fiber-reinforced plastic portion, which is a base material thereof, and with a high-emissivity layer having a higher emissivity than the corrosion-resistant layer on the corrosion-resistant layer.
- the aforementioned high-emissivity layer may be an oxide film layer obtained by oxidizing the surface of a metal coating film formed on the corrosion-resistant layer, or a DLC layer formed by performing DLC coating treatment on the corrosion-resistant layer.
- the fixed member of a vacuum pump that is disposed opposite the rotating body of the vacuum pump in accordance with the present invention faces the inner circumferential surface or outer circumferential surface of the rotating body of the vacuum pump, which is entirely or partially constituted by a fiber-reinforced plastic, and forms, between the fixed member and the rotating body, a spiral thread groove exhaust flow channel for exhausting gas, wherein a high-emissivity layer having a higher emissivity than the base material of the fixed member is provided on a surface of the fixed member that faces a fiber-reinforced plastic portion of the rotating body.
- the high-emissivity layer may be an oxide film layer obtained by oxidizing the surface of an aluminum alloy which is the base material of the fixed member, or a coating film layer formed by coating the surface of the fixed member with a material having a higher emissivity than the aluminum alloy of the base material.
- the vacuum pump in accordance with the present invention is provided with the abovementioned rotating body of a vacuum pump, or with the abovementioned rotating body and the fixed member of a vacuum pump.
- the rotating body in a specific configuration of the rotating body of a vacuum pump, is provided with a corrosion-resistant layer on the fiber-reinforced plastic portion, which is the base material of the rotating body, and a high-emissivity layer having a higher emissivity than the corrosion-resistant layer is provided on the corrosion-resistant layer.
- the fixed member in a specific configuration of the fixed member disposed opposite the rotating body of a vacuum pump, the fixed member is provided with a high-emissivity layer having a higher emissivity than the base material of the fixed member on the surface (opposing surface) facing the fiber-reinforced plastic portion of the rotating body.
- the heat generated in the fiber-reinforced plastic portion of the rotating body is smoothly and efficiently radiated by emission to the fixed member side and, therefore, the temperature of the fiber-reinforced plastic portion of the rotating body can be effectively prevented from increasing and surpassing the temperature allowed for the fiber-reinforced plastic portion of the rotating body under the effect of heat (friction heat) generated by the friction between the exhausted gas and the rotating body, and it is possible to obtain a highly reliable vacuum pump in which the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust can be increased at the same time.
- FIG. 1 is a cross-sectional view of a vacuum pump using the present invention
- FIG. 2 is an enlarged sectional view of the first tubular body made from a fiber-reinforced plastic and constituting the rotor which is the rotating body of the vacuum pump shown in FIG. 1 and the part of the thread groove pump portion stator which is the fixed member of the vacuum pump facing the first rotating body; and
- FIG. 3 is an enlarged sectional view of the first tubular body made from a fiber-reinforced plastic and constituting the rotor which is the rotating body of the vacuum pump shown in FIG. 1 and the part of the thread groove pump portion stator which is the fixed member of the vacuum pump facing the first rotating body.
- FIG. 1 is a cross-sectional view of a vacuum pump using the present invention.
- a vacuum pump P shown in the figure can be used, for example, as gas exhaust means for a process chamber or another sealed chamber in a semiconductor production device, a flat panel display production device, or a solar panel production device.
- the vacuum pump P has inside an outer case 1 a vane exhaust portion Pt that exhausts gas with a rotating vane 13 and a fixed vane 14 , a thread groove pump portion Ps that exhausts gas by using thread grooves 19 A, 19 B, and a drive system therefor.
- the outer case 1 has an open-end cylindrical shape obtained by integrally joining a tubular pump case 1 A and an open-end tubular pump base 1 B with bolts in the axial direction thereof.
- the upper end side of the pump case 1 A is open as a gas intake port 2
- the side surface at the lower end of the pump base 1 B is provided with a gas exhaust port 3 .
- the gas intake port 2 is connected to a sealed chamber (not shown in the figure) under a high vacuum, such as a process chamber of a semiconductor production device, with bolts (not shown in the figure) provided in a flange 1 C at the upper edge of the pump case 1 A.
- the gas exhaust port 3 is connected so as to communicate with an auxiliary pump (not shown in the figure).
- a cylindrical stator column 4 containing inside thereof various electric devices is provided in the central portion inside the pump case 1 A, and the stator column 4 is provided in a vertical condition in which the lower end side thereof is fixed with screws to the pump base 1 B.
- a rotor shaft 5 is provided inside the stator column 4 , and the rotor column 5 is disposed so that the upper end portion thereof faces in the direction of the gas intake port 2 , whereas the lower end portion thereof faces in the direction of the pump base 1 B.
- the upper end portion of the rotor shaft 5 is provided so as to protrude upward form the upper end surface of the cylindrical shape of the stator column 4 .
- the rotor shaft 5 is rotatably supported in the radial direction and axial diction by radial magnetic bearings 10 and an axial magnetic bearing 11 and rotationally driven in this state by a drive motor 12 .
- the drive motor 12 has a structure constituted by a stator 12 A and a rotor 12 B and is provided substantially close to the center of the rotor shaft 5 .
- the stator 12 A of the drive motor 12 is disposed inside the stator column 4 , and the rotor 12 B of the drive motor 12 is integrally mounted on the outer circumferential surface side of the rotor shaft 5 .
- the radial magnetic bearings 10 are disposed by one above and below the drive motor 12 , and one axial magnetic bearing 11 is disposed at the lower end side of the rotor shaft 5 .
- the two radial magnetic bearings 10 are each constituted by a radial electromagnet target 10 A attached to the outer circumferential surface of the rotor shaft 5 , a plurality of radial electromagnets 10 B disposed on the inner side surface of the stator column 4 opposite thereto, and a radial displacement sensor 10 C.
- the radial electromagnet target 10 A is constituted by a laminated steel plate obtained by laminating steel sheets which are materials with a high magnetic permeability.
- the radial magnets 10 B attract the rotor shaft 5 by a magnetic force in the radial direction through the radial electromagnet target 10 A.
- the radial displacement sensor 10 C detects the radial displacement of the rotor shaft 5 .
- the axial magnetic bearing 11 is constituted by a disk-shaped armature disk 11 A attached to the outer circumference of the lower end portion of the rotor shaft 5 , axial electromagnets 11 B sandwiching the armature disk 11 A from above and below, and an axial displacement sensor 11 C disposed at a position slightly separated from the lower end surface of the rotor shaft 5 .
- the armature disk 11 A is constituted by a material with a high magnetic permeability, and the upper and lower axial electromagnets 11 B attract the armature disk 11 A by magnetic forces from above and below.
- the axial displacement sensor 11 C detects the axial displacement of the rotor shaft 5 .
- a rotor 6 is provided as a rotating body of the vacuum pump P outside of the stator column 4 .
- the rotor 6 has a cylindrical shape surrounding the outer circumference of the stator column 4 and has a structure in which two tubular bodies (a first tubular body 61 and a second tubular body 62 ) of different diameters are joined in the axial direction thereof, with a support member 60 of an annular plate shape being interposed therebetween.
- the support member is positioned in a substantially middle portion to the cylindrical shape.
- the support member 60 is integrally provided at the lower end of the second tubular body 62 , and a ring-shaped protruding portion 60 A is integrally provided at the outer circumferential portion at the rear surface of the support member 60 .
- the first tubular body 61 and the second tubular body 62 are joined in the axial direction thereof by press fitting and mounting the first tubular body 61 on the outer circumference of the ring-shaped protruding portion 60 A.
- An end member 63 is provided at the upper end of the second tubular body 62 , and the rotor 6 and the rotor shaft 5 are integrated, with the end member 63 being interposed therebetween.
- a boss hole 7 is provided in the center of the end member 63 and a step-like shoulder portion (referred to hereinbelow as “rotor shaft shoulder portion 9 ”) is formed at the outer circumference of the upper end portion of the rotor shaft 5 .
- the distal end portion of the rotor shaft 5 located above the rotor shaft shoulder portion 9 is inserted into the boss hole 7 of the end member 63 , and the end member 63 and the rotor shaft shoulder portion 9 are tightened and fixed by bolts to integrate the rotor 6 with the rotor shaft 5 .
- the first tubular body 61 is formed from a fiber-reinforced plastic such as aramide fiber-reinforced plastic (AFRP), boron fiber-reinforced plastic (BFRP), carbon fiber-reinforced plastic (CFRP), polyethylene fiber reinforced plastic (DFRP), and glass fiber-reinforced plastic (GFRP) in order to reduce the weight of the entire pump and increase the revolution speed of the rotor 6 .
- AFRP aramide fiber-reinforced plastic
- BFRP boron fiber-reinforced plastic
- CFRP carbon fiber-reinforced plastic
- DFRP polyethylene fiber reinforced plastic
- GFRP glass fiber-reinforced plastic
- the structural components of the rotor other than the first tubular body 61 more specifically, the second tubular body 62 , support member 60 , and end member 63 , are all formed from a lightweight metal material such as aluminum or an aluminum alloy.
- the vacuum pump P shown in FIG. 1 uses the rotor 6 configured to include the first tubular body 61 made from a fiber-reinforced plastic, as an example of a rotating body partially constituted by a fiber-reinforced plastic.
- the rotor 6 is supported to be rotatable about the axial center thereof (rotor shaft 5 ) by the radial magnetic bearings 10 and the axial magnetic bearing 11 via the rotor shaft 5 . Therefore, in the vacuum pump P shown in FIG. 1 , the rotor shaft 5 , radial magnetic bearings 10 and axial magnetic bearing 11 function as support means for supporting the rotor 6 so that the rotor could rotate about the axial center thereof. Further, since the rotor 6 rotates integrally with the rotor shaft 5 , the drive motor 12 rotationally driving the rotor shaft 5 functions as drive means for rotationally driving the rotor 6 .
- the zone upstream of the substantially middle portion of the rotor 6 (zone from the substantially middle portion of the rotor 6 to the end portion of the rotor 6 on the gas intake port 2 side) is configured to function as the vane exhaust portion Pt.
- the vane exhaust portion Pt is described hereinbelow in greater detail.
- a plurality of rotating vanes 13 are integrally provided at the outer circumferential surface of the rotor 6 upstream of the substantially middle portion of the rotor 6 (more specifically, at the outer circumferential surface of the second tubular body 62 ).
- the plurality of rotating vanes 13 is arranged radially about the rotating shaft center (rotor shaft 5 ) of the rotor 6 or the axial center of the outer case 1 (referred to hereinbelow as “pump axial center”).
- a plurality of fixed vanes 14 is provided at the inner circumferential surface side of the pump case 1 A. Those fixed vanes 14 are disposed radially about the pump axial center.
- the rotating vanes 13 and the fixed vanes 14 are disposed alternately in multiple stages along the pump axial center, thereby forming the vane exhaust portion Pt.
- All of the rotating vanes 13 are blade-shaped machined parts obtained by cutting integrally with the outer-diameter machined portion of the rotor 6 and are inclined at an angle optimum for exhausting gas molecules. All of the fixed vanes 14 are also inclined at an angle optimum for exhausting gas molecules.
- the rotor shaft 5 , rotor 6 , and plurality of rotating vanes 13 are integrally rotationally driven when the drive motor 12 is started, and the rotating vane 13 of the uppermost stage imparts a momentum in the direction from the gas intake port 2 to the gas exhaust port 3 to the gas molecules that have entered from the gas intake port 2 .
- the gas molecules having such a momentum in the exhaust direction are fed by the fixed vanes 14 to the rotating vane 13 of the next stage.
- the gas molecules on the gas intake port 2 side are exhausted so as to travel successively toward the downstream side of the rotor 6 .
- the zone downstream of the substantially middle portion of the rotor 6 (zone from the substantially middle portion of the rotor 6 to the end portion of the rotor 6 on the gas exhaust port 3 side) is configured to function as the thread groove pump portion Ps.
- the thread groove pump portion Ps is described hereinbelow in greater detail.
- the rotor 6 downstream of the substantially middle portion of the rotor 6 (more specifically, the portion of the first tubular body 61 ) rotates as the rotating member of the thread groove pump portion Ps and is configured to be inserted and accommodated between outer and inner double-wall cylindrical thread groove pump portion stators 18 A, 18 B of an inner-outer double-wall tubular configuration of the thread groove pump portion Ps, with a certain gap being present between the rotor and the two stators.
- the outer thread groove pump portion stator 18 A is disposed so as to surround the outer circumference of the rotor 6 (portion downstream of the substantially middle portion of the rotor 6 ), as the fixed member of the vacuum pump P positioned on the outside of the rotor 6 , and, therefore, is provided so as to face the outer circumferential surface of the rotor 6 .
- a thread groove 19 A with a depth changing to a taper cone shape that reduces in diameter in the downward direction is formed in the inner circumferential portion of the outer thread groove pump portion stator 18 A.
- the thread groove 19 A is cut spirally from the upper end to the lower end of the thread groove pump portion stator 18 A, and a spiral thread groove pump flow channel (referred to hereinbelow as “outer thread groove pump flow channel S 1 ”) is formed between the rotor 6 and the outer thread groove pump portion stator 18 A by this thread groove 19 A.
- the lower end portion of the outer thread groove pump portion stator 18 A is supported by the pump base 1 B.
- the inner thread groove pump portion stator 18 B is disposed so as to be surrounded by the inner circumference of the rotor 6 , as the fixed member of the vacuum pump P positioned on the inside of the rotor 6 , and, therefore, is provided so as to face the inner circumferential surface of the rotor 6 . Further, a thread groove 19 B is likewise formed in the outer circumferential portion of the inner thread groove pump portion stator 18 B.
- the thread groove 19 B forms a spiral thread groove pump flow channel (referred to hereinbelow as “inner thread groove pump flow channel S 2 ”) between the rotor 6 and the inner thread groove pump portion stator 18 B.
- the lower end portion of the inner thread groove pump portion stator 18 B is also supported by the pump base 1 B.
- outer thread groove pump flow channel S 1 or inner thread groove pump flow channel S 2 may be also provided by forming the thread grooves 19 A, 19 B, which have been explained hereinabove, in the outer circumferential surface or inner circumferential surface of the rotor 6 (this configuration is not shown in the figures).
- the depth of the thread groove 19 A is set to be the largest at the upstream inlet side of the outer thread groove pump flow channel S 1 (passage opening end that is closer to the gas intake port 2 ) and to be the smallest at the downstream outlet side (passage opening end that is closer to the gas exhaust port 3 ), so that the gas be transferred, while being compressed, by the drag effect at the outer circumferential surface of the thread groove 19 A and the rotor 6 or the drag effect at the inner circumferential surface of the thread groove 19 B and the rotor 6 .
- the thread groove 19 B has a similar depth.
- the upstream inlet of the outer thread groove pump flow channel S 1 is configured to communicate with a gap (referred to hereinbelow as “last gap G”) between the vane of the lowest stage (the fixed vane 14 in the example shown in FIG. 1 ), from among the rotating vanes 13 and the fixed vanes 14 disposed in multiple stages, and the upstream end of the below-described communication opening portion H.
- the downstream outlet of the same passage S 1 is configured to communicate with the gas exhaust port 3 side.
- the upstream inlet of the inner thread groove pump flow channel S 2 is opened toward the inner circumferential surface of the rotor 6 in the substantially middle portion of the rotor 6 , and the downstream outlet of the same passage S 2 is configured to merge with the downstream outlet of the outer thread groove pump flow channel S 1 and communicate with the gas exhaust port 3 .
- the communication opening portion H is opened in the substantially middle portion of the rotor 6 .
- the communication opening portion H is formed so as to pass through from the front surface to the rear surface of the support member 60 and, therefore, functions to guide part of the gas present at the outer circumferential side of the rotor 6 into the inner thread groove pump flow channel S 2 .
- the rotor 6 has a structure in which a corrosion-resistant layer L 1 is provided on the fiber-reinforced plastic portion, which is the base material of the rotor (in the example shown in the figure, the surface of the first tubular body 61 ), and then a high-emissivity layer L 3 with an emissivity higher than that of the corrosion-resistant layer L 1 is provided on the corrosion-resistant layer L 1 .
- the corrosion-resistant layer L 1 protects the surface of the first tubular member 61 , as mentioned hereinabove, as means for protecting the fiber-reinforced plastic portion (in the example shown in the figure, the first tubular body 61 ) of the rotor 6 , so that the pump could be used in the environment in which such a corrosive gas that decomposes plastic components is exhausted.
- the corrosion-resistant layer L 1 has a lower emissivity than the fiber-reinforced plastic in the underlying layer, the amount of heat released by emission from the first tubular body 61 is greatly reduced.
- the fiber-reinforced plastic forming the first tubular body 61 which is part of the rotor, is lower in thermal conductivity than aluminum or an alloy thereof, which forms the other portion of the rotor 6 , and a temperature distribution easily occurs.
- the first tubular body 61 is heated to a comparatively high temperature by the heat (friction heat) generated by the friction with gas that is exhausted in the end portion on the gas exhaust port 3 side where the pressure is high.
- the corrosion-resistant layer L 1 is provided on the first tubular body 61 (fiber-reinforced plastic portion of the rotor 6 ), and the high-emissivity layer L 3 is provided on the corrosion-resistant layer L 1 , whereby the emissivity of the first tubular body 61 is increased. Therefore, the heat generated in the first tubular body 61 is easily released by emission, and inside the outer and inner thread groove pump flow channels S 1 and S 2 , the circumference of the end portion on the exhaust port side of the first tubular body 61 where the pressure is high can be prevented from being heated by the aforementioned friction heat to a high temperature exceeding the temperature allowed for the fiber-reinforced plastic.
- the corrosion-resistant layer L 1 on the inner and outer circumferential surfaces of the rotor 6 is constituted by a first metal coating film with excellent corrosion resistance, such as a nickel alloy film, and formed such as to cover the entire outer circumferential surface of the first tubular body 61 .
- the high-emissivity layer L 3 covering the corrosion-resistant layer L 1 forms a second metal coating film L 2 from an aluminum alloy or a nickel alloy on the corrosion-resistant layer L 1 and is constituted by an oxide film layer obtained by oxidizing the surface of the second metal coating film L 2 .
- the high-emissivity layer is formed to cover the entire corrosion-resistant layer L 1 .
- a method can be also considered by which the surface of the first metal coating film (corrosion-resistant layer L 1 ) is oxidized and the resultant oxide film layer is used as the high-emissivity layer L 3 .
- the corrosion-resistant layer L 1 is formed by electroless Ni—P plating
- pinholes are formed in the corrosion-resistant layer L 1 and the corrosion-resistant layer L 1 can be easily damaged and fractured in the vicinity of the pinholes by the oxidation of the corrosion-resistant layer L 1 having the pinholes.
- the resultant problem is that the protective function of the corrosion-resistant layer L 1 with respect to the first tubular body 61 (made from the fiber-reinforced plastic) is lost.
- the high-emissivity layer L 3 be formed by the above-described method, that is, by the method in which the corrosion-resistant layer L 1 is protected by the second metal coating film L 2 by forming the second metal coating film L 2 on the corrosion-resistant layer (first metal coating film) L 1 and then the surface of the second metal coating film L 2 is oxidized.
- the corrosion-resistant layer L 1 (first metal coating film) or the second metal coating film L 2 explained hereinabove can be formed, for example, by electroplating, electroless plating, or sputtering.
- the high-emissivity layer L 3 provided on the corrosion-resistant layer L 1 it is possible to use a DLC film formed by coating diamond-like carbon (DLC) on the corrosion-resistant layer L 1 (this configuration is not shown in the figures).
- DLC diamond-like carbon
- a high-emissivity layer L 4 having a higher emissivity than the base material (for example, aluminum or alloys thereof) of the fixed members is provided on the fixed members facing the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 , more specifically, on the opposing surfaces of the outer thread groove pump portion stator 18 A and the inner thread groove pump portion stator 18 B.
- the high-emissivity layer L 4 provided on the opposing surfaces may form the thread peaks of the thread grooves 19 A, 19 B and also the inner surfaces and side surfaces of the thread grooves 19 A, 19 B.
- the high-emissivity layer L 4 on the opposing surfaces of the fixed members can be in the form of an oxide film layer obtained by oxidizing the surface of the base material (aluminum or an alloy thereof).
- a coating film layer obtained by coating the surface of the fixed members with a material having a higher emissivity than aluminum or an alloy thereof, which is the base material of the fixed members (thread groove pump portion stators 18 A, 18 B), such as a fluororesin or an epoxy resin, or a DLC layer formed by coating DLC on the surface of the fixed members can be also used.
- the thread groove pump portion stators 18 A, 18 B are used as means for guiding the heat from inside the pump to the outside.
- the thread groove pump portion stators 18 A, 18 B are formed from a metal material with a high thermal conductivity, such as aluminum or an alloy thereof.
- the emissivity of the surface thereof is low and the ability to receive the heat of the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 by emission is low.
- this ability is improved by the high-emissivity layer L 4 .
- the thread groove pump portion stators 18 A, 18 B can efficiently receive the heat of the fiber-reinforced plastic portion of the rotor 6 by emission and the received heat can be guided out to the outside. Therefore, the amount of heat accumulated in the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 is reduced and the temperature of the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 can be effectively prevented from rising and exceeding the temperature allowed for the fiber-reinforced plastic under the effect of the heat (friction heat) generated by the friction between the exhausted gas and the rotor 6 .
- the corrosion-resistant layer L 1 from among the components of the above-described configuration, may be omitted as shown in FIG. 3 .
- the emissivity of the fiber-reinforced plastic used for forming the first tubular body 61 of the rotor 6 is higher than that of aluminum or an alloy thereof that is used for forming structural components (second tubular body 62 , support member 60 , and end member 63 ) of the rotor other than the first tubular body 61
- the high-emissivity layer L 3 and also the second metal coating film L 2 from among the components of the above-described configuration, may be omitted as shown in FIG. 3 .
- a high-emissivity layer L 4 having a higher emissivity than aluminum or an alloy thereof, which is the base material of the thread groove pump portion stators 18 A, 18 B may be provided in the above-described configuration increasing the emissivity of the fixed members (thread groove pump portion stators 18 A, 18 B) facing the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 , more specifically on the opposing surfaces of the thread groove pump portion stators 18 A, 18 B (fixed members of the vacuum pump P) that face the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 (see FIG.
- the heat released by emission from the fiber-reinforced plastic portion of the rotor 6 can be efficiently received by the high-emissivity layers of the thread groove pump portion stators 18 A, 18 B. Therefore, the amount of heat accumulated in the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 is reduced and the temperature of the fiber-reinforced plastic portion (first tubular body 61 ) of the rotor 6 can be effectively prevented from rising and exceeding the temperature allowed for the fiber-reinforced plastic under the effect of the heat (friction heat) generated by the friction between the exhausted gas and the rotor 6 .
- the embodiment explained hereinabove is an example in which the present invention is applied to a structure in which part (more specifically, the portion of the first tubular body 61 ) of the rotor 6 , which is the rotating body of the vacuum pump P, is constituted by a fiber-reinforced plastic, but the present invention is not limited to this example and can be also applied to a structure in which the entire rotor 6 (including the rotating vanes 13 ) is constituted by a fiber-reinforced plastic.
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Abstract
A rotating body of a vacuum pump is partially constituted by a fiber-reinforced plastic and configured to exhaust gas by rotation. A corrosion-resistant layer is provided on the fiber-reinforced plastic portion which is the base material of the rotating body. A high-emissivity layer having a higher emissivity than the corrosion-resistant layer is provided on the corrosion-resistant layer. Fixed members facing the rotating body of the vacuum pump are each provided with a high-emissivity layer having a higher emissivity than the base material of the fixed members on the surfaces facing the fiber-reinforced plastic portion of the rotating body.
Description
- This Application is a Section 371 National Stage Application of International Application No. PCT/JP2011/077301, filed Nov. 28, 2011, which is incorporated by reference in its entirety and published as WO 2012/105116 on Aug. 9, 2012, not in English, and which claims priority to Japanese Patent Application No. 2011-022923, filed Feb. 4, 2011.
- 1. Field of the Invention
- The present invention relates to a rotating body of a vacuum pump that can be used, for example, for evacuating a process chamber or another sealed chamber in a semiconductor production device, a flat panel display production device, or a solar panel production device, and relates to a fixed member disposed opposite the rotating body, and to a vacuum pump provided with the rotating body and fixed member. In accordance with the present invention, the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust (=maximum flow rate) can be increased at the same time.
- 2. Description of the Related Art
- For example, a composite turbomolecular pump described in Japanese Patent Publication No. 3098139 is known as the conventional vacuum pump of this type. As follows from Japanese Patent Publication No. 3098139 (
FIG. 1 ,claim 1, and description of paragraphs [0012] and [0013]), this composite turbomolecular pump is provided with a turbomolecular pump portion (2) as a vane exhaust portion that exhausts gas by interaction of rotating vanes (2 a) and fixed vanes (2 b), and a thread groove pump portion (3) that exhausts gas with a thread groove (7 a). A rotor (4 a) of the turbomolecular pump portion (2) is made from an aluminum alloy, and a rotor (6) of the thread groove pump portion (3) is made from a carbon fiber reinforced plastic (CFRP). - In the composite turbomolecular pump constituted by the turbomolecular pump portion (2) and the thread groove pump portion (3) such as descried in the aforementioned Japanese Patent Publication No. 3098139, the rotor (6) of the thread groove pump portion (3) is formed from a lightweight fiber-reinforced plastic material having a high strength. Therefore, the circumferential speed of the rotor (6) can be increased and the exhaust performance of the thread groove pump portion (3) can be improved over those attained with the rotor in which the aforementioned portion is formed from an aluminum alloy by increasing the revolution speed of the rotor (6) or enlarging the diameter of the rotor (6).
- However, when the circumferential speed of the rotor (6) is increased in the above-described manner, the circumferential speed of the rotor (6) in the thread groove pump portion (3) becomes close to the sound velocity of the exhausted gas. As a result, the temperature of the rotor (6) is raised by the heat (friction heat) generated by the friction between the rotor (6) and the gas exhausted in the thread groove pump portion (3) and the temperature of the CFRP, which is the structural material of the rotor (6), exceeds the temperature allowed therefor, thereby causing problems associated with heat resistance. In other words, the strength of the CFRP material decreases and the rotor (6) becomes susceptible to brittle fracture due to thermal transformation of the CFRP material. For this reason, in a pump in which the exhaust performance is improved by increasing the circumferential speed of the rotor (6), it is difficult to improve the exhaust performance and increase the maximum flow rate at the same time.
- The heat accumulated in the rotor (6) is generally radiated by thermal conduction via the exhausted gas (first heat radiation route), thermal conduction via the bearing of the rotor (6) (second heat radiation route), and emission from the surface of the rotor (6) (third heat radiation route). However, when a contactless bearing such as a magnetic bearing is used as the bearing of the rotor (6), the radiation of heat from the rotor (6) via the second heat radiation route cannot be expected. Further, for certain types of the exhausted gas, the radiation of heat from the rotor (6) via the first heat radiation route practically cannot be expected.
- Therefore, the radiation of heat from the rotor (6) in the case in which a contactless bearing is used as the bearing of the rotor (6), as described hereinabove, proceeds mainly via the third heat radiation route. However, the thermal conductivity of the CFRP, which is the structural material of the rotor (6), is lower than that of the aluminum alloy, which is the structural material of the rotor (4 a) or rotating vanes (2 a) of the turbomolecular pump portion (2), and a temperature distribution can easily occur therein. In particular, when the revolution speed of the rotor (6) is increased, as described hereinabove, or the configuration is used in which the diameter of the rotor (6) is enlarged, the circumference of the lower end portion of the rotor (6), which is close to the exhaust port (8) where the pressure is high and friction with gas is significant in the thread groove pump (3), can be easily fractured by the increase in temperature caused by the aforementioned friction heat.
- The reference numerals in parentheses hereinabove are same as those used in Japanese Patent Publication No. 3098139.
- The present invention has been created to resolve the abovementioned problems and it is an object thereof to provide a rotating body of a vacuum pump that is advantageous for obtaining a highly reliable vacuum pump in which the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust can be increased at the same time, and also a fixed member facing the rotating body, and a vacuum pump provided with the rotating body and the fixed member.
- To attain the above-described object, the present invention provides a rotating body of a vacuum pump that is entirely or partially constituted by a fiber-reinforced plastic and that exhausts gas by rotation, wherein the rotating body is provided with a corrosion-resistant layer on a fiber-reinforced plastic portion, which is a base material thereof, and with a high-emissivity layer having a higher emissivity than the corrosion-resistant layer on the corrosion-resistant layer.
- In the rotating body of a vacuum pump in accordance with the present invention, the aforementioned high-emissivity layer may be an oxide film layer obtained by oxidizing the surface of a metal coating film formed on the corrosion-resistant layer, or a DLC layer formed by performing DLC coating treatment on the corrosion-resistant layer.
- The fixed member of a vacuum pump that is disposed opposite the rotating body of the vacuum pump in accordance with the present invention faces the inner circumferential surface or outer circumferential surface of the rotating body of the vacuum pump, which is entirely or partially constituted by a fiber-reinforced plastic, and forms, between the fixed member and the rotating body, a spiral thread groove exhaust flow channel for exhausting gas, wherein a high-emissivity layer having a higher emissivity than the base material of the fixed member is provided on a surface of the fixed member that faces a fiber-reinforced plastic portion of the rotating body.
- In the fixed member disposed opposite the rotating body of the vacuum pump in accordance with the present invention, the high-emissivity layer may be an oxide film layer obtained by oxidizing the surface of an aluminum alloy which is the base material of the fixed member, or a coating film layer formed by coating the surface of the fixed member with a material having a higher emissivity than the aluminum alloy of the base material.
- The vacuum pump in accordance with the present invention is provided with the abovementioned rotating body of a vacuum pump, or with the abovementioned rotating body and the fixed member of a vacuum pump.
- In accordance with the present invention, in a specific configuration of the rotating body of a vacuum pump, the rotating body is provided with a corrosion-resistant layer on the fiber-reinforced plastic portion, which is the base material of the rotating body, and a high-emissivity layer having a higher emissivity than the corrosion-resistant layer is provided on the corrosion-resistant layer. Therefore, for example, even when the circumferential speed of the rotating body is increased by using a method of increasing the revolution speed of the rotating body or enlarging the diameter of the fiber-reinforced plastic portion of the rotating body as means for improving the exhaust performance, where a similar high-emissivity layer is provided on the opposing surface of the fixed member facing the fiber-reinforced plastic portion of the rotating body, the heat generated in the fiber-reinforced plastic portion of the rotating body is smoothly and efficiently radiated by emission to the fixed member side and, therefore, the temperature of the fiber-reinforced plastic portion of the rotating body can be effectively prevented from increasing and surpassing the temperature allowed for the fiber-reinforced plastic portion of the rotating body under the effect of heat (friction heat) generated by the friction between the exhausted gas and the rotating body, and it is possible to obtain a highly reliable vacuum pump in which the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust can be increased at the same time.
- Further, in accordance with the present invention, in a specific configuration of the fixed member disposed opposite the rotating body of a vacuum pump, the fixed member is provided with a high-emissivity layer having a higher emissivity than the base material of the fixed member on the surface (opposing surface) facing the fiber-reinforced plastic portion of the rotating body. Therefore, for example, even when the circumferential speed of the rotating body is increased by the aforementioned method, the heat generated in the fiber-reinforced plastic portion of the rotating body is smoothly and efficiently radiated by emission to the fixed member side and, therefore, the temperature of the fiber-reinforced plastic portion of the rotating body can be effectively prevented from increasing and surpassing the temperature allowed for the fiber-reinforced plastic portion of the rotating body under the effect of heat (friction heat) generated by the friction between the exhausted gas and the rotating body, and it is possible to obtain a highly reliable vacuum pump in which the exhaust performance can be improved and the gas flow rate attainable in continuous exhaust can be increased at the same time.
-
FIG. 1 is a cross-sectional view of a vacuum pump using the present invention; -
FIG. 2 is an enlarged sectional view of the first tubular body made from a fiber-reinforced plastic and constituting the rotor which is the rotating body of the vacuum pump shown inFIG. 1 and the part of the thread groove pump portion stator which is the fixed member of the vacuum pump facing the first rotating body; and -
FIG. 3 is an enlarged sectional view of the first tubular body made from a fiber-reinforced plastic and constituting the rotor which is the rotating body of the vacuum pump shown inFIG. 1 and the part of the thread groove pump portion stator which is the fixed member of the vacuum pump facing the first rotating body. - The best mode for carrying out the present invention will be explained in greater detail hereinbelow with reference to the appended drawings.
-
FIG. 1 is a cross-sectional view of a vacuum pump using the present invention. A vacuum pump P shown in the figure can be used, for example, as gas exhaust means for a process chamber or another sealed chamber in a semiconductor production device, a flat panel display production device, or a solar panel production device. The vacuum pump P has inside an outer case 1 a vane exhaust portion Pt that exhausts gas with a rotatingvane 13 and a fixedvane 14, a thread groove pump portion Ps that exhausts gas by usingthread grooves - The
outer case 1 has an open-end cylindrical shape obtained by integrally joining atubular pump case 1A and an open-endtubular pump base 1B with bolts in the axial direction thereof. The upper end side of thepump case 1A is open as agas intake port 2, and the side surface at the lower end of thepump base 1B is provided with agas exhaust port 3. - The
gas intake port 2 is connected to a sealed chamber (not shown in the figure) under a high vacuum, such as a process chamber of a semiconductor production device, with bolts (not shown in the figure) provided in aflange 1C at the upper edge of thepump case 1A. Thegas exhaust port 3 is connected so as to communicate with an auxiliary pump (not shown in the figure). - A
cylindrical stator column 4 containing inside thereof various electric devices is provided in the central portion inside thepump case 1A, and thestator column 4 is provided in a vertical condition in which the lower end side thereof is fixed with screws to thepump base 1B. - A
rotor shaft 5 is provided inside thestator column 4, and therotor column 5 is disposed so that the upper end portion thereof faces in the direction of thegas intake port 2, whereas the lower end portion thereof faces in the direction of thepump base 1B. The upper end portion of therotor shaft 5 is provided so as to protrude upward form the upper end surface of the cylindrical shape of thestator column 4. - The
rotor shaft 5 is rotatably supported in the radial direction and axial diction by radialmagnetic bearings 10 and an axialmagnetic bearing 11 and rotationally driven in this state by adrive motor 12. - The
drive motor 12 has a structure constituted by astator 12A and arotor 12B and is provided substantially close to the center of therotor shaft 5. Thestator 12A of thedrive motor 12 is disposed inside thestator column 4, and therotor 12B of thedrive motor 12 is integrally mounted on the outer circumferential surface side of therotor shaft 5. - The radial
magnetic bearings 10 are disposed by one above and below thedrive motor 12, and one axialmagnetic bearing 11 is disposed at the lower end side of therotor shaft 5. - The two radial
magnetic bearings 10 are each constituted by aradial electromagnet target 10A attached to the outer circumferential surface of therotor shaft 5, a plurality ofradial electromagnets 10B disposed on the inner side surface of thestator column 4 opposite thereto, and aradial displacement sensor 10C. Theradial electromagnet target 10A is constituted by a laminated steel plate obtained by laminating steel sheets which are materials with a high magnetic permeability. Theradial magnets 10B attract therotor shaft 5 by a magnetic force in the radial direction through theradial electromagnet target 10A. Theradial displacement sensor 10C detects the radial displacement of therotor shaft 5. By controlling the excitation current of theradial magnets 10B on the basis of the detection value in theradial displacement sensor 10C (radial displacement of the rotor shaft 5), it is possible to support floatably therotor shaft 5 at a predetermined position in the radial direction. - The axial
magnetic bearing 11 is constituted by a disk-shaped armature disk 11A attached to the outer circumference of the lower end portion of therotor shaft 5,axial electromagnets 11B sandwiching thearmature disk 11A from above and below, and anaxial displacement sensor 11C disposed at a position slightly separated from the lower end surface of therotor shaft 5. Thearmature disk 11A is constituted by a material with a high magnetic permeability, and the upper and loweraxial electromagnets 11B attract thearmature disk 11A by magnetic forces from above and below. Theaxial displacement sensor 11C detects the axial displacement of therotor shaft 5. By controlling the excitation current in the upper and loweraxial electromagnets 11B on the basis of the detection value (axial displacement of the rotor shaft 5) in theaxial displacement sensor 11C, it is possible to support floatably therotor shaft 5 by magnetic forces at a predetermined position in the axial direction. - A
rotor 6 is provided as a rotating body of the vacuum pump P outside of thestator column 4. Therotor 6 has a cylindrical shape surrounding the outer circumference of thestator column 4 and has a structure in which two tubular bodies (a firsttubular body 61 and a second tubular body 62) of different diameters are joined in the axial direction thereof, with asupport member 60 of an annular plate shape being interposed therebetween. The support member is positioned in a substantially middle portion to the cylindrical shape. As an example of the joined structure, in the vacuum pump P shown inFIG. 1 , thesupport member 60 is integrally provided at the lower end of the secondtubular body 62, and a ring-shaped protrudingportion 60A is integrally provided at the outer circumferential portion at the rear surface of thesupport member 60. The firsttubular body 61 and the secondtubular body 62 are joined in the axial direction thereof by press fitting and mounting the firsttubular body 61 on the outer circumference of the ring-shaped protrudingportion 60A. - An
end member 63 is provided at the upper end of the secondtubular body 62, and therotor 6 and therotor shaft 5 are integrated, with theend member 63 being interposed therebetween. As an example of such an integrated structure, in the vacuum pump P shown inFIG. 1 , a boss hole 7 is provided in the center of theend member 63 and a step-like shoulder portion (referred to hereinbelow as “rotor shaft shoulder portion 9”) is formed at the outer circumference of the upper end portion of therotor shaft 5. The distal end portion of therotor shaft 5 located above the rotor shaft shoulder portion 9 is inserted into the boss hole 7 of theend member 63, and theend member 63 and the rotor shaft shoulder portion 9 are tightened and fixed by bolts to integrate therotor 6 with therotor shaft 5. - In the vacuum pump P shown in
FIG. 1 , the firsttubular body 61 is formed from a fiber-reinforced plastic such as aramide fiber-reinforced plastic (AFRP), boron fiber-reinforced plastic (BFRP), carbon fiber-reinforced plastic (CFRP), polyethylene fiber reinforced plastic (DFRP), and glass fiber-reinforced plastic (GFRP) in order to reduce the weight of the entire pump and increase the revolution speed of therotor 6. The structural components of the rotor other than the firsttubular body 61, more specifically, the secondtubular body 62,support member 60, and endmember 63, are all formed from a lightweight metal material such as aluminum or an aluminum alloy. - As follows from the explanation above, the vacuum pump P shown in
FIG. 1 uses therotor 6 configured to include the firsttubular body 61 made from a fiber-reinforced plastic, as an example of a rotating body partially constituted by a fiber-reinforced plastic. - The
rotor 6 is supported to be rotatable about the axial center thereof (rotor shaft 5) by the radialmagnetic bearings 10 and the axialmagnetic bearing 11 via therotor shaft 5. Therefore, in the vacuum pump P shown inFIG. 1 , therotor shaft 5, radialmagnetic bearings 10 and axialmagnetic bearing 11 function as support means for supporting therotor 6 so that the rotor could rotate about the axial center thereof. Further, since therotor 6 rotates integrally with therotor shaft 5, thedrive motor 12 rotationally driving therotor shaft 5 functions as drive means for rotationally driving therotor 6. - In the vacuum pump P shown in
FIG. 1 , the zone upstream of the substantially middle portion of the rotor 6 (zone from the substantially middle portion of therotor 6 to the end portion of therotor 6 on thegas intake port 2 side) is configured to function as the vane exhaust portion Pt. The vane exhaust portion Pt is described hereinbelow in greater detail. - A plurality of
rotating vanes 13 are integrally provided at the outer circumferential surface of therotor 6 upstream of the substantially middle portion of the rotor 6 (more specifically, at the outer circumferential surface of the second tubular body 62). The plurality ofrotating vanes 13 is arranged radially about the rotating shaft center (rotor shaft 5) of therotor 6 or the axial center of the outer case 1 (referred to hereinbelow as “pump axial center”). Meanwhile, a plurality of fixedvanes 14 is provided at the inner circumferential surface side of thepump case 1A. Those fixedvanes 14 are disposed radially about the pump axial center. The rotatingvanes 13 and the fixedvanes 14 are disposed alternately in multiple stages along the pump axial center, thereby forming the vane exhaust portion Pt. - All of the
rotating vanes 13 are blade-shaped machined parts obtained by cutting integrally with the outer-diameter machined portion of therotor 6 and are inclined at an angle optimum for exhausting gas molecules. All of the fixedvanes 14 are also inclined at an angle optimum for exhausting gas molecules. - In the vane exhaust portion Pt of the above-descried configuration, the
rotor shaft 5,rotor 6, and plurality ofrotating vanes 13 are integrally rotationally driven when thedrive motor 12 is started, and the rotatingvane 13 of the uppermost stage imparts a momentum in the direction from thegas intake port 2 to thegas exhaust port 3 to the gas molecules that have entered from thegas intake port 2. The gas molecules having such a momentum in the exhaust direction are fed by the fixedvanes 14 to the rotatingvane 13 of the next stage. As a result of the above-described operations of imparting the momentum to the gas molecules and feeding the gas molecules, the gas molecules on thegas intake port 2 side are exhausted so as to travel successively toward the downstream side of therotor 6. - In the vacuum pump P shown in
FIG. 1 , the zone downstream of the substantially middle portion of the rotor 6 (zone from the substantially middle portion of therotor 6 to the end portion of therotor 6 on thegas exhaust port 3 side) is configured to function as the thread groove pump portion Ps. The thread groove pump portion Ps is described hereinbelow in greater detail. - The
rotor 6 downstream of the substantially middle portion of the rotor 6 (more specifically, the portion of the first tubular body 61) rotates as the rotating member of the thread groove pump portion Ps and is configured to be inserted and accommodated between outer and inner double-wall cylindrical thread groovepump portion stators - Among the outer and inner double-wall cylindrical thread groove
pump portion stators pump portion stator 18A is disposed so as to surround the outer circumference of the rotor 6 (portion downstream of the substantially middle portion of the rotor 6), as the fixed member of the vacuum pump P positioned on the outside of therotor 6, and, therefore, is provided so as to face the outer circumferential surface of therotor 6. Further, athread groove 19A with a depth changing to a taper cone shape that reduces in diameter in the downward direction is formed in the inner circumferential portion of the outer thread groovepump portion stator 18A. Thethread groove 19A is cut spirally from the upper end to the lower end of the thread groovepump portion stator 18A, and a spiral thread groove pump flow channel (referred to hereinbelow as “outer thread groove pump flow channel S1”) is formed between therotor 6 and the outer thread groovepump portion stator 18A by thisthread groove 19A. The lower end portion of the outer thread groovepump portion stator 18A is supported by thepump base 1B. - The inner thread groove
pump portion stator 18B is disposed so as to be surrounded by the inner circumference of therotor 6, as the fixed member of the vacuum pump P positioned on the inside of therotor 6, and, therefore, is provided so as to face the inner circumferential surface of therotor 6. Further, athread groove 19B is likewise formed in the outer circumferential portion of the inner thread groovepump portion stator 18B. Thethread groove 19B forms a spiral thread groove pump flow channel (referred to hereinbelow as “inner thread groove pump flow channel S2”) between therotor 6 and the inner thread groovepump portion stator 18B. The lower end portion of the inner thread groovepump portion stator 18B is also supported by thepump base 1B. - The abovementioned outer thread groove pump flow channel S1 or inner thread groove pump flow channel S2 may be also provided by forming the
thread grooves - In the thread groove pump portion Ps, the depth of the
thread groove 19A is set to be the largest at the upstream inlet side of the outer thread groove pump flow channel S1 (passage opening end that is closer to the gas intake port 2) and to be the smallest at the downstream outlet side (passage opening end that is closer to the gas exhaust port 3), so that the gas be transferred, while being compressed, by the drag effect at the outer circumferential surface of thethread groove 19A and therotor 6 or the drag effect at the inner circumferential surface of thethread groove 19B and therotor 6. Thethread groove 19B has a similar depth. - The upstream inlet of the outer thread groove pump flow channel S1 is configured to communicate with a gap (referred to hereinbelow as “last gap G”) between the vane of the lowest stage (the fixed
vane 14 in the example shown inFIG. 1 ), from among the rotatingvanes 13 and the fixedvanes 14 disposed in multiple stages, and the upstream end of the below-described communication opening portion H. The downstream outlet of the same passage S1 is configured to communicate with thegas exhaust port 3 side. The upstream inlet of the inner thread groove pump flow channel S2 is opened toward the inner circumferential surface of therotor 6 in the substantially middle portion of therotor 6, and the downstream outlet of the same passage S2 is configured to merge with the downstream outlet of the outer thread groove pump flow channel S1 and communicate with thegas exhaust port 3. - The communication opening portion H is opened in the substantially middle portion of the
rotor 6. The communication opening portion H is formed so as to pass through from the front surface to the rear surface of thesupport member 60 and, therefore, functions to guide part of the gas present at the outer circumferential side of therotor 6 into the inner thread groove pump flow channel S2. - The gas molecules that have reached the upstream inlet of the outer thread groove pump flow channel S1 and the last gap G due to the transfer induced by the exhaust action of the above-described vane exhaust portion Pt move to the outer thread groove pump flow channel S1, or from the communication opening portion H to the inner thread groove pump flow channel S2. Under the effect generated by the rotation of the
rotor 6, that is, the drag effect at the outer circumferential surface of therotor 6 and thethread groove 19A or the drag effect at the inner circumferential surface of therotor 6 and thethread groove 19B, those gas molecules move toward thegas exhaust port 3, while being compressed from a transitional flow into a viscous flow, and are eventually exhausted to the outside through an auxiliary pump (not shown in the figure). - As shown in
FIG. 2 , therotor 6 has a structure in which a corrosion-resistant layer L1 is provided on the fiber-reinforced plastic portion, which is the base material of the rotor (in the example shown in the figure, the surface of the first tubular body 61), and then a high-emissivity layer L3 with an emissivity higher than that of the corrosion-resistant layer L1 is provided on the corrosion-resistant layer L1. - In the vacuum pump P shown in
FIG. 1 , the corrosion-resistant layer L1, for example from a nickel alloy, protects the surface of the firsttubular member 61, as mentioned hereinabove, as means for protecting the fiber-reinforced plastic portion (in the example shown in the figure, the first tubular body 61) of therotor 6, so that the pump could be used in the environment in which such a corrosive gas that decomposes plastic components is exhausted. - Since the corrosion-resistant layer L1 has a lower emissivity than the fiber-reinforced plastic in the underlying layer, the amount of heat released by emission from the first
tubular body 61 is greatly reduced. The fiber-reinforced plastic forming the firsttubular body 61, which is part of the rotor, is lower in thermal conductivity than aluminum or an alloy thereof, which forms the other portion of therotor 6, and a temperature distribution easily occurs. In particular, where the diameter of the firsttubular body 61 is enlarged and the circumferential speed of the firsttubular body 61 is increased as means for improving the exhaust performance of the vacuum pump P, inside the outer and inner thread groove pump flow channels S1 and S2, the firsttubular body 61 is heated to a comparatively high temperature by the heat (friction heat) generated by the friction with gas that is exhausted in the end portion on thegas exhaust port 3 side where the pressure is high. - However, in the vacuum pump P shown in
FIG. 1 , as explained hereinabove, the corrosion-resistant layer L1 is provided on the first tubular body 61 (fiber-reinforced plastic portion of the rotor 6), and the high-emissivity layer L3 is provided on the corrosion-resistant layer L1, whereby the emissivity of the firsttubular body 61 is increased. Therefore, the heat generated in the firsttubular body 61 is easily released by emission, and inside the outer and inner thread groove pump flow channels S1 and S2, the circumference of the end portion on the exhaust port side of the firsttubular body 61 where the pressure is high can be prevented from being heated by the aforementioned friction heat to a high temperature exceeding the temperature allowed for the fiber-reinforced plastic. - The corrosion-resistant layer L1 on the inner and outer circumferential surfaces of the
rotor 6 is constituted by a first metal coating film with excellent corrosion resistance, such as a nickel alloy film, and formed such as to cover the entire outer circumferential surface of the firsttubular body 61. Further, the high-emissivity layer L3 covering the corrosion-resistant layer L1 forms a second metal coating film L2 from an aluminum alloy or a nickel alloy on the corrosion-resistant layer L1 and is constituted by an oxide film layer obtained by oxidizing the surface of the second metal coating film L2. The high-emissivity layer is formed to cover the entire corrosion-resistant layer L1. - In another embodiment of the high-emissivity layer L3 explained hereinabove, a method can be also considered by which the surface of the first metal coating film (corrosion-resistant layer L1) is oxidized and the resultant oxide film layer is used as the high-emissivity layer L3. However, with such a method, for example, when the corrosion-resistant layer L1 is formed by electroless Ni—P plating, pinholes are formed in the corrosion-resistant layer L1 and the corrosion-resistant layer L1 can be easily damaged and fractured in the vicinity of the pinholes by the oxidation of the corrosion-resistant layer L1 having the pinholes. The resultant problem is that the protective function of the corrosion-resistant layer L1 with respect to the first tubular body 61 (made from the fiber-reinforced plastic) is lost.
- It follows from above, that in the case in which the present vacuum pump P is used in the environment in which such a corrosive gas that decomposes plastic components is exhausted, it is preferred that the high-emissivity layer L3 be formed by the above-described method, that is, by the method in which the corrosion-resistant layer L1 is protected by the second metal coating film L2 by forming the second metal coating film L2 on the corrosion-resistant layer (first metal coating film) L1 and then the surface of the second metal coating film L2 is oxidized.
- The corrosion-resistant layer L1 (first metal coating film) or the second metal coating film L2 explained hereinabove can be formed, for example, by electroplating, electroless plating, or sputtering.
- As another embodiment of the high-emissivity layer L3 provided on the corrosion-resistant layer L1, it is possible to use a DLC film formed by coating diamond-like carbon (DLC) on the corrosion-resistant layer L1 (this configuration is not shown in the figures). Configuration Increasing Emissivity of Fixed Members (Thread Groove
Pump Portion Stators Rotor 6 - In
FIG. 1 , a high-emissivity layer L4 having a higher emissivity than the base material (for example, aluminum or alloys thereof) of the fixed members is provided on the fixed members facing the fiber-reinforced plastic portion (first tubular body 61) of therotor 6, more specifically, on the opposing surfaces of the outer thread groovepump portion stator 18A and the inner thread groovepump portion stator 18B. - Since the
thread grooves pump portion stator 18A and the inner thread groovepump portion stator 18B, the high-emissivity layer L4 provided on the opposing surfaces may form the thread peaks of thethread grooves thread grooves - For example, where the fixed members are formed from aluminum or an alloy thereof, the high-emissivity layer L4 on the opposing surfaces of the fixed members (thread groove
pump portion stators - As another embodiment of the high-emissivity layer L4, a coating film layer obtained by coating the surface of the fixed members with a material having a higher emissivity than aluminum or an alloy thereof, which is the base material of the fixed members (thread groove
pump portion stators - In the vacuum pump P shown in
FIG. 1 , the thread groovepump portion stators pump portion stators rotor 6 by emission is low. However, in the vacuum pump P shown inFIG. 1 , this ability is improved by the high-emissivity layer L4. Therefore, the thread groovepump portion stators rotor 6 by emission and the received heat can be guided out to the outside. Therefore, the amount of heat accumulated in the fiber-reinforced plastic portion (first tubular body 61) of therotor 6 is reduced and the temperature of the fiber-reinforced plastic portion (first tubular body 61) of therotor 6 can be effectively prevented from rising and exceeding the temperature allowed for the fiber-reinforced plastic under the effect of the heat (friction heat) generated by the friction between the exhausted gas and therotor 6. - In the above-described section relating to the configuration increasing the emissivity of the rotor 6 (rotating body of the vacuum pump P), a specific example is described in which the feature of providing the corrosion-resistant layer L1 on the fiber-reinforced plastic portion (first tubular body 61) and providing the high-emissivity layer L3 on the corrosion-resistant layer L1 is applied to the case in which the vacuum pump P shown in
FIG. 1 is used in the environment in which such a corrosive gas that decomposes plastic components is exhausted. Therefore, where the vacuum pump P shown inFIG. 1 is used in the environment in which non-aggressive gas is exhausted, the corrosion-resistant layer L1, from among the components of the above-described configuration, may be omitted as shown inFIG. 3 . Further, since the emissivity of the fiber-reinforced plastic used for forming the firsttubular body 61 of therotor 6 is higher than that of aluminum or an alloy thereof that is used for forming structural components (secondtubular body 62,support member 60, and end member 63) of the rotor other than the firsttubular body 61, the high-emissivity layer L3 and also the second metal coating film L2, from among the components of the above-described configuration, may be omitted as shown inFIG. 3 . - Essentially, where the vacuum pump P shown in
FIG. 1 is used in the environment in which non-aggressive gas is exhausted, only a high-emissivity layer L4 having a higher emissivity than aluminum or an alloy thereof, which is the base material of the thread groovepump portion stators pump portion stators rotor 6, more specifically on the opposing surfaces of the thread groovepump portion stators FIG. 3 ). With such a configuration, the heat released by emission from the fiber-reinforced plastic portion of therotor 6 can be efficiently received by the high-emissivity layers of the thread groovepump portion stators rotor 6 is reduced and the temperature of the fiber-reinforced plastic portion (first tubular body 61) of therotor 6 can be effectively prevented from rising and exceeding the temperature allowed for the fiber-reinforced plastic under the effect of the heat (friction heat) generated by the friction between the exhausted gas and therotor 6. - The embodiment explained hereinabove is an example in which the present invention is applied to a structure in which part (more specifically, the portion of the first tubular body 61) of the
rotor 6, which is the rotating body of the vacuum pump P, is constituted by a fiber-reinforced plastic, but the present invention is not limited to this example and can be also applied to a structure in which the entire rotor 6 (including the rotating vanes 13) is constituted by a fiber-reinforced plastic. - Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are disclosed as example forms of implementing the claims.
Claims (6)
1. A rotating body of a vacuum pump that is entirely or partially constituted by a fiber-reinforced plastic and exhausts gas by rotation, wherein
the rotating body is provided with a corrosion-resistant layer on a fiber-reinforced plastic portion, which is a base material thereof, and with a high-emissivity layer having a higher emissivity than the corrosion-resistant layer on the corrosion-resistant layer.
2. The rotating body of a vacuum pump according to claim 1 , wherein
the high-emissivity layer is an oxide film layer obtained by oxidizing a surface of a metal coating film formed on the corrosion-resistant layer, or a DLC layer formed by performing DLC coating treatment on the corrosion-resistant layer.
3. A fixed member of a vacuum pump that faces an inner circumferential surface or outer circumferential surface of a rotating body of the vacuum pump, which is entirely or partially constituted by a fiber-reinforced plastic, the fixed member forming, between the fixed member and the rotating body, a spiral thread groove exhaust flow channel for exhausting gas, wherein
a high-emissivity layer having a higher emissivity than a base material of the fixed member is provided on a surface of the fixed member that faces a fiber-reinforced plastic portion of the rotating body.
4. A fixed member disposed opposite the rotating body of a vacuum pump according to claim 3 , wherein
the high-emissivity layer is an oxide film layer obtained by oxidizing a surface of an aluminum alloy which is a base material of the fixed member, or a coating film layer formed by coating the surface of the fixed member with a material having a higher emissivity than the aluminum alloy of the base material.
5. A vacuum pump comprising the rotating body according to claim 1 .
6. A vacuum pump comprising the fixed member according to claim 3 .
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011022923 | 2011-02-04 | ||
JP2011-022923 | 2011-02-04 | ||
PCT/JP2011/077301 WO2012105116A1 (en) | 2011-02-04 | 2011-11-28 | Rotating body of vacuum pump, fixed member placed to be opposed to same, and vacuum pump provided with them |
Publications (1)
Publication Number | Publication Date |
---|---|
US20130309076A1 true US20130309076A1 (en) | 2013-11-21 |
Family
ID=46602348
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/982,412 Abandoned US20130309076A1 (en) | 2011-02-04 | 2011-11-28 | Rotating Body of Vacuum Pump, Fixed Member Disposed Opposite Rotating Body, and Vacuum Pump Provided with Rotating Body and Fixed Member |
Country Status (3)
Country | Link |
---|---|
US (1) | US20130309076A1 (en) |
CN (1) | CN103299083A (en) |
WO (1) | WO2012105116A1 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20130183185A1 (en) * | 2012-01-12 | 2013-07-18 | Vacuubrand Gmbh + Co Kg | Screw rotor for a screw type vacuum pump |
US20140294565A1 (en) * | 2011-11-30 | 2014-10-02 | Arisawa Mfg. Co., Ltd. | Vacuum pump |
US20150275914A1 (en) * | 2014-03-28 | 2015-10-01 | Shimadzu Corporation | Vacuum pump |
US20160290343A1 (en) * | 2013-11-12 | 2016-10-06 | Oerlikon Leybold Vacuum Gmbh | Rotor device for a vacuum pump, and vacuum pump |
CN112867867A (en) * | 2018-10-31 | 2021-05-28 | 埃地沃兹日本有限公司 | Vacuum pump and vacuum pump component |
US11255220B1 (en) * | 2019-10-02 | 2022-02-22 | Battelle Memorial Institute | Heating assemblies, heat exchange assemblies, methods for providing and/or exchanging heat, turbine combustion engines, and methods for powering turbine combustion engines |
US20240295221A1 (en) * | 2021-01-18 | 2024-09-05 | Edwards Japan Limited | Vacuum pump and rotating body thereof |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014203172A1 (en) | 2014-02-21 | 2015-08-27 | Oerlikon Leybold Vacuum Gmbh | Coated CFRP surfaces of turbomolecular pumps |
JP6758865B2 (en) * | 2016-03-04 | 2020-09-23 | エドワーズ株式会社 | Vacuum pump |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070148462A1 (en) * | 2005-12-22 | 2007-06-28 | Hon Hai Precision Industry Co., Ltd. | Article having diamond-like carbon composite film and method for manufacturing the same |
US7572096B2 (en) * | 2004-05-10 | 2009-08-11 | Boc Edwards Japan Limited | Vacuum pump |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3792318B2 (en) * | 1996-10-18 | 2006-07-05 | 株式会社大阪真空機器製作所 | Vacuum pump |
JP2000161286A (en) * | 1998-11-25 | 2000-06-13 | Shimadzu Corp | Turbo molecular pump |
JP2003254285A (en) * | 2002-02-28 | 2003-09-10 | Boc Edwards Technologies Ltd | Pump device |
JP2005155403A (en) * | 2003-11-25 | 2005-06-16 | Boc Edwards Kk | Vacuum pump |
JP2006046074A (en) * | 2004-07-30 | 2006-02-16 | Boc Edwards Kk | Vacuum pump |
JP2006233978A (en) * | 2006-06-05 | 2006-09-07 | Mitsubishi Heavy Ind Ltd | Turbo-molecular pump |
-
2011
- 2011-11-28 WO PCT/JP2011/077301 patent/WO2012105116A1/en active Application Filing
- 2011-11-28 CN CN2011800654999A patent/CN103299083A/en active Pending
- 2011-11-28 US US13/982,412 patent/US20130309076A1/en not_active Abandoned
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7572096B2 (en) * | 2004-05-10 | 2009-08-11 | Boc Edwards Japan Limited | Vacuum pump |
US20070148462A1 (en) * | 2005-12-22 | 2007-06-28 | Hon Hai Precision Industry Co., Ltd. | Article having diamond-like carbon composite film and method for manufacturing the same |
Non-Patent Citations (1)
Title |
---|
Masashi, JPH10122179, 12-5-98, english translation of the description * |
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140294565A1 (en) * | 2011-11-30 | 2014-10-02 | Arisawa Mfg. Co., Ltd. | Vacuum pump |
US9835170B2 (en) * | 2011-11-30 | 2017-12-05 | Edwards Japan Limited | Vacuum pump with fiber-reinforced resin cylinder |
US20130183185A1 (en) * | 2012-01-12 | 2013-07-18 | Vacuubrand Gmbh + Co Kg | Screw rotor for a screw type vacuum pump |
US20160290343A1 (en) * | 2013-11-12 | 2016-10-06 | Oerlikon Leybold Vacuum Gmbh | Rotor device for a vacuum pump, and vacuum pump |
US20150275914A1 (en) * | 2014-03-28 | 2015-10-01 | Shimadzu Corporation | Vacuum pump |
US10253778B2 (en) * | 2014-03-28 | 2019-04-09 | Shimadzu Corporation | Vacuum pump |
CN112867867A (en) * | 2018-10-31 | 2021-05-28 | 埃地沃兹日本有限公司 | Vacuum pump and vacuum pump component |
US20210388840A1 (en) * | 2018-10-31 | 2021-12-16 | Edwards Japan Limited | Vacuum pump and vacuum pump component |
US12044241B2 (en) * | 2018-10-31 | 2024-07-23 | Edwards Japan Limited | Vacuum pump and vacuum pump component |
US11255220B1 (en) * | 2019-10-02 | 2022-02-22 | Battelle Memorial Institute | Heating assemblies, heat exchange assemblies, methods for providing and/or exchanging heat, turbine combustion engines, and methods for powering turbine combustion engines |
US20240295221A1 (en) * | 2021-01-18 | 2024-09-05 | Edwards Japan Limited | Vacuum pump and rotating body thereof |
US12270405B2 (en) * | 2021-01-18 | 2025-04-08 | Edwards Japan Limited | Vacuum pump and rotating body thereof |
Also Published As
Publication number | Publication date |
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CN103299083A (en) | 2013-09-11 |
WO2012105116A1 (en) | 2012-08-09 |
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