US20030021672A1 - Vacuum pump - Google Patents
Vacuum pump Download PDFInfo
- Publication number
- US20030021672A1 US20030021672A1 US10/187,566 US18756602A US2003021672A1 US 20030021672 A1 US20030021672 A1 US 20030021672A1 US 18756602 A US18756602 A US 18756602A US 2003021672 A1 US2003021672 A1 US 2003021672A1
- Authority
- US
- United States
- Prior art keywords
- rotor
- circumferential surface
- pump case
- outer circumferential
- vacuum pump
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000005260 corrosion Methods 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims abstract description 30
- 229920005989 resin Polymers 0.000 claims abstract description 18
- 239000011347 resin Substances 0.000 claims abstract description 18
- 229920001187 thermosetting polymer Polymers 0.000 claims abstract description 16
- 238000005520 cutting process Methods 0.000 claims description 13
- 230000007797 corrosion Effects 0.000 abstract description 13
- 230000006378 damage Effects 0.000 abstract description 10
- 230000008021 deposition Effects 0.000 abstract description 6
- 239000010408 film Substances 0.000 description 24
- 229910000838 Al alloy Inorganic materials 0.000 description 16
- 239000007789 gas Substances 0.000 description 11
- 238000004519 manufacturing process Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 8
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 239000004065 semiconductor Substances 0.000 description 6
- 230000000694 effects Effects 0.000 description 5
- 238000007747 plating Methods 0.000 description 5
- 238000005536 corrosion prevention Methods 0.000 description 4
- 238000005336 cracking Methods 0.000 description 3
- BHEPBYXIRTUNPN-UHFFFAOYSA-N hydridophosphorus(.) (triplet) Chemical compound [PH] BHEPBYXIRTUNPN-UHFFFAOYSA-N 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 2
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 229910052801 chlorine Inorganic materials 0.000 description 2
- 239000000460 chlorine Substances 0.000 description 2
- YNAAFGQNGMFIHH-UHFFFAOYSA-N ctk8g8788 Chemical compound [S]F YNAAFGQNGMFIHH-UHFFFAOYSA-N 0.000 description 2
- 239000003822 epoxy resin Substances 0.000 description 2
- 239000011737 fluorine Substances 0.000 description 2
- 229910052731 fluorine Inorganic materials 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229920000647 polyepoxide Polymers 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 239000010409 thin film Substances 0.000 description 2
- 238000003483 aging Methods 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000001312 dry etching Methods 0.000 description 1
- 238000001035 drying Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 238000005211 surface analysis Methods 0.000 description 1
Images
Classifications
-
- 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
-
- 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
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/662—Balancing of rotors
-
- 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
-
- 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
-
- 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
- F05D2300/44—Resins
-
- 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 vacuum pump used for a semiconductor manufacturing apparatus, an electron microscope, a surface analysis apparatus, a mass spectrometer, a particle accelerator, an experimental fusion apparatus, or the like.
- the invention relates to a vacuum pump in which anti-corrosive processing is necessary, like one used in a semiconductor manufacturing apparatus.
- a vacuum pump such as a turbo molecular pump is used as means for exhausting gas within a processing chamber, for forming a given high vacuum degree.
- a rotational body of this type of vacuum pump is normally formed of an aluminum alloy.
- an anti-corrosive processing is performed in which the surface of a rotational body made from an aluminum alloy is coated with an anti-corrosive prevention film such as a nickel phosphorous alloy plating.
- the aluminum alloy of the rotational body itself is exposed in the portion cut off for balancing, and if debris or the like generated by etching a wafer surface in a semiconductor manufacturing process is mixed into the inside of the vacuum pump, then the debris will adhere to the surface of the aluminum in the cut off portion, and will be deposited as a product.
- the debris will be easily deposited on the surface of the deposited product, and if chain deposition of the product on the surface of the rotational body progresses in this manner, then the clearance between the fixed side of the vacuum pump and the rotational body will become smaller. Accordingly, there is a concern that the fixed side will have critical damage when the product deposited on the rotating body contacts the fixed side.
- an object of the present invention is to provide a vacuum pump in which destruction of a rotational body due to corrosion can be prevented, and in which the deposition of the product is reduced, preventing damage due to contact between the rotational body and a fixed side.
- a vacuum pump is provided with: a pump case having a gas inlet port opened in its top surface; a rotor shaft rotatably supported within the pump case; a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed with in the pump case; a plurality of stator blades fixed with in the pump case and positioned alternately with the plurality of rotor blades; a driving motor for rotating the rotor shaft; an anti-corrosive film layer formed on a surface of the rotor; and a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor, the vacuum pump being characterized in that anti-corrosion process is performed on the balancing hole.
- the anti-corrosion process employed here means a process in which a thermosetting resin film layer is formed on a surface of the balancing hole.
- Synthetic resins having superior heat resistance characteristics and superior anti-corrosion characteristics such as epoxy resins and fluorine resins, for example, can be used as the thermosetting resin.
- a vacuum pump is provided with: a pump case having a gas inlet port opened in its top surface; a rotor shaft rotatably supported within the pump case; a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed within the pump case; a plurality of stator blades fixed within the pump case and positioned alternately with the plurality of rotor blades; a driving motor for rotating the rotor shaft; and a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor; the vacuum pump being characterized in that an anti-corrosive film layer is formed on a surface of the rotor.
- FIG. 1 is a vertical cross sectional diagram showing the structure of a first embodiment of a vacuum pump according to the present invention.
- FIG. 2 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram for explaining an example of forming balancing holes in a rotor using a cutting tool.
- FIG. 3 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram showing a state after performing anti-corrosion process to the rotor balancing holes.
- FIG. 4 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram showing a second embodiment of an anti-corrosion process performed on the rotor balancing holes.
- FIG. 1 is a vertical cross sectional diagram showing the structure of a first embodiment of a vacuum pump according to the present invention.
- a vacuum pump P of this embodiment is roughly structured from a pump case 1 composed of a cylindrical portion 1 - 1 and a base 1 - 2 attached to a lower end of the cylindrical portion 1 - 1 , and a pump mechanism portion housed in the pump case 1 .
- An upper surface of the pump case 1 is opened, serving as a gas inlet port 2 , and a not shown vacuum container, such as a process chamber, is screwed into the gas inlet port 2 and fixed with a bolt, and an exhaust pipe that serves as a gas exhaust port 3 is formed in one side surface of a lower portion of the pump case 1 .
- a lower base of the pump case 1 is covered by a rear cover 1 - 3 , and a stator column 4 is disposed above the rear cover 1 - 3 in a standing manner toward an inside portion of the pump case 1 and is screwed into and fixed to the base 1 - 2 .
- a rotor shaft 5 is bearing-supported in the radial direction and in the axial direction by a radial direction electromagnet 6 - 1 and an axial direction electromagnet 6 - 2 , respectively, which are formed in an inside portion of the stator column 4 so that the rotor 5 passing through between both ends of the stator column 4 is able to rotate.
- reference numeral 7 denotes a ball bearing to which a dry lubricant has been applied. The ball bearing 7 protects the rotor shaft 5 and the electromagnets 6 - 1 and 6 - 2 from contacting and supports the rotor shaft 5 when an electric power source for the magnetic bearings fails, the electromagnets not being in contact with the rotor shaft 5 during normal operation.
- a rotor 8 formed in a cylindrical shape is disposed in the inside portion of the pump case 1 so as to surround the stator column 4 , an upper end of the rotor 8 extends to the vicinity of the gas inlet port 2 , and is fixed to the rotor shaft 5 by screwing with a bolt.
- a driving motor 9 composed of a high frequency motor or the like is provided between the rotor shaft 5 and the stator column 4 , and the rotor shaft 5 and the rotor 8 are rotated at high speed by the driving motor 9 .
- the pump mechanism portion of the vacuum pump P of this embodiment is housed within the pump case 1 and employs a composite type pump mechanism composed of turbo molecular pump mechanism portion P A of upper half, and thread groove pump mechanism portion P B of lower half, which are defined between an outer circumferential surface of the rotor 8 and an inner circumferential surface of the pump case 1 .
- the turbo molecular pump mechanism portion P A is structured by rotator blades 10 that rotate at high speed and static stator blades 11 that are fixed.
- a plurality of processed blade shape rotor blades 10 , 10 , . . . are formed on the outer circumferential surface of the upper half of the rotor 8 from the gas inlet port 2 side in a direction to a central rotation axis L of the rotor 8 .
- a plurality of stator blades 11 , 11 , . . . disposed alternately between the plurality of rotor blades 10 , 10 , . . . are formed on the inner circumferential surface of the upper half of the pump case 1 , and are fixed through spacers 12 , 12 , . . .
- the thread groove pump mechanism portion P B is structured by a cylindrical surface 8 a of the rotor 8 rotating at high speed and a static thread groove 13 .
- the outer circumferential surface of the lower half of the rotor 8 serves as the flat cylindrical surface 8 a
- a cylindrical screw stator 14 is disposed so as to oppose the cylindrical surface 8 a of the rotor 8 with a narrow gap.
- the thread groove 13 is carved in the screw stator 14 .
- the thread groove 13 can be carved in the outer circumferential surface of the lower half of the rotor 8 .
- an opposing surface of the screw stator 14 provided on the inner circumference of the lower half of the pump case 1 , to the rotor 8 can be formed in the flat cylindrical surface.
- the vacuum pump P of this embodiment is used under a severe environment exposed to corrosive chlorine and fluorine sulfide gasses during semiconductor manufacturing processes, an anti-corrosive process is performed as shown in FIG. 2 for forming an even coating of an anti-corrosive film layer 15 by means of a plating, such as a nickel phosphorous oxide plating, at a thickness on the order of 10 to 20 ⁇ m on the outer circumferential surface 8 a and the inner circumferential surface 8 b of the rotor 8 , which is formed by an aluminum alloy or the like.
- a plating such as a nickel phosphorous oxide plating
- the stator blades 11 and the screw stator 14 fixed to the cylindrical portion 1 - 1 of the pump case 1 may be temporarily removed, and as shown in FIG. 2, balancing holes 16 , 16 , . . .
- the balancing holes 16 may be formed by partially cutting off the surface of the anti-corrosive film layer 15 formed in the outer circumferential surface 8 a or the inner circumferential surface 8 b of the rotor 8 using a cutting tool 20 such as a drill or a router; changing the mass of the rotor 8 and performing fine adjustments of the balance of the rotational body; and then an anti-corrosion process is performed on the surface of the balancing holes 16 .
- the surface of the balancing holes 16 after performing the rotational body balancing is in a state in which a portion of the aluminum alloy of main body of the rotor 8 is exposed because a portion of the anti-corrosive film layer 15 coated on the surface of the outer circumferential surface 8 a and the inner circumferential surface 8 b of the rotor 8 is cut off, as shown in FIG. 2.
- thermosetting resin film layer 17 having superior heat resistance characteristics and superior anti-corrosion characteristics, such as an epoxy resin, a fluorine resin, or the like is formed on the surface of the balancing holes 16 , as shown in FIG. 3.
- thermosetting resin has good adhesive characteristics with respect to metallic materials and has strong adhesive force with respect to curved surfaces like the inner circumferential surface 8 b and the outer circumferential surface 8 a of the rotor 8 , and therefore peeling due to centrifugal force of the rotational body will not occur. Further, the thermosetting resin has superior oxygen barrier characteristics, and therefore anti-corrosion process can be performed by a relatively simple method of only forming the thermosetting resin film layer 17 on the surface of the balancing holes 16 .
- thermosetting resin film layer 17 As a method of forming the thermosetting resin film layer 17 , a known spray application process using a spray gun or the like, followed by age hardening by the rotor 8 at room temperature or a required temperature may be employed, whereby conducting a uniform application at least on the surface of the aluminum alloy of the balancing holes 16 at a thickness of 10 to 20 ⁇ m.
- thermosetting resin film layer 17 is formed into a thick film, anti-corrosion performance can be increased, and corrosion of the balancing holes 16 can be prevented over a long period of time.
- the gap between the outer circumferential surface 8 a of the rotor 8 and the screw stator 14 becomes narrower, the rotational body and the fixed side of the vacuum pump come into contact, and the fixed side is damaged, the aforementioned film thickness range is appropriate.
- the weight of the thermosetting resin film layer 17 after hardening and drying is set on the order of 1 to 10 mg with respect to the number of balancing holes 16 , and considering the increase in weight due to the thermosetting resin film layer 17 , it is necessary to form the synthetic resin film layer 17 after performing a little excess amount of material cutting for balancing.
- the aluminum alloy surface of the balancing holes 16 formed in the surface of the outer circumferential surface 8 a or the inner circumferential surface 8 b of the rotor 8 is covered by the thermosetting resin film layer 17 as an anti-corrosion process, and therefore corrosion due to a corrosive gas does not develop in the aluminum alloy surface of the balancing holes 16 , stress corrosion cracking of the balancing holes due to high speed rotation of the rotational body can be prevented, and rotor destruction due to corrosion can be prevented from happening.
- thermosetting resin film layer 17 can be formed on the aluminum alloy surface of the balancing holes 16 b into a thin film as an anti-corrosion process, and deposition of the product adhering to the aluminum alloy can be reduced, and therefore damage due to contact between the rotational body and the fixed side can be prevented.
- the basic structure of the vacuum pump in this second embodiment is similar to the vacuum pump shown in FIG. 1, and therefore identical reference numerals are attached to identical portions, and a detailed explanation of those portions is omitted.
- the vacuum pump in this second embodiment is characterized in that the balancing holes 16 are formed by removing a portion of the inner circumferential surface 8 b or the outer circumferential surface 8 a of the rotor 8 , and in that the corrosion prevention layer 15 is formed on the inner circumferential surface 8 b and the outer circumferential surface 8 a of the rotor 8 , as shown in FIG. 4.
- a portion of the outer circumferential surface 8 a or the inner circumferential surface 8 b of the rotor 8 formed by the aluminum alloy or the like is removed by using the cutting tool 20 such as a drill or a router, changing the mass of the rotor 8 and performing fine adjustments of the balance of the rotational body, after which the corrosion prevention film layer 15 is uniformly coated to a thickness on the order of 10 to 20 ⁇ m by plating a nickel phosphorous alloy plating or the like, performing anti-corrosion process at the same time to the rotor 8 and to the balancing holes 16 .
- the process step for forming the thermosetting resin film layer 17 for anti-corrosion process of the balancing holes 16 can be omitted, anti-corrosion process of the balancing holes 16 can be simplified, and the manufacturing costs of the vacuum pump relating to anti-corrosion process can be lowered.
- the corrosion prevention film layer 15 is formed uniformly over the entire surface of the rotor 8 after performing balancing as stated above, and therefore it is not necessary to remove an excess amount of material in order to adjust the balance.
- thermosetting resin film layer can be formed as a thin film on the aluminum alloy surface of the balancing holes for the heat resistance process, and deposition of the product adhering to the aluminum alloy can be reduced, and therefore damage due to contact between the rotational body and the fixed side can be prevented.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Non-Positive Displacement Air Blowers (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
To provide a vacuum pump in which destruction of a rotational body due to corrosion can be prevented, and in which deposition of product is reduced, preventing damage due to contact between the rotational body and a fixed side. The pump case having the gas inlet port opened on its upper surface, the rotor shaft supported within the pump case such that it is capable of rotating, the plurality of the rotor blades formed in the outer circumferential surface of the rotor that is fixed to the rotor shaft, the plurality of the stator blades fixed within the pump case, positioned alternately with the plurality of the rotor blades, and the driving motor for rotating the rotor shaft are provided. The corrosion preventing film layer is formed on the inner circumferential surface and the outer circumferential surface of the rotor, and the balancing holes are formed by removing a portion of the inner circumferential surface or the outer circumferential surface of the rotor, and the thermosetting resin film layer is formed on the surface of the balancing holes as an anti-corrosion process.
Description
- 1. Field of the Invention
- The present invention relates to a vacuum pump used for a semiconductor manufacturing apparatus, an electron microscope, a surface analysis apparatus, a mass spectrometer, a particle accelerator, an experimental fusion apparatus, or the like. In particular, the invention relates to a vacuum pump in which anti-corrosive processing is necessary, like one used in a semiconductor manufacturing apparatus.
- 2. Description of the Related Art
- Conventionally, in a process step performing a processing within a high vacuum chamber, such as a process step of dry etching or CVD in a semiconductor manufacturing process, a vacuum pump such as a turbo molecular pump is used as means for exhausting gas within a processing chamber, for forming a given high vacuum degree.
- A rotational body of this type of vacuum pump is normally formed of an aluminum alloy. However, in case of a vacuum pump that is used under such a severe environment as a semiconductor manufacturing process, in which the vacuum pump is exposed to corrosive chlorine and fluorine sulfide gasses, an anti-corrosive processing is performed in which the surface of a rotational body made from an aluminum alloy is coated with an anti-corrosive prevention film such as a nickel phosphorous alloy plating.
- On the other hand, in vacuum pumps having a rotational body as stated above, it becomes necessary to perform balancing of the rotational body during high speed rotation at the pump assembly stage of manufacturing. As a balancing method, a method is generally known in which the mass of the rotational body is changed by partially cutting off the outer circumferential surface or the inner circumferential surface of the rotational body by using a cutting tool such as a drill or a router, thus performing fine adjustments of the balance.
- However, balancing is performed by cutting in the above-stated manner after conducting the anti-corrosion process, and a portion of the anti-corrosive film coated on the surface of the rotational body is removed by the cutting tool such as a drill or a router. Therefore, corrosion develops in a cut off portion where the aluminum alloy of the rotational body itself is exposed due to a corrosive gas, stress corrosion cracks progress in the cut off portion due to high speed rotation of the rotational body, and in the worst case, this may lead to destruction of the rotational body, affecting the outside of the vacuum pump as well.
- Further, as stated above, the aluminum alloy of the rotational body itself is exposed in the portion cut off for balancing, and if debris or the like generated by etching a wafer surface in a semiconductor manufacturing process is mixed into the inside of the vacuum pump, then the debris will adhere to the surface of the aluminum in the cut off portion, and will be deposited as a product.
- In particular, the debris will be easily deposited on the surface of the deposited product, and if chain deposition of the product on the surface of the rotational body progresses in this manner, then the clearance between the fixed side of the vacuum pump and the rotational body will become smaller. Accordingly, there is a concern that the fixed side will have critical damage when the product deposited on the rotating body contacts the fixed side.
- In view of the aforementioned matters in dispute, an object of the present invention is to provide a vacuum pump in which destruction of a rotational body due to corrosion can be prevented, and in which the deposition of the product is reduced, preventing damage due to contact between the rotational body and a fixed side.
- In order to achieve the aforementioned objective, a vacuum pump according to the present invention is provided with: a pump case having a gas inlet port opened in its top surface; a rotor shaft rotatably supported within the pump case; a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed with in the pump case; a plurality of stator blades fixed with in the pump case and positioned alternately with the plurality of rotor blades; a driving motor for rotating the rotor shaft; an anti-corrosive film layer formed on a surface of the rotor; and a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor, the vacuum pump being characterized in that anti-corrosion process is performed on the balancing hole.
- The anti-corrosion process employed here means a process in which a thermosetting resin film layer is formed on a surface of the balancing hole. Synthetic resins having superior heat resistance characteristics and superior anti-corrosion characteristics, such as epoxy resins and fluorine resins, for example, can be used as the thermosetting resin.
- Further, a vacuum pump according to the present invention is provided with: a pump case having a gas inlet port opened in its top surface; a rotor shaft rotatably supported within the pump case; a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed within the pump case; a plurality of stator blades fixed within the pump case and positioned alternately with the plurality of rotor blades; a driving motor for rotating the rotor shaft; and a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor; the vacuum pump being characterized in that an anti-corrosive film layer is formed on a surface of the rotor.
- FIG. 1 is a vertical cross sectional diagram showing the structure of a first embodiment of a vacuum pump according to the present invention.
- FIG. 2 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram for explaining an example of forming balancing holes in a rotor using a cutting tool.
- FIG. 3 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram showing a state after performing anti-corrosion process to the rotor balancing holes.
- FIG. 4 is a blow-up cross sectional diagram of necessary portions of the vacuum pump shown in FIG. 1, and is a diagram showing a second embodiment of an anti-corrosion process performed on the rotor balancing holes.
- An embodiment of the present invention is explained in detail below with reference to the attached drawings.
- FIG. 1 is a vertical cross sectional diagram showing the structure of a first embodiment of a vacuum pump according to the present invention.
- As shown in FIG. 1, a vacuum pump P of this embodiment is roughly structured from a pump case 1 composed of a cylindrical portion 1-1 and a base 1-2 attached to a lower end of the cylindrical portion 1-1, and a pump mechanism portion housed in the pump case 1.
- An upper surface of the pump case 1 is opened, serving as a
gas inlet port 2, and a not shown vacuum container, such as a process chamber, is screwed into thegas inlet port 2 and fixed with a bolt, and an exhaust pipe that serves as agas exhaust port 3 is formed in one side surface of a lower portion of the pump case 1. - A lower base of the pump case 1 is covered by a rear cover 1-3, and a
stator column 4 is disposed above the rear cover 1-3 in a standing manner toward an inside portion of the pump case 1 and is screwed into and fixed to the base 1-2. - A
rotor shaft 5 is bearing-supported in the radial direction and in the axial direction by a radial direction electromagnet 6-1 and an axial direction electromagnet 6-2, respectively, which are formed in an inside portion of thestator column 4 so that therotor 5 passing through between both ends of thestator column 4 is able to rotate. Note thatreference numeral 7 denotes a ball bearing to which a dry lubricant has been applied. The ball bearing 7 protects therotor shaft 5 and the electromagnets 6-1 and 6-2 from contacting and supports therotor shaft 5 when an electric power source for the magnetic bearings fails, the electromagnets not being in contact with therotor shaft 5 during normal operation. - A
rotor 8 formed in a cylindrical shape is disposed in the inside portion of the pump case 1 so as to surround thestator column 4, an upper end of therotor 8 extends to the vicinity of thegas inlet port 2, and is fixed to therotor shaft 5 by screwing with a bolt. - In a nearly center portion of the
rotor shaft 5 in the axial direction, a drivingmotor 9 composed of a high frequency motor or the like is provided between therotor shaft 5 and thestator column 4, and therotor shaft 5 and therotor 8 are rotated at high speed by thedriving motor 9. - Further, the pump mechanism portion of the vacuum pump P of this embodiment is housed within the pump case 1 and employs a composite type pump mechanism composed of turbo molecular pump mechanism portion PA of upper half, and thread groove pump mechanism portion PB of lower half, which are defined between an outer circumferential surface of the
rotor 8 and an inner circumferential surface of the pump case 1. - The turbo molecular pump mechanism portion P A is structured by
rotator blades 10 that rotate at high speed andstatic stator blades 11 that are fixed. - That is, a plurality of processed blade
10, 10, . . . are formed on the outer circumferential surface of the upper half of theshape rotor blades rotor 8 from thegas inlet port 2 side in a direction to a central rotation axis L of therotor 8. A plurality of 11, 11, . . . disposed alternately between the plurality ofstator blades 10, 10, . . . are formed on the inner circumferential surface of the upper half of the pump case 1, and are fixed throughrotor blades 12, 12, . . .spacers - On the other hand, the thread groove pump mechanism portion P B is structured by a
cylindrical surface 8 a of therotor 8 rotating at high speed and astatic thread groove 13. - That is, the outer circumferential surface of the lower half of the
rotor 8 serves as the flatcylindrical surface 8 a, and in the inner circumferential surface of the lower half of the pump case 1 acylindrical screw stator 14 is disposed so as to oppose thecylindrical surface 8 a of therotor 8 with a narrow gap. Thethread groove 13 is carved in thescrew stator 14. - Note that the
thread groove 13 can be carved in the outer circumferential surface of the lower half of therotor 8. Also, an opposing surface of thescrew stator 14 provided on the inner circumference of the lower half of the pump case 1, to therotor 8 can be formed in the flat cylindrical surface. - Incidentally, the vacuum pump P of this embodiment is used under a severe environment exposed to corrosive chlorine and fluorine sulfide gasses during semiconductor manufacturing processes, an anti-corrosive process is performed as shown in FIG. 2 for forming an even coating of an
anti-corrosive film layer 15 by means of a plating, such as a nickel phosphorous oxide plating, at a thickness on the order of 10 to 20 μm on the outercircumferential surface 8 a and the innercircumferential surface 8 b of therotor 8, which is formed by an aluminum alloy or the like. - Further, the following may be performed as means for performing balancing of the rotational body composed of the
rotor shaft 5, therotor 8, and therotor blades 10 during high speed rotation: thestator blades 11 and thescrew stator 14 fixed to the cylindrical portion 1-1 of the pump case 1 may be temporarily removed, and as shown in FIG. 2, balancing 16, 16, . . . may be formed by partially cutting off the surface of theholes anti-corrosive film layer 15 formed in the outercircumferential surface 8a or the innercircumferential surface 8 b of therotor 8 using acutting tool 20 such as a drill or a router; changing the mass of therotor 8 and performing fine adjustments of the balance of the rotational body; and then an anti-corrosion process is performed on the surface of thebalancing holes 16. - The surface of the
balancing holes 16 after performing the rotational body balancing is in a state in which a portion of the aluminum alloy of main body of therotor 8 is exposed because a portion of theanti-corrosive film layer 15 coated on the surface of the outercircumferential surface 8 a and the innercircumferential surface 8 b of therotor 8 is cut off, as shown in FIG. 2. - Therefore, in order to prevent stress corrosion cracking of, and deposition of the product on the surface of the aluminum alloy of the
balancing holes 16, a thermosettingresin film layer 17 having superior heat resistance characteristics and superior anti-corrosion characteristics, such as an epoxy resin, a fluorine resin, or the like is formed on the surface of thebalancing holes 16, as shown in FIG. 3. - The aforementioned thermosetting resin has good adhesive characteristics with respect to metallic materials and has strong adhesive force with respect to curved surfaces like the inner
circumferential surface 8 b and the outercircumferential surface 8 a of therotor 8, and therefore peeling due to centrifugal force of the rotational body will not occur. Further, the thermosetting resin has superior oxygen barrier characteristics, and therefore anti-corrosion process can be performed by a relatively simple method of only forming the thermosettingresin film layer 17 on the surface of thebalancing holes 16. - As a method of forming the thermosetting
resin film layer 17, a known spray application process using a spray gun or the like, followed by age hardening by therotor 8 at room temperature or a required temperature may be employed, whereby conducting a uniform application at least on the surface of the aluminum alloy of thebalancing holes 16 at a thickness of 10 to 20 μm. - Provided that the thermosetting
resin film layer 17 is formed into a thick film, anti-corrosion performance can be increased, and corrosion of thebalancing holes 16 can be prevented over a long period of time. However, by reason that manufacturing cost rises, the gap between the outercircumferential surface 8 a of therotor 8 and thescrew stator 14 becomes narrower, the rotational body and the fixed side of the vacuum pump come into contact, and the fixed side is damaged, the aforementioned film thickness range is appropriate. - Further, the weight of the thermosetting
resin film layer 17 after hardening and drying is set on the order of 1 to 10 mg with respect to the number ofbalancing holes 16, and considering the increase in weight due to the thermosettingresin film layer 17, it is necessary to form the syntheticresin film layer 17 after performing a little excess amount of material cutting for balancing. - In accordance with the vacuum pump of this embodiment, the aluminum alloy surface of the
balancing holes 16 formed in the surface of the outercircumferential surface 8 a or the innercircumferential surface 8 b of therotor 8 is covered by the thermosettingresin film layer 17 as an anti-corrosion process, and therefore corrosion due to a corrosive gas does not develop in the aluminum alloy surface of thebalancing holes 16, stress corrosion cracking of the balancing holes due to high speed rotation of the rotational body can be prevented, and rotor destruction due to corrosion can be prevented from happening. - Further, as stated above, the thermosetting
resin film layer 17 can be formed on the aluminum alloy surface of the balancing holes 16 b into a thin film as an anti-corrosion process, and deposition of the product adhering to the aluminum alloy can be reduced, and therefore damage due to contact between the rotational body and the fixed side can be prevented. - Next, a second embodiment of a vacuum pump according to the present invention is explained based on FIG. 4.
- The basic structure of the vacuum pump in this second embodiment is similar to the vacuum pump shown in FIG. 1, and therefore identical reference numerals are attached to identical portions, and a detailed explanation of those portions is omitted.
- The vacuum pump in this second embodiment is characterized in that the
balancing holes 16 are formed by removing a portion of the innercircumferential surface 8 b or the outercircumferential surface 8 a of therotor 8, and in that thecorrosion prevention layer 15 is formed on the innercircumferential surface 8 b and the outercircumferential surface 8 a of therotor 8, as shown in FIG. 4. - That is, in this second embodiment, a portion of the outer
circumferential surface 8 a or the innercircumferential surface 8 b of therotor 8 formed by the aluminum alloy or the like is removed by using thecutting tool 20 such as a drill or a router, changing the mass of therotor 8 and performing fine adjustments of the balance of the rotational body, after which the corrosionprevention film layer 15 is uniformly coated to a thickness on the order of 10 to 20 μm by plating a nickel phosphorous alloy plating or the like, performing anti-corrosion process at the same time to therotor 8 and to thebalancing holes 16. - In accordance with the vacuum pump of this second embodiment, in addition to the effects obtained by the above stated first embodiment, the process step for forming the thermosetting
resin film layer 17 for anti-corrosion process of thebalancing holes 16 can be omitted, anti-corrosion process of thebalancing holes 16 can be simplified, and the manufacturing costs of the vacuum pump relating to anti-corrosion process can be lowered. - Further, the corrosion
prevention film layer 15 is formed uniformly over the entire surface of therotor 8 after performing balancing as stated above, and therefore it is not necessary to remove an excess amount of material in order to adjust the balance. - Note that although an example of applying the present invention to a turbo molecular pump is explained in the aforementioned embodiments, the present invention can also be applied, of course, to other pumps that utilize rotation of a rotating body, such as a drag pump, and it is also possible to suitably change the locations in which the balancing holes are formed for design reasons.
- As explained in detail above, the following effects can be obtained in accordance with the vacuum pump according to the present invention.
- (1) An effect in which corrosion due to corrosive gas does not develop on the aluminum alloy surface of the balancing holes formed in the rotor surface, stress corrosion cracking of the balancing holes due to high speed rotation of the rotational body can be prevented, and therefore, destruction of the rotor due to corrosion can be prevented from happening.
- (2) An effect in which the thermosetting resin film layer can be formed as a thin film on the aluminum alloy surface of the balancing holes for the heat resistance process, and deposition of the product adhering to the aluminum alloy can be reduced, and therefore damage due to contact between the rotational body and the fixed side can be prevented.
- (3) An effect in which anti-corrosion process of the balancing holes can be simplified provided that the structure is employed in which the corrosion prevention film is formed uniformly over the entire surface of the rotor after performing balancing, and manufacturing costs for the vacuum pump relating to anti-corrosion process can be reduced.
Claims (3)
1. A vacuum pump comprising:
a pump case having a gas inlet port opened in its top surface;
a rotor shaft rotatably supported within the pump case;
a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed within the pump case;
a plurality of stator blades fixed within the pump case and positioned alternately with the plurality of rotor blades;
a driving motor for rotating the rotor shaft;
an anti-corrosive film layer formed on a surface of the rotor; and
a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor, and performed anti-corrosion process.
2. A vacuum pump according to claim 1 , wherein the anti-corrosion process comprises forming a thermosetting resin film layer on a surface of the balancing hole.
3. A vacuum pump comprising:
a pump case having a gas inlet port opened in its top surface;
a rotor shaft rotatably supported within the pump case;
a plurality of rotor blades formed on an outer circumferential surface of a rotor that is fixed to the rotor shaft and housed within the pump case;
a plurality of stator blades fixed within the pump case and positioned alternately with the plurality of rotor blades;
a driving motor for rotating the rotor shaft;
a balancing hole formed by partially cutting off an inner circumferential surface or an outer circumferential surface of the rotor; and
an anti-corrosive film layer formed on a surface of the rotor.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2001-202297 | 2001-07-03 | ||
| JP2001202297A JP2003021092A (en) | 2001-07-03 | 2001-07-03 | Vacuum pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20030021672A1 true US20030021672A1 (en) | 2003-01-30 |
Family
ID=19039128
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/187,566 Abandoned US20030021672A1 (en) | 2001-07-03 | 2002-07-03 | Vacuum pump |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20030021672A1 (en) |
| EP (1) | EP1273802A1 (en) |
| JP (1) | JP2003021092A (en) |
| KR (1) | KR20030004118A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030021673A1 (en) * | 2001-07-05 | 2003-01-30 | Yasushi Maejima | Vacuum pump |
| US20050249618A1 (en) * | 2004-05-10 | 2005-11-10 | Boc Edwards Japan Limited | Vacuum pump |
| US20130129482A1 (en) * | 2010-08-06 | 2013-05-23 | Shimadzu Corporation | Vacuum pump |
| US20150225593A1 (en) * | 2011-07-21 | 2015-08-13 | Tohoku University | Method for smoothing a perfluoro alkoxy alkane film surface |
| US10585291B2 (en) | 2017-04-28 | 2020-03-10 | Yonatan Gerlitz | Eye safety system for lasers |
| US11333154B2 (en) * | 2018-10-15 | 2022-05-17 | Shimadzu Corporation | Vacuum pump with a rotary body in a case with the rotary body having at least three balance correction portions accessible from an outside of the case for balance correction by an n-plane method |
| EP4279746A4 (en) * | 2021-01-18 | 2025-02-19 | Edwards Japan Limited | VACUUM PUMP AND ROTATING BODY FOR IT |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102011105806A1 (en) * | 2011-05-05 | 2012-11-08 | Pfeiffer Vacuum Gmbh | Vacuum pump with rotor |
| DE102014103060B4 (en) * | 2014-03-07 | 2019-01-03 | Pfeiffer Vacuum Gmbh | Method for balancing a rotor of a vacuum pump or a rotor of a rotary unit for a vacuum pump |
| JP7108377B2 (en) * | 2017-02-08 | 2022-07-28 | エドワーズ株式会社 | Vacuum pumps, rotating parts of vacuum pumps, and unbalance correction methods |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5350275A (en) * | 1992-06-05 | 1994-09-27 | Zaidan Houjin Shinku Kagaku Kenkyujo | Turbomolecular pump having vanes with ceramic and metallic surfaces |
| US5536148A (en) * | 1993-09-17 | 1996-07-16 | Hitachi, Ltd. | Turbo vacuum pump |
| US5938406A (en) * | 1997-04-18 | 1999-08-17 | Varian, Inc. | Rotor for turbomolecular pump |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB687976A (en) * | 1949-12-23 | 1953-02-25 | Vickers Electrical Co Ltd | Improved curing process for thermosetting resinous coatings |
| DE4239391C2 (en) * | 1991-11-27 | 1996-11-21 | Electro Chem Eng Gmbh | Objects made of aluminum, magnesium or titanium with an oxide ceramic layer filled with fluoropolymers and process for their production |
| IT1296155B1 (en) * | 1996-04-05 | 1999-06-09 | Varian Spa | TURBOMOLECULAR PUMP ROTOR |
| JP3836160B2 (en) * | 1998-02-13 | 2006-10-18 | 株式会社荏原製作所 | Rotor for vacuum pump and method for manufacturing the same |
-
2001
- 2001-07-03 JP JP2001202297A patent/JP2003021092A/en not_active Withdrawn
-
2002
- 2002-06-27 EP EP02254522A patent/EP1273802A1/en not_active Withdrawn
- 2002-07-02 KR KR1020020037959A patent/KR20030004118A/en not_active Withdrawn
- 2002-07-03 US US10/187,566 patent/US20030021672A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5350275A (en) * | 1992-06-05 | 1994-09-27 | Zaidan Houjin Shinku Kagaku Kenkyujo | Turbomolecular pump having vanes with ceramic and metallic surfaces |
| US5536148A (en) * | 1993-09-17 | 1996-07-16 | Hitachi, Ltd. | Turbo vacuum pump |
| US5938406A (en) * | 1997-04-18 | 1999-08-17 | Varian, Inc. | Rotor for turbomolecular pump |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20030021673A1 (en) * | 2001-07-05 | 2003-01-30 | Yasushi Maejima | Vacuum pump |
| US6709226B2 (en) * | 2001-07-05 | 2004-03-23 | Boc Edwards Technologies Limited | Vacuum pump |
| US20050249618A1 (en) * | 2004-05-10 | 2005-11-10 | Boc Edwards Japan Limited | Vacuum pump |
| US7572096B2 (en) * | 2004-05-10 | 2009-08-11 | Boc Edwards Japan Limited | Vacuum pump |
| US20130129482A1 (en) * | 2010-08-06 | 2013-05-23 | Shimadzu Corporation | Vacuum pump |
| US20150225593A1 (en) * | 2011-07-21 | 2015-08-13 | Tohoku University | Method for smoothing a perfluoro alkoxy alkane film surface |
| US9957406B2 (en) * | 2011-07-21 | 2018-05-01 | Tohoku University | Method for smoothing a perfluoro alkoxy alkane film surface |
| US10585291B2 (en) | 2017-04-28 | 2020-03-10 | Yonatan Gerlitz | Eye safety system for lasers |
| US11333154B2 (en) * | 2018-10-15 | 2022-05-17 | Shimadzu Corporation | Vacuum pump with a rotary body in a case with the rotary body having at least three balance correction portions accessible from an outside of the case for balance correction by an n-plane method |
| EP4279746A4 (en) * | 2021-01-18 | 2025-02-19 | Edwards Japan Limited | VACUUM PUMP AND ROTATING BODY FOR IT |
| US12270405B2 (en) | 2021-01-18 | 2025-04-08 | Edwards Japan Limited | Vacuum pump and rotating body thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| JP2003021092A (en) | 2003-01-24 |
| KR20030004118A (en) | 2003-01-14 |
| EP1273802A1 (en) | 2003-01-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: BOC EDWARDS TECHNOLOGIES LIMITED, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:MAEJIMA, YASUSHI;SAKAGUCHI, YOSHIYUKI;REEL/FRAME:013360/0736 Effective date: 20020912 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |