US20100209259A1 - Evacuation apparatus - Google Patents
Evacuation apparatus Download PDFInfo
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- US20100209259A1 US20100209259A1 US12/769,284 US76928410A US2010209259A1 US 20100209259 A1 US20100209259 A1 US 20100209259A1 US 76928410 A US76928410 A US 76928410A US 2010209259 A1 US2010209259 A1 US 2010209259A1
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- Prior art keywords
- pump
- vacuum pump
- rotors
- vacuum
- motor
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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
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
- F04C28/08—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by varying the rotational speed
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C16/00—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes
- C23C16/44—Chemical coating by decomposition of gaseous compounds, without leaving reaction products of surface material in the coating, i.e. chemical vapour deposition [CVD] processes characterised by the method of coating
- C23C16/4412—Details relating to the exhausts, e.g. pumps, filters, scrubbers, particle traps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/007—General arrangements of parts; Frames and supporting elements
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/126—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with radially from the rotor body extending elements, not necessarily co-operating with corresponding recesses in the other rotor, e.g. lobes, Roots type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/08—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C18/12—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C18/14—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C18/16—Rotary-piston pumps specially adapted for elastic fluids of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with helical teeth, e.g. chevron-shaped, screw type
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/001—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids of similar working principle
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/005—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids of dissimilar working principle
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C25/00—Adaptations of pumps for special use of pumps for elastic fluids
- F04C25/02—Adaptations of pumps for special use of pumps for elastic fluids for producing high vacuum
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01J—ELECTRIC DISCHARGE TUBES OR DISCHARGE LAMPS
- H01J37/00—Discharge tubes with provision for introducing objects or material to be exposed to the discharge, e.g. for the purpose of examination or processing thereof
- H01J37/32—Gas-filled discharge tubes
- H01J37/32431—Constructional details of the reactor
- H01J37/32798—Further details of plasma apparatus not provided for in groups H01J37/3244 - H01J37/32788; special provisions for cleaning or maintenance of the apparatus
- H01J37/32816—Pressure
- H01J37/32834—Exhausting
Definitions
- the present invention relates to an evacuation apparatus for evacuating a vacuum chamber of a substrate processing apparatus.
- An evacuation apparatus is widely used for evacuating a process gas that has been supplied to a vacuum chamber of a substrate processing apparatus.
- this substrate processing apparatus such as a CVD apparatus or an etching apparatus, it is required to evacuate the process gas from the vacuum chamber to produce a constant vacuum state therein, and a plurality of vacuum pumps connected in series are used to achieve a desired pumping speed and a desired ultimate pressure.
- the above-mentioned evacuation apparatus comprises a booster pump connected to the vacuum chamber, and a main pump connected to the booster pump.
- Both the booster pump and the main pump are a positive-displacement vacuum pump having a pair of pump rotors disposed in a rotor casing.
- a small gap is formed between the pump rotors and also between the pump rotors and an inner surface of the rotor casing, so that these pump rotors can be rotated in the rotor casing in a non-contact manner.
- a single-stage vacuum pump having a pair of Roots-type single-stage pump rotors is used as the booster pump. This is because the conventional CVD apparatus and etching apparatus do not require a large quantity of the process gas for processing a substrate and thus a quantity of the process gas to be evacuated is not so large.
- the present invention has been made in view of the above drawbacks. It is therefore an object of the present invention to provide an evacuation apparatus which can evacuate a large quantity of a gas and can prevent a motor thereof from being overloaded.
- an evacuation apparatus comprising: a first vacuum pump connected to a vacuum chamber; and a second vacuum pump connected to the first vacuum pump; wherein the first vacuum pump has a pair of multistage pump rotors.
- each of the multistage pump rotors has an inlet-side rotor and an outlet-side rotor, and an axial width of the inlet-side rotor is larger than an axial width of the outlet-side rotor.
- a load on a motor of the first vacuum pump can be small. Therefore, a pumping speed (l/min, a volume of a gas evacuated per unit time) can be large, and hence a large quantity of gas can be evacuated.
- the first vacuum pump is started after the second vacuum pump is started.
- the first vacuum pump can be started after an outlet-side pressure, i.e., a back pressure, of the first vacuum pump is lowered by the second vacuum pump.
- a rotational speed of the multistage pump rotors is controlled based on a temperature of a gas delivered by the evacuation apparatus, a pressure of the gas, a temperature of a rotor casing for housing the multistage pump rotors, or electric current flowing into a motor for rotating the multistage pump rotors.
- the multistage pump rotors can be prevented from expanding due to heat of compression of the gas and heat of the motor. Therefore, it is possible to prevent the multistage pump rotors from being brought into contact with an inner surface of the rotor casing. Further, the motor can be prevented from being overloaded, and hence heat generation and the power consumption of the motor can be reduced.
- the first vacuum pump and the second vacuum pump are accommodated in a single enclosure.
- FIG. 1 is a side view showing an evacuation apparatus according to an embodiment of the present invention
- FIG. 2 is a cross-sectional view showing a first vacuum pump shown in FIG. 1 ;
- FIGS. 3A through 3D are schematic views illustrating the manner in which a gas is delivered
- FIG. 4 is a cross-sectional view showing a second vacuum pump shown in FIG. 1 ;
- FIG. 5 is a graph illustrating rotational speeds of the first vacuum pump and the second vacuum pump and a pressure of a gas measured by a pressure sensor
- FIG. 6 is a schematic view showing a substrate processing apparatus incorporating the evacuation apparatus according to the embodiment of the present invention.
- FIG. 1 is a side view showing an evacuation apparatus according to the embodiment of the present invention.
- FIG. 2 is a cross-sectional view showing a first vacuum pump shown in FIG. 1 .
- FIGS. 3A through 3D are schematic views illustrating the manner in which a gas is delivered.
- the evacuation apparatus comprises a first vacuum pump 1 serving as a booster pump, a second vacuum pump 2 serving as a main pump, and a housing (an enclosure) 3 for accommodating the first vacuum pump 1 and the second vacuum pump 2 therein.
- the housing 3 is fixed to an upper surface of a bottom plate 4
- the second vacuum pump 2 is installed on this bottom plate 4 .
- Four wheels 5 (two of which are shown in FIG. 1 ) are fixed to a lower portion of the bottom plate 4 , thus allowing the evacuation apparatus to be transportable.
- the first vacuum pump 1 is a Roots-type positive-displacement vacuum pump having a pair of Roots-type pump rotors 20 (only one of which is shown in FIG. 1 ), and the second vacuum pump 2 is a screw-type positive-displacement vacuum pump having a pair of screw-type pump rotors 40 (only one of which is shown in FIG. 1 ). That is, the pump rotors of the first vacuum pump 1 and the second vacuum pump 2 have different shapes from each other.
- the first vacuum pump 1 and the second vacuum pump 2 are disposed in parallel with each other in the housing 3 , and the first vacuum pump 1 is disposed above the second vacuum pump 2 .
- the first vacuum pump 1 has an inlet port 23 a communicating with an inlet pipe 6 , and the inlet pipe 6 is connected to a vacuum chamber (not shown in FIG. 1 ) incorporated in a substrate processing apparatus.
- the substrate processing apparatus include an etching apparatus and a CVD apparatus for respectively performing an etching process and a CVD process on a substrate such as a semiconductor wafer or a liquid crystal panel.
- An outlet port 23 b is formed in a lower portion of the first vacuum pump 1 , and this outlet port 23 b is connected to an inlet port 43 a of the second vacuum pump 2 via a connecting pipe 7 .
- An outlet port 43 b of the second vacuum pump 2 is connected to an outlet pipe 8 , so that a gas (e.g., a process gas) is discharged to the exterior through the outlet pipe 8 .
- a gas e.g., a process gas
- the first vacuum pump 1 and the second vacuum pump 2 are connected in series and the second vacuum pump 2 is disposed downstream of the first vacuum pump 1 .
- the first vacuum pump 1 is disposed at a vacuum side (a vacuum-chamber side), and the second vacuum pump 2 is disposed at an atmospheric side.
- This second vacuum pump 2 is designed such that it can be started under an atmospheric pressure.
- the first vacuum pump 1 cannot be started by itself under the atmospheric pressure. Specifically, the first vacuum pump 1 is allowed to be started after an outlet-side pressure (i.e., a back pressure) of the first vacuum pump 1 is lowered to a certain degree.
- This first vacuum pump (i.e., the booster pump) 1 serves to increase a pumping speed of the second vacuum pump (i.e., the main pump) 2 .
- the second vacuum pump (the main pump) 2 can be operated at pressures ranging from a vacuum to the atmospheric pressure, and serves to lower the outlet-side pressure (i.e., the back pressure) of the first vacuum pump 1 .
- a pumping speed ratio of the first vacuum pump 1 to the second vacuum pump 2 is 50,000:2,500. If a degree of vacuum that is required for the vacuum chamber is higher than the ultimate pressure of the evacuation apparatus of the present embodiment, an ultra-high vacuum pump such as a turbo-molecular pump may be further disposed upstream of the first vacuum pump 1 .
- a motor driver D 1 for supplying electric current to a motor M 1 of the first vacuum pump 1 and a motor driver D 2 for supplying electric current to a motor M 2 of the second vacuum pump 2 are installed on an upper portion of the housing 3 .
- the rotational speeds of the motor M 1 and the motor M 2 are independently controlled by a control panel (a control unit) 10 via the motor drivers D 1 and D 2 , respectively.
- the rotational speeds of the motor M 1 and the motor M 2 can be controlled by varying the frequency of the electric currents supplied respectively to the motor M 1 and the motor M 2 .
- both the motor M 1 and the motor M 2 are a two-axes brushless DC motor.
- the first vacuum pump 1 comprises the pair of the multistage pump rotors 20 facing each other, and a rotor casing 23 in which the multistage pump rotors 20 are disposed.
- a small gap is formed between the pump rotors 20 and also between the pump rotors 20 and an inner surface of the rotor casing 23 , so that these pump rotors 20 can be rotated in the rotor casing 23 in a non-contact manner.
- Each of the pump rotors 20 has a first-stage Roots rotor (an inlet-side rotor) 20 a disposed at an inlet side, a second-stage Roots rotor (an outlet-side rotor) 20 b disposed at an outlet side, and a rotating shaft 21 to which these Roots rotors 20 a and 20 b are fixed.
- An axial width W 1 of the first-stage Roots rotor 20 a is larger than an axial width W 2 of the second-stage Roots rotor 20 b .
- a ratio of the axial width W 1 of the first-stage Roots rotor 20 a to the axial width W 2 of the second-stage Roots rotor 20 b is 2 ⁇ 10:1, preferably 5 ⁇ 10:1. In this embodiment, this ratio is 5:1.
- the axial width W 1 of the first-stage Roots rotor 20 a is two to ten times, preferably five to ten times the axial width W 2 of the second-stage Roots rotor 20 b .
- a pumping speed of the first-stage Roots rotor 20 a is in the range of 20,000 to 100,000 (l/min), preferably in the range of 50,000 to 100,000 (l/min). In this embodiment, the pumping speed of the first-stage Roots rotor 20 a is 50,000 (1/min).
- the pumping speed of the second-stage Roots rotor 20 b of this embodiment is 10,000 (1/min).
- Each of the rotating shafts 21 is rotatably supported by an inlet-side bearing 22 A and an outlet-side bearing 22 B.
- the inlet port 23 a is formed in the rotor casing 23 and is located above the first-stage Roots rotor 20 a .
- the outlet port 23 b is also formed in the rotor casing 23 and is located below the second-stage Roots rotor 20 b.
- the motor M 1 which drives the first vacuum pump 1 comprises two motor rotors M 1 - 1 fixed respectively to end portions of the rotating shafts 21 , and motor stators M 1 - 2 disposed radially outwardly of the motor rotors M 1 - 1 .
- the motor rotors M 1 - 1 and the motor stators M 1 - 2 are covered with a motor casing 24 .
- FIG. 2 one of the two motor rotors M 1 - 1 and one of the two motor stators M 1 - 2 are illustrated.
- the motor stators M 1 - 2 are connected to the above-mentioned motor driver D 1 .
- the rotating shafts 21 By supplying electric current to the motor stators M 1 - 2 , the rotating shafts 21 , i.e., the pump rotors 20 , are rotated synchronously in opposite directions.
- a cooling pipe 25 B is embedded in a circumferential wall of the motor casing 24 , so that the motor M 1 is cooled by a cooling liquid flowing through the cooling pipe 25 B.
- a pair of timing gears 28 which mesh with each other, are fixed to the other end portions of the rotating shafts 21 . These timing gears 28 are housed in a gear casing 29 .
- a cooling pipe 25 A is embedded in a circumferential wall of the gear casing 29 , so that the timing gears 28 and the bearings 22 A are cooled by a cooling liquid flowing through the cooling pipe 25 A. Since the synchronous rotation of the pump rotors 20 is performed by the motor M 1 , the function of the timing gears 28 is to prevent the synchronous rotation of the pump rotors 20 from being disturbed due to accidental causes.
- Shaft sleeves 31 A (one of which is shown in FIG. 2 ) are fixed respectively to the rotating shafts 21 at a position between the bearing 22 A and the first-stage Roots rotor 20 a .
- Labyrinth seals 32 A (one of which is shown in FIG. 2 ) are disposed so as to surround outer surfaces of the shaft sleeves 31 A, respectively.
- shaft sleeves 31 B (one of which is shown in FIG. 2 ) are fixed respectively to the rotating shafts 21 at a position between the bearing 22 B and the second-stage Roots rotor 20 b
- labyrinth seals 32 B (one of which is shown in FIG. 2 ) are disposed so as to surround outer surfaces of the shaft sleeves 31 B, respectively.
- These labyrinth seals 32 A and 32 B prevent a gas (a process gas) compressed by the pump rotors 20 from entering regions where the bearings 22 A, the bearings 22 B, and the motor M 1 are located. Oil is used as lubricant of the bearings 22 A and 22 B, so that even when by-products of the process gas are deposited on the bearings 22 A and 22 B, such by-products are removed by the oil flowing through the bearings 22 A and 22 B.
- the bearings 22 A and the labyrinth seals 32 A are covered with a bearing casing 33 A, and the bearings 22 B and the labyrinth seals 32 B are covered with a bearing casing 33 B.
- the rotor casing 23 , the motor casing 24 , and the bearing casings 33 A and 33 B are provided separately from each other, and the rotor casing 23 , the bearing casings 33 A and 33 B, and the motor casing 24 are assembled in this order.
- supply ports 35 A and 35 B for supplying a clean gas are provided in the gear casing 29 and the bearing casing 33 B, respectively.
- the clean gas supplied from the supply port 35 A fills the interior space of the gear casing 29 , and then flows through the bearings 22 A and the labyrinth seals 32 A in this order, thus preventing the bearings 22 A and the labyrinth seals 32 A from being exposed to the process gas.
- the clean gas supplied from the supply port 35 B flows through the bearings 22 B and the labyrinth seals 32 B in this order, thus preventing the bearings 22 B and the labyrinth seals 32 B from being exposed to the process gas.
- the clean gas may comprise a stable gas, such as air or nitrogen (an inert gas), which does not react with the process gas.
- the first-stage Roots rotors 20 a (and the second-stage Roots rotors 20 b ) are disposed so as to face each other in the rotor casing 23 .
- the Roots rotors 20 a i.e., the pump rotors 20
- a gas at inlet side is confined in a space defined by the Roots rotor 20 a and the inner surface of the rotor casing 23 , and then delivered to the outlet side.
- Such delivery of the gas is continuously performed, and hence the gas is evacuated from the vacuum chamber connected to the inlet port 23 a (see FIG. 2 ).
- the Roots-type rotor is used in this embodiment, a screw-type or claw-type rotor may be used alternatively.
- the pump rotor is in the form of a multistage pump rotor having multistage rotors arranged in the axial direction.
- the number of stages of the pump rotor 20 is not limited to two.
- a pair of pump rotors each having three or more stages may be used.
- the load on the motor M 1 can be small, and hence the power consumption of the motor M 1 can be reduced. Further, it is possible to prevent the motor M 1 from generating heat and thus to prevent the pump rotors 20 from being brought into contact with the inner surface of the rotor casing 23 .
- FIG. 4 is a cross-sectional view showing the second vacuum pump shown in FIG. 1 .
- This second vacuum pump is different from the first vacuum pump in that pump rotors are of a screw-type.
- Other components of the second vacuum pump are the same as those of the first vacuum pump, and will not be described below repetitively.
- a pair of screw-type multistage pump rotors 40 are disposed in a rotor casing 43 so as to face each other. These pump rotors 40 are rotated synchronously in opposite directions by a motor M 2 comprising motor rotors M 2 - 1 and motor stators M 2 - 2 .
- Each of the pump rotors 40 has a first-stage screw rotor (inlet-side rotor) 40 a , a second-stage screw rotor (outlet-side rotor) 40 b , and a rotating shaft 41 to which these screw rotors 40 a and 40 b are fixed.
- the first-stage and second-stage screw rotors 40 a and 40 b are disposed so as to mesh with each other, respectively.
- the first-stage screw rotors 40 a have a larger axial width and a larger pitch than those of the second-stage screw rotors 40 b .
- the screw-type rotors are used in the second vacuum pump 2 of this embodiment, Roots-type or claw-type rotors may be used alternatively.
- a small gap is formed between the pump rotors 40 and also between the pump rotors 40 and an inner surface of the rotor casing 43 , so that these pump rotors 40 can be rotated in the rotor casing 43 in a non-contact manner.
- An inlet port 43 a is formed in the rotor casing 43 and is located above the first-stage screw rotors 40 a .
- An outlet port 43 b is also formed in the rotor casing 43 and is located below the second-stage screw rotors 40 b .
- the inlet port 43 a is connected to the above-mentioned outlet port 23 b (see FIGS. 1 and 2 ) of the first vacuum pump 1 via the connecting pipe 7 .
- a gas e.g., a process gas
- a gas discharged from the first vacuum pump 1 is introduced into the rotor casing 43 from the inlet port 43 a through the connecting pipe 7 .
- the gas is compressed by the rotation of the first-stage screw rotors 40 a and the second-stage screw rotors 40 b , and is then discharged from the outlet port 43 b.
- a largest pumping speed is achieved by the first-stage Roots rotors 20 a , followed by the second-stage Roots rotors 20 b , the first-stage screw rotors 40 a , and the second-stage screw rotors 40 b.
- the second vacuum pump 2 Since the second vacuum pump 2 is positioned closer to an atmospheric region than the first vacuum pump 1 , an internal pressure of the second vacuum pump 2 is higher than that of the first vacuum pump 1 . Accordingly, the by-products of the process gas are likely to be deposited in the second vacuum pump 2 . In this embodiment, since the second vacuum pump 2 employs the screw-type pump rotors 40 , the by-products deposited in the second vacuum pump 2 are scraped off by the rotation of the pump rotors 40 .
- the screw rotors 40 a and 40 b are suitable for eliminating the by-products.
- the connecting pipe 7 has a pressure sensor 50 therein for measuring a pressure of a gas (e.g., a process gas) discharged from the first vacuum pump 1 .
- the pressure sensor 50 is connected to the control panel 10 (see FIG. 1 ), so that the rotational speed of the pump rotors 20 (see FIGS. 1 and 2 ) of the first vacuum pump 1 is controlled by the control panel 10 based on an output signal (i.e., a pressure of the gas) of the pressure sensor 50 .
- FIG. 5 is a graph illustrating rotational speeds of the first vacuum pump and the second vacuum pump and a pressure of a gas measured by the pressure sensor.
- the second vacuum pump 2 is firstly started, and the rotational speed of the pump rotors 40 of the second vacuum pump 2 is increased until it reaches a rated rotational speed S 4 . Thereafter, the second vacuum pump 2 is operated so as to keep the rated rotational speed. After a predetermined period of time PT has passed from when the second vacuum pump 2 is started, the first vacuum pump 1 is started. As an alternative manner, the first vacuum pump 1 may be started after the pressure of the gas reaches a predetermine pressure P 0 which is within an allowable range of an evacuating pressure of the second vacuum pump 2 . After the rotational speed of the pump rotors 20 of the first vacuum pump 1 reaches S 3 , the pump rotors 20 are rotated at a constant rotational speed (S 3 ).
- the pressure of the gas (the process gas) is further lowered.
- the rotational speed of the pump rotors 20 is further increased.
- the rotational speed of the pump rotors 20 reaches S 2 , the pump rotors 20 are rotated so as to keep the rotational speed S 2 .
- the rotational speed of the pump rotors 20 is further increased to reach a rated rotational speed S 1 .
- the pump rotors 20 are rotated at a constant rotational speed (S 1 ). If the pressure of the gas is increased due to some sort of cause after the pump rotors 20 reach the rated rotational speed, then the pump rotors 20 is operated to decrease its rotational speed to S 2 or S 3 .
- the rotational speed of the pump rotors 20 of the first vacuum pump 1 is changed according to the pressure of the gas delivered by the evacuation apparatus, whereby the load on the motor M 1 can be reduced.
- the pressure sensor 50 is disposed in the connecting pipe 7 in this embodiment, the pressure sensor may be disposed in the rotor casing 43 of the second vacuum pump 2 at a position between the first-stage screw rotors 40 a and the second-stage screw rotors 40 b .
- the pressure sensor may be disposed in the inlet pipe 6 (see FIG. 1 ), the rotor casing 23 of the first vacuum pump 1 , or the inlet port 23 a.
- the rotational speed of the pump rotors 20 of the first vacuum pump 1 may be changed based on a temperature of the gas being delivered by the evacuation apparatus, a temperature of the rotor casing 23 of the first vacuum pump 1 , or electric current flowing into the motor M 1 of the first vacuum pump 1 .
- a temperature sensor for measuring the temperature of the gas is disposed in the rotor casing 23 of the first vacuum pump 1 , for example.
- a temperature sensor is disposed on an outer surface of the rotor casing 23 .
- a current sensor for measuring the electric current flowing into the motor M 1 is incorporated in the control panel 10 .
- FIG. 6 is a schematic view showing a substrate processing apparatus incorporating the evacuation apparatus according to the embodiment of the present invention.
- a process gas supply source 61 is disposed upstream of a vacuum chamber 60 so that a process gas is supplied from the process gas supply source 61 to the vacuum chamber 60 .
- the vacuum chamber 60 is connected to the evacuation apparatus 63 according to the present embodiment via a pipe 62 .
- This pipe 62 has a valve 64 . By opening this valve 64 , the vacuum chamber 60 and the evacuation apparatus 63 communicate with each other through the pipe 62 .
- An exhaust gas cleaning apparatus 65 for treating an exhaust gas (i.e., the process gas) to be harmless is disposed downstream of the evacuation apparatus 63 .
- the exhaust gas cleaning apparatus 65 include several types such as a dry type, a wet type, a combustion type, and a catalytic type.
- a first control unit 67 is connected to the vacuum chamber 60 , so that process conditions under which a substrate is processed in the vacuum chamber 60 are controlled by the first control unit 67 (hereinafter, a process performed on the substrate in the vacuum chamber 60 will be referred to as a main process).
- the control conditions include a type and a temperature of the process gas supplied to the vacuum chamber 60 , for example.
- a second control unit 68 is connected to the evacuation apparatus 63 and the valve 64 , so that operating conditions of the evacuation apparatus 63 and open-close operation of the valve 64 are controlled by the second control unit 68 .
- the operating conditions of the evacuation apparatus 63 include the rotational speeds of the pump rotors 20 and 40 (see FIG. 1 ) and timings of starting the first and second vacuum pumps 1 and 2 , for example.
- the second control unit 68 is connected to the first control unit 67 , so that the first control unit 67 sends the process conditions as a signal to the second control unit 68 .
- the second control unit 68 controls the evacuating apparatus 63 and the valve 64 based on the signal (i.e., the process conditions).
- a third control unit 66 for controlling a whole process is connected to the first control unit 67 .
- This third control unit 66 sends the signal, which indicates the above-mentioned process conditions for the main process suitable for the whole process, to the first control unit 67 .
- the first control unit 67 controls the main process based on this signal. Several kinds of results of the main process that has been performed in the vacuum chamber 60 are fed back to the first control unit 67 .
- a substrate (not shown) is transferred into the vacuum chamber 60 .
- the evacuation apparatus 63 is started while the valve 64 is opened, and is operated at a rated rotational speed.
- the process gas is supplied from the process gas supply source 61 to the vacuum chamber 60 , whereby a predetermined process (the main process) is performed on the substrate.
- the valve 64 is closed and then the substrate is removed from the vacuum chamber 60 . While the valve 64 is closed, the evacuation apparatus 63 can be operated at a lower rotational speed than the rated rotational speed, or the operation of the evacuation apparatus 63 can be stopped. Accordingly, a power consumption of the evacuation apparatus 63 can be reduced. In a case where the degree of vacuum developed in the vacuum chamber 60 is not required to be kept constant, the evacuation apparatus 63 may be operated at a lower rotational speed than the rated rotational speed while the valve 64 is opened.
- the present invention is applicable to an evacuation apparatus for evacuating a vacuum chamber of a substrate processing apparatus.
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Abstract
The present invention relates to an evacuation apparatus for evacuating a vacuum chamber of a substrate processing apparatus for processing a substrate such as a semiconductor wafer or liquid crystal panel. An evacuation apparatus according to the present invention includes a first vacuum pump connected to a vacuum chamber, and a second vacuum pump connected to the first vacuum pump. The first vacuum pump has a pair of multistage pump rotors.
Description
- This application is a division of U.S. application Ser. No. 10/563,255, filed on Jun. 9, 2006, which is a 371 of International Application No. PCT/JP2004/015563 filed on Oct. 14, 2004, which is based upon and claims the benefit of priority from the prior Japanese Patent Application No. 2003-358424, filed on Oct. 17, 2003, the entire contents of which are incorporated herein by reference.
- The present invention relates to an evacuation apparatus for evacuating a vacuum chamber of a substrate processing apparatus.
- An evacuation apparatus is widely used for evacuating a process gas that has been supplied to a vacuum chamber of a substrate processing apparatus. In this substrate processing apparatus such as a CVD apparatus or an etching apparatus, it is required to evacuate the process gas from the vacuum chamber to produce a constant vacuum state therein, and a plurality of vacuum pumps connected in series are used to achieve a desired pumping speed and a desired ultimate pressure.
- The above-mentioned evacuation apparatus comprises a booster pump connected to the vacuum chamber, and a main pump connected to the booster pump. Both the booster pump and the main pump are a positive-displacement vacuum pump having a pair of pump rotors disposed in a rotor casing. In this type of vacuum pump, a small gap is formed between the pump rotors and also between the pump rotors and an inner surface of the rotor casing, so that these pump rotors can be rotated in the rotor casing in a non-contact manner.
- Generally, a single-stage vacuum pump having a pair of Roots-type single-stage pump rotors is used as the booster pump. This is because the conventional CVD apparatus and etching apparatus do not require a large quantity of the process gas for processing a substrate and thus a quantity of the process gas to be evacuated is not so large.
- However, as a substrate such as a semiconductor wafer or a liquid crystal panel, which is an object to be processed, becomes large in size, there has been an increasing need for evacuating a large quantity of the process gas. In order to evacuate the process gas in large quantity, it is required to use large-sized pump rotors or to increase a rotational speed of the pump rotors so as to increase a pumping speed. However, with such a structure, a motor for driving the booster pump is overloaded, resulting in increased power consumption. In addition, the pump rotors are likely to expand due to heat of compression of the process gas and heat generated by the motor, and hence the pump rotors may be brought into contact with the inner surface of the rotor casing, resulting in operation failure. Accordingly, it is difficult for the conventional evacuation apparatus having the single-stage booster pump to evacuate a large quantity of the process gas while maintaining a vacuum state in the vacuum chamber. Under such circumstances, there has been a need for an evacuation apparatus which can evacuate a large quantity of a gas (e.g., a process gas) and can prevent a motor thereof from being overloaded.
- The present invention has been made in view of the above drawbacks. It is therefore an object of the present invention to provide an evacuation apparatus which can evacuate a large quantity of a gas and can prevent a motor thereof from being overloaded.
- In order to achieve the above object, according to one aspect of the present invention, there is provided an evacuation apparatus comprising: a first vacuum pump connected to a vacuum chamber; and a second vacuum pump connected to the first vacuum pump; wherein the first vacuum pump has a pair of multistage pump rotors.
- In a preferred aspect of the present invention, each of the multistage pump rotors has an inlet-side rotor and an outlet-side rotor, and an axial width of the inlet-side rotor is larger than an axial width of the outlet-side rotor.
- According to the present invention, even in a case where the axial width of the rotor (the inlet-side rotor) of the first vacuum pump is designed to be large, a load on a motor of the first vacuum pump can be small. Therefore, a pumping speed (l/min, a volume of a gas evacuated per unit time) can be large, and hence a large quantity of gas can be evacuated.
- In a preferred aspect of the present invention, the first vacuum pump is started after the second vacuum pump is started.
- According to the present invention, the first vacuum pump can be started after an outlet-side pressure, i.e., a back pressure, of the first vacuum pump is lowered by the second vacuum pump.
- In a preferred aspect of the present invention, a rotational speed of the multistage pump rotors is controlled based on a temperature of a gas delivered by the evacuation apparatus, a pressure of the gas, a temperature of a rotor casing for housing the multistage pump rotors, or electric current flowing into a motor for rotating the multistage pump rotors.
- According to the present invention, the multistage pump rotors can be prevented from expanding due to heat of compression of the gas and heat of the motor. Therefore, it is possible to prevent the multistage pump rotors from being brought into contact with an inner surface of the rotor casing. Further, the motor can be prevented from being overloaded, and hence heat generation and the power consumption of the motor can be reduced.
- In a preferred aspect of the present invention, the first vacuum pump and the second vacuum pump are accommodated in a single enclosure.
-
FIG. 1 is a side view showing an evacuation apparatus according to an embodiment of the present invention; -
FIG. 2 is a cross-sectional view showing a first vacuum pump shown inFIG. 1 ; -
FIGS. 3A through 3D are schematic views illustrating the manner in which a gas is delivered; -
FIG. 4 is a cross-sectional view showing a second vacuum pump shown inFIG. 1 ; -
FIG. 5 is a graph illustrating rotational speeds of the first vacuum pump and the second vacuum pump and a pressure of a gas measured by a pressure sensor; and -
FIG. 6 is a schematic view showing a substrate processing apparatus incorporating the evacuation apparatus according to the embodiment of the present invention. - An evacuation apparatus according to an embodiment of the present invention will be described below with reference to the drawings.
-
FIG. 1 is a side view showing an evacuation apparatus according to the embodiment of the present invention.FIG. 2 is a cross-sectional view showing a first vacuum pump shown inFIG. 1 .FIGS. 3A through 3D are schematic views illustrating the manner in which a gas is delivered. - As shown in
FIG. 1 , the evacuation apparatus comprises afirst vacuum pump 1 serving as a booster pump, asecond vacuum pump 2 serving as a main pump, and a housing (an enclosure) 3 for accommodating thefirst vacuum pump 1 and thesecond vacuum pump 2 therein. Thehousing 3 is fixed to an upper surface of abottom plate 4, and thesecond vacuum pump 2 is installed on thisbottom plate 4. Four wheels 5 (two of which are shown inFIG. 1 ) are fixed to a lower portion of thebottom plate 4, thus allowing the evacuation apparatus to be transportable. - The
first vacuum pump 1 is a Roots-type positive-displacement vacuum pump having a pair of Roots-type pump rotors 20 (only one of which is shown inFIG. 1 ), and thesecond vacuum pump 2 is a screw-type positive-displacement vacuum pump having a pair of screw-type pump rotors 40 (only one of which is shown inFIG. 1 ). That is, the pump rotors of thefirst vacuum pump 1 and thesecond vacuum pump 2 have different shapes from each other. Thefirst vacuum pump 1 and thesecond vacuum pump 2 are disposed in parallel with each other in thehousing 3, and thefirst vacuum pump 1 is disposed above thesecond vacuum pump 2. - The
first vacuum pump 1 has aninlet port 23 a communicating with aninlet pipe 6, and theinlet pipe 6 is connected to a vacuum chamber (not shown inFIG. 1 ) incorporated in a substrate processing apparatus. Examples of the substrate processing apparatus include an etching apparatus and a CVD apparatus for respectively performing an etching process and a CVD process on a substrate such as a semiconductor wafer or a liquid crystal panel. Anoutlet port 23 b is formed in a lower portion of thefirst vacuum pump 1, and thisoutlet port 23 b is connected to aninlet port 43 a of thesecond vacuum pump 2 via a connectingpipe 7. Anoutlet port 43 b of thesecond vacuum pump 2 is connected to an outlet pipe 8, so that a gas (e.g., a process gas) is discharged to the exterior through the outlet pipe 8. In this manner, thefirst vacuum pump 1 and thesecond vacuum pump 2 are connected in series and thesecond vacuum pump 2 is disposed downstream of thefirst vacuum pump 1. Specifically, thefirst vacuum pump 1 is disposed at a vacuum side (a vacuum-chamber side), and thesecond vacuum pump 2 is disposed at an atmospheric side. Thissecond vacuum pump 2 is designed such that it can be started under an atmospheric pressure. - On the other hand, the
first vacuum pump 1 cannot be started by itself under the atmospheric pressure. Specifically, thefirst vacuum pump 1 is allowed to be started after an outlet-side pressure (i.e., a back pressure) of thefirst vacuum pump 1 is lowered to a certain degree. This first vacuum pump (i.e., the booster pump) 1 serves to increase a pumping speed of the second vacuum pump (i.e., the main pump) 2. The second vacuum pump (the main pump) 2 can be operated at pressures ranging from a vacuum to the atmospheric pressure, and serves to lower the outlet-side pressure (i.e., the back pressure) of thefirst vacuum pump 1. - In this embodiment, a pumping speed ratio of the
first vacuum pump 1 to thesecond vacuum pump 2 is 50,000:2,500. If a degree of vacuum that is required for the vacuum chamber is higher than the ultimate pressure of the evacuation apparatus of the present embodiment, an ultra-high vacuum pump such as a turbo-molecular pump may be further disposed upstream of thefirst vacuum pump 1. - A motor driver D1 for supplying electric current to a motor M1 of the
first vacuum pump 1 and a motor driver D2 for supplying electric current to a motor M2 of thesecond vacuum pump 2 are installed on an upper portion of thehousing 3. The rotational speeds of the motor M1 and the motor M2 are independently controlled by a control panel (a control unit) 10 via the motor drivers D1 and D2, respectively. The rotational speeds of the motor M1 and the motor M2 can be controlled by varying the frequency of the electric currents supplied respectively to the motor M1 and the motor M2. In this embodiment, both the motor M1 and the motor M2 are a two-axes brushless DC motor. - As shown in
FIG. 2 , thefirst vacuum pump 1 comprises the pair of themultistage pump rotors 20 facing each other, and arotor casing 23 in which themultistage pump rotors 20 are disposed. A small gap is formed between thepump rotors 20 and also between thepump rotors 20 and an inner surface of therotor casing 23, so that thesepump rotors 20 can be rotated in therotor casing 23 in a non-contact manner. Each of thepump rotors 20 has a first-stage Roots rotor (an inlet-side rotor) 20 a disposed at an inlet side, a second-stage Roots rotor (an outlet-side rotor) 20 b disposed at an outlet side, and arotating shaft 21 to which theseRoots rotors stage Roots rotor 20 a is larger than an axial width W2 of the second-stage Roots rotor 20 b. Specifically, a ratio of the axial width W1 of the first-stage Roots rotor 20 a to the axial width W2 of the second-stage Roots rotor 20 b is 2˜10:1, preferably 5˜10:1. In this embodiment, this ratio is 5:1. In other words, the axial width W1 of the first-stage Roots rotor 20 a is two to ten times, preferably five to ten times the axial width W2 of the second-stage Roots rotor 20 b. A pumping speed of the first-stage Roots rotor 20 a is in the range of 20,000 to 100,000 (l/min), preferably in the range of 50,000 to 100,000 (l/min). In this embodiment, the pumping speed of the first-stage Roots rotor 20 a is 50,000 (1/min). The pumping speed of the second-stage Roots rotor 20 b of this embodiment is 10,000 (1/min). - Each of the
rotating shafts 21 is rotatably supported by an inlet-side bearing 22A and an outlet-side bearing 22B. Theinlet port 23 a is formed in therotor casing 23 and is located above the first-stage Roots rotor 20 a. Theoutlet port 23 b is also formed in therotor casing 23 and is located below the second-stage Roots rotor 20 b. - The motor M1 which drives the
first vacuum pump 1 comprises two motor rotors M1-1 fixed respectively to end portions of therotating shafts 21, and motor stators M1-2 disposed radially outwardly of the motor rotors M1-1. The motor rotors M1-1 and the motor stators M1-2 are covered with amotor casing 24. InFIG. 2 , one of the two motor rotors M1-1 and one of the two motor stators M1-2 are illustrated. The motor stators M1-2 are connected to the above-mentioned motor driver D1. By supplying electric current to the motor stators M1-2, the rotatingshafts 21, i.e., thepump rotors 20, are rotated synchronously in opposite directions. A coolingpipe 25B is embedded in a circumferential wall of themotor casing 24, so that the motor M1 is cooled by a cooling liquid flowing through thecooling pipe 25B. - A pair of timing gears 28, which mesh with each other, are fixed to the other end portions of the
rotating shafts 21. These timing gears 28 are housed in agear casing 29. A coolingpipe 25A is embedded in a circumferential wall of thegear casing 29, so that the timing gears 28 and thebearings 22A are cooled by a cooling liquid flowing through thecooling pipe 25A. Since the synchronous rotation of thepump rotors 20 is performed by the motor M1, the function of the timing gears 28 is to prevent the synchronous rotation of thepump rotors 20 from being disturbed due to accidental causes. -
Shaft sleeves 31A (one of which is shown inFIG. 2 ) are fixed respectively to therotating shafts 21 at a position between the bearing 22A and the first-stage Roots rotor 20 a. Labyrinth seals 32A (one of which is shown inFIG. 2 ) are disposed so as to surround outer surfaces of theshaft sleeves 31A, respectively. In addition,shaft sleeves 31B (one of which is shown inFIG. 2 ) are fixed respectively to therotating shafts 21 at a position between the bearing 22B and the second-stage Roots rotor 20 b, andlabyrinth seals 32B (one of which is shown inFIG. 2 ) are disposed so as to surround outer surfaces of theshaft sleeves 31B, respectively. These labyrinth seals 32A and 32B prevent a gas (a process gas) compressed by thepump rotors 20 from entering regions where thebearings 22A, thebearings 22B, and the motor M1 are located. Oil is used as lubricant of thebearings bearings bearings - The
bearings 22A and the labyrinth seals 32A are covered with a bearing casing 33A, and thebearings 22B and the labyrinth seals 32B are covered with a bearingcasing 33B. Therotor casing 23, themotor casing 24, and thebearing casings rotor casing 23, thebearing casings motor casing 24 are assembled in this order. - In order to prevent the by-products of the process gas from being deposited on the
bearings supply ports gear casing 29 and the bearingcasing 33B, respectively. The clean gas supplied from thesupply port 35A fills the interior space of thegear casing 29, and then flows through thebearings 22A and the labyrinth seals 32A in this order, thus preventing thebearings 22A and the labyrinth seals 32A from being exposed to the process gas. In the same manner, the clean gas supplied from thesupply port 35B flows through thebearings 22B and the labyrinth seals 32B in this order, thus preventing thebearings 22B and the labyrinth seals 32B from being exposed to the process gas. The clean gas may comprise a stable gas, such as air or nitrogen (an inert gas), which does not react with the process gas. - As shown in
FIGS. 3A and 3B , the first-stage Roots rotors 20 a (and the second-stage Roots rotors 20 b) are disposed so as to face each other in therotor casing 23. When theRoots rotors 20 a (i.e., the pump rotors 20) are synchronously rotated by the motor M1, a gas at inlet side is confined in a space defined by theRoots rotor 20 a and the inner surface of therotor casing 23, and then delivered to the outlet side. Such delivery of the gas is continuously performed, and hence the gas is evacuated from the vacuum chamber connected to theinlet port 23 a (seeFIG. 2 ). Although the Roots-type rotor is used in this embodiment, a screw-type or claw-type rotor may be used alternatively. In each case where any one of these types is used, the pump rotor is in the form of a multistage pump rotor having multistage rotors arranged in the axial direction. The number of stages of thepump rotor 20 is not limited to two. For example, a pair of pump rotors each having three or more stages may be used. - As described above, according to the present embodiment using the
multistage pump rotors 20, even if the axial width W1 of the first-stage Roots rotor 20 a is designed to be large compared to the conventional pump, the load on the motor M1 can be small, and hence the power consumption of the motor M1 can be reduced. Further, it is possible to prevent the motor M1 from generating heat and thus to prevent thepump rotors 20 from being brought into contact with the inner surface of therotor casing 23. -
FIG. 4 is a cross-sectional view showing the second vacuum pump shown inFIG. 1 . This second vacuum pump is different from the first vacuum pump in that pump rotors are of a screw-type. Other components of the second vacuum pump are the same as those of the first vacuum pump, and will not be described below repetitively. - As shown in
FIG. 4 , a pair of screw-type multistage pump rotors 40 (only one of which is illustrated inFIG. 4 ) are disposed in arotor casing 43 so as to face each other. Thesepump rotors 40 are rotated synchronously in opposite directions by a motor M2 comprising motor rotors M2-1 and motor stators M2-2. Each of thepump rotors 40 has a first-stage screw rotor (inlet-side rotor) 40 a, a second-stage screw rotor (outlet-side rotor) 40 b, and arotating shaft 41 to which thesescrew rotors stage screw rotors stage screw rotors 40 a have a larger axial width and a larger pitch than those of the second-stage screw rotors 40 b. Although the screw-type rotors are used in thesecond vacuum pump 2 of this embodiment, Roots-type or claw-type rotors may be used alternatively. - A small gap is formed between the
pump rotors 40 and also between thepump rotors 40 and an inner surface of therotor casing 43, so that thesepump rotors 40 can be rotated in therotor casing 43 in a non-contact manner. Aninlet port 43 a is formed in therotor casing 43 and is located above the first-stage screw rotors 40 a. Anoutlet port 43 b is also formed in therotor casing 43 and is located below the second-stage screw rotors 40 b. Theinlet port 43 a is connected to the above-mentionedoutlet port 23 b (seeFIGS. 1 and 2 ) of thefirst vacuum pump 1 via the connectingpipe 7. - With such an arrangement, a gas (e.g., a process gas) discharged from the
first vacuum pump 1 is introduced into the rotor casing 43 from theinlet port 43 a through the connectingpipe 7. The gas is compressed by the rotation of the first-stage screw rotors 40 a and the second-stage screw rotors 40 b, and is then discharged from theoutlet port 43 b. - In this embodiment, a largest pumping speed is achieved by the first-
stage Roots rotors 20 a, followed by the second-stage Roots rotors 20 b, the first-stage screw rotors 40 a, and the second-stage screw rotors 40 b. - Since the
second vacuum pump 2 is positioned closer to an atmospheric region than thefirst vacuum pump 1, an internal pressure of thesecond vacuum pump 2 is higher than that of thefirst vacuum pump 1. Accordingly, the by-products of the process gas are likely to be deposited in thesecond vacuum pump 2. In this embodiment, since thesecond vacuum pump 2 employs the screw-type pump rotors 40, the by-products deposited in thesecond vacuum pump 2 are scraped off by the rotation of thepump rotors 40. Specifically, even if the by-products are deposited on the first-stage and second-stage screw rotors rotor casing 43, such by-products are scraped off and then delivered to theoutlet port 43 b by the rotation of thescrew rotors screw rotors - The connecting
pipe 7 has apressure sensor 50 therein for measuring a pressure of a gas (e.g., a process gas) discharged from thefirst vacuum pump 1. Thepressure sensor 50 is connected to the control panel 10 (seeFIG. 1 ), so that the rotational speed of the pump rotors 20 (seeFIGS. 1 and 2 ) of thefirst vacuum pump 1 is controlled by thecontrol panel 10 based on an output signal (i.e., a pressure of the gas) of thepressure sensor 50. - Next, operation of the evacuation apparatus according to this embodiment will be described with reference to
FIG. 5 . -
FIG. 5 is a graph illustrating rotational speeds of the first vacuum pump and the second vacuum pump and a pressure of a gas measured by the pressure sensor. - As shown in
FIG. 5 , thesecond vacuum pump 2 is firstly started, and the rotational speed of thepump rotors 40 of thesecond vacuum pump 2 is increased until it reaches a rated rotational speed S4. Thereafter, thesecond vacuum pump 2 is operated so as to keep the rated rotational speed. After a predetermined period of time PT has passed from when thesecond vacuum pump 2 is started, thefirst vacuum pump 1 is started. As an alternative manner, thefirst vacuum pump 1 may be started after the pressure of the gas reaches a predetermine pressure P0 which is within an allowable range of an evacuating pressure of thesecond vacuum pump 2. After the rotational speed of thepump rotors 20 of thefirst vacuum pump 1 reaches S3, thepump rotors 20 are rotated at a constant rotational speed (S3). - As the
first vacuum pump 1 and thesecond vacuum pump 2 are operated, the pressure of the gas (the process gas) is further lowered. When the pressure of the gas is lowered to reach P2, the rotational speed of thepump rotors 20 is further increased. When the rotational speed of thepump rotors 20 reaches S2, thepump rotors 20 are rotated so as to keep the rotational speed S2. Thereafter, when the pressure of the gas reaches P1, the rotational speed of thepump rotors 20 is further increased to reach a rated rotational speed S1. Then, thepump rotors 20 are rotated at a constant rotational speed (S1). If the pressure of the gas is increased due to some sort of cause after thepump rotors 20 reach the rated rotational speed, then thepump rotors 20 is operated to decrease its rotational speed to S2 or S3. - In this manner, the rotational speed of the
pump rotors 20 of thefirst vacuum pump 1 is changed according to the pressure of the gas delivered by the evacuation apparatus, whereby the load on the motor M1 can be reduced. Although thepressure sensor 50 is disposed in the connectingpipe 7 in this embodiment, the pressure sensor may be disposed in therotor casing 43 of thesecond vacuum pump 2 at a position between the first-stage screw rotors 40 a and the second-stage screw rotors 40 b. Alternatively, the pressure sensor may be disposed in the inlet pipe 6 (seeFIG. 1 ), therotor casing 23 of thefirst vacuum pump 1, or theinlet port 23 a. - Further, the rotational speed of the
pump rotors 20 of thefirst vacuum pump 1 may be changed based on a temperature of the gas being delivered by the evacuation apparatus, a temperature of therotor casing 23 of thefirst vacuum pump 1, or electric current flowing into the motor M1 of thefirst vacuum pump 1. In the case of utilizing the temperature of the gas, it is desirable that a temperature sensor for measuring the temperature of the gas is disposed in therotor casing 23 of thefirst vacuum pump 1, for example. In the case of utilizing the temperature of therotor casing 23 of thefirst vacuum pump 1, it is desirable that a temperature sensor is disposed on an outer surface of therotor casing 23. In the case of utilizing the electric current of the motor M1, it is desirable that a current sensor for measuring the electric current flowing into the motor M1 is incorporated in thecontrol panel 10. - Next, an example in which the evacuation apparatus of this embodiment is connected to a vacuum chamber of a substrate processing apparatus will be described with reference to
FIG. 6 .FIG. 6 is a schematic view showing a substrate processing apparatus incorporating the evacuation apparatus according to the embodiment of the present invention. - As shown in
FIG. 6 , a processgas supply source 61 is disposed upstream of avacuum chamber 60 so that a process gas is supplied from the processgas supply source 61 to thevacuum chamber 60. Thevacuum chamber 60 is connected to theevacuation apparatus 63 according to the present embodiment via apipe 62. Thispipe 62 has avalve 64. By opening thisvalve 64, thevacuum chamber 60 and theevacuation apparatus 63 communicate with each other through thepipe 62. - An exhaust
gas cleaning apparatus 65 for treating an exhaust gas (i.e., the process gas) to be harmless is disposed downstream of theevacuation apparatus 63. Examples of the exhaustgas cleaning apparatus 65 include several types such as a dry type, a wet type, a combustion type, and a catalytic type. Afirst control unit 67 is connected to thevacuum chamber 60, so that process conditions under which a substrate is processed in thevacuum chamber 60 are controlled by the first control unit 67 (hereinafter, a process performed on the substrate in thevacuum chamber 60 will be referred to as a main process). The control conditions include a type and a temperature of the process gas supplied to thevacuum chamber 60, for example. Asecond control unit 68 is connected to theevacuation apparatus 63 and thevalve 64, so that operating conditions of theevacuation apparatus 63 and open-close operation of thevalve 64 are controlled by thesecond control unit 68. The operating conditions of theevacuation apparatus 63 include the rotational speeds of thepump rotors 20 and 40 (seeFIG. 1 ) and timings of starting the first andsecond vacuum pumps - The
second control unit 68 is connected to thefirst control unit 67, so that thefirst control unit 67 sends the process conditions as a signal to thesecond control unit 68. - The
second control unit 68 controls the evacuatingapparatus 63 and thevalve 64 based on the signal (i.e., the process conditions). Athird control unit 66 for controlling a whole process is connected to thefirst control unit 67. Thisthird control unit 66 sends the signal, which indicates the above-mentioned process conditions for the main process suitable for the whole process, to thefirst control unit 67. Thefirst control unit 67 controls the main process based on this signal. Several kinds of results of the main process that has been performed in thevacuum chamber 60 are fed back to thefirst control unit 67. - Operation sequence of this substrate processing apparatus will be carried out as follows: First, a substrate (not shown) is transferred into the
vacuum chamber 60. Thereafter, theevacuation apparatus 63 is started while thevalve 64 is opened, and is operated at a rated rotational speed. Subsequently, while a degree of vacuum developed in thevacuum chamber 60 is being kept constant, the process gas is supplied from the processgas supply source 61 to thevacuum chamber 60, whereby a predetermined process (the main process) is performed on the substrate. - After the supply of the process gas is stopped to finish the main process, the
valve 64 is closed and then the substrate is removed from thevacuum chamber 60. While thevalve 64 is closed, theevacuation apparatus 63 can be operated at a lower rotational speed than the rated rotational speed, or the operation of theevacuation apparatus 63 can be stopped. Accordingly, a power consumption of theevacuation apparatus 63 can be reduced. In a case where the degree of vacuum developed in thevacuum chamber 60 is not required to be kept constant, theevacuation apparatus 63 may be operated at a lower rotational speed than the rated rotational speed while thevalve 64 is opened. - As described above, according to the present invention, it is possible to evacuate a large quantity of gas without imparting an excessive load on the motor that drives the first vacuum pump.
- The present invention is applicable to an evacuation apparatus for evacuating a vacuum chamber of a substrate processing apparatus.
Claims (3)
1. An evacuation apparatus comprising:
a booster pump having a pair of multistage pump rotors; and
a main pump coupled to said booster pump, said main pump being arranged downstream of said booster pump.
2. An evacuation apparatus according to claim 1 , wherein said main pump has a pair of multistage pump rotors.
3. A method of operating an evacuation apparatus having a booster pump coupled to a vacuum chamber and a main pump coupled to the booster pump, the booster pump having a pair of multistage pump rotors, said method comprising:
starting the main pump;
starting the booster pump after a predetermined period of time has passed from said starting of the main pump; and
when current of the booster pump is lowered to a predetermined value, increasing the rotational speed of the booster pump.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US12/769,284 US20100209259A1 (en) | 2003-10-17 | 2010-04-28 | Evacuation apparatus |
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
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JP2003358424A JP4218756B2 (en) | 2003-10-17 | 2003-10-17 | Vacuum exhaust device |
JP2003-358424 | 2003-10-17 | ||
PCT/JP2004/015563 WO2005038255A2 (en) | 2003-10-17 | 2004-10-14 | Evacuation apparatus |
US56325506A | 2006-06-09 | 2006-06-09 | |
US12/769,284 US20100209259A1 (en) | 2003-10-17 | 2010-04-28 | Evacuation apparatus |
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PCT/JP2004/015563 Division WO2005038255A2 (en) | 2003-10-17 | 2004-10-14 | Evacuation apparatus |
US56325506A Division | 2003-10-17 | 2006-06-09 |
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US20100209259A1 true US20100209259A1 (en) | 2010-08-19 |
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US10/563,255 Active 2028-10-07 US9541088B2 (en) | 2003-10-17 | 2004-10-14 | Evacuation apparatus |
US12/769,284 Abandoned US20100209259A1 (en) | 2003-10-17 | 2010-04-28 | Evacuation apparatus |
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US10/563,255 Active 2028-10-07 US9541088B2 (en) | 2003-10-17 | 2004-10-14 | Evacuation apparatus |
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US20140030112A1 (en) * | 2012-07-24 | 2014-01-30 | Ellcie Industries Gmbh | Vacuum device |
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US20150007569A1 (en) * | 2012-02-29 | 2015-01-08 | Eaton Corporation | Volumetric energy recovery device and systems |
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Also Published As
Publication number | Publication date |
---|---|
EP1673539A2 (en) | 2006-06-28 |
WO2005038255A3 (en) | 2005-11-03 |
JP4218756B2 (en) | 2009-02-04 |
US9541088B2 (en) | 2017-01-10 |
JP2005120955A (en) | 2005-05-12 |
EP1673539B1 (en) | 2019-07-31 |
TW200514919A (en) | 2005-05-01 |
TWI326330B (en) | 2010-06-21 |
US20070104587A1 (en) | 2007-05-10 |
WO2005038255A2 (en) | 2005-04-28 |
WO2005038255B1 (en) | 2005-12-29 |
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