Vacuum pump
11542950 · 2023-01-03
Assignee
Inventors
Cpc classification
F04D29/584
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2240/51
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/044
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2260/231
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2280/1021
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D19/046
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2280/5004
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/5853
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/048
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F04D19/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/048
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A vacuum pump capable of suppressing the solidification of gas in a normal operation of a pump is provided. Provided is a vacuum pump including a casing that has an inlet port for sucking gas from outside and an outlet port for exhausting the gas to the outside; a turbo-molecular-pump mechanism that is disposed in the casing and includes rotor blades and stator blades alternately arranged in multiple stages in an axial direction; a thread-groove-pump mechanism that is disposed in the casing and is connectedly disposed on an exhaust side of the turbo-molecular-pump mechanism; first temperature regulating means that is configured to regulate cooling of the turbo-molecular-pump mechanism; and second temperature regulating means that is configured to regulate heating of the thread-groove-pump mechanism.
Claims
1. A vacuum pump comprising: a casing, the casing having an inlet port for sucking gas from outside and an outlet port for exhausting the gas to the outside; a turbo-molecular-pump mechanism, the turbo-molecular-pump mechanism being disposed in the casing and including rotor blades and stator blades alternately arranged in multiple stages in an axial direction; a thread-groove-pump mechanism, the thread-groove-pump mechanism being disposed in the casing and being connectedly disposed on an exhaust side of the turbo-molecular-pump mechanism; a bearing, the bearing rotatably holding a rotating portion of the turbo-molecular-pump mechanism and a rotating portion of the thread-groove-pump mechanism; and a motor portion configured to rotate the rotating portions, the vacuum pump further comprising: first temperature regulating means configured to regulate cooling of the turbo-molecular-pump mechanism; and second temperature regulating means configured to regulate heating of the thread-groove-pump mechanism, wherein the turbo-molecular-pump mechanism is divided into an upper-stage-group gas transfer unit that is disposed downstream from the inlet port and is cooled by the first temperature regulating means, and a lower-stage-group gas transfer unit that is disposed upstream of the thread-groove-pump mechanism and is heated by the second temperature regulating means, and heat insulating means is provided between the first temperature regulating means and the lower-stage-group gas transfer unit, wherein a portion of the heat insulation means extends axially adjacent the lower-stage-group gas transfer unit.
2. The vacuum pump according to claim 1, further comprising: a second heat insulating means, the second heat insulating means being provided between a stator of the thread-groove-pump mechanism and a stator of the motor portion.
3. The vacuum pump according to claim 1, wherein the bearing and a stator of the motor portion are always cooled.
4. The vacuum pump according to claim 1, wherein a stator of the turbo-molecular-pump mechanism includes a first temperature sensor and a cooling structure; a stator of the thread-groove-pump mechanism includes a second temperature sensor and a heating structure; the first temperature regulating means regulates a temperature of the cooling structure of the turbo-molecular-pump mechanism based on a temperature detected by the first temperature sensor of the turbo-molecular-pump mechanism, and the second temperature regulating means regulates a temperature of the heating structure of the thread-groove-pump mechanism based on a temperature detected by the second temperature sensor of the thread-groove-pump mechanism.
5. The vacuum pump according to claim 1, wherein a temperature of the lower-stage-group gas transfer unit is regulated by the second temperature regulating means via the thread-groove-pump mechanism.
6. The vacuum pump according to claim 1, wherein the heat insulating means is in contact with the lower-stage-group gas transfer unit and is disposed with a clearance created between the heat insulating means and the upper-stage-group gas transfer unit.
7. The vacuum pump according to claim 5, wherein the turbo-molecular-pump mechanism includes a clearance that axially separates the upper-stage-group gas transfer unit from the lower-stage-group gas transfer unit.
8. The vacuum pump according to claim 1, wherein the heat insulating means is a stainless material.
9. The vacuum pump according to claim 5, wherein the first temperature regulating means regulates a temperature of the upper-stage-group gas transfer unit based on a temperature detected by a first temperature sensor for detecting the temperature of the upper-stage-group gas transfer unit, and the second temperature regulating means regulates a temperature of the thread-groove-pump mechanism based on a temperature detected by a second temperature sensor for detecting the temperature of the thread-groove-pump mechanism.
10. The vacuum pump according to claim 1, wherein the bearing and a bearing portion of the motor portion are magnetic bearings.
11. The vacuum pump according to claim 1, wherein the second temperature regulating means controls the temperature with reference to a sublimation curve based on a relationship between a temperature and a pressure of the gas.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
DETAILED DESCRIPTION
(6) In order to attain an object of suppressing the solidification of gas in a normal operation of a pump, the present invention is implemented by providing a vacuum pump, including: a casing, the casing having an inlet port for sucking gas from outside and an outlet port for exhausting the gas to the outside; a turbo-molecular-pump mechanism, the turbo-molecular-pump mechanism being disposed in the casing and including rotor blades and stator blades alternately arranged in multiple stages in an axial direction; a thread-groove-pump mechanism, the thread-groove-pump mechanism being disposed in the casing and being connectedly disposed on an exhaust side of the turbo-molecular-pump mechanism; a bearing, the bearing rotatably holding a rotating portion of the turbo-molecular-pump mechanism and a rotating portion of the thread-groove-pump mechanism; and a motor portion configured to rotate the rotating portions, the vacuum pump further including: first temperature regulating means configured to regulate cooling of the turbo-molecular-pump mechanism; and second temperature regulating means configured to regulate heating of the thread-groove-pump mechanism.
(7) An embodiment for implementing the present invention will be specifically described below in accordance with the accompanying drawings. In the description, expressions indicating vertical and horizontal directions are not definite expressions. These expressions are appropriate in the drawings of the portions of the vacuum pump according to the present invention but the interpretation should be changed according to a change of the orientation of the vacuum pump.
Embodiment
(8)
(9) The vacuum pump 10 includes the casing 11, a rotor 15 having a rotor shaft 14 rotatably supported in the casing 11, an electric motor 16 for rotating the rotor shaft 14, and a base 18 including a stator column 18B accommodating a portion of the rotor shaft 14 and the electric motor 16.
(10) The casing 11 is shaped like a cylinder with a closed end. The casing 11 has the function of a stator for the turbo-molecular-pump mechanism PA and includes a tube portion 11A and a water-cooled spacer 11B. Moreover, a heater spacer 11C shaped like a circular pipe is disposed inside the lower portion of the water-cooled spacer 11B. The water-cooled spacer 11B is fixed to the tube portion 11A with bolts 20 and forms a vacuum-pump housing with the casing 11. Furthermore, an outlet port 11a is disposed on the side of the lower portion of the water-cooled spacer 11B and an inlet port 11b is disposed at the center of the top of the casing 11.
(11) In the casing 11, the water-cooled spacer 11B is fixed onto a base body 18A of the base 18 with a heat insulator 42 interposed between the water-cooled spacer 11B and the base body 18A, and the heater spacer 11C is similarly fixed onto the base body 18A of the base 18 with the heat insulator 42 interposed between the heater spacer 11C and the base body 18A. This insulates the water-cooled spacer 11B and the heater spacer 11C from the base 18 via the heat insulator 42. Moreover, a clearance S3 for heat insulation is provided between the water-cooled spacer 11B and the heater spacer 11C. The water-cooled spacer 11B and the heater spacer 11C are insulated from each other by the clearance S3. Alternatively, the water-cooled spacer 11B and the heater spacer 11C may be insulated from each other by providing a heat insulator between the water-cooled spacer 11B and the heater spacer 11C.
(12) In the water-cooled spacer 11B, a water-cooled tube 22 and a first temperature sensor 37 are embedded. Cooling water passes through the water-cooled tube 22, thereby adjusting the temperature of the water-cooled spacer 11B. A temperature change of the water-cooled spacer 11B is detected by the first temperature sensor 37 serving as a water-cooled valve temperature sensor.
(13) The first temperature sensor 37 is connected to first temperature regulating means 39. The first temperature regulating means 39 is connected to a control unit, which is not illustrated. The first temperature regulating means 39 opens and closes a valve (not illustrated) for cooling water passing through the water-cooled tube 22 and regulates the flow rate of cooling water so as to control the temperature of the water-cooled spacer 11B to a predetermined temperature (e.g., 50° C. to 100° C.).
(14) The base 18 includes the base body 18A to which the heater spacer 11C and the water-cooled spacer 11B are attached with the heat insulator 42 interposed between the base body 18A and the spacers, and the stator column 18B that protrudes upward from the center of the base body 18A and serves as the stator of the electric motor 16. Embedded in the base body 18A is a water-cooled tube 17. The water-cooled tube 17 has a structure in which cooling water always cools the base body 18A, a magnetic bearing 24, which will be described later, a touchdown bearing 27, and the electric motor 16. In the present embodiment, a temperature is not controlled by the water-cooled tube 17 in which cooling water always flows to keep a temperature of 25° C. to 70° C.
(15) The tube portion 11A is attached to a vacuum vessel, e.g., a chamber, which is not illustrated, via a flange 11c. The inlet port 11b is connected so as to communicate with the vacuum vessel. The outlet port 11a is connected so as to communicate with an auxiliary pump, which is not illustrated.
(16) The rotor 15 includes the rotor shaft 14 and rotor blades 23 that are fixed to the upper portion of the rotor shaft 14 and are concentrically placed around the axis of the rotor shaft 14.
(17) The rotor shaft 14 is supported by the magnetic bearing 24 in a noncontact manner. The magnetic bearing 24 includes a radial electromagnet 25 and an axial electromagnet 26. The radial electromagnet 25 and the axial electromagnet 26 are connected to the control unit, which is not illustrated.
(18) The control unit controls the magnetizing currents of the radial electromagnet 25 and the axial electromagnet 26 based on the detected values of a radial displacement sensor 25a and an axial displacement sensor 26a, so that the rotor shaft 14 is supported while being floated at a predetermined position.
(19) The upper and lower portions of the rotor shaft 14 are inserted into the touchdown bearing 27. If the rotor shaft 14 is placed out of control, the rotor shaft 14 rotating at a high speed comes into contact with the touchdown bearing 27 and prevents damage to the vacuum pump 10.
(20) A bolt 29 is inserted and screwed into a rotor flange 30 while the upper portion of the rotor shaft 14 is inserted into a boss hole 28, so that the rotor blades 23 are integrally attached to the rotor shaft 14. Hereinafter, the axial direction of the rotor shaft 14 will be referred to as “rotor axial direction A” and the radial direction of the rotor shaft 14 will be referred to as “rotor radial direction R.”
(21) The electric motor 16 includes a rotor 16A attached to outer periphery of the rotor shaft 14 and a stator 16B surrounding the rotor 16A. The stator 16B is connected to the control unit, which is not illustrated. The control unit controls the rotation of the rotor shaft 14.
(22) The turbo-molecular-pump mechanism PA acting as the exhaust function unit 12 disposed substantially in the upper half of the vacuum pump 10 will be described below.
(23) The turbo-molecular-pump mechanism PA includes an upper-stage-group gas transfer unit PA1 that is disposed near the inlet port 11b and a lower-stage-group gas transfer unit PA2 that is disposed next to the thread-groove-pump mechanism PB and is connected to the thread-groove-pump mechanism PB. The upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2 include the rotor blades 23 of the rotor 15 and stator blades 31, respectively. The stator blades 31 are disposed at predetermined intervals between the rotor blades 23. The rotor blades 23 and the stator blades 31 are alternately placed in multiple stages along the rotor axial direction A. In the upper-stage-group gas transfer unit PA1 of the present embodiment, the rotor blades 23 are placed in seven stages and the stator blades 31 are placed in six stages. In the lower-stage-group gas transfer unit PA2, the rotor blades 23 are placed in four stages and the stator blades 31 are placed in three stages. Moreover, a predetermined clearance S1 for heat insulation is provided between the rotor blade 23 of the final stage of the upper-stage-group gas transfer unit PA1 and the rotor blade 23 of the first stage of the lower-stage-group gas transfer unit PA2.
(24) The rotor blade 23 includes a blade tilted at a predetermined angle and is integrated with the outer surface of the upper portion of the rotor 15. The rotor blades 23 are radially attached around the axis of the rotor 15.
(25) The stator blade 31 includes a blade tilted opposite to the rotor blade 23. The stator blades 31 are placed in multiple stages on the inner wall surface of the tube portion 11A. The stator blades 31 are held at fixed intervals in the rotor axial direction A by spacers 41. The stator blades 31 of the upper-stage-group gas transfer unit PA1 are fixed to the water-cooled spacer 11B, whereas the stator blades 31 of the lower-stage-group gas transfer unit PA2 are fixed to the upper end of the heater spacer 11C along with an annular heat insulating spacer 32.
(26) The heat insulating spacer 32 is heat insulating means for heat insulation between the heater spacer 11C and the water-cooled spacer 11B. The heat insulating spacer 32 is made of a material having low heat conductivity, that is, a material hardly conducting heat, for example, an aluminum material or a stainless material (a stainless material in the present embodiment). The heat insulating spacer 32 is in close contact with the lower-stage-group gas transfer unit PA2 and is separated from the inner surface of the water-cooled spacer 11B connected to the upper-stage-group gas transfer unit PA1. The separation from the inner surface of the heat insulating spacer 32 forms a clearance S2 for heat insulation between the water-cooled spacer 11B and the heat insulating spacer 32 so as to communicate with the clearance S1 for heat insulation between the rotor blade 23 of the final stage of the upper-stage-group gas transfer unit PA1 and the rotor blade 23 of the first stage of the lower-stage-group gas transfer unit PA2. In other words, the heat insulating spacer 32 and the clearances S1 and S2 for heat insulation are provided between the upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2, so that the upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2 are independent of each other and the temperatures of the transfer units PA1 And PA2 do not affect each other.
(27) The clearances between the rotor blades 23 and the stator blades 31 gradually become narrow from above toward a lower position in the rotor axial direction A. Moreover, the rotor blades 23 and the stator blades 31 gradually become shorter from above toward a lower position in the rotor axial direction A.
(28) The turbo-molecular-pump mechanism PA is configured such that gas sucked from the inlet port 11b is transferred downward (to the thread-groove-pump mechanism PB) in the rotor axial direction A by the rotations of the rotor blades 23.
(29) The thread-groove-pump mechanism PB disposed substantially in the lower half of the vacuum pump 10 will be described below.
(30) The thread-groove-pump mechanism PB includes a rotor cylindrical portion 33 that is disposed in the lower portion of the rotor 15 and extends along the rotor axial direction A, and the substantially cylindrical heater spacer 11C that surrounds an outer surface 33a of the rotor cylindrical portion 33 and serves as the stator of the thread-groove-pump mechanism PB.
(31) Carved on an inner surface 18b of the heater spacer 11C is a thread groove portion 35. The heater spacer 11C is provided with a cartridge heater 36 acting as heating means and a second temperature sensor 38 acting as a heater temperature sensor for detecting a temperature in the heater spacer 11C.
(32) The cartridge heater 36 is stored in a heater storage portion 43 of the heater spacer 11C and generates heats when being energized. The temperature of the heater spacer 11C is regulated by the generated heat. A temperature change of the heater spacer 11C is detected by the second temperature sensor 38.
(33) The cartridge heater 36 and the second temperature sensor 38 are connected to second temperature regulating means 40. The cartridge heater 36 is connected to the second temperature regulating means 40. The second temperature regulating means 40 is connected to the control unit, which is not illustrated, controls power supply to the cartridge heater 36, and keeps a heater space at a predetermined temperature (e.g., 100° C. to 150° C.).
(34) The operations of the vacuum pump 10 configured thus will be described below. In the vacuum pump 10, as described above, the flange 11c of the casing 11 having the inlet port 11b is attached to a vacuum vessel, e.g., a chamber that is not illustrated. In this state, when the electric motor 16 of the vacuum pump 10 is driven, the rotor blades 23 are rotated at high speed with the rotor 15. Thus, gas from the inlet port 11b flows into the vacuum pump 10. The gas is sequentially transferred into the upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2 in the turbo-molecular-pump mechanism PA and the thread groove portion 35 of the thread-groove-pump mechanism PB and then is exhausted from the outlet port 11a of the casing 11. In other words, the vacuum vessel is evacuated.
(35) In the vacuum pump 10, gas is sucked from the inlet port 11b of the vacuum pump 10, is transferred into the casing 11, and is exhausted from the outlet port 11a. The gas being transferred from the inlet port 11b to the outlet port 11a is gradually compressed and pressurized.
(36)
(37) As is evident from
(38) In consideration of the relationship between the temperature and strength of the rotor blades 23 and the stator blades 31, typically in the turbo-molecular-pump mechanism PA, the rotor blades 23 and the stator blades 31 may decrease in strength and rupture at an extremely high temperature during an operation. Furthermore, in consideration of the relationship between a temperature and electric parts and the electric motor in the vacuum pump 10, the electric parts and the electric motor may typically suffer performance degradation at an extremely high temperature.
(39) Hence, in the vacuum pump of the present embodiment, the heat insulating spacer 32 serving as heat insulating means is provided between the rotor blade 23 of the final stage of the upper-stage-group gas transfer unit PA1 and the rotor blade 23 of the first stage of the lower-stage-group gas transfer unit PA2. Thus, the upper-stage-group gas transfer unit PA1 as a medium temperature portion regulated at 50° C. to 100° C. and the lower-stage-group gas transfer unit PA2 as a high temperature portion regulated at 100° C. to 150° C. are independent of each other, so that the temperatures of the transfer units PA1 And PA2 do not affect each other. Furthermore, in the temperature control of the upper-stage-group gas transfer unit PA1 and the temperature control of the lower-stage-group gas transfer unit PA2, the upper-stage-group gas transfer unit PA1 as a medium temperature portion is controlled by the first temperature regulating means 39, and the lower-stage-group gas transfer unit PA2 as a high temperature portion and the thread-groove-pump mechanism PB are controlled by the second temperature regulating means 40. The control by the first temperature regulating means 39 and the second temperature regulating means 40 is adjusted such that the temperature of each portion falls below the sublimation curve f of
(40) As described above, in the vacuum pump 10 of the present embodiment, the cooling of the turbo-molecular-pump mechanism PA is regulated by the first temperature regulating means 39 and the heating of the thread-groove-pump mechanism PB is regulated by the second temperature regulating means 40, so that the temperature of the turbo-molecular-pump mechanism PA and the temperature of the thread-groove-pump mechanism PB are separately controlled. Thus, the temperature of gas passing through the gas transfer units PA1 and PA2 can be minutely controlled in each portion of the casing 11. In other words, the temperature can be minutely controlled without adversely affecting the electric parts in the vacuum pump 10 and the electric motor 16 for rotating the rotor and without affecting a decrease in the strength of the rotor 15 and the stator. This achieves a normal operation of the pump while efficiently suppressing the solidification of gas.
(41) As schematically illustrated in
(42) The magnetic bearing 24, the touchdown bearing 27, and the stator of a motor portion (stator column) have such a structure that the water-cooled tube 17 is embedded in the base body 18A and cooling water passing through the water-cooled tube 17 always cools the base body 18A, the magnetic bearing 24, the touchdown bearing 2727, and the electric motor 16. Thus, the temperature of the turbo-molecular-pump mechanism PA and the temperature of the thread-groove-pump mechanism PB can be separately controlled without affecting the magnetic bearing 24, the touchdown bearing 27, and the electric motor 16.
(43) In the temperature regulation of the stator (heater spacer) of the turbo-molecular-pump mechanism PA, the cooling structure of the turbo-molecular-pump mechanism PA is controlled and regulated by the first temperature regulating means 39 based on a temperature detected by the first temperature sensor 37 of the turbo-molecular-pump mechanism PA. In the temperature regulation of the stator of the thread-groove-pump mechanism PB, the heating structure (cartridge heater 36) of the thread-groove-pump mechanism PB is controlled by the second temperature regulating means 40 based on a temperature detected by the second temperature sensor 38 of the thread-groove-pump mechanism PB. Thus, the temperature of the turbo-molecular-pump mechanism PA and the temperature of the thread-groove-pump mechanism PB can be separately controlled.
(44) In the embodiment, gas is solidified (or liquefied) unless the compression stage (lower-stage-group gas transfer unit PA2) of the turbo-molecular-pump mechanism PA and the thread-groove-pump mechanism PB are heated. The heat insulating spacer 32 is provided between the upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2. However, if the solidification (or liquefaction) of gas is prevented by heating only the thread-groove-pump mechanism PB, the turbo-molecular-pump mechanism PA may not be divided into the upper-stage-group gas transfer unit PA1 and the lower-stage-group gas transfer unit PA2.
(45)
(46) In the vacuum pump 10 of
(47) The present invention can be modified in various ways without departing from the scope of the present invention. The present invention is naturally extended to the modifications.
(48) Although elements have been shown or described as separate embodiments above, portions of each embodiment may be combined with all or part of other embodiments described above.
(49) Although the subject matter has been described in language specific to structural features and/or methodological acts, it is to be understood that the subject matter defined in the appended claims is not necessarily limited to the specific features or acts described above. Rather, the specific features and acts described above are described as example forms of implementing the claims.