EP0226039A1 - Vacuum pump apparatus - Google Patents
Vacuum pump apparatus Download PDFInfo
- Publication number
- EP0226039A1 EP0226039A1 EP86115640A EP86115640A EP0226039A1 EP 0226039 A1 EP0226039 A1 EP 0226039A1 EP 86115640 A EP86115640 A EP 86115640A EP 86115640 A EP86115640 A EP 86115640A EP 0226039 A1 EP0226039 A1 EP 0226039A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- pump
- gas
- stage
- suction port
- vacuum
- 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.)
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Links
- 230000006835 compression Effects 0.000 claims abstract description 47
- 238000007906 compression Methods 0.000 claims abstract description 47
- 238000004891 communication Methods 0.000 claims description 4
- 229940000425 combination drug Drugs 0.000 claims 1
- 238000010276 construction Methods 0.000 abstract description 7
- 238000011144 upstream manufacturing Methods 0.000 abstract description 3
- 239000007789 gas Substances 0.000 description 54
- 239000000543 intermediate Substances 0.000 description 10
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 6
- 239000001307 helium Substances 0.000 description 6
- 229910052734 helium Inorganic materials 0.000 description 6
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 6
- 239000001257 hydrogen Substances 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 229910052757 nitrogen Inorganic materials 0.000 description 3
- 150000002431 hydrogen Chemical class 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
- F04D19/046—Combinations of two or more different types of pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/16—Centrifugal pumps for displacing without appreciable compression
- F04D17/168—Pumps specially adapted to produce a vacuum
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D23/00—Other rotary non-positive-displacement pumps
- F04D23/008—Regenerative 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
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
Definitions
- the present invention relates to a vacuum pump apparatus of the type in which the discharge side of the pump is maintained at the atmospheric pressure. More particularly, the present invention is concerned with a vacuum pump apparatus of unitary construction type which is capable of producing a high level of vacuum at its suction side when used in sucking gases having small molecular weights, such as hydrogen, helium, and so forth.
- a vacuum pump apparatus of unitary construction type in which a turbo molecular pump is combined with other types of vacuum pump.
- An example of such a vacuum pump apparatus as of unitary construction type is disclosed in United States Patent No. 3,969,039.
- This pump has a plurality of stages: namely, a first stage constituted by an axial turbo-molecular pump, a second stage constituted by a spiral molecular drag pump, a third stage constituted by a centrifugal compressor, and a final stage constituted by a vortex diode pump. These stages are arranged in series within a common housing and between suction and discharge ports of the unitary-construction type vacuum pump.
- the centrifugal compressor stage and the vortex diode pump stage operate in the viscous flow region of a gas.
- the compression ratio between the centrifugal compressor stage and across the vortex diode pump stage vary depending on the molecular weight of the gas flowing through these pumps. In general, the greater the molecular weight, the greater the compression reatio and, the smaller the molecular weight, the smaller the compression ratio.
- the compression ratio across the stages constituted by the centrifugal compression pump and the vortex diode pumps is so small that the axial turbo-molecular pump and the spiral molecular drag pump disposed upstream thereof are obliged to operate in the viscous flow region rather than in the intermediate or molecular flow region.
- the compression ratio across the vaccum pump is too small accordingly. That is, the vacuum pump apparatus cannot establish the desired very level of vacuum when it is used for sucking a gas having a comparatively small molecular weight.
- the prior art has not paid any attention to this point.
- a vacuum pump apparatus having a plurality of pump stages of different types arranged in series between suction and discharge ports of a housing and a gas passage means through which a gas different from the gas sucked through the suction port is introduced into the pump stage which is spaced downstream from the suction port by more than one pump stage.
- a vacuum pump apparatus having a plurality of pump stages of different types arranged in series between suction and discharge ports in a housing and a gas passage means through which a gas different from the gas sucked through the suction port is introduced into the pump stage which operates in viscous flow region.
- a rotary shaft 1 extends through a housing 4 having a suction port 2 and a discharge port 3.
- the shaft 1 is rotatably supported by the housing 4 through bearings 18 and is connected at its lower end to a motor 19.
- a centrifugal compressor stage 5 and a circumferential-flow pump stage 6 are arranged in series in the housing 4 between the suction port 2 and the discharge port 3.
- the centrifugal compressor stage 5 has open-type impellers 7 mounted on the shaft 1 and stationary disks 8 which are fixed to the inner surface of the housing 4.
- the impellers 7 and the stationary disks 8 are arranged alternately in the axial direction.
- each impeller 7 has one side provided with a plurality of vanes 9 which are curved such that they progressively approach the axis of rotation of the impeller 7 as viewed in the direction of rotation.
- Figs. 2 to 3 each impeller 7 has one side provided with a plurality of vanes 9 which are curved such that they progressively approach the axis of rotation of the impeller 7 as viewed in the direction of rotation.
- each stationary disk 8 is provided with a plurality of stationary vanes 10 which are formed on the surface thereof which faces the rear surface of the adjacent impeller 7, i.e., the surface of the impeller 7 having no vane.
- the stationary vanes 10 also are curved such that they progressively approach the axis of rotation as viewed in the direction of rotation of the impeller 7.
- the circumferential-flow pump stage 6 has a plurality of impellers 12 mounted on the shaft 1 and a plurality of stationary disks 13 fixed to the inner surface of the housing 4.
- the impellers 12 and the stationary disks 13 are arranged alternately in the axial direction.
- Each impeller 12 has one side provided with a plurality of radial vanes 11 formed in its radially outer peripheral zone, while each stationary disk 13 is provided with a circumferentially extending groove 14 of a U-shaped section formed in the surface thereof facing the radial vanes 11 on an adjacent impeller 12.
- a port 15 is formed in each stationary disk 13 at one terminal end of the U-shaped groove 14.
- the port 15 and the groove 14 constitute a gas passage 16.
- a reference numeral 17 designates a member such as a pipe which provides a communication between a gas inlet 4a formed in the housing 14 and a port 13a formed in the stationary disk 13 of the first stage of the circumferential-flow pump stage 6.
- the arrangement is such that a gas of a small molecular weight which is to be pumped by the vacuum pump apparatus is sucked through the suction port 2, while another kind of gas having a greater molecular weight is introduced into the inlet side of the circumferential-flow pump stage 6 from the gas inlet 4a in the housing 4 through the pipe 17.
- the circumferential-flow compression pump stage 6 In operation, when the gas sucked through the suction port 2 has a large molecular weight as in the case of air or nitrogen, the circumferential-flow compression pump stage 6 operates in the viscous flow region so that a large compression ratio is obtained across each stage of the circumferential-flow compression pump 6. In consequence, a high level of vacuum, say less than several Torr., is established at the inlet side of the circumferential-flow compression stage. 6. This in turn causes the centrifugal compressor stage 5 to operate as a spiral molecular drag pump in the intermediate flow region or molecular flow region so as to develop a large pressure difference across this stage. Consequently, a very high level of vacuum on the order of 10 ⁇ 3 to 10 ⁇ 4 Torr. is established at the inlet port 2 of the vacuum pump apparatus.
- the molecular weight and the specific heat ratio of air are 29 and 1.4, respectively, while those of helium gas are 4 and 1.67, respectively.
- a compression pump stage can produce a compression ratio of 2 when it compresses air at 20°C. If the same pump stage is used for helium gas, the compression ratio is as small as 1.11.
- a vacuum pump system is constituted by 8 (eight) such stages and that the discharge pressure is the atmospheric pressure, the pressure levels at the suction side of the vacuum pump system are 3 Torr. for air and 300 Torr. for helium gas.
- the conventional vacuum pump system could not provide very high degree of vacuum when used for pumping gases of small molecular weights.
- this problem is overcome by introducing a gas of a larger molecular weight than the gas sucked through the suction port 2, e.g., nitrogen or air into one of the compression pump stages which is spaced downstream from the suction port 2 by more than one stage, i.e., into the circumferential-flow compression pump stage 6, through the pipe 17 connected between the gas inlet 4a provided in the wall of the housing 4 and the inlet port 13a in the stationary disk 13 of the first stage of the circumferential-flow compression pump stage 6.
- the gas having large molecular weight advantageously increases the compression ratios across subsequent stages, so that a high degree of vacuum is established at the suction side of the vacuum pump apparatus.
- the gas of the larger molecular weight introduced through the pipe 17 causes the circumferential-flow compression pump stage 6 to operate in the viscous flow region, so that the pressure at the inlet side of this pump stage 6 can be lowered to several Torr.
- the flow through this pump stage becomes to be equal to the total of the amount of the gas supplied and the amount of the gas discharged, with a result that the pumping effect of this pump stage is lowered undesirably. It will be understood that, by supplying a gas of a large molecular weight in the viscous flow region, it is possible to enable the pump stage to operate to pump a gas of small molecular weight with a large compression ratio and a high efficiency.
- Figs. 8 to 10 show another embodiment of the vacuum pump apparatus according to the present invention.
- This embodiment comprises a first pump stage constituted by a spiral molecular drag pump 20, an intermediate stage constituted by a centrifugal compression pump or compressor 5 and a final stage constituted by a circumferential-flow compression pump 6.
- the pump stages are arranged between the suction port 2 and the discharge port 3 within the housing 4.
- a gas passage 17 provides a communication between a gas inlet 4a formed in the housing 4 and the inlet side of the centrifugal compressor stage 5.
- the constructions of the centrifugal compressor stage 5 and the circumferential-flow compression pump stage 6 are the same as those in the first embodiment and, therefore, detailed description thereof is omitted.
- the spiral molecular drag pump 20 has rotary disks 21 fixed to the rotary shaft 1 and stationary disks 22 fixed to the inner surface of the housing 4.
- the rotary disks 21 and the stationary disks 22 are arranged alternately in the direction of the axis of the rotary shaft 1.
- Each of the stationary disks 22 is provided with a spiral groove 23 formed in the surface thereof facing the adjacent rotary disk 21.
- the gas passage 17 may alternatively be connected to the inlet side of the circumferential-flow compression pump stage 6 constituting the final stage, rather than to the inlet side of the centrifugal compressor stage 5 as in the illustrated embodiment.
- each pump stage of the vacuum pump apparatus can produce large compression ratio due to introduction of a gas having a large molecular weight into an intermediate or final pump stage, so that a high degree of vacuum can be obtained at the suction side of the vacuum pump apparatus even when a gas sucked through the suction port has a small molecular weight.
Abstract
Description
- The present invention relates to a vacuum pump apparatus of the type in which the discharge side of the pump is maintained at the atmospheric pressure. More particularly, the present invention is concerned with a vacuum pump apparatus of unitary construction type which is capable of producing a high level of vacuum at its suction side when used in sucking gases having small molecular weights, such as hydrogen, helium, and so forth.
- High levels of vacuum are often required in various field of technology such as nuclear fusion, semi-conductor manufacture, electron-microscopic examination, and so on. Hitherto, turbo molecular pump apparatus, which exhibit superior throughput characteristics in the molecular flow region, have been used for establishing such high levels of vacuum. Unfortunately, however, the turbo molecular pump apparatus have a drawback that the throughput characteristics of this type of pump largely depends on the pressure at the discharge side thereof. For instance, in order that a turbo molecular pump apparatus may create the required high level of vacuum, it is necessary that a high vacuum on the order of 10⁻² to 10⁻³ Torr. has to be maintained at the discharge side of this pump. To this end, an auxiliary vacuum pump is required so as to establish a high vacuum at the discharge side of the molecular pump in advance of the operation of the molecular pump. Usually, a rotary vacuum pump is used as the auxiliary vacuum pump.
- In consequence, the overall size of the vacuum pump apparatus incorporating a turbo molecular pump is increased and the control of such apparatus is complicated due to the present of the auxiliary vacuum pump. This undersirably limits the use of a turbo molecular pump which inherently is capable of establishing a high level of vacuum.
- This in turn gives rise to a demand for a vacuum pump apparatus of unitary construction type in which a turbo molecular pump is combined with other types of vacuum pump. An example of such a vacuum pump apparatus as of unitary construction type is disclosed in United States Patent No. 3,969,039. This pump has a plurality of stages: namely, a first stage constituted by an axial turbo-molecular pump, a second stage constituted by a spiral molecular drag pump, a third stage constituted by a centrifugal compressor, and a final stage constituted by a vortex diode pump. These stages are arranged in series within a common housing and between suction and discharge ports of the unitary-construction type vacuum pump.
- The centrifugal compressor stage and the vortex diode pump stage operate in the viscous flow region of a gas. Provided that the factors such as the shapes of impellers, vanes and so forth, as well as the rotational speed of a shaft, are the same, the compression ratio between the centrifugal compressor stage and across the vortex diode pump stage vary depending on the molecular weight of the gas flowing through these pumps. In general, the greater the molecular weight, the greater the compression reatio and, the smaller the molecular weight, the smaller the compression ratio.
- In the prior art vacuum pump apparatus of the unitary-construction type referred to above, therefore, a high compression ratio is obtained across the centrifugal compressor stage and across the vortex diode pump stage particularly when a gas sucked through the suction port has a large molecular weight as in the case of nitrogen, air, and so forth. In such a case, the axial turbo-molecular pump and the spiral molecular drag pump, which are disposed upstream of the centrifugal compressor stage, can operate in an intermediate flow region or molecular flow region, so that a high level of vacuum is established at the suction port of the vacuum pump.
- However, when the gas sucked by the vacuum pump has a small molecular weight as in the case of hydrogen or helium, the compression ratio across the stages constituted by the centrifugal compression pump and the vortex diode pumps is so small that the axial turbo-molecular pump and the spiral molecular drag pump disposed upstream thereof are obliged to operate in the viscous flow region rather than in the intermediate or molecular flow region. In such a case, the compression ratio across the vaccum pump is too small accordingly. That is, the vacuum pump apparatus cannot establish the desired very level of vacuum when it is used for sucking a gas having a comparatively small molecular weight. The prior art has not paid any attention to this point.
- According to one feature of the present invention, there is provided a vacuum pump apparatus having a plurality of pump stages of different types arranged in series between suction and discharge ports of a housing and a gas passage means through which a gas different from the gas sucked through the suction port is introduced into the pump stage which is spaced downstream from the suction port by more than one pump stage.
- According to another feature of the invention, there is also provided a vacuum pump apparatus having a plurality of pump stages of different types arranged in series between suction and discharge ports in a housing and a gas passage means through which a gas different from the gas sucked through the suction port is introduced into the pump stage which operates in viscous flow region.
- By these features of the present invention, because a gas having a greater molecular weight can be introduced through the gas passage into an intermediate pump stage, it is possible to obtain a large compression ratio across each pump stage and, thus, establish a high level of vacuum at the suction port of the vacuum pump apparatus even when the gas sucked through the suction port has a small molecular weight.
- The above and other objects, features and advantages of the present invention will be made more apparent by the following description with reference to the accompanying drawings.
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- Fig. 1 is an axial sectional view of an embodiment of a vacuum pump apparatus in accordance with the present invention;
- Fig. 2 is an enlarged fragmentary view of an essential portion of a centrifugal compression pump stage in the vacuum pump apparatus embodying the present invention;
- Fig. 3 is an end view of an impeller of the centrifugal compressor stage taken in the direction of an arrow III shown in Fig. 2;
- Fig. 4 is an end view of a stationary disk in the centrifugal compressor stage taken in the direction of an arrow IV shown in Fig. 2;
- Fig. 5 is an enlarged fragmentary sectional view of an essential portion of a circumferential-flow compression pump stage incorporated in the vacuum pump apparatus embodying the present invention;
- Fig. 6 is an end view of an impeller of the circumferential-flow compressoin pump taken in the direction of an arrow VI in Fig. 5;
- Fig. 7 is an end view of a stationary disk of the circumferential-flow compression pump taken in the direction of an arrow VII in Fig. 5;
- Fig. 8 is an axial sectional view of another embodiment of the vacuum pump apparatus in accordance with the present invention;
- Fig. 9 is an enlarged fragmentary sectional view of an essential portion of a spiral molecular drag pump incorporated in the vacuum pump apparatus embodying the present invention; and
- Fig. 10 is a plan view of a stationary disk of the spiral molecular drag pump shown in Fig. 9.
- Preferred embodiments of the vacuum pump apparatus of the present invention will be described hereinunder with reference to the accompanying drawings.
- Referring first to Fig. 1 which is an axial sectional view of an embodiment of the vacuum pump apparatus of the invention, a
rotary shaft 1 extends through ahousing 4 having asuction port 2 and adischarge port 3. Theshaft 1 is rotatably supported by thehousing 4 throughbearings 18 and is connected at its lower end to amotor 19. A centrifugal compressor stage 5 and a circumferential-flow pump stage 6 are arranged in series in thehousing 4 between thesuction port 2 and thedischarge port 3. - The centrifugal compressor stage 5 has open-
type impellers 7 mounted on theshaft 1 andstationary disks 8 which are fixed to the inner surface of thehousing 4. Theimpellers 7 and thestationary disks 8 are arranged alternately in the axial direction. As will be seen in Figs. 2 to 3, eachimpeller 7 has one side provided with a plurality ofvanes 9 which are curved such that they progressively approach the axis of rotation of theimpeller 7 as viewed in the direction of rotation. Similarly, as will be seen in Figs. 2 and 4, eachstationary disk 8 is provided with a plurality ofstationary vanes 10 which are formed on the surface thereof which faces the rear surface of theadjacent impeller 7, i.e., the surface of theimpeller 7 having no vane. Thestationary vanes 10 also are curved such that they progressively approach the axis of rotation as viewed in the direction of rotation of theimpeller 7. - As shown in Figs. 5 to 7, the circumferential-
flow pump stage 6 has a plurality ofimpellers 12 mounted on theshaft 1 and a plurality ofstationary disks 13 fixed to the inner surface of thehousing 4. Theimpellers 12 and thestationary disks 13 are arranged alternately in the axial direction. Eachimpeller 12 has one side provided with a plurality of radial vanes 11 formed in its radially outer peripheral zone, while eachstationary disk 13 is provided with a circumferentially extendinggroove 14 of a U-shaped section formed in the surface thereof facing the radial vanes 11 on anadjacent impeller 12. As shown in Figs. 5 and 7, aport 15 is formed in eachstationary disk 13 at one terminal end of theU-shaped groove 14. Theport 15 and thegroove 14 constitute agas passage 16. - A
reference numeral 17 designates a member such as a pipe which provides a communication between agas inlet 4a formed in thehousing 14 and aport 13a formed in thestationary disk 13 of the first stage of the circumferential-flow pump stage 6. The arrangement is such that a gas of a small molecular weight which is to be pumped by the vacuum pump apparatus is sucked through thesuction port 2, while another kind of gas having a greater molecular weight is introduced into the inlet side of the circumferential-flow pump stage 6 from thegas inlet 4a in thehousing 4 through thepipe 17. - In operation, when the gas sucked through the
suction port 2 has a large molecular weight as in the case of air or nitrogen, the circumferential-flowcompression pump stage 6 operates in the viscous flow region so that a large compression ratio is obtained across each stage of the circumferential-flow compression pump 6. In consequence, a high level of vacuum, say less than several Torr., is established at the inlet side of the circumferential-flow compression stage. 6. This in turn causes the centrifugal compressor stage 5 to operate as a spiral molecular drag pump in the intermediate flow region or molecular flow region so as to develop a large pressure difference across this stage. Consequently, a very high level of vacuum on the order of 10⁻³ to 10⁻⁴ Torr. is established at theinlet port 2 of the vacuum pump apparatus. - On the other hand, when the gas sucked through the
suction port 2 of the vacuum pump apparatus has a small molecular weight as in the case of hydrogen, helium or the like, only a small compression ratio is developed across the circumferential-flowcompression pump stage 6, so that the pressure at the inlet side of the circumferential-flow compression pump stage is as high as several tens to several hundreds of Torr. In this case, the centrifugal compressor stage 5 also operates in the viscous flow region, so that it cannot work as the spiral molecular drag pump. This means that the compression ratio obtained across the centrifugal compressor stage is not so large, with the result that the pressure at thesuction port 2 of the vacuum pump apparatus is still as high as several to several tens of Torr. - A description will be made hereinunder as to the reason why the vacuum pump apparatus fails to create a high level of vacuum when the pumped gas has a small molecular weight.
- Generally, when a centrifugal compressor and a circumferential-flow compression pump operate in the viscous flow region, these pumps function as compressors of turbine type, and the following relationship exists between the compression ratio π and adiabatic head Had:
- In the described embodiment of the invention, this problem is overcome by introducing a gas of a larger molecular weight than the gas sucked through the
suction port 2, e.g., nitrogen or air into one of the compression pump stages which is spaced downstream from thesuction port 2 by more than one stage, i.e., into the circumferential-flowcompression pump stage 6, through thepipe 17 connected between thegas inlet 4a provided in the wall of thehousing 4 and theinlet port 13a in thestationary disk 13 of the first stage of the circumferential-flowcompression pump stage 6. The gas having large molecular weight advantageously increases the compression ratios across subsequent stages, so that a high degree of vacuum is established at the suction side of the vacuum pump apparatus. - Namely, the gas of the larger molecular weight introduced through the
pipe 17 causes the circumferential-flowcompression pump stage 6 to operate in the viscous flow region, so that the pressure at the inlet side of thispump stage 6 can be lowered to several Torr. This in turn permits the centrifugal compression pump stage 5 to operate in the intermediate or molecular flow region, so that the pressure at the suction side of this pump stage 5 can be lowered to a high degree of vacuum on the order of 10⁻² to 10⁻³ Torr. It is thus possible to create the desired high degree of vacuum even when the gas pumped by the vacuum pump apparatus has a small molecular weight. - The reason why a gas which has a greater molecular weight than that of the gas sucked through the suction port of the vacuum pump apparatus is introduced into the pump stage which inherently operates in the viscous flow region will be described hereinunder. If a gas supplied to the pump stage which inherently operates mainly in the viscous flow region has a small molecular weight, the pump stage which inherently operates in the intermediate or molecular flow region cannot provide a required high compression ratio. On the other hand, if a gas having a large molecular weight is introduced into the pump stage which inherently operates in the intermediate or molecular flow region, the pump stage provides a large compression ratio. However, the flow through this pump stage becomes to be equal to the total of the amount of the gas supplied and the amount of the gas discharged, with a result that the pumping effect of this pump stage is lowered undesirably. It will be understood that, by supplying a gas of a large molecular weight in the viscous flow region, it is possible to enable the pump stage to operate to pump a gas of small molecular weight with a large compression ratio and a high efficiency.
- Figs. 8 to 10 show another embodiment of the vacuum pump apparatus according to the present invention. This embodiment comprises a first pump stage constituted by a spiral
molecular drag pump 20, an intermediate stage constituted by a centrifugal compression pump or compressor 5 and a final stage constituted by a circumferential-flow compression pump 6. The pump stages are arranged between thesuction port 2 and thedischarge port 3 within thehousing 4. Agas passage 17 provides a communication between agas inlet 4a formed in thehousing 4 and the inlet side of the centrifugal compressor stage 5. The constructions of the centrifugal compressor stage 5 and the circumferential-flowcompression pump stage 6 are the same as those in the first embodiment and, therefore, detailed description thereof is omitted. - The spiral molecular drag pump 20 has
rotary disks 21 fixed to therotary shaft 1 andstationary disks 22 fixed to the inner surface of thehousing 4. Therotary disks 21 and thestationary disks 22 are arranged alternately in the direction of the axis of therotary shaft 1. Each of thestationary disks 22 is provided with aspiral groove 23 formed in the surface thereof facing theadjacent rotary disk 21. - The
gas passage 17 may alternatively be connected to the inlet side of the circumferential-flowcompression pump stage 6 constituting the final stage, rather than to the inlet side of the centrifugal compressor stage 5 as in the illustrated embodiment. - In operation, when the gas sucked through the
suction port 2 of the vacuum pump apparatus has a small molecular weight, another gas of a larger molecular weight is simultaneously introduced into the inlet side of the centrifugal compressor stage 5 through thegas passage 17. In consequence, the centrifugal compressor stage 5 and the circumferential-flowcompression pump stage 6 are allowed to operate in the viscous flow region and thus produce large compression ratios across these stages, so that the pressure at the inlet side of the centrifugal compression pump stage 5 is lowered to several Torr. This in turn enables the spiral molecular drag pump 20 to operate in the intermediate or molecular flow region so as to establish a desired high degree of vacuum, say 10⁻² to 10⁻³ Torr. at the inlet side thereof, i.e., at the suction side of the vacuum pump apparatus. - As has been described, according to the invention, each pump stage of the vacuum pump apparatus can produce large compression ratio due to introduction of a gas having a large molecular weight into an intermediate or final pump stage, so that a high degree of vacuum can be obtained at the suction side of the vacuum pump apparatus even when a gas sucked through the suction port has a small molecular weight.
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP25271185A JPS62113887A (en) | 1985-11-13 | 1985-11-13 | Vacuum pump |
JP252711/85 | 1985-11-13 |
Publications (1)
Publication Number | Publication Date |
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EP0226039A1 true EP0226039A1 (en) | 1987-06-24 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86115640A Withdrawn EP0226039A1 (en) | 1985-11-13 | 1986-11-11 | Vacuum pump apparatus |
Country Status (2)
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EP (1) | EP0226039A1 (en) |
JP (1) | JPS62113887A (en) |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2208895A (en) * | 1987-08-24 | 1989-04-19 | Pfeiffer Vakuumtechnik | Multi-stage molecular pump |
EP0340685A2 (en) * | 1988-04-30 | 1989-11-08 | Nippon Ferrofluidics Corporation | Composite vacuum pump |
EP0445855A1 (en) * | 1990-03-09 | 1991-09-11 | VARIAN S.p.A. | Improved turbomolecular pump |
US5238362A (en) * | 1990-03-09 | 1993-08-24 | Varian Associates, Inc. | Turbomolecular pump |
EP0643227A1 (en) * | 1993-09-10 | 1995-03-15 | The BOC Group plc | Vacuum pumps |
EP0731278A1 (en) * | 1995-03-10 | 1996-09-11 | Balzers-Pfeiffer GmbH | Molecular vacuum pump with cooling gas device |
EP0959253A2 (en) * | 1998-05-20 | 1999-11-24 | The BOC Group plc | Vacuum pump |
GB2360066A (en) * | 2000-03-06 | 2001-09-12 | Boc Group Plc | Vacuum pump |
EP1363027A1 (en) * | 1996-05-03 | 2003-11-19 | The BOC Group plc | Vacuum pump |
WO2004055378A1 (en) * | 2002-12-17 | 2004-07-01 | The Boc Group Plc | Vacuum pumping arrangement and method of operating same |
WO2008142435A1 (en) * | 2007-05-18 | 2008-11-27 | Edwards Limited | Method of operating a lithography tool |
US7645116B2 (en) * | 2005-04-28 | 2010-01-12 | Ebara Corporation | Turbo vacuum pump |
WO2015132196A1 (en) * | 2014-03-03 | 2015-09-11 | Nuovo Pignone Srl | Method and system for operating a back-to-back compressor with a side stream |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2559436B2 (en) * | 1987-12-23 | 1996-12-04 | 株式会社日立製作所 | Vacuum pump with gas purge |
US5020969A (en) * | 1988-09-28 | 1991-06-04 | Hitachi, Ltd. | Turbo vacuum pump |
Citations (4)
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DE2408257A1 (en) * | 1974-02-21 | 1975-09-04 | Leybold Heraeus Gmbh & Co Kg | Turbo molecular vacuum pump with first stage auxiliary pump - admits gas with molecular weight above 10 on pre-vacuum side |
DE2507430A1 (en) * | 1975-02-21 | 1976-08-26 | Franz Josef Dipl Phys Schittke | Hybrid type molecular vacuum pump - has high density gas bled in on inlet to increase compression ration and efficiency of pumping action |
DE2526164A1 (en) * | 1975-06-12 | 1976-12-30 | Leybold Heraeus Gmbh & Co Kg | Turbo molecular vacuum pump - has means for gas inlet to ring shaped channel between stator and bell shaped rotor inner surface |
EP0143684A1 (en) * | 1983-10-25 | 1985-06-05 | Bertin & Cie | Multi-stage series compressor |
-
1985
- 1985-11-13 JP JP25271185A patent/JPS62113887A/en active Pending
-
1986
- 1986-11-11 EP EP86115640A patent/EP0226039A1/en not_active Withdrawn
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2408257A1 (en) * | 1974-02-21 | 1975-09-04 | Leybold Heraeus Gmbh & Co Kg | Turbo molecular vacuum pump with first stage auxiliary pump - admits gas with molecular weight above 10 on pre-vacuum side |
DE2507430A1 (en) * | 1975-02-21 | 1976-08-26 | Franz Josef Dipl Phys Schittke | Hybrid type molecular vacuum pump - has high density gas bled in on inlet to increase compression ration and efficiency of pumping action |
DE2526164A1 (en) * | 1975-06-12 | 1976-12-30 | Leybold Heraeus Gmbh & Co Kg | Turbo molecular vacuum pump - has means for gas inlet to ring shaped channel between stator and bell shaped rotor inner surface |
EP0143684A1 (en) * | 1983-10-25 | 1985-06-05 | Bertin & Cie | Multi-stage series compressor |
Cited By (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2208895A (en) * | 1987-08-24 | 1989-04-19 | Pfeiffer Vakuumtechnik | Multi-stage molecular pump |
GB2208895B (en) * | 1987-08-24 | 1991-01-23 | Pfeiffer Vakuumtechnik | Multi-stage molecular pump |
EP0340685A2 (en) * | 1988-04-30 | 1989-11-08 | Nippon Ferrofluidics Corporation | Composite vacuum pump |
EP0340685A3 (en) * | 1988-04-30 | 1990-08-01 | Nippon Ferrofluidics Corporation | Composite vacuum pump |
EP0445855A1 (en) * | 1990-03-09 | 1991-09-11 | VARIAN S.p.A. | Improved turbomolecular pump |
US5238362A (en) * | 1990-03-09 | 1993-08-24 | Varian Associates, Inc. | Turbomolecular pump |
EP0643227A1 (en) * | 1993-09-10 | 1995-03-15 | The BOC Group plc | Vacuum pumps |
US5611660A (en) * | 1993-09-10 | 1997-03-18 | The Boc Group Plc | Compound vacuum pumps |
EP0731278A1 (en) * | 1995-03-10 | 1996-09-11 | Balzers-Pfeiffer GmbH | Molecular vacuum pump with cooling gas device |
EP1363027A1 (en) * | 1996-05-03 | 2003-11-19 | The BOC Group plc | Vacuum pump |
EP0959253A3 (en) * | 1998-05-20 | 2001-03-14 | The BOC Group plc | Vacuum pump |
EP0959253A2 (en) * | 1998-05-20 | 1999-11-24 | The BOC Group plc | Vacuum pump |
GB2360066A (en) * | 2000-03-06 | 2001-09-12 | Boc Group Plc | Vacuum pump |
WO2004055378A1 (en) * | 2002-12-17 | 2004-07-01 | The Boc Group Plc | Vacuum pumping arrangement and method of operating same |
US7645116B2 (en) * | 2005-04-28 | 2010-01-12 | Ebara Corporation | Turbo vacuum pump |
US7938619B2 (en) | 2005-04-28 | 2011-05-10 | Ebara Corporation | Turbo vacuum pump |
WO2008142435A1 (en) * | 2007-05-18 | 2008-11-27 | Edwards Limited | Method of operating a lithography tool |
WO2015132196A1 (en) * | 2014-03-03 | 2015-09-11 | Nuovo Pignone Srl | Method and system for operating a back-to-back compressor with a side stream |
CN106062374A (en) * | 2014-03-03 | 2016-10-26 | 诺沃皮尼奥内股份有限公司 | Method and system for operating a back-to-back compressor with a side stream |
RU2667563C2 (en) * | 2014-03-03 | 2018-09-21 | Нуово Пиньоне СРЛ | Method and system for operating back-to-back compressor with side stream |
CN106062374B (en) * | 2014-03-03 | 2019-09-10 | 诺沃皮尼奥内股份有限公司 | For running the method and system for having the back-to-back compressor of effluent |
US10473109B2 (en) | 2014-03-03 | 2019-11-12 | Nuovo Pignone Srl | Method and system for operating a back-to-back compressor with a side stream |
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Inventor name: IKEMURA, KAZUHIKOHITACHI KOMEIRYO Inventor name: GYOBU, ICHIRO Inventor name: MASE, MASAHIRO Inventor name: NAGAOKA, TAKASHI |