US3826588A - Turbomolecular vacuum pump - Google Patents
Turbomolecular vacuum pump Download PDFInfo
- Publication number
- US3826588A US3826588A US00371372A US37137273A US3826588A US 3826588 A US3826588 A US 3826588A US 00371372 A US00371372 A US 00371372A US 37137273 A US37137273 A US 37137273A US 3826588 A US3826588 A US 3826588A
- Authority
- US
- United States
- Prior art keywords
- blade
- pump
- stator
- blades
- rotor
- 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.)
- Expired - Lifetime
Links
- 230000006835 compression Effects 0.000 claims abstract description 15
- 238000007906 compression Methods 0.000 claims abstract description 15
- 230000006872 improvement Effects 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 description 4
- 230000008859 change Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/04—Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
- F04D19/042—Turbomolecular vacuum pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
- F04D29/324—Blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/541—Specially adapted for elastic fluid pumps
- F04D29/542—Bladed diffusers
- F04D29/544—Blade shapes
Definitions
- This invention relates to a turbomolecular vacuum pump of the type that has a stator to which there are affixed stator blade wheels and a rotor carrying rotor blade wheels arid in which the stator blade wheels are in an interleavingrelationship with the rotor blade wheels.
- the pitch angle of the blades defined by their inclination with respect to the plane of the blade wheels, changes in the radial direction.
- the blade wheels of the rotor which may be driven with a high rpm, cooperate as runner wheels in a turbine-like manner with the stationary blade wheels of the stator which is affixed to the pump housing.
- the pitch angle of the blades in at leastone stage formed of a rotor blade wheel and a stator blade wheel increases radially outwardly from the attached end of the blades in such a manner that the compression ratio of that pump stage remains at least approximately constant at radially different locations.
- FIG. 1 of three circumferentially successive blades belonging to the same rotor blade wheel.
- FIGS. 5a and 5b illustrate plan views of parts of rotor blades with different blade distances.
- FIGS. 6, 7 and 8 illustrate developed sections as in FIGS. 2, 3, and 4, wherein the blade widths are radially constant.
- FIG. 1 there is illustrated a stator 1 which is rigidly affixed to the pump housing and which surrounds a rotor 2'supported for rotation about a vertical axis 6. To the stator 1 there are affixed stator blade wheels 3 whereas the rotor 2 is provided with rotor blade wheels 4. To the housing, 1, at the high vacuum side of the pump, there is attached a coupling flange 5. Further technical details of this pump with regard to drive means, seals and rotor supports are considered conventional and are described, for example, in Garnier et al., US. Pat. No. 3,168,977.
- FIGS. 2, 3, and 4 it is seen that along the cylinder surface I (FIG. 2) the blades have, at their foot zones (that is, in the vicinity of their attachment) the small pitch angle a, of approximately 20; along the cylinder surface II (FIG. 3) the same blades have, approximately in their mid zone, an increased pitch angle a of approximately 35; and along the cylinder surface III (FIG. 4) the same blades have, in their peripheral end zones a maximum pitch angle a, of approximately 45.
- a degree of overlap (which is expressed by the ratio s:b, that is, the ratio of the distance s between two adjacent blades of the same blade wheel to the blade width b) which is approximately constant in the radial direction, the blade width b is increased radially outwardly (that is, b b b because of the radially outward increase of the blade distance s (that is, s s s
- the blades may have other shapes wherein the blade widths are radially constant.
- At least the blades of a high vacuum stage are, at least in their peripheral zone, not in an optical overlap, that is, s/b 1.
- the change of the blade pitch angle may expediently be continuous at least along subsequent length portions in the radial direction.
- FIG. A illustrates a part of a rotor blade having continuously changing blade distances s s and s and blade widths b b and b
- the dimensions s and b that have identical index numbers are measured along the same circle concentric with the blade wheel.
- the blades may be advantageously made in such a manner that the change of the pitch angle is periodically discontinued. This may be accomplished, for example, by twisting the blade in different pitch angle zones.
- Such a rotor blade is shown in FIG. 512. Between the lines A, B, C, and D are zones with different in each zone constant pitch angle. The number of zones can be changed.
- both the stator and v the rotor blade wheels have radially outwardly increasing pitch angles.
- the blade wheels may be made of circular, radially slotted stamped sheet metal according to known manufacturing methods.
- the invention is not limited to the single-flow turbomolecular vacuum pump with vertically arranged rotors in accordance with the described embodiment, but it may also find application in known two-flow structures in which the rotor in general is arranged to be rotated about a horizontal axis.
- each stator blade wheel being formed of a plurality of circumferentially spaced stator blades each having one end attached to said stator and each extending in a radial direction with respect to said axis, a rotor arranged axially coextensive with said stator, a plurality of axially spaced rotor blade wheels carried by said rotor, each rotor blade wheel being formed of a plurality of circumferentially spaced rotor blades each having one end attached to said rotor and each extending in a radial direction, each blade having a pitch angle defined by the inclination of the blade to the plane of the blade wheel, said stator blade wheels being in an interleaving relationship with said rotor blade wheels, each stator blade wheel forming a pump stage with an adjacent, cooperating rotor blade
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Non-Positive Displacement Air Blowers (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2229724A DE2229724B2 (de) | 1972-06-19 | 1972-06-19 | Turbomolekularpumpe |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3826588A true US3826588A (en) | 1974-07-30 |
Family
ID=5848074
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00371372A Expired - Lifetime US3826588A (en) | 1972-06-19 | 1973-06-19 | Turbomolecular vacuum pump |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3826588A (en:Method) |
| CH (1) | CH564692A5 (en:Method) |
| DE (1) | DE2229724B2 (en:Method) |
| FR (1) | FR2190184A5 (en:Method) |
| GB (1) | GB1397179A (en:Method) |
Cited By (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4108620A (en) * | 1975-04-24 | 1978-08-22 | Battelle-Institut E.V. | Device for the separation of gaseous mixtures into components of different molecular mass |
| US4422822A (en) * | 1980-08-11 | 1983-12-27 | Norman Milleron | Rotating fiber array molecular driver and molecular momentum transfer device constructed therewith |
| US5033936A (en) * | 1988-08-24 | 1991-07-23 | Seiko Seiki Kabushiki Kaisha | Rotor blades of turbomolecular pump |
| US5052887A (en) * | 1988-02-26 | 1991-10-01 | Novikov Nikolai M | Turbomolecular vacuum pump |
| US5158426A (en) * | 1990-02-16 | 1992-10-27 | Varian Associates, Inc. | Stator assembly for a turbomolecular pump |
| US5188514A (en) * | 1989-11-03 | 1993-02-23 | Varian Associates, Inc. | Process for manufacturing an impeller by electrical discharge machining and articles so obtained |
| US5528618A (en) * | 1992-09-23 | 1996-06-18 | The United States Of America As Represented By The Secretary Of The Air Force | Photolytic iodine laser system with turbo-molecular blower |
| EP0829645A3 (en) * | 1996-09-12 | 1998-11-11 | Seiko Seiki Kabushiki Kaisha | Turbomolecular pump |
| EP1041287A3 (en) * | 1999-03-31 | 2002-01-16 | Seiko Seiki Kabushiki Kaisha | Vacuum pump |
| US6474940B1 (en) * | 1998-06-17 | 2002-11-05 | Seiko Instruments Inc. | Turbo molecular pump |
| US20040091351A1 (en) * | 2000-09-20 | 2004-05-13 | Ralf Adamietz | Turbomolecular vacuum pump with rows of rotor blades and rows of stator blades |
| US20110064562A1 (en) * | 2008-02-15 | 2011-03-17 | Shimadzu Corporation | Turbomolecular Pump |
| US20140205432A1 (en) * | 2013-01-22 | 2014-07-24 | Agilent Technologies, Inc. | Rotary vacuum pump |
| CN104047871A (zh) * | 2013-03-13 | 2014-09-17 | 株式会社岛津制作所 | 真空泵 |
| EP2341251B1 (en) | 2008-10-03 | 2018-12-26 | Shimadzu Corporation | Turbo-molecular pump |
| JP2020505546A (ja) * | 2017-01-20 | 2020-02-20 | エドワーズ リミテッド | 段間入口を有する多段ターボ分子ポンプ |
| CN111503021A (zh) * | 2019-01-30 | 2020-08-07 | 株式会社岛津制作所 | 涡轮分子泵 |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2128687B (en) * | 1982-10-13 | 1986-10-29 | Rolls Royce | Rotor or stator blade for an axial flow compressor |
| DE3317868A1 (de) * | 1983-05-17 | 1984-11-22 | Leybold-Heraeus GmbH, 5000 Köln | Reibungspumpe |
| DE3507274A1 (de) * | 1985-03-01 | 1986-09-04 | Arthur Pfeiffer Vakuumtechnik Wetzlar Gmbh, 6334 Asslar | Scheiben mit schaufeln hoher stabilitaet fuer turbomolekularpumpen |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3748055A (en) * | 1970-07-15 | 1973-07-24 | W Becker | Rotor and stator wheel construction for a turbo molecular pump |
-
1972
- 1972-06-19 DE DE2229724A patent/DE2229724B2/de not_active Withdrawn
-
1973
- 1973-03-28 CH CH448873A patent/CH564692A5/xx not_active IP Right Cessation
- 1973-06-15 FR FR7322024A patent/FR2190184A5/fr not_active Expired
- 1973-06-18 GB GB2890673A patent/GB1397179A/en not_active Expired
- 1973-06-19 US US00371372A patent/US3826588A/en not_active Expired - Lifetime
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3748055A (en) * | 1970-07-15 | 1973-07-24 | W Becker | Rotor and stator wheel construction for a turbo molecular pump |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4108620A (en) * | 1975-04-24 | 1978-08-22 | Battelle-Institut E.V. | Device for the separation of gaseous mixtures into components of different molecular mass |
| US4422822A (en) * | 1980-08-11 | 1983-12-27 | Norman Milleron | Rotating fiber array molecular driver and molecular momentum transfer device constructed therewith |
| US5052887A (en) * | 1988-02-26 | 1991-10-01 | Novikov Nikolai M | Turbomolecular vacuum pump |
| US5033936A (en) * | 1988-08-24 | 1991-07-23 | Seiko Seiki Kabushiki Kaisha | Rotor blades of turbomolecular pump |
| US5188514A (en) * | 1989-11-03 | 1993-02-23 | Varian Associates, Inc. | Process for manufacturing an impeller by electrical discharge machining and articles so obtained |
| US5158426A (en) * | 1990-02-16 | 1992-10-27 | Varian Associates, Inc. | Stator assembly for a turbomolecular pump |
| US5528618A (en) * | 1992-09-23 | 1996-06-18 | The United States Of America As Represented By The Secretary Of The Air Force | Photolytic iodine laser system with turbo-molecular blower |
| EP0829645A3 (en) * | 1996-09-12 | 1998-11-11 | Seiko Seiki Kabushiki Kaisha | Turbomolecular pump |
| US6474940B1 (en) * | 1998-06-17 | 2002-11-05 | Seiko Instruments Inc. | Turbo molecular pump |
| EP1041287A3 (en) * | 1999-03-31 | 2002-01-16 | Seiko Seiki Kabushiki Kaisha | Vacuum pump |
| US20040091351A1 (en) * | 2000-09-20 | 2004-05-13 | Ralf Adamietz | Turbomolecular vacuum pump with rows of rotor blades and rows of stator blades |
| US20110064562A1 (en) * | 2008-02-15 | 2011-03-17 | Shimadzu Corporation | Turbomolecular Pump |
| US8668436B2 (en) * | 2008-02-15 | 2014-03-11 | Shimadzu Corporation | Turbomolecular pump |
| EP2341251B1 (en) | 2008-10-03 | 2018-12-26 | Shimadzu Corporation | Turbo-molecular pump |
| US20140205432A1 (en) * | 2013-01-22 | 2014-07-24 | Agilent Technologies, Inc. | Rotary vacuum pump |
| US9670931B2 (en) * | 2013-01-22 | 2017-06-06 | Agilent Technologies Inc. | Rotary vacuum pump |
| CN104047871A (zh) * | 2013-03-13 | 2014-09-17 | 株式会社岛津制作所 | 真空泵 |
| JP2020505546A (ja) * | 2017-01-20 | 2020-02-20 | エドワーズ リミテッド | 段間入口を有する多段ターボ分子ポンプ |
| CN111503021A (zh) * | 2019-01-30 | 2020-08-07 | 株式会社岛津制作所 | 涡轮分子泵 |
| US11293447B2 (en) * | 2019-01-30 | 2022-04-05 | Shimadzu Corporation | Turbo-molecular pump blade design |
Also Published As
| Publication number | Publication date |
|---|---|
| DE2229724B2 (de) | 1980-06-04 |
| FR2190184A5 (en:Method) | 1974-01-25 |
| DE2229724A1 (de) | 1974-01-10 |
| GB1397179A (en) | 1975-06-11 |
| CH564692A5 (en:Method) | 1975-07-31 |
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