JPS6385290A - Vacuum pump - Google Patents
Vacuum pumpInfo
- Publication number
- JPS6385290A JPS6385290A JP61228179A JP22817986A JPS6385290A JP S6385290 A JPS6385290 A JP S6385290A JP 61228179 A JP61228179 A JP 61228179A JP 22817986 A JP22817986 A JP 22817986A JP S6385290 A JPS6385290 A JP S6385290A
- Authority
- JP
- Japan
- Prior art keywords
- pump stage
- flow
- housing
- stage
- centrifugal
- 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.)
- Pending
Links
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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Non-Positive Displacement Air Blowers (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は、排気口を大気圧とする真空ポンプに係り、例
えば半導体製造装置における清浄な真空を作り出すのに
好適な真空ポンプに関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a vacuum pump whose exhaust port is set to atmospheric pressure, and relates to a vacuum pump suitable for creating a clean vacuum in, for example, semiconductor manufacturing equipment.
従来の真空ポンプの構造を第6図に示す、吸気口2Aと
排気口28tt備えたケーシング2内には軸受7で回転
自在に支持されたロータ1が納められている。全体は軸
流ターボ分子ポンプ段3.付加分子ポンプ4.遠心圧縮
ポンプ段5.渦流圧縮ポンプ段6を吸気口側から排気口
側へ順次連設して構成されている。The structure of a conventional vacuum pump is shown in FIG. 6. A rotor 1 rotatably supported by a bearing 7 is housed in a casing 2 having an intake port 2A and an exhaust port 28tt. The whole consists of three axial flow turbomolecular pump stages. Additional molecular pump 4. Centrifugal compression pump stage5. The vortex compression pump stages 6 are successively arranged from the intake port side to the exhaust port side.
上記の構成からなる真空ポンプを排気口2Bでの圧力が
大気圧の状態で運転し、吸気口2Aでの圧力が十分値下
した定常運転状態では、真空ポンプ内の気体の流れは、
吸気側より排気側へ向かって、分子流、中間流、粘性流
と変化する。一方、各ポンプ段が最も有効に排気作用を
する気力範囲はそれぞれ異なり、軸流ターボ分子ポンプ
段3゜付加分子ポンプ段4は分子流域で、遠心圧楠ポン
プ段5は分子流〜中間流域で、渦流圧縮ポンプ段6は中
間流〜粘性流域での性能が良いという特性を持っている
。When the vacuum pump configured as described above is operated with the pressure at the exhaust port 2B at atmospheric pressure and the pressure at the intake port 2A has dropped sufficiently, the flow of gas inside the vacuum pump is as follows.
From the intake side to the exhaust side, the flow changes to molecular flow, intermediate flow, and viscous flow. On the other hand, the air pressure range in which each pump stage is most effective for evacuation is different, with the axial flow turbomolecular pump stage 3 and the additional molecular pump stage 4 in the molecular region, and the centrifugal pressure Kusunoki pump stage 5 in the molecular flow to intermediate region. The vortex compression pump stage 6 has a characteristic of good performance in the intermediate flow to viscous region.
なお、この種の真空ポンプとして関連するものには例え
ば特開昭51−38113号が挙げら九る。Incidentally, related vacuum pumps of this type include, for example, Japanese Patent Application Laid-Open No. 51-38113.
上記従来技術による真空ポンプにおいて、過渡運転状態
など吸気口2Aでの圧力が十分低下していない状態では
、 !If:気速度が大巾に低下するという問題があっ
た。これは、吸気02人での圧力が高く軸流ターボ分子
ポンプ段3.付加分子ポンプ段4での気体の流れが中間
流、粘性流となった状態では、軸流ターボ分子ポンプ段
3.付加分子ポンプ段4における排気速度が大巾に低下
するためであり、この状態では遠心圧縮ポンプ段5と渦
流圧縮ポンプ段6で排気作用の大部分を受けもっことに
なる。このとき、遠心圧縮ポンプ段5の背圧は、渦流圧
縮ポンプ段6の性能に左右されるが。In the vacuum pump according to the above-mentioned prior art, in a state where the pressure at the intake port 2A is not sufficiently reduced, such as in a transient operating state, ! If: There was a problem that the air speed decreased drastically. This is because the pressure at the intake 02 is high and the axial flow turbomolecular pump stage 3. When the gas flow in the additional molecular pump stage 4 becomes an intermediate flow or a viscous flow, the axial flow turbo molecular pump stage 3. This is because the pumping speed in the additional molecular pump stage 4 is significantly reduced, and in this state, the centrifugal compression pump stage 5 and the vortex compression pump stage 6 take on most of the pumping action. At this time, the back pressure of the centrifugal compression pump stage 5 depends on the performance of the vortex compression pump stage 6.
本従来例で使用されているような渦流圧縮ポンプ段6は
、有効作動圧力範囲が比較的狭く、大気圧近傍の圧力範
囲での性能の低下が激しいため、十分な圧縮比が得られ
ず、遠心圧縮ポンプ段5の背圧は上昇し、遠心圧縮ポン
プ段5の性能が低下し。The vortex compression pump stage 6 used in this conventional example has a relatively narrow effective operating pressure range, and its performance deteriorates sharply in the pressure range near atmospheric pressure, making it impossible to obtain a sufficient compression ratio. The back pressure of the centrifugal compression pump stage 5 increases and the performance of the centrifugal compression pump stage 5 decreases.
排気速度が低下しやすくなる。このように、上記従来技
術は軸流ターボ分子ポンプ段3での流れが中間流となり
、渦流圧縮ポンプ段6での圧力が大気圧近傍まで上昇し
た状態での、排気速度の大巾な低下に対しては配慮がな
されておらず、真空ポンプの有効作動圧力範囲が狭いと
いう問題があった。Pumping speed tends to decrease. As described above, the above-mentioned conventional technology has a problem in that the flow in the axial turbo-molecular pump stage 3 becomes an intermediate flow and the pumping speed is drastically reduced when the pressure in the vortex compression pump stage 6 increases to near atmospheric pressure. However, there was a problem that the effective operating pressure range of the vacuum pump was narrow.
本発明の目的は、広い圧力範囲で有効に作動する真空ポ
ンプを提供することにある。An object of the present invention is to provide a vacuum pump that operates effectively over a wide pressure range.
上記目的は、分子流、中間流域におけるポンプ段として
、細流ターボ分子ポンプ段よりも高い圧力範囲で有効に
排気作用をするジーグバーンポンプ段を、軸流ターボ分
子ポンプ段の後流側に設け、さらに、ジーグバーンポン
プ段の後流側に遠心圧縮ポンプ段1円周流圧縮ポンプ段
を設けることにより達成される。The above object is to provide a Siegbahn pump stage, which effectively performs evacuation in a higher pressure range than a trickle turbo-molecular pump stage, as a pump stage in the molecular flow and intermediate region, on the downstream side of the axial-flow turbo-molecular pump stage; Furthermore, this is achieved by providing a centrifugal compression pump stage 1 and a circumferential flow compression pump stage downstream of the Siegbahn pump stage.
上記のように、真空ポンプを吸入側より軸流ターボ分子
ポンプ段、ジーグバーンポンプ段、遠心圧縮ポンプ段1
円周流圧縮ポンプ段を連設することにより構成すれば、
吸気口圧力が上昇し軸流ターボ分子ポンプ段で流れが中
間流となり排気速度が急激に低下しても、ジーグバーン
ポンプ段が同圧力範囲で有効に作動するため、真空ポン
プ全体としての排気速度の低下は小さい、また1円周流
圧縮ポンプ段は渦流圧縮ポンプ段に比べ高い圧力状態で
の圧縮性能が良いため、遠心圧縮ポンプ段の背圧を低く
維持することができ、遠心圧縮ポンプ段の性能低下を防
ぐことができる。この結果、真空ポンプを分子流域から
粘性流域までの広い圧力範囲で有効に作動させることが
可能になる。As mentioned above, the vacuum pump is installed from the suction side into the axial flow turbomolecular pump stage, the Siegbahn pump stage, and the centrifugal compression pump stage 1.
If configured by connecting circumferential flow compression pump stages,
Even if the inlet pressure rises and the flow becomes intermediate flow in the axial turbomolecular pump stage and the pumping speed decreases rapidly, the Siegbahn pump stage operates effectively within the same pressure range, so the pumping speed as a whole of the vacuum pump decreases. Since the reduction in 1-circumferential-flow compression pump stage is small, and the compression performance of the 1-circumferential-flow compression pump stage is better than that of the vortex-flow compression pump stage under high pressure conditions, the back pressure of the centrifugal compression pump stage can be maintained low, and the centrifugal compression pump stage performance can be prevented from deteriorating. As a result, the vacuum pump can be effectively operated in a wide pressure range from the molecular region to the viscous region.
以下、本発明の一実施例を第1図により説明する。第1
図は、本発明の一実施例による真空ポンプの全体構造を
示す図である。An embodiment of the present invention will be described below with reference to FIG. 1st
The figure is a diagram showing the overall structure of a vacuum pump according to an embodiment of the present invention.
第1図において、回転軸1は吸気口2人と排気口2Bを
有するハウジング2内で軸受7によって回転自在に支持
されており、前記回転軸1に取り付けられたモータ10
により駆動される。ハウジング2内には吸気口側より順
に1回転軸1に取り付けられた軸流羽根車3A(第2図
(b))とハウジング2内に固定された固定羽根3B(
第2図(C))を交互に並置して構成される細流ターボ
分子ポンプ段と、同じく回転円板9A(第3図(a))
と固定円板9B(第3図(b)を交互に並置して構成さ
れるジーグバーンポンプ段9と。In FIG. 1, a rotating shaft 1 is rotatably supported by a bearing 7 within a housing 2 having two intake ports and an exhaust port 2B, and a motor 10 attached to the rotating shaft 1
Driven by. Inside the housing 2, in order from the intake port side, there are an axial flow impeller 3A (Fig. 2(b)) attached to the one-rotation shaft 1 and a fixed impeller 3B fixed inside the housing 2 (see Fig. 2(b)).
A trickle turbomolecular pump stage configured by alternately arranging the pumps (Fig. 2(C)) and the rotating disk 9A (Fig. 3(a))
and a Siegbahn pump stage 9 constructed by alternately arranging fixed discs 9B (FIG. 3(b)).
同じく回転軸1に取り付けられた遠心羽根車5A(第4
図(b))とハウジング2内に固定された固定円板5B
(第4図(C))を交互に並置して構成される遠心圧縮
ポンプ段5と、同じく円周流羽根車10A(第5図(b
))と固定円板10B(第5図(C))を交互に並置し
て構成される円周流圧縮ポンプ段10が連設されている
。Centrifugal impeller 5A (fourth
Figure (b)) and the fixed disk 5B fixed in the housing 2
(Fig. 4(C)) and a centrifugal compression pump stage 5 configured by alternately arranging the pumps (Fig. 4(C)) and a circumferential flow impeller 10A (Fig. 5(b)
)) and fixed disks 10B (FIG. 5(C)) are arranged in series with circumferential flow compression pump stages 10.
上記真空ポンプを、排気口2Bでの気力が大気圧の状態
で運転し、吸気口2Aの圧力が十分に低下し、気体の流
れが分子流となった状態では、各ポンプ段はそれぞれ特
性の最もよい圧力範囲で作動している。一方、吸気口2
人の圧力が上昇した状態では、軸流ターボ分子ポンプ段
3での気体の流れは中間流となり、性能が低下するが、
ジーグバーンポンプ段9が、分子流〜中間流の広い圧力
範囲で有効に作動し、かつ円周流圧縮ポンプ段10での
圧縮作用により遠心圧縮ポンプ段5が有効に作動する圧
力状態に保持されるため、吸気口2Aでの圧力上昇によ
る性能低下は小さい、この結果、真空ポンプは広い圧力
範囲で有効に作動するようになる。When the above vacuum pump is operated with the air pressure at the exhaust port 2B at atmospheric pressure, and the pressure at the intake port 2A is sufficiently reduced and the gas flow becomes a molecular flow, each pump stage has its own characteristics. Operating in the best pressure range. On the other hand, intake port 2
When the human pressure increases, the gas flow in the axial turbomolecular pump stage 3 becomes an intermediate flow, and the performance decreases.
The Siegbahn pump stage 9 operates effectively in a wide pressure range from molecular flow to intermediate flow, and the compression action in the circumferential flow compression pump stage 10 maintains the pressure state at which the centrifugal compression pump stage 5 operates effectively. Therefore, performance degradation due to pressure increase at the intake port 2A is small, and as a result, the vacuum pump can operate effectively over a wide pressure range.
上記実施例において、ジーグバーンポンプ段の代りにね
じ圧縮ポンプ段を用いても同様の効果が得られる。Similar effects can be obtained by using a screw compression pump stage in place of the Siegbahn pump stage in the above embodiments.
本発明によれば、吸気口圧力の上昇による真空ポンプの
性能低下を小さくできるので、広い圧力範囲で有効に作
動する真空ポンプが得られる。According to the present invention, a decrease in the performance of the vacuum pump due to an increase in intake port pressure can be reduced, so that a vacuum pump that operates effectively over a wide pressure range can be obtained.
第1図は本発明の真空ポンプの全体構造を示す縦断面図
、第2図(a)〜第2図(c)は第1図の軸流ターボ分
子ポンプ段の詳細図、第3図(a)および(b)は第1
図のジーグバーンポンプ段の詳細図、第4図(a)〜第
4図(c)は第1図の遠心圧縮ポンプ段の詳細図、第5
図(a)〜第5図(c)は第1図の円周流圧縮ポンプ段
の詳細図、第6図は従来の真空ポンプの断面図である。
2A・・・吸気0.2B・・・排気口、3・・・軸流タ
ーボ分子ポンプ段、5・・・遠心圧縮ポンプ段、9・・
・ジーグ+ミl!:5
代理人 弁理士 小川勝男 8ノ
第 l 目
第 2 口
(す
(す
第30
(α)
<b)
98・・・固rL円孜
(、、)第4 囚
<b)
10F3・・・引延り木に
椿 5 l
(す
10B・・・固定巴不叉FIG. 1 is a vertical sectional view showing the overall structure of the vacuum pump of the present invention, FIGS. 2(a) to 2(c) are detailed views of the axial flow turbomolecular pump stage in FIG. 1, and FIG. a) and (b) are the first
4(a) to 4(c) are detailed views of the centrifugal compression pump stage of FIG.
5(a) to 5(c) are detailed views of the circumferential flow compression pump stage of FIG. 1, and FIG. 6 is a sectional view of a conventional vacuum pump. 2A... Intake 0.2B... Exhaust port, 3... Axial turbo molecular pump stage, 5... Centrifugal compression pump stage, 9...
・Jigue + Mil! :5 Agent Patent attorney Katsuo Ogawa 8th l eye 2nd mouth (su(su 30th (α) <b) 98...KrL Enkei (,,) 4th prisoner <b) 10F3... Camellia on a stretched tree 5 l (Su10B...fixed tomoe
Claims (1)
ング内に国定されたスタータと、前記ハウジング内に回
転自在に支承されたロータから成り、該ロータの回転に
伴い、前記吸気口から吸込まれた気体を、前記排気口か
ら直接大気に排気する一体型の真空ポンプにおいて、前
記吸気口に隣接して前記ロータに設けられた軸流羽根車
と前記ハウジング内に固定された固定板を交互に並置し
て形成される軸流ターボ分子ポンプ段、前記軸流ターボ
分子ポンプ段の後流側で前記ロータに設けられた回転円
板と前記ハウジング内に固定された固定円板の一方ある
いは両方にねじ状の溝を設けて形成されるジーグバーン
ポンプ段、前記ジーグバーンポンプ段の後流側で前記ロ
ータに設けられた遠心羽根車と前記ハウジング内に固定
された固定板を交互に並置して形成される遠心圧縮ポン
プ段、前記遠心圧ポンプ段の後流側で前記ロータに設け
られた円周流羽根車と前記ハウジング内に固定された固
定板を交互に並置して形成される円周流圧縮ポンプ段を
連設して構成したことを特徴とする真空ポンプ。1. Consists of a housing having an intake port and an exhaust port, a starter provided within the housing, and a rotor rotatably supported within the housing, and as the rotor rotates, air is sucked in from the intake port. In an integrated vacuum pump that exhausts gas directly to the atmosphere from the exhaust port, an axial flow impeller provided on the rotor adjacent to the intake port and a fixed plate fixed in the housing are alternately arranged side by side. an axial-flow turbomolecular pump stage formed by the axial-flow turbomolecular pump stage, and a screw on one or both of a rotating disk provided on the rotor and a fixed disk fixed in the housing on the downstream side of the axial-flow turbomolecular pump stage. A Siegbahn pump stage is formed by providing a shaped groove, and a centrifugal impeller provided on the rotor and a fixed plate fixed in the housing are alternately juxtaposed on the downstream side of the Siegbahn pump stage. a centrifugal compression pump stage; a circumferential flow formed by alternately juxtaposing a circumferential flow impeller provided on the rotor and a fixed plate fixed in the housing on the downstream side of the centrifugal pressure pump stage; A vacuum pump characterized by being configured by connecting compression pump stages.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61228179A JPS6385290A (en) | 1986-09-29 | 1986-09-29 | Vacuum pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP61228179A JPS6385290A (en) | 1986-09-29 | 1986-09-29 | Vacuum pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6385290A true JPS6385290A (en) | 1988-04-15 |
Family
ID=16872449
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP61228179A Pending JPS6385290A (en) | 1986-09-29 | 1986-09-29 | Vacuum pump |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6385290A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0275796A (en) * | 1988-09-12 | 1990-03-15 | Osaka Shinku Kiki Seisakusho:Kk | Composite vacuum pump |
| JPH02136595A (en) * | 1988-11-16 | 1990-05-25 | Anelva Corp | Vacuum pump |
| JPH0524994U (en) * | 1991-09-05 | 1993-04-02 | 日本原子力研究所 | Compound vacuum pump |
| US5490761A (en) * | 1992-04-29 | 1996-02-13 | Varian Associates, Inc. | High performance turbomolecular vacuum pumps |
| JP2002519575A (en) * | 1998-06-30 | 2002-07-02 | 株式会社荏原製作所 | Turbo molecular pump |
-
1986
- 1986-09-29 JP JP61228179A patent/JPS6385290A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0275796A (en) * | 1988-09-12 | 1990-03-15 | Osaka Shinku Kiki Seisakusho:Kk | Composite vacuum pump |
| JPH02136595A (en) * | 1988-11-16 | 1990-05-25 | Anelva Corp | Vacuum pump |
| JPH0524994U (en) * | 1991-09-05 | 1993-04-02 | 日本原子力研究所 | Compound vacuum pump |
| US5490761A (en) * | 1992-04-29 | 1996-02-13 | Varian Associates, Inc. | High performance turbomolecular vacuum pumps |
| US5498125A (en) * | 1992-04-29 | 1996-03-12 | Hablanian; Marsbed | High performance turbomolecular vacuum pumps |
| JP2002519575A (en) * | 1998-06-30 | 2002-07-02 | 株式会社荏原製作所 | Turbo molecular pump |
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