JPH03115797A - Vacuum pump - Google Patents

Vacuum pump

Info

Publication number
JPH03115797A
JPH03115797A JP3254890A JP3254890A JPH03115797A JP H03115797 A JPH03115797 A JP H03115797A JP 3254890 A JP3254890 A JP 3254890A JP 3254890 A JP3254890 A JP 3254890A JP H03115797 A JPH03115797 A JP H03115797A
Authority
JP
Japan
Prior art keywords
impeller
pump stage
pump
vacuum pump
flow
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.)
Granted
Application number
JP3254890A
Other languages
Japanese (ja)
Other versions
JP2680156B2 (en
Inventor
Takashi Nagaoka
隆司 長岡
Masahiro Mase
正弘 真瀬
Yoshitsugu Tsutsumi
芳紹 堤
Minoru Taniyama
実 谷山
Makoto Terajima
寺島 信
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP2032548A priority Critical patent/JP2680156B2/en
Publication of JPH03115797A publication Critical patent/JPH03115797A/en
Application granted granted Critical
Publication of JP2680156B2 publication Critical patent/JP2680156B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

PURPOSE:To obtain a large pumping speed under the transition condition in the initial time of the operation and perform the sufficient compression work against the molecular flow under the steady state by providing an open type impeller having retreating vanes and a fixed round plate to be located opposite to the front surface of the open type impeller in a centrifugal compression pump stage of pump stages. CONSTITUTION:A centrifugal compression pump stage 13 works as a centrifugal compressor under the transition condition in the initial time of the pump operation, and as a result, a large pumping speed can be obtained, and since it works as a siegbahn molecular pump against the molecular flow under the steady state, the sufficient compression work against the molecular flow can be obtained. Namely, against the viscous flow in the initial time of the pump operation, the viscous flow is centrifugally compressed by an open type impeller 13A having multiple retreating vanes, and under the steady state to be the high vacuum condition, the molecular flow can be compressed to the constant direction with the work of the retreating vanes of the open type impeller 13A and the fixed round plate 13B located opposite to the front surface of the open type impeller 13A.

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、特に
半導体製造装置等において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 at atmospheric pressure, and particularly to a vacuum pump suitable for creating a clean vacuum in semiconductor manufacturing equipment and the like.

〔従来の技術〕[Conventional technology]

従来の真空ポンプとしては、特開昭51−38113号
公報に記載されたものが知られている。この真空ポンプ
の構造を第8図により説明する。図にお」: 対称となっているので、奏半部側について説明する。
As a conventional vacuum pump, one described in Japanese Unexamined Patent Publication No. 51-38113 is known. The structure of this vacuum pump will be explained with reference to FIG. In the figure: Since it is symmetrical, I will explain about the instrumental side.

1は吸気口IAおよび排気口IBを有するハウジング、
2はハウジング1内に軸受7を介して回転自在に支持さ
れけた回転軸を示し、前記ハウジング1内に、軸流ター
ボ分子ポンプ段3、付加分子ポンプ段4、遠心圧縮ポン
プ段5および渦流圧縮ポンプ段6を、前記吸気口IA側
から排気口IB側に亘って順次配設している。
1 is a housing having an intake port IA and an exhaust port IB;
Reference numeral 2 denotes a rotating shaft rotatably supported in the housing 1 via a bearing 7, and the housing 1 includes an axial flow turbomolecular pump stage 3, an additional molecular pump stage 4, a centrifugal compression pump stage 5, and a vortex compression pump stage. Pump stages 6 are sequentially arranged from the intake port IA side to the exhaust port IB side.

前記軸流ターボ分子ポンプ段3は、ハウジング1の内壁
に取付けた固定板3Bと、回転軸2に取付けた回転円板
3Aとを交互に組合せて構成されている。
The axial turbomolecular pump stage 3 is constructed by alternately combining fixed plates 3B attached to the inner wall of the housing 1 and rotating disks 3A attached to the rotating shaft 2.

前記付加分子ポンプ段4は、ハウジング1内壁に取付け
た固定板4Bと、回転軸2に取付けた円板状羽根車4A
とを交互に組合せて構成されている。前記遠心圧縮ポン
プ段5は、ハウジング1内壁に取付けたデイフユーザ固
定板5Bと、回転軸2に取付けた羽根車5Aとを交互に
組合せて構成している。前記渦流圧縮ポンプ段6は、ハ
ウジング1内壁に取付けた固定板6Bと、回転軸2に取
付けた回転円板6Aとを交互に組合せて構成されている
The additional molecular pump stage 4 includes a fixed plate 4B attached to the inner wall of the housing 1 and a disc-shaped impeller 4A attached to the rotating shaft 2.
It is composed of an alternating combination of The centrifugal compression pump stage 5 is constructed by alternately combining differential user fixing plates 5B attached to the inner wall of the housing 1 and impellers 5A attached to the rotating shaft 2. The vortex compression pump stage 6 is constructed by alternately combining fixed plates 6B attached to the inner wall of the housing 1 and rotating disks 6A attached to the rotating shaft 2.

一方、回転軸2は駆動タービン8を介して駆動され、こ
の駆動タービン8はハウジング1の側壁に設けた空気人
口9Aと空気出口9Bに連結されている。
On the other hand, the rotating shaft 2 is driven via a drive turbine 8, and the drive turbine 8 is connected to an air outlet 9A and an air outlet 9B provided on the side wall of the housing 1.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

前述の如き構成の真空ポンプにおいて、定常状態に達し
たときには、各ポンプ段が十分な圧縮作用をし、吸込口
の圧力、すなわち到達真空圧力は十分低い圧力に達する
ことができる。しかし、ポンプ運転の初期のいわゆる過
渡状態においては、大きな排気速度を得ることができな
い。それは、このような過渡状態においてはポンプ内の
圧力が高いため、本来気体の流れが分子流、中間流で有
効な軸流ターボ分子ポンプ段3、付加分子ポンプ段4は
ほとんど圧縮作用をせず、特に付加分子ポンプ段は流路
断面積が狭いため、逆に流体抵抗が大きく、大流量に対
しては圧力損失を発生することになるからである。
In the vacuum pump configured as described above, when a steady state is reached, each pump stage performs a sufficient compression action, and the pressure at the suction port, that is, the ultimate vacuum pressure, can reach a sufficiently low pressure. However, in a so-called transient state at the beginning of pump operation, a large pumping speed cannot be obtained. This is because in such a transient state, the pressure inside the pump is high, so the axial turbo-molecular pump stage 3 and the additional molecular pump stage 4, which are normally effective when the gas flow is a molecular flow or an intermediate flow, have almost no compression effect. This is because, in particular, the additional molecular pump stage has a narrow flow path cross-sectional area, and therefore has a large fluid resistance, resulting in a pressure loss for a large flow rate.

本発明の目的は、ポンプ運転初期の過渡状態において大
きな排気速度を得ることができ、かつ定常状態における
分子流に対しても十分な圧縮作用をする真空ポンプを得
ることにある。
An object of the present invention is to obtain a vacuum pump that can obtain a large pumping speed in a transient state at the beginning of pump operation, and that also has a sufficient compression effect on molecular flow in a steady state.

〔課題を解決するための手段〕[Means to solve the problem]

上記目的を達成するため本発明は、吸気口、排気口及び
ポンプ作用をするポンプ段を有し、定常状態においては
分子流圧力領域の希薄気体を前記吸気口から吸込み圧縮
して前記排気口から排出するようにした真空ポンプにお
いて、前記ポンプ段は少なくとも遠心圧縮ポンプ段を有
し、遠心圧縮ポンプ段は、回転軸に取付けられ複数個の
後退羽根を有するオープン形羽根車と、この羽根車の前
面に対向するように配置された固定円板とを備えている
ことを特徴とするものである。
In order to achieve the above object, the present invention has an intake port, an exhaust port, and a pump stage that performs a pumping action, and in a steady state, dilute gas in a molecular flow pressure region is sucked and compressed from the intake port, and is then released from the exhaust port. In the vacuum pump, the pump stage has at least a centrifugal compression pump stage, and the centrifugal compression pump stage includes an open impeller mounted on a rotating shaft and having a plurality of retracting blades; It is characterized by comprising a fixed disc disposed to face the front surface.

本発明の他の特徴は、吸気口、排気口及びポンプ作用を
するポンプ段を有し、定常状態においては分子流圧力領
域の希薄気体を前記吸気口から吸込み圧縮して前記排気
口から排出するようにした真空ポンプにおいて、前記ポ
ンプ段は少なくとも遠心圧縮ポンプ段を有し、この遠心
圧縮ポンプ段は、回転軸に取付けられ複数個の後退羽根
を有するオープン形羽根車と、この羽根車の前面に対向
するように配置さするように配置された固定円板と、こ
の固定円板の羽根車裏面側に羽根車の回転方向に内向き
に設けられた羽根とを備えていることにある。
Another feature of the present invention is that it has an inlet port, an exhaust port, and a pump stage that performs a pumping action, and in a steady state, dilute gas in a molecular flow pressure region is sucked in from the inlet port, compressed, and discharged from the exhaust port. In the vacuum pump, the pump stage has at least a centrifugal compression pump stage, and the centrifugal compression pump stage includes an open impeller mounted on a rotating shaft and having a plurality of retracting blades, and a front surface of the impeller. The present invention includes a fixed disk disposed to face the impeller, and blades provided on the back side of the impeller on the fixed disk facing inward in the rotational direction of the impeller.

〔作用〕[Effect]

前記遠心圧縮ポンプ段は、ポンプ運転初期の過渡状態に
おいては遠心圧縮機として働き、この結果大きな排気速
度を得るこができ、かつ定常状態における分子流に対し
てはジーグバーン分子ポンプとして働くので、分子流に
対しても十分な圧縮作用が得られる。すなわちポンプ運
動初期の粘性流に対しては複数個の後退羽根を有するオ
ープン形羽根車によって粘性流が遠心圧縮され、高真空
となる定常状態においては、オープン形羽根車の後退羽
根とこのオ−プン形羽根車の前面に対向するように配置
された固定円板との作用によって分子流を一定の方向に
圧縮することができる。
The centrifugal compression pump stage works as a centrifugal compressor in a transient state at the beginning of pump operation, resulting in a large pumping speed, and works as a Siegbahn molecular pump for molecular flow in a steady state. Sufficient compressive action can also be obtained against the flow. In other words, the viscous flow at the beginning of the pump movement is centrifugally compressed by the open impeller having a plurality of retreating vanes, and in a steady state of high vacuum, the retreating vanes of the open impeller and this The molecular flow can be compressed in a fixed direction by the action of a fixed disk placed opposite the front surface of the impeller.

また、オープン形羽根車の裏面に対向する固定円板と、
この固定円板の羽根車裏面側に羽根車の回転方向に内向
きに設けられた羽根とを備えたものにおいては、上記作
用が得られることはもちろんのうえ。
In addition, a fixed disk facing the back side of the open type impeller,
It goes without saying that the above-mentioned effect can be obtained by providing the fixed disk with blades provided on the back side of the impeller facing inward in the direction of rotation of the impeller.

羽根車裏面側も定常状態においてはジーグバーンポンプ
として働かせることができるので、定常状態における圧
縮作用を更に向上することができる2〔実施例〕 以下、本発明の一実施例を第1図ないし第7図に基づい
て説明する。第1図は本発明による真空ポンプの全体構
造を示すもので、第1図において、この真空ポンプは、
吸気口11Aおよび排気口11Bを有するハウジング1
1と、このハウジング11内に軸受21を介して回転自
在に支持された回転軸12と、吸気口11A側から排気
口11B側に至る間のハウジング11内に順次配設され
た遠心圧縮ポンプ段13および円周流圧縮ポンプ段14
とを備えている。回転軸12はこれに連結したモータ1
5により駆動されるようになっている。
Since the back side of the impeller can also function as a Siegbahn pump in a steady state, the compression action in a steady state can be further improved.2 [Embodiment] Hereinafter, an embodiment of the present invention will be described with reference to FIGS. This will be explained based on FIG. FIG. 1 shows the overall structure of a vacuum pump according to the present invention. In FIG.
Housing 1 having an intake port 11A and an exhaust port 11B
1, a rotating shaft 12 rotatably supported within the housing 11 via a bearing 21, and centrifugal compression pump stages sequentially arranged within the housing 11 from the intake port 11A side to the exhaust port 11B side. 13 and circumferential flow compression pump stage 14
It is equipped with The rotating shaft 12 is connected to the motor 1.
5.

前記遠心圧縮ポンプ段13は、第2図、第3図に示すよ
うに、裏面に回転方向に対して内向きの羽根16を複数
固有し、かつ回転軸12に取付けられたオープン羽根車
13Aと、第2図、第4図に示すように、ハウジング1
1内壁に取付けられ、かつ前記羽根車13Aの裏面(羽
根16を設けない面)と対向する面に回転方向に対して
内向きの羽根17を複数個設けた固定円板13Bとを交
互に並列に配置して構成されている。この遠心圧縮ポン
プ段13の回転体の径は後述する円周流圧縮ポンプ段1
4の回転体の径より大きく構成されている。
As shown in FIGS. 2 and 3, the centrifugal compression pump stage 13 has a plurality of blades 16 facing inward with respect to the rotational direction on its back surface, and an open impeller 13A attached to the rotating shaft 12. , as shown in FIGS. 2 and 4, the housing 1
Fixed discs 13B are attached to the inner wall of the impeller 13A and have a plurality of blades 17 facing inward with respect to the rotation direction on a surface opposite to the back surface of the impeller 13A (the surface on which the blades 16 are not provided). It is arranged and configured. The diameter of the rotating body of this centrifugal compression pump stage 13 is the diameter of the rotating body of the centrifugal compression pump stage 1, which will be described later.
The diameter of the rotating body 4 is larger than that of the rotating body 4.

前記円周流圧縮ポンプ段14は、第5図、第6図に示す
ように、回転軸12に取付けられ、かつ外周面に複数個
の羽根18を放射状に設けた羽根車14Aと、第5図、
第7図に示すように、ハウジング11内壁に取付けられ
、かつ前記羽根車14Aの表面(羽根18を設けている
面)と対向する面にU字状の溝19を有する固定円板1
4Bとを交互に並列に配置して構成されると共に、第5
図、第7図に示すように前記119の終端部に孔19A
を穿って通風路20を形成している。この円周流圧縮ポ
ンプ段14の回転体の出口側の径はその入口側の径より
も小さく構成されている。これにより、この部分の回転
動力を小さくすることができる。
As shown in FIGS. 5 and 6, the circumferential flow compression pump stage 14 includes an impeller 14A attached to the rotating shaft 12 and having a plurality of blades 18 radially provided on the outer circumferential surface, and a fifth impeller 14A, as shown in FIGS. figure,
As shown in FIG. 7, a fixed disk 1 is attached to the inner wall of the housing 11 and has a U-shaped groove 19 on the surface facing the surface of the impeller 14A (the surface on which the blades 18 are provided).
4B are arranged alternately in parallel, and the 5th
As shown in FIG.
A ventilation passage 20 is formed by drilling the hole. The diameter on the outlet side of the rotating body of the circumferential flow compression pump stage 14 is smaller than the diameter on the inlet side. Thereby, the rotational power of this portion can be reduced.

次に本実施例の作用について説明する。Next, the operation of this embodiment will be explained.

ポンプ運転初期の過渡状態においては、ポンプ内部は全
体が大気圧に近い高い圧力下にあり、気体の流れは粘性
流となるので、遠心圧縮ポンプ段13は遠心圧縮機とし
て作用する。すなわち、遠心圧縮ポンプ段羽根車13A
は圧縮機羽根車として働き、羽根車13Aと固定円板1
3Bの間の羽根17にはさまれて形成される流路は、流
れを外径側から内径mlに案内するリターンチャンネル
として働く、また羽根車13Aが圧縮作用をするので、
遠心圧縮ポンプ段13としては、圧力損失部としてより
は圧縮機として大流量を流す作用をすることができる。
In a transient state at the beginning of pump operation, the entire inside of the pump is under a high pressure close to atmospheric pressure, and the gas flow becomes a viscous flow, so that the centrifugal compression pump stage 13 acts as a centrifugal compressor. That is, the centrifugal compression pump stage impeller 13A
acts as a compressor impeller, and the impeller 13A and fixed disk 1
The flow path formed between the blades 17 between the blades 3B acts as a return channel that guides the flow from the outer diameter side to the inner diameter ml, and since the impeller 13A acts as a compressor,
The centrifugal compression pump stage 13 can act as a compressor to provide a large flow rate rather than as a pressure loss section.

円周流圧縮ポンプ段14の圧縮比が大きくなって、円周
流圧縮ポンプ段の入口の圧力が十分に低くなった定常状
態、すなわちこの圧力が数Torr以下になった定常状
態においては、遠心圧縮ポンプ段13の入口、すなわち
真空ポンプの吸気口11Aの付近の気体の流れは、中間
流、又は分子流となり、遠心圧縮ポンプ段13は、ジー
グバーン分子ポンプとして作用する。すなわち、羽根1
6を有する羽根車13Aは、ら旋溝を加工した回転円板
として作用し、固定円板13Bの裏面(羽根17を設け
ない面)との組合せで、内径側から外径側に向けて圧縮
作用を固定円板として作用し、羽根車13Aの裏面(羽
根16を設けない面)との組合せで、外径側から内径側
に向けて圧縮作用をするジーグバーン分子ポンプとして
働く。
In a steady state in which the compression ratio of the circumferential flow compression pump stage 14 is increased and the pressure at the inlet of the circumferential flow compression pump stage is sufficiently low, that is, in a steady state in which this pressure is several Torr or less, centrifugal The gas flow near the inlet of the compression pump stage 13, ie, the vacuum pump inlet 11A, is an intermediate flow or molecular flow, and the centrifugal compression pump stage 13 acts as a Siegbahn molecular pump. That is, feather 1
The impeller 13A having 6 acts as a rotating disk with a spiral groove processed, and in combination with the back surface of the fixed disk 13B (the surface where the blades 17 are not provided), compresses from the inner diameter side to the outer diameter side. It acts as a fixed disk, and in combination with the back surface of the impeller 13A (the surface on which the blades 16 are not provided), it functions as a Siegbahn molecular pump that compresses from the outer diameter side toward the inner diameter side.

また同じく定常状態ににおいては、前記円周流圧縮ポン
プ段14に流入する気体は前記遠心圧縮ポンプ段13に
おいて十分圧縮されているため、体積流量はほとんど零
に近い。すなわち、円周流圧縮ポンプ段14は、締切状
態に近い状態で運転されることになるが1円周流圧縮ポ
ンプ段は締切状態で高い圧縮比が得られるという特性が
あるため、少ない段数で十分低い到達圧力に達すること
ができる。
Similarly, in a steady state, the gas flowing into the circumferential compression pump stage 14 is sufficiently compressed in the centrifugal compression pump stage 13, so that the volumetric flow rate is almost zero. In other words, the circumferential flow compression pump stage 14 is operated in a state close to the closed state, but since the first circumferential flow compression pump stage has the characteristic of obtaining a high compression ratio in the closed state, it is possible to operate with a small number of stages. A sufficiently low ultimate pressure can be reached.

遠心圧縮ポンプ段13、円周流圧縮ポンプ段14の段数
、及びポンプ回転数は、定常運転状態において1両段の
境の圧力が粘性流と中間流の切替わり点、すなおち数T
orrになるよう設定する。通常、遠心圧縮ポンプ段を
1〜3段、円周流圧縮ポンプ段を6〜10段組合わせる
ことにより、ポンプの吸気口11Aの圧力は10−”〜
10−’T o r rに達することができる。
The number of stages of the centrifugal compression pump stage 13 and the circumferential flow compression pump stage 14 and the pump rotation speed are determined at the point where the pressure at the boundary between the two stages switches between the viscous flow and the intermediate flow in a steady operating state, that is, the number of holes T.
Set it to be orr. Usually, by combining 1 to 3 stages of centrifugal compression pump stages and 6 to 10 stages of circumferential flow compression pump stages, the pressure at the pump intake port 11A is 10-"~
10-'T o r r can be reached.

〔発明の効果〕〔Effect of the invention〕

本発明によれば、遠心圧縮ポンプ段が、ポンプ運転初期
の過渡状態においては遠心圧縮機として鋤き、大きな排
気速度を得ることができる。また、定常状態における分
子流に対してはジーグバーン分子ポンプとして働き、十
分な圧縮作用を得ることができるという効果がある。
According to the present invention, the centrifugal compression pump stage operates as a centrifugal compressor in a transient state at the beginning of pump operation, and a large pumping speed can be obtained. In addition, it works as a Siegbahn molecular pump for molecular flow in a steady state, and has the effect of being able to obtain a sufficient compression effect.

【図面の簡単な説明】[Brief explanation of drawings]

第1@は本発明による真空ポンプの全体構造を示す縦断
面図、第2図は第1図に示す真空ポンプの遠心圧縮ポン
プ段の詳細を示す断面図、第3図は第2図の■−■矢視
図、第4図は第2図のIV−■矢視図、第5図は第1図
に示す真空ポンプの円周流圧縮ポンプ段の詳細を示す断
面図、第6図は第5図のVI−VI矢視図、第7図は第
5図の■−■矢視図、第8図は従来の真空ポンプの縦断
面図である。 11・・・ハウジング、IIA・・・吸気口、IIB・
・・排気口、12・・・回転軸、13・・・遠心圧縮ポ
ンプ段。 13A・・・オープン形羽根車、13B・・・固定円板
、14・・・円周流圧縮ポンプ段、14A・・・羽根車
、14B・・・固定円板、16.17.18・・・羽根
1 is a vertical sectional view showing the overall structure of the vacuum pump according to the present invention, FIG. 2 is a sectional view showing details of the centrifugal compression pump stage of the vacuum pump shown in FIG. 1, and FIG. -■ arrow view, Figure 4 is a view from IV-■ arrow in Figure 2, Figure 5 is a sectional view showing details of the circumferential flow compression pump stage of the vacuum pump shown in Figure 1, and Figure 6 is FIG. 5 is a view taken along the VI-VI arrow in FIG. 5, FIG. 7 is a view taken along the ■-■ arrow in FIG. 5, and FIG. 8 is a longitudinal sectional view of a conventional vacuum pump. 11...Housing, IIA...Intake port, IIB・
...Exhaust port, 12... Rotating shaft, 13... Centrifugal compression pump stage. 13A...Open type impeller, 13B...Fixed disc, 14...Circumferential flow compression pump stage, 14A...Impeller, 14B...Fixed disc, 16.17.18...・Feathers.

Claims (1)

【特許請求の範囲】 1、吸気口、排気口及びポンプ作用をするポンプ段を有
し、定常状態においては分子流圧力領域の希薄気体を前
記吸気口から吸込み圧縮して前記排気口から排出するよ
うに真空ポンプにおいて、前記ポンプ段は少なくとも遠
心圧縮ポンプ段を有し、この遠心圧縮ポンプ段は、回転
軸に取付けられ複数個の後退羽根を有するオープン形羽
根車と、この羽根車の前面に対向するように配置された
固定円板とを備えていることを特徴とする真空ポンプ。 2、吸気口、排気口及びポンプ作用をするポンプ段を有
し、定常状態においては分子流圧力領域の希薄気体を前
記吸気口から吸込み圧縮して前記排気口から排出するよ
うにした真空ポンプにおいて、前記ポンプ段は少なくと
も遠心圧縮ポンプ段を有し、この遠心圧縮ポンプ段は、
回転軸に取付けられ複数個の後退羽根を有するオープン
形羽根車と、この羽根車の前面に対向するように配置さ
れた固定円板と、前記オープン形羽根車の裏面に対向す
るように配置された固定円板と、この固定円板の羽根車
裏面側に羽根車の回転方向に内向きに設けられた羽根と
を備えていることを特徴とする真空ポンプ。 3、特許請求の範囲第2項において、前記オープン形羽
根車の裏面側に対向する固定円板に取付けられた羽根を
複数枚としたことを特徴とする真空ポンプ。 4、特許請求の範囲第2項または第3項において、前記
遠心圧縮ポンプ段を多段に設けたことを特徴とする真空
ポンプ。
[Claims] 1. It has an intake port, an exhaust port, and a pump stage that performs a pumping action, and in a steady state, dilute gas in the molecular flow pressure region is sucked in from the intake port, compressed, and discharged from the exhaust port. In a vacuum pump, the pump stage has at least a centrifugal compression pump stage, and the centrifugal compression pump stage includes an open impeller mounted on a rotating shaft and having a plurality of retreating vanes, and a front surface of the impeller. A vacuum pump comprising fixed discs arranged to face each other. 2. A vacuum pump having an intake port, an exhaust port, and a pump stage that performs a pumping action, and in a steady state, a dilute gas in a molecular flow pressure region is sucked in from the intake port, compressed, and discharged from the exhaust port. , the pump stage comprises at least a centrifugal compression pump stage, the centrifugal compression pump stage comprising:
an open-type impeller attached to a rotating shaft and having a plurality of retreating blades; a fixed disk disposed to face the front surface of the impeller; and a fixed disk disposed to face the back surface of the open-type impeller. 1. A vacuum pump comprising: a fixed disk; and blades provided on the back side of the impeller of the fixed disk facing inward in the rotational direction of the impeller. 3. The vacuum pump according to claim 2, characterized in that a plurality of blades are attached to a fixed disc facing the back side of the open type impeller. 4. A vacuum pump according to claim 2 or 3, characterized in that the centrifugal compression pump stages are provided in multiple stages.
JP2032548A 1990-02-15 1990-02-15 Vacuum pump Expired - Lifetime JP2680156B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2032548A JP2680156B2 (en) 1990-02-15 1990-02-15 Vacuum pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2032548A JP2680156B2 (en) 1990-02-15 1990-02-15 Vacuum pump

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
JP60088624A Division JPS61247893A (en) 1985-04-26 1985-04-26 Vacuum pump

Publications (2)

Publication Number Publication Date
JPH03115797A true JPH03115797A (en) 1991-05-16
JP2680156B2 JP2680156B2 (en) 1997-11-19

Family

ID=12361987

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2032548A Expired - Lifetime JP2680156B2 (en) 1990-02-15 1990-02-15 Vacuum pump

Country Status (1)

Country Link
JP (1) JP2680156B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5536148A (en) * 1993-09-17 1996-07-16 Hitachi, Ltd. Turbo vacuum pump

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6009193B2 (en) 2012-03-30 2016-10-19 株式会社荏原製作所 Vacuum exhaust device

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5138113A (en) * 1974-08-01 1976-03-30 American Optical Corp
JPS60125795A (en) * 1983-12-09 1985-07-05 Osaka Shinku Kiki Seisakusho:Kk Composite vacuum pump
JPS60230598A (en) * 1984-04-30 1985-11-16 Shimadzu Corp Turbo-molecular pump

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5138113A (en) * 1974-08-01 1976-03-30 American Optical Corp
JPS60125795A (en) * 1983-12-09 1985-07-05 Osaka Shinku Kiki Seisakusho:Kk Composite vacuum pump
JPS60230598A (en) * 1984-04-30 1985-11-16 Shimadzu Corp Turbo-molecular pump

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5536148A (en) * 1993-09-17 1996-07-16 Hitachi, Ltd. Turbo vacuum pump

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