JPH03237295A - Turbo-molecular pump - Google Patents

Turbo-molecular pump

Info

Publication number
JPH03237295A
JPH03237295A JP2030510A JP3051090A JPH03237295A JP H03237295 A JPH03237295 A JP H03237295A JP 2030510 A JP2030510 A JP 2030510A JP 3051090 A JP3051090 A JP 3051090A JP H03237295 A JPH03237295 A JP H03237295A
Authority
JP
Japan
Prior art keywords
ring
turbo
shaped
rotary
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.)
Pending
Application number
JP2030510A
Other languages
Japanese (ja)
Inventor
Shigeo Kawasue
繁雄 川末
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.)
Shimadzu Corp
Original Assignee
Shimadzu Corp
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 Shimadzu Corp filed Critical Shimadzu Corp
Priority to JP2030510A priority Critical patent/JPH03237295A/en
Publication of JPH03237295A publication Critical patent/JPH03237295A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/04Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps
    • F04D19/048Multi-stage pumps specially adapted to the production of a high vacuum, e.g. molecular pumps comprising magnetic bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0606Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump

Abstract

PURPOSE:To shorten the shaft length of a pump itself so as to reduce its size and weight by connecting respective rotary vanes of a molecular pump to ring shaped-rotators of a ring type electric motor. CONSTITUTION:An annular holding cylinder 5 for storing and holding fixedly a ring shaped outer stator 6 and a ring-shaped inner stator 7 which are arranged face to face at a constant interval, is inserted around the top part of the central fixed holding shaft 4. And a ring shaped-rotator 8 is inserted into the clearance between the outer stator 6 and the inner stator 7, and the top end thereof is fixed through a connecting annulus 9 integratedly on a rotary cylinder 10 which is the base of a rotary vane 3. The rotary cylinder 10 is supported by magnetic bearings 12, 13, and the magnetic bearing 12 is maintained by a supporting annulus 14 fixed on a fixed holding shaft 4. The rotary vans 3, 3' are driven in high rotating speed by two upper and lower ring shaped-electric motors RM, RM' so as to carry out exhaust.

Description

【発明の詳細な説明】 A、産業上の利用分野 この発明は、固定翼と回転翼との相対的回転によるター
ボ機構によって分子の流れを方向づけ気体分子を排出し
て真空を得るターボ分子ポンプに関するものである。
DETAILED DESCRIPTION OF THE INVENTION A. Industrial Application Field This invention relates to a turbomolecular pump that directs the flow of molecules and exhausts gas molecules to create a vacuum using a turbo mechanism based on the relative rotation of fixed blades and rotary blades. It is something.

B、従来の技術 従来に於けるこの種ターボ分子ポンプにおいては回転翼
の回転は電動機によって行っているが、たとえば特開昭
61−247894号「ターボ分子ポンプ」にも示され
るように電動機の出力軸端に回転翼が直結された状態で
ある。この構成は縦形のみならず横形の場合でも同様で
ある。
B. Prior Art In conventional turbo-molecular pumps of this type, the rotor blades are rotated by an electric motor, but the output of the electric motor is The rotor blade is directly connected to the shaft end. This configuration applies not only to the vertical type but also to the horizontal type.

C4発明が解決しようとする問題点 従来のターボ分子ポンプの場合、回転翼と固定翼との組
合わせは多段であるがそれらは一体的になっていてこれ
らが1個の電動機により回転駆動される構成になってい
る。したがって各段の排気特性を変化させるためには翼
の大きさを変化させる必要がある。しかしこの場合は加
工を複雑にする。他方電動機の出力軸端に回転翼が連結
されているので、ポンプ全体の軸芯長が非常に大きくな
らざるを得ない。
C4 Problems to be solved by the invention In the case of conventional turbomolecular pumps, the rotary blades and fixed blades are combined in multiple stages, but they are integrated and are driven to rotate by a single electric motor. It is configured. Therefore, in order to change the exhaust characteristics of each stage, it is necessary to change the size of the blades. However, in this case, processing becomes complicated. On the other hand, since the rotor blade is connected to the end of the output shaft of the electric motor, the axial length of the entire pump must be extremely large.

大容量の場合は電動機の大形となりこの傾向は増大する
。軸芯長の増大はポンプの大形化、重量化を招来する。
If the capacity is large, the motor will be large and this tendency will increase. An increase in the shaft core length results in an increase in the size and weight of the pump.

この発明はこのような問題点を解決するターボ分子ポン
プを提供せんとするものである。
The present invention aims to provide a turbomolecular pump that solves these problems.

D1問題点を解決するための手段 この発明によるターボ分子ポンプは、電動機としてリン
グ形電動機を採用するとともにこの電動機を複数個設置
する。このリング形電動機は、一定の空隙をおいて対向
配置された外側固定子および内側固定子と、これらの空
隙間に挿入されたリング状回転子から成り、内固定子と
回転子間の電磁力作用によりリング状回転子にトルクを
発生させる構成のものである。このリング形電動機のそ
れぞれのリング状回転子に前記分子ポンプの回転翼をそ
れぞれ連結して構成するのである。同時に各電動機の駆
動を別々に制御するものである。
Means for Solving Problem D1 The turbo-molecular pump according to the present invention employs a ring-type motor as the motor, and a plurality of these motors are installed. This ring-shaped electric motor consists of an outer stator and an inner stator that are placed opposite each other with a certain gap between them, and a ring-shaped rotor that is inserted into these gaps, and the electromagnetic force between the inner stator and the rotor is It is configured to generate torque in the ring-shaped rotor by its action. The rotor blades of the molecular pump are connected to each ring-shaped rotor of this ring-shaped electric motor. At the same time, the drive of each electric motor is controlled separately.

E 作用 リング状回転子に対して連結される分子ポンプの回転翼
はそのリングの内方または外方に位置することができる
から軸芯長はリング形電動機の軸芯長になる。したがっ
て軸芯方向にリング形電動機を複数段の形で設置できる
E. Effect Since the rotor blades of the molecular pump connected to the ring-shaped rotor can be located inside or outside the ring, the axial length becomes the axial length of the ring-shaped electric motor. Therefore, the ring type electric motor can be installed in multiple stages in the axial direction.

F、実膝例 以下、図面に示す実施例にしたがってこの発明を説明す
る。
F. Practical Knee Example The present invention will now be described according to the embodiment shown in the drawings.

第1図はこの発明によるターボ分子ポンプの構成全体を
示す縦断面図であり、第2図は第1図におけるII−I
I面図である。第2図はリング形電動機のの構成を説明
するためのもので、その軸芯と垂直の断面が示されてい
る。第3図は各リング形電動機の制御回路を示している
FIG. 1 is a longitudinal cross-sectional view showing the entire configuration of a turbomolecular pump according to the present invention, and FIG.
It is an I side view. FIG. 2 is for explaining the structure of a ring type electric motor, and shows a cross section perpendicular to its axis. FIG. 3 shows a control circuit for each ring type motor.

図示例ではリング形電動機を2段設置した例が示されて
おり、下段は上段と同一であるので、符号については−
を付して示している。ターボ分子ポンプならびにリング
形電動機の説明としては上段を中心に説明する。
The illustrated example shows an example in which ring-shaped motors are installed in two stages, and the lower stage is the same as the upper stage, so the symbols are -
It is shown with . The explanation of the turbomolecular pump and ring type electric motor will focus on the upper part.

まず第1図にしたがってターボ分子ポンプの構成につい
て説明する0図において2が固定翼であってポンプケー
シング1の内壁側に一定の間隔で複数段固定付設されて
いる。3はこの固定翼2に対し回転筒10に一定の間隔
で複数段固定付設され外方に延設された回転翼である。
First, the structure of a turbo-molecular pump will be explained in accordance with FIG. 1. In FIG. 0, reference numeral 2 denotes fixed blades, which are fixedly attached to the inner wall of the pump casing 1 in multiple stages at regular intervals. Reference numeral 3 designates rotor blades which are fixedly attached to the rotary cylinder 10 in multiple stages at regular intervals and extend outward from the fixed blade 2.

固定翼2と回転翼3は交互に組合わされて両者によって
ターボ機構が構成されるのである。そして回転翼3の高
速回転によって固定翼2と回転翼3間に相対的回転をつ
くり、分子の流れを方向づけ、気体分子を吸気口Pから
排気口Hへと排出し、吸気口Pに連接される被排気室(
図示せず)の真空を得るのである。15は脚である。
The fixed blades 2 and the rotary blades 3 are alternately combined to form a turbo mechanism. Then, the high-speed rotation of the rotor blade 3 creates relative rotation between the fixed blade 2 and the rotor blade 3, directs the flow of molecules, and discharges gas molecules from the intake port P to the exhaust port H, which is connected to the intake port P. Exhaust chamber (
(not shown) to obtain a vacuum. 15 is a leg.

以上は従来と異なるところはなく公知の技術である。The above is no different from the conventional technology and is a known technology.

さてこの発明は以上の構成において、回転翼3と3の高
速回転をリング形電動機RMで行わせるようにしたとこ
ろに特徴を有するものである。
The present invention is characterized in that, in the above configuration, the rotary blades 3 and 3 are rotated at high speed by the ring-shaped electric motor RM.

この点を第2図も合せながら説明する。すなわち図にお
いて5はリング形電動機RHをmrli、する一部品で
あって、一定の空隙をおいて対向配置されたリング状の
外側固定子6および内側固定子7を固定的に収納保持す
る環状保持筒であり、中央の固定保持軸4の上部に嵌挿
されている。そして8は外側固定子6および内側固定子
7の空隙間に挿入されたリング状回転子で、その上端は
接続環9を介して回転筒10に一体的に固定されている
。この回転筒10が回転翼3の基体となっているのであ
る。
This point will be explained with reference to FIG. That is, in the figure, 5 is a part of the ring-shaped electric motor RH, and is an annular holder that fixedly houses and holds the ring-shaped outer stator 6 and inner stator 7, which are arranged opposite to each other with a certain gap. It is a cylinder and is fitted into the upper part of the fixed holding shaft 4 in the center. A ring-shaped rotor 8 is inserted into the gap between the outer stator 6 and the inner stator 7, and its upper end is integrally fixed to the rotary cylinder 10 via a connecting ring 9. This rotary cylinder 10 serves as the base of the rotor blade 3.

この回転筒10は磁気軸受装置12.13によって支持
される。磁気軸受装置12は固定保持軸4に固定された
支持環14に保持されている。磁気軸受装置13は回転
筒10の内方環状部で構成されている。
This rotary cylinder 10 is supported by magnetic bearing arrangements 12.13. The magnetic bearing device 12 is held by a support ring 14 fixed to the fixed holding shaft 4 . The magnetic bearing device 13 is constituted by the inner annular portion of the rotating cylinder 10.

したがって上下2個のリング形電動機RHRHによって
回転翼3と3が高速回転駆動されることによって排気が
行われるのである。
Therefore, the rotary blades 3 and 3 are driven to rotate at high speed by the two upper and lower ring-shaped electric motors RHRH, thereby performing exhaust gas.

しかも上下2個のリング形電動機RHRMは第3図、に
示すように駆動制御回路CBによって個々に制御される
。 ESは電源部でる。この駆動制御回路CBは被排気
室Cの真空度に応じて作動する。すなわち被排気室Cの
真空度がセンサSによって感知され検出器にから真空度
に応じた信号が駆動制御回路CBに入力される。駆動制
御回路C8はその入力を受けて2個のリング形電動fi
RHRHをそれぞれ適した速度で回転駆動させるのであ
る。
Furthermore, the two upper and lower ring motors RHRM are individually controlled by a drive control circuit CB as shown in FIG. ES comes out from the power supply section. This drive control circuit CB operates according to the degree of vacuum in the chamber C to be evacuated. That is, the degree of vacuum in the chamber C to be evacuated is sensed by the sensor S, and a signal corresponding to the degree of vacuum is input from the detector to the drive control circuit CB. The drive control circuit C8 receives the input and controls two ring-shaped electric fi
The RHRHs are rotated at appropriate speeds.

この発明の特徴は以上のとおりであるが、上記ならびに
図示例に限定されない、たとえば、リング形電動機を3
段設置してもよい、また被排気室の真空度に応じて回転
速度を制御されるのではなくて、適宜必要によって手動
で制御するようにしてもよい。
The features of the present invention are as described above, but are not limited to the above and illustrated examples.
They may be installed in stages, and the rotational speed may not be controlled according to the vacuum degree of the chamber to be evacuated, but may be controlled manually as needed.

この発明はこれらすべてを包含する。This invention includes all of these.

G3発明の効果 この発明は以上説明したとおりであるから、各リング形
電動機の回転速度を制御することによって排気特性を調
整でき、各ターボ機構の大きさを変える必要がない。し
たがってターボ機構の翼の大きさは同一とでき加工、メ
ンテナンスなどに有利である。
G3 Effects of the Invention Since the present invention has been described above, the exhaust characteristics can be adjusted by controlling the rotational speed of each ring type electric motor, and there is no need to change the size of each turbo mechanism. Therefore, the blades of the turbo mechanism can have the same size, which is advantageous for processing, maintenance, etc.

しかもポンプ自体の軸長は極力短くできポンプの小形、
軽量化を可能とすることができる。
Moreover, the shaft length of the pump itself can be made as short as possible, making the pump compact.
It is possible to reduce the weight.

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

第1図はこの発明によるターボ分子ポンプの構成全体を
示す縦断面図、第2図は第1図における■■面図、第3
図は制御回路図である。 1・・・ポンプケーシング、2・・・固定翼、3・・・
回転翼4・・・固定保持軸、5・・・環状保持筒。
FIG. 1 is a vertical sectional view showing the entire configuration of a turbomolecular pump according to the present invention, FIG. 2 is a side view of FIG. 1, and FIG.
The figure is a control circuit diagram. 1... Pump casing, 2... Fixed blade, 3...
Rotor blade 4... fixed holding shaft, 5... annular holding cylinder.

Claims (2)

【特許請求の範囲】[Claims] (1)固定翼と回転翼との相対的回転によるターボ機構
によって分子の流れを方向づけ気体分子を排出して真空
を得る分子ポンプであって、前記ターボ機構を複数個段
設するとともに各ターボ機構における回転翼の回転駆動
を別々に制御する制御機構を設けたことを特徴とするタ
ーボ分子ポンプ
(1) A molecular pump that directs the flow of molecules and generates a vacuum by discharging gas molecules by using a turbo mechanism based on the relative rotation of a fixed blade and a rotary blade, in which a plurality of the turbo mechanisms are provided, and each turbo mechanism A turbo-molecular pump characterized by having a control mechanism for separately controlling the rotational drive of the rotor blades in the pump.
(2)固定翼と回転翼との相対的回転によるターボ機構
によって分子の流れを方向づけ気体分子を排出して真空
を得る分子ポンプであって、一定の空隙をおいて対向配
置された外側固定子および内側固定子と、これらの空隙
間に挿入されたリング状回転子から成り、両固定子と回
転子間の電磁力作用によりリング状回転子にトルクを発
生させるリング形電動機を複数個設け、この各リング形
電動機のリング状回転子にそれぞれ前記分子ポンプの回
転翼を連結するとともに、各リング形電動機の回転駆動
をそれぞれ制御する制御機構を設けたことを特徴とする
ターボ分子ポンプ。
(2) A molecular pump that generates a vacuum by directing the flow of molecules and discharging gas molecules using a turbo mechanism based on the relative rotation of fixed blades and rotary blades, with outer stators facing each other with a certain gap in between. and an inner stator, and a ring-shaped rotor inserted into these gaps, and a plurality of ring-shaped electric motors are provided that generate torque in the ring-shaped rotor by electromagnetic force between both stators and the rotor. A turbo-molecular pump characterized in that a rotor blade of the molecular pump is connected to the ring-shaped rotor of each ring-shaped electric motor, and a control mechanism is provided for controlling the rotational drive of each ring-shaped electric motor.
JP2030510A 1990-02-09 1990-02-09 Turbo-molecular pump Pending JPH03237295A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2030510A JPH03237295A (en) 1990-02-09 1990-02-09 Turbo-molecular pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2030510A JPH03237295A (en) 1990-02-09 1990-02-09 Turbo-molecular pump

Publications (1)

Publication Number Publication Date
JPH03237295A true JPH03237295A (en) 1991-10-23

Family

ID=12305810

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2030510A Pending JPH03237295A (en) 1990-02-09 1990-02-09 Turbo-molecular pump

Country Status (1)

Country Link
JP (1) JPH03237295A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6508631B1 (en) 1999-11-18 2003-01-21 Mks Instruments, Inc. Radial flow turbomolecular vacuum pump
EP2413483A1 (en) 2010-07-30 2012-02-01 Siemens Aktiengesellschaft Electric drive device for an aircraft
JP2016109137A (en) * 2014-12-08 2016-06-20 プファイファー・ヴァキューム・ゲーエムベーハー Vacuum pump

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6415493A (en) * 1987-07-07 1989-01-19 Ebara Corp Gas pump
JPH01234033A (en) * 1988-03-14 1989-09-19 Yoshio Yano Motor of pump without seal for slurry liquid
JPH01277698A (en) * 1988-04-30 1989-11-08 Nippon Ferrofluidics Kk Compound vacuum pump

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6415493A (en) * 1987-07-07 1989-01-19 Ebara Corp Gas pump
JPH01234033A (en) * 1988-03-14 1989-09-19 Yoshio Yano Motor of pump without seal for slurry liquid
JPH01277698A (en) * 1988-04-30 1989-11-08 Nippon Ferrofluidics Kk Compound vacuum pump

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6508631B1 (en) 1999-11-18 2003-01-21 Mks Instruments, Inc. Radial flow turbomolecular vacuum pump
EP2413483A1 (en) 2010-07-30 2012-02-01 Siemens Aktiengesellschaft Electric drive device for an aircraft
WO2012013594A2 (en) 2010-07-30 2012-02-02 Siemens Aktiengesellschaft Electric drive device for an aircraft
JP2016109137A (en) * 2014-12-08 2016-06-20 プファイファー・ヴァキューム・ゲーエムベーハー Vacuum pump

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