JP2002202089A - Turbo dry vacuum pump - Google Patents

Turbo dry vacuum pump

Info

Publication number
JP2002202089A
JP2002202089A JP2001001014A JP2001001014A JP2002202089A JP 2002202089 A JP2002202089 A JP 2002202089A JP 2001001014 A JP2001001014 A JP 2001001014A JP 2001001014 A JP2001001014 A JP 2001001014A JP 2002202089 A JP2002202089 A JP 2002202089A
Authority
JP
Japan
Prior art keywords
gas
bearing
rotating body
pump
turbo
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
JP2001001014A
Other languages
Japanese (ja)
Inventor
Koji Horikawa
浩司 堀川
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 JP2001001014A priority Critical patent/JP2002202089A/en
Publication of JP2002202089A publication Critical patent/JP2002202089A/en
Pending legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To provide a turbo dry vacuum pump preventing a compound generated from reaction gas from accumulating in a narrow opening in a pump, and preventing bearing lubricating oil from mixing in. SOLUTION: A hanging bell shaped rotor 1b connected to a shaft 21 of a high frequency motor 3a is provided with a multi stage circumferential flow pump part 16 at the outer circumference part and rotates at a high speed. Reaction gas is sucked from a suction opening 6 and is compressed between a screw groove pump part 18 and the multi stage circumferential flow pump part 16. Inert gas is supplied in a labyrinth seal 19 part of a shaft seal part 5a from a gas supply passage 22, flows in a gas flow passage 23, passes through plural through holes 17 provided on cylindrical part of the rotor 1b in a radius and rotation direction, flows in a narrow opening connecting between gas compression parts at a high speed, and is discharged with reaction gas sucked from an upper part, in order to prevent lubricating oil 10 from leaking out during rotating.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、ターボ形ドライ真
空ポンプに係わり、特に、半導体製造装置等のプロセス
過程で発生する反応生成ガスに対処するターボ形ドライ
真空ポンプに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a turbo-type dry vacuum pump, and more particularly to a turbo-type dry vacuum pump for dealing with a reaction product gas generated in a process of a semiconductor manufacturing apparatus or the like.

【0002】[0002]

【従来の技術】気体分子に一定の方向の運動量を回転翼
などで機械的に与えることにより、気体を輸送する真空
ポンプとして、ドライ真空ポンプ、分子ドラッグポン
プ、ターボ分子ポンプ等がある。ドライ真空ポンプは、
大気圧から低真空までの排気をするもので、ポンプ内の
ガス通路に一切油を使用することなく、回転翼、スクリ
ュー翼、メカニカルブースタなどの機構で気体を排気す
るものである。分子ドラッグポンプは、気体分子に運動
量を与えるための高速回転子表面が常にその面と平行に
動く形式のもので、例えば、スクリュー形状の翼部が高
速回転体に取り付けられ、翼部の高速の回転により高真
空を得ることができるものである。ターボ分子ポンプ
は、気体分子どうしの衝突が無視できるような低い圧力
の条件下で、円板に斜めにスリットを切った回転翼と、
それとほぼ同じ形状で、スリットの傾きが回転翼とは反
対の固定翼とが、交互に配置された構造で、回転翼は極
めて高い回転速度で駆動され、両翼の隙間を通って気体
分子が通過し、真空に排気され超高真空を得ることがで
きるものである。分子ポンプとして一般に分子ドラッグ
ポンプとターボ分子ポンプが挙げられるが、これらの真
空排気系には背圧用のポンプとして油回転ポンプやメカ
ニカルブースタポンプやドライ真空ポンプ等が必要にな
る。
2. Description of the Related Art There are dry vacuum pumps, molecular drag pumps, turbo molecular pumps and the like as vacuum pumps for transporting gas by mechanically imparting momentum in a certain direction to gas molecules by a rotary blade or the like. Dry vacuum pump
It exhausts gas from atmospheric pressure to low vacuum, and exhausts gas using a mechanism such as a rotary wing, screw wing, or mechanical booster without using any oil in a gas passage in the pump. A molecular drag pump is a type in which a high-speed rotor surface for giving momentum to gas molecules always moves parallel to the surface.For example, a screw-shaped wing is attached to a high-speed rotating body, and the high-speed High vacuum can be obtained by rotation. The turbo-molecular pump is composed of a rotor blade with a slanted slit in a disk under conditions of low pressure such that collisions between gas molecules can be ignored.
The fixed blades, which have the same shape as the rotating blades and have the same inclination as the rotating blades, are arranged alternately.The rotating blades are driven at an extremely high rotational speed, and gas molecules pass through the gap between the two blades. Then, it is evacuated to a vacuum and an ultra-high vacuum can be obtained. Molecular pumps generally include a molecular drag pump and a turbo molecular pump. These vacuum pumping systems require an oil rotary pump, a mechanical booster pump, a dry vacuum pump, or the like as a back pressure pump.

【0003】図3に、ターボ形ドライ真空ポンプの断面
を示す。この真空ポンプは、上部にガスの吸気口6を設
けて気体を吸気し、ケース13の側面のガスの排気口1
4から気体を吐き出すもので、ケース13内の円筒部2
内部に、回転体1が軸4を介して上部の転がり軸受7と
下部の転がり軸受8によって保持され、回転体1の下部
の軸4に高周波モータ3の回転子を備えて、ケース12
の高周波モータ3により高速回転するもので、回転体1
の上部の外周部分に回転翼1aが複数段に配列され、こ
れと対向して円筒部2の内側に固定翼2aが複数段に配
列されている。回転体1を高速で回転することにより、
ポンプ作用が生じ、ガスの吸気口6側とガスの排気口1
4側の圧力差が生じる。そして、モータ室9の下部に設
けられたケース12内に、潤滑油10を溜める空間が設
けられ、転がり軸受8及び転がり軸受7に、潤滑油10
が供給される。一方、軸封部5に設けられた転がり軸受
7を通してモータ室9から、潤滑油10のミストが排気
室に侵入しないように、ガス供給口15から軸封ガス、
例えば窒素などの不活性ガスが導入され、排気口14の
方向に、ガスを強制的に流している。
FIG. 3 shows a cross section of a turbo type dry vacuum pump. This vacuum pump is provided with a gas intake port 6 at an upper portion to inhale gas, and a gas exhaust port 1 on a side surface of the case 13.
4 is to discharge gas from the cylindrical portion 2 in the case 13.
Inside, the rotating body 1 is held by an upper rolling bearing 7 and a lower rolling bearing 8 via a shaft 4, and the lower shaft 4 of the rotating body 1 is provided with a rotor of the high-frequency motor 3, and a case 12 is provided.
Rotating at high speed by the high frequency motor 3 of
The rotating blades 1a are arranged in a plurality of stages on the outer peripheral portion of the upper part of the upper surface, and the stationary blades 2a are arranged in a plurality of stages inside the cylindrical portion 2 in opposition thereto. By rotating the rotating body 1 at a high speed,
A pump action occurs, and the gas inlet 6 side and the gas outlet 1
A pressure difference on the four side occurs. A space for storing the lubricating oil 10 is provided in a case 12 provided below the motor chamber 9, and the lubricating oil 10 is provided in the rolling bearings 8 and 7.
Is supplied. On the other hand, the gas supply port 15 prevents the mist of the lubricating oil 10 from entering the exhaust chamber from the motor chamber 9 through the rolling bearing 7 provided in the shaft seal portion 5.
For example, an inert gas such as nitrogen is introduced, and the gas is forced to flow in the direction of the exhaust port 14.

【0004】[0004]

【発明が解決しようとする課題】従来のターボ形ドライ
真空ポンプは以上のように構成されているが、CVD装
置、エッチング装置の排気ポンプとしてターボ形ドライ
真空ポンプを使用する場合、原料ガスがポンプ内で分解
して、生成物をポンプ内に堆積させたり、プロセス過程
での反応生成物のガスが、ポンプ内部で固体状に析出し
たりすることで、ポンプ内部の隙間等が埋められて、ポ
ンプの運転ができなくなるという問題がある。これを防
ぐために排気ガス中にガス組成を変えるために、ポンプ
のステータ側(固定側)からガス圧縮部(ガス圧縮流
路)に向かい不活性ガスを供給している。堆積物により
隙間が埋められる部分に、ガスを供給するためには、狭
い部分に不活性ガス流路を設ける必要があり、その加工
が困難で手間がかかるという問題がある。また、不活性
ガス流路とは別に、転がり軸受を用いている場合、真空
ガス流路に潤滑油が混入しないように、不活性ガスの流
路を設ける必要がある。
The conventional turbo-type dry vacuum pump is constructed as described above. However, when a turbo-type dry vacuum pump is used as an exhaust pump for a CVD apparatus or an etching apparatus, the source gas is pumped. Decomposes in the inside, the product is deposited in the pump, or the gas of the reaction product in the process, the solid precipitates inside the pump, filling the gaps inside the pump, There is a problem that the pump cannot be operated. In order to prevent this, in order to change the gas composition in the exhaust gas, an inert gas is supplied from the stator side (fixed side) of the pump toward the gas compression section (gas compression flow path). In order to supply gas to the portion where the gap is filled with the deposit, it is necessary to provide an inert gas flow path in a narrow portion, and there is a problem that the processing is difficult and time-consuming. Further, when a rolling bearing is used separately from the inert gas flow path, it is necessary to provide an inert gas flow path so that lubricating oil does not enter the vacuum gas flow path.

【0005】本発明は、このような事情に鑑みてなされ
たものであって、CVD装置などのガス反応生成装置に
排気ポンプとして使用する場合、反応ガスによる生成物
がポンプ内のガス圧縮部間を結ぶ狭い隙間等に堆積しな
いようにし、かつ、軸受から真空ガス流路に潤滑油が混
入しないようにした、加工が容易なターボ形ドライ真空
ポンプを提供することを目的とする。
The present invention has been made in view of such circumstances, and when used as an exhaust pump in a gas reaction generating apparatus such as a CVD apparatus, the product of the reaction gas is generated between the gas compression sections in the pump. It is an object of the present invention to provide a turbo-type dry vacuum pump which is easy to work and which is prevented from accumulating in a narrow gap connecting between the bearings and lubricating oil from a bearing into a vacuum gas flow path.

【0006】[0006]

【課題を解決するための手段】上記の目的を達成するた
め、本発明のターボ形ドライ真空ポンプは、回転により
ガス圧縮を可能とする複数段の回転円板を設けた多段円
周流ポンプ部と、それを駆動する高周波モータの回転子
が連結された軸からなる回転体が上部と下部の軸受で保
持され、ガスの吸気を可能とするターボ形ドライ真空ポ
ンプにおいて、前記多段円周流ポンプ部の回転体を釣り
鐘円筒形状とし、その円筒に複数段に設けられた前記回
転円板の各間の周上に複数個の貫通穴を半径方向に備え
るものである。
In order to achieve the above-mentioned object, a turbo-type dry vacuum pump according to the present invention comprises a multi-stage circumferential pump having a plurality of stages of rotating disks capable of compressing gas by rotation. And a rotary body consisting of a shaft to which a rotor of a high-frequency motor driving the rotor is connected is held by upper and lower bearings, and the multi-stage circumferential flow pump is a turbo-type dry vacuum pump capable of taking in gas. The rotating body of the portion has a cylindrical shape of a bell, and a plurality of through holes are provided in the radial direction on the circumference between the rotating disks provided in a plurality of stages in the cylinder.

【0007】そして、多段円周流ポンプ部の回転体の円
筒に設けられた複数個の貫通穴の向きを回転体の回転方
向と同方向とし、回転により内側から外側にガスが流れ
るようにしたものである。
The direction of the plurality of through holes provided in the cylinder of the rotating body of the multi-stage circumferential flow pump is set to the same direction as the rotating direction of the rotating body, so that the gas flows from the inside to the outside by the rotation. Things.

【0008】さらに、回転体を保持する軸受に転がり軸
受を用い、軸受用の潤滑油がガス圧縮部に混入しないよ
うに、外部から不活性ガスを軸受部に供給し、その不活
性ガスが回転体の円筒内側面を通過するガス流路を備え
るものである。
Further, a rolling bearing is used as a bearing for holding the rotating body, and an inert gas is supplied to the bearing from the outside so that lubricating oil for the bearing does not mix into the gas compression section. It has a gas flow path passing through the inner surface of the cylinder of the body.

【0009】また、回転体を保持する軸受に動圧ガス軸
受を用い、外部から不活性ガスを軸受部に供給し、その
不活性ガスが回転体の円筒内側面を通過するガス流路を
備えるものである。
Further, a dynamic pressure gas bearing is used as a bearing for holding the rotating body, and an inert gas is supplied to the bearing portion from the outside, and the inert gas is provided with a gas flow path passing through the inner side surface of the cylinder of the rotating body. Things.

【0010】また、回転体を保持する軸受に静圧ガス軸
受を用い、外部から不活性ガスを軸受部に供給し、その
不活性ガスが回転体の円筒内側面を通過するガス流路を
備えるものである。
In addition, a static pressure gas bearing is used as a bearing for holding the rotating body, an inert gas is supplied to the bearing portion from the outside, and a gas flow path is provided through which the inert gas passes through the inner surface of the cylinder of the rotating body. Things.

【0011】本発明のターボ形ドライ真空ポンプは上記
のように構成されており、ポンプの回転体を釣り鐘円筒
形状とし、その円筒外周に複数段の回転翼を有した円板
を設け、その各回転円板の各間の周上に半径方向に複数
個の貫通穴を設け、回転により内側に設けられたガス流
路から外側にガスが流れるように、貫通穴の向きを回転
体の回転方向と同方向にしている。そして、回転体を保
持する軸受に転がり軸受を用い、軸受用の潤滑油がガス
圧縮部に混入しないように、外部から不活性ガスを軸受
部に供給し、その不活性ガスが回転体の円筒内側面のガ
ス流路を通過する。また、回転体を保持する軸受に動圧
ガス軸受又は静圧ガス軸受を用い、外部から不活性ガス
を軸受部に供給し、その不活性ガスが回転体の円筒内側
面のガス流路を通過する。上記の構造により、ガス圧縮
を可能とする多段円周流ポンプ部は、外側でガス圧縮を
し、内側に不活性ガス流路を設けて、外部から軸受部に
不活性ガスを供給し、不活性ガス流路側をガス圧縮流路
側と同等、あるいは高圧とする。その圧力差によって不
活性ガス流路から複数個の貫通穴に不活性ガスが流れ、
ポンプ内の軸受部、ガス圧縮部間を結ぶ狭い隙間に、確
実に不活性ガスを高速で供給でき、潤滑油の侵入やガス
反応生成物の堆積を防止することができる。また、多段
円周流ポンプ部は、複数の回転円板を積層して組立てる
ことができるので、不活性ガスのガス供給路、ガス流
路、貫通穴などの加工も容易に行なうことができる。
The turbo-type dry vacuum pump of the present invention is constituted as described above. The rotary body of the pump has a cylindrical shape of a bell, and a disk having a plurality of stages of rotary blades is provided on the outer periphery of the cylinder. A plurality of through-holes are provided in the radial direction on the circumference between each of the rotating disks, and the direction of the through-holes is adjusted so that gas flows outward from a gas flow path provided inside by rotation. And the same direction. A rolling bearing is used as the bearing that holds the rotating body, and an inert gas is supplied to the bearing from the outside so that lubricating oil for the bearing does not enter the gas compression section. It passes through the gas flow path on the inner surface. In addition, a dynamic pressure gas bearing or a static pressure gas bearing is used as a bearing for holding the rotating body, and an inert gas is supplied to the bearing portion from the outside, and the inert gas passes through a gas flow path on the inner surface of the cylinder of the rotating body. I do. With the above-described structure, the multi-stage circumferential flow pump section that enables gas compression performs gas compression on the outside, provides an inert gas flow path on the inside, and supplies inert gas from the outside to the bearing section. The active gas channel side is equal to the gas compression channel side or has a high pressure. Due to the pressure difference, the inert gas flows from the inert gas channel to the plurality of through holes,
The inert gas can be reliably supplied at a high speed to a narrow gap between the bearing portion and the gas compression portion in the pump, and the intrusion of lubricating oil and the accumulation of gaseous reaction products can be prevented. Further, since the multi-stage circumferential flow pump section can be assembled by laminating a plurality of rotating disks, the processing of the gas supply path, the gas flow path, the through hole, etc. of the inert gas can be easily performed.

【0012】[0012]

【発明の実施の形態】本発明のターボ形ドライ真空ポン
プの一実施例を、図1、図2を参照しながら説明する。
図1は本発明のターボ形ドライ真空ポンプの断面を示す
図である。図2(a)は釣り鐘状の回転体1bの多段円
周流ポンプ部16の垂直断面図を、図2(b)は平面の
断面図を示す。本ターボ形ドライ真空ポンプは、上方に
円筒状の外周部にネジ溝ポンプ部18を有する回転体1
aと、下方に釣り鐘円筒形状の外周に複数段に回転翼
(ポンプ溝20)を備えた回転円板を有し回転円板の各
間の周上に複数個の貫通穴17を半径方向にかつ回転方
向に設け多段円周流ポンプ部16を備えた回転体1b
と、回転体1aと回転体1bを一つにして、下方に高周
波モータ3aの回転子を取付け、転がり軸受7aおよび
転がり軸受8aによって支持され回転する軸21と、軸
21を高速に回転する高周波モータ3aと、上部に外部
ガスを吸気する吸気口6を有し、内側部にネジ溝ポンプ
部18と多段円周流ポンプ部16を有し、下方側部に圧
縮されたガスを排気する排気口14aを有し、ラビリン
スシール19および転がり軸受7aの軸封部5aに不活
性ガスを供給するガス供給口15aおよびガス供給路2
2を有し、釣り鐘状の回転体1bの内側にガス流路23
の空間を設け、下部に潤滑油10を溜めた円筒部2aと
から構成されている。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of a turbo-type dry vacuum pump according to the present invention will be described with reference to FIGS.
FIG. 1 is a view showing a cross section of a turbo type dry vacuum pump of the present invention. FIG. 2A is a vertical cross-sectional view of the multistage circumferential pumping unit 16 of the bell-shaped rotating body 1b, and FIG. 2B is a plan cross-sectional view. The turbo-type dry vacuum pump has a rotating body 1 having a cylindrical grooved pump portion 18 on a cylindrical outer peripheral portion.
a, a rotating disk having a plurality of stages of rotating blades (pump grooves 20) on the outer periphery of a bell-shaped cylindrical shape below, and a plurality of through holes 17 in the radial direction on the circumference between each rotating disk. Rotator 1b provided with a multi-stage circumferential pump section 16 provided in the rotation direction
The rotor 1a and the rotor 1b are combined into one, and the rotor of the high-frequency motor 3a is attached below, and the shaft 21 supported and rotated by the rolling bearings 7a and 8a, and the high-frequency rotating the shaft 21 at high speed. A motor 3a, an intake port 6 for taking in external gas at an upper part, a thread groove pump part 18 and a multi-stage circular pump part 16 at an inner part, and an exhaust part for exhausting compressed gas at a lower side part. A gas supply port 15a for supplying an inert gas to the labyrinth seal 19 and the shaft sealing portion 5a of the rolling bearing 7a;
2 and a gas flow path 23 inside the bell-shaped rotator 1b.
And a cylindrical portion 2a in which a lubricating oil 10 is stored at a lower portion.

【0013】本ターボ形ドライ真空ポンプは、回転体1
aにネジ溝ポンプ部18、および、回転体1bに多段円
周流ポンプ部16を装着して、高周波モータ3aにより
回転体1a、1bを数万rpmで高速回転させるように
したもので、回転体1bを釣り鐘形状にしたこと、軸封
部5aから潤滑油10が漏れないように、軸受を選択
し、不活性ガスを流すためのガス供給路22及びガス流
路23を設けたこと、そしてガス反応生成物が多段円周
流ポンプ部16の隙間に堆積しないように貫通穴17を
回転方向と同じ方向に設けたことを特徴としている。
[0013] The turbo-type dry vacuum pump comprises a rotating body 1
a, a thread groove pump section 18 is mounted on the rotating body 1b, and a multi-stage circumferential pump section 16 is mounted on the rotating body 1b, and the rotating bodies 1a, 1b are rotated at a high speed of tens of thousands of rpm by the high frequency motor 3a. That the body 1b has a bell shape, that a bearing is selected and that a gas supply passage 22 and a gas passage 23 for flowing an inert gas are provided so that the lubricating oil 10 does not leak from the shaft sealing portion 5a; The through-hole 17 is provided in the same direction as the rotation direction so that the gas reaction product does not accumulate in the gap of the multi-stage circumferential flow pump section 16.

【0014】ネジ溝ポンプ部18は、ポンプの上部に設
けられ、円筒部2a側に螺旋状の溝が設けられ、回転体
1aが高速回転することで、ガス反応装置からの反応後
のガスを吸気口6から吸引するものである。多段円周流
ポンプ部16は、ポンプの下部に設けられ、釣り鐘状の
回転体1bの円筒部の外周に複数段に設けられた、回転
翼のポンプ溝20を備えた回転円板と、それに対向して
円筒部2aに設けられたリング状の溝付き部材からな
り、回転体1bが高速に回転することによって、前段の
ネジ溝ポンプ部18からのガスを圧縮して吸引するもの
である。ガス供給路22は、円筒部2aの外部から、所
定の圧力で不活性ガスをガス供給口15aから軸封部5
aに導入するための通路で、円筒部2aに機械加工で形
成される。軸封部5aは、高速回転する軸21の上部を
保持する転がり軸受7aと、高周波モータの潤滑油10
が転がり軸受7aを通ってガス流路23に漏れ出すこと
がないように設けられたラビリンスシール19とから構
成された部分を示すものである。ラビリンスシール19
は、相対運動する二面間に、微小な食い違いすきま部
(迷路:Labylinth)を設け、流体をシールす
る非接触シールで、その作用は、狭いすき間を漏れる気
体は、流出面積が一定の場合には、そのもれ量はその前
後の圧力差および流れに対する流動抵抗により決まる。
漏れ量を小さくするにはすき間をできるだけ小さくする
ことであるが、それには限度があるので、通路の流動抵
抗を増すことが必要である。したがって流路を複雑にす
ればするほど漏れ量は減少する。ここでは、さらに、ガ
ス流路23に不活性ガスを所定の圧力で導入すること
で、ガス流路23と高周波モータ3aの空間との前後の
圧力差を設けて、潤滑油10がガス流路23に漏れ出さ
ないようにしている。ガス流路23は、釣り鐘状の回転
体1bの内側と、軸21を転がり軸受7aで保持し、そ
の転がり軸受7aを保持している固定側の円筒部2a間
との間に設けられ、外部からガス供給路22を介して、
導入された不活性ガスを流す流路である。貫通穴17
は、回転体1bの釣り鐘円筒形状の外周に、複数段に積
層された回転円板の各間の周上に複数個、半径方向に、
かつ回転方向に向けて設けられたものである。不活性ガ
ス導入によってガス流路23内のガス圧が高くなり、回
転方向に向けて貫通穴17が加工されているので、回転
時にガス流の流れを速め、そのため、ポンプ運転中は釣
り鐘状の内側は、外側(ポンプ圧縮側)に対し高圧とな
て、圧力差を生じ、不活性ガスはこの貫通穴17を通
り、ガス圧縮部間を結ぶ狭い上下の隙間(0.1〜0.
4mm程度)を高速で通過する。これにより、この狭い
隙間にガス反応生成物が堆積するということがなくな
る。そして、貫通穴17の加工は、回転円板一段毎に貫
通穴17を加工し、それを多段に積層することで、釣り
鐘状の多段円周流ポンプ部16を容易に形成することが
できる。
The thread groove pump section 18 is provided on the upper part of the pump, and has a spiral groove on the side of the cylindrical section 2a. When the rotating body 1a rotates at a high speed, the gas after the reaction from the gas reaction apparatus is removed. The suction is performed through the intake port 6. The multi-stage circumferential flow pump section 16 is provided at the lower part of the pump, and is provided at a plurality of stages on the outer periphery of the cylindrical portion of the bell-shaped rotating body 1b. It consists of a ring-shaped grooved member provided on the cylindrical portion 2a opposite thereto, and compresses and sucks gas from the preceding thread groove pump portion 18 by rotating the rotating body 1b at high speed. The gas supply passage 22 is provided with an inert gas at a predetermined pressure from the outside of the cylindrical portion 2 a through the gas supply port 15 a to the shaft sealing portion 5.
This is a passage for introduction into the cylindrical portion 2a, and is formed by machining in the cylindrical portion 2a. The shaft sealing portion 5a includes a rolling bearing 7a for holding an upper portion of a shaft 21 rotating at a high speed, and a lubricating oil 10 for a high frequency motor.
Shows a part constituted by a labyrinth seal 19 provided so as not to leak to the gas flow passage 23 through the rolling bearing 7a. Labyrinth seal 19
Is a non-contact seal that provides a small stagger gap (maze: Labyrinth) between two surfaces that move relative to each other, and seals the fluid. The effect of this is that gas leaking through a narrow gap has a constant outflow area. The amount of leakage depends on the pressure difference before and after the leakage and the flow resistance to the flow.
In order to reduce the amount of leakage, it is necessary to make the gap as small as possible. However, since there is a limit, it is necessary to increase the flow resistance of the passage. Therefore, as the flow path becomes more complicated, the amount of leakage decreases. Here, by introducing an inert gas at a predetermined pressure into the gas flow path 23, a pressure difference between the gas flow path 23 and the space of the high-frequency motor 3a is provided, so that the lubricating oil 10 23 so as not to leak. The gas passage 23 is provided between the inside of the bell-shaped rotator 1b and the fixed-side cylindrical portion 2a that holds the shaft 21 with the rolling bearing 7a and holds the rolling bearing 7a. Through the gas supply passage 22,
This is a flow path through which the introduced inert gas flows. Through hole 17
Are arranged on the outer periphery of the cylindrical shape of the bell of the rotating body 1b, on the circumference between the rotating disks stacked in a plurality of stages, a plurality of them in the radial direction,
And it is provided toward the rotation direction. The introduction of the inert gas increases the gas pressure in the gas flow path 23, and the through holes 17 are formed in the direction of rotation, so that the flow of the gas flow is increased during rotation. The inner side becomes high pressure with respect to the outer side (pump compression side) to generate a pressure difference, and the inert gas passes through the through hole 17 and a narrow upper and lower gap (0.1-0.
(About 4 mm) at a high speed. This prevents gas reaction products from being deposited in the narrow gap. The processing of the through-holes 17 is such that the through-holes 17 are formed for each stage of the rotating disk and are stacked in multiple stages, whereby the bell-shaped multi-stage circumferential pumping unit 16 can be easily formed.

【0015】次に、不活性ガスの流れについて説明す
る。不活性ガスは、ガス供給口15aからガス供給路2
2を通って軸封部5aのガス流路23に導入される。そ
して、ラビリンスシール19及び転がり軸受7aの上部
を流れ、回転体1bの釣り鐘状の内側部に、円筒部2a
との間にガス流路23が設けられており、外圧によって
導入された不活性ガスはここを流れる。回転体1bの回
転円板の各間の周上に複数個の貫通穴17が半径方向
に、かつ回転方向に設けられており、ポンプ運転中は釣
り鐘状の貫通穴17に対し外側(ポンプ圧縮側)に対し
高圧となるため、内外の圧力差によって、不活性ガスは
この貫通穴17を通り、ガス圧縮部間を結ぶ狭い上下の
隙間(0.1〜0.4mm程度)を通り、回転体1bの
ポンプ溝20でさらに押し出され、最後に排気口14a
から、上部からの吸気ガスと共に外部に排気される。こ
のように、不活性ガスは、軸封部5aを通過し、ガス流
路23を流れ、貫通穴17を通り、ガス圧縮部間を結ぶ
狭い隙間を高速で通過するので、潤滑油の侵入やガス反
応生成物の堆積を防止することができる。
Next, the flow of the inert gas will be described. The inert gas is supplied from the gas supply port 15a to the gas supply path 2
2 and is introduced into the gas passage 23 of the shaft sealing portion 5a. Then, it flows over the labyrinth seal 19 and the upper part of the rolling bearing 7a, and the cylindrical portion 2a
And a gas flow path 23 is provided between them, and the inert gas introduced by the external pressure flows therethrough. A plurality of through holes 17 are provided in the radial direction and in the rotation direction on the circumference between the rotating disks of the rotating body 1b. Side), the inert gas passes through the through-holes 17 and the narrow upper and lower gaps (about 0.1 to 0.4 mm) connecting between the gas compression parts, and rotates due to the pressure difference between the inside and outside. It is further pushed out by the pump groove 20 of the body 1b, and finally the exhaust port 14a
And is exhausted to the outside together with the intake gas from above. As described above, the inert gas passes through the shaft sealing portion 5a, flows through the gas passage 23, passes through the through hole 17, and passes through the narrow gap connecting the gas compression portions at a high speed. Accumulation of gaseous reaction products can be prevented.

【0016】そして、本ターボ形ドライ真空ポンプで
は、軸封部5aの軸受として、転がり軸受7aについて
説明してきたが、動圧ガス軸受、静圧ガス軸受を用いる
こともできる。動圧ガス軸受は、軸の回転によってくさ
び形状の軸受すきま内に潤滑剤が押し込められて、圧力
が発生する軸受である。軸21は数万rpmで高速回転
するので、軸封部5aに不活性ガスを流すことにより、
その回転により発生するガス圧でラジアル方向の荷重を
支えることができる。静圧ガス軸受は、軸受外部から圧
力をかけた潤滑剤を強制的に供給する軸受である。この
場合は軸受部に不活性ガスを強制的に圧力をかける機構
を要する。これらの軸受は、流体潤滑状態で運転され、
潤滑膜に発生する圧力によって負荷を支える。請求項3
に記載する転がり軸受7a、8aでは、潤滑油10を用
いた液体潤滑軸受が使用され、請求項4、5に記載する
動圧ガス軸受、静圧ガス軸受では、不活性ガスの気体を
用いた気体潤滑軸受(気体軸受)が使用される。
In this turbo type dry vacuum pump, the rolling bearing 7a has been described as a bearing for the shaft sealing portion 5a, but a dynamic pressure gas bearing or a static pressure gas bearing can also be used. The dynamic pressure gas bearing is a bearing in which a lubricant is pushed into a wedge-shaped bearing clearance by rotation of a shaft, and pressure is generated. Since the shaft 21 rotates at high speed at tens of thousands of rpm, by flowing an inert gas through the shaft sealing portion 5a,
The radial pressure can be supported by the gas pressure generated by the rotation. A hydrostatic gas bearing is a bearing that forcibly supplies a pressurized lubricant from outside the bearing. In this case, a mechanism for forcibly applying an inert gas pressure to the bearing portion is required. These bearings are operated in fluid lubrication,
The load is supported by the pressure generated in the lubricating film. Claim 3
In the rolling bearings 7a and 8a described in (1), a liquid lubricating bearing using the lubricating oil 10 is used, and in the dynamic pressure gas bearing and the static pressure gas bearing according to claims 4 and 5, an inert gas is used. Gas lubricated bearings (gas bearings) are used.

【0017】なお、上記実施例では、上部にネジ溝ポン
プ部18を設けているが、ネジ溝ポンプ部18を有さな
いターボ型ドライ真空ポンプにも本発明を適用すること
ができる。
In the above embodiment, the thread groove pump portion 18 is provided on the upper portion. However, the present invention can be applied to a turbo type dry vacuum pump having no thread groove pump portion 18.

【0018】[0018]

【発明の効果】本発明のターボ形ドライ真空ポンプは上
記のように構成されており、釣り鐘円筒形状をした円筒
外周に複数段に設けられた、回転翼を有した各回転円板
の各間の周上に、半径方向に複数個の貫通穴を回転方向
に設けて、回転により内側から外側にガスが流れるよう
にしている。そして、軸受に転がり軸受を用い、軸受用
の潤滑油がガス圧縮部に混入しないように、外部から不
活性ガスを軸受部に供給し、その不活性ガスを回転体の
円筒内側面に設けられたガス流路に流し、そのガスを上
記の貫通穴に高速で流して、ガス圧縮部間を結ぶ狭い隙
間に、ガス反応生成物が堆積することを防止することが
できる。また、多段円周流ポンプ部は積層構造で組立て
ることができるので、不活性ガスのガス供給路、ガス流
路、貫通穴などの加工も容易に行なうことができる。
The turbo-type dry vacuum pump according to the present invention is constructed as described above, and is provided between a plurality of rotating disks having rotating blades, which are provided in a plurality of stages on the outer periphery of a bell-shaped cylindrical shape. A plurality of through-holes are provided in the rotation direction on the circumference of in the radial direction so that the gas flows from the inside to the outside by the rotation. Then, a rolling bearing is used as the bearing, and an inert gas is supplied to the bearing portion from the outside so that lubricating oil for the bearing does not enter the gas compression portion, and the inert gas is provided on a cylindrical inner surface of the rotating body. The gas is flowed through the gas flow path, and the gas is flowed through the above-mentioned through hole at a high speed, so that the gas reaction product can be prevented from being deposited in a narrow gap connecting the gas compression parts. In addition, since the multi-stage circumferential flow pump section can be assembled in a laminated structure, the processing of the gas supply path, the gas flow path, the through hole, and the like of the inert gas can be easily performed.

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

【図1】 本発明のターボ形ドライ真空ポンプの一実施
例を示す図である。
FIG. 1 is a view showing one embodiment of a turbo type dry vacuum pump of the present invention.

【図2】 本発明のターボ形ドライ真空ポンプの多段円
周流ポンプ部の構造を説明するための図である。
FIG. 2 is a view for explaining a structure of a multistage circumferential flow pump section of the turbo type dry vacuum pump of the present invention.

【図3】 従来のターボ形ドライ真空ポンプの断面構造
を示す図である。
FIG. 3 is a diagram showing a cross-sectional structure of a conventional turbo-type dry vacuum pump.

【符号の説明】[Explanation of symbols]

1、1a、1b…回転体 2、2a…円筒部 3、3a…高周波モータ 4、21…軸 5、5a…軸封部 6…吸気口 7、7a、8、8a…転がり軸受 9…モータ室 10…潤滑油 12、13…ケース 14、14a…排気口 15、15a…ガス供給口 16…多段円周流ポンプ部 17…貫通穴 18…ネジ溝ポンプ部 19…ラビリンスシール 20…ポンプ溝 21…軸 22…ガス供給路 23…ガス流路 1, 1a, 1b ... Rotating body 2, 2a ... Cylindrical part 3, 3a ... High frequency motor 4, 21 ... Shaft 5, 5a ... Shaft sealing part 6 ... Intake port 7, 7a, 8, 8a ... Rolling bearing 9 ... Motor chamber DESCRIPTION OF SYMBOLS 10 ... Lubricating oil 12, 13 ... Case 14, 14a ... Exhaust port 15, 15a ... Gas supply port 16 ... Multistage circular flow pump part 17 ... Through-hole 18 ... Screw groove pump part 19 ... Labyrinth seal 20 ... Pump groove 21 ... Shaft 22: gas supply path 23: gas flow path

Claims (5)

【特許請求の範囲】[Claims] 【請求項1】回転によりガス圧縮を可能とする複数段の
回転円板を設けた多段円周流ポンプ部と、それを駆動す
る高周波モータの回転子が連結された軸からなる回転体
が上部と下部の軸受で保持され、ガスの吸気を可能とす
るターボ形ドライ真空ポンプにおいて、前記多段円周流
ポンプ部の回転体を釣り鐘円筒形状とし、その円筒に複
数段に設けられた前記回転円板の各間の周上に複数個の
貫通穴を半径方向に備えることを特徴とするターボ形ド
ライ真空ポンプ。
1. A rotating body comprising a multi-stage circumferential pump having a plurality of stages of rotating disks capable of compressing gas by rotation and a shaft connected to a rotor of a high-frequency motor for driving the pump. And a turbo-type dry vacuum pump which is held by a lower bearing and allows gas to be taken in, wherein the rotating body of the multi-stage circumferential flow pump section has a bell-shaped cylindrical shape, and the rotating circle provided in a plurality of stages in the cylinder. A turbo-type dry vacuum pump characterized in that a plurality of through holes are radially provided on the circumference between each of the plates.
【請求項2】多段円周流ポンプ部の回転体の円筒に設け
られた複数個の貫通穴の向きを回転体の回転方向と同方
向とし、回転により内側から外側にガスが流れるように
したことを特徴とする請求項1記載のターボ形ドライ真
空ポンプ。
2. The direction of a plurality of through holes provided in a cylinder of a rotating body of a multi-stage circumferential flow pump unit is set to be the same direction as the rotating direction of the rotating body, so that the gas flows from the inside to the outside by the rotation. The turbo-type dry vacuum pump according to claim 1, wherein:
【請求項3】回転体を保持する軸受に転がり軸受を用
い、軸受用の潤滑油がガス圧縮部に混入しないように、
外部から不活性ガスを軸受部に供給し、その不活性ガス
が回転体の円筒内側面を通過するガス流路を備えること
を特徴とする請求項1記載のターボ形ドライ真空ポン
プ。
3. A rolling bearing is used as a bearing for holding a rotating body, and lubricating oil for the bearing is prevented from being mixed into the gas compression section.
2. The turbo-type dry vacuum pump according to claim 1, further comprising a gas flow path that supplies an inert gas to the bearing portion from the outside, and the inert gas passes through a cylindrical inner surface of the rotating body.
【請求項4】回転体を保持する軸受に動圧ガス軸受を用
い、外部から不活性ガスを軸受部に供給し、その不活性
ガスが回転体の円筒内側面を通過するガス流路を備える
ことを特徴とする請求項1記載のターボ形ドライ真空ポ
ンプ。
4. A dynamic pressure gas bearing is used as a bearing for holding a rotating body, an inert gas is supplied to the bearing portion from the outside, and a gas flow path through which the inert gas passes through a cylindrical inner surface of the rotating body is provided. The turbo-type dry vacuum pump according to claim 1, wherein:
【請求項5】回転体を保持する軸受に静圧ガス軸受を用
い、外部から不活性ガスを軸受部に供給し、その不活性
ガスが回転体の円筒内側面を通過するガス流路を備える
ことを特徴とする請求項1記載のターボ形ドライ真空ポ
ンプ。
5. A static pressure gas bearing is used as a bearing for holding a rotating body, an inert gas is supplied from outside to a bearing portion, and the inert gas is provided with a gas flow path passing through a cylindrical inner surface of the rotating body. The turbo-type dry vacuum pump according to claim 1, wherein:
JP2001001014A 2001-01-09 2001-01-09 Turbo dry vacuum pump Pending JP2002202089A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2001001014A JP2002202089A (en) 2001-01-09 2001-01-09 Turbo dry vacuum pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2001001014A JP2002202089A (en) 2001-01-09 2001-01-09 Turbo dry vacuum pump

Publications (1)

Publication Number Publication Date
JP2002202089A true JP2002202089A (en) 2002-07-19

Family

ID=18869698

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001001014A Pending JP2002202089A (en) 2001-01-09 2001-01-09 Turbo dry vacuum pump

Country Status (1)

Country Link
JP (1) JP2002202089A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006503229A (en) * 2002-10-14 2006-01-26 ザ ビーオーシー グループ ピーエルシー Rotating piston vacuum pump with cleaning equipment
JP2008248754A (en) * 2007-03-29 2008-10-16 Tokyo Electron Ltd Turbo-molecular pump, substrate process device, and deposit adhesion inhibition method for turbo-molecular pump

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6079579A (en) * 1983-10-05 1985-05-07 Tokyo Electric Co Ltd Magnetic disc recording device
JPH0389986A (en) * 1989-09-01 1991-04-15 Kubota Corp Apparatus for washing piercing passage
JPH09158162A (en) * 1995-12-07 1997-06-17 Sutabii:Kk Accurately detecting method of soft and hard place of ground
JPH11311198A (en) * 1998-04-27 1999-11-09 Shimadzu Corp Turbo type vacuum evacuation device
JP2000274391A (en) * 1999-03-23 2000-10-03 Seiko Seiki Co Ltd Over hang type turbo molecular pump

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6079579A (en) * 1983-10-05 1985-05-07 Tokyo Electric Co Ltd Magnetic disc recording device
JPH0389986A (en) * 1989-09-01 1991-04-15 Kubota Corp Apparatus for washing piercing passage
JPH09158162A (en) * 1995-12-07 1997-06-17 Sutabii:Kk Accurately detecting method of soft and hard place of ground
JPH11311198A (en) * 1998-04-27 1999-11-09 Shimadzu Corp Turbo type vacuum evacuation device
JP2000274391A (en) * 1999-03-23 2000-10-03 Seiko Seiki Co Ltd Over hang type turbo molecular pump

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006503229A (en) * 2002-10-14 2006-01-26 ザ ビーオーシー グループ ピーエルシー Rotating piston vacuum pump with cleaning equipment
JP2008248754A (en) * 2007-03-29 2008-10-16 Tokyo Electron Ltd Turbo-molecular pump, substrate process device, and deposit adhesion inhibition method for turbo-molecular pump

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