JPH01219393A - Molecular vacuum pump - Google Patents

Molecular vacuum pump

Info

Publication number
JPH01219393A
JPH01219393A JP63047762A JP4776288A JPH01219393A JP H01219393 A JPH01219393 A JP H01219393A JP 63047762 A JP63047762 A JP 63047762A JP 4776288 A JP4776288 A JP 4776288A JP H01219393 A JPH01219393 A JP H01219393A
Authority
JP
Japan
Prior art keywords
blade
blades
stationary
rotor
resin
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
JP63047762A
Other languages
Japanese (ja)
Inventor
Takao Matsumoto
隆夫 松本
Ryuichi Sakamoto
隆一 坂本
Isamu Taruya
樽谷 勇
Shigeki Hagiwara
萩原 茂喜
Bunichi Taniguchi
谷口 文一
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.)
Daikin Industries Ltd
Original Assignee
Daikin Industries 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 Daikin Industries Ltd filed Critical Daikin Industries Ltd
Priority to JP63047762A priority Critical patent/JPH01219393A/en
Publication of JPH01219393A publication Critical patent/JPH01219393A/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
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • 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
    • F04D19/042Turbomolecular vacuum pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/40Organic materials
    • F05D2300/43Synthetic polymers, e.g. plastics; Rubber

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Non-Positive Displacement Air Blowers (AREA)

Abstract

PURPOSE:To aim at reduction in working manhour and improvement in accuracy of finishing as well as to get rid of such an accident as cutting operator's hands by installing an axial flow type pumping element, arranged with a moving blade and a stationary blade alternately, in space between an inlet and an outlet, and forming the stationary blade with plastics. CONSTITUTION:An axial flow type pumping element 7, where plural pieces of moving blades 5 being rotated by a rotor 4 and plural pieces of stationary blades 6 being fixed to a casing 1 are set up in space between a inlet 2 and an outlet 3. Both first and second stationary blades 61, 62 constituting the stationary blades 6 are formed with plastics. Thus, working manhour for the stationary blade 6 is reducible, and that forming accuracy for the stationary blade 6 is securable. In addition, such a possibility that an operator or the like may cut his hands by its edge part can be lessened as little as negligible.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明は、動翼と静翼とをもつ軸流形ポンプ要素を備え
、おおむね1ト一ル程度の低真空から10−@ )−ル
程度の超高真空に至る広範囲な真空度を達成し、例えば
半導体製造部門等での使用に好適な分子式真空ポンプに
関する。
DETAILED DESCRIPTION OF THE INVENTION (Field of Industrial Application) The present invention is equipped with an axial flow pump element having rotor blades and stator vanes, and is capable of pumping from a low vacuum of approximately 1 torr to 10 torr. The present invention relates to a molecular vacuum pump that achieves a wide range of degrees of vacuum up to an ultra-high vacuum, and is suitable for use, for example, in the semiconductor manufacturing sector.

(従来の技術) この種真空ポンプは、特公昭47−33446号公報等
により古くから知られ、かつ、第10゜図に示すように
、円周上に複数の羽根(a)をもつ動翼(A)と、同じ
く円周上に複数の羽根(b)をもつ静翼(B)とを交互
に積層した軸流形ポンプ要素CP)を備え、動翼(A)
を支持するロータ(R)を高速回転させて吸気口(L)
から排気口(H)に向けて真空引きを行うようにしてい
る。ところで、動翼(A)及び静翼(B)は、円周上に
複数の羽根(a)(b)をもち、これら翼(A)(B)
が交互に積層されて、しかも動翼(A)が静翼(B)の
間で高速回転されることから、これら翼(A)(B)に
は高精度な加工が要求され、該6翼(A)(B)を得る
には、−般には削り出しによる機械加工が採用される。
(Prior art) This type of vacuum pump has been known for a long time from Japanese Patent Publication No. 47-33446, etc., and as shown in Fig. 10, a moving blade having a plurality of blades (a) on the circumference. (A) and stator vanes (B) having a plurality of vanes (b) on the circumference are alternately stacked.
Rotate the rotor (R) that supports the intake port (L) at high speed.
Vacuuming is performed from the inside toward the exhaust port (H). By the way, the rotor blade (A) and the stationary blade (B) have a plurality of blades (a) and (b) on the circumference, and these blades (A) and (B)
These six blades (A) and (B) require high-precision machining because they are alternately stacked and the rotor blades (A) are rotated at high speed between the stationary blades (B). To obtain (A) and (B), machining by cutting is generally employed.

しかし、削り出し加工によれば、加工そのものが煩雑で
加工時間も長時間を要し、又、削りくずが無駄に捨てら
れて材料歩留りも悪い。
However, according to the machining process, the machining itself is complicated and takes a long time, and the shavings are wasted and the material yield is poor.

こうしたことから、実開昭θ0−143192号公報に
開示され、第11図に示すように、−枚の金属板(W)
から動翼(A)及び静翼(B)を打ち抜いた後、各羽根
(a)(b)をプレス加工により援って傾斜させるよう
にしたものや、特開昭81−215492号公報に開示
され、第12図に示すように、鋸刃(K)を有した一対
のプレス金型(M)で金属板(W)をサントイフチ状に
プレスして、各羽根(a)(b)の間を切り離すと同時
に傾斜させる加工技術が提案され、加工性改善を図るべ
くしている。
For this reason, as disclosed in Japanese Utility Model Application Publication No. 0-143192, as shown in FIG.
After punching the rotor blades (A) and stationary blades (B) from a blank, the blades (a) and (b) are supported by press processing to make them inclined, and the method disclosed in Japanese Patent Application Laid-Open No. 81-215492. As shown in Fig. 12, the metal plate (W) is pressed into a square shape with a pair of press dies (M) having saw blades (K), and the spaces between each blade (a) and (b) are A processing technique has been proposed in which the material is separated and tilted at the same time, with the aim of improving processability.

(発明が解決しようとする課題) しかし、前者の改善案では、打ち抜き加工と捩り加工と
の2工程を要するし、金属材料を用いていることから羽
根(a)(b)のエッヂ部分等で積層作業時等に作業者
が手を切ってしまう虞もある。又、後者の改善案では、
1工程で加工が行えるが、鋸刃(K)によるシャープな
切口ができ、作業者への安全性が全く図れない。更に、
両者共、1枚の金属板(W)を変形させて羽根(a)(
b)を傾斜させているため、材料の残留応力等により傾
斜角度等に狂いが生じる虞もある。
(Problem to be solved by the invention) However, the former improvement plan requires two steps, punching and twisting, and since metal materials are used, the edges of the blades (a) and (b), etc. There is also a risk that workers may cut their hands during lamination work. Also, in the latter improvement plan,
Processing can be done in one step, but the saw blade (K) creates a sharp cut, which does not provide any safety for the worker. Furthermore,
In both cases, a single metal plate (W) is deformed to form a blade (a) (
b) is inclined, there is a risk that the angle of inclination may be distorted due to residual stress of the material, etc.

その上、この種の真空ポンプが用いられる半導体製造部
門等ではフッ素系や塩素系の腐食性ガス等が多用され、
該腐食性ガスが充填されたチャンバー等をも真空引きす
ることがあるが、こうした場合、金属材料では腐食し易
いことから、一般に耐腐食性の樹脂コーティング処理を
別途行う必要もある。
Furthermore, corrosive gases such as fluorine-based and chlorine-based gases are frequently used in the semiconductor manufacturing sector where this type of vacuum pump is used.
A chamber filled with the corrosive gas may also be evacuated, but in such a case, since metal materials are easily corroded, it is generally necessary to separately apply a corrosion-resistant resin coating treatment.

更に、第9図に概略示すように、一般に、金属材料では
、該金属中に含まれる気体分子の初期含n量は少ない(
樹脂に比べて)が、該金属からの分子放出には長時間を
要する(樹脂に比べて)という物理的な特性があり、真
空引きを進行させても、6翼(A)(B)から長期にわ
たって放出される分子により真空度が阻害される懸念も
ある。
Furthermore, as schematically shown in FIG. 9, in metal materials, the initial content of gas molecules contained in the metal is generally small (
However, it has a physical property that it takes a long time for the molecules to be released from the metal (compared to resin), and even if vacuuming progresses, it will not be possible to release molecules from the six wings (A) and (B). There is also a concern that the vacuum level may be impaired by molecules released over a long period of time.

以上のことから、本発明では、樹脂による成形加工に注
目したのであるが、ただこの場合、動翼側は高速回転さ
れて剛性をある程度保証する必要があるため樹脂化への
積極的な対象とすることは見送り、任意的なものとし、
少なくとも静翼を樹脂化することにより、加工工数の削
減と加工精度の向上を図ると共に、エッヂ部分で作業者
等が手を切る懸念も少な(シ、又、耐腐食性ガスや含何
分子放出による悪影響も低減できる分子式真空ポンプを
提供することを目的とする。
Based on the above, in the present invention, we focused on molding using resin, but in this case, since the rotor blade side is rotated at high speed and it is necessary to guarantee a certain degree of rigidity, we decided to actively use resin. The matter will be postponed and left as a matter of discretion.
By making at least the stator blades resin, it is possible to reduce the number of machining steps and improve machining accuracy, and there is also less concern that workers will cut their hands at the edges (also, there is no possibility of releasing corrosive gases or molecules containing them). The purpose of the present invention is to provide a molecular vacuum pump that can also reduce the adverse effects caused by.

(課題を解決するための手段) そこで、本発明では、吸気口(2)と排気口(3)との
間に、動翼(5)と静翼(θ)とを交互に配列した軸流
形ポンプ要素(7)を設けた分子式真空ポンプにおいて
、前記静翼(6)を合成樹脂で形成することとした。
(Means for Solving the Problems) Therefore, the present invention provides an axial flow system in which rotor blades (5) and stationary blades (θ) are alternately arranged between the intake port (2) and the exhaust port (3). In the molecular vacuum pump provided with a shaped pump element (7), the stationary blade (6) is made of synthetic resin.

(作用) 静翼(θ)を樹脂化することにより、該静翼(6)を成
形により一度に加工が行え、その加工工数が削減できる
と共に、羽根の傾斜角度が後に狂う弊も排除できる。又
、同樹脂化により該静翼(6)のエッヂ部分での鋭さが
緩和でき積層作業等の安全性が確保できる。更に、腐食
性ガスによる腐食も低減できる。その上、樹脂材料は、
気体分子の初期含有量は多いものの、短期間でその大半
が放出される特質をもつため、真空引が進行された段階
では真空度が阻害される難も低減できる。
(Function) By making the stator vane (θ) resin, the stator vane (6) can be processed at once by molding, the number of processing steps can be reduced, and the disadvantage that the inclination angle of the blade becomes incorrect later can also be eliminated. Furthermore, by using the same resin, the sharpness at the edge portion of the stator vane (6) can be alleviated, and safety in lamination work, etc. can be ensured. Furthermore, corrosion due to corrosive gases can also be reduced. Moreover, the resin material is
Although the initial content of gas molecules is large, most of them are released in a short period of time, so it is possible to reduce the problem of the degree of vacuum being disturbed once the vacuum is drawn down.

(実施例) 第1図において、(1)は概略円筒を呈するケーシング
であり、−側に設ける吸気口(2)と他側に設ける排気
口(3)との間に、ロータ(4)で回転される複数枚の
動翼(5)と、ケーシング(1)に固定される複数枚の
静翼(6)とを交互配列した軸流形ポンプ要素(7)を
配設し、モータ(40)によるロータ(4)の高速回転
(例えば3θOOOrpm)により、動翼(5)を分子
速度に近い200〜400m/s程度の周速度で動かし
、吸気口フランジ(20)に取付ける半導体ウェハ等の
チャンバー(21)内の真空引きを行うようにしている
(Example) In Fig. 1, (1) is a casing having a roughly cylindrical shape, and a rotor (4) is connected between an intake port (2) provided on the negative side and an exhaust port (3) provided on the other side. An axial pump element (7) is provided, in which a plurality of rotating rotor blades (5) and a plurality of stationary blades (6) fixed to the casing (1) are arranged alternately, and a motor (40 ) by rotating the rotor (4) at high speed (e.g. 3θOOOrpm), the rotor blade (5) is moved at a circumferential speed of about 200 to 400 m/s, which is close to the molecular speed, and the chamber for semiconductor wafers etc. is attached to the inlet flange (20). (21) The inside is evacuated.

尚、モータ(40)は架構(41)に支持され、下方に
備える油滴め(42)からオイルピックアップ(43)
を介して駆動軸(44)内の給油路(45)に油を汲上
げ、上下の軸受(46)(47)に給油を行うと共に、
モータ室<4g>を区画蓋(49)にて、吸気口(2)
から排気口(3)に至る排気流路(23)側とオイルシ
ールするようにしている。又、第1図のものは、軸流ポ
ンプ要素(7)と組合わせて、ロータ(4)のスカート
部を利用した回転内筒(6)と、静翼(6)の支持部を
兼ねる静止外筒(6)とを備え、かつ、回転内筒(6)
に吸気側で深く排気側で浅いネジ溝(10)を設けたネ
ジ形ポンプ要素(11)を併用するものであるが、軸流
ポンプ要素(7)の単独構成のものでもよい。
The motor (40) is supported by a frame (41), and an oil pickup (43) is provided from an oil droplet (42) provided below.
The oil is pumped up to the oil supply passage (45) in the drive shaft (44) through the oil supply passageway (45), and is supplied to the upper and lower bearings (46) (47).
Separate the motor chamber <4g> with the compartment lid (49) and the air intake port (2).
The exhaust flow path (23) side from the exhaust port (3) to the exhaust port (3) is sealed with oil. In addition, the one in Fig. 1 is a rotating inner cylinder (6) that uses the skirt of the rotor (4) in combination with an axial flow pump element (7), and a stationary pump that also serves as a support for the stationary blades (6). an outer cylinder (6), and a rotating inner cylinder (6).
Although a screw-type pump element (11) having a thread groove (10) deep on the intake side and shallow on the exhaust side is used in combination with the pump element, the axial flow pump element (7) alone may be used.

動翼(5)は、第2図及び第3図に明示するように、羽
根形状を異にする二群を備え、吸気口(2)に近い側の
第1動翼(51)(第2図)に形成する羽根(510)
の長さ(Ll)及び傾斜角度(θ1)を、遠い側の第2
動翼(52)(第3図)に形成する羽根(520)のそ
れ(L2)(θ2)よりそれぞれ太き(している。同様
に、静翼(6)も第4図及び第5図に明示するように二
群備え、第1動翼(51)に対応する第1静翼(C31
)(第4図)の羽根(610)の長さ(L3)及び傾斜
角度(θ3)を、第2動翼(52)に対応する第2静翼
(82)(第5図)の羽根(620)のそれ(L4)(
θ4)より大きくしている。
As clearly shown in FIGS. 2 and 3, the rotor blade (5) includes two groups of blades with different shapes, and includes a first rotor blade (51) (a second rotor blade) on the side closer to the intake port (2). Feather (510) formed on the figure)
The length (Ll) and inclination angle (θ1) of the second
They are thicker (L2) (θ2) than those of the blades (520) formed on the rotor blades (52) (Fig. 3).Similarly, the stator blades (6) are also As shown in the figure, there are two groups, and the first stationary blade (C31
) (Fig. 4), the length (L3) and inclination angle (θ3) of the blade (610) of the second stationary blade (82) (Fig. 5) corresponding to the second moving blade (52) ( 620) that of (L4) (
θ4).

以上の構成において、静翼(6)を構成する第1及び第
2静翼(61)(82)を合成樹脂化する。該樹脂には
、例えば、カーボンファイバー等を複合したFRP等が
適している。
In the above configuration, the first and second stator blades (61) and (82) constituting the stator blade (6) are made of synthetic resin. For example, FRP composited with carbon fiber or the like is suitable for the resin.

又、各静翼(81)Cf32)は、動翼(51)(52
)をロータ(4)の上部支持筒(50)に積層して組立
てた後に、該各動翼の間に挿入できるように、各々二分
割構造(81a、81b)(82a、82b)としてい
る。これには、各静翼(81)(62)を円板状に樹脂
で一体形成した後に中央で切断するとよい。又、静翼(
81)  (62)を樹脂化するに際し、予め2部材を
別型にて形成し、第6図に示すように、各部材の円周方
向付き合わせ部分(61aと81b1及び、82aと6
2b)に、一対の段部(11)(12)と、一対の保合
突起(13)及びその保合孔(14)とを設け、2部材
の確実な付き合わせが行えるようにしてもよい。これら
段部(11)等は、樹脂成形により容易に形成できる。
In addition, each stator blade (81) Cf32) is a rotor blade (51) (52).
) are stacked and assembled on the upper support cylinder (50) of the rotor (4), and then the two-split structure (81a, 81b) (82a, 82b) can be inserted between the rotor blades. For this purpose, each stator vane (81) (62) may be integrally formed into a disk shape with resin and then cut at the center. Also, static wings (
81) When converting (62) into resin, two members are formed in advance using separate molds, and as shown in FIG.
2b) may be provided with a pair of step portions (11) and (12), a pair of retaining protrusions (13), and a retaining hole (14) thereof, so that the two members can be reliably brought into contact with each other. . These step portions (11) etc. can be easily formed by resin molding.

各静翼(61)(82)は、ケーシング(1)側への支
持部を兼ねる静止外筒(9)の上部にに、−枚毎に第7
図に示す円環本体(15)に静翼(61又は62)の支
持面(16)及び押え面(17)と、インロー保合部(
16)及び被係合部(19)とを形成したスペーサ(6
0)を介して積層される。この場合、該スペーサ(60
)も樹脂化するのが好ましい。又、第8図に示すように
、静翼(81)(132)の各外周部に、厚肉状の円環
部(800)を一体形成しスペーサ(60)の代わりに
してもよい。
Each stationary blade (61) (82) is provided with a seventh blade at the top of the stationary outer cylinder (9) which also serves as a support to the casing (1) side.
The support surface (16) and pressing surface (17) of the stationary blade (61 or 62) are attached to the annular main body (15) shown in the figure, and the spigot retaining portion (
16) and a spacer (6) formed with an engaged portion (19).
0). In this case, the spacer (60
) is also preferably made into a resin. Further, as shown in FIG. 8, thick-walled annular portions (800) may be integrally formed on the outer periphery of each of the stationary blades (81) and (132) in place of the spacer (60).

以上の構成によれば、各静翼(81)(82)は、樹脂
で一度に成形加工が行え、しかも、羽根(θ10)(θ
20)のエッヂ部分等で作業者が手を切ったりする弊も
防止できる。更に、前記チャンバー(21)からフッ素
系や塩素系の腐食性ガスが排気されるような場合でも、
各静翼(81)(62)は、合成樹脂で形成されている
ため、腐食による損傷を受けることもない。その上、第
9図に示すように、樹脂材料は、気体分子の初期含有量
は多いものの、短期間でその大半が放出される特質をも
つため、真空引きがある程度進行された段階では真空度
が阻害される難も低減できる。
According to the above configuration, each stationary blade (81) (82) can be molded at once with resin, and the blade (θ10) (θ
20) can also prevent the worker from cutting his or her hand on the edge part. Furthermore, even if fluorine-based or chlorine-based corrosive gas is exhausted from the chamber (21),
Since each stationary blade (81) (62) is made of synthetic resin, it will not be damaged by corrosion. Furthermore, as shown in Figure 9, although resin materials have a large initial content of gas molecules, most of them are released in a short period of time, so once the vacuum has been drawn to a certain extent, the vacuum level The difficulty of being inhibited can also be reduced.

(発明の効果) 本発明では、静翼(6)の樹脂化により、該静翼(6)
の加工工数を削減でき、しかも該静翼(6)の形成精度
を確保できると共に、エッヂ耶分で作業者等が手を切る
懸念も少なくできる。
(Effect of the invention) In the present invention, by making the stator blade (6) resin, the stator blade (6)
It is possible to reduce the number of processing steps for the stator blade (6), ensure the formation accuracy of the stationary blade (6), and reduce the fear that the operator will cut his/her hand due to the edge.

又、例えば半導体製造部門等でフッ素系や塩素系等の腐
食性ガスが充填されたチャンバーの排気を行うような場
合でも、静翼(6)が腐食損傷を受けることがなく、耐
久性が向上できる。
Furthermore, even when a chamber filled with corrosive gases such as fluorine or chlorine gases is evacuated in the semiconductor manufacturing sector, the stationary blades (6) will not be damaged by corrosion, resulting in improved durability. can.

更に、樹脂材料は、気体分子の初期含有量は多いものの
、短期間でその大半が放出される特質をもつため、実使
用段階で真空度が阻害される懸念も低減できる。
Furthermore, although the resin material initially contains a large amount of gas molecules, most of the gas molecules are released in a short period of time, so that the concern that the degree of vacuum will be impaired during actual use can be reduced.

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

第1図は本発明真空ポンプの縦断面図、第2図及び第3
図は動翼の形状を示す図、第4図及び第5図は静翼の形
状を示す図、第6図は二分割した静翼の付き合わせ部分
の構造例を示す拡大断面図、第7図は静翼のスペーサの
断面図、第8図は静翼の他の実施例を示す断面図、第9
図は含有分子の放出特性を示す図、第10図は従来ポン
プの縦断面図、第11図及び第12図は従来の翼加工技
術の説明図である。 (2)・・・・吸気口 (3)・・・・排気口 (5)・・・・動翼 (6)・・・・静翼 (7)・・・・軸流形ポンプ要素 出願人 ダイキン工業株式会社化 第8図 第4図 6 jl       01θ 第5図 j 6Z            σ2θ第8図 時閉 第10図
Fig. 1 is a vertical sectional view of the vacuum pump of the present invention, Fig. 2 and Fig. 3 are
Figure 4 shows the shape of the moving blade, Figures 4 and 5 show the shape of the stator blade, Figure 6 is an enlarged sectional view showing an example of the structure of the mating part of the stator blade divided into two parts, and Figure 7 shows the shape of the stator blade. The figure is a cross-sectional view of a spacer of a stator blade, FIG. 8 is a cross-sectional view showing another embodiment of a stator blade, and FIG.
10 is a longitudinal sectional view of a conventional pump, and FIGS. 11 and 12 are illustrations of conventional blade processing technology. (2)... Intake port (3)... Exhaust port (5)... Moving blade (6)... Stator vane (7)... Axial flow pump element Applicant Daikin Industries, Ltd. Figure 8 Figure 4 Figure 6 jl 01θ Figure 5 j 6Z σ2θ Figure 8 Closed Figure 10

Claims (1)

【特許請求の範囲】[Claims] 1)吸気口(2)と排気口(3)との間に、動翼(5)
と静翼(6)とを交互に配列した軸流形ポンプ要素(7
)を設けた分子式真空ポンプにおいて、前記静翼(6)
を合成樹脂で形成していることを特徴とする分子式真空
ポンプ。
1) Between the intake port (2) and the exhaust port (3), there is a rotor blade (5)
An axial pump element (7) in which stator vanes (6) are arranged alternately.
), the stator blade (6)
A molecular vacuum pump characterized by being made of synthetic resin.
JP63047762A 1988-02-29 1988-02-29 Molecular vacuum pump Pending JPH01219393A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP63047762A JPH01219393A (en) 1988-02-29 1988-02-29 Molecular vacuum pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP63047762A JPH01219393A (en) 1988-02-29 1988-02-29 Molecular vacuum pump

Publications (1)

Publication Number Publication Date
JPH01219393A true JPH01219393A (en) 1989-09-01

Family

ID=12784383

Family Applications (1)

Application Number Title Priority Date Filing Date
JP63047762A Pending JPH01219393A (en) 1988-02-29 1988-02-29 Molecular vacuum pump

Country Status (1)

Country Link
JP (1) JPH01219393A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006170217A (en) * 1997-06-27 2006-06-29 Ebara Corp Turbo molecular pump
JP2006348935A (en) * 2005-06-11 2006-12-28 Pfeiffer Vacuum Gmbh Stator disk for turbo molecular pump
WO2015000700A1 (en) * 2013-07-05 2015-01-08 Oerlikon Leybold Vacuum Gmbh Stator disk for a turbomolecular pump, having with continuous and closed transitions between blades and disk ring
CN104747465A (en) * 2013-12-25 2015-07-01 株式会社岛津制作所 Vacuum pump
EP2894347A4 (en) * 2012-09-06 2016-04-20 Edwards Japan Ltd Fixed-side member and vacuum pump
GB2557679A (en) * 2016-12-15 2018-06-27 Edwards Ltd Stator blade unit for a turbomolecular pump

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4711358Y1 (en) * 1968-09-27 1972-04-26
JPS5136384Y2 (en) * 1972-05-19 1976-09-07

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4711358Y1 (en) * 1968-09-27 1972-04-26
JPS5136384Y2 (en) * 1972-05-19 1976-09-07

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006170217A (en) * 1997-06-27 2006-06-29 Ebara Corp Turbo molecular pump
JP2006348935A (en) * 2005-06-11 2006-12-28 Pfeiffer Vacuum Gmbh Stator disk for turbo molecular pump
EP2894347A4 (en) * 2012-09-06 2016-04-20 Edwards Japan Ltd Fixed-side member and vacuum pump
US10704555B2 (en) 2012-09-06 2020-07-07 Edwards Japan Limited Stator-side member and vacuum pump
WO2015000700A1 (en) * 2013-07-05 2015-01-08 Oerlikon Leybold Vacuum Gmbh Stator disk for a turbomolecular pump, having with continuous and closed transitions between blades and disk ring
CN104747465A (en) * 2013-12-25 2015-07-01 株式会社岛津制作所 Vacuum pump
US10132329B2 (en) 2013-12-25 2018-11-20 Shimadzu Corporation Vacuum pump
GB2557679A (en) * 2016-12-15 2018-06-27 Edwards Ltd Stator blade unit for a turbomolecular pump

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