JP2010096007A - Rotor of molecular pump - Google Patents

Rotor of molecular pump Download PDF

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JP2010096007A
JP2010096007A JP2008264834A JP2008264834A JP2010096007A JP 2010096007 A JP2010096007 A JP 2010096007A JP 2008264834 A JP2008264834 A JP 2008264834A JP 2008264834 A JP2008264834 A JP 2008264834A JP 2010096007 A JP2010096007 A JP 2010096007A
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rotor
molecular pump
rotating shaft
flange surface
pump
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JP5211408B2 (en
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Takahiro Uehara
孝浩 上原
Soro Yoshida
素朗 吉田
Shigeyoshi Nakatsuji
重義 中辻
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Osaka Vacuum Ltd
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Osaka Vacuum Ltd
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Abstract

<P>PROBLEM TO BE SOLVED: To prevent the loosening of the engagement of a rotor and a rotating shaft caused by the deformation of the rotor by centrifugal forces acting a large number of rotating blades which are protrusively arranged at the external periphery of the rotor, in the rotor of a turbo-molecular pump which has the rotating shaft at its center and rotates at high speed. <P>SOLUTION: The rotor 1 of the molecular pump has rotor blade stages comprising the plurality of rotor blades 1 and installed in a radially protruding manner and in multiple stages at the external periphery of a cylindrical hollow hub 1a. The rotor 1 is formed in a cup shape with a boss 1c provided at an end of the hub part 1a and axially protruding. An end of the rotating shaft 2 is fitted in a shaft hole 1d formed at the boss 1c, and the rotor is fastened to the rotating shaft 2 with a nut 3 screwed to a screw 2a at the end of the rotating shaft. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

本発明は、中真空から高真空にわたる圧力範囲の真空発生に使用されるターボ分子ポンプや複合分子ポンプ等の分子ポンプのロータに関する。   The present invention relates to a rotor of a molecular pump such as a turbo molecular pump or a composite molecular pump used for generating a vacuum in a pressure range from a medium vacuum to a high vacuum.

一般のターボ分子ポンプ又は複合分子ポンプのロータは、中心部に回転軸を有してケーシング内に立設され、毎分数万回の高速回転を行なう。   A rotor of a general turbo molecular pump or a composite molecular pump has a rotating shaft at the center and is erected in a casing and rotates at a high speed of several tens of thousands of times per minute.

このような分子ポンプの例として、油循環ポンプ装置を具備した分子ポンプが知られている(特許文献1参照。)。   As an example of such a molecular pump, a molecular pump provided with an oil circulation pump device is known (see Patent Document 1).

特開2002−61592号公報JP 2002-61592 A

従来のターボ分子ポンプのロータの一例を図5に示した。   An example of a conventional turbomolecular pump rotor is shown in FIG.

ロータaはアルミ合金等からなり、複数の動翼a1を放射状に且つ多段にハブ部a2の外方へ突出させている。   The rotor a is made of an aluminum alloy or the like, and has a plurality of moving blades a1 projecting radially outward from the hub portion a2.

bは回転軸で、該回転軸bは玉軸受c1、c2等により軸支されていると共に、嵌合部b1においてロータaのボス部a3と嵌合しており、袋ナットdによってロータaと回転軸bとが締結されている。   b is a rotary shaft, and the rotary shaft b is pivotally supported by ball bearings c1, c2, etc., and is fitted to the boss portion a3 of the rotor a at the fitting portion b1, and is connected to the rotor a by a cap nut d. The rotating shaft b is fastened.

然して前記ハブ部a2は、内側にボス部a3が形成されている部分の外周部にも動翼a1を突出させて有している。   However, the hub part a2 has a moving blade a1 protruding from the outer peripheral part of the part where the boss part a3 is formed inside.

しかしながら、高速回転をするロータaは、動翼a1等にかかる遠心力によって各部に変形をきたす。   However, the rotor a that rotates at a high speed deforms each part due to the centrifugal force applied to the rotor blades a1 and the like.

このロータaの変形が回転軸bとの嵌合部b1のあるボス部a2に及んだときは、ボス部a2の軸孔径が変形して拡大し、回転軸bとの締結力が弱くなり、ロータaと回転軸bとの間に滑りを生ずることがあるという問題があった。又、前記遠心力によってロータaに生ずる応力が過大となり、応力が材料の弾性限界を超えた場合には材料が降伏を起こし、甚だしい場合にはロータaが破断したりすることがあるという問題があった。   When the deformation of the rotor a reaches the boss part a2 having the fitting part b1 with the rotating shaft b, the shaft hole diameter of the boss part a2 is deformed and enlarged, and the fastening force with the rotating shaft b is weakened. There is a problem that slippage may occur between the rotor a and the rotating shaft b. Further, the stress generated in the rotor a by the centrifugal force becomes excessive, and when the stress exceeds the elastic limit of the material, the material yields, and in a severe case, the rotor a may break. there were.

本発明はこれらの問題点を解消し、ロータと回転軸との嵌合部の締結力が弱くならないような分子ポンプのロータを提供することを目的とする。   An object of the present invention is to provide a molecular pump rotor that solves these problems and does not weaken the fastening force of the fitting portion between the rotor and the rotating shaft.

本発明は上記の目的を達成すべく、ターボ分子ポンプ、又はターボ分子ポンプ部とこれに連通するねじ溝ポンプ部とからなる複合分子ポンプにおいて、前記ターボ分子ポンプ又は前記ターボ分子ポンプ部のロータは、複数の動翼からなる動翼段を中空の円筒状のハブ部の外周に放射状に突設すると共に、該ハブ部の末端部に軸方向へ突出するボス部を設けて該ロータをカップ状に形成し、該ボス部を介して該ロータを回転軸に固定するようにした。   In order to achieve the above object, the present invention provides a turbo molecular pump or a composite molecular pump comprising a turbo molecular pump part and a thread groove pump part communicating with the turbo molecular pump part, wherein the turbo molecular pump or the rotor of the turbo molecular pump part is A rotor blade stage composed of a plurality of rotor blades is projected radially on the outer periphery of a hollow cylindrical hub portion, and a boss portion protruding in the axial direction is provided at the end portion of the hub portion so that the rotor is cup-shaped. And the rotor is fixed to the rotating shaft through the boss.

本発明によれば、ターボ分子ポンプ又は複合分子ポンプのターボ分子ポンプ部の高速回転をするロータにおいて、ロータと回転軸との間の嵌合が翼の遠心力により緩むことがなく、従ってロータと回転軸との間に滑りを生じないので、安全な分子ポンプを提供できる効果を有している。   According to the present invention, in a rotor that rotates at a high speed of a turbo molecular pump or a turbo molecular pump part of a composite molecular pump, the fitting between the rotor and the rotating shaft is not loosened by the centrifugal force of the blade, and therefore Since no slip occurs between the rotating shaft and the rotating shaft, a safe molecular pump can be provided.

本発明を実施するための最良の形態の実施例を以下に示す。   Examples of the best mode for carrying out the present invention are shown below.

本発明の実施例1を図1により説明する。   A first embodiment of the present invention will be described with reference to FIG.

図1は本実施例のターボ分子ポンプのロータ1の縦断面図である。   FIG. 1 is a longitudinal sectional view of a rotor 1 of a turbo molecular pump according to this embodiment.

ロータ1はアルミ合金等からなり、中空の円筒状のハブ部1aの外周上に多数の動翼1bを放射状に且つ多段に突出させて有している。   The rotor 1 is made of an aluminum alloy or the like, and has a large number of blades 1b projecting radially and in multiple stages on the outer periphery of a hollow cylindrical hub portion 1a.

前記ロータ1の下端部にはボス部1cが軸方向に突出して設けられており、回転軸2が該ボス部1cの軸孔1dに嵌合して係止されている。   A boss portion 1c is provided at the lower end portion of the rotor 1 so as to protrude in the axial direction, and the rotary shaft 2 is fitted and locked in the shaft hole 1d of the boss portion 1c.

ロータ1は前記ハブ部1aと前記ボス部1cとでカップ状に形成されており、前記多段の動翼翼列は前記ボス部1cに設けられてなく、前記ハブ部1aの内側が中空の部分の外周部にだけ突設している。   The rotor 1 is formed in a cup shape with the hub portion 1a and the boss portion 1c, and the multistage rotor blade row is not provided on the boss portion 1c, and the inside of the hub portion 1a is a hollow portion. It protrudes only at the outer periphery.

3は袋ナットを示し、4はスペーサ、5a及び5bはそれぞれ玉軸受である。   3 is a cap nut, 4 is a spacer, 5a and 5b are ball bearings, respectively.

次に本実施例のターボ分子ポンプのロータ1の使用方法及びその効果について説明する。   Next, a method of using the rotor 1 of the turbo molecular pump of this embodiment and the effects thereof will be described.

ロータ1は、回転軸2を軸支する玉軸受5a、5bを介してターボ分子ポンプのケース(図示せず)内に支承され、モータ(図示せず)によって高速回転する。   The rotor 1 is supported in a turbo molecular pump case (not shown) via ball bearings 5a and 5b that support the rotating shaft 2, and is rotated at high speed by a motor (not shown).

回転軸2はボス部1cに設けた軸孔1dにおいてロータ1と嵌合し、該回転軸2の先端のねじ部2aに螺合する袋ナット3によって回転軸2とロータ1が締結固定される。   The rotary shaft 2 is fitted to the rotor 1 in a shaft hole 1d provided in the boss portion 1c, and the rotary shaft 2 and the rotor 1 are fastened and fixed by a cap nut 3 that is screwed into the screw portion 2a at the tip of the rotary shaft 2. .

ロータ1が高速回転をした場合、動翼1bの遠心力はハブ部1aにおけるフープテンションとして或る程度吸収することができるので、ボス部1cにおける変形を緩和して、軸孔部1dと回転軸2との嵌合が緩むのを防止することができる。   When the rotor 1 rotates at a high speed, the centrifugal force of the moving blade 1b can be absorbed to some extent as a hoop tension in the hub portion 1a. Therefore, the deformation in the boss portion 1c is alleviated, and the shaft hole portion 1d and the rotating shaft 2 can be prevented from loosening.

本発明の実施例2を図2により説明する。   A second embodiment of the present invention will be described with reference to FIG.

図2は本実施例の複合分子ポンプのロータ11の縦断面図であり、12がターボ分子ポンプ部のロータ、13がねじ溝ポンプ部ロータを示す。   FIG. 2 is a longitudinal sectional view of the rotor 11 of the composite molecular pump of the present embodiment, wherein 12 is a turbo molecular pump part rotor and 13 is a thread groove pump part rotor.

ロータ11はアルミ合金等からなり、ターボ分子ポンプ部のロータ12は中空の円筒状のハブ部11aの外周上へ多数の動翼11bを放射状に且つ多段に突出させて有している。   The rotor 11 is made of an aluminum alloy or the like, and the rotor 12 of the turbo molecular pump part has a large number of blades 11b projecting radially and in multiple stages on the outer periphery of a hollow cylindrical hub part 11a.

前記ねじ溝ポンプ部ロータ13は円盤状のディスク部13aと円筒状のロータ部13bとからなり、該ディスク部13aは前記中空の円筒状のハブ部11aの外周部に前記ターボ分子ポンプ部の動翼11bからなる動翼段の下部に連設されている。   The thread groove pump portion rotor 13 is composed of a disk-shaped disk portion 13a and a cylindrical rotor portion 13b, and the disk portion 13a is arranged on the outer periphery of the hollow cylindrical hub portion 11a. It is connected to the lower part of the moving blade stage composed of the blade 11b.

前記ロータ部13bは前記ディスク部13aに直結して下方に円筒状に突出して設けられており、該ロータ部13bの外周部にはねじ溝(図示せず)が刻設されていて、該ロータブ13bの外周部に狭い間隔で対向して設置されているステータ(図示せず)と組み合わさってねじ溝ポンプとして作動する。   The rotor portion 13b is directly connected to the disk portion 13a and protrudes downward in a cylindrical shape. A screw groove (not shown) is formed on the outer peripheral portion of the rotor portion 13b. It operates as a thread groove pump in combination with a stator (not shown) that is installed on the outer peripheral portion of 13b so as to be opposed to each other at a narrow interval.

尚、前記円筒状のハブ部11aの下端部にはボス部11cが軸方向に突出して設けられ、ターボ分子ポンプ部のロータ12はカップ状に形成されている。   A boss portion 11c is provided in the lower end portion of the cylindrical hub portion 11a so as to protrude in the axial direction, and the rotor 12 of the turbo molecular pump portion is formed in a cup shape.

このように多数の動翼11bからなるターボ分子ポンプ部の動翼段と、ねじ溝ポンプ部のロータ部13bを下方へ突出させた円盤状のディスク部13aとは中空の円筒状のハブ部11aの部分に設置されており、これら動翼11bやディスク部13aに生じている遠心力は前記ハブ部11aにおけるフープテンションとして或る程度吸収されて、該ボス部11cと回転軸2との嵌合が緩むことはない。   In this way, the rotor blade stage of the turbo molecular pump part composed of a large number of rotor blades 11b and the disk-like disk part 13a in which the rotor part 13b of the thread groove pump part protrudes downward are a hollow cylindrical hub part 11a. The centrifugal force generated in the rotor blade 11b and the disk portion 13a is absorbed to some extent as the hoop tension in the hub portion 11a, and the boss portion 11c and the rotary shaft 2 are fitted to each other. Will not loosen.

本発明の実施例3を図3により説明する。   A third embodiment of the present invention will be described with reference to FIG.

図3は本実施例のターボ分子ポンプのロータ21の縦断面図である。   FIG. 3 is a longitudinal sectional view of the rotor 21 of the turbo molecular pump of this embodiment.

ターボ分子ポンプのロータ21は、中空円筒状のハブ部21aの外周部の末端部即ち下端部にディスク部22を全周にわたって外方に突設し、該ディスク部22の外方縁部から下方に円筒状の補助ハブ部21bを垂設し、前記ハブ部21aの外周部及び該補助ハブ部12bの外周部に複数の動翼23を放射状にそれぞれ突設している。   The rotor 21 of the turbo molecular pump has a disk portion 22 projecting outward from the outer peripheral portion of the hollow cylindrical hub portion 21a at the end portion, that is, the lower end portion of the hollow cylindrical hub portion 21a. A cylindrical auxiliary hub portion 21b is vertically suspended from the outer peripheral portion of the hub portion 21a and the outer peripheral portion of the auxiliary hub portion 12b.

このように動翼23が突設されている個所はハブ部21aと補助ハブ部21bの外周部であり、ハブ部21aの下端部で回転軸2が嵌合しているボス部21cが前記補助ハブ部21b内に隔離して配置されているので、前記動翼23及びハブ部21aと補助ハブ部21bに生ずる遠心力がボス部21cに及ぼす影響が削減されるので、ボス部21cと回転軸2との嵌合が緩むのを防止することができる。   The portion where the rotor blade 23 is projected in this way is the outer peripheral portion of the hub portion 21a and the auxiliary hub portion 21b, and the boss portion 21c into which the rotating shaft 2 is fitted at the lower end portion of the hub portion 21a is the auxiliary portion. Since the centrifugal force generated in the moving blade 23, the hub portion 21a, and the auxiliary hub portion 21b is reduced, the influence on the boss portion 21c is reduced, so that the boss portion 21c and the rotating shaft are arranged. 2 can be prevented from loosening.

本発明の実施例4を図4により説明する。   A fourth embodiment of the present invention will be described with reference to FIG.

図4は本実施例のターボ分子ポンプのロータ31の縦断面図である。   FIG. 4 is a longitudinal sectional view of the rotor 31 of the turbo molecular pump of this embodiment.

本実施例では、ロータ31と回転軸7との固定手段をフランジ結合とした点が前記実施例1とは異なっている。   The present embodiment is different from the first embodiment in that the fixing means for the rotor 31 and the rotary shaft 7 is a flange connection.

即ち、ロータ31は中空円筒状のハブ部31aの外周部に多数の動翼31bを放射状に且つ多段に突設しており、該ハブ部31aの下端部にはボス部31cが軸方向に突出して形成されている。   That is, the rotor 31 has a large number of blades 31b projecting radially and in multiple stages on the outer periphery of a hollow cylindrical hub portion 31a, and a boss portion 31c projects in the axial direction at the lower end portion of the hub portion 31a. Is formed.

該ボス部31cは下面に複数の締結用ねじ孔8aを有する第1フランジ面7aが形成されており、該第1フランジ面7aの中心部には係止凹部7a1が円形の穴状に凹設されている。   The boss portion 31c is formed with a first flange surface 7a having a plurality of fastening screw holes 8a on the lower surface, and a locking recess 7a1 is formed in a circular hole shape at the center of the first flange surface 7a. Has been.

又、他方の回転軸7の上面には前記第1フランジ面7aと係合可能な第2フランジ面7bが形成されており、該第2フランジ面7bの中心部には係止凸部7b1が円形の棒状に凸設されている。   A second flange surface 7b that can be engaged with the first flange surface 7a is formed on the upper surface of the other rotary shaft 7, and a locking projection 7b1 is formed at the center of the second flange surface 7b. Projected in a circular bar shape.

かくて、前記第1フランジ面7aと第2フランジ面7bとを係合させたとき、これら係止凹部7a1と係止凸部7b1とが嵌合して、前記ロータ31と回転軸7とが常に同芯に係合する。   Thus, when the first flange surface 7a and the second flange surface 7b are engaged with each other, the locking recess 7a1 and the locking projection 7b1 are fitted, and the rotor 31 and the rotary shaft 7 are connected. Always engage concentric.

又、複数のボルト8bによって第1フランジ面7aと第2フランジ面7bとが締結固定されるので、前記動翼31bにかかる遠心力はロータ31と回転軸7が係合する前記第1フランジ面7a及び第2フランジ面7bに悪影響を及ぼすことがない。   Since the first flange surface 7a and the second flange surface 7b are fastened and fixed by the plurality of bolts 8b, the centrifugal force applied to the rotor blade 31b is the first flange surface on which the rotor 31 and the rotary shaft 7 are engaged. 7a and the second flange surface 7b are not adversely affected.

尚、この実施例の第1フランジ面7aと第2フランジ面7bとの係合によるロータ31と回転軸7との固定手段を第2実施例又は第3実施例に適用してもよい。   The fixing means for the rotor 31 and the rotary shaft 7 by the engagement of the first flange surface 7a and the second flange surface 7b of this embodiment may be applied to the second embodiment or the third embodiment.

本発明は中真空から高真空にわたる圧力範囲の真空発生に使用されるターボ分子ポンプのロータに利用される。   The present invention is applied to a turbomolecular pump rotor used for generating a vacuum in a pressure range from a medium vacuum to a high vacuum.

本発明の実施例1のターボ分子ポンプのロータの縦断面図である。It is a longitudinal cross-sectional view of the rotor of the turbo-molecular pump of Example 1 of this invention. 実施例2の複合分子ポンプのロータの縦断面図である。4 is a longitudinal sectional view of a rotor of a complex molecular pump of Example 2. FIG. 実施例3のターボ分子ポンプのロータの縦断面図である。6 is a longitudinal sectional view of a rotor of a turbo molecular pump of Example 3. FIG. 実施例4のターボ分子ポンプのロータの縦断面図である。6 is a longitudinal sectional view of a rotor of a turbo molecular pump of Example 4. FIG. 従来のターボ分子ポンプのロータの縦断面図である。It is a longitudinal cross-sectional view of the rotor of the conventional turbo molecular pump.

符号の説明Explanation of symbols

1、11、21、31 ロータ
1a、11a、21a、31a ハブ部
1b、11b、23、31b 動翼
1c、11c、21c、31c ボス部
2、7 回転軸
3 ナット
7a 第1フランジ面
7a1 係止凹部
7b 第2フランジ面
7b1 係止凸部
13 ねじ溝ポンプ部ロータ
21b 補助ハブ部
22 ディスク部
1, 11, 21, 31 Rotor 1a, 11a, 21a, 31a Hub portion 1b, 11b, 23, 31b Rotor blade 1c, 11c, 21c, 31c Boss portion 2, 7 Rotating shaft 3 Nut 7a First flange surface 7a1 Locking Concave part 7b Second flange surface 7b1 Locking convex part 13 Thread groove pump part rotor 21b Auxiliary hub part 22 Disk part

Claims (6)

ターボ分子ポンプ、又はターボ分子ポンプ部とこれに連通するねじ溝ポンプ部とからなる複合分子ポンプにおいて、前記ターボ分子ポンプ又は前記ターボ分子ポンプ部のロータは、複数の動翼からなる動翼段を中空の円筒状のハブ部の外周に放射状に突設すると共に、該ハブ部の末端部に軸方向へ突出するボス部を設けて該ロータをカップ状に形成し、該ボス部を介して該ロータを回転軸に固定するようにした分子ポンプのロータ。   In a turbomolecular pump, or a complex molecular pump comprising a turbomolecular pump section and a thread groove pump section communicating with the turbomolecular pump section, the turbomolecular pump or the rotor of the turbomolecular pump section includes a moving blade stage composed of a plurality of moving blades. A radial cylindrical protrusion is provided on the outer periphery of the hollow cylindrical hub portion, and a boss portion protruding in the axial direction is provided at the end portion of the hub portion to form the rotor in a cup shape. A rotor of a molecular pump that fixes the rotor to a rotating shaft. 前記ボス部に前記回転軸が嵌合する軸孔を設けると共に該軸孔を挿通する回転軸の先端部にねじ部を設けて、該ねじ部に螺合するナットを用いて前記ロータを前記回転軸に締結するように形成した請求項1に記載の分子ポンプのロータ。   The boss portion is provided with a shaft hole into which the rotating shaft is fitted, and a screw portion is provided at a tip portion of the rotating shaft that is inserted through the shaft hole, and the rotor is rotated using a nut that is screwed into the screw portion. The rotor of the molecular pump according to claim 1, wherein the rotor is configured to be fastened to a shaft. 前記ボス部の端面部に複数の締結用ねじ孔を有する第1フランジ面を形成すると共に該第1フランジ面に係合可能な第2フランジ面を前記回転軸の上端部に形成して、複数のボルトを用いて前記第1フランジ面と第2フランジ面とを締結して前記ロータを前記回転軸に固定するように形成した請求項1に記載の分子ポンプのロータ。   A first flange surface having a plurality of fastening screw holes is formed on an end surface portion of the boss portion, and a second flange surface that can be engaged with the first flange surface is formed on an upper end portion of the rotating shaft. 2. The molecular pump rotor according to claim 1, wherein the first flange surface and the second flange surface are fastened by using a bolt of 5 to secure the rotor to the rotating shaft. 前記第1フランジ面の中心部に円形の係止凹部を凹設すると共に前記第2フランジ面の
中心部に円形の係止凸部を突設して、第1フランジ面と第2フランジ面とを係合させたと
きに、これら係止凹部と係止凸部とが嵌合する構造とした請求項3に記載の分子ポンプの
ロータ。
A circular locking recess is provided at the center of the first flange surface, and a circular locking protrusion is provided at the center of the second flange surface to provide a first flange surface and a second flange surface. The rotor of the molecular pump according to claim 3, wherein the engaging recess and the engaging protrusion are fitted to each other when engaged with each other.
前記中空の円筒状のハブ部の外周部に前記ターボ分子ポンプ部の動翼段に続いて、円筒状のねじ溝ポンプ部ロータを連設した請求項1乃至請求項4のいずれか1に記載の分子ポンプのロータ。   5. The cylindrical thread groove pump part rotor is continuously provided on the outer peripheral part of the hollow cylindrical hub part, following the rotor blade stage of the turbo molecular pump part. 6. Molecular pump rotor. 前記中空の円筒状のハブ部の外周部の末端部よりディスク部を全周にわたって外方に突設し、該ディスク部の外方縁部から円筒状の補助ハブ部を設け、該補助ハブ部の外周部に複数の動翼からなる動翼段を放射状に突設した請求項1乃至請求項4のいずれか1に記載の分子ポンプのロータ。   A disk part is projected outwardly from the end part of the outer peripheral part of the hollow cylindrical hub part, and a cylindrical auxiliary hub part is provided from the outer edge part of the disk part. The rotor of the molecular pump of any one of Claims 1 thru | or 4 which provided the blade stage which consists of a some blade on the outer peripheral part of this.
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5541464B2 (en) * 2009-02-18 2014-07-09 株式会社島津製作所 Turbo molecular pump
CN108678975A (en) * 2018-07-17 2018-10-19 中国工程物理研究院机械制造工艺研究所 A kind of anti-vibration molecular pump

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09310696A (en) * 1996-03-21 1997-12-02 Osaka Shinku Kiki Seisakusho:Kk Molecular drag pump
JPH10131887A (en) * 1996-10-08 1998-05-19 Varian Assoc Inc Vacuum pumping device
JP2002541378A (en) * 1999-04-03 2002-12-03 ライボルト ヴァークウム ゲゼルシャフト ミット ベシュレンクテル ハフツング Friction vacuum pump with rotor unit consisting of shaft and rotor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09310696A (en) * 1996-03-21 1997-12-02 Osaka Shinku Kiki Seisakusho:Kk Molecular drag pump
JPH10131887A (en) * 1996-10-08 1998-05-19 Varian Assoc Inc Vacuum pumping device
JP2002541378A (en) * 1999-04-03 2002-12-03 ライボルト ヴァークウム ゲゼルシャフト ミット ベシュレンクテル ハフツング Friction vacuum pump with rotor unit consisting of shaft and rotor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5541464B2 (en) * 2009-02-18 2014-07-09 株式会社島津製作所 Turbo molecular pump
CN108678975A (en) * 2018-07-17 2018-10-19 中国工程物理研究院机械制造工艺研究所 A kind of anti-vibration molecular pump

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