JPH02103980A - Gas-laser oscillating apparatus - Google Patents

Gas-laser oscillating apparatus

Info

Publication number
JPH02103980A
JPH02103980A JP25805588A JP25805588A JPH02103980A JP H02103980 A JPH02103980 A JP H02103980A JP 25805588 A JP25805588 A JP 25805588A JP 25805588 A JP25805588 A JP 25805588A JP H02103980 A JPH02103980 A JP H02103980A
Authority
JP
Japan
Prior art keywords
gas
blower
grease
laser
bearing
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
JP25805588A
Other languages
Japanese (ja)
Inventor
Norio Karube
規夫 軽部
Tsutomu Funakubo
舟久保 勤
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.)
Fanuc Corp
Original Assignee
Fanuc 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 Fanuc Corp filed Critical Fanuc Corp
Priority to JP25805588A priority Critical patent/JPH02103980A/en
Priority to EP89910925A priority patent/EP0392027B1/en
Priority to DE68916941T priority patent/DE68916941T2/en
Priority to US07/476,411 priority patent/US5022039A/en
Priority to PCT/JP1989/001005 priority patent/WO1990004274A1/en
Publication of JPH02103980A publication Critical patent/JPH02103980A/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
    • F04D29/05Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
    • F04D29/056Bearings
    • F04D29/059Roller bearings
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01SDEVICES USING THE PROCESS OF LIGHT AMPLIFICATION BY STIMULATED EMISSION OF RADIATION [LASER] TO AMPLIFY OR GENERATE LIGHT; DEVICES USING STIMULATED EMISSION OF ELECTROMAGNETIC RADIATION IN WAVE RANGES OTHER THAN OPTICAL
    • H01S3/00Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
    • H01S3/02Constructional details
    • H01S3/03Constructional details of gas laser discharge tubes
    • H01S3/036Means for obtaining or maintaining the desired gas pressure within the tube, e.g. by gettering, replenishing; Means for circulating the gas, e.g. for equalising the pressure within the tube
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K5/00Casings; Enclosures; Supports
    • H02K5/04Casings or enclosures characterised by the shape, form or construction thereof
    • H02K5/16Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
    • H02K5/173Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using bearings with rolling contact, e.g. ball bearings
    • H02K5/1732Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using bearings with rolling contact, e.g. ball bearings radially supporting the rotary shaft at both ends of the rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Power Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Optics & Photonics (AREA)
  • Support Of The Bearing (AREA)
  • Lasers (AREA)

Abstract

PURPOSE:To make a blower compact, to absorb vibration pulsating flow and to obtain stable laser light source by forming the blower with 7 turbo blades, and using a grease-filled squeezed film dampers for the bearings for a driving shaft of the blower. CONSTITUTION:A cooling blower is formed of turbo blades 16. The blades are turned at a high speed with a shaft 17. Ball bearings are used for the bearings of the shaft 17. Inner rings 22 and 23 are fixed to the shaft 17, and outer rings 26 and 27 are fixed to sleeves 28 and 29. Specified gaps are provided between the sleeves 28 and 29 and bearing housings 34 and 35. The gaps are filled with grease, and squeezed film dampers are formed. As the damper material, grease whose vapor pressure is low is used. The dampers are shielded from the outside with O-rings 30 to 33 for preventing the splashing of the grease. In this way, the blower can be made compact, and a stable laser light source wherein resonant vibration is eliminated by the dampers can be obtained.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は加工用Go!レーザなどの高出力の気体レーザ
発振装置に関し、更に詳細にはCO□レーザに用いられ
るターボブロワを改良した気体レーザ発振装置に関する
[Detailed Description of the Invention] [Industrial Application Field] The present invention is a processing Go! The present invention relates to a high-output gas laser oscillation device such as a laser, and more particularly to a gas laser oscillation device that is an improved turbo blower used in a CO□ laser.

〔従来の技術〕[Conventional technology]

第3図に従来技術によるCO□レーザの構成を示す0図
中放電管1の両端には出力結合鏡2と全反射鏡3が設置
されている。又放電管の外側には2枚の金属電極4およ
び5が取り付けられており、その間に高周波電圧が高周
波型aI6によって印加される。その時放電管内に高周
波グロー放電が発生してレーザ励起が行われる。共振器
内のレーザビーム光軸を13で、また出力結合鏡2から
外部に取り出されるレーザビーム光軸を14でそれぞれ
示す。
FIG. 3 shows the configuration of a CO□ laser according to the prior art. In FIG. 3, an output coupling mirror 2 and a total reflection mirror 3 are installed at both ends of a discharge tube 1. Further, two metal electrodes 4 and 5 are attached to the outside of the discharge tube, and a high frequency voltage is applied between them by a high frequency type aI6. At this time, a high frequency glow discharge is generated within the discharge tube and laser excitation is performed. The optical axis of the laser beam inside the resonator is indicated by 13, and the optical axis of the laser beam taken out from the output coupling mirror 2 is indicated by 14.

レーザ発振装置起動時には先ず最初に真空ポンプ12に
よって装置内部全体が排気される。ついでバルブ11が
開放になり所定流量のレーザガスがボンベIOから導か
れ装置内のガス圧は規定値に達しその後は真空ポンプ1
2の排気と補給ガス導入が続くのでガス圧は規定値に保
たれたままレーザガスの一部は継続して新鮮ガスに置換
されることになりガス汚染を防止する。
When the laser oscillation device is started, the entire interior of the device is first evacuated by the vacuum pump 12. Then, the valve 11 is opened, and a predetermined flow rate of laser gas is led from the cylinder IO, and the gas pressure inside the device reaches the specified value, after which the vacuum pump 1
Since the exhaust gas and the supply gas introduced in step 2 continue, part of the laser gas is continuously replaced with fresh gas while the gas pressure is maintained at the specified value, thereby preventing gas contamination.

さらに第3図ではルーツブロワ9によってレーザガスを
装置内で循環している。この目的はレーザガスの冷却に
ある。CO□レーザでは注入電気エネルギーの約20%
がレーザ光に変換され他はガス加熱に用いられる。所が
理論によればレーザ発振利得は絶対温度Tの−(3/2
)乗に比例するので発振効率を上昇させるためにレーザ
ガスの強制冷却が必要なのである。レーザガスは約10
0m/se(の流速で放電管内を通過し矢印で示す方向
に流れ冷却器8に導かれる。ここでは主として放電によ
る加熱エネルギーが除去される。ルーツブロワ9では圧
縮熱が発生するのでガスは放電管1に再度導かれる前に
冷却器7を通過する。
Furthermore, in FIG. 3, a roots blower 9 circulates the laser gas within the apparatus. Its purpose is to cool the laser gas. About 20% of the injected electrical energy in CO□ laser
One part is converted into laser light and the other part is used for gas heating. However, according to theory, the laser oscillation gain is -(3/2) of the absolute temperature T.
), so forced cooling of the laser gas is necessary to increase the oscillation efficiency. Laser gas is about 10
The gas passes through the discharge tube at a flow rate of 0 m/sec (in the direction shown by the arrow) and is guided to the cooler 8. Here, the heating energy due to the discharge is mainly removed. In the Roots blower 9, compression heat is generated, so the gas flows through the discharge tube. It passes through a cooler 7 before being redirected to 1.

これらの冷却器は通常方式によるものであるのでここで
は説明は省略する。
Since these coolers are of the normal type, their explanation will be omitted here.

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

しかし、従来技術には次に述べる課題がある。 However, the conventional technology has the following problems.

第一はルーツブロワが低速回転の容積型送風機であるの
で大きさ、重量ともに過大なものであり、レーザ発振器
そのものを過大なものにしてしまう。
First, since the Roots blower is a positive displacement blower that rotates at a low speed, it is excessive in size and weight, making the laser oscillator itself excessively large.

第二には同じく送風に脈流がありレーザ発振特性に影響
することである。第三には同じく振動があってレーザビ
ームのボインテングスタビリテーに影響することである
Second, there is a pulsating flow in the airflow, which affects the laser oscillation characteristics. Thirdly, there is also vibration, which affects the intensification stability of the laser beam.

一方、ルーツブロワの代わりにターボブロワを高速で回
転させると、高速回転時に発生する共振振動によって、
ターボブロワが破損する危険性がある。
On the other hand, if a turbo blower is rotated at high speed instead of a roots blower, the resonance vibration that occurs during high speed rotation will cause
There is a risk of damage to the turbo blower.

本発明はこのような点に鑑みてなされたものであり、タ
ーボブロワを使用し、かつ高速回転時の共振振動を防止
した気体レーザ発振装置を提供することを目的とする。
The present invention has been made in view of these points, and an object of the present invention is to provide a gas laser oscillation device that uses a turbo blower and prevents resonance vibration during high-speed rotation.

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

本発明では上記課題を解決するために、気体放電によっ
てレーザ励起をする放電管、レーザ発振を行わせる光共
振器、送風機および冷却器によってレーザガスを強制冷
却させるガス循環装置などから構成される気体レーザ発
振装置において、 送風機がレーザガス中で回転する電動機駆動のターボ翼
から構成され、かつ電動機駆動用軸受がグリース充填の
スキーズドフィルムダンパー軸受であることを特徴とす
る気体レーザ発振装置が、提供される。
In order to solve the above problems, the present invention provides a gas laser that is composed of a discharge tube that excites the laser by gas discharge, an optical resonator that performs laser oscillation, and a gas circulation device that forcibly cools the laser gas using a blower and a cooler. Provided is a gas laser oscillation device, wherein the blower is composed of an electric motor-driven turbo blade that rotates in laser gas, and the electric motor drive bearing is a grease-filled squeezed film damper bearing. .

〔作用] ターボブロワによって、回転数に逆比例して体積を小さ
くすることができる。一方、スキーズドフィルムダンパ
ー軸受のグリース等の非弾性効果による制動によって、
振動を防止する。
[Operation] The turbo blower allows the volume to be reduced in inverse proportion to the rotation speed. On the other hand, due to the braking effect due to the inelastic effect of grease etc. in the squeezed film damper bearing,
Prevent vibration.

〔実施例〕〔Example〕

以下、本発明の一実施例を図面に基づいて説明する。 Hereinafter, one embodiment of the present invention will be described based on the drawings.

第1図に本発明の一実施例の気体レーザ発振装置の全体
構成図を示す。第3図に示す従来技術との共通部分は同
一の番号で示し、動作も概略は同一であるのでその説明
は省略し、異なる部分のみの説明をする。ルーツブロワ
9の代りに図1ではターボブロワ15が用いられている
。ターボブロワはルーツブロワよりも効率が格段に高い
ので圧縮熱は無視でき、第3図に示す後段の冷却器7は
省略することができ、第1図では省略しであるが勿論設
置する場合もある。
FIG. 1 shows an overall configuration diagram of a gas laser oscillation device according to an embodiment of the present invention. Portions common to the prior art shown in FIG. 3 are indicated by the same numerals and the operations are generally the same, so a description thereof will be omitted and only the different portions will be described. In place of the roots blower 9, a turbo blower 15 is used in FIG. Since the efficiency of the turbo blower is much higher than that of the roots blower, the heat of compression can be ignored, and the cooler 7 shown in the latter stage shown in FIG. 3 can be omitted, and although it is omitted in FIG. 1, it may of course be installed in some cases.

第2図にルーツブロワの一構成例を示す。ここでは遠心
翼16が示されているがターボ翼は斜流翼であっても軸
流翼であっても構わない。ターボ翼はシャフト17に取
り付けられておりレーザガスきょう体とは別のきょう体
18中に設置されたモータ19及び20によって約10
万RPMの高速回転数で回転される。そのため低速のル
ーツブロワに比較して回転数に逆比例して体積が小さく
なっている。
FIG. 2 shows an example of the configuration of a roots blower. Although centrifugal blades 16 are shown here, the turbo blades may be diagonal flow blades or axial flow blades. The turbo blades are mounted on a shaft 17 and driven by motors 19 and 20 installed in a housing 18 separate from the laser gas housing.
It rotates at a high speed of 10,000 RPM. Therefore, compared to a low-speed Roots blower, the volume is smaller in inverse proportion to the rotation speed.

本発明は特にブロワ翼の高速回転時に発生する共振振動
を防止するという特徴がある。第2図に示すのは一実施
例であるがそこでは玉軸受が使用されている。この玉軸
受の内輪22.23はシャフト17に固定されている。
The present invention is particularly characterized in that it prevents resonance vibrations that occur when the blower blades rotate at high speed. FIG. 2 shows one embodiment in which ball bearings are used. The inner rings 22, 23 of this ball bearing are fixed to the shaft 17.

24及び25は軸受のボールを示す。実際には図には示
されていない多数のボールが存在する。26.27は軸
受の外輪であり、スリーブ28.29に固定されている
24 and 25 indicate the balls of the bearing. There are actually many balls not shown in the diagram. 26.27 is the outer ring of the bearing, which is fixed to the sleeve 28.29.

本発明の特徴はこれらのスリーブ28.29が軸受ハウ
ジング34.35に固定されていないことである。スリ
ーブがハウジングに固定されていると次に述べる危険が
発生する。シャフト17の回転時には回転速度を上げて
いくと順次1.2及び3次の危険速度に遭遇する。回転
体は回転釣り合いが完全ではないと遠心力によって回転
数が危険速度を通過する時に破壊の可能性がある。−船
釣に3次の危険速度は常用回転数に比較して十分に高回
転側に設計することができるが1.2次の振動は安全に
通過する必要がある。回転釣り合いとハウジング加工を
極端に高精度にて行なう必要性を無くすことは重要な課
題である。
A feature of the invention is that these sleeves 28,29 are not fixed to the bearing housing 34,35. If the sleeve is fixed to the housing, the following dangers arise: When the shaft 17 rotates, as the rotational speed increases, critical speeds of 1.2 and 3rd orders are sequentially encountered. If the rotational balance of a rotating body is not perfect, there is a possibility of destruction due to centrifugal force when the rotational speed passes through a critical speed. - For boat fishing, the third-order critical speed can be designed to be sufficiently high compared to the normal rotation speed, but the first and second-order vibrations must pass safely. Eliminating the need for extremely high precision rotational balancing and housing machining is an important issue.

本発明ではスリーブと軸受ハウジングを相互に固定しな
いで両者間に10〜100μのギャップを設けそこにグ
リースを充填しグリースの非弾性効果によってスリーブ
に発生する振動に制動を与える。第2図ではこのグリー
ス36.37を斜線で示した。本発明では軸受はレーザ
ガス中に位置するがレーザガスの汚染は回避しなければ
ならないのでこのダンパー材料に蒸気圧の低いグリース
を使用し、さらにグリースの飛散を防止するためにグリ
ースの存在領域を0−リング30.31ならびに32.
33の対で外部から遮断するのである。ここでは玉軸受
を使用した例を示したがこれはすべり軸受でもよい。
In the present invention, the sleeve and the bearing housing are not fixed to each other, but a gap of 10 to 100 microns is provided between them, and grease is filled in the gap to damp vibrations generated in the sleeve by the inelastic effect of the grease. In FIG. 2, the grease 36 and 37 are shown with diagonal lines. In the present invention, the bearing is located in the laser gas, but contamination of the laser gas must be avoided, so a grease with low vapor pressure is used as the damper material, and the area where the grease exists is set to 0-0 to prevent the grease from scattering. Rings 30.31 and 32.
Thirty-three pairs are used to isolate it from the outside. Although an example using a ball bearing is shown here, a sliding bearing may also be used.

また、この種のダンパー構造の採用によってスリーブと
軸受ハウジング間には数十μのギャップがあることにな
るので、従来ハウジング加工には必要であった超精密仕
上げが不要になり加工が極めて簡単になる。第2図には
電動機発熱を冷却するための冷却水コイル21がハウジ
ング34及び35の周囲に設けられている。
In addition, by adopting this type of damper structure, there is a gap of several tens of microns between the sleeve and the bearing housing, which eliminates the need for ultra-precision finishing that was previously required for housing machining, making machining extremely easy. Become. In FIG. 2, a cooling water coil 21 is provided around housings 34 and 35 for cooling the heat generated by the motor.

本発明は特に高周波放電励起COtレーザに有用である
。直流放電励起の場合は一様放電を得るためにガス流に
乱流の発生を必要とするので送風機には高い圧縮比が要
求されルーツプロワがこの目的には最適である。一方高
周波放電励起では乱流は不必要であり、低圧縮比、大送
風容量と云うターボブロワの特徴が生きて(るのである
The present invention is particularly useful for high frequency discharge pumped COt lasers. In the case of DC discharge excitation, it is necessary to generate turbulence in the gas flow in order to obtain a uniform discharge, so the blower is required to have a high compression ratio, and a Roots blower is ideal for this purpose. On the other hand, high-frequency discharge excitation does not require turbulence, and the turbo blower's characteristics of low compression ratio and large airflow capacity are utilized.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明では、ルーツプロワを使用し
、ルーツプロワの回転軸にスキーズドフィルムダンパー
を使用したので、ブロワ及び装置全体の小型軽量化がは
かれる。また、振動、脈流がなくなりポインテングスタ
ビリテーや出力の高速安定性などのビーム特性が改良さ
れる。更に、高速回転体に不可避であった共振振動現象
による破壊を回避することができる。
As described above, in the present invention, a Roots blower is used and a squeezed film damper is used on the rotating shaft of the Roots blower, so that the blower and the entire device can be made smaller and lighter. In addition, vibration and pulsation are eliminated, and beam characteristics such as pointing stability and high-speed output stability are improved. Furthermore, it is possible to avoid destruction due to resonance vibration phenomena that are inevitable in high-speed rotating bodies.

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

第1図は本発明の一実施例の気体レーザ発振装置の全体
構成図、 第2図はターボブロワの一構成例を示す図、第3図は従
来の気体レーザ発振装置の構成図である。 4. 7、 1−・   放電管 2・−・−・−・・・・・−出力結合鏡3−−−−−−
−一〜・−・−全反射鏡5・−一−−−−・・−一−−
−−電極6−−−−−−−一・−一−−−−高周波電源
8−−−−−−−・−・・・冷却器 9−・−・−・−・・・−・ルーツプロワ0・−・−・
−・−・・・−、#スボンベト−・・・−・−・・・・
・−バルブ ■ 22.2 24.2 26、2 28、2 30〜3 34、3 36.3 2−・・−・−−−−−−一・真空ポンプ3・・−・−
・・−・−共振器内レーザビーム光軸4・・・−・・・
・−・・−同性レーザビーム光軸5−・−・・−−−一
−・−・ターボプロワ6    ターボ翼 7−・−・・−・−−−m−・・−シャフト8・−・−
・・・・・・・・−駆動系きょう体9−・・−・−−−
−−・〜・電動機ロータ0・・−・・・・・・・−・・
・・電動機ステータト一・・・−・・・・・−・・冷却
水コイル3−・−・−・−・−・・・・・・軸受内輪5
−・・・・・−・−・−ボール 7・・・−・−・・・−・・軸受外輪 9・−・−・−一−−−・・−・−スリーブ2−・・−
・−・・・−・−・0−リング5−・・−・・−・−・
−=軸受ハウジング7−・−・−・−・・〜グリース 特許出願人 ファナック株式会社 代理人   弁理士  服部毅巖 第2図 手続補正書 (自発) 1゜ 事件の表示 昭和63年特許願第258055号 2゜ 発明の名称 気体レーザ発振装置 3゜ 補正をする者 事件との関係
FIG. 1 is an overall configuration diagram of a gas laser oscillation device according to an embodiment of the present invention, FIG. 2 is a diagram showing an example of the configuration of a turbo blower, and FIG. 3 is a configuration diagram of a conventional gas laser oscillation device. 4. 7, 1-・Discharge tube 2・−・−・−・・・Output coupling mirror 3−−−−−−
−1~・−・−Total reflection mirror 5・−1−−−−・・−1−−
--Electrode 6-----------1・-1----High frequency power supply 8------------Cooler 9-----Roots blower 0・−・−・
−・−・・・・−, #Sbonbeto−・−・−・・・
・-Valve■ 22.2 24.2 26, 2 28, 2 30-3 34, 3 36.3 2-・・-・−−−−−−1・Vacuum pump 3・・−・−
...--Intra-cavity laser beam optical axis 4...-
・−・・−Same laser beam optical axis 5−・−・・−−1−・−・Turbo blower 6 Turbo blade 7−・−・・−・−−−m−・・−Shaft 8・−・−
......-Drive system housing 9--...
−−・〜・Electric motor rotor 0・−・・・・・・・−・・
・・Electric motor stator ・・・・・・・・・Cooling water coil 3 −・−・−・−・−・・・・・Bearing inner ring 5
−・・・−・−・−Ball 7・−・−・・・Bearing outer ring 9・−・−・−1−−−・・−・−Sleeve 2−・・−
・−・−・−・0−Ring 5−・・−・・−・−・
−=Bearing housing 7−・−・−・−・・・Grease patent applicant Fanuc Co., Ltd. agent Patent attorney Takeshi Hattori Diagram 2 Procedural amendment (voluntary) 1゜Indication of incident 1988 Patent application No. 258055 No. 2゜Name of the invention Gas laser oscillation device 3゜Relationship with the person making the amendment case

Claims (4)

【特許請求の範囲】[Claims] (1) 気体放電によってレーザ励起をする放電管、レ
ーザ発振を行わせる光共振器、送風機および冷却器によ
ってレーザガスを強制冷却させるガス循環装置などから
構成される気体レーザ発振装置において、 送風機がレーザガス中で回転する電動機駆動のターボ翼
から構成され、かつ電動機駆動用軸受がグリース充填の
スキーズドフィルムダンパー軸受であることを特徴とす
る気体レーザ発振装置。
(1) In a gas laser oscillation device consisting of a discharge tube that excites the laser by gas discharge, an optical resonator that performs laser oscillation, and a gas circulation device that forcibly cools the laser gas using a blower and a cooler, the blower is used to cool the laser gas. 1. A gas laser oscillation device comprising a turbo blade driven by an electric motor that rotates at a speed of 100 degrees, and characterized in that the bearing for driving the electric motor is a squeezed film damper bearing filled with grease.
(2) グリース充填部がO−リングによって外部から
密閉される構造になっていることを特徴とする特許請求
の範囲第1項記載の気体レーザ発振装置。
(2) The gas laser oscillation device according to claim 1, wherein the grease filling portion is sealed from the outside by an O-ring.
(3) 前記軸受が玉軸受であることを特徴とする特許
請求の範囲第1項記載の気体レーザ発振装置。
(3) The gas laser oscillation device according to claim 1, wherein the bearing is a ball bearing.
(4) 前記軸受がすべり軸受であることを特徴とする
特許請求の範囲第1項記載の気体レーザ発振装置。
(4) The gas laser oscillation device according to claim 1, wherein the bearing is a sliding bearing.
JP25805588A 1988-10-13 1988-10-13 Gas-laser oscillating apparatus Pending JPH02103980A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP25805588A JPH02103980A (en) 1988-10-13 1988-10-13 Gas-laser oscillating apparatus
EP89910925A EP0392027B1 (en) 1988-10-13 1989-09-29 Gas laser oscillator
DE68916941T DE68916941T2 (en) 1988-10-13 1989-09-29 GAS LASER OSCILLATOR.
US07/476,411 US5022039A (en) 1988-10-13 1989-09-29 Gas laser oscillator device
PCT/JP1989/001005 WO1990004274A1 (en) 1988-10-13 1989-09-29 Gas laser oscillator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP25805588A JPH02103980A (en) 1988-10-13 1988-10-13 Gas-laser oscillating apparatus

Publications (1)

Publication Number Publication Date
JPH02103980A true JPH02103980A (en) 1990-04-17

Family

ID=17314911

Family Applications (1)

Application Number Title Priority Date Filing Date
JP25805588A Pending JPH02103980A (en) 1988-10-13 1988-10-13 Gas-laser oscillating apparatus

Country Status (1)

Country Link
JP (1) JPH02103980A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005001309A1 (en) * 2003-06-25 2005-01-06 Nsk Ltd. Worm speed reducer and electric power steering device
EP1760319A1 (en) * 2004-06-25 2007-03-07 Osaka Vacuum, Ltd. Bearing support structure for turbomolecular pump
WO2014131678A1 (en) * 2013-03-01 2014-09-04 Oerlikon Leybold Vacuum Gmbh Vacuum pump

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62159795A (en) * 1986-01-04 1987-07-15 フオルツナ−ベルケ・マシ−ネン フアブリ−ク・ゲ−エムベ−ハ− Fan

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS62159795A (en) * 1986-01-04 1987-07-15 フオルツナ−ベルケ・マシ−ネン フアブリ−ク・ゲ−エムベ−ハ− Fan

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005001309A1 (en) * 2003-06-25 2005-01-06 Nsk Ltd. Worm speed reducer and electric power steering device
US7360467B2 (en) 2003-06-25 2008-04-22 Nsk, Ltd. Worm reduction gear and electric power steering apparatus
US7455149B2 (en) 2003-06-25 2008-11-25 Nsk Ltd. Worm reduction gear and electric power steering apparatus
US7455148B2 (en) 2003-06-25 2008-11-25 Nsk Ltd. Worm reduction gear and electric power steering apparatus
EP1760319A1 (en) * 2004-06-25 2007-03-07 Osaka Vacuum, Ltd. Bearing support structure for turbomolecular pump
EP1760319A4 (en) * 2004-06-25 2010-07-07 Osaka Vacuum Ltd Bearing support structure for turbomolecular pump
WO2014131678A1 (en) * 2013-03-01 2014-09-04 Oerlikon Leybold Vacuum Gmbh Vacuum pump

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