JPH022697A - Laser oscillator - Google Patents

Laser oscillator

Info

Publication number
JPH022697A
JPH022697A JP14892088A JP14892088A JPH022697A JP H022697 A JPH022697 A JP H022697A JP 14892088 A JP14892088 A JP 14892088A JP 14892088 A JP14892088 A JP 14892088A JP H022697 A JPH022697 A JP H022697A
Authority
JP
Japan
Prior art keywords
blower
laser
bearing
gas
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
JP14892088A
Other languages
Japanese (ja)
Inventor
Tsutomu Funakubo
舟久保 勤
Norio Karube
規夫 軽部
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 JP14892088A priority Critical patent/JPH022697A/en
Publication of JPH022697A publication Critical patent/JPH022697A/en
Pending legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Optics & Photonics (AREA)
  • Lasers (AREA)

Abstract

PURPOSE:To improve strength, wear resistance and heat resistance of a rolling element or the like of a bearing, preventing a bearing from being damaged in a short time by a method wherein a blower for a gas circulator consists of a turbo blower which rotates in laser gas and the bearing of the blower is made of ceramic. CONSTITUTION:In a laser oscillator consisting of a discharge tube which laser- excites with gas discharge, an optical resonator which generates laser oscillation, a blower and a gas circulator which forcedly cools laser gas with a cooler, said blower is composed of a turbo blower which rotates in laser gas, and a bearing of the blower is made of ceramic. For example, rolling elements 24, 25 between an inner wheel and an outer wheel of antifriction bearings 19, 20 are made of ceramic with alumina contained as a main component. This increases strength of the rolling element by 3 to 4 times, preventing damage of bearings caused by fatigue due to repetitive load application on raceway surfaces of inner and outer wheels and on the raceway surface of the rolling element, and damage caused by deterioration of fatigue limitation due to wear caused by friction and friction heat.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は加工用CO□レーザ等の高出力レーザに関し、
詳細には小型軽量化し、発振特性、信頼性、保守性を改
良したCO,レーザ発振装置に関する。
[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a high-power laser such as a CO□ laser for processing,
Specifically, the present invention relates to a CO laser oscillation device that is smaller and lighter and has improved oscillation characteristics, reliability, and maintainability.

〔従来の技術〕[Conventional technology]

第3図に従来技術によるCO,レーザのレーザ発振装置
の構成を示す。図において、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1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電源6によっ、て印加さ
れ、放電管1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。放電管1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 conventional CO laser oscillation device. In the figure, 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 1, and a high frequency voltage is applied between them by a high frequency power source 6, and a high frequency glow discharge is generated inside the discharge tube 1 to generate a laser beam. Excitation takes place. The optical axis of the laser beam inside the discharge tube 1 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10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
12の排気と補給ガス導入が続き、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 guided from the cylinder 10, and the gas pressure inside the device reaches the specified value.After that, the vacuum pump 12 continues to exhaust and supply gas is introduced, and the gas pressure is maintained at the specified value. However, part of the laser gas is continuously replaced with fresh gas, thereby preventing gas contamination.

さらに第4図では送風機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。
Furthermore, in FIG. 4, the laser gas is circulated within the apparatus by a blower 9. Its purpose is to cool the laser gas.

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、他はガス加熱に消費される。ところが
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である。レーザガスは約100m
/ s e c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。送風機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。これらの冷却器7及び8は周知である
ので詳細な説明は省略する。
In CO, laser, about 20% of the injected electrical energy is converted into laser light, and the rest is consumed 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 approximately 100m
The liquid passes through the discharge tube at a flow rate of /sec, flows in the direction shown by the arrow, and is guided to the cooler 8. Here, heating energy mainly due to discharge is removed. Since compression heat is generated in the blower 9, the gas passes through the cooler 7 before being led to the discharge tube 1 again. Since these coolers 7 and 8 are well known, detailed explanation will be omitted.

第4図に従来のターボブロワの構造を示す。ターボ翼1
6はシャフト26に取り付けたロータ17と、ステータ
18から構成されるモータによって、約10万RPMの
高速回転で回転される。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. 4 shows the structure of a conventional turbo blower. turbo wing 1
6 is rotated at a high speed of about 100,000 RPM by a motor consisting of a rotor 17 attached to a shaft 26 and a stator 18. Therefore, compared to a low-speed Roots blower, the volume is smaller in inverse proportion to the rotation speed.

さらに、シャフト26の支持に軸受損失が小さいことや
コストからころがり軸受19及び20を使用している。
Furthermore, rolling bearings 19 and 20 are used to support the shaft 26 due to low bearing loss and cost.

ころがり軸受19及び20の転動体の材質は高炭素クロ
ム軸受1in(JIS規格番号5UJ2〜4)が使用さ
れている。軸受の潤滑は高速回転のためオイルを定期的
に軸受に供給するオイルジェットやオイルエア潤滑が使
用されている。第5図においてはころがり軸19および
20にオイル供給ユニッ1−21が空気を使用してオイ
ルを霧化し通路22あるいは23よりころがり軸受に供
給している。
The rolling elements of the rolling bearings 19 and 20 are made of 1 inch high carbon chromium bearing (JIS standard number 5UJ2-4). For bearing lubrication, oil-jet or oil-air lubrication is used to periodically supply oil to the bearings due to high-speed rotation. In FIG. 5, an oil supply unit 1-21 uses air to atomize oil to the rolling shafts 19 and 20, and supplies the atomized oil to the rolling bearings through passages 22 or 23.

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

第3図及び第4図に示す従来のレーザ発振装置では以下
のような課題がある。
The conventional laser oscillation device shown in FIGS. 3 and 4 has the following problems.

ころがり軸受の転動体が鋼であるため、内輪及び外輪の
軌道及び転動体の軌道面にかかる繰り返し荷重による転
動体の疲労や軌道面での摩擦による摩耗および摩擦熱に
よる疲労限界の低下のため短期間に軸受破損を発生して
いる。
Since the rolling elements of rolling bearings are made of steel, the rolling elements may fatigue due to repeated loads applied to the raceway of the inner and outer rings and the raceway surface of the rolling element, wear due to friction on the raceway surface, and fatigue limit decrease due to frictional heat. Bearing damage occurred during this period.

本発明はこのような点に鑑みてなされたものであり、送
風機の軸受がセラミックであるガスレーザ装置を提供す
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 device in which the bearing of the blower is made of ceramic.

〔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ニヨってレーザガスを強制冷
却させるガス循環装置等から構成されるレーザ発振装置
において、該送風機がレーザガス中で回転するターボブ
ロワから構成され、該送風機の軸受がセラミックである
ことを特徴とするレーザ発振装置が、提供される。
In order to solve the above problems, the present invention consists of a discharge tube that excites the laser by gas discharge, an optical resonator that performs laser oscillation, a gas circulation device that forcibly cools the laser gas by using a blower and a cooler, etc. A laser oscillation device is provided, wherein the blower is comprised of a turbo blower rotating in laser gas, and the blower has a bearing made of ceramic.

さらに、2個のターボ翼をスラスト力が逆方向にかかる
ように配置したレーザ発振装置が、提供される。
Furthermore, a laser oscillation device is provided in which two turbo blades are arranged so that thrust forces are applied in opposite directions.

〔作用〕[Effect]

ターボブロワの送風機において、ころがり軸受の転動体
等にセラミックを使用することによって転動体の強度、
耐摩耗性、耐熱性を向上し短期間での軸受破損を防止す
る。
In turbo blowers, the strength of the rolling elements is improved by using ceramics for the rolling elements of rolling bearings, etc.
Improves wear resistance and heat resistance to prevent bearing damage in a short period of time.

さらに、ターボ翼をスラスト力が逆方向にかかるように
配置したので、スラスト方向の力がバランスして、安全
性が増し、しかも軸受にかかるスラスト荷重も小さくな
るので軸受寿命も長くなる。
Furthermore, since the turbo blades are arranged so that thrust forces are applied in opposite directions, the forces in the thrust direction are balanced, increasing safety, and the thrust load applied to the bearings is also reduced, extending the life of the bearings.

〔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図に本発明のレーザ発振装置の一実施例の構成図を
示す、第4図と同一の構成要素には同一の符合が付して
あり、その詳細な説明は省略する。
FIG. 1 shows a configuration diagram of an embodiment of the laser oscillation device of the present invention. The same components as in FIG. 4 are given the same reference numerals, and detailed explanation thereof will be omitted.

ここで、ターボ翼16は遠心翼を示しているが斜流翼で
あっても軸流翼であってもよい。
Although the turbo blades 16 are shown as centrifugal blades, they may be diagonal flow blades or axial flow blades.

ころがり軸受19および20の内輪と外輪との間の転動
体24と25はセラミックでできている。
The rolling elements 24 and 25 between the inner and outer rings of the rolling bearings 19 and 20 are made of ceramic.

例えばアルミナ(ALz Ox )を主成分としたセラ
ミックの転動体の強度は330 kg/cdであり、硬
度はビッカース1500である。それに対し、従来の高
炭素クロム鋼は100kg/ciiであり、硬度はビッ
カース360である。故に、転動体の強度が3〜4倍に
増加することによって内輪及び外輪の軌道面及び転動体
の軌道面にかかる繰り返し荷重による疲労や軌道面での
摩擦による摩耗および摩擦熱による疲労限界の低下によ
る軸受破損が防止できる。
For example, the strength of a ceramic rolling element mainly composed of alumina (ALz Ox) is 330 kg/cd, and the hardness is Vickers 1500. In contrast, conventional high carbon chromium steel has a hardness of 100 kg/cii and Vickers 360. Therefore, by increasing the strength of the rolling elements by 3 to 4 times, fatigue due to repeated loads applied to the raceway surfaces of the inner and outer rings and the raceway surfaces of the rolling elements, wear due to friction on the raceway surfaces, and fatigue limits due to frictional heat are reduced. Bearing damage caused by this can be prevented.

上記の説明ではころがり軸受の転動体をセラミックとし
たが、セラミックのすべり軸受を使用することにより同
様な効果が得られる。
In the above explanation, the rolling elements of the rolling bearing are made of ceramic, but similar effects can be obtained by using a ceramic sliding bearing.

第1図のターボブロワは出力IKW程度のレーザ発振装
置に適用されるが、さらに高出力化のためには大型のタ
ーボ翼を使用してもよいが、コスト的には同−翼を使用
することが望ましい。第2図にレーザ出力2KW程度の
ターボブロワの構造を示す0図において31はターボブ
ロワであり、軸受は第1図と同じであるので省略しであ
る。なお、図中の矢印はレーザガスの流れる方向を示す
The turbo blower shown in Fig. 1 is applied to a laser oscillation device with an output of approximately IKW, but larger turbo blades may be used to achieve even higher output, but from a cost standpoint, using the same blade is preferable. is desirable. FIG. 2 shows the structure of a turbo blower with a laser output of about 2 KW. In FIG. 0, reference numeral 31 is a turbo blower, and the bearings are the same as those in FIG. 1, so they are omitted. Note that the arrow in the figure indicates the direction in which the laser gas flows.

シャフトの上下にターボ翼16と32が2個取り付けら
れている。この構成で軸受けと駆動モータが1セツトで
ターボ翼2個を回転できるのでコスト上有利である。1
7はロータ、18はステータである。ここでは、ターボ
翼を同一シャフトに取り付けることにより、スラスト方
向の荷重変動を打ち消しあい、スラスト荷重が非常に小
さくなり、安定性が向上し、寿命が非常に長くなる。
Two turbo blades 16 and 32 are attached above and below the shaft. With this configuration, two turbo blades can be rotated with one set of bearing and drive motor, which is advantageous in terms of cost. 1
7 is a rotor, and 18 is a stator. Here, by attaching the turbo blades to the same shaft, load fluctuations in the thrust direction are canceled out, resulting in a very small thrust load, improved stability, and a very long life.

第4図は従来のターボブロワの構成図である。FIG. 4 is a configuration diagram of a conventional turbo blower.

〔発明の効果〕〔Effect of the invention〕

以上説明したように本発明では、ころがり軸受の転動体
等にセラミックを使用したので、軸受の転動体等の強度
、耐摩耗性、耐熱性を向上し短期間での軸受破損を防止
できる。
As explained above, in the present invention, since ceramic is used for the rolling elements of the rolling bearing, the strength, wear resistance, and heat resistance of the rolling elements of the bearing can be improved, and damage to the bearing can be prevented in a short period of time.

さらに、ターボ翼をスラスト力が逆方向にかかるように
配置したので、スラスト方向の力がバランスして、安定
性が増し、しかも軸受けにかかるスラスト荷重も小さく
なるので軸受寿命も長くなる。
Furthermore, since the turbo blades are arranged so that thrust forces are applied in opposite directions, the forces in the thrust direction are balanced, increasing stability, and the thrust load applied to the bearings is also reduced, extending the life of the bearings.

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

第1図は本発明のレーザ出力IKW程度のターボブロワ
の構造図、 第2図はレーザ出力2KW程度のターボブロワの構造図
、 第3図は従来のCO□レーザのレーザ発振装置の構成図
、 1・・・・−・−・・・・−放電管 2−・−−−−一−−−−−−−・出力結合鏡3・  
・−全反射鏡 4.5−・−−−一−−−−・−電極 6−   ・−高周波電源 7.8−−−−−−−−−一・−・・・冷却器9−・−
−−−−−−・−・・・・・送風機o−−−−−−−−
−−−−−−ガスボンベ2・・・−・・・・−−−−−
・真空ポンプ3・・−・・−・・−共振器内レーザビー
ム光軸4−・・−・・−−−−−・−共振器外レーザビ
ーム光軸6−・−一−−−−−・・−ターボ翼 7・・−・−・−・−−−−一ロータ 8−・−m−〜−・−・−ステータ
Fig. 1 is a structural diagram of a turbo blower with a laser output of about IKW according to the present invention, Fig. 2 is a structural diagram of a turbo blower with a laser output of about 2 KW, and Fig. 3 is a structural diagram of a conventional CO□ laser oscillation device. ...−・−・・−Discharge tube 2−・−−−−1−−−−−−−・Output coupling mirror 3・
- Total reflection mirror 4.5 - - - - - Electrode 6 - - High frequency power supply 7.8 - - - - - - - - Cooler 9 - - −
−−−−−−・−・・・Blower o−−−−−−−−
−−−−−−Gas cylinder 2・・・−・・・・−−−−−
・Vacuum pump 3・・・・−・・−Intra-cavity laser beam optical axis 4−・・−・・−−−−−・−Outer cavity laser beam optical axis 6−・−−1−−−− −・・−Turbo blade 7・・−・−・−・−−−−One rotor 8−・−m−~−・−・−Stator

Claims (5)

【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等から構成
されるレーザ発振装置において、該送風機がレーザガス
中で回転するターボブロワから構成され、該送風機の軸
受がセラミックであることを特徴とするレーザ発振装置
(1) In a laser oscillation device consisting of a discharge tube that excites the laser by gas discharge, an optical resonator that performs laser oscillation, a gas circulation device that forcibly cools the laser gas using a blower and a cooler, the blower is in the laser gas. 1. A laser oscillation device comprising a turbo blower that rotates at a speed of 100.degree. C., the blower having a bearing made of ceramic.
(2)前記軸受がころがり軸受であり、該ころがり軸受
の転動体がセラミックであることを特徴とする特許請求
の範囲第1項記載のレーザ発振装置。
(2) The laser oscillation device according to claim 1, wherein the bearing is a rolling bearing, and the rolling elements of the rolling bearing are ceramic.
(3)前記軸受がセラミック製の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項記載のレーザ発振装
置。
(3) The laser oscillation device according to claim 1, wherein the bearing is a ceramic sliding bearing.
(4)前記ターボブロワが、1個のターボ翼から構成さ
れていることを特徴とする特許請求の範囲第1項記載の
レーザ発振装置。
(4) The laser oscillation device according to claim 1, wherein the turbo blower is composed of one turbo blade.
(5)前記ターボブロワが、同一シャフトに、逆方向に
スラスト荷重がかかるように設けられた2個のターボ翼
を有することを特徴とする特許請求の範囲第1項記載の
レーザ発振装置。
(5) The laser oscillation device according to claim 1, wherein the turbo blower has two turbo blades provided on the same shaft so that thrust loads are applied in opposite directions.
JP14892088A 1988-06-16 1988-06-16 Laser oscillator Pending JPH022697A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14892088A JPH022697A (en) 1988-06-16 1988-06-16 Laser oscillator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14892088A JPH022697A (en) 1988-06-16 1988-06-16 Laser oscillator

Publications (1)

Publication Number Publication Date
JPH022697A true JPH022697A (en) 1990-01-08

Family

ID=15463617

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14892088A Pending JPH022697A (en) 1988-06-16 1988-06-16 Laser oscillator

Country Status (1)

Country Link
JP (1) JPH022697A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100705544B1 (en) * 2006-08-07 2007-04-09 김종길 Portable instrument for medical alcohol cotton

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55113391A (en) * 1979-02-21 1980-09-01 Hitachi Ltd Gas flow type laser device
JPS5879786A (en) * 1981-11-06 1983-05-13 Hitachi Ltd Carbonic acid gas laser device
JPS6040816A (en) * 1983-08-12 1985-03-04 Hitachi Ltd Ceramic sliding bearing
JPS61199687A (en) * 1985-03-01 1986-09-04 Mitsubishi Electric Corp Gas circulation type laser oscillator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55113391A (en) * 1979-02-21 1980-09-01 Hitachi Ltd Gas flow type laser device
JPS5879786A (en) * 1981-11-06 1983-05-13 Hitachi Ltd Carbonic acid gas laser device
JPS6040816A (en) * 1983-08-12 1985-03-04 Hitachi Ltd Ceramic sliding bearing
JPS61199687A (en) * 1985-03-01 1986-09-04 Mitsubishi Electric Corp Gas circulation type laser oscillator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100705544B1 (en) * 2006-08-07 2007-04-09 김종길 Portable instrument for medical alcohol cotton

Similar Documents

Publication Publication Date Title
US7510369B2 (en) Sacrificial inner shroud liners for gas turbine engines
US5124997A (en) Turbo blower for a laser device and a laser oscillator device
RU2118714C1 (en) Compressor
WO1989012921A1 (en) Laser oscillator
EP0392027B1 (en) Gas laser oscillator
JP2793612B2 (en) Laser turbo blower and laser oscillation device
JPH022697A (en) Laser oscillator
JPH022695A (en) Laser oscillator
JP2690098B2 (en) Laser oscillation device
JPH01205585A (en) Laser emission device
JPH01189974A (en) Laser oscillator
EP0411134B1 (en) Turbo-blower for laser and laser oscillator using the same
JP2001020895A (en) Motor-driven turbomachine
JPH0344082A (en) Turbo-blower for laser and laser oscillator using same
JPH022696A (en) Laser oscillator
JP2008039129A (en) Turbine unit for air cycle refrigerator
JPH02103980A (en) Gas-laser oscillating apparatus
JPH0351517A (en) High speed bearing and turboblower for laser using high speed bearing and laser transmitter
JPH04311075A (en) Laser turbo-blower
JPH04142787A (en) Laser turbo-blower
JPH02174282A (en) Gas laser oscillator
JPH07154010A (en) Turboblower for laser
JPH0316285A (en) Turbo-blower for laser and lasing device using same
JPH01189975A (en) Laser oscillator
JPH02174281A (en) Gas laser oscillator