JPH022697A - Laser oscillator - Google Patents
Laser oscillatorInfo
- 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
Links
- 238000005096 rolling process Methods 0.000 claims abstract description 29
- 230000010355 oscillation Effects 0.000 claims abstract description 21
- 239000000919 ceramic Substances 0.000 claims abstract description 14
- 230000003287 optical effect Effects 0.000 claims abstract description 7
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 abstract description 2
- 230000006866 deterioration Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 230000003252 repetitive effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 5
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 2
- 238000005461 lubrication Methods 0.000 description 2
- FXNGWBDIVIGISM-UHFFFAOYSA-N methylidynechromium Chemical group [Cr]#[C] FXNGWBDIVIGISM-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000011109 contamination Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005284 excitation Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01S—DEVICES 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
- H01S3/00—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range
- H01S3/02—Constructional details
- H01S3/03—Constructional details of gas laser discharge tubes
- H01S3/036—Means 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
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.
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.
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.
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.
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.
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.
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.
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)
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.
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.
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.
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.
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.
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)
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)
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 |
-
1988
- 1988-06-16 JP JP14892088A patent/JPH022697A/en active Pending
Patent Citations (4)
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100705544B1 (en) * | 2006-08-07 | 2007-04-09 | 김종길 | Portable instrument for medical alcohol cotton |
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