JPS5889886A - Laser oscillator - Google Patents
Laser oscillatorInfo
- Publication number
- JPS5889886A JPS5889886A JP18867681A JP18867681A JPS5889886A JP S5889886 A JPS5889886 A JP S5889886A JP 18867681 A JP18867681 A JP 18867681A JP 18867681 A JP18867681 A JP 18867681A JP S5889886 A JPS5889886 A JP S5889886A
- Authority
- JP
- Japan
- Prior art keywords
- mirror
- main body
- laser
- resonator
- mirror position
- 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
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
- H01S3/05—Construction or shape of optical resonators; Accommodation of active medium therein; Shape of active medium
- H01S3/08—Construction or shape of optical resonators or components thereof
- H01S3/086—One or more reflectors having variable properties or positions for initial adjustment of the resonator
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Lasers (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Optics & Photonics (AREA)
Abstract
Description
【発明の詳細な説明】 本発明はガスレーザ発振器に関するものである。[Detailed description of the invention] The present invention relates to a gas laser oscillator.
通常ガスレーザ発振器におけるミラーの位置調整は可視
レーザ光線を利用するか、望遠鏡を利用し、大気中で行
なうが、レーザ発振時悼ミラー又はミラーホルダの外面
は大気圧(760Torr )に、内面iレーザガス圧
(例えば30Torr)になり、その差圧と断面積の積
だけの外力をミラーが受けるため、ミラー面が微少変動
し光軸が変動するので出力やビーム断面形状、ビームモ
ードが変化し最良の特性を安定に維持することが困難で
あった。Normally, the position of the mirror in a gas laser oscillator is adjusted using a visible laser beam or a telescope in the atmosphere. During laser oscillation, the outer surface of the mirror or mirror holder is at atmospheric pressure (760 Torr), and the inner surface is under the laser gas pressure. (for example, 30 Torr), and the mirror receives an external force equal to the product of the differential pressure and the cross-sectional area, so the mirror surface changes slightly and the optical axis changes, which changes the output, beam cross-sectional shape, and beam mode to achieve the best characteristics. It was difficult to maintain stable conditions.
第1図は従来のミラ′−の位置調整機構の911を示す
もので、全反射鏡ll1t例に説明するO2 。FIG. 1 shows a conventional mirror position adjustment mechanism 911, which will be explained using an example of a total reflection mirror.
図において、1は光学共振器の基台で本体7ラン、ジ1
Q1が固定されている02はレーザ管で同7ランジ20
1により本体フランジ1o1へ固定されている。202
は気密用0リングである03は全反射鏡でミラーホルダ
4に保持されている0401は気密珀0リング、402
は冷却液ノズルである。6はミラー受7ランジ、6はミ
ラー位置調整用微調整ねじである。7はベローズ特のフ
レキシブル継手で、この図では本体7ランジ101とミ
ラー受7ランジ5をつなぐ引張げねの役割も兼ねている
。In the figure, 1 is the base of the optical resonator, with 7 runs on the main body and 1 on the base of the optical resonator.
02 to which Q1 is fixed is a laser tube with 7 lunges 20
1 to the main body flange 1o1. 202
03 is a total reflection mirror held in the mirror holder 4. 0401 is an airtight O-ring, 402
is the coolant nozzle. 6 is a mirror receiver 7 lange, and 6 is a fine adjustment screw for adjusting the mirror position. Reference numeral 7 designates a flexible joint made of bellows, which in this figure also serves as a tension spring connecting the flange 101 of the main body 7 and the flange 5 of the mirror holder 7.
このような従来の構造では、光学共振器内部へ空気を導
入し大気圧下にて矢印a方向から可視レーザ光線等を全
反射鏡3へ照射しその反射光を観測しながら微調整ねじ
6によりミラーの位置調整を行なうが、レーザ発振時蝶
光学共振器内部が低いガス圧(例えば30Torr)
となるため、大気によりミラーがレーザ管の方向へ押
され、ミラーの位置を狂わせ、光軸が光学共振器の中心
からずれるため、レーザ出力が低下する。ビームの一部
がカットされ円形であるはずの断面形状が楕円形になる
。ビームのモードが変rヒする。In such a conventional structure, air is introduced into the optical resonator, and under atmospheric pressure, a visible laser beam or the like is irradiated onto the total reflection mirror 3 from the direction of arrow a, and while observing the reflected light, the fine adjustment screw 6 is used to Adjust the mirror position, but the gas pressure inside the butterfly optical resonator is low (e.g. 30 Torr) during laser oscillation.
Therefore, the atmosphere pushes the mirror toward the laser tube, displacing the mirror and shifting the optical axis from the center of the optical resonator, resulting in a decrease in laser output. A part of the beam is cut and the cross-sectional shape, which should be circular, becomes elliptical. The beam mode changes.
光学共振器の内壁の一部にビームψ:近づいたり当った
りして、局部的な温度上昇をきたすので熱歪が発生し時
間の経過と共に安定性を失なわせたり、最悪の場合は内
部で自己破壊を起すなどの欠点があった。The beam ψ approaches or hits a part of the inner wall of the optical resonator, causing a local temperature rise, causing thermal distortion and causing loss of stability over time, or in the worst case, internal damage. It had drawbacks such as self-destruction.
大気圧の影響によるミラー面の狂いは、大気圧を受ける
ことによりミラーを保持する周辺の部、品が圧縮された
り撓んだりまた第2図に示す様に微調整ねじ6が本体7
ランジ101に接する当り面が変形す7るなどミラー面
の位置、角度を決定している要素が不均一変動するため
である0これらの変動は発振器の運転、停止を繰り返す
度に発生しく共振器内の圧力が変わるため)その量を大
きくしていくので、たとえミラー&[g’11i t
−[1時のガ入圧下で行っても長期間の安定性を得るこ
とができず、最大出力、最適モード等を確保するために
短期間毎にミラーの再調整が必要である0多段折返しを
行なう場合、ミラー位置調整機構も増えるのでその影響
は多大である。Misalignment of the mirror surface due to the influence of atmospheric pressure can be caused by compression or bending of the surrounding parts and parts that hold the mirror due to the atmospheric pressure, or by the fact that the fine adjustment screw 6 is
This is because the elements that determine the position and angle of the mirror surface vary non-uniformly, such as when the abutting surface in contact with the flange 101 deforms.7 These variations occur every time the oscillator is started and stopped, and the resonator Because the pressure inside changes), the amount increases, so even if the mirror &[g'11i t
-[Long-term stability cannot be obtained even under the gas pressure of 1 o'clock, and it is necessary to readjust the mirror every short period of time to ensure maximum output, optimal mode, etc. 0 Multi-stage folding When doing this, the number of mirror position adjustment mechanisms increases, which has a significant impact.
本発明はこれらの問題点を解決するためにミラー 4t
trttt1竪 機構を光学共振器のレーザガスを有
する蓉器内に設けたもので、ミラー(立[/j!7#(
後のミラー面の変動を防止し、共振器の安定性を、高め
ることを目的とするものである。The present invention aims to solve these problems by using mirror 4t.
trttt1vertical The mechanism is installed inside the mirror that has the laser gas of the optical resonator, and the mirror (vertical [/j!7#(
The purpose of this is to prevent subsequent fluctuations in the mirror surface and improve the stability of the resonator.
以下本発明の一実施例を詳細に説明する。An embodiment of the present invention will be described in detail below.
第3図は本発明の一実施例を示しミラー位置調整機構は
本体フランジ1o1と本体キャップ102の中に組込ま
れ大気と遮断されている。FIG. 3 shows an embodiment of the present invention, and a mirror position adjustment mechanism is incorporated into a main body flange 1o1 and a main body cap 102, and is isolated from the atmosphere.
眺ミラー受7ランジで、ミラーの傾きを調整する微調整
ねじ6が取付けられている。8は固定板でミラー受7ラ
ンジ5との間に圧縮ばね9がセットされている。ミラー
ホルダー4の冷却は給排液チューブ4o3(実際には2
本あるが図でld1本で図示しである)がbからb′へ
とミラー受フランジ6の外周を通って接続されて固定台
404で固定板8と共に本体7ランジ101へねじで固
定されている0固定台404を通った液は冷却液ノズル
406全通して容器外へつながっている0給−7
排液チューブ403のbからb′の間は銅のような可撓
性の高い材質で作られており、ミラー位置調整時のミラ
ーホルダの微少な動きを十分吸収できる構造となってい
る。逆にノズル406に外力がかかっても固定台404
が本体7ランジ101へ固定されているから、ミ2−の
傾きに少しの影響もない。また冷却液の圧力でミラーホ
ルダ4が変形することのない機中央部に補強柱400を
設け、冷却液はその外周を流れる様工夫さ、れている。A fine adjustment screw 6 for adjusting the tilt of the mirror is attached to the view mirror holder 7 lunge. A fixed plate 8 has a compression spring 9 set between it and the mirror holder 7 and the flange 5. The mirror holder 4 is cooled using the liquid supply and drainage tube 4o3 (actually 2
(Although there are books, one ld is shown in the figure) is connected from b to b' through the outer periphery of the mirror receiving flange 6, and is fixed to the main body 7 flange 101 together with the fixing plate 8 with screws on the fixing base 404. The liquid that has passed through the zero fixing table 404 passes through the entire cooling liquid nozzle 406 and is connected to the outside of the container. It has a structure that can sufficiently absorb minute movements of the mirror holder when adjusting the mirror position. Conversely, even if an external force is applied to the nozzle 406, the fixed base 404
Since it is fixed to the main body 7 lunge 101, there is no influence on the inclination of Mi2-. Further, a reinforcing column 400 is provided at the center of the machine so that the mirror holder 4 will not be deformed by the pressure of the coolant, and the coolant is designed to flow around the outer circumference of the column.
Oリング103と406は気密を保持するためのもので
あるが、602は巣にミラーを押しつけるための緩衝材
としての働きをなすものである0503は通気口でミラ
ーの両面での圧力差をなくすためにあけられている。本
実権例では第1図のベローズ3の様に気密を保ちながら
可動する部分がないことからシール構造が簡単になる。O-rings 103 and 406 are used to maintain airtightness, while 602 acts as a buffer to press the mirror against the nest.0503 is a vent that eliminates the pressure difference on both sides of the mirror. It is opened for In this practical example, unlike the bellows 3 in FIG. 1, there is no part that moves while maintaining airtightness, so the seal structure is simple.
本実施例の装置(おけるミラーの位置調整は次の手順で
行なう。まず本体キャップ102を取りはずし、共振器
の内部を含めて大気圧下でミラーの位置調整を行なう。The position adjustment of the mirror in the apparatus of this embodiment is carried out in the following steps. First, the main body cap 102 is removed, and the position of the mirror including the inside of the resonator is adjusted under atmospheric pressure.
羊の詳細は従来例で説明した通りの方法であり、説明は
省略する。ミラーイrtftIfI髭が終了したら本体
キャップ102を取付け、光学共振器内を排気し所定の
圧力のレーザガスを供給し、レーザ発振を行なう訳であ
るが、ミラーItIt fil tA 終了時点から
レーザ発振に至る迄ミラーの両面にはほとんど圧力差が
発生しないC通気口503iガスが流れる時には微少圧
力差が発生する)からミラー面が変動せず、調整終了時
点から狂うことはない〇
更に必要によりミラー位置調整の補正を行ないたい場合
は第4図に示す様に微調整ドライバモ1を設けることに
より更に機能が拡大する。62は気密用0リング、10
はドライバー61のスラスト荷重がミラーアライメント
に影響(与えない様に設けた間隙である。The details of the sheep are the same as explained in the conventional example, and the explanation will be omitted. When the mirror is finished, the main body cap 102 is attached, the inside of the optical resonator is evacuated, and laser gas at a predetermined pressure is supplied to perform laser oscillation. Since there is almost no pressure difference on both sides of the C vent 503i (a slight pressure difference occurs when gas flows), the mirror surface will not fluctuate and will not go out of order from the time the adjustment is completed. Also, if necessary, correct the mirror position adjustment. If it is desired to perform this, the functions can be further expanded by providing a fine adjustment driver motor 1 as shown in FIG. 62 is an airtight O-ring, 10
is a gap provided so that the thrust load of the driver 61 does not affect mirror alignment.
またレーザの出力が小さい場合は液冷が不要なため、液
冷系統を省略することができる。Furthermore, if the output of the laser is small, liquid cooling is not necessary, so the liquid cooling system can be omitted.
きたが、出力結合鏡部についても同様に適用することが
出来る。その−例を第6図に示す。However, the same can be applied to the output coupling mirror section. An example thereof is shown in FIG.
ミラーホルダ4Fi中央をビームが通過できる様にド−
ナツ状に作られ、本体キャップ102の中央部には当該
レーザビームの透過率の高い材質で形成された透過窓1
04が気密用Oリング106を介して止を板1−O6で
固定される。107は冷却液ノズルである。又31.が
出力結合鏡である。Adjust the door so that the beam can pass through the center of mirror holder 4Fi.
A transmission window 1 formed in the center of the nut-shaped main body cap 102 is made of a material with high transmittance for the laser beam.
04 is fixed with a stop plate 1-O6 via an airtight O-ring 106. 107 is a cooling liquid nozzle. Also 31. is the output coupling mirror.
以上述べた様に本発明はミラー位置調整機構を大気と遮
断し、光学共振器のレーザガスを有する系の容器内に設
けたもので、ミラー位置調整機構は常に光学共振器内の
圧力下にあるため、従来構、造の欠点を克服し、最適条
件下で長期の安定性を確保することができると共に7、
ミラー位置調整機構を室内の塵埃力(も守ることができ
る。As described above, the present invention isolates the mirror position adjustment mechanism from the atmosphere and provides it in a container of a system containing the laser gas of the optical resonator, and the mirror position adjustment mechanism is always under pressure within the optical resonator. Therefore, it is possible to overcome the drawbacks of conventional structures and ensure long-term stability under optimal conditions7.
The mirror position adjustment mechanism can also protect against indoor dust.
第1図は従来のレーザ発振器のミラー位置調整機構の一
例を示す断面図、第2図はそのご部拡大断面図、−第3
図は本発明の一実施例におけるレーザ発振器のミラー位
at調整機構の断面図、第4図および第6図は本発明能
の実施例のレーザ発振器のミラー位置調整機構の一部断
面図である。
1・・!9・・基台、2・拳・・・・レーザ管、3・・
・・・・全反射鏡、4軸・・・・ミラーホルダ、6・−
・@−・ミラー受7ランジ、6・・―・0微調整ねじ、
7・Φ・・・・ベローズ、8・QΦΦ・拳固定板、9・
・・・・Φ圧縮ばね、404・・−!・・固定台、40
6・・・・Φ・冷却液ノズル、102・0・・・本体キ
ャップ、61・・・・・・微調整用ドライバー、31・
・・ΦΦ・出力結合鏡、104・・・・・・透過窓。
代理人の氏名 弁理士中 尾 敏 男 ほか1名第1図
第3図
第4図Fig. 1 is a sectional view showing an example of a mirror position adjustment mechanism of a conventional laser oscillator, Fig. 2 is an enlarged sectional view of its part, -3.
The figure is a sectional view of a mirror position adjustment mechanism of a laser oscillator according to an embodiment of the present invention, and FIGS. 4 and 6 are partial sectional views of the mirror position adjustment mechanism of a laser oscillator according to an embodiment of the present invention. . 1...! 9. Base, 2. Fist... Laser tube, 3.
...Total reflection mirror, 4 axes...Mirror holder, 6.-
・@-・Mirror holder 7 lange, 6...0 fine adjustment screw,
7・Φ・・・Bellows, 8・QΦΦ・Fist fixing plate, 9・
...Φ compression spring, 404...-!・・Fixed stand, 40
6...φ・Cooling liquid nozzle, 102・0...Body cap, 61...Fine adjustment screwdriver, 31・
...ΦΦ・Output coupling mirror, 104...Transmission window. Name of agent: Patent attorney Toshio Nakao and one other person Figure 1 Figure 3 Figure 4
Claims (1)
ザガスを有する系の容器内に設けたことを特徴とする羊
;レーザ発振器。A laser oscillator, characterized in that a mirror position adjustment mechanism is isolated from the atmosphere and provided in a container of a system containing a laser gas of an optical resonator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18867681A JPS5889886A (en) | 1981-11-24 | 1981-11-24 | Laser oscillator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18867681A JPS5889886A (en) | 1981-11-24 | 1981-11-24 | Laser oscillator |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5889886A true JPS5889886A (en) | 1983-05-28 |
Family
ID=16227892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP18867681A Pending JPS5889886A (en) | 1981-11-24 | 1981-11-24 | Laser oscillator |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5889886A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01218081A (en) * | 1988-02-26 | 1989-08-31 | Fanuc Ltd | Laser oscillator |
JPH0245661U (en) * | 1988-09-22 | 1990-03-29 | ||
JPH0595142A (en) * | 1991-10-01 | 1993-04-16 | Mitsubishi Electric Corp | Laser oscillator |
JP2011159901A (en) * | 2010-02-03 | 2011-08-18 | Mitsubishi Electric Corp | Gas laser device |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS448530Y1 (en) * | 1965-03-08 | 1969-04-04 | ||
JPS4827663U (en) * | 1971-08-02 | 1973-04-03 |
-
1981
- 1981-11-24 JP JP18867681A patent/JPS5889886A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS448530Y1 (en) * | 1965-03-08 | 1969-04-04 | ||
JPS4827663U (en) * | 1971-08-02 | 1973-04-03 |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH01218081A (en) * | 1988-02-26 | 1989-08-31 | Fanuc Ltd | Laser oscillator |
JPH0245661U (en) * | 1988-09-22 | 1990-03-29 | ||
JPH0595142A (en) * | 1991-10-01 | 1993-04-16 | Mitsubishi Electric Corp | Laser oscillator |
JP2011159901A (en) * | 2010-02-03 | 2011-08-18 | Mitsubishi Electric Corp | Gas laser device |
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