JPS6342428B2 - - Google Patents
Info
- Publication number
- JPS6342428B2 JPS6342428B2 JP57050176A JP5017682A JPS6342428B2 JP S6342428 B2 JPS6342428 B2 JP S6342428B2 JP 57050176 A JP57050176 A JP 57050176A JP 5017682 A JP5017682 A JP 5017682A JP S6342428 B2 JPS6342428 B2 JP S6342428B2
- Authority
- JP
- Japan
- Prior art keywords
- mode
- tem
- carbon dioxide
- laser
- reflecting mirror
- 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.)
- Expired
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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
- H01S3/08018—Mode suppression
- H01S3/08022—Longitudinal modes
- H01S3/08031—Single-mode emission
- H01S3/08036—Single-mode emission using intracavity dispersive, polarising or birefringent elements
-
- 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
- H01S3/08018—Mode suppression
- H01S3/0804—Transverse or lateral modes
- H01S3/0805—Transverse or lateral modes by apertures, e.g. pin-holes or knife-edges
-
- 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
- H01S2301/00—Functional characteristics
- H01S2301/20—Lasers with a special output beam profile or cross-section, e.g. non-Gaussian
-
- 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
- H01S2301/00—Functional characteristics
- H01S2301/20—Lasers with a special output beam profile or cross-section, e.g. non-Gaussian
- H01S2301/206—Top hat profile
-
- 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
- H01S3/08059—Constructional details of the reflector, e.g. shape
- H01S3/08063—Graded reflectivity, e.g. variable reflectivity mirror
-
- 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
- H01S3/14—Lasers, i.e. devices using stimulated emission of electromagnetic radiation in the infrared, visible or ultraviolet wave range characterised by the material used as the active medium
- H01S3/22—Gases
- H01S3/223—Gases the active gas being polyatomic, i.e. containing two or more atoms
- H01S3/2232—Carbon dioxide (CO2) or monoxide [CO]
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- Plasma & Fusion (AREA)
- Optics & Photonics (AREA)
- Lasers (AREA)
Description
【発明の詳細な説明】
〔発明の技術分野〕
本発明は炭酸ガスレーザ装置に係り、特に
TEM01*モードのレーザ光を選択して得られる
構造からなる炭酸ガスレーザ装置に関するもので
ある。[Detailed Description of the Invention] [Technical Field of the Invention] The present invention relates to a carbon dioxide laser device, and particularly to a carbon dioxide laser device.
This relates to a carbon dioxide laser device having a structure obtained by selecting the TEM 01 * mode of laser light.
ガスレーザ装置の一例を第1図により説明する
と、例えば炭酸ガスを含有するレーザ媒質1を間
において全反射鏡2と半反射鏡3が対向して設け
られ、全反射鏡2及び半反射鏡3のレーザ媒質1
側にはアパーチヤ41の穿設された絞り板4が配
設されている。
An example of a gas laser device will be described with reference to FIG. 1. For example, a total reflection mirror 2 and a half reflection mirror 3 are provided facing each other with a laser medium 1 containing carbon dioxide gas in between. Laser medium 1
A diaphragm plate 4 with an aperture 41 is disposed on the side.
このようなガスレーザ装置においてはレーザ媒
質1をグロー放電により励起し、その励起による
光エネルギーを全反射鏡2と半反射鏡3間でポン
ピングし共振させると、半反射鏡3からはレーザ
光5が射出されるようになつている。 In such a gas laser device, when the laser medium 1 is excited by glow discharge and the optical energy resulting from the excitation is pumped between the total reflection mirror 2 and the half-reflection mirror 3 to cause resonance, the laser beam 5 is emitted from the half-reflection mirror 3. It is starting to be ejected.
この様なガスレーザ装置においてレーザ光の発
振横モードはレーザ媒質1のグロー放電による励
起状態、全反射鏡2や半反射鏡3の曲率半径や間
隔などできまる共振器構成と絞り板4のアパーチ
ヤ41の形状、大きさによつて決定される。そし
てこのレーザの発振横モードは、Transverse
Electromagnetic波の略号を用いてTEMmn(但
しm,nはモードの次数である)と表記され、そ
れぞれのモードには特有の電界強度分布が対応し
ている。 In such a gas laser device, the oscillation transverse mode of the laser beam is determined by the excited state of the laser medium 1 due to glow discharge, the resonator configuration determined by the radius of curvature and spacing of the total reflection mirror 2 and the half reflection mirror 3, and the aperture 4 of the aperture plate 4. Determined by the shape and size of 1 . The oscillation transverse mode of this laser is Transverse
It is expressed as TEMmn (where m and n are the orders of the modes) using the abbreviation for electromagnetic waves, and each mode corresponds to a unique electric field intensity distribution.
このTEMmnモードには第2図に示すTEM00
モード7第3図に示すTEM01*モード8、第4
図に示すTEM10モード9第5図に示すTEM11モ
ード10、第6図に示すTEM02モード11、第
7図に示すマルチモード12などがある。 This TEMmn mode has TEM 00 as shown in Figure 2.
Mode 7 TEM 01 shown in Figure 3 *Mode 8, 4th
There are TEM 10 mode 9 shown in the figure, TEM 11 mode 10 shown in FIG. 5, TEM 02 mode 11 shown in FIG. 6, and multimode 12 shown in FIG. 7.
これら曲線よりモード次数が低いものほどレー
ザ光のビーム径は小さくなり、モード次数が高い
ほどレーザ光のビーム径が大きくなることがわか
る。 It can be seen from these curves that the lower the mode order, the smaller the beam diameter of the laser light, and the higher the mode order, the larger the beam diameter of the laser light.
そしてこれら各モードのレーザ光をレンズなど
の光学系を介して集光して被加工物を加工する場
合、レーザ光のもつ特性により、低次のモードの
ものほどそのスポツト径が小さく、高次のものほ
どスポツト径が大きくなり、さらにマルチモード
12ではその波面が不ぞろいなためさらに集光性
が悪くなる。 When processing a workpiece by concentrating laser light in each of these modes through an optical system such as a lens, due to the characteristics of the laser light, the spot diameter of the lower mode is smaller and the higher the The larger the spot diameter, the larger the spot diameter, and in the case of multi-mode 12, the wavefront is uneven, which further deteriorates the light focusing ability.
しかしながら、レーザ媒質中にグロー放電を生
じさせて均一に放電励起された領域中に共振路を
組む場合には、レーザ装置としての出力は明らか
にその共振路に含まれるレーザ媒質の体積に比例
する。そのため均一な放電励起を生じさせるレー
ザ装置においては、その発振モードが低く、ビー
ム径が小さいほどレーザ出力は低く、高次モード
ではレーザ出力が大きい。実際にはシングルモー
ド(TEM00モード相当)ではレーザ出力が小さ
く、マルチモード(高次モード混合)ではレーザ
出力が大きい。 However, when a glow discharge is generated in a laser medium and a resonant path is formed in a uniform discharge-excited region, the output of the laser device is clearly proportional to the volume of the laser medium included in the resonant path. . Therefore, in a laser device that generates uniform discharge excitation, the lower the oscillation mode and the smaller the beam diameter, the lower the laser output, and the higher the laser output in higher-order modes. In reality, the laser output is small in single mode (equivalent to TEM 00 mode), and large in multimode (higher-order mode mixture).
しかるに従来この発振モードは第1図で説明し
たようにレーザ媒質1を間において設けられた全
反射鏡2と半反射鏡3のレーザ媒質1側にアパー
チヤ41の穿設された絞り板4を設けこのアパー
チヤ41により、その発振横モードのビーム外径
を共振器内で制限することによつて選択している
が、この場合外径の小さいTEM00モードは選択
できても、それ以上のモードはTEM00モードよ
りもそのビーム径が大きいためアパーチヤ41径
を大きくしなければならず、その結果TEM00モ
ードが同時に発生し単一のモードが選択できない
問題点があつた。 However, conventionally, this oscillation mode is achieved by using a diaphragm plate 4 with an aperture 41 formed on the side of the laser medium 1 of the total reflection mirror 2 and the half reflection mirror 3, which are provided with the laser medium 1 in between, as explained in FIG. This aperture 41 is used to select the beam outer diameter of the oscillation transverse mode by limiting it within the resonator, but in this case, although the TEM 00 mode with a small outer diameter can be selected, the larger diameter Since the beam diameter of the mode is larger than that of the TEM 00 mode, the diameter of the aperture 41 must be made larger, and as a result, the TEM 00 mode occurs simultaneously, resulting in the problem that a single mode cannot be selected.
本発明は前記従来の問題点に鑑みなされたもの
であり、シングルモードとマルチモードの中間に
あり、これら両者の利点を兼ねそなえたTEM01
*モードを選択することが可能な炭酸ガスレーザ
装置を提供することを目的としている。
The present invention was made in view of the above-mentioned conventional problems, and is a TEM 01 which is between single mode and multimode and has the advantages of both.
*The purpose is to provide a carbon dioxide laser device that allows mode selection.
即ち、本発明は少なくとも2枚の反射鏡を対向
して配設し、反射鏡間に炭酸ガスを含有するレー
ザ媒質を循環させ、このレーザ媒質中にグロー放
電を発生させレーザ光を発生するように構成され
た炭酸ガスレーザ装置において、反射鏡の少くと
も1枚のレーザ媒質側に所定径のアパーチヤの穿
設された絞り板を配設すると共に反射鏡の少なく
とも1枚を環状にしたことを特徴とし、更にアパ
ーチヤがTEM10モード以上の発振のゲインを抑
制する大きさであり、環状の中心部がTEM00モ
ード発振のゲインを抑制する大きさであることを
特徴としている。
That is, the present invention arranges at least two reflecting mirrors facing each other, circulates a laser medium containing carbon dioxide gas between the reflecting mirrors, and generates a glow discharge in the laser medium to generate laser light. The carbon dioxide laser device is characterized in that a diaphragm plate with an aperture of a predetermined diameter is disposed on the laser medium side of at least one of the reflecting mirrors, and at least one of the reflecting mirrors is formed into an annular shape. Further, the aperture has a size that suppresses the gain of oscillation in TEM 10 mode or higher, and the annular center has a size that suppresses the gain of TEM 00 mode oscillation.
実験によればTEM01*モードの集光性は
TEM00モードの場合とほぼ同等であり、またそ
のビーム径はTEM00モードの1.5倍あるため、均
一な放電励起領域に共振路を組み込んだ場合、
TEM00モードの場合の2倍以上のレーザ出力が
得られる。またTEM01*モードは第3図を見て
もわかるようにそのエネルギー分布がドーナツツ
状をしているため、総合出力を考えると、明らか
に単位面積あたりのエネルギー密度が低い。また
面積に比例した総合出力もTEM00モードより低
くすることができる。このことは反射鏡特に出力
側の半反射鏡に対するエネルギー損失による熱負
荷を非常に緩和することが可能となる。さらにレ
ーザ光を通過させるために周辺冷却のみしかでき
ない構造の出力側の半反射鏡においては、そのレ
ーザ光の吸収によつて発生する熱源をできるだけ
周辺部分におくことにより冷却効果を極めて大き
くすることができる。これに対しTEM00モード
のものは、第2図を見てもわかるようにそのエネ
ルギー分布が中央部が極めて高くなつているの
で、出力側の半反射鏡に対するエネルギー損失に
よる熱負荷が高く、周辺冷却のみしかできない構
造の半反射鏡ではレーザ光の吸収によつて発生す
る熱源が中央にあるため、出力を上げると半反射
鏡を劣化、破壊する危険性が極めて高くなる。
According to experiments, the light focusing ability of TEM 01 *mode is
It is almost the same as the TEM 00 mode, and the beam diameter is 1.5 times that of the TEM 00 mode, so when a resonant path is incorporated in a uniform discharge excitation region,
More than twice the laser output as in TEM 00 mode can be obtained. Furthermore, as can be seen from Figure 3, the energy distribution of the TEM 01 * mode is donut-shaped, so when considering the total output, the energy density per unit area is clearly low. Also, the total output proportional to area can be lower than in TEM 00 mode. This makes it possible to greatly reduce the thermal load due to energy loss on the reflecting mirror, especially the semi-reflecting mirror on the output side. Furthermore, for the semi-reflector on the output side, which has a structure in which only peripheral cooling is possible in order to allow the laser beam to pass through, the cooling effect can be maximized by placing the heat source generated by the absorption of the laser beam as close to the peripheral area as possible. Can be done. On the other hand, in the TEM 00 mode, as can be seen from Figure 2, the energy distribution is extremely high in the center, so the heat load due to energy loss to the output side semi-reflector is high, and In a semi-reflecting mirror that can only be cooled, the heat source generated by absorption of laser light is located in the center, so increasing the output increases the risk of deteriorating or destroying the semi-reflecting mirror.
このため本発明はTEM01*モードのみを選択
的に発生させ、TEM00モード、及びTEM10モー
ド以上を除去するようになつている。 Therefore, the present invention selectively generates only the TEM 01 * mode and eliminates the TEM 00 mode and the TEM 10 mode or higher.
次に本発明の炭酸ガスレーザ装置の最も簡単な
第1の実施例を第8図により説明する。 Next, the simplest first embodiment of the carbon dioxide laser device of the present invention will be described with reference to FIG.
即ち、炭酸ガスを含有するレーザ媒質21は図
示しない循環機構により循環されており、このレ
ーザ媒質21を間において凹面の全反射鏡22と
同じく凹面の半反射鏡23が対向して設けられ、
全反射鏡22及び半反射鏡23のレーザ媒質21
にはアパーチヤ241の穿設された絞り板24が
配設されているのは従来のものとほぼ同様である
が、本実施例においては全反射鏡22を環状にし
この環状の中心部221をレーザ光の吸収または
散乱などによりエネルギーの損失を行なわせる所
謂エネルギーの損失領域としている。 That is, a laser medium 21 containing carbon dioxide gas is circulated by a circulation mechanism (not shown), and a concave total reflection mirror 22 and a concave semi-reflection mirror 23 are provided facing each other with the laser medium 21 in between.
Laser medium 21 of total reflection mirror 22 and half reflection mirror 23
The diaphragm plate 24 with an aperture 24 1 is disposed therein, which is almost the same as the conventional one, but in this embodiment, the total reflection mirror 22 is annular and the center part 22 1 of this annular shape is formed. This is a so-called energy loss region where energy is lost due to absorption or scattering of laser light.
このような構造にすることにより、アパーチヤ
241をTEM10モード以上の発振のゲインを抑制
する大きさとし、中心部221のエネルギーの損
失領域でTEM00モードの発振のゲインを抑制す
る大きさとし、レーザ媒質21をグロー放電によ
り励起し、この励起による光エネルギーを全反射
鏡22と半反射鏡23間で共振させると、半反射
鏡23からはTEM01*モードのレーザ光25の
みが選択されて射出されることになる。 With such a structure, the aperture 24 1 is made large enough to suppress the gain of oscillation in TEM 10 mode or higher, and the aperture 24 1 is made large enough to suppress the gain of oscillation in TEM 00 mode in the energy loss region of the central portion 22 1 , When the laser medium 21 is excited by glow discharge and the light energy resulting from this excitation is caused to resonate between the total reflection mirror 22 and the half-reflection mirror 23, only the laser beam 25 in the TEM 01 * mode is selected from the half-reflection mirror 23. It will be ejected.
本実施例を更に詳細に説明すると、共振器内部
での発振モードのビーム径は2ω0として特徴づけ
られる。ここで、このω0はTEM00モードのエネ
ルギー分布を示したとき、その中心のエネルギー
強度1/e2のエネルギー強度になるところの半径
である。 To explain this example in more detail, the beam diameter of the oscillation mode inside the resonator is characterized as 2ω 0 . Here, this ω 0 is the radius at which the energy intensity at the center becomes 1/e 2 when the energy distribution of the TEM 00 mode is shown.
次にその分布式をTEM00モード、TEM01*モ
ード、TEM10モードについて示すと共に第9図
乃至第11図に曲線で示す。 Next, the distribution formulas are shown for TEM 00 mode, TEM 01 * mode, and TEM 10 mode, and are also shown as curves in FIGS. 9 to 11.
先ずTEM00モードの場合は中心の強度をI0と
すると
I=I0 exp(−2r2/ω0 2)
で表わされ、第9図の曲線27に示す分布とな
る。 First, in the case of TEM 00 mode, when the intensity at the center is I 0 , it is expressed as I=I 0 exp (−2r 2 /ω 0 2 ), resulting in a distribution shown by curve 27 in FIG.
次にTEM01*モードの場合は中心での強度を
I0とすると
I=I0(2r2/ω0 2)exp(−2r2/ω0 2)
で表わされ、第10図の曲線28に示す分布とな
る。 Next, in the case of TEM 01 * mode, change the intensity at the center.
If I 0 , then I=I 0 (2r 2 /ω 0 2 )exp(−2r 2 /ω 0 2 ), resulting in a distribution shown by curve 28 in FIG.
またTEM10モードの場合は中心での強度をI0
とすると
I=I0(1−2r2/ω0 2)2exp(−2r2/ω0 2)
で表わされ、第11図の曲線29に示す分布とな
る。 In addition, in the case of TEM 10 mode, the intensity at the center is I 0
Then, I=I 0 (1−2r 2 /ω 0 2 ) 2 exp(−2r 2 /ω 0 2 ), resulting in a distribution shown by curve 29 in FIG.
更にこれらを用いてアパーチヤ241によるエ
ネルギーの損失を示したのが第12図の曲線群3
0,31,32であり、曲線30はTEM00モー
ド、曲線31はTEM01*モード、曲線32は
TEM10モードを示しており、この第12図によ
りTEM01*モードの損失とTEM10モードの損失
を適切に選択すればよいが実験の結果から見ると
アパーチヤ241の半径は1.69ω0〜1.95ω0の範囲
にすることが最も良好である。 Furthermore, curve group 3 in Figure 12 shows the energy loss due to the aperture 24 1 using these.
0, 31, 32, curve 30 is TEM 00 mode, curve 31 is TEM 01 * mode, curve 32 is
The TEM 10 mode is shown, and the loss of the TEM 01 * mode and the loss of the TEM 10 mode can be appropriately selected according to this figure 12, but from the experimental results, the radius of the aperture 24 1 is 1.69ω 0 ~ 1.95 It is best to set it in the range of ω 0 .
また全反射鏡22の中心部221の損失領域に
よるエネルギー損失を示したのが第13図の曲線
群33,34,35であり、曲線33はTEM00
モード、曲線34はTEM01*モード、曲線35
はTEM10モードを示しており、この第13図に
よりTEM00モードの損失とTEM01*モードの損
失を適切に選択すればよいが、実験の結果から見
ると中心部221の半径は0.01ω0〜0.30ω0にする
ことが最も良好である。 Furthermore, curve groups 33, 34, and 35 in FIG. 13 show the energy loss due to the loss region of the central portion 22 1 of the total reflection mirror 22, and the curve 33 is TEM 00
Mode, curve 34 is TEM 01 *Mode, curve 35
shows the TEM 10 mode, and the loss of the TEM 00 mode and the loss of the TEM 01 * mode can be appropriately selected according to Fig. 13, but from the experimental results, the radius of the center 22 1 is 0.01ω. It is best to set it to 0 to 0.30ω 0 .
これらの値を第8図に当てはめてみると、絞り
板24は黒アルマイト処理され、そのアパーチヤ
241の直径は21mm、全反射鏡22は外径50mm、
中心部221の内径が2mm、曲率半径が20mの凹
面鏡、半反射鏡23は曲率20mの凹面鏡、また全
反射鏡22と半反射鏡23の間隔は7.5mにとら
れており、この共振器構成によりレーザエネルギ
ー2.5KWのTEM01*モードのレーザ光が得られ
た。 Applying these values to Fig. 8, we find that the diaphragm plate 24 is black alumite treated, the diameter of the aperture 241 is 21 mm, the outer diameter of the total reflection mirror 22 is 50 mm,
The center part 221 has a concave mirror with an inner diameter of 2 mm and a radius of curvature of 20 m, and the semi-reflecting mirror 23 is a concave mirror with a curvature of 20 m.The interval between the total reflecting mirror 22 and the semi-reflecting mirror 23 is 7.5 m. Depending on the configuration, a TEM 01 * mode laser beam with a laser energy of 2.5KW was obtained.
前記実施例では絞り板24を全反射鏡22側及
び半反射鏡23側の両方に設けたが、半反射鏡2
3側には設けなくとも同様な効果が得られる。 In the embodiment described above, the diaphragm plate 24 was provided on both the total reflection mirror 22 side and the half reflection mirror 23 side.
The same effect can be obtained even if it is not provided on the third side.
次に本発明の第2の実施例を第14図により説
明する。図中第1の実施例と同一符号は同一部分
を示し特に説明を行なわない。 Next, a second embodiment of the present invention will be described with reference to FIG. In the drawings, the same reference numerals as in the first embodiment indicate the same parts and will not be particularly described.
即ち、本実施例は折りかえし形の共振器構造で
あり、第1の実施例の他に、平面全反射鏡26を
1対設けたことを特徴としており、このような折
りかえし形にすることにより、炭酸ガスレーザ装
置を小さくすることが可能である。 That is, this embodiment has a folded resonator structure, and is characterized by providing a pair of flat total reflection mirrors 26 in addition to the first embodiment. Therefore, it is possible to downsize the carbon dioxide laser device.
次に本発明の応用例を第15図に示す。図中第
1の実施例と同一符号は同一部分を示し、特に説
明を行なわない。 Next, an application example of the present invention is shown in FIG. In the figure, the same reference numerals as those in the first embodiment indicate the same parts, and no particular explanation will be given.
即ち、本応用例においては環状の全反射鏡22
の中心部221を利用して外部から可視レーザ光
をだす例えばHe―Neレーザ装置41からのレー
ザ光431を1対の反射鏡42により反射した反
射レーザ光432を炭酸ガスレーザ装置の中心部
を通るように導き共振器用反射鏡22,23のア
ライメントに用いると共にレーザ出力ビームの案
内としている。 That is, in this application example, the annular total reflection mirror 22
For example, a laser beam 43 1 from a He-Ne laser device 41 is reflected by a pair of reflecting mirrors 42 and reflected laser beam 43 2 is emitted from the outside using the central portion 22 1 of the carbon dioxide laser device. It is used to align the resonator reflecting mirrors 22 and 23 and also to guide the laser output beam.
上述したように本発明の炭酸ガスレーザ装置に
よればシングルモードとマルチモードの中間で、
これら両者の利点をTEM01*モードを選択して
取り出すことが可能であり、高エネルギーのレー
ザ光が得られるし、またこのTEM01*モードは
そのエネルギー分布がドーナツツ状となり、周辺
冷却のみしかできない出力側の半反射鏡を劣化、
破壊する危険性も極めて少ない良好な装置であ
り、その工業的価値は極めて大である。
As mentioned above, according to the carbon dioxide laser device of the present invention, between single mode and multimode,
It is possible to take out the advantages of both by selecting TEM 01 * mode, and a high-energy laser beam can be obtained. Also, in this TEM 01 * mode, the energy distribution is donut-shaped, and only peripheral cooling is possible. Deterioration of the output side semi-reflector,
It is a good device with very little risk of destruction, and its industrial value is extremely large.
第1図は従来のレーザ装置の説明図、第2図乃
至第7図は各モードの波形を示す図であり、第2
図はTEM00モードの波形を示すグラフ、第3図
はTEM01*モードの波形を示すグラフ、第4図
はTEM10モードの波形を示すグラフ、第5図は
TEM11モードの波形を示すグラフ、第6図は
TEM02モードの波形を示すグラフ、第7図は高
次モードの混合波形を示すグラフ、第8図は本発
明の炭酸ガスレーザ装置の一実施例を示す説明
図、第9図乃至第11図は各モードのビーム半径
と出力密度との関係を示す図であり、第9図は
TEM00モードの波形を示すグラフ、第10図は
TEM01*モードの波形を示すグラフ、第11図
はTEM10モードの波形を示すグラフ、第12図
はアパーチヤによる出力損失とアパーチヤの半径
との関係におけるTEM00、TEM01*、TEM10各
モードの関係を示すグラフ、第13図は中心部の
損失領域による出力損失と損失領域半径との関係
におけるTEM00、TEM01*、TEM10各モードの
関係を示すグラフ、第14図は本発明の第2の実
施例を示す説明図、第15図は本発明の応用例を
示す説明図である。
1,21…レーザ媒質、2,22…全反射鏡、
3,23…半反射鏡、4,24…絞り板、41,
241…アパーチヤ、5,25…レーザ光、221
…中央部、41…He―Neレーザ装置。
FIG. 1 is an explanatory diagram of a conventional laser device, and FIGS. 2 to 7 are diagrams showing waveforms of each mode.
The figure is a graph showing the waveform of TEM 00 mode, Fig. 3 is a graph showing the waveform of TEM 01 * mode, Fig. 4 is a graph showing the waveform of TEM 10 mode, and Fig. 5 is a graph showing the waveform of TEM 10 mode.
The graph showing the waveform of TEM 11 mode, Figure 6 is
Graph showing the waveform of TEM 02 mode, FIG. 7 is a graph showing the mixed waveform of higher order mode, FIG. 8 is an explanatory diagram showing one embodiment of the carbon dioxide laser device of the present invention, and FIGS. 9 to 11 are FIG. 9 is a diagram showing the relationship between the beam radius and power density of each mode.
The graph showing the waveform of TEM 00 mode, Figure 10 is
Graph showing the waveform of TEM 01 * mode, Figure 11 is a graph showing the waveform of TEM 10 mode, Figure 12 is the relationship between output loss due to aperture and aperture radius for TEM 00 , TEM 01 *, and TEM 10 modes. 13 is a graph showing the relationship between the TEM 00 , TEM 01 *, and TEM 10 modes in the relationship between the output loss due to the loss region in the center and the radius of the loss region. FIG. 15 is an explanatory diagram showing the second embodiment, and FIG. 15 is an explanatory diagram showing an application example of the present invention. 1, 21... Laser medium, 2, 22... Total reflection mirror,
3, 23... Semi-reflector, 4, 24... Diaphragm plate, 4 1 ,
24 1 ...Aperture, 5, 25...Laser light, 22 1
...Central part, 41...He-Ne laser device.
Claims (1)
前記反射鏡間に炭酸ガスを含有するレーザ媒質を
循環し、このレーザ媒質中にグロー放電を発生さ
せレーザ光を発生するように構成された炭酸ガス
レーザ装置において、前記反射鏡の少くとも1枚
の前記レーザ媒質側に所定径のアパーチヤの穿設
された絞り板を配設すると共に前記反射鏡の少な
くとも1枚を環状にしたことを特徴とする炭酸ガ
スレーザ装置。 2 対向して配設された反射鏡が全反射鏡と半反
射鏡とからなり、これら全反射鏡と半反射鏡間の
レーザ媒質側にそれぞれ、または前記全反射鏡側
のみにアパーチヤの穿設された絞り板を配設する
と共に、前記全反射鏡を中心部にエネルギーの損
失領域を有する環状にしたことを特徴とする特許
請求の範囲第1項記載の炭酸ガスレーザ装置。 3 対向して配設された反射鏡がレーザ光の光路
順に全反射鏡第1の全反射鏡、第2の全反射鏡及
び半反射鏡からなり、前記全反射鏡と半反射鏡間
のレーザ媒質側にそれぞれ、または全反射鏡側の
みにアパーチヤの穿設された絞り板を配設すると
共に前記全反射鏡を環状にしたことを特徴とする
特許請求の範囲第1項記載の炭酸ガスレーザ装
置。 4 他のレーザ装置からの可視レーザ光が環状の
全反射鏡の中心部を通過したのち、半反射鏡を介
して案内光とされていることを特徴とする特許請
求の範囲第1項乃至第3項いずれかに記載の炭酸
ガスレーザ装置。 5 アパーチヤがTEM10モード以上の発振のゲ
インを抑制する大きさであり、環状の中心部が
TEM00モード発振のゲインを抑制する大きさで
あることを特徴とする特許請求の範囲第1項乃至
第4項いずれかに記載の炭酸ガスレーザ装置。[Claims] 1. At least two reflecting mirrors are arranged facing each other,
In the carbon dioxide laser device configured to circulate a laser medium containing carbon dioxide gas between the reflecting mirrors and generate a glow discharge in the laser medium to generate laser light, at least one of the reflecting mirrors A carbon dioxide laser device characterized in that a diaphragm plate having an aperture of a predetermined diameter is disposed on the laser medium side, and at least one of the reflecting mirrors is annular. 2 The reflecting mirrors arranged facing each other are composed of a total reflecting mirror and a semi-reflecting mirror, and an aperture is formed on the laser medium side between the total reflecting mirror and the semi-reflecting mirror, or only on the total reflecting mirror side. 2. The carbon dioxide laser device according to claim 1, wherein the total reflection mirror has an annular shape having an energy loss region in the center thereof. 3 The reflecting mirrors arranged opposite to each other are composed of a first total reflecting mirror, a second total reflecting mirror, and a half reflecting mirror in the order of the optical path of the laser beam, and the laser beam between the totally reflecting mirror and the half reflecting mirror is The carbon dioxide laser device according to claim 1, characterized in that a diaphragm plate with an aperture is provided on each of the medium side or only on the total reflection mirror side, and the total reflection mirror is formed into an annular shape. . 4. Claims 1 to 4, characterized in that the visible laser light from another laser device passes through the center of the annular total reflection mirror and then becomes guided light via the semi-reflection mirror. The carbon dioxide laser device according to any one of Item 3. 5 The aperture is large enough to suppress the gain of oscillations in TEM 10 mode and above, and the annular center is
The carbon dioxide laser device according to any one of claims 1 to 4, characterized in that the size is such that the gain of TEM 00 mode oscillation is suppressed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57050176A JPS58168288A (en) | 1982-03-30 | 1982-03-30 | Carbon dioxide gas laser device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP57050176A JPS58168288A (en) | 1982-03-30 | 1982-03-30 | Carbon dioxide gas laser device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58168288A JPS58168288A (en) | 1983-10-04 |
| JPS6342428B2 true JPS6342428B2 (en) | 1988-08-23 |
Family
ID=12851883
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP57050176A Granted JPS58168288A (en) | 1982-03-30 | 1982-03-30 | Carbon dioxide gas laser device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58168288A (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01258482A (en) * | 1988-04-08 | 1989-10-16 | Fanuc Ltd | Discharge tube for gas laser device |
| JPH02166778A (en) * | 1988-12-21 | 1990-06-27 | Amada Co Ltd | Optical resonator for gas laser |
| WO2012035953A1 (en) * | 2010-09-17 | 2012-03-22 | 三菱電機株式会社 | Gas laser device and laser processing device |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5752584B2 (en) * | 1973-05-23 | 1982-11-08 | ||
| JPS5177340A (en) * | 1974-12-27 | 1976-07-05 | Ritsuo Hasumi | FUAIBAA HANSHAKYO |
| JPS5754291Y2 (en) * | 1977-05-09 | 1982-11-24 | ||
| JPS5441692A (en) * | 1977-09-09 | 1979-04-03 | Mitsubishi Electric Corp | Laser unit |
| JPS56114390A (en) * | 1980-02-15 | 1981-09-08 | Sumitomo Electric Ind Ltd | Laser apparatus |
-
1982
- 1982-03-30 JP JP57050176A patent/JPS58168288A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58168288A (en) | 1983-10-04 |
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