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JPH0317232B2 - - Google Patents
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JPH0317232B2 - - Google Patents

Info

Publication number
JPH0317232B2
JPH0317232B2 JP13125083A JP13125083A JPH0317232B2 JP H0317232 B2 JPH0317232 B2 JP H0317232B2 JP 13125083 A JP13125083 A JP 13125083A JP 13125083 A JP13125083 A JP 13125083A JP H0317232 B2 JPH0317232 B2 JP H0317232B2
Authority
JP
Japan
Prior art keywords
gas
flow
discharge tube
laser
medium gas
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 - Lifetime
Application number
JP13125083A
Other languages
Japanese (ja)
Other versions
JPS6022387A (en
Inventor
Yasuyuki Morita
Reiji Sano
Hidemi Takahashi
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.)
Panasonic Holdings Corp
Original Assignee
Matsushita Electric Industrial Co Ltd
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 Matsushita Electric Industrial Co Ltd filed Critical Matsushita Electric Industrial Co Ltd
Priority to JP58131250A priority Critical patent/JPS6022387A/en
Publication of JPS6022387A publication Critical patent/JPS6022387A/en
Publication of JPH0317232B2 publication Critical patent/JPH0317232B2/ja
Granted 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)

Description

【発明の詳細な説明】 産業上の利用分野 本発明は高出力のレーザ発振器に関するもので
ある。
DETAILED DESCRIPTION OF THE INVENTION Field of Industrial Application The present invention relates to a high-power laser oscillator.

従来例の構成とその問題点 高出力のレーザ発振器として高速軸流型レーザ
発振器が知られている。
Conventional configuration and its problems A high-speed axial flow laser oscillator is known as a high-output laser oscillator.

第1図は高速軸流型レーザ発振器の一般的な構
成を示すものである。1が放電管、2,4が熱交
換器、3がガス循環ポンプである。7は媒質ガス
導入部、5は配管、6はガス流方向、矢印8はレ
ーザ光線である。
FIG. 1 shows the general configuration of a high-speed axial flow laser oscillator. 1 is a discharge tube, 2 and 4 are heat exchangers, and 3 is a gas circulation pump. 7 is a medium gas inlet, 5 is a pipe, 6 is a gas flow direction, and arrow 8 is a laser beam.

前記構成において、レーザガスはガス循環ポン
プ3により配管5を通つて媒質ガス導入部7を介
して放電管1内に供給されるが、この媒質ガス導
入部7の構造により放電管1内の流速分布が左右
される。
In the above configuration, the laser gas is supplied into the discharge tube 1 by the gas circulation pump 3 through the pipe 5 and through the medium gas introduction section 7. is influenced by

第2図は放電管1内を流れるガスの流速分布図
で、aはガス流分布が不均一な場合、bは均一な
場合を示す。bはaと比較的して放電体積が大き
く放電が安定で投入電力も多くできるので出力も
大きい。
FIG. 2 is a flow velocity distribution diagram of gas flowing inside the discharge tube 1, where a shows a case where the gas flow distribution is non-uniform and b shows a case where the gas flow distribution is uniform. Compared to a, b has a large discharge volume, stable discharge, can input a large amount of power, and has a large output.

従つて媒質ガス導入部7の構造を工夫すること
により放電管1内の流速分布をb図の状態に近づ
けることが試みられている。
Therefore, attempts have been made to make the flow velocity distribution within the discharge tube 1 closer to the state shown in diagram b by devising the structure of the medium gas introduction section 7.

第3図から第6図迄が従来の媒質ガス導入部の
構造である。以下順を追つて説明する。
3 to 6 show the structure of a conventional medium gas introduction section. A step-by-step explanation will be given below.

第3図はオリフイス型開口部の例である。1が
放電管、70は反射鏡、71がオリフイス板であ
る。配管5を通つてきたガス流6はオリフイス板
71を通過すると乱流化が促進され流速分布が第
2図bの様にほゞ一様になつて放電管1内に流入
する。
FIG. 3 is an example of an orifice type opening. 1 is a discharge tube, 70 is a reflecting mirror, and 71 is an orifice plate. When the gas flow 6 that has passed through the pipe 5 passes through the orifice plate 71, turbulence is promoted, and the flow velocity distribution becomes substantially uniform as shown in FIG. 2b before flowing into the discharge tube 1.

第4図はドーナツ型開口部の例である。72が
開口部で放電管1の円筒の端面と媒質ガス導入部
7の内管の端面が作るドーナツ状のすき間からガ
スを噴出させることにより一様な流速分布を得て
いる。
FIG. 4 is an example of a donut-shaped opening. Reference numeral 72 denotes an opening, and a uniform flow velocity distribution is obtained by ejecting gas from a donut-shaped gap formed by the cylindrical end surface of the discharge tube 1 and the inner tube end surface of the medium gas introduction section 7.

第5図は媒質ガス導入部の内部にスリツト73
を有する場合の例である。
Figure 5 shows a slit 73 inside the medium gas introduction part.
This is an example of a case where

第6図はノズル型で、レーザガスはノズル74
から噴出され、直角に曲つて放電管1内に流入す
る場合の例である。
Figure 6 shows the nozzle type, and the laser gas is fed through the nozzle 74.
This is an example in which the liquid is ejected from the discharge tube 1, curves at a right angle, and flows into the discharge tube 1.

これら従来例ではいずれも開口部の断面積を小
さくし開口部の前後で圧力差を得ることにより局
所的に高速流を得て乱流化の促進をはかつてい
る。このため開口部のコンダクタンスが小さくな
りガス循環ポンプは圧縮比が大きく、(例えば開
口部入口が60Torr、出口、つまり放電管内が
30Torrとすれば圧縮比2である。)、かつ高圧下
で(上記例では60Torr以上)で排気能力が大き
いことが要求される。又、ポンプの型式が限定さ
れる事、大型化して消費電力も増大すること、発
熱による損出量も大きくなりポンプの冷却のため
の冷却器も大型になり装置全体の価格もこの循環
ポンプ系が大きな比重を占めていた。
In all of these conventional examples, the cross-sectional area of the opening is made small and a pressure difference is obtained before and after the opening, thereby obtaining a locally high-speed flow and promoting turbulence. For this reason, the conductance of the opening is small, and the compression ratio of the gas circulation pump is large (for example, the inlet of the opening is 60Torr, and the inside of the discharge tube is 60Torr).
If it is 30Torr, the compression ratio is 2. ), and requires a large exhaust capacity under high pressure (more than 60 Torr in the above example). In addition, the types of pumps are limited, the size of the pump increases, power consumption increases, the amount of loss due to heat generation increases, the cooler for cooling the pump becomes large, and the price of the entire device decreases. occupied a large proportion.

発明の目的 本発明は以上の様な従来の問題点を解決するた
めになされたもので放電管入口のガス噴出口のコ
ンダクタンスを大きくとりながら従来以上の乱流
化促進と流速分布の均一化をはかり出力の増大化
とポンプの小型化、低コスト化を達成することを
目的としている。
Purpose of the Invention The present invention has been made to solve the above-mentioned conventional problems, and by increasing the conductance of the gas jet port at the inlet of the discharge tube, it promotes turbulence and makes the flow velocity distribution more uniform than before. The aim is to increase scale output, downsize the pump, and reduce costs.

発明の構成 本発明は上記目的を達成するもので、レーザ管
内に媒質ガスを導入する媒質ガス導入部を備え、
レーザ管内に媒質ガスを高速で流通させる構造を
有し、前記媒質ガス導入部にガス流で回動可能な
回転翼を設け、ガスが回転翼を通過する時にガス
の流れの方向が変えられ、乱流化が促進されると
共に、ガス流に回転が加わり内壁付近の流速をよ
り増大化させ流速分部の均一化をはかり、ガス循
環ポンプの負荷を小さくするものである。
Structure of the Invention The present invention achieves the above object, and includes a medium gas introduction section for introducing medium gas into the laser tube,
The laser tube has a structure that allows medium gas to flow at high speed in the laser tube, and the medium gas introduction part is provided with rotary blades that can be rotated by the gas flow, and when the gas passes through the rotary blade, the direction of the gas flow is changed, In addition to promoting turbulence, rotation is added to the gas flow to further increase the flow velocity near the inner wall, making the flow velocity portion uniform, and reducing the load on the gas circulation pump.

実施例の説明 以下本発明の一実施例を図面を用いて説明す
る。第7図は本発明の一実施例である。1は放電
管、75が回転翼で媒質ガス導入部7の内管に回
転軸受76を介て保持されている。5は配管、6
はガス流方向、70は反射鏡である。第8図に回
転翼の一例を示す。各羽根は回転軸に対しねじり
θを有している。
DESCRIPTION OF EMBODIMENTS An embodiment of the present invention will be described below with reference to the drawings. FIG. 7 shows an embodiment of the present invention. 1 is a discharge tube, and 75 is a rotary blade which is held in the inner tube of the medium gas introduction section 7 via a rotary bearing 76. 5 is piping, 6
is the gas flow direction, and 70 is a reflecting mirror. FIG. 8 shows an example of a rotor blade. Each blade has a twist θ about the axis of rotation.

ガス流6が羽根に当ると回転翼75を回転させ
ると共にガス流自身も曲げられてレーザガス全体
としては放電管1内を螺旋運動を行ないながら進
行し、管壁付近の流速を高め均一な流速分布をつ
くる。又、羽根のエツジに当るガス及びエツジか
ら離れるガスは乱流化を一層促進することにな
る。又、開口部でのコンダクタンスの低下も発生
しない。
When the gas flow 6 hits the blades, it rotates the rotor blades 75 and the gas flow itself is also bent, so that the laser gas as a whole moves through the discharge tube 1 in a spiral motion, increasing the flow velocity near the tube wall and creating a uniform flow velocity distribution. Create. Further, the gas hitting the edge of the blade and the gas leaving the edge further promote turbulence. Further, there is no reduction in conductance at the opening.

この様に本実施例によれば、従来方式の様に開
口部を狭くして乱流化をはかる必要がなく、コン
ダクタンスを低下させずに理想的な流速分布及
び、乱流化促進を行なわせることができる。
As described above, according to this embodiment, there is no need to narrow the opening to create turbulence as in the conventional system, and it is possible to achieve an ideal flow velocity distribution and promote turbulence without reducing conductance. be able to.

回転翼入口側のガス圧を従来と同じく60Torr
とすれば放電管内ガス圧は約50Torr(従来は
30Torr)となり循環ポンプの圧縮比が1.2(従来
は2.0)と小さく、従来のポンプで余裕を持つて
運転することが出来るのでポンプからの発熱量が
著しく減少しポンプの冷却系が小型化される。
又、放電管1内ガス圧の上昇により約1.7倍の出
力を得ることができる。このことは、同じ出力を
得るためにはより小型の循環ポンプで良く大巾な
コストダウンが実現できる。
The gas pressure on the rotor inlet side is kept at 60 Torr, the same as before.
Therefore, the gas pressure inside the discharge tube is approximately 50 Torr (conventionally
30Torr), and the compression ratio of the circulation pump is as small as 1.2 (previously 2.0), allowing conventional pumps to operate with sufficient margin, resulting in a significant reduction in heat generation from the pump and downsizing of the pump cooling system. .
Furthermore, by increasing the gas pressure inside the discharge tube 1, it is possible to obtain approximately 1.7 times the output. This means that in order to obtain the same output, a smaller circulation pump is required and a significant cost reduction can be achieved.

さらに回転翼の慣性によりポンプの小さな脈流
を吸収する効果があり出力の安定性に寄与するこ
と大である。
Furthermore, the inertia of the rotor blades has the effect of absorbing small pulsating flows from the pump, which greatly contributes to output stability.

発明の効果 以上のように本発明は、媒質ガス導入部を介し
てレーザ管内に媒質ガスを流通させる構造を有
し、前記媒質ガス導入部に、ガス流によつて回動
可能な回転翼を設けたレーザ発振器を提供するも
ので、レーザ管内の媒質ガスの乱流化促進と流速
分布の均一化、出力の増大化、循環ポンプの小型
化、低コスト化を達成することができる利点を有
する。
Effects of the Invention As described above, the present invention has a structure in which a medium gas flows into a laser tube through a medium gas introduction part, and a rotor blade that can be rotated by the gas flow is provided in the medium gas introduction part. This laser oscillator has the advantages of promoting turbulence in the medium gas in the laser tube, making the flow velocity distribution uniform, increasing the output, making the circulation pump smaller, and lowering the cost. .

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

第1図は高速軸流型レーザ発振器の一般的構成
を示す概略図、第2図はレーザ管内の流速分布を
示す図で、aはガス流速分布の不均一な例、bは
ガス流速分布の均一な例を示す。第3図〜第6図
は従来の媒質ガス導入部の断面図、第7図は本発
明の一実施例における媒質ガス導入部の断面図、
第8図は本発明の一実施例に使用される回転翼の
斜視図である。 1……レーザ管、5……配管、6……ガス流、
7……媒質ガス導入部、70……反射鏡、75…
…回転翼、76……回転軸受。
Figure 1 is a schematic diagram showing the general configuration of a high-speed axial flow laser oscillator, and Figure 2 is a diagram showing the flow velocity distribution in the laser tube, where a is an example of a nonuniform gas flow velocity distribution, and b is an example of a gas flow velocity distribution. Here is a uniform example. 3 to 6 are cross-sectional views of a conventional medium gas introduction part, and FIG. 7 is a cross-sectional view of a medium gas introduction part in an embodiment of the present invention.
FIG. 8 is a perspective view of a rotor blade used in one embodiment of the present invention. 1... Laser tube, 5... Piping, 6... Gas flow,
7...Medium gas introduction part, 70...Reflector, 75...
...rotor blade, 76...rotary bearing.

Claims (1)

【特許請求の範囲】[Claims] 1 媒質ガス導入部を介してレーザ管内に媒質ガ
スを流通させるように構成され、前記媒質ガス導
入部に、ガス流によつて回動可能な回転翼を設け
たことを特徴とするレーザ発振器。
1. A laser oscillator configured to flow a medium gas into a laser tube through a medium gas introduction section, and characterized in that the medium gas introduction section is provided with rotary blades that are rotatable by the gas flow.
JP58131250A 1983-07-18 1983-07-18 Laser oscillator Granted JPS6022387A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP58131250A JPS6022387A (en) 1983-07-18 1983-07-18 Laser oscillator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58131250A JPS6022387A (en) 1983-07-18 1983-07-18 Laser oscillator

Publications (2)

Publication Number Publication Date
JPS6022387A JPS6022387A (en) 1985-02-04
JPH0317232B2 true JPH0317232B2 (en) 1991-03-07

Family

ID=15053511

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58131250A Granted JPS6022387A (en) 1983-07-18 1983-07-18 Laser oscillator

Country Status (1)

Country Link
JP (1) JPS6022387A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6031064B2 (en) 2014-05-15 2016-11-24 ファナック株式会社 Gas circulation laser oscillator

Also Published As

Publication number Publication date
JPS6022387A (en) 1985-02-04

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