JPS63124589A - Cas laser apparatus - Google Patents

Cas laser apparatus

Info

Publication number
JPS63124589A
JPS63124589A JP27126686A JP27126686A JPS63124589A JP S63124589 A JPS63124589 A JP S63124589A JP 27126686 A JP27126686 A JP 27126686A JP 27126686 A JP27126686 A JP 27126686A JP S63124589 A JPS63124589 A JP S63124589A
Authority
JP
Japan
Prior art keywords
gas
blower
flow path
bypass
heat exchanger
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
JP27126686A
Other languages
Japanese (ja)
Inventor
Masaki Kuzumoto
昌樹 葛本
Masaaki Tanaka
正明 田中
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric 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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP27126686A priority Critical patent/JPS63124589A/en
Publication of JPS63124589A publication Critical patent/JPS63124589A/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 obtain a stable gas stream readily even in a high pressure loss region, by providing a main flow path through a discharge part, a heat exchanger and a blower as a gas flow path, and providing a bypass, through which the gas is made to flow to the blower from a part other than the discharge part. CONSTITUTION:Small holes 10 are provided in a duct 9, which is provided in a main flow path. Thus a bypass, which is circulated through the small holes 10, a heat exchanger 5 and a blower 4 and without through a discharge part 14, is provided. The flow rate of gas, which is made to flow into the blower 4, can be increased by regulating the number of the small holes 10. Therefore, this apparatus can be used stably even in a region, in which pressure loss is larger than the surge limit of the blower 4. Thus the gas stream system is simplified, and the compact gas laser apparatus can be obtained.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明はガスレーザ装置、と(にその送風系の改良に
関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a gas laser device and an improvement in its ventilation system.

〔従来の技術〕[Conventional technology]

第4 図(a)(b) u各々例えば特開昭55−15
4190号公報に示された従来のao2レーザ装置を示
す縦断面構成図及び横断面構成図であシ図において。
Fig. 4 (a) (b) u each, for example, JP-A-55-15
4190 is a longitudinal cross-sectional configuration diagram and a cross-sectional configuration diagram showing a conventional AO2 laser device shown in Japanese Patent Publication No. 4190.

0υa2は電極、α3はこの電極に接続された電源、α
4は電極antta間に生じる放電、(2)は取シ出し
鏡、(3)に反射鏡、(4)は送風機、(5)は熱交換
器、(61は筐体。
0υa2 is the electrode, α3 is the power supply connected to this electrode, α
4 is a discharge generated between the electrodes antta, (2) is a take-out mirror, (3) is a reflector, (4) is a blower, (5) is a heat exchanger, (61 is a housing).

(7)はレーザビーム、(8)はガス流方向を示す矢印
である。
(7) is a laser beam, and (8) is an arrow indicating the gas flow direction.

次に動作について説明するつ筐体内には数十〜百数十’
rorr の圧力で002 、 He w N2等より
なるレーザガスが封入されている。iI!極αυG2間
で発生した放電α4によ9002分子が励起され2元共
振器をなす鏡+2) il+によシレーザビーム(刀と
して外に取ジ田されるつ放電安定化及び放電部のガス温
度上昇を抑えるため送風機(4)により放電部を数10
m/sの速さでレーザガスが矢印181方向に循環する
Next, I will explain the operation.
A laser gas consisting of 002, Hew N2, etc. is sealed at a pressure of 0.002 mm, Hew N2, etc. iI! 9002 molecules are excited by the discharge α4 generated between the poles αυG2, forming a binary resonator (mirror+2), and a laser beam (taken outside as a sword) stabilizes the discharge and increases the gas temperature in the discharge part. In order to suppress the electrical discharge, the blower (4) is used to
Laser gas circulates in the direction of arrow 181 at a speed of m/s.

また、放電部で昇温したガスを冷却するために熱交換器
(5)がガスの流路中に備えられている。
Further, a heat exchanger (5) is provided in the gas flow path in order to cool the gas whose temperature has risen in the discharge section.

第5図は送風機の性能を示す曲線図であり、横軸はガス
流量Q、縦軸は送風機の静圧ΔPである。
FIG. 5 is a curve diagram showing the performance of the blower, where the horizontal axis is the gas flow rate Q and the vertical axis is the static pressure ΔP of the blower.

実線月が送風機の動作特性を示し、破線111はサージ
リミット、実線にはレーザガス流体系の動作特性を示す
ウ 一般に送風機にはサージリミットがアシ、図において破
mFより左側の領域ではガスの逆流あるいは羽根の失速
等を招き使用できない領域であり。
The solid line 111 indicates the operating characteristics of the blower, the dashed line 111 indicates the surge limit, and the solid line indicates the operating characteristics of the laser gas fluid system.Usually, the blower has a surge limit. This is an area that cannot be used because it may cause the blades to stall.

破線?より右側でのみ使用可能である。ところで従来は
この右側の領域で使用するために、ガスダクトの幅を広
くとり、ガス流体の 圧力損失ΔPf小さくして第5図
点りで示される動作特性で使用されているう 〔発明が解決しようとする問題点〕 従来のガスレーザ装置は以上のように構成されているの
で、ガスのダクト幅を太き(しなければならず従って筐
体が大きなものとなる問題があったり また。流体設計上も送風機のサージリミットを考慮の上
安全率を見込んで余裕をもたせた設計をせざるを得なく
、また1ランク上の送風機を選定することもしばしばあ
った。
Broken line? Can only be used on the right side. Conventionally, in order to use this region on the right, the width of the gas duct is widened, the pressure loss ΔPf of the gas fluid is reduced, and the operating characteristics shown by the dots in Figure 5 are obtained. Since conventional gas laser devices are configured as described above, there is a problem in that the width of the gas duct must be widened, which results in a large housing. However, the design had to be designed with a margin of safety in consideration of the surge limit of the blower, and it was often necessary to select a blower that was one rank higher.

この発明は上記のような問題点を解消するためになされ
たものでサージIJ ミントの左側即ち大きな差圧ΔP
でも送風機が安定に動作し、従ってガス流体系を簡素化
してコンパクトなガスレーザ装置を得ることを目的とす
る。
This invention was made to solve the above-mentioned problems.
The purpose of this invention is to obtain a compact gas laser device in which the blower operates stably, thus simplifying the gas fluid system.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係るガスレーザ装置はガス流路として放電部
、熱交換器及び送風機を通る主流路と。
The gas laser device according to the present invention has a main flow path that passes through a discharge section, a heat exchanger, and a blower as a gas flow path.

放電部以外から送風機へガスを流すバイパス流路を設け
たものである。
A bypass flow path is provided to allow gas to flow to the blower from areas other than the discharge section.

〔作用〕[Effect]

この発明におけるガスレーザ装置は主流路に加え、バイ
パス流路を通ってレーザガスが送風機へ送られるので送
風機へ流すガス流量が増大され。
In the gas laser device of the present invention, the laser gas is sent to the blower through the bypass passage in addition to the main passage, so the gas flow rate to the blower is increased.

送風機のサージリミットよシ圧損の大きな領域でも安定
に使用できるっ 〔実施例〕 以下、この発明の実施例を図について説明する。
It can be used stably even in areas where the pressure loss is large beyond the surge limit of the blower. [Example] Hereinafter, an example of the present invention will be described with reference to the drawings.

第1図(8)(b)は各々この発明の一実施例によるガ
スレーザ装置を示す横断面構成図及び縦断面構成図であ
り9図においてi91は放電部、熱又換器(5)及び送
風機(4)を通る主流路に設けられた。送風機へのガス
吸入用ダクト、αIHこのダクト(9)に開けられた複
数個の小孔である。
FIGS. 1(8) and 1(b) are a cross-sectional configuration diagram and a longitudinal sectional configuration diagram respectively showing a gas laser device according to an embodiment of the present invention, and in FIG. (4) was provided in the main flow path passing through. The duct for gas intake to the blower, αIH, is a plurality of small holes drilled into this duct (9).

吟、ダクト(9)に小孔(tlがおいている場合と、そ
うでない場合について第2図に示す送風機の動作曲線よ
シ説明する。第2図において一点鎖線F′はサージリミ
ットを示す曲線である。゛送風機はこの線?の右側で使
用されなければならないのは前述の通りである。ところ
で曲MGe  H,工、Jはそれぞれダクト(9)に小
孔α1がない場合、小孔α1が不足の場合、小孔Hが適
量の場合、小孔α1が多すぎる場合を示している。
The operation curve of the blower shown in Fig. 2 will be explained with reference to the case where the duct (9) has a small hole (tl) and the case where it does not. In Fig. 2, the dashed line F' is the curve indicating the surge limit. As mentioned above, the blower must be used on the right side of this line. By the way, in the curves MGe H, ENG, and J, if there is no small hole α1 in the duct (9), the small hole α1 , a case where the number of small holes α1 is insufficient, a case where there is an appropriate amount of small holes H, and a case where there are too many small holes α1 are shown.

上記のそれぞれの動作点ばA、  B、  O,Dで与
えられる。ところがサージリミットの左側にあるとき(
点AtB)fl使用できないため9点0.  Dの場合
のみが使用を許される。
The operating points of each of the above are given by A, B, O, and D. However, when it is on the left side of the surge limit (
Point AtB) fl cannot be used, so 9 points and 0. Only case D is allowed.

上記結果を第3図によシ具体的に説明する、小孔t11
のない場合、ΔP1にてQl  のガス流量が流れる系
即ち主流路(8リ を考える。主流路に設けられたダク
ト9)に小孔(1Gを設けることによ汎放電部を通らず
、小孔Qlを通って熱交換器(5)、送風機(4)と循
環するバイパス流路(82)を考え、小孔!10の数を
一節することによ汎バイパス流路(82)にΔP1にて
Q2 t Q、3 e Q、4ノガス流1(fiれるよ
うになったとする。
The above results are explained in detail in Fig. 3, the small hole t11.
In the case where there is no gas flow rate of Ql at ΔP1, a small hole (1G is provided in the system in which the gas flow rate of Ql flows, that is, the main channel (8. Considering the bypass flow path (82) that circulates through the hole Ql to the heat exchanger (5) and the blower (4), by adjusting the number of small holes !10, the general bypass flow path (82) is set to ΔP1. Suppose now that Q2 t Q, 3 e Q, 4 no gas flow 1 (fi) is obtained.

送風機+41からみれば点0.Diサージリミットの右
側であるから安定なガスの流れが得られる。
Point 0 from the point of view of the blower +41. Since it is on the right side of the Di surge limit, a stable gas flow can be obtained.

この時主流路(8つ に流れるガス流fikは各々X。At this time, the gas flow fik flowing through the main channels (8) is X.

Yであシ、主流路(8リ ヘ最大限ガスが流れる点aの
場合が有効であることが解かるつつまクバイパス流路の
流量を調節し、動作特性がサージリミット上あるいは若
干右側にくるようにすれば安定に動作し、かつ主流路に
最大流量を流せることがわかるう なお、上記実施例ではダクト(9)に小孔(11をろけ
た場合について示したが、バイパス流路を構成するため
に他の配管を用いてもよい。
It turns out that point a where the maximum gas flows is effective in the case of point a where the maximum gas flows.Adjust the flow rate of the bypass flow path so that the operating characteristics are above the surge limit or slightly to the right. It can be seen that it will operate stably and allow the maximum flow rate to flow through the main flow path if Other piping may be used for this purpose.

ま九小孔の数でバイパス流路のガス流量を調整したが、
バルブ等の流量v8整装置を使用しても同様の効果を奏
する。
The gas flow rate in the bypass flow path was adjusted by the number of small holes, but
A similar effect can be obtained by using a flow rate v8 regulating device such as a valve.

また、ガスレーザ装置の構成は第1図のものの他、第4
図で示される構成のものくおいて、バイパス流路を設け
るようにしてもよいう 〔発明の効果〕 以上のように、この発明によればガス流路として放電部
、熱交換器、及び送風機を通る主流路と。
In addition to the configuration of the gas laser device shown in FIG.
In the structure shown in the figure, a bypass flow path may be provided. [Effects of the Invention] As described above, according to the present invention, the gas flow path includes a discharge section, a heat exchanger, and a blower. with the main flow path passing through.

放1部以外から送風機へガスを流すバイパス流路を設け
たので、従来使用できなかった高圧損の領域でも容易に
安定なガス流が得られ、しいてはガス流体系を簡素化し
てコンパクトなガスレーザ装置が得られる効果がある。
By providing a bypass flow path that allows gas to flow to the blower from areas other than the first section, a stable gas flow can be easily obtained even in areas with high pressure loss that could not be used in the past, and the gas flow system can be simplified to create a compact design. This has the effect of providing a gas laser device.

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

第1図(a)(1))は各々この発明の一実施例による
ガスレーザ装置を示す横断面構成図及び縦断面構成図、
第2図はこの発明の一実施例に係る送風機の動作特性を
示す特性図、第3図はこの発明の一実施例に係るガス流
路を説明する説明図、第4図(8)(b)は各々従来の
ガスレーザ装置を示す縦断面賛成図及び横断面構成図、
並びに第5図に従来の送風機の動作特性を示す特性図で
あろう +ol、 a2i’?を極、(141[放111!、 
+41t−j送風機、 151?1熱交換器、(7)は
レーザビーム、(8)はガス流方向、(9)はダク)、
(IIは孔、(8リ は主流路e  (82)  はバ
イパス流路 なお9図中、同一符号に同−又は相当部分を示すつ
FIG. 1(a)(1)) is a cross-sectional configuration diagram and a vertical cross-sectional configuration diagram showing a gas laser device according to an embodiment of the present invention, respectively;
FIG. 2 is a characteristic diagram showing the operating characteristics of a blower according to an embodiment of the present invention, FIG. 3 is an explanatory diagram illustrating a gas flow path according to an embodiment of the present invention, and FIG. ) are a vertical cross-sectional view and a cross-sectional configuration diagram showing a conventional gas laser device, respectively.
Also, Fig. 5 is a characteristic diagram showing the operating characteristics of a conventional blower. +ol, a2i'? The pole, (141 [release 111!,
+41t-j blower, 151?1 heat exchanger, (7) is laser beam, (8) is gas flow direction, (9) is duct),
(II is the hole, (8) is the main flow channel e (82) is the bypass flow channel. In Figure 9, the same reference numerals indicate the same or equivalent parts.

Claims (4)

【特許請求の範囲】[Claims] (1)放電部、この放電部にレーザガスを循環する送風
機、上記レーザガスを冷却する熱交換器、上記放電部、
熱交換器及び送風機を経由して上記レーザガスが流れる
主流路、並びに上記放電部以外を経由し、上記送風機へ
流すガス流量を増大させるバイパス流路を備えたガスレ
ーザ装置。
(1) a discharge section, a blower that circulates the laser gas in the discharge section, a heat exchanger that cools the laser gas, the discharge section,
A gas laser device comprising a main flow path through which the laser gas flows via a heat exchanger and a blower, and a bypass flow path that increases the flow rate of gas flowing to the blower through a region other than the discharge section.
(2)バイパス流路を流れるガス流量が調節可能な特許
請求の範囲第1項記載のガスレーザ装置。
(2) The gas laser device according to claim 1, wherein the gas flow rate flowing through the bypass channel is adjustable.
(3)主流路に設けられた、送風機へのガス吸入用ダク
ト部に、複数個の孔をあけてバイパス流路を構成した特
許請求の範囲第1項又は第2項記載のガスレーザ装置。
(3) The gas laser device according to claim 1 or 2, wherein a plurality of holes are formed in a duct portion for sucking gas into the blower provided in the main flow path to constitute a bypass flow path.
(4)孔の数を調節してバイパス流路を流れるガス流量
を調節した特許請求の範囲第3項記載のガスレーザ装置
(4) The gas laser device according to claim 3, wherein the number of holes is adjusted to adjust the flow rate of gas flowing through the bypass channel.
JP27126686A 1986-11-14 1986-11-14 Cas laser apparatus Pending JPS63124589A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP27126686A JPS63124589A (en) 1986-11-14 1986-11-14 Cas laser apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP27126686A JPS63124589A (en) 1986-11-14 1986-11-14 Cas laser apparatus

Publications (1)

Publication Number Publication Date
JPS63124589A true JPS63124589A (en) 1988-05-28

Family

ID=17497685

Family Applications (1)

Application Number Title Priority Date Filing Date
JP27126686A Pending JPS63124589A (en) 1986-11-14 1986-11-14 Cas laser apparatus

Country Status (1)

Country Link
JP (1) JPS63124589A (en)

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