JPH01292800A - Accumulation accelerator for charged particle - Google Patents
Accumulation accelerator for charged particleInfo
- Publication number
- JPH01292800A JPH01292800A JP12187788A JP12187788A JPH01292800A JP H01292800 A JPH01292800 A JP H01292800A JP 12187788 A JP12187788 A JP 12187788A JP 12187788 A JP12187788 A JP 12187788A JP H01292800 A JPH01292800 A JP H01292800A
- Authority
- JP
- Japan
- Prior art keywords
- kicker
- force
- deflector
- charged particles
- charged particle
- 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
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- Particle Accelerators (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の目的〕
(産業上の利用分野)
本発明は荷電粒子の加速リング(例えばシンクロトロン
)からの出射装置を改良した小形の荷電粒子の加速蓄積
装置に関する。DETAILED DESCRIPTION OF THE INVENTION OBJECTS OF THE INVENTION (Industrial Field of Application) The present invention relates to a compact charged particle accelerating and accumulating device that is an improved device for ejecting charged particles from an accelerating ring (for example, a synchrotron).
(従来の技術)
荷電粒子の加速蓄積装置は一般に低エネルギの荷電粒子
入射器(インジェクタとも言う)と、低エネルギの荷電
粒子を所定の高エネルギまで加速する為の加速リング(
例えばシンクロトロン)と、加速リングから取り出され
た荷電粒子を長時間蓄積する為の蓄積リング(ストレー
ジリングとも言う)から構成される。(Prior Art) Charged particle accelerating and accumulating devices generally include a low-energy charged particle injector (also called an injector) and an acceleration ring (also called an injector) for accelerating the low-energy charged particles to a predetermined high energy.
For example, it consists of a synchrotron) and an accumulation ring (also called a storage ring) for storing charged particles taken out from an acceleration ring for a long time.
第5図は一般的な荷電粒子の加速蓄積装置の構成図であ
る。第5図において入射器(1)からの低エネルギ荷電
粒子は入射用ビームダクト(2)を通り、加速リング用
インフレクタ(3)を用いて略円形の加速リング(30
)内に入射され、加速リング(30)で所定のエネルギ
まで加速された後、キッカ(4)、ディフレクタ(5)
、出射用ビームダクト(6)を用いて加速リング(30
)の外へ出射され、さらに蓄積リング用インフレクタ(
7)を介して蓄積リング(31)へ入射蓄積し、蓄積リ
ング用偏向電磁石(13)からLSI露光用の光を生成
する。FIG. 5 is a block diagram of a general charged particle accelerating and accumulating device. In Fig. 5, low-energy charged particles from the injector (1) pass through the injecting beam duct (2), and are moved through the approximately circular accelerating ring (30) using the accelerating ring inflector (3).
), and after being accelerated to a predetermined energy by the acceleration ring (30), the kicker (4) and the deflector (5)
, the acceleration ring (30
) is emitted to the outside of the storage ring inflector (
7), the light enters and accumulates in the storage ring (31), and the storage ring bending electromagnet (13) generates light for LSI exposure.
第5図において加速リング(30)とは加速リング用イ
ンフレクタ(3)、キッカ(4)、ディフレクタ(5)
、加速リング用ビームダクト(8)、加速リング用高周
波加速空洞(9)、加速リング用偏向電磁石(10)か
ら構成される装置の呼称である。In Fig. 5, the acceleration ring (30) is the acceleration ring inflector (3), kicker (4), and deflector (5).
, is the name of a device consisting of an acceleration ring beam duct (8), an acceleration ring high frequency acceleration cavity (9), and an acceleration ring bending electromagnet (10).
蓄積リング(31)は蓄積リング用インフレクタ(7)
、蓄積リング用ビームダクト(11)、蓄積リング用高
周波加速空洞(12)、LSI露光用の光を生成する発
光部を有する蓄積リング用偏向電磁石(13)から構成
される装置の呼称である。The storage ring (31) is the storage ring inflector (7)
, a storage ring beam duct (11), a storage ring high frequency acceleration cavity (12), and a storage ring bending electromagnet (13) having a light emitting section that generates light for LSI exposure.
第3図は第5図に示した荷電粒子の加速蓄積装置の従来
例の荷電粒子の出射経路を示したものである。FIG. 3 shows the emission path of charged particles in a conventional example of the charged particle accelerating and accumulating device shown in FIG.
第3図において加速された荷電粒子は本来の回転軌道(
15)からキラ力(4)で蹴り出され、さらにディフレ
クタ(5)で曲げられ、出射用ビームダクト(6)内を
通って出射軌道(16)の方向に取り出される。出射の
基本動作は加速リング(30)内を回転運動している荷
電粒子を磁場で偏向して平衡軌道から外し、加速リング
外へ取り出すことであるが、取り出す為には必要な偏向
角は数〜10数度である。In Fig. 3, the accelerated charged particles have their original rotational orbits (
15) by the killer force (4), is further bent by the deflector (5), passes through the output beam duct (6), and is taken out in the direction of the output trajectory (16). The basic operation of ejection is to deflect the charged particles rotating inside the accelerator ring (30) using a magnetic field to remove them from the equilibrium orbit and take them out of the accelerator ring. ~10 degrees.
又、粒子が取り出される為にはキラ力(4)の偏向磁場
の立上り時間は粒子が加速リング内を一周する時間より
も短い必要がある。なぜなら磁場が所定の値に達しない
内に取り出し用の磁石すなわちキラ力(4)を通過した
荷電粒子は取り出し口への軌道からずれているため、デ
ィフレクタ(5)又はビームダクト(6)に衝突して失
われてしまうためである。Furthermore, in order for the particles to be taken out, the rise time of the deflection magnetic field of the Kira force (4) needs to be shorter than the time it takes for the particles to make one revolution inside the accelerator ring. This is because the charged particles that pass through the extraction magnet, that is, the Kira force (4) before the magnetic field reaches a predetermined value, deviate from the trajectory toward the extraction port and collide with the deflector (5) or beam duct (6). This is because the data will be lost.
第4図はこれを説明するための曲線図である。FIG. 4 is a curve diagram for explaining this.
横軸はキラ力励磁開始時刻を原点にとった時間t。The horizontal axis is time t with the origin at the Kira force excitation start time.
縦軸はキラ力(4)の磁場強度Bを示す、第3図に於い
て実線のカーブはキラ力(4)の磁場強度を示し、B
wax、 B winは各々荷電粒子を取り出しの軌道
に正しく導く為に必要な磁場の範囲を示す最大値と最小
値である。したがってt工はキラ力(4)が有効に働き
始める時刻である。言いかえれば時刻0〜t1の間にキ
ラ力(4)を通過した荷電粒子は出射用ビームダクト(
6)と衝突して失われてしまう。The vertical axis shows the magnetic field strength B of the Kira force (4). In Fig. 3, the solid curve shows the magnetic field strength B of the Kira force (4).
wax and B win are the maximum and minimum values, respectively, indicating the range of the magnetic field required to correctly guide the charged particles to the extraction trajectory. Therefore, the time t is the time when the Kira force (4) starts to work effectively. In other words, the charged particles that have passed through the Kira force (4) between time 0 and t1 are sent to the exit beam duct (
6) and is lost due to collision.
荷電粒子が加速リングを一周する時間をTとすると、出
射効率ηは
η=(T−t、)/T=1−t□/T
となる。つまり速い立上りを持つキラ力(4)を用いれ
ば高い効率で荷電粒子を取り出すことができるが、立上
り時間がTよりも長い場合は効率ηは零となり全く荷電
粒子を取り出せないことになる。When the time for a charged particle to go around the acceleration ring is T, the output efficiency η is η=(T-t,)/T=1-t□/T. In other words, charged particles can be extracted with high efficiency by using the Kira force (4) with a fast rise, but if the rise time is longer than T, the efficiency η becomes zero and no charged particles can be extracted.
一般に電子用の加速リングでは、リング局長は数10〜
数100程度であるから
T=数10〜数100m/C
C=3X10”m/Sとすると、T=数〜数10nse
cである。この速い立上り時間と数〜10数度の偏向角
を実現させるキラ力(4)の製作は技術的に極めて困難
である。そこで通常は第3図に示すように荷電粒子を微
小角(数〜10数mrad)偏向するキラ力(4)によ
り、荷電粒子を通常の回転軌道からずらし、通常の回転
軌道の外に設けられたディフレクタ(5)に入射する。In general, in an electron acceleration ring, the number of ring directors is several tens or more.
Since it is about several 100, T=several 10 to several 100 m/C If C=3X10"m/S, T=several to several 10 nanoseconds
It is c. It is technically extremely difficult to manufacture the Kira force (4) that achieves this fast rise time and deflection angle of several to ten degrees. Therefore, normally, as shown in Figure 3, a chira force (4) that deflects charged particles by a minute angle (several to tens of mrad) is used to shift the charged particles from their normal rotational orbits, and to set them outside the normal rotational orbits. incident on the deflector (5).
そして、ディフレクタ(5)は荷電粒子の通常の回転軌
道の外に設けるので、キラ力(4)が動作する以前から
ゆっくり立上げればよいので荷電粒子を大きく曲げるの
に必要十分な磁場を発生させることができた。このよう
に通常はキラ力(4)とディフレクタ(5)の組み合わ
せにより、立上り数10nsac、偏向角10数度の出
射装置を実現している。Since the deflector (5) is installed outside the normal rotational orbit of the charged particles, it is only necessary to slowly start up the deflector (5) before the Kira force (4) operates, thereby generating a magnetic field necessary and sufficient to bend the charged particles significantly. I was able to do that. In this way, the combination of the Kira force (4) and the deflector (5) usually realizes an emission device with a rise number of 10 nsac and a deflection angle of 10 degrees.
(発明が解決しようとする課題)
しかし最近、超LSI露光用光源として注目を浴びてい
る小形S OR(Synchrotron 0rbit
alRadiation)装置では、リング局長が、l
O数mであるので、キラ力(4)の立上りが数10ns
acでは荷電粒子はほとんど出射出来ない、即ち、例え
ばリング周長L=15mの場合
T = L/C=15m/ 3 XlO”m/5=5
0nsecであるから、キラ力の立上り時間は50ns
ecより十分短く、立上りを速くしなければならない。(Problem to be solved by the invention) However, recently, small SOR (Synchrotron 0rbit) has been attracting attention as a light source for VLSI exposure.
alRadiation) equipment, the ring director
Since it is several meters, the rise of the Kira force (4) is several tens of ns.
In AC, almost no charged particles can be emitted.For example, when the ring circumference L=15m, T=L/C=15m/3XlO"m/5=5
Since it is 0nsec, the rise time of Kira force is 50ns
It must be sufficiently shorter than ec and have a faster rise.
本発明の目的は、キラ力によって出射される荷電粒子の
立上り時間を充分短く、即ち立上りを速くした荷電粒子
出射装置を備えた荷電粒子の加速蓄積装置を提供するこ
とにある。SUMMARY OF THE INVENTION An object of the present invention is to provide an accelerating and accumulating device for charged particles that includes a charged particle emitting device in which the rise time of charged particles emitted by a chira force is sufficiently short, that is, the rise is fast.
(課題を解決するための手段)
上記目的を達成するために5本発明においては、キラ力
とディフレクタとの間に予め励磁されておリキッカと逆
特性に減磁される補助キラ力を設ける。(Means for Solving the Problems) In order to achieve the above object, in the present invention, an auxiliary killer force is provided between the killer force and the deflector, which is previously excited and demagnetized to have a characteristic opposite to that of the rikicker.
(作 用)
このようにすると、従来の構成ではビームダクト外に衝
突して失われていた荷電粒子を速い立上り時間で有効に
出射することができる。(Function) In this way, charged particles that collided with and were lost outside the beam duct in the conventional configuration can be effectively emitted with a fast rise time.
(実施例)
以下、本発明の一実施例について、第1図を参照して説
明する。(Example) An example of the present invention will be described below with reference to FIG.
この実施例においては、キラ力(4)とディフレクタ(
5)との間に予め励磁されており、キラ力(4)に対し
て逆特性に減磁される補助キラ力(18)を設ける。他
は第5図のディフレクタ(5)の位置を加速リング(3
0)の回転軌道(15)より外側へ移して改良した従来
例の第3図と同様である。従って上記要部を改良した以
外は第5図に示した一般的なものと同様である。In this example, the kill force (4) and the deflector (
An auxiliary killer force (18) is provided between the magnet and the killer force (18), which is previously excited and is demagnetized with a characteristic opposite to that of the killer force (4). Other than that, change the position of the deflector (5) in Figure 5 to the acceleration ring (3).
This is similar to the conventional example shown in FIG. 3, which is improved by moving the rotary orbit (15) to the outside of the rotary orbit (15) of 0). Therefore, it is the same as the general one shown in FIG. 5 except that the above-mentioned main parts have been improved.
次にこの実施例の動作原理について第2図(a)、(b
)、 (C)を参照して説明する。Next, the operating principle of this embodiment is explained in Figs. 2(a) and (b).
) and (C).
第2図(a)はキラ力(4)とディフレクタ(5)のみ
の場合を示し、第2図(b)は補助キラ力(18)のみ
の場合を示し、第2図(c)は前記(a)、(b)を合
成した動作原理を示すタイムチャートである。第2図(
a)はキラ力(4)とディフレクタ(5)のみであるか
ら、荷電粒子の取り出し効率はキラ力(4)の立上り時
間t2で決まる。Fig. 2(a) shows the case with only the Kira force (4) and the deflector (5), Fig. 2(b) shows the case with only the auxiliary Kira force (18), and Fig. 2(c) shows the case with the It is a time chart which shows the principle of operation which combined (a) and (b). Figure 2 (
Since a) includes only the killer force (4) and the deflector (5), the charged particle extraction efficiency is determined by the rise time t2 of the killer force (4).
一例として数値を当てはめてみる。リング周長L =1
5m、キッカ立上り時間t 、 = 40nsecの場
合、荷電粒子の取り出し効率はη=l−t、/T=1−
40ns150nsac= 1−0.8=0.2つまり
80%のビームはビームダクトに衝突して失われてしま
い、20%のビームのみ取り出せることになる。Let's use numerical values as an example. Ring circumference L = 1
5 m, kicker rise time t = 40 nsec, the extraction efficiency of charged particles is η = l-t, /T = 1-
40ns150nsac=1-0.8=0.2 That is, 80% of the beam collides with the beam duct and is lost, and only 20% of the beam can be extracted.
そこで第1図に示す本発明の如く補助キラ力(18)を
キラ力(4)とディフレクタ(5)の間に設け。Therefore, as in the present invention shown in FIG. 1, an auxiliary squirting force (18) is provided between the squirting force (4) and the deflector (5).
補助キラ力(18)を予め破線で示すように励磁してお
き、キラ力(4)の励磁特性と逆に補助キラ力(18)
を減磁する。そうすることにより、従来システムではほ
とんどすべて死んでいた時間0〜t2間の荷電粒子もデ
ィフレクタ(5)に導くことが出来る。The auxiliary killer force (18) is excited in advance as shown by the broken line, and the auxiliary killer force (18) is opposite to the excitation characteristic of the killer force (4).
demagnetize. By doing so, charged particles between time 0 and t2, which were almost all dead in the conventional system, can also be guided to the deflector (5).
従って出射効率はほぼ100%になる。Therefore, the output efficiency is approximately 100%.
以上説明したように本発明によれば、従来システムのキ
ラ力とディフレクタの間に予め励磁された補助キラ力を
設はキラ力と逆特性に減磁することにより、従来システ
ムでは取り出すことが出来なかったキラ力の立上り時間
0−1.間の荷電粒子も取り出すことが出来、小形で極
めて出射効率の良い出射装置を有する荷電粒子の加速蓄
積装置が得られる。As explained above, according to the present invention, the auxiliary kill force that is previously excited between the kill force of the conventional system and the deflector is demagnetized to have a characteristic opposite to that of the kill force, which cannot be extracted with the conventional system. The rise time of the Kira force was 0-1. Charged particles in between can also be taken out, and a charged particle accelerating and accumulating device having a small emission device with extremely high emission efficiency can be obtained.
第1図は本発明の一実施例の要部を示す原理説明図、第
2図(a)、 (b)、(e)は第1図のキラ力と補助
キラ力とディフレクタの時間に対する磁場強度の変化を
示す曲線図、第3図は第5図の従来例のディフレクタの
位置を改良した要部を示す原理説明図、第4図は第3図
の従来例の時間に対する磁場強度の変化を示す曲線図、
第5図は一般的な荷電粒子の加速蓄積装置を示す部品配
置図である。
30・・・加速リング 31・・・蓄積リン
グ4・・・キラ力 5・・・ディフレ
クタ6・・・出射用ビームダクト 18・・・補助キ
ッ力代理人 弁理士 大 胡 典 夫
第 3 図
B
Oそ/ 7時1Fig. 1 is a principle explanatory diagram showing the main part of an embodiment of the present invention, and Fig. 2 (a), (b), and (e) show the magnetic field of the magnetic field versus time of the magnetic force, auxiliary force, and deflector shown in Fig. 1. A curve diagram showing the change in strength. Figure 3 is a principle explanatory diagram showing the main part of the conventional example shown in Figure 5 with an improved position of the deflector. Figure 4 is a diagram showing the change in magnetic field strength with respect to time in the conventional example shown in Figure 3. A curve diagram showing
FIG. 5 is a component layout diagram showing a general charged particle accelerating and accumulating device. 30...Acceleration ring 31...Storage ring 4...Kira force 5...Deflector 6...Output beam duct 18...Auxiliary kick force agent Patent attorney Norio Ogo 3rd figure B Oso/ 7:01
Claims (1)
速リングと、加速リングからキッカとディフレクタと出
射用ビームダクトとを介して出射された荷電粒子を受入
れて蓄積し超LSI露光用の光を生成する発光部を有す
る蓄積リングとを備えた荷電粒子の加速蓄積装置におい
て、キッカとディフレクタとの間に、予め励磁されてお
りキッカと逆特性に減磁される補助キッカを設けたこと
を特徴とする荷電粒子の加速蓄積装置。An acceleration ring that accelerates low-energy charged particles to a predetermined high energy, and receives and accumulates the charged particles emitted from the acceleration ring via a kicker, a deflector, and an output beam duct to generate light for VLSI exposure. A device for accelerating and accumulating charged particles comprising a storage ring having a light-emitting portion, characterized in that an auxiliary kicker is provided between the kicker and the deflector, and is previously excited and demagnetized to have opposite characteristics to the kicker. Accelerating and accumulating charged particles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12187788A JPH01292800A (en) | 1988-05-20 | 1988-05-20 | Accumulation accelerator for charged particle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12187788A JPH01292800A (en) | 1988-05-20 | 1988-05-20 | Accumulation accelerator for charged particle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01292800A true JPH01292800A (en) | 1989-11-27 |
Family
ID=14822135
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12187788A Pending JPH01292800A (en) | 1988-05-20 | 1988-05-20 | Accumulation accelerator for charged particle |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01292800A (en) |
-
1988
- 1988-05-20 JP JP12187788A patent/JPH01292800A/en active Pending
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