JPS60236499A - Accelerating tube for linear accelerator - Google Patents

Accelerating tube for linear accelerator

Info

Publication number
JPS60236499A
JPS60236499A JP9108084A JP9108084A JPS60236499A JP S60236499 A JPS60236499 A JP S60236499A JP 9108084 A JP9108084 A JP 9108084A JP 9108084 A JP9108084 A JP 9108084A JP S60236499 A JPS60236499 A JP S60236499A
Authority
JP
Japan
Prior art keywords
tube
exhaust
accelerator
linear accelerator
acceleration
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.)
Granted
Application number
JP9108084A
Other languages
Japanese (ja)
Other versions
JPH0470760B2 (en
Inventor
高木 望
岡本 耕輔
菊池 理一
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.)
Ulvac Inc
Original Assignee
Ulvac Inc
Nihon Shinku Gijutsu KK
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 Ulvac Inc, Nihon Shinku Gijutsu KK filed Critical Ulvac Inc
Priority to JP9108084A priority Critical patent/JPS60236499A/en
Publication of JPS60236499A publication Critical patent/JPS60236499A/en
Publication of JPH0470760B2 publication Critical patent/JPH0470760B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Particle Accelerators (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 本発明は線型加速器用加速管に関する。[Detailed description of the invention] The present invention relates to an acceleration tube for a linear accelerator.

荷電粒子をマイクロ波で形成した電界に二り加速する線
型加速器は、超高真空下で運転しなければならない。
Linear accelerators, which accelerate charged particles through electric fields created by microwaves, must operate under ultrahigh vacuum conditions.

しかしながら、前記加速管は荷電粒子を加速するために
その管内に互に連通する軸方向に沿つた多数個の空洞共
振器により形成されており、しかも長いので、その両端
から真空ポンプで排気した場合へ加速管内壁からの放出
ガスによる管の中央部の圧力は両端部のように低くなら
ず、また管壁かも急激なガス放出があった場合、管内の
圧力が低下するのに要する時間が長い。
However, since the accelerator tube is formed of a large number of cavity resonators along the axial direction that communicate with each other in the tube in order to accelerate charged particles, and is long, it is necessary to exhaust the gas from both ends with a vacuum pump. The pressure in the center of the tube due to gas released from the inner wall of the accelerating tube is not as low as at both ends, and if there is a sudden release of gas from the tube wall, it takes a long time for the pressure inside the tube to decrease. .

本発明は加速管内壁からの放出ガスに基づく加速管内の
圧力がビーム加速運転できる値まで低下するのに要する
時間を短かくシ、″また運転時の加速管内圧力を低くす
ることをその目的としたもので、多数個の直列につなが
る空洞共振器から成る長尺の加速管内をその端部から真
空ボンデで排気し、超高真空下の該加速管内で荷電粒子
をマイクロ波で形成した電界にエリ加速する線型加速器
において、各空洞共振器の管壁に縦横比の大きい軸方向
に長尺の排気孔を複数個軸対称に設け、該排気孔を通し
て該加速管を抱く排気管による排気を付加したことを特
徴とする。
The purpose of the present invention is to shorten the time required for the pressure inside the acceleration tube, which is based on the gas released from the inner wall of the acceleration tube, to drop to a value that allows beam acceleration operation, and to lower the pressure inside the acceleration tube during operation. A long acceleration tube consisting of a large number of cavity resonators connected in series is evacuated from its end using a vacuum bonder, and charged particles are exposed to an electric field generated by microwaves inside the acceleration tube under ultra-high vacuum. In a linear accelerator that accelerates areas, a plurality of elongated exhaust holes with a large aspect ratio are provided in the tube wall of each cavity resonator in an axially symmetrical manner, and exhaust air is added by an exhaust pipe that hugs the acceleration tube through the exhaust holes. It is characterized by what it did.

以下本発明の実施例を図面につき説明する。Embodiments of the present invention will be described below with reference to the drawings.

図面において、(1)は長尺の加速管で、該加速管(1
)は内壁に軸方向に沿って所定間隔毎に中心に一孔(2
)を有する隔壁板(3)が一体に形成されて複数個の空
洞(4)が形成され、適宜個所から導入されたマイクロ
波に対し各空洞(4)を共振器として作用させて荷電粒
子を加速するようにしたものである。(51は加速管(
1)の管壁に軸方向に長尺の排気孔で、該排気孔(5)
は例えば4個を軸対称に設けた。(6)は該排気孔(5
)に連なり適所から図示しない真空ポンプで排気される
排気管である。
In the drawing, (1) is a long acceleration tube;
) has one hole (2
) is integrally formed with a plurality of cavities (4), and each cavity (4) acts as a resonator for microwaves introduced from appropriate locations to emit charged particles. It is designed to accelerate. (51 is the acceleration tube (
1) is an axially long exhaust hole in the pipe wall, and the exhaust hole (5)
For example, four are provided axially symmetrically. (6) is the exhaust hole (5
) is an exhaust pipe that is evacuated from a suitable location by a vacuum pump (not shown).

前記排気孔151 rt、その管の周方向の幅を管内の
マイクロ波による軸対象電磁場に悪影響な及はさない程
度の大きさとし、管の軸方向の長さをその孔(5)の数
と関連するが、必要なガス排出性能が得られる大きさと
し、また適所から導入されたマイクロ波が外部に対して
遮断される大きさ以下とした。
The width of the exhaust hole 151 rt in the circumferential direction of the tube is set to a size that does not adversely affect the axially symmetrical electromagnetic field caused by microwaves in the tube, and the length of the tube in the axial direction is equal to the number of holes (5). On a related note, the size was chosen so that the necessary gas exhaust performance could be obtained, and the size was chosen so that microwaves introduced from a suitable location were blocked from the outside.

次にその作動について説明する。Next, its operation will be explained.

加速管(1)は、図示しない真空ボンデにより両端から
排気され、同時にその軸に沿つ・て穿設された軸方向に
長尺の排気孔(5)から排気管(6)を介して排気され
て伝るので、管内の中央部及び両端部は一様に排気され
て圧力が低下し、また何等かの原因で管壁等から急激な
ガス放出があって管内圧力が上昇しても速やかに圧力が
低下する。
The acceleration tube (1) is evacuated from both ends by a vacuum bonder (not shown), and at the same time is exhausted through an axially long exhaust hole (5) drilled along its axis via an exhaust pipe (6). As the gas is transmitted through the pipe, the center and both ends of the pipe are evacuated uniformly, resulting in a drop in pressure.Also, even if gas is suddenly released from the pipe wall for some reason and the pressure inside the pipe rises, it is quickly removed. The pressure decreases.

かくてこの管内に図示しない荷電粒子源から荷電粒子例
えば電子が入射すると、該電子は管内に一人されたマイ
クロ波で形成された軸方向の電界によって超高真空下を
軸(7)に沿って支障なく加速される。
When a charged particle, such as an electron, enters this tube from a charged particle source (not shown), the electron moves along the axis (7) under ultra-high vacuum due to the axial electric field formed by the microwave placed inside the tube. Accelerates without any problem.

前記排気孔(5)は管の周方向の長さが短いので、マイ
クロ波による軸対称電磁場に与える影響が少なく、また
管の軸方向の長さが長いので、管の周方向に電流が流れ
るのを妨げるように作用し、その結果、ビームの管軸か
らの発散の原因となりうる非軸対称電磁場が発生しにく
くなる。
Since the length of the exhaust hole (5) in the circumferential direction of the tube is short, it has little effect on the axisymmetric electromagnetic field caused by microwaves, and since the length of the exhaust hole (5) in the axial direction of the tube is long, current flows in the circumferential direction of the tube. As a result, non-axisymmetric electromagnetic fields that can cause the beam to diverge from the tube axis are less likely to occur.

したがって、軸方向に長尺の排気孔151はその周方向
の長さに等しい丸孔に比べて電子の加速性能が高い、更
にまた、該丸孔に比べて(排気孔151の軸方向の長さ
r)/(周方向の長さr/)倍の排気性能が得られる。
Therefore, the axially long exhaust hole 151 has a higher electron acceleration performance than a round hole whose circumferential length is equal to the length of the exhaust hole 151. An exhaust performance that is twice the circumferential length (r)/(circumferential length r/) can be obtained.

このように本発明によるときは、多数の空洞共振器から
なる長尺の加速管内をその端部から真空ポンプで排気し
、超高速真空下の加速管内で荷電粒子をマイクロ波で形
成した電界により加速する線型加速器において、前記各
空洞共振器の管壁に軸方向に長尺の排気孔を軸対称に設
けることにより、加速管内の中央部及び端部な一様に排
気することができ、このため加速管内壁からの放出ガス
による圧力を短時間のうちに低下させ装置の運転を始め
ることができる。また加速管内において急激なガスの放
出があった場合でも速やかに圧力を低下させることがで
きる。
As described above, according to the present invention, the inside of a long acceleration tube consisting of a large number of cavity resonators is evacuated from its end with a vacuum pump, and charged particles are generated by an electric field generated by microwaves inside the acceleration tube under an ultrahigh-speed vacuum. In a linear accelerator that accelerates, by providing elongated exhaust holes in the axial direction in the tube wall of each cavity resonator in an axially symmetrical manner, it is possible to uniformly exhaust the center and ends of the acceleration tube. Therefore, the pressure due to the gas released from the inner wall of the accelerator tube can be reduced in a short time, and the device can be started operating. Furthermore, even if there is a sudden release of gas within the accelerator tube, the pressure can be quickly reduced.

このときマイクロ波で形成される電界を悪化することが
ないため電子の加速に支障を生じない効果を有する。
At this time, since the electric field formed by the microwave is not deteriorated, there is an effect that acceleration of electrons is not hindered.

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

第1図は本発明の一実施例の要部の断面図、第2図は第
1図のA −A線断面図を示す。 (1)・・・加速管 C)・・・孔 (3)・・・隔壁板 (4)・・・空洞151・・・排
気孔 (61・・・排気管(7)・・・軸 特許出願人 日本真空技術株式会社
FIG. 1 is a sectional view of a main part of an embodiment of the present invention, and FIG. 2 is a sectional view taken along line A--A in FIG. 1. (1)... Accelerating pipe C)... Hole (3)... Partition plate (4)... Cavity 151... Exhaust hole (61... Exhaust pipe (7)... Shaft patent Applicant: Japan Vacuum Technology Co., Ltd.

Claims (1)

【特許請求の範囲】[Claims] 多数個の直列につながる空洞共振器から成る長尺の加速
管内をその端部から真空ポンプで排気し、超高真空下の
該加速管内で荷電粒子をマイクロ波で形成した電界によ
り加速する線型加速器において、各空洞共振器の管壁に
縦横比の大きい軸方向に長尺の排気孔を複数個軸対称に
設け、該排気孔を通して該加速管を抱く排気管による排
気を付加したことを特徴とする線型加速器用加速管。
A linear accelerator in which a long acceleration tube consisting of a large number of cavity resonators connected in series is evacuated from the end with a vacuum pump, and charged particles are accelerated in the tube under ultra-high vacuum by an electric field created by microwaves. A plurality of elongated exhaust holes having a large aspect ratio in the axial direction are provided in the tube wall of each cavity resonator in an axially symmetrical manner, and exhaust air is added by an exhaust pipe that embraces the accelerator tube through the exhaust holes. Accelerator tube for linear accelerator.
JP9108084A 1984-05-09 1984-05-09 Accelerating tube for linear accelerator Granted JPS60236499A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9108084A JPS60236499A (en) 1984-05-09 1984-05-09 Accelerating tube for linear accelerator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9108084A JPS60236499A (en) 1984-05-09 1984-05-09 Accelerating tube for linear accelerator

Publications (2)

Publication Number Publication Date
JPS60236499A true JPS60236499A (en) 1985-11-25
JPH0470760B2 JPH0470760B2 (en) 1992-11-11

Family

ID=14016531

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9108084A Granted JPS60236499A (en) 1984-05-09 1984-05-09 Accelerating tube for linear accelerator

Country Status (1)

Country Link
JP (1) JPS60236499A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014096202A (en) * 2012-11-07 2014-05-22 Mitsubishi Heavy Ind Ltd Acceleration tube

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014096202A (en) * 2012-11-07 2014-05-22 Mitsubishi Heavy Ind Ltd Acceleration tube
US9237641B2 (en) 2012-11-07 2016-01-12 Mitsubishi Heavy Industries, Ltd. Accelerating structure

Also Published As

Publication number Publication date
JPH0470760B2 (en) 1992-11-11

Similar Documents

Publication Publication Date Title
US5021702A (en) Electron beam apparatus including a plurality of ion pump blocks
US3936695A (en) Electron collector having means for trapping secondary electrons in a linear beam microwave tube
US2617961A (en) Electron tube for very high frequencies
JPS60236499A (en) Accelerating tube for linear accelerator
GB1065945A (en) Improvements in or relating to magnetrons
EP0502429A2 (en) Fast atom beam source
US3096457A (en) Traveling wave tube utilizing a secondary emissive cathode
US3205398A (en) Long-slot coupled wave propagating circuit
US9237641B2 (en) Accelerating structure
JPH0613822A (en) High frequency amplifier
US4027193A (en) Klystron-resonant cavity accelerator system
US4413207A (en) Multicavity klystron
CA1264375A (en) Free electron diode oscillator
JP3707932B2 (en) High frequency electron gun
US2688106A (en) Traveling wave amplifying tube with a magnetic field
US2828441A (en) Apertured vane magnetron
US3127538A (en) Packaged traveling wave electron discharge device having magnetic directing means
US3073987A (en) Electron discharge device with getter
US3169693A (en) Ion pump
US2838711A (en) Electric discharge devices
US2624867A (en) Gas discharge tube
GB2292001A (en) Electron beam tubes
US2539210A (en) Electronic tube apparatus embodying a cavity resonator
US2951174A (en) Travelling wave tubes
JPH03283400A (en) Linear accelerator