JPH07296998A - Resonance frequency adjusting tuner of high-frequency accelerating cavity - Google Patents

Resonance frequency adjusting tuner of high-frequency accelerating cavity

Info

Publication number
JPH07296998A
JPH07296998A JP8829094A JP8829094A JPH07296998A JP H07296998 A JPH07296998 A JP H07296998A JP 8829094 A JP8829094 A JP 8829094A JP 8829094 A JP8829094 A JP 8829094A JP H07296998 A JPH07296998 A JP H07296998A
Authority
JP
Japan
Prior art keywords
bellows
tuner
frequency
cavity
high frequency
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
JP8829094A
Other languages
Japanese (ja)
Inventor
Koji Inoue
浩司 井上
Kojin Furukawa
行人 古川
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.)
Kobe Steel Ltd
Original Assignee
Kobe Steel 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 Kobe Steel Ltd filed Critical Kobe Steel Ltd
Priority to JP8829094A priority Critical patent/JPH07296998A/en
Publication of JPH07296998A publication Critical patent/JPH07296998A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To provide a resonance frequency adjusting tuner for high frequency accelerating cavity for making RF contact between the tuner body and a tuning plunger without resorting to slide contacting. CONSTITUTION:Airtight bellows 5 are furnished to enable advancing and retreating a tuning plunger 3 while the vacuum condition in an accelerating cavity 10 is maintained, and at the periphery of the bellows 5, high frequency shield bellows 6 for making high frequency connections of the plunger 3 with the tuner body 2 are provided as an RF contact, which is to be installed for preventing the airtight bellows 5 from being influenced by the electromagnetic waves in the cavity 10. The high frequency shield bellows 6 are not of the conventional type with which high frequency connections are generated by slide contacting, but of a new type in which high frequency connections are maintained by a bellows construction expanding and contracting with the advancing/retreating motions of a tuning plunger 3, and therefore, it is free from generation of gas associate with slide contacting. fusion attachment of the contact, production of powder from machining, etc., and a stable and lasting effect of RF contact can be obtained.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は,高周波電力により荷電
粒子を加速する高周波加速空洞の共振周波数を調整する
ための高周波加速空洞の共振周波数調整用チューナに関
する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a resonance frequency adjusting tuner for adjusting the resonance frequency of a high frequency acceleration cavity for accelerating charged particles by high frequency power.

【0002】[0002]

【従来の技術】高周波加速空洞では使用する高周波電力
の周波数と,空洞形状によって決定される空洞共振周波
数とが一致するように設計される。しかしながら,空洞
の製作誤差,温度上昇による空洞の形状変化,ビームロ
ーディングによるリアクタンス成分の発生により,高周
波電力周波数と空洞共振周波数との間にずれが発生する
ので,これを補正する必要がある。この周波数ずれの調
整のために,加速空洞に共振周波数調整用チューナ(以
下,チューナと記載する)が設けられる。図3は上記高
周波加速空洞のビーム加速方向下流側から見た断面図
で,加速空洞31の外郭に設けられた各ポートに高周波
電力入力カプラ40,高次モードダンパ41,メクラ蓋
42,そして,上記チューナ30が取り付けられてい
る。上記チューナ30は,円筒状導体の加速空洞内への
挿入量を調整することによって,加速空洞を等価回路で
表現したときのインダクタンスを変化させて共振周波数
を調整するプランジャタイプのものが図示されている。
このチューナによる共振周波数の調整は,共振周波数変
動を検出した帰還回路の情報に基づいて自動調整され,
加速空洞の共振周波数が常に一定に保たれるよう調整さ
れる。
2. Description of the Related Art In a high frequency accelerating cavity, the frequency of the high frequency power to be used is designed to match the cavity resonance frequency determined by the shape of the cavity. However, there is a gap between the high frequency power frequency and the cavity resonance frequency due to a cavity manufacturing error, a cavity shape change due to temperature rise, and a reactance component due to beam loading, which must be corrected. In order to adjust this frequency shift, a resonance frequency adjusting tuner (hereinafter referred to as a tuner) is provided in the acceleration cavity. FIG. 3 is a cross-sectional view of the high-frequency acceleration cavity as seen from the downstream side in the beam acceleration direction. The high-frequency power input coupler 40, the high-order mode damper 41, the blind cover 42, and The tuner 30 is attached. The tuner 30 is of a plunger type that adjusts the resonance frequency by adjusting the amount of insertion of the cylindrical conductor into the acceleration cavity to change the inductance when the acceleration cavity is represented by an equivalent circuit. There is.
The resonance frequency adjustment by this tuner is automatically adjusted based on the information of the feedback circuit that detected the resonance frequency fluctuation.
The resonant frequency of the accelerating cavity is adjusted so that it always remains constant.

【0003】上記目的のために採用されるチューナ30
の従来例構成を図4に示す。図4において,高周波加速
空洞31の外郭に形成されたチューナ取付ポート32に
真空フランジ33を用いてチューナ30が装着されてい
る。チューナ30は,上記チューナ取付ポート32と同
軸に配置されるチューニングプランジャ34をチューナ
本体36に設けられた駆動手段(図示せず)によりプラ
ンジャロッド35を介して進退駆動させることにより,
加速空洞31内への挿入量を調整し,加速空洞31の共
振周波数が調整される。上記加速空洞31内は真空排気
されるので,この真空状態を保つため,チューニングプ
ランジャ34とチューナ本体36との間に伸縮構造を有
する気密ベローズ37が配設され,真空と大気との間を
遮断しつつチューニングプランジャ34の進退駆動を可
能にしている。又,チューナ30の同軸構造により加速
空洞31内の電磁波がチューナ30内に引き込まれるた
め,上記気密ベローズ37に電圧が発生する。この発生
電圧によりベローズ37にピンホール等の損傷が発生す
ることを防止するため,チューナ本体36に接続されベ
ローズ37の周囲をとり囲むように配設された複数の金
属片38のそれぞれの先端に取り付けられた接触子39
をチューニングプランジャ34に摺動接触させてチュー
ナ本体36とチューニングプランジャ34との間を高周
波接続するRFコンタクトにより,電磁波の気密ベロー
ズ37への漏れ込みを防いでいる。
Tuner 30 adopted for the above purpose
FIG. 4 shows the configuration of a conventional example of the above. In FIG. 4, the tuner 30 is mounted on the tuner mounting port 32 formed on the outer periphery of the high frequency acceleration cavity 31 by using a vacuum flange 33. The tuner 30 drives the tuning plunger 34, which is arranged coaxially with the tuner mounting port 32, forward and backward through a plunger rod 35 by a driving means (not shown) provided in the tuner main body 36.
The resonance frequency of the acceleration cavity 31 is adjusted by adjusting the amount of insertion into the acceleration cavity 31. Since the inside of the acceleration cavity 31 is evacuated to vacuum, an airtight bellows 37 having an expansion and contraction structure is provided between the tuning plunger 34 and the tuner body 36 in order to maintain this vacuum state and shuts off the vacuum from the atmosphere. While allowing the tuning plunger 34 to move forward and backward. Further, since the electromagnetic wave in the acceleration cavity 31 is drawn into the tuner 30 due to the coaxial structure of the tuner 30, a voltage is generated in the airtight bellows 37. In order to prevent the occurrence of damage such as pinholes on the bellows 37 due to this generated voltage, the tip of each of the plurality of metal pieces 38 connected to the tuner body 36 and arranged so as to surround the circumference of the bellows 37 is prevented. Mounted contact 39
The electromagnetic contact is prevented from leaking into the airtight bellows 37 by an RF contact that makes a sliding contact with the tuning plunger 34 and connects the tuner body 36 and the tuning plunger 34 at a high frequency.

【0004】[0004]

【発明が解決しようとする課題】上記従来構成におい
て,進退駆動するチューニングプランジャ34とチュー
ナ本体36との間のRFコンタクトが摺動接触によりな
されているため,以下に示すような問題点があった。 (1)摺動のための接触子39としてカーボングラファ
イトを用いた場合,高周波電流によるジュール損失によ
る発熱により発生する気体が加速空洞内に放出され,空
洞内の高真空の維持ができなくなること。 (2)又,接触子39としてベリリウム銅系の金属を用
いた場合には,接触抵抗が大きくなるため,過大な電流
が流れたとき接触部に溶着が生じてチューニングプラン
ジャの駆動動作に支障を与えること。 (3)固体同士の摺動接触による切削粉末が生じるの
で,摺動部の焼き付きや放電により共振周波数離調の原
因となりやすいこと。 本発明が目的とするところは,チューナ本体とチューニ
ングプランジャとの間のRFコンタクトを摺動接触によ
らずに行うことにより,上記のごとき従来構成による問
題点を解決することにある。
In the above-mentioned conventional structure, since the RF contact between the tuning plunger 34 and the tuner main body 36, which are driven forward and backward, is made by sliding contact, there are the following problems. . (1) When carbon graphite is used as the contact 39 for sliding, gas generated by heat generation due to Joule loss due to high-frequency current is released into the accelerating cavity, and it becomes impossible to maintain high vacuum in the cavity. (2) Further, when a beryllium copper-based metal is used as the contact 39, the contact resistance becomes large, so that welding occurs at the contact portion when an excessive current flows, which hinders the driving operation of the tuning plunger. To give. (3) Since cutting powder is generated due to sliding contact of solids with each other, seizure or discharge of sliding parts easily causes detuning of the resonance frequency. An object of the present invention is to solve the above-mentioned problems with the conventional configuration by making RF contact between the tuner body and the tuning plunger without using sliding contact.

【0005】[0005]

【課題を解決するための手段】上記目的を達成するため
に本発明が採用する手段は,高周波加速空洞の外郭部に
装着され,空洞内側に配置されたチューニングプランジ
ャと空洞外側に配置されたチューナ本体との間を気密性
が高く,且つ伸縮自在の気密ベローズで接続すると共
に,上記チューニングプランジャを上記加速空洞に対し
て進退駆動させることにより上記チューニングプランジ
ャの空洞内への挿入量を調整して,上記高周波加速空洞
の共振周波数を調整する高周波加速空洞の共振周波数調
整用チューナにおいて,上記ベローズの外周側に上記チ
ューニングプランジャとチューナ本体との間を高周波接
続するチューニングプランジャ方向に伸縮自在の高周波
シールドベローズを設けてなることを特徴とする高周波
加速空洞の共振周波数調整用チューナとして構成されて
いる。
[Means for Solving the Problems] The means adopted by the present invention in order to achieve the above object are as follows: a tuning plunger mounted inside the cavity of a high frequency accelerating cavity, a tuning plunger located inside the cavity, and a tuner located outside the cavity. The body is connected to the main body with a highly airtight and expandable airtight bellows, and the amount of insertion of the tuning plunger into the cavity is adjusted by driving the tuning plunger forward and backward with respect to the acceleration cavity. In a tuner for adjusting the resonance frequency of the high-frequency acceleration cavity for adjusting the resonance frequency of the high-frequency acceleration cavity, a high-frequency shield expandable and contractable in the direction of the tuning plunger for high-frequency connection between the tuning plunger and the tuner body on the outer peripheral side of the bellows. Resonant frequency of high-frequency accelerating cavity characterized by being provided with bellows It is configured as adjustment tuner.

【0006】[0006]

【作用】本発明によれば,加速空洞内の真空状態を保ち
つつチューニングプランジャの進退駆動を可能にするた
めの気密ベローズに,加速空洞内の電磁波の影響が及ぶ
ことを防止するために設けられるRFコンタクトとし
て,上記気密ベローズの外周側に,上記チューニングプ
ランジャとチューナ本体との間を高周波接続する高周波
シールドベローズが設けられる。該高周波シールドベロ
ーズは,従来用いられている摺動接触により高周波接続
するものでなく,チューニングプランジャの進退駆動に
伴って伸縮するベローズ構造よって高周波接続が保たれ
るので,摺動接触に伴う気体の発生,接触点の溶着,切
削粉末の発生等がなく,安定したRFコンタクトの効果
が持続する。
According to the present invention, the airtight bellows for enabling the tuning plunger to move forward and backward while maintaining the vacuum state in the acceleration cavity is provided in order to prevent the influence of the electromagnetic wave in the acceleration cavity. As an RF contact, a high-frequency shield bellows that provides a high-frequency connection between the tuning plunger and the tuner body is provided on the outer peripheral side of the airtight bellows. The high-frequency shield bellows is not conventionally used for high-frequency connection by sliding contact, but the high-frequency connection is maintained by the bellows structure that expands and contracts as the tuning plunger moves forward and backward. There is no generation, welding of contact points, generation of cutting powder, etc., and the effect of stable RF contact continues.

【0007】[0007]

【実施例】続いて,添付図面を参照して本発明を具体化
した実施例につき説明し,本発明の理解に供する。尚,
以下に示す実施例は本発明を具体化した一例であって,
本発明の技術的範囲を限定するものではない。ここに,
図1は本発明の一実施例に係る高周波加速空洞の共振周
波数調整用チューナの構成を示す断面図。図2(a)
(b)は実施例に係る高周波シールドベローズの構成例
を示す斜視図である。図1において,本実施例に係る高
周波加速空洞の共振周波数調整用チューナ(以下,チュ
ーナと略記する)1は,高周波加速空洞(以下,空洞と
略記する)10の外郭に設けられた取付用ポート11に
真空フランジ構造を用いて装着される。チューナ1は,
チューナ本体2と該チューナ本体に設けられた駆動手段
(図示せず)によって進退駆動されるチューニングプラ
ンジャ3とにより主構成されている。上記チューニング
プランジャ3の空洞10内への進退移動により空洞10
の共振周波数の調整がなされる。チューニングプランジ
ャ3の進退駆動は,チューニングプランジャ3の中心軸
線上に固定されたチューニングロッド7をチューナ本体
2に設けられた駆動手段により進退駆動することによっ
てなされる。上記構成において,チューナ1の取付ポー
ト11への装着筒部4内は,空洞10内と連通している
ので真空状態であり,一方,チューナ本体2側は大気圧
の状態にあるので,この間を気密状態に保ちつつ上記チ
ューニングプランジャ3の進退動作を行わせる必要があ
る。その気密保持手段として,気密ベローズ5がチュー
ニングプランジャ3とチューナ本体2との間に配設され
ている。
Embodiments of the present invention will now be described with reference to the accompanying drawings to provide an understanding of the present invention. still,
The following embodiment is an example embodying the present invention,
It does not limit the technical scope of the present invention. here,
FIG. 1 is a cross-sectional view showing the configuration of a resonance frequency adjusting tuner of a high frequency accelerating cavity according to an embodiment of the present invention. Figure 2 (a)
(B) is a perspective view showing an example of composition of a high frequency shield bellows concerning an example. In FIG. 1, a resonance frequency adjusting tuner (hereinafter abbreviated as a tuner) 1 of a high frequency acceleration cavity according to the present embodiment is a mounting port provided on an outer contour of a high frequency acceleration cavity (hereinafter abbreviated as a cavity) 10. 11 is mounted using a vacuum flange structure. Tuner 1
The tuner main body 2 and a tuning plunger 3 that is driven back and forth by a drive means (not shown) provided on the tuner main body are mainly configured. By moving the tuning plunger 3 back and forth into the cavity 10, the cavity 10 is moved.
The resonance frequency is adjusted. The forward / backward driving of the tuning plunger 3 is performed by forward / backward driving of the tuning rod 7 fixed on the central axis of the tuning plunger 3 by a driving means provided in the tuner body 2. In the above configuration, the inside of the mounting cylinder portion 4 of the tuner 1 to the mounting port 11 is in a vacuum state because it communicates with the inside of the cavity 10. On the other hand, since the tuner body 2 side is in an atmospheric pressure state, the space between It is necessary to move the tuning plunger 3 back and forth while maintaining the airtight state. An airtight bellows 5 is arranged between the tuning plunger 3 and the tuner body 2 as the airtight holding means.

【0008】又,上記装着筒部4は,チューニングプラ
ンジャ3を中心とする同軸構造であるため,空洞10内
に発生する電磁波が引き込まれる。この電磁波により金
属素材で形成される上記気密ベローズ5に電圧が発生
し,流れる電流の作用により気密ベローズ5にピンホー
ル等の損傷が発生することの予防措置として,気密ベロ
ーズ5の外周側に電磁波を遮断するための高周波シール
ドベローズ6が配設される。上記高周波シールドベロー
ズ6は,図2(a)(b)に示すように構成することが
できる。図示するように金属素材で円筒状に形成された
高周波シールドベローズ6は,その両端部はチューニン
グプランジャ3とチューナ本体2に固定され,進退駆動
されるチューニングプランジャ3の動作に伴って蛇腹状
に伸縮するので,チューニングプランジャ3の進退動作
を妨げることなく,気密ベローズ5への電磁波の漏れ込
みを防止する。
Further, since the mounting cylinder portion 4 has a coaxial structure centered on the tuning plunger 3, electromagnetic waves generated in the cavity 10 are drawn in. As a preventive measure against the occurrence of damage to the airtight bellows 5 such as pinholes due to the action of a flowing current, a voltage is generated in the airtight bellows 5 formed of a metal material by this electromagnetic wave, and an electromagnetic wave is applied to the outer circumference of the airtight bellows 5. A high-frequency shield bellows 6 is provided for shutting off. The high frequency shield bellows 6 can be configured as shown in FIGS. As shown in the figure, the high-frequency shield bellows 6 formed in a cylindrical shape with a metal material has its both ends fixed to the tuning plunger 3 and the tuner body 2, and expands and contracts in a bellows shape in accordance with the operation of the tuning plunger 3 driven forward and backward. Therefore, the electromagnetic wave is prevented from leaking into the airtight bellows 5 without hindering the forward / backward movement of the tuning plunger 3.

【0009】図2(a)に示す構成では,金属筒状体の
伸縮性を柔軟に保つと共に,空洞10内の真空排気時に
チューナ1内の気体の排気が効率よくなされるようにす
るための開口部8が全周に設けられている。この開口部
8の開口径は加速周波数及び主要な高次モード周波数の
遮断波長よりも小さくなるように形成されるので,高周
波電力の気密ベローズ5への透過が阻止される。図2
(b)に示す構成では,金属筒状体が金網9によって形
成されている。図示するように金網9の網組み方向を伸
縮方向に対して斜め方向にすることによって伸縮性の向
上が図られると共に,真空排気の開口面積の増加がなさ
れている。上記構成になる高周波シールドベローズ6に
よって,気密ベローズ5への電磁波の漏れ込みが防止さ
れるので,従来構成にみられたような摺動構造による接
触部分がなく,摺動接触に伴う気体の発生や溶着,ある
いは切削粉末の発生は生じない。
In the structure shown in FIG. 2 (a), the elasticity of the metal cylinder is kept flexible, and the gas in the tuner 1 is efficiently exhausted when the vacuum in the cavity 10 is exhausted. The opening 8 is provided all around. Since the opening diameter of the opening 8 is formed so as to be smaller than the cutoff wavelengths of the acceleration frequency and the main higher-order mode frequencies, the high frequency power is prevented from passing through the airtight bellows 5. Figure 2
In the configuration shown in (b), the metal tubular body is formed by the wire net 9. As shown in the drawing, the meshing direction of the wire net 9 is set to be an oblique direction with respect to the expansion / contraction direction to improve the elasticity and increase the opening area of the vacuum exhaust. Since the high-frequency shield bellows 6 having the above structure prevents the electromagnetic waves from leaking into the airtight bellows 5, there is no contact portion due to the sliding structure as in the conventional structure, and gas is generated by the sliding contact. No welding, welding, or generation of cutting powder.

【0010】[0010]

【発明の効果】以上の説明の通り本発明によれば,加速
空洞内の真空状態を保ちつつチューニングプランジャの
進退駆動を可能にするための気密ベローズに,加速空洞
内の電磁波の影響が及ぶことを防止するために設けられ
るRFコンタクトとして,上記ベローズの外周側に,上
記チューニングプランジャとチューナ本体との間を高周
波接続する高周波シールドベローズが設けられる。該高
周波シールドベローズは,従来用いられている摺動接触
により高周波接続するものでなく,チューニングプラン
ジャの進退駆動に伴って伸縮するベローズ構造によって
高周波接続が保たれるので,摺動接触に伴う気体の発
生,接触点の溶着,切削粉末の発生等がなく,安定した
RFコンタクトの効果が持続する効果を奏する。
As described above, according to the present invention, the airtight bellows for enabling the tuning plunger to move forward and backward while maintaining the vacuum state in the acceleration cavity is affected by the electromagnetic wave in the acceleration cavity. As an RF contact provided to prevent the above, a high-frequency shield bellows that provides a high-frequency connection between the tuning plunger and the tuner body is provided on the outer peripheral side of the bellows. The high frequency shield bellows is not conventionally used for high frequency connection by sliding contact, but the high frequency connection is maintained by the bellows structure which expands and contracts as the tuning plunger moves forward and backward. There is no generation, no welding of contact points, no generation of cutting powder, etc., and the effect of stable RF contact is maintained.

【図面の簡単な説明】[Brief description of drawings]

【図1】 本発明の一実施例に係る高周波加速空洞の共
振周波数調整用チューナの構成を示す断面図。
FIG. 1 is a cross-sectional view showing the configuration of a resonance frequency adjusting tuner of a high-frequency acceleration cavity according to an embodiment of the present invention.

【図2】 実施例に係る高周波シールドベローズの構成
を示す斜視図。
FIG. 2 is a perspective view showing a configuration of a high frequency shield bellows according to an embodiment.

【図3】 高周波加速空洞へのチューナの取付状態を示
す断面図。
FIG. 3 is a sectional view showing how the tuner is attached to the high-frequency acceleration cavity.

【図4】 従来例に係る共振周波数調整用チューナの構
成を示す断面図。
FIG. 4 is a sectional view showing a configuration of a resonance frequency adjusting tuner according to a conventional example.

【符号の説明】[Explanation of symbols]

1…共振周波数調整用チューナ 2…チューナ本体 3…チューニングプランジャ 5…気密ベローズ 6…高周波シールドベローズ 10…高周波加速空洞 11…取付ポート 1 ... Tuner for adjusting resonance frequency 2 ... Tuner body 3 ... Tuning plunger 5 ... Airtight bellows 6 ... High frequency shield bellows 10 ... High frequency accelerating cavity 11 ... Mounting port

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 高周波加速空洞の外郭部に装着され,空
洞内側に配置されたチューニングプランジャと空洞外側
に配置されたチューナ本体との間を気密性が高く,且つ
伸縮自在の気密ベローズで接続すると共に,上記チュー
ニングプランジャを上記加速空洞に対して進退駆動させ
ることにより上記チューニングプランジャの空洞内への
挿入量を調整して,上記高周波加速空洞の共振周波数を
調整する高周波加速空洞の共振周波数調整用チューナに
おいて,上記ベローズの外周側に,上記チューニングプ
ランジャとチューナ本体との間を高周波接続するチュー
ニングプランジャ方向に伸縮自在の高周波シールドベロ
ーズを設けてなることを特徴とする高周波加速空洞の共
振周波数調整用チューナ。
1. A high-airtight and expandable airtight bellows is connected between a tuning plunger mounted inside the outer periphery of the high-frequency acceleration cavity and arranged inside the cavity and a tuner body arranged outside the cavity. At the same time, by adjusting the amount of insertion of the tuning plunger into the cavity by driving the tuning plunger forward and backward with respect to the acceleration cavity, the resonance frequency of the high frequency acceleration cavity is adjusted. In the tuner, for adjusting the resonance frequency of a high-frequency accelerating cavity, a high-frequency shield bellows is provided on the outer peripheral side of the bellows, the high-frequency shield bellows extending and contracting in the direction of the tuning plunger for high-frequency connection between the tuning plunger and the tuner body. Tuner.
JP8829094A 1994-04-26 1994-04-26 Resonance frequency adjusting tuner of high-frequency accelerating cavity Pending JPH07296998A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8829094A JPH07296998A (en) 1994-04-26 1994-04-26 Resonance frequency adjusting tuner of high-frequency accelerating cavity

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8829094A JPH07296998A (en) 1994-04-26 1994-04-26 Resonance frequency adjusting tuner of high-frequency accelerating cavity

Publications (1)

Publication Number Publication Date
JPH07296998A true JPH07296998A (en) 1995-11-10

Family

ID=13938785

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8829094A Pending JPH07296998A (en) 1994-04-26 1994-04-26 Resonance frequency adjusting tuner of high-frequency accelerating cavity

Country Status (1)

Country Link
JP (1) JPH07296998A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012043475A1 (en) 2010-09-27 2012-04-05 大学共同利用機関法人高エネルギー加速器研究機構 Photo-cathode high-frequency electron-gun cavity apparatus
FR3036232A1 (en) * 2015-05-15 2016-11-18 Commissariat Energie Atomique ACCORDING DEVICE FOR RADIO FREQUENCY ACCELERATOR CAVITY

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012043475A1 (en) 2010-09-27 2012-04-05 大学共同利用機関法人高エネルギー加速器研究機構 Photo-cathode high-frequency electron-gun cavity apparatus
US9224571B2 (en) 2010-09-27 2015-12-29 Inter-University Research Institute Corporation Photocathode high-frequency electron-gun cavity apparatus
FR3036232A1 (en) * 2015-05-15 2016-11-18 Commissariat Energie Atomique ACCORDING DEVICE FOR RADIO FREQUENCY ACCELERATOR CAVITY
WO2016185103A1 (en) * 2015-05-15 2016-11-24 Commissariat A L'energie Atomique Et Aux Energies Alternatives Tuning device for a radio-frequency accelerating cavity

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