JPH08250298A - Input coupler for superconductor accelerating cavity system - Google Patents
Input coupler for superconductor accelerating cavity systemInfo
- Publication number
- JPH08250298A JPH08250298A JP5081295A JP5081295A JPH08250298A JP H08250298 A JPH08250298 A JP H08250298A JP 5081295 A JP5081295 A JP 5081295A JP 5081295 A JP5081295 A JP 5081295A JP H08250298 A JPH08250298 A JP H08250298A
- Authority
- JP
- Japan
- Prior art keywords
- rectangular
- hollow
- superconducting
- flange
- circular
- 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.)
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Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、超伝導加速空洞システ
ムのインプットカプラに関し、特に超伝導加速空洞の真
空度を保つためシール性能を高くする場合等に適用して
有用なものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an input coupler for a superconducting accelerating cavity system, and is particularly useful when applied to the case where the sealing performance is improved to maintain the vacuum degree of the superconducting accelerating cavity.
【0002】[0002]
【従来の技術】図3は、超伝導加速空洞システムの一例
を示す説明図である。同図に示す超伝導加速空洞システ
ムは、導波管12、インプットカプラ11、ヘリウム液
化装置20、高周波発生器13、真空槽18、液体ヘリ
ウム槽16、窒素シールド板17、パイプ15a,15
b,19a,19b及び超伝導加速空洞14を有する。2. Description of the Related Art FIG. 3 is an explanatory view showing an example of a superconducting accelerated cavity system. The superconducting accelerating cavity system shown in the figure includes a waveguide 12, an input coupler 11, a helium liquefier 20, a high frequency generator 13, a vacuum tank 18, a liquid helium tank 16, a nitrogen shield plate 17, and pipes 15a, 15.
b, 19a, 19b and the superconducting acceleration cavity 14.
【0003】これらのうち超伝導加速空洞14は、左右
両端が開口した中空の部材であって、液体ヘリウム21
で満された液体ヘリウム槽16の内部に設けられてい
る。また液体ヘリウム槽16は、窒素シールド板17の
内部に設けられている。更に窒素シールド板17は、真
空槽18の内部に設けられている。Of these, the superconducting accelerating cavity 14 is a hollow member whose left and right ends are open.
It is provided inside the liquid helium tank 16 filled with. The liquid helium tank 16 is provided inside the nitrogen shield plate 17. Further, the nitrogen shield plate 17 is provided inside the vacuum chamber 18.
【0004】パイプ15a,15bは、その一端が超伝
導加速空洞14の左右両端の各々に接続されるとともに
液体ヘリウム槽16、窒素シールド板17及び真空槽1
8を貫通し、その他端が真空槽18の外部に各々通じて
いる。ヘリウム液化装置20は、ヘリウムを液化すると
ともに、この液化された液体ヘリウム21を液体ヘリウ
ム槽16に接続されたパイプ19a,19bを通じて循
環する。One end of each of the pipes 15a and 15b is connected to each of the left and right ends of the superconducting acceleration cavity 14, and the liquid helium tank 16, the nitrogen shield plate 17 and the vacuum tank 1 are connected.
8 and the other ends thereof communicate with the outside of the vacuum chamber 18, respectively. The helium liquefying device 20 liquefies helium and circulates the liquefied liquid helium 21 through pipes 19 a and 19 b connected to the liquid helium tank 16.
【0005】インプットカプラ11は、超伝導加速空洞
14の右端部に取り付けられるとともに、その先端部が
導波管12の下端部に接続されており、導波管12によ
って伝搬される高周波を超伝導加速空洞14の内部へ導
入する。また、導波管12は、液体ヘリウム槽16、窒
素シールド板17及び真空槽18を貫通し、真空槽18
の外部にある高周波発生器13にその上端部が接続され
ている。The input coupler 11 is attached to the right end portion of the superconducting acceleration cavity 14 and has its tip end connected to the lower end portion of the waveguide 12 to superconduct the high frequency wave propagated by the waveguide 12. It is introduced inside the acceleration cavity 14. Further, the waveguide 12 penetrates the liquid helium tank 16, the nitrogen shield plate 17, and the vacuum tank 18, and
The upper end of the high frequency generator 13 is connected to the outside.
【0006】上記超伝導加速空洞システムによれば、ヘ
リウム液化装置20によって循環される液体ヘリウム2
1によって冷却された超伝導加速空洞14の内部に、パ
イプ15aを通じて荷電粒子ビーム22aが流入され、
同時に高周波発生器13で発生された高周波が、導波管
12によって伝搬された後インプットカプラ11によっ
て超伝導加速空洞14の内部に導かれる。このため荷電
粒子ビーム22aは、前記高周波に同期し、加速され
る。加速後の荷電粒子ビーム22bは、パイプ15bを
通じて真空槽18の外部に流出される。According to the superconducting accelerating cavity system described above, the liquid helium 2 circulated by the helium liquefier 20 is circulated.
The charged particle beam 22a flows into the superconducting acceleration cavity 14 cooled by 1 through the pipe 15a,
At the same time, the high frequency generated by the high frequency generator 13 is propagated by the waveguide 12 and then guided by the input coupler 11 into the superconducting acceleration cavity 14. Therefore, the charged particle beam 22a is accelerated in synchronization with the high frequency. The accelerated charged particle beam 22b flows out of the vacuum chamber 18 through the pipe 15b.
【0007】上述の如き超伝導加速空洞システムに用い
られるインプットカプラ11は、この超伝導加速空洞の
性能を左右する重要な部材であって、従来、同軸タイプ
カプラと方形導波管タイプカプラの2種類があった。図
4は、従来技術に係る方形導波管タイプカプラ及び同軸
タイプカプラを示す説明図である。The input coupler 11 used in the superconducting accelerating cavity system as described above is an important member that influences the performance of the superconducting accelerating cavity, and has conventionally been classified into a coaxial type coupler and a rectangular waveguide type coupler. There were types. FIG. 4 is an explanatory view showing a rectangular waveguide type coupler and a coaxial type coupler according to the related art.
【0008】同図(a)に示すように方形導波管タイプ
カプラ31は、直方体状で横断面が方形であり、その上
端部が開口した中空の本体31aと、前記上端部に設け
られた方形のフランジ部31bを有する。この方形導波
管タイプカプラ31によれば、高周波は、中空部31c
を伝搬し、超伝導加速空洞14内へ導かれる。As shown in FIG. 1 (a), a rectangular waveguide type coupler 31 has a rectangular parallelepiped shape and a rectangular cross section, and has a hollow main body 31a having an open upper end, and is provided at the upper end. It has a square flange portion 31b. According to this rectangular waveguide type coupler 31, a high frequency wave is generated in the hollow portion 31c.
And is guided into the superconducting acceleration cavity 14.
【0009】また同図(b)に示すように同軸タイプカ
プラ41は、横断面が同心円となるように設けられた外
導体41aと内導体41b、及びこれら外導体41aと
内導体41bとの間に設けられた誘電体41cを有す
る。この同軸タイプカプラ41によれば、高周波は、誘
電体41cを伝搬し、超伝導加速空洞14内に導かれ
る。Further, as shown in FIG. 1B, a coaxial type coupler 41 has an outer conductor 41a and an inner conductor 41b which are provided so as to have concentric cross sections, and between the outer conductor 41a and the inner conductor 41b. Has a dielectric 41c provided in. According to the coaxial type coupler 41, the high frequency propagates through the dielectric 41c and is guided into the superconducting acceleration cavity 14.
【0010】[0010]
【発明が解決しようとする課題】上述の如き従来技術に
係るインプットカプラのうち、方形導波管タイプカプラ
31は、放電が起こりにくく、該放電が起きない範囲で
本体31aの厚みa2 を小さくすることによって超伝導
加速空洞14の全長における加速寄与分14aの長さの
割合を大きくすることができ、また前記全長を短くする
ことができるためその分超伝導加速空洞システム全体を
小型化できるという利点を有するが、その反面フランジ
部31bが方形となるためシール性能が比較的悪いとい
う問題点を有する。つまり超伝導加速空洞14は、その
性能を保持し、荷電粒子ビーム22aを安定して加速す
る目的で内部を高真空(1×10-10 Torr程度)に保つ
必要がある。このため方形導波管タイプカプラ31と方
形導波管との接続に際し、通常インジウム等でできたシ
ール部材をフランジ部31bと前記方形導波管のフラン
ジ部(方形)との間に挾み、両フランジ間のシールを行
う。しかしながら方形のフランジ部31bでは、前記シ
ール部材に対して均一に荷重を加えることが困難である
ため前記シール部材のつぶれ方に片寄りが生じリークの
原因となり易い。Among the input couplers according to the prior art as described above, the rectangular waveguide type coupler 31 is less likely to cause discharge, and the thickness a 2 of the main body 31a is reduced within a range where the discharge does not occur. By doing so, it is possible to increase the ratio of the length of the acceleration contribution 14a to the total length of the superconducting acceleration cavity 14 and to shorten the total length, so that the entire superconducting acceleration cavity system can be downsized accordingly. Although it has an advantage, it has a problem that the sealing performance is relatively poor because the flange portion 31b is square. That is, the superconducting accelerating cavity 14 must be kept in a high vacuum (about 1 × 10 -10 Torr) for the purpose of maintaining its performance and accelerating the charged particle beam 22a in a stable manner. Therefore, when connecting the rectangular waveguide type coupler 31 and the rectangular waveguide, a sealing member usually made of indium or the like is sandwiched between the flange portion 31b and the flange portion (square) of the rectangular waveguide, Seal between both flanges. However, since it is difficult to apply a uniform load to the seal member at the rectangular flange portion 31b, the collapse of the seal member tends to cause deviation, which easily causes a leak.
【0011】また同軸タイプカプラ41は、外導体41
aと内導体41bの大きさを調整することによって小型
化が可能であるという利点を有するが、その反面構造が
複雑であるうえ、電界が集中し易い形状であり放電が起
こり易いという問題点を有する。Further, the coaxial type coupler 41 includes an outer conductor 41.
Although there is an advantage that the size can be reduced by adjusting the sizes of a and the inner conductor 41b, on the other hand, there is a problem that the structure is complicated and the electric field is likely to be concentrated so that discharge easily occurs. Have.
【0012】本発明は、上記従来技術に鑑み、超伝導加
速空洞の全長を短かくすることができ、しかもシール性
能が良い超伝導加速空洞システムのインプットカプラを
提供することを目的とする。In view of the above-mentioned prior art, it is an object of the present invention to provide an input coupler for a superconducting accelerating cavity system which can shorten the total length of the superconducting accelerating cavity and has good sealing performance.
【0013】[0013]
【課題を解決するための手段】上記目的を達成する本発
明の構成は、超伝導加速空洞に取り付けられるととも
に、その先端部が導波管に接続され、該導波管内を伝搬
してくる高周波を前記超伝導加速空洞の内部へ導入する
超伝導加速空洞システムのインプットカプラであって、
超伝導加速空洞に取り付けられるとともに、直方体状で
その一端が開口した中空の方形部と、円筒状のフランジ
部と、前記方形部の開口端から前記フランジ部へと続き
両者を一体的に連結する中空の連結部とを有することを
特徴とする。The structure of the present invention which achieves the above object is a high frequency wave which is attached to a superconducting accelerating cavity and whose tip is connected to a waveguide and propagates in the waveguide. An input coupler of a superconducting accelerating cavity system for introducing into the superconducting accelerating cavity,
It is attached to a superconducting accelerating cavity, and has a rectangular parallelepiped shape and a hollow rectangular portion whose one end is open, a cylindrical flange portion, and an opening end of the rectangular portion that continues to the flange portion to integrally connect the two. And a hollow connecting portion.
【0014】[0014]
【作用】上記構成の本発明によれば、インプットカプラ
のフランジ部と導波管のフランジ部とを接続する際、両
フランジ部が円形であるため該両フランジの間に挾むシ
ール部材に対して前記両フランジ部から均一の荷重が加
えられ、前記両フランジ部間がシールされる。According to the present invention having the above-mentioned structure, when the flange portion of the input coupler and the flange portion of the waveguide are connected to each other, since both the flange portions are circular, the sealing member sandwiched between the both flanges is provided. As a result, a uniform load is applied from the both flange portions to seal between the both flange portions.
【0015】[0015]
【実施例】以下に本発明の実施例を図面に基づき詳細に
説明する。なお、図3と同様の部分には同一記号を付し
て重複する説明は省略する。Embodiments of the present invention will be described below in detail with reference to the drawings. The same parts as those in FIG. 3 are designated by the same reference numerals and the duplicate description will be omitted.
【0016】図1は本発明の実施例に係る超伝導加速空
洞システムのインプットカプラを示す説明図である。同
図に示すように本実施例に係るインプットカプラ1は、
方形部1a、連結部1b、及びフランジ部1cを有す
る。FIG. 1 is an explanatory view showing an input coupler of a superconducting accelerating cavity system according to an embodiment of the present invention. As shown in the figure, the input coupler 1 according to the present embodiment is
It has a rectangular portion 1a, a connecting portion 1b, and a flange portion 1c.
【0017】これらのうち方形部1aは、図4に示す方
形導波管タイプカプラ31の本体31aと同様な形状を
有する部分、すなわち直方体状で横断面が方形であり、
その一端が開口した中空の部分であって、超伝導加速空
洞14への取り付け部である。また方形部1aの厚みa
1 は、方形導波管タイプカプラ31と同様に、放電が起
きない範囲で小さくすることができる。Of these, the rectangular portion 1a is a portion having the same shape as the main body 31a of the rectangular waveguide type coupler 31 shown in FIG. 4, that is, a rectangular parallelepiped shape and a rectangular cross section.
It is a hollow portion having one end opened, and is a mounting portion to the superconducting acceleration cavity 14. Also, the thickness a of the rectangular portion 1a
As with the rectangular waveguide type coupler 31, the value of 1 can be reduced within the range where no discharge occurs.
【0018】フランジ部1cは、円筒状であり、このた
め円形導波管との接続が可能である。図2は、円形導波
管の一例を示す説明図である。同図に示すように円形導
波管42は、円筒状の本体42aと、この本体42aの
両端部に設けられた円形のフランジ部42b,42cと
を有する。The flange portion 1c has a cylindrical shape and therefore can be connected to a circular waveguide. FIG. 2 is an explanatory diagram showing an example of a circular waveguide. As shown in the figure, the circular waveguide 42 has a cylindrical main body 42a and circular flange portions 42b and 42c provided at both ends of the main body 42a.
【0019】連結部1bは、方形部1aの開口端からフ
ランジ部1cへと続き、両者を一体的に連結する中空の
部分である。すなわち連結部1bは、方形部1a側の端
部では横断面が方形であって、フランジ部1c側の端部
では横断面が円形である。The connecting portion 1b is a hollow portion which continues from the open end of the rectangular portion 1a to the flange portion 1c and integrally connects the both. That is, the connecting portion 1b has a rectangular cross section at the end on the side of the rectangular portion 1a and a circular cross section at the end on the side of the flange portion 1c.
【0020】上記実施例によれば、インプットカプラ1
のフランジ部1cと円形導波管42のフランジ部42b
とを接続する場合、両フランジ部1c,42bが円形で
あるため両フランジ部1c,42bの間に挾むインジウ
ム等でできたシール部材に対して、両フランジ部1c,
42bから比較的容易に均一の荷重が加えられ、両フラ
ンジ部1c,42b間がシールされる。According to the above embodiment, the input coupler 1
Flange portion 1c of the circular waveguide 42 and the flange portion 42b of the circular waveguide 42
When connecting with, both flange portions 1c, 42b have a circular shape, and therefore the sealing members made of indium or the like sandwiched between the both flange portions 1c, 42b are different from the flange portions 1c, 42b.
A uniform load is relatively easily applied from 42b to seal between the flange portions 1c and 42b.
【0021】[0021]
【発明の効果】以上実施例とともに具体的に説明したよ
うに本発明は、インプットカプラの先端に円形のフラン
ジ部を設け、円形導波管との接続を可能としたため、シ
ール性能が向上し、超伝導加速空洞の内部を高真空に保
つことができる。As described above in detail with the embodiments, the present invention provides a circular flange portion at the tip of the input coupler and enables connection with a circular waveguide, thus improving the sealing performance. A high vacuum can be maintained inside the superconducting acceleration cavity.
【0022】また、超伝導加速空洞への取り付け部であ
る方形部は、横断面が方形であるため、電界集中が少な
く放電が起こりにくい。従って前記放電が起こらない範
囲で方形部の厚みを小さくすることができるため、超伝
導加速空洞の全長における加速寄与分の長さの割合を大
きくすることができ、また前記全長を短くすることがで
きるためその分超伝導加速空洞システム全体を小型化で
きる。Further, since the rectangular portion, which is a portion to be attached to the superconducting accelerating cavity, has a rectangular cross section, electric field concentration is small and discharge is unlikely to occur. Therefore, since the thickness of the rectangular portion can be reduced within the range where the discharge does not occur, it is possible to increase the ratio of the length of the acceleration contribution portion to the total length of the superconducting acceleration cavity, and to shorten the total length. Therefore, the entire superconducting accelerating cavity system can be downsized accordingly.
【図1】本発明の実施例に係る超伝導加速空洞システム
のインプットカプラを示す説明図である。FIG. 1 is an explanatory view showing an input coupler of a superconducting acceleration cavity system according to an embodiment of the present invention.
【図2】円形導波管を示す説明図である。FIG. 2 is an explanatory diagram showing a circular waveguide.
【図3】超伝導加速空洞システムの一例を示す説明図で
ある。FIG. 3 is an explanatory diagram showing an example of a superconducting accelerated cavity system.
【図4】従来技術に係る超伝導加速空洞システムのイン
プットカプラを示す説明図である。FIG. 4 is an explanatory diagram showing an input coupler of a superconducting accelerating cavity system according to the related art.
1,11 インプットカプラ 1a 方形部 1b 連結部 1c フランジ部 12 導波管 14 超伝導加速空洞 42 円形導波管 42a 本体 42b,42c フランジ部 1, 11 Input coupler 1a Square part 1b Connection part 1c Flange part 12 Waveguide 14 Superconducting acceleration cavity 42 Circular waveguide 42a Main body 42b, 42c Flange part
Claims (1)
に、その先端部が導波管に接続され、該導波管内を伝搬
してくる高周波を前記超伝導加速空洞の内部へ導入する
超伝導加速空洞システムのインプットカプラであって、 超伝導加速空洞に取り付けられるとともに、直方体状で
その一端が開口した中空の方形部と、円筒状のフランジ
部と、前記方形部の開口端から前記フランジ部へと続き
両者を一体的に連結する中空の連結部とを有することを
特徴とする超伝導加速空洞システムのインプットカプ
ラ。1. A superconducting accelerating cavity which is attached to a superconducting accelerating cavity and whose tip is connected to a waveguide to introduce high frequency waves propagating in the waveguide into the superconducting accelerating cavity. An input coupler of the system, which is attached to the superconducting acceleration cavity and has a rectangular parallelepiped hollow rectangular portion with one end open, a cylindrical flange portion, and an opening end of the rectangular portion to the flange portion. An input coupler for a superconducting accelerating cavity system, which further comprises a hollow connecting portion that integrally connects the both.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP07050812A JP3073421B2 (en) | 1995-03-10 | 1995-03-10 | Input coupler of superconducting accelerating cavity system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP07050812A JP3073421B2 (en) | 1995-03-10 | 1995-03-10 | Input coupler of superconducting accelerating cavity system |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH08250298A true JPH08250298A (en) | 1996-09-27 |
JP3073421B2 JP3073421B2 (en) | 2000-08-07 |
Family
ID=12869184
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP07050812A Expired - Lifetime JP3073421B2 (en) | 1995-03-10 | 1995-03-10 | Input coupler of superconducting accelerating cavity system |
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Country | Link |
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JP (1) | JP3073421B2 (en) |
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JP6612143B2 (en) | 2016-02-05 | 2019-11-27 | 三菱重工機械システム株式会社 | Acceleration cavity input coupler and accelerator |
-
1995
- 1995-03-10 JP JP07050812A patent/JP3073421B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
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JP3073421B2 (en) | 2000-08-07 |
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