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JPS6366043B2 - - Google Patents
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JPS6366043B2 - - Google Patents

Info

Publication number
JPS6366043B2
JPS6366043B2 JP6537183A JP6537183A JPS6366043B2 JP S6366043 B2 JPS6366043 B2 JP S6366043B2 JP 6537183 A JP6537183 A JP 6537183A JP 6537183 A JP6537183 A JP 6537183A JP S6366043 B2 JPS6366043 B2 JP S6366043B2
Authority
JP
Japan
Prior art keywords
container
outside
liquid helium
liquid nitrogen
vacuum container
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.)
Expired
Application number
JP6537183A
Other languages
Japanese (ja)
Other versions
JPS59191308A (en
Inventor
Hisanao Ogata
Takeo Nemoto
Yoshinori Shiraku
Yasuomi Yagi
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP58065371A priority Critical patent/JPS59191308A/en
Priority to DE8484103052T priority patent/DE3471998D1/en
Priority to EP19840103052 priority patent/EP0122498B1/en
Priority to US06/593,375 priority patent/US4502296A/en
Publication of JPS59191308A publication Critical patent/JPS59191308A/en
Publication of JPS6366043B2 publication Critical patent/JPS6366043B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C13/00Details of vessels or of the filling or discharging of vessels
    • F17C13/08Mounting arrangements for vessels
    • F17C13/086Mounting arrangements for vessels for Dewar vessels or cryostats
    • F17C13/087Mounting arrangements for vessels for Dewar vessels or cryostats used for superconducting phenomena
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/08Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
    • F17C3/085Cryostats
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2201/00Vessel construction, in particular geometry, arrangement or size
    • F17C2201/01Shape
    • F17C2201/0104Shape cylindrical
    • F17C2201/0119Shape cylindrical with flat end-piece
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/03Thermal insulations
    • F17C2203/0391Thermal insulations by vacuum
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2203/00Vessel construction, in particular walls or details thereof
    • F17C2203/06Materials for walls or layers thereof; Properties or structures of walls or their materials
    • F17C2203/068Special properties of materials for vessel walls
    • F17C2203/0687Special properties of materials for vessel walls superconducting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0153Details of mounting arrangements
    • F17C2205/018Supporting feet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/014Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/016Noble gases (Ar, Kr, Xe)
    • F17C2221/017Helium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2223/00Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
    • F17C2223/01Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
    • F17C2223/0146Two-phase
    • F17C2223/0153Liquefied gas, e.g. LPG, GPL
    • F17C2223/0161Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/05Applications for industrial use
    • F17C2270/0509"Dewar" vessels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Containers, Films, And Cooling For Superconductive Devices (AREA)

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は、中空の常温空間に磁界を発生し、か
つ熱損失の小さい超電導マグネツト用クライオス
タツトに関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a cryostat for a superconducting magnet that generates a magnetic field in a hollow room temperature space and has low heat loss.

〔従来の技術〕 従来、この種のクライオスタツトは上蓋を支点
とし懸垂型で使用する縦形円筒タイプのものが多
かつた。
[Prior Art] Conventionally, this type of cryostat has often been of a vertical cylindrical type that is used in a suspended manner with the upper lid as a fulcrum.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

しかし近年は常温空間を水平に設けることが望
まれており、この場合は横形円筒タイプのクライ
オスタツトになるが、このような装置は構造が複
雑になる上、熱損失も大きいという欠点があつ
た。
However, in recent years, it has become desirable to provide a room-temperature space horizontally, and in this case a horizontal cylindrical type cryostat is used, but such equipment has the drawbacks of a complex structure and large heat loss. .

本発明の目的は、構造を単純化し、組み立てが
容易でしかも熱損失の少ない横形円筒状のクライ
オスタツトを得ることである。
SUMMARY OF THE INVENTION An object of the present invention is to provide a horizontal cylindrical cryostat that has a simple structure, is easy to assemble, and has low heat loss.

〔課題を解決するための手段〕[Means to solve the problem]

本発明の特徴は、超電導コイル1及び液体ヘリ
ウム2を内蔵する液体ヘリウム容器3、その外側
を包囲する熱しやへい板4,7、さらにその外側
を取り巻く液体窒素容器5、該容器の外側に巻か
れた多層断熱材8、及びその外側を囲み中空の常
温空間17を形成する真空容器9とを主な構成物
とするクライオスタツトにおいて、上記液体ヘリ
ウム容器3の側壁に複数個の突起物13を設け、
この各突起物13と該突起物に対応して液体窒素
容器5の側壁に設けた支持部材14との間に、多
重の低熱伝導性薄肉円筒をその端部と中央部で交
互に連結してそれらの中間部に熱しやへい板43
を取り付けた支持構造物15を設け(すなわち支
持構造物15は複数個配置し)、上記液体窒素容
器を低熱伝導性の棒状部材で上記真空容器内に支
持したことにある。尚、以上の文中( )の数字
は代表例示図面第1図の該当符号を示すが図に表
わした形状等はあくまで例示に過ぎない。
The features of the present invention include a liquid helium container 3 containing a superconducting coil 1 and liquid helium 2, heat shield plates 4 and 7 surrounding the outside of the superconducting coil 1, a liquid nitrogen container 5 surrounding the outside of the container, and a liquid nitrogen container 5 wrapped around the outside of the container. In a cryostat whose main components are a multilayer insulation material 8 and a vacuum container 9 surrounding the outside and forming a hollow normal temperature space 17, a plurality of protrusions 13 are provided on the side wall of the liquid helium container 3. established,
Between each projection 13 and a support member 14 provided on the side wall of the liquid nitrogen container 5 corresponding to the projection, multiple thin cylinders with low thermal conductivity are connected alternately at their ends and center. A heat-resistant plate 43 is placed in the middle between them.
The liquid nitrogen container is supported within the vacuum container by a rod-shaped member having low thermal conductivity. Note that the numbers in parentheses in the above text indicate the corresponding symbols in FIG. 1 of the representative illustrative drawing, but the shapes etc. shown in the drawings are merely illustrative.

〔作用〕[Effect]

上記構成にすると液体ヘリウム容器等は円筒体
の側面でのみ支持することになるから構造は簡単
であるし組立ても容易である。支持構造物は低熱
伝導性の薄肉多重円筒と熱しやへい板43の中間
冷却能により十分な荷重を伝えながらも熱の伝達
量は低く抑えることが可能となる。
With the above configuration, the liquid helium container and the like are supported only on the side surfaces of the cylindrical body, so the structure is simple and assembly is easy. The support structure can transmit sufficient load while keeping the amount of heat transferred low due to the thin multi-layered cylinders with low thermal conductivity and the intermediate cooling ability of the heat shielding plate 43.

〔実施例〕〔Example〕

以下、実施例に従つて本発明の内容を説明す
る。
Hereinafter, the content of the present invention will be explained according to Examples.

第1図は本発明の一実施例に係る水平の常温空
間部を有するクライオスタツトの部分断面図であ
り、第2図,第3図は夫々この実施例の部分断面
斜視図である。第2図は真空容器9の一端を多層
断熱材8面(液体窒素容器5の端面近傍)で切り
他端も途中で切りかつ真空容器9の側面一部を切
除して内部構造を説明するようにした図である。
また第3図は第1図の端面91をはずして多層断
熱材8の端部を除いた図である。
FIG. 1 is a partial cross-sectional view of a cryostat having a horizontal normal temperature space according to an embodiment of the present invention, and FIGS. 2 and 3 are respectively partial cross-sectional perspective views of this embodiment. In Figure 2, one end of the vacuum container 9 is cut at the multilayer insulation material 8 side (near the end surface of the liquid nitrogen container 5), the other end is also cut halfway, and a part of the side surface of the vacuum container 9 is removed to explain the internal structure. This is a diagram.
Moreover, FIG. 3 is a diagram in which the end surface 91 of FIG. 1 is removed and the end portion of the multilayer heat insulating material 8 is removed.

超電導マグネツト1は液体ヘリウム容器3内に
収納され、該液体ヘリウム容器3には該超電導マ
グネツト1を浸漬するように冷却剤である液体ヘ
リウム2を入れてある。この液体ヘリウム容器3
は円筒10と同心円に円管状に形成されており、
超電導マグネツト1は該液体ヘリウム容器3内の
内側面に沿つてリング状に配置されている。
The superconducting magnet 1 is housed in a liquid helium container 3, and liquid helium 2, which is a coolant, is placed in the liquid helium container 3 so as to immerse the superconducting magnet 1. This liquid helium container 3
is formed in a cylindrical shape concentrically with the cylinder 10,
The superconducting magnet 1 is arranged in a ring shape along the inner surface of the liquid helium container 3.

液体ヘリウム容器3の周囲は間隙をもつて第1
の熱しやへい板4が覆つており、更にその周囲を
第2の熱しやへい板7が覆つている。第2の熱し
やへい板7の外方はこれと熱的につながつた液体
窒素容器5が形成され、内部に液体窒素6を収納
している。更にその外側は多層断熱材8で巻かれ
ている。この多層断熱材は、アルミニウム又はア
ルミニウムを蒸着した高分子膜と熱の不良導体を
交互に重ねたりしたものである。9は常温の真空
容器であり、10は中空常温空間10′を形成す
る円筒である。11は液体ヘリウムや超電導マグ
ネツトへの電流を導出入するためのポート、12
は液体窒素の導出入ポートである。13は液体ヘ
リウム容器3に設けられた円柱状の突起物、14
は液体窒素容器5の側壁に設けられた中空円筒か
らなる支持部材である。突起物13は液体ヘリウ
ム容器3の両端面について夫々2〜3個設けられ
ており、夫々の突起物13に中空円筒14がかぶ
さつている。
The periphery of the liquid helium container 3 is the first one with a gap.
A heating shield plate 4 covers the heating shield, and a second heating shield plate 7 covers the surrounding area. A liquid nitrogen container 5 is formed on the outside of the second heat shielding plate 7 and is thermally connected thereto, and stores liquid nitrogen 6 therein. Further, the outside thereof is wrapped with a multilayer insulation material 8. This multilayer insulation material is made by alternately stacking aluminum or a polymer film on which aluminum is deposited and a poor thermal conductor. 9 is a vacuum container at room temperature, and 10 is a cylinder forming a hollow room temperature space 10'. 11 is a port for introducing/inputting current to liquid helium or superconducting magnet; 12
is the liquid nitrogen inlet/outlet port. 13 is a cylindrical projection provided on the liquid helium container 3; 14
is a support member made of a hollow cylinder provided on the side wall of the liquid nitrogen container 5. Two to three protrusions 13 are provided on each end surface of the liquid helium container 3, and a hollow cylinder 14 covers each protrusion 13.

中空円筒14は熱しやへい板7と熱的に連らな
り、この中空円筒14の更に周囲にも多層断熱材
8が覆つている。15は多重の薄肉円筒をその両
端と中央部で交互に連結した支持構造物で、中間
部分に第1の熱しやへい板4と熱的につながる熱
しやへい板43が挿入されている。この薄肉円筒
は炭素繊維強化樹脂あるいはガラス繊維強化樹脂
が適している。熱しやへい板43の端部は熱しや
へい板41が蓋となり、熱しやへい板7の端部は
熱しやへい板71が蓋となつている。このように
熱しやへい板は各円柱状突起13を二重に覆うよ
うに配置され、この為各熱しやへい板4,7の端
部は各突起物13に沿うように断差が付けられて
いる。更に真空容器9の両端部は蓋91で閉じら
れている。尚、真空容器9も当然にして円管10
の周囲にドーナツ様に位置するものである。中空
円筒14と真空容器9は低熱伝導性の棒16など
でつながれている。真空容器9の内部17は
10-5Torr以下の圧力になつている。
The hollow cylinder 14 is thermally connected to the heat shield plate 7, and the hollow cylinder 14 is further covered with a multilayer heat insulating material 8. Reference numeral 15 denotes a support structure in which multiple thin-walled cylinders are alternately connected at both ends and the center, and a heat shield plate 43 that is thermally connected to the first heat shield plate 4 is inserted in the middle part. Carbon fiber reinforced resin or glass fiber reinforced resin is suitable for this thin cylinder. At the end of the heat shield plate 43, the heat shield plate 41 serves as a lid, and at the end of the heat shield plate 7, the heat shield plate 71 serves as a lid. In this way, the heat shielding plates are arranged so as to double cover each cylindrical projection 13, and for this reason, the ends of each heat shield plate 4, 7 are cut along each projection 13. ing. Further, both ends of the vacuum container 9 are closed with lids 91. Incidentally, the vacuum container 9 is naturally also a circular tube 10.
It is located like a donut around the . The hollow cylinder 14 and the vacuum container 9 are connected by a rod 16 having low thermal conductivity or the like. The inside 17 of the vacuum container 9 is
The pressure is below 10 -5 Torr.

棒16と中空円筒14との関係を第4図及び第
5図の断面図で示す。5は液体ヘリウム容器や第
1の熱しやへい板を内蔵する液体窒素容器、9は
真空容器、14は液体窒素容器の側壁に設けた中
空円筒、16はこれを真空容器に支持する棒であ
る。第4図は、中空円筒14が片側壁面に2個、
全面(両端)で4個の場合、第5図は、片側壁面
に3個、全体(両端)で6個の場合である。棒1
6の配置は適宜変更してもよい。また、棒23は
棒状部材であればよく、例えば中空円筒などでも
よい。
The relationship between the rod 16 and the hollow cylinder 14 is shown in cross-sectional views in FIGS. 4 and 5. 5 is a liquid nitrogen container containing a liquid helium container and a first heating shield, 9 is a vacuum container, 14 is a hollow cylinder provided on the side wall of the liquid nitrogen container, and 16 is a rod that supports this in the vacuum container. . FIG. 4 shows two hollow cylinders 14 on one side wall,
In the case where there are four pieces on the entire surface (both ends), FIG. 5 shows the case where there are three pieces on one side wall and six pieces on the whole (both ends). stick 1
The arrangement of 6 may be changed as appropriate. Moreover, the rod 23 may be any rod-shaped member, such as a hollow cylinder.

次に組立て手順を説明すれば、先ず超電導マグ
ネツト1を円管状の液体ヘリウム容器3に組み込
む。この周囲(内外双方共)に間隙が形成される
ように二重の熱しやへい板4,7(いずれも円管
状)を配置して夫々と容器3との端部を支持構造
物15にて固定する。次いで熱しやへい板41,
71で蓋をして後多層断熱材8でこれらの周囲を
覆う。尚、ポート11,12はこの段階では取り
付けていない。こうして組み立てられた内部構造
物を真空容器9の円筒に納めて位置決めし、しか
る後棒16にて各々中空円筒14と真空容器9と
の関係を固定する。次にポート11,12を真空
容器9の上方2ケ所の穴部から挿入して溶接す
る。最後に真空容器9の両端部を蓋91にて閉
じ、併せて円筒10を挿入して組み立てを終え
る。
Next, the assembly procedure will be explained. First, the superconducting magnet 1 is assembled into a cylindrical liquid helium container 3. Double heat shielding plates 4 and 7 (both cylindrical) are arranged so that a gap is formed around this (both inside and outside), and the ends of each and the container 3 are connected to the support structure 15. Fix it. Next, the heating plate 41,
After covering with a lid 71, the multi-layer insulation material 8 covers the surroundings thereof. Note that the ports 11 and 12 are not attached at this stage. The internal structure thus assembled is housed and positioned in the cylinder of the vacuum container 9, and then the relationship between the hollow cylinder 14 and the vacuum container 9 is fixed using the rods 16. Next, the ports 11 and 12 are inserted through the two holes above the vacuum container 9 and welded. Finally, both ends of the vacuum container 9 are closed with lids 91, and the cylinder 10 is also inserted to complete the assembly.

このような構成では、液体ヘリウム容器3及び
第1の熱しやへい板4を円筒体の側面でのみ支持
するから構造が単純で組立が容易である。また、
多層断熱材8の施行が手間どるところであるが、
すでに液体窒素容器まで組み上がつているので、
その周囲に巻きつけるだけでよい。これを円筒状
の真空容器9に挿入し、両側の端面を開いた状態
で棒16を張り、両者の相対位置を決定する。最
後に端面に蓋91を当てて円筒10を挿入すれば
簡単に組み立てが終る。薄肉多重円筒を形成する
繊維強化樹脂の熱伝導率は金属に比べてもかなり
低く、薄肉多重円筒からなる支持構造物15は折
り返して伝導距離を長くとつてあり、しかも20〜
50Kの熱しやへい板4で中間冷却して、外側の温
度の高い円筒からの輻射熱を吸収するので、十分
な荷重を伝達しながらも熱の伝達量は数mW級に
抑制することができる。多層断熱材8を貫通する
ものがあると断熱性能が劣化するが、棒状部材で
あれば断面積が小さいのでその影響を最小限にと
どめることができる。
In such a configuration, the liquid helium container 3 and the first heat shielding plate 4 are supported only on the side surfaces of the cylindrical body, so the structure is simple and assembly is easy. Also,
Although the implementation of multilayer insulation material 8 is time-consuming,
The liquid nitrogen container has already been assembled, so
Just wrap it around it. This is inserted into a cylindrical vacuum container 9, the rods 16 are stretched with both end faces open, and the relative positions of the two are determined. Finally, by placing the lid 91 on the end face and inserting the cylinder 10, assembly is easily completed. The thermal conductivity of the fiber-reinforced resin forming the thin-walled multi-cylinder is considerably lower than that of metal, and the support structure 15 consisting of the thin-walled multi-cylinder is folded back to ensure a long conduction distance.
Since the 50K heating plate 4 performs intermediate cooling and absorbs the radiant heat from the high temperature cylinder on the outside, the amount of heat transferred can be suppressed to several milliwatts while transmitting sufficient load. If something penetrates the multilayer heat insulating material 8, the heat insulating performance will deteriorate, but if the rod-shaped member has a small cross-sectional area, the effect can be kept to a minimum.

第6図は本発明の別の実施例を示すもので第1
図の支持構造物15の周辺のみを示す。クライオ
スタツトを設置前に輸送する必要が生ずる。断熱
性能を確保するため、支持構造物15や棒16は
極力断面積を抑えているので強度的には必ずしも
十分な安全が見込まれていない。そこで、運搬時
には真空容器9の端面フランジをはずし、円柱状
突起物13を露出させる。円柱状突起物には例え
ばねじ穴などが開けてあり、真空容器9の端面か
ら直接に太いねじのような強度部材30で強固に
円柱状突起物13を固定する。運搬終了後、設置
時には真空容器9の端面を開き熱しやへい板41
及び42及び多層断熱材8を正規の状態に復元す
る。
FIG. 6 shows another embodiment of the present invention.
Only the periphery of the support structure 15 in the figure is shown. It becomes necessary to transport the cryostat before installation. In order to ensure heat insulation performance, the cross-sectional area of the support structure 15 and the rods 16 is suppressed as much as possible, so sufficient safety is not necessarily expected in terms of strength. Therefore, during transportation, the end flange of the vacuum container 9 is removed to expose the cylindrical protrusion 13. For example, a screw hole or the like is opened in the cylindrical projection 13, and the cylindrical projection 13 is firmly fixed directly from the end face of the vacuum container 9 with a strength member 30 such as a thick screw. After transportation, when installing, open the end face of the vacuum container 9 and insert the heat shield plate 41.
and 42 and the multilayer insulation material 8 are restored to their normal state.

このように、運搬にも十分耐えられるような支
持方法が断熱部分にわずかの手を加えるだけで可
能となる。
In this way, it is possible to create a support method that can withstand transportation with just a few changes to the insulation part.

〔発明の効果〕〔Effect of the invention〕

以上述べた如く、本発明によれば、構造が単純
で、組立が容易で、かつ熱損失の小さいクライオ
スタツトが得られる。また、支持構造物を利用し
て運搬のための支持が容易にできるなどの大きな
利点がある。
As described above, according to the present invention, a cryostat with a simple structure, easy assembly, and low heat loss can be obtained. Another great advantage is that it can be easily supported for transportation using a support structure.

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

第1図は本発明の一実施例を示す側断面図、第
2図、第3図は夫々第1図の実施例装置の部分断
面斜視図、第4図、第5図は夫々本発明の一実施
例を示す模式正横断面図、第6図は本発明の他の
実施例を示す部分側断面図である。 3……液体ヘリウム容器、4……第1の熱しや
へい板、5,20……液体窒素容器、8……多層
断熱材、9,21……真空容器、13……円柱状
突起物、14,22……中空円筒、15……支持
構造物、16,23……棒、30……強度部材。
FIG. 1 is a side sectional view showing one embodiment of the present invention, FIGS. 2 and 3 are partial sectional perspective views of the embodiment device of FIG. 1, and FIGS. 4 and 5 are respectively FIG. 6 is a schematic front cross-sectional view showing one embodiment, and FIG. 6 is a partial side sectional view showing another embodiment of the present invention. 3... Liquid helium container, 4... First heating plate, 5, 20... Liquid nitrogen container, 8... Multilayer insulation material, 9, 21... Vacuum container, 13... Cylindrical protrusion, 14, 22... Hollow cylinder, 15... Support structure, 16, 23... Rod, 30... Strength member.

Claims (1)

【特許請求の範囲】[Claims] 1 超電導コイル及び液体ヘリウムを内蔵する液
体ヘリウム容器、その外側を包囲する熱しやへい
板、さらにその外側を取り巻く液体窒素容器、該
容器の外側に巻かれた多層断熱材、及びその外側
を囲み中空の常温空間を形成する真空容器を主な
構成物とするクライオスタツトにおいて、上記液
体ヘリウム容器の側壁に複数個の突起物を設け、
該各突起物と該突起物に対応して液体窒素容器の
側壁に設けた支持部材との間に支持構造物を設
け、該各支持構造物は前記突起物と支持部材との
間において多重の低熱伝導性薄肉円筒をその端部
と中央部で交互に連結しつつ中間部に熱しやへい
板を取り付けてなり、上記液体窒素容器を低熱伝
導性の棒状部材で上記真空容器内に支持したこと
を特徴とするクライオスタツト。
1. A liquid helium container containing a superconducting coil and liquid helium, a heat shielding plate surrounding the outside, a liquid nitrogen container surrounding the outside, a multilayer insulation material wrapped around the outside of the container, and a hollow space surrounding the outside. In a cryostat whose main component is a vacuum container forming a normal temperature space, a plurality of protrusions are provided on the side wall of the liquid helium container,
A support structure is provided between each of the protrusions and a support member provided on the side wall of the liquid nitrogen container corresponding to the protrusion, and each of the support structures has multiple support structures between the protrusion and the support member. Thin cylinders with low thermal conductivity are alternately connected at their ends and central portions, and a heat shield plate is attached to the middle portion, and the liquid nitrogen container is supported within the vacuum container by a rod-shaped member with low thermal conductivity. A cryostat featuring:
JP58065371A 1983-04-15 1983-04-15 cryostat Granted JPS59191308A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP58065371A JPS59191308A (en) 1983-04-15 1983-04-15 cryostat
DE8484103052T DE3471998D1 (en) 1983-04-15 1984-03-20 Cryostat
EP19840103052 EP0122498B1 (en) 1983-04-15 1984-03-20 Cryostat
US06/593,375 US4502296A (en) 1983-04-15 1984-03-26 Cryostat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP58065371A JPS59191308A (en) 1983-04-15 1983-04-15 cryostat

Publications (2)

Publication Number Publication Date
JPS59191308A JPS59191308A (en) 1984-10-30
JPS6366043B2 true JPS6366043B2 (en) 1988-12-19

Family

ID=13285037

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58065371A Granted JPS59191308A (en) 1983-04-15 1983-04-15 cryostat

Country Status (1)

Country Link
JP (1) JPS59191308A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6043729A (en) * 1998-11-13 2000-03-28 General Electric Company Tube suspension assembly for superconductive magnets

Also Published As

Publication number Publication date
JPS59191308A (en) 1984-10-30

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