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JPS6236369B2 - - Google Patents
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JPS6236369B2 - - Google Patents

Info

Publication number
JPS6236369B2
JPS6236369B2 JP55149472A JP14947280A JPS6236369B2 JP S6236369 B2 JPS6236369 B2 JP S6236369B2 JP 55149472 A JP55149472 A JP 55149472A JP 14947280 A JP14947280 A JP 14947280A JP S6236369 B2 JPS6236369 B2 JP S6236369B2
Authority
JP
Japan
Prior art keywords
helical coil
support
coil
support structure
support ring
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
JP55149472A
Other languages
Japanese (ja)
Other versions
JPS5773906A (en
Inventor
Masakata Nishikawa
Masao Yamada
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Atomic Power Industries Inc
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 Mitsubishi Atomic Power Industries Inc filed Critical Mitsubishi Atomic Power Industries Inc
Priority to JP55149472A priority Critical patent/JPS5773906A/en
Publication of JPS5773906A publication Critical patent/JPS5773906A/en
Publication of JPS6236369B2 publication Critical patent/JPS6236369B2/ja
Granted legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F6/00Superconducting magnets; Superconducting coils
    • H01F6/06Coils, e.g. winding, insulating, terminating or casing arrangements therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E30/00Energy generation of nuclear origin
    • Y02E30/10Nuclear fusion reactors

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Containers, Films, And Cooling For Superconductive Devices (AREA)

Description

【発明の詳細な説明】 この発明は核融合装置において使用する超電導
ヘリカルコイルを支持するために使用する支持構
造に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a support structure used to support a superconducting helical coil used in a nuclear fusion device.

核融合装置においては、磁場形成のために超電
導ヘリカルコイルを使用する。この超電導ヘリカ
ルコイルは真空容器にほぼ対応するトーラス面に
沿つてら旋状に巻回されて配設されている。
In fusion devices, superconducting helical coils are used to generate the magnetic field. This superconducting helical coil is helically wound along a torus surface that substantially corresponds to the vacuum vessel.

ヘリカルコイルの支持としては、従来から、第
1図に示すようにヘリカルコイル1を真空容器2
外に配置し、かつこのヘリカルコイル1を真空容
器2に支持するものと、第2図に示す如くヘリカ
ルコイル1を真空容器2内に配置し、かつこのヘ
リカルコイル1を真空容器2に支持するものとが
ある。しかるに、このようなコイル支持方法は常
に電導コイルを使用している場合には大きな問題
は発生しないが、コイルが超電導化された場合に
は次のような不具合が生じる。すなわち、真空容
器は常温またはそれ以上の温度で運転され、他方
コイルは極低温で運転される。したがつて、支持
構造は真空容器とコイル間の相対変位を吸収でき
るような構造でなければならない。しかるに真空
容器とコイルの間の空間は狭く、このような機能
を持つた支持構造を設ける事は困難である。ま
た、上述した真空容器およびコイルの温度差によ
り支持部を介して真空容器からコイルへの熱侵入
がある。この熱侵入量は極力小さい事が望まし
く、このためには熱流入経路の長さすなわち支持
脚3,3′の長さが長い方が望ましい。しかるに
前述したように真空容器とコイルの間の空間は狭
く、熱侵入を防止するのに充分な長さの支持構造
を設ける事は困難である。
Conventionally, to support a helical coil, a helical coil 1 is placed in a vacuum vessel 2 as shown in FIG.
The helical coil 1 is placed outside and supported by the vacuum vessel 2, and the helical coil 1 is placed inside the vacuum vessel 2 and the helical coil 1 is supported by the vacuum vessel 2 as shown in FIG. There is something. However, although such a coil support method does not cause any major problems when a conductive coil is always used, the following problems occur when the coil is made superconducting. That is, the vacuum vessel is operated at room temperature or above, while the coil is operated at cryogenic temperatures. Therefore, the support structure must be of a structure that can absorb the relative displacement between the vacuum vessel and the coil. However, the space between the vacuum vessel and the coil is narrow, and it is difficult to provide a support structure with such a function. Further, due to the temperature difference between the vacuum container and the coil described above, heat may enter the coil from the vacuum container via the support portion. It is desirable that the amount of heat intrusion be as small as possible, and for this purpose, it is desirable that the length of the heat inflow path, that is, the length of the support legs 3, 3' be long. However, as described above, the space between the vacuum vessel and the coil is narrow, and it is difficult to provide a support structure of sufficient length to prevent heat from entering.

この発明は上記の如き事情に鑑みてなされたも
のであつて、真空容器およびヘリカルコイル間の
相対変位および熱侵入に対するコイル支持の問題
点を解消した核融合装置用超電導ヘリカルコイル
の支持構造を提供することを目的とするものであ
る。
The present invention has been made in view of the above circumstances, and provides a support structure for a superconducting helical coil for a nuclear fusion device that eliminates the problems of supporting the coil against relative displacement and heat penetration between the vacuum vessel and the helical coil. The purpose is to

この目的に対応して、この発明の核融合装置用
超電導ヘリカルコイルの支持構造は、トーラス面
にほぼ沿つてら旋状に巻回しているヘリカルコイ
ルの支持構造であつて、トーラス面の外側にトー
ラス方向に間隔をおいて複数の支持リングを配置
し、かつ、支持リングを固定ロツドにより相互に
連結固定してなることを特徴としている。
Corresponding to this purpose, the support structure for a superconducting helical coil for a nuclear fusion device of the present invention is a support structure for a helical coil wound spirally almost along a torus surface, and is provided on the outside of the torus surface. It is characterized in that a plurality of support rings are arranged at intervals in the torus direction, and the support rings are connected and fixed to each other by fixing rods.

以下この発明の詳細を一実施例を示す図面につ
いて説明する。
The details of this invention will be explained below with reference to the drawings showing one embodiment.

第3図には、この発明の核融合装置用超電導ヘ
リカルコイルの支持構造が概念図として示されて
いる。すなわち、第3図に示す如く、支持構造1
1は、支持リング12及び固定ロツド13を揃え
ている。ヘリカルコイル1は仮想のトーラス面
2′に沿つてら旋状に巻回し、このヘリカルコイ
ル1は支持リング12に支持される。支持リング
12はトーラス方向に間隔を置いて複数個配置さ
れ、仮想のトーラス面2′の外側に位置する。そ
れぞれの支持リング12は分割部14により二分
割可能な構造となつている。ヘリカルコイル1と
支持リング12の間の結合は機械的に充分な強度
をもつものであればよく、断熱性および熱膨張に
対する配慮は不要であり、例えばボルト結合でそ
の目的を達成できる。
FIG. 3 shows a conceptual diagram of a support structure for a superconducting helical coil for a nuclear fusion device according to the present invention. That is, as shown in FIG.
1 aligns the support ring 12 and fixing rod 13. The helical coil 1 is spirally wound along an imaginary torus surface 2', and is supported by a support ring 12. A plurality of support rings 12 are arranged at intervals in the torus direction and are located outside the imaginary torus surface 2'. Each support ring 12 has a structure that can be divided into two by a dividing portion 14. The connection between the helical coil 1 and the support ring 12 only needs to have sufficient mechanical strength, and there is no need to consider heat insulation and thermal expansion, and the purpose can be achieved by, for example, bolt connection.

以上のようなヘリカルコイル支持構造を実際の
核融合装置に適用する場合は第4図に示すように
なる。すなわち、支持リング12には自重支持用
のアーム15が設けられている。支持アーム15
には、ピンジヨイント16,16′と支持ロツド
17を介して常温の支持台18に支持する。支持
リング12および固定ロツド13は非磁性かつ熱
膨張率がヘリカルコイル1と同一の材料を使用す
るものとする。プラズマを取り囲む真空容器2は
ヘリカルコイル1の内側に配置され、容器支持脚
19によりヘリカルコイル1とは独立に支持され
る。ヘリカルコイル1と真空容器2の間には断熱
層21が挿入される。これらのヘリカルコイル1
および支持リング12等は、真空断熱のための大
型真空槽22内に一式として設置されている。大
型真空槽22の内側には断熱材を設置する。
When the helical coil support structure as described above is applied to an actual nuclear fusion device, it will be as shown in FIG. 4. That is, the support ring 12 is provided with an arm 15 for supporting its own weight. Support arm 15
In this case, it is supported on a support stand 18 at room temperature via pin joints 16, 16' and support rods 17. The support ring 12 and the fixed rod 13 are made of a material that is non-magnetic and has the same coefficient of thermal expansion as the helical coil 1. A vacuum vessel 2 surrounding the plasma is arranged inside the helical coil 1 and is supported independently of the helical coil 1 by vessel support legs 19. A heat insulating layer 21 is inserted between the helical coil 1 and the vacuum vessel 2. These helical coils 1
The support ring 12 and the like are installed as a set in a large vacuum chamber 22 for vacuum insulation. A heat insulating material is installed inside the large vacuum chamber 22.

ヘリカルコイル1と支持リング12の組立手順
としては、まずヘリカルコイル1を組立て、次に
分割部14で二分割された支持リング12をヘリ
カルコイル1にかぶせ、支持リング12とヘリカ
ルコイル1を一体に組立て、さらに支持リング1
2間に固定ロツド13を取付ける。
The procedure for assembling the helical coil 1 and the support ring 12 is to first assemble the helical coil 1, then cover the helical coil 1 with the support ring 12 that has been divided into two parts at the dividing part 14, and integrate the support ring 12 and the helical coil 1. Assembly and further support ring 1
Attach the fixing rod 13 between the two.

このようなヘリカルコイル支持構造においては
第5図に概念図で示す如く支持リング12と固定
ロツド13は全体として一体構造となる。したが
つて、ヘリカルコイル1に作用する電磁力はこの
鳥篭状の構造物で支持できる。支持リング12お
よび固定ロツド13はヘリカルコイル1からの熱
伝達または支持リング12に液体ヘリウム冷却パ
イプを取付ける事により極低温になる。このた
め、支持リング12とヘリカルコイル1はほぼ同
一の温度であり、ヘリカルコイル1と支持リング
12間には熱膨張差は殆んど無く、したがつて熱
応力も実用上問題なく、また、断熱支持の必要も
なくなる。また、一体化されたヘリカルコイル−
支持リング系の自重は、支持ロツド17を介して
常温の支持台18で支持され、かつ、支持ロツド
17と支持アーム15、支持台18の間はピンジ
ヨイントで接合される結果、熱収縮に対する変位
で吸収できる。また、支持ロツド17の長さを充
分にとり、また熱伝導率の低い材料を使用する事
によりヘリカルコイル部分への熱流入量を小さく
する事ができる。ヘリカルコイル1の内側に置か
れる真空容器2は以上に述べたヘリカルコイル系
とは独立に支持し、また真空容器とヘリカルコイ
ル1の間には断熱層21が挿入されているので、
常温またはそれ以上の温度で運転される真空容器
からヘリカルコイルに対する熱侵入は充分に小さ
くできる。
In such a helical coil support structure, the support ring 12 and the fixing rod 13 are integrally constructed as a whole, as shown in a conceptual diagram in FIG. Therefore, the electromagnetic force acting on the helical coil 1 can be supported by this birdcage-like structure. The support ring 12 and fixed rod 13 are brought to a cryogenic temperature by heat transfer from the helical coil 1 or by attaching a liquid helium cooling pipe to the support ring 12. Therefore, the support ring 12 and the helical coil 1 are at almost the same temperature, and there is almost no difference in thermal expansion between the helical coil 1 and the support ring 12, so there is no practical problem with thermal stress. There is no need for thermal insulation support. In addition, the integrated helical coil
The weight of the support ring system is supported by the support stand 18 at room temperature via the support rod 17, and the support rod 17, the support arm 15, and the support stand 18 are joined by pin joints, so that the weight of the support ring system is reduced by displacement due to heat shrinkage. It can be absorbed. Furthermore, by making the support rod 17 sufficiently long and using a material with low thermal conductivity, the amount of heat flowing into the helical coil portion can be reduced. The vacuum container 2 placed inside the helical coil 1 is supported independently of the helical coil system described above, and a heat insulating layer 21 is inserted between the vacuum container and the helical coil 1.
Heat intrusion into the helical coil from a vacuum vessel operated at room temperature or higher can be sufficiently reduced.

なお、ヘリカルコイル1の周辺にポロイダルコ
イルが存在する場合には、第6図に示す如く、上
記の構造を持つ支持リング12にポロイダルコイ
ル支持脚23を取付けた構造の支持リング12′
を用い、そのポロイダルコイル支持脚23にポロ
イダルコイル24を固定する。この場合、ヘリカ
ルコイル−支持リング系とポロイダルコイル24
は常に同一温度であり、既に述べたと同様に熱応
力の問題が発生せず、構造的に複雑な断熱固定と
する必要がない。
In addition, when a poloidal coil exists around the helical coil 1, as shown in FIG.
The poloidal coil 24 is fixed to the poloidal coil support leg 23 using the poloidal coil support leg 23. In this case, the helical coil-support ring system and the poloidal coil 24
are always at the same temperature, and as mentioned above, there is no problem of thermal stress, and there is no need for structurally complex heat-insulating fixing.

以上の説明から明らかな通り、この発明によれ
ば、ヘリカルコイルに支持枠を設ける事によりヘ
リカルコイル自身が電磁力に耐える自立的構造物
として自重を真空容器から独立に支持することに
より真空容器およびヘリカルコイル間の相対変位
を許容し、かつ、熱侵入の問題を解消することが
でき、しかも、ヘリカルコイル以外にその近傍に
あるポロイダルコイルも同時に支持することが可
能な核融合装置用超電導ヘリカルコイルの支持構
造を得ることができる。
As is clear from the above description, according to the present invention, by providing a support frame to the helical coil, the helical coil itself becomes a self-supporting structure that can withstand electromagnetic force and supports its own weight independently from the vacuum vessel. A superconducting helical coil for a nuclear fusion device that allows relative displacement between helical coils, solves the problem of heat intrusion, and can simultaneously support poloidal coils in the vicinity of the helical coil. A support structure can be obtained.

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

第1図は従来のヘリカルコイル支持構造の一例
を示す説明図、第2図は従来のヘリカルコイル支
持構造の他の例を示す説明図、第3図はこの発明
の一実施例に係るヘリカルコイル支持構造でヘリ
カルコイルを支持した状態の概念を示す説明図、
第4図はヘリカルコイル支持構造を核融合装置に
組込んだ状態を示す横断面説明図、第5図はこの
発明の一実施例に係るヘリカルコイル支持構造の
概念を示す説明図、及び第6図はこの発明の他の
実施例に係るヘリカルコイル支持構造の部分斜視
説明図である。 1……ヘリカルコイル、2……真空容器、11
……支持構造、12……支持リング、13……固
定ロツド、23……ポロイダルコイル支持脚、2
4……ポロイダルコイル。
FIG. 1 is an explanatory diagram showing an example of a conventional helical coil support structure, FIG. 2 is an explanatory diagram showing another example of a conventional helical coil support structure, and FIG. 3 is a helical coil according to an embodiment of the present invention. An explanatory diagram showing the concept of a state in which a helical coil is supported by a support structure,
FIG. 4 is an explanatory cross-sectional view showing a helical coil support structure incorporated into a nuclear fusion device, FIG. 5 is an explanatory view showing the concept of a helical coil support structure according to an embodiment of the present invention, and FIG. The figure is a partial perspective explanatory view of a helical coil support structure according to another embodiment of the invention. 1...Helical coil, 2...Vacuum container, 11
... Support structure, 12 ... Support ring, 13 ... Fixed rod, 23 ... Poloidal coil support leg, 2
4... Poloidal coil.

Claims (1)

【特許請求の範囲】 1 トーラス面にほぼ沿つてら旋状に巻回してい
るヘリカルコイルの支持構造であつて、前記トー
ラス面の外側にトーラス方向に間隔をおいて複数
の支持リングを配置し、かつ、前記支持リングを
固定ロツドにより相互に連結固定してなることを
特徴とする核融合装置用超電導ヘリカルコイルの
支持構造。 2 前記支持リングは、ポロイダルコイルを支持
するための支持脚を半径方向外方に延出させて備
えることを特徴とする特許請求の範囲第1項記載
の核融合装置用超電導ヘリカルコイルの支持構
造。
[Scope of Claims] 1. A support structure for a helical coil wound spirally almost along a torus surface, wherein a plurality of support rings are arranged at intervals in the torus direction on the outside of the torus surface. A support structure for a superconducting helical coil for a nuclear fusion device, characterized in that the support rings are connected and fixed to each other by fixing rods. 2. The support structure for a superconducting helical coil for a nuclear fusion device according to claim 1, wherein the support ring includes support legs extending radially outward for supporting the poloidal coil.
JP55149472A 1980-10-27 1980-10-27 Supporting structure for superconducting helical coil for nuclear fusion device Granted JPS5773906A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP55149472A JPS5773906A (en) 1980-10-27 1980-10-27 Supporting structure for superconducting helical coil for nuclear fusion device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55149472A JPS5773906A (en) 1980-10-27 1980-10-27 Supporting structure for superconducting helical coil for nuclear fusion device

Publications (2)

Publication Number Publication Date
JPS5773906A JPS5773906A (en) 1982-05-08
JPS6236369B2 true JPS6236369B2 (en) 1987-08-06

Family

ID=15475880

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55149472A Granted JPS5773906A (en) 1980-10-27 1980-10-27 Supporting structure for superconducting helical coil for nuclear fusion device

Country Status (1)

Country Link
JP (1) JPS5773906A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2653693C2 (en) * 2013-02-18 2018-05-14 Открытое акционерное общество Всероссийский научно-исследовательский, проектно-конструкторский и технологический институт кабельной промышленности (ВНИИ КП) Superconducting winding

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2653693C2 (en) * 2013-02-18 2018-05-14 Открытое акционерное общество Всероссийский научно-исследовательский, проектно-конструкторский и технологический институт кабельной промышленности (ВНИИ КП) Superconducting winding

Also Published As

Publication number Publication date
JPS5773906A (en) 1982-05-08

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