JPH0511646B2 - - Google Patents
Info
- Publication number
- JPH0511646B2 JPH0511646B2 JP62076271A JP7627187A JPH0511646B2 JP H0511646 B2 JPH0511646 B2 JP H0511646B2 JP 62076271 A JP62076271 A JP 62076271A JP 7627187 A JP7627187 A JP 7627187A JP H0511646 B2 JPH0511646 B2 JP H0511646B2
- Authority
- JP
- Japan
- Prior art keywords
- cryogenic refrigerant
- inner cylinder
- refrigerant injection
- cryogenic
- 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 - Lifetime
Links
- 239000003507 refrigerant Substances 0.000 claims description 42
- 238000002347 injection Methods 0.000 claims description 30
- 239000007924 injection Substances 0.000 claims description 30
- 238000005259 measurement Methods 0.000 claims description 14
- 239000001307 helium Substances 0.000 description 28
- 229910052734 helium Inorganic materials 0.000 description 28
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 28
- 239000007789 gas Substances 0.000 description 16
- 239000007788 liquid Substances 0.000 description 12
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 230000008020 evaporation Effects 0.000 description 3
- 238000001704 evaporation Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 230000003068 static effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 238000005481 NMR spectroscopy Methods 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 238000002591 computed tomography Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
Landscapes
- Magnetic Resonance Imaging Apparatus (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〕
本発明は超電導装置に係り、特に医療用核磁気
共鳴−コンピユータ断層撮影装置(以下MRI装
置と称す)に好適な超電導装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a superconducting device, and particularly to a superconducting device suitable for a medical nuclear magnetic resonance computer tomography device (hereinafter referred to as an MRI device).
一般に、ある種の金属を極低温状態にすると電
気抵抗が零となる、いわゆる超電導状態を示すこ
とが知られている。この現象を利用すれば、強力
で安定な静磁界を電力の損失なく得ることができ
る。この特徴を生かした超電導コイルは種々の分
野で採用され、特に、高均一高安定な静磁界が要
求される医療用MRI装置への適用が脚光を浴び
てきている。この種装置において、発生静磁界空
間の利用の容易さから磁界中心軸方向を水平方向
に設置した横置型超電導装置が広く採用され、例
えば特開昭61−63007号公報で紹介されており、
これを第5図に示している。
It is generally known that when certain metals are brought to an extremely low temperature, they exhibit a so-called superconducting state in which the electrical resistance becomes zero. By utilizing this phenomenon, a strong and stable static magnetic field can be obtained without loss of power. Superconducting coils that take advantage of this feature have been adopted in various fields, and in particular, their application to medical MRI equipment, which requires a highly uniform and highly stable static magnetic field, has been in the spotlight. Among this type of devices, horizontal superconducting devices in which the center axis of the magnetic field is installed horizontally are widely adopted because of the ease of use of the generated static magnetic field space.
This is shown in FIG.
超電導コイル20は、極低温冷媒である液体ヘ
リウム(4.2K)の中で初めて安定に動作させる
ことができるため、ヘリウム容器1の中の液体ヘ
リウムに浸漬されている。この液体ヘリウムは常
温(300K)外部からの熱侵入に対して熱的に遮
断されている必要があり、通常はヘリウム容器1
の周囲を約20Kのガスヘリウムシールド板2と、
約80Kの液体窒素シールド板3とで覆い、更にそ
れらを断熱真空容器4に収納し、真空断熱によつ
て熱侵入量を抑え、高価な液体ヘリウムの蒸発量
を極力抑える構造となつている。 The superconducting coil 20 is immersed in liquid helium in the helium container 1 because it can operate stably for the first time in liquid helium (4.2K), which is a cryogenic refrigerant. This liquid helium must be kept at room temperature (300K) and thermally isolated from heat intrusion from the outside, and is usually kept in a helium container 1.
Around 20K gas helium shield plate 2,
It is covered with a liquid nitrogen shield plate 3 of approximately 80K, and is further housed in an insulated vacuum container 4, so that the amount of heat intrusion is suppressed by vacuum insulation, and the amount of evaporation of expensive liquid helium is suppressed as much as possible.
またヘリウム容器1内の液体ヘリウムは蒸発す
るため、その量の減少分を補給したり、蒸発した
ガスヘリウムを外部へ放出したりしなければなら
ない。更に、超電導コイル20を動作させるため
に常温外部から電流を供給する必要がある。この
ため、液体ヘリウムの液面を計測する計測リード
や、液体ヘリウムを注入する注入管や、蒸発した
ガスヘリウムを外部へ放出する放出管や、電流通
電用のパワーリードが必要であり、これらのため
に極低温冷媒注入用ポート6を構成している。こ
の極低温冷媒注入用ポート6で上述の計測リー
ド、液体ヘリウム注入管、ガスヘリウム放出管お
よびパワーリードを常温外部からヘリウム容器1
内へ導入する内筒7は、常温部(約300K)から
極低温状態のヘリウム容器1への熱侵入を極力減
らすため、熱伝導長を充分に大きくすると共に、
20Kのガスヘリウムシールド板2および約80Kの
液体窒素シールド板3からのサーマルアンカ8,
9を設けている。 Further, since the liquid helium in the helium container 1 evaporates, it is necessary to replenish the decreased amount or to release the evaporated gas helium to the outside. Furthermore, in order to operate the superconducting coil 20, it is necessary to supply current from outside at room temperature. For this reason, measurement leads to measure the level of liquid helium, injection tubes to inject liquid helium, discharge tubes to release evaporated gas helium to the outside, and power leads for current flow are required. Therefore, a cryogenic refrigerant injection port 6 is configured. The above-mentioned measurement lead, liquid helium injection pipe, gas helium discharge pipe, and power lead are connected to the helium container 1 from outside at room temperature using this cryogenic refrigerant injection port 6.
The inner cylinder 7 to be introduced into the helium container 7 has a sufficiently large heat conduction length in order to reduce as much as possible the heat intrusion from the room temperature part (approximately 300K) to the helium container 1 in the cryogenic state.
Thermal anchor 8 from the 20K gas helium shield plate 2 and the approximately 80K liquid nitrogen shield plate 3,
There are 9.
従つて、この極低温冷媒注入用ポート6によつ
て病院等の狭い部屋内に収納するのが困難にな
る。そこで、極低温冷媒注入用ポート6を装置の
周方向に図示の如く傾斜させている。ただし、サ
ーマルアンカ8,9は、通常の垂直に極低温冷媒
注入用ポートを形成した場合と同様に、内筒7に
対し垂直に設置されていた。これは、常温外部か
ら80Kのサーマルアンカ9までの伝熱距離、また
80Kのサーマルアンカ9から20Kのサーマルアン
カ8までの伝熱距離、更にサーマルアンカ8から
4.2Kの極低温部までの伝熱距離を最大にするた
めである。 Therefore, this cryogenic refrigerant injection port 6 makes it difficult to accommodate it in a narrow room such as a hospital. Therefore, the cryogenic refrigerant injection port 6 is inclined in the circumferential direction of the device as shown. However, the thermal anchors 8 and 9 were installed perpendicularly to the inner cylinder 7, as in the case where a cryogenic refrigerant injection port is formed vertically. This is the heat transfer distance from the outside at room temperature to the thermal anchor 9 at 80K, and
Heat transfer distance from 80K thermal anchor 9 to 20K thermal anchor 8, and further from thermal anchor 8
This is to maximize the heat transfer distance to the cryogenic part of 4.2K.
従来の横置型超電導装置は上述の如き構成であ
つたため、内筒7内のガスヘリウムは、物性的に
温度の低いもとが重力鉛直下方に溜り、温度の高
いものが上方に溜ることが以後の検討で明らかに
なつた。このため、この内筒7の温度分布は、内
筒7の軸線に対して直角方向に等温度線を持つも
のではなく、ガスヘリウムとの熱交換によつて重
力鉛直方向に対して直角方向、つまり水平方向に
等温度線を持つことが分かつた。従つて、従来の
ように内筒7の軸線に対して直角方向にサーマル
アンカ8,9を構成したものは、重力鉛直方向の
下方に位置する部分から、ガスヘリウムの対流と
熱交換によつて直接極低温部へ熱が侵入してしま
うという欠点があつた。
Since the conventional horizontal superconducting device had the above-mentioned configuration, the helium gas in the inner cylinder 7, which has a low physical temperature, accumulates in the downward vertical direction due to gravity, and from now on, the helium with a high temperature accumulates in the upper part. This was made clear through the study. Therefore, the temperature distribution of the inner cylinder 7 does not have isothermal lines perpendicular to the axis of the inner cylinder 7, but due to heat exchange with the gas helium, the temperature distribution In other words, it was found that there are isothermal lines in the horizontal direction. Therefore, in the case where the thermal anchors 8 and 9 are constructed in a direction perpendicular to the axis of the inner cylinder 7 as in the past, the thermal anchors 8 and 9 are connected by convection and heat exchange of gas helium from the portion located below in the vertical direction of gravity. The drawback was that heat could directly enter the cryogenic area.
そこで、第6図に示すように、内筒7のサーマ
ルアンカ8,9をほぼ水平方向に設け、内筒7内
のガスヘリウムの対流と熱交換によつて極低温部
へ直接熱侵入が生じないようにすることが、本件
出願と同一出願人によつて提案されている。 Therefore, as shown in FIG. 6, the thermal anchors 8 and 9 of the inner cylinder 7 are installed in a substantially horizontal direction, and direct heat intrusion into the cryogenic part occurs due to the convection and heat exchange of gas helium within the inner cylinder 7. It has been proposed by the same applicant as the present application to avoid this.
しかしながら、第6図の−線に沿つた断面
図である第7図に示すように、内筒7は、パワー
リード11、液体ヘリウム注入管12、計測リー
ド13の三者全体を囲み、残余空間をガスヘリウ
ム放出管21としていたため、内筒7の直径をD
とすると△Lだけ、従来の垂直に設置した極低温
冷媒注入用ポートよりも長いものになつてしまう
という問題点があつた。 However, as shown in FIG. 7, which is a cross-sectional view taken along the - line in FIG. was used as the gas helium discharge tube 21, so the diameter of the inner cylinder 7 was set to D.
In this case, there was a problem that ΔL would be longer than the conventional vertically installed cryogenic refrigerant injection port.
本発明はこの問題点を解消するもので、その目
的とするところは極低温部への熱侵入を抑えた極
低温冷媒注入用ポートを有する超電導装置を提供
するにある。 The present invention aims to solve this problem, and its purpose is to provide a superconducting device having a cryogenic refrigerant injection port that suppresses heat intrusion into the cryogenic part.
本発明は上記目的を達成するために、従来より
も小さな内筒を少なくとも2つ形成し、これら内
筒に、パワーリード、極低温冷媒用注入管および
計測リードを分割して配置し、各内筒とその内部
に配置したものとの間にガス放出部を形成し、上
記各内筒外にほぼ水平に形成したサーマルアンカ
を設けたことを特徴とする。
In order to achieve the above object, the present invention forms at least two inner cylinders smaller than conventional ones, and divides and arranges a power lead, a cryogenic refrigerant injection pipe, and a measurement lead in these inner cylinders. The present invention is characterized in that a gas discharge portion is formed between the cylinder and something disposed inside the cylinder, and a thermal anchor formed approximately horizontally is provided outside each of the inner cylinders.
本発明は上述の如き構成としたため、複数に分
割された内筒の外部にほぼ水平になるようサーマ
ルアンカを形成すると、このサーマルアンカの重
力鉛直方向下部に形成された部分、すなわち従来
の△Lは小さくなり、ここから極低温部への熱侵
入を抑えることができる。
Since the present invention has the above-described configuration, when the thermal anchor is formed almost horizontally on the outside of the inner cylinder divided into a plurality of parts, the part formed at the lower part of the thermal anchor in the vertical direction of gravity, that is, the conventional △L becomes small, and it is possible to suppress heat from entering the cryogenic part.
以下本発明の実施例を図面によつて説明する。 Embodiments of the present invention will be described below with reference to the drawings.
第1図は横置型超電導装置を示しており、従来
の場合と概略構成において類似している。 FIG. 1 shows a horizontally placed superconducting device, which is similar in schematic structure to a conventional device.
超電導コイル20は、磁界中心軸がほぼ水平と
なるように配置されると共に、極低温冷媒容器1
内の極低温冷媒に浸漬されている。この極低温冷
媒容器1の周囲を覆うようにガスヘリウムシール
ド板2および液体窒素シールド板3とから成る断
熱シールド板が設けられており、この断熱シール
ド板により常温外部から極低温冷媒容器1内への
熱侵入が防止されている。更にその外周には断熱
真空容器4が配置されている。極低温冷媒容器1
の周方向に傾斜して極低温冷媒注入用ポート6を
構成しており、この実施例ではほぼ45°の傾斜角
となつている。この極低温冷媒注入用ポート6に
は、詳細を後述する内筒と、この内筒と断熱シー
ルド板とを接続したサーマルアンカ8,9が設け
られており、サーマルアンカ8,9はほぼ水平に
形成されている。内筒とその内部に配置されるパ
ワーリード11、極低温冷媒注入管12、計測リ
ード13およびガス放出部、更ひサーマルアンカ
8,9の詳細構成を、第1図の要部拡大図である
第2図と第3図で説明する。 The superconducting coil 20 is arranged so that the central axis of the magnetic field is substantially horizontal, and the superconducting coil 20
immersed in cryogenic refrigerant inside. A heat insulating shield plate consisting of a gas helium shield plate 2 and a liquid nitrogen shield plate 3 is provided to cover the periphery of the cryogenic refrigerant container 1, and this heat insulating shield plate allows the leakage of the cryogenic refrigerant from the room temperature outside into the cryogenic refrigerant container 1. heat intrusion is prevented. Furthermore, a heat insulating vacuum container 4 is arranged around the outer periphery. Cryogenic refrigerant container 1
The cryogenic refrigerant injection port 6 is inclined in the circumferential direction, and in this embodiment, the inclination angle is approximately 45°. This cryogenic refrigerant injection port 6 is provided with an inner cylinder whose details will be described later, and thermal anchors 8 and 9 that connect this inner cylinder and a heat insulating shield plate, and the thermal anchors 8 and 9 are placed almost horizontally. It is formed. This is an enlarged view of the main parts of FIG. 1 showing the detailed configuration of the inner cylinder, the power lead 11, the cryogenic refrigerant injection pipe 12, the measurement lead 13, the gas discharge part, and the thermal anchors 8 and 9 arranged inside the inner cylinder. This will be explained with reference to FIGS. 2 and 3.
特に、第3図から分かるように外部をサーマル
アンカ8,9に接続した内筒は従来よりも小さな
3つの内筒7a,7b,7cを有している。各内
筒7a,7b,7cにはそれぞれパワーリード1
1、極低温冷媒注入管12、計測リード13が配
置されており、これら内筒とその内部に配置した
ものとの間に形成した間隙はガス放出部、つまり
従来のガスヘリウム放出管となつている。従つ
て、各内筒7a,7b,7cの直径Dは従来より
も小さくなつており、それぞれにほぼ水平となる
ようサーマルアンカ8,9を形成すると△Lは第
6図に示す改良前よりも小さくなる。従つて、極
低温冷媒注入用ポート6は、その軸線をほぼ垂直
に成して構成した場合とほぼ同じ軸長で、極低温
冷媒の蒸発量の少ない経済的な超電導装置とする
ことができる。 In particular, as can be seen from FIG. 3, the inner cylinder connected to the thermal anchors 8, 9 on the outside has three inner cylinders 7a, 7b, 7c smaller than the conventional one. Each inner cylinder 7a, 7b, 7c has a power lead 1, respectively.
1. A cryogenic refrigerant injection pipe 12 and a measurement lead 13 are arranged, and the gap formed between these inner cylinders and what is arranged inside becomes a gas release part, that is, a conventional gas helium release pipe. There is. Therefore, the diameter D of each inner cylinder 7a, 7b, 7c is smaller than before, and if the thermal anchors 8, 9 are formed almost horizontally, △L will be smaller than before the improvement shown in FIG. becomes smaller. Therefore, the cryogenic refrigerant injection port 6 has approximately the same axial length as when its axis is substantially perpendicular, and an economical superconducting device with less evaporation of the cryogenic refrigerant can be achieved.
第4図は本発明の他の実施例による極低温冷媒
注入用ポート6の横断面図である。第3図との比
較から分かるように、本実施例においては2つの
内筒7a,7b内に、パワーリード11、極低温
冷媒注入管12、計測リード13を配置してい
る。極低温冷媒注入管12および計測リード13
は、パワーリード11よりも細いので1つの内筒
7b内にまとめて配置している。 FIG. 4 is a cross-sectional view of a cryogenic refrigerant injection port 6 according to another embodiment of the present invention. As can be seen from a comparison with FIG. 3, in this embodiment, a power lead 11, a cryogenic refrigerant injection pipe 12, and a measurement lead 13 are arranged within the two inner cylinders 7a and 7b. Cryogenic refrigerant injection pipe 12 and measurement lead 13
are thinner than the power lead 11, so they are arranged together in one inner cylinder 7b.
この実施例から分かるように、内筒は複数設け
られていれば良く、その中にパワーリード11、
極低温冷媒注入管12および計測リード13を分
散配置すれば良い。一般に、計測リード13やパ
ワーリード11は内移内に位置する挿入管を有し
ているが、同じ挿入管内に配置しても良い。 As can be seen from this embodiment, it is sufficient if a plurality of inner cylinders are provided, and the power lead 11,
The cryogenic refrigerant injection pipe 12 and the measurement leads 13 may be arranged in a distributed manner. Generally, the measurement lead 13 and the power lead 11 have an insertion tube located inside the introduction tube, but they may be placed in the same insertion tube.
以上説明したように本発明は、内筒を複数設け
て、これら内筒内にパワーリード、極低温冷媒注
入管および計測リードを分割して配置したため、
極低温冷媒注入用ポートを斜めに配置すると共に
サーマルアンカをほぼ水平に構成しても、極低温
冷媒注入用ポートの下方部の長さを抑えることが
でき、これによつて熱侵入量を減少すると共に極
低温冷媒の蒸発量の少ない超電導装置が得られ
る。
As explained above, in the present invention, a plurality of inner cylinders are provided, and the power lead, the cryogenic refrigerant injection pipe, and the measurement lead are arranged separately within these inner cylinders.
Even if the cryogenic refrigerant injection port is arranged diagonally and the thermal anchor is configured almost horizontally, the length of the lower part of the cryogenic refrigerant injection port can be suppressed, thereby reducing the amount of heat intrusion. At the same time, a superconducting device in which the amount of evaporation of cryogenic refrigerant is small can be obtained.
第1図は本発明による超電導装置の縦断面図、
第2図は第1図の要部拡大図、第3図は第2図の
−線に沿つた断面図、第4図は本発明の他の
実施例による超電導装置の要部断面図、第5図は
従来の超電導装置の縦断面図、第6図は先に提案
された超電導装置の要部断面図、第7図は第6図
の−線に沿つた断面図である。
1……極低温冷媒容器、2……ガスヘリウムシ
ールド板、3……液体窒素シールド板、4……断
熱真空容器、6……極低温冷媒注入用ポート、7
a,7b,7c……内筒、8,9……サーマルア
ンカ、11……パワーリード、12……極低温冷
媒注入管、13……計測リード。
FIG. 1 is a longitudinal cross-sectional view of a superconducting device according to the present invention;
2 is an enlarged view of the main part of FIG. 1, FIG. 3 is a sectional view taken along the - line in FIG. 2, and FIG. 4 is a sectional view of the main part of a superconducting device according to another embodiment of the present invention. 5 is a longitudinal cross-sectional view of a conventional superconducting device, FIG. 6 is a cross-sectional view of a main part of the previously proposed superconducting device, and FIG. 7 is a cross-sectional view taken along the line - in FIG. 6. 1...Cryogenic refrigerant container, 2...Gas helium shield plate, 3...Liquid nitrogen shield plate, 4...Insulated vacuum container, 6...Cryogenic refrigerant injection port, 7
a, 7b, 7c... Inner cylinder, 8, 9... Thermal anchor, 11... Power lead, 12... Cryogenic refrigerant injection pipe, 13... Measurement lead.
Claims (1)
超電導コイルと、この超電導コイルを極低温冷媒
中に浸漬するように収納したほぼ円筒状の極低温
冷媒容器と、この極低温冷媒容器の周囲を覆い外
部と熱的に遮断する断熱シールド板と、これら全
体を収納する断熱真空容器と、上記極低温冷媒容
器を常温外部と連通する内筒および上記断熱シー
ルド板と上記内筒を接続したサーマルアンカとを
有する極低温冷媒注入用ポートと、上記内筒内に
配置したパワーリード、極低温冷媒注入管および
計測リードとを備え、上記極低温冷媒注入用ポー
トを上記極低温冷媒容器の周方向に傾斜させて設
けた超電導装置において、上記サーマルアンカは
上記傾斜した極低温冷媒注入用ポート内でほぼ水
平に配置し、上記内筒は少なくとも2個形成し、
これら内筒内に上記パワーリード、上記極低温冷
媒注入管および上記計測リードを分けて配置し、
上記各内筒とその内部に配置したものとの間にガ
ス放出部を形成したことを特徴とする超電導装
置。 2 上記特許請求の範囲第1項記載のものにおい
て、上記内筒は2個形成し、一方の内筒内に上記
パワーリードを配置すると共に他方の内筒に上記
極低温冷媒注入管および上記計測リードを配置し
たことを特徴とする超電導装置。[Claims] 1. A superconducting coil arranged so that the central axis of the magnetic field is in the horizontal direction, a substantially cylindrical cryogenic refrigerant container in which the superconducting coil is immersed in a cryogenic refrigerant, and A heat insulating shield plate that covers the periphery of the low temperature refrigerant container and thermally isolates it from the outside, a heat insulating vacuum container that houses the whole of these, an inner cylinder that communicates the cryogenic refrigerant container with the room temperature outside, the heat insulating shield plate and the inner cylinder. A cryogenic refrigerant injection port having a thermal anchor connected to a cylinder, a power lead, a cryogenic refrigerant injection pipe, and a measurement lead arranged in the inner cylinder, the cryogenic refrigerant injection port having a thermal anchor connected to the cylinder, In the superconducting device provided inclined in the circumferential direction of the refrigerant container, the thermal anchor is arranged substantially horizontally within the inclined cryogenic refrigerant injection port, and at least two inner cylinders are formed,
The power lead, the cryogenic refrigerant injection pipe, and the measurement lead are arranged separately in these inner cylinders,
A superconducting device characterized in that a gas discharge part is formed between each of the inner cylinders and something arranged inside the inner cylinder. 2. In the device described in claim 1, two inner cylinders are formed, and the power lead is disposed in one inner cylinder, and the cryogenic refrigerant injection pipe and the measurement tube are arranged in the other inner cylinder. A superconducting device characterized by the arrangement of leads.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP62076271A JPS63244721A (en) | 1987-03-31 | 1987-03-31 | superconducting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP62076271A JPS63244721A (en) | 1987-03-31 | 1987-03-31 | superconducting device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63244721A JPS63244721A (en) | 1988-10-12 |
| JPH0511646B2 true JPH0511646B2 (en) | 1993-02-16 |
Family
ID=13600576
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP62076271A Granted JPS63244721A (en) | 1987-03-31 | 1987-03-31 | superconducting device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63244721A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007005573A (en) * | 2005-06-24 | 2007-01-11 | Hitachi Ltd | Superconducting magnet device and refrigerant injection method for superconducting magnet device |
-
1987
- 1987-03-31 JP JP62076271A patent/JPS63244721A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63244721A (en) | 1988-10-12 |
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