Superconductive device for helping shield magnetic field

BACKGROUND OF THE INVENTION AND DESCRIPTION OF THE RELATED ART
The present invention relates to a superconductive device for helping shield magnetic field as well as to a method for manufacturing such a superconductive device.
Ferromagnetic materials such as permalloy or ferrite has been utilized to reduce the effects of magnetic field into that of a certain space. Currently many devices have been introduced to help shield magnetic field by Meissner effect of superconductors. For example, in Japanese Patent Laid Open No. 1-134998 (1989) superconductive materials are arranged to the innermost side of the space in which the magnetic field is shielded. In U.S. patent appliction Ser. No. 509,438 a superconducting magnetic shielding tube, i.e. a tube for shielding magnetic field, has been proposed by the present applicants that comprises at least two layers which include a layer of a substrate and a layer of superconductor arranged in this order from the magnetic source to be shielded.
As the structure of superconductive oxides becomes larger due to a demand of its application, it becomes more difficult to integrally form a structure of superconductive oxides and to form a homogeneous layer of superconductive oxide. Besides, it is not industrially preferable to enlarge the apparatus for manufacturing them. Therefore, the necessity is growing to prepare structures of superconductive oxide and combine them later.
However, a large device for helping shield magnetic field using superconductive oxide for actual practice has still remained in a developing stage at present mainly due to a problem in connecting layers of superconductive oxide. Magnetic field has been known to leak through joints in conventional methods of joining the layers, and high performance in shielding magnetic field cannot be achieved due to the leak.
SUMMARY OF THE INVENTION
An object of the present invention is to provide a large-scale superconductive device for helping shield magnetic field with excellent superconductive properties exerted by effectively connecting layers containing superconductive oxide as well as to a method of manufacturing such a superconductive device.
Another object of the present invention is to provide a superconductive device in a cylindrical tube helping shield magnetic field with satisfactory superconductive properties to shield the magnetic field inside itself from outside or vice versa.
One aspect of the present invention is to provide a superconductive device for helping shield magnetic field, comprising: at least two members; a layer containing superconductive oxide over each of said members; means for connecting said members to form a substrate; and means for connecting said layers containing superconductive oxide along a joint in which said members are connected.
Another aspect of the present invention is to provide superconductive device for helping shield magnetic field, comprising: at least two members; a layer containing superconductive oxide over each of said members; means for connecting said members to form a substrate; and at least one portion containing superconductive oxide that contacts with both sides of said layers containing superconductive oxide along a joint in which said members are connected.
Another object of the present invention is to provide a method for manufacturing a superconductive device for helping shield magnetic field comprising: a step of placing compounds to become a layer containing superconductive oxide over at least two members to form green members; a step of firing the green members to prepare members with a layer containing superconductive oxide; a step of connecting the members with a layer containing superconductive oxide into a substrate with a layer containing superconductive oxide by appropriate means; and a step of connecting the layers containing superconductive oxide over the substrate along a joint in which the members are connected.

BRIEF DESCRIPTION OF THE DRAWINGS
FIGS. 1 to 8 show explanatory views illustrating shapes of members, modes of combining members, and shapes of cylindrical tubes in the present invention.
FIG. 9 to FIG. 11 show cross sections of a cylindrical tube with a bottom portion having a smaller cylindrical tube.
FIG. 12 illustrates a mode of combining flat members into a large-scale flat substrate in the present invention.
FIG. 13 to FIG. 19 show cross sections of joints between laminated members.
FIG. 20(a), FIG. 20(b), FIG. 21(a), and FIG. 21(b) illustrate a method of controlling an atmosphere during firing a joint to connect the layers in the present invention and during a subsequent heat treatment.
FIG. 22 to FIG. 28 illustrate methods of heating a joint portion.

DETAILED DESCRIPTION OF THE INVENTION
The present invention is hereinafter described in detail.
The present invention resides in a superconductive device for helping shield magnetic field made of at least two members, with a layer containing superconductive oxide, connected along with the layers containing superconductive oxide over the members, as well as in a method for manufacturing such a device.
The present invention is characterized in a method that a layer containing superconductive oxide placed over a member is connected to the layer placed over an adjacent member connected to the former member such that magnetic field does not pierce through the joint in the resultant device.
In the device according to the present invention first at least two members with a layer containing superconductive oxide over each of the members is prepared. In some applications a layer containing superconductive oxide is directly placed on a member, while in others the layer is placed on an intermediate medium placed on a member. In either case a member includes a layer containing superconductive oxide, and such a member with a laminated structure is called a "laminated member."
A shape of the device of the present invention is not restricted and can be appropriately adjusted depending on its applications. The device of the present invention can take, for example, a planar form, a cylindrical tube, a rectangular shell, etc.
When the device of the present invention has a shape of a cylindrical tube, the device may shield the magnetic field inside itself from the perturbation outside; thus the magnetic field inside the device has low magnetic field. Alternatively, the device may shield the magnetic field inside having a source of strong magnetic field from affecting the field outside. Many times a superconductive device for helping shield magnetic field having a shape of a cylindrical tube is referred to herein as a cylindrical tube.
A cross section of a cylindrical tube is not limited to a circle but eclipse, truncated circle, triangle, rectangle, polygon, etc. are included. Likewise, the axis of a cylindrical tube is not restricted to be perpendicular to the top or the bottom plane of the cylindrical device to be formed. However, the axis of the cylindrical tube is preferred to be perpendicular to the bottom plane of itself.
Moreover, when the device of the present invention has a shape of a cylindrical tube, the device may have a bottom portion in a cylindrical tube open in some applications and may have it closed with a member or members protruding outside the device in other applications.
As material for a member, any may be used that has enough mechanical strength to support itself and numerous layers placed on it. For example, such ceramic materials as zirconia and titania as well as noble metals, alloys and such metals as stainless steel (SUS 430, SUS 310, and SUS 320, specified in JIS), Inconel, Incolloy, and hasteloy can be used. There is no restriction on the thickness of a substrate.
Then a layer containing superconductive oxide placed over a member is another essential ingredient in this invention. However, in many cases it is preferred to place the intermediate medium between a member and a layer containing superconductive oxide. First it works to prevent superconductive oxide from reacting with a metal used as a member. When a common metal or an alloy other than noble metals and a superconductive oxide are used as materials for a member and a superconductive oxide layer, respectively, the metal and the superconductive oxide react significantly during firing, resulting in poor performance in superconductivity in the final product. It is preferred to include at least one layer in the intermediate medium, for instance a noble metal layer, to prevent the reaction between the member and a layer containing superconductive oxide.
Moreover, it is also preferred that the intermediate medium have excellent adhesion onto the member over a wide range of temperatures from the sintering temperature of superconductive oxide to a cryogenic temperature, like that of liquid nitrogen. This function of adhesion can be attained by placing another layer for adhesion in the intermediate medium between the layer to prevent the reaction and the member; this adhesive layer is made out of such binding materials as glass, various kind of ceramics, metal pastes and noble metal pastes.
Furthermore, it is preferred that the intermediate medium can attain the foregoing functions and also act as a moderator to moderate thermal impact shocks exerted in cold/heat cycles when the tube is applied to repeated cycles between two drastically different temperatures such as cryogenic temperature and room temperature. In other words, in applications it is quite expected that the tube in the present invention undergoes drastic temperature changes in a short period of time; for example, a tube in the present invention is cooled down by liquid nitrogen to exert superconductive properties, and then the tube is left at room temperature.
Therefore, it is preferred that the intermediate medium includes another layer of glass as an adhesive layer placed on a member and contacted with a layer of a noble metal. It is preferred to dispose the glass layer partially, not entirely, over the surface of a member, in a preferable manner, for example, in stripes, numerous dots, a lattice pattern, random pattern, and any combinations of these. The partial coverage of the glass layer over the surface of a member is suitable. This local structure can moderate shocks due to thermal impact during cold/heat cycles so that the tube maintains stable performance to shield the magnetic field inside itself.
The intermediate medium can be formed on a member by any of the known methods, which can be selected properly depending on the type of the intermediate medium. To prepare a layer of glass or ceramic in the intermediate medium, a slurry of the ingredients for the layer in a slurry is spray coated, and the ingredients are baked. To prepare a layer of metal a metal foil independently prepared is combined to a member or a layer of glass or ceramic by glass binding, diffusion bonding, or a plasma flame spraying.
Superconductive oxide in the present invention has no particular restriction on materials and can be any of superconductive oxide and its combination such as rare earth superconductive oxides having a multi-layered perovskite structure with a M-Ba-Cu-O system in which M is one or more of the rare earth elements selected from Sc, Y and lanthanides such as La, Eu, Gd, Er, Yb and Lu. Another example are superconductive oxides in a Bi series having such compositions as Bi.sub.2 Sr.sub.2 Ca.sub.1 Cu.sub.2 O.sub.x and Bi.sub.2 Sr.sub.2 Ca.sub.2 Cu.sub.3 O.sub.x.
No particular restriction applies to the thickness of a layer containing superconductive oxide. In general it is preferred to have a thickness of 50 to 2000 .mu.m after firing. When the thickness is less than 50 .mu.m, practically the layer is too thin to satisfactorily shield magnetic field. On the contrary when the thickness is larger than 2000 .mu.m, the difference in temperature in the direction perpendicular to the layer is too large and causes inhomogeneity in superconductive properties in the final product. When metal is used as a member or when the intermediate medium contains a layer of metal, preferably the thickness of a layer containing superconductive oxide after firing ranges from 50 to 500 .mu.m. Since the heat conductivity of metal is larger than that of superconductive oxide, upon firing the differences in temperatures between the metal and the superconductive oxide become insignificant.
The layer containing superconductive oxide binds onto the intermediate medium by any of known methods such as coating, spraying, and doctor blading. Usually spray coating is applied to the surface of the intermediate medium, followed by sintering at about 800.degree. to about 1200.degree. C. to form a layer containing superconductive oxide.
Then the member with a layer containing superconductive oxide is connected along a joint to another member with the layer. The corresponding intermediate media on the two members are connected along the joint when they are present. Finally, the corresponding layers containing superconductive oxide over the two members are connected.
There are numerous variations in members for their shapes, sizes, and the number and types of layers on them, etc. FIGS. 13-19 show typical structures of a laminated member 5 and modes of joining such laminated members. In FIGS. 13-15, 18, and 19 a member 1 includes a flange, and flanged portions 6 of two adjacent members are connected by nuts 7 and a bolt 8. In FIGS. 16 and 17 members do not contain a flange. The joint 9 between two adjacent members abutted against each other is connected by an appropriate method. Typically welding and glass binding are used when the members are made of metal and ceramics, respectively.
In FIGS. 13 and 14, a flanged portion forms only to a member 1, while in FIG. 15, a flanged portion 6 is present in a member and an Ag plate 3. In FIGS. 18 and 19, a flanged portion 6 is formed with all of a member 1, an intermediate medium (glass layer 2 and Ag plate 3) and a layer containing superconductive oxide 4, and FIGS. 16 and 17 show a case without such a flanged portion 6.
First a member with layers is connected to an adjacent one with layers. Then a layer on one member is connected to another layer on the member. When the laminated members 5 formed as described above are combined and Joined into a desired shape, the Ag plate 3 In the intermediate medium is also joined in the same manner as the member 1. In this case, the Ag plate 3 may be joined depending on the mode of joining the member 1.
For instance, in the mode shown In FIGS. 13 and 17, one edge of an Ag plate 3a on one side is extended into above the edge of the Ag plate 3b on the other side to be connected to stack the Ag plates in an area along the joint to make it into a dual structure. Then, a contact 10 between the top end of the upper Ag plate 3a and the lower Ag plate 3b in the dual structure along the joint is joined by welding or by an Ag paste. In FIGS. 14, 15 and 16, two adjacent Ag plates 3 are joined at the contact 10 of the Ag plates 3a by welding or by an Ag paste. When the Ag paste is used to complete connecting the plates, baking was applied between 800.degree. and 900.degree. C. after the coating of the Ag paste.
To connect a layer containing superconductive oxide 4 over a member with the layer containing superconductive oxide over another member in which the former member is joined, firstly a gap 11 between the two layers along the joint of the laminated members has to be filled with materials to become a portion 12 containing superconductive oxide that can be in one application the same as and in another different from the superconductive oxide in the layer containing superconductive oxide. For example, they can be a mixture of starting compounds for a desired oxide in appropriate stoichiometry. Alternatively they can be frit or calcined powders of a desired superconductive oxide.
There are many ways to fill the gap by materials to become a portion 12 containing superconductive oxide between the two adjacent layers containing superconductive oxide, depending on a laminated structure of the two members that have been connected. They are applied by spray coating or brush coating
FIGS. 18 and 19 show a local structure along a joint in which the gap between two layers containing superconductive oxide is not necessarily filled by these materials because the two layers containing superconductive oxide are already in contact each other. Without filling the gap an area around the gap can be heated to connect the two layers to result in a a dent 30 along the joint as shown in FIG. 19. Alternatively the gap can be filled with appropriate materials to become a superconductive oxide; after heating an area around the gap, the surface around the joint becomes flat (FIG. 18).
There is no particular restriction on a method for heating a gap 11 to be connected (FIGS. 22-28). Methods for heating an area around the gap include a direct radiation by a heater (FIG. 22), irradiation by a laser beam (FIG. 23), a direct hot blow (FIG. 24), indirect heating due to radiation by a heater from the side of a member 1 (FIG. 25), radiations by heaters from both sides of a member and a layer containing superconductive oxide 4 (FIG. 26), electric heating (FIG. 27), and induction by high-frequency wave (FIG. 28).
Then the materials placed in the gap by one of the methods above between two adjacent layers containing superconductive oxide are fired to form a portion containing superconductive oxide, followed by a heat treatment to grow its crystals of the appropriate phase. By this heat treatment the interface between a layer containing superconductive oxide and a portion containing superconductive oxide become homogeneous. When the superconductive oxide contained in a portion containing superconductive oxide is the same compound as the superconductive oxide contained in a layer containing superconductive oxide, the portion and the layer may become an integral part. It is preferred in many applications that the superconductive oxide contained in a portion containing superconductive oxide is the same compound as the superconductive oxide contained in a layer containing superconductive oxide. In this case appropriate heat treatment is especially preferable which makes a joint along the two layers containing superconductive oxide to be connected homogeneous.
A firing temperature and a temperature range in a heat treatment are adjusted to a type of superconductive oxide formed in a gap between two layers. When frit or calcined powders of YBa.sub.2 Cu.sub.3 O.sub.x and Bi.sub.2 Sr.sub.2 Ca.sub.2 Cu.sub.3 O.sub.x are used to fill a gap between two adjacent layers containing superconductive oxide, ranges of firing temperatures are from 900.degree. C. to 1200.degree. C. and from 830.degree. C. to 860 .degree. C., respectively. In either case during firing a sample can be placed under an atmosphere with oxygen content over 20%, favorably over 80%.
Superconductive oxide in a gap between two layers is not restricted to be the same as that of either superconductive oxide contained in a layer to be connected. For example, when frit or calcined powders of Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x forms upon firing in a gap between two layers containing Bi.sub.2 Sr.sub.2 Ca.sub.2 Cu.sub.3 O.sub.y, the temperature for firing ranging from 830.degree. C. to 860.degree. C. is much lower than a temperature required for partial melting of Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x. In some applications it is preferable not to melt a layer containing superconductive oxide.
When the superconductive oxide to be formed in a gap between two layers and/or the superconductive oxide in the two layers are mainly Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x, there are two methods for firing and subsequent heat treatment. In one method the surface of a sample is partitioned into two regions, and each region is independently subjected to appropriate temperatures and atmospheres. In the other method a partition is not used and the whole sample is kept in one atmosphere all the time.
In following examples both the superconductive oxide to be formed gap between two layers and the superconductive oxide in the two layers are mainly Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x, thus such experimental conditions as temperatures for firing and for a heat treatment in this section correspond to those for Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x as superconductive oxide. However, the choice of this particular superconductive oxide should be taken as an example of this present invention, and this invention is not limited as such.
In one method for firing and a subsequent heat treatment regarding Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x, as shown in FIG. 21, no partition is employed, and a whole sample is kept under one atmosphere. In the other method, as shown in FIG. 20, a sample is partitioned into two regions, and each region is controlled in a certain temperature under a certain atmosphere.
In one method for firing and a subsequent heat treatment partition of a sample is not employed, and an entire sample is kept under an atmosphere at one time (FIG. 21).
To fill a gap between two adjacent layers containing superconductive oxide by superconductive oxide, the starting materials in the gap are fired at a temperature between about 875.degree. C. and about 900.degree. C. under an atmosphere with oxygen content over 20%, favorably over 80%, or more favorably over 98%. Such an atmosphere will be referred to as an oxidative atmosphere. On firing the materials to connect the layers, area around the gap is locally heated in any of the methods mentioned before (FIGS. 22-28). In this method without a partition the area with temperatures higher than about 280.degree. C. in this step of firing is loosely defined as region A.
Then the sample is remained to be kept under an oxidative atmosphere for stable growth of crystals formed in the gap upon firing when the highest temperature in the area around the gap is higher than 850.degree. C. or preferably higher than 780.degree. C.
Then the region A is cooled under an atmosphere with oxygen content over 15%, preferably over 20% until the maximum temperature in the region A reaches to 780.degree. C., preferably to 750.degree. C.
Then the temperature and the atmosphere in region A are further changed for a subsequent heat treatment in one of the two ways. In one way first the atmosphere is changed, and then the temperature for a heat treatment is controlled. In another first the temperature for a heat treatment is controlled, and then the atmosphere is changed. Though the two ways tend to give similar results, the former way is sometimes preferable.
In one way the atmosphere is changed into an atmosphere with oxygen content under 15% or preferably under 3% before the temperature of the region does not change very much. Such an atmosphere will be referred to an inert atmosphere. Then at least all of region A is kept in the temperature range between about 780.degree. C. and about 280.degree. C., preferably between about 750.degree. C. and 450.degree. C. (FIG. 21b). If necessary, the area to be heated in region A to maintain this temperature range is larger than the area heated during firing.
In the other way after the maximum temperature in the region A reaches to 780.degree. C., preferably to 750.degree. C., the temperatures in the region is controlled so that at least all of region A is kept in the temperature range between about 780.degree. C. and about 280.degree. C., preferably between about 750.degree. C. and 450.degree. C. (FIG. 21b). Then the oxidative atmosphere is changed into an inert atmosphere. The sample undergoes a heat treatment in this given temperature range under this atmosphere, followed by cooling it to temperature below 280.degree. C.
During this heat treatment the areas outside region A are optionally kept under an inert atmosphere (FIG. 21b), though this is not required. Temperatures in these areas are not required to be controlled as long as they are lower than the highest temperature in region A. The temperature distribution in these regions is not restricted.
In either method for firing and a subsequent heat treatment with or without a partition, the subsequent heat treatment is not restricted to follow immediately after the firing. As a permissible alternative procedure after firing, region A is cooled down under an oxidative atmosphere to temperature below 280 .degree. C., then the oxidative atmosphere is changed into an inert atmosphere at this temperature below 280.degree. C., the region is heated to a temperature between 780.degree. C. and 280.degree. C. or preferably between about 750.degree. C. and 450.degree. C., followed by a heat treatment at the temperature under the inert atmosphere, and finally the region is cooled down below 280.degree. C. under the inert atmosphere.
In the other method a using partition for firing and a subsequent treatment frit or calcined powders of Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x in a gap between two layers containing Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x are fired at a temperature between about 875.degree. C. and about 900.degree. C. under an oxidative atmosphere, i.e., as defined before an atmosphere with oxygen content over 20%, favorably over 80%, or more favorably over than 98% (FIG. 20a). Temperature distribution inside this region is not restricted as long as this whole region is kept in the temperature range.
During this firing the region in which temperatures are higher than 780.degree. C., preferably higher than 750.degree. C., is partitioned from the other region and kept under the same oxidative atmosphere as that around the gap being fired. Naturally this region, referred to region A, under the oxidative atmosphere includes and is closer to the gap being fired than the other region, referred to region B, in which temperatures are lower than 780.degree. C., or preferably lower than 750 .degree. C.
During the firing region B, in which temperatures are lower than 780.degree. C. or 750.degree. C., is kept under an inert atmosphere, i.e. an atmosphere with oxygen content under 15% or preferably under 3% (FIG. 20b). The temperature distribution inside region B is not restricted. The partition of the two regions at the temperature of 780.degree. C. is chosen because superconductive oxide in layers begins to decompose at temperatures over 780.degree. C. under an inert atmosphere.
After the firing, the region A is kept under an oxidative atmosphere for stable growth of crystals in the joint as long as its maximum temperature is higher than 850.degree. C. or preferably 780.degree. C.
Then the region A, including the oxide thus formed in the gap between two layers, is cooled to temperatures lower than 780.degree. C. under an atmosphere with oxygen content over 15%, preferably over 20%. Subsequently its atmosphere is changed into an inert atmosphere, and the region under the inert atmosphere is kept at a temperature range between 780.degree. C. and 280.degree. C., especially between 750.degree. C. and 450.degree. C. (FIG. 20b). In this step part of oxygen in the superconductive oxide of region A is released to the atmosphere. This release of oxygen from the oxide is essential in exerting superconductivity because during firing the superconductive oxide in the whole region A absorbed oxygen under an oxidative atmosphere.
During this heat treatment of region A region B is remained to be kept under an inert atmosphere (FIG. 20b). The release of oxygen from Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x under an inert atmosphere in this temperature range, i.e. between 780.degree. C. and 280.degree. C. or preferably between 750.degree. C. and 450.degree. C., is reversible, and the oxide can absorb oxygen under an atmosphere rich in oxygen in the same temperature range, which tends to result in too large oxygen composition, leading to deterioration in superconductive properties. Bi.sub.2 Sr.sub.2 CaCu.sub.2 O.sub.x can adsorb oxygen in an atmosphere when it is kept at temperatures higher than 280 .degree. C. under an atmosphere with oxygen content over 20%. The rate of this oxygen absorption by this oxide under such an atmosphere is markedly accelerated at temperatures higher than 450.degree. C. This is the reason the region B is kept under an inert atmosphere to prevent potential oxygen absorption.
The temperature range of this heat treatment under an inert atmosphere is mainly affected by the stability of and the release of oxygen form the superconductive oxide of region A. The upper limit in the temperature range is 780.degree. C. because of the possible decomposition of superconductive oxide at higher temperatures. Temperatures lower than 750.degree. C. are especially preferred since under this condition possible thermal decomposition of the superconductive oxide becomes more unlikely. The lower limit of the temperature range is 280.degree. C. because at a temperature lower than this the superconductive oxide in the region A does not release oxygen from itself. Especially temperatures higher than 450.degree. C. are preferable since the rate of oxygen release from the oxide in the region A is accelerated.
To place starting materials on surface of a cylindrical tube having either or both of the two restrictions given below and to subsequently fire it, the present inventors have found, leads to unevenness in the thickness of the superconductive layer and/or uneven distribution in superconductive properties that adversely affect satisfactory performance in shielding magnetic field inside itself from outside:
(1) a cylindrical tube with a length in excess of 500 mm,
(2) a cylindrical tube having a layer containing superconductive oxide formed on the inner surface and with a ratio of L/D for the length L and inner diameter D of the cylindrical tube of: L/D .gtoreq.4.
The present inventors have also found that the unevenness In the thickness of the superconductive layer is mainly caused by difficulty in evenly distributing starting materials over the surface. Particularly it is noted that it is not practically easy to evenly place starting materials to a large tube and to the inner surface of a cylindrical tube with a large ratio of L/D, i.e. a tube with the small diameter or a tube with the long length; here the length of a tube is referred to the height of a tube.
Likewise the uneven distribution in superconductive properties is caused by difficulty in maintaining even temperature distribution over a tube; this problem is especially aggravated by a large tube, for example those satisfying the restriction (1), and a long tube, for example those satisfying the condition (2).
These difficulties lie on a particular form and size of a cylindrical tube, and thus it is overcome by this present invention in which a cylindrical tube is formed by connecting members with a layer containing superconductive oxide. As mentioned before, a size and a shape of a member can be appropriately chosen to prepare an even layer containing superconductive oxide. Therefore, in this invention a tube having either or both of the two restrictions is prepared with satisfactory performance to shield magnetic field.
Moreover, this invention is not restricted to a cylindrical tube having a layer containing superconductive oxide formed on the inner surface. This invention also includes a cylindrical tube having a layer containing superconductive oxide formed on the outer surface and a cylindrical tube having a layer containing superconductive oxide formed on the inner and the outer surfaces.
Furthermore, by a method in this invention a cylindrical tube having a layer containing superconductive oxide formed at the inner surface and with the ratio of L/D .gtoreq.4, is prepared much better than by a method in the prior art. Besides, a cylindrical tube having a layer containing superconductive oxide formed at the inner surface and with the ratio of L/D between 2 and 4, is also prepared better than by a method in prior art.
Various modes in combining members into a cylindrical tube are available, and a preferable mode can be chosen depending on its application. The factors to consider for the preferable mode include the purpose of the application, actual conditions of the application, the intermediate medium, superconductive oxide in a layer, methods of binding members, methods of placing the intermediate medium upon the substrate, etc.
FIGS. 1-8 and 12 illustrate typical modes of combining members :into a cylindrical tube. In FIGS. 1 and 2 a cylindrical tube without a member in a bottom plane are shown. In FIGS. 1 and 2 the joints of the members are parallel and perpendicular to the axial direction of the cylindrical tube to be formed, respectively.
FIGS. 3-8 illustrate a general structure that contains one bottom plane of a cylindrical tube closed; the other bottom plane can be either open or closed. In FIGS. 3-5 the joints of the members are parallel to the axial direction of the cylindrical tube to be formed while in FIGS. 6 and 7 they are perpendicular to the axial direction.
FIGS. 4-7 show an example that the portion for a bottom plane in a cylindrical tube to be formed is independently prepared to the portion for the side in a tube, in FIGS. 4 and 7 the portion for a bottom plane in a tube to be formed is composed of more than two members while in FIGS. 5 and 6 the portion for a bottom plane is composed of only one member. In FIG. 7 the joints in the side portion of a tube to be formed are parallel to the axial direction of the tube while the joints in the portion for a bottom plane are perpendicular to the axial direction of the tube.
In FIG. 8 one member becomes both the portion for a bottom plane and part of the side portion in a cylindrical tube to be formed.
FIGS. 9 and 10 show structures of the bottom portion having a small cylinder in a cylindrical tube to be formed. This structure corresponds to a structure that a small cylinder is inserted to the bottom portion in a cylindrical tube as shown in FIG. 5, 6 or 8. FIG. 11 also illustrates the bottom structure with a small cylinder in a cylindrical tube in which a small cylinder is connected to the bottom portion in, for example, FIG. 5, 6 or 8. In these cylindrical tubes with bottom portions having small cylinders, wirings for a sensor or the like can be introduced into the small cylindrical tubes in the bottom portions.
When the superconductive device in the present invention contains bottom members, it is preferable that the bottom members are connected to a rim of the tube with smooth curvature or an angle ranging from 90.degree. to 270.degree.. When a bottom member is connected to a rim of the tube with a right angle or an acute angle, or when the radius of the curvature is less than 5 mm at the connection part of rim, the properties of the tube to shield the magnetic field inside itself significantly deteriorate due to cracks around the connected portion caused by mechanical stress generated by the thermal shock by the cold/heat thermal cycle.
EXAMPLES
The present invention will now be described more in details but it shall not be limited to the following examples.
EXAMPLE 1
Four pieces of a member having flanges at two positions were manufactured out of inconel such that a tube of 500 mm.phi. in diameter and 1000 mm in height in the direction parallel to the main axis was formed by combining them along the joints in parallel with the axial direction of the tube as shown in FIG. 1. Each of the member is applied with a surface treatment by sand blasting. Then, except for the flange portion glass slurry was spray coated onto each of the members under masking of a paper tape in a lattice-like pattern each of 30 mm interval, followed by firing between about 800.degree. and about 900.degree. C. for one hour to form a glass layer of a lattice-like pattern with thickness between about 100 and 200 .mu.m.
Subsequently, Ag foils with thickness of 300 .mu.m were placed over the glass layer on the inconel member such that the Ag foil extended slightly beyond the side of the flange. Then the glass layer and the Ag foil were bound by heating about 850.degree. and 900.degree. C. for about one hour.
On the Ag layer on the members thus obtained, slurry containing oxides that give upon firing was spray coated, and the resultant tube was heated under oxygen atmosphere between 875.degree. C. and 900.degree. C. for 30 min to form superconductive oxide that is partially melted, followed by gradual cooling down, or annealing, to 850.degree. C. in the rate of 0.5.degree. C./min. They were stood at about 850.degree. C. for 15 hrs to crystallize superconductive oxide on the outermost surface. Then after changing the oxygen atmosphere into that of nitrogen the member was treated at a temperature between about 700.degree. C. and 250.degree. C. for 10 hr to result in the tube coated with superconductive oxide containing Bi with thickness between about 250 to about 350 .mu.m.
The respective flanges of the four members laminated with the intermediate medium on a member and a layer containing superconductive oxide on the medium, abutted against each other and fixed by bolts and nuts in the mode shown in FIG. 13 to form a cylindrical tube. The contact on the overlapped portion of the Ag foils was connected by welding.
A slurry containing Bi.sub.2 Sr.sub.2 Ca.sub.1 Cu.sub.2 O.sub.x was spray coated into each of the gaps between layers containing superconductive oxide along the joints in which the members were connected while the other parts on the surface of the tube were masked. The slurry in the joints were heated by radiation of a heater as shown in FIG. 22 under a method controlling two atmospheres in three areas as shown in FIG. 20. The tube thus obtained has satisfactory appearance by visual observation, and had satisfactory evaluations after cold/heat cycles and local Jc tests. These results are shown in Table 1.
The performance to shield magnetic field inside a tube was measured by a gauss meter situated in a tube while magnetic field outside the tube increased by an electromagnet outside. The magnetic field outside was recorded when the magnetic field inside a tube just began to increase from background.
As evaluation for the cold/heat cycle, the tube at room temperature was first immersed in liquid nitrogen. Then after the temperature of the tube itself was maintained at the liquid nitrogen temperature for 30 min, the performance to shield magnetic field inside itself was measured in the liquid. Subsequently the tube was taken out of the liquid and left at room temperature. After the temperature of the entire tube reached to the room temperature, the tube is left at room temperature for 30 min, and ready for immersing it in liquid nitrogen in the next cycle. This whole process completes one cycle, and five cycles were done.
The performance to shield the magnetic field inside itself from outside at the fifth cycle is compared to that at the first cycle by the following equation and evaluated as ".largecircle." for more than 80% as satisfactory, ".DELTA." for more than 50% as good, and "x" for less than 50% as failure. ##EQU1##
TABLE 1__________________________________________________________________________ Device for BiMaterial shielding system Num- Joining Mode for magnetic super- ber Thick-Ex- member field conduc- Divi- of ness of Evaluationam- of Shape tive sional divi- Ref. Sub- Silver silver Heating Firing Apper-ple substance Size layer mode sion Figure strate plate plate Method schedule ance 1 2__________________________________________________________________________1 Inconel Cylinder Outside FIG. 1 4 FIG. 13 Flange Welding 300 .mu.m FIG. 22 First Good .smallcircle. .smallcircle. 1 .phi.500 .times. 1000 mm2 Inconel Cylinder Outside FIG. 1 4 FIG. 14 Flange Welding 300 .mu.m FIG. 23 First Good .smallcircle. .smallcircle. 1 .phi.500 .times. 1000 mm3 Inconel Cylinder Outside FIG. 1 4 FIG. 17 Welding Welding 300 .mu.m FIG. 24 First Good .smallcircle. .smallcircle. 6 .phi.500 .times. 1000 mm4 Inconel Cylinder Outside FIG. 1 4 FIG. 16 Welding Ag paste 300 .mu.m FIG. 25 First Good .smallcircle. .smallcircle. . .phi.500 .times. 1000 mm5 Inconel Cylinder Inside FIG. 1 4 FIG. 13 Flange Ag paste 300 .mu.m FIG. 26 First Good .smallcircle. .smallcircle. 7 .phi.500 .times. 1000 mm6 Inconel Cylinder Inside FIG. 1 4 FIG. 13 Flange Welding 300 .mu.m FIG. 27 First Good .smallcircle. .smallcircle. 1 .phi.500 .times. 1000 mm7 Inconel Cylinder Inside FIG. 1 4 FIG. 16 Welding Welding 300 .mu.m FIG. 28 First Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm8 Inconel Cylinder Inside FIG. 1 4 FIG. 16 Welding Ag paste 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm9 Inconel Cylinder Inside FIG. 1 4 FIG. 15 Flange Welding 300 .mu.m FIG. 24 Second Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm10 Inconel Cylinder Inside FIG. 1 4 FIG. 18 Flange Ag paste 300 .mu.m FIG. 25 Second Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm11 Inconel Cylinder Outside FIG. 1 4 FIG. 19 Flange Ag paste 300 .mu.m FIG. 26 Second Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm12 SUS 304 Cylinder Outside FIG. 1 4 FIG. 17 Welding Welding 300 .mu.m FIG. 27 Second Good .smallcircle. .smallcircle. N .phi.500 .times. 1000 mm__________________________________________________________________________
EXAMPLES 2 to 37
Each of the superconductive tubes for shield magnetic field having or not having bottom portion tubes or flat plates shown in Table 1 was obtained in the same procedures as those in Example 1, with the material for the member, mode of, number of division, mode of connecting members, thickness of the Ag plate in the intermediate medium, heating method for the joined portion, and backing schedule being determined respectively as shown in Table 1 to Table 3. The evaluation was made for the appearance and the cold/heat cycle (evaluation (1) in Table 1 to Table 3) and local Jc evaluation (evaluation (2) in Table 1 to Table 3). The results are shown in Table 1 to Table 3.
Examples 34 to 36 are for the bottomed cylindrical tube each with a small cylinder shown in FIGS. 9, 10 and 11. FIG. 9 show a bottomed cylindrical tube having a layer containing superconductive oxide formed on the outer side and FIG. 10 shows a bottomed cylindrical tube 20 having a layer containing superconductive oxide formed on the inner side in which a small cylinder 21 is inserted and formed to the bottom of the bottomed cylindrical tube 20. Further, FIG. 11 shows a bottomed cylindrical tube 20 in which a small cylinder 21 is joined to the bottom. In the drawing, 22 represents a joined portion on which a starting material 23 for superconductor is formed by coating.
TABLE 2__________________________________________________________________________ Device for BiMaterial shielding system Num- Joining Mode for magnetic super- ber Thick-Ex- member field conduc- Divi- of ness of Evaluationam- of Shape tive sional divi- Ref. Sub- Silver silver Heating Firing Apper-ple substance Size layer mode sion Figure strate plate plate Method schedule ance 1 2__________________________________________________________________________13 SUS 430 Cylinder Outside FIG. 1 4 FIG. 16 Welding Ag paste 300 .mu.m FIG. 28 Second Good .smallcircle. .smallcircle. O .phi.500 .times. 1000 mm14 SUS Cylinder Inside FIG. 1 4 FIG. 13 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. 310S .phi.500 .times. 1000 mm15 Inconel Bottomed Outside FIG. 3 4 FIG. 13 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. cylinder .phi.500 .times. 1000 mm16 Inconel Bottomed Outside FIG. 4 8 FIG. 13 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. cylinder .phi.500 .times. 1000 mm17 Inconel Cylinder Inside FIG. 2 2 FIG. 15 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. .phi.500 .times. 1000 mm18 Inconel Bottomed Inside FIG. 6 3 FIG. 15 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. cylinder .phi.500 .times. 1000 mm19 Inconel Cylinder Inside FIG. 1 4 FIG. 15 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. N .phi.650 .times. 2000 mm20 Inconel Cylinder Inside FIG. 2 4 FIG. 15 Flange Welding 300 .mu.m FIG. 22 Second Good .smallcircle. .smallcircle. O .phi.650 .times. 2000 mm21 Inconel Bottomed Inside FIG. 5 5 FIG. 15 Flange Welding 300 .mu.m FIG. 23 First Good .smallcircle. .smallcircle. cylinder .phi.650 .times. 2000 mm22 Inconel Bottomed Inside FIG. 7 8 FIG. 16 Welding Welding 300 .mu.m FIG. 23 First Good .smallcircle. .smallcircle. N cylinder .phi.650 .times. 2000 mm23 Inconel Bottomed Outside FIG. 6 5 FIG. 16 Welding Welding 300 .mu.m FIG. 24 First Good .smallcircle. .smallcircle. O cylinder .phi.650 .times. 2000 mm24 Inconel Cylinder Outside FIG. 1 6 FIG. 16 Welding Welding 300 .mu.m FIG. 24 First Good .smallcircle. .smallcircle. .phi.800 .times. 3000 mm__________________________________________________________________________
TABLE 3__________________________________________________________________________ Device for BiMaterial shielding system Num- Joining Mode for magnetic super- ber Thick-Ex- member field conduc- Divi- of ness of Evaluationam- of Shape tive sional divi- Ref. Sub- Silver silver Heating Firing Apper-ple substance Size layer mode sion Figure strate plate plate Method schedule ance 1 2__________________________________________________________________________25 SUS 430 Cylinder Inside FIG. 2 6 FIG. Flange Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. .phi.800 .times. 14 24 3000 mm26 SUS Cylinder Inside FIG. 4 12 FIG. Flange Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. 310S .phi.800 .times. 13 24 3000 mm27 Inconel Cylinder Inside FIG. 6 7 FIG. Welding Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. .phi.800 .times. 17 25 3000 mm28 Inconel Cylinder Inside FIG. 8 7 FIG. Flange Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. N .phi.800 .times. 15 25 3000 mm29 Inconel Cylinder Inside FIG. 2 10 FIG. Flange Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. O .phi.1000 .times. 14 22 5000 mm30 Inconel Cylinder Outside FIG. 6 5 FIG. Flange Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. .phi.650 .times. 14 22 2000 mm31 Inconel Cylinder Inside FIG. 5 5 FIG. Welding Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. .phi.650 .times. 16 22 2000 mm32 Inconel Cylinder Outside -- -- -- -- -- 300 .mu.m -- Integral Good .smallcircle. .smallcircle. .phi.100 .times. baking 200 mm33 Inconel Cylinder Inside -- -- -- -- -- 300 .mu.m -- Integral Good .smallcircle. .smallcircle. .phi.100 .times. baking 200 mm34 Inconel Formed -- FIG. 9 2 -- -- -- 300 .mu.m FIG. First Good .smallcircle. .smallcircle. by join- 22 ing Ex- amples 30 and 3235 Inconel Formed -- FIG. 2 -- -- -- 300 .mu.m FIG. First Good .smallcircle. .smallcircle. N by join- 10 22 ing Ex- amples 30 and 3236 Inconel Formed -- FIG. 2 -- -- -- 300 .mu.m FIG. First Good .smallcircle. .smallcircle. O by join- 11 22 ing Ex- amples 30 and 3237 Inconel 900 mm -- FIG. 11 FIG. Welding Welding 300 .mu.m FIG. First Good .smallcircle. .smallcircle. Flat 12 17 22 plate .phi.800 .times. 3000 mm__________________________________________________________________________
COMPARATIVE EXAMPLES 1 to 17
Each of the oxide superconductor magnetic shielding bodies shown in the following Table 4 was obtained in the same procedures as those in Example 1, excepting for integrally forming bottomed or bottomless cylinders or flat plates each comprising a substrate, intermediate medium, composed of a glass layer and a silver layer, placed on the substrate, and a layer containing superconductive oxide. Then, evaluation was made for the appearance and the cold/heat cycle (evaluation (1) in Table 4), local Jc (evaluation (2) in Table 4). The results are shown in Table 4.
TABLE 4__________________________________________________________________________ Device for shielding Material Bi system magnetic field for super- Shape member of Silver conductive EvaluationComparative Example Size substrate plate layer Appearance 1 2__________________________________________________________________________1 300 mm Flat plate Inconel 300 .mu.m -- Good .smallcircle. .smallcircle.2 300 mm Flat plate US 430 300 .mu.m -- Good .smallcircle. .smallcircle.3 Cylinder Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. .phi.100 .times. 400 mm4 Cylinder Inconel 300 .mu.m Inside (A) x x .phi.100 .times. 400 mm5 Cylinder Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. .phi.250 .times. 500 mm6 Cylinder Inconel 300 .mu.m Inside (A) .smallcircle. .DELTA. .phi.250 .times. 500 mm7 .phi.500 .times. 500 mm Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. Cylinder8 .phi.500 .times. 500 mm Inconel 300 .mu.m Inside Good .smallcircle. .smallcircle. Cylinder9 .phi.500 .times. 1000 mm Inconel 500 .mu.m Outside (B) x x Cylinder10 .phi.650 .times. 2000 mm Inconel 500 .mu.m Outside (B) x x Cylinder11 .phi.650 .times. 2000 mm Inconel 500 .mu.m Inside (B) x x Cylinder12 .phi.800 .times. 3000 mm Inconel 500 .mu.m Inside (B) x x Cylinder13 .phi.80 .times. 500 mm Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. Bottomed cylinder14 .phi.150 .times. 450 mm Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. Bottomed cylinder15 900 mm Flat plate Inconel 300 .mu.m -- (C) x x16 .phi.250 .times. 500 mm Inconel 300 .mu.m Outside Good .smallcircle. .smallcircle. Bottomed cylinder17 .phi.250 .times. 500 mm Inconel 300 .mu.m Inside (A) .smallcircle. .DELTA. Bottomed cylinder__________________________________________________________________________ (A): Uneven thickness in a layer containing superconductive oxide (B): Failure in firing around the edges of a tube (C): Failure in firing in some parts
As apparent from the foregoing examples and comparative examples, when the small flat plate or the cylindrical tube of a relatively short length, the tubes in the present invention of the examples formed by using members with a laminated structure in which an layer containing superconductive oxide is placed over a member, are excellent in evaluations for the appearance, the cold/heat cycle, and for the local Jc, in time same extent as the integrally formed tube of the comparative examples. However, when the flat plate of a relatively large size or time cylindrical tube of a relatively long length, it can be seen that the evaluations for the appearance, for the cold/heat cycle, and for the local Jc of the tube in the present invention of the examples can be improved as compared with those in the comparative examples.

Number	Name	Date	Kind
3895432	Diepers et al.	Jul 1975
5061685	Kosuge et al.	Oct 1991

Number	Date	Country
0390517A2	Oct 1990	EPX
0488717A1	Jun 1992	EPX
3905424A1	Aug 1990	DEX

Superconductive device for helping shield magnetic field

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