US3778895A - Method of fabricating an aluminum clad multiplex superconductor - Google Patents
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- US3778895A US3778895A US00300345A US3778895DA US3778895A US 3778895 A US3778895 A US 3778895A US 00300345 A US00300345 A US 00300345A US 3778895D A US3778895D A US 3778895DA US 3778895 A US3778895 A US 3778895A
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- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N60/00—Superconducting devices
- H10N60/20—Permanent superconducting devices
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- H10N60/0128—Manufacture or treatment of composite superconductor filaments
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- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N60/00—Superconducting devices
- H10N60/01—Manufacture or treatment
- H10N60/0156—Manufacture or treatment of devices comprising Nb or an alloy of Nb with one or more of the elements of group 4, e.g. Ti, Zr, Hf
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- Y—GENERAL 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
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- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9265—Special properties
- Y10S428/93—Electric superconducting
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- Y—GENERAL 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
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- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S505/00—Superconductor technology: apparatus, material, process
- Y10S505/80—Material per se process of making same
- Y10S505/815—Process of making per se
- Y10S505/818—Coating
- Y10S505/821—Wire
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- Y—GENERAL 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
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- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S505/00—Superconductor technology: apparatus, material, process
- Y10S505/825—Apparatus per se, device per se, or process of making or operating same
- Y10S505/917—Mechanically manufacturing superconductor
- Y10S505/926—Mechanically joining superconductive members
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- Y—GENERAL 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
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- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S505/00—Superconductor technology: apparatus, material, process
- Y10S505/825—Apparatus per se, device per se, or process of making or operating same
- Y10S505/917—Mechanically manufacturing superconductor
- Y10S505/928—Metal deforming
- Y10S505/93—Metal deforming by drawing
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49014—Superconductor
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- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/12743—Next to refractory [Group IVB, VB, or VIB] metal-base component
Definitions
- An aluminum clad multiplex superconductor comprises an aluminum alloy cladding and a multiplex superconductor inserted into the cladding and is constructed with a plurality of unit superconductors twisted or braided with each other, each of which unit superconductors is constructed with a strand of a pinrality of superconductive wires, an intermediate aluminum layer and a relatively hard aluminum alloy layer surrounding the intermediate layer.
- the intermediate aluminum layer serves to prevent the flowing phenomenon during the withdrawing of the unit superconductor.
- the present invention relates to a method of fabricating an aluminum clad multiplex superconductor.
- the resistivity of aluminum is 3 X 10" cm) and that of copper is 1 2 X *(0 cm) as shown in FIG. 1.
- the thermal conductivities of aluminum and copper in the vicinity of 4.2K they are 33('W/cml() and 3(W/cmK), respectively, as shown in FIG. 2'.
- the thermal diffusion coeffi- .ciency Dth which is defined as (thermal conductivity (K)/specific heat (C) X specific gravity (d)
- those of copper (OFHC, 99.99%) and aluminum (purer than 99.995%) are 0.12 X 10 and 43 X 10, respectively.
- the magnetic diffusion coefficiency Dm which is defined as (electric resistance (R)/,u. (magnetic permeability)
- that of copper is 1 2 X l0"/p. while that of aluminum is 3 X 10' 1.,
- the heat discharging ratio of aluminum to copper for unit cross Dth(Al)/1-(Al) yq Dth(A l Dm(A1)) Dth(C u )/1-(Cu) 8.95 Dth(Cu) Dm(Cu) 2.70 r gofso Since the heat and/or magnetic flux pass through the surface of the superconductor, the value of the ratio for unit coating thickness becomes V 3 (T- V6 0, that is, the heat discharging capability of aluminum is 5.5 7.7 times that of copper.
- FIG. 3 shows the current density for the total cross sectional area of the coated superconductor, in percentage, when a unit current I is flowing through the superconductive core line and the cross sectional area ratio of the core line to the coating metal is selected as l 2.
- the area ratio of the superconductive wire to a copper cladding is 1 4
- the ratio of the superconductive wire to the pure aluminum can be on the order of l 0.2 to obtain substantially the same stability as that obtained by the copper cladding. That is, when the pure aluminum is employed with the same sized core wire, the current density for the total cross sectional area of the superconductor can be increased from 17% to i.e., the current density becomes 4.4 times that obtained with the copper coating.
- aluminum oxide electrical insulating film of very hard alumite
- This film has excellent voltage withstanding characteristics and the thermal conductivity thereof in the radial direction through the insulating film to helium, when compared with the conventional polyvinylformal coating on copper cladding, b'ecomes about one thousand times that of the conventional organic film since the thermal conductivity of the organic film is 0.00154 W/cmC while that of the alumite is 0.164 W/cmC, and the thickness of the alumite can be about one tenth of the organic film.
- the mechanical strength, i.e., the tension strength of aluminum is 4kg/mm at 20C and considerably less than that of copper the value of which is 24ltg/mm at 20C even though the value of aluminum at 4.2K'becomes several times that at 20C.
- a primary object of the present invention is to provide a method of fabricating an aluminum clad multiplex superconductor having the above described many advantages in actual use.
- FIG. I shows the temperature vs electric resistance characteristics of aluminum and copper
- FIG. 2 shows the temperature vs thermal conductivity characteristics of aluminum and copper
- FIG. 3 shows the current density, in percentage with respect to a unit current flowing through a superconductive wire when a superconductor constituted with a superconductive wire and a coating of either aluminum or copper is wound to form a fully packed solenoid with a cross sectional area ratio of the wire to the coating being 1 2 and the unit current flowing through the wire is averaged over the total cross sectional area of the wire and the coating,
- FIG. 4 shows the magneto-resistance characteristics of aluminum and copper and FIG. 5 shows the relation between the workability (area reduction factor) and Vickers hardness;
- FIG. 6(A) is a cross section of unit superconductor according to the present invention prior to the wiredrawing thereof;
- FIG. 6(B) is a formation of twisted superconductive cylinders or wires
- FIG. 7 is a cross section of unit superconductor according to the present invention after the wire-drawing thereof;
- FIGS. 8A and 8B show the current vs voltage characteristics (thermal hysterisis) of the present unit super conductor constituted with a superconductive wire having a copper and a aluminum coating respectively;
- FIGS. 9A and 9B show examples of the present aluminum clad multiplex superconductor constructed with a plurality of the unit superconductors.
- FIG. 6 there is shown the fundamental structure of a unit superconductor ofthe present invention prior to the wiredrawing thereof, in which, in order to prevent the highly pure aluminum cladding from being stretched alone, a strand of three superconductive twisted cylinders or wires 1 is inserted into a pipe 2 of 99.99% aluminum and then the pipe 2 is inserted into anothrpipe 3 of aluminum alloy having a suitable hardness, to thereby constitute a triple layer structure.
- the pure aluminum pipe 2 is deformed initially to fill up the screw gaps 4 with a portion of the volume of the pipe 2.
- the flowing between the aluminum pipe, the aluminum alloy pipe and the strand of superconductive wires can be re- .,..,stnctett.to less mamflmheu the P 3 is made of 2.5% Mg 0.25% Cr Al alloy, the Jamar the flowlig after the filling up of the gaps with the pure aluminum being determined by the hardness of the aluminum alloy.
- FIGS. 8(A) and 8(8) Experimental data of the unit superconductor having copper cladding and the present unit superconductor are shown in FIGS. 8(A) and 8(8) respectively. It will be clear from these data that the unit superconductor having a copper cladding has a thermal hysterisis while the present unit superconductor having aluminum cladding has no thermal hysterisis. In FIGS. 8(A) and 8(B), the data were obtained by standardizing the cross sectional area ratios.
- the unit superconductor having aluminum cladding thus produced through the aforementioned process is furtherworked, in order to make it suitable for use in a large scale electromagnet. Thereafter a plurality of the present unit superconductors each having an aluminum cladding are bundled and twisted, or braided.
- the unit superconductors are, as required, twisted or braided after being treated to provide them with an alumite coating.
- the multiplex superconductor may be inserted into a sheath of aluminum alloy such as 2.5 Mg 0.25 Cr Al or duralumin, etc. or may be surrounded by a sheet of such aluminum alloy, and then pressed or drawn, if necessary.
- the present multiplex superconductor is made completely of non-organic materials it is clear that it can be heat-treated for a suitable time at a suitable temperature, after the mechanical process for forming the multiplex superconductor structure is completed and- /or the alumite forming process for the respective unit superconductors is performed. Since the melting point of the alumite layer is very high, no burning occurs and the mechanical strength thereof is considerably large.
- the aluminum clad multiplex superconductor fabricated in accordance with the present invention may be further suitably worked. For example, another electric insulator layer having reasonable mechanical strength may be provided electrically on the outer surface of the outermost aluminum sheath.
- the present multiplex superconductor having aluminum cladding can be easily wound as a solenoid.
- FIGS. 9A and 9B are cross-sectional views of a multiplex superconductor fabricated in accordance with the present invention, the structure of the multiplex superconductor being constituted with a plurality of the unit superconductors each having the triple layer structure.
- the unit superconductors are inserted into a pipe or sheath of aluminum alloy, etc. (FIG. 9 (A)) or surrounded by a sheet of aluminum alloy (FIG. 9(B)). Areas shown in white represent highly pure aluminum and the areas of oblique lines show the aluminum alloy and/or alumite claddings.
- a metal wire of high tensile strength such as stainless steel wire or piano wire can be twisted together with or transposal for a part of the aluminum clad superconductors to reinforce the multiplex superconductor against said forces.
- the multiplex superconductor fabricated in accordance with the present invention can be widely applied to such electro-magnets as those which are used to produce high magnetic fields and are subjected to a very high Lorenty force, those which are used for maintaining a linear motor in floating condition and are required to be light weight, compact and capable of carrying a very high current density (In practice, the weight and the volume of a magnet constructed with the present superconductor can respectively be reduced to at least one sixth and one fourth those of the conventional magnet.), those used for MHD, particle acceleration, spark chambers and bubble chambers, those used for enclosing the plasma of a nuclear fusion reactor, those used for the electric lens of an electron microscope, those used for electric power transmission cable, etc.
- a method of fabricating an aluminum clad multiplex superconductor comprising the steps of inserting a pipe of highly pure aluminum into another pipe of aluminum alloy having more than 50 of Vickers hardness, inserting a strand of more than three superconductive twisted cylinders or wires into said pure aluminum pipe, wire-drawing an assembly of said pipe and said strand to form a unit superconductor, bundling and twisting or braiding a plurality of said unit superconductors to form a multiplex superconductor, and surrounding the outer surface of said multiplex superconductor with an aluminum alloy layer.
- a method of fabricating an aluminum clad multiplex superconductor as set forth in claim 1 further comprising the steps of providing an electric insulating layer on the outer surface of said aluminum alloy layer surrounding said multiplex superconductor by alumite treatment of the outer surface of said aluminum alloy layer.
Abstract
An aluminum clad multiplex superconductor comprises an aluminum alloy cladding and a multiplex superconductor inserted into the cladding and is constructed with a plurality of unit superconductors twisted or braided with each other, each of which unit superconductors is constructed with a strand of a plurality of superconductive wires, an intermediate aluminum layer and a relatively hard aluminum alloy layer surrounding the intermediate layer. The intermediate aluminum layer serves to prevent the flowing phenomenon during the withdrawing of the unit superconductor.
Description
United States Patent [191 Nomura et al.
[451 Dec. 18, 1973 METHOD OF FABRICATING AN ALUMINUM CLAD MULTIPLEX SUPERCONDUCTOR [75] Inventors: Harehiko Nomura; Susumu Shimamoto, both of Tokyo, Japan [73] Assignee: Agency of Industrial Science &
Technology, Tokyo, Japan 221 Filed: 0a. 24, 1972 [21] Appl. No.: 300,345
Related US. Application Data [62} Division of Ser. No. 212,199, Dec. 27, 1971, Pat. No.
[30] Foreign Application Priority Data Dec. 28, 1970 Japan 45/120120 [52] US. Cl. 29/599, 29/199, l74/DlG. 6 [51] Int. Cl l-l0lv 11/00 [58] Field of Search 29/599, 194, 199;
174/126 CP, DIG. 6; 335/216 [56] References Cited UNITED STATES PATENTS 3,708,606 1/1973 Shattes et a1. 174/126 CP Resistivity (n-cm) 12/1971 Roberts et al. 29/599 X 11/1971 Barber et al 29/599 Primary Examiner-Richard J. Herbst Assistant Examiner-Donald C. Reiley, lll Attorney-Kurt Kelman [5 7] ABSTRACT An aluminum clad multiplex superconductor comprises an aluminum alloy cladding and a multiplex superconductor inserted into the cladding and is constructed with a plurality of unit superconductors twisted or braided with each other, each of which unit superconductors is constructed with a strand of a pinrality of superconductive wires, an intermediate aluminum layer and a relatively hard aluminum alloy layer surrounding the intermediate layer. The intermediate aluminum layer serves to prevent the flowing phenomenon during the withdrawing of the unit superconductor.
4 Claims, 12 Drawing Figures 1 Temperature (10 PATENIEUUEF. 18 I975 3778. 95 SGIET 1 [F 5 Fig.1
Temperature (K) 1'0. 160360 Temperature (9K) PMENTEUUEC i 8 i975 3778.895
Fig-3 Current Density Relative to Core Wires (lo) (1 (Area Ratio) In Case of Fully Packed Solenoid A 8 F lg 4 E 9 N d 0/ "is 6 0 K a :2 g V qis/// 3 4 a 0 s? C)// a v I 2 i Al 99.9957, K
0 2'0 4'0 6'0 8 0 ic'iov Magnetic Flux (Kilogauss) Magneto Resistance Characteristics I ATENIEHUEI: 19 mm SHEET 30F 5 Reduction Factor (l) mmwc mI mmmx PATENTEUUEP. 18 I975 3.778.895 SHEET 50F 5 I -Fig.8(A)
I K 4 I i Copper Coating i LLWLVANJ 40KG 50A in Ic lOOpV .F i g 8(B) I 2/ Aluminum Coating Ic (N ot. less than Thermal Hysterisis Fig 9(B.)
Aluminum Alloy etc.
' area and for unit time becomes as follows,
METHOD OF FABRICATING AN ALUMINUM CLAD MULTIPLEX SUPERCONDUCTOR CROSS-REFERENCE TO RELATED APPLICATIONS I This is a division of copending application Ser. No. 212,199, filed Dec. 27, 1971, now US. Pat. No. 3,714,371.
The present invention relates to a method of fabricating an aluminum clad multiplex superconductor.
Many attempts have been made to obtain electrically and thermally stable properties in electro-magnets etc. which utilize superconductive wires, by providing copper cladding around the superconductive wires. The superconductor, in general, generates considerable heat upon spatial variations of magnetic flux applied thereto with time. If this heat is not discharged promptly to the exterior of the superconductor, the superconductor becomes very unstable, resulting in transition to the normal conductive state. With respect to this point, let us consider the thermal, electrical and magnetical properties of the superconductor when it is provided with copper and aluminum claddings respectively.
Firstly, considering the resistivities of aluminum and copper in the vicinity of liquid helium temperature (4.2K), the resistivity of aluminum is 3 X 10" cm) and that of copper is 1 2 X *(0 cm) as shown in FIG. 1. As to the thermal conductivities of aluminum and copper in the vicinity of 4.2K, they are 33('W/cml() and 3(W/cmK), respectively, as shown in FIG. 2'. Further, as to the thermal diffusion coeffi- .ciency Dth which is defined as (thermal conductivity (K)/specific heat (C) X specific gravity (d)), those of copper (OFHC, 99.99%) and aluminum (purer than 99.995%) are 0.12 X 10 and 43 X 10, respectively. Further, as to the magnetic diffusion coefficiency Dm which is defined as (electric resistance (R)/,u. (magnetic permeability)), that of copper is 1 2 X l0"/p. while that of aluminum is 3 X 10' 1.,,.
As will be clear from the above mentioned proper-' ties, since the amount of heat generation tends to increase with the increase of magnetic flux, the magnetic diffusion coefficiency acts to soften the flux variation. Assuming the relaxation time with respect to the flux change is put as r, the relation between Dm and r is represented by Dm l/r. Accordingly, the heat discharging ratio of aluminum to copper for unit cross Dth(Al)/1-(Al) yq Dth(A l Dm(A1)) Dth(C u )/1-(Cu) 8.95 Dth(Cu) Dm(Cu) 2.70 r gofso Since the heat and/or magnetic flux pass through the surface of the superconductor, the value of the ratio for unit coating thickness becomes V 3 (T- V6 0, that is, the heat discharging capability of aluminum is 5.5 7.7 times that of copper. This means that, when'highly, pure aluminum is used as a cladding material to obtain the same stability as that obtained by using a copper coating, an aluminum coating of about one thirtieth of thearea and about two elevenths of the thickness of the copper coating are sufficient. The lesser area and thickness provide the following advantages when a superconductor is multi-wound to form a solenoid.
FIG. 3 shows the current density for the total cross sectional area of the coated superconductor, in percentage, when a unit current I is flowing through the superconductive core line and the cross sectional area ratio of the core line to the coating metal is selected as l 2. Where the area ratio of the superconductive wire to a copper cladding is 1 4, it is clear from the above consideration that the ratio of the superconductive wire to the pure aluminum can be on the order of l 0.2 to obtain substantially the same stability as that obtained by the copper cladding. That is, when the pure aluminum is employed with the same sized core wire, the current density for the total cross sectional area of the superconductor can be increased from 17% to i.e., the current density becomes 4.4 times that obtained with the copper coating. in other words, if pure aluminum is used to obtain substantially the same stability as that obtained by the copper coating, the volume and weight of the solenoid respectively become one fourth and one sixth of those of the solenoid using copper coating. The effect of the higher magnetic field increasing the electric resistance, shown in FIG. 4, i.e.,
' the magneto-resistance effect of highly pure aluminum saturates at 0.6 X 10' (0 cm) at high magnetic field while that for copper rises to several times the value when no magnetic field is applied. That is, the aforementioned effect is improved for aluminum coating which it is degraded for copper coating.
When the outermost shell of aluminum clad superconductor is used as an anode in an electrolyte and an electric current is passed therethrough, aluminum oxide (electrical insulating film of very hard alumite) can be produced on the surface of the shell. This film has excellent voltage withstanding characteristics and the thermal conductivity thereof in the radial direction through the insulating film to helium, when compared with the conventional polyvinylformal coating on copper cladding, b'ecomes about one thousand times that of the conventional organic film since the thermal conductivity of the organic film is 0.00154 W/cmC while that of the alumite is 0.164 W/cmC, and the thickness of the alumite can be about one tenth of the organic film.
The reasons aluminum has not been employed in spite of the above described advantages over the conventional materials are as follows:
1. The mechanical strength, i.e., the tension strength of aluminum is 4kg/mm at 20C and considerably less than that of copper the value of which is 24ltg/mm at 20C even though the value of aluminum at 4.2K'becomes several times that at 20C.
2. Since the Vickers hardness of the superconductive wire (Nb Ti) is larger than as shown in H0. 5, there is a very large difference in hardness between the superconductive wire and highly pure aluminum and therefore a large strain may be produced by an electro-magnetic force applied thereto externally.
3. When a coating of highly pure aluminum is provided directly on a superconductive wire of, for example, Nb Ti alloy and the resulting superconductor is drawn, only the aluminum coating is stretched due to the extreme difference in hardness therebetween. That is, a flowing phenomenon may occur and the superconductive wire and the coating are not both deformed uniformly.
Therefore, a primary object of the present invention is to provide a method of fabricating an aluminum clad multiplex superconductor having the above described many advantages in actual use.
Other objects and advantages of the present invention will become apparent from the following description of embodiments of the present invention with reference to the attached drawings, in which;
FIG. I shows the temperature vs electric resistance characteristics of aluminum and copper,
FIG. 2 shows the temperature vs thermal conductivity characteristics of aluminum and copper,
FIG. 3 shows the current density, in percentage with respect to a unit current flowing through a superconductive wire when a superconductor constituted with a superconductive wire and a coating of either aluminum or copper is wound to form a fully packed solenoid with a cross sectional area ratio of the wire to the coating being 1 2 and the unit current flowing through the wire is averaged over the total cross sectional area of the wire and the coating,
FIG. 4 shows the magneto-resistance characteristics of aluminum and copper and FIG. 5 shows the relation between the workability (area reduction factor) and Vickers hardness;
FIG. 6(A) is a cross section of unit superconductor according to the present invention prior to the wiredrawing thereof;
FIG. 6(B) is a formation of twisted superconductive cylinders or wires;
FIG. 7 is a cross section of unit superconductor according to the present invention after the wire-drawing thereof;
FIGS. 8A and 8B show the current vs voltage characteristics (thermal hysterisis) of the present unit super conductor constituted with a superconductive wire having a copper and a aluminum coating respectively; and
FIGS. 9A and 9B show examples of the present aluminum clad multiplex superconductor constructed with a plurality of the unit superconductors.
Referring to the drawings, in particular, to FIG. 6, there is shown the fundamental structure of a unit superconductor ofthe present invention prior to the wiredrawing thereof, in which, in order to prevent the highly pure aluminum cladding from being stretched alone, a strand of three superconductive twisted cylinders or wires 1 is inserted into a pipe 2 of 99.99% aluminum and then the pipe 2 is inserted into anothrpipe 3 of aluminum alloy having a suitable hardness, to thereby constitute a triple layer structure. When the unit superconductor having this structure is drawn, the pure aluminum pipe 2 is deformed initially to fill up the screw gaps 4 with a portion of the volume of the pipe 2. In the next stage of the wire-drawing, the flowing between the aluminum pipe, the aluminum alloy pipe and the strand of superconductive wires can be re- .,..,stnctett.to less mamflmheu the P 3 is made of 2.5% Mg 0.25% Cr Al alloy, the Jamar the flowlig after the filling up of the gaps with the pure aluminum being determined by the hardness of the aluminum alloy. That is, after the filling up of the screw gaps 4 and in the intermediate stage of the wire-drawing, a hydrostatic pressure is applied to the outer surface of the superconductive strand causing a force to be exerted on the surface radially inwardly and thus a finished unit superconductor having a surface reduction factor on the order of 95% is obtained as shown in FIG. 7. The mechanical strength of aluminum alloy of this kind is 23kg/mm which is substantially the same as that of copper.
Experimental data of the unit superconductor having copper cladding and the present unit superconductor are shown in FIGS. 8(A) and 8(8) respectively. It will be clear from these data that the unit superconductor having a copper cladding has a thermal hysterisis while the present unit superconductor having aluminum cladding has no thermal hysterisis. In FIGS. 8(A) and 8(B), the data were obtained by standardizing the cross sectional area ratios.
The unit superconductor having aluminum cladding thus produced through the aforementioned process is furtherworked, in order to make it suitable for use in a large scale electromagnet. Thereafter a plurality of the present unit superconductors each having an aluminum cladding are bundled and twisted, or braided. In this case, in order to completely eliminate any electromagnetic coupling between the adjacent wires due to any change in magnetic flux density of the magnet, which may cause such unstable phenomena in the superconductor as flux-jumping, diamagnetic current, uniform current and eddy current, etc., the unit superconductors are, as required, twisted or braided after being treated to provide them with an alumite coating. Carrying out the alumite coating treatment prior to the twisting or braiding of the aluminum clad superconductors gives excellent effect in eliminating degradation (for example, current degradation or induced current degradation) due to transitional magnetic flux or alternating field flux. The multiplex superconductor may be inserted into a sheath of aluminum alloy such as 2.5 Mg 0.25 Cr Al or duralumin, etc. or may be surrounded by a sheet of such aluminum alloy, and then pressed or drawn, if necessary.
Since the present multiplex superconductor is made completely of non-organic materials it is clear that it can be heat-treated for a suitable time at a suitable temperature, after the mechanical process for forming the multiplex superconductor structure is completed and- /or the alumite forming process for the respective unit superconductors is performed. Since the melting point of the alumite layer is very high, no burning occurs and the mechanical strength thereof is considerably large. The aluminum clad multiplex superconductor fabricated in accordance with the present invention may be further suitably worked. For example, another electric insulator layer having reasonable mechanical strength may be provided electrically on the outer surface of the outermost aluminum sheath. The present multiplex superconductor having aluminum cladding can be easily wound as a solenoid.
FIGS. 9A and 9B are cross-sectional views of a multiplex superconductor fabricated in accordance with the present invention, the structure of the multiplex superconductor being constituted with a plurality of the unit superconductors each having the triple layer structure. The unit superconductors are inserted into a pipe or sheath of aluminum alloy, etc. (FIG. 9 (A)) or surrounded by a sheet of aluminum alloy (FIG. 9(B)). Areas shown in white represent highly pure aluminum and the areas of oblique lines show the aluminum alloy and/or alumite claddings.
In cases where the Lorenty force or other physical forces are very large as when the magnetic field is strong and/or electromagnetic is of huge scale, a metal wire of high tensile strength such as stainless steel wire or piano wire can be twisted together with or transposal for a part of the aluminum clad superconductors to reinforce the multiplex superconductor against said forces.
As described hereinbefore, the multiplex superconductor fabricated in accordance with the present invention can be widely applied to such electro-magnets as those which are used to produce high magnetic fields and are subjected to a very high Lorenty force, those which are used for maintaining a linear motor in floating condition and are required to be light weight, compact and capable of carrying a very high current density (In practice, the weight and the volume of a magnet constructed with the present superconductor can respectively be reduced to at least one sixth and one fourth those of the conventional magnet.), those used for MHD, particle acceleration, spark chambers and bubble chambers, those used for enclosing the plasma of a nuclear fusion reactor, those used for the electric lens of an electron microscope, those used for electric power transmission cable, etc.
What is claimed is:
l. A method of fabricating an aluminum clad multiplex superconductor comprising the steps of inserting a pipe of highly pure aluminum into another pipe of aluminum alloy having more than 50 of Vickers hardness, inserting a strand of more than three superconductive twisted cylinders or wires into said pure aluminum pipe, wire-drawing an assembly of said pipe and said strand to form a unit superconductor, bundling and twisting or braiding a plurality of said unit superconductors to form a multiplex superconductor, and surrounding the outer surface of said multiplex superconductor with an aluminum alloy layer.
2. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 1 further comprising the steps of providing an electric insulating layer on the outer surface of said aluminum alloy layer surrounding said multiplex superconductor by alumite treatment of the outer surface of said aluminum alloy layer.
3. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 1, further comprising the steps of providing an electric insulating layer on said unit superconductor by alumite treatment of the outer surface of said unit superconductor before the formation of said multiplex superconductor.
4. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 3, further comprising the steps of providing an electric insulating layer on the outer surface of said aluminum alloy layer surrounding said multiplex superconductor by alumite treatment of the outer surface of said aluminum alloy layer.
Claims (3)
- 2. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 1 further comprising the steps of providing an electric insulating layer on the outer surface of said aluminum alloy layer surrounding said multiplex superconductor by alumite treatment of the outer surface of said aluminum alloy layer.
- 3. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 1, further comprising the steps of providing an electric insulating layer on said unit superconductor by alumite treatment of the outer surface of said unit superconductor before the formation of said multiplex superconductor.
- 4. A method of fabricating an aluminum clad multiplex superconductor as set forth in claim 3, further comprising the steps of providing an electric insulating layer on the outer surface of said aluminum alloy layer surrounding said multiplex superconductor by alumite treatment of the outer surface of said aluminum alloy layer.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP45120120A JPS5036159B1 (en) | 1970-12-28 | 1970-12-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3778895A true US3778895A (en) | 1973-12-18 |
Family
ID=14778441
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00300345A Expired - Lifetime US3778895A (en) | 1970-12-28 | 1972-10-24 | Method of fabricating an aluminum clad multiplex superconductor |
Country Status (4)
Country | Link |
---|---|
US (1) | US3778895A (en) |
JP (1) | JPS5036159B1 (en) |
DE (1) | DE2165130B2 (en) |
FR (1) | FR2124675A5 (en) |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4078299A (en) * | 1972-09-11 | 1978-03-14 | The Furukawa Electric Co. Ltd. | Method of manufacturing flexible superconducting composite compound wires |
US4109374A (en) * | 1975-08-28 | 1978-08-29 | Aluminum Company Of America | Superconductor composite and method of making the same |
US4148129A (en) * | 1976-11-01 | 1979-04-10 | Airco, Inc. | Aluminum-stabilized multifilamentary superconductor and method of its manufacture |
US4171464A (en) * | 1977-06-27 | 1979-10-16 | The United State of America as represented by the U. S. Department of Energy | High specific heat superconducting composite |
US4200767A (en) * | 1976-01-13 | 1980-04-29 | Agency Of Industrial Science & Technology | Superconductor covered with reinforced aluminum matrix |
US4659007A (en) * | 1981-05-28 | 1987-04-21 | Agency Of Industrial Science & Technology | The method for producing an Al-stabilized superconducting wire |
US4739200A (en) * | 1986-04-23 | 1988-04-19 | The United States Of America As Represented By The Secretary Of The Air Force | Cryogenic wound rotor for lightweight, high voltage generators |
US4743713A (en) * | 1984-02-10 | 1988-05-10 | United States Department Of Energy | Aluminum-stabilized NB3SN superconductor |
US4757161A (en) * | 1985-11-12 | 1988-07-12 | Siemens Aktiengesellschaft | Composite superconducting conductor with several conductor strands and a method for manufacturing the same |
US4927985A (en) * | 1988-08-12 | 1990-05-22 | Westinghouse Electric Corp. | Cryogenic conductor |
US6428858B1 (en) | 2001-01-25 | 2002-08-06 | Jimmie Brooks Bolton | Wire for thermal spraying system |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59132511A (en) * | 1983-01-19 | 1984-07-30 | 住友電気工業株式会社 | Method of producing aluminum stabilized superconductive conductor |
DE3905805C2 (en) * | 1988-03-14 | 1993-10-14 | Nat Research Inst For Metals T | A method of making a wire-form superconducting composite article |
IT1266848B1 (en) * | 1994-05-31 | 1997-01-21 | Europa Metalli Lmi | METHOD FOR THE PRODUCTION OF SUPERCONDUCTIVE ELEMENTS SUITABLE FOR THE CONSTRUCTION OF CMS A MAGNETS FOR OTHER SIMILAR USES AND ELEMENT |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3618205A (en) * | 1967-04-27 | 1971-11-09 | Imp Metal Ind Kynoch Ltd | Method of fabricating a composite superconducting wire |
US3625662A (en) * | 1970-05-18 | 1971-12-07 | Brunswick Corp | Superconductor |
US3708606A (en) * | 1970-05-13 | 1973-01-02 | Air Reduction | Cryogenic system including variations of hollow superconducting wire |
-
1970
- 1970-12-28 JP JP45120120A patent/JPS5036159B1/ja active Pending
-
1971
- 1971-12-28 DE DE19712165130 patent/DE2165130B2/en not_active Ceased
- 1971-12-28 FR FR7147093A patent/FR2124675A5/fr not_active Expired
-
1972
- 1972-10-24 US US00300345A patent/US3778895A/en not_active Expired - Lifetime
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3618205A (en) * | 1967-04-27 | 1971-11-09 | Imp Metal Ind Kynoch Ltd | Method of fabricating a composite superconducting wire |
US3708606A (en) * | 1970-05-13 | 1973-01-02 | Air Reduction | Cryogenic system including variations of hollow superconducting wire |
US3625662A (en) * | 1970-05-18 | 1971-12-07 | Brunswick Corp | Superconductor |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4078299A (en) * | 1972-09-11 | 1978-03-14 | The Furukawa Electric Co. Ltd. | Method of manufacturing flexible superconducting composite compound wires |
US4109374A (en) * | 1975-08-28 | 1978-08-29 | Aluminum Company Of America | Superconductor composite and method of making the same |
US4285120A (en) * | 1976-01-13 | 1981-08-25 | Harehiko Nomura | Superconductor covered with reinforced aluminum matrix and method for manufacture thereof |
US4200767A (en) * | 1976-01-13 | 1980-04-29 | Agency Of Industrial Science & Technology | Superconductor covered with reinforced aluminum matrix |
US4148129A (en) * | 1976-11-01 | 1979-04-10 | Airco, Inc. | Aluminum-stabilized multifilamentary superconductor and method of its manufacture |
US4242536A (en) * | 1976-11-01 | 1980-12-30 | Airco, Inc. | Aluminum-stabilized multifilamentary superconductor |
US4171464A (en) * | 1977-06-27 | 1979-10-16 | The United State of America as represented by the U. S. Department of Energy | High specific heat superconducting composite |
US4659007A (en) * | 1981-05-28 | 1987-04-21 | Agency Of Industrial Science & Technology | The method for producing an Al-stabilized superconducting wire |
US4743713A (en) * | 1984-02-10 | 1988-05-10 | United States Department Of Energy | Aluminum-stabilized NB3SN superconductor |
US4757161A (en) * | 1985-11-12 | 1988-07-12 | Siemens Aktiengesellschaft | Composite superconducting conductor with several conductor strands and a method for manufacturing the same |
US4739200A (en) * | 1986-04-23 | 1988-04-19 | The United States Of America As Represented By The Secretary Of The Air Force | Cryogenic wound rotor for lightweight, high voltage generators |
US4927985A (en) * | 1988-08-12 | 1990-05-22 | Westinghouse Electric Corp. | Cryogenic conductor |
US6428858B1 (en) | 2001-01-25 | 2002-08-06 | Jimmie Brooks Bolton | Wire for thermal spraying system |
US6861612B2 (en) | 2001-01-25 | 2005-03-01 | Jimmie Brooks Bolton | Methods for using a laser beam to apply wear-reducing material to tool joints |
Also Published As
Publication number | Publication date |
---|---|
DE2165130B2 (en) | 1977-12-22 |
JPS5036159B1 (en) | 1975-11-21 |
DE2165130A1 (en) | 1972-07-20 |
FR2124675A5 (en) | 1972-09-22 |
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