US3346467A - Method of making long length superconductors - Google Patents
Method of making long length superconductors Download PDFInfo
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- US3346467A US3346467A US364176A US36417664A US3346467A US 3346467 A US3346467 A US 3346467A US 364176 A US364176 A US 364176A US 36417664 A US36417664 A US 36417664A US 3346467 A US3346467 A US 3346467A
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- 239000002887 superconductor Substances 0.000 title description 9
- 238000004519 manufacturing process Methods 0.000 title description 6
- 238000000576 coating method Methods 0.000 claims description 24
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 23
- 239000011248 coating agent Substances 0.000 claims description 23
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims description 18
- 238000000034 method Methods 0.000 claims description 14
- KAYZQFIFFVGBSR-UHFFFAOYSA-N bis(lambda2-stannanylidene)niobium Chemical compound [Nb].[Sn].[Sn] KAYZQFIFFVGBSR-UHFFFAOYSA-N 0.000 claims description 12
- 239000010955 niobium Substances 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 7
- 238000009792 diffusion process Methods 0.000 claims description 6
- 238000009713 electroplating Methods 0.000 claims description 6
- 238000005097 cold rolling Methods 0.000 claims description 5
- 238000007598 dipping method Methods 0.000 claims description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 12
- 229910052733 gallium Inorganic materials 0.000 description 12
- 229910052720 vanadium Inorganic materials 0.000 description 11
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 11
- CHLICZRVGGXEOD-UHFFFAOYSA-N 1-Methoxy-4-methylbenzene Chemical compound COC1=CC=C(C)C=C1 CHLICZRVGGXEOD-UHFFFAOYSA-N 0.000 description 7
- 238000007747 plating Methods 0.000 description 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 229910001134 stannide Inorganic materials 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 3
- 239000011261 inert gas Substances 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 238000007792 addition Methods 0.000 description 2
- 230000001464 adherent effect Effects 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 101150051314 tin-10 gene Proteins 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000000356 contaminant Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000001995 intermetallic alloy Substances 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 239000000523 sample Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229910001281 superconducting alloy Inorganic materials 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 238000001771 vacuum deposition Methods 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/08—Tin or alloys based thereon
-
- 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
- H10N60/0184—Manufacture or treatment of devices comprising intermetallic compounds of type A-15, e.g. Nb3Sn
-
- 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
- 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
- Y10S505/918—Mechanically manufacturing superconductor with metallurgical heat treating
- Y10S505/919—Reactive formation of superconducting intermetallic compound
- Y10S505/921—Metal working prior to treating
-
- 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
Definitions
- the present invention relates to superconductors, particularly in the form of elongated wires or ribbons which can be wound into solenoids or used :as long transmission lines.
- the present invention contemplates the passage of a niobium wire through a tin bath or a vanadium wire through a gallium bath to form a primer coat which is uniform and highly adherent. Then the coat is adjusted to a desired thickness by plating. The wire is then cold rolled to flatten it to the form of a ribbon with rounded edges. Such a ribbon is readily coated with plastic insulation compared to prior art ribbons with sheared edges. The final ribbon form is particularly suitable because it has greater resistance to certain modes of field penetration than a wire. Yet, in the present process the ribbon is not formed until after coating and plating steps which might tend to create twists in a ribbon and pose other handling problems.
- the invention accordingly comprises an improved process of forming superconductive niobium stannide and vanadium gallide superconductors and the products of said process, characterized by an improved structure.
- FIG. 1 is a schematic view of a vacuum coating apparatus
- FIG. 2 is a schematic, cross-section of a tin coated niobium wire
- FIG. 3 is a schematic cross-section of a flattened stannide-coated niobium wire.
- molten tin 10 is held in a graphite pot 12 and heated by a heater to a temperature of 700 C.-900 C., temperatures above 750 C. being preferred.
- a heater 22 is used to pretreat the wire to a dull red to clean the wire before dipping. If the bath temperature is 800-900" C., preheating is unnecessary.
- Niobium wire, .0005 to .025 in diameter is fed from a roll 18 through the-molten tin at a rate of about feet per minute for a residence time in the molten tin of less than one second. It the bath temperature is 700-800" C., the wire is fed at 50-100 feet per minute.
- the wire is fed at 100-200 feet per minute.
- the coated niobium wire is wound into roll 20.
- This coated niobium wire shown in cross-section in FIG. 2 comprises a uniform, bright adherent tin coating with a thickness of about .0001 inch.
- the coating process is carried out in a vacuum chamber 221 evacuated by convention vacuum pumping system 26 to a pressure of less than .0001 mm. Hg.
- the coating could also be carried out under an atmosphere of an inert gas with similar purity.
- the chamber 22 is air released and the coated wire is passed through an electroplat'ng bath to adjust the final thickness of the coating by addition or removal of tin.
- the initial dip coating serves as an excellent primer coat to insure ease of plating and uniformity of plating thickness.
- the coated wire is then cold rolled flat to a ribbon form having a thickness of about one-tenth to one-third the original wire diameter.
- the ribbon is then treated with a separating agent, and coiled into a tight spool.
- the spool is heat treated in a mufile furnace, under an atmosphere of purified argon, at 950 C. for 1-4 hours.
- the muffie is water cooled and cut open.
- the spool can be unwound and the ribbon can be subsequently wound into a solenoid, rotor coil, or other desired shape.
- the ribbon will have the cross-section form indicated in FIG. 3.
- the central core of niobium will be free of substantial diffusion and the coating will comprise an intermetallic alloy having the characteristic Nb Sn crystal structure.
- the edges of the final ribbon are rounded. This avoids the possibility of cutting through an interleaved plastic insulation foil when winding solenoids. It also makes it possible to directly coat the ribbon with a plastic insulation by passing through a bath o through extrusion or heat shrinking techniques. The plastic adheres easily to the rounded edge.
- Example Tin (Vulcan extra pure-99.999%) was melted and maintained at 750 C. in a graphite pot in a vacuum chamber using the procedure outlined above. A spool of 0.010" diameter niobium wire was unwound in the chamber, fed through the molten tin bath and rewound.
- the ribbons were bent around test probes and current was passed through them while they Were under liquid helium temperatures and external magnetic fields, applied perpendicular to the widths of the ribbon.
- the critical current of the ribbons were comparable to those obtain-able from clad ribbons of comparable size.
- niobium wire Very long lengths of niobium wire can be obtained in comparison to available lengths of ribbon for-med directly from niobium ingots or powder compacts.
- the present invention has particular application to requirements where lengths of over 3,000 feet are necessary.
- wire lengths of 3,0005,000 feet can be welded end to end to form Wires in excess of 30,000 feet.
- the composite wire can be coated, as disclosed, with assur-ance of continuity and uniformity of coating. After electroplating, the composite wire can be rolled to produce a straight ribbon suitable for heat treating and subsequent fabrication into solenoids and the like, with or Without insulation. 7
- the process of the present invention can also be applied to the production of vanadium gallide diffusion layers on a vanadium ribbon. This is particularly important since gallium is more difiicult to handle than tin and the vanadium gallide superconducting alloy is more brittle than the niobium stannide.
- Vanadium wire is treated in a gallium bath and then plated .as in the tin coating of wire. Bath temperatures of 700-800 C. are used for the gallium bath. An important difference is that the vanadium wire is removed to a protective atmosphere of argon or nitrogen after dipping to form the primer coat of gallium. Exposure to contaminant gases such as oxygen is avoided in transferring the vanadium wire from the molten gallium bath to the plating bath. During the rolling step, the rolls are water cooled to remove heat from the gallium coating.
- the vanadium and gallium can be doped with small amounts of other materials such as silicon to form ternary vanadium gallide alloys in the diffusion coating.
- the heat treating step is carried out as described above with respect to niobium stannide.
- a method of preparing a superconductive niobium stannide ribbon comprising the steps of continuously feeding a niobium wire having a length in excess of 3,000 feet through a molten tin bath maintained at a temperature between 700 C. and 900 C. under a contaminant-free atmosphere whereby the wire is uniformly coated with tin, subsequently cold rolling the wire to flatten it to a ribbon having a thickness between and /3 the original wire diameter and rounded edges, heat treating the ribbon to react the tin coating with the niobium ribbon to form a diffusion layer of niobium stannide at the surface of the ribbon whereby the ribbon demonstrates a critical temperature of about 18 K. wherein the tin coated wire is subjected to an elecroplating step after dipping to control the final thickness of the coating.
- niobium stannide at the ribbon surface having a thickness of 0.1-0.5 mil, whereby a long ductile ribbon having a uniform coating of superconductive niobium stannide having a critical temperature of about 18 W. is produced.
- a method of preparing a superconductive vanadium gallide ribbon comprising the steps of feeding a vanadium wire at least 5 mils in diameter through a molten gallium bath maintained at a temperature between 700 C. and 900 C. under vacuum to provide a uniform primer coat of gallium on said vanadium wire, then feeding said coated wire to a protective atmosphere of inert gas, subsequently electroplating gallium on said coated wire to build up the coating thickness to 0.5-1 mil, the electroplating being ca-rried out under a protective atmosphere of inert gas, subsequently cold rolling said plated wire to form a ribbon having rounded edges and a thickness less than half the wire diameter, removing heat from the wire during the cold rolling, then heat treating the plated ribbon to form a diffusion coating of vanadium gallide having a critical temperature of about 16.5 W.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Manufacturing & Machinery (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Coating With Molten Metal (AREA)
Description
Oct. 10, 1967 L. R. ALLEN METHOD OF MAKING LONG LENGTH SUPERCONDUCTORS Filed May 1, 1964 United States Patent 3,346,467 METHCD OF MAKING LONG LENGTH SUPERCONDUCTORS Lloyd R. Allen, Belmont, Mass., assignor to National Research Corporation, Cambridge, Mass., a corporation of Massachusetts Filed May 1, 1964, Ser. No. 364,176 4 Claims. (Cl. 204-37) ABSTRACT OF THE DISCLOSURE Long lengths of hard superconductor-niobium stannide or vanadium gallideare prepared by running a long wire of the niobium or vanadium through a molten bath of the tin or gallium, respectively, very rapidly to form a thin coating, then electroplating to build up the coating to a desired thickness, then flattening the wire to ribbon form and finally heating for diifusion.
The present invention relates to superconductors, particularly in the form of elongated wires or ribbons which can be wound into solenoids or used :as long transmission lines.
A principal difficulty in the commercial applicationof superconductivity is that the materials having the best electrical properties under high magnetic fieldsniobium stannide and vanadium gallideare very difiicult to fabricate on a production line basis. Several new methods have been devised for overcoming these difiiculties, with respect to niobium stannide; these are described in US. Patent 3,124,455, to Kunzler and Buehler, copending application S.N. 133,653, of Allen and Stautfer, and now abandoned, and copending application S.N. 207,320, of Allen, Das and Stauffer, now US. Patent No. 3,218,693.
It is the principal object of the present invention to provide a new method of forming niobium stannide superconductors which is particularly-suitable for very long lengths.
It is a further object of the invention to provide a long superconductor which is easy to insulate.
It is a further object of the invention to provide a process of making a niobium stannide superconductor which has improved reliability and economy compared to the prior :art processes.
Finally, it is an object of the invention to provide a manufacturing process for long superconductors comprising vanadium gallide.
In general, the present invention contemplates the passage of a niobium wire through a tin bath or a vanadium wire through a gallium bath to form a primer coat which is uniform and highly adherent. Then the coat is adjusted to a desired thickness by plating. The wire is then cold rolled to flatten it to the form of a ribbon with rounded edges. Such a ribbon is readily coated with plastic insulation compared to prior art ribbons with sheared edges. The final ribbon form is particularly suitable because it has greater resistance to certain modes of field penetration than a wire. Yet, in the present process the ribbon is not formed until after coating and plating steps which might tend to create twists in a ribbon and pose other handling problems.
The invention accordingly comprises an improved process of forming superconductive niobium stannide and vanadium gallide superconductors and the products of said process, characterized by an improved structure.
For a more detailed explanation of the invention, as applied in a preferred embodiment, reference should be had to the following discussion, taken in connection with the accompanying drawings wherein:
Patented Oct. 10, 1967 "ice FIG. 1 is a schematic view of a vacuum coating apparatus;
FIG. 2 is a schematic, cross-section of a tin coated niobium wire; and
FIG. 3 is a schematic cross-section of a flattened stannide-coated niobium wire.
Referring now to FIG. 1, molten tin 10 is held in a graphite pot 12 and heated by a heater to a temperature of 700 C.-900 C., temperatures above 750 C. being preferred. When the tin temperature is less than 800 C., a heater 22 is used to pretreat the wire to a dull red to clean the wire before dipping. If the bath temperature is 800-900" C., preheating is unnecessary. Niobium wire, .0005 to .025 in diameter is fed from a roll 18 through the-molten tin at a rate of about feet per minute for a residence time in the molten tin of less than one second. It the bath temperature is 700-800" C., the wire is fed at 50-100 feet per minute. If the bath temperature is 800900 C., the wire is fed at 100-200 feet per minute. The coated niobium wire is wound into roll 20. This coated niobium wire shown in cross-section in FIG. 2 comprises a uniform, bright adherent tin coating with a thickness of about .0001 inch.
The coating process is carried out in a vacuum chamber 221 evacuated by convention vacuum pumping system 26 to a pressure of less than .0001 mm. Hg. The coating could also be carried out under an atmosphere of an inert gas with similar purity.
After the coating step, the chamber 22 is air released and the coated wire is passed through an electroplat'ng bath to adjust the final thickness of the coating by addition or removal of tin. The initial dip coating serves as an excellent primer coat to insure ease of plating and uniformity of plating thickness. The coated wire is then cold rolled flat to a ribbon form having a thickness of about one-tenth to one-third the original wire diameter.
The ribbon is then treated with a separating agent, and coiled into a tight spool. The spool is heat treated in a mufile furnace, under an atmosphere of purified argon, at 950 C. for 1-4 hours. At the end of the heating step, the muffie is water cooled and cut open. The spool can be unwound and the ribbon can be subsequently wound into a solenoid, rotor coil, or other desired shape. At this stage the ribbon will have the cross-section form indicated in FIG. 3. The central core of niobium will be free of substantial diffusion and the coating will comprise an intermetallic alloy having the characteristic Nb Sn crystal structure. Other elements may be substituted for tin in the lattice, as taught in the work of Saur, copending application S.N. 307,896, filed Sept. 10, 1963, now Patent No. 3,244,490. This can be accomplished by dissolving alloying additions in the molten tin 10 (FIG. 1). It is also possible to strengthen the niobium substrate without adversely affecting the formation of an intermetallic superconductive coating or the ductility of the final coated ribbon. For instance, 15% by weight of zirconium or titanium can be alloyed with niobium informing the original wire 16 supplied on spoon 18.
Referring again to FIG. 3, it is seen that the edges of the final ribbon are rounded. This avoids the possibility of cutting through an interleaved plastic insulation foil when winding solenoids. It also makes it possible to directly coat the ribbon with a plastic insulation by passing through a bath o through extrusion or heat shrinking techniques. The plastic adheres easily to the rounded edge.
Example Tin (Vulcan extra pure-99.999%) was melted and maintained at 750 C. in a graphite pot in a vacuum chamber using the procedure outlined above. A spool of 0.010" diameter niobium wire was unwound in the chamber, fed through the molten tin bath and rewound.
rate pieces were then flattened by a rolling mill to produce ribbons about .0025" thick by .045 wide with rounded edges. The ribbon sections were straight.
After heat treatment, the ribbons were bent around test probes and current was passed through them while they Were under liquid helium temperatures and external magnetic fields, applied perpendicular to the widths of the ribbon. The critical current of the ribbons were comparable to those obtain-able from clad ribbons of comparable size.
Very long lengths of niobium wire can be obtained in comparison to available lengths of ribbon for-med directly from niobium ingots or powder compacts. Thus, the present invention has particular application to requirements where lengths of over 3,000 feet are necessary. Where necessary, wire lengths of 3,0005,000 feet can be welded end to end to form Wires in excess of 30,000 feet. The composite wire can be coated, as disclosed, with assur-ance of continuity and uniformity of coating. After electroplating, the composite wire can be rolled to produce a straight ribbon suitable for heat treating and subsequent fabrication into solenoids and the like, with or Without insulation. 7
The process of the present invention can also be applied to the production of vanadium gallide diffusion layers on a vanadium ribbon. This is particularly important since gallium is more difiicult to handle than tin and the vanadium gallide superconducting alloy is more brittle than the niobium stannide.
Vanadium wire is treated in a gallium bath and then plated .as in the tin coating of wire. Bath temperatures of 700-800 C. are used for the gallium bath. An important difference is that the vanadium wire is removed to a protective atmosphere of argon or nitrogen after dipping to form the primer coat of gallium. Exposure to contaminant gases such as oxygen is avoided in transferring the vanadium wire from the molten gallium bath to the plating bath. During the rolling step, the rolls are water cooled to remove heat from the gallium coating.
The vanadium and gallium can be doped with small amounts of other materials such as silicon to form ternary vanadium gallide alloys in the diffusion coating. The heat treating step is carried out as described above with respect to niobium stannide.
What is claimed is:
1. A method of preparing a superconductive niobium stannide ribbon comprising the steps of continuously feeding a niobium wire having a length in excess of 3,000 feet through a molten tin bath maintained at a temperature between 700 C. and 900 C. under a contaminant-free atmosphere whereby the wire is uniformly coated with tin, subsequently cold rolling the wire to flatten it to a ribbon having a thickness between and /3 the original wire diameter and rounded edges, heat treating the ribbon to react the tin coating with the niobium ribbon to form a diffusion layer of niobium stannide at the surface of the ribbon whereby the ribbon demonstrates a critical temperature of about 18 K. wherein the tin coated wire is subjected to an elecroplating step after dipping to control the final thickness of the coating.
2. The method of claim 1 wherein said stannide coated ribbon is further coated with a plastic to form an insula-' stannide ribbon comprising the steps of precleaning and continuously feeding a niobium wire having a length in excess of 3,000 feet through a molten tin bath maintained at a temperature of between 700 C.800 C. at a rate between 50100 feet per minute to provide a residence time in the molten bath of less than one second, during which time a thin coating of tin is formed on the wire, the said precleaning and feeding through a molten bath being conducted under vacuum, subsequently electroplating an additional tin coating on the dip coated wire to provide a uniform tin coating with a thickness on the order of one mil, cold rolling said wire to a ribbon having a thickness less than half the original wire diameter, and having rounded edges, heat treating the cold formed ribbon under an inert atmosphere at a temperature of 900- 1000 C. for one to four hours to form a diifusion layer of niobium stannide at the ribbon surface having a thickness of 0.1-0.5 mil, whereby a long ductile ribbon having a uniform coating of superconductive niobium stannide having a critical temperature of about 18 W. is produced.
4. A method of preparing a superconductive vanadium gallide ribbon comprising the steps of feeding a vanadium wire at least 5 mils in diameter through a molten gallium bath maintained at a temperature between 700 C. and 900 C. under vacuum to provide a uniform primer coat of gallium on said vanadium wire, then feeding said coated wire to a protective atmosphere of inert gas, subsequently electroplating gallium on said coated wire to build up the coating thickness to 0.5-1 mil, the electroplating being ca-rried out under a protective atmosphere of inert gas, subsequently cold rolling said plated wire to form a ribbon having rounded edges and a thickness less than half the wire diameter, removing heat from the wire during the cold rolling, then heat treating the plated ribbon to form a diffusion coating of vanadium gallide having a critical temperature of about 16.5 W.
References Cited UNITED STATES PATENTS 2,802,897 8/1957 Hurd et a1. 174110 3,218,693 11/1965 Allen et .al 29-155.5 3,251,715 5/1966 Miles et a1. 117--212 3,252,832 5/1966 Saur 117-212 JOHN H. MACK, Primary Examiner.
W. VAN SISE, Assistant Examiner.
Claims (1)
1. A METHOD OF PREPARING A SUPECONDUCTIVE NIOBIUM STANNIDE RIBBON COMPRISING THE STEPS OF CONTINUOUSLY FEEDING A NIOBIUM WIRE HAIVNG A LENGTH IN EXCESS OF 3,000 FEET THROUGH A MOLTEN TIN BATH MAINTAINED AT A TEMPERATURE BETWEEN 700*C. AND 900*C. UNDER A CONTAMINANT-FREE ATMOSPHERE WHEREBY THE WIRE IS UNIFORMLY COATED WITH TIN, SUBSEQUENTLY COLD ROLLING THE WIRE TO FLATTEN IT TO A RIBBON HAVING A THICKNESS BETWEEN 1/10 AND 1/3 THE ORIGINAL WIRE DIAMETER AND ROUNDED EDGES, HEAT TREATING THE RIBBON TO REACT THE TIN COATING WITH THE NIOBIUM RIBBON TO FORM A DIFFUSION LAYER OF NIOBIUM STANNIDE AT THE SURFACE OF THE RIBBON WHEREBY THE RIBBON DEMONSTRATES A CRITICAL TEMPERATURE OF ABOUT 18*K. WHEREIN THE TINE COATED WIRE IS SUBJECTED TO AN ELECTROPLATING STEP AFTER DIPPING TO CONTROL THE FINAL THICKNESS OF THE COATING.
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Application Number | Priority Date | Filing Date | Title |
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US364176A US3346467A (en) | 1964-05-01 | 1964-05-01 | Method of making long length superconductors |
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US364176A US3346467A (en) | 1964-05-01 | 1964-05-01 | Method of making long length superconductors |
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US3346467A true US3346467A (en) | 1967-10-10 |
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US364176A Expired - Lifetime US3346467A (en) | 1964-05-01 | 1964-05-01 | Method of making long length superconductors |
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US (1) | US3346467A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3533919A (en) * | 1965-02-24 | 1970-10-13 | Nat Res Dev | Manufacture of superconductors |
US4008102A (en) * | 1973-11-02 | 1977-02-15 | Siemens Aktiengesellschaft | Method of the manufacture of a superconductor with a layer of the A-15 phase of the system Nb-Al-Si |
US4018942A (en) * | 1973-11-02 | 1977-04-19 | Siemens Aktiengesellschaft | Method for the manufacture of a superconductor with a layer of the A-15 phase of the system Nb-Al or Nb-Al-Ge |
US4081573A (en) * | 1975-07-21 | 1978-03-28 | Siemens Aktiengesellschaft | Method for preparing superconductive Nb3 Sn layers on niobium surfaces for high-frequency applications |
EP0690143A1 (en) * | 1994-06-27 | 1996-01-03 | General Electric Company | Method of coating niobium foil |
EP0691691A1 (en) * | 1994-07-05 | 1996-01-10 | General Electric Company | Method for making triniobium tin superconductor |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2802897A (en) * | 1952-07-18 | 1957-08-13 | Gen Electric | Insulated electrical conductors |
US3218693A (en) * | 1962-07-03 | 1965-11-23 | Nat Res Corp | Process of making niobium stannide superconductors |
US3251715A (en) * | 1961-06-13 | 1966-05-17 | Little Inc A | Method of forming a laminar superconductor |
US3252832A (en) * | 1962-07-10 | 1966-05-24 | Bbc Brown Boveri & Cie | Method of making magnetically hard superconducting wires |
-
1964
- 1964-05-01 US US364176A patent/US3346467A/en not_active Expired - Lifetime
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2802897A (en) * | 1952-07-18 | 1957-08-13 | Gen Electric | Insulated electrical conductors |
US3251715A (en) * | 1961-06-13 | 1966-05-17 | Little Inc A | Method of forming a laminar superconductor |
US3218693A (en) * | 1962-07-03 | 1965-11-23 | Nat Res Corp | Process of making niobium stannide superconductors |
US3252832A (en) * | 1962-07-10 | 1966-05-24 | Bbc Brown Boveri & Cie | Method of making magnetically hard superconducting wires |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3533919A (en) * | 1965-02-24 | 1970-10-13 | Nat Res Dev | Manufacture of superconductors |
US4008102A (en) * | 1973-11-02 | 1977-02-15 | Siemens Aktiengesellschaft | Method of the manufacture of a superconductor with a layer of the A-15 phase of the system Nb-Al-Si |
US4018942A (en) * | 1973-11-02 | 1977-04-19 | Siemens Aktiengesellschaft | Method for the manufacture of a superconductor with a layer of the A-15 phase of the system Nb-Al or Nb-Al-Ge |
US4081573A (en) * | 1975-07-21 | 1978-03-28 | Siemens Aktiengesellschaft | Method for preparing superconductive Nb3 Sn layers on niobium surfaces for high-frequency applications |
EP0690143A1 (en) * | 1994-06-27 | 1996-01-03 | General Electric Company | Method of coating niobium foil |
EP0691691A1 (en) * | 1994-07-05 | 1996-01-10 | General Electric Company | Method for making triniobium tin superconductor |
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