US3243871A - Method of making ductile superconductors - Google Patents
Method of making ductile superconductors Download PDFInfo
- Publication number
- US3243871A US3243871A US301494A US30149463A US3243871A US 3243871 A US3243871 A US 3243871A US 301494 A US301494 A US 301494A US 30149463 A US30149463 A US 30149463A US 3243871 A US3243871 A US 3243871A
- Authority
- US
- United States
- Prior art keywords
- tube
- ribbon
- alloy
- sheath
- core
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- 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
-
- 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
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/9265—Special properties
- Y10S428/93—Electric superconducting
-
- 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
- Y10S505/80—Material per se process of making same
- Y10S505/812—Stock
- Y10S505/813—Wire, tape, or film
-
- 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
- Y10S505/80—Material per se process of making same
- Y10S505/815—Process of making per se
-
- 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
- Y10S505/80—Material per se process of making same
- Y10S505/815—Process of making per se
- Y10S505/818—Coating
-
- 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
- Y10S505/912—Metal founding
- Y10S505/913—Casting process
- Y10S505/915—Making composite product
-
- 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
-
- 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
-
- 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
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49988—Metal casting
-
- 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
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
Definitions
- FIG. 1 is a schematic view of the first step of the process of the invention
- FIG. 2 is a cross-section of the product of the invention at an early stage of treatment
- FIG. 3 is a cross-section of the product at a later stage 5' 7 of treatment
- FIG. 4 is a schematic view of a still further treatment
- FIG. 5 is a cross section of'the product after the treatment indicated in FIG. 4, the section being typical of any cross-section along the length of the product except for the ends thereof;
- FIGS. 6 and 7 are typical cross-sections of the product after further treatments
- FIG. 8 is a block diagram of final treatments
- FIG. 9 shows the resultant product in cross-section.
- Steps 1 and 4 and the anneals of Step 3 are carried out m a vacuum furnace.
- the temperature of the niobium tube and molten tin in Step 4 should be maintained at about 300 C., after initially annealing the niobium at higher temperature, with the vacuum furnace method of Allen, Das andStaufler, disclosed in the copending United States applications, S.N. 193,281 filed May 8,1962 and S.N. 278,723, filed May 7, 1963.
- This The ingot 20 is pressed into the form of a disk as shown in FIG. 2.
- the disk is spun into the form of a tube 24, shown in FIG. 3, having a inch outer diameter and .040 inch wall thickness.
- the tube 24 is thus of high purity and free of seams or other join
- the niobium tube 24 is returned to the vacuum chamber 10. where it is annealed under a vacuum of 10- mm. V C. and 1400 C. for one hour.
- the chamber is provided-with a crucible 6 and crucible pivots 28. Tin is melted in the crucible at 300 C. and under a vacuum of 10- mm. Hg. Then :he crucible is tilted to vacuum cast the tin into tube 24. Tube 24 is cooled and then removed from the furnace.
- the resultant product is a cylinder 32 comprising a niobium sheath 24 and a solid tin core 30, as shown in FIG. 5.
- Cylinder 32 is capped by crimping the open end. Then cylinder 32 is rolled and drawn down to wire size to form the wire 34 of FIG. 6. The rolling and drawing is carried out in accord with the teachings of Allen, Das and Stautfer in their US. patent application, S.N. 193,281, filed May 8, 1962.
- the diameter of the resultant wire 34 is on the order of .010 to .020 inch after a reduction of cross-section area in excess of 30:1. The extensive reduction creates new surface at the niobium-tin interface, thus dispersing the residual contaminants therein to improve the cleanliness of the interface.
- Wire 34 is flattened between pressure rolls to form the ribbon 36 of FIG. 7.
- Ribbon 36 is -then drawn to form a reduced thickness ribbon which is less than about .002 inch thick.
- the ribbon comprises an unbroken, sea-mless sheath of niobium surrounding a flattened core
- the ribbon is then fabricated into a solenoid according to the steps outlined in FIG. 8.
- the heating is carried out between 900 C. and 1200 C. for /z to two hours.
- the clean-niobium surface is readily wettable by molten tin and the reaction proceeds rapidly and uniformly.
- the ribbon is removed from the furnace and cooled in air.
- the ribbon may then be insulated by a conventional plastic whereas the insulation of prior art core wires would be a special high temperature ceramic insulation because the prior art cores must be insulated before heat treatment.
- FIG. 9 shows the ribbon at the end of the heat treatment step.
- the sheath 24 then comprises a diffusion layer 40 of Nb Sn at the inner surface of the sheath.
- the core 30 comprises residual tin and small void spaces. Essentially, no niobium or Nb Sn particlesare found in the core, apart from the niobium and Nb Sn trapped in the sheaths inner diffusion layer.
- the present invention is particularly applicable to vanadium gallium which can only be formed with great difiiculty in prior art core wires and is a very brittle compound.
- the tube 24 of FIG. 4 (which would be vanadium) should be capped by inserting a stopper in the open end of the tube after pouring the gallium and indenting the tube into depressions in the stopper. This will hold the low melting gallium during the drawing process.
- the process of the present invention guards the highly reactive gallium from contamination.
- a principal advantage of the present invention is that the ribbon is heat treated before insulating and forming into a coil. It is not necessary to apply an expensive ceramic insulation as in prior art core wires. A cheap plastic insulation can be used.
- a related advantage is thatthe reactive tin or gallium or indium, etc. is trapped inside the ribbon.
- the ribbon can be wound into a compact spiral, inserted into a furnace muflie, and then heat treated and readily unwound after heat treatment.
- a ribbon with the low melting component on an outer surface would pose problems of adjacent turns sticking if wound into a tight spiral and heated.
- the above-described preferred embodiment has several advantages over the prior art.
- the flattened form of the final product permits a higher ratio of length of Nb Sn diffusion layer to total cross-section area than a round wire because the geometry of a ribbon is inherently more favorable and because ribbons can be cold worked to smaller thicknesses more readily than wires.
- the ribbon form inhibits the formation of voids during the heat treatment and is a more favorable shape than round wire for winding coils.
- the wire 34 comprising a soft core 30 of tin and no hard materials, is readily flattened.
- the process permits the use of high purity sheath material and vacuum degassed core material.
- the clean core material is degassed while held in crucible 26 and while being transferred from vacuum degassing crucible 26 to tube 24.
- the tin is then trapped in the tube without exposure to oxidizing agents and other contaminants which would limit the effectiveness of the subsequent heat treatment.
- the present invention offers the further advantage of confining the superconductive alloy to a thin diffusion layer which permits bending of the finished product and entails shorter times of heat treatment compared to the '20 hour heat treatments needed for prior art core wires.
- a method of making ductile superconductors providing high current densities through an internal layer of an intermetallic alloy hard superconductor comprising the steps of placing a tube made of a higher melting component of the alloy in a non-oxidizing atmosphere and annealing it, maintaining the lower melting point component of the alloy in a non-oxidizing atmosphere in molten state to degas it, pouring the molten metal into the tube while maintaining their temperatures below the reaction temperature at which their brittle intermetallic alloys are formed, cooling the tube, cold working the tube down to wire size to extend the interface between the core and sheath thereby making the sheath readily wettable by the core materials, cold rolling the wire to flatten it to ribbon form and to further reduce its cross section thickness after flattening the wire to ribbon form, and then heating the ribbon at the reaction temperature to form the desired intermetallic, hard superconductor alloy as a diffusion layer inside the ribbon.
Description
April 5, 1966 E. J. SAUR METHOD OF MAKING DUCTILE SUPERCONDUOTORS Filed Aug. 12, 1963 WIND INTO Fig.8
INVENTOR. EU GEN J. SAUR United States Patent Ofiice 3,243,871 Patented Apr. 5, 1966 3,243,871 NLETHOD F AKING DUCTILE SUPERCONDUCTORS Eugen J. Saur, Giessen, Germanyg assignor to National Research Corporation, Cambridge, Mass., a corporation of Massachusetts Filed, Aug. 12, 1963, Ser. No. 301,494
Claims. (Cl. 29-1555) The invention is applicable to hard superconductor alloys comprising, as a higher melting point component,
indium.
For a fuller understanding of the nature and objects of the Invention, reference should be had to the following detailed description in conjunction with the accompanying FIG. 1 is a schematic view of the first step of the process of the invention;
FIG. 2 is a cross-section of the product of the invention at an early stage of treatment; 1
FIG. 3 is a cross-section of the product at a later stage 5' 7 of treatment; 1
FIG. 4 is a schematic view of a still further treatment; FIG. 5 is a cross section of'the product after the treatment indicated in FIG. 4, the section being typical of any cross-section along the length of the product except for the ends thereof;
FIGS. 6 and 7 are typical cross-sections of the product after further treatments;
I FIG. 8 is a block diagram of final treatments; and
FIG. 9 shows the resultant product in cross-section.
(2) Pressing into a disk.
(3) Spinning the disk into a tube (several passes with vacuum annealing after each pass).
(4) Vacuum casting tin into the tube.
(5) Furnace cooling.
(6) Rolling and drawing the tube down to wire.
Conventional metallurgical processes are utilized in all the steps. Steps 1 and 4 and the anneals of Step 3 are carried out m a vacuum furnace. The temperature of the niobium tube and molten tin in Step 4 should be maintained at about 300 C., after initially annealing the niobium at higher temperature, with the vacuum furnace method of Allen, Das andStaufler, disclosed in the copending United States applications, S.N. 193,281 filed May 8,1962 and S.N. 278,723, filed May 7, 1963. This The ingot 20 is pressed into the form of a disk as shown in FIG. 2. The disk is spun into the form of a tube 24, shown in FIG. 3, having a inch outer diameter and .040 inch wall thickness. The tube 24 is thus of high purity and free of seams or other join The niobium tube 24 is returned to the vacuum chamber 10. where it is annealed under a vacuum of 10- mm. V C. and 1400 C. for one hour. The chamber is provided-with a crucible 6 and crucible pivots 28. Tin is melted in the crucible at 300 C. and under a vacuum of 10- mm. Hg. Then :he crucible is tilted to vacuum cast the tin into tube 24. Tube 24 is cooled and then removed from the furnace. The resultant product is a cylinder 32 comprising a niobium sheath 24 and a solid tin core 30, as shown in FIG. 5. Cylinder 32 is capped by crimping the open end. Then cylinder 32 is rolled and drawn down to wire size to form the wire 34 of FIG. 6. The rolling and drawing is carried out in accord with the teachings of Allen, Das and Stautfer in their US. patent application, S.N. 193,281, filed May 8, 1962. The diameter of the resultant wire 34 is on the order of .010 to .020 inch after a reduction of cross-section area in excess of 30:1. The extensive reduction creates new surface at the niobium-tin interface, thus dispersing the residual contaminants therein to improve the cleanliness of the interface.
FIG. 9 shows the ribbon at the end of the heat treatment step. The sheath 24 then comprises a diffusion layer 40 of Nb Sn at the inner surface of the sheath. The core 30 comprises residual tin and small void spaces. Essentially, no niobium or Nb Sn particlesare found in the core, apart from the niobium and Nb Sn trapped in the sheaths inner diffusion layer.
The present invention is particularly applicable to vanadium gallium which can only be formed with great difiiculty in prior art core wires and is a very brittle compound. In applying the technique of the present invention, the tube 24 of FIG. 4 (which would be vanadium) should be capped by inserting a stopper in the open end of the tube after pouring the gallium and indenting the tube into depressions in the stopper. This will hold the low melting gallium during the drawing process. The process of the present invention guards the highly reactive gallium from contamination.
A principal advantage of the present invention is that the ribbon is heat treated before insulating and forming into a coil. It is not necessary to apply an expensive ceramic insulation as in prior art core wires. A cheap plastic insulation can be used. A related advantage is thatthe reactive tin or gallium or indium, etc. is trapped inside the ribbon. The ribbon can be wound into a compact spiral, inserted into a furnace muflie, and then heat treated and readily unwound after heat treatment. A ribbon with the low melting component on an outer surface would pose problems of adjacent turns sticking if wound into a tight spiral and heated.
The above-described preferred embodiment has several advantages over the prior art. The flattened form of the final product permits a higher ratio of length of Nb Sn diffusion layer to total cross-section area than a round wire because the geometry of a ribbon is inherently more favorable and because ribbons can be cold worked to smaller thicknesses more readily than wires. The ribbon form inhibits the formation of voids during the heat treatment and is a more favorable shape than round wire for winding coils. The wire 34, comprising a soft core 30 of tin and no hard materials, is readily flattened.
The process permits the use of high purity sheath material and vacuum degassed core material. The clean core material is degassed while held in crucible 26 and while being transferred from vacuum degassing crucible 26 to tube 24. The tin is then trapped in the tube without exposure to oxidizing agents and other contaminants which would limit the effectiveness of the subsequent heat treatment.
Other advantages are afforded by maintaining a continuous sheath of pure niobium about the core throughout the cold work and heating steps. The leakage of tin is prevented and the niobium-tin interface is protected from contaminants.
In comparison to the known core wires of the prior art,
the present invention offers the further advantage of confining the superconductive alloy to a thin diffusion layer which permits bending of the finished product and entails shorter times of heat treatment compared to the '20 hour heat treatments needed for prior art core wires.
Since certain changes can be made in the above product and process without departing from the scope of the invention herein involved, it is intended that all matter contained in the above description shall be interpreted as illustrative and not in a limiting sense.
What is claimed is:
1. A method of making ductile superconductors providing high current densities through an internal layer of an intermetallic alloy hard superconductor comprising the steps of placing a tube made of a higher melting component of the alloy in a non-oxidizing atmosphere and annealing it, maintaining the lower melting point component of the alloy in a non-oxidizing atmosphere in molten state to degas it, pouring the molten metal into the tube while maintaining their temperatures below the reaction temperature at which their brittle intermetallic alloys are formed, cooling the tube, cold working the tube down to wire size to extend the interface between the core and sheath thereby making the sheath readily wettable by the core materials, cold rolling the wire to flatten it to ribbon form and to further reduce its cross section thickness after flattening the wire to ribbon form, and then heating the ribbon at the reaction temperature to form the desired intermetallic, hard superconductor alloy as a diffusion layer inside the ribbon.
2. A method of making ductile superconductors providing high current densities through an internal layer of an intermetallic alloy hard superconductor comprising the steps of placing a tube made of a higher melting component of the alloy in a non-oxidizing atmosphere, maintaining the lower melting component of the alloy in said atmosphere, in molten state, pouring the molten metal into the tube while maintaining the temperatures of the tube and molten metal below the reaction temperature at which their brittle intermetallic alloys are formed, cooling the tube, then drawing the filled tube down to wire size, to extend the interface between the core and sheath thereby making the sheath readily wettable by the core materials, then flattening the tube to ribbon, and then heating the ribbon at the reaction temperature to form the desired intermetallic alloy as diffusion layer at the inner surface of the sheath.
3. The method of claim 2 wherein the higher melting component is niobium and the lower melting component is selected from the class consisting of tin, gallium, thallium, silicon, aluminum, germanium, indium, and mixtures thereof.
4. The method of claim 3 wherein the higher melting component is niobium and the lower melting component is tin and the reaction temperature is maintained between 900 and 1200 C. a
5. The method of claim 4 wherein the ribbon is cold rolled to reduce its cross section thickness to less than .002 inch before heat treating at the reaction temperature.
6 6. The method of claim 2 wherein the higher melting 2,887,763 5/1959 Snavely 29-1555 component is selected from the class consisting of niobium, 3,060,557 10/1962 Rostoker et a]. 29-194 tantalum and vanadium, and mixtures thereof. 3,057,048 10/1963 Hirakis 29-194 3,181,936 5/1965 Denny et a1. 7 References Cited by the Examiner 5 UNITED STATES PATENTS WHITMORE A. WILTZ, Primary Examiner. 2,877,539 3/1959 Kinnan 55 5 P. M. COHEN, Assistant Examiner.
Claims (1)
1. A METHOD OF MAKING DUCTILE SUPERCONDUCTORS PROVIDING HIGH CURRENT DENSITIES THROUGH AN INTERNAL LAYER OF AN INTERMETALLIC ALLOY HARD SUPERCONDUCTOR COMPRISING THE STEPS OF PLACING A TUBE MADE OF A HIGHER MELTING COMPONENT OF THE ALLOY IN A NON-OXIDIZING ATMOSPHERE AND ANNEALING IT, MAINTAINING THE LOWER MELTING POINT COMPONENT OF THE ALLOY IN A NON-OXIDIZING ATMOSPHERE IN MOLTEN STATE TO DEGAS IT, POURING THE MOLTEN METAL INTO THE TUBE WHILE MAINTAINING THEIR TEMPERATURES BELOW THE REACTION TEMPERATURE AT WHICH THEIR BRITTLE INTERMETALLIC ALLOYS ARE FORMED, COOLING THE TUBE, COLD WORKING THE TUBE DOWN TO WIRE SIZE TO EXTEND THE INTERFACE BETWEEN THE CORE AND SHEATH THEREBY MAKING THE SHEATH READILY WETTABLE BY THE CORE MATERIALS, COLD ROLLING THEWIRE TO FLATTEN IT TO RIBBON FORM AND TO FURTHER REDUCE ITS CROSS SECTION THICKNESS AFTER FLATTENING THE WIRE TO RIBBON FORM, AND THEN HEATING THE RIBBON AT THE REACTION TEMPERATURE TO FROM THE DESIRED INTERMETALLIC, HARD SUPERCONDUCTOR ALLOY AS A DIFFUSION LAYER INSIDE THE RIBBON.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US301494A US3243871A (en) | 1963-08-12 | 1963-08-12 | Method of making ductile superconductors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US301494A US3243871A (en) | 1963-08-12 | 1963-08-12 | Method of making ductile superconductors |
Publications (1)
Publication Number | Publication Date |
---|---|
US3243871A true US3243871A (en) | 1966-04-05 |
Family
ID=23163637
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US301494A Expired - Lifetime US3243871A (en) | 1963-08-12 | 1963-08-12 | Method of making ductile superconductors |
Country Status (1)
Country | Link |
---|---|
US (1) | US3243871A (en) |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3341308A (en) * | 1963-09-30 | 1967-09-12 | Nat Res Corp | Superconductor comprising a niobium substrate having a coating of niobium stannide and particles of a ferromagnetic material |
US3344508A (en) * | 1963-02-20 | 1967-10-03 | Commissariat Energie Atomique | Process for producing cladded fuel elements |
US3395000A (en) * | 1965-01-27 | 1968-07-30 | Rca Corp | Composite metal articles |
US3408235A (en) * | 1964-03-17 | 1968-10-29 | Philips Corp | Method of manufacturing wound nb3sn-containing bodies |
US3423824A (en) * | 1965-04-21 | 1969-01-28 | Commissariat Energie Atomique | Method for fixing superconducting magnetic coils |
US3429032A (en) * | 1963-10-15 | 1969-02-25 | Gen Electric | Method of making superconductors containing flux traps |
US3465429A (en) * | 1966-01-27 | 1969-09-09 | Imp Metal Ind Kynoch Ltd | Superconductors |
US3471925A (en) * | 1965-11-17 | 1969-10-14 | Avco Corp | Composite superconductive conductor and method of manufacture |
US3644987A (en) * | 1970-03-02 | 1972-02-29 | Kabel Und Metallwerke Gutchoff | Method for manufacturing superconductors |
US3665595A (en) * | 1968-10-31 | 1972-05-30 | Tohoku University The | Method of manufacturing superconductive materials |
US3710844A (en) * | 1967-02-24 | 1973-01-16 | Hitachi Ltd | Method of producing superconducting strips |
US3778260A (en) * | 1970-09-09 | 1973-12-11 | Hitachi Ltd | Superconducting materials |
US4088512A (en) * | 1977-01-21 | 1978-05-09 | The United States Of America As Represented By The United States Department Of Energy | Quench-age method for the fabrication of niobium-aluminum superconductors |
US5049539A (en) * | 1989-01-31 | 1991-09-17 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low cost, formable, high TC superconducting wire |
WO1994000886A1 (en) * | 1992-06-30 | 1994-01-06 | American Superconductor Corporation | High tc superconductor and method of making |
US6103669A (en) * | 1987-09-28 | 2000-08-15 | Hitachi, Ltd. | Superconducting wire and method of producing the same |
US6112410A (en) * | 1997-09-19 | 2000-09-05 | The Research Corporation Of State University Of New York | Methods for fabricating a structural beam |
US20060201206A1 (en) * | 2001-07-16 | 2006-09-14 | Gilles Benoit | Fiber waveguides and methods of making the same |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2877539A (en) * | 1954-10-19 | 1959-03-17 | George Franklin Dales | Method of making thermostats |
US2887763A (en) * | 1949-07-07 | 1959-05-26 | Benjamin L Snavely | Assembly molding process for electrical elements |
US3057048A (en) * | 1958-11-06 | 1962-10-09 | Horizons Inc | Protection of niobium |
US3060557A (en) * | 1957-03-25 | 1962-10-30 | Armour Res Found | Metal cladding process and products resulting therefrom |
US3181936A (en) * | 1960-12-30 | 1965-05-04 | Gen Electric | Superconductors and method for the preparation thereof |
-
1963
- 1963-08-12 US US301494A patent/US3243871A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2887763A (en) * | 1949-07-07 | 1959-05-26 | Benjamin L Snavely | Assembly molding process for electrical elements |
US2877539A (en) * | 1954-10-19 | 1959-03-17 | George Franklin Dales | Method of making thermostats |
US3060557A (en) * | 1957-03-25 | 1962-10-30 | Armour Res Found | Metal cladding process and products resulting therefrom |
US3057048A (en) * | 1958-11-06 | 1962-10-09 | Horizons Inc | Protection of niobium |
US3181936A (en) * | 1960-12-30 | 1965-05-04 | Gen Electric | Superconductors and method for the preparation thereof |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3344508A (en) * | 1963-02-20 | 1967-10-03 | Commissariat Energie Atomique | Process for producing cladded fuel elements |
US3341308A (en) * | 1963-09-30 | 1967-09-12 | Nat Res Corp | Superconductor comprising a niobium substrate having a coating of niobium stannide and particles of a ferromagnetic material |
US3429032A (en) * | 1963-10-15 | 1969-02-25 | Gen Electric | Method of making superconductors containing flux traps |
US3408235A (en) * | 1964-03-17 | 1968-10-29 | Philips Corp | Method of manufacturing wound nb3sn-containing bodies |
US3395000A (en) * | 1965-01-27 | 1968-07-30 | Rca Corp | Composite metal articles |
US3423824A (en) * | 1965-04-21 | 1969-01-28 | Commissariat Energie Atomique | Method for fixing superconducting magnetic coils |
US3471925A (en) * | 1965-11-17 | 1969-10-14 | Avco Corp | Composite superconductive conductor and method of manufacture |
US3465429A (en) * | 1966-01-27 | 1969-09-09 | Imp Metal Ind Kynoch Ltd | Superconductors |
US3710844A (en) * | 1967-02-24 | 1973-01-16 | Hitachi Ltd | Method of producing superconducting strips |
US3665595A (en) * | 1968-10-31 | 1972-05-30 | Tohoku University The | Method of manufacturing superconductive materials |
US3644987A (en) * | 1970-03-02 | 1972-02-29 | Kabel Und Metallwerke Gutchoff | Method for manufacturing superconductors |
US3778260A (en) * | 1970-09-09 | 1973-12-11 | Hitachi Ltd | Superconducting materials |
US4088512A (en) * | 1977-01-21 | 1978-05-09 | The United States Of America As Represented By The United States Department Of Energy | Quench-age method for the fabrication of niobium-aluminum superconductors |
US6103669A (en) * | 1987-09-28 | 2000-08-15 | Hitachi, Ltd. | Superconducting wire and method of producing the same |
US5049539A (en) * | 1989-01-31 | 1991-09-17 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low cost, formable, high TC superconducting wire |
WO1994000886A1 (en) * | 1992-06-30 | 1994-01-06 | American Superconductor Corporation | High tc superconductor and method of making |
US6218340B1 (en) * | 1992-06-30 | 2001-04-17 | American Superconductor Corporation | Method of manufacturing superconductors including isostatic pressing |
US6112410A (en) * | 1997-09-19 | 2000-09-05 | The Research Corporation Of State University Of New York | Methods for fabricating a structural beam |
US20060201206A1 (en) * | 2001-07-16 | 2006-09-14 | Gilles Benoit | Fiber waveguides and methods of making the same |
US8516856B2 (en) * | 2001-07-16 | 2013-08-27 | Massachusetts Institute Of Technology | Methods of making fiber waveguides from multilayer structures |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3243871A (en) | Method of making ductile superconductors | |
US3465430A (en) | Method of making superconductor stock | |
US4078299A (en) | Method of manufacturing flexible superconducting composite compound wires | |
US3623221A (en) | Method of fabricating a tubular superconductor assembly | |
US3838503A (en) | Method of fabricating a composite multifilament intermetallic type superconducting wire | |
US4223434A (en) | Method of manufacturing a niobium-aluminum-germanium superconductive material | |
US6251529B1 (en) | Nb-Sn compound superconducting wire precursor, method for producing the same and method for producing Nb-Sn compound superconducting wire | |
US3918998A (en) | Method for producing superconducting wire and products of the same | |
GB1561751A (en) | Superconductor composite and method of making the same | |
JPS63285816A (en) | Manufacture of superconductor covered with normal conducting metal | |
US3509622A (en) | Method of manufacturing composite superconductive conductor | |
JP4996084B2 (en) | Manufacturing method of superconducting element | |
RU2105370C1 (en) | Conductor for superconducting wire and conductor for multicore superconducting wire | |
US3239919A (en) | Method of producing high energy permanent magnets | |
US3836404A (en) | Method of fabricating composite superconductive electrical conductors | |
US3710844A (en) | Method of producing superconducting strips | |
US4532703A (en) | Method of preparing composite superconducting wire | |
US3644987A (en) | Method for manufacturing superconductors | |
JP5065582B2 (en) | Superconducting device and manufacturing method thereof | |
JP3433937B2 (en) | Method of manufacturing superconducting alloy | |
US3346467A (en) | Method of making long length superconductors | |
US6699821B2 (en) | Nb3Al superconductor and method of manufacture | |
US3465429A (en) | Superconductors | |
US3857173A (en) | Method of producing a composite superconductor | |
US4037313A (en) | Method for the manufacture of a superconductor |