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US4094060A Expired / Lapsed US ⏱️ 0.0 years remaining

Superconducting members and methods of manufacture thereof

Assignee: United Kingdom Atomic Energy Authority
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Filing: 1975-06-09
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Granted: 1978-06-13
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Expires: 1995-06-09
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Abstract

Abstract A superconducting member is manufactured by mechanical fabrication to final dimensions of a matrix comprising a base material, such as niobium, an alloy essentially consisting of a carrier material and at least one element, such as tin, a metal for stabilization and a barrier material protecting the metal for stabilization. After mechanical fabrication a superconducting compound of the base material and the element is formed by heat treatment to cause a solid state reaction. The barrier material prevents diffusion of any of the components into the metal for stabilization.

Inventors

  • 👤 Peter Emil Madsen
  • 👤 John Philip Charlesworth
  • 👤 Derek Armstrong

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 20:01
CPC Classifications
H; H10; H10N; H10N60/00; H10N60/01; H10N60/0184; Y; Y10; Y10S; Y10S505/00; Y10S505/825; Y10S505/917; Y10S505/918; Y10S505/919; Y10S505/92; Y10S505/921; Y10T; Y10T29/00; Y10T29/49; Y10T29/49002; Y10T29/49014

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 234 words
A method of manufacturing a superconducting member, which method comprises the steps of forming an alloy consisting essentially of a carrier material and at least one element from the group consisting of aluminium, gallium, indium, silicon, germanium, gold, platinum, antimony, rhodium, zirconium, palladium, osmium, ruthenium, cobalt, thallium, lead, arsenic, bismuth, iridium and tin; contacting the alloy with a base material consisting essentially of niobium or vanadium; consolidating into a unitary structure components comprising the alloy and the base material together with a metal, which is eventually to provide stabilisation, a barrier material consisting essentially of tantalum or molybdenum being present and positioned to protect the said metal from diffusion thereinto of any of the other components; mechanically working the said unitary structure to form a wire therefrom, and heat treating the said wire to cause a solid state reaction between the base material and the element or elements from the said group to form a superconducting compound therewith, the carrier material being so selected as to be substantially non-reactive with the base material under the heat treatment and the barrier material being so selected and positioned as to prevent permeation therethrough of the element from the said group and to be insoluble in and substantially non-reactive with the said metal, and the heat treatment temperature being controlled for avoiding melting of the alloy in contact with the base material at any stage during reaction.
Claim 2
Independent Claim 234 words
A method of manufacturing a superconducting member, which method comprises the steps of forming an alloy consisting essentially of a carrier material and at least one element from the group consisting of aluminium, gallium, indium, silicon, germanium, gold, platinum, antimony, rhodium, zirconium, palladium, osmium, ruthenium, cobalt, thallium, lead, arsenic, bismuth, iridium and tin; contacting the alloy with a base material consisting essentially of niobium or vanadium; consolidating into a unitary structure components comprising the alloy and the base material together with a metal, which is eventually to provide stabilisation, a barrier material consisting essentially of tantalum or molybdenum being present and positioned to protect the said metal from diffusion thereinto of any of the other components; mechanically working the said unitary structure to form a wire therefrom, and heat treating the said wire to cause a solid state reaction between the base material and the element or elements from the said group to form a superconducting compound therewith, the carrier material being so selected as to be substantially non-reactive with the base material under the heat treatment and the barrier material being so selected and positioned as to prevent permeation therethrough of the element from the said group and to be insoluble in and substantially non-reactive with the said metal, and the heat treatment temperature being controlled for avoiding melting of the alloy in contact with the base material at any stage during reaction.
Claim 3
Dependent Claim 47 words
A method as claimed in claim 1, wherein the alloy and the base material are in contact in the said wire along regions in which the superconducting compound is formed, the said regions being in the form of discrete filaments extending along the length of the wire.
Claim 4
Dependent Claim 67 words
A method as claimed in claim 1, wherein one of the components of the said unitary structure comprises a block having bores extending therethrough and at least one of the other components comprises rods or tubes received in the bores, the mechanical working of the unitary structure forming the block into a wire and the rods or tubes into a plurality of filaments embedded in the wire.
Claim 5
Dependent Claim 40 words
A method as claimed in claim 1, wherein all the components of the unitary structure are in the form of rods or tubes bundled together and the mechanical working forms the unitary structure into an extended wire having multifilamentary components.
Claim 6
Independent Claim 353 words
A method of manufacturing a superconducting member, which method comprises forming a block of pure copper with bores extending therethrough, inserting into the said bores rods comprising an outer tubular sheath of niobium and an inner core of an alloy consisting essentially of a carrier material and at least one element from the group consisting of aluminium, gallium, indium, silicon, germanium, and tin, there being spaces within the said alloy core which spaces are filled with pure or essentially pure element or mixture of elements from the said group, said element or mixture of elements filling said spaces being the same as the element or mixture of elements present in the carrier as a dispersion or solid solution constituent of the alloy, the said filled spaces thus providing reservoirs of the essentially pure element or mixture of elements, said reservoirs being wholly separated from contact with base material by alloy interposed therebetween, mechanically working the block to form the block into a wire and the rod into filaments embedded in the wire, and heat treating the wire to cause a solid state reaction between the niobium and the element or elements from the said group within the alloy contacting the niobium, the pure or essentially pure element or elements from the said group in the said reservoirs diffusing, during the heat treatment, into the alloy thereby making up for depletion of the element or mixture of elements in the alloy as a consequence of the said solid state reaction and ensuring that there is an adequate supply of said elements or mixture of elements dispersed or in solid solution in the alloy in contact with the niobium to form an adequately thick layer of superconducting compound Nb 3 B where B is the said element or mixture of elements, the thickness and concentrations of the niobium and the B element or elements respectively being such that Nb 3 B superconductor formation does not extend wholly through the niobium sheath and the heat treatment temperature being controlled for avoiding melting of the alloy in contact with the niobium at any stage during the reaction.
Claim 7
Independent Claim 353 words
A method of manufacturing a superconducting member, which method comprises forming a block of pure copper with bores extending therethrough, inserting into the said bores rods comprising an outer tubular sheath of niobium and an inner core of an alloy consisting essentially of a carrier material and at least one element from the group consisting of aluminium, gallium, indium, silicon, germanium, and tin, there being spaces within the said alloy core which spaces are filled with pure or essentially pure element or mixture of elements from the said group, said element or mixture of elements filling said spaces being the same as the element or mixture of elements present in the carrier as a dispersion or solid solution constituent of the alloy, the said filled spaces thus providing reservoirs of the essentially pure element or mixture of elements, said reservoirs being wholly separated from contact with base material by alloy interposed therebetween, mechanically working the block to form the block into a wire and the rod into filaments embedded in the wire, and heat treating the wire to cause a solid state reaction between the niobium and the element or elements from the said group within the alloy contacting the niobium, the pure or essentially pure element or elements from the said group in the said reservoirs diffusing, during the heat treatment, into the alloy thereby making up for depletion of the element or mixture of elements in the alloy as a consequence of the said solid state reaction and ensuring that there is an adequate supply of said elements or mixture of elements dispersed or in solid solution in the alloy in contact with the niobium to form an adequately thick layer of superconducting compound Nb 3 B where B is the said element or mixture of elements, the thickness and concentrations of the niobium and the B element or elements respectively being such that Nb 3 B superconductor formation does not extend wholly through the niobium sheath and the heat treatment temperature being controlled for avoiding melting of the alloy in contact with the niobium at any stage during the reaction.

References Cited (Backward Citations)

US3665595A Cited
US3652967A Cited
US3813764A Cited
US3728165A Cited
US3625662A Cited
US3868768A Cited
US3874074A Cited
FR2195090A1 Cited
GB1394724A Cited
US3876473A Cited
US3996661A Cited
US3958327A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-06-12 1981-12-12 1982-06-13 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-06-12 1985-12-12 1986-06-13 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-06-12 1989-12-12 1990-06-13 $7700.00 Window Closed / Lapsed

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