Claims
- 1. A monofilament rod for use in preparing a multifilament oxide superconducting strand, comprising:
an oxide filament in a ductile metal matrix, said oxide comprising an oxide superconductor or precursor thereto; and wherein said rod has a cross-sectional geometry of a quadrilateral having two opposing sides of same or unequal length connected by two linear sides of the same or unequal length.
- 2. The rod of claim 1 wherein the two opposing sides comprise two concentric arcs of unequal length comprising a larger outer arc and a smaller inner arc.
- 3. The rod of claim 1 wherein the quadrilateral is selected from the group consisting of a trapezoid and a trapezium.
- 4. The rod of claim 1 wherein the length of the outer arc is greater than the length of the inner arc such that an angle between the two linear sides of the quadrilateral is from about 10 to about 180 degrees.
- 5. The rod of claim 4 wherein the angle is from about 20 to about 60 degrees.
- 6. The rod of claim 4 wherein the angle is about 20 to about 45 degrees.
- 7. The rod of claim 1 wherein the cross-sectional geometry of the rod comprises a trapezoid.
- 8. The rod of claim 1, wherein the ductile metal matrix comprises silver or a silver alloy.
- 9. The rod of claim 1 wherein the oxide superconductor comprises a bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 10. The rod of claim 1 wherein the oxide superconductor comprises a lead-bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 11. A monofilament rod for use in preparing a multifilament oxide superconducting strand comprising:
an oxide filament in a ductile metal matrix, said oxide comprising an oxide superconductor or precursor thereto, wherein said rod possesses a space-filling geometry such that, when multiple monofilament rods are assembled into a billet, such assembly is characterized by the absence of sharp angles.
- 12. The rod of claim 11 wherein the billet comprises a cylindrical tube containing an array of monofilaments having a cross-section geometry of a quadrilateral and said monofilaments are arranged about a central core.
- 13. The rod of claim 11 wherein the quadrilateral comprises a trapezoid.
- 14. The rod of claim 11 wherein the oxide superconductor comprises a bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 15. The rod of claim 11 wherein the oxide superconductor comprises a lead-bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 16. A multifilamentary assembly for forming a superconducting composite article comprising:
a plurality of oxide superconducting filaments in a conductive, ductile metal matrix arranged about a central core to form a filament bundle, wherein each filament has a cross-sectional geometry of a quadrilateral having two opposing sides of same or unequal length connected by two linear sides of the same or unequal length.
- 17. The multifilamentary assembly of claim 16 further comprising:
a metallic sheath having an outer diameter and an inner diameter which substantially surrounds the outermost surface of the multifilamentary assembly.
- 18. The multifilamentary assembly of claim 16 wherein the two opposing sides comprise two concentric arcs of unequal length comprising a larger outer arc and a smaller inner arc.
- 19. The multifilamentary assembly of claim 16 wherein the quadrilateral is selected from the group consisting of a trapezoid and a trapezium.
- 20. The multifilamentary assembly of claim 16 wherein the length of the outer arc is greater than the length of the inner arc such that an angle between the two linear sides of the quadrilateral is from about 10 to about 180 degrees.
- 21. The multifilamentary assembly of claim 20 wherein the angle is from about 20 to about 60 degrees.
- 22. The multifilamentary assembly of claim 20 wherein the angle is about 20 to about 45 degrees.
- 23. The multifilamentary assembly of claim 16 wherein the cross-sectional geometry of the each filament comprises a trapezoid.
- 24. The multifilamentary assembly of claim 16 wherein the ductile metal matrix comprises silver or a silver alloy.
- 25. The multifilamentary assembly of claim 16 wherein each filament possesses a space-filling geometry such that, when multiple monofilament rods are assembled into a billet, such assembly is characterized by the absence of sharp angles.
- 26. The multifilamentary assembly of claim 16 wherein the central core comprises an array of filaments having a cross-section geometry of a quadrilateral and said filaments are arranged about a second central core.
- 27. The multifilamentary assembly of claim 17 wherein the assembly has a fill factor of superconducting material of greater than about 35%.
- 28. The multifilamentary assembly of claim 17 wherein the assembly has a fill factor of superconducting material of greater than about 40%.
- 29. The multifilamentary assembly of claim 16 wherein the filaments are arranged about a central core selected from the group consisting of an electrically resistive core, a conductive core, and an oxide superconductor core.
- 30. The multifilamentary assembly of claim 16 wherein the filaments are arranged in a single concentric layer about the central core.
- 31. The multifilamentary assembly of claim 16 wherein the filaments are arranged in multiple concentric layers about the central core.
- 32. The multifilamentary assembly of claim 31 wherein a first concentric layer is comprised of filaments having arcs of uniform length, and a second concentric layer is comprised of filaments having arcs of uniform length different from that of the first concentric layer.
- 33. The multifilamentary assembly of claim 32 wherein a first concentric layer is comprised of filaments having arcs of unequal length and linear sides of uniform length arranged about the central core, and a second concentric layer arranged about the first concentric layer, the second concentric layer comprised of filaments having arcs of unequal length and linear sides of uniform length.
- 34. The multifilamentary assembly of claim 16 wherein the assembly is comprised of from about 3 to about 1000 oxide superconducting filaments.
- 35. The multifilamentary assembly of claim 16 wherein the assembly is comprised of 6-50 oxide superconducting filaments.
- 36. The multifilamentary assembly of claim 16 wherein the assembly is comprised of 6-18 oxide superconducting filaments.
- 37. The multifilamentary assembly of claim 16 wherein the oxide superconductor comprises a bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 38. The multifilamentary assembly of claim 16 wherein the oxide superconductor comprises a lead-bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 39. The multifilamentary assembly of claim 17 wherein the filaments are arranged around a core to form a filament bundle and the diameter of the filament bundle is less than the inner diameter of the metallic sheath by less than about 10%.
- 40. The multifilamentary assembly of claim 17 wherein the filaments are arranged around a core to form a filament bundle and the diameter of the filament bundle is about 2% less than the inner diameter of the metallic sheath.
- 41. A method of making a multifilamentary superconducting composite article, comprising the steps of:
forming an elongated multifilamentary assembly comprising a plurality of oxide filaments in a ductile metal matrix assembled about a central core to form a filament bundle, wherein each filament has a cross-sectional geometry of a quadrilateral having two opposing sides of same or unequal length connected by two linear sides of the same or unequal length, and said oxide comprises an oxide superconductor or precursor thereto; processing the assembly to reduce composite cross-sectional area, to adhere assembly elements to one another, and to induce texture in the precursor oxide filaments; and converting the precursor oxide into an oxide superconductor, whereby a multifilamentary superconducting composite is obtained.
- 42. The method of claim 41, wherein the step of forming an elongated multifilamentary composite comprises:
introducing a metallic sheath around the filament bundle to produce a filament bundle/sheath composite; and deforming the composite to reduce the diameter of a cross-section of the composite.
- 43. The method of claim 41 wherein the two opposing sides comprise two concentric arcs of unequal length comprising a larger outer arc and a smaller inner arc.
- 44. The method of claim 41 wherein the quadrilateral is selected from the group consisting of a trapezoid and a trapezium.
- 45. The method of claim 41 wherein the length of the outer arc is greater than the length of the inner arc such that an angle between the two linear sides of the quadrilateral is from about 10 to about 180 degrees.
- 46. The method of claim 41 wherein the angle is from about 20 to about 60 degrees.
- 47. The method of claim 41 wherein the angle is about 20 to about 45 degrees.
- 48. The method of claim 41 wherein the cross-sectional geometry of the each filament comprises a trapezoid.
- 49. The method of claim 41 wherein the ductile metal matrix comprises silver or a silver alloy.
- 50. The method of claim 41 wherein each filament possesses a space-filling geometry such that, when multiple monofilament rods are assembled into a filament bundle, such bundle is characterized by the absence of sharp angles.
- 51. The method of claim 41 wherein the central core comprises an array of filaments having a cross-section geometry of a quadrilateral and said filaments are arranged about a second central core.
- 52. The method of claim 41 wherein the assembly has a fill factor of superconducting material of greater than about 35%.
- 53. The method of claim 41 wherein the assembly has a fill factor of superconducting material of greater than about 40%.
- 54. The method of claim 41 wherein the filaments are arranged about a central core selected from the group consisting of an electrically resistive core, a conductive core, and an oxide superconductor core.
- 55. The method of claim 41 wherein the filaments are arranged in a single concentric layer about the central core.
- 56. The method of claim 41 wherein the filaments are arranged in multiple concentric layers about the central core.
- 57. The method of claim 41 wherein a first concentric layer is comprised of filaments having arcs of uniform length, and a second concentric layer is comprised of filaments having arcs of uniform length different from that of the first concentric layer.
- 58. The method of claim 41 wherein a first concentric layer is comprised of filaments having arcs of unequal length and linear sides of uniform length arranged about the central core, and a second concentric layer arranged about the first concentric layer, the second concentric layer comprised of filaments having arcs of unequal length and linear sides of uniform length.
- 59. The method of claim 41 wherein the assembly is comprised of from about 3 to about 1000 oxide superconducting filaments.
- 60. The method of claim 41 wherein the assembly is comprised of 6-50 oxide superconducting filaments.
- 61. The method of claim 41 wherein the assembly is comprised of 6-18 oxide superconducting filaments.
- 62. The method of claim 41 wherein the oxide superconductor comprises a bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 63. The method of claim 41 wherein the oxide superconductor comprises a lead-bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 64. The method of claim 41wherein the diameter of the filament bundle is less than the inner diameter of the metallic sheath by less than about 10%.
- 65. The method of claim 41 wherein the diameter of the filament bundle is less than the inner diameter of the metallic sheath by less than about 2%.
- 66. The method of claim 41, wherein the core is solid.
- 67. The method of claim 41, wherein the composite is textured by a large reduction rolling on the order of 40-85% reduction in thickness.
- 68. The method of claim 67, wherein the composite is textured in a constrained rolling operation.
- 69. A superconducting composite article comprising a plurality of oxide superconducting filaments in a conductive ductile metal matrix, produced according to the method of claim 41, wherein the article has a cross-sectional width in the range of 100-8000 μm and a cross-sectional thickness in the range of 25-500 μm.
- 70. The composite article of claim 69, wherein the article has a cross-sectional width less than 300 μm and a cross-sectional thickness less than 100 μm.
- 71. The composite article of claim 69, wherein the conductive matrix metal comprises silver or a silver alloy.
- 72. The composite article of claim 69, wherein the article is comprised of from about 3 to about 1000 oxide superconducting filaments.
- 73. The composite article of claim 69, wherein the article is comprised of about 6 to about 50 oxide superconducting filaments.
- 74. The composite article of claim 69, wherein the article is comprised of from about 6 to about 18 oxide superconducting filaments.
- 75. The composite article of claim 69, wherein the article has a cross-sectional aspect ratio of less than 20:1.
- 76. The composite article of claim 69, wherein the article has a cross-sectional aspect ratio of about 2:1 to about 5:1.
- 77. The composite article of claim 69, wherein the oxide superconductor comprises a bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
- 78. The composite article of claim 69, wherein the oxide superconductor comprises a lead-bismuth-strontium-calcium-copper oxide (BSCCO) superconductor.
Parent Case Info
[0001] This application is related to a PCT International Application and an U.S. application entitled, “Superconducting Articles Having Low AC Loss,” filed on an even day herewith. This application claims the priority of U.S. Provisional Application No. 60/232,732, filed Sep. 15, 2000.
Provisional Applications (1)
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Number |
Date |
Country |
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60232732 |
Sep 2000 |
US |