Bi-Layer Barrier Assembly for Iron-Based Superconductor and Associated Methods
Bi-layer barrier assemblies for iron-based superconductor (IBS) and associated sheathed wire fabrication methods employ insulating material to prevent interdiffusion between inner silver (Ag) and outer matrix components at heat treatments. A superconductor assembly comprises a core IBS material (e.g., mono-filamentary or multi-filamentary IBS powder) layered, in turn, with an AG barrier material, an insulating barrier material (e.g., niobium (Nb), tantalum (Ta), and/or a Nb—Ta alloy); and a matrix material (e.g., copper (Cu), Cu alloy, and/or monel). Assembly comprises 1) packing the IBS material into the Ag sheath (barrier) material, defining a packed first assembly; 2) layering the insulating barrier material upon the Ag sheath material, defining an insulated second assembly; and 3) layering the matrix material upon the insulating material, defining a matrixed third assembly. Additional steps may comprise respective drawing of the packed first assembly, the insulated second assembly, and/or the matrixed third assembly, and/or stacking for multi-filamentary implementations.
1 . A superconductor assembly comprising:
at least one iron-based superconductor (IBS) material [ 310 ];
a silver (Ag) barrier material layered upon a respective first outer surface of each of the at least one IBS material [ 310 ];
an insulating barrier material layered upon a second outer surface of the Ag barrier material opposite the at least one IBS material [ 310 ]; and
a matrix material layered upon a third outer surface of the insulating barrier material opposite the Ag barrier material [ 320 ].
2 . The superconductor assembly according to claim 1 , wherein the at least one IBS material is of one of a mono-filamentary type and a multi-filamentary type [ 200 ].
3 . The superconductor assembly according to claim 1 , wherein the insulating barrier material comprises at least one of niobium (Nb), tantalum (Ta), and a Nb—Ta alloy.
4 . The superconductor assembly according to claim 1 , wherein the matrix material comprises at least one of copper (Cu), Cu alloy, or monel.
5 . A method of superconductor fabrication comprising the steps of:
applying a silver (Ag) sheath material to a respective first circumference of each of at least one iron-based superconductor (IBS) material [ 310 ], to define a packed first assembly [ 510 ];
applying an insulating material to a second circumference of the Ag sheath material opposite the at least one IBS material [ 310 ], to define an insulated second assembly [ 514 ]; and
applying a matrix material to a third circumference of the insulating material opposite the Ag sheath material [ 320 ], to define a matrixed third assembly [ 518 ].
6 . The method according to claim 5 , wherein the at least one IBS material is of one of a mono-filamentary type and a multi-filamentary type [ 200 ].
7 . The method according to claim 5 , wherein the insulating material comprises one of niobium (Nb) and tantalum (Ta).
8 . The method according to claim 5 , where the applying the Ag sheath further comprises the step of:
packing the at least one iron-based superconductor (IBS) material into the Ag sheath material [ 320 ].
9 . The method according to claim 5 , where the applying the insulating material further comprises the step of:
drawing the insulating material onto the second circumference of the Ag sheath material [ 320 ].
10 . The method according to claim 5 , where the applying the matrix material further comprises the step of:
drawing the matrix material onto the third circumference of the insulating material [ 330 ].
11 . A method of superconductor fabrication comprising the steps of:
packing at least one iron-based superconductor (IBS) material into a silver (Ag) sheath material [ 320 ], to define a packed first assembly [ 510 ];
layering an insulating material comprising at least one of niobium (Nb), tantalum (Ta), and Nb—Ta alloy upon the Ag sheath material opposite the at least one IBS material [ 310 ], to define an insulated second assembly [ 514 ]; and
layering a matrix material upon the insulating material opposite the Ag sheath material [ 320 ], to define a matrixed third assembly [ 518 ].
12 . The method according to claim 11 , wherein the at least one IBS material is of one of a mono-filamentary type and a multi-filamentary type [ 200 ].
13 . The method according to claim 12 , wherein the at least one IBS material is of a mono-filamentary type and is characterized by a core radius less than one (1) millimeter (mm).
14 . The method according to claim 11 , wherein the Ag sheath material is characterized by a first-layer thickness less than one (1) millimeter (mm).
15 . The method according to claim 11 , wherein the insulating material is characterized by a second-layer thickness less than one (1) millimeter (mm).
16 . The method according to claim 11 , wherein the matrix material is characterized by a third-layer thickness less than one (1) millimeter (mm).
17 . The method according to claim 11 , further comprising the step of drawing the packed first assembly [ 510 ].
18 . The method according to claim 11 , further comprising the step of drawing the insulated second assembly [ 514 ].
19 . The method according to claim 11 , further comprising the step of drawing the matrixed third assembly [ 518 ].
20 . The method according to claim 11 , further comprising the step of preventing, using the insulating material of the matrixed third assembly at a heat treatment, an interdiffusion between the Ag sheath material and the matrix material [ 340 ].