INSULATION-COATED COMPOUND SUPERCONDUCTING WIRE AND REWINDING METHOD THEREOF

Abstract

An insulation-coated compound superconducting wire includes a compound superconducting wire having a compound superconducting part which includes a first matrix and a plurality of compound superconducting filaments containing compound superconducting phases, a reinforcing part disposed on the outer circumferential side of the compound superconducting part and includes a plurality of reinforced filaments, a second matrix and a second stabilizing material. A stabilizing part is disposed on at least one side among the inner circumferential side and the outer circumferential side of the reinforcing part. An electrical insulation part covers the outer circumferential surface of the compound superconducting wire, in which the insulation-coated compound superconducting wire has a critical current value (Ic) larger than that of the compound superconducting wire before being covered with the electrical insulation part.

Claims

1. An insulation-coated compound superconducting wire, comprising: a compound superconducting wire comprising a core-like compound superconductor part, a cylindrical reinforcing part, and a cylindrical stabilizing part; and an electric insulation part coating an outer circumferential surface of the compound superconducting wire, wherein the core-like compound superconductor part comprises a plurality of compound superconducting filaments and a first matrix, the compound superconducting filaments each comprising a compound superconducting phase, the first matrix comprising the plurality of compound superconducting filaments embedded therein and a first stabilizing material, wherein the cylindrical reinforcing part is disposed on an outer circumferential side of the compound superconductor part, and comprises a plurality of reinforcing filaments and a second matrix, the second matrix comprising the plurality of reinforcing filaments embedded therein and a second stabilizing material, wherein the cylindrical stabilizing part is disposed on at least one side of an inner circumferential side and an outer circumferential side of the reinforcing part, and comprises a third stabilizing material, and wherein the insulation-coated compound superconducting wire has a critical current value (Ic) larger than that of the compound superconducting wire before being coated with the electric insulation part.

2. The insulation-coated compound superconducting wire according to claim 1, wherein the compound superconducting phase comprises Nb.sub.3Sn, and each of the critical current value (Ic) is obtained by applying predetermined tensile stress of 150 MPa or more and 250 MPa or less at room temperature to the insulation-coated compound superconducting wire or the compound superconducting wire before being coated with the electric insulation part, followed by unloading, then cooling the wire to a temperature of 4.2 K, and then conducting electric current through the wire in a state of being unloaded the tensile stress and being applied an external magnetic field of 14.5 T.

3. The insulation-coated compound superconducting wire according to claim 1, wherein the compound superconducting phase comprises Nb.sub.3Sn, and each of the critical current value (Ic) is obtained by cooling the insulation-coated compound superconducting wire or the compound superconducting wire before being coated with the electric insulation part to a temperature of 4.2 K, and then conducting electric current through the wire in a state of being applied a predetermined tensile stress of 150 MPa or more and 250 MPa or less and being applied an external magnetic field of 14.5 T.

4. The insulation-coated compound superconducting wire according to claim 3, wherein the insulation-coated compound superconducting wire has a smaller tensile stress at which the critical current value (Ic) becomes maximum than that of the compound superconducting wire before being coated with the electric insulation part.

5. The insulation-coated compound superconducting wire according to claim 1, further comprising a Sn diffusion prevention part between the compound superconductor part and the reinforcing part.

6. The insulation-coated compound superconducting wire according to claim 5, wherein the compound superconducting phase comprises Nb.sub.3Sn, the first stabilizing material comprises Cu or a Cu alloy, the Sn diffusion prevention part comprises Nb or Ta, or an alloy or composite thereof, the reinforcing filament comprises at least one metal or an alloy of two or more metals selected from the group consisting of Nb, Ta, V, W, Mo, Fe, Ti, and Hf, the second stabilizing material comprises Cu or a Cu alloy, and the third stabilizing material comprises Cu or a Cu alloy.

7. The insulation-coated compound superconducting wire according to claim 1, wherein the electric insulation part comprises a resin material.

8. The insulation-coated compound superconducting wire according to claim 7, wherein the resin material is enamel coating or polyimide tape.

9. The insulation-coated compound superconducting wire according to claim 1, wherein a volume ratio of the reinforcing part relative to the compound superconducting wire is larger than a volume ratio of the compound superconductor part relative to the compound superconducting wire.

10. The insulation-coated compound superconducting wire according to claim 1, wherein a total of a volume ratio of the second stabilizing material relative to the compound superconducting wire and a volume ratio of the third stabilizing material relative to the compound superconducting wire is 45% or more.

11. The insulation-coated compound superconducting wire according to claim 5, wherein a total of a volume ratio of the reinforcing filament relative to the compound superconducting wire and a volume ratio of the Sn diffusion prevention part relative to the compound superconducting wire is 7% or more.

12. The insulation-coated compound superconducting wire according to claim 11, wherein the total of the volume ratio of the reinforcing filament relative to the compound superconducting wire and the volume ratio of the Sn diffusion prevention part relative to the compound superconducting wire is 15% or more.

13. The insulation-coated compound superconducting wire according to claim 1, further comprising a heat-resistant plated part having a thickness of 1 μm or less between the outer circumferential surface of the compound superconducting wire and the electric insulation part.

14. The insulation-coated compound superconducting wire according to claim 1, wherein the insulation-coated compound superconducting wire is obtained by, within a temperature range from room temperature to 500° C., applying tensile strain of 0.2% or less to the compound superconducting wire and applying bending strain within ±0.5% to the compound superconductor part at least 10 times, between the time of forming the compound superconducting wire by performing heat treatment of the compound superconducting phase in a state of being bent and wound a compound superconducting precursor strand around a winding member with a bending diameter corresponding to 100 times larger than the maximum diameter of the compound superconductor part, and the time of finishing the coating of the electric insulation part to the outer circumferential surface of the compound superconducting wire.

15. The insulation-coated compound superconducting wire according to claim 14, further comprising a mark on a surface of the electric insulation part along a longitudinal direction of the insulation-coated compound superconducting wire, the mark indicating a direction in which the insulation-coated compound superconducting wire should be bent.

16. A method for rewinding the insulation-coated compound superconducting wire according to claim 1, from a first winding member to a second winding member, the method comprising: winding off the insulation-coated compound superconducting wire from the first winding member in a tangential direction of the first winding member; and winding the insulation-coated compound superconducting wire around the second winding member, while bending the insulation-coated compound superconducting wire in the same direction as the direction in which the insulation-coated compound superconducting wire was wound around the first winding member.

17. The insulation-coated compound superconducting wire according to claim 2, further comprising a Sn diffusion prevention part between the compound superconductor part and the reinforcing part.

18. The insulation-coated compound superconducting wire according to claim 2, wherein the electric insulation part comprises a resin material.

19. The insulation-coated compound superconducting wire according to claim 2, wherein a volume ratio of the reinforcing part relative to the compound superconducting wire is larger than a volume ratio of the compound superconductor part relative to the compound superconducting wire.

20. The insulation-coated compound superconducting wire according to claim 2, wherein a total of a volume ratio of the second stabilizing material relative to the compound superconducting wire and a volume ratio of the third stabilizing material relative to the compound superconducting wire is 45% or more.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0049] FIG. 1 is a schematic diagram illustrating a cross-section of an insulation-coated compound superconducting wire according to an embodiment of the present invention;

[0050] FIG. 2 is a graph of critical currents of the insulation-coated compound superconducting wire of Example 5A and the compound superconducting wire (without insulation coating) of Comparative Example 5 measured under measurement condition B;

[0051] FIG. 3 is a typical process flow chart for illustrating a production method of the insulation-coated compound superconducting wire according to an embodiment of the present invention;

[0052] FIG. 4 is a schematic drawing showing an example of arrangement of bending pulleys which constitute a bending strain application apparatus used in pre-bending strain application step S3;

[0053] FIG. 5 is a schematic drawing showing another example of arrangement of bending pulleys which constitute the bending strain application apparatus used in pre-bending strain application step S3; and

[0054] FIG. 6 is a drawing for explaining a bending diameter in the rewinding method of the insulation-coated compound superconducting wire according to the embodiment of the present invention.

PREFERRED MODE FOR CARRYING OUT THE INVENTION

[0055] Subsequently, preferable embodiments of the insulation-coated compound superconducting wire according to the present invention is explained in detail below.

[Insulation-Coated Compound Superconducting Wire]

[0056] FIG. 1 is a schematic diagram illustrating a cross-section structure of the insulation-coated compound superconducting wire 1 according to an embodiment of the invention. The insulation-coated compound superconducting wire 1 of the present embodiment illustrated in FIG. 1 mainly includes a compound superconducting wire 10 and an electric insulation part 30 coating an outer circumferential surface of the compound superconducting wire 10.

<Compound Superconducting Wire>

[0057] The compound superconducting wire 10 mainly includes a compound superconductor part 11, a reinforcing part 12, and a stabilizing part 13.

(Compound Superconductor Part)

[0058] The compound superconductor part 11 mainly includes a plurality of compound superconducting filaments 15 each including a compound superconducting phase, and a first matrix 16 including the plurality of compound superconducting filaments 15 embedded therein and a first stabilizing material. The compound superconductor part 11 forms a core-like shape as a whole.

[0059] The compound superconducting phase is preferably a metal compound superconducting phase including Nb.sub.3Sn (niobium-tin), but is not limited thereto, and may include, for example, Nb.sub.3Al (niobium-aluminum) or other compound superconducting phases having superconducting properties.

[0060] The first stabilizing material constituting the first matrix 16 is preferably copper (Cu) or a copper alloy. By disposing the first matrix 16, it is possible to achieve an effect of suppressing damage to the compound superconductive filament 15, providing magnetic stabilization, and thermal stabilization in the insulation-coated compound superconducting wire 1.

[0061] Note that FIG. 1 shows a compound superconductor part 11 produced by a so-called bronze process, in which a plurality of Nb filaments are embedded in a first matrix precursor (first matrix before heat treatment) of Cu—Sn (copper-tin)-base alloy, which is the first stabilizing material, the embedded Nb filaments are subjected to drawing processing, etc. to form a compound superconducting precursor strand; the compound superconducting precursor strand is subjected to heat treatment; this diffuses Sn in the first matrix precursor and allows the Sn to react with surfaces of Nb filaments; and thereby an Nb.sub.3Sn filament is formed from the Nb filament. The enlarged view of the compound superconductor part 11 shown in FIG. 1 indicates a case in which a core portion 17 of unreacted Nb remaining without reacting with Sn exists. However, with respect to the compound superconductor part 11, it is possible to produce the compound superconducting filament 15 after heat treatment as a filament in which the core portion 17 of unreacted Nb does not exist and all of which consists of Nb.sub.3Sn, depending on the amount of Sn contained in the first matrix precursor and a diameter size of the Nb filament before heat treatment.

[0062] Further, Cu—Sn (copper-tin) base alloy of the first matrix precursor can contain 15.8 mass % of Sn at the maximum (solid solution limit). In addition, elements other than Cu and Sn may be contained as long as they are in small amounts, and it is preferable to contain, for example, Ti or the like in a range of 0.2 to 0.3 mass %.

[0063] On the other hand, it is necessary to take into consideration that even though an Sn content in the Cu—Sn base alloy which constitutes the first matrix 16 is typically reduced to about 1 to 2 mass % after the Nb.sub.3Sn generation heat treatment, depending on the heat treatment conditions, as a result of being used to produce an Nb.sub.3Sn filament 15, a function as a stabilizer substantially corresponding to Cu is not exhibited.

(Reinforcing Part)

[0064] The reinforcing part 12 includes a plurality of reinforcing filaments 18 and a second matrix 19 including a second stabilizing material 20, is disposed on the outer circumferential side of the compound superconductor part 11, and has a cylindrical shape as a whole. Further, the reinforcing part 12 is obtained by embedding a plurality of reinforcing filaments 18 in the second matrix 19.

[0065] It is preferable that the reinforcing filament 18 is formed by mainly containing at least one metal or an alloy of two or more metals selected from the group consisting of Nb, Ta, V, W, Mo, Fe, Ti, and Hf. Herein, it should be noted that the reinforcing filament 18 “mainly contains” refers to the point that unavoidable impurities may be contained therein.

[0066] For example, a reinforcing filament 18 which mainly contains Nb may contain some unavoidable impurities including O: 150 ppm or less, H: 15 ppm or less, C: 100 ppm or less, N: 100 ppm or less, Fe: 50 ppm or less, Ni:50 ppm or less, Ti: 20 ppm or less, Si: 50 ppm or less, W: 300 ppm or less, and Ta: 1,000 ppm or less. Further, a reinforcing filament 18 which mainly contains Ta may contain some unavoidable impurities including O, H, C, N, Fe, Ni, Ti, Si, W, Nb, and Mo.

[0067] Since these metals or alloys constituting the reinforcing filament 18 do not easily dissolve in Cu as a solid during the heat treatment of the compound superconductor generation, a compound with Cu is unlikely to be easily formed. Therefore, these metals or alloys effectively contribute to improvement in bending strain properties. It should be noted that in the embodiment of the present invention, as a material constituting the reinforcing filament 18, Nb, Ta, V, W, Mo and Hf which do not exhibit ferromagnetism are preferred, considering an effect on the insulation-coated compound superconducting wire 1, and further, Nb, Ta or V is preferred from the viewpoint of workability.

[0068] Further, as the alloy including two or more metals selected from the above-described group, an Nb—Ta alloy is preferred in the point of excellency in composite workability with copper or a copper alloy. As an alloy including a metal selected from the group and copper, a Cu—Nb alloy or a Cu—V alloy is preferred in the point of excellency in composite workability with copper or a copper alloy.

[0069] It should be noted that the description “not easily dissolve in Cu” as described above refers to the point that a metal or an alloy constituting the reinforcing filament 18 dissolves in Cu as a solid in a content of less than 1 at. % at a temperature during the heat treatment (e.g., 600° C. to 750° C.) to form the compound superconductor.

[0070] As described above, by adopting a configuration of the reinforcing part 12 in which a plurality of the reinforcing filaments 18 mainly containing a metallic material which does not easily dissolve in Cu as a solid are embedded in the second matrix 19, it is possible to suppress the formation (existence) of an intermetallic compound in the reinforcing filament 18 in the reinforcing part 12, and thereby to form a reinforcing member having high strength against tensile strain and bending strain. It should be noted that in FIG. 1, the second stabilizing material 20 constituting the reinforcing part 12 is configured by a portion 20a which embeds the reinforcing filaments 18 and a cylindrical outer circumferential portion 20b surrounding the outer circumference of the embedding portion 20a as different portions. However, these portions 20a and 20b can may be integrally configured.

[0071] It is preferable that the second stabilizing material 20 mainly contains copper or a copper alloy. It should be noted that the second stabilizing material 20 “mainly contains” refers to the point that unavoidable impurities may be contained. Herein, the unavoidable impurities include O, Fe, S and Bi. By disposing the second stabilizing material 20, it is possible to achieve effects that the reinforcing part 12 can have not only a strengthening function but also a stabilizing function.

[0072] Further, the volume ratio of the reinforcing part 12 relative to the compound superconducting wire 10 is preferably 40% or more, and more preferably 45% or more. By setting the volume ratio to 40% or more, the tensile strength can be effectively improved. It should be noted that the upper limit of the volume ratio is preferably set to 65% or less, from the viewpoint of ensuring a critical current.

[0073] The volume ratio (%) of the reinforcing part 12 relative to the compound superconducting wire 10 is preferably larger than the volume ratio (%) of the compound superconductor part 11 relative to the compound superconducting wire 10. Specifically, the volume ratio (%) of the reinforcing part 12 relative to the compound superconducting wire 10 is preferably 4% or more, and more preferably 10% or more. Generally, when the volume ratio of the reinforcing part 12 is larger than the volume ratio of the compound superconductor part 11, the tensile strength as the compound superconducting wire 10 is increased, but the critical current tends to decrease. This is because the volume ratio of the compound superconductor part 11 becomes relatively small. In the present invention, as described below, the critical current can be increased by providing the insulation coating and thereby it is possible to improve the tensile strength while suppressing a decrease in the critical current and maintaining the critical current at the same level as the critical current of prior art. It should be noted that if the volume ratio (%) of the reinforcing part 12 relative to the compound superconducting wire 10 is too large, good superconducting properties cannot be obtained. Therefore, the volume ratio (%) of the reinforcing part 12 is preferably not larger than 45% with respect to the volume ratio (%) of the compound superconductor part 11 relative to the compound superconducting wire 10.

(Stabilizing Part)

[0074] The stabilizing part 13 is disposed on at least one side of the inner circumferential side and the outer circumferential side of the reinforcing part 12. In FIG. 1, the stabilizing parts 13 are disposed on both the inner circumferential side and the outer circumferential side of the reinforcing part 12. The stabilizing part 13 includes a third stabilizing material and forms a cylindrical shape as a whole. By disposing the stabilizing part 13, it is possible to suppress abnormal deformation during processing of the reinforcing part 12 and to provide a stabilizing function.

[0075] It is preferable that the third stabilizing material mainly includes copper or a copper alloy. It should be noted that “mainly includes” in the third stabilizing material refers to the point that unavoidable impurities may be contained. Here, the unavoidable impurities include O, Fe, S and Bi.

[0076] Further, it is preferable that the total of the volume ratio (%) of the second stabilizing material constituting the reinforcing part 12 and the volume ratio of the third stabilizing material constituting the stabilizing part 13 relative to the compound superconducting wire 10 is 45% or more. By setting the total of the volume ratio of the second stabilizing material in the reinforcing part 12 and the volume ratio of the third stabilizing material constituting the stabilizing part 13, which are disposed on the outer side of the compound superconductor part 11, to 45% or more, the insulation-coated compound superconducting wire 1 can have stabilizing materials at a sufficiently large volume ratio, and it is possible to ensure the electrification stability.

[0077] In the insulation-coated compound superconducting wire 1 of the present invention, the first stabilizing material constituting the compound superconductor part 11, the second stabilizing material constituting the reinforcing part 12, and the third stabilizing material constituting the stabilizing part 13 are used, herein the “stabilizing material” refers to a material, generally a metal, which is electrically and/or thermally in contact with a superconductor so as to ensure thermal contact with a refrigerant and/or act as an electric shunt circuit, as defined in JIS H 7005: 2005. The stabilizing material refers to normal conducting metal material which is complexed to a superconductor to enhance stability of the superconductor. Specifically, normal conducting metals such as copper and aluminum have good thermal conductivity and low specific resistance at cryogenic temperature, so that when used as a matrix for a superconducting wire, electric current flows through these normal conducting metals as bypass even if there is transition from the superconducting state to the normal conducting state. Thus, heat generation is suppressed, and the generated heat is rapidly propagated and diffused, and then it is cooled. Furthermore, normal conducting metals such as copper and aluminum, which dump external magnetic flux variation and do not directly transmit magnetic flux variation to the superconductor, are widely used as the stabilizing material for the superconducting wire.

(Optional Component of Compound Superconducting Wire)

[0078] A compound superconducting wire 10 constituting the insulation-coated compound superconducting wire 1 of the present invention includes the compound superconductor part 11, the reinforcing part 12, and the stabilizing part 13 as essential components, but may further have other components.

[0079] For example, it is possible to dispose a Sn diffusion prevention part 14 between the compound superconductor part 11 and the reinforcing part 12. It is also possible to provide a heat-resistant plated part 29 having a thickness of 1 μm or less between the outer circumferential surface of the compound superconducting wire 10 and the electric insulation part 30.

[0080] The Sn diffusion prevention part 14 preferably includes Nb or Ta or an alloy or composite thereof. The Sn diffusion prevention part 14 has a function of preventing Sn in a Cu—Sn base alloy, which constitutes the first matrix 16 to form the Nb.sub.3Sb filament in the compound superconductor part 11, from diffusing into the reinforcing part 12 or the stabilizing part 13, and thereby not only suppressing decrease in the residual resistance ratio of the second and third stabilizing materials, which constitute the reinforcing part 12 and the stabilizing part 13, but also retaining a Sn quantity required to react with an Nb filament to produce Nb.sub.3Sn in the Cu—Sn base alloy.

[0081] The total of the volume ratio of the reinforcing filament 18 constituting the reinforcing part 12 and the volume ratio of the Sn diffusion prevention part 14 relative to the compound superconducting wire 10 is preferably 7% or more, and more preferably 15% or more. Since the total of the volume ratio of the reinforcing filament 18 in the reinforcing part 12 and the volume ratio of the Sn diffusion prevention part 14 is 7% or more, it is possible to enhance the strength of the compound superconducting wire 10 itself, to improve rewindability of the compound superconducting wire 10, and to facilitate the react-and-wind process. These volume ratios can be freely designed depending on the characteristics and volume of the compound superconductor part 11.

[0082] Further, the total of the volume ratio of the compound superconductor part 11 and the volume ratio of the Sn diffusion prevention layer 14 can be freely designed according to the critical current required in the compound superconducting wire 10, but is preferably 20% or more, and more preferably 30% or more. When the total of the volume ratio is 20% or more, it is possible to attain a practical critical current value in the superconducting wire obtained by using the react-and-wind process.

[0083] Furthermore, a current-carrying capacity can be increased by using as the compound superconducting wire 10, which constitutes the insulation-coated compound superconducting wire 1 of the present invention, having a large wire diameter. Further, an allowable bending diameter can be decreased by using a superconducting wire 10 having a small wire diameter. Thereby, it is possible to obtain an appropriate superconducting wire, depending upon each of the superconducting application apparatuses. The wire diameter of the compound superconducting wire 10 is preferably in a range of 0.2 mm or more and 2.0 mm or less. This is because when the wire diameter is larger than 2.0 mm, flexibility becomes poor, and the handling property tends to be poor, and when the wire diameter becomes smaller than 0.2 mm, the strength of the compound superconducting wire 10 itself becomes weak, so that the handling property tends to be poor.

<Electric Insulation Part>

[0084] In the insulation-coated compound superconducting wire 1 of the present embodiment, an electric insulation part 30 covers the outer circumferential surface of the compound superconducting wire 10, and thereby, the critical current value (Ic) of the insulation-coated compound superconducting wire 1 is larger than the critical current value (Ic) of the compound superconducting wire 10 before being covered with the electric insulation part 30.

[0085] The electric insulation part 30 preferably includes a resin material. The resin material is not particularly limited, but it is preferable to use enamel coating or polyimide tape. Examples of the enamel coating include polyvinyl formal resin (PVF), polyamideimide resin (PAI), polyimide resin (PI), etc. The polyimide tape may be coated with a self-fusing resin or a prepreg resin.

[0086] Herein, for example, in the conventional compound superconducting wire having an enamel coating as described in Patent Document 1 or the like, a reinforcing part such as Cu—Nb is not disposed on the outer circumferential side of an assembly (compound superconductor part) of compound superconducting fine wires. Therefore, the strength of the wire before the enamel coating is applied is low, and the condition of a pre-bending strain application step described below and the processing condition of the enamel coating must be strictly controlled so as not to damage the wire like applications of bending strain and internal stress. Additionally, the strength of the entire compound superconducting wire after the enamel coating is also low, and when the winding as in react-and-wind process accompanies rewinding, the compound superconducting wire is easily damaged. These damages to the compound superconducting wire lower the critical current values (Ic) of the compound superconducting wire.

[0087] In addition, Patent Document 5 and the like proposed by the present applicant disclose an Example in which an insulating coating of the polyimide tape was applied to the compound superconducting wire having a reinforcing material. However, at that time, control of the strain of the compound superconducting wire was not sufficient. Further, since the insulating coating was merely applied to the compound superconducting wire only to provide the compound superconducting wire with insulation performance, the insulation-coated compound superconducting wire shown in the Example was not the one obtained by forming insulating coating in order to improve the superconductive characteristics as compared with the compound superconducting wire before the insulation coating was applied.

[0088] In contrast, the present inventors have found that a decrease in residual strain generated in the compound superconducting wire when forming the electric insulation part improves the critical current value (Ic), and as a result, the critical current value (Ic) of the insulation-coated compound superconducting wire 1 can be made larger than the critical current value (Ic) of the compound superconducting wire 10 before being coated with the electric insulation part 30.

[0089] With respect to the measurement conditions of the critical current value Ic of the insulation-coated compound superconducting wire 1 and the compound superconducting wire 10, the critical current value can be measured according to any of the following <measurement condition A> and <measurement condition B> when the compound superconducting phase is, for example, Nb.sub.3Sn.

{Measure of Critical Current Value Ic}

<Measurement Condition A>

[0090] A predetermined tensile stress of 150 MPa or more and 250 MPa or less is applied at room temperature to each of the insulation-coated compound superconducting wire 1 and the compound superconducting wire 10 before being coated with the electric insulation part 30, followed by unloading, then each of the wires is cooled to a temperature of 4.2 K, and the critical current value (Ic) is measured by conducting electric current through each of the wires while the tensile stress is unloaded and an external magnetic field of 14.5 T is applied. Herein, a strain rate for applying the predetermined tensile stress is set to 10.sup.−4 to 10.sup.−3/s. It should be noted that the “room temperature” in the present invention refers to a temperature in the range from 10° C. to 35° C. Further, the tensile stress of the insulation-coated compound superconducting wire 1 is obtained by excluding the electric insulation part 30 from the insulation-coated compound superconducting wire 1, that is, the tensile stress of the insulation-coated compound superconducting wire 1 is per compound superconducting wire. To measure the critical current value (Ic), a four-terminal method is applied. A sample length is set to 40 mm or more, a distance between voltage taps is set to 10 mm or more, and the critical current value is determined following the definition of 10 μV/m, using an n value determined in the electric field of 100 μV/m to 1,000 μV/m based on the characteristics (V is proportional to I.sup.n) of conducted current I measured and generated voltage V. It should be noted that in order to attach electrodes to the insulation-coated compound superconducting wire 1, when the critical current value (Ic) is measured, the electric insulation part 30 may be removed from the insulation-coated compound superconducting wire 1. The electric insulation part 30 may be completely removed or partially removed at both ends. When the electric insulation part 30 is removed, attention should be paid so that stress to an extent that changes the critical current values (Ic) of the insulation-coated compound superconducting wire 1 is not applied to the compound superconducting wire 10.

<Measurement Condition B>

[0091] Each of the insulation-coated compound superconducting wire 1 and the compound superconducting wire 10 before being coated with the electric insulation part 30 is cooled to a temperature of 4.2 K, and the critical current value (Ic) is measured by conducting electric current through each of the wires while a predetermined tensile stress of 150 MPa or more and 250 MPa or less and an external magnetic field of 14.5 T are applied. Other conditions are the same as those of the measurement condition A described above.

[0092] Generally, it is known that when a magnet is constructed by making a superconducting wire into a coil-like shape and then this magnet is cooled to operate in a superconducting state, tensile stress is applied to the superconducting wire in the axial direction of the superconducting wire by an electromagnetic force (hoop force). Therefore, when the critical current of a superconducting wire used for magnet is evaluated, it is necessary to measure the critical current while tensile stress reflecting actual operation conditions is applied so as to experience tensile strain for the superconducting wire.

[0093] In the measurement condition B, it is assumed that when magnets each including the insulation-coated compound superconducting wire 1 or the compound superconducting wire 10 before being coated with the electric insulation part 30 are cooled to 4.2 K and operated in superconducting states, a hoop force is generated in the respective superconducting wires 1 and 10. The critical currents are measured while applying tensile stress at 4.2 K to each of the superconducting wires 1 and 10 in the axial direction. By applying tensile strain to the respective superconducting wires 1 and 10, a state of strain in the compound superconductor part changes. When the compressive strain applied to the compound superconductor in the initial state becomes zero due to application of tensile strain, the critical current value reaches a maximum, and thereafter, the critical current value decreases with increasing tensile strain. When excessive tensile strain is applied, breakage of superconducting filament in the compound superconducting wire occurs and deterioration occurs, and the critical current value does not return to the original value even when the tensile strain is unloaded. In particular, a superconducting filament in which deterioration of the critical current due to superconducting filament breakage occurs at a strain corresponding to predetermined tensile stress of 150 MPa or more and 250 MPa or less at 4.2 K is not suitable for practical use.

[0094] In the measurement condition A, a tensile stress equivalent to that applied in the measurement condition B is applied at room temperature, followed by unloading (preloading treatment), and then the critical current is measured at 4.2 K. This preloading treatment can change the final residual strain after cooling to 4.2 K, which is residual strain subjected to the compound superconducting filaments, widely from compression to zero and even to tensile (preloading effect) by changing load stress level.

[0095] Measurement condition A allows a simple and convenient evaluation since tensile stress can be applied at room temperature. However, when the strength of the superconducting wire itself is insufficient, or when the compressive stress of the compound superconductor is overly relaxed, for example, due to pre-bending strain, application of excessive tensile strain at room temperature results in localized filament breakage of the superconducting filament beyond the elastic strain range. Thus, after unloading, deterioration of the critical current measured at 4.2 K occurs. In particular, if breakage of superconducting filament occurs in a state in which strain corresponding to a predetermined tensile stress of 150 MPa or more and 250 MPa or less is applied at room temperature, followed by unloading, deterioration of the critical current after cooling to 4.2 K occurs. Therefore, it is not suitable for practical use in the react-and-wind process.

[0096] However, when evaluated under any of the conditions, no event of concern occurred, and the insulation-coated compound superconducting wire 1 according to the present invention was confirmed to have a critical current increased after the electric insulation part 30 was formed.

[0097] Thus, in the practically usable evaluation of superconducting characteristics of the insulation-coated compound superconducting wire 1, which is a rewindable insulation-coated compound conductive layer wire produced by, for example, the react-and-wind process, and in which the compound superconducting phase includes Nb.sub.3Sn, an evaluation value of the measurement condition A, in which the measurement is convenient, can be used as a substitute for an evaluation value of the measurement condition B. In addition, when the compound superconducting phase is other than Nb.sub.3Sn, the critical magnetic field and the critical temperature change. Therefore, by appropriately reviewing the magnetic field condition and the temperature condition, the same measurement can be performed.

[0098] Further, in both the measurement conditions A and B, the ground based on which the upper limit value of the predetermined tensile stress is set to 250 MPa is as follows.

[0099] Non-Patent Documents 5 and 6 disclose that when a tensile stress of about 240 MPa is applied, the critical current value Ic at 4.2 K increases over a wide magnetic field range of from 7 T (tesla) to 15 T due to the room temperature preloading effect on the critical current of the Nb.sub.3Sn multicore superconducting composite wire, but when a tensile stress of more than the above-mentioned amount is applied, breakage of Nb.sub.3Sn filament occurs, and decrease in the critical current value Ic occurs. Therefore, as evaluation conditions for confirming an increase in the critical current value after the formation of electric insulation part, which is an effect of the present invention, the tensile stress of 150 MPa or more and 250 MPa or less, in which 240 MPa is included, and the external magnetic field of 14.5 T are selected.

{Relationship Between Critical Current Value Ic (Maximum Value Thereof) and Tensile Stress}

[0100] As another embodiment, it is preferable that the tensile stress when the critical current value Ic of the insulation-coated compound superconducting wire 1 becomes maximum is smaller than that of the compound superconducting wire 10 before being coated with the electric insulation part 30. The relationship between the critical current value Ic (maximum value thereof) and the tensile stress (tensile strain) of the insulation-coated compound superconducting wire 1 can be measured at each stage of the manufacturing process of the insulation-coated compound superconducting wire 1, while conducting electric current through each of the insulation-coated compound superconducting wire 1 and the compound superconducting wire 10 at 4.2 K.

[0101] In each of the superconducting wires 1 and 10, upon comparing the insulation-coated compound superconducting wire 1 to which the insulation coating has been provided with an electric insulation material such as PVF (polyvinyl formal) and the compound superconducting wire 10 before the electric insulation part 30 is formed, it is seen in the relationship between the critical current value Ic and the tensile stress that the tensile stress at which the critical current value Ic becomes maximum decreases and the maximum value itself of the critical current value Ic increases after the formation of the electric insulation part 30. FIG. 2 is a graph as an example obtained by measuring the critical current value under the measurement condition B with respect to the insulation-coated compound superconducting wire (Example 5A) and the compound superconducting wire (without insulation coating) (Comparative Example 5).

[0102] As described above, considering stress relaxation history which is thermally and mechanically generated due to application of the insulation coating with the electric insulation part 30, a pre-bending strain application step is performed. Namely, the electric-insulation part 30 is formed on the outer circumferential surface of the compound superconducting wire 10 so that the maximum value of the critical current value Ic is finally obtained at a smaller tensile strain and smaller tensile stress than when the pre-bending is applied. The stress relaxation history generated thermally and mechanically is imparted, and thereby it is possible to obtain a further increased critical current Ic, compared to the critical current Ic of the compound superconducting wire 10 after performing the pre-bending strain application step.

{Other Embodiments of Insulation-Coated Compound Superconducting Wire}

[0103] As another embodiment, heat treatment to form the compound superconducting phase is applied while the compound superconducting precursor strand before the heat treatment to form the compound superconducting phase is bent and wound around a winding member having a bending diameter corresponding to 100 times or larger than the maximum dimension of the compound superconductor part 11; and during a time period after forming the compound superconducting wire 10 by the heat treatment until coating the electric insulation part 30 on the outer circumferential surface of the compound superconducting wire 10 is finished, it is preferable that the tensile strain to the compound superconducting wire is 0.2% or less and the bending strain within ±0.5% to the compound superconductor part 11 is applied in the positive and negative directions at least 10 times within a temperature range from room temperature to 500° C. Thereby, it is possible to properly control the residual strain present in the compound superconducting wire 10 before the electric insulation part is formed.

[0104] Further, it is preferable that a mark is provided on the surface of the electric insulation part 30, along the longitudinal direction of the insulation-coated compound superconducting wire, to indicate the direction in which the insulation-coated compound superconducting wire 1 should be bent. Thereby, in order to properly control the residual strain of the compound superconducting wire, based on the history of the applied direction of the pre-bending strain applied to the insulation-coated compound superconducting wire 1, it is possible to easily know the direction in which the insulation-coated compound superconducting wire 1 should be bent at the time of rewinding the insulation-coated compound superconducting wire 1. For example, when the insulation-coated compound superconducting wire 1 is rewound to a superconducting coil, it is easy to rewind so that the state of the residual strain in the insulation-coated compound superconducting wire 1 does not significantly change. It should be noted that it is sufficient that the mark indicating the direction in which the insulation-coated compound superconducting wire 1 should be bent may be provided so as to show a winding direction, and for example, the mark may be hidden inside rather than on a front side.

[Method for Producing Insulation-Coated Compound Superconducting Wire]

[0105] Subsequently, a method for producing the insulation-coated compound superconducting wire 1 of the present embodiment is described below. FIG. 3 is a flow chart showing steps of the production method of the insulation-coated compound superconducting wire of the present embodiment. The method for producing the insulation-coated compound superconducting wire in the embodiment shown in FIG. 3 mainly includes a wire forming step S1, a heat treatment step S2, a pre-bending strain application step S3, an insulation coating step S4, and a pure bending strain application step S5.

[0106] By the method for producing the insulation-coated compound superconducting wire of the present embodiment, it is possible to produce coils by the react-and-wind process. Depending upon the cross-sectional structure of the strand, the internal strain of the compound superconductor part 11 is controlled through a series of manufacturing steps S1 to S5 described above, and the wire is less likely to be damaged during the manufacturing. Further, since a method of use with regard to the winding direction when performing winding of a magnet has been clarified, it is possible to obtain excellent electrical conduction characteristics during operation of the produced magnet. Thus, it is possible to design a magnet at a proper operation safety factor, resulting in reduction of a wire cost. Hereinafter, the respective steps are described below by referring, as an example, to an insulation-coated compound superconducting wire, in which the compound superconducting phase includes Nb.sub.3Sn, the production method is the bronze process, a composite material including a Cu—Nb alloy is used as the reinforcing part, and enamel coating has been applied.

(Wire Forming Step)

[0107] The wire forming step S1 is a step which includes: providing a compound superconducting precursor part including a plurality of Nb filaments and a matrix including a Cu—Sn base alloy in which these Nb filaments are embedded; sequentially arranging on the outer circumferential side of the compound superconducting precursor part, an Sn diffusion prevention part 14, a reinforcing part 12, and a stabilizing part 13 to form a billet; extruding the billet; and then performing wire drawing to form a wire which is a compound superconducting precursor strand before the heat treatment step S2 for forming a compound superconducting phase. As the wire forming step S1, for example, when the compound superconducting phase includes Nb.sub.3Sn, a known wire forming step for producing an Nb.sub.3Sn wire such as an internal tin (Sn) diffusion method or a powder in tube (PIT) method can be applied in addition to the above bronze process.

(Heat Treatment Step)

[0108] The heat treatment step S2 is a heat treatment step for forming a compound superconducting phase. After performing the heat treatment in the heat treatment step S2, when the temperature is lowered from the heat treatment temperature (e.g., 670° C., 96 hours) to room temperature (e.g., 20° C.), compressive stress (compressive strain) remains in the Nb.sub.3Sn filaments constituting the compound superconductor part 11 and the Sn diffusion prevention part 14 including Ta, Nb, etc., due to difference in the thermal expansion coefficient of members constituting the wire. Further, tensile stress (tensile strain) remains in the first stabilizing material (Cu—Sn base alloy material) of the first matrix constituting the compound superconductor part 11, the second stabilizing material constituting the reinforcing part 12, and the third stabilizing material constituting the stabilizing part 1:3. Under such a state, when a wire in which a reinforcing material is not disposed as described in, for example, Patent Document 1, is stretched or bent at room temperature, the Sn diffusion prevention part 14 which has not yielded, or Nb.sub.3Sn filaments constituting the compound superconductor part 11 serve as a member to be subject to tension within the cross section of the wire.

[0109] In contrast, in the present invention, the reinforcing part 12 including Cu—Nb having a large thermal expansion coefficient and large yield stress is disposed on the outer circumference of the Nb.sub.3Sn filament group, and thereby even when the wire is stretched or bent at room temperature, the reinforcing part 12 can be subject to the tension in the cross section of the wire. Therefore, the Nb.sub.3Sn filaments are less likely to be damaged, compared to conventional compound superconducting wire in which a reinforcing part is not disposed and in which only the Sn diffusion prevention part 14 or Nb.sub.3Sn filaments are subject to the tension. Further, by choosing the magnitude of repeated bending strain depending upon the cross-sectional structure of the compound superconducting wire, it is possible to increase the strength in the reinforcing part 12 and relax the compressive stress of the Nb.sub.3Sn filament group, resulting in improvement in the superconductive performance under the use environment of the magnet. If the heat treatment is performed while a compound superconducting wire is wound around a winding member such as a heat treatment bobbin, an Nb.sub.3Sn filament is formed in a shape based on its winding diameter Dh.

(Pre-Bending Strain Application Step)

[0110] The pre-bending strain application step S3 is a step in which bending procession is applied to the superconducting wire W obtained in the heat treatment step S2, to add a predetermined bending strain. It should be noted that when the critical current value (Ic) of the insulation-coated compound superconducting wire 1 can be increased as compared with that of the compound superconducting wire 10 before being coated with the electric insulation part 30, only by the formation of the electric insulation part 30 to be performed in the subsequent insulation coating step S4, the pre-bending strain application step S3 may be omitted. FIGS. 4 and 5 illustrate an example of the arrangement of bending pulleys constituting the bending strain application apparatus to be used in the pre-bending strain application step S3. In particular, FIG. 4 shows arrangement of pulleys 43 of a bending strain application apparatus 40, in which the superconducting wire W wound around a heat treatment bobbin 41 is linearly wound off without making the superconducting wire W rotate in the axial direction thereof, then the superconducting wire W is made to pass the ten positive direction bending pulleys 43 so that bending strain is sequentially added to the superconducting wire W in the positive direction, and then the superconducting wire W is wound up by the winding member 44. It is possible to apply bending strain in the positive direction 10 times and to apply bending strain in the reverse direction 11 times by returning to linear line state. Meanwhile, FIG. 5 shows arrangement of pulleys of a bending strain application apparatus 40A, in which the superconducting wire W wound around a heat treatment bobbin 41 is linearly wound off without making the superconducting wire W rotate in the axial direction thereof, then the superconducting wire W is made to pass five reverse direction bending pulleys 42 and five positive direction bending pulleys 43 alternatively, so that bending strain in the positive and reverse directions is applied five times each, and then the superconducting wire W is wound up by the winding member 44.

[0111] When the superconducting wire W which is wound around the heat treatment bobbin 41 in an arc shape is wound off without making the superconducting wire W to rotate axially and is linearly bent so as to be deformed, the superconducting wire W is subject to bending strain ε.sub.b-straight indicated in the following equation (1A) due to a curved linear state. More specifically, the superconducting wire W is bent in a straight line from an arc shape, and thereby the outer side portion (outer winding portion) of the surface of the wire W which has been wound around the bobbin 41 is subject to strain in the compression direction (− sign), whereas the inner side portion (inner winding portion) of the surface of the wire W is subject to tensile strain (+ sign) in the direction opposite to the direction in which the outer side of the surface is subject to the compressive strain. Here, the neutral line (or neutral plane) of the bending strain is assumed to be in the center of the wire W.

[00001]$\left[\mathrm{Mathematical}\mathrm{Formula}1\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{b\text{-}\mathrm{straight}}=\pm d\left(-\frac{1}{D_h+d}\right)\cong \mp d\left(\frac{1}{D_h}\right)& \left(1A\right)\end{array}$

[0112] Note that d represents the diameter (mm) of the compound superconducting wire 10 constituting the insulation-coated compound superconducting wire 1 (see FIG. 1), and D.sub.h represents the diameter of the heat treatment bobbin 41 (see FIG. 6).

[0113] Thereafter, when the insulation-coated compound superconducting wire 1 is wound around a positive direction bending pulley 43 with a diameter of D1, which is arranged in the same direction (positive direction) as when it was wound around the heat treatment bobbin 41, the insulation-coated compound superconducting wire 1 is subject to positive direction bending strain ε.sub.b-positive indicated in the following formula (2A). More particularly, the outer side portion of the surface of the wire W is subject to tensile strain, and the inner side portion of the surface of the wire W is subject to compressive strain in the direction opposite to the direction in which the outer side portion of the surface is subject to the tensile strain.

[00002]$\left[\mathrm{Mathematical}\mathrm{Formula}2\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{b\text{-}\mathrm{positive}}=\pm d\left(\frac{1}{D_1+d}-\frac{1}{D_h+d}\right)\cong \pm d\left(\frac{1}{D_1}-\frac{1}{D_h}\right)& \left(2A\right)\end{array}$

[0114] Note that d represents the diameter (mm) of the compound superconducting wire 10 constituting the insulation-coated compound superconducting wire 1 (see FIG. 1), and D.sub.h represents the diameter of the heat treatment bobbin 41 (see FIG. 6).

[0115] On the other hand, when the insulation-coated compound superconducting wire 1 is wound around a reverse direction bending pulley 42 with a diameter of D2, which is arranged in the opposite direction (reverse direction) as when it was wound around the heat treatment bobbin 41, the insulation-coated compound superconducting wire 1 is subject to reverse direction bending strain ε.sub.b-negative indicated in the following formula (3A). More specifically, the outer side portion of the surface of the wire W is subject to compressive strain, and the inner side portion of the surface of the wire W is subject to tensile strain in the direction opposite to the direction in which the outer side portion of the surface is subject to the compressive. strain.

[00003]$\left[\mathrm{Mathematical}\mathrm{Formula}3\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{b\text{-}\mathrm{negative}}=\pm d\left(-\frac{1}{D_2+d}-\frac{1}{D_h+d}\right)\cong \mp d\left(\frac{1}{D_2}+\frac{1}{D_h}\right)& \left(3A\right)\end{array}$

[0116] In the pre-bending strain application step including applying repeated bending strain to the wire W after the heat treatment step S3, the bending directivity of the wire W is maintained by controlling the bending direction, bending diameter, and tensile stress. As a result, residual strain distribution in the cross section continuously over the longitudinal direction of the wire W is maintained. Therefore, the stabilizing material located near the neutral line of bending has a lower strength than the stabilizing material located on the outer side or the inner side of the bending direction subject to the bending strain. When a difference is significant, the difference can be detected by micro Vickers hardness test. By controlling a holding direction of the bending directivity of the wire W to the same direction as the bending direction side during heat treatment, more specifically, the spring back direction (the original direction to which the wire tries to return) toward the direction in which the wire has been wound around the heat treatment bobbin in an arc shape, not only in the pre-bending strain application step S3 but also in a subsequent step, reverse direction bending strain exceeding the allowable limit is applied. Thus, it is possible to prevent the compound superconducting filament from being broken. It should be noted that the allowable limit strain at which the compound superconducting filament is broken varies depending on the material of the superconductor, the cross-sectional structure of the wire, the heat treatment condition, the pre-bending strain application condition, etc.

(Insulation Coating Step)

[0117] The insulation coating step S4 is a step including coating the outer circumferential surface of the compound superconducting wire 10 with the electric insulation part 30, so that the critical current value (Ic) of the insulation-coated compound superconducting wire 1 coated with the electric insulation part 30 is larger than that of the compound superconducting wire 10 before being coated with the electric insulation part 30.

[0118] Specifically, the electric insulation part may be formed in the insulation coating step S4 by setting: the maximum temperature of the compound superconducting wire 10 to less than 500° C.; the maximum value of the bending strain to be applied to the compound superconducting wire 10 to less than the bending strain to be applied in the pre-bending strain application step S3; and the tensile strain to 0.2% or less. The maximum temperature of the compound superconducting wire 10 during forming the electric insulation part of 500° C. or higher is undesirable, since the superconducting properties and mechanical strength may be adversely affected.

[0119] Note that, before the insulation coating step S4, it is also possible to further form a heat-resistant plated part 29 having a thickness of 1 μm or less on the outer circumferential surface of the compound superconducting wire 10. The heat-resistant plated part 29 to be applied to the surface of the compound superconducting wire 10 aims at preventing the superconducting wires 10 from adhering to each other to reliably separate the superconducting wires 10 when the superconducting wires 10 are in contact with each other in the heat treatment to form the compound superconducting phase, or at preventing coating malfunction occurrence in the insulation coating step S4. The coating malfunction may be due to irregularity occurrence on the surface of the superconducting wire 10 caused by softening shape change. When the thickness of the heat-resistant plated part 29 is larger than 1 μm, diffusion into the stabilizing part 13 and the stabilizing material of the reinforcing part 12 is occurred during the compound superconducting layer forming heat treatment, this resulting in an increase in the resistance value of the stabilizing material. In addition, there is a possibility of disadvantage in terms of manufacturing cost. Therefore, the thickness of the heat-resistant plated part 29 is preferably equal to or less than 1 μm. It is desirable to select presence or absence of plating depending on the application. Further, the lower limit of the thickness of heat-resistant plated part 29 is not particularly limited, but may be set to 0.1 μm or more from the viewpoint that, in manufacturing, the coating thickness is easily stabilized and the effect of the present invention is easily obtained. Furthermore, not only single metal plating such as Cr, Ni, etc., but also alloy plating such as Ni—P, Ni—B, Cr—C, or Ni—W can be applied as the material. When the compound superconductor is Nb.sub.3Sn, the plating material is preferably Cr.

(Pure Bending Strain Application Step)

[0120] The pure bending strain application step S5 is a step including winding the insulation-coated compound superconducting wire 1 after the insulation coating step S4 around a winding member 44, while limiting the bending strain ε.sub.pure,bend loaded to the insulation-coated compound superconducting wire, to form the superconducting coil.

[0121] The outer side portion of the surface and the inner side portion of the surface of the insulation-coated compound superconducting wire 1 wound around the winding member 44 having a diameter of D.sub.3 is subject to the pure bending strain indicated in the following formula (4A).

[00004]$\left[\mathrm{Mathematical}\mathrm{Formula}4\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{\mathrm{pure}.\mathrm{bend}}=\pm d\left(\frac{1}{D_3+d}-\frac{1}{D_h+d}\right)\cong \pm d\left(\frac{1}{D_3}-\frac{1}{D_h}\right)& \left(4A\right)\end{array}$

[0122] The maximum bending strain to which the filament in the outer circumferential portion of the group of filaments is subject can be calculated by replacing dimension d as a reference in the formulas (1A) to (4A) with a diameter (diameter of the group of filaments) dfb of the compound superconductor part 11. It should be noted that the neutral line of the bending strain is assumed to be in the center of the group of filaments.

[0123] Given that bending strain when the wire is wound off from the heat treatment bobbin with a drum diameter of Dh and is made linear is ε0 (=ε.sub.fb-straight), ε0 can be represented by the following formula (1B).

[00005]$\left[\mathrm{Mathematical}\mathrm{Formula}5\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{\mathrm{fb}\text{-}\mathrm{straight}}=\pm d_{\mathrm{fb}}\left(-\frac{1}{D_h+d}\right)\cong \mp d_{\mathrm{fb}}\left(\frac{1}{D_h}\right)& \left(1B\right)\end{array}$

[0124] Given that positive direction bending strain when the wire is bent in the positive direction by the positive direction bending pulley 43 having a diameter of D1 is ε1 (=ε.sub.fb-positive), ε1 can be represented by the following formula (2B).

[00006]$\left[\mathrm{Mathematical}\mathrm{Formula}6\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{\mathrm{fb}\text{-}\mathrm{positive}}=\pm d_{\mathrm{fb}}\left(\frac{1}{D_1+d}-\frac{1}{D_h+d}\right)\cong \pm d_{\mathrm{fb}}\left(\frac{1}{D_1}-\frac{1}{D_h}\right)& \left(2B\right)\end{array}$

[0125] Given that reverse direction bending strain when the wire is bent in the reverse direction by the reverse direction bending pulley 42 having a diameter of D2 is ε2 (=ε.sub.fb-negative), ε2 can be represented by the following formula (3B).

[00007]$\left[\mathrm{Mathematical}\mathrm{Formula}7\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{\mathrm{fb}\text{-}\mathrm{negative}}=\pm d_{\mathrm{fb}}\left(-\frac{1}{D_2+d}-\frac{1}{D_h+d}\right)\cong \mp d_{\mathrm{fb}}\left(\frac{1}{D_2}+\frac{1}{D_h}\right)& \left(3B\right)\end{array}$

[0126] Given that pure bending strain when the wire is bent and wound in the positive direction around a drum with a diameter of D3 after the insulation processing is ε3 (==ε.sub.fb-pure,bend), ε3 can be represented by the following formula (4B).

[00008]$\left[\mathrm{Mathematical}\mathrm{Formula}8\right]$$\begin{array}{cc}{\mathrm{.Math.}}_{\mathrm{fb}\text{-}\mathrm{pure}.\mathrm{bend}}=\pm d_{\mathrm{fb}}\left(\frac{1}{D_3+d}-\frac{1}{D_h+d}\right)\cong \pm d_{\mathrm{fb}}\left(\frac{1}{D_3}-\frac{1}{D_h}\right)& \left(4B\right)\end{array}$

[0127] The maximum strain subject to the compound superconducting filament can be discussed by summing up the tensile strain by tension in the axial direction and the maximum tensile bending strain which is applied during wire winding due to the bending diameter. That is, it is necessary for the maximum strain subject to the compound superconducting filament not to exceed the strain at which filament damage occurs. In particular, as indicated by the formula (3B), it is necessary to control the maximum strain applied when the wire is bent in the reverse direction with respect to the bending direction during the heat treatment. Further, operation current of the magnet is decided by considering the superconducting characteristics under the maximum pure bending strain to which the filament is subject after magnet wire winding indicated by the formula (4B).

[Method for Rewinding Insulation-Coated Compound Superconducting Wire]

[0128] The method for rewinding the insulation-coated compound superconducting wire according to the present invention is a rewinding method of the insulation-coated compound superconducting wire described above. As shown in FIG. 6, when the insulation-coated compound superconducting wire W is rewound from a first winding member, e.g., a heat treatment bobbin 21, to a second winding member, e.g., a winding-up bobbin 24 for forming, for example, a superconducting coil, via a positive direction bending pulley 22 and a reverse direction bending pulley 23, it is preferred that the insulation-coated compound superconducting wire 1 is wound off (unwound) from the heat treatment bobbin 21 in the tangential direction of the heat treatment bobbin 21 and wound up around the winding-up bobbin 24 while bending the insulation-coated compound superconducting wire 1 in the same direction as the direction in which the insulation-coated compound superconducting wire 1 has been wound around the heat treatment bobbin 21.

OTHER EMBODIMENTS

[0129] It should be noted that the embodiments described above are exemplified to facilitate understanding of specific embodiments of the present invention and the present invention is not limited to these embodiments. The present invention should be widely construed, without violating the spirit and range of the invention disclosed in the claims. The explanation above is given focusing on the structure of a strand having a round cross section having a diameter of d and a diameter of the group of superconducting filaments of d.sub.fb. However, with respect to the effects of the present invention, similar effects can be obtained even when the cross section is rectangular, etc. When the cross section has a rectangular shape with a thickness of d.sup.t and a width of d.sup.w, as the thickness dimension of the group of superconducting filaments d.sub.fb.sup.t and the width dimension d.sub.fb.sup.w, values of d and d.sub.fb in the case of a round wire are replaced with d.sup.t and d.sub.fb.sup.t when the wire is bent in a flatwise direction and are replaced with d.sup.w and d.sub.fb.sup.w when the wire is bent in an edgewise direction.

[0130] The insulation-coated compound superconducting wire 1 in the present invention maintains its wire winding direction during the heat treatment step for forming the compound superconducting phase in the processing onward until a superconducting magnet is wound. A good wire winding property can be obtained by making a winding direction of a wire to a magnet identical to the winding direction in the heat treatment step. In the case of a general compound superconducting wire such as Nb.sub.3Sn superconducting wire, deterioration of the insulation-coated compound superconducting wire 1 can be suppressed by winding the wire around a winding member (e.g., superconducting coil) having a diameter (drum diameter) to which bending strain being 0.5% or more of the maximum dimension d.sub.fb of the compound superconductor part 11 is not applied, in the same direction as the direction in which the wire is wound around the heat treatment bobbin.

<Use of Insulation-Coated Compound Superconducting Wire>

[0131] The insulation-coated compound superconducting wire 1 of the present invention is preferably used for a magnet in MRI (magnetic resonance imaging apparatus), medical particle accelerators, magnets for scientific research (e.g., magnetization measuring apparatus), magnets for manufacturing instruments in a variety of industries such as semiconductors, and magnets for generating high magnetic field.

EXAMPLES

[0132] Below, the present invention is further described in detail based on the Examples, but the present invention is not limited only to these Examples.

Test Example 1

Example 1

[0133] An Nb filament, which was a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-14 mass % Sn-0.2 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Nb was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-20 volume % Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 0.80 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part, and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 41%, 4%, 35%, and 20%, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter D; of 500 mm so that the bending diameter was 100 times or larger than the maximum dimension dib (0.51 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was produced. Subsequently, using the pre-bending application apparatus shown in FIG. 5, the Nb.sub.3Sn superconducting strand was reverted to a linear state without bending in the reverse direction with respect to the bending direction during the heat treatment. Then, using a same direction (positive direction) bending pulley having a diameter D1 of 125 mm and an opposite direction (reverse direction) bending pulley having a diameter D2 of 250 mm, bending strain within ±0.31% in the positive direction and the reverse direction alternatively 5 times each, i.e., 10 times in total were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 20 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Comparative Example 1A

[0134] A compound superconducting wire having the same configuration as Example 1 was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Comparative Example 1B

[0135] A compound superconducting wire having the same configuration as Example 1 was prepared, except that the reinforcing part was not disposed, the stabilizing part had a volume ratio of 55%, and the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Example 2

[0136] An Nb filament, which was a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-14 mass % Sn-0.2 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Nb was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-20 volume % Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 0.80 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part, and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 41%, 4%, 35%, and 20%, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter Dt, of 150 mm so that the bending diameter was 100 times or larger than the maximum dimension d.sub.fb (0.51 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was produced. Subsequently, using the pre-bending application apparatus (one direction bending) shown in FIG. 4, the Nb.sub.3Sn superconducting strand was reverted to a linear state with respect to the bending direction during the heat treatment. Then, using only a same direction (positive direction) bending pulley having a diameter D1 of 250 mm, reverse direction bending strain of −0.34% of eleven times in total by reverting to the linear state were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 40 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Comparative Example 2

[0137] A compound superconducting wire having the same configuration as Example 2 was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Example 3

[0138] A Nb filament, which is a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-14 mass % Sn-0.2 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Ta was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-20 volume % Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 0.80 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 41%, 4%, 35%, and 20%, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter DE, of 500 mm so that the bending diameter was 100 times or larger than the maximum dimension dib (0.51 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was prepared. Subsequently, using the pre-bending application apparatus shown in FIG. 5, the Nb.sub.3Sn superconducting strand was reverted to a linear state without bending in the reverse direction with respect to the bending direction during the heat treatment. Then, using a same direction (positive direction) bending pulley having a diameter D1 of 125 mm and an opposite direction (reverse direction) bending pulley having a diameter D2 of 250 mm, bending strain within 10.31% in the positive direction and the reverse direction alternatively 5 times each, i.e., 10 times in total were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 40 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Comparative Example 3

[0139] A compound superconducting wire having the same configuration as Example 3 was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Example 4A

[0140] A Nb filament, which is a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-14 mass % Sn-0.2 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Ta was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-20 volume % Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 0.80 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part, and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 41%, 4%, 35%, and 20%, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter D.sub.h of 500 mm so that the bending diameter was 100 times or larger than the maximum dimension d.sub.fb (0.51 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was produced. Subsequently, the Nb.sub.3Sn superconducting strand was reverted to a linear state without bending in the reverse direction with respect to the bending direction during the heat treatment. Then, using a same direction (positive direction) bending pulley having a diameter D1 of 165 mm and an opposite direction (reverse direction) bending pulley having a diameter D2 of 400 mm, positive direction bending strain of +0.21% of twice and reverse direction bending strain of −0.23% of once were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 40 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Example 4B

[0141] A compound superconducting wire having the same configuration as Example 4A was prepared, except that a chromium (Cr) plating of 0.5 μm was applied on the surface of the Nb.sub.3Sn superconducting precursor strand having a diameter of 0.80 mm.

Comparative Example 4

[0142] A compound superconducting wire having the same configuration as Example 4A was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Example 5A

[0143] A Nb filament, which is a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-15.7 mass % Sn-0.3 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Ta was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-20 volume % Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 1.30 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 36%, 4%, 40%, and 20?, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter D), of 700 mm so that the bending diameter was 100 times or larger than the maximum dimension d.sub.fb (0.78 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was produced. Subsequently, the Nb.sub.3Sn superconducting strand was reverted to a linear state without bending in the reverse direction with respect to the bending direction during the heat treatment. Then, using only a same direction (positive direction) bending pulley having a diameter D1 of 270 mm, positive direction bending strain of +0.18% of 10 times and reverse direction bending strain of −0.11% of 11 times were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 40 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Example 5B

[0144] An insulation-coated compound superconducting wire having the same configuration as Example 5A was prepared, except that the electric insulation part (total thickness of 50 μm) was formed by winding polyimide tape with a thickness of 25 μm around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, by ⅓ lap.

Comparative Example 5

[0145] A compound superconducting wire having the same configuration as Example 5 was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand.

Example 6

[0146] A Nb filament, which is a precursor of a compound superconducting filament before heat treatment, was embedded in a first matrix precursor, which was before being subjected to heat treatment and which consisted of Cu-15.7 mass % Sn-0.3 mass % Ti. A plurality of the above was bundled and twisted to form a compound superconducting precursor part. Additionally, an Sn diffusion prevention part consisting of Ta was disposed around the outer circumference of the compound superconducting precursor part, a reinforcing part consisting of Cu-25 volume, Nb was disposed around the outer circumference thereof, and a stabilizing part consisting of oxygen free copper was further disposed around the outer circumference thereof to prepare an Nb.sub.3Sn superconducting precursor strand having a diameter of 1.02 mm. The diameter of the Nb filament, which is a superconducting precursor, was set to about 3 μm. The compound superconducting precursor part, the Sn diffusion prevention part, the reinforcing part, and the stabilizing part, which constitute the Nb.sub.3Sn superconducting precursor strand, had a volume ratio of 25%, 5%, 50%, and 20%, respectively. Subsequently, heat treatment for forming the compound superconducting phase was carried out at 670° C. for 96 hours, while the Nb.sub.3Sn superconducting precursor strand was wound around a heat treatment bobbin having a diameter D; of 500 mm so that the bending diameter was 100 times or larger than the maximum dimension d.sub.fb (0.51 mm) of the compound superconductor part. The compound superconducting precursor part was converted to a compound superconductor part, and thereby an Nb.sub.3Sn superconducting strand was produced. Subsequently, the Nb.sub.3Sn superconducting strand was reverted to a linear state without bending in the reverse direction with respect to the bending direction during the heat treatment. Then, using a same direction (positive direction) bending pulley having a diameter D1 of 125 mm and an opposite direction (reverse direction) bending pulley having a diameter D2 of 250 mm, bending strain within ±0.31% in the positive direction and the reverse direction alternatively 5 times each, i.e., 10 times in total were applied to the compound superconductor part. Subsequently, an electric insulation part consisting of polyvinyl formal (PVF) of 40 μm was formed around the outer circumference of the Nb.sub.3Sn superconducting strand, which is a compound superconducting wire, to produce an insulation-coated compound superconducting wire. During a time period after the Nb.sub.3Sn formation heat treatment until finishing the electric insulation coating, the tensile strain applied to the Nb.sub.3Sn superconducting strand was 0.2% or less, bending strain applied to the compound superconductor part was within a range of ±0.5%, and the temperature was in a range from room temperature to 500° C.

Comparative Example 6

[0147] A compound superconducting wire having the same configuration as Example 6 was prepared, except that the electric insulation part was not formed around the outer circumference of the Nb.sub.3Sn superconducting strand. Specifications of the configurations of the insulation-coated compound superconducting wires of Examples 1 to 6 and the compound superconducting wires of Comparative Examples 1 to 6 are indicated in Table 1.

(Evaluation Method)

[0148] Below, methods of tests and evaluations are described in detail.

(1) Measurement Method of Superconductive Characteristics (Cryogenic Characteristics)

(1-1) Measurement Condition A

[0149] Tensile stress of 150, 200, or 250 MPa was applied to the superconducting wire at room temperature with a strain rate of 10.sup.−4 to 10.sup.−3/s, followed by unloading, and then the superconducting wire was cooled to 4.2 K. A critical current value Ic (A) was measured under application of an external magnetic field of 14.5 T. The measurement results of the critical current are shown in Table 2.

(1-2) Measurement Condition B

[0150] The superconducting wire was cooled to 4.2 K. A critical current value Ic (A) was measured, by conducting electric current to the superconducting wire while applying tensile stress of 150, 200, or 250 MPa, under application of an external magnetic field of 14.5 T. The measurement results of the critical current are indicated in Table 2.

(2) Measurement of Strength (0.2% Proof Stress) During Tension

[0151] Strength was measured at room temperature (25° C.) and cryogenic temperature (4.2 K) according to JIS H 7303: 2013, and 0.2% proof stress was calculated by using an unloading curve. The measurement results are indicated in Table 2.

(3) Wire Winding Property

(3-1) Winding-Off Property

[0152] The winding-off property was evaluated with or without generation of local wire bending due to drop or the like of the strand, in the work of winding off the superconducting wire which was traversely wound to a bobbin having a drum portion diameter φ of 400.

(3-2) Winding-Up Property

[0153] The winding-up property was evaluated with or without occurrence of winding turbulence due to twisting, bending or the like of the wire, in the work of aligned winding the superconducting wire to a bobbin having a drum portion diameter φ of 400.

TABLE-US-00001 TABLE 1-1 Comparative Item Symbol Unit Example 1 Example 1A Insulation- Compound Strand diameter d mm 0.80 0.80 coated superconducting Compound Type — — Nb.sub.3Sn filament Nb.sub.3Sn filament compound wire superconducting and Cu—Sn and Cu—Sn superconducting wire matrix matrix wire Diameter of compound dfb mm 0.51 0.51 superconductor part Volume ratio of V1 % 41 41 compound superconductor part (Relative to compound superconducting wire) Reinforcing Type — — Cu—Nb Cu—Nb part Volume ratio V2 of V2 % 35 35 reinforcing part (Relative to compound superconducting wire) Volume ratio of V21 % 20 20 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of V22 % 80 80 second stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type — — Nb Nb prevention Volume ratio of V3 % 4 4 part Sn diffusion prevention part (Relative to compound superconducting wire) Total volume V5 (=V2 .Math. V21/ % 11 11 ratio of reinforcing 100 + V3) filament and Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type — — Oxygen free Oxygen free part copper copper Volume ratio V4 % 20 20 of stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume V6 (=V2 .Math. V22/ % 48 48 ratio of 100 + V4) second and third stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type — — None None plated part Thickness — μm — — Electric insulation part Type — — PVF None Comparative Comparative Item Example 1B Example 2 Example 2 Insulation- Compound Strand diameter 0.80 0.80 0.80 coated superconducting Compound Type Nb.sub.3Sn filament Nb.sub.3Sn filament Nb.sub.3Sn filament compound wire superconducting and Cu—Sn and Cu—Sn and Cu—Sn superconducting wire matrix matrix matrix wire Diameter of compound 0.51 0.51 0.51 superconductor part Volume ratio of 41 41 41 compound superconductor part (Relative to compound superconducting wire) Reinforcing Type None Cu—Nb Cu—Nb part Volume ratio V2 of — 35 35 reinforcing part (Relative to compound superconducting wire) Volume ratio of — 20 20 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of — 80 80 second stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type Nb Nb Nb prevention Volume ratio of 4 4 4 part Sn diffusion prevention part (Relative to compound superconducting wire) Total volume 4 11 11 ratio of reinforcing filament and Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type Oxygen free Oxygen free Oxygen free part copper copper copper Volume ratio 55 20 20 of stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume 55 48 48 ratio of second and third stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type None None None plated part Thickness — — — Electric insulation part Type None PVF None

TABLE-US-00002 TABLE 1-2 Comparative Comparative Comparative Item Symbol Unit Example 1 Example 1A Example 1B Example 2 Example 2 Heat treatment Diameter of winding member Dh mm 500 500 500 150 150 step S2 (heat treatment bobbin) Ratio of heat treatment bobbin Dh/dfb — 980 980 980 294 294 diameter/compound superconductor part diameter Pre-bending Number of pre-bending strain — times 5 5 5 11 11 strain application application (positive direction) step S3 Number of pre-bending strain — times 5 5 5 0 0 application (reverse direction) Number of pre-bending strain — times 10 10 10 11 11 application (total) Diameter of positive direction D1 mm 125 125 125 250 250 bending pulley Diameter of reverse direction D2 mm 250 250 250 None None bending pulley Positive direction bending strain ε1 % 0.31 0.31 0.31 — — Reverse direction bending strain ε2 % −0.31 −0.31 −0.31 −0.34 −0.34 Maximum tension strain to compound — % 0.1 0.1 0.1 0.1 0.1 superconducting wire Insulation coating Type of electric insulation part — — PVF None None PVF None step S4 Thickness of insulation coating — μm 20 — — 40 — Maximum temperature during T1 ° C. 500° C. or less — — 500° C. or less — insulation treatment Maximum tension strain to — % 0.1 0.1 0.1 0.1 0.1 compound superconducting wire Pure bending Diameter of winding wire for D3 mm 400 400 400 400 400 strain application superconducting coil step S5 Pure bending strain ε3 % 0.03 0.03 0.03 −0.21 −0.21

TABLE-US-00003 TABLE 1-3 Comparative Item Symbol Unit Example 3 Example 3 Insulation- Compound Strand diameter d mm 0.80 0.80 coated compound superconducting Compound Type — — Nb.sub.3Sn filament Nb.sub.3Sn filament superconducting wire superconducting and Cu—Sn and Cu—Sn wire wire matrix matrix Diameter of compound dfb mm 0.51 0.51 superconductor part Volume ratio of compound V1 % 41 41 superconductor part (Relative to compound superconducting wire) Reinforcing Type — — Cu—Nb Cu—Nb part Volume ratio V2 of V2 % 35 35 reinforcing part (Relative to compound superconducting wire) Volume ratio of V21 % 20 20 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of second V22 % 80 80 stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type — — Ta Ta prevention part Volume ratio of Sn V3 % 4 4 diffusion prevention part (Relative to compound superconducting wire) Total volume ratio of V5 (=V2 .Math. V21/ % 11 11 reinforcing filament and 100 + V3) Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type — — Oxygen free Oxygen free part copper copper Volume ratio of V4 % 20 20 stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume ratio V6(=V2 .Math. V22/ % 48 48 of second and third 100 + V4) stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type — — None None plated part Thickness — μm — — Electric insulation part Type — — PVF None Comparative Item Example 4A Example 4B Example 4 Insulation- Compound Strand diameter 0.80 0.80 0.80 coated compound superconducting Compound Type Nb.sub.3Sn filament Nb.sub.3Sn filament Nb.sub.3Sn filament superconducting wire superconducting and Cu—Sn and Cu—Sn and Cu—Sn wire wire matrix matrix matrix Diameter of compound 0.51 0.51 0.51 superconductor part Volume ratio of compound 41 41 41 superconductor part (Relative to compound superconducting wire) Reinforcing Type Cu—Nb Cu—Nb Cu—Nb part Volume ratio V2 of 35 35 35 reinforcing part (Relative to compound superconducting wire) Volume ratio of 20 20 20 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of second 80 80 80 stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type Ta Ta Ta prevention part Volume ratio of Sn 4 4 4 diffusion prevention part (Relative to compound superconducting wire) Total volume ratio of 11 11 11 reinforcing filament and Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type Oxygen free Oxygen free Oxygen free part copper copper copper Volume ratio of 20 20 20 stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume ratio 48 48 48 of second and third stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type None Cr None plated part Thickness — 0.5 — Electric insulation part Type PVF PVF None

TABLE-US-00004 TABLE 1-4 Comparative Comparative Item Symbol Unit Example 3 Example 3 Example 4A Example 4B Example 4 Heat treatment Diameter of winding Dh mm 500 500 500 500 500 step S2 member (heat treatment bobbin) Ratio of heat treatment Dh/dfb — 980 980 980 980 980 bobbin diameter/compound superconductor part diameter Pre-bending Number of pre-bending — times 5 5 2 2 2 strain application strain application (positive step S3 direction) Number of pre-bending — times 5 5 1 1 1 strain application (reverse direction) Number of pre-bending strain — times 10 10 3 3 3 application (total) Diameter of positive direction D1 mm 125 125 165 165 165 bending pulley Diameter of reverse direction D2 mm 250 250 400 400 400 bending pulley Positive direction bending ε1 % 0.31 0.31 0.21 0.21 0.21 strain Reverse direction bending ε2 % −0.31 −0.31 −0.23 −0.23 −0.23 strain Maximum tension strain to — % 0.1 0.1 0.1 0.1 0.1 compound superconducting wire Insulation Type of electric insulation — — PVF None PVF PVF None coating part step S4 Thickness of insulation — μm 40 — 40 40 — coating Maximum temperature during T1 ° C. 500° C. or less — 500° C. or less 500° C. or less — insulation treatment Maximum tension strain to — % 0.1 0.1 0.1 0.1 0.1 compound superconducting wire Pure bending Diameter of winding wire D3 mm 400 400 400 400 400 strain application for superconducting coil step S5 Pure bending strain ε3 % 0.03 0.03 0.03 0.03 0.03

TABLE-US-00005 TABLE 1-5 Item Symbol Unit Example 5A Example 5B Insulation- Compound Strand diameter d mm 1.30 1.30 coated compound superconducting Compound Type — — Nb.sub.3Sn filament Nb.sub.3Sn filament superconducting wire superconducting and Cu—Sn and Cu—Sn wire wire matrix matrix Diameter of compound dfb mm 0.78 0.78 superconductor part Volume ratio of V1 % 36 36 compound superconductor part (Relative to compound superconducting wire) Reinforcing Type — — Cu—Nb Cu—Nb part Volume ratio V2 of V2 % 40 40 reinforcing part (Relative to compound superconducting wire) Volume ratio of V21 % 20 20 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of second V22 % 80 80 stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type — — Ta Ta prevention part Volume ratio of Sn V3 % 4 4 diffusion prevention part (Relative to compound superconducting wire) Total volume ratio of V5 (=V2 .Math. V21/ % 12 12 reinforcing filament and 100 + V3) Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type — — Oxygen free Oxygen free part copper copper Volume ratio of V4 % 20 20 stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume ratio V6(=V2 .Math. V22/ % 52 52 of second and third 100 + V4) stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type — — None None plated part Thickness — μm — — Electric insulation part Type — — PVF Polyimide tape Comparative Comparative Item Example 5 Example 6 Example 6 Insulation- Compound Strand diameter 1.30 1.02 1.02 coated compound superconducting Compound Type Nb.sub.3Sn filament Nb.sub.3Sn filament Nb.sub.3Sn filament superconducting wire superconducting and Cu—Sn and Cu—Sn and Cu—Sn wire wire matrix matrix matrix Diameter of compound 0.78 0.51 0.51 superconductor part Volume ratio of 36 25 25 compound superconductor part (Relative to compound superconducting wire) Reinforcing Type Cu—Nb Cu—Nb Cu—Nb part Volume ratio V2 of 40 50 50 reinforcing part (Relative to compound superconducting wire) Volume ratio of 20 25 25 reinforcing filament (Nb) (Relative to reinforcing part) Volume ratio of second 80 75 75 stabilizing material (Cu) (Relative to reinforcing part) Sn diffusion Type Ta Ta Nb prevention part Volume ratio of Sn 4 5 5 diffusion prevention part (Relative to compound superconducting wire) Total volume ratio of 12 17.5 17.5 reinforcing filament and Sn diffusion prevention part (Relative to compound superconducting wire) Stabilizing Type Oxygen free Oxygen free Oxygen free part copper copper copper Volume ratio of 20 20 20 stabilizing part (third stabilizing material) (Relative to compound superconducting wire) Total volume ratio 52 57.5 57.5 of second and third stabilizing materials (Relative to compound superconducting wire) Heat-resistant Type None None None plated part Thickness — — — Electric insulation part Type None PVF None

TABLE-US-00006 TABLE 1-6 Comparative Comparative Item Symbol Unit Example 5A Example 5B Example 5 Example 6 Example 6 Heat treatment Diameter of winding member Dh mm 700 700 700 500 500 step S2 (heat treatment bobbin) Ratio of heat treatment Dh/dfb — 897 897 897 980 980 bobbin diameter/compound superconductor part diameter Pre-bending Number of pre-bending — times 10 10 10 5 5 strain application strain application (positive step S3 direction) Number of pre-bending strain — times 11 11 11 5 5 application (reverse direction) Number of pre-bending strain — times 21 21 21 10 10 application (total) Diameter of positive direction D1 mm 270 270 270 125 125 bending pulley Diameter of reverse direction D2 mm None None None 250 250 bending pulley Positive direction bending ε1 % 0.18 0.18 0.18 0.31 0.31 strain Reverse direction bending ε2 % −0.11 −0.11 −0.11 −0.31 −0.31 strain Maximum tension strain to — % 0.1 0.1 0.1 0.1 0.1 compound superconducting wire Insulation coating Type of electric insulation — — PVF Polyimide tape None PVF None step S4 part Thickness of insulation — μm 40 50 — 40 — coating Maximum temperature during T1 ° C. 500° C. or less 35 — 500° C. or less — insulation treatment Maximum tension strain — % 0.1 0.1 0.1 0.1 0.1 to compound superconducting wire Pure bending Diameter of winding wire D3 mm 400 400 400 400 400 strain application for superconducting coil step S5 Pure bending strain ε3 % 0.08 0.08 0.08 0.03 0.03

TABLE-US-00007 TABLE 2-1 Comparative Item Symbol Unit Example 1 Example 1A Evaluation of Superconducting General Critical current value when Ic.sub.0 A 115 112 characteristics characteristics measurement measured after cooling to Increasing rate % 103 (Compared to — (cryogenic condition 4.2 K from room temperature, of Ic.sub.0 Comparative characteristics) without applying tensile Example 1A) stress (Measured under application of external magnetic field of 14.5 T) Critical current value measured Ic.sub.A-250 A 118 113 by applying tensile stress of Increasing rate % 105 (Compared to — 250 MPa at room temperature, of I.sub.CA-250 Comparative followed by unloading, cooling Example 1A to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured Ic.sub.A-200 A 116 113 Measurement by applying tensile stress of Increasing rate % 103 (Compared to — condition A 250 MPa at room temperature, of Ic.sub.A-200 Comparative followed by unloading, cooling Example 1A) to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured Ic.sub.A-150 A 113 112 by applying tensile stress of Increasing rate % 101 (Compared to — 150 MPa at room temperature, of Ic.sub.A-150 Comparative followed by unloading, cooling Example 1A) to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured Ic.sub.B-250 A 117 110 by cooling to 4.2 K while Increasing rate % 106 (Compared to — applying tensile stress of 250 of Ic.sub.B-250 Comparative MPa (Measured under application Example 1A of external magnetic field of 14.5 T) Critical current value measured Ic.sub.B-200 A 120 115 Measurement by cooling to 4.2 K while Increasing rate % 104 (Compared to — condition B applying tensile stress of 200 of Ic.sub.B-200 Comparative MPa (Measured under application Example 1A) of external magnetic field of 14.5 T) Critical current value measured Ic.sub.B-150 A 115 110 by cooling to 4.2 K while Increasing rate % 105 (Compared to — applying tensile stress of 150 of Ic.sub.B-150 Comparative MPa (Measured under application Example 1A of external magnetic field of 14.5 T) Tensile 0.2% proof stress (25° C.) YS.sub.25 MPa 250 240 characteristics 0.2% proof stress (4.2 K) YS.sub.4.2 MPa 300 280 Wire winding Malfunction during — — Absent Absent property winding-off (presence or absence of generation of local wire bending) Malfunction during — — Absent Absent winding-up (presence or absence of generation of local wire bending) Comparative Comparative Item Example 1B Example 2 Example 2 Evaluation of Superconducting General Critical current value when 100 101  96 characteristics characteristics measurement measured after cooling to — 105 (Compared to — (cryogenic condition 4.2 K from room temperature, Comparative characteristics) without applying tensile Example 2) stress (Measured under application of external magnetic field of 14.5 T) Critical current value measured  80 107 102 by applying tensile stress of — 105 (Compared to — 250 MPa at room temperature, Comparative followed by unloading, cooling Example 2) to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured  95 106 100 Measurement by applying tensile stress of — 106 (Compared to — condition A 250 MPa at room temperature, Comparative followed by unloading, cooling Example 2) to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured 105 105  98 by applying tensile stress of — 107 (Compared to 150 MPa at room temperature, Comparative followed by unloading, cooling Example 2) to 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured — 108 100 by cooling to 4.2 K while — 108 (Compared to — applying tensile stress of 250 Comparative MPa (Measured under application Example 2) of external magnetic field of 14.5 T) Critical current value measured — 112 107 Measurement by cooling to 4.2 K while — 105 (Compared to — condition B applying tensile stress of 200 Comparative MPa (Measured under application Example 2) of external magnetic field of 14.5 T) Critical current value measured — 110 105 by cooling to 4.2 K while — 105 (Compared to — applying tensile stress of 150 Comparative MPa (Measured under application Example 2) of external magnetic field of 14.5 T) Tensile 0.2% proof stress (25° C.) 130 240 230 characteristics 0.2% proof stress (4.2 K) 160 290 280 Wire winding Malfunction during Present Absent Absent property winding-off (presence or absence of generation of local wire bending) Malfunction during Present Absent Absent winding-up (presence or absence of generation of local wire bending)

TABLE-US-00008 TABLE 2-2 Comparative Item Symbol Unit Example 3 Example 3 Evaluation of Super General Critical current value when measured Ic.sub.0 A 109  99 characteristics conducting measurement after cooling to 4.2 K Increasing rate % 110 (Compared to — characteristics condition from room temperature, of Ic.sub.0 Comparative (cryogenic without applying tensile Example 3) characteristies) stress (Measured under application of external magnetic field of 14.5 T) Critical current value measured I.sub.CA-250 A 119 114 by applying tensile stress of Increasing rate % 104 (Compared to — 250 MPa at room temperature, of g Ic.sub.A-250 Comparative followed by unloading, cooling to Example 3) 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured Ic.sub.A-200 A 117 112 Measurement by applying tensile stress of Increasing rate % 104 (Compared to — condition A 250 MPa at room temperature, of Ic.sub.A-200 Comparative followed by unloading, cooling to Example 3) 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by Ic.sub.A-150 A 114 110 applying tensile stress of 150 MPa Increasing rate % 104 (Compared to — at room temperature, followed by of g Ic.sub.A-150 Comparative unloading, cooling to 4.2 K in a Example 3) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by Ic.sub.B-250 A 120 115 cooling to 4.2 K while applying Increasing rate % 104 (Compared to — tensile stress of 250 MPa (Measured of Ic.sub.B-250 Comparative under application of external magnetic Example 3) field of 14.5 T) Critical current value measured by Ic.sub.B-200 A 122 117 Measurement cooling to 4.2 K while applying tensile Increasing rate % 104 (Compared to — condition B stress of 200 MPa (Measured under of Ic.sub.B-200 Comparative application of external magnetic field Example 3) of 14.5 T) Critical current value measured by Ic.sub.B-150 A 120 115 cooling to 4.2 K while applying Increasing rate % 104 (Compared to — tensile stress of 150 MPa (Measured of Ic.sub.B-150 Comparative under application of external magnetic Example 3) field of 14.5 T) Tensile 0.2% proof stress (25° C.) YS.sub.25 MPa 250 240 characteristics 0.2% proof stress (4.2K) YS.sub.4.2 MPa 300 300 Wire winding Malfunction during winding-off — — Absent Absent property (presence or absence of generation of local wire bending) Malfunction during winding-up — — Absent Absent (presence or absence of generation of local wire bending) Comparative Item Example 4A Example 4B Example 4 Evaluation of Super General Critical current value when measured  93  94  83 characteristics conducting measurement after cooling to 4.2 K 112 (Compared to 113 (Compared to — characteristics condition from room temperature, Comparative Comparative (cryogenic without applying tensile Example 4) Example 4) characteristies) stress (Measured under application of external magnetic field of 14.5 T) Critical current value measured 118 119 113 by applying tensile stress of 104 (Compared to 105 (Compared to — 250 MPa at room temperature, Comparative Comparative followed by unloading, cooling to Example 4) Example 4) 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured 106 107 104 Measurement by applying tensile stress of 102 (Compared to 103 (Compared to — condition A 250 MPa at room temperature, Comparative Comparative followed by unloading, cooling to Example 4) Example 4) 4.2 K in a state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by 100 101  98 applying tensile stress of 150 MPa 102 (Compared to 103 (Compared to — at room temperature, followed by Comparative Comparative unloading, cooling to 4.2 K in a Example 4) Example 4) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by 113 114 110 cooling to 4.2 K while applying 103 (Compared to 104 (Compared to — tensile stress of 250 MPa (Measured Comparative Comparative under application of external magnetic Example 4) Example 4) field of 14.5 T) Critical current value measured by 107 108 104 Measurement cooling to 4.2 K while applying tensile 103 (Compared to 105 (Compared to — condition B stress of 200 MPa (Measured under Comparative Comparative application of external magnetic field Example 4) Example 4) of 14.5 T) Critical current value measured by 101 103  98 cooling to 4.2 K while applying 103 (Compared to 105 (Compared to — tensile stress of 150 MPa (Measured Comparative Comparative under application of external magnetic Example 4) Example 4) field of 14.5 T) Tensile 0.2% proof stress (25° C.) 230 240 200 characteristics 0.2% proof stress (4.2K) 270 280 240 Wire winding Malfunction during winding-off Absent Absent Absent property (presence or absence of generation of local wire bending) Malfunction during winding-up Absent Absent Absent (presence or absence of generation of local wire bending)

TABLE-US-00009 TABLE 2-3 Item Symbol Unit Example 5A Example 5B Evaluation of Super General Critical current value when measured Ic.sub.0 A 259 254 characteristics conducting measurement after cooling to 4.2 K from room Increasing rate % 118 (Compared to 116 (Compared to characteristics condition temperature, without applying tensile of Ic.sub.0 Comparative Comparative (cryogenic stress (Measured under application of Example 5) Example 5) characteristics) external magnetic field of 14.5 T) Critical current value measured by I.sub.CA-250 A 283 285 applying tensile stress of 250 MPa Increasing rate % 107 (Compared to 108 (Compared to at room temperature, followed by of g Ic.sub.A-250 Comparative Comparative unloading, cooling to 4.2 K in a Example 5) Example 5) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by Ic.sub.A-200 A 268 268 Measurement applying tensile stress of 250 MPa Increasing rate % 109 (Compared to 109 (Compared to condition A at room temperature, followed by of g Ic.sub.A-200 Comparative Comparative unloading, cooling to 4.2 K in a Example 5) Example 5) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by Ic.sub.A-150 A 262 263 applying tensile stress of 150 MPa Increasing rate % 111 (Compared to 112 (Compared to at room temperature, followed by of g Ic.sub.A-150 Comparative Comparative unloading, cooling to 4.2 K in a Example 5) Example 5) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by Ic.sub.B-250 A 245 247 cooling to 4.2 K while applying Increasing rate % 102 (Compared to 102 (Compared to tensile stress of 250 MPa (Measured of Ic.sub.B-25 Comparative Comparative under application of external Example 5) Example 5) magnetic field of 14.5 T) Critical current value measured by Ic.sub.B-200 A 257 267 Measurement cooling to 4.2 K while applying Increasing rate % 102 (Compared to 106 (Compared to condition B tensile stress of 200 MPa (Measured of Ic.sub.B-200 Comparative Comparative under application of external Example 5) Example 5) magnetic field of 14.5 T) Critical current value measured by Ic.sub.B-150 A 262 268 cooling to 4.2 K while applying Increasing rate % 111 (Compared to 113 (Compared to tensile stress of 150 MPa (Measured of Ic.sub.B-150 Comparative Comparative under application of external Example 5) Example 5) magnetic field of 14.5 T) Tensile 0.2% proof stress (25° C.) YS.sub.25 MPa 250 240 characteristics 0.2% proof stress (4.2K) YS.sub.4.2 MPa 290 270 Wire winding Malfunction during winding-off — — Absent Absent property (presence or absence of generation of local wire bending) Malfunction during winding-up — — Absent Absent (presence or absence of generation of local wire bending) Comparative Comparative Item Example 5 Example 6 Example 6 Evaluation of Super General Critical current value when measured 219 120 110 characteristics conducting measurement after cooling to 4.2 K from room — 109 (Compared to — characteristics condition temperature, without applying tensile Comparative (cryogenic stress (Measured under application of Example 6) characteristics) external magnetic field of 14.5 T) Critical current value measured by 264 123 115 applying tensile stress of 250 MPa — 107 (Compared to — at room temperature, followed by Comparative unloading, cooling to 4.2 K in a Example 6) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by 247 122 113 Measurement applying tensile stress of 250 MPa — 108 (Compared to — condition A at room temperature, followed by Comparative unloading, cooling to 4.2 K in a Example 6) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by 235 121 112 applying tensile stress of 150 MPa — 108 (Compared to — at room temperature, followed by Comparative unloading, cooling to 4.2 K in a Example 6) state of tensile stress unloaded (Measured under application of external magnetic field of 14.5 T) Critical current value measured by 241 115 110 cooling to 4.2 K while applying — 105 (Compared to — tensile stress of 250 MPa (Measured Comparative under application of external Example 6) magnetic field of 14.5 T) Critical current value measured by 252 113 106 Measurement cooling to 4.2 K while applying — 107 (Compared to — condition B tensile stress of 200 MPa (Measured Comparative under application of external Example 6) magnetic field of 14.5 T) Critical current value measured by 237 111 103 cooling to 4.2 K while applying — 108 (Compared to — tensile stress of 150 MPa (Measured Comparative under application of external Example 6) magnetic field of 14.5 T) Tensile 0.2% proof stress (25° C.) 220 280 260 characteristics 0.2% proof stress (4.2K) 260 340 310 Wire winding Malfunction during winding-off Absent Absent Absent property (presence or absence of generation of local wire bending) Malfunction during winding-up Absent Absent Absent (presence or absence of generation of local wire bending)

[0154] From the evaluation results indicated in Table 2, it can be seen that each of the insulation-coated compound superconducting wires of Examples 1 to 6 had an increased critical current over each of the compound superconducting wires without the insulating coating of Comparative Examples 1 to 6, under any of general measurement condition and the measurement conditions A and B, and had excellent superconducting properties. Further, the insulation-coated compound superconducting wires of Examples 1 to 6 had 0.2% proof stress equal to or larger than that of the compound superconducting wires without the insulating coating of Comparative Examples 1 to 6, and had both a good winding-off property and a good winding-up property. In Example 4B, since Cr plating was applied to the surface of the strand, adhesion between the strands during the Nb.sub.3Sn formation heat treatment was prevented. Consequently, it was confirmed that the quality of the PVF-coated surface was improved over the surface quality of Example 4A. Example 5A exhibited critical current characteristics equivalent to those of Example 5B.

EXPLANATION OF REFERENCE NUMERALS

[0155] 1 Insulation-coated compound superconducting wire [0156] 10 Compound superconducting wire [0157] 11 Compound superconductor part [0158] 12 Reinforcing part [0159] 13 Stabilizing part [0160] 14 Sn diffusion prevention layer [0161] 15 Compound superconducting filament [0162] 16 First matrix [0163] 17 Core portion of unreacted Nb [0164] 18 Reinforcing filament [0165] 19 Second matrix [0166] 20, 20a, 20b Second stabilizing material [0167] 21, 41 Heat treatment bobbin [0168] 22, 43 Positive direction bending pulley [0169] 23, 42 Reverse direction bending pulley [0170] 24, 44 Winding-up member (or winding-up bobbin) [0171] 29 Heat-resistant plated part [0172] 30 Electric insulation part