MAGNETIC CORE, METHOD OF MANUFACTURING SAME, AND COIL COMPONENT

Description

FIELD OF THE INVENTION

The present invention relates to a magnetic core, a method of manufacturing the magnetic core, and a coil device.

RELATED ART

In accordance with the recent miniaturization of power devices, further miniaturization of transformers and coils, which occupy a lot of space in the power devices, is desired. Patent Document 1 discloses that a metal soft magnetic material is used as a material of a magnetic core for transformers and coils. Moreover, forming a magnetic core by lamination is studied.

When the magnetic core is formed by lamination with a soft magnetic metal material as the magnetic material, however, there is a problem with difficulty in punching due to hardness of the metal soft magnetic material itself and with deterioration in soft magnetic characteristics (particularly, increase in coercivity) due to the stress applied at the time of punching.

PRIOR ART

Patent Document

Patent Document 1: JPH1174108 (A)

SUMMARY OF THE INVENTION

Problem to be Solved by the Invention

The present invention has been achieved under the circumstances. It is an object of the invention to provide a magnetic core etc. having stable soft magnetic characteristics.

Means for Solving the Problem

To achieve the above object, a magnetic core according to the first aspect of the present invention includes laminated soft magnetic layers having cracks, wherein

the soft magnetic layers include Fe as a main component,

the soft magnetic layers have a composition formula of (Fe_{(1−(α+β))}X1_αX2_β)_{(1−(a+b+c+d+e+f))}M_aB_bP_cSi_dC_eS_f, in which X1 is one or more selected from a group consisting of Co and Ni, X2 is one or more selected from a group consisting of Al, Mn, Ag, Zn, Sn, As, Sb, Cu, Cr, Bi, N, O, and rare earth elements, and M is one or more selected from a group consisting of Nb, Hf, Zr, Ta, Mo, V, and W,

0≤a≤0.140, 0.020<b≤0.200, 0≤c≤0.150, 0≤d≤0.180, 0≤e<0.040, 0≤f≤0.030, α≥0, β≥0, and 0≤α+β≤0.50 are satisfied,

one or more of a, c, and d are larger than zero, and

a nanohetero structure including an amorphous phase and fine crystals existing in the amorphous phase is observed in the soft magnetic layers.

The fine crystals may have an average grain size of 0.3-5 nm.

A magnetic core according to the second aspect of the present invention includes laminated soft magnetic layers having cracks, wherein

the soft magnetic layers include Fe as a main component,

the soft magnetic layers have a composition formula of (Fe_{(1−(α+β))}X1_αX2_β)_{(1−(a+b+c+d+e+f))}M_aB_bP_cSi_dC_eS_f, in which X1 is one or more selected from a group consisting of Co and Ni, X2 is one or more selected from a group consisting of Al, Mn, Ag, Zn, Sn, As, Sb, Cu, Cr, Bi, N, O, and rare earth elements, and M is one or more selected from a group consisting of Nb, Hf, Zr, Ta, Mo, V, and W,

0≤a≤0.140, 0.020<b≤0.200, 0≤c≤0.150, 0≤d≤0.180, 0≤e<0.040, 0≤f≤0.030, α≥0, β≥0, and 0≤α+β≤0.50 are satisfied,

one or more of a, c, and d are larger than zero, and

a structure including Fe based nanocrystals is observed in the soft magnetic layers.

The Fe based nanocrystals may have an average grain size of 5-30 nm.

It is possible to provide a magnetic core etc. having stable soft magnetic characteristics using the magnetic core according to the present invention.

In the magnetic core according to the present invention, the soft magnetic layers may be fragmented so as to have an average crack interval of 0.015 mm or more and 1.0 mm or less.

In the magnetic core according to the present invention, a space factor of a magnetic material of the magnetic core may be 70.0% or more and 99.5% or less.

In the magnetic core according to the present invention, 0.020≤a≤0.100 may be satisfied.

In the magnetic core according to the present invention, 0.730≤1−(a+b+c+d+e+f)≤0.950 may be satisfied.

In the magnetic core according to the present invention, α=0 may be satisfied.

In the magnetic core according to the present invention, β=0 may be satisfied.

A coil device according to the present invention includes any of the magnetic cores and a coil.

A method of manufacturing a magnetic core according to the present invention includes the steps of: fragmenting each of a plurality of soft magnetic ribbons, and laminating the fragmented soft magnetic ribbons in a thickness direction.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic plane view of a magnetic core according to an embodiment of the present invention.

FIG. 2 is a schematic cross-sectional view of a magnetic core according to an embodiment of the present invention.

FIG. 3 is a schematic cross-sectional view of a soft magnetic layer contained in a magnetic core according to an embodiment of the present invention.

FIG. 4 is a chart obtained by X-ray crystal structure analysis.

FIG. 5 is a pattern obtained by profile fitting of the chart of FIG. 4.

EMBODIMENTS FOR CARRYING OUT THE INVENTION

Hereinafter, the present invention is explained based on an embodiment shown in the figures.

A configuration of a magnetic core 10 according to the present embodiment is explained. FIG. 1 is a schematic plane view viewed from one wide where a center plane A of a cylindrical magnetic core 10 is extended. FIG. 2 is a schematic cross-sectional view of the magnetic core 10 of FIG. 1 cut along the line II-II. FIG. 3 is a schematic cross-sectional view of a soft magnetic layer 12 of FIG. 2 cut along the cutting line III-III. The observation range of FIG. 3 is 4 mm×4 mm.

As shown in FIG. 2, the magnetic core 10 according to the present embodiment is formed by alternately laminating a plurality of soft magnetic layers 12 and adhesive layers 14. FIG. 2 illustrates a case where the magnetic core 10 includes a plurality of soft magnetic layers 12, but the number of laminated layers may be changed as desired and may be one. When the soft magnetic layers 12 included in the magnetic core according to the present embodiment are plural (e.g., two layers or more and 10000 layers or less), it is most preferable that all of the soft magnetic layers 12 have a plurality of cracks mentioned below.

The magnetic core 10 of the present embodiment includes the soft magnetic layers 12 and the adhesive layers 14 as main members, but may include other components as long as the effects of the present invention are not impaired. On the contrary, the soft magnetic layers 12 may be laminated without using the adhesive layers 14.

Preferably, the volume ratio (space factor) of the magnetic material in the magnetic core 10 is 70% or more and 99.5% or less. When the space factor of the magnetic material is 70% or more, the saturation magnetic flux density can be sufficiently high, and the magnetic core 10 can be effectively used as a magnetic core. When the space factor of the magnetic material is 99.5% or less, the magnetic core 10 is less likely to be damaged and is easy to handle as a magnetic core. The space factor of the magnetic material may be 72% or more and 96% or less. In the present embodiment, the volume of the magnetic material substantially corresponds to that of the soft magnetic layers 12.

As shown in FIG. 3, a plurality of cracks C is formed in each of the soft magnetic layers 12 included in the magnetic core 10 according to the present embodiment. Each of the soft magnetic layers 12 is divided into a plurality of small pieces by the plurality of cracks C. For example, each of the cracks C may have a width of 10 nm or more and 1000 nm or less.

In the magnetic core 10 according to the present embodiment, a plurality of cracks C is formed in each of the soft magnetic layers 12, and each of the soft magnetic layers 12 is divided into a plurality of small pieces, so that the change in soft magnetic characteristics due to the stress in the manufacture (particularly, increase in coercivity) is restrained, and a favorable magnetic core 10 can be provided.

In the present embodiment, when virtual lines B are drawn in a region divided and fragmented by the cracks C, the number of intersections D between the virtual lines B and the cracks C is divided by a total length of the virtual lines B and is defined as an average crack interval.

Hereinafter, a method of calculating an average crack interval is explained with reference to a specific case shown in FIG. 3. FIG. 3 illustrates a square observation area. In FIG. 3, the cracks C are shown by solid lines, and the virtual lines B are shown by dotted lines.

The virtual lines B extend in one direction (the horizontal direction in the figure) of the observation area. 10 virtual lines B extend at equal intervals in parallel to the vertical direction of the figure. At this time, the number of intersections D between the virtual lines B and the cracks C is counted. The number of intersections D is a total number of cracks C intersecting the virtual lines B. An average crack interval is obtained by dividing the total length of the virtual lines B by the total number of cracks C intersecting the virtual line B (the number of intersections D) and is represented by Formula (1).

Average Crack Interval (mm)=(Total Length of Virtual Lines B)/(Number of Intersections D)  Formula (1)

In the example shown in FIG. 3, if the observation area is a square (one side: 4 mm), the total length of the virtual lines B is 40 mm, and the number of intersections D is 43, so that the average crack interval is 40/43 [mm] and about 0.93 mm.

The average crack interval varies depending on a selected observation area and is thereby preferably averaged by being calculated in a plurality of observation areas. Preferably, the average crack interval is averaged by being calculated in three or more different observation areas. Moreover, it is preferable to decide how to select the observation areas. For example, when the ring-shaped magnetic core 10 is used as the present embodiment, the observation areas can be selected to include the center plane A in calculating the average crack interval. Incidentally, the average crack interval is measured in any manner and can be measured, for example, using SEM.

In the present embodiment, the average crack interval is not limited, but it is preferable that cracks are formed in the soft magnetic layers 12 so that the average crack interval is 0.015 mm or more and 1.0 mm or less. When the average crack interval is smaller than 0.015 mm, the magnetic permeability of the soft magnetic layers 12 is likely to decrease, the inductance Ls of the magnetic core 10 is likely to be low, and the performance of the magnetic core 10 is likely to decrease. When the average crack interval is larger than 1.0 mm, it becomes difficult to punch soft magnetic ribbons with a weak force in a punching step of a method of manufacturing the magnetic core 10 mentioned below. As a result, the stress generated on a cut surface in the punching of soft magnetic ribbons reaches widely, and this reduces the effect of dividing soft magnetic layers into small pieces by a plurality of cracks. Preferably, the average crack interval is 0.015 mm or more and 0.75 mm or less. More preferably, the average crack interval is 0.075 mm or more and 0.75 mm or less.

Since the magnetic core 10 according to the present embodiment includes the adhesive layers 14, it is possible to reduce the falling of the small pieces. The adhesive layers 14 can be made of known materials, such as a base body coated with an acrylic type adhesive, an adhesive made of silicone resin, butadiene resin, etc., hot melt, or the like. A PET film is a typical material for the base material. In addition to the PET film, however, the base body may be a resin film, such as a polyimide film, a polyester film, a polyphenylene sulfide (PPS) film, a polypropylene (PP) film, and a fluororesin film like polytetrafluoroethylene (PTFE). Moreover, the adhesive layers 14 may be an acrylic resin etc. directly applied onto a main surface of the soft magnetic ribbon after a heat treatment mentioned below.

The magnetic core 10 may include protective films 13 on one end and the other end in the lamination direction (the z-axis direction in FIG. 1 and FIG. 2). The protective films 13 can be known films, such as PET film, polyimide film, and aramid film.

The soft magnetic layers 12 have a plurality of cracks and are divided into small pieces by the cracks.

The soft magnetic layers 12 include Fe as a main component,

the soft magnetic layers have a composition formula of (Fe_{(1−(α+β))}X1_αX2_β)_{(1−(a+b+c+d+e+f))}M_aB_bP_cSi_dC_eS_f, in which X1 is one or more selected from a group consisting of Co and Ni, X2 is one or more selected from a group consisting of Al, Mn, Ag, Zn, Sn, As, Sb, Cu, Cr, Bi, N, O, and rare earth elements, and M is one or more selected from a group consisting of Nb, Hf, Zr, Ta, Mo, V, and W,

0≤a≤0.140, 0.020<b≤0.200, 0≤c≤0.150, 0≤d≤0.180, 0≤e<0.040, 0≤f≤0.030, α≥0, β≥0, and 0≤α+β≤0.50 are satisfied, and

one or more of a, c, and d are larger than zero.

In addition, a nanohetero structure (the above-mentioned first aspect) or a structure including Fe based nanocrystals (the above-mentioned second aspect) is observed in the soft magnetic layers 12 according to the present embodiment.

The nanohetero structure refers to a structure including an amorphous phase and fine crystals existing in the amorphous phase. Including an amorphous phase and fine crystals means that the fine crystals are scattered in the amorphous phase. The fact that the fine crystals are scattered in the amorphous phase means that an amorphous ratio X measured by a normal X-ray diffraction (XRD) is 85% or more, and crystal phases can be confirmed by electron diffraction image and high resolution image with transmission electron microscope. The fine crystals refer to crystals each having a particle size of 30 nm or less. Incidentally, the fine crystals may have an average particle size of 0.3-5 nm.

The Fe based nanocrystals are crystals whose particle size is nano-order (specifically, average particle size: about 30 nm or less) and whose crystal structure of Fe is body-centered cubic (bcc). In the present embodiment, it is preferable to deposit Fe based nanocrystals having an average particle size of 5-30 nm. The structure including Fe based nanocrystals is a structure including Fe based nanocrystals and having an amorphous ratio X of less than 85%.

When the soft magnetic layers 12 according to the present embodiment has a composition falling within the above-mentioned specific range and a nanohetero structure or a structure including Fe based nanocrystals, the soft magnetic layers 12 easily have cracks by the following fragmentation treatment during the manufacture of the magnetic core 10. Then, when the soft magnetic layers 12 according to the present embodiment have cracks C, the soft magnetic ribbons 12 can be punched with a weak force. Moreover, it is possible to manufacture the magnetic core 10 whose magnetic characteristics are favorable and whose change in soft magnetic characteristics due to the stress during manufacture (particularly, increase in coercivity) is restrained.

Moreover, when the soft magnetic layers have a structure including Fe based nanocrystals, the saturation magnetic flux density is likely to be high, and the coercivity is likely to be low.

Hereinafter, the composition of the soft magnetic layers 12 according to the present embodiment is explained in more detail.

M is one or more selected from a group consisting of Nb, Hf, Zr, Ta, Ti, Mo, V, and W. Preferably, M is Nb.

The M content (a) satisfies 0≤a≤0.140. That is, M may not be contained. When M is not contained, however, the magnetostriction constant tends to be high, and the coercivity tends to be high. The M content (a) is preferably 0.020≤a≤0.100, more preferably 0.040≤a≤0.100, and still more preferably 0.050≤a≤0.080. When the M content (a) is large, the coercivity easily increases in the manufacture of the magnetic core 10.

The B content (b) satisfies 0.020<b≤0.200. The B content (b) is preferably 0.025≤b≤0.200, more preferably 0.025≤b≤0.120, and most preferably 0.060≤b≤0.120. When the B content (b) is small, a crystal phase composed of crystals having a particle size of larger than 30 nm is easily generated in the manufacture of soft magnetic alloy ribbons mentioned below, and it is difficult to obtain the nanohetero structure or the structure including Fe based nanocrystals. When the B content (b) is large, the coercivity easily increases in the manufacture of the magnetic core 10.

The P content (c) satisfies 0≤c≤0.150. That is, P may not be contained. When P is contained, the coercivity easily decreases. From the viewpoint of reducing the coercivity and improving the inductance Ls of the magnetic core 10, 0.050≤c≤0.150 is preferable, and 0.050≤c≤0.080 is more preferable. From the viewpoint of making it difficult to increase the coercivity in the manufacture of the magnetic core 10, 0≤c≤0.030 is preferable. When the P content (c) is large, the coercivity easily increases in the manufacture of the magnetic core 10.

The Si content (d) satisfies 0≤d≤0.180. That is, Si may not be contained. 0≤d≤0.175 may be satisfied. Preferably, 0≤d≤0.060 is satisfied. When 0.070≤d≤0.180 is satisfied, the soft magnetic layers 12 and the magnetic core 10 having favorable soft magnetic characteristics tend to be easily obtained by reducing the M content (a) and the P content (c).

The C content (e) satisfies 0≤e<0.040. That is, C may not be contained. From the viewpoint of reducing the coercivity, 0≤e≤0.030 is preferable, and 0.001≤e≤0.010 is more preferable. When the C content (e) is large, the coercivity easily increases in the manufacture of the magnetic core 10.

The S content (f) satisfies 0≤f≤0.030. That is, S may not be contained. From the viewpoint of reducing coercivity, 0≤f≤0.001 is preferable. When the S content (f) is large, a crystal phase composed of crystals having a particle size of larger than 30 nm is easily generated in the manufacture of soft magnetic alloy ribbons mentioned below, and it is difficult to obtain the nanohetero structure or the structure including Fe based nanocrystals.

One or more of “a”, “c”, and “d” are larger than zero. One or more of “a”, “c”, and “d” may be 0.001 or more or may be 0.010 or more. That is, the soft magnetic layers 12 according to the present embodiment contains one or more of M, P, and Si. This makes it easy to obtain the nanohetero structure or the structure including Fe based nanocrystals.

The Fe content {(1−(a+b+c+d+e+f))} is not limited, but 0.730≤1−(a+b+c+d+e+f)≤0.950 is preferably satisfied. More preferably, 0.730≤1−(a+b+c+d+e+f)≤0.900 is preferably satisfied. When 0.730<1−(a+b+c+d+e+f) is satisfied, saturation magnetic flux density is easily improved. When 1−(a+b+c+d+e+f)≤0.950 is satisfied, it is easy to obtain the nanohetero structure or the structure including Fe based nanocrystals.

In the soft magnetic alloy according to the present embodiment, a part of Fe may be substituted by X1 and/or X2.

X1 is one or more selected from a group consisting of Co and Ni. The X1 content (α) may be a=0. That is, X1 may not be contained. Preferably, the number of atoms of X1 is 40 at % or less if the number of atoms of the entire composition is 100 at %. That is, 0≤α{1−(a+b+c+d+e+f)}≤0.40 is preferably satisfied.

X2 is one or more selected from a group consisting of Al, Mn, Ag, Zn, Sn, As, Sb, Cu, Cr, Bi, N, O, and rare earth elements. The content X2 (β) may be β=0. That is, X2 may not be contained. Preferably, the number of atoms of X2 is 3.0 at % or less if the number of atoms of the entire composition is 100 at %. That is, 0≤β{1−(a+b+c+d+e+f)}≤0.030 is preferably satisfied.

The substitution amount of Fe by X1 and/or X2 is half or less of Fe based on the number of atoms. That is, 0≤α+β≤0.50 is satisfied. When α+β>0.50 is satisfied, it is difficult to obtain the nanohetero structure or the structure including Fe based nanocrystals.

Incidentally, the soft magnetic layers 12 according to the present embodiment may contain elements other than the above-mentioned elements as unavoidable impurities as long as the characteristics are not affected. For example, 1 wt % or less of unavoidable impurities may be contained with respect to 100 wt % of the soft magnetic layers 12.

Hereinafter, explained is a method of manufacturing the magnetic core 10 according to the present embodiment.

First, explained is a method of manufacturing a soft magnetic ribbon to be the soft magnetic layers 12 included in the magnetic core 10 by lamination. Hereinafter, the soft magnetic ribbon may be simply referred to as a ribbon.

The soft magnetic ribbons are manufactured in any manner. For example, the soft magnetic ribbons according to the present embodiment are manufactured by a single-roller melt-spinning method. The ribbons may be continuous ribbons.

In the single-roller melt-spinning method, pure metals of respective metal elements contained in a soft magnetic alloy finally obtained are initially prepared and weighed so that a composition identical to that of the soft magnetic alloy finally obtained is obtained. Then, the pure metals of the respective metal elements are melted and mixed to make a base alloy. Incidentally, the pure metals are melted in any manner. For example, the pure metals are melted by high-frequency heating after a chamber is evacuated. Incidentally, the base alloy and the soft magnetic alloy including Fe based nanocrystals finally obtained normally have the same composition.

Next, the prepared base alloy is melted by heating to obtain a molten metal. The temperature of the molten metal is not limited and may be, for example, 1100-1350° C.

In the single-roller melt-spinning method, the thickness of the ribbon to be obtained can be controlled by mainly controlling the rotating speed of the roller, but can also be controlled by, for example, controlling the distance between the nozzle and the roller, the temperature of the molten metal, or the like. The thickness of the ribbon is not limited, but may be 14-30 for example. Incidentally, the thickness of the ribbon and the thickness of each of the soft magnetic layers 12 included in the magnetic core 10 to be finally obtained are substantially the same.

There is no limit to the temperature and the rotation speed of the roller or the atmosphere inside the chamber. The temperature of the roller is substantially a room temperature or higher and 80° C. or lower. The lower the temperature of the roller is, the smaller the average grain size of the fine crystals tends to be. The higher the rotation speed of the roller is, the smaller the average grain size of the fine crystals tends to be. For example, the rotation speed of the roller is 10-30 m/sec. From the viewpoint of cost, the atmosphere inside the chamber is preferably atmospheric air.

Before a heat treatment mentioned below, the ribbon has an amorphous structure, that is, a structure composed of only amorphous phases or the nanohetero structure. A ribbon having a structure including Fe based nanocrystals can be obtained by being subjected to a heat treatment mentioned below. A ribbon having the nanohetero structure may be obtained by the heat treatment.

Whether the ribbon of the soft magnetic alloy has an amorphous structure or a crystal structure can be confirmed by a normal X-ray diffraction measurement (XRD).

Specifically, an X-ray structural analysis is carried out by XRD to calculate an amorphous ratio X (%) shown by the following formula (1). When the amorphous ratio X (%) is 85% or more, the ribbon of the soft magnetic alloy has an amorphous structure. When the amorphous ratio X (%) is less than 85%, the ribbon of the soft magnetic alloy has a crystal structure.

X (%)=100−(Ic/(Ic+Ia)×100)  (1)

Ic: scattering integrated intensity of crystal phase

Ia: scattering integrated intensity of amorphous phase

For calculation of the amorphous ratio X, the soft magnetic alloy according to the present embodiment is subjected to an X-ray crystal structural analysis by XRD to obtain the chart shown in FIG. 4. This chart is subjected to a profile fitting using the Lorentz function of the following formula (2).

f  ( x ) = h 1 + ( x - u ) 2 w 2 + b ( 2 )

h: peak height

u: peak position

w: hail-value width

b: background height

As a result of the profile fitting, obtained are a crystalline component pattern α_c denoting a scattering integrated intensity of crystal phase, an amorphous component pattern α_a denoting a scattering integrated intensity of amorphous phase, and a pattern α_c+a obtained by combining them shown in FIG. 5. From the obtained patterns, obtained are a scattering integrated intensity of crystal phase Ic and a scattering integrated intensity of amorphous phase Ia. Incidentally, the measurement range is a diffraction angle 2θ, in which a halo derived from amorphousness can be confirmed, and is specifically 2θ=30° to 60°. In this range, an error between the actually measured integrated intensity with XRD and the integrated intensity calculated by the Lorentz function is set to be within 1%.

In the present embodiment, when the soft magnetic alloy is obtained in the shape of a ribbon by the single-roller melt-spinning method mentioned below, an amorphous ratio (X_A) on the surface in contact with the roller surface and an amorphous ratio (X_B) on the surface not in contact with the roller surface may be different from each other. In this case, an average of the X_A and the X_B is an amorphous ratio X.

The ribbon before the heat treatment may have a structure composed of only amorphous phases, but preferably has a nanohetero structure. The grain size of the fine crystals in the nanohetero structure is not limited, but the average grain size is preferably 0.3-5 nm.

The existence and average particle size of the fine crystals in case of a nanohetero structure can be observed by, for example, obtaining an electron diffraction image and a high resolution image of a sample thinned by ion milling using a transmission electron microscope. When an electron diffraction image is used, a ring-shaped diffraction is formed in case of a structure composed of only amorphous phases in the diffraction pattern, whereas diffraction spots caused by the fine crystals are generated in case of a structure including fine crystals. When a high resolution image is used, the existence and average particle size of the fine crystals can be observed visually at a magnification of 1.00×10⁵ to 3.00×10⁵.

There is no limit to heat treatment conditions for manufacturing a ribbon having a structure including Fe based nanocrystals or a ribbon having a nanohetero structure. The preferable heat treatment conditions differ depending on the composition of the soft magnetic ribbon. Normally, a heat-treatment temperature is preferably about 400-700° C., and a heat-treatment time is preferably about 0.1-6 hours, but favorable heat-treatment temperature and heat-treatment time may be in a range deviated from the above ranges depending on the composition. The heat treatment is carried out in any atmosphere, such as an active atmosphere of air and an inert atmosphere of Ar gas, N₂ gas, etc. Due to the heat treatment, the soft magnetic ribbon becomes brittle and is turned into a state easily subjected to a fragmentation treatment. In addition, residual strain in the soft magnetic ribbon is removed.

Incidentally, if the ribbon has a nanohetero structure at the stage of being manufactured, no heat treatment may be carried out. For the above-mentioned reasons, however, the heat treatment is preferably carried out. The heat treatment may be carried out after the manufacture of the magnetic core 10 mentioned below.

The average grain size of crystals contained in the obtained soft magnetic ribbon is calculated in any manner, such as observation using a transmission electron microscope. The crystal structure of body-centered cubic (bcc) structure is also confirmed in any manner, such as X-ray diffraction measurement.

A method of manufacturing a magnetic core 10 according to the present embodiment mainly includes an adhesive-layer formation step, a crack formation step (fragmentation step), a punching step, and a lamination step. Hereinafter, the outline of each step is explained.

(Adhesive-Layer Formation Step)

The adhesive layer is formed on each of the soft magnetic ribbons subjected to the heat treatment. The adhesive layer can be formed using a known method. For example, the adhesive layer may be formed by thinly applying a solution containing a resin to the soft magnetic ribbons and drying the solvent. In addition, a double-sided tape may be adhered to the soft magnetic ribbons as an adhesive layer. For example, the double-sided tape is a polyethylene terephthalate (PET) film whose both surfaces are coated with an adhesive.

(Crack Formation Step (Fragmentation Step))

Each of the multiple soft magnetic ribbons with the adhesive layers is fragmented by generating cracks. A known method can be used for the generation of cracks. For example, cracks may be generated by applying an external force to the soft magnetic ribbons. For example, applying an external force to the soft magnetic ribbons is carried out by pressing with a mold, bending through a rolling roller, or the like. The mold and the rolling roller may be provided with a predetermined uneven pattern.

Then, each of the soft magnetic ribbons is fragmented by generating a plurality of cracks so that the average crack interval is within the above-mentioned range. The average crack interval is controlled in any manner. When the soft magnetic ribbons are pressed to be fragmented with a mold, for example, the average crack interval can be appropriately changed by changing the pressure during pressing. When the soft magnetic ribbons are bent through a rolling roller, for example, the average crack interval can be appropriately changed by changing the number of times where the soft magnetic ribbons are passed through the rolling roller.

When the adhesive layers are formed in advance, it becomes easy to prevent small pieces divided by the cracks from scattering. That is, the soft magnetic ribbons after forming the cracks are divided into a plurality of small pieces, but the locations of all of the small pieces are fixed via the adhesive layers, and the shape before forming the cracks is thereby substantially maintained as a whole. If the cracks can be formed while maintaining the overall shape of the soft magnetic ribbons even without using the adhesive layers, however, the adhesive layers are not necessarily formed before the cracks are formed.

(Punching Step)

Next, each of the multiple fragmented soft magnetic ribbons with the cracks is punched into a predetermined shape. In the present embodiment, as shown in FIG. 1, a central part of each of the ribbons is punched into a circular shape. The punching step can be carried out using a known method. For example, the punching step can be performed by sandwiching the soft magnetic ribbons between a punching die having a desired shape and a facing plate and pressurizing them from the facing plate to the punching die or from the punching die to the facing plate. Incidentally, when the adhesive layers are formed on the soft magnetic ribbons before the punching, the soft magnetic ribbons are punched together with the adhesive layers.

The soft magnetic ribbons composed of the soft magnetic material according to the present embodiment is hard and is thereby difficult to be punched with a weak force. When the soft magnetic ribbons are punched, a stress is generated by cutting the punched portion and the remaining portion. The stronger the force of the punching is, the larger the stress becomes. This stress is transmitted to the remaining portion of the soft magnetic ribbons and deteriorates soft magnetic characteristics. That is, coercivity becomes large.

However, each of the soft magnetic ribbons according to the present embodiment has cracks and is fragmented. Thus, each of the soft magnetic ribbons according to the present embodiment can be punched with a weaker force compared to when a soft magnetic ribbon has no cracks and is not fragmented. Thus, the stress becomes small. Moreover, the portion near the cut surface where the stress is generated at the time of punching and the other portion are physically distant from each other. Thus, the stress is not transmitted to most part other than the portion near the cut surface. Then, the deterioration of soft magnetic characteristics caused by the stress can be minimized.

Therefore, in the soft magnetic ribbons according to the present embodiment, the deterioration of soft magnetic characteristics due to punching (increase in coercivity) is reduced, and the soft magnetic characteristics of the magnetic core 10 finally obtained are improved. Furthermore, since the soft magnetic ribbons according to the present embodiment can be punched with a comparatively weak force, the soft magnetic ribbons can be easily processed into a desired shape and is excellent in productivity.

(Lamination Step)

The magnetic core 10 according to the present embodiment can be obtained by overlapping and laminating the multiple punched soft magnetic ribbons via the adhesive layers in the thickness direction. Protective films 13 may be formed on one end and the other end in the lamination direction (the z-axis direction in FIG. 1 and FIG. 2). The protective films 13 are formed in any manner.

Incidentally, the steps other than the crack formation step and the lamination step are not essential steps. Furthermore, the order of each step may be rearranged appropriately.

The magnetic core 10 according to the present embodiment has a structure in which the space factor of the magnetic material (the soft magnetic layers 12) is increased by laminating a plurality of soft magnetic ribbons and is strong and easy to handle.

Since the magnetic core 10 according to the present embodiment is formed by laminating a plurality of soft magnetic ribbons, the current path is divided at a plurality of locations in the lamination direction. In the magnetic core 10 according to the present embodiment, since each of the soft magnetic ribbons (the soft magnetic layers 12) has cracks and is fragmented, the current path is also divided at a plurality of locations in a direction intersecting the lamination direction. Therefore, in the coil device according to the present embodiment, the eddy current path accompanying the change of the magnetic flux in the alternating magnetic field is divided in all directions, and the eddy current loss can be greatly reduced.

FIG. 1 illustrates a cylindrical magnetic core, but the magnetic core according to the present embodiment may have any known shape, such as a rectangular cylindrical shape. The magnetic core according to the present embodiment may be formed by combining a plurality of cores, such as E-type cores.

The magnetic core 10 is used for any purposes, such as for coil devices including a conductor (e.g., transformer, choke coil, magnetic sensor).

EXAMPLES

Experimental Example 1

<Preparation of Soft Magnetic Ribbon>

Raw material metals were weighed so as to have the alloy composition of each example and comparative example shown in the following tables and were melted by high frequency heating to prepare base alloys.

After that, the prepared base alloys were melted by heating and turned into a molten metal at 1250° C. This metal was sprayed against a roller of 60° C. rotating at 20 m/sec. in the air (single-roller melt-spinning method) to form a ribbon. Incidentally, the thickness of the ribbon was about 20 and the width of the ribbon was about 50 mm.

Next, whether the obtained ribbon had an amorphous structure (a structure composed of only amorphous phases or a nanohetero structure) or a crystal structure was determined by a normal X-ray diffraction (XRD) measurement. The results are shown in Table 1.

After that, a heat treatment was carried out for the ribbons of all examples except for Samples 1 and 12 in Tables 1 and 2. The heat treatment conditions of Samples 2-6 and 13-17 were 500° C. (heat treatment temperature), 60 minutes (holding time), 1° C./min (heating rate), and 1° C./min (cooling rate). The heat treatment conditions of Samples 7-11 and 18-22 were 570° C. (heat treatment temperature), 60 minutes (holding time), 1° C./min (heating rate), and 1° C./min (cooling rate).

<Evaluation of Soft Magnetic Ribbons>

The fine structure of each ribbon after the heat treatment was confirmed by X-ray diffraction measurement (XRD) and observation using a transmission electron microscope (TEM). Specifically, observed was which structure (a structure including Fe based nanocrystals, a nanohetero structure, or a structure composed of only amorphous phases) each of the ribbons had. Incidentally, the structure including Fe based nanocrystals was bcc.

Then, when the fine structure of each ribbon after the heat treatment was a nanohetero structure, it was confirmed that the average grain size of the fine crystals was 0.3-5.0 nm in all Examples. When the fine structure of each ribbon after the heat treatment was a structure including Fe based nanocrystals, it was confirmed that the average grain size of the Fe based nanocrystals was 5.0 nm or more and 30 nm or less in all examples.

Furthermore, a saturation magnetic flux density Bs and a coercivity Hca of each ribbon after the heat treatment were measured. The saturation magnetic flux density was measured in a magnetic field of 1000 kA/m using a vibrating sample magnetometer (VSM). The coercivity was measured in a magnetic field of 5 kA/m using a DC BH tracer.

<Manufacture of Magnetic Core>

First, a resin solution was applied to the obtained soft magnetic ribbons. Then, the solvent was dried, and adhesive layers each having a thickness of about 1-2 μm were formed on both surfaces of each of the soft magnetic ribbons to manufacture a magnetic sheet having the adhesive layers.

Next, the manufactured magnetic sheet was subjected to a crack formation treatment so that the average crack interval of each of the soft magnetic ribbons would be the value shown in Table 2, and a fragmented magnetic sheet was manufactured. Incidentally, the magnetic sheets of Samples 1 and 12, which used the soft magnetic ribbons whose fine structure was amorphous, could not form cracks and could not be fragmented.

Next, the fragmented magnetic sheet was punched into a ring shape (outer diameter: 18 mm, inner diameter: 10 mm). Specifically, this punching was performed by sandwiching the fragmented magnetic sheet between a punching die and a facing plate and applying pressure from the facing plate to the punching die. Incidentally, the magnetic sheets of Samples 1 and 12, which could not be fragmented, could not be punched with a force equivalent to that of the fragmented magnetic sheets of the other examples.

Next, the punched-out fragmented magnetic sheets were attached to each other so as to have a height of about 5 mm and laminated to obtain a magnetic core. The space factor of the obtained soft magnetic layers of the magnetic core was about 85%. Furthermore, 30 magnetic cores were manufactured for each sample in the same procedure.

<Evaluation of Magnetic Cores>

As with the coercivity Hca of the ribbons, the coercivity Hcb of the magnetic cores was measured in a magnetic field of 5 kA/m using a DC BH tracer. The coercivity of each of the 30 magnetic cores was measured and averaged to obtain Hcb.

Then, a change in coercivity ΔHc (=Hcb−Hca) was calculated from the obtained Hca and Hcb. In addition, a coercivity change rate (%) was calculated. Specifically, the coercivity change rate (%) was calculated by substituting ΔHc and Hca into the formula of (ΔHc/Hca)×100(%). A coercivity change rate of less than 100% was regarded as favorable.

Finally, a coil was wound around each of the magnetic cores along the circumferential direction to form 30 coil devices, and the inductance of each coil at 100 kHz was measured using an LCR meter and averaged to obtain Ls.

TABLE 1
						Saturation	Coercivity
	Example/					Magnetic Flux	of Ribbons
Sample	Comparative		XRD Before	Heat	Fine Structure After	Density of	Hca
No.	Example	Composition	Heat Treatment	Treatment	Heat Treatment	Ribbons Bs (T)	(A/m)

1	Comp. Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	no	amorphous	1.17	2.10
2	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
3	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
4	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
4a	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
4b	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
5	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
5a	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
5b	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
6	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	nanotehero	1.18	1.20
7	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
8	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
9	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
9a	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
9b	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
10	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
10a	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
10b	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
11	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.50
12	Comp. Ex.	Fe0.84Nb0.07B0.09	amorphous	no	amorphous	0.50	2.10
13	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
14	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
15	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
15a	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
15b	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
16	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
16a	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
16b	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
17	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	nanotehero	1.34	4.80
18	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
19	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
20	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
20a	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
20b	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
21	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
21a	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
21b	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50
22	Ex.	Fe0.84Nb0.07B0.09	amorphous	yes	Fe based nanocrystal	1.51	5.50

TABLE 2
			Average		Coercivity	ΔHc	Coercivity
	Example/		Crack		of Core	[Hcb −	Change
Sample	Comparative		Interval	Punching	Hcb	Hca]	Rate	Ls
No.	Example	Fragmentation	(mm)	Possibility	(A/m)	(A/m)	(%)	(μH)
1	Comp. Ex.	impossible	—	impossible	—	—	—	—
2	Ex.	yes	0.17	possible	2.21	1.01	84	346
3	Ex.	yes	0.50	possible	2.12	0.92	77	552
4	Ex.	yes	0.015	possible	2.21	1.01	84	33
4a	Ex.	yes	0.030	possible	2.22	1.02	85	76
4b	Ex.	yes	0.075	possible	2.22	1.02	85	190
5	Ex.	yes	0.010	possible	2.28	1.08	90	20
5a	Ex.	yes	0.10	possible	2.21	1.01	84	250
5b	Ex.	yes	0.30	possible	2.19	0.99	83	480
6	Ex.	yes	0.75	possible	2.21	1.01	84	626
7	Ex.	yes	0.17	possible	0.86	0.36	72	356
8	Ex.	yes	0.50	possible	0.82	0.32	65	598
9	Ex.	yes	0.015	possible	0.86	0.36	73	33
9a	Ex.	yes	0.030	possible	0.88	0.38	76	83
9b	Ex.	yes	0.075	possible	0.85	0.35	70	210
10	Ex.	yes	0.010	possible	0.90	0.40	80	20
10a	Ex.	yes	0.10	possible	0.88	0.38	76	254
10b	Ex.	yes	0.30	possible	0.83	0.33	66	504
11	Ex.	yes	0.75	possible	0.79	0.29	59	701
12	Comp. Ex.	impossible	—	impossible	—	—	—	—
13	Ex.	yes	0.17	possible	8.64	3.84	80	322
14	Ex.	yes	0.50	possible	8.27	3.47	72	472
15	Ex.	yes	0.015	possible	8.75	3.95	82	33
15a	Ex.	yes	0.030	possible	8.70	3.90	81	75
15b	Ex.	yes	0.075	possible	8.55	3.75	78	188
16	Ex.	yes	0.010	possible	8.57	3.77	79	20
16a	Ex.	yes	0.10	possible	8.55	3.75	78	240
16b	Ex.	yes	0.30	possible	8.50	3.70	77	418
17	Ex.	yes	0.75	possible	8.34	3.54	74	514
18	Ex.	yes	0.17	possible	9.36	3.86	70	346
19	Ex.	yes	0.50	possible	9.14	3.64	66	554
20	Ex.	yes	0.015	possible	9.33	3.83	70	33
20a	Ex.	yes	0.030	possible	9.31	3.81	69	80
20b	Ex.	yes	0.075	possible	9.30	3.80	69	190
21	Ex.	yes	0.010	possible	9.32	3.82	70	20
21a	Ex.	yes	0.10	possible	9.33	3.83	70	257
21b	Ex.	yes	0.30	possible	9.24	3.74	68	483
22	Ex.	yes	0.75	possible	9.09	3.59	65	637

According to Table 1 and Table 2, the soft magnetic ribbon of each example was able to be fragmented and punched, and the magnetic cores of each example had a favorable coercivity change rate. The reason why the magnetic cores of each example had a favorable coercivity change rate is explained below.

Since the soft magnetic ribbons were fragmented, the force during punching was able to be reduced. In addition, since the soft magnetic ribbons were fragmented, the stress generated near the cross section at the time of punching was less likely to be transmitted to the inside. As a result, the deterioration of soft magnetic characteristics (increase in coercivity and decrease in inductance) was restrained. In addition, the inductance Ls was higher as the average crack interval was larger and the size of each small piece was larger.

On the other hand, the soft magnetic ribbons of each comparative example, whose fine structure was amorphous, could not be fragmented or punched.

When the fine structure was a nanohetero structure or a structure including Fe based nanocrystals, the soft magnetic ribbons were able to be fragmented probably because the crystal grain boundaries served as a starting point of fragmentation at the time of applying an external force. On the other hand, the reason why the soft magnetic ribbons could not be fragmented when the fine structure was amorphous was that there were no grain boundaries or starting points of fragmentation.

Experimental Example 2

Except for changing the composition of the soft magnetic ribbons within the ranges shown in Tables 3-12, Experimental Example 2 was carried out with the same conditions as Samples No. 7-11 of Experimental Example 1.

	TABLE 3
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

24	Ex.	0.840	0.020	0.090	0.050	0.000	0.000	0.000	amorphous	1.58	2.80	0.17	4.84	2.04	73	351
25	Ex.	0.820	0.040	0.090	0.050	0.000	0.000	0.000	amorphous	1.56	2.40	0.17	4.23	1.83	76	359
26	Ex.	0.810	0.050	0.090	0.050	0.000	0.000	0.000	amorphous	1.53	1.90	0.17	3.35	1.45	76	371
45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
27	Ex.	0.780	0.080	0.090	0.050	0.000	0.000	0.000	amorphous	1.48	1.80	0.17	3.39	1.59	88	369
28	Ex.	0.760	0.100	0.090	0.050	0.000	0.000	0.000	amorphous	1.44	2.30	0.17	4.20	1.90	83	360
29	Ex.	0.740	0.120	0.090	0.050	0.000	0.000	0.000	amorphous	1.42	2.70	0.17	5.04	2.34	87	350
30	Ex.	0.720	0.140	0.090	0.050	0.000	0.000	0.000	amorphous	1.38	2.70	0.17	5.09	2.39	89	352
31	Comp. Ex.	0.710	0.150	0.090	0.050	0.000	0.000	0.000	amorphous	1.22	2.90	0.17	5.80	2.90	100	335

	TABLE 4
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

34	Comp. Ex.	0.870	0.060	0.020	0.050	0.000	0.000	0.000	crystal	1.60	217	0.17	438	221	102	7
35	Ex.	0.865	0.060	0.025	0.050	0.000	0.000	0.000	amorphous	1.62	2.60	0.17	4.29	1.69	65	351
36	Ex.	0.830	0.060	0.060	0.050	0.000	0.000	0.000	amorphous	1.57	2.10	0.17	3.70	1.60	76	363
37	Ex.	0.810	0.060	0.080	0.050	0.000	0.000	0.000	amorphous	1.56	1.80	0.17	3.21	1.41	78	371
45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
38	Ex.	0.770	0.060	0.120	0.050	0.000	0.000	0.000	amorphous	1.45	2.00	0.17	3.72	1.72	86	366
39	Ex.	0.740	0.060	0.150	0.050	0.000	0.000	0.000	amorphous	1.40	2.50	0.17	4.76	2.26	90	358
40	Ex.	0.690	0.060	0.200	0.050	0.000	0.000	0.000	amorphous	1.35	2.70	0.17	5.09	2.39	88	353
41	Comp. Ex.	0.680	0.060	0.210	0.050	0.000	0.000	0.000	amorphous	1.20	2.90	0.17	5.83	2.93	101	332

	TABLE 5
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

42	Ex.	0.850	0.060	0.090	0.000	0.000	0.000	0.000	amorphous	1.71	4.80	0.17	8.16	3.36	70	308
43	Ex.	0.840	0.060	0.090	0.010	0.000	0.000	0.000	amorphous	1.73	4.60	0.17	7.84	3.24	70	311
44	Ex.	0.820	0.060	0.090	0.030	0.000	0.000	0.000	amorphous	1.66	4.20	0.17	7.48	3.28	78	320
45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
46	Ex.	0.770	0.060	0.090	0.080	0.000	0.000	0.000	amorphous	1.47	2.20	0.17	3.98	1.78	81	361
47	Ex.	0.750	0.060	0.090	0.100	0.000	0.000	0.000	amorphous	1.44	2.50	0.17	4.75	2.25	90	356
48	Ex.	0.700	0.060	0.090	0.150	0.000	0.000	0.000	amorphous	1.37	2.70	0.17	5.08	2.38	88	353
49	Comp. Ex.	0.690	0.060	0.090	0.160	0.000	0.000	0.000	amorphous	1.28	2.80	0.17	5.78	2.98	107	329

	TABLE 6
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
50	Ex.	0.799	0.060	0.090	0.050	0.000	0.001	0.000	amorphous	1.51	1.40	0.17	2.59	1.19	85	377
51	Ex.	0.795	0.060	0.090	0.050	0.000	0.005	0.000	amorphous	1.51	1.20	0.17	2.27	1.07	89	384
52	Ex.	0.790	0.060	0.090	0.050	0.000	0.010	0.000	amorphous	1.50	1.50	0.17	2.66	1.16	78	377
53	Ex.	0.770	0.060	0.090	0.050	0.000	0.030	0.000	amorphous	1.48	1.70	0.17	3.05	1.35	79	376
54	Comp. Ex.	0.760	0.060	0.090	0.050	0.000	0.040	0.000	amorphous	1.43	3.20	0.17	6.56	3.36	105	342

	TABLE 7
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
55	Ex.	0.799	0.060	0.090	0.050	0.000	0.000	0.001	amorphous	1.53	2.10	0.17	3.80	1.70	81	368
56	Ex.	0.795	0.060	0.090	0.050	0.000	0.000	0.005	amorphous	1.51	2.30	0.17	4.23	1.93	84	364
57	Ex.	0.790	0.060	0.090	0.050	0.000	0.000	0.010	amorphous	1.52	2.20	0.17	4.01	1.81	82	364
58	Ex.	0.770	0.060	0.090	0.050	0.000	0.000	0.030	amorphous	1.43	2.40	0.17	4.48	2.08	87	356
59	Comp. Ex.	0.760	0.060	0.090	0.050	0.000	0.000	0.040	crystal	1.48	345	0.17	724	379	110	3

	TABLE 8
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-	Compar-		M						Before	Density of	Ribbons	Crack	Core	[Hcb −	Change
ple	ative		(Nb)	B	P	Si	C	S	Heat	Ribbons	Hca	Interval	Hcb	Hca]	Rate	Ls
No.	Example	Fe	a	b	c	d	e	f	Treatment	Bs (T)	(A/m)	(mm)	(A/m)	(A/m)	(%)	(μH)
45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
60	Ex.	0.795	0.060	0.090	0.050	0.005	0.000	0.000	amorphous	1.53	1.70	0.17	3.15	1.45	86	370
61	Ex.	0.790	0.060	0.090	0.050	0.010	0.000	0.000	amorphous	1.52	1.60	0.17	2.82	1.22	76	377
62	Ex.	0.780	0.060	0.090	0.050	0.020	0.000	0.000	amorphous	1.50	1.60	0.17	2.99	1.39	87	372
63	Ex.	0.770	0.060	0.090	0.050	0.030	0.000	0.000	amorphous	1.46	2.10	0.17	3.96	1.86	88	367
64	Ex.	0.740	0.060	0.090	0.050	0.060	0.000	0.000	amorphous	1.42	2.50	0.17	4.61	2.11	85	358
65	Ex.	0.810	0.030	0.090	0.000	0.070	0.000	0.000	amorphous	1.45	4.80	0.17	8.50	3.70	77	327
66	Ex.	0.790	0.030	0.090	0.000	0.090	0.000	0.000	amorphous	1.35	4.50	0.17	8.26	3.76	84	330
67	Ex.	0.745	0.030	0.090	0.000	0.135	0.000	0.000	amorphous	1.31	4.80	0.17	8.87	4.07	85	330
68	Ex.	0.725	0.030	0.090	0.000	0.155	0.000	0.000	amorphous	1.20	4.30	0.17	8.03	3.73	87	329
69	Ex.	0.705	0.030	0.090	0.000	0.175	0.000	0.000	amorphous	1.18	3.20	0.17	6.13	2.93	92	336

	TABLE 9
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-

Compar-

M

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

(Nb)

B

P

Si

C

S

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Fe

a

b

c

d

e

f

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

70a	Ex.	0.860	0.000	0.090	0.050	0.000	0.000	0.000	amorphous	1.75	10.90	0.17	18.20	7.30	67	205
70	Ex.	0.850	0.000	0.090	0.050	0.010	0.000	0.000	amorphous	1.74	10.80	0.17	18.16	7.36	68	209
71	Ex.	0.830	0.000	0.090	0.050	0.030	0.000	0.000	amorphous	1.73	9.50	0.17	16.57	7.07	74	223
72	Ex.	0.810	0.000	0.090	0.050	0.050	0.000	0.000	amorphous	1.70	9.30	0.17	16.58	7.28	78	228
73	Ex.	0.790	0.000	0.090	0.050	0.070	0.000	0.000	amorphous	1.66	9.20	0.17	16.69	7.49	81	229
74	Ex.	0.770	0.000	0.090	0.050	0.090	0.000	0.000	amorphous	1.64	9.40	0.17	17.29	7.89	84	227
74a	Ex.	0.820	0.000	0.090	0.000	0.090	0.000	0.000	amorphous	1.73	9.50	0.17	16.70	7.20	76	225

	TABLE 10
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

Example/

Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf

XRD

Flux

of

Average

of

ΔHc

civity

Sam-	Compar-		M						Before	Density of	Ribbons	Crack	Core	[Hcb −	Change
ple	ative		(Nb)	B	P	Si	C	S	Heat	Ribbons	Hca	Interval	Hcb	Hca]	Rate	Ls
No.	Example	Fe	a	b	c	d	e	f	Treatment	Bs (T)	(A/m)	(mm)	(A/m)	(A/m)	(%)	(μH)
75	Ex.	0.730	0.080	0.120	0.070	0.000	0.000	0.000	amorphous	1.40	2.90	0.17	5.39	2.49	86	350
45	Ex.	0.800	0.060	0.090	0.050	0.000	0.000	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
76	Ex.	0.880	0.040	0.030	0.050	0.000	0.000	0.000	amorphous	1.67	2.70	0.17	4.58	1.88	70	354
77	Ex.	0.900	0.030	0.030	0.040	0.000	0.000	0.000	amorphous	1.70	2.60	0.17	4.36	1.76	68	354

	TABLE 11
	Saturation	Coer-		Coer-
	Magnetic	civity		civity		Coer-

	Example/	Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf	XRD	Flux	of	Average	of	ΔHc	civity
Sam-	Compar-	(b~f were the same as those of Sample No. 45)	Before	Density of	Ribbons	Crack	Core	[Hcb −	Change
ple	ative	M	Heat	Ribbons	Hca	Interval	Hcb	Hca]	Rate	Ls

No.	Example	Type	a	Treatment	Bs (T)	(A/m)	(mm)	(A/m)	(A/m)	(%)	(μH)
45	Ex.	Nb	0.060	amorphous	1.50	1.80	0.17	3.17	1.37	76	371
78	Ex.	Hf	0.060	amorphous	1.51	1.80	0.17	3.16	1.36	76	369
79	Ex.	Zr	0.060	amorphous	1.52	1.70	0.17	3.08	1.38	81	375
80	Ex.	Ta	0.060	amorphous	1.53	1.70	0.17	3.11	1.41	83	378
81	Ex.	Mo	0.060	amorphous	1.50	2.00	0.17	3.68	1.68	84	371
82	Ex.	W	0.060	amorphous	1.50	2.00	0.17	3.66	1.66	83	379
83	Ex.	V	0.060	amorphous	1.51	1.90	0.17	3.40	1.50	79	382
84	Ex.	Ti	0.060	amorphous	1.51	2.00	0.17	3.62	1.62	81	380
85	Ex.	Nb0.5Hf0.5	0.060	amorphous	1.52	1.80	0.17	3.28	1.48	82	374
86	Ex.	Zr0.5Ta0.5	0.060	amorphous	1.53	1.90	0.17	3.51	1.61	85	376
87	Ex.	Nb0.4Hf0.3Zr0.3	0.060	amorphous	1.51	2.00	0.17	3.62	1.62	81	380

	TABLE 12
		Fe(1 − (α + β)) X1αX2β		Saturation	Coer-		Coer-
		(The type of M and a-f were the		Magnetic	civity		civity		Coer-
	Example/	same as those of Sample No. 45)	XRD	Flux	of	Average	of	ΔHc	civity

Sam-

Compar-

X1

X2

Before

Density of

Ribbons

Crack

Core

[Hcb −

Change

ple

ative

α{1 − (a + b +

β{1 − (a + b +

Heat

Ribbons

Hca

Interval

Hcb

Hca]

Rate

Ls

No.

Example

Type

c + d + e + f)}

Type

c + d + e + f)}

Treatment

Bs (T)

(A/m)

(mm)

(A/m)

(A/m)

(%)

(μH)

45	Ex.	—	0.000	—	0.000	amorphous	1.50	1.80	0.17	3.33	1.53	85	370
89	Ex.	Co	0.010	—	0.000	amorphous	1.53	2.10	0.17	3.78	1.68	80	365
90	Ex.	Co	0.100	—	0.000	amorphous	1.55	2.50	0.17	4.65	2.15	86	359
91	Ex.	Co	0.400	—	0.000	amorphous	1.60	2.90	0.17	5.50	2.60	90	354
92	Ex.	Ni	0.010	—	0.000	amorphous	1.51	1.80	0.17	3.19	1.39	77	373
93	Ex.	Ni	0.100	—	0.000	amorphous	1.47	1.70	0.17	3.10	1.40	82	373
94	Ex.	Ni	0.400	—	0.000	amorphous	1.42	1.60	0.17	2.76	1.16	72	377
95	Ex.	—	0.000	Al	0.001	amorphous	1.52	1.80	0.17	3.19	1.39	77	374
96	Ex.	—	0.000	Al	0.005	amorphous	1.51	1.80	0.17	3.18	1.38	77	371
97	Ex.	—	0.000	Al	0.010	amorphous	1.51	1.70	0.17	2.97	1.27	75	370
98	Ex.	—	0.000	Al	0.030	amorphous	1.50	1.80	0.17	3.22	1.42	79	372
99	Ex.	—	0.000	Zn	0.001	amorphous	1.50	1.80	0.17	3.25	1.45	81	372
100	Ex.	—	0.000	Zn	0.005	amorphous	1.52	1.90	0.17	3.44	1.54	81	370
101	Ex.	—	0.000	Zn	0.010	amorphous	1.50	1.80	0.17	3.23	1.43	79	375
102	Ex.	—	0.000	Zn	0.030	amorphous	1.51	1.90	0.17	3.46	1.56	82	372
103	Ex.	—	0.000	Sn	0.001	amorphous	1.52	1.80	0.17	3.27	1.47	82	374
104	Ex.	—	0.000	Sn	0.005	amorphous	1.51	1.90	0.17	3.49	1.59	84	367
105	Ex.	—	0.000	Sn	0.010	amorphous	1.52	1.90	0.17	3.47	1.57	83	375
106	Ex.	—	0.000	Sn	0.030	amorphous	1.50	2.00	0.17	3.68	1.68	84	368
107	Ex.	—	0.000	Cu	0.001	amorphous	1.52	1.60	0.17	2.84	1.24	77	376
108	Ex.	—	0.000	Cu	0.005	amorphous	1.52	1.70	0.17	3.06	1.36	80	373
109	Ex.	—	0.000	Cu	0.010	amorphous	1.52	1.50	0.17	2.74	1.24	83	377
110	Ex.	—	0.000	Cu	0.030	amorphous	1.54	1.60	0.17	2.77	1.17	73	375
111	Ex.	—	0.000	Cr	0.001	amorphous	1.52	1.80	0.17	3.26	1.46	81	371
112	Ex.	—	0.000	Cr	0.005	amorphous	1.51	1.70	0.17	3.10	1.40	82	376
113	Ex.	—	0.000	Cr	0.010	amorphous	1.50	1.80	0.17	3.23	1.43	79	370
114	Ex.	—	0.000	Cr	0.030	amorphous	1.51	1.90	0.17	3.36	1.46	77	370
115	Ex.	—	0.000	Bi	0.001	amorphous	1.51	1.80	0.17	3.21	1.41	78	375
116	Ex.	—	0.000	Bi	0.005	amorphous	1.50	1.70	0.17	3.07	1.37	80	371
117	Ex.	—	0.000	Bi	0.010	amorphous	1.49	1.80	0.17	3.28	1.48	82	374
118	Ex.	—	0.000	Bi	0.030	amorphous	1.48	2.00	0.17	3.71	1.71	85	365
119	Ex.	—	0.000	La	0.001	amorphous	1.52	1.80	0.17	3.23	1.43	80	378
120	Ex.	—	0.000	La	0.005	amorphous	1.51	1.90	0.17	3.45	1.55	82	370
121	Ex.	—	0.000	La	0.010	amorphous	1.49	2.10	0.17	3.94	1.84	88	369
122	Ex.	—	0.000	La	0.030	amorphous	1.48	2.10	0.17	3.85	1.75	83	362
123	Ex.	—	0.000	Y	0.001	amorphous	1.51	1.90	0.17	3.53	1.63	86	368
124	Ex.	—	0.000	Y	0.005	amorphous	1.49	1.80	0.17	3.29	1.49	83	370
125	Ex.	—	0.000	Y	0.010	amorphous	1.48	1.80	0.17	3.22	1.42	79	372
126	Ex.	—	0.000	Y	0.030	amorphous	1.49	2.00	0.17	3.74	1.74	87	369
127	Ex.	—	0.000	N	0.001	amorphous	1.49	2.00	0.17	3.60	1.60	80	368
128	Ex.	—	0.000	O	0.001	amorphous	1.50	1.90	0.17	3.37	1.47	77	369
129	Ex.	Co	0.100	Al	0.050	amorphous	1.52	2.10	0.17	3.96	1.86	89	368
130	Ex.	Co	0.100	Zn	0.050	amorphous	1.54	2.20	0.17	4.07	1.87	85	366
131	Ex.	Co	0.100	Sn	0.050	amorphous	1.53	2.20	0.17	4.07	1.87	85	362
132	Ex.	Co	0.100	Cu	0.050	amorphous	1.53	2.00	0.17	3.75	1.75	87	372
133	Ex.	Co	0.100	Cr	0.050	amorphous	1.53	2.10	0.17	3.94	1.84	87	370
134	Ex.	Co	0.100	Bi	0.050	amorphous	1.51	2.20	0.17	4.08	1.88	86	365
135	Ex.	Co	0.100	La	0.050	amorphous	1.52	2.30	0.17	4.24	1.94	85	359
136	Ex.	Co	0.100	Y	0.050	amorphous	1.53	2.30	0.17	4.34	2.04	89	364
137	Ex.	Ni	0.100	Al	0.050	amorphous	1.48	1.70	0.17	3.06	1.36	80	374
138	Ex.	Ni	0.100	Zn	0.050	amorphous	1.47	1.70	0.17	3.15	1.45	85	373
139	Ex.	Ni	0.100	Sn	0.050	amorphous	1.48	1.60	0.17	2.81	1.21	76	373
140	Ex.	Ni	0.100	Cu	0.050	amorphous	1.49	1.60	0.17	2.79	1.19	74	374
141	Ex.	Ni	0.100	Cr	0.050	amorphous	1.47	1.70	0.17	2.97	1.27	75	373
142	Ex.	Ni	0.100	Bi	0.050	amorphous	1.48	1.80	0.17	3.27	1.47	82	370
143	Ex.	Ni	0.100	La	0.050	amorphous	1.46	1.80	0.17	3.29	1.49	83	369
144	Ex.	Ni	0.100	Y	0.050	amorphous	1.45	1.80	0.17	3.31	1.51	84	376

In the soft magnetic ribbons of all of the above-mentioned examples, the fine structure was a structure including Fe based nanocrystals, and the Fe based nanocrystals had an average grain size of 5.0 nm or more and 30 nm or less. The examples whose soft magnetic ribbons had a composition falling within the specific range had a favorable coercivity change rate as compared with that of the comparative examples whose soft magnetic ribbons had a composition falling out of the specific range. In Sample 34 (too small B content (b)) and Sample 59 (too large S content (f)), the fine structure of the soft magnetic ribbons before the heat treatment was a crystal structure, Fe based nanocrystals could not be deposited by the heat treatment, and the coercivity was significantly high. In addition, the inductance Ls of the magnetic cores was significantly low.

Experimental Example 3

Except for changing the temperature of the molten metal obtained by heating the base alloys and further changing the existence of the heat treatment, the heat treatment temperature, and the heat treatment time, Experimental Example 3 was carried out with the same conditions as Sample No. 45 of Experimental Example 2. The results are shown in Table 13 and Table 14. In examples and comparative examples of Table 13 not subjected to the heat treatment, for the sake of convenience, the crystal average particle size and the fine structure before the heat treatment were the same as those after the heat treatment.

	TABLE 13
	Fe(1 − (a + b + c + d + e + f))MaBbPcSidCeSf (a-f were the same as those of Sample No. 45)

				Crystal				Crystal		Saturation	Coer-
		Temperature		Average				Average		Magnetic	civity
	Example/	for Manu-	XRD	Particle Size	Fine	Heat	Heat	Grain Size	Fine	Flux	of
Sam-	Compar-	facturing	Before	Before Heat	Structure	Treatment	Treatment	After Heat	Structure	Density of	Ribbons
ple	ative	Ribbons	Heat	Treatment	Before Heat	Temperature	Time	Treatment	After Heat	Ribbons	Hca
No.	Example	(° C.)	Treatment	(nm)	Treatment	(° C.)	(h)	(nm)	Treatment	Bs (T)	(A/m)

145	Comp. Ex.	1200	amorphous	no fine	amorphous	no heat treatment	no fine	amorphous	0.70	8.90
				crystals			crystals
146	Ex.	1225	amorphous	0.1	nanohetero	no heat treatment	0.1	nanohetero	1.21	10.10
147	Ex.	1250	amorphous	0.3	nanohetero	no heat treatment	0.3	nanohetero	1.25	9.70
148	Ex.	1250	amorphous	0.3	nanohetero	no heat treatment	0.3	nanohetero	1.25	9.70
149	Ex.	1250	amorphous	0.3	nanohetero	no heat treatment	0.3	nanohetero	1.25	9.70
150	Ex.	1250	amorphous	0.3	nanohetero	no heat treatment	0.3	nanohetero	1.25	9.70
151	Ex.	1275	amorphous	10	nanohetero	no heat treatment	10	nanohetero	1.31	8.50
152	Ex.	1275	amorphous	10	nanohetero	no heat treatment	10	nanohetero	1.31	8.50
153	Ex.	1300	amorphous	15	nanohetero	no heat treatment	15	nanohetero	1.32	7.80
154	Ex.	1300	amorphous	15	nanohetero	no heat treatment	15	nanohetero	1.32	7.80

155	Ex.	1200	amorphous	no fine	amorphous	600	1	10	nanohetero	1.45	2.00
				crystals
156	Ex.	1225	amorphous	0.1	nanohetero	450	1	3	nanohetero	1.48	2.00
157	Ex.	1250	amorphous	0.3	nanohetero	500	1	5	nanohetero	1.50	1.90
158	Ex.	1250	amorphous	0.3	nanohetero	550	1	10	Fe based	1.50	1.80
									nanocrystal
159	Ex.	1250	amorphous	0.3	nanohetero	575	1	13	Fe based	1.51	1.70
									nanocrystal
160	Ex.	1250	amorphous	0.3	nanohetero	600	1	10	Fe based	1.52	1.80
									nanocrystal
161	Ex.	1275	amorphous	10	nanohetero	600	1	12	Fe based	1.52	1.90
									nanocrystal
162	Ex.	1275	amorphous	10	nanohetero	650	1	30	Fe based	1.52	1.90
									nanocrystal
163	Ex.	1300	amorphous	15	nanohetero	600	1	17	Fe based	1.51	2.30
									nanocrystal
164	Ex.	1300	amorphous	15	nanohetero	650	10	50	Fe based	1.43	2.90
									nanocrystal

TABLE 14
			Average		Coercivity	ΔHc	Coercivity
	Example/		Crack		of Core	[Hcb −	Change
Sample	Comparative		Interval	Punching	Hcb	Hca]	Rate	Ls
No.	Example	Fragmentation	(mm)	Possibility	(A/m)	(A/m)	(%)	(μH)
145	Comp. Ex.	impossible	—	impossible	—	—	—	—
146	Ex.	yes	0.17	possible	18.93	8.83	87	231
147	Ex.	yes	0.17	possible	17.61	7.91	82	241
148	Ex.	yes	0.17	possible	17.76	8.06	83	237
149	Ex.	yes	0.17	possible	17.71	8.01	83	237
150	Ex.	yes	0.17	possible	17.71	8.01	83	241
151	Ex.	yes	0.17	possible	15.21	6.71	79	249
152	Ex.	yes	0.17	possible	14.87	6.37	75	252
153	Ex.	yes	0.17	possible	14.56	6.76	87	254
154	Ex.	yes	0.17	possible	14.65	6.85	88	248
155	Ex.	yes	0.17	possible	3.53	1.53	77	360
156	Ex.	yes	0.17	possible	3.54	1.54	77	367
157	Ex.	yes	0.17	possible	3.48	1.58	83	370
158	Ex.	yes	0.17	possible	3.23	1.43	79	371
159	Ex.	yes	0.17	possible	3.01	1.31	77	372
160	Ex.	yes	0.17	possible	3.27	1.47	82	371
161	Ex.	yes	0.17	possible	3.36	1.46	77	375
162	Ex.	yes	0.17	possible	3.53	1.63	86	374
163	Ex.	yes	0.17	possible	4.09	1.79	78	350
164	Ex.	yes	0.17	possible	5.38	2.48	86	328

According to Table 13 and Table 14, even if the temperature of the molten metal obtained by heating the base alloys was changed, and the existence of heat treatment, the heat treatment temperature, and the heat treatment time were further changed, when the fine structure of the soft magnetic ribbons finally used was a nanohetero structure or a structure including Fe based nanocrystals, the soft magnetic ribbons were able to be fragmented and punched, and the coercivity change rate was favorable. On the other hand, when the fine structure of the soft magnetic ribbons finally used was an amorphous structure, the soft magnetic ribbons could not be fragmented or punched out.

Experimental Example 4

Except for changing the space factor of the magnetic material, Experimental Example 4 was carried out with the same conditions as Sample No. 7 of Experimental Example 1. The results are shown in Table 15 and Table 16.

TABLE 15
						Saturation	Coercivity
	Example/					Magnetic Flux	of Ribbons
Sample	Comparative		XRD Before	Heat	Fine Structure After	Density of	Hca
No.	Example	Composition	Heat Treatment	Treatment	Heat Treatment	Ribbons Bs (T)	(A/m)

7	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.5
165	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.5
166	Ex.	Fe0.735Nb0.03B0.09Si0.135Cu0.01	amorphous	yes	Fe based nanocrystal	1.21	0.5

TABLE 16
			Average			Coercivity	ΔHc	Coercivity
	Example/		Crack			of Core	[Hcb −	Change
Sample	Comparative		Interval	Punching	Space	Hcb	Hca]	Rate	Ls
No.	Example	Fragmentation	(mm)	Possibility	Factor	(A/m)	(A/m)	(%)	(μH)

7	Ex.	yes	0.17	possible	85%	0.86	0.36	72	356
165	Ex.	yes	0.17	possible	96%	0.87	0.37	74	361
166	Ex.	yes	0.17	possible	72%	0.85	0.35	70	271

According to Table 15 and Table 16, even if the space factor was changed, the coercivity change rate was favorable in examples having a space factor of 70% or more and 99.5% or less. Incidentally, the higher the space factor was, the higher the inductance Ls tended to be, and the larger the coercivity change rate tended to be.

NUMERICAL REFERENCES

• 10 . . . magnetic core
• 12 . . . soft magnetic layer
• 13 . . . protective film
• 14 . . . adhesive layer
• A . . . center plane
• B . . . virtual line
• C . . . crack
• D . . . intersection