WO2019078321A1

WO2019078321A1 - Composite magnetic material, magnet containing said material, motor using said magnet, and method for producing said composite magnetic material

Info

Publication number: WO2019078321A1
Application number: PCT/JP2018/038922
Authority: WO
Inventors: 笹栗　大助; 西村　直樹; 正宣大塚
Original assignee: キヤノン株式会社
Priority date: 2017-10-20
Filing date: 2018-10-19
Publication date: 2019-04-25

Abstract

Provided is a composite magnetic material which has excellent magnetic characteristics. A composite magnetic material 1 according to the present invention is configured such that a plurality of hard magnetic particles 3 are dispersed like islands in a soft magnetic phase 2. The hard magnetic particles 3 have an average particle diameter of 2 nm or more, and are present in the soft magnetic phase 2 with an average interparticle distance of 100 nm or less.

Description

Composite magnetic material, magnet including the material, motor using the magnet, and method of manufacturing the composite magnetic material

The present invention relates to a composite magnetic material, a magnet including the material, a motor using the magnet, and a method of manufacturing the composite magnetic material.

A magnet using a rare earth element such as neodymium has a high residual magnetic flux density and a high coercive force, and has excellent magnetic properties, and thus has been widely used conventionally. However, because rare earth elements are rare metals and are distributed unevenly on the earth, they are expensive, etc., attempts are being made to manufacture high-performance magnets in which the amount of rare earth elements used is reduced. ing. As an example thereof, a nanocomposite magnet having a hard magnetic material with high coercivity and a soft magnetic material with high saturation magnetic flux density is known. In the nanocomposite magnet, a hard magnetic material having a high coercive force and a soft magnetic material having a high saturation magnetic flux density are magnetically coupled by an exchange coupling action, and exhibit excellent magnetic properties.

In Patent Document 1, a core made of a hard magnetic material containing epsilon iron oxide (ε-Fe ₂ O ₃ ), and a shell made of a soft magnetic material containing alpha iron (α-Fe), which covers the core, A magnetic particle having a core-shell structure is disclosed. Thereby, the hard magnetic material and the soft magnetic material are magnetically coupled in the magnetic particles to improve the magnetic characteristics.

JP 2011-35006 A

Patent Document 1 describes that the magnetic particles having the core-shell structure described above are densified to form a nanocomposite magnet. However, in this case, even when the above-mentioned magnetic particles are densified by close packing, voids of about 26% in volume ratio are generated between the particles. As a result of examination by the present inventors, it was found that the presence of such a large number of voids tends to block the exchange interaction between the magnetic particles. That is, it is difficult to say that Patent Document 1 can realize a nanocomposite magnet with sufficiently enhanced magnetic properties.

Further, in Patent Document 1, optimization of the particle diameter of the hard magnetic particles and the distance between the hard magnetic particles in the state of the nanocomposite magnet in which the above-described magnetic particles are densified is not sufficiently performed. From this point of view as well, it is difficult to say that Patent Document 1 can realize a nanocomposite magnet with sufficiently enhanced magnetic properties.

As described above, in the conventional nanocomposite magnet, at present, the residual magnetic flux density and the coercive force are lowered due to the blocking of exchange coupling and the dispersion of the magnetic anisotropy, and sufficient magnet performance is not achieved at present.

The present invention has been made in view of the above problems, and provides a composite magnetic material having excellent magnetic properties, a magnet including the material, a motor using the magnet, and a method of manufacturing the composite magnetic material. With the goal.

In the composite magnetic material according to one aspect of the present invention, a plurality of hard magnetic particles are dispersed in the form of islands in the soft magnetic phase, and the hard magnetic particles have an average particle diameter of 2 nm or more and 2 adjacent The average distance between the two hard magnetic particles is 100 nm or less.

The composite magnetic material according to another aspect of the present invention is characterized in that a plurality of hard magnetic particles are dispersed in the form of islands in the soft magnetic phase, and the soft magnetic phase is a continuous body.

According to the present invention, a composite magnetic material excellent in magnetic properties can be obtained. Moreover, if the magnetic material is used, it is possible to obtain a magnet which is lightweight and has excellent magnetic characteristics. And, by using such a magnet, it is possible to obtain a lightweight motor with a short start-up time and low power consumption.

The schematic diagram which shows the structure of the composite magnetic material in connection with embodiment of this invention. The schematic diagram which shows the structure and magnetization state at the time of using a ferrimagnetic body for hard magnetic particle. The figure which shows MH loop of the composite magnetic material in connection with embodiment of this invention. The figure which shows the magnetization state of the composite magnetic material in connection with embodiment of this invention. The figure which plotted the particle size of the hard magnetic particle in connection with embodiment of this invention, and the optimal value of interparticle distance by making the volume fraction of hard magnetic particle a parameter. The schematic diagram which shows the crystal orientation in embodiment of this invention. The schematic diagram which shows the crystal orientation in a comparative example. FIG. 6 is a graph showing the relationship between the volume fraction of the hard magnetic particles, the residual magnetic flux density Br, and the coercive force Hc according to the embodiment of the present invention. The figure which shows the relationship of the volume fraction of the hard magnetic particle and the maximum energy product which concern on embodiment of this invention. The figure which shows the relationship of the volume fraction and specific gravity (density) of the hard magnetic particle in connection with embodiment of this invention. The figure which shows the relationship between a weight and the maximum energy product about the magnet of embodiment of this invention, and a comparative example. FIG. 5 shows the relationship between weight and maximum energy product for a conventional magnet including embodiments of the present invention and a comparative example. The figure which shows MH loop of the composite magnetic material in connection with a comparative example. The figure which shows the magnetization state of the composite magnetic material in connection with a comparative example. Typical sectional drawing which looked at an example of a structure of the moving part (rotor) using the magnet of this invention from the rotating shaft direction. FIG. 9B is a schematic cross-sectional view of the moving unit (rotor) shown in FIG. 9A viewed from the direction orthogonal to the rotation axis. Typical sectional drawing which shows an example of a structure of the motor which has a moving part (rotor) using the magnet of this invention. The figure which shows the time response of the rotation speed of a motor when it drives by a predetermined | prescribed procedure. The figure which shows the time response of the rotation speed of a motor when it drives by another procedure. The figure which shows the time response of the rotation speed of a motor when it drives by another procedure. FIG. 6 is a view showing time dependency of rotation speeds in Example 1 and Comparative Example 1; FIG. 6 is a diagram showing time dependency of current consumption in Example 1 and Comparative Example 1. The figure which shows the reduction rate of motor weight with respect to the ratio of magnet weight.

The composite magnetic material of the present invention is a composite magnetic material in which a plurality of hard magnetic particles are dispersed in the form of islands in the soft magnetic phase. The hard magnetic particles as one aspect of the present invention have an average particle diameter of 2 nm or more and exist in the soft magnetic phase at an average interparticle distance of 100 nm or less. The definition of the size of the hard magnetic particles and the distance between the islands can be performed, for example, by deriving an optimum value from simulation results. In the composite magnetic material according to another aspect of the present invention, the soft magnetic phase is a continuum. In this composite magnetic material, it is preferable that substantially no nonmagnetic material such as silica or a portion blocking magnetic coupling such as an air gap exists between islands. Also, in the soft magnetic phase in which the variation of the magnetization easy axis has been suppressed, a plurality of hard magnetic particles are dispersed in the form of islands, and the magnetization easy axis of the hard magnetic particles is also easy to magnetize the soft magnetic phase It is preferred to be oriented with the axis. The fact that it is a continuum means, for example, that the cross section of the composite magnetic material is observed with an electron microscope to suppress nonmagnetic materials, voids and the like, and the soft magnetic phase becomes continuous between at least two adjacent hard magnetic particles. Can be verified by confirming that Here, between two adjacent hard magnetic particles refers to the space between another hard magnetic particle present closest to one hard magnetic particle.

Hereinafter, embodiments of the present invention will be described using the drawings. The present invention is not limited to the following embodiments, and various modifications, improvements, etc. can be made to the following embodiments based on the ordinary knowledge of those skilled in the art without departing from the spirit of the present invention. What was done is also included in the scope of the present invention.
In the present specification, the magnet includes a so-called permanent magnet which contains a magnetic material and generates a magnetic field without applying energy from the outside such as a current. On the other hand, in the present specification, the electromagnet is treated as one that generates a magnetic field by applying a current to a coil.

First Embodiment
(Structure of composite magnetic material)
The composite magnetic material according to the present embodiment is fine in which two phases of a soft magnetic material phase (soft magnetic phase) and a hard magnetic material phase (hard magnetic particles) are adjacent to each other on the order of nm (nanometer). It has a mixed structure. By having such a fine mixed structure, it is possible to exert an exchange coupling action between the soft magnetic phase and the hard magnetic particles. When the exchange coupling action is acting between the soft magnetic phase and the hard magnetic particles, the magnetization reversal of the soft magnetic phase is suppressed by the magnetization of the exchange-coupled hard magnetic particles when a reverse magnetic field is applied. At this time, the magnetization curve behaves as if it were a single-phase magnet as if it were a soft magnetic phase and hard magnetic particles due to the exchange coupling action. Therefore, a magnetization curve having a large saturation magnetic flux density of the soft magnetic phase and a large coercive force of the hard magnetic particles is realized. As a result, a high energy product BHmax can be realized. A magnet which exerts an exchange coupling action between the soft magnetic phase and the hard magnetic phase as described above is known as a nanocomposite magnet or a replacement spring magnet.

FIG. 1 is a schematic view showing a structural example of a composite magnetic material according to the present embodiment. The composite magnetic material 1 has a sea-island structure in which a plurality of hard magnetic particles 3 are dispersed like islands in the soft magnetic phase 2. The soft magnetic phase of the composite magnetic material of the present embodiment is characterized in that it is not particulate but continuous. For this reason, a void does not occur in principle in the soft magnetic phase. As a result, there is substantially no part where the exchange coupling force between the soft magnetic phase and the hard magnetic particles is interrupted. In addition, since the plurality of hard magnetic particles are surrounded by the continuous soft magnetic phase, the exchange coupling between the soft magnetic phase and the hard magnetic particles effectively acts. The exchange coupling force between the hard magnetic particles via the soft magnetic phase also works effectively. Furthermore, since the soft magnetic phase is a continuum, the structure is such that the axis of easy magnetization can be uniformly taken in the same direction. Therefore, the magnetization is easily oriented in one direction. Note that the description of one direction or the same direction indicates that the easy magnetization axis is not separated but is at an angle within a specific range, and all the easy magnetization axes are in the same direction. It is not a thing.

Therefore, the ratio (square ratio) of the residual magnetization to the saturation magnetization in the residual magnetic flux density and the coercivity of the composite magnetic material 1 and the MH loop (M is magnetization, H is an external magnetic field) can be made high. Here, the residual magnetization is magnetization when the magnetic field is zero, and the saturation magnetization is magnetization saturated by applying a sufficient external magnetic field. For example, the squareness ratio can be 0.7 or more. Thus, a high maximum energy product BHmax can be obtained when producing a magnet.

In addition, a void may be generated partially in the soft magnetic phase or between the soft magnetic phase and the hard magnetic particles due to manufacturing variations at the time of production. However, the air gaps in the composite magnetic material 1 need to be suppressed to such an extent that the performance is not degraded. Specifically, the volume fraction of voids with respect to the total volume of the composite magnetic material is preferably 20% or less, more preferably 10% or less, and still more preferably 5% or less. In this way, the aforementioned exchange coupling can be achieved sufficiently effectively.

In addition, the composite magnetic material may partially include a nonmagnetic material that is neither a soft magnetic material nor a hard magnetic material. However, in this case, the content of the nonmagnetic material needs to be suppressed to such an extent that the performance is not degraded. Specifically, the volume fraction of the nonmagnetic material relative to the total volume of the composite magnetic material is preferably 10% or less, more preferably 5% or less, and still more preferably 2% or less. Examples of nonmagnetic materials include alloys containing iron group elements (Fe, Co, Ni) or materials other than oxides, and typically have oxides such as SiO _2, and magnetic properties such as Cu, Si, Al, etc. Metals, organic substances (such as resin materials), etc.

In the above, an example of a sea-island structure in which the soft magnetic phase of the continuum is the sea and the hard magnetic material is the island of particle shape has been described, but the hard magnetic material is the sea and the soft magnetic material is the island in particle shape It may be a sea-island structure.

(Exchange coupling)
FIG. 2 shows how the hard magnetic particles 3a and the hard magnetic particles 3b are exchange-coupled through the soft magnetic phase 2 in the composite magnetic material 1 of the present embodiment. The arrows indicate the respective magnetization directions, and the hard magnetic particles 3a and the hard magnetic particles 3b indicate the magnetization directions of the difference among the magnetizations directed antiparallel to the ferrimagnetic material. As shown in FIG. 2, since the soft magnetic phase 2 has the hard magnetic particles 3 with high coercivity around the periphery, the exchange coupling force with the hard magnetic particles increases the magnetic field required for reversal, and the soft magnetic phase and the hard magnetic The particles reverse at the same time in high magnetic fields.

FIG. 3A shows the MH loop of the composite magnetic material of this embodiment. FIG. 3B shows the structure and magnetization state of the composite magnetic material of the present embodiment in an external magnetic field of zero magnetic field. The magnetization in the zero magnetic field, that is, the remanent magnetization Mr, is such that the magnetization directions of the hard magnetic particles 3 and the soft magnetic phase 2 are aligned in one direction, and show substantially the same value as at saturation, and the squareness ratio is approximately one.

(Hard magnetic particles)
The hard magnetic particles of the present embodiment include a hard magnetic material that is a magnetic material having high coercivity. Specifically, it is preferable to include a magnetic material containing a ferrimagnetic substance or an antiferromagnetic substance as a main component. In the present specification, “mainly contained” means containing at least 50% by mass. Although these materials have high coercivity, their magnetization tends to be small. In addition, materials having high magnetocrystalline anisotropy are mentioned as candidates. As the hard magnetic material, a material having a coercive force of 500 Oe or more is preferable, and a material having 1 kOe or more is more preferable. Moreover, the material which is 5 kOe or more is further preferable, and the material which is 10 kOe or more is particularly preferable. As the hard magnetic material, a magnetic material containing at least one element selected from the group consisting of Fe, Co, Mn, and Ni is preferably used, and it is more preferable to use a magnetic material containing Fe. The hard magnetic material preferably contains substantially no rare earth element such as Nd, and the content of the Nd element is preferably 3% by mass or less.

For example, as the ferrimagnetic material, iron oxides such as ε-Fe ₂ O ₃ , γ-Fe ₂ O ₃ , Fe ₃ O ₄ , and ferrite magnetic materials are used. Among iron oxides, ε-Fe ₂ O ₃ is more desirable because it has a particularly high coercivity at room temperature. Note that part of Fe atoms in ε-Fe ₂ O ₃ may be substituted with another metal element. In particular, part of Fe atoms in ε-Fe ₂ O ₃ may be substituted by at least one element selected from the group consisting of Co, Ni, Al, and Ga. The ferrite magnetic material is, for example, hexagonal ferrite AFe ₁₂ O ₁₉ . Here, A is an element containing, for example, at least one of Ba, Sr, and Pb. Or spinel ferrite BFe ₂ O ₄ . Here, B is an element containing, for example, at least one of Mn, Co, Ni, Cu, and Zn.

The hard magnetic particles may be a magnetic material whose magnetization is smaller than that of the soft magnetic phase and whose magnetization is zero such as an antiferromagnetic material. Examples of the antiferromagnet include NiO, FeMn, MnO, CoO and the like, and NiO having a Neel temperature of room temperature or more is desirable. However, the total magnetization of the composite magnetic material is the sum of the products of the respective magnetizations of the hard magnetic particles and the soft magnetic phase and the respective volume fractions. Therefore, it is preferable to use a ferrimagnetic material, and when hard magnetic particles having a small magnetization are used, the volume fraction thereof is preferably as small as possible to obtain a sufficient coercive force.

(Size and distance of hard magnetic particles)
The particle diameter of the hard magnetic particles is made large to such an extent that the coercivity does not decrease, and made small to such an extent that the magnetization can be maintained. Specifically, the average particle diameter of the hard magnetic particles is preferably 2 nm or more, more preferably 5 nm or more, and still more preferably 10 nm or more. The reason for setting the thickness to 5 nm or more is that the coercive force of the hard magnetic particles starts to fall rapidly as the particle diameter decreases from around 5 nm. The reason why the thickness is 2 nm or more is that this is the limit for maintaining the magnetization. The upper limit of the average particle diameter of the hard magnetic particles is not particularly limited, but is preferably 1000 nm or less, more preferably 500 nm or less, still more preferably 300 nm or less, and 200 nm or less Furthermore, it is preferable. In particular, 150 nm or less is preferable.

The width of the soft magnetic phase, that is, the distance between two adjacent hard magnetic particles is preferably 2 nm or more on average. The soft magnetic material and the hard magnetic material are preferably magnetically coupled by the exchange coupling action. Therefore, assuming that the distance at which the exchange coupling action works from the interface between the island and the sea (hereinafter referred to as "exchange coupling distance") is a, in composite magnetic material 1, the average distance d between two adjacent islands It is preferable that d satisfies d ≦ 2a. That is, the average distance between two adjacent islands is preferably not more than twice the exchange coupling distance. Specifically, it is preferably 100 nm or less, more preferably 70 nm or less, still more preferably 50 nm or less, and particularly preferably 30 nm or less.

In FIG. 4, the optimum value of the particle diameter of the hard magnetic particles and the interparticle distance of the hard magnetic particles is taken as a parameter of the volume fraction of the hard magnetic particles (hard magnetic particles / (hard magnetic particles and soft magnetic phase)). The figure which plotted is shown. According to FIG. 4, it is desirable to set the particle diameter and interparticle distance of the hard magnetic particles in accordance with the volume fraction of the hard magnetic particles.

The average particle diameter and the average interparticle distance of the hard magnetic particles can be obtained from an electron microscope image of a cross section of the composite magnetic material. Specifically, for example, an electron microscope image (electron micrograph) of the cross section of the composite magnetic material is obtained using a scanning electron microscope (SEM), and the average of the hard magnetic particles is obtained by image processing based on the image. The particle size and the average interparticle distance may be measured. In this case, it is preferable to obtain an electron microscope image by adjusting the magnification so that at least 10, preferably several tens to several hundreds of hard magnetic particles are present in one electron microscope image. The above measurement may be performed for a plurality of fields of view to calculate the average particle diameter and the average interparticle distance, but if a statistically sufficient amount of particles appear in one field of view, the average particle size in one field of view The diameter and the average interparticle distance may be calculated.

As described above, if the particle diameter and interparticle distance of the hard magnetic particles satisfy the preferable conditions, the requirement that the soft magnetic phase is a continuum may be relaxed to some extent. That is, the present invention can be achieved as long as sufficient exchange coupling action is achieved between the soft magnetic phase and the hard magnetic particles and between two adjacent hard magnetic particles, even if some gaps etc. exist in the soft magnetic phase. In some cases, it is suitable as a composite magnetic material of On the contrary, if the soft magnetic phase is sufficiently continuous, the requirements of the particle diameter and interparticle distance of the hard magnetic particles may be relaxed to some extent. That is, even if the inter-particle distance of the hard magnetic particles is somewhat large, there are cases where it is suitable as the composite magnetic material of the present invention as long as sufficient exchange coupling action is achieved when the portion that blocks exchange coupling is sufficiently small.

(Soft magnetic phase)
The soft magnetic material is a material having a larger saturation magnetic flux density (saturation magnetization) than the hard magnetic material. The soft magnetic phase preferably contains a ferromagnet as a main component. The ferromagnet has a large saturation magnetization because there is no part where the magnetization is antiparallel inside the magnetic material. The soft magnetic phase particularly preferably contains α-Fe as a main component, but is not limited thereto. The soft magnetic material is preferably a material having a magnetization of 50 emu / g or more, more preferably a material having 100 emu / g or more, and still more preferably a material having 150 emu / g or more.

Specifically, the soft magnetic material preferably contains a single metal of Fe or Co, or an alloy or nitride containing Fe or Co, and more preferably contains a single metal of Fe or an FeM alloy. Here, M represents at least one element selected from the group consisting of Co, Ni, Al, Ga, and Si, and the composition ratio of each element in the FeM alloy can be arbitrarily selected. Among them, the soft magnetic material more preferably contains α-Fe (α iron), and particularly preferably consists of α-Fe alone. The soft magnetic material may not necessarily have crystallinity. The single metal of Fe may be iron other than α-type. Iron (Fe) changes into three forms depending on temperature, α-Fe (α iron), γ-Fe (γ iron), and δ-Fe (δ iron). Among them, α-Fe (α-iron) exhibits magnetization at room temperature, so α-Fe (α-iron) is preferably used. Further, since iron nitride has a large magnetization, a magnetic material containing iron nitride as a main component may be used as the soft magnetic material. The soft magnetic material preferably contains substantially no rare earth element such as Nd, and the content of the Nd element is preferably 3% by mass or less.

(Crystal orientation)
In the composite magnetic material of the present embodiment, it is desirable that the magnetization easy axis of the hard magnetic particles be oriented in one direction among the plurality of hard magnetic particles. Thereby, the magnetizations of the hard magnetic particles in the composite magnetic material can be aligned in one direction, and the coercive force of the composite magnetic material as a whole can be further increased. As a result, the ratio (square ratio) of the saturation magnetization to the remanent magnetization of the MH loop can be increased, and a magnet using this composite magnetic material can have a high maximum energy product. It is desirable that the magnetization easy axes of the hard magnetic particles be aligned in one direction among the plurality of hard magnetic particles, but they may be aligned to some extent even if they are not completely aligned. Specifically, the angle between the direction of the magnetization easy axis of the hard magnetic particles and the predetermined one direction is preferably 15 degrees or less for all of the plurality of hard magnetic particles, and is 10 degrees or less Is more preferable, and is more preferably 5 degrees or less. In other words, the variation in the direction of the magnetization easy axis of the plurality of hard magnetic particles in the composite magnetic material is preferably within the range of 15 degrees or less. The region in which the magnetization easy axis of the hard magnetic particles is oriented in one direction among the plurality of hard magnetic particles is preferably 70% or more by volume ratio with respect to the entire composite magnetic material. In addition, this volume ratio can be acquired from the electron microscope image of the cross section of a composite magnetic material similarly to the measurement of the average particle diameter of hard magnetic particle, and the distance between average particles.

Moreover, in the composite magnetic material of the present embodiment, it is desirable that the magnetization easy axis of the soft magnetic phase also forms the sea and is oriented in one direction over a wide range surrounding a plurality of hard magnetic particles. It is particularly desirable to be oriented in one direction. Thereby, the magnetization of the soft magnetic material constituting the soft magnetic phase in the composite magnetic material can be aligned in one direction, and the saturation magnetic flux density (saturation magnetization) of the composite magnetic material as a whole can be further increased.

The orientation of the magnetization easy axis of the soft magnetic phase is also preferably aligned in one direction as in the case of the hard magnetic particles, but it may be aligned to some extent even if it is not completely aligned. Specifically, the angle between the direction of the magnetization easy axis of the soft magnetic phase and the predetermined one direction is preferably 15 degrees or less in the soft magnetic phase within the range including the plurality of hard magnetic particles, and 10 degrees It is more preferable that it is the following, and it is more preferable that it is 5 degrees or less. In other words, the variation in the direction of the magnetization easy axis of the soft magnetic phase is preferably within the range of 15 degrees or less. The orientation of the magnetization easy axis of the soft magnetic phase is preferably unidirectional in at least the entire soft magnetic phase existing between two adjacent hard magnetic particles. The region in which the magnetization easy axis of the soft magnetic phase is oriented in one direction is preferably 70% or more by volume ratio with respect to the entire composite magnetic material. In addition, this volume ratio can be acquired from the electron microscope image of the cross section of a composite magnetic material similarly to the measurement of the average particle diameter of hard magnetic particle, and the distance between average particles.

In the composite magnetic material of the present embodiment, the direction of the magnetization easy axis of the soft magnetic phase is preferably aligned with the direction of the magnetization easy axis of the hard magnetic particles. The magnetization easy axes of the two are preferably aligned in one direction, but as described above, it may be aligned to some extent. Specifically, the variation in the direction of the magnetization easy axis of the soft magnetic phase and the hard magnetic particles is preferably within the range of 15 degrees or less. Further, the region in which the magnetization easy axis of the soft magnetic phase and the hard magnetic particles is oriented in one direction is more preferably 70% or more by volume ratio with respect to the entire composite magnetic material. In addition, this volume ratio can be acquired from the electron microscope image of the cross section of a composite magnetic material similarly to the measurement of the average particle diameter of hard magnetic particle, and the distance between average particles.

FIGS. 5A and 5B schematically show the crystal structure and crystal orientation of at least one of the hard magnetic particles and the soft magnetic phase of the composite magnetic material of the present embodiment. Here, the square shown in FIGS. 5A and 5B shows the crystal structure in the case of using a body-centered cubic lattice of α-Fe as the soft magnetic phase, and the arrow shows the magnetization direction. As shown in FIG. 5A, when the crystal orientations are aligned, the soft magnetic phase can mediate the exchange force exerted from the hard magnetic particles, and it becomes easy for the hard magnetic particles to exchange-bond with each other. On the other hand, as shown in FIG. 5B, in the case where the crystal orientations are not aligned and are randomly arranged, it is difficult to exchange-bond hard magnetic particles through the soft magnetic phase, which is not suitable.

An example of the crystal structure in the case of using ε-Fe ₂ O ₃ as hard magnetic particles is shown below. ε-Fe ₂ O ₃ has a crystal structure of a cuboidal system (Pna 21), and the lattice constant is approximately a = 5.1 angstroms, b = 8.7 angstroms, c = 9.4 angstroms is there. In this rectangular crystal structure, the c axis is the easy magnetization axis. It is desirable that the crystal direction in the c-axis direction be aligned in one direction by applying an external magnetic field or the like at the time of production of the composite magnetic material. When α-Fe is used as the soft magnetic phase, α-Fe is a crystal structure of a body-centered cubic lattice, and its easy axis of magnetization is the a-axis, b-axis or c-axis, and these should be aligned in one direction desirable. Furthermore, in order to mediate the exchange force that the soft magnetic phase works from the hard magnetic particles, it is desirable to align the easy magnetization axes of the hard magnetic particles and the soft magnetic phase. Therefore, it is desirable that the c-axis of ε-Fe ₂ O ₃ and any one of the a-axis, b-axis, and c-axis of α-Fe be aligned in one direction.

Crystal orientation can be confirmed directly by transmission electron microscopy (TEM). Further, as a substitute method of TEM, estimation may be made from squareness ratio etc. obtained in the magnetization loop.

The soft magnetic phase and the hard magnetic particles may either be in an amorphous state or in a crystalline state, but are preferably in a crystalline state. Since the soft magnetic phase and the hard magnetic particles are crystals themselves, the saturation magnetization of the composite magnetic material can be increased, and the direction of the magnetization easy axis can be easily aligned. Even when the soft magnetic phase and the hard magnetic particles are in an amorphous state, the magnetization easy axes of the soft magnetic phase and the hard magnetic particles are preferably oriented in one direction.

(Volume fraction and characteristics)
The composite magnetic material of the present invention is a mixture of hard magnetic particles and a soft magnetic phase, but the magnetic properties of the composite magnetic material depend on the mixing ratio of the hard magnetic particles and the soft magnetic phase, and the mixing ratio There is an optimal range for The optimum range was calculated as follows.

First, using the magnetization Mh of the composite magnetic material, the magnetization Mh of the hard magnetic particles, the magnetization Ms of the soft magnetic phase, the volume fraction Vh of the hard magnetic particles, and the volume fraction Vs of the soft magnetic phase, Is represented by
Mt = Vh · Mh + Vs · Ms Formula (1)
Further, the anisotropic energy Kt of the composite magnetic material is the anisotropic energy Kh of the hard magnetic particles, the anisotropic energy Ks of the soft magnetic phase, the volume fraction Vh of the hard magnetic particles, the volume fraction Vs of the soft magnetic phase It is represented by following formula (2) using.
Kt = Vh · Kh + Vs · Ks Formula (2)
Furthermore, the coercive force Hc of the composite magnetic material is expressed by the following formula (3).
Hc = 2 · Mt / Kt equation (3)
In the SI unit system, the magnetic flux density B (T) is represented by the following formula (4) using the magnetic field H (A / m) and the magnetization M (A / m). Here, in the following formula (4), μ _o is the permeability of vacuum. B = μ _o (H + M) Formula (4)
Substituting I = μ _o M in the equation (4), the following equation (5) is obtained, and I becomes the same unit (T) as the magnetic flux density.
B = μ _o H + I equation (5)

6A and 6B are diagrams showing the relationship between the mixing ratio of hard magnetic particles and soft magnetic phase, and the residual magnetic flux density Br and the coercive force Hc of the composite magnetic material and the maximum energy product BHmax in the composite magnetic material according to the present embodiment. It is. 6A and 6B, the horizontal axis indicates the volume fraction Vh / (Vs + Vh) of the hard magnetic particles, which is the mixing ratio of the hard magnetic material and the soft magnetic phase. Here, Vs represents the volume of the soft magnetic phase, and Vh represents the volume of the hard magnetic particles. In FIG. 6A, the vertical axis represents the residual magnetic flux density Br and the coercivity Hc, and in FIG. 6B, the vertical axis represents the maximum energy product BHmax.

FIGS. 6A and 6B are based on the calculation results of the hard magnetic material constituting the hard magnetic particles as ε-Fe ₂ O ₃ and the soft magnetic material constituting the soft magnetic phase as α-Fe. Here, the saturation magnetization of the hard magnetic particles is 0.1 T, the anisotropy energy is 0.77 MJ / m ³ , the saturation magnetization of the soft magnetic material is 2.15 T, and the anisotropy energy is 0.05 MJ / m ³ . I did the calculation. FIG. 6A illustrates the dependence of the residual magnetic flux density and the coercive force on the volume fraction of the hard magnetic particles using these values and the equations (1) to (5). Further, FIG. 6B shows the maximum energy product BHmax based on the result of FIG. 6A.

The maximum energy product BHmax is a characteristic that indicates the performance of the magnet when the magnet is used as a motor or the like. Magnetization Mt when the external magnetic field is 0, that is, the residual magnetization and Mr, if the coercive force Hc is greater than Mr / 2 is a BHmax μ _o Mr ^2/4, if the coercive force Hc Mr / 2 less than , BHmax was calculated as μ _o MrHc / 2.

It can be understood from FIG. 6B that when the mixing ratio of the hard magnetic particles and the soft magnetic phase is changed, the maximum energy product BHmax of the composite magnetic material shows a maximum at a predetermined mixing ratio, here 0.4. The In the case of FIG. 6B, in order to set BHmax to 170 kJ / m ³ or more, the volume fraction of the hard magnetic particles is set to 0.2 or more and 0.6 or less, and to set BHmax to 250 kJ / m ³ or more. It is understood that the volume fraction of the hard magnetic particles is preferably 0.3 or more and 0.5 or less.

The above is the case of a sintered magnet manufactured by sintering the composite magnetic material, but the specific gravity of the bonded magnet manufactured by mixing the magnetic material with the resin is lower than that of the sintered magnet. For example, the specific gravity of a neodymium bonded magnet is about 1/4 to 1/8 of that of a neodymium sintered magnet. The specific gravity of the bonded magnet depends on the selection of the resin material and the molding method. When using the composite magnetic material adjusted so that the BHmax of the sintered magnet of the present invention is 170 kJ / m ³ , in the bonded magnet, when the specific gravity decreases to 1/4, 1/6, and 1/8, the BHmax is respectively 43, 28, 21 kJ / m ³ . If BHmax of the sintered magnet of the present invention is 250 kJ / ^{m 3,} in the bonded magnet, the specific gravity is reduced to 1 / 4,1 / 6,1 / 8, respectively BHmax the 63,42,31kJ / ^{m 3} Become. Therefore, the maximum energy product BHmax of the bonded magnet of the present invention is preferably 21 kJ / m ³ or more, 31 kJ / m ³ or more, and more preferably 42 kJ / m ³ or more.

Similar to FIGS. 6A and 6B, FIG. 6C shows the specific gravity of the composite magnetic material of the present embodiment on the vertical axis, with the volume fraction of hard magnetic particles on the horizontal axis. In the composite magnetic material of the present embodiment, the maximum energy is the largest when the volume fraction of hard magnetic particles is around 0.4, but the specific gravity of the composite magnetic material at this time is about 6.7 g / cm ³ ( Hereinafter, for the sake of convenience, the unit of density, which is essentially dimensionless, is described with g / cm ³ which is a unit of density). The specific gravity of the NdFeB magnet is about 7.6 g / cm ³ , and the specific gravity of the SmCo magnet is about 8.4 g / cm ³ . Since the specific gravity of the magnet of the present invention is about 6.7 g / cm ³ when the volume fraction of hard magnetic particles is 0.4 in the representative example, the weight reduction by about 12% as compared with the NdFeB magnet, SmCo It is 20% lighter than a magnet.

When a magnetic material is mixed with a resin to produce a bonded magnet, the specific gravity of the resin is generally lower than that of the magnetic material, so the specific gravity of the bonded magnet is lower than that of a sintered magnet in which the magnetic material is solidified. . Roughly speaking, when the specific gravity of the bond magnet is ρb, the volume ratio of the magnetic material is Vm, the specific gravity of the magnetic material in a sintered state is ρm, and the specific gravity of the resin is pp, equation (6) is obtained.
b b = V m × m m + (1-V m) × (b Equation (6)
For example, a composite magnetic material of ρm is the invention of 6.7 g / cm ^3, .rho.p is a resin of ^{1g / cm 3, Vm = 0.7} ( volume ratio 7: 3) prepared by mixing with, Bond The specific gravity bb of the magnet is 5 g / cm ³ .

The above is the case where the volume fraction of the hard magnetic material is 0.4, but in the case of 0.6, the specific gravity mm of the sintered magnet is 6.1 g / cm ³ . When producing a bonded magnet, Vm is changed in the range of 0.5 to 0.8 depending on the resin material, the molding method and the use application. When the volume fraction Vh of the hard magnetic material is 0.6 and Vm in the equation (6) is 0.5, 0.7, 0.8, the specific gravity of the bonded magnet is 3.6, 4.6, 5 respectively. It will be .1 g / cm ³ . When the volume fraction Vh of the hard magnetic material is 0.4 and Vm in the equation (6) is 0.5, 0.7, 0.8, the specific gravity of the bonded magnet is 3.9, 5.0, 5 respectively. It will be .6 g / cm ³ . When the volume fraction Vh of the hard magnetic material is 0.2 and Vm of the equation (6) is 0.5, 0.7, 0.8, the specific gravity of the bonded magnet is 4.1, 5.4, 6 respectively It will be .0 g / cm ³ . The typical performance of the magnet is the maximum energy product and specific gravity. In the example of FIG. 6B, the volume ratio of the hard magnetic material is approximately the same as the maximum energy product at 0.3 and 0.5, but the specific gravity is 0.5 Is small.
In view of the above points, the specific gravity of the bonded magnet of the present invention is desirably 5 g / cm ³ or less.

(Magnetic powder resin mixture)
What mixed magnetic powder containing the composite magnetic material of this embodiment with a binder (binder) (hereinafter, referred to as a magnetic powder-resin mixture) can be used when producing a bonded magnet. As the binder, resin materials such as thermoplastic resin and thermosetting resin, or low melting metals such as Al, Pb, Sn, Zn, Mg, or alloys containing these low melting metals can be used. . The thermoplastic resin is made of nylon, polyethylene or EVA (ethylene-vinyl acetate copolymer) and the like, and the thermosetting resin contains epoxy resin, melamine resin, phenol resin and the like. These magnetic powder-resin mixtures are in the form of pellets, and a magnet can be made by a molding machine.

(magnet)
The composite magnetic material according to the present embodiment can be formed into a desired shape to be a nanocomposite magnet. The nanocomposite magnet according to the present embodiment contains the above-described composite magnetic material. The nanocomposite magnet according to the present embodiment may be a sintered magnet or a bonded magnet as described below.

[1] Sintered Magnet A sintered magnet can be obtained by forming the composite magnetic material according to the present embodiment into a desired shape, and heat treating the resulting molded body in an inert atmosphere or under vacuum. A sintered magnet can also be obtained by sintering a compact by plasma activated sintering (PAS) or spark plasma sintering (SPS). Also, by molding in a magnetic field, an anisotropic sintered magnet can be obtained.

[2] Bonded magnet The desired magnetization of a molded product obtained by forming the magnetic powder-resin mixture into a desired shape by injection molding, compression molding or extrusion using a molding die in the same manner as known plastic molding etc. A bonded magnet is obtained by magnetizing the pattern. The magnetization pattern may be simultaneously magnetized at the time of molding. Also, by molding the composite magnetic material in a magnetic field, an anisotropic bonded magnet can be obtained.

(Magnetic characteristics)
When using a magnetic material for the magnet, preferably a maximum energy product is 170kJ / ^{m 3} or more, more preferably 200 kJ / ^{m 3} or more, and still more preferably 250 kJ / ^{m 3} or more. From FIG. 6B, in the present embodiment, the volume fraction of the hard magnetic material is preferably 0.18 or more and 0.60 or less, and more preferably 0.30 or more and 0.50 or less.

(Magnet weight reduction)
FIG. 7A is a view showing the relationship between the weight of the magnet and the maximum energy BHE regarding the magnet example according to the present embodiment and the neodymium bonded magnet as the comparative example. The maximum energy BHE is a value defined such that the unit is energy by multiplying the maximum energy product BHmax by the volume of the magnet. The magnet according to the present embodiment is formed by mixing the resin into the composite magnetic material according to the present embodiment so that the volume ratio is composite magnetic material: resin = 7: 3 (weight ratio 94: 6). Make Also, neodymium bonded magnets are produced by mixing resin with neodymium magnetic powder at the same weight ratio. For comparison, the maximum energy product BHmax is 70 kJ / m ³ in any of the magnets. As can be seen from FIG. 7A, according to the present embodiment, the weight can be reduced by about 12% with respect to the neodymium bonded magnet with the same performance (same BHE).

FIG. 7B is a combination of the ferrite sintered magnet and the ferrite bond magnet in the two examples shown in FIG. 7A. Those ferrite sintered magnet maximum energy product BHmax of characteristics of 28kJ / ^{m 3,} a ferrite bond magnet is what BHmax of characteristics of 10 kJ / ^{m 3,} was used as a representative example of each magnet. From FIG. 7B, according to the present embodiment, it can be understood that the weight can be further reduced with the same performance (the same BHE) as compared to the ferrite magnet.

(motor)
When a magnet is employed for the motor, it is necessary to determine the maximum energy product in consideration of the permeance straight line in the magnet shape suitable for the motor. In some cases where the highest maximum energy product can be obtained without considering the magnet shape, the shape may be an elongated magnet. When the maximum energy product BHmax is the highest, the coercivity Hc is equal to Mr / 2, and the characteristic of the magnetic material is most effectively utilized for the magnetic characteristic. This state is the case where the maximum energy product BHmax in FIG. 6B is the highest and the volume fraction of the hard magnetic material is around 0.4.

When the composite magnetic material according to the present embodiment is sintered as magnetic powder and used as a magnet, high residual magnetization (residual magnetic flux density) and high coercivity can be obtained without using a rare earth element, and the maximum energy product BHmax is high. You can get a magnet. Furthermore, by using the magnet according to the present embodiment, a motor with low cost and high performance (for example, high torque) can be obtained. Further, as described above, since the weight of the magnet can be reduced while having the same performance as the neodymium bonded magnet, the weight of the motor can be reduced. In addition, in the motor in which the magnet is mounted on the rotating portion, the weight of the rotating portion is reduced, so that there is an advantage that power consumption can be reduced.

FIGS. 9A and 9B are diagrams showing an example of a moving part (rotor) provided with a magnet manufactured using the composite magnetic material of the present invention. The moving unit (rotor) 4 is configured such that the magnet 5 and the yoke 6 are connected to a shaft 7 which is a central axis, via a lid 8. FIG. 9A is a view as viewed from the top surface (rotational axis direction), and FIG. 9B is a view as viewed from a side surface (direction orthogonal to the rotation axis). FIG. 10 is a view showing an example of a motor using the moving unit (rotor) 4. The motor 9 includes an electromagnet 10 including a coil provided to the cover 11 and a moving unit (rotor) 4. The motor 9 detects the magnetic pole of the magnet 5 by a Hall IC (not shown), and causes the moving unit (rotor) 1 to rotate by causing a current to flow through the electromagnet 10 to generate a magnetic field according to the result.

The motor shown in FIG. 10 is a kind of what is called a brushless motor, and has a magnet in its rotating part. The brushless motor in which the rotating part is inside the electromagnet is an inner rotor type brushless motor, and the brushless motor in which the rotating part is outside the electromagnet is an outer rotor type brushless motor. The magnet of the present invention is also applicable to an outer rotor type brushless motor.

Moreover, although the rotor which is a part of motor as a moving part is described in this specification as an application example of a magnet, the magnet of this invention is not limited to a rotor. For the purpose of shortening the acceleration rotation period and reducing the power consumption due to the weight reduction, the moving unit may not be rotated, but may be, for example, moved to the left, right, up and down, or on the circumference. For example, the magnets on the electromagnets may be moved by arranging a plurality of electromagnets in a row and changing the direction of the current of the electromagnets.

Second Embodiment
11A to 11C show the time t response of the number of revolutions RPM of the motor. It is a drive sequence which controls the voltage and current of the coil of a motor so that it may become a response like FIG. 11A. The drive sequence is set to a sequencer that drives the motor. The form provided with such a sequencer and a motor is called a motor unit. The rotation speed increases with the start of driving and reaches the specified rotation speed Rp at the rise time (startup time) t1. The state of the rotation speed Rp is maintained for t2 and the rotation speed becomes zero at the fall time t3 and stops. . The rise time t1 or fall time t3, or rise time t1 and fall time t3 of the time from when the motor starts rotation until it stops (t1 + t2 + t3), or until the constant rotation speed is sustained (t1 + t2) It is desirable that the ratio of is small because the time taken to start and stop is short compared to the use time of the motor.

FIG. 11B is a case where the period t2 of holding the specified rotational speed Rp in FIG. 11A becomes zero and the start and stop are repeated. Further, FIG. 11C shows a case where, in addition to the period t2 for holding the specified rotational speed Rp being zero, after the rotational speed Rp of the forward rotation is reached, reverse rotation is performed to make the rotational speed −Rp. In the case of FIGS. 11B and 11C, it is desirable that the rising time t1 or the falling time t3, or the rising time t1 and the falling time t3 be short.

For example, in FIG. 11A, when t1 and t3 are the same, the ratio of the acceleration rotation period and the fall time in one cycle time (t1 + t2 + t3) is 2t1 / (t2 + 2t1). For example, in the case of t2 = 2t1, when t1 is 1⁄2, one cycle time is 1⁄2. In FIG. 11B, one cycle time (t1 + t3) is 2t1 when t1 and t3 are the same. For example, when t1 is 1/2, one cycle time is 1/4. In FIG. 11C, when one cycle time (2t1 + 2t3) is the same as t1 and t3, when t1 is 1⁄2, one cycle time is 1⁄8.

As described above, when using the motor of the present invention, the motor of the present invention is driven at a constant speed to rotate at a constant speed for a period of twice or less of a period for accelerating rotation, and further to start rotation to a constant rotation speed. In the case of stopping immediately after it has become, and further, in the case of repeating normal rotation and reverse rotation, the tact time can be shortened and the effect becomes remarkable.

As shown in FIG. 11C, in the case of using a manufacturing apparatus having a mechanical unit that operates repeatedly in forward and reverse rotations, if the number of rotations reaches a predetermined number of times in a predetermined time, the tact time of the manufacturing process becomes short and production It is possible to improve the quality. Therefore, a motor using the lightweight magnet of the present invention for the moving part (rotor) is useful. A crusher that crushes the material to be crushed with a bladed blade connected to a motor as a device having a mechanical unit that operates repeatedly in reverse rotation, and changes the rotation direction of the stirring rod when stirring the mixture For example, a stirring device to be carried out, an assembly device in which parts are rotated and attached in one direction and then assembled in the reverse direction, and the like, such as a device requiring high torque and short start and reverse time are exemplified.

Third Embodiment
The magnet of the present invention is effective in that the weight of the motor itself can be reduced even when provided in the fixed portion (stator portion) in addition to the moving portion (rotor portion) of the motor.

FIG. 13 shows the weight ratio of magnets in the motor and the weight reduction rate of the motor itself. The three lines in the figure show the ratio Rρ (%) of the specific gravity of the neodymium magnet of the comparative example to the magnet of the present invention, and the equation (6)
Rρ = (1-specific gravity of magnet of the present invention / specific gravity of neodymium magnet) × 100 Formula (6)
The value R 割合 of Equation 6 is calculated for each of the cases of 10%, 12%, and 14%. As shown in the example of FIG. 6C, these manufacture composite magnetic materials by setting the volume fraction of hard magnetic particles to 0.45, 0.40, 0.35, and the specific gravity of the magnet of the present invention is 6.8 g / cm. ³ , 6.7 g / cm ³ and 6.6 g / cm ³ . In the calculation, 7.6 g / cm ³ was used as the specific gravity of the neodymium magnet. The motor weight reduction rate comparing the motor using the neodymium magnet and the motor using the magnet of the present invention is preferably 1% or more, preferably 2% or more, and more preferably 4% or more. Therefore, from FIG. 13, the ratio of the magnet of the present invention in the motor is preferably about 8% or more, preferably about 15% or more, and more preferably about 20% or more.

In recent years, an airplane gear has been utilized as a device equipped with a plurality of motors for rotating a propeller. A typical example is an aeroplane called a drone, which mounts four to eight or more motors in order to rotate a propeller. There is a demand for using drone or drone as small and light as possible, to improve accessories by adding accessories such as cameras and batteries as much as possible, and to carry as heavy a thing as possible. For this reason, a motor as light as possible having characteristics (torque, rotational speed, etc.) necessary for propeller rotation for flight is required. The motor of the present invention is effective for this purpose.

As a configuration example of drone, 4 units of 65g motor, frame of 120g (including propeller), flight controller of 50g, camera of 10g, camera control unit of 30g, battery of 170g, total drone 640g It becomes. Here, when the weight reduction rate of the motor is 4%, the total weight is about 630 g. The entire drone will be about 10g lighter, so one more camera can be added.

As another configuration example of drone, when using one 65g motor, 8 frames of 120g (including propeller), 50g flight controller, 10g camera, 30g camera control unit, 170g battery, drone It is 900g in total. Here, when the weight reduction rate of the motor is 2%, the total weight is about 890 g. The entire drone is reduced in weight by about 10g, and another camera can be added. When the weight reduction rate of the motor is 4%, the total weight is about 880 g. The overall weight of the drone is reduced by about 20g, so two more cameras can be added.

Several comparative examples of the above embodiment will be described.
(Comparative example: particle size and distance between particles of hard magnetic particles / porosity)
In the technology described in Patent Document 1, the ε-Fe ₂ O ₃ particles are subjected to reduction treatment to form a shell containing Fe around them, thereby obtaining magnetic particles having the above-mentioned core-shell structure. In this method, it is formed a nanocomposite magnet by densifying the plurality of magnetic particles obtained, the distance between the ε-Fe ₂ O ₃ particles, the particle size reduction treatment before the ε-Fe ₂ O ₃ particles However, it is difficult to control the particle size of the hard magnetic particles and the distance between the hard magnetic particles. In addition, even if the particulate matter is densified, when contacting spherical particles, the contact area is close to zero and the exchange force is extremely small. It is known that if the powder, which is an aggregate of particles, is compressed, the contact surface is formed between the particles and the porosity is reduced, but in the case of nanoparticles having a particle diameter of several hundred nm or less, the particle diameter is small. Then, the bulk density of the powder becomes low, and it is difficult to reduce the porosity even if compressed. Therefore, even if the core-shell particles described in Patent Document 1 are densified, a structure in which a plurality of hard magnetic particles are dispersed in the soft magnetic phase of the continuous body can not be obtained as in the present embodiment. I will.

(Comparative example: MH loop)
FIG. 8A shows an MH loop showing the relationship between the magnetization M and the magnetic field H when the magnet is manufactured to have a core-shell structure as a comparative example. Moreover, FIG. 8B shows the structure and magnetization state of the magnet material 10 containing the core-shell type magnetic material 11 of the comparative example in a zero magnetic field. Here, the core-shell magnetic material 11 has a core 11 b containing a hard magnetic material and a shell 11 a containing a soft magnetic material. In this comparative example, the direction of magnetization of each core-shell structure tends to be randomly oriented in a zero magnetic field, so that the residual magnetization Mr becomes significantly smaller than the saturation magnetization, and the squareness ratio (ratio of residual magnetization to saturation magnetization) is small. Become.

(Method of manufacturing composite magnetic material)
Next, steps of a method of manufacturing the composite magnetic material according to the present embodiment will be described.
[1] Step of Uniformly Dispersing Hard Magnetic Particles in Solution This step is a step of uniformly dispersing hard magnetic particles in the state of a composite magnetic material. First, the hard magnetic particles are placed in an aqueous solution. In order to prevent aggregation of the hard magnetic particles and increase in particle size, glass beads are added and stirred by a planetary bead mill. As a result, the aggregation state is eliminated, and the particle size distribution is made close to the original particles (primary particles). Furthermore, it is filtered through a filter to remove large particle size and make the particle size uniform.

[2] A process of dispersing hard magnetic material particles in a solution containing ions containing a transition metal element (at least one transition metal element contained in a soft magnetic material) to obtain a dispersion liquid The hard magnetic particles are dispersed in a solution containing ions containing an element to prepare a dispersion. In the present embodiment, the soft magnetic material in the composite magnetic material contains a transition metal element, and in this step, a solution of ions containing the transition metal element is prepared. The transition metal element is preferably at least one selected from the group consisting of Fe, Co, Mn, and Ni as described above. As said solution, when the said transition metal element is Fe, aqueous solution, such as iron chloride (II), iron chloride (III), iron sulfate (III), iron nitrate (III), is used suitably, for example.

In this step, hard magnetic particles are dispersed in the above solution to obtain a dispersion. At this time, the ions may be contained in the aqueous solution in which the hard magnetic particles are dispersed in advance in the first step as described above, or the hard magnetic particles may be dispersed in the solution containing the ions as described above. You may

[3] The step of adding an additive to the dispersion to precipitate particles containing the transition metal element In this step, the additive is added to the dispersion to cause the ions to react and transition metal element. Precipitate particles or precipitates contained. In the above step [2], since the hard magnetic particles are dispersed in the dispersion, the ions are present around the hard magnetic particles in the dispersion so as to surround the hard magnetic particles. . Ions react in this state, and particles or precipitates containing transition metal elements in the ions precipitate, so that particles or precipitates precipitate in a form surrounding the hard magnetic particles. Thus, a mixture having a structure in which a plurality of hard magnetic particles are dispersed like islands in a precipitate group containing a transition metal element is obtained. At this time, by sufficiently dispersing the hard magnetic particles in the step [2], the dispersibility of the hard magnetic particles in the mixture can be enhanced, and the distance between the hard magnetic particles can be adjusted.

As the additive, it is preferable to use a reducing agent or a basic solution. By using a reducing agent as an additive, ions including a transition metal element can be reduced to reduce the valence of the transition metal element and precipitate. By properly selecting the reducing agent, it is possible to directly deposit a single metal or alloy containing a transition metal element. For example, by adding NaBH ₄ as a reducing agent to a dispersion in a state where hard magnetic particles (such as ε-Fe ₂ O ₃ ) are dispersed in an aqueous iron (II) chloride solution, iron chloride (II) can be added Can be reduced to iron to precipitate α-Fe fine particles around the hard magnetic particles.

In the precipitation of α-Fe fine particles, the particle size can be changed under the addition conditions of the reducing agent. For example, when the droplet size of the reducing agent to be added is reduced, the region which causes a reduction reaction can be miniaturized, and the α-Fe particles can be reduced in size. In addition, when adding a reducing agent, for example, when using an iron (II) chloride solution, the particle size can be changed even if the temperature is changed, and by increasing the solution temperature, the size of α-Fe particles can be increased. The particle size can be reduced. In the preparation of the composite magnetic material, either the reduction of the reducing agent or the increase in the temperature of the iron ion solution may be selected, or both may be selected simultaneously, and the size of the necessary α-Fe particles may be selected. It can be selected according to

In addition, in the precipitation of α-Fe fine particles, the particle size can also be changed by the solvent condition of the solution of the ion containing the transition metal element. For example, after dissolving iron (II) chloride not in water but in methanol as an organic solvent, the reduction in particle size of α-Fe particles can be achieved by adding a reducing agent. The reason why such micronization can be achieved is not clear, but it is believed that the micronization can be achieved because the organic solvent has the effect of reducing the surface energy of the α-Fe particles during precipitation. It has the effect of reducing the surface energy of α-Fe particles, that is, as an organic solvent having good wettability with α-Fe, for example, methanol, ethanol, 2-propanol, acetone, dimethyl sulfoxide, tetrahydrofuran, ethylene glycol, diethylene glycol Etc. One of these solvents may be selected, or may be mixed and used as needed. However, solvents such as acetone and dimethyl sulfoxide are not efficient because they have the property of being partially reduced by the reducing agent. In the case of using an organic solvent in the solvent of the solution of the transition metal element in the preparation of the composite magnetic material, it is preferable to use the organic solvent as the solvent for dissolving the hard magnetic particles and the solvent for dissolving the reducing agent. It is preferable to carry out dehydration treatment or dissolved oxygen removal treatment in advance.

In the case of mixing and preparing soft magnetic particles such as α-Fe particles and hard magnetic particles such as ε-Fe ₂ O ₃ particles, the soft magnetic particles are aggregated to form ε-Fe ₂ O ₃ particles. The particle size of the soft magnetic particles tends to be large beyond the range where the exchange coupling acts. However, this method can avoid that. The reduction to iron from a dispersion in which iron is dissolved as ions may be directly performed by a reducing agent, but particles or precipitates are precipitated by adjusting the pH of the dispersion by adding a basic solution as an additive. And then reduce the particles or precipitates.

That is, by using a basic solution, typically ammonia water, as an additive, the pH of the dispersion is changed to react the above-mentioned ions with, for example, hydroxide ions, and a precursor containing a transition metal element Can be deposited. For example, when the ion containing a transition metal element is Fe ²⁺ or Fe ³⁺ , adding aqueous ammonia allows iron hydroxide (Fe (OH) ₃ etc.), triiron tetraoxide (Fe ₃ O ₄ ) etc. Can be deposited.

For example, ammonia water is added to a dispersion containing an aqueous solution of iron (III) nitrate, and iron hydroxide (Fe (OH) ₃ ) is precipitated to surround the hard magnetic particles. After that, by heat treatment in a reducing atmosphere, iron hydroxide (Fe (OH) ₃ ) can be reduced to iron (such as α-Fe). Similarly, ammonia water may be added to iron (II) chloride solution to precipitate triiron tetraoxide (Fe ₃ O ₄ ), which may be reduced to iron by heat treatment in a reducing atmosphere. Note that this heat treatment may also serve as a heat treatment step described later.

[4] Drying and Heat Treatment Step After forming the sea portion of the soft magnetic material around a plurality of hard magnetic particles, the aqueous solution is immediately replaced with ethanol. This is to prevent the oxidation of soft magnetic materials such as iron. After this, it is dried to remove ethanol.

In this step, heat treatment is applied to the powder of the obtained mixture to convert the soft magnetic material into a continuous body. Specifically, the soft magnetic material obtained by the above-described steps is in the form of particles, or contains voids or the like. Therefore, heat treatment is performed in this step to melt or sinter the particles, and the soft magnetic material is formed into a continuous body to form a sea-like soft magnetic phase. At this time, heat treatment may be performed after the mixture is compression molded, or compression molding may be performed after the heat treatment, or heat treatment may be performed during compression molding. The heat treatment is preferably performed under any of an inert gas atmosphere, a reducing atmosphere, and a vacuum, particularly when the soft magnetic material is a material that is easily oxidized such as iron.

Also, in the case of hard magnetic materials such as ε-Fe ₂ O ₃ or the like, in which the magnetic properties deteriorate due to high heat, plasma activated sintering (PAS) or spark plasma sintering (SPS: Spark Plasma) It is preferable to sinter the shaped body by Sintering, PECS (Pulse electric current sintering) or the like. Plasma activation sintering and discharge plasma sintering are one of sintering methods in which heat treatment is performed during compression molding. There are two types of materials for compression molding molds used at that time: cemented carbide metal represented by tungsten carbide and graphitic carbon, if roughly classified, followability of sintering set temperature due to high electric resistance Graphite carbon is preferable in terms of cost and cost. Although the maximum value and the minimum value of the preferable range of the compression molding pressure at the time of sintering are difficult to say in general because they are influenced by the specifications of the apparatus used and the specifications of the mold, 10 MPa to 500 MPa is preferable. If the compression molding pressure during sintering is lower than 10 MPa, the contact between the sample and the die set may be insufficient, and the entire compact is not heated by the local energization. If the pressure is higher than 500 MPa, the mold may be damaged. More preferably, 20 MPa to 200 MPa is preferable. Also, the sintering temperature during compression molding is preferably 60 ° C to 250 ° C, and more preferably selected from 70 ° C to 150 ° C. When the sintering temperature during compression molding is less than 60 ° C., the soft magnetic material is less likely to become a continuous body, and when it is higher than 250 ° C., the magnetic properties of ε-Fe ₂ O ₃ as a hard magnetic material deteriorate. The "sintering temperature" referred to here is a monitoring temperature by a thermocouple inserted in the mold, and strictly different from the temperature of the sample itself. Next, the temperature rising rate is preferably selected from the range of 10 ° C./minute to 200 ° C./minute, and more preferably selected from the range of 20 ° C./minute to 100 ° C./minute. If the temperature rise rate is less than 10 ° C./min, the time for which ε-Fe ₂ O ₃ as a hard magnetic material is exposed to high temperature is not preferable because the time is increased, and the temperature rise rate is more than 200 ° C./min If it is fast, soaking of the sample may be insufficient, which may induce sintering temperature unevenness. In addition, the holding time at the sintering reaching temperature is difficult to say in general because it is influenced by the sintering temperature and the compression molding pressure, but it is preferably 0 minutes or more and 10 minutes or less, more preferably 0 minutes or more and 3 minutes or less preferable. Here, "0 minutes" means that cooling starts immediately upon reaching the sintering temperature without substantially providing a holding time.

When ε-Fe ₂ O ₃ is used as a hard magnetic material, nanoparticles of iron oxide or iron hydroxide are formed using a chemical process in solution, and the generated nanoparticles are heated in an oxidizing atmosphere. Ε-Fe ₂ O ₃ particles can be synthesized relatively easily. As a chemical process in a solution, for example, a reverse micelle method or a sol-gel method using iron nitrate hydrate as a starting material can be used. In the step of synthesizing the _ε-Fe 2 _{O 3} particles may be added a step of coating the surface of the _ε-Fe 2 _{O 3} particles with silica (SiO _2).

EXAMPLES Hereinafter, the present invention will be described in more detail using examples, but the present invention is not limited to the following examples. In addition, unless otherwise indicated, "%" used below is a mass reference | standard.

Example 1
In Example 1, ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron chloride (II) hydrate (FeCl ₂ .4H ₂ O) is dissolved, and a reducing agent NaBH ₄ is added to add Fe. By depositing, a composite magnetic material including a sea-island structure in which Fe was in the sea and ε-Fe ₂ O ₃ particles became islands was produced.

(Preparation of ε-Fe ₂ O ₃ particles)
The hard magnetic material ε-Fe ₂ O ₃ particles were produced in the following procedure. (1) First, two types of micelle solutions (micellar solution (A) and micelle solution (B)) were prepared as follows.

(1-1) In a reaction vessel, 30 mL of pure water, 92 mL of n-octane and 19 mL of 1-butanol were added and mixed. Thereto, 6 g of iron nitrate hydrate (Fe (NO ₃ ) ₃ .9H ₂ O) was added and sufficiently dissolved with stirring. Next, cetyltrimethylammonium bromide as a surfactant is added in an amount such that the molar ratio represented by (the number of moles of pure water) / (the number of moles of the surfactant) is 30, and stirring is performed. It was dissolved. Thus, a micelle solution (A) was obtained.

(1-2) In a separate reaction vessel, 10 mL of 28% aqueous ammonia was mixed with 20 mL of pure water and stirred, and then 92 mL of n-octane and 19 mL of 1-butanol were further added and stirred well. In the solution, cetyltrimethylammonium bromide as a surfactant is used, and the molar ratio represented by (number of moles of ((pure water + water in ammonia)) / (number of moles of surfactant) is 30. The amount was added and dissolved by stirring. Thus, a micelle solution (B) was obtained.

(2) The micelle solution (B) was dropped to the micelle solution (A) while well stirring the micelle solution (A). After the addition was completed, stirring was continued for 30 minutes.

(3) While stirring the obtained mixture, 7.5 mL of tetraethoxysilane (TEOS) was added to the mixture, and the stirring was continued for 1 day. In this step, a silica layer was formed on the surface of the iron-containing particles in the mixed solution.

(4) The obtained solution was set in a centrifuge and centrifuged for 30 minutes at a rotational speed of 4500 rpm to collect a precipitate. The collected precipitate was washed several times with ethanol.

(5) After drying the obtained precipitate, it was put in a baking furnace of an air atmosphere and heat-treated at 1150 ° C. for 4 hours.

(6) The heat-treated powder was dispersed in a 2 mol / L aqueous NaOH solution and stirred for 24 hours to remove the silica layer on the particle surface. Thereafter, the resultant was filtered, washed with water and dried to obtain ε-Fe ₂ O ₃ particles. Moreover, as a result of analyzing the crystal structure of the obtained ε-Fe ₂ O ₃ particles by X-ray diffraction (XRD), a diffraction peak of ε-Fe ₂ O ₃ is confirmed, and diffraction peaks derived from other crystal structures Was not confirmed.

The obtained ε-Fe ₂ O ₃ particles were dispersed in an aqueous solution. In this state, since the particle size increases due to aggregation, the average particle size is coarsened with a roll mill to 64 nm, further finely divided with a homogenizer to an average particle size of 42 nm, and filtered through a filter to obtain an average particle size of about It was 36 nm.

(Preparation of dispersed solution)
3 g of iron (II) chloride hydrate (FeCl ₂ .4H ₂ O) was weighed and dissolved in 75 mL of pure water to obtain an aqueous iron chloride solution. Next, 0.36 g of ε-Fe ₂ O ₃ particles were weighed, added to an aqueous iron chloride solution, and a dispersion liquid sufficiently dispersed by an ultrasonic dispersion machine was prepared.

(Fe precipitation by reduction treatment)
2 g of sodium tetrahydroborate (NaBH ₄ ), which is a reducing agent, was weighed, and a reducing agent solution dissolved in 20 mL of pure water was prepared. Next, the reducing agent solution was added while stirring the dispersion. As a result, iron (II) chloride was reduced, and α-Fe was precipitated in a form containing a plurality of ε-Fe ₂ O ₃ particles. NaBH ₄ was added in the form of a mist of several hundred μL with a spray device to make the particle size as small as possible. When the particle size of α-Fe in the obtained composite particles was observed with a scanning electron microscope (SEM), the particle size of α-Fe was 50 nm to 70 nm. The observation was performed with a magnification of 50,000 to 100,000. The magnification is the same in the following examples.

(Drying and heat treatment process)
After replacing the water in the aqueous solution containing α-Fe and ε-Fe ₂ O ₃ particles with ethanol and drying it, 1 g of composite particles of α-Fe and ε-Fe ₂ O ₃ particles is used as a 10 MPa pressure molding machine Processed to produce a molded body. Next, the obtained molded body was set in an electric furnace and subjected to heat treatment. Nitrogen gas was used as the atmosphere gas for the primary firing, and the flow rate of the gas was set to 300 sccm. The temperature during the heat treatment was 260 ° C., held at 260 ° C. for 5 hours, and cooled to room temperature. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. The powder obtained by the coarse crushing was again set in an electric furnace, and heat treated at 400 ° C. for 3 hours in a nitrogen atmosphere as secondary firing to obtain a nanocomposite magnetic particle material.

(Structural analysis of composite magnetic materials)
As a result of analyzing the crystal structure of the obtained composite magnetic material by XRD, a diffraction peak of ε-Fe ₂ O _{3 and} a diffraction peak of α-Fe can be confirmed respectively, and diffraction peaks derived from other crystal structures are confirmed It was not done.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 22 nm and the standard deviation was 6 nm.

(Magnetic characterization of composite magnetic materials)
The magnetic properties (residual magnetization and coercivity) of the composite magnetic material were evaluated. The results are shown in Table 1 below. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

Example 2
In Example 2, ammonia water is added to a dispersion in which ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron nitrate hydrate (Fe (NO ₃ ) ₃ .9H ₂ O) is dissolved, and the pH is determined by It was changed to precipitate Fe (OH) ₃ particles. This formed composite particles of Fe (OH) ₃ and ε-Fe ₂ O ₃ particles. Thereafter, Fe (OH) ₃ was reduced with hydrogen gas to form Fe, thereby producing a composite magnetic material including a sea-island structure in which Fe is in the sea and ε-Fe ₂ O ₃ particles are islands.

(Preparation of dispersion solution containing ions of soft magnetic material)
6 g of Fe (NO ₃ ) ₃ .9H ₂ O was weighed and dissolved in 75 mL of pure water to obtain an aqueous iron nitrate solution. Next, 0.36 g of ε-Fe ₂ O ₃ particles were weighed, added to an aqueous iron nitrate solution, and a dispersion liquid sufficiently dispersed by an ultrasonic dispersion machine was prepared.

(Precipitate of precursor particles)
While stirring the dispersion, 75 mL of 28% aqueous ammonia was added to precipitate Fe (OH) ₃ as precursor particles to form composite particles with ε-Fe ₂ O ₃ particles. The particle diameter of the iron hydroxide particles in the obtained composite particles was observed with a scanning electron microscope (SEM), and the particles were 10 nm to 20 nm.

(Drying and heat treatment process)
After replacing the water in the aqueous solution containing Fe (OH) ₃ and ε-Fe ₂ O ₃ particles with ethanol and drying, 1 g of composite particles of Fe (OH) ₃ and ε-Fe ₂ O ₃ particles is 10 MPa It processed with a pressure forming machine, and the molded object was produced. Next, the obtained molded body was set in an electric furnace and subjected to heat treatment. As the primary firing, a mixed gas of 2% hydrogen and 98% nitrogen was used as the atmosphere gas, and the flow rate of the mixed gas was set to 300 sccm. The temperature during the heat treatment was 260 ° C., held at 260 ° C. for 5 hours, and cooled to room temperature. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. Set to powder again electric furnace obtained by coarse grinding, the secondary firing as hydrogen and nitrogen mixed gas _{_{(2% H 2 -98% N}} 2) atmosphere, and heat-treated for 3 hours at 500 ° C., Fe (OH) ₃ was reduced to α-Fe to obtain a composite magnetic particle material.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. ε-Fe ₂ O ₃ was distributed almost all over α-Fe. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 18 nm and the standard deviation was 4 nm. In addition, the particle diameter of the island ε-Fe ₂ O ₃ was 30 nm.

(Magnetic characterization of composite magnetic materials)
The magnetic properties (residual magnetization and coercivity) of the obtained composite magnetic material were evaluated using a vibrating sample magnetometer. The results are shown in Table 1. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

[Example 3]
In Example 3, ammonia water is added to a dispersion in which ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron (II) chloride hydrate (FeCl ₂ · 4H ₂ O) is dissolved, and the pH is changed. by by depositing a _Fe 3 _{O 4} particles to form composite particles of _Fe 3 _{O 4} with _ε-Fe 2 _{O 3} particles. Thereafter, Fe ₃ O ₄ was reduced with hydrogen gas to form Fe, thereby producing a composite magnetic material including a sea-island structure in which Fe was in the sea and ε-Fe ₂ O ₃ particles became islands.

(Preparation of dispersed solution)
3 g of FeCl ₂ · 4H ₂ O was weighed and dissolved in 75 mL of pure water to obtain an aqueous solution of iron chloride. Next, 0.36 g of ε-Fe ₂ O ₃ particles obtained in the same manner as in Example 1 was weighed and added to an aqueous solution of iron chloride, and a dispersion liquid sufficiently dispersed by an ultrasonic dispersion machine was produced.

(Precipitate of precursor particles)
While stirring the dispersion, 75 mL of 28% aqueous ammonia was added to precipitate Fe ₃ O ₄ as precursor particles, thereby forming composite particles with ε-Fe ₂ O ₃ particles. The particle diameter of the Fe ₃ O ₄ particles in the obtained composite particles was observed with a scanning electron microscope (SEM) and found to be particles of 50 nm to 80 nm.

(Drying and heat treatment process)
After replacing the water in the aqueous solution containing Fe ₃ O ₄ and ε-Fe ₂ O ₃ particles with ethanol and drying, 1 g of composite particles of Fe ₃ O ₄ and ε-Fe ₂ O ₃ particles is pressurized at 10 MPa It processed by the molding machine and produced the molded object. Next, the obtained molded body was set in an electric furnace and subjected to heat treatment. As the primary firing, a mixed gas of 2% hydrogen and 98% nitrogen was used as the atmosphere gas, and the flow rate of the mixed gas was set to 300 sccm. The temperature during the heat treatment was 260 ° C., held at 470 ° C. for 5 hours, and cooled to room temperature. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. Set to powder again electric furnace obtained by coarse grinding, the secondary firing as hydrogen and nitrogen mixed gas _{_{(2% H 2 -98% N}} 2) atmosphere, and heat-treated for 3 hours at 470 ° C., Fe ₃ O ₄ was reduced to α-Fe to obtain a nanocomposite magnetic particle material.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. ε-Fe ₂ O ₃ was distributed almost all over α-Fe. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 45 nm and the standard deviation was 12 nm. Further, the particle diameter of the island ε-Fe ₂ O ₃ was 20 nm.

Example 4
In Example 4, ammonia water is added to a dispersion solution in which ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron chloride (II) hydrate (FeCl ₂ .4H ₂ O) is dissolved as in Example 3. The pH was changed by addition to precipitate Fe ₃ O ₄ particles. This formed composite particles of Fe ₃ O ₄ and ε-Fe ₂ O ₃ particles. Thereafter, Fe ₃ O ₄ was reduced with hydrogen gas to form Fe, thereby producing a composite magnetic material including a sea-island structure in which Fe is an island and ε-Fe ₂ O ₃ particles are an island. In Example 4, compared with Example 3, the particle size of Fe ₃ O ₄ particles to be precipitated was made smaller to prepare a magnetic material.

(Preparation of dispersed solution)
1.5 g of FeCl ₂ · 4H ₂ O was weighed and dissolved in 150 mL of pure water to obtain an aqueous solution of iron chloride. Next, 0.18 g of ε-Fe ₂ O ₃ particles obtained in the same manner as in Example 1 was weighed and added to an aqueous solution of iron chloride, and a dispersion liquid sufficiently dispersed by an ultrasonic dispersion machine was produced.

(Precipitate of precursor particles)
While stirring the dispersion, 75 mL of 28% aqueous ammonia was added to precipitate Fe ₃ O ₄ as precursor particles, thereby forming composite particles with ε-Fe ₂ O ₃ particles. The particle diameter of the Fe ₃ O ₄ particles in the obtained composite particles was observed with a scanning electron microscope (SEM), and it was particles of 10 nm to 30 nm.

(Drying and heat treatment process)
After water in an aqueous solution containing Fe ₃ O ₄ and ε-Fe ₂ O ₃ particles is replaced with ethanol and dried, 0.5 g of composite particles of Fe ₃ O ₄ and ε-Fe ₂ O ₃ particles is added at 10 MPa. It processed with the pressure forming machine and produced the molded object. Next, the obtained molded body was set in an electric furnace and subjected to heat treatment. The atmosphere gas for the primary firing was a mixed gas of 2% hydrogen and 98% nitrogen, and the flow rate of the mixed gas was 300 sccm. The temperature during the heat treatment was 260 ° C., held at 260 ° C. for 5 hours, and cooled to room temperature. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. Set to powder again electric furnace obtained by coarse grinding, the secondary firing as hydrogen and nitrogen mixed gas _{_{(2% H 2 -98% N}} 2) atmosphere, and heat-treated for 3 hours at 450 ° C., Fe ₃ O ₄ was reduced to α-Fe to obtain a nanocomposite magnetic particle material.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. ε-Fe ₂ O ₃ was distributed almost all over α-Fe. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 20 nm and the standard deviation was 6 nm. Further, the particle diameter of the island ε-Fe ₂ O ₃ was 20 nm.

[Example 5]
A sea-island structure in which α-Fe is a sea and ε-Fe ₂ O ₃ particles are an island by the same method as in Example 1 except that an external magnetic field of 20 kOe is applied when producing a molded body in Example 1 Nanocomposite magnetic particle materials were produced. The crystal structure and the crystallographic orientation axis were confirmed by XRD and TEM. The crystal structure of ε-Fe ₂ O ₃ is a cuboid system (Pna 21), and the lattice constant is 5.1 Å for the a axis and 8. It was 7 angstrom and c axis was 9.4 angstrom. Among these, the c axis, which is the easy axis of magnetization, had a region of ± 8 degrees or less at 80% or more in volume fraction.

The crystal structure of α-Fe is a body-centered cubic structure, the lattice constant is about 2.9 angstroms, and the a-axis (the b-axis and c-axis are the same as the easy axis) is ± 9% or less However, the volume fraction was over 80%. The angle between the easy axis of ε-Fe ₂ O _{3 and} the easy axis of α-Fe was about ± 6 degrees or less.

The magnetic properties (residual magnetization and coercivity) of the composite magnetic material were evaluated using a vibrating sample magnetometer. The results are shown in Table 1. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

[Example 6]
A composite magnetic material having a diameter of 10 mm was produced in the same manner as in Example 1 except that the pressure was changed from 10 MPa to a pressure of 50 MPa when producing a molded body with a pressure molding machine in Example 1. The porosity of the composite magnetic material was measured and found to be 7% or less. In the measurement of the relative density of the solidified body, the specific gravity is calculated from the buoyancy received by applying the resin on the surface and dipping in pure water after polishing the surface of the solidified body with emery paper and bubbling (Archimedes) And expressed as a ratio to the theoretical specific gravity.

The magnetic properties (residual magnetization and coercivity) of the composite magnetic material were evaluated. The results are shown in Table 1. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

[Example 7]
Similarly to the method described in Example 1, ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron chloride (II) hydrate (FeCl ₂ · 4H ₂ O) is dissolved, and NaBH ₄ as a reducing agent is dispersed. Was added to precipitate Fe, thereby producing a composite magnetic material including a sea-island structure in which Fe is in the sea and ε-Fe ₂ O ₃ particles are islands. However, in order to narrow the distance between islands containing ε-Fe ₂ O ₃ , the particles were prepared under the condition of reducing the particle size of precipitated Fe. The ε-Fe ₂ O ₃ particles were produced under the same conditions as in Example 1.

(Preparation of dispersed solution)
1.5 g of iron (II) chloride hydrate (FeCl ₂ · 4H ₂ O) was weighed and dissolved in 75 mL of pure water to obtain an aqueous iron chloride solution. Next, 0.36 g of ε-Fe ₂ O ₃ particles were weighed, added to an aqueous iron chloride solution, and a dispersion liquid sufficiently dispersed by an ultrasonic dispersion machine was prepared.

(Precipitation of reduced particle size Fe)
2 g of sodium tetrahydroborate (NaBH ₄ ), which is a reducing agent, was weighed, and a reducing agent solution dissolved in 20 mL of pure water was prepared. Next, the dispersion was heated in a water bath so as to be stable at 95 ° C. while stirring. The reducing agent solution was then added by spraying with a spray device. As a result, iron (II) chloride was reduced, and α-Fe was precipitated in a form containing a plurality of ε-Fe ₂ O ₃ particles. NaBH ₄ was added in the form of a mist of about 0.1 μL, which is smaller than Example 1. When the particle size of α-Fe in the obtained composite particles was observed with a scanning electron microscope (SEM), the particle size of α-Fe was 30 nm to 50 nm.

(Drying and heat treatment process)
In the subsequent drying / heat treatment step, a composite magnetic material was produced under the same conditions as in Example 1.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 18 nm and the standard deviation was 5 nm.

[Example 8]
The present example is the same as the method shown in Example 1 except that the step of preparing the dispersion solution and the step of depositing the Fe particles by reduction are the same as in the method described in Example 1, except that Fe is sea and ε-Fe ₂ O ₃ particles are islands. A composite magnetic material containing a sea-island structure was produced. However, in order to narrow the distance of the island containing ε-Fe ₂ O ₃ , it was manufactured under the condition of reducing the particle size of Fe to be reduced. The ε-Fe ₂ O ₃ particles were produced under the same conditions as in Example 1.
(Preparation of dispersed solution)
1.62 g of iron (II) bromide (FeBr ₂ ) was weighed and dissolved in 150 mL of methanol to obtain a solution of iron bromide in methanol. Next, 0.36 g of ε-Fe ₂ O ₃ particles were weighed, added to an iron bromide methanol solution, and a dispersion liquid sufficiently dispersed by an ultrasonic disperser was prepared.

(Precipitation of Fe particles by reduction)
2 g of reducing agent sodium tetrahydroborate (NaBH ₄ ) was weighed, and a reducing agent solution in which 20 mL of dehydrated methanol was dissolved was prepared. Next, the reducing agent solution was added dropwise while stirring the dispersion. Thereby, iron (II) bromide was reduced to precipitate α-Fe in a form including a plurality of ε-Fe ₂ O ₃ particles. When the particle size of α-Fe in the obtained composite particles was observed with a scanning electron microscope (SEM), the particle size of α-Fe was 10 nm to 20 nm. The ε-Fe ₂ O ₃ particles were produced under the same conditions as in Example 1 except that they were dispersed in dehydrated methanol. In this state, since the particle size increases due to aggregation, the average particle size is coarsened with a roll mill to 64 nm, further finely divided with a homogenizer to an average particle size of 42 nm, and filtered through a filter to obtain an average particle size of about It was 36 nm.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) containing α-Fe. The structure was confirmed. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 12 nm and the standard deviation was 4 nm.

(Magnet of composite magnetic material)
The magnetic properties (residual magnetization and coercivity) of the composite magnetic material were evaluated. The results are shown in Table 1 below. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

[Example 9]
Similarly to the method described in Example 1, ε-Fe ₂ O ₃ particles are dispersed in a solution in which iron chloride (II) hydrate (FeCl ₂ · 4H ₂ O) is dissolved, and NaBH ₄ as a reducing agent is dispersed. Was added to precipitate Fe, thereby producing a composite magnetic material including a sea-island structure in which Fe is in the sea and ε-Fe ₂ O ₃ particles are islands. However, in order to narrow the distance of the island containing ε-Fe ₂ O ₃ , it was manufactured under the condition of reducing the particle size of Fe to be reduced. The ε-Fe ₂ O ₃ particles were produced under the same conditions as in Example 1. The present embodiment differs from the eighth embodiment in that pulse current sintering is performed in the drying and heat treatment steps.

(Preparation of dispersed solution)
1.62 g of iron (II) bromide (FeBr ₂ ) was weighed and dissolved in 150 ml of methanol to obtain a solution of iron bromide in methanol. Next, 0.36 g of ε-Fe ₂ O ₃ particles were weighed, added to an iron bromide methanol solution, and a dispersion liquid sufficiently dispersed by an ultrasonic disperser was prepared.

(Drying and heat treatment process)
The drying / heat treatment step of the next step was performed according to the following procedure to produce a sintered magnet.

In a glove box held in an argon atmosphere, methanol was evaporated from a methanol slurry containing ε-Fe ₂ O ₃ particles and α-Fe particles to obtain a composite magnetic material powder. 0.6 g of the composite magnetic material powder was weighed and filled in a graphite die set with an inner diameter of 10 mm. Then, it was set in a pulse current sintering apparatus (LABOX-650F: manufactured by Sinterland Co., Ltd.) equipped with a pressing mechanism without exposure to the atmosphere.

Next, after setting the sintering chamber in a vacuum atmosphere of 2 Pa or less, a compressive pressure of 60 MPa was applied to the composite magnetic material powder, and the powder was immediately unloaded. A compression pressure of 60 MPa was applied again, and while maintaining this pressure, the temperature was raised from room temperature to 90 ° C. at a heating rate of 50 ° C./min, and cooling was performed immediately without holding when reaching 90 ° C. After confirming cooling to room temperature, the pressure was returned to atmospheric pressure, and the die set was taken out.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), it is found that there is a plurality of islands containing ε-Fe ₂ O ₃ in the sea (continuum) made of α-Fe. The structure was confirmed. When the inter-island distance was calculated from 10 points of the observation image and the average inter-island distance and its standard deviation were calculated, the average inter-island distance was 11 nm and the standard deviation was 3 nm.

A comparative example to the above embodiment will be described.
Comparative Example 1
In Comparative Example 1, composite magnetic particles containing α-Fe particles and ε-Fe ₂ O ₃ particles are produced by respectively preparing α-Fe nanoparticles and ε-Fe ₂ O ₃ particles and mixing them and heat treating them. The material was made.

(Preparation of α-Fe nanoparticles)
The soft magnetic material α-Fe nanoparticles were produced by the following procedure.
First, 6 g of iron nitrate hydrate (Fe (NO ₃ ) ₃ .9H ₂ O) was weighed and dissolved in 75 mL of pure water to obtain an iron nitrate aqueous solution. While stirring 75 mL of 28% ammonia water, an aqueous iron nitrate solution was added to the ammonia water to precipitate iron hydroxide (Fe (OH) ₃ ) as precursor particles. The precipitated iron hydroxide was recovered by filter filtration, thoroughly washed with pure water, and then vacuum dried to obtain iron hydroxide nanoparticles. As a result of measuring the particle size of the obtained iron hydroxide nanoparticles by dynamic light scattering (DLS), the volume-based average particle size was 8 nm.

Next, the obtained iron hydroxide nanoparticles were put into an alumina crucible, and the iron hydroxide nanoparticles were heat-treated in a reducing atmosphere to obtain α-Fe nanoparticles. A mixed gas of 2% hydrogen and 98% nitrogen was used as an atmosphere gas in the heat treatment, and the flow rate of the mixed gas was set to 300 sccm. The temperature during the heat treatment was 500 ° C., held at 500 ° C. for 5 hours, and cooled to room temperature. As a result of measuring the particle size of the obtained α-Fe nanoparticles by DLS, the volume-based average particle size was 25 nm. Moreover, as a result of analyzing the crystal structure of the obtained α-Fe nanoparticles by XRD, a diffraction peak of α-Fe (alpha iron) was confirmed, and no diffraction peak derived from other crystal structures was confirmed.

(Preparation of composite magnetic material)
0.48 g and 0.2 g of each of the α-Fe nanoparticles and the ε-Fe ₂ O ₃ particles prepared by the above-mentioned method were weighed and mixed in a nitrogen gas atmosphere using a planetary ball mill. Next, this mixed powder was processed by a 10 MPa pressure molding machine to obtain a molded body. The resulting set in the molded body in an electric furnace, primary firing as hydrogen and nitrogen mixed gas _{_{(2% H 2 -98% N}} 2) atmosphere for 5 hours of heat treatment at 260 ° C.. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. Set to powder again electric furnace obtained by coarse grinding, the secondary firing as hydrogen and nitrogen mixed gas _{(2% H 2 -98% N} 2) atmosphere, and heat-treated for 3 hours at 260 ° C., the composite Magnetic grain material was obtained.

(Structural analysis of composite magnetic materials)
As a result of analyzing the crystal structure of the obtained composite magnetic material by XRD, a diffraction peak of ε-Fe ₂ O _{3 and} a diffraction peak of α-Fe can be confirmed respectively, and diffraction peaks derived from other crystal structures are confirmed. It was not. In addition, as a result of observing a cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), a structure in which α-Fe particles and ε-Fe ₂ O ₃ particles are mixed was observed.

Comparative Example 2
In Comparative Example 2, ε-Fe ₂ O ₃ particles are produced by the same method as Comparative Example 1, and the produced ε-Fe ₂ O ₃ particles are subjected to reduction treatment to obtain a core of ε-Fe ₂ O ₃ and α A composite magnetic material containing a -Fe shell was prepared.

(Preparation of composite magnetic material)
The _ε-Fe 2 _{O 3} particles obtained in the same manner as in Comparative Example 1 was set in an electric furnace, a gas mixture of hydrogen and nitrogen _{_{(2% H 2 -98% N}} 2) atmosphere, heating at 350 ° C. 30 minutes It was processed. After cooling to room temperature, it was roughly crushed under a nitrogen gas atmosphere using a planetary ball mill. Set to powder again electric furnace obtained by coarse grinding, the gas mixture _{(2% H 2 -98% N} 2) under an atmosphere of hydrogen and nitrogen, and heat-treated for 3 hours at 260 ° C., to obtain a composite magnetic material The

(Structural analysis of composite magnetic materials)
As a result of analyzing the crystal structure of the obtained composite magnetic material by XRD, a diffraction peak of ε-Fe ₂ O _{3 and} a diffraction peak of α-Fe can be confirmed respectively, and diffraction peaks derived from other crystal structures are confirmed. It was not.

In addition, as a result of observing the cross section of the particulate composite magnetic material with a scanning electron microscope (SEM), an aggregate of a core-shell structure including a core of ε-Fe ₂ O ₃ and a shell of α-Fe could be confirmed.

Comparative Example 3
In Patent Document 1, a hard magnetic particle and a soft magnetic particle are mixed to obtain a nanocomposite magnet. The exchange force acting between the hard magnetic material and the soft magnetic material is proportional to the contact area. For this reason, it is desirable that the contact area of the hard magnetic material and the soft magnetic material be as large as possible, but when spherical particles are in contact, the contact area is close to zero and the exchange force is extremely small. However, it is known that if the powder which is an aggregate of particles is compressed, the contact surface is formed between the particles and the porosity decreases. However, nanoparticles with a particle size of 100 nm or less tend to have a low bulk density of the powder as the particle size decreases, making it difficult to reduce the porosity even after compression.

In Comparative Example 3, the composite magnetic material was manufactured by densifying the ε-Fe ₂ O ₃ particles and the Fe particles in Comparative Example 1, and the porosity was measured. The ε-Fe ₂ O ₃ particles having an average particle diameter of 30 nm and the Fe particles having an average particle diameter of 25 nm prepared by the same method as Comparative Example 1 are washed with pure water, and the respective washed particles are contained in an organic acid solution. And both solutions were mixed together. Both particles were made into a nanocomposite by mixing the solution while being irradiated with ultrasonic waves for about 40 minutes. The volume fraction of ε-Fe ₂ O ₃ particles and Fe particles was set to a ratio of 4: 6, and after ultrasonic mixing, the nanocomposite particles were recovered by a centrifugal separator.

The nanocomposite particles were subjected to a pressure of 50 MPa with a compression molding machine to produce a composite magnetic material having a diameter of 10 mm. The porosity of the composite magnetic material was determined in the same manner as in Example 6 to be 25.3%.

The magnetic properties (residual magnetization and coercivity) of the obtained composite magnetic material were evaluated using a vibrating sample magnetometer. The results are shown in Table 1. In addition, the magnetic characteristic was shown by the value normalized with respect to the comparative example 5 mentioned later.

Comparative Example 4
Moreover, the porosity was 22.4% when the compacting pressure was changed to 300 MPa and a composite magnetic material was manufactured by the same method as Comparative Example 3.

Comparative Example 5
Further, in the same manner as in Comparative Example 3, the porosity was 21.5% when the composite magnetic material was manufactured by changing the molding pressure to 550 MPa. The magnetic properties (residual magnetization and coercivity) of the obtained composite magnetic material were evaluated using a vibrating sample magnetometer. The results are shown in Table 1.

Comparative Example 6
About the composite magnetic material of Comparative Example 1, when the crystal structure and the crystal orientation axis were confirmed by XRD and TEM in the same manner as in Example 5, the magnetization easy axis was about ± 25 degrees of ε-Fe ₂ O ₃ and α-Fe Was about ± 28 degrees. Comparative Example 6 is not shown in Table 1 below.

As shown in Table 1, in Examples 1 to 8, both the remanent magnetization and the coercivity were improved relative to Comparative Examples 1 to 5. Further, as shown in Example 9, when the heat treatment was performed by pulse current sintering, the improvement of the residual magnetization and the coercivity was remarkable. From the above results, high performance magnetic properties can be achieved by depositing soft magnetic material particles from a dispersion obtained by dispersing particles containing a hard magnetic material in a solution obtained by ionizing and dissolving a soft magnetic material. It turned out that the material can be manufactured.

[Example 10]
In the inner rotor type brushless motor shown in FIGS. 9A and 9B and FIG. 10, motors of different shapes were manufactured. Table 3 shows the outer diameter and thickness of the magnet 5 in FIG. 9A, and the length of the magnet 5 in FIG. 9B. Table 4 shows the thickness (cylindrical thickness) of the yoke 6 in FIG. 9A and the thickness (lid thickness) of the movable portion (rotor) lid 8 in FIG. 9B. Table 5 shows the diameter of the shaft 7 in FIG. 9A and the length of the shaft 7 in FIG. 9B. Further, in Tables 3, 4 and 5, the specific gravity and weight of each part, and the weight occupancy in the entire moving part (rotor) 4 are shown. Table 5 shows the weight of the entire moving part (rotor).

In FIG. 12A, for the case of Example 1 in Tables 3, 4, and 5, the rotational speed w of the motor is the maximum rotational speed wmax, the normalized value w / wmax is the vertical axis, and the time t from the start of rotation Is shown on the horizontal axis. In FIG. 12A, the present invention (solid line) is used. FIG. 12B is a diagram showing the current consumption of the motor on the vertical axis and the time t from the start of rotation on the horizontal axis in the case of the first embodiment in Tables 3, 4, and 5. In FIG. 12B, the present invention (solid line) is used. The bonded magnet including the composite magnetic material applied to this example contains hard magnetic particles ε-Fe ₂ O ₃ with an average particle diameter of 5 nm at a volume fraction of 0.4, an interparticle distance of 30 nm, and a specific gravity of 6.7 g / a composite magnetic material cm ^3, and a resin having a specific gravity ρp is 1 g / cm ^3, the volume fraction Vm = 0.7 (volume ratio 7: 3) those prepared by mixing in. The specific gravity bb of the bonded magnet applied to the present embodiment is 5 g / cm ³ .

Table 2 describes the start-up time (the time when the rotational speed w is 98% of the maximum speed wmax) and the energy required for one second. The measurement was performed at a voltage of 10 V, and the energy was determined from the integral value of the current and voltage for one second. As a result, in the motor of the present invention, the start-up time was 0.12 seconds, and the energy was 4.53 J.

Comparative Example 7
As compared with Example 10, the results measured with a motor having the same structure except that the magnet is changed from the magnet of the present invention to a neodymium magnet having the same maximum energy product are shown by broken lines in FIGS. 12A and 12B. In the motor of the comparative example, the start time was 0.60 seconds, and the energy was 9.41 J. Therefore, it was found that, in the motor using the magnet of the present invention for the moving part (rotor), the start-up time is short and the energy consumption (power consumption) is small.

[Example 11]
As shown in Tables 3, 4 and 5, a motor having the same structure as in Example 10 was produced except that the shape was changed. The startup time was 0.35 seconds.

[Example 12]
As shown in Tables 3, 4 and 5, a motor having the same structure as in Example 10 was produced except that the shape was changed. The startup time was 0.42 seconds.

Comparative Example 8
As shown in Tables 3, 4 and 5, a motor having the same structure as in Example 11 was produced except that the magnet of the present invention was changed to a neodymium magnet having the same maximum energy product. The startup time was 0.81 seconds.

Comparative Example 9
As shown in Tables 3, 4 and 5, a motor having the same structure as in Example 12 was produced except that the magnet of the present invention was changed to a neodymium magnet having the same maximum energy product. The startup time was 0.76 seconds.

As described above, the activation time of Example 10 is 20% of the activation time of Comparative Example 7, the activation time of Example 11 is 43% of the activation time of Comparative Example 8, and the activation time of Example 12 is the activation time of Comparative Example 9. It was 55%. Although the rotor weight is different in each example, the motor of the present invention has a shorter start-up time as compared with the motor of the comparative example, and the effect of shortening the start-up time is high according to the weight occupancy rate in the rotor (rotating portion) .

The present invention is not limited to the above embodiment, and various changes and modifications can be made without departing from the spirit and scope of the present invention. Accordingly, the following claims are attached to disclose the scope of the present invention.

Priority is claimed on Japanese Patent Application No. 2017-203059 filed Oct. 20, 2017, Japanese Patent Application No. 2018-196167 filed Oct. 17, 2018, and Japanese Patents filed Oct. 17, 2018. The present application claims priority based on Japanese Patent Application No. 2018-196169, the entire contents of which are incorporated herein by reference.

1 composite magnetic material 2 soft magnetic phase 3 hard magnetic particles 4 moving part (rotor)
5 magnet 6 yoke 7 shaft 8 lid 9 motor 10 electromagnet 11 cover

Claims

A plurality of hard magnetic particles are dispersed in the form of islands in the soft magnetic phase,
The composite magnetic material, wherein the hard magnetic particles have an average particle diameter of 2 nm or more and an average distance between two adjacent hard magnetic particles is 100 nm or less.
The composite magnetic material according to claim 1, wherein the soft magnetic phase is a continuous body.
A composite magnetic material comprising a plurality of hard magnetic particles dispersed in the form of islands in a soft magnetic phase, wherein the soft magnetic phase is a continuous body.
The hard magnetic particle includes a magnetic material mainly composed of a ferrimagnetic material or an antiferromagnetic material, and the soft magnetic phase preferably includes a magnetic material mainly composed of a ferromagnetic material. Composite magnetic material as described in any one of to 3.
The composite magnetic material according to claim 4, wherein the hard magnetic particles contain iron oxide as a main component.
The composite magnetic material according to claim 5, wherein the hard magnetic particles contain ε-Fe 2 O 3 as a main component.
The composite magnetic material according to any one of claims 4 to 6, wherein the soft magnetic phase contains Fe or Co as a main component.
The composite magnetic material according to claim 7, wherein the soft magnetic phase contains α-Fe as a main component.
The composite magnetic material according to claim 1, wherein an angle formed by the direction of the magnetization easy axis of the hard magnetic particles and a predetermined one direction is 15 degrees or less for each of the plurality of hard magnetic particles. The composite magnetic material according to any one of 8.
In the composite magnetic material, the angle between the direction of the magnetization easy axis of the soft magnetic phase and a predetermined one direction is 15 degrees or less over the entire soft magnetic phase existing between two adjacent hard magnetic particles. The composite magnetic material according to any one of claims 1 to 9, characterized in that:
The composite magnetic material according to any one of claims 1 to 10, wherein a volume fraction of voids in the composite magnetic material is 20% or less.
The composite magnetic material according to any one of claims 1 to 11, wherein the content of the nonmagnetic material in the composite magnetic material is 10% or less by volume fraction.
The composite magnetic material according to any one of claims 1 to 12, wherein a squareness ratio of a magnetization curve represented by a relation between an external magnetic field and magnetization is 0.7 or more.
The composite magnetic material according to any one of claims 1 to 13, wherein an average particle diameter of the hard magnetic particles is 1000 nm or less.
The mixing ratio of the hard magnetic particles and the soft magnetic phase is 0.2 or more and 0.6 or less in volume fraction Vh / (Vs + Vh) (Vs is the volume of the soft magnetic phase, and Vh is the hard magnetic particles The composite magnetic material according to any one of claims 1 to 14, characterized in that
The composite magnetic material according to any one of claims 1 to 15, wherein two adjacent hard magnetic particles are exchange-coupled to each other via the soft magnetic phase.
The composite magnetic material according to any one of claims 1 to 16, wherein the content of the Nd element is 3% by mass or less.
A magnet comprising the composite magnetic material according to any one of claims 1 to 17.
Magnet according to claim 18, the maximum energy product is characterized in that at 170kJ / m 3 or more.
The magnet according to claim 18 or 19, comprising the composite magnetic material and a resin material.
The magnet according to claim 20, which has a specific gravity of 5 g / cm 3 or less.
22. A magnet according to claim 20 or 21, wherein the maximum energy product is 21 kJ / m < 3 > or more.
A motor comprising the magnet according to any one of claims 18 to 22.
A motor comprising a rotor or a stator including the magnet according to any one of claims 18 to 22.
A motor unit comprising: the motor according to claim 23 or 24; and a sequencer driven in a drive sequence in which the period for rotating the motor at a constant speed is twice or less the period for accelerating and rotating. .
A motor unit comprising: the motor according to claim 23 or 24; and a sequencer for driving the motor in a drive sequence which repeats forward rotation and reverse rotation.
An aircraft unit comprising the motor according to claim 23 or 24.
A method of manufacturing a composite magnetic material containing a soft magnetic material and a hard magnetic material, comprising:
The soft magnetic material comprises at least one transition metal element,
A first step of dispersing particles containing the hard magnetic material in a solution containing ions containing the transition metal element to obtain a dispersion;
A second step of adding an additive to the dispersion liquid to precipitate particles containing the transition metal element, and manufacturing the composite magnetic material.
The method of claim 28, wherein the additive is a reducing agent.
The additive is a basic solution,
In the second step, the basic solution is added to the dispersion to change the pH of the dispersion, thereby depositing the precursor containing the transition metal element around the particles containing the hard magnetic material. The method of manufacturing a composite magnetic material according to claim 28, wherein the precursor is reduced to form the soft magnetic material after being allowed to form.
31. A method of manufacturing a composite magnetic material according to any one of claims 28 to 30, further comprising a third step of performing heat treatment after the second step.
The method of manufacturing a composite magnetic material according to claim 31, wherein the third heat treatment step is pulse current sintering.