JP2009123968A - POROUS MATERIAL FOR R-Fe-B BASED PERMANENT MAGNET, AND MANUFACTURING METHOD THEREOF - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a porous material for an R-Fe-B based permanent magnet that exhibits higher magnetic characteristics, particularly, higher squareness compared with a conventional bond magnet and has a higher degree of shape freedom than a conventional sintered magnet. <P>SOLUTION: The method for manufacturing a porous material for an R-Fe-B based permanent magnet includes a process for preparing R-Fe-B based rare-earth alloy powder having an average particle size of <20 μm, a process for forming a green compact by molding the R-Fe-B based rare-earth alloy powder, a process for causing a hydrogenation and disproportionation reaction by applying heat treatment to the green compact at a temperature of ≥550°C and <650°C in hydrogen gas, and a process for causing a dehydrogenation and recombination reaction by applying heat treatment to the green compact at a temperature of ≥550°C and <1,000°C in vacuum or in an inert atmosphere. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to a porous magnet material for R—Fe—B permanent magnets produced using the HDDR method and a method for producing the same.

R-Fe-B rare earth magnets (R is a rare earth element, Fe is iron, B is boron), which is a typical high performance permanent magnet, has a ternary tetragonal compound R ₂ Fe ₁₄ B phase as the main phase. It has a containing structure and exhibits excellent magnetic properties. Such R—Fe—B rare earth magnets are roughly classified into sintered magnets and bonded magnets. The sintered magnet is manufactured by compressing and molding a fine powder (average particle size: several μm) of an R—Fe—B based magnet alloy with a press machine. On the other hand, bond magnets are usually manufactured by compression molding or injection molding a mixture (compound) of R-Fe-B magnet alloy powder (particle size: about 100 μm, for example) and a binding resin. The

  In the case of a sintered magnet, since a powder having a relatively small particle size is used, each powder particle has magnetic anisotropy. For this reason, when compressing powder with a press machine, an orientation magnetic field is applied to the powder, thereby producing a green compact in which the powder particles are oriented in the direction of the magnetic field.

  The green compact obtained in this manner is usually sintered at a temperature of 1000 ° C. to 1200 ° C. and becomes a permanent magnet by heat treatment as necessary. As an atmosphere during sintering, a vacuum atmosphere or an inert atmosphere is mainly used in order to suppress oxidation of rare earth elements.

  On the other hand, in the bonded magnet, in order to develop magnetic anisotropy, it is necessary that the easy magnetization axes of the hard magnetic phase in the powder particles to be used are arranged in one direction. In order to obtain a coercive force necessary for practical use, it is necessary to reduce the crystal grains of the hard magnetic phase constituting the powder particles to about the single-domain critical particle size. Therefore, in order to produce an excellent anisotropic bonded magnet, it is necessary to obtain a rare earth alloy powder satisfying these conditions.

Currently, an HDDR (Hydrogenation-Deposition-Desorption-Recombination) treatment method is generally employed to produce rare earth alloy powders for anisotropic bonded magnets. “HDDR” means a process of sequentially performing hydrogenation and disproportionation, dehydrogenation and recombination. According to the known HDDR treatment, an R-Fe-B alloy ingot or powder is maintained at a temperature of 500 ° C. to 1000 ° C. in an H ₂ gas atmosphere or a mixed atmosphere of an H ₂ gas and an inert gas. It said after ingot or powder in a hydrogen is occluded, such as H ₂ pressure is 13Pa or less of vacuum atmosphere, or H ₂ partial pressure is dehydrogenated at a temperature 500 ° C. to 1000 ° C. until the following inactive atmosphere 13Pa by Then, it is cooled.

In the above treatment, typically, the following reaction proceeds. That is, the hydrogenation and recombination reaction (both are referred to as “HD reaction” together with the heat treatment for causing hydrogen occlusion), examples of reaction formula: Nd ₂ Fe ₁₄ B + 2H ₂ → 2NdH ₂ + 12Fe + Fe ₂ B) proceed. A fine structure is formed. Next, by performing heat treatment for dehydrogenation, dehydrogenation and disproportionation reaction (both are referred to as “DR reaction”. Example of reaction formula: 2NdH ₂ + 12Fe + Fe ₂ B → Nd ₂ Fe ₁₄ B + 2H ₂ ) Occurs, and an alloy containing a fine R ₂ Fe ₁₄ B crystal phase is obtained.

The R—Fe—B alloy powder produced by the HDDR treatment has a large coercive force and exhibits magnetic anisotropy. The reason for having such a property is that the metallographic structure is substantially as fine as 0.1 μm to 1 μm, and a crystal with easy magnetization axes aligned in one direction by appropriately selecting reaction conditions and composition. It is because it becomes the aggregate of. More specifically, since the grain size of the ultrafine crystal obtained by the HDDR treatment is close to the single domain critical grain size of the tetragonal R ₂ Fe ₁₄ B-based compound, a high coercive force is exhibited. An aggregate of very fine crystals of this tetragonal R ₂ Fe ₁₄ B-based compound is referred to as “recrystallized texture”. A method for producing an R—Fe—B alloy powder having a recombination texture by performing HDDR processing is disclosed in, for example, Patent Document 1 and Patent Document 2.

  Magnetic powder produced by HDDR processing (hereinafter referred to as “HDDR powder”) is usually mixed with a binder resin (binder) to form a mixture (compound), and then compression molding or injection molding in a magnetic field. Thus, an anisotropic bonded magnet is formed. Since HDDR powder normally aggregates after HDDR processing, it is used as a powder after being agglomerated for use as an anisotropic bonded magnet. For example, in Patent Document 1, the preferable range of the particle size of the obtained magnet powder is 2 μm to 500 μm, and in Example 1, the aggregate obtained by HDDR treatment of the powder having an average particle size of 3.8 μm is obtained in a mortar. After pulverizing to obtain a powder having an average particle size of 5.8 μm, a bonded magnet is produced by mixing with pismaleimide triazine resin and compression molding.

  In addition, a technique has been proposed in which HDDR powder is oriented and then bulked using a hot forming method such as hot pressing or hot isostatic pressing (HIP), which is disclosed in Patent Document 3, for example. By using the hot forming method, it can be densified at a low temperature, so that a bulk magnet can be produced while maintaining the recrystallized texture of the HDDR powder.

  Further, various methods for producing R—Fe—B permanent magnets using the characteristics of the HDDR method have been proposed. For example, in Patent Document 4, an R—Fe—B alloy obtained by melting in a high-frequency melting furnace is subjected to a solution treatment as necessary and then pulverized after cooling, and this is 1 to 10 μm by a jet mill or the like. And then molded in a magnetic field, and thereafter sintered in a high vacuum of 1000 to 1140 ° C. or in an inert atmosphere, and then held in a hydrogen atmosphere in the range of 600 to 1100 ° C. Then, it is disclosed that the main phase is refined to 0.01 to 1 μm by subsequently performing heat treatment in a high vacuum.

  In the method disclosed in Patent Document 5, first, a fine powder of less than 10 μm obtained by pulverizing a homogenized alloy with a pulverizer such as a jet mill is formed in a magnetic field to produce a green compact. Thereafter, the green compact is treated at a temperature of 600 ° C. to 1000 ° C. in hydrogen and then at a temperature of 1000 ° C. to 1150 ° C. The process performed on the green compact corresponds to the HDDR process, but the temperature of the DR process is high. According to the method of Patent Document 5, since the sintering proceeds by high-temperature DR treatment, the green compact is densely sintered as it is. Patent Document 5 describes that in order to form a high-density sintered body, it is necessary to perform sintering at a temperature of 1000 ° C. or higher.

  On the other hand, in the method disclosed in Patent Document 6, first, after coarsely pulverizing to an average particle size of 50 to 500 μm by the hydrogen storage and collapse method, the coarsely pulverized powder is shaped into a predetermined shape (molded in a magnetic field as necessary) Make a green compact. Then, a well-known HDDR process is performed with respect to a green compact, and a bonded magnet is manufactured by performing resin impregnation or resin immersion to the obtained green compact.

In both methods disclosed in Patent Documents 5 and 6, HDDR processing is performed on the green compact. However, in the method of Patent Document 5, mechanical strength is increased by densification by high-temperature sintering, whereas in the method of Patent Document 6, mechanical strength is increased using a resin.
JP-A-1-132106 JP-A-2-4901 JP-A-4-253304 Japanese Patent Laid-Open No. 4-165012 Japanese Patent Laid-Open No. 6-112027 JP-A-9-148163

  R-Fe-B rare earth sintered magnets can obtain superior magnetic properties as compared to bonded magnets, but have limitations on the shapes that can be produced. One reason is that it is difficult to obtain a desired shape due to shrinkage anisotropy during sintering. Specifically, the shrinkage rate in the direction parallel to the orientation magnetic field is larger than the shrinkage rate in the direction perpendicular to the orientation magnetic field, and the ratio is a large value exceeding 2. Here, the “shrinkage ratio” is defined by (“dimension before sintering” − “dimension after sintering”) ÷ “dimension before sintering”. In this specification, a direction parallel to the orientation magnetic field is referred to as an “orientation direction”, and a direction perpendicular to the “orientation direction” is referred to as a “mold direction”.

On the other hand, although the R-Fe-B based bonded magnet has a magnetic property lower than that of a sintered magnet, a magnet having a shape that is difficult to manufacture with a sintered magnet can be manufactured relatively easily. In particular, anisotropic bonded magnets manufactured using anisotropic magnetic powder can be expected to be applied to motors and the like because relatively high magnetic properties can be obtained. R-Fe-B anisotropic magnetic powder can be obtained by the HDDR method. The average particle diameter of anisotropic magnetic powder (HDDR magnetic powder) obtained by the HDDR method is usually in the range of several tens of μm to several hundreds of μm, and is kneaded with a binder resin and then molded. However, HDDR magnetic powder is easily cracked by the pressure applied during molding. As a result, the magnetic properties are deteriorated, and the bond magnet obtained by the conventional method can obtain only (BH) _{max of} about 60% of the magnetic powder used.

Furthermore, the conventional R—Fe—B anisotropic bonded magnet has a problem that the demagnetization curve (the second quadrant portion of the hysteresis curve) has poor squareness. This contributes to the deterioration of heat resistance, and high heat resistance cannot be obtained unless the coercive force H _cJ is set higher than that of the R—Fe—B based sintered magnet. However, if the coercive force H _cJ is increased, the magnetization characteristics are deteriorated, which places restrictions on the design of the magnetic circuit.

  As described in Patent Document 3 and the like, in a manufacturing method in which HDDR powder is oriented in a magnetic field and then bulked using a hot forming method such as hot pressing, the magnet shape is determined by the die shape. For this reason, the problem of shrinkage anisotropy, which is a problem with sintered magnets, is essentially difficult to occur. However, since the hot forming method is extremely poor in productivity, it causes an increase in manufacturing cost, and for example, it is difficult to mass-produce at a cost that can be used as a general-purpose motor.

  In the manufacturing method of Patent Document 4, the main phase is refined by subjecting the sintered body to HDDR treatment. However, in the HDDR reaction, a volume change occurs in the HD reaction or DR reaction, so that there is a problem that cracking is likely to occur when the sintered body is subjected to HDDR treatment, and production cannot be performed with a high yield. In addition, since the HDDR process is performed on the already densified bulk body (sintered body), the diffusion path of hydrogen, which is essential for the HD reaction, is limited, resulting in inhomogeneity of the structure in the magnet, The processing takes a long time, and as a result, the size of the magnet that can be produced is limited.

  Patent Document 5 describes that higher magnetic properties can be obtained than a general R—Fe—B sintered magnet. However, similar to a general sintered magnet, sintering can be performed at a high temperature of 1000 ° C. or higher. As a result, the anisotropy of shrinkage becomes apparent. For this reason, it has the same problem as a sintered magnet in that the shape that can be produced is limited. Furthermore, according to the study of the present inventor, if sintering is performed at 1000 ° C. or higher in the DR treatment, it is difficult to densify while maintaining fine crystal grains, and rather abnormal grain growth occurs remarkably. Therefore, there are many cases where the magnetic properties are deteriorated as compared with a normal sintered magnet.

  The method of Patent Document 6 is noted in that it can avoid the problems of conventional R—Fe—B based anisotropic bonded magnet manufacturing methods (decrease in magnetic properties and difficulty in orientation due to magnetic powder crushing during molding). Deserve. However, the green compact obtained after HDDR processing by this method has only a strength that does not collapse, and is difficult to handle after HDDR processing. In addition, it is essential to increase the mechanical strength with the bonding resin after the HDDR treatment.

  The present invention has been made to solve the above-mentioned problems, and a main object of the present invention is to exhibit high magnetic properties, particularly high squareness, as compared with a conventional bonded magnet, and a conventional sintered magnet. An object of the present invention is to provide a porous material for an R—Fe—B permanent magnet having a higher degree of freedom in shape.

  The method for producing a porous material for an R—Fe—B permanent magnet according to the present invention is selected from the group consisting of R—Fe—B rare earth alloy powders having an average particle size of less than 20 μm (where R is a rare earth element containing Y and Sc). Prepared at least one kind) (A), forming the green compact by molding the R-Fe-B rare earth alloy powder, and forming the green compact in hydrogen gas. On the other hand, a heat treatment is performed at a temperature of 550 ° C. or more and less than 650 ° C., thereby causing hydrogenation and disproportionation reaction, and 550 ° C. or more and less than 1000 ° C. with respect to the green compact in a vacuum or an inert atmosphere. (D) which heat-processes by the temperature of this, and raise | generates a dehydrogenation and a recombination reaction by it.

  In a preferred embodiment, the step (B) includes a step of performing molding in a magnetic field.

  In a preferred embodiment, the R—Fe—B rare earth alloy powder is 10 atomic% ≦ R ≦ 30 atomic%, 3 atomic% ≦ Q ≦ 15 atomic% (R is a rare earth element, Q is boron or boron and boron). The composition satisfies the relationship of the sum of carbons partially substituted).

In a preferred embodiment, when at least one transition metal element selected from the group consisting of Fe, Co, and Ni is T, at the start of the step (C), the following (1 ) The composition of the rare earth element R is set so that the rare earth amount R ′ represented by the formula R ′ ≧ 0 atomic%, and the amount of oxygen in the steps from the step (A) to the start of the step (C) ( O) is controlled.
(1) R ′ = “atomic% of R” − “atomic% of T” × 1 / 7− “atomic% of O” × 2/3

  In a preferred embodiment, the R—Fe—B rare earth alloy powder is a pulverized powder of a quenched alloy.

  In a preferred embodiment, the quenched alloy is a strip cast alloy.

  In a preferred embodiment, the step (C) includes a step of raising the temperature in an inert atmosphere or vacuum and a step of introducing hydrogen gas at a temperature of 550 ° C. or higher and lower than 650 ° C.

  In a preferred embodiment, the partial pressure of hydrogen gas in the step (C) is 1 kPa or more and 100 kPa or less.

  The porous material for an R—Fe—B permanent magnet of the present invention is obtained by any one of the production methods described above.

  The method for producing a composite bulk material for an R—Fe—B permanent magnet according to the present invention includes the step (E) of preparing the porous material for an R—Fe—B permanent magnet and the R—Fe—B by a wet treatment. A step (F) of introducing a material different from the R-Fe-B porous material into the pores of the -B porous material.

  The method for producing an R—Fe—B permanent magnet according to the present invention comprises a step of preparing a composite bulk material for an R—Fe—B permanent magnet obtained by the above production method, and the R—Fe—B permanent magnet. Forming the R—Fe—B permanent magnet by further heating the composite bulk material.

  The method for producing a composite bulk material for an R—Fe—B permanent magnet according to the present invention includes the step (E) of preparing the porous material for an R—Fe—B permanent magnet and the R—Fe—B permanent permanent material. A step (F ′) of introducing at least one of a rare earth metal, a rare earth alloy, and a rare earth compound into the surface of the porous material for magnet and / or inside the pores.

  In a preferred embodiment, the porous material for an R—Fe—B permanent magnet is heated simultaneously with the step (F ′) or after the step (F ′).

  In the method for producing an R—Fe—B permanent magnet according to the present invention, the R—Fe—B permanent magnet porous material is pressurized at a temperature of 600 ° C. or more and less than 900 ° C., and the R—Fe—B— A step of densifying the porous material for the B-based permanent magnet to 95% or more of the true density.

  In the present invention, the average particle size of the R—Fe—B rare earth alloy powder to be subjected to HDDR treatment is limited to less than 20 μm, and then the HDDR treatment is performed after producing a green compact of such powder. . Since the powder particles are relatively small, the uniformity of the HDDR reaction is improved and the mechanical strength after the HDDR treatment is sufficiently high. In the present invention, the green compact after HDDR treatment has sufficient strength as a porous material for permanent magnets, and can be used as it is as a bulk magnet body. This eliminates the need for crushing and crushing after the HDDR process and does not deteriorate the magnet characteristics, so that finally, the magnet characteristics superior to the conventional bonded magnet, particularly high squareness can be exhibited.

  Moreover, since the shrinkage when forming a porous material for a permanent magnet from a green compact by HDDR treatment is isotropic, the effect of improving the degree of freedom in shape design is also obtained as compared with conventional sintered magnets. .

  Conventional HDDR processing has been carried out in order to produce magnet powder for bonded magnets, and the processing target was powder having a relatively large average particle size. This is because when the average particle size is lowered, it becomes difficult to break up the powder aggregated by the HDDR process into discrete powder particles. On the other hand, as described in the prior art, it has been proposed to perform the HDDR process after forming the green compact, but in the green compact after the HDDR process, the bonding between the particles is smaller than that of a normal sintered magnet. The strength is low, and the brittleness that is difficult to handle as it is cannot be used as a bulk magnet body.

  The inventor dared to increase the mechanical strength of the green compact after the HDDR treatment without taking the approach of increasing the processing temperature of the HDDR as used in Patent Document 5 without using the approach. Decided to make it smaller. As a result, it was found that a porous material for permanent magnets having sufficiently high mechanical strength can be obtained by appropriately setting the average particle size of the powder particles and the HDDR treatment temperature, and the present invention has been completed.

The porous material for R—Fe—B permanent magnets obtained by the production method of the present invention has a texture of Nd ₂ Fe ₁₄ B type crystal phase having an average crystal grain size of 0.01 μm or more and 2 μm or less. The part is porous having pores having a major axis of 1 μm or more and 20 μm or less. The porous material of the present invention need not be entirely occupied by the porous portion. Here, the “porous portion” is a portion in which a texture and pores are mixed, and more specifically, an assembly of Nd ₂ Fe ₁₄ B type crystal phases having an average crystal grain size of 0.01 μm to 2 μm. This is a portion where a tissue and pores having a major axis of 1 μm or more and 20 μm or less exist. Such a porous portion preferably occupies a region of 20% or more, preferably 30% or more, more preferably 50% or more in terms of volume fraction with respect to the whole porous material.

  The “average crystal grain size” in this specification is an average size of fine crystal grains constituting the texture obtained by the HDDR process. The average crystal grain size of 2 μm or less is smaller than the average crystal grain size (over 3 μm) of the R—Fe—B based sintered magnet. In addition, the “major axis” in the present specification is the length of the longest straight line connecting two arbitrary points on the contour of the region constituting the pores of the “porous portion” described above. When the entire porous material is occupied by the porous portion, the major axis of the pores may be evaluated for an arbitrary region of the porous material, for example, the central portion of the porous material. On the other hand, when a part of the porous material is non-porous, a region included in the porous portion may be selected to evaluate the long diameter of the pores.

FIG. 1 is an SEM photograph showing a fracture surface of a porous material for an R—Fe—B permanent magnet obtained by the production method of the present invention in an example described in detail later. As can be seen from FIG. 1, the pores present in the porous material are voids that exist between the powder particles that are bonded to each other in the HDDR processing step, and communicate with each other in a three-dimensional network. The individual powder particles constituting the green compact are combined with the adjacent powder particles by the HDDR process to form a three-dimensional structure exhibiting rigidity, and within each powder particle, fine Nd ₂ Fe _{14 A} texture of B-type crystal phase is formed. In addition, the pores are not filled with resin and are in communication with the atmosphere.

The density (volume ratio of magnetic powder) of the porous material for R—Fe—B permanent magnet obtained by the production method of the present invention is equivalent to the density of the R—Fe—B bond magnet produced by conventional compression molding. Or less, that is, 3.5 g / cm ³ or more and 7.0 g / cm ³ or less. Even when there are gaps between the powder particles, the particles are bonded to each other, and sufficient mechanical strength and excellent magnetic properties are obtained. Demonstrate the characteristics.

As shown in FIG. 2, the porous material for R—Fe—B based permanent magnet obtained by the production method of the present invention is obtained by pulverizing a raw material alloy having an R—Fe—B phase and having an R of an average particle size of less than 20 μm. Step S10 for preparing a Fe—B rare earth alloy powder, Step S12 for compressing the powder to produce a green compact (molded body), and Step S14 for performing HDDR processing on the green compact. Manufactured by performing. The porous material for R—Fe—B permanent magnets obtained by the production method of the present invention applies a magnetic field in step S12, and orients the easy magnetization axis of the powder particles before HDDR treatment in a predetermined direction. Thus, the easy magnetization axis of the fine Nd ₂ Fe ₁₄ B type crystal phase in the texture formed by the HDDR process can also be oriented in a predetermined direction over the entire magnet.

  Next, with reference to FIGS. 3A and 3B, the change in the material structure before and after step S14 (HDDR processing) in FIG. 2 will be described.

  Fig.3 (a) is a schematic diagram of the green compact (molded object) obtained by process S12. The individual fine particles constituting the powder are pressed and compacted by molding, and for example, the particles A1 and the particles A2 are in contact with each other. In addition, voids B exist in the green compact.

FIG. 3B is a schematic view of the material after the HDDR process (S14) is performed on the green compact. The powder particles such as the particles A1 and A2 all have a texture composed of fine Nd ₂ Fe ₁₄ B type crystal phase having an average crystal grain size of 0.01 μm to 2 μm by the HDDR reaction. Individual particles (for example, particle A1) are strongly bonded to other particles (for example, particle A2) by diffusion of elements accompanying the HDDR reaction. In FIG. 3 (b), the connection part of the particles A1 and A2 is indicated by the reference symbol “C”.

As shown in FIG. 3B, the void B existing inside the green compact becomes smaller or disappears as the sintering proceeds along with the element diffusion described above. However, complete densification is not achieved by HDDR processing, and remains as “pores” after HDDR processing. In FIG. 3B, the major axis of the _pore is indicated by the symbol “d _pore ”. The average particle size of the powder particles can be evaluated by measuring the size d _{grain of} the portion sandwiched between the pores for each particle. Depending on the progress of the sintering, it may be difficult to accurately measure the average particle size of the powder particles in the porous portion shown in FIG. 3B, but according to the present invention, the density of the porous portion is Is in the range of 3.5 g / cm ³ or more and 7.0 g / cm ³ or less, as described above, the measured values of the long diameter and material density of the pores in the porous portion are within the above range. Thus, it is possible to evaluate whether or not the porous structure of FIG. 3B is formed. In the case where the void portion is actively used, such as for the purpose of introducing a different material described later, the density of the porous portion is more preferably 6.0 g / cm ³ or less, and 5.0 g / Cm ³ or less is more preferable. In the present invention, since the HDDR process is performed at a temperature lower than the temperature applied in the conventional manufacturing process of HDDR magnetic powder, the density of the porous portion can be reduced (pores can be enlarged), which is suitable for introduction of different materials. Used for.

In FIG. 3 (b), only the Nd ₂ Fe ₁₄ B type crystal phase having an average crystal grain size of 0.01 μm or more and 2 μm or less is drawn as a texture. May be included.

  In the present invention, unlike the bonded magnet, a resin for binding the powder particles is not required, and the magnet characteristics can be exhibited in a porous form in which voids between the powder particles form pores. The reason why sufficient mechanical strength can be obtained in spite of such voids is not always clear. Perhaps the powder particles used to form the green compact are small, and the reaction due to hydrogen diffusion during HDDR processing advances the sintering between the particles at a relatively low temperature, improving the bond strength between the particles. The reason is that it contributes.

  Conventionally, when the HDDR process is performed on the green compact, the powder particles aggregated by the HDDR process are crushed apart and then used for manufacturing a bonded magnet, or the green compact is impregnated with a resin and mechanically The strength was increased. The reason is that the mechanical strength of the green compact after the HDDR treatment is extremely low, and as such, it cannot be used as a magnet.

  In the present invention, by improving the mechanical strength, not only handling is easy, but also machining (cutting or grinding) for obtaining higher dimensional accuracy can be performed. For this reason, the porous material for R—Fe—B permanent magnets obtained by the production method of the present invention does not need to be impregnated with resin so as to fill the pores, and can be used as a permanent magnet as it is. .

  Since the porous material after HDDR treatment has a porous structure (open pore structure) communicating with the atmosphere, a composite bulk magnet can be easily produced by introducing a different material into the inside or the surface of the hole. Or the characteristics of the porous material can be improved.

  By hot-working the obtained porous material by a method such as hot pressing, it is possible to obtain a fluence bulk magnet while maintaining the excellent characteristics of the porous material. By applying these hot working to the composite material into which the above-mentioned different materials are introduced, for example, a composite magnet in which a hard magnetic phase and a soft magnetic phase are magnetostatically coupled can be obtained.

  According to the present invention, a high-performance composite magnetic component in which a soft magnetic yoke and a magnet are integrated by performing hot forming after combining a porous material for a permanent magnet with a molded body of a soft magnetic material. Can also be produced.

[Embodiment]
Hereinafter, preferred embodiments of the method for producing a porous material for an R—Fe—B permanent magnet according to the present invention will be described in detail.

<Starting alloy>
First, an RTQ-based alloy (starting alloy) having an R—Fe—B phase as a hard magnetic phase is prepared. Here, “R” is a rare earth element, and contains Nd and / or Pr of 50 atomic% (at%) or more. The rare earth element R in the present specification may include yttrium (Y) and scandium (Sc). “T” is at least one transition metal element selected from the group consisting of Fe, Co, and Ni, and is a transition metal element containing 50% or more of Fe. “Q” is B or a part of B and B substituted with C.

This RTQ-based alloy (starting alloy) contains an Nd ₂ Fe ₁₄ B type compound phase (hereinafter abbreviated as “R ₂ T ₁₄ Q”) in a volume ratio of 50% or more.

Most of the rare earth elements R contained in the starting alloy constitute R ₂ T ₁₄ Q, but some constitute R ₂ O ₃ and other phases. The composition ratio of the rare earth element R is preferably 10 atom% or more and 30 atom% or less, and more preferably 12 atom% or more and 17 atom% or less of the entire starting alloy. Moreover, the coercive force can be improved by setting a part of R to Dy and / or Tb.

The composition ratio of the rare earth element R is preferably set so that an “excess rare earth amount R ′” at the start of HD processing described later is 0 atomic% or more, and R ′ at the start of HD processing is 0.1 It is more preferable to set it to be at least atomic%, and it is even more preferable to set it to be at least 0.3 atomic%. Here, the “excess rare earth amount R ′” is calculated by the following equation.
R ′ = “atomic% of R” − “atomic% of T” × 1 / 7− “atomic% of O” × 2/3

Excess rare earth amount R ', among the rare earth elements R contained in R-T-Q based alloy (starting alloy), without configuring the R ₂ T ₁₄ B and _{R 2 O 3, R 2 T} 14 B and The composition ratio of rare earth elements existing in a form other than R ₂ O ₃ is shown. Unless the composition ratio of the rare earth element R is set so that the surplus rare earth amount R ′ at the start of HD processing is 0 atomic% or more, fine crystals having an average crystal grain size of 0.01 to 2 μm are formed by the method of the present invention. It becomes difficult to obtain. The rare earth element R may be oxidized by oxygen or moisture present in the atmosphere in the subsequent pulverization process or molding process. Oxidation of the rare earth element R causes a reduction in the surplus rare earth amount R ′. For this reason, it is preferable to perform the process up to the start of the HD process in an atmosphere in which the amount of oxygen (O) is suppressed as much as possible. However, since it is difficult to completely remove oxygen in the atmosphere, the starting alloy R The composition ratio is preferably set in consideration of a decrease in R ′ due to oxidation in a later step.

The upper limit of R 'is not particularly limited, considering the reduction in the corrosion resistance and B _r, preferably 8 atomic% or less, more preferably 5 atomic% or less, more preferably 3 atomic% or less, 2.5 atomic% The following is more preferable. It is preferable that R ′ is 8 atomic% or less and the composition ratio of the rare earth element R does not exceed 30 atomic%.

  The amount of oxygen (O) in the green compact at the start of the HD treatment is preferably suppressed to 1% by mass or less, and more preferably to 0.6% by mass or less.

  The composition ratio of Q is preferably 3 atom% or more and 15 atom% or less, more preferably 5 atom% or more and 8 atom% or less, and further preferably 5.5 atom% or more and 7.5 atom% or less.

  T occupies the remainder. As described above, T is at least one transition metal element selected from the group consisting of Fe, Co, and Ni, and is a transition metal element containing 50% or more of Fe. When a part of T is Co and / or Ni, it is desirable to select Co rather than Ni. Further, the total amount of Co with respect to the entire alloy is preferably 20 atomic percent or less, and more preferably 5 atomic percent or less, from the viewpoint of cost and the like. High magnetic properties can be obtained even when Co is not contained at all, but more stable magnetic properties can be obtained when Co of 0.5 atomic% or more is contained.

  In order to obtain effects such as improvement of magnetic characteristics, elements such as Al, Ti, V, Cr, Ga, Nb, Mo, In, Sn, Hf, Ta, W, Cu, Ag, Bi, Si, and Zr are appropriately added. May be. However, since an increase in the amount of addition causes a decrease in saturation magnetization in particular, the total amount is preferably 10 atomic% or less.

In the conventional HDDR magnet powder manufacturing method and the manufacturing method described in Patent Document 6, the average particle size of the magnet powder to be subjected to HDDR processing is 30 μm or more, typically 50 μm or more. In order for each particle of the magnet powder to exhibit excellent magnetic anisotropy after the HDDR treatment, it is necessary that the easy magnetization axes are aligned in one direction among the particles of the raw material powder. For this reason, the starting alloy in the stage before pulverization is prepared so that the average size of the region where the crystal orientations of R ₂ T ₁₄ Q are aligned in the same direction is larger than the average particle diameter of the pulverized powder particles. It was.

  As a result, in the conventional HDDR magnet powder production method and the method described in Patent Document 6, a raw material alloy is produced using a method such as a book mold method or a centrifugal casting method, and further subjected to a heat treatment such as a homogenization heat treatment. The crystal phase was growing.

However, according to the study by the present inventors, in the raw material alloy in which the crystal grain size of R ₂ T ₁₄ Q is increased by the book mold method or the centrifugal casting method, α-Fe that is the primary crystal of casting is completely removed. It has been found that α-Fe remaining in the raw material alloy has a bad influence on the magnetic properties after HDDR treatment.

In the manufacturing method of the present invention, since powder having an average particle size of less than 20 μm is used, the size of the region where the crystal orientations of R ₂ T ₁₄ Q in the raw material alloy are aligned in the same direction is the case of the conventional manufacturing method of HDDR magnet powder. There is no need to make it larger. Therefore, high anisotropy can be obtained after HDDR treatment even when an alloy (strip cast alloy) obtained by quenching and solidifying a molten alloy by a strip casting method is used. Further, by crushing such a rapidly cooled alloy into a powder, the amount of α-Fe can be reduced compared to a raw material alloy (starting alloy) by a conventional book mold method or the like, so that the magnetic properties after HDDR treatment are deteriorated. Can be suppressed, and good squareness can be obtained.

  Note that the porous material of the present invention can also be produced using a raw material alloy produced by a rapid cooling method (for example, an atomizing method) other than the strip casting method, a book mold method, a centrifugal casting method, or the like. In addition, for the purpose of homogenizing the structure of the raw material alloy, heat treatment may be performed on the raw material alloy before pulverization. Such heat treatment can be performed in a vacuum or inert atmosphere, typically at a temperature of 1000 ° C. or higher.

<Raw material powder>
Next, a raw material powder is produced by pulverizing the raw material alloy (starting alloy) by a known method. In the present embodiment, first, the starting alloy is coarsely pulverized using a mechanical crushing method such as a jaw crusher or a hydrogen occlusion pulverizing method to produce coarsely pulverized powder having a size of about 50 μm to 1000 μm. The coarsely pulverized powder is finely pulverized by a jet mill or the like to produce a raw material powder typically having an average particle size of less than 20 μm.

  In order to obtain a porous bulk material having sufficient mechanical strength, it is effective to optimize the average particle size of the raw material powder, but the alloy composition (particularly, the rare earth amount R and the excess rare earth amount R ′) and HDDR conditions It is also effective to adjust (especially HDDR temperature).

  From the viewpoint of handling, the average particle diameter of the raw material powder is preferably 1 μm or more. When the average particle size is less than 1 μm, the raw material powder easily reacts with oxygen in the air atmosphere, and the risk of heat generation and ignition due to oxidation increases. In order to make handling easier, it is preferable to set the average particle size to 3 μm or more. From the viewpoint of improving the mechanical strength of the molded article, the preferable upper limit of the average particle diameter is 9 μm, and the more preferable upper limit is 8 μm.

  The average particle size of the conventional HDDR magnet powder is over 20 μm, and usually about 50 to 500 μm. According to the study by the present inventors, when the HDDR treatment is performed on the raw material powder having such a large average particle diameter, sufficient magnetic properties (particularly high coercive force and demagnetization curve squareness) are obtained. In some cases, or the magnetic properties may become extremely low. The cause of the deterioration of the magnetic properties is due to the heterogeneity of the reaction during the HDDR process (particularly the HD reaction process), but the reaction becomes more easily heterogeneous as the size of the powder particles increases. When the reaction of HDDR proceeds inhomogeneously, the structure and crystal grain size become inhomogeneous inside the powder particles, or an unreacted portion is generated, resulting in deterioration of magnetic properties.

  In order to make the HDDR reaction proceed uniformly, it is effective to shorten the time required for the HDDR reaction, but if the reaction rate is increased by adjusting the hydrogen pressure or the like, the degree of crystal orientation will be lowered this time. . When the degree of crystal orientation is lowered, the anisotropy of the magnet powder is lowered, and as a result, high squareness cannot be obtained.

  In the present invention, the HDDR process is performed on the green compact formed by compressing the raw material powder. The inside of the green compact has a sufficiently large gap between the powder particles in which hydrogen gas can move and diffuse. It exists. In the present invention, since the raw material powder having an average particle diameter of typically 1 μm or more and less than 20 μm is used, it is easy for hydrogen to diffuse while reacting to the inside of the powder particles, and the HD reaction and The DR reaction can proceed in a short time. In this way, since the structure after HDDR is homogenized, high magnetic properties, particularly good squareness can be obtained, and the time required for the HDDR process can be shortened. Further, the HDDR treatment can be performed at a low temperature at which the reaction did not sufficiently proceed in the conventional HDDR magnetic powder manufacturing method.

<Molding of green compact>
Next, a green compact is formed using the above raw material powder. The step of forming the green compact is preferably performed in a magnetic field of 0.5 T to 20 T (static magnetic field, pulse magnetic field, etc.) by applying a pressure of 10 MPa to 200 MPa. By carrying out in a magnetic field, the easy magnetization axis of the fine Nd ₂ Fe ₁₄ B type crystal phase in the texture formed by the HDDR process is obtained by orienting the easy magnetization axis of the powder particles before the HDDR process in a predetermined direction. The axis can also be oriented in a predetermined direction throughout the magnet. Molding can be performed by a known powder press apparatus. Compact density (green density) when removed from the powder press device is 3.5g / cm ³ ~5.2g / cm ³ order.

  You may perform said shaping | molding process, without applying a magnetic field. When magnetic field orientation is not performed, an isotropic porous material is finally obtained. However, in order to obtain higher magnetic characteristics, it is preferable to execute a molding step while performing magnetic field orientation and finally obtain an anisotropic porous material.

  As described above, the starting alloy pulverization step and the raw material powder forming step described above are performed in order to prevent the amount of excess rare earth R ′ in the green compact immediately before the HD treatment from falling below 0 atomic%. It is preferable to carry out while suppressing oxidation. In order to suppress the oxidation of the raw material powder, it is desirable to perform each process and the handling between the processes in an inert atmosphere in which the amount of oxygen is suppressed as much as possible. A commercially available powder having R ′ of a predetermined value or more may be purchased and used after controlling each subsequent process and the handling atmosphere between the processes.

  Further, for the purpose of improving magnetic properties, etc., a mixture of other alloys may be finely pulverized before the starting alloy pulverization step, and the green compact may be formed after the fine pulverization. Alternatively, after the starting alloy is pulverized, powders of other metals, alloys and / or compounds may be mixed to produce a green compact. Furthermore, the green compact may be impregnated with a liquid in which another metal, alloy and / or compound is dispersed or dissolved, and then the solvent may be evaporated. The composition of the alloy powder when these methods are applied is desirably within the above-mentioned range as a whole of the mixed powder.

<HDDR processing>
Next, the HDDR process is performed on the green compact (molded body) obtained by the molding step.

  In the present embodiment, even if cracking occurs in the raw material powder particles during molding, the HDDR reaction is performed thereafter, so that the magnetic properties are not affected.

  The conditions for the HDDR process are appropriately selected depending on the alloy composition, the type and amount of the additive element, and can be determined with reference to the process conditions in the conventional HDDR method. In the present embodiment, since the green compact of relatively fine powder particles having an average particle diameter of 1 to 20 μm is used, the HDDR reaction can be completed at a low temperature where the reaction did not sufficiently proceed in the conventional HDDR magnetic powder manufacturing method. it can.

The temperature raising step for the HD reaction is performed in a hydrogen gas atmosphere with a hydrogen partial pressure of 1 kPa to 500 kPa, or a mixed atmosphere of hydrogen gas and an inert gas (Ar, He, etc.), an inert gas atmosphere, or a vacuum. . When the temperature raising step is performed in an inert gas atmosphere or vacuum, the following effects can be obtained.
(1) Suppression of green compact collapse due to hydrogen occlusion during temperature rise process (2) Suppression of magnetic property degradation due to difficulty in controlling reaction rate during temperature rise (3) Rare earth alloy with low melting point due to temperature rise And / or the rare earth compound is melted and the compaction of the green compact is advanced, and a high-strength porous material for a permanent magnet can be obtained.

  The HD treatment is performed at 550 ° C. or more and less than 650 ° C. in a hydrogen gas atmosphere having a hydrogen partial pressure of 1 kPa or more and 500 kPa or less or a mixed atmosphere of hydrogen gas and inert gas (Ar, He, or the like). The hydrogen partial pressure during HD processing is more preferably 1 kPa or more and 200 kPa or less. Furthermore, 10 kPa or more and 100 kPa or less are more preferable in order to control the reaction rate and suppress the decrease in anisotropy due to HDDR treatment. In the present embodiment, the HDDR reaction can be completed at a low temperature at which the reaction did not sufficiently proceed in the conventional HDDR magnetic powder manufacturing method. The treatment temperature is more preferably 600 ° C. or more and less than 650 ° C. The time required for HD processing is 5 minutes or more and 10 hours or less, and is typically set in the range of 10 minutes or more and 5 hours or less.

  When T in the RTQ-based alloy is 3 atomic percent or less with respect to the composition of the entire alloy, the hydrogen partial pressure during temperature rise and / or HD treatment is 5 kPa or more and 100 kPa or less, More preferably, by setting the pressure to 10 kPa or more and 50 kPa or less, a decrease in anisotropy in HDDR processing can be suppressed. In addition, it goes without saying that conditions such as changing the hydrogen partial pressure during HD processing stepwise can be adopted to optimize the HD reaction and obtain high characteristics.

  DR processing is performed after HD processing. The HD process and the DR process can be performed continuously in the same apparatus, but can also be performed discontinuously using separate apparatuses.

  The DR treatment is performed at 550 ° C. or more and less than 1000 ° C. in a vacuum or an inert gas atmosphere. However, in order to reduce residual hydrogen after the DR treatment and obtain high magnetic properties, it is more preferably performed at 650 ° C. or more and 1000 ° C. or less. preferable. The treatment time is usually 5 minutes or more and 10 hours or less, and is typically set in the range of 10 minutes or more and 5 hours or less. Needless to say, the atmosphere can be controlled stepwise (for example, the hydrogen partial pressure can be lowered stepwise or the reduced pressure can be lowered stepwise).

  A sintering reaction occurs throughout the HDDR process including the above-described temperature raising process before the HD reaction. For this reason, the green compact is a porous sintered material having pores having a major axis of 1 μm to 20 μm. The sintering mechanism generated at this time should be different from the sintering mechanism performed when manufacturing an ordinary R—Fe—B based sintered magnet, but the details are not clear at present.

  Due to the sintering reaction that occurs in the HDDR process, the green compact has a shrinkage ratio ((molded body size before HDDR treatment−molded body size after HDDR treatment) / molded body size before HDDR treatment × 100%). Although contracted to some extent, the anisotropy of the contraction is small. In this embodiment, the shrinkage ratio (shrinkage rate in the magnetic field direction / shrinkage rate in the mold direction) is about 1.1 to 1.6. For this reason, it becomes possible to manufacture porous materials having various shapes that were difficult to manufacture with conventional sintered magnets (typical shrinkage ratio is 2 or more).

  Since the entire HDDR process is performed in an atmosphere in which the amount of oxygen is reduced, the surplus rare earth amount R ′ immediately before the HD process described above is substantially equal to or more than R ′ immediately after the DR process. Therefore, by measuring R ′ immediately after the DR process, it is possible to confirm that the value of R ′ immediately before the HD process is greater than or equal to a desired value. However, since the surface layer of the porous material may be oxidized and blackened due to a trace amount of oxygen and moisture contained in the atmosphere during HDDR processing, R ′ immediately after the DR processing removes the oxidized surface layer. It is preferable to measure after

  In the present embodiment, since the HDDR process is performed on the green compact (molded body) after the molding process, the powder molding is not performed after the HDDR process. For this reason, the magnetic powder is not pulverized by the pressurization for molding after the HDDR treatment, and higher magnetic characteristics can be obtained as compared with the bonded magnet that compresses the HDDR powder. Thus, according to this embodiment, since the squareness of the demagnetization curve is improved, it is possible to achieve both magnetization and heat resistance.

  Furthermore, according to the present embodiment, the problems of orientation and residual magnetism of an anisotropic bonded magnet manufactured using a conventional HDDR powder are solved, and radial anisotropy and polar anisotropy can be imparted. it can. Further, there is no problem that the productivity inherent in the hot forming method is low.

  In addition, according to the present embodiment, the density of the green compact is improved while the HDDR reaction proceeds, so that problems such as cracking of the porous material due to the volume change due to the HD reaction or the DR reaction can be avoided. it can. Furthermore, since the HDDR reaction proceeds almost simultaneously on the surface and inside of the green compact, a large porous material can be easily produced.

<Heat compression treatment of porous material>
The porous material obtained by the above method can be used as it is as a bulk permanent magnet, but is further densified by using a heat compression treatment such as a hot press method to obtain a full-density magnet. You can also An example of a specific embodiment will be shown below for full condensation by heat compression treatment. Heat compression for the porous material can be performed using a known heat compression technique. For example, it is possible to perform a heat compression process such as hot pressing, SPS (spark plasma sintering), HIP, hot rolling and the like. Especially, the hot press and SPS which are easy to obtain a desired shape can be used suitably. In this embodiment, hot pressing is performed according to the following procedure.

  In this embodiment, a hot press apparatus having the configuration shown in FIG. 4 is used. This apparatus includes a die (die) 27 having an opening in the center, an upper punch 28a and a lower punch 28b for pressurizing a porous material, and drive units 30a and 30b for raising and lowering these punches 28a and 28b. It has.

A porous material (indicated by reference numeral “10” in FIG. 4) produced by the method described above is loaded into the mold 27 shown in FIG. At this time, it is preferable to perform loading so that the magnetic field direction (orientation direction) and the pressing direction coincide. The mold 27 and the punches 28a and 28b are formed of a material that can withstand the heating temperature and the applied pressure in the atmosphere gas to be used. Such a material is preferably a cemented carbide such as carbon or tungsten carbide. In addition, anisotropy can be increased by setting the outer dimension of the porous material 10 to be smaller than the opening dimension of the mold 27. Next, the mold 27 loaded with the porous material 10 is set in a hot press apparatus. The hot press apparatus preferably includes a chamber 26 that can be controlled to an inert gas atmosphere or a vacuum of 10 ⁻¹ Torr or more. In the chamber 26, for example, a heating device such as a carbon heater by resistance heating and a cylinder for pressurizing and compressing the sample are provided.

After filling the chamber 26 with a vacuum or an inert gas atmosphere, the mold 27 is heated by a heating device, and the temperature of the porous material 10 loaded in the mold 27 is raised to 600 ° C. to 900 ° C. At this time, the porous material 10 is pressurized with a pressure P of 0.1 to 3.0 ton / cm ² . The pressurization to the permanent magnet porous material 10 is preferably started after the temperature of the mold 27 reaches a set level. While maintaining the pressure at 600 to 900 ° C. for 10 minutes or more, it is cooled. After the magnet obtained by fluidization by heat compression is cooled to a low temperature (about 100 ° C. or less) that does not oxidize by contacting with the atmosphere, the magnet of this embodiment is taken out from the chamber. Thus, the R—Fe—B magnet of the present embodiment can be obtained from the above porous material.

  The density of the magnet thus obtained reaches 95% or more of the true density. In addition, according to the present embodiment, in the final crystal phase texture, the crystal grains in which the ratio b / a of the shortest grain size a to the longest grain size b of each crystal grain is less than 2 are 50 of the total crystal grains. It exists by volume% or more. In this respect, the magnet of the present embodiment is greatly different from the conventional anisotropic bulk magnet by hot plastic working described in, for example, Japanese Patent Laid-Open No. 02-39503. In such a crystal structure of a magnet, flat crystal grains in which the ratio b / a between the shortest particle diameter a and the longest particle diameter b exceeds 2 are dominant.

  Such heat compression treatment can be applied not only to the porous material used in the present embodiment, but also to a porous material in which a different material is introduced into the pores, which will be described later.

<Introduction of dissimilar materials into porous materials>
The pores of the R—Fe—B porous material obtained by the above-described method communicate with the atmosphere to the inside, and different materials can be introduced into the pores. As the introduction method, dry processing or wet processing is used. Examples of different materials include rare earth metals, rare earth alloys and / or rare earth compounds, iron and alloys thereof. An example of those specific embodiments is shown below.

(1) Introduction of dissimilar materials by wet treatment The wet treatment applied to the R-Fe-B porous material includes electrolytic plating treatment, electroless plating treatment, chemical conversion treatment, alcohol reduction method, metal carbonyl decomposition method, sol-gel method, etc. It can be done using the method. According to such a method, a film or a layer of fine particles can be formed on the surface of the porous material inside the pores by a chemical reaction. The wet treatment in the present invention can also be performed by preparing a colloidal solution in which fine particles are dispersed in an organic solvent and impregnating the pores of the R—Fe—B porous material. In this case, by evaporating the organic solvent of the colloidal solution introduced into the pores of the porous material, the pores can be covered with a layer of fine particles dispersed in the colloidal solution. When wet processing is performed by these methods, heat treatment or application of ultrasonic waves may be additionally performed in order to promote a chemical reaction or to ensure that fine particles are impregnated into the porous material.

  Hereinafter, the wet process performed using the colloidal solution will be described in detail.

  The fine particles to be dispersed in the colloidal solution can be produced by a known method such as a gas phase method such as a plasma CVD method or a liquid phase method such as a sol-gel method. When the fine particles are produced by adopting the liquid phase method, the solvent may be the same as or different from the solvent of the colloidal solution.

  The average particle diameter of the fine particles is preferably 100 nm or less. This is because if the average particle size exceeds 100 nm and becomes too large, it is difficult to penetrate the colloidal solution into the inside of the R—Fe—B based porous material. The lower limit of the particle size of the fine particles is not particularly limited as long as the colloidal solution is stable. In general, when the particle size of the fine particles is less than 5 nm, the stability of the colloidal solution often decreases. Therefore, the particle size of the fine particles is preferably 5 nm or more.

  The solvent in which the fine particles are dispersed is appropriately selected depending on the particle size, chemical properties, and the like of the fine particles, but it is preferable to use a non-aqueous solvent because the corrosion resistance of the R—Fe—B porous material is not high. In order to prevent aggregation of fine particles, a dispersant such as a surfactant may be contained in the colloidal solution.

  The concentration of the fine particles in the colloidal solution is appropriately selected depending on the particle size of the fine particles, the chemical properties, the type of the solvent and the dispersant, and is set within a range of, for example, about 1% by mass to 50% by mass.

  When the rare earth porous material is immersed in such a colloidal solution, the colloidal solution penetrates to the pores inside the rare earth porous material by capillary action. In order to perform the penetration (impregnation) of the colloidal solution into the porous material more reliably, it is useful to remove the air present in the pores inside the porous material. It is effective that the pressure is once reduced or reduced to a vacuum atmosphere and then returned to normal pressure or increased.

  In the porous material before the impregnation treatment, processing scraps such as grinding may possibly block pores on the surface of the porous material, and reliable impregnation may be prevented. For this reason, it is preferable to clean the surface of the porous material by ultrasonic cleaning or the like before the impregnation.

  After impregnating the porous material, the solvent in the colloidal solution is evaporated. The evaporation of the solvent varies depending on the type of the solvent and may be sufficiently evaporated in the air at room temperature. However, it is preferable to promote the evaporation by heating and / or reducing the pressure as necessary.

  The material introduced by the wet treatment does not need to fill the entire pores, and may be present on the pore surface, but it is preferable to cover at least the pore surface. In order to avoid oxidation of the porous material having a large surface area, these series of operations, particularly drying operations, are preferably performed in an inert gas atmosphere such as argon (or in a vacuum if possible) as much as possible. .

  Further, a porous material for permanent magnets is obtained by using a resin such as acrylic or urethane as a material different from the R—Fe—B based porous material, and impregnating the resin, and then curing the resin by a method such as heating. The environmental resistance can be improved.

  The R-Fe-B porous material in which a material different from the R-Fe-B porous material is introduced into the pores by wet processing is further subjected to heat treatment for the purpose of improving characteristics. You may carry out. The temperature of the heat treatment is appropriately set according to the purpose of heating. However, when the heating temperature is 1000 ° C. or higher, the texture in the R—Fe—B porous material becomes coarse and causes a decrease in magnetic properties. Therefore, the heating temperature is preferably less than 1000 ° C. The heating atmosphere is preferably performed in a vacuum or in an inert gas atmosphere such as Ar, from the viewpoint of suppressing deterioration in magnetic properties due to oxidation or nitridation of the R—Fe—B porous material.

Depending on the combination of the R—Fe—B based porous material and a different material, the R—Fe—B based porous material may not have an intrinsic coercive force (H _cJ ). A permanent magnet material capable of expressing an intrinsic coercive force (H _cJ ) of 400 kA / m or more can be produced by this step or heat compression treatment.

  The HD process and the DR process are not necessarily executed continuously. Further, a metal, an alloy and / or a compound as a different material may be introduced into the green compact after the HD treatment by the same method as described above, and then the DR treatment may be performed. In this case, the green compact after the HD treatment has progressed in diffusion bonding between particles, and the handling property is improved as compared with the green compact before the HD treatment. Therefore, the metal, alloy and / or compound can be easily added. Can be introduced.

  Further, when the above-described heat compression treatment is applied to the porous material (composite bulk material) after the wet treatment, a composite bulk magnet densified to 95% or more of the true density can be obtained.

  As mentioned above, although the method to introduce | transduce a dissimilar material by wet processing was described, when introduce | transducing rare earth elements as a dissimilar material, the method demonstrated below can be employ | adopted suitably.

(2) Introduction of rare earth element The rare earth metal, rare earth alloy, and rare earth compound introduced into the surface and / or pores of the R-Fe-B porous material are limited as long as they contain at least one kind of rare earth element. It will never be done. In order to effectively exhibit the effects of the present invention, it is desirable to include at least one of Nd, Pr, Dy, and Tb.

  There are various methods for introducing at least one of a rare earth metal, a rare earth alloy, and a rare earth compound into the surface and / or inside the pores of the R—Fe—B based porous material. It is not limited to this method. The introduction methods that can be used are roughly classified into dry processing and wet processing. Hereinafter, each method will be specifically described.

(A) Dry treatment As the dry treatment, a physical vapor deposition method such as a known sputtering method, vacuum vapor deposition method, or ion plating can be used. In addition, at least one powder of rare earth metal, rare earth alloy, rare earth compound (hydride, etc.) is mixed with an R—Fe—B porous material and heated to thereby convert the rare earth element into an R—Fe—B porous material. It may be diffused into the material. Further, as described in PCT / JP2007 / 53892, a method (vapor deposition diffusion method) in which rare earth elements are vaporized and evaporated from a rare earth-containing material and diffused into an R-Fe-B porous material is used. May be.

  The temperature of the porous material during the dry treatment may be room temperature or may be raised by heating. However, when the temperature is 1000 ° C. or higher, the texture in the R—Fe—B porous material becomes coarse and causes a decrease in magnetic properties. Therefore, the temperature of the porous material during the dry processing is set to less than 1000 ° C. It is preferable to do. By appropriately adjusting the temperature and time during the dry process, coarsening of the texture can be suppressed. Depending on the conditions of such heat treatment, the densification of the porous material may proceed. However, when heat treatment is performed so as to suppress the coarsening of the texture, pores remain in the porous material. For this reason, in order to fully condense, it is necessary to heat-treat the porous material while applying pressure.

  The atmosphere during the dry treatment is appropriately selected depending on the process to be applied. When oxygen or nitrogen is present in the atmosphere, there is a possibility that the magnetic properties are deteriorated due to oxidation or nitridation during the treatment. Therefore, the treatment is preferably performed in a vacuum or an inert atmosphere (such as argon).

(B) Wet treatment As the wet treatment, the above-described known methods can be used as appropriate. In particular, a method of preparing a liquid in which fine particles are dispersed in an organic solvent (hereinafter referred to as “treatment liquid”) and impregnating the pores of the R—Fe—B porous material can be suitably employed. In this case, the organic solvent of the colloidal solution introduced into the pores of the porous material can be evaporated to cover the pores with a fine particle layer dispersed in the treatment liquid. When wet processing is performed by these methods, heat treatment or application of ultrasonic waves may be additionally performed in order to promote a chemical reaction or to ensure that fine particles are impregnated into the porous material.

  The fine particles dispersed in the treatment liquid are produced by a known method such as a gas phase method such as a plasma CVD method or a liquid phase method such as a sol-gel method. When the fine particles are produced by adopting the liquid phase method, the solvent (dispersion medium) may be the same as or different from the solvent of the treatment liquid.

  The fine particles dispersed in the treatment liquid preferably contain at least one kind of rare earth oxide, fluoride, and oxyfluoride. In particular, when fluoride or oxyfluoride is used, the rare earth element can be efficiently diffused to the grain boundaries of the crystal grains constituting the porous material by heat treatment described later, and the effect of the present invention is great.

  The average particle diameter of the fine particles is preferably 1 μm or less. If the average particle diameter exceeds 1 μm and becomes too large, it becomes difficult to disperse the fine particles in the treatment liquid or it is difficult to penetrate the treatment liquid into the R-Fe-B porous material. is there. The average particle diameter is more preferably 0.5 μm or less, and further preferably 0.1 μm (100 nm) or less. The lower limit of the particle size of the fine particles is not particularly limited as long as the treatment liquid is stable. Generally, when the particle size of the fine particles is less than 1 nm, the stability of the treatment liquid often decreases. Therefore, the particle size of the fine particles is preferably 1 nm or more, more preferably 3 nm or more, and more preferably 5 nm or more. More preferably it is.

  The solvent (dispersion medium) for dispersing the fine particles is appropriately selected depending on the particle size, chemical properties, etc. of the fine particles, but the non-aqueous solvent is used because the corrosion resistance of the R—Fe—B porous material is not high. Is preferred. In order to prevent aggregation of the fine particles, a dispersant such as a surfactant may be included in the treatment liquid, or the fine particles may be surface-treated in advance.

  The concentration of the fine particles in the treatment liquid is appropriately selected depending on the particle size of the fine particles, the chemical properties, the kind of the solvent and the dispersant, and is set within a range of, for example, about 1% by mass to 50% by mass.

  When the rare earth porous material is immersed in such a treatment liquid, the treatment liquid penetrates to the pores inside the rare earth porous material by capillary action. In order to more reliably infiltrate (impregnate) the treatment liquid into the porous material, it is useful to remove the air present in the pores inside the porous material. It is effective to carry out under normal pressure or pressurization after temporarily reducing the pressure or vacuum atmosphere.

  In the porous material before the impregnation treatment, processing scraps such as grinding may possibly block pores on the surface of the porous material, and reliable impregnation may be prevented. For this reason, it is preferable to clean the surface of the porous material by ultrasonic cleaning or the like before the impregnation.

  After impregnating the porous material, the solvent (dispersion medium) in the processing liquid is evaporated. The evaporation of the solvent varies depending on the type of the solvent and may be sufficiently evaporated in the air at room temperature. However, it is preferable to promote the evaporation by heating and / or reducing the pressure as necessary.

  The material introduced by the wet treatment does not need to fill the entire pores, and may be present on the pore surface, but it is preferable to cover at least the pore surface.

  By the above method, the R-Fe-B porous material having a rare earth element introduced on the surface and / or inside the pores is further subjected to heat treatment for the purpose of improving the characteristics, particularly the coercive force. You may do it. The temperature of the heat treatment is appropriately set according to the purpose of heating. However, when the heating temperature is 1000 ° C. or higher, the texture in the R—Fe—B porous material becomes coarse and causes a decrease in magnetic properties. Therefore, the heating temperature is preferably less than 1000 ° C. The heating atmosphere is preferably performed in a vacuum or in an inert gas atmosphere such as Ar, from the viewpoint of suppressing deterioration in magnetic properties due to oxidation or nitridation of the R—Fe—B porous material.

Depending on the combination of the R—Fe—B based porous material and the rare earth metal, rare earth alloy, and / or rare earth compound, the R—Fe—B based porous material may have an intrinsic coercive force (H _cJ ) may not be provided, and in this case, a permanent magnet material capable of _exhibiting a high intrinsic coercive force (H _cJ ) can be _obtained by this step or the heat compression treatment described later.

  As described above, the introduction of the rare earth element by the dry process or the wet process does not necessarily need to continuously execute the HD process and the DR process. Furthermore, the rare earth element may be introduced into the green compact after the HD treatment by the same method as described above, and then the DR treatment may be performed. In this case, the green compact after the HD treatment has progressed in diffusion bonding between particles, and the handling property is improved as compared with the green compact before the HD treatment. Therefore, the metal, alloy and / or compound can be easily added. Can be introduced.

  Moreover, when the above-described heat compression treatment is applied to the porous material (composite bulk material) after the rare earth introduction treatment, a composite bulk magnet densified to 95% or more of the true density can be obtained.

  Ultimately, a magnetizing step for expressing a high intrinsic coercive force, which is one of the effects of the present invention, is performed, but the timing for performing the magnetizing step is preferably after the wet processing. When performing a heat compression process, it is preferable to carry out after the process.

  In addition, after pulverizing and pulverizing the porous material for permanent magnets, the flude magnet, the composite magnet, and the like obtained by the above-described method, it can be used as a raw material powder such as a bond magnet.

<Composite parts using porous materials>
Various composite parts can be produced by using the porous material obtained by the present invention. As one application example, a rare earth magnet compact and a soft magnetic material powder are obtained by hot press-molding (heating and compressing) a porous material and a soft magnetic material powder in a powder state or a temporary compact of the soft magnetic material powder. A specific embodiment of a method for obtaining a molded part in which the molded body is integrated will be described.

  In the present embodiment, porous materials 12a ′ and 12b ′ having the shape shown in FIG. 5A are prepared by the above-described method, while soft magnetic material powder (for example, soft magnetic metal powder such as iron powder) is separately prepared. ) Is press-molded to produce a soft magnetic material powder temporary compact 22 'shown in FIG. 5 (b). This step can be performed by a known press molding method. A preferable pressure is 300 MPa or more and 1 GPa or less. At this time, the density (bulk density) of the temporary molded body 22 'of the soft magnetic material powder is preferably in the range of about 70% to about 90% of the true density, and more preferably about 75% to about 80%. preferable. If the pressure is lower than the above range, the amount of deformation (shrinkage) in the integration process by hot pressing becomes excessive, and the relative position of the magnet part and soft magnetic part will shift, so magnetic circuit parts with high dimensional accuracy. May be difficult to mold. On the other hand, if the pressure is higher than the above range, sufficient bonding strength may not be obtained in the subsequent integration step. The molding temperature is preferably about 15 ° C. or more and about 40 ° C. or less, and it is not necessary to perform heating or cooling. The atmosphere is preferably performed in an inert gas (including rare gas and nitrogen) atmosphere in order to prevent oxidation of the rare earth magnet powder.

  According to the manufacturing method of the present invention, the deformation amount (volume change rate) in the integration step is 30% or less, and a magnetic circuit component can be manufactured with high dimensional accuracy. As described above, after preparing a plurality of porous materials 12a ′, 12b ′ and a temporary molded body 22 ′ of soft magnetic material powder, as shown in FIG. 5C, the porous materials 12a ′, 12b ′ and The soft magnetic material powder temporary compact 22 'is set in a mold and hot press-molded. By this hot pressing, the porous materials 12a 'and 12b' are compressed and changed into magnet molded bodies 12a and 12b with improved density. In this way, a rotor (magnetic circuit component) 100 in which a plurality of magnet molded bodies 12a, 12b and a molded body 22 of soft magnetic material powder are integrated as shown in FIG. 6 is obtained.

  A preferable pressure in the above hot press molding is 20 MPa or more and 500 MPa or less. When the pressure is lower than the above range, the bonding strength between the magnet part and the soft magnetic material powder compact may not be sufficiently obtained. If the pressure is higher than the above range, the press device itself may be deformed in the hot press process, and a large-scale device is required to prevent this, leading to an increase in manufacturing cost. is there. The molding temperature is preferably 400 ° C. or higher and lower than 1000 ° C., more preferably 600 ° C. or higher and 900 ° C. or lower, and most preferably 700 ° C. or higher and 800 ° C. or lower. When the molding temperature is lower than 400 ° C., the magnet compact and the soft magnetic material powder compact may not be sufficiently densified. On the other hand, when the molding temperature is 1000 ° C. or higher, the crystal grains become coarse and the magnetic properties of the porous material may be deteriorated. Further, the time for holding at the above temperature and pressure (hereinafter referred to as “molding time”) is preferably 10 seconds or longer and 1 hour or shorter, and is a short time of 1 minute or longer and 10 minutes or shorter from the viewpoint of productivity. More preferably. Of course, the molding time is appropriately set in relation to the molding temperature and the molding pressure. However, if the molding time is shorter than 10 seconds, the compact may not be sufficiently densified, and more than 1 hour. If the length is long, the magnetic properties may deteriorate due to the coarsening of crystal grains. In addition, the hot pressing step is preferably performed in an inert gas (including rare gas and nitrogen) atmosphere in order to prevent oxidation of the porous material.

  The density of the magnet compacts 12a and 12b in the rotor 100 thus obtained is about 95% or more of the true density, and the density of the compact 22 of the soft magnetic material powder is about 95% or more of the true density. Here, an example in which the soft magnetic material powder temporary molded body 22 ′ is formed in advance separately from the porous materials 12a ′ and 12b ′ and then integrated by hot pressing is described. It is also possible to integrate the porous materials 12a ′ and 12b ′ and the soft magnetic material powder in a powder state by hot press molding without previously forming the temporary powder compact 22 ′. However, in order to obtain a magnetic circuit component with high dimensional accuracy, as described above, a process in which a temporary molded body of a soft magnetic component and a porous material are produced in advance and then integrated is preferable.

[Example 1]
An alloy having the composition shown in Table 1 below (target composition: Nd _15.9 Fe _bal Co _1.0 B _6.2 Al _0.5 Cu _0.1 Ga _0.1 (atomic%)) was prepared, and the porous structure for rare earth permanent magnets was manufactured by the manufacturing method of the above-described embodiment. A quality material was produced. The unit of numerical values in Table 1 is mass%. Hereinafter, a manufacturing method of this example will be described.

First, a rapidly solidified alloy having the composition shown in Table 1 was produced by strip casting. The obtained rapidly solidified alloy was coarsely pulverized into a powder having a particle size of 425 μm or less by the hydrogen occlusion / disintegration method, and then the coarse powder was finely pulverized using a jet mill to obtain a fine powder having an average particle size of 4.3 μm. The “average particle size” is a 50% volume center particle size (D ₅₀ ) in a laser diffraction type particle size distribution measuring apparatus (manufactured by Sympatec, HEROS / RODOS).

The fine powder was filled in a mold of a press machine, and a green compact was produced by applying a pressure of 20 MPa in a direction perpendicular to the magnetic field in a magnetic field of 1.5 Tesla (T). The density of the green compact was calculated to be 3.95 g / cm ³ based on dimensions and unit weight.

Next, the above-mentioned HDDR process was performed on the green compact. Specifically, the green compact is heated to 600 ° C. in an argon flow of 100 kPa (atmospheric pressure), and then the atmosphere is mixed gas flow (total atmospheric pressure) of H ₂ partial pressure 33 kPa + Ar partial pressure 67 kPa. After switching, the hydrogenation / disproportionation reaction was carried out at 600 ° C. for 4 hours. Thereafter, the temperature was raised to 700 ° C., and kept for 4 hours in an argon flow reduced to 5.3 kPa to perform dehydrogenation / recombination treatment. Next, it cooled to room temperature in atmospheric pressure Ar flow, and the sample of the Example was obtained.

  The dimensions of the sample thus obtained were measured and compared with the dimensions before the heat treatment. The shrinkage ratio in the magnetic field direction and the shrinkage ratio in the mold direction were calculated and the shrinkage ratio was determined to be 1.31. Here, the shrinkage rate (%) is represented by (size before heat treatment−size after heat treatment) ÷ size before heat treatment × 100, and the shrinkage ratio is (shrinkage rate in the magnetic field direction / shrinkage rate in the mold direction). It is represented by

  Further, the result of measuring the oxygen content in the sample immediately after the DR treatment was 0.62% by mass, and the surplus rare earth content R ′ obtained from Nd, Fe, and Co in Table 1 was 2.82 atomic%.

A surface perpendicular to the magnetic field application direction of the sample was evaluated with an X-ray diffractometer. As a result, it was confirmed that it had an Nd ₂ Fe ₁₄ B phase and the easy magnetization axis direction was oriented in the magnetic field direction. Further, the fracture surface of the sample was observed with a scanning electron microscope (SEM). FIG. 7 is an SEM photograph showing a fracture surface of the sample. 7 is different from FIG. 1 in the magnification. In FIG. 7, powder particles A bonded to each other and voids B (pores having a major axis of 1 μm to 20 μm) positioned between the powder particles A are shown. The powder particle A has a texture of an Nd ₂ Fe ₁₄ B type crystal phase having an average crystal grain size of 0.01 μm or more and 2 μm or less inside. The powder particles A in FIG. 7 correspond to the powder particles A1 and A2 schematically shown in FIG. 3B, and the void B in FIG. 7 corresponds to the void B in FIG. 3B. . Further, a region C in FIG. 7 corresponds to the particle coupling portion C in FIG.

  As is apparent from FIG. 7, the material of the example has a porous structure in which pores of 1 μm to 20 μm are dispersed. Such a porous structure is formed by sintering powder particles having an average particle size of less than 20 μm, but unlike a normal sintered magnet, it is not densified and has a low density. Such a structure can be obtained by carrying out the HDDR treatment at a temperature sufficiently lower than the normal sintering temperature (about 1100 ° C.). If the DR treatment is performed at a high temperature (1000 to 1150 ° C.), the density of the sintered body is improved and a porous material cannot be obtained. Further, when the DR treatment is performed at such a high temperature, the grain growth proceeds to an abnormal level, and there is a high possibility that the magnet characteristics are greatly deteriorated.

  In the sample of this example, unlike the ordinary sintered magnet, the HDDR process proceeds during the sintering process, so that a texture composed of a fine crystal phase of 0.01 μm to 2 μm is formed inside each powder particle. The

  Further, the texture constituting the powder particles in FIG. 7 is composed of a region composed of relatively angular fine crystals, such as region a, and a relatively rounded microcrystal, such as region a ′. Two types of aspects are observed. When compared with the conventional HDDR magnetic powder as described in Patent Document 1, the relatively rounded fine crystals such as the region a ′ are not crushed after HDDR processing in the conventional HDDR magnetic powder. Consistent with the individual particle surface aspects of On the other hand, a region composed of relatively square crystals such as region a corresponds to the aspect of the fracture surface of individual particles when the powder is crushed after HDDR processing in the conventional HDDR magnetic powder. In view of these points, the region a in FIG. 7 is the form of the fracture surface (that is, the inside of the powder particle) of the individual powder particles combined by the HDDR process, and the region a ′ is the compact. It turns out that it is the form of the particle | grain surface after the HDDR process of each powder particle which comprised the body. In the fracture surface of the sample, such an embodiment having two fine crystal forms of a and a ′ is a permanent product obtained by the HDDR treatment of the production method of the present invention, that is, a powdered green compact. This is one of the characteristics of the porous material for magnets.

  Next, the surface of the sample was ground with a surface grinder and processed into a prism having a size of 10 × 11 × 12 mm.

  Note that no cracking or chipping of the sample due to polishing was observed.

The density of the sample was calculated from the sample dimensions and unit weight to be 4.56 g / cm ³ . The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 2.

In Table 2, J _max is the maximum measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, and the higher the H _k / H _cJ , the better the squareness of the demagnetization curve. H _k / H _cJ of an anisotropic bonded magnet manufactured using ordinary HDDR magnetic powder is 0.6 or less, but as shown in Table 2, the sample obtained in the present invention is H _k / H _cJ was 0.69, and it was confirmed that the squareness was excellent.

[Example 2]
The porous material of Example 1 was pulverized in a mortar and classified in an argon atmosphere to prepare a powder having a particle size of 75 to 300 μm. This powder was put into a cylindrical holder and fixed with paraffin while being oriented in a magnetic field of 800 kA / m. The obtained sample was magnetized with a pulse magnetic field of 4.8 MA / m, and the magnetic properties were measured with a vibrating sample magnetometer (VSM: device name VSM5 (manufactured by Toei Kogyo Co., Ltd.)). Note that demagnetizing field correction is not performed. Table 3 shows the measurement results.

J _max and B _r in the table, the true density of the samples was determined by calculation as being 7.60 g / cm ^3. Note that J _max is a measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample, taking into account the mirror image effect in VSM measurement. This is a corrected value. Thus, the magnet powder obtained by pulverizing the porous material also exhibits excellent magnetic properties. Such magnet powder is suitably used for bonded magnets.

As can be seen from the measurement and observation results regarding each of the above examples, the porous material for permanent magnets of the present invention is excellent in the squareness of the demagnetization curve. Further, the anisotropy of shrinkage during the heat treatment is as small as 1.31 (normal sintered magnets are 2 or more). Moreover, it has the strength which can be machined sufficiently, and can be used as a bulk magnet body without performing resin impregnation as it is. Furthermore, even if the porous material is pulverized and pulverized, the coercive force H _{cJ does not} decrease much and can be used as magnetic powder for bonded magnets.

[Example 3]
In this example, the density of the porous material of Example 1 was increased using the hot press apparatus shown in FIG. Specifically, the porous material of Example 1 was prepared, the porous material was ground, and then set in a carbon die. This die was set in a hot press apparatus and compressed in a vacuum at 700 ° C. under a pressure of 50 MPa.

The density of the fluence magnet after hot pressing was 7.58 g / cm ³ . The magnetic properties of the fluence magnet were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Engineering Co., Ltd.)). The results are shown in Table 4. J _max is the maximum measured value of the magnetization J (T) of the sample when the external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample.

  From the above results, by using the manufacturing method of the present invention, the squareness of the demagnetization curve is excellent, and the shrinkage anisotropy during heat treatment is as small as 1.31 (normal sintered magnets are 2 or more) A porous material was obtained. Further, this porous material had a strength sufficient for machining. In addition, since it has crystal grains that are one or more orders of magnitude larger than a sintered magnet, there is little decrease in magnetic properties due to surface deterioration when processed into a thin object. Furthermore, high density can be easily achieved by heat compression such as hot pressing and hot rolling.

  As described above, if the porous material according to the present invention is heated and compressed to increase the density, the following advantageous effects can be obtained as compared with the prior art.

  (1) Since the raw material powder having an average particle size of 20 μm or less is used, the contact area between the magnetic powders is increased as compared with the case of using conventional HDDR magnetic powders. The press pressure during molding can be reduced, and industrial mass productivity is excellent. Further, by suppressing the density of the green compact, it is possible to increase the density of the green compact and to suppress the orientation disturbance that occurs.

  (2) Since the magnetic powder before the HDDR treatment has a low coercive force, it is easy to demagnetize the green compact by forming it in a magnetic field to produce a green compact. Further, since the green compact is completely demagnetized by the HDDR process, it is possible to perform heat compression (hot working) in a state in which handling is easy.

  (3) Since the porous material obtained after the HDDR reaction has such a strength that it can be machined, it becomes a die (die) at the time of heat compression required for a full-fluid magnet using conventional HDDR magnetic powder. Is not necessarily required. In addition, since it is possible to obtain an already oriented material at the porous material stage, it is not necessary to make it anisotropic by magnetic field orientation or hot plastic working in the mold immediately before heat compression. For this reason, it is possible to obtain a magnet having excellent industrial mass productivity and higher magnetic characteristics and design freedom.

  (4) Since the porous material used in the present invention exhibits better squareness than conventional HDDR magnetic powder, it can maintain good squareness even after heat compression for full condensation.

  (5) In the heating and compression process, even when anisotropy by hot plastic working is applied, a magnet having higher anisotropy can be obtained with higher productivity than using conventional magnetic powder.

[Example 4]
First, porous materials 12a ′ and 12b ′ were obtained by the same method as described in Example 1. In this embodiment, as shown in FIGS. 8A to 8D, “hot press molding” is performed on the porous materials 12a ′ and 12b ′ and the iron core temporary molded body 22 ′. .

  The hot press apparatus shown in FIG. 8A includes a die 32 having a hole capable of forming a cavity having a predetermined shape, and lower punches 42a and 42b capable of moving in the hole of the die 32. A center shaft 42c, a lower ram 52 that supports them and can move up and down as needed, and upper punches 44a and 44b that can move in the holes of the die 32, and support them as needed. The upper ram 54 is movable up and down accordingly. The lower punch 42a and the upper punch 44a are for pressing the porous material 12a'12b ', and the lower punch 42b and the upper punch 44b are for pressing the iron core temporary molded body 22'. In this way, by using a press device (sometimes called a “multi-axis press device”) that can pressurize the porous material 12a′12b ′ and the iron core temporary molded body 22 ′ independently. It is preferable because a pressure process suitable for each temporary molded body can be performed and the difference in the amount of compressive deformation between the temporary molded bodies, which is large in the initial stage of compression, can be absorbed. Although not shown in the figure, the hot press device includes a heating device, and the lower ram 52, the die 32, the upper and lower punches 42a, 42b, 44a, 44b, and the center shaft 42c are heated to a predetermined temperature. The

  First, as shown in FIG. 8A, the porous materials 12 a ′ and 12 b ′ and the iron core temporary molded body 22 ′ are assembled at predetermined positions on the die 32. At this time, the porous materials 12a ′ and 12b ′ and the iron core temporary molded body 22 ′ are assembled as shown in FIG. 5C, and the center shaft 42c passes through the hole 22a ′ of the iron core temporary molded body. .

  Next, as shown in FIG. 8B, the lower punches 42a and 42b and the upper punches 44a and 44b are moved up and down, and the assembled porous materials 12a 'and 12b' and the iron core temporary molded body 22 ' Is inserted into a cavity formed in the die 32. Thereafter, the temperature of the cavity is maintained at about 800 ° C., for example.

Next, as shown in FIG. 8C, the porous materials 12a ′ and 12b ′ and the iron core temporary molded body 22 ′ are moved by moving the lower punches 42a and 42b and the upper punches 44a and 44b up and down. Pressurize. The pressure is ² ton / cm ² and the pressure is applied for 5 minutes.

  Next, as shown in FIG. 8D, the magnet parts 12a and 12b and the iron core (soft magnetic part) 22 are integrated by moving the lower punches 42a and 42b and the upper punches 44a and 44b up and down. The obtained rotor 100 is taken out from the die 32.

  Thereafter, the rotor 100 is obtained by cooling to room temperature. After this, there is no need to perform a sintering process.

The density of the magnetic parts 12a and 12b prototyped by the above manufacturing method is, for example, 7.4 g / cm ³ , which is 97.4% of the true density (7.6 g / cm ³ ), which is equal to the density of a normal sintered magnet. Met. The density of the iron core 22 was 7.7 g / cm ³ , which was 98.7% of the true density (7.8 g / cm ³ ).

  The prototyped rotor did not break even at 33,000 revolutions, for example, and had sufficient joint strength. The joint strength between the magnet parts 12a and 12b and the iron core 22 measured by the shear test was 57 MPa. The surface magnetic flux density was 0.42T.

  In addition, in order to further improve the mass productivity, the following process can be performed.

  First, the assembly process shown in FIG. 8A is performed in a die and punch set prepared separately from the hot press apparatus, and preliminarily heated to a temperature at which crystal growth does not occur (for example, about 600 ° C.). To do. After reaching a predetermined temperature, the set is moved to a hot press machine where the temperature is raised to an optimum temperature (for example, 800 ° C.) in a short time by high-frequency induction heating or current heating, and then the press is integrated for a short time. I do. In addition, a plurality of die and punch sets are prepared, and a plurality of treatments are continuously performed using, for example, a pusher furnace method in a reduced pressure or inert gas atmosphere from the preliminary heating step to the integrated pressing step. More efficient production is possible.

[Example 5]
First, the same porous material as the porous material of Example 1 is prepared. Next, this porous material was processed into a size of 7 mm × 7 mm × 5 mm by a peripheral blade cutting machine and a grinding machine. No cracking or chipping of the porous material due to this processing was observed. After performing ultrasonic cleaning on the porous material, the porous material was immersed in the nanoparticle-dispersed colloidal solution. This colloidal solution was a colloidal solution in which Co nanoparticles were dispersed. The average particle diameter of Co particles was about 10 μm, the solvent was tetradecane, and the solid content concentration was 60% by mass. The nanoparticle-dispersed colloid solution was placed in a glass container, inserted into a vacuum desiccator with the porous material immersed therein, and placed under reduced pressure. The atmospheric pressure during the treatment was adjusted to about 130 Pa.

  Bubbles were generated in the porous material and the nanoparticle-dispersed colloidal solution due to the reduced pressure. After the generation of bubbles stopped, the pressure was returned to atmospheric pressure. Thereafter, the porous material was inserted into a vacuum dryer, heated to 200 ° C. under an atmospheric pressure of about 130 Pa, the solvent was evaporated, and drying was performed. Thus, a sample of the composite bulk material according to the present invention was obtained.

The composite bulk material obtained by the above method was set in a hot press apparatus and compressed in a vacuum at a pressure of 50 MPa under a condition of 700 ° C. The density of the fluence composite bulk magnet after hot pressing was 7.73 g / cm ³ .

  The sample of this example was magnetized with a 3.2 MA / m pulse magnetic field, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (Metron Giken Co., Ltd.)). The results are shown in Table 5.

  In this example, the entire porous material was immersed in the nanoparticle-dispersed colloidal solution. However, since the solution can penetrate into the porous material using capillary action, only a part of the porous material is used. It may be immersed in the nanoparticle-dispersed colloidal solution.

First, a porous material was produced by the same method as in Example 1 above. Here, as a reference example, a magnet that was fully condensed by a hot forming method was produced as it was without impregnating the porous material, and the characteristics were evaluated. Specifically, the porous material obtained by the above method was set in a hot press apparatus, and compressed at a pressure of 50 MPa in a vacuum at 700 ° C. The density of the fluence magnet after hot pressing was 7.58 g / cm ³ . After magnetizing the obtained full-density magnet with a pulse magnetic field of 3.2 MA / m or more, the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken Co., Ltd.). Table 6 shows.

As can be seen from the above results, in the composite bulk magnet (composite magnet) produced by using the method of the present invention, a reference example in which the porous material is fully formed by hot forming without impregnation treatment is used. The residual magnetic flux density _Br was improved as compared with the magnets. Further, in the examples, no inflection point is observed in the demagnetization curve in the easy magnetization direction, and the composite bulk magnet is a composite in which a hard magnetic phase (Nd ₂ Fe ₁₄ B type compound) and a soft magnetic phase (metal nanoparticles) are mixed. It was confirmed to operate as a magnet.

[Example 6]
First, the same porous material as the porous material of Example 1 is prepared. Next, this porous material was processed into a size of 20 mm × 20 mm × 20 mm by a peripheral blade cutting machine and a grinding machine. No cracking or chipping of the porous material due to this processing was observed. After performing ultrasonic cleaning on the porous material, the porous material was immersed in the DyF ₃ fine particle dispersion. This is a liquid in which DyF ₃ fine particles having a particle diameter of 0.05 to 0.5 μm are dispersed in dodecane. The DyF ₃ fine particle dispersion was placed in a glass container, inserted into a vacuum desiccator with the porous material immersed therein, and placed under reduced pressure. The atmospheric pressure during the treatment was adjusted to about 130 Pa.

Bubbles were generated in the porous material and the DyF ₃ fine particle dispersion due to the reduced pressure. After the generation of bubbles stopped, the pressure was returned to atmospheric pressure. Thereafter, the porous material was inserted into a vacuum dryer, heated to 200 ° C. under an atmospheric pressure of about 130 Pa, the solvent was evaporated, and drying was performed. Thus, a sample of the composite bulk material according to the present invention was obtained.

The composite bulk material obtained by the above method was set in a hot press apparatus and compressed in a vacuum at a pressure of 50 MPa under a condition of 700 ° C. The density of the fluence composite bulk magnet after hot pressing was 7.55 g / cm ³ .

  Thereafter, the obtained flude composite bulk magnet was heated at 800 ° C. for 3 hours and then cooled.

  The sample of this example was magnetized with a 3.2 MA / m pulse magnetic field, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (Metron Giken Co., Ltd.)). The results are shown in Table 7.

In this example, the entire porous material was immersed in the DyF ₃ fine particle dispersion. However, since the solution can penetrate into the porous material using capillary action, only a part of the porous material is used. DyF ₃ may be immersed in the fine particle dispersion.

As can be seen from the above results, in the composite bulk magnet produced using the method of the present invention, the porous material was not impregnated, and compared with the magnet of the reference example which was fluoridized by hot forming as it was. Thus, the intrinsic coercive force H _cJ is improved.

[Example 7]
Rapidly solidified alloys B to F having the target compositions shown in Table 8 below were produced by strip casting. The obtained rapidly solidified alloy was coarsely pulverized and finely pulverized and molded in a magnetic field using the same method as in Example 1 to produce a green compact having a density of 4.18 to 4.22 g / cm ³ . . The average particle diameter of the fine powder is as shown in Table 8 (the measurement method is the same as in Example 1, and the 50% center particle diameter (D ₅₀ ) is the average particle diameter).

Next, the HDDR process described above was performed on the green compact. Specifically, the green compact is heated to an HD temperature shown in Table 8 in an argon stream of 100 kPa (atmospheric pressure), and then the atmosphere is mixed gas stream of H ₂ partial pressure 33 kPa + Ar partial pressure 67 kPa (total After switching to atmospheric pressure, the hydrogenation / disproportionation reaction was carried out at the HD temperature and time shown in Table 8. Then, it heated up at 700 degreeC and hold | maintained for 4 hours in the argon air pressure-reduced to 5.3 kPa, and dehydrogenation and the recombination reaction were performed. Next, the sample was cooled to room temperature in an atmospheric pressure argon flow to obtain a sample of the example. As a result of observing the fracture surface of each of the obtained samples, it was confirmed that the sample was composed of fine crystal textures and pores having the same mode as in FIG.

Next, the surface of the sample was processed with a surface grinder, and the density of the sample was calculated from the size and unit weight of the sample after processing. The results are shown in Table 9. In addition, since the crack of the porous material by processing, etc. were not seen, it confirmed that the sample had sufficient mechanical strength. The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 9. In Table 9, J _max is the maximum measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, as in the first embodiment.

  From the results of this study, it was confirmed that in any R—Fe—Q alloy composition, a porous material having excellent squareness, which is the effect of the present invention, was obtained, and a part of Fe was converted to Co. It has been confirmed that the same effect can be obtained even when substituted with Ni.

[Example 8]
Rapidly solidified alloys G to L having the target compositions shown in Table 10 below were produced by strip casting. The obtained rapidly solidified alloy was coarsely pulverized and finely pulverized and molded in a magnetic field using the same method as in Example 1 to produce a green compact having a density of 3.96 to 3.98 g / cm ³ . . The average particle size of the fine powder is as shown in Table 10 (the measurement method is the same as in Example 1, and the 50% center particle size (D ₅₀ ) is the average particle size).

Next, the HDDR process described above was performed on the green compact. Specifically, the green compact is heated to 600 ° C. in an argon flow of 100 kPa (atmospheric pressure), and then the atmosphere is mixed gas flow (total atmospheric pressure) of H ₂ partial pressure 33 kPa + Ar partial pressure 67 kPa. After switching, the hydrogenation / disproportionation reaction was carried out by maintaining at 600 ° C. for 4 hours. Thereafter, the temperature was raised to 700 ° C. and kept for 4 hours in an argon stream depressurized to 5.3 kPa to perform dehydrogenation and recombination reaction. Next, the sample was cooled to room temperature in an atmospheric pressure argon flow to obtain a sample of the example. As a result of observing the fracture surface of each of the obtained samples, it was confirmed that the sample was composed of fine crystal textures and pores having the same mode as in FIG.

Next, the surface of the sample was processed with a surface grinder, and the density of the sample was calculated from the size and unit weight of the sample after processing. The results are shown in Table 11. In addition, since the crack of the porous material by processing, etc. were not seen, it confirmed that the sample had sufficient mechanical strength. The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 11. In Table 11, J _max is the maximum measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, as in the first embodiment.

  From the results of this study, it was confirmed that a porous material having excellent squareness, which is an effect of the present invention, can be obtained even if various elements are added to any R—Fe—Q alloy composition.

[Example 9]
Rapidly solidified alloys MP having target compositions shown in Table 12 below were produced by strip casting. The obtained rapidly solidified alloy was coarsely and finely pulverized and molded in a magnetic field using the same method as in Example 1 to produce a green compact with a density of 3.96 g / cm ³ . The average particle size of the fine powder is as shown in Table 12 (the measurement method is the same as in Example 1, and the 50% center particle size (D ₅₀ ) is the average particle size).

Next, the HDDR process described above was performed on the green compact. Specifically, the green compact is heated to 600 ° C. in an argon flow of 100 kPa (atmospheric pressure), and then the atmosphere is mixed gas flow (total atmospheric pressure) of H ₂ partial pressure 33 kPa + Ar partial pressure 67 kPa. After switching, the hydrogenation / disproportionation reaction was carried out by maintaining at 600 ° C. for 4 hours. Then, it heated up at 700 degreeC and hold | maintained for 4 hours in the argon air pressure-reduced to 5.3 kPa, and dehydrogenation and the recombination reaction were performed. Next, the sample was cooled to room temperature in an atmospheric pressure argon flow to obtain a sample of the example. As a result of observing the fracture surface of each of the obtained samples, it was confirmed that the sample was composed of fine crystal textures and pores having the same mode as in FIG.

  Next, the surface of the sample is processed with a surface grinder, and the components of the sample after processing are processed with an ICP emission spectroscopic analyzer (device name: ICPV-1017 manufactured by Shimadzu Corporation) and the oxygen amount is analyzed with a gas analyzer ( Table 13 shows the evaluation results of the apparatus name: EGMA-620W (manufactured by Horiba, Ltd.)) and the value of surplus rare earth amount R ′ calculated from the results. In calculating the surplus rare earth amount, all impurities other than the elements shown in Table 13 were calculated as Fe.

The density of the sample was calculated from the dimensions and unit weight of the sample after processing. The results are shown in Table 14. In addition, since the crack of the porous material by processing, etc. were not seen, it confirmed that the sample had sufficient mechanical strength. The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 14. In Table 14, J _max is the maximum measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, as in the first embodiment.

From the results of this study, it was confirmed that a porous material having excellent squareness, which is the effect of the present invention, can be obtained for each composition having various R amounts. It was also confirmed that a relatively high coercive force H _cJ can be obtained by _setting the surplus rare earth amount R ′ to 1 atomic% or more.

[Example 10]
Alloys N and Q having target compositions shown in Table 15 below were produced. Alloy N is the same as alloy N in Example 9. On the other hand, the alloy Q is obtained by melting an alloy having the same target composition as that of the alloy N by a high-frequency melting method and then homogenizing and heat-treating the ingot produced by casting in a water-cooled mold in an Ar atmosphere at 1000 ° C. for 8 hours. Each alloy was coarsely and finely pulverized and molded in a magnetic field using the same method as in Example 1 to produce a green compact with a density of 3.96 g / cm ³ . The average particle diameter of the fine powder is as shown in Table 15 (the measurement method is the same as in Example 1, and the 50% center particle diameter (D ₅₀ ) is the average particle diameter).

Next, the HDDR process described above was performed on the green compact. Specifically, the green compact is heated to 600 ° C. in an argon flow of 100 kPa (atmospheric pressure), and then the atmosphere is mixed gas flow (total atmospheric pressure) of H ₂ partial pressure 33 kPa + Ar partial pressure 67 kPa. After switching, the hydrogenation / disproportionation reaction was carried out by maintaining at 600 ° C. for 4 hours. Then, it heated up at 700 degreeC and hold | maintained for 4 hours in the argon air pressure-reduced to 5.3 kPa, and dehydrogenation and the recombination reaction were performed. Next, the sample was cooled to room temperature in an atmospheric pressure argon flow to obtain a sample of the example. As a result of observing the fracture surface of each of the obtained samples, it was confirmed that the sample was composed of fine crystal textures and pores having the same mode as in FIG.

Next, the surface of the sample was processed with a surface grinder, and the density of the sample was calculated from the size and unit weight of the sample after processing. The results are shown in Table 16. In addition, since the crack of the porous material by processing, etc. were not seen, it confirmed that the sample had sufficient mechanical strength. The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 16. In Table 16, J _max is the maximum measured value of the magnetization J (T) of the sample when the external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, as in the first embodiment.

From the results of this study, it was confirmed that a porous material having excellent squareness, which is an effect of the present invention, can be obtained for various raw material production methods. Moreover, it was confirmed that a relatively high H _k / H _cJ can be obtained by applying the strip casting method as a rapid cooling method in which the α-Fe phase is hard to be generated.

[Example 11]
The following experiment was conducted using the alloy P (reproduced in Table 17) used in Example 9. Using the same method as in Example 1, coarse pulverization and fine pulverization were performed. The average particle size of the fine powder is as shown in Table 17 (the measurement method is the same as in Example 1, and the 50% center particle size (D ₅₀ ) is the average particle size).

Next, as shown in Table 18, molding was performed in a non-magnetic field or in a magnetic field to produce a green compact having a density of 3.96 g / cm ³ . Next, various HDDR processes were performed on the green compact. Specifically, the mixture was heated to 600 ° C. in a temperature rising atmosphere shown in Table 18, then switched to the atmosphere shown in Table 18, and then held at 600 ° C. for 4 hours to perform a hydrogenation / disproportionation reaction. Thereafter, the temperature was raised to 700 ° C. and kept for 4 hours in an argon stream depressurized to 5.3 kPa to perform dehydrogenation and recombination reaction. Next, the sample was cooled to room temperature in an atmospheric pressure argon flow to obtain a sample of the example.

  As a result of observing the fracture surface of each of the obtained samples, it was confirmed that the sample was composed of fine crystal textures and pores having the same mode as in FIG.

Next, the surface of the sample was processed with a surface grinder, and the density of the sample was calculated from the size and unit weight of the sample after processing. The results are shown in Table 19. In addition, since the crack of the porous material by processing, etc. were not seen, it confirmed that the sample had sufficient mechanical strength. The ground sample was magnetized with a pulse magnetic field of 3.2 MA / m, and then the magnetic properties were measured with a BH tracer (device name: MTR-1412 (manufactured by Metron Giken)). The results are shown in Table 19. In Table 19, J _max is the maximum measured value of the magnetization J (T) of the sample when an external magnetic field H is applied up to 2 Tesla (T) in the magnetization direction of the magnetized sample. H _k is the value of the external magnetic field H that is B _r × 0.9, as in the first embodiment.

  From the results of this study, it was confirmed that a porous material having the aspect of the present invention can be obtained for various treatment methods.

[Example 12]
The porous material produced by the same method as in Example 1 was processed into a size of 7 mm × 7 mm × 5 mm by a peripheral blade cutting machine and a grinding machine. No cracking or chipping of the porous material due to this processing was observed. After performing ultrasonic cleaning on the porous material, the porous material was immersed in the nanoparticle-dispersed colloidal solution. This colloidal solution was a colloidal solution in which Fe nanoparticles whose surface was oxidized were dispersed. The average particle diameter of Fe particles was about 7 nm, the solvent was dodecane, and the solid content concentration was 1.5% by volume. The nanoparticle dispersion solution was placed in a glass container, inserted into a vacuum desiccator with the porous material immersed therein, and placed under reduced pressure. The atmospheric pressure during the treatment was adjusted to about 130 kPa.

  Bubbles were generated in the porous material and the nanoparticle-dispersed colloidal solution due to the reduced pressure. After the generation of bubbles stopped, the pressure was returned to atmospheric pressure. Thereafter, the porous material was inserted into a vacuum dryer, heated to 200 ° C. under an atmospheric pressure of about 130 Pa, the solvent was evaporated, and drying was performed. Thus, a sample of the composite bulk material according to the present invention was obtained.

  From the above results, it was confirmed that a composite bulk body of soft magnetic Fe nanoparticles that can be expected to have high magnetization and a porous material that is a hard magnetic material can be produced.

  The porous material for R—Fe—B permanent magnets obtained by the production method of the present invention exhibits higher magnetic properties than bond magnets, particularly excellent squareness, and is shaped more than conventional sintered magnets. Since the degree of freedom of design is high, it can be suitably used for various applications in which conventional bonded magnets and sintered magnets have been used.

It is a SEM photograph which shows the fracture surface in the Example of the porous material for permanent magnets by this invention. It is a flowchart which shows the method to manufacture the porous material for permanent magnets of this invention. (A) is a schematic diagram of the green compact (molded body) obtained in step S12 shown in the flowchart of FIG. 2, and (b) is a diagram of the material after the HDDR process (S14) is performed on the green compact. It is a schematic diagram. It is a figure which shows the structural example of the apparatus for heat-compressing with respect to a porous magnet. (A)-(c) is a schematic diagram for demonstrating the manufacturing method of the rotor 100 of embodiment by this invention. It is a schematic diagram which shows the structure of the rotor 100 manufactured by the manufacturing method of embodiment by this invention. It is another SEM photograph which shows the torn surface in the Example of the porous material for permanent magnets by this invention. (A)-(d) is typical sectional drawing for demonstrating the hot press formation process in the manufacturing method of the rotor 100 of embodiment by this invention.

Explanation of symbols

12a ′, 12b ′ Porous material for R—Fe—B based permanent magnet 12a, 12b Magnet molded body (magnet part)
22 'Temporary molded body of soft magnetic material powder (iron core temporary molded body)
22 Molded body of soft magnetic material powder (soft magnetic parts, iron core)
26 Chamber 27 Mold 28a Upper punch 28b Lower punch 32 Die 42a, 42b Lower punch 42c Center shaft 44a, 44b Upper punch 52 Lower ram

Claims (14)

Preparing an R—Fe—B rare earth alloy powder (R is at least one selected from the group consisting of rare earth elements including Y and Sc) having an average particle diameter of less than 20 μm (A);
Forming the green compact by molding the R-Fe-B rare earth alloy powder (B);
A step (C) of subjecting the green compact to a heat treatment at a temperature of 550 ° C. or higher and lower than 650 ° C. in hydrogen gas, thereby causing hydrogenation and disproportionation reactions;
R-Fe-B system comprising a step (D) of subjecting the green compact to a heat treatment at a temperature of 550 ° C. or higher and lower than 1000 ° C. in a vacuum or an inert atmosphere, thereby causing dehydrogenation and recombination reaction. A method for producing a porous material for a permanent magnet.   The said process (B) is a manufacturing method of the porous material for R-Fe-B permanent magnets of Claim 1 including the process of shape | molding in a magnetic field.   The R—Fe—B based rare earth alloy powder is 10 atomic% ≦ R ≦ 30 atomic%, 3 atomic% ≦ Q ≦ 15 atomic% (R is a rare earth element, Q is boron or boron and a part of boron are substituted) The method for producing a porous material for an R-Fe-B permanent magnet according to claim 1, wherein the composition satisfies a relationship of (total carbon). In the case where T is at least one transition metal element selected from the group consisting of Fe, Co, and Ni,
At the start of the step (C), the composition of the rare earth element R is set so that the rare earth amount R ′ represented by the following formula (1) in the green compact is R ′ ≧ 0 atomic%, and The method for producing a porous material for an R-Fe-B permanent magnet according to claim 1, wherein the amount of oxygen (O) in the steps from the step (A) to the start of the step (C) is controlled.
(1) R ′ = “atomic% of R” − “atomic% of T” × 1 / 7− “atomic% of O” × 2/3   The method for producing a porous material for an R-Fe-B permanent magnet according to claim 1, wherein the R-Fe-B rare earth alloy powder is a pulverized powder of a quenched alloy.   The method for producing a porous material for an R—Fe—B permanent magnet according to claim 5, wherein the quenched alloy is a strip cast alloy.   The R-Fe-B according to claim 1, wherein the step (C) includes a step of raising the temperature in an inert atmosphere or vacuum and a step of introducing hydrogen gas at a temperature of 550 ° C or higher and lower than 650 ° C. For producing a porous material for a permanent magnet.   The method for producing a porous material for an R-Fe-B permanent magnet according to claim 1, wherein the partial pressure of hydrogen gas in the step (C) is 1 kPa or more and 100 kPa or less.   A porous material for an R—Fe—B based permanent magnet obtained by the production method according to claim 1. Preparing a porous material for an R-Fe-B permanent magnet according to claim 9 (E);
A step (F) of introducing a material different from the R-Fe-B porous material into the pores of the R-Fe-B porous material by wet processing;
For producing a composite bulk material for R-Fe-B permanent magnets, comprising: Preparing a composite bulk material for an R-Fe-B permanent magnet obtained by the production method according to claim 10;
Forming the R-Fe-B permanent magnet by further heating the composite bulk material for the R-Fe-B permanent magnet;
Of producing an R—Fe—B permanent magnet comprising Preparing a porous material for an R-Fe-B permanent magnet according to claim 9 (E);
Introducing at least one of a rare earth metal, a rare earth alloy and a rare earth compound into the surface and / or inside the pores of the porous material for R-Fe-B permanent magnets (F ′);
For producing a composite bulk material for R-Fe-B permanent magnets, comprising:   The porous material for an R-Fe-B permanent magnet according to claim 12, wherein the porous material for an R-Fe-B permanent magnet is heated simultaneously with the step (F ') or after the step (F'). Production method.   The porous material for R-Fe-B based permanent magnet according to claim 9 is pressurized at a temperature of 600 ° C. or higher and lower than 900 ° C., and the porous material for R—Fe—B based permanent magnet is subjected to true density. The manufacturing method of the R-Fe-B type permanent magnet including the process of densifying to 95% or more.