Manufacturing method of rare-earth magnet

Abstract

A manufacturing method of a rare-earth magnet includes: manufacturing a first sealing body by filling a graphite container with a magnetic powder to be a rare-earth magnet material and by sealing the graphite container; manufacturing a sintered body by sintering the first sealing body to manufacture a second sealing body in which the sintered body is accommodated; and manufacturing a rare-earth magnet by performing hot plastic working on the second sealing body to give magnetic anisotropy to the sintered body.

Claims

1. A manufacturing method of a rare-earth magnet, comprising: manufacturing a first sealing body by filling a first graphite container with a magnetic powder to be a rare-earth magnet material, then inserting an open end of the first graphite container into an open end of a second graphite container to form a third graphite container, and sealing the third graphite container, wherein the third graphite container is constituted by the first graphite container and the second graphite container; manufacturing a sintered body by sintering the first sealing body to manufacture a second sealing body in which the sintered body is accommodated; and manufacturing a rare-earth magnet by performing hot plastic working on the second sealing body to give magnetic anisotropy to the sintered body, wherein an inside dimension of the second graphite container is larger than an inside dimension of the first graphite container, each of the first graphite container and the second graphite container is a tube-shaped body constituted by a deformed graphite sheet and having a rectangular section or a circular section, and the tube-shaped body has a closed end provided with a graphite base plate; the method further comprising: forming the tube-shaped body by deforming a graphite sheet along a side surface of a tube-shaped stand, the side surface having a rectangular section or a circular section, the tube-shaped stand including a bottom face provided on an end surface of the side surface, and the bottom face having a through-hole; filling graphite powder into the tube-shaped stand by moving the tube-shaped stand relative to the tube-shaped body; and forming the base plate on an open end of the tube-shaped body by pushing the tube-shaped stand downward to perform press molding on the graphite powder after the graphite powder falls down below the bottom face of the tube-shaped stand through the through-hole.

2. The manufacturing method of a rare-earth magnet according to claim 1, further comprising manufacturing the graphite base plate by performing press molding on graphite powder filled into the tube-shaped body.

3. A manufacturing method of a rare-earth magnet, comprising: manufacturing a first sealing body by filling a graphite container with a magnetic powder to be a rare-earth magnet material, disposing a graphite top plate on an open end of the graphite container, and sealing the graphite container; manufacturing a sintered body by sintering the first sealing body to manufacture a second sealing body in which the sintered body is accommodated; and manufacturing a rare-earth magnet by performing hot plastic working on the second sealing body to give magnetic anisotropy to the sintered body; wherein the graphite container is a tube-shaped body constituted by a deformed graphite sheet and having a rectangular section or a circular section, and the tube-shaped body has a closed end provided with a graphite base plate; the method further comprising: forming the tube-shaped body by deforming a graphite sheet along a side surface of a tube-shaped stand, the side surface having a rectangular section or a circular section, the tube-shaped stand including a bottom face provided on an end surface of the side surface, and the bottom face having a through-hole; filling graphite powder into the tube-shaped stand by moving the tube-shaped stand relative to the tube-shaped body; and forming the base plate on an open end of the tube-shaped body by pushing the tube-shaped stand downward to perform press molding on the graphite powder after the graphite powder falls down below the bottom face of the tube-shaped stand through the through-hole.

4. The manufacturing method of a rare-earth magnet according to claim 3, further comprising manufacturing the graphite top plate by performing press molding on graphite powder.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Features, advantages, and technical and industrial significance of exemplary embodiments of the invention will be described below with reference to the accompanying drawings, in which like numerals denote like elements, and wherein:

(2) FIG. 1 is a schematic view illustrating a manufacturing method of a magnetic powder to be used in a first step of a manufacturing method of a rare-earth magnet according to an embodiment of the present invention;

(3) FIG. 2A is a schematic view illustrating a manufacturing step of a graphite container;

(4) FIG. 2B is a view when viewed from a direction of an arrow b in FIG. 2A;

(5) FIG. 3 is a schematic view illustrating a manufacturing step of the graphite container, following the step in FIG. 2A;

(6) FIG. 4A is a schematic view illustrating a manufacturing step of the graphite container, following the step in FIG. 3;

(7) FIG. 4B is a schematic view illustrating a manufacturing step of the graphite container, following the step in FIG. 4A;

(8) FIG. 5 is a schematic view illustrating a manufacturing step of the graphite container, following the step in FIG. 4B;

(9) FIG. 6 is a perspective view of the graphite container manufactured in the step in FIG. 5, when viewed from its bottom side;

(10) FIG. 7A is a schematic view illustrating a first step of manufacturing one example of a first sealing body, which first step is included in the manufacturing method of a rare-earth magnet according to the embodiment of the present invention;

(11) FIG. 7B is a perspective view illustrating the one example of the first sealing body manufactured in the step in FIG. 7A;

(12) FIG. 8A is a schematic view illustrating a first step of manufacturing one example of the first sealing body, which first step is included in the manufacturing method of a rare-earth magnet according to the embodiment of the present invention;

(13) FIG. 8B is a perspective view illustrating the one example of the first sealing body manufactured in the step in FIG. 8A;

(14) FIG. 9 is a schematic view illustrating a second step of the manufacturing method of a rare-earth magnet according to the embodiment of the present invention;

(15) FIG. 10 is a schematic view illustrating a third step of the manufacturing method of a rare-earth magnet according to the embodiment of the present invention;

(16) FIG. 11A is a view illustrating a microstructure of a sintered body illustrated in FIG. 9;

(17) FIG. 11B is a view illustrating a microstructure of a rare-earth magnet illustrated in FIG. 10;

(18) FIG. 12A is a view illustrating an experimental result related to a relationship between with or without a graphite container and an oxygen concentration inside a manufactured rare-earth magnet;

(19) FIG. 12B is a view illustrating an experimental result related to a relationship between with or without a graphite container and a coercive force inside a manufactured rare-earth magnet;

(20) FIG. 13 is a view illustrating an experimental result related to a relationship between an oxygen concentration of an outside atmosphere at the time of manufacturing a sintered body and an oxygen concentration inside the sintered body thus manufactured, in a case where a graphite container is used;

(21) FIG. 14 is a view illustrating an experimental result related to a relationship between a press burning temperature at the time of manufacturing a sintered body and an oxygen concentration inside the sintered body thus manufactured, in a case where a graphite container is used;

(22) FIG. 15 is a view illustrating an experimental result related to usability and high-temperature friction coefficient in the following cases: a case where a rare-earth magnet is manufactured by use of a graphite container made of a graphite sheet; and a case where a rare-earth magnet is manufactured by applying, as lubricant, graphite particles or material particles other than the graphite particles to a molding die;

(23) FIG. 16 is a view illustrating an experimental result related to heating duration in the following cases: a case where a rare-earth magnet is manufactured by use of a graphite container made of a graphite sheet; and a case where a rare-earth magnet is manufactured by applying, as lubricant, graphite particles or material particles other than the graphite particles to a molding die; and

(24) FIG. 17 is a view illustrating an experimental result related to an oxygen concentration inside a rare-earth magnet in the following cases: a case where the rare-earth magnet is manufactured by use of a graphite container made of a graphite sheet; and a case where the rare-earth magnet is manufactured by applying, as lubricant, graphite particles or material particles other than the graphite particles to a molding die.

DETAILED DESCRIPTION OF EMBODIMENTS

(25) With reference to the drawings, the following describes a manufacturing method of a rare-earth magnet according to an embodiment of the present invention. The manufacturing method of a rare-earth magnet according to the embodiment of the present invention includes a first step, a second step, and a third step.

(26) FIG. 1 is a schematic view illustrating a manufacturing method of a magnetic powder to be used in the first step. In the first step, a graphite container is filled with a magnetic powder to be a rare-earth magnet material and then sealed, so as to manufacture a first sealing body. In a furnace (not shown) in which a pressure is decreased to 50 kPa or less, for example, a melt spinning method using a single roll is performed such that an alloy ingot is melted at a high frequency and molten metal having a composition that provides a rare-earth magnet is jetted to a copper roll R, so as to manufacture rapidly cooled strips B (rapidly cooled ribbons).

(27) The rapidly cooled strips B thus manufactured are roughly crushed, so as to manufacture a magnetic powder. Here, a diameter range of the magnetic powder is adjusted to be within a range of 75 to 300 m.

(28) Next will be described a manufacturing method of a graphite container to be used in the first step, with reference to FIGS. 2A to 6. First, as illustrated in FIGS. 2A, 2B, a tube-shaped stand T including a side surface T1 having a rectangular section and a bottom face T2 provided on one end surface of the side surface T1 and having a through-hole T2 is prepared. By deforming a graphite sheet SH along the side surface T1 of the tube-shaped stand T, a tube-shaped body 1a, which is a component of a graphite container having a rectangular section as illustrated in FIG. 3, is manufactured. Note that, as illustrated in FIG. 3, an overlap margin 1a1 is pressed from its outside by an external force q of about 1 kN, so that ends of the graphite sheet SH adhere to each other.

(29) The tube-shaped body la thus formed around the tube-shaped stand T and the tube-shaped stand T are accommodated in a cavity of a molding die K as illustrated in FIG. 4A.

(30) Then, as illustrated in FIG. 4B, the tube-shaped stand T inside the tube-shaped body 1a is moved upward (in an X1-direction) relative to the tube-shaped body 1a, so as to form a space below the bottom face T2 of the tube-shaped stand T, and a graphite powder GF is filled into the tube-shaped stand T (in an X2-direction). The graphite powder GF thus filled falls down into a space formed below the bottom face T2, through the through-hole T2of the bottom face T2 of the tube-shaped stand T.

(31) When a predetermined amount of the graphite powder GF falls down into the space, the tube-shaped stand T is pushed downward as illustrated in FIG. 5 so as to perform press molding (in an X3-direction). Hereby, as illustrated in FIG. 6, a graphite container 1 constituted by the tube-shaped body la and a base plate lb is manufactured. As described above, the tube-shaped body 1a is constituted by a deformed graphite sheet, and has a rectangular section. The base plate 1b is formed by performing press molding on the graphite powder GF in one open end of the tube-shaped body 1a. The tube-shaped body 1a has a closed end closed by the base plate 1b and an open end on the other end.

(32) In the first step, the graphite container 1 thus manufactured is filled with a magnetic powder and sealed, so as to manufacture a first sealing body. The first sealing body may be manufactured in steps illustrated in FIGS. 7A and 7B, or in steps illustrated in FIGS. 8A, 8B. These steps are described below sequentially.

(33) First, in a manufacturing method of the first sealing body as illustrated in FIGS. 7A, 7B, a first graphite container 1 and a second graphite container 1 are prepared as illustrated in FIG. 7A. After the first graphite container 1 is filled with a magnetic powder MF, the first graphite container 1 is covered with an open end of the second graphite container 1 from an open end side of the first graphite container 1. In other words, the open end of the first graphite container 1 is inserted into the open end of the second graphite container F. Thus, a first sealing body 10 in which the magnetic powder is sealed by the first graphite container 1 and the second graphite container F is manufactured as illustrated in FIG. 7B.

(34) In a manufacturing method of the first sealing body as illustrated in FIGS. 8A, 8B, a top plate 1c manufactured by performing press molding on a graphite powder is used as well as a graphite container 1, as illustrated in FIG. 8A. After the graphite container 1 is filled with a magnetic powder MF, the top plate 1c is fitted into an open end of the graphite container 1, and then, a predetermined pressure is applied to the graphite container 1 from its outside, so as to cause an inner surface of the graphite container 1 to make close contact with an end surface of the top plate 1c. Thus, a first sealing body 10A in which the magnetic powder is sealed is manufactured.

(35) After the first sealing body 10 or the first sealing body 10A is manufactured by a method of either the steps of FIGS. 7A, 7B or the steps of FIGS. 8A, 8B, manufacturing of a sintered body, which is the second step, is performed. Herein, the following description is made with reference to the first sealing body 10.

(36) FIG. 9 is a schematic view illustrating the second step of the manufacturing method. As illustrated in FIG. 9, the first sealing body 10 is accommodated in a cavity defined by a cemented carbide die D and a cemented punch P sliding in a hollow of the cemented carbide die D. Then, while a pressure is increased by the cemented punch P (in a Z-direction), a current is flowed in a pressure direction so as to perform heating by current application at around 800 C. Hereby, a sintered body S accommodated in a second sealing body 20 obtained by crushing the first sealing body 10 is manufactured (the second step). The sintered body S includes, for example, a main phase of NdFeB of a nanocrystal structure (with an average particle diameter of 300 nm or less, e.g., a grain size of around 50 nm to 200 nm), and a grain boundary phase of NdX alloy (X: metal element) provided around the main phase.

(37) The Nd-X alloy constituting the grain boundary phase of the sintered body S is made of Nd and at least one type of alloy selected from Co, Fe, Ga, and the like. The NdX alloy is at least one of NdCo, NdFe, NdGa, NdCoFe, and NdCoFeGa, or two or more thereof in combination, and includes Nd relatively abundantly.

(38) The second sealing body 20 accommodating therein the sintered body S manufactured in the second step is accommodated again in the cavity defined by the cemented carbide die D and the cemented punch P, as illustrated in FIG. 10. Then, hot plastic working is performed while a pressure is increased by the cemented punch P (in the Z-direction). Hereby, a rear-earth magnet C (oriented magnet) accommodated in a third sealing body 30 obtained by crushing the second sealing body 20 is manufactured (the third step). Magnetic anisotropy is given to the sintered body S by the third step. Note that a strain rate at the time of the hot plastic working is preferably adjusted to be 0.1/sec or more. Further, in a case where a machining ratio (compressibility) due to the hot plastic working is large, for example, in a case where the compressibility is around 10% or more, the hot plastic working can be called strong processing, but the hot plastic working is preferably performed at a processing rate of around 60 to 80%.

(39) As illustrated in FIG. 11A, the sintered body S manufactured in the second step exhibits an isotropic crystal structure in which the grain boundary phase BP is filled between nanocrystal grains MP (the main phase). In contrast, as illustrated in FIG. 11B, the rare-earth magnet C manufactured in the third step exhibits a magnetically anisotropic crystal structure.

(40) According to the manufacturing method of the rare-earth magnet of the present invention, the first sealing body 10 is manufactured by accommodating the magnetic powder MF in the graphite container 1; the sintered body S is manufactured by performing hot press working on the first sealing body 10; and the rare-earth magnet is manufactured (in a state of the third sealing body 30) such that hot plastic working is performed in a state (a state of the second sealing body 20) where the sintered body S is accommodated in the graphite container 1. Accordingly, in the manufacturing process of the rare-earth magnet, the magnetic powder MF, the sintered body S in a high temperature state, and the rare-earth magnet C in a high temperature state are shielded from the atmospheric air efficiently. Further, the graphite container 1 is a strongly oxidizing material as compared to the rare-earth magnet material, and oxidizes prior to the rare-earth magnet material. Because of this, the rare-earth magnet C with a low oxygen concentration can be manufactured without the need of manufacture under an inert gas atmosphere. Further, graphite forming the graphite container 1 has a good lubrication action inside the cemented carbide die D, so that application of lubricant to the cemented carbide die D is unnecessary, thereby achieving excellent manufacture efficiency.

(41) The inventors of the present invention carried out an experiment to specify a relationship between with or without a graphite container and an oxygen concentration inside a manufactured rare-earth magnet, and an experiment to specify a relationship between with or without a graphite container and a coercive force inside a manufactured rare-earth magnet, in the following manner.

(42) A test specimen in Example 1 is described below. Predetermined amounts of rare-earth magnet materials (an alloy composition is 29.8 Nd-0.2 Pr-4 Co-0.9 B-0.6 Ga-Bal.Fe (mass %)) were blended and then melted under an

(43) Ar-gas atmosphere. After that, resultant molten metal was ejected from an orifice to a rotating roller, which is made of Cu and plated with Cr, and then cooled down rapidly, so as to manufacture rapidly cooled strips. The rapidly cooled strips were then crushed so as to obtain a magnetic powder. Then, 30 g of the magnetic powder was accommodated in a container (a graphite container) manufactured by a graphite sheet of 7.228.260 mm, and a pressure was applied to a top face so as to be sealed. The container was placed in a cemented carbide die heated to 650 C. under the atmospheric air, and then subjected to press burning at a load of 400 MPa. After a sintered body was manufactured by press burning, the sintered body was maintained for 60 seconds, and then taken out from the die. A height of the sintered body was 20 mm. The sintered body was then accommodated in a forging die prepared separately, and hot plastic working was performed at a heating temperature of 750 C., a processing rate of 75%, and a strain rate of 1.0/sec, so as to manufacture a rare-earth magnet. A test specimen with a size of 4.04.02.0 mm was cut out from the rare-earth magnet thus manufactured, and magnetic characteristics thereof were evaluated.

(44) In comparison with the test specimen of Example 1, a test specimen of Comparative Example 1 was manufactured without using a graphite sheet in a manufacturing process thereof, and the other manufacturing conditions and the like are the same as in Example 1.

(45) Respective oxygen concentrations of the test specimens were measured by use of an oxygen analyzer, and respective coercive forces of the test specimens were measured by use of a vibrating sample magnetometer (VSM). FIG. 12A is a view illustrating an experimental result related to the oxygen concentrations inside the rare-earth magnets. FIG. 12B is a view illustrating an experimental result related to the coercive forces inside the rare-earth magnets.

(46) From FIG. 12A, it is demonstrated that Example 1 manufactured by use of a graphite container had an oxygen concentration of 1000 ppm or less, Comparative Example 1 manufactured without using a graphite container had an oxygen concentration of around 5000 ppm, and thus, Example 1 can reduce the oxygen concentration by 20% or less relative to Comparative Example 1.

(47) Further, from FIG. 12B, it is demonstrated that the coercive force of Comparative Example 1 was 10 kOe or less, whereas the coercive force of Example 1 was 16 kOe, and thus, the coercive force of Example 1 is higher than that of Comparative Example 1 by about 60%.

(48) This can be described from a relationship between the oxygen concentration and the coercive force of the rare-earth magnet. That is, in Example 1 manufactured by use of a graphite container, the container prevents the magnetic powder from making contact with the atmospheric air, so that oxidation of the sintered body does not proceed, thereby making it possible to attain an expected high coercive force. In contrast, in Comparative Example 1 manufactured without using a graphite container, the magnetic powder and the sintered body make contact with the atmospheric air in a normal-temperature transfer process and a high-temperature forming process, so that oxidation thereof proceeds. As a result, an oxide is formed due to a reaction between oxygen and a rear-earth element in a grain boundary phase that has a large effect to coercive force performance, so that a percentage of the grain boundary phase contributing to the coercive force decreases and a percentage of the grain boundary phase magnetically dividing the main phase decreases, thereby presumably decreasing the coercive force.

(49) The inventors of the present invention carried out an experiment to specify a relationship between an oxygen concentration of an outside atmosphere at the time of manufacturing a sintered body and an oxygen concentration inside the sintered body thus manufactured, in a case where a graphite container is used. Note that Example 1 in this experiment is the same as Example 1 in the previously explained experiment.

(50) An outside oxygen concentration in a manufacturing process of Example 1 was 20% (the atmospheric air). Outside oxygen concentrations in a manufacturing process of Reference Example 1 were set to 0.01%, 1.0%, 3.0%, 5.0%. The other manufacturing conditions and the like are the same as in Example 1.

(51) An experimental result is shown in FIG. 13. According to FIG. 13, even if the outside oxygen concentrations were reduced, respective oxygen concentrations inside manufactured rare-earth magnets were 1000 ppm, which is not different from Example 1. As a result, it was found that, in a process of manufacturing a rare-earth magnet by use of a graphite container, it is not necessary to reduce the outside oxygen concentration, and even if the manufacturing was performed under the atmospheric air, a rare-earth magnet with a low internal oxygen concentration can be manufactured.

(52) The inventors of the present invention carried out an experiment to specify a relationship between a press burning temperature at the time of manufacturing a sintered body and an oxygen concentration inside the sintered body thus manufactured, in a case where a graphite container is used. Note that Example 1 in this experiment is the same as Example 1 in the previously explained experiment.

(53) A temperature at the time of press burning in a manufacturing process of Example 1 was 650 C. Temperatures at the time of press burning in a manufacturing process of Reference Example 2 were set to 700 C., 750 C. The other manufacturing conditions and the like are the same as in Example 1.

(54) An experimental result is shown in FIG. 14. From FIG. 14, even if the press burning temperatures were increased, respective oxygen concentrations of rare-earth magnets were 1000 ppm or less, which is not different from Example 1. One conceivable reason thereof is as follows: an oxidation temperature of graphite used in the container exceeds 800 C., and even if the container is exposed to high temperatures below this temperature, the container is not consumed to cause CO or CO.sub.2. Thus, airtightness can be maintained.

(55) The inventors of the present invention further carried out an experiment related to usability and high-temperature wet performance, an experiment related to heating duration, and an experiment related to an oxygen concentration inside a rear-earth magnet, each in the following cases: a case where a rare-earth magnet is manufactured by use of a graphite container made of a graphite sheet; and a case where a rare-earth magnet is manufactured by applying, as lubricant, graphite particles or material particles other than the graphite particles to a molding die.

(56) With the use of a graphite sheet having a thickness of 60 m, a graphite container illustrated in FIG. 6 was manufactured by employing the manufacturing method illustrated in FIGS. 2A to 5. In the graphite container, a magnetic powder having an average grain size of 150 nm with a magnitude of 45 to 300 m was accommodated. The graphite container was then accommodated in a molding die, and hot-press was performed so as to manufacture a sintered body. The sintered body was then subjected to hot plastic working, so as to manufacture a test specimen (a rectangular solid having a dimension of 301018 mm) of Example 2 of the rare-earth magnet.

(57) A sintered body manufactured by performing hot-press on the same magnetic powder as in Example 2 was immersed into glass lubricant. Then, the sintered body was taken out and accommodated in a molding die, and subjected to hot forming under an Ar-gas atmosphere (with an oxygen concentration of 1000 ppm or less), so as to manufacture a test specimen of Comparative Example 2.

(58) A sintered body obtained by performing hot-press on the same magnetic powder as Example 2 was immersed in graphite lubricant. Then, the sintered body was taken out and accommodated in a molding die, and subjected to hot forming under an

(59) Ar-gas atmosphere (with an oxygen concentration of 1000 ppm or less), so as to manufacture a test specimen of Comparative Example 3.

(60) A sintered body obtained by performing hot-press on the same magnetic powder as Example 2 was immersed in glass lubricant. Then, the sintered body was taken out and accommodated in a molding die, and subjected to hot forming under the atmospheric air, so as to manufacture a test specimen of Comparative Example 4.

(61) High-temperature wet performance was evaluated in a ring compression test. Here, the ring compression test is performed such that, with the use of a compression apparatus using a vertical 1000-ton hydraulic press that can freely adjust a rolling speed from 1.0 to 7.8 mm/sec, a ring-shaped test piece is sandwiched between upper and lower anvils to which lubricant is applied and a compression test is performed.

(62) By the compression test, a high-temperature friction coefficient as an evaluation index of high-temperature wettability was calculated as for Example 2 and Comparative Examples 2, 3.

(63) In the meantime, in terms of Example 2 and Comparative Examples 2, 3, qualitative evaluation on usability of each lubricant was also performed. Here, the usability indicates both continuous productivity and maintainability. The continuous productivity is an index indicative of whether or not manufacture is stopped (the facility is stopped) because a solidified substance of lubricant is attached to a molding die or the like and remains or attached to the facility at the time when the lubricant is used and applied to the molding die or a compact to be formed. When a removal operation is performed frequently, the continuous productivity is low. In the meantime, in terms of the maintainability, in a case where a deposition amount of lubricant or the like is small and a removal time is not required at the time when a molding die is fixed or a general maintenance action is performed in facility check, the maintainability is high.

(64) Further, as a heating test, high-frequency induction heating is applied to Example 2, heating in a molding die is applied to Comparative Examples 2 to 4, and a heating duration before a material temperature reaches 700 C. was measured by a noncontact thermometer.

(65) Further, respective test specimens of Example 2 and Comparative Examples 3, 4, were rapidly heated to 2700 C., and respective oxygen concentrations in generated gas were measured by use of an oxygen amount/nitrogen amount measuring device.

(66) FIG. 15 is a view illustrating an experimental result related to the usability and the high-temperature friction coefficient, FIG. 16 is a view illustrating an experimental result related to the heating duration, and FIG. 17 is a view illustrating an experimental result related to the oxygen concentration inside a rare-earth magnet.

(67) According to FIG. 15, Example 2 had a low high-temperature friction coefficient and good usability. Further, in terms of Comparative Example 2, although a high-temperature friction coefficient was low, the glass lubricant was difficult to be removed because hardened glass was attached to an inner surface of the mold, a surface of the sintered body, and the like after the temperature decreased, so that usability of Comparative Example 2 was poor.

(68) In the meantime, it was found from FIG. 16 that respective heating durations of Comparative Examples were 300 seconds, whereas a heating duration of Example 2 was around 10 seconds, which was relatively short.

(69) Further, it was found from FIG. 17 that, although Example 2 was manufactured in the atmospheric air, its internal oxygen concentration was at the same level as Comparative Example 3 manufactured under the Ar-gas atmosphere. This is presumably because the graphite container prevented the magnetic powder from making contact with the atmospheric air, so that oxidation of the sintered body did not proceed.

(70) The embodiment of the present invention has been described above, but the present invention is not limited to the embodiment. The embodiment may be modified appropriately in design without departing from the gist of the present invention.