Patent Application
20170250015
1. Field of the Invention
The present invention relates to an R-T-B based permanent magnet whose main components are a rare earth element (R), at least one or more kinds of iron element essentially including Fe or Fe and Co (T), and boron (B).
2. Description of the Related Art
R-T-B based permanent magnets have excellent magnetic properties and are thus used for home electric appliances, various kinds of motors such as voice coil motors (VCM) of hard disk drive and motors mounted on hybrid cars, and the like. When the R-T-B based permanent magnet is used for the motor or so, it is required to be excellent in heat resistance for responding to a use environment of high temperature and further have a high coercivity.
As a method for improving coercivity (HcJ) of the R-T-B based permanent magnet, the rare earth element R to which a light rare earth element of Nd, Pr etc. is mainly applied is partially substituted with a heavy rare earth element of Dy, Tb etc. in order to improve crystal magnetic anisotropy of R2T14B phases. It tends to be hard to manufacture a magnet having coercivity large enough to be used for the motors without using the heavy rare earth element.
Dy and Tb, however, are more rare in yield and more expensive than Nd and Pr. In recent years, supply instability of Dy and Tb has been worsening due to rapidly expanding demand in R-T-B based permanent magnets of high coercivity type using a large amount of Dy and Tb. It is thus required to obtain coercivity needed for application to the motors or so even in case of a composition containing Dy and Tb as little as possible.
Under such circumstances, research and development for improving coercivity of R-T-B based permanent magnets without using Dy or Tb have been actively conducted. In the research and development, it is reported that coercivity is improved by a composition using less amount of B than an ordinary R-T-B based permanent magnet.
For example, Patent Document 1 reports that an R-T-B based rare earth sintered magnet using less amount of Dy and having a high coercivity is obtained by having a content of B lower than an ordinary R-T-B based alloy and containing one or more kinds of metal element M selected from Al, Ga, and Cu so as to generate an R2T17 phase, and by sufficiently securing a volume ratio of a transition metal rich phase (R6T13M) generated by using the R2T17 phase as raw material.
Patent Document 2 reports that an R-T-B based sintered magnet having high residual magnetic flux density and coercivity is obtained by having a content of B lower than an ordinary R-T-B based sintered magnet, having a predetermined range of contents of R, B, Al, Cu, Co, Ga, C, and O, and having a ratio of B to Nd and Pr and an atom ratio of Ga and C to B, both of which respectively satisfy a specific relation.
Patent Document 3 reports that an R-T-B sintered magnet having a high Br and a high HcJ is obtained without using Dy by having a composition whose amount of R, amount of B, and amount of Ga are within specific ranges to form a thick two-grain boundary.
Patent Document 1: JP 2013-216965 A
Patent Document 2: WO 2013/191276
Patent Document 3: WO 2014/157448
As described above, the method for improving coercivity of the R-T-B based permanent magnet with a composition of a reduced B content is known, but the R-T-B based permanent magnet still tends to have an insufficient coercivity obtained by reducing contents of Dy and Tb as magnets used for the motors under high temperature environment such as drive motor of hybrid vehicles.
The present invention has been achieved under the above circumstances. It is an object of the invention to provide an R-T-B based permanent magnet capable of obtaining a high coercivity under high temperature environment even if a use amount of a heavy rare earth element is reduced.
To achieve the object, the R-T-B based permanent magnet of the present invention is an R-T-B based permanent magnet including main phase grains composed of R2T14B type compound, wherein
the R-T-B based permanent magnet contains at least C, Ga, and M (M is at least one kind selected from a group of Zr, Ti, and Nb) in addition to R, T, and B,
B is contained at 0.71 mass % or more and 0.88 mass % or less,
C is contained at 0.15 mass % or more and 0.34 mass % or less,
Ga is contained at 0.40 mass % or more and 1.40 mass % or less,
M is contained at 0.25 mass % or more and 2.50 mass % or less, and
a formula (1) of 0.14≦[C]/([B]+[C])≦0.30 and a formula (2) of 5.0≦[B]+[C]−[M]≦5.6 are satisfied, where [B] is a B content represented by atom %, [C] is a C content represented by atom %, and [M] is a M content represented by atom %.
The R-T-B based permanent magnet of the present invention makes it possible to obtain a high coercivity even with a composition of reduced contents of Dy and Tb. The present inventors conceive as below the reason why a high coercivity can be obtained only at the time of the above-mentioned specific composition balance with a composition of including a small content of B and predetermined amounts of C, Ga, and M.
(1) When a raw material where a certain amount of C is added to a composition having a less amount of B than stoichiometric composition is used as a starting raw material, the amount of B for forming an R2T14B type compound constituting the main phase grains is lacked. Thus, C is solid soluted into a B site of the R2T14B type compound of the main phase grains, and the R2T14B type compound represented by a composition formula of R2T14BxC(1-x) is formed. It is conceivable that at least part of added Ga and the element of M is also solid soluted into the R2T14B type compound.
(2) When the permanent magnet is manufactured, a grain boundary phase changes to a liquid phase at the time of an aging treatment at around 500° C. In this step, an outermost surface portion of the main phase grains is partially dissolved and incorporated into the liquid phase. In case of conventional R-T-B based permanent magnets, an R2T14B type compound of an outermost surface portion of main phase grains dissolved by an aging treatment is deposited once again on the surface of the main phase grains as the R2T14B type compound when the liquid phase is once again changed to the solid phase by being cooled. Thus, there is no large change to a volume ratio of the main phase grains of the R-T-B based permanent magnet.
(3) However, the R-T-B based permanent magnet of the present invention contains a certain amount of M. M has a standard generation free energy of a carbide that is lower than that of the rare earth element R, and thus is combined with C and easily forms a carbide. It is thus conceivable that C is combined with M and generates a carbide of M among elements contained in the compound represented by the composition formula of R2T14BxC(1-x) dissolved from the outermost surface of the main phase grains by the aging treatment.
(4) When C out of the elements dissolved from the outermost surface of the main phase grains is consumed, T becomes excessive by a consumption amount of C even if the R2T14B type compound is attempted to be generated once again after being cooled. It is normally conceivable that a soft magnetic R2T17 compound is generated and adversely affects magnetic properties with a composition where T is excessive. The R-T-B based permanent magnet of the present invention, however, contains a certain amount of Ga, and thus makes it possible to generate an R-T-Ga compound typified by R6T13Ga.
(5) That is, in the R-T-B based permanent magnet of the present invention, an amount of R2T14C out of the elements contained in R2T14BxC(1-x) of the outermost surface portion of the main phase grains dissolved by the aging treatment is consumed in generation of the carbide of M and the R-T-Ga compound. Then, the compound represented by the composition formula of R2T14B is re-deposited on the outermost surface of the main phase grains at the time of cooling. That is, a ratio of the main phase grains decreases and a ratio of the grain boundary phases increases by the amount of R2T14C of the elements contained in R2T14BxC(1-x) of the outermost surface portion of the main phase grains dissolved by the aging treatment.
(6) According to such a mechanism, it is conceivable in the R-T-B based permanent magnet of the present invention that a thick two-grain boundary is formed between the main phase grains by the aging treatment at around 500° C. It is conceivable that when the thick two-grain boundary is formed, the main phase grains are easily magnetically separated, and magnetization reversal of one main phase grain is hard to be transmitted to adjacent main phase grains, whereby a high coercivity is expressed.
(7) Thus, the following two conditions are needed for securely forming a sufficiently thick two-grain boundary between the main phase grains by the aging treatment at around 500° C. and obtaining a high coercivity: (i) a sufficient amount of C is solid soluted in the R2T14B type compound of the main phase; and (ii) there exists an appropriate amount of M capable of consuming C of R2T14BxC(1-x) of the outermost surface of the main phase dissolved during the aging treatment. It is thus conceivable that a high coercivity is expressed only when two parameters of (i) [C]/([B]+[C]) and (ii) [B]+[C]−[M] are in an appropriate balance.
Furthermore, in the present invention, a formula (3) of 5.2≦[B]+[C]−[M]≦5.4 is satisfied, where [B] is a B content represented by atom %, [C] is a C content represented by atom %, and [M] is a M content represented by atom %.
With a composition within such a range, it tends to become easier to form a sufficiently thick two-grain boundary between the main phase grains and obtain a further higher coercivity.
In the R-T-B based permanent magnet according to the present invention, R may be contained at 29 mass % or more and 37 mass % or less.
The R-T-B based permanent magnet according to the present invention may further include Cu, and Cu may be contained at 0.05 mass % or more and 1.5 mass % or less.
The R-T-B based permanent magnet according to the present invention may further include Al, and Al may be contained at 0.03 mass % or more and 0.6 mass % or less.
In the R-T-B based permanent magnet according to the present invention, Co may be contained at 0.3 mass % or more and 4.0 mass % or less.
In the R-T-B based permanent magnet according to the present invention, the main phase grains composed of R2T14B type compound and a grain boundary may be contained, and the grain boundary may contain an R-T-Ga phase including R, T, and Ga and a carbide phase of M.
In the R-T-B based permanent magnet according to the present invention, B may be contained at 0.71 mass % or more and 0.85 mass % or less.
In the R-T-B based permanent magnet according to the present invention, C may be contained at 0.15 mass % or more and 0.30 mass % or less.
In the R-T-B based permanent magnet according to the present invention, Ga may be contained at 0.70 mass % or more and 1.40 mass % or less.
In the R-T-B based permanent magnet according to the present invention, M may be contained at 0.65 mass % or more and 2.50 mass % or less.
The present invention makes it possible to provide the R-T-B based permanent magnet capable of obtaining a high coercivity even if a use amount of a heavy rare earth element is reduced.
Hereinafter, the present invention will be described based on embodiments shown in the figures.
The first embodiment of the present invention is directed to an R-T-B based sintered magnet that is a kind of R-T-B based permanent magnets.
The R-T-B based sintered magnet according to the first embodiment of the present invention will be described. As shown in
The main phase grains contained in the R-T-B based sintered magnet according to the present embodiment are composed of R2T14B type compound having crystal structure of R2T14B type tetragonal.
R represents at least one kind of rare earth elements. Rare earth elements are Sc, Y, and lanthanoid elements belonging to Group 3 in the long-periodic table. For example, lanthanoid elements include La, Ce, Pr, Nd, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu etc. Rare earth elements are divided into light rare earth elements and heavy rare earth elements. Heavy rare earth elements represent Gd, Tb, Dy, Ho, Er, Tm, Yb, and Lu, and light rare earth elements represent the other rare earth elements.
In the present embodiment, T represents one or more kinds of iron group element containing Fe or Fe and Co. T may be only Fe, or may be Fe whose part is substituted with Co. When part of Fe is substituted with Co, temperature properties can be improved without deteriorating magnetic properties.
In the R2T14B type compound according to the present embodiment, part of B can be substituted with carbon (C). This makes it easier to form thick two-grain boundaries during aging treatment and has an effect of easily improving coercivity.
The R2T14B type compound constituting the main phase particles 4 according to the present embodiment may contain various known additive elements, specifically, may contain at least one kind of element of Ti, V, Cu, Cr, Mn, Ni, Zr, Nb, Mo, Hf, Ta, W, Al, Ga, Si, Bi, Sn, etc.
In the present embodiment, an average grain size of the main phase grains is obtained by analyzing a cross section of the R-T-B based sintered magnet using a means of image processing or so. Specifically, a cross sectional area of each main phase grain on the cross section of the R-T-B based sintered magnet is obtained by image analysis, and a diameter of a circle having this cross sectional area (circle equivalent diameter) is defined as a grain size of the main phase grain on the cross section. Furthermore, grain sizes with respect to all of the main phase grains present in a visual field subjected to analysis on the cross section are obtained, and an arithmetic average value represented by (a total value of the grain sizes of the main phase grains)/(the number of the main phase grains) is defined as an average grain size of the main phase grains in the R-T-B based sintered magnet. Incidentally, in case of an anisotropy magnet, a cross section that is parallel to axes of easy magnetization of the R-T-B based sintered magnet is used for analysis.
The main phase grains contained in the R-T-B based sintered magnet according to the present embodiment may have an average grain size of 5 μm or less, or may have an average grain size of 3 μm or less. When the main phase grains have an average grain size in such a range, it tends to obtain a higher coercivity. The average grain size of the main phase grains has no lower limit, but may be 0.8 μm or more in view of favorably maintaining magnetization property of the R-T-B based sintered magnet.
The grain boundary of the R-T-B based sintered magnet according to the present embodiment may contain an R-T-Ga phase including R, T, and Ga and a carbide phase of M. At the time of a condition where such phases are formed by the aging treatment, a thick two-grain boundary tends to be formed, and a high coercivity tends to be expressed. Furthermore, the R-T-Ga phase may contain R6T13Ga having a La6Co11Ga3 type crystal structure. R6T13Ga is a compound having a low magnetization, and thus each of the main phase grains can be sufficiently magnetically separated even if R6T13Ga is present in the two-grain boundary. A compound contained in the carbide phase of M includes ZrC, TiC, and NbC.
The grain boundary of the R-T-B based sintered magnet according to the present embodiment may further contain an R-rich phase whose concentration of R is higher than that of the R-T-Ga phase, and may contain a B-rich phase whose concentration of boron (B) is high, an R oxide phase, an R carbide phase, or the like in addition to the R-rich phase.
In the R-T-B based sintered magnet according to the present embodiment, R may be contained at 29 mass % or more and 37 mass % or less, or may be contained at 29.5 mass % or more and 35 mass % or less. When R is contained at 29 mass % or more, the R2T14B type compound to be the main phase of the R-T-B based sintered magnet is easily sufficiently generated. This makes it hard to deposit a-Fe or so with soft magnetism and makes it easier to improve magnetic properties. When R is contained at 37 mass % or less, a ratio of the R2T14B type compound contained in the R-T-B based sintered magnet is increased, and thus residual magnetic flux density tends to improve. Furthermore, R may be contained at 30 mass % or more and 34 mass % or less in view of improving coercivity. Incidentally, the content of R is rounded off to the closest whole number or rounded off to the first decimal place. In the present embodiment, the heavy rare earth element(s) contained as R may be contained at 1.0 mass % or less in view of cost reduction and resource risk avoidance.
In the R-T-B based sintered magnet according to the present embodiment, B is contained at 0.71 mass % or more and 0.88 mass % or less. In the present embodiment, the fact that the content of B is in such a range that is significantly lower than stoichiometric composition of the R2T14B type compound is a necessary condition for forming a thick two-grain boundary at the time of the aging treatment and obtaining a high coercivity. B may be contained at 0.71 mass % or more and 0.85 mass % or less.
As described above, T is one or more kinds of iron element containing Fe or Fe and Co. When Co is contained as T, Co may be contained at 0.3 mass % or more and 4.0 mass % or less, or may be contained at 0.5 mass % or more and 1.5 mass % or less. When Co is contained at 4 mass % or less, residual magnetic flux density tends to improve, and it tends to be easier to reduce cost of the R-T-B based sintered magnet according to the present embodiment. When Co is contained at 0.3 mass % or more, corrosion resistance tends to be high. The content of Fe in the R-T-B based sintered magnet according to the present embodiment is a substantial remaining part of constituent of the R-T-B based sintered magnet.
The R-T-B based sintered magnet according to the present embodiment contains carbon (C) in a range of 0.15 mass % or more and 0.34 mass % or less. As described above, when C is contained in such a range in case of a B content that is significantly lower than stoichiometric composition of the R2T14B type compound, C is solid soluted into a B site of the R2T14B type compound of the main phase grains, and the R2T14B type compound represented by a composition formula of R2T14BxC(1-x) is formed. This makes it easier to form a thick two-grain boundary during the aging treatment and obtain a high coercivity. Thus, when C is contained at less than 0.15 mass %, a thick two-grain boundary is hard to be formed, and coercivity tends to decrease. When C is contained at more than 0.34 mass %, excessive C that cannot be solid soluted into the main phase grains tends to be formed, and coercivity tends to easily decrease. C may be contained at 0.15 mass or more and 0.30 mass % or less.
The R-T-B based sintered magnet according to the present embodiment contains Ga at 0.40 mass % or more. When Ga is contained in such a range, a thick two-grain boundary is easily formed by forming the R-T-Ga phase during the aging treatment as described above, and a high coercivity is easily obtained. Ga may be contained at 1.40 mass % or less. When Ga is contained at 1.40 mass % or less, residual magnetic flux density tends to be improve. Ga may be contained at 0.70 mass % or more and 1.40 mass % or less.
The R-T-B based sintered magnet according to the present embodiment contains M (M is at least one kind selected from a group of Zr, Ti, and Nb) at 0.25 mass % or more. M has a standard generation free energy of a carbide that is lower than that of the rare earth element R, and thus tends to be more easily combined with C than R. Thus, it becomes easy to form a thick two-grain boundary and improve coercivity by an effect of forming a carbide and C contained in R2T14BxC(1-x) dissolved from the outermost surface of the main phase grains during the aging treatment. An optimal content of M changes depending on contents of B and C, but M may be contained in a range of 2.50 mass % or less in view of prevention of decrease in residual magnetic flux density. M may be contained at 0.25 mass % or more and 2.50 mass % or less. Furthermore, M has an effect of preventing abnormal grain growth during sintering. Abnormal grain growth particularly easily occurs when a finely pulverized powder has a small pulverization particle size, and M may be contained at 0.65 mass % or more if an R-T-B based sintered magnet whose main phase grains have an average grain size of 3 μm or less is desired to be obtained. M may be Zr in view of prevention of abnormal grain growth during sintering. M may be contained at 0.65 mass % or more and 2.50 mass % or less.
The R-T-B based sintered magnet according to the present embodiment may contain Cu. Cu may be contained at 0.05 mass % or more and 1.5 mass % or less, or may be contained at 0.10 mass % or more and 1.0 mass % or less. Containing Cu makes it possible to have higher coercivity, higher corrosion resistance, and improved temperature properties of the magnet to be obtained. When Cu is contained at 1.5 mass % or less, residual magnetic flux density tends to improve. When Cu is contained at 0.05 mass % or more, coercivity tends to improve.
The R-T-B based sintered magnet according to the present embodiment may contain Al. Containing Al makes it possible to have higher coercivity, higher corrosion resistance, and improved temperature properties of the magnet to be obtained. Al may be contained at 0.03 mass % or more and 0.6 mass % or less, or may be contained at 0.10 mass % or more and 0.40 mass % or less.
The R-T-B based sintered magnet according to the present embodiment may contain an additive element other than the above elements, such as V, Cr, Mn, Ni, Mo, Hf, Ta, W, Si, Bi, and Sn. The additive element of the above elements may be contained at 2.0 mass % or less in total provided that the entire R-T-B based sintered magnet is 100 mass %.
The R-T-B based sintered magnet according to the present embodiment may contain oxygen (O) at about 0.5 mass % or less. Oxygen may be contained at 0.05 mass % or more in view of corrosion resistance, or may be 0.20 mass % or less in view of magnetic properties. Oxygen may be contained at 0.05 mass % or more and 0.15 mass % or less.
The R-T-B based sintered magnet according to the present embodiment may contain a certain amount of nitrogen (N). This certain amount changes by other parameters or so and is appropriately determined, but nitrogen may be contained at 0.01 mass % or more and 0.2 mass % or less in view of magnetic properties. Nitrogen may be contained at 0.04 mass % or more and 0.08 mass % or less.
In the R-T-B based sintered magnet according to the present embodiment, contents of each element are in the above-mentioned ranges, and contents of B and C satisfy the following specific relation. That is, a relation of 0.14≦[C]/([B]+[C])≦0.30 is satisfied, where each of [B] and [C] represents a content of B and C by atom %. When a content of B is in a range that is significantly lower than stoichiometric composition of the R2T14B type compound as described above, a ratio of C of R2T14BxC(1-x) contained in the main phase grains after sintering can be high by containing C in such a range in accordance with the content of B. This makes it possible to form a thick two-grain boundary during the aging treatment and obtain a high coercivity according to the above-mentioned mechanism. When a value of [C]/([B]+[C]) is less than 0.14, a thick two-grain boundary is hard to be formed, and coercivity decreases. When a value of [C]/([B]+[C]) is more than 0.30, it becomes impossible to substitute C with a B site of the R2T14B type compound, and coercivity easily decreases.
Furthermore, in the R-T-B based sintered magnet according to the present embodiment, contents of B, C, and M satisfy the following specific relation. That is, a relation of 5.0≦[B]+[C]−[M]≦5.6 is satisfied, where each of [B], [C], and [M] represents a content of B, C, and M by atom %. In case of a composition satisfying the relation of 5.0≦[B]+[C]−[M]≦5.6, as described above, it is possible to form a carbide due to a reaction between M and C of R2T14BxC(1-x) of the outermost surface of the main phase dissolved at the time of the aging treatment in an appropriate balance, and it is possible to form a thick two-grain boundary. This is conceived to obtain a high coercivity. When [B]+[C]−[M] is more than 5.6, M is lacking with respect to C contained in R2T14BxC(1-x) dissolved from the outermost surface of the main phase grains, which thus fails to form a sufficiently thick two-grain boundary and decreases coercivity. When [B]+[C]−[M] is less than 5.0, a different phase such as R2T17 phase of soft magnetism becomes easy to be deposited as M is contained too much, and coercivity decreases.
Furthermore, the R-T-B based sintered magnet according to the present embodiment may have a composition satisfying a relation of 5.2≦[B]+[C]−[M]≦5.4. A composition satisfying this relation makes it possible to obtain a further high coercivity.
The contents of each element in the R-T-B based sintered magnet can be measured by a generally known method, such as X-ray fluorescent analysis (XRF) and inductively coupled plasma emission spectroscopic analysis (ICP-AES). A content of oxygen is measured by inert gas fusion—non-dispersive infrared absorption method, for example. A content of carbon is measured by combustion in an oxygen airflow—infrared absorption method, for example. A content of nitrogen is measured by inert gas fusion—thermal conductivity method, for example.
In the present embodiment, the contents of B, C, and M represented by atom % are obtained by the following procedures.
(1) First, contents of each element contained in the R-T-B based sintered magnet are analyzed by the above-mentioned analysis methods to obtain analysis values (X1) by mass % of the contents of each element. Elements to be analyzed are elements contained in the R-T-B based sintered magnet at 0.05 mass % or more, oxygen, carbon, and nitrogen.
(2) The analysis values (X1) by mass % of the contents of each element are divided by atomic weights of each element to obtain values (X3).
(3) Ratios of the values (X3) of each element with respect to a total value of the values (X3) of all of the analyzed elements represented by percentage are calculated and defined as contents (X2) of each element represented by atom %.
The R-T-B based sintered magnet according to the present embodiment is generally machined into any shape and used. The R-T-B based sintered magnet according to the present embodiment has any shape, such as rectangular parallelepiped shape, hexahedron, flat plate, and square pillar. The R-T-B based sintered magnet according to the present embodiment may have any cross sectional shape, such as C shaped cylindrical shape. The square pillar may be one whose bottom surface is rectangular or square, for example.
The R-T-B based sintered magnet according to the present embodiment includes both magnet products that are magnetized after machining the magnet and magnet products in which the magnet is not magnetized.
The figure is used to describe a method for manufacturing the R-T-B based sintered magnet according to the present embodiment having the above-mentioned structure.
(a) Alloy preparing step for preparing a raw material alloy (Step S11)
(b) Pulverization step for pulverizing the raw material alloy (Step S12)
(c) Pressing step for pressing the pulverized raw material powder (Step S13)
(d) Sintering step for sintering a green compact to obtain an R-T-B based sintered magnet (Step S14)
(e) Aging treatment step for performing an aging treatment to the R-T-B based sintered magnet (Step S15)
(f) Cooling step for cooling the R-T-B based sintered magnet (Step S16)
A raw material alloy of the R-T-B based sintered magnet according to the present embodiment is prepared (alloy preparing step (Step S11)). In the alloy preparing step, raw material metals corresponding to the composition of the R-T-B based sintered magnet according to the present embodiment are melted in a vacuum or in an inert gas atmosphere of Ar gas or so, and are subjected to casting so as to prepare a raw material alloy having a desired composition. Incidentally, a one-alloy method using a single alloy as a raw material alloy is described in the present embodiment, but a two-alloy method that prepares a raw material powder by mixing two kinds of alloys of a first alloy and a second alloy may be employed.
As the raw material metals, for example, rare earth metals, rare earth alloys, pure iron, ferroboron, alloy or compound of these, or the like can be used. The raw material metals are casted by ingot casting method, strip casting method, book molding method, centrifugal casting method, or the like. The obtained raw material alloy is subjected to a homogenization treatment as necessary in the presence of solidification segregation. The homogenization treatment of the raw material alloy is conducted in a vacuum or an inert gas atmosphere at a temperature of 700° C. to 1500° C. for 1 hour or longer. The alloy for the R-T-B based sintered magnet is melted and homogenized by this treatment.
In the present embodiment, an alloy for the R-T-B based sintered magnet containing carbon may be manufactured in a manner that at least part of carbon finally contained in the R-T-B based sintered magnet is melted with the raw material metal in the alloy preparing step to perform casting. When carbon is added in the alloy step, this makes it easier to form the main phase grains containing the R2T14B type compound represented by the composition formula of R2T14BxC(1-x) and form a thick two-grain boundary during the aging treatment. The carbon source used for the casting is a substance containing carbon. A substance having a high content of carbon, such as graphite and carbon black, can be used.
After the raw material alloy is prepared, this raw material alloy is pulverized (pulverization step: Step S12). The pulverization step includes a coarse pulverization step (Step S12-1) for pulverizing the raw material alloy until particle sizes become about hundreds m to several mm and a fine pulverization step (Step S12-2) for finely pulverizing the raw material alloy until particle sizes become about several μm.
The raw material alloy is coarsely pulverized until particle sizes respectively become about hundreds m to several mm (coarse pulverization step (Step S12-1)). This obtains a coarsely pulverized powder of the raw material alloy. The coarse pulverization can be carried out by causing a self-collapsed pulverization in such manner that hydrogen is stored in the raw material alloy, and that hydrogen is released based on differences in the storage amount of hydrogen among different phases to perform dehydrogenation (hydrogen storage pulverization).
Incidentally, the coarse pulverization step (Step S12-1) may be carried out using a coarse pulverization machine, such as stamp mill, jaw crusher, and brown mill, in an inert gas atmosphere except for using the above-mentioned hydrogen storage pulverization.
The atmosphere in each step from the pulverization step (Step S12) to the sintering step (Step S15) may be a low oxygen concentration to obtain high magnetic properties. The oxygen concentration is adjusted by controlling the atmosphere in each manufacturing step or so. When the oxygen concentration in each manufacturing step is high, the rare earth elements in the raw material alloy powder are oxidized, and the oxygen amount of the R-T-B based sintered magnet is increased to cause decrease in coercivity of the R-T-B based sintered magnet. Thus, the oxygen concentration in each step may be 100 ppm or less, for example.
After the raw material alloy is coarsely pulverized, the coarsely pulverized powder of the obtained raw material alloy is finely pulverized until an average particle size becomes about several m (fine pulverization step (Step S12-2)). This obtains a finely pulverized powder of the raw material alloy. The coarsely pulverized powder may be further finely pulverized to obtain a finely pulverized powder having particles whose average particle size is 0.1 μm or more and 4.0 μm or less. This average particle size may be 0.5 μm or more and 3.0 μm or less. When the finely pulverized powder is configured to have such an average particle size, it tends to have a small average grain size of the main phase grains after sintering and obtain a high coercivity.
The fine pulverization is carried out by further pulverizing the coarsely pulverized powder using a fine pulverization machine, such as jet mil and bead mill, while conditions of pulverization time or so are appropriately adjusted. A jet mill is a dry pulverization method by releasing a high pressure inert gas (e.g. N2 gas) from a narrow nozzle to generate a high speed gas flow and accelerating the coarsely pulverized powder of the raw material alloy using this high speed gas flow to cause collision among the coarsely pulverized powder of the raw material alloy and collision with a target or a container wall.
In particular, when a finely pulverized powder having a small particle size is obtained using a jet mill, the surface of the pulverized powder is very active, which easily generates reaggregation of the pulverized powder and adhesion thereof to a container wall and tends to have a low yield. Thus, when the coarsely pulverized powder of the raw material alloy is finely pulverized, a finely pulverized powder can be obtained at a high yield by adding a pulverization aid of zinc stearate, oleic amide, or the like to prevent reaggregation of the powder and adhesion thereof to a container wall. A finely pulverized powder that can be oriented easily during pressing can be obtained by adding a pulverization aid. An addition amount of a pulverization aid changes based on a particle size of the finely pulverized powder and a kind of the pulverization aid to be added, but may be about 0.01% to 1% by mass %.
There is a wet pulverization method other than a dry pulverization method like a jet mill. A bead mill for performing a high speed stirring using a small diameter bead can be employed as the wet pulverization method. A multiple pulverization for conducting a dry pulverization using a jet mill and further conducting a wet pulverization using a bead mill may be carried out.
After the raw material alloy is finely pulverized, the finely pulverized powder is pressed into a desired shape (pressing step (Step S13)). In the pressing step (Step S13), the finely pulverized powder is filled in a press mold arranged in an electromagnet and is pressed into any shape. This operation is carried out while a magnetic field is applied to generate a predetermined orientation of the finely pulverized powder and orient crystal axis. This obtains a green compact. A green compact to be obtained is oriented in a specific direction, and thus an R-T-B based sintered magnet having anisotropy with stronger magnetism is obtained.
The finely pulverized powder may be pressed at 30 MPa to 300 MPa. The magnetic field to be applied may be at 950 kA/m to 1600 kA/m. The magnetic field to be applied is not limited to a static magnetic field, and may be a pulsed magnetic field. A static magnetic field and a pulsed magnetic field may be used at the same time as the magnetic field to be applied.
Incidentally, a wet pressing for pressing a slurry where the finely pulverized powder is dispersed in a solvent of oil or so can be applied to the pressing method other than a dry pressing for pressing the finely pulverized powder as it is as described above.
The green compact obtained by pressing the finely pulverized powder has any shape, such as parallel piped shape, flat plate shape, column shape, and ring shape, based on a desired shape of the R-T-B based sintered magnet.
The green compact obtained by being pressed in a magnetic field and pressing into a desired shape is sintered in a vacuum or an inert gas atmosphere to obtain the R-T-B based sintered magnet (sintering step (Step S14)). The green compact is sintered by being heated in a vacuum or in the presence of an inert gas at 900° C. to 1200° C. for 1 hour to 72 hours, for example. This causes the finely pulverized powder to have liquid phase sintering, and an R-T-B based sintered magnet (a sintered body of an R-T-B based magnet) whose main phase has an improved volume ratio is obtained.
After the green compact is sintered, the sintered body may be rapidly cooled in view of improving manufacturing efficiency.
After the green compact is sintered, the R-T-B based sintered magnet is subjected to an aging treatment (aging treatment step (Step S15)). After the sintering, the R-T-B based sintered magnet is subjected to an aging treatment by being held at a temperature that is lower than the temperature during the sintering. The aging treatment can be carried out by conducting a heating treatment in a vacuum or in the presence of an inert gas at 400° C. to 900° C. for 10 minutes to 10 hours, for example. If necessary, the aging treatment may be carried out multiple times at different temperatures. Such an aging treatment can improve magnetic properties of the R-T-B based sintered magnet.
The aging treatment of the R-T-B based sintered magnet of the present embodiment may include a treatment for holding the R-T-B based sintered magnet at 450° C. to 550° C. for 10 minutes to 10 hours. Aging treatment temperature and aging treatment time are appropriately adjusted in the ranges based on conditions of composition, difference between grain size and grain size distribution, and the like. This makes it possible to form thick two-grain boundaries and thus obtain a high coercivity.
After the R-T-B based sintered magnet is subjected to the aging treatment, the R-T-B based sintered magnet is rapidly cooled in an Ar gas atmosphere (cooling step (Step S16)). Then, the R-T-B based sintered magnet according to the present embodiment can be obtained. To form thick two-grain boundaries and obtain a high coercivity, a cooling rate may be 30° C./min or more.
The R-T-B based sintered magnet obtained through the above steps may be machined into a desired shape as necessary. This machining method may be a shaping process, such as cutting and grinding, a chamfering process, such as barrel polishing, or the like.
There may be a step for further diffusing heavy rare earth elements to the grain boundaries of the machined R-T-B based sintered magnet. This grain boundary diffusion can be carried out by performing a heat treatment after a compound containing heavy rare earth elements is adhered on the surface of the R-T-B based sintered magnet by application, vapor deposition, or the like, or by performing a heat treatment against the R-T-B based sintered magnet in an atmosphere containing a vapor of heavy rare earth elements. This makes it possible to further improve coercivity of the R-T-B based sintered magnet.
The obtained R-T-B based sintered magnet may be subjected to a surface treatment, such as plating, resin coating, oxidation treatment, and chemical conversion treatment. This makes it possible to further improve corrosion resistance.
The R-T-B based sintered magnet according to the present embodiment is preferably used as a magnet of, for example, a surface magnet type (Surface Permanent Magnet: SPM) motor where a magnet is attached on the surface of a rotor, an interior magnet embedded type (Interior Permanent Magnet: IPM) motor such as inner rotor type brushless motor, and a Permanent magnet Reluctance Motor (PRM). Specifically, the R-T-B based sintered magnet according to the present embodiment is preferably used for a spindle motor for a hard disk rotary drive or a voice coil motor of a hard disk drive, a motor for an electric vehicle or a hybrid car, an electric power steering motor for an automobile, a servo motor for a machine tool, a motor for vibrator of a cellular phone, a motor for a printer, a motor for a magnet generator and the like.
The second embodiment of the present invention is directed to an R-T-B based permanent magnet manufactured by hot working. Matters of the second embodiment that are not described below are identical to those of the first embodiment. The term of “sintering” in the first embodiment shall be replaced as necessary.
The method for manufacturing the R-T-B based permanent magnet according to the present embodiment has the following steps.
(a) Melt rapid cooling step for melting a raw material metal and rapidly cooling an obtained molten metal to obtain a ribbon
(b) Pulverization step for pulverizing the ribbon to obtain a flaky raw material powder
(c) Cold forming step for performing cold forming to the pulverized raw material powder
(d) Preliminary heating step for preliminarily heating the cold-formed body
(e) Hot forming step for performing hot forming to the preliminarily heated cold-formed body
(f) Hot plastic working step for plastically deforming the hot-formed body into a predetermined shape
(g) Aging treatment step for performing an aging treatment to the R-T-B based permanent magnet
(a) The melt rapid cooling step is a step for melting a raw material metal and rapidly cooling an obtained molten metal to obtain a ribbon. The raw material metal is melted by any method as long as a molten metal whose component is uniform and fluidity is capable of rapid cooling solidification is obtained. The temperature of the molten metal is not limited, but may be 1000° C. or higher.
Next, the molten metal is rapidly cooled to obtain a ribbon. Specifically, the ribbon is obtained by dropping the molten metal to a rotary roll. A cooling rate of the molten metal can be adjusted by controlling a rotating speed of the rotary roll and a drop amount of the molten metal. The rotating speed is normally 10 to 30 m/sec.
(b) The pulverization step is a step for pulverizing the ribbon obtained in the melt rapid cooling step (a). There is no limit for the pulverization method. The pulverization obtains a flaky alloy powder composed of fine crystal grains of about 20 nm.
(c) The cold forming step is a step for performing cold forming to the flaky raw material powder obtained in the pulverization step (b). The cold forming is carried out by filling the raw material powder into a mold and then pressing this at a room temperature. The pressing is carried out at any pressure. The higher the pressure is, the higher the density of a cold-formed body to be obtained becomes. The density is, however, saturated if the pressure becomes a certain value or higher. Thus, no effect is demonstrated if pressure is added more than necessary. The pressing pressure is appropriately selected based on composition, particle size, and the like of the alloy powder.
There is no limit for the pressing time either. The longer the pressing time is, the higher the density of a cold-formed body to be obtained becomes. The density is, however, saturated if the pressing time becomes a certain value or longer. The density is normally saturated when the pressing time is 1 to 5 seconds.
(d) The preliminary heating step is a step for preliminarily heating the cold-formed body obtained in the cold forming step (c). The preliminary heating temperature is not limited, but is normally 500° C. or higher and 850° C. or lower. Conditions of the preliminary heating are optimized to obtain a formed body whose crystal structure is uniform and fine in the hot forming step (e) and to further improve a magnetic orientation degree in the hot plastic working step (f).
When the preliminary heating temperature is 500° C. or higher, grain boundary phases can be sufficiently liquefied in the hot forming step, and cracks of the formed body become hard to occur during the hot forming. The preliminary heating temperature may be 600° C. or higher, or may be 700° C. or higher. In contrast, when the preliminary heating temperature is 850° C. or lower, it becomes easier to prevent crystal grains from being coarse and to further prevent oxidation of magnetic materials. The preliminary heating temperature may be 800° C. or lower, or may be 780° C. or lower.
The preliminary heating time is a time where the cold-formed body reaches a certain temperature. The preliminary heating time is appropriately controlled to sufficiently liquefy grain boundary phases in the hot forming step, to prevent cracks of the formed body from occurring during the hot forming, and to make it easier to prevent crystal grains from being coarse. The preliminary heating time may be appropriately selected based on size of the formed body, the preliminary heating temperature, and the like. In general, the larger the size of the formed body becomes, the longer a preferable preliminary heating time becomes. Also, the lower the preliminary heating temperature becomes, the longer a preferable preliminary heating time becomes. The atmosphere during the preliminary heating is not limited, but may be an inert atmosphere or a reducing atmosphere in view of preventing oxidation of magnetic materials and decrease in magnetic properties.
(e) The hot forming step is a step for performing hot pressing to the preliminarily heated cold-formed body obtained in the preliminary heating step (d). The hot forming step can densify magnet materials.
The term of “hot forming” is a so-called hot pressing method. When the cold-formed body is hotly pressed using a hot pressing method, pores remaining in the cold-formed body disappear to achieve densification of the cold-formed body.
The hot forming using a hot pressing method is carried out by any method, such as a method for preliminarily heating the cold-formed body, inserting the preliminarily heated cold-formed body into a mold that is heated to a predetermined temperature, and pressing the cold-formed body at a predetermined pressure for a predetermined time. Hereinafter, the hot forming by this method will be described.
Conditions of the hot pressing are optimally selected based on composition, required properties, and the like. In general, when the hot pressing temperature is 750° C. or higher, grain boundary phases can be sufficiently liquefied, the formed body is sufficiently densified, and cracks of the formed body become hard to occur. In contrast, when the hot pressing temperature is 850° C. or lower, it becomes easier to prevent crystal grains from being coarse, and magnetic properties can be consequently improved.
The hot pressing is carried out at any pressure. The higher the pressure is, the higher the density of a hot-formed body to be obtained becomes. The density is, however, saturated if the pressure becomes a certain value or higher. Thus, no effect is demonstrated if pressure is added more than necessary. The hot pressing pressure is appropriately selected based on composition, particle size, and the like of the alloy powder.
The hot pressing time is not limited either. The longer the hot pressing time is, the higher the density of a hot-formed body to be obtained becomes. Crystal grains may, however, be coarse if the hot pressing time is longer more than necessary. The hot pressing time is appropriately selected based on composition, particle size, and the like of the alloy powder.
The atmosphere during the hot pressing is not limited, but may be an inert atmosphere or a reducing atmosphere in view of preventing oxidation of magnetic materials and decrease in magnetic properties.
(f) The hot plastic working step is a step for obtaining a magnet material by plastically deforming the hot-formed body obtained in the hot forming step (e) into a predetermined shape. The hot plastic working step is carried out by any method, but is particularly preferably carried out by a method of hot extrusion in view of productivity.
The working temperature is not limited. In general, when the working temperature is 750° C. or higher, grain boundary phases are sufficiently liquefied, the formed body is sufficiently densified, and cracks of the formed body become hard to occur. In contrast, when the working temperature is 850° C. or lower, it becomes easier to prevent crystal grains from being coarse, and magnetic properties can be consequently improved. An R-T-B based permanent magnet having desired composition and shape is obtained by carrying out a post machining as necessary after the hot plastic working step.
(g) The aging treatment step is a step for performing an aging treatment to the R-T-B based permanent magnet obtained in the hot plastic working step (f). The aging treatment is performed to the R-T-B based permanent magnet by holding the obtained the R-T-B based permanent magnet at a temperature that is lower than the temperature during the hot plastic working step after the hot plastic working, for example. The aging treatment can be carried out by performing a heating treatment in a vacuum or in the presence of an inert gas at 400° C. to 700° C. for 10 minutes to 10 hours, for example. The aging treatment may be carried out multiple times by changing the temperature as necessary. Such an aging treatment can improve magnetic properties of the R-T-B based permanent magnet. In the R-T-B based permanent magnet of the present embodiment, the temperature during the aging treatment is particularly preferably in a range of 400° C. to 600° C. In this temperature range, aging treatment temperature and aging treatment time are appropriately adjusted based on conditions, such as composition and difference between grain size and grain size distribution. This makes it possible to form thick two-grain boundaries and thus obtain a high coercivity.
Hereinafter, a mechanism how an R-T-B based permanent magnet having magnetic anisotropy can be obtained by the hot forming step and the hot plastic working step will be described.
The inside of the hot-formed body consists of crystal grains and grain boundary phases. The grain boundary phases begin to liquefy when the formed body becomes high temperature during the hot forming. Then, when the heating temperature becomes higher, the crystal grains are surrounded by the liquefied grain boundary phases. Then, the crystal grains become possible to rotate. In this stage, however, the directions of axes of easy magnetization, that is, the directions of magnetization are nonuniform (equalization state). That is, the hot-formed body has normally no magnetic anisotropy.
Next, the obtained hot-formed body is subjected to the hot plastic working to plastically deform the hot-formed body and obtain a magnet material having a desired shape. At this time, the crystal grains are compressed in a pressurizing direction and plastically deformed, and the axes of easy magnetization are oriented in the pressurizing direction at the same time. Thus, an R-T-B based permanent magnet having magnetic anisotropy is obtained.
Incidentally, the present invention is not limited to the above embodiments, but can be variously changed within the scope thereof.
Hereinafter, the invention will be described in more detail based on the examples, but is not limited thereto.
First, raw material alloys were prepared. Raw materials were blended so that R-T-B based sintered magnets having compositions shown in Table 1 were obtained, melted, and casted by a strip casting method. Then, flaky raw material alloys were obtained. The raw material alloys were prepared so that the R-T-B based sintered magnets finally obtained the compositions shown in Table 1 by adjusting a carbon amount of the raw materials using graphite and considering a carbon amount mixed from a pulverization aid during a fine pulverization so as to reduce an amount that is expected to increase by the pulverization aid from the charge composition.
Next, a hydrogen pulverization treatment (coarse pulverization) for respectively storing hydrogen in these raw material alloys at room temperatures and respectively performing dehydrogenation at 400° C. for 1 hour in an Ar atmosphere was carried out.
Incidentally, in the present examples, each step from this hydrogen pulverization treatment to sintering (fine pulverization and pressing) was carried out in an inert gas atmosphere having an oxygen concentration of less than 50 ppm (the same shall apply to the following experimental examples).
Next, an oleic amide of 0.07 mass % as a pulverization aid was added to the coarsely pulverized powder subjected to the hydrogen pulverization treatment, and a fine pulverization was subsequently performed thereto using a jet mill. In the fine pulverization, a particle size of the finely pulverized powder was adjusted so that the main phase grains of the R-T-B based sintered magnet had an average grain size of 3 m by adjusting a classification condition of the jet mill.
The obtained finely pulverized powder was filled in a press mold arranged in an electromagnet and pressed at 120 MPa while a magnetic field of 1200 kA/m was applied, whereby a green compact was obtained.
Thereafter, the obtained green compact was sintered. The green compact was sintered by being held in a vacuum at 1050° C. for 12 hours and rapidly cooled, whereby a sintered body (R-T-B based sintered magnet) was obtained. Then, the obtained sintered body was subjected to an aging treatment performed at 500° C. for 1 hour (both of which were in an Ar atmosphere), whereby R-T-B sintered magnets of Experimental Examples 1 to 7 were respectively obtained.
Table 1 shows results of composition analysis with respect to the R-T-B based sintered magnets of Experimental Examples 1 to 7. In the contents of each element shown in Table 1, the contents of Nd, Pr, Dy, Tb, Fe, Co, Ga, Al, Cu, Zr, Ti, and Nb were measured by a fluorescent X-ray analysis, the content of B was measured by an ICP emission analysis, the content of O was measured by an inert gas fusion—non-dispersive infrared absorption method, the content of C was measured by a combustion in oxygen airflow-infrared absorption method, and the content of N was measured by an inert gas fusion—thermal conductivity method. [B]+[C]−[M] and [C]/([B]+[C]) were calculated by converting the contents of each element by mass % obtained by these methods into contents by atom %. Incidentally, T.RE in Tables is a summation of the contents of Nd, Pr, Dy, and Tb and represents a total content of the rare earth elements in the R-T-B based sintered magnet.
A B-H tracer was used to measure magnetic properties of the R-T-B based sintered magnets obtained in Experimental Examples 1 to 7. Residual magnetic flux density Br and coercivity HcJ were measured as the magnetic properties. These results are also shown in Table 1.
Judging from the results of the composition analysis, the R-T-B based sintered magnets of Experimental Examples 3 to 6 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 1, 2, and 7 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 3 to 6 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 1, 2, and 7, as shown in Table 1, it can be said that a high coercivity is obtained when both 0.14≦[C]/([B]+[C])≦0.30 and 5.0≦[B]+[C]−[M]≦5.6 are satisfied.
The cross section of the R-T-B based sintered magnet of Experimental Example 3 was processed by a focused ion beam (FIB), and the structure of the sintered body was observed using a scanning electron microscope (SEM).
R-T-B based sintered magnets of Experimental Examples 8 to 14 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 2 were obtained. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 2.
Table 2 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 8 to 14. The R-T-B based sintered magnets of Experimental Examples 9 to 13 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 8 and 14 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 9 to 13 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 8 and 14, it can be said that a high coercivity is obtained when both 0.14≦[C]/([B]+[C]) 0.30 and 5.0≦[B]+[C]−[M]≦5.6 are satisfied. In particular, it was also confirmed that Experimental Examples 10 and 11 satisfying 5.2≦[B]+[C]−[M]≦5.4 had higher values of coercivity.
When the fracture surfaces of the respective R-T-B based sintered magnets of Experimental Examples 8 to 14 were checked, it was confirmed that main phase grains enlarged to about 10 μm grain size or more due to abnormal grain growth during sintering were found, and that more such enlarged main phase grains were found particularly in the R-T-B based sintered magnet of Experimental Example 8 having the least amount of Zr.
R-T-B based sintered magnets of Experimental Examples 15 to 21 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 3 were obtained. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 3.
Table 3 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 15 to 21. The R-T-B based sintered magnets of Experimental Examples 16 to 20 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 15 and 21 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 16 to 20 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 15 and 21, it can be said that a high coercivity is obtained when both 0.14≦[C]/([B]+[C]) 0.30 and 5.0≦[B]+[C]−[M]≦5.6 are satisfied. In particular, it was also confirmed that Experimental Examples 17 to 19 satisfying 5.2≦[B]+[C]−[M]≦5.4 had higher values of coercivity.
R-T-B based sintered magnets of Experimental Examples 22 to 28 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 4 were obtained. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 4.
Table 4 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 22 to 28. The R-T-B based sintered magnets of Experimental Examples 23 to 27 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 22 and 28 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 23 to 27 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 22 and 28, it can be said that a high coercivity is obtained when both 0.14≦[C]/([B]+[C]) 0.30 and 5.0=[B]+[C]−[M]≦5.6 are satisfied. In particular, it was also confirmed that Experimental Examples 25 and 26 satisfying 5.2≦[B]+[C]−[M]≦5.4 had higher values of coercivity.
R-T-B based sintered magnets of Experimental Examples 29 to 34 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 5 were obtained by changing an amount of Ga. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 5.
Table 5 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 29 to 34. The R-T-B based sintered magnets of Experimental Examples 30 to 34 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnet of Experimental Example 29 corresponds to Comparative Example as it fails to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 30 to 34 containing Ga at 0.40 mass % or more have a higher coercivity than that of the R-T-B based sintered magnet of Experimental Example 29, it was confirmed that a high coercivity is obtained when Ga is contained at 0.40 mass % or more. It was also found that Experimental Example 34 containing Ga at more than 1.40 mass % tends to have a low value of residual magnetic flux density.
R-T-B based sintered magnets of Experimental Examples 35 to 41 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 6 were obtained by using Ti as M instead of Zr. Also, an R-T-B based sintered magnet of Experimental Example 38a containing Zr and Ti as M was obtained. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 6.
Table 6 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 35 to 41. The R-T-B based sintered magnets of Experimental Examples 36 to 40 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 35 and 41 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 36 to 40 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 35 and 41, it was confirmed that a high coercivity is obtained in the ranges of 0.14≦[C]/([B]+[C]) 0.30 and 5.0≦[B]+[C]−[M]≦5.6 even if Ti is used as M. In particular, it was also confirmed that Experimental Examples 38 and 39 satisfying 5.2≦[B]+[C]−[M]≦5.4 had higher values of coercivity.
Experimental Example 38a using Ti and Zr as M also obtained a high coercivity in the same manner as the other experimental examples using only Ti as M.
R-T-B based sintered magnets of Experimental Examples 42 to 48 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 7 were obtained by using Nb as M instead of Zr. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 7.
Table 7 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 42 to 48. The R-T-B based sintered magnets of Experimental Examples 43 to 47 correspond to Examples as they satisfy the conditions of the present invention, and the R-T-B based sintered magnets of Experimental Examples 42 and 48 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. Since the R-T-B based sintered magnets of Experimental Examples 43 to 47 have a higher coercivity than that of the R-T-B based sintered magnets of Experimental Examples 42 and 48, it was confirmed that a high coercivity is obtained in the ranges of 0.14≦[C]/([B]+[C])≦0.30 and 5.0≦[B]+[C]−[M]≦5.6 even if Nb is used as M. In particular, it was also confirmed that Experimental Examples 45 and 46 satisfying 5.2≦[B]+[C]−[M]≦5.4 had higher values of coercivity.
R-T-B based sintered magnets of Experimental Examples 49 to 54 were respectively obtained in the same manner as Experimental Examples 1 to 7 except that raw materials were blended so that the R-T-B based sintered magnets having compositions shown in Table 8 were obtained. Each of the obtained R-T-B based sintered magnets was subjected to composition analysis in the same manner as Experimental Examples 1 to 7. The results of composition analysis are shown in Table 8.
Table 8 also shows measurement results of magnetic properties of the R-T-B based sintered magnets of Experimental Examples 49 to 54. The R-T-B based sintered magnets of Experimental Examples 50 and 53 correspond to Examples as they satisfy the conditions of the present invention, and the respective R-T-B based sintered magnets of Experimental Examples 49, 51, 52, and 54 correspond to Comparative Examples as they fail to satisfy the conditions of the present invention. It was confirmed that a high coercivity is obtained in the ranges of 0.14≦[C]/([B]+[C])≦0.30 and 5.0≦[B]+[C]−[M]≦5.6 even with a composition containing a very small amount of Dy and Tb like the present experimental examples.
| Number | Date | Country | Kind |
|---|---|---|---|
| 2016-035104 | Feb 2016 | JP | national |
