PERMANENT MAGNETIC ALLOY WITH EXCELLENT HEAT RESISTANCE AND PROCESS FOR PRODUCING THE SAME

Description

TECHNICAL FIELD OF THE INVENTION

[0001] The present invention relates to a permanent magnet alloy based on R (wherein R represents yttrium (Y) or a rare-earth element), boron (B), carbon (C), cobalt (Co) and iron (Fe), which exhibits particularly improved heat resistance as such that little degradation occurs on the magnetic force even in case it is used under ambient at a temperature as high as 200 °C.

BACKGROUND OF THE INVENTION

[0002] A Sm-Co based magnet is known as a rare-earth magnet having improved heat resistance, but is expensive. The term "heat resistance" as referred herein particularly signifies that the magnetic force of the magnet does not degrade by heat. As disclosed in Japanese Patent Public Disclosure No. 4-116144 (Patent No. 2740981), one of inventors of the present invention and others have proposed a R-B-C-Co-Fe based permanent magnet alloy as a rare-earth magnet reduced in cost and yet improved in heat resistance. This magnet alloy contains carbon (C) as an essential alloy element, and utilizes a combination of a light rare-earth element and a heavy rare-earth element for the rare-earth element (R). The disclosure teaches that the irreversible demagnetization of the magnet alloy is improved remarkably (i.e., the negative irreverible demagnetization values approach 0%) by the incorporation of C, and that the irreversible demagnetization is further improved by partly incorporating a heavy rare-earth element for R.

OBJECT OF THE INVENTION

[0003] In case a permanent magnet is assembled in appliances that are installed in the vicinity of a heat-emitting source, it is essential that the magnetic force of the permanent magnet does not drop when brought to higher temperatures, i.e., that the residual magnetic flux density (Br) does not undergo degradation when heated. However, there are cases in which the magnet is used under conditions as such that the operation temperature approaches ca. 200 °C (e.g., automobile engine appliances are operated at ca. 200 °C, and as a matter of course, the same holds true for motors of electric automotive vehicles). Then, Sm-Co based magnets are the only type of known magnets applicable to this field. However, as stated above, Sm-Co based magnets are expensive, and the ordinary Nd-Fe(Co)-B based rare-earth magnets are unfeasible for such high temperature (e.g., 200 °C) applications.

[0004] Although the aforementioned Japanese Patent Public Disclosure No. 4-116144 teaches that the incorporation of C (carbon) as the alloying element in a permanent magnet improves the irreversible demagnetization and that the partial replacement of R by a heavy rare-earth element further improves the irreversible demagnetization, there is not shown any magnet that does not undergo demagnetization when heated to 200 °C.

[0005] In the light of such circumstances, an object of the present invention is to provide a permanent magnet having improved heat resistance feasible for use at such a high temperature of 200 °C, yet at a low production cost.

SUMMARY OF THE INVENTION

[0006] In order to achieve the object above based on the fundamental concept of incorporating C to improve the heat resistance of the permanent magnet alloy, as proposed in Japanese Patent Public Disclosure No. 4-116144, the present inventors investigated and studied the influence of each of the heavy rare-earth elements on the heat resistance. As a result, in addition to the incorporation of the basic rare-earth elements such as Nd and Pr, it has been newly found that the addition of Dy and Tb in combination and in proper quantities, particularly when they are added in relation to each other, greatly improves the heat resistance of the permanent magnet.

[0007] Thus, in accordance with the present invention, there is provided a permanent magnet alloy having an improved heat resistance as set forth in claim 1.

[0008] Also provided is a process for producing such a permanent magnet alloy as set forth in claim 7.

[0009] Preferred embodiments of the present invention may be gathered from the dependent claims.

BRIEF EXPLANATION OF THE DRAWINGS

[0010] 

FIG. 1 is a diagram showing the distribution of irreversible demagnetization, in which the values of irreversible demagnetization at 200 °C of the magnets shown in Table 2 are arranged in terms of the content of Dy and Tb;

FIG. 2 is a diagram showing the observed irreversible demagnetization values at differing temperatures for the magnet described in Example 24 disclosed in Japanese Patent Public Disclosure No. 4-116144 and those of Example 2 according to the present invention, in which the specimens are each shaped as such that the permeance coefficient (Pc) be 3 and magnetized by applying 50 KOe; and

FIG. 3 is a diagram showing the observed irreversible demagnetization values similar to those shown in Fig. 2, except that the specimens are shaped as such that they may yield a permeance coefficient (Pc) of 1.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0011] In designing appliances which may be operated under cases as such that the magnet assembled therein is brought at a temperature of 200 °C, the irreversible demagnetization at 200 °C serves as an index. More specifically, it is preferred to select a design that the value (a negative value) of irreversible demagnetization (200 °C) according to equation

(1) above approaches 0 % as possible.

[0012] When a proper amount of C is incorporated into a R-B-Co-Fe based sintered alloy, where R is representatively Nd or a combination of Nd and Pr, the value (negative value) of irreversible demagnetization (160 °C) approaches zero. This fact is shown in the example of Japanese Patent Public Disclosure No. 4-116144. However, the irreversible demagnetization (160 °C) described in this disclosure is obtained by replacing the value of A₂₀₀ by A₁₆₀ (where A₁₆₀ is the flux value of a magnet measured on a specimen maintained at 160 °C for a duration of 120 minutes and then cooled to room temperature), and is an observed value for a permeance coefficient (Pc) of 3. That is, the irreversible demagnetization (160 °C) is a value obtained by magnetizing a specimen shaped as such that Pc be 3 and magnetized at 50 KOe, and by measuring the flux values A₂₅ and A₁₆₀. As described in the disclosure, the incorporation of C is known to be effective for improving the heat resistance (and for imparting resistance against oxidation). However, nothing is known about the irreversible demagnetization at 200 °C. Furthermore, in the existing R-(Fe,Co)-B based sintered magnet alloys (which do not contain C as the alloy element), none is found to yield an irreversible demagnetization (200 °C) in a range of 0% to -20 %.

[0013] Since the proposal of the disclosure above, the present inventors have continued various types of tests and researches on the composition of the alloy and the process for the production thereof with an aim to improve the heat resistance of the R-Fe-Co-C-B based sintered magnet alloys, and have found that the combined addition of Dy and Tb in proper quantities results in a magnet alloy having a considerably low irreversible demagnetization. The effect of the addition is not remarkable when Dy or Tb is added independent to each other, but a favorable heat resistance is achieved in case the both are added in combination.

[0014] The reason for confining the content of each of the components constituting the magnet allow according to the present invention is outlined below, together with the process for producing the alloy magnet according to the present invention. In the following description, " at.% signifies % by atomic, that is percentage on an atomic basis".

C: 0.1 - 15 at.%

[0015] As described in Japanese Patent Public Disclosure No. 4-116144, the disadvantageous characteristic of a rare-earth magnet. i.e., the tendency prone to oxidation, can be modified by the addition of C while favorably maintaining the magnetic properties of the magnet alloy. Carbon also contributes to the reduction of irreversible demagnetization. If the addition of C is less than 0.1 at.%, the effect thereof on improving the oxidation-resistance and the heat resistance is not sufficient. If the addition of C should exceed 15 at.%, on the other hand, the value of Br begins to drop. Accordingly, C is incorporated at a content in a range of 0.1 to 15 at.%, but a preferred range is 1.0 - 10 at.%, and more preferably, is in the range of 2.5 to 7 at.%.

B: 0.5 to 15 at.%

[0016] Boron (B) is necessary for the formation of a magnetic phase, and it should be present at least 0.5 at.%. However, the addition of B in excessive amount reversibly deteriorates the magnetic properties. Accordingly, B is added in an amount of 0.5 to 15 at.%, preferably 1.0 to 10 at.%, and more preferably, 1.5 to 7 at.%.

C and B in total: 2 to 30 at.%

[0017] For the formation of a magnetic phase and the improvement of the resistance against oxidation, C and B in total must account for at least 2 at.%. However, the incorporation of C and B in total exceeding 30 at.% impairs the magnetic properties; accordingly, C and B in total must account for 2 to 30 at.%.

Co: 40 at.% or less

[0018] Cobalt elevates the Curie point while maintaining the magnetic properties. Thus, the addition of Co is essential, but an addition thereof in an amount exceeding 40 at.% considerably decreases the coercive force of the magnet. Accordingly, the addition of Co must be 40 at.% or less.

Dy and Tb in total: 0.5 to 5 at.%

[0019] Dysprosium (Dy) and terbium (Tb) are the characteristic elements of the magnet of the present invention, and their combined addition remarkably lowers the irreversible demagnetization. For this purpose, Dy and Tb must be added at an amount of 0.5 at.% or more in total, but their effect on improving the heat resistance saturates if a total addition of them is in excess of 5 at.% and it may reversibly affect the magnetic properties. Accordingly, their addition in total must be 0.5 to 5 at. %. As shown hereinafter in the comparative example, the addition of Dy or Tb alone does not contribute to the reduction of irreversible demagnetization. Presumably, Dy and Tb function synergetically to lower the irreversible demagnetization. Furthermore, those elements are preferably added at a Tb(at.%)/Dy( at.%) ratio, expressed by percentage on atomic basis, in the range of 0.1 to 0.8. As shown in the examples hereinafter, the addition of 0.3 to 4.9 at.% of Dy and 0.1 to 4.7 at.% of Tb enables a magnet having improved heat resistance with a irreversible demagnetization at 200 °C at a permeance coefficient of 1 in a range of 0 to -20%, preferably 0 to -15%.

R: 8 to 20 at.%

[0020] As rare-earth elements other than Dy and Tb, at least one element selected from the group consisting of Nd, Pr, Ce, La, Y, Gd, Ho, Er and Tm may be added either singly or in combination thereof at an amount of 8 to 20 at.%. By the addition of R, a magnetic phase and a grain boundary phase are developed in the sintered magnet alloy to maintain iHc and Br at high values. Among the elements for R, particularly preferred are Nd and Pr, and the addition of Nd alone or a combination of Nd with Pr is most preferred. If the addition of R is less than 8 at.%, a sufficient high Br cannot be achieved, and the addition of R in excess of 20 at.% results in an insufficient value of Br. A preferred range of R is 13 to 18 at.%.

[0021] A permanent magnet alloy according to the present invention having the composition above yields an irreversible demagnetization (200 °C) in accordance with equation (1) above at a low level as such in a range of 0 to -20 %, preferably 0 to -15 %, and most preferably, 0 to -5 %. Thus, the present invention provides for the first time, a permanent magnet alloy other than a Sm-Co based magnet suitable for high temperature use. For high temperature applications, known boron-containing rare-earth magnets having higher coercive force were used by taking the demagnetization at higher temperatures into account. However, since the magnet according to the present invention is almost free of demagnetization even at elevated temperatures, it can be used as it is as a permanent magnet having a high magnetic force. In particular, the magnet according to the present invention can maintain the magnetic properties for use at elevated temperatures at an iHc of 13 KOe or higher, and preferably 15 KOe or higher. Considering that the existing magnets required a considerably high iHc for use in applications at elevated temperatures, the magnet according to the present invention can be regarded as an effective permanent magnet alloy.

[0022] The permanent magnet alloy according to the present invention can be produced by a process consisting of sequential steps of melting, casting, crushing, molding, and sintering. As a melt casting process, there can be employed processes such as vacuum melting and casting, melting and casting under an inert gas atmosphere, quench rolling, atomization, etc. In order to obtain a sintered magnet having improved magnetic characteristics and heat resistance, it is preferred to incorporate a step of heat treatment between the steps of casting and crushing so as to subject the product before crushing to a heat treatment at a temperature of 600 °C or higher under an inert gas atmosphere. In this manner, the irreversible demagnetization can be further lowered. In the sintering step, it is preferred to sinter the molding in the temperature range of 1,000 to 1,200 °C under an inert gas atmosphere and gradually cooling from the sintering temperature to a temperature in a range of 600 to 900 °C, followed by quenching therefrom. The irreversible demagnetization can be further lowered by the quenching performed after the sintering.

[0023] The sintered magnet alloy according to the present invention can be produced in accordance with the production method for a sintered magnet described in Japanese Patent Public Disclosure No. 4-116144, except for the heat treatment and the quench treatment after the sintering described above. The process of production is outlined below.

[0024] The raw materials weighed as such to yield the desired alloy composition are molten in a vacuum melting furnace at a temperature of 1,600 °C or higher, and are casted by quenching in a water-cooled casting mold. As described above, the cast ingot thus obtained is thermally treated under gaseous Ar at a temperature of 600 °C or higher, and subjected to coarse crushing by using a jaw crusher. The coarse-grained powder thus prepared was finely milled by using a vibration ball mill to obtain a powder consisting of particles having an average diameter in a range of 2 to 10 µm. Those steps for such size reduction are carried out under gaseous Ar atmosphere. A part of the raw material for C can be added in the latter step of milling. That is, a part of the raw material for C is charged into the vacuum melting furnace, and the rest is added in this step of fine milling. Carbon black is suitable for use as the raw material of C, but also usable are organic materials containing C, such as an aliphatic hydrocarbon, a higher fatty acid alcohol, a higher fatty acid, a higher fatty acid amide, a metal soap, a fatty acid ester, etc.

[0025] Then, the powder thus obtained is compaction molded while applying an external magnetic field. The preferred range for the molding pressure is 1 to 5 t/cm². and that for the external magnetic field is 15 KOe or higher. The molding step also is preferably carried out under a gaseous Ar atmosphere. The molded product thus obtained is then sintered under gaseous Ar in the temperature range of 1,000 to 1,200 °C for a duration of about 2 hours. Then, as stated above, the resulting product is gradually cooled to a temperature in the range of 600 to 900 °C, and quenched from the temperature. To initiate the quenching from a temperature in the range of 600 to 900 °C, there can be employed a method of spraying a low temperature inert gas or a method of immersing the sintered product into water, an oil, or a liquid similar thereto, and preferably, rapid cooling is performed from the quench initiation temperature in the range of 600 to 900 °C to a temperature of 400 °C or lower at a cooling rate of -50 °C/min or higher, preferably -100 °C/min or higher.

[0026] Thus, in accordance with the present invention, there is provided a process for producing a permanent magnet alloy having an improved heat resistance comprising melting and casting each of the raw materials of the alloying elements, subjecting the resulting alloy to pulverizing, compaction molding the resulting powder, and sintering the molding under an inert gas atmosphere in a temperature range of 1,000 to 1,200 °C to obtain a sintered magnet alloy, characterized in that the alloy before pulverizing is thermally treated under an inert gas atmosphere at a temperature of 600 °C or higher, and/or that the process further comprises, after sintering the molding under an inert gas atmosphere in a temperature range of 1,000 to 1,200 °C, gradually cooling the sinter from the sintered temperature to a temperature range of 600 to 900 °C, followed by quenching. In the process, a part of the raw material of C may be added during melting, and the rest may be added during the pulverizing of the alloy.

[0027] The magnet according to the present invention is described in further detail below by making reference to representative examples.

EXAMPLE 1

[0028] An alloy having the composition below was produced by a process described hereinafter.

[Chemical composition of the alloy (at.%)]
C	5.0 at.%
B	1.8 at.%
Co	12.0 at.%
Nd	13.0 at.%
Dy	2.5 at.%
Tb	0.5 at.%
Fe	65.2 at.%

Where, C and B in total account for 6.8 at.%, Dy and Tb in total account for 3.0 at.%, and the ratio of Tb/Dy is 0.2.

[Production Process]

[0029] Each of the raw materials weighed as such to yield the desired alloy composition above were molten in a vacuum melting furnace. A part of the raw material for C was not fed into the melting furnace but was reserved. The melt thus obtained was quench cast in a water-cooled copper casting mold from 1,600 °C to obtain a cast alloy ingot. After heat treating under gaseous Ar at a temperature shown in Table 1, or without applying the heat treatment, the cast alloy ingot was coarsely crushed by using a jaw crusher, and the coarsely crushed product was fed into a vibration ball mill together with the reserved rest of the raw material for C to perform milling. Thus was obtained a powder having an average particle diameter of 5 µm.

[0030] The powder product thus obtained was molded under a magnetic field by applying a pressure of 2 t/cm² and an external magnetic field of 15 KOe. The resulting molding was sintered under gaseous Ar at 1,100 °C for a duration of 2 hours, and was gradually cooled from the sintering temperature to the temperature of initiating quenching shown in Table 1, at which temperature rapid cooling was started at a cooling rate also given in Table 1 by blowing gaseous Ar to the molding. The magnetic properties, heat resistance, and oxidation resistance of the resulting sinter were evaluated to obtain the results given in Table 1. The heat resistance and the oxidation resistance of the sinter were evaluated as follows.

[Evaluation of heat resistance]

(1) Measurement of irreversible demagnetization at 200 °C

[0031] The specimen was shaped in such a manner that the permeance coefficient (Pc) thereof be 1. More specifically, the specimen was cut out to a size of 2.5 mm × 2.5 mm × 1.05 mm.

[0032] The specimen thus obtained was magnetized by applying an external magnetic field of 50 KOe to measure the flux value at room temperature (25 °C). A flux meter manufactured by Toyo Jiki Kogyo Co. Ltd. equipped with an iron core coil was used to obtain the flux value. The flux value thus obtained was designated A₂₅.

[0033] The magnetized specimen thus obtained was maintained at 200 °C for a duration of 120 minutes. The heating held for a duration of 120 minutes was carried out in an oil bath filled with silicone oil. The temperature of the oil bath was precisely controlled so that the fluctuation in temperature may fall within a range of ± 0.1 °C. The specimen taken out from the oil bath was cooled sufficiently at room temperature to measure the flux value again by using the flux meter above. The flux value thus obtained was designated A₂₀₀. The irreversible demagnetization was calculated by using the observed A₂₅ and A₂₀₀ in accordance with the following equation:

(2) Measurement of irreversible demagnetization at 160 °C

[0034] The same procedure as that described in the measurement of irreversible demagnetization at 200 °C above was followed to obtain observed values A₂₅ and A₁₆₀, except for shaping the specimen in such a manner that the permeance coefficient (Pc) be 3 similar to the specimen described in the example of Japanese Patent Public Disclosure No. 4-116144, and for heating the specimen in the oil bath at 160 °C for a duration of 120 minutes. Thus, irreversible demagnetization was calculated according to the equation above.

(3) Magnetization measurements and the temperature coefficient of coercive force

[0035] After magnetizing the specimen by applying an external magnetic field of 50 KOe, the magnetization measurements at room temperature (RT; 25 °C) were conducted by using a vibrating-sample magnetometer. The temperature coefficient of coercive force was calculated in accordance with the following equation:

where, B₀ is the coercive force at room temperature, and B₁ is the coercive force obtained at 160 °C by using the same vibrating-sample magnetometer.

(4) Measurement of oxidation resistance

[0036] The progressive formation of rust was measured by performing pressure cooker test (PCT). More specifically, the specimen was held in a testing chamber manufactured by Tabai Espec Corp. at 120 °C, 2 atm, and 100 % RH (saturated condition) for a duration of 100 hours, and the generation of rust was visually observed.

[0037] As shown in the results of Table 1 above, permanent magnet alloys having an irreversible demagnetization (200 °C) of -3 % were obtained (see, for example, Table 1a). Referring to Table 1, the irreversible demagnetization (160 °C) for alloy a is -0.7 %, a value very close to 0 %. Thus, it can be understood that a high magnetic force is achieved for the alloy even when used at high temperatures.

[0038] With respect to the conditions of production, it can be clearly seen by comparing the alloy a with the alloy b that the irreversible demagnetization can be lowered by performing heat treatment on the cast ingot. Furthermore, by comparing the results for alloys a, c and d, the coercive force can be improved and the irreversible demagnetization can be lowered by quenching the sintered alloy from a temperature of at least 700 °C or higher.

EXAMPLES 2 TO 16 AND COMPARATIVE EXAMPLES 1 TO 6

[0039] Sinters were prepared under the same production conditions as those employed for alloy a in example 1, except for changing the composition of the alloys as shown in Table 2. The characteristics of the thus obtained sintered magnets were obtained in the same manner as described in example 1, and the results were given in Table 2.

[0040] As shown in Table 3, the permanent magnet alloys of Examples 2 to 16 in which both Dy and Tb are added all yield a low irreversible demagnetization at 200 °C, and the irreversible demagnetization at 160 °C also is very close to 0 %. Furthermore, it can be seen that they not only have a low temperature coefficient of coercive force, but also exhibit excellent oxidation resistance.

[0041] In contrast to the permanent magnet alloys of the examples above, the irreversible demagnetization at 200 °C for Comparative Example 1, in which no Dy nor Tb is added, is as large as -95 %, that for Comparative Example 2 containing no Tb and 0.5 at.% Dy is -95 %, and that for Comparative Example 4 containing no Dy and 0.5% by atomic Tb is -91 %. It can be understood therefrom that these permanent magnet alloys completely lose their magnetic force when heated to 200 °C. That is, the addition of Dy alone or Tb alone has no effect on the irreversible demagnetization at 200 °C. Although the addition of Dy alone in a large amount, as shown in Comparative Example 3, lowers the irreversible demagnetization to some extent, the effect is not sufficient. Referring to Comparative Example 5, the oxidation resistance is inferior because the content of C falls lower than the range specified in the present invention. The alloy of Comparative Example 6 contains 3.0 at.% of Tb but no Dy. It can be seen that, although a favorable heat resistance is obtained, the irreversible demagnetization at 200 °C is as low as -30 %.

[0042] Fig. 1 is a diagram showing how the values of irreversible demagnetization at 200 °C are influenced by the contents of Dy and Tb; all of the magnets given in Table 2 are plotted in the diagram wherein the abscissa shows the content of Dy (at.%) and the ordinate shows the content of Tb (at. %). The numerals provided in Fig. 1 each show the irreversible demagnetization at 200 °C for the plotted values.

[0043] Referring to Fig. 1, it can be understood that a peak (a point closest to 0 %) in irreversible demagnetization at 200 °C is present for the area defined by 2 to 3 at.% Dy and 0.3 to 1.5 at.% Tb. More specifically, the straight lines indicated by numerals (1), (2), (3), (4), (5) and (6) define the areas with particular content of Dy and Tb, and the area which yield an irreversible demagnetization at 200 °C in the range of 0 to -20 % can be defined by the crossing points A, B, C and D. Similarly, the area which yield an irreversible demagnetization at 200 °C in a range of 0 to -15 % can be defined by the crossing points B, C, H, E, F and G. The straight lines (1) to (6) can be expressed by the following equations:











The coordinates (Dy at.%, Tb at.%) of the points A to H are obtained as follows:

Point A (0.3, 4.7)

Point B (0.3, 0.2)

Point C (0.4, 0.1)

Point D (4.9, 0.1)

Point E (4.5, 0.5)

Point F (2.8, 2,2)

Point G (0.3, 0.24)

Point H (1.0, 0.1)

[0044] Referring to Figs. 2 and 3, Fig. 2 shows the observed irreversible demagnetization values at different temperatures for the magnet having the highest heat resistance among the magnets disclosed in Japanese Patent Public Disclosure No. 4-116144 as described in Example 24 thereof and those of Example 2 according to the present invention, in which the specimens are each shaped as such that the permeance coefficient (Pc) be 3 and magnetized by applying an external magnetic field of 50 KOe. Similarly, Fig. 3 is a diagram showing the observed irreversible demagnetization values similar to those shown in Fig. 2, except that the specimens are shaped as such that they may yield a permeance coefficient (Pc) of 1. The magnet of Example 24 disclosed in Japanese Patent Public Disclosure No. 4-116144 (referred to hereinafter as "disclosed magnet") has a composition expressed by 9Nd-9Dy-59Fe-15Co-1B-7C and an irreversible demagnetization at 160 °C at Pc = 3, according to the disclosure.

[0045] Referring to Fig. 2, the values of irreversible demagnetization at 160 °C for the specimens shaped as such to yield Pc = 3 are -1.0 % (disclosed magnet) and -0.7 % (Example 2 of the present invention); i.e., the difference between them is not so large. Concerning the values of irreversible demagnetization at 200 °C, however, the value of the magnet according to Example 2 of the present invention is improved to -1.9 %, which can be contrasted to the value of -12.9 % for the disclosed magnet. This tendency can be more clearly observed on the specimens shaped to yield Pc = 1, as shown in Fig. 3. More specifically, at Pc = 1, the values of irreversible demagnetization at 160 °C for the disclosed magnet is -9.4 %, whereas that for the magnet according to Example 2 of the present invention is improved to -1.7 %; moreover, the values of irreversible demagnetization at 200 °C for the disclosed magnet is -22.3 %, whereas that for the magnet according to Example 2 of the present invention is far improved to -4 %.

[0046] As described in detail above, the present invention provides a permanent magnet alloy having superior heat resistance and oxidation resistance never achieved in the field of R-Fe(Co)-B based magnets. Accordingly, the present invention provides materials having excellent magnetic properties at low cost, which can be advantageously assembled in appliances usable at elevated temperatures.

Claims

1. A permanent magnet alloy having an improved heat resistance comprising, in terms of percent by atom (at.%):

0.1 to 15 at.% C

0.5 to 15 at.% B,

provided that C and B in total account for 2 to 30 at.%;

40 at.% or less Co (exclusive of zero percent),

0.3 to 4.9 at.% Dy,

0.1 to 4.7 at.% Tb,

provided that Dy and Tb in total account for 0.5 to 5 at.%;

8 to 20 at.% R,

where R represents at least one element selected from the group consisting of Nd, Pr, Ce, La, Y, Gd, Ho, Er, and Tm;
with the balance being Fe and unavoidable incidental impurities;
wherein the irreversible demagnetization (at 200 °C) according to the following equation (1) is in the range of 0% to -20%, where iHc is 13 KOe or higher:

where,
A₂₅ represents a flux value of a magnet measured at room temperature (25 °C), on a specimen prepared into a shape such that its permeance coefficient Pc be 1 and magnetized at 50 KOe; and
A₂₀₀ represents a flux value of a magnet measured on the same specimen subjected to the measurement of A₂₅, which was maintained at 200 °C for 120 minutes and then cooled to room temperature (25 °C), for the measurement.

2. A permanent magnet alloy according to claim 1, wherein the content (at.%) of Dy and Tb in total fall in the range defined by the points B, C, H, E, F, and G plotted in Fig. 1, and the irreversible demagnetization at 200 °C is in the range of 0% to -15%.

3. A permanent magnet alloy according to claim 1, wherein the irreversible demagnetization (at 200 °C) is in the range of 0% to -5%.

4. A permanent magnet alloy having an improved heat resistance according to claim 1 wherein the ratio Tb(at.%)/Dy( at.%) is in a range of from 0.1 to 0.8.

5. A permanent magnet alloy having an improved heat resistance according to any of claims 1 to 4 wherein the content of C is in the range of 1 to 10 at.%.

6. A permanent magnet alloy having an improved heat resistance according to any of claims 1 to 5, wherein R is Nd alone or a combination of Nd and Pr.

7. A process for producing a permanent magnet alloy having an improved heat resistance according to any of the preceding claims, said process comprising the steps of: melting and casting each of the raw materials of the alloying elements, subjecting the resulting alloy to pulverizing, compression molding the resulting powder, and sintering the molding under an inert gas atmosphere in a temperature range of 1,000 to 1, 200 °C to obtain a sintered magnet alloy characterized in that the alloy before pulverizing is thermally treated under an inert gas atmosphere at a temperature of 600 °C or higher.

8. A process for producing a permanent magnet alloy according to claim 7 wherein the process further comprises, after sintering the molding under an inert gas atmosphere in a temperature range of 1,000 to 1,200 °C, gradually cooling the sinter from the sintered temperature to a temperature range of 600 to 900 °C, followed by quenching.

9. A process for producing a permanent magnet alloy according to claim 7 or 8 wherein a part of the raw material of C is added during melting, and the rest is added during the pulverizing of the alloy.

Ansprüche

1. Eine Permanentmagnetlegierung mit verbessertem Wärmewiderstand, die folgendes in Atomprozent (at.%) aufweist:

0,1 bis 15 at.% C,

0,5 bis 15 at.% B,

vorausgesetzt, dass C and B insgesamt 2 bis 30 at.% umfassen;

40 at.% oder weniger Co (ausschließlich Null Prozent),

0,3 bis 4,9 at.% Dy,

0,1 bis 4,7 at.% Tb,

vorausgesetzt, dass Dy und Tb in einer Gesamtmenge von 0,5 bis 5 at.% vorhanden sind;

8 bis 20 at.% R,

wobei R mindestens ein Element repräsentiert, welches aus der aus folgendem bestehenden Gruppe ausgewählt ist: Nd, Pr, Ce, La, Y, Gd, Ho, Er und Tm;
wobei der Rest Fe und nichtvermeidbare zufällige Verunreinigungen sind;
wobei ferner die irreversible Entmagnetisierung (bei 200°C) gemäß der folgenden Gleichung (1) im Bereich von 0% bis -20% liegt, wobei iHc 13 KOe oder höher ist:

wobei folgendes gilt:

A₂₅ repräsentiert einen Flusswert eines Magneten gemessen bei Raumtemperatur (25°C) an einer Probe hergestellt in einer Form derart, dass deren Permeanzkoeffizient Pc 1 ist und zwar magnetisiert bei 50 KOe; und

A₂₀₀ repräsentiert einen Flusswert eines Magneten gemessen an der gleichen der Messung von A₂₅ ausgesetzten Probe, wobei die Probe auf 200°C 120 Minuten lang gehalten wurde und sodann auf Raumtemperatur (25°C) für die Messung abgekühlt wurde.

2. Permanentmagnetlegierung nach Anspruch 1, wobei der Gehalt (at.%) von Dy und Tb insgesamt in den durch die Punkte B, C, H, E, F und G gemäß Fig. 1 definierten Bereich fallen und wobei die irreversible Entmagnetisierung bei 200°C im Bereich von 0% bis -15% liegt.

3. Permanentmagnetlegierung nach Anspruch 1, wobei die irreversible Entmagnetisierung (bei 200 °C) in einem Bereich von 0% bis -5% liegt.

4. Permanentmagnetlegierung mit einem verbesserten Wärmewiderstand gemäß Anspruch 1, wobei das Verhältnis von Tb (at.%) / Dy (at.%) im Bereich von 0,1 bis 0,8 liegt.

5. Permanentmagnetlegierung mit einem verbesserten Wärmewiderstand nach einem der Ansprüche 1 bis 4 , wobei der Gehalt an C im Bereich von 1 bis 10 at.% liegt.

6. Permanentmagnetlegierung mit einem verbesserten Wärmewiderstand nach einem der Ansprüche 1 bis 5, wobei R allein Nd oder eine Kombination von Nd und Pr ist.

7. Ein Verfahren zur Herstellung einer Permanentmagnetlegierung mit einem verbesserten Wärmewiderstand gemäß einem der vorhergehenden Ansprüche, wobei das Verfahren die folgenden Schritte vorsieht: Schmelzen und Gießen jedes der Rohmaterialien der Legierungselemente, Aussetzen der sich ergebenden Legierung gegenüber einer Pulverisierung, Kompressionsformung des sich ergebenden Pulvers und Sintern des Formlings unter einer in InertGasatmosphäre in einem Temperaturbereich von 1000 bis 1200°C , um eine gesinterte Magnetlegierung zu erhalten,
   dadurch gekennzeichnet, dass die Legierung vor der Pulverisierung thermisch in einer inerten Gasatmosphäre bei einer Temperatur von 600°C oder höher behandelt wird.

8. Verfahren zur Herstellung einer Permanentmagnetlegierung gemäß Anspruch 7, wobei das Verfahren ferner folgendes aufweist: nach dem Sintern des Formlings unter einer inerten Gasatmosphäre in einem Temperaturbereich von 1000 bis 1200°C allmähliches Abkühlen des gesinterten Körpers von der Sintertemperatur auf einen Temperaturbereich von 600 bis 900°C, gefolgt von einem Abkühlvorgang.

9. Verfahren zur Herstellung einer Permanentmagnetlegierung gemäß Anspruch 7 oder 8, wobei ein Teil des Rohmaterials C während des Schmelzens zugegeben wird und der Rest während der Pulverisierung der Legierung zugegeben wird.

Revendications

1. Alliage d'aimant permanent à résistance à la chaleur améliorée comprenant, en atomes pourcent (at.%) :

0,1 à 15 at.% de C,

0,5 à 15 at.% de B,

pourvu que C et B ensemble forment de 2 à 30 at. % ;

40 at.% ou moins de Co (mais pas zéro pourcent),

0,3 à 4,9 at.% de Dy,

0,1 à 4,7 at.% de Tb,

pourvu que Dy et Tb forment ensemble de 0,5 à 5 at. % ;

de 8 à 20 at.% de R,

où R représente au moins un élément choisi dans le groupe comprenant Nd, Pr, Ce, La, Y, Gd, Ho, Er et Tm ;
le reste étant du fer et des impuretés accidentelles inévitables ;
   dans lequel la désaimantation irréversible (à 200°C) selon l'équation (1) suivante est dans la plage de 0 à -20 %, où iHc est de 13 kOe ou plus :

où,
A₂₅ représente une valeur de flux d'un aimant mesurée à température ambiante (25°C) sur un spécimen préparé selon une forme telle que son coefficient de perméance Pc est de 1 et aimanté à 50 kOe ; et
A₂₀₀ représente une valeur de flux d'un aimant mesurée sur le même spécimen soumis à la mesure de A₂₅ qui a été maintenu à 200°C pendant 120 minutes puis refroidi à température ambiante (25°C) pendant la mesure.

2. Alliage d'aimant permanent selon la revendication 1, dans lequel le contenu total (at.%) de Dy et Tb tombe dans la plage définie par les points B, C, H, E, F et G représentés en figure 1, et la désaimantation irréversible à 200°C est dans la plage de 0 à -15 %.

3. Alliage d'aimant permanent selon la revendication 1, dans lequel la désaimantation irréversible (à 200°C) est dans la plage de 0 % à -5 %.

4. Alliage d'aimant permanent à résistance à la chaleur améliorée selon la revendication 1, dans lequel le rapport Tb (at.%)/Dy (at.%) est dans la plage de 0,1 à 0,8.

5. Alliage d'aimant permanent à résistance à la chaleur améliorée selon l'une quelconque des revendications 1 à 4, dans lequel le contenu en C est dans la plage de 1 à 10 at.%.

6. Alliage d'aimant permanent à résistance à la chaleur améliorée selon l'une quelconque des revendications 1 à 5, dans lequel R est Nd seul ou une combinaison de Nd et Pr.

7. Procédé de fabrication d'un alliage d'aimant permanent à résistance à la chaleur améliorée selon l'une quelconque des revendications précédentes, ce procédé comprenant les étapes consistant à fondre et mouler chacun des matériaux bruts des éléments d'alliage, soumettre l'alliage résultant à une pulvérisation, mouler sous pression la poudre résultante et fritter le moulage sous une atmosphère de gaz inerte dans une plage de température de 1000 à 1200 °C pour obtenir un alliage d'aimant fritté, caractérisé en ce que l'alliage avant pulvérisation est traité thermiquement dans une atmosphère de gaz inerte à une température supérieure ou égale à 600°C.

8. Procédé de formation d'un alliage d'aimant permanent selon la revendication 7, comprenant en outre, après frittage du moulage dans une atmosphère de gaz inerte dans une plage de température de 1000 à 1200°C, un refroidissement progressif de la fritte depuis la température de frittage jusqu'à une plage de température de 600 à 900°C, suivi d'une trempe.

9. Procédé de fabrication d'un alliage d'aimant permanent selon la revendication 7 ou 8, dans lequel une partie de la matière brute de C est ajoutée pendant la fusion et le reste est ajouté pendant la pulvérisation de l'alliage.

Drawing