Background of the invention
[0001] The present invention relates to a rare earth-based permanent magnet or, more particularly,
to a rare earth-based permanent magnet prepared by the powder metallurgical method.
[0002] Among the various types of rare earth-based permanent magnets, those on neodymium,
iron and boron, referred to as the Nd-Fe-B magnets hereinbelow, are prominently highlighted
in recent years by virtue of their outstandingly high magnetic properties in comparison
with the rare earth-based permanent magnets of other types. These Nd-Fe-B magnets
are expected to be a material used in large quantities, especially, in electric motors
for which more and more powerful permanent magnets are required from the standpoint
of energy saving or when more compact but more powerful motors are desired.
[0003] One of the problems in these Nd-Fe-B permanent magnets, however, is the relatively
large temperature dependency of the magnetic properties thereof so that the Nd-Fe-B
magnets at an elevated temperature cannot exhibit the magnetic properties as high
as at low or room temperature. For example, it is not rare that the temperature of
an electric motor under continuous running is increased to reach 100 to 150°C so that
the Nd-Fe-B magnets built in the motor can no longer exhibit the desired magnetic
properties. In this regard, it is an important technical problem to develop a rare
earth-based permanent magnet which can retain the high magnetic properties even at
elevated temperatures.
[0004] To give a more detailed explanation of this problem, it is known that the Nd-Fe-B
magnets have coefficients of temperature dependency of about -0.13%/°C and -0.6%/°C
for the residual magnetization B, and coercive force ;H
c, respectively. Namely, the temperature dependency of the coercive force is considerably
larger than that of the residual magnetization and should desirably be much smaller.
A coefficient of temperature dependency of -0.6 %/° C means that the coercive force
of the magnet at 100 ° C is only about a half of the value at room temperature. This
large temperature dependency is the reason for the relatively low upper limit of 50
to 70°C at the highest of the temperature range in which the Nd-Fe-B magnets can be
practically used.
[0005] Various attempts and proposals have been made hitherto in order to improve the large
temperature dependency of the magnetic properties or, in particular, coercive force
of the Nd-Fe-B magnets. Two types of means have been proposed for the improvement
of the Nd-Fe-B magnets. For example, as is taught in Japanese Patent Kokai 5 989 401
and 6 032 306 and practiced with some success, the temperature dependency in the coercive
force of the magnets can be improved by the admixture of the magnet alloy with a so-called
heavy rare earth element such as dysprosium and terbium, light metal element such
as aluminium or transition metal element such as niobium and vanadium. Alternatively,
the magnetic properties of the Nd-Fe-B magnets could be improved when the metallographic
structure of the magnet alloy be converted to the precipitation- hardening type although
no successful results have yet been obtained by this means.
[0006] The principle of the former method by the additional alloying elements is to impart
the Nd-Fe-B magnet with a further increased coercive force so that the magnet can
retain a value of the coercive force still in an acceptable range even at an elevated
terrtpera- ture to cause decrease in the coercive force. This improvement in the coercive
force is naturally obtained at the sacrifice of the residual magnetization B
r. Namely, aluminium, niobium and vanadium as an additional alloying element are each
non-magnetic so that the addition thereof to the magnet alloy is necessarily accompanied
by the decrease in the residual magnetization in proportion to the added amount of
these elements or even larger. The heavy rare earth elements, such as dysprosium and
terbium, have a magnetic moment aligned anti-parallel to that of the transition metal
elements so that the decrease in the residual magnetization of the Nd-Fe-B magnets
by the addition thereof is even larger than by the addition of aluminium, niobium
or vanadium. As a consequence, the neodymium-based permanent magnets of the high coercive
force type in the prior art unavoidably have a greatly decreased residual magnetization
in comparison with conventional Nd-Fe-B magnets.
[0007] As is taught in Journal of Applied Physics, volume 55, page 2083 (1984), the coercive
force of the neodymium-based magnet is exhibited by the mechanism of nucleation. A
presumption of the reason thereof is that, while the extremely smooth and clean grain
boundaries of the crystallites inhibit incipience of reverse magnetic domains even
under impression of a magnetic field in a direction reverse to that of the magnetization,
the magnetic domain walls are strongly constrained to the narrow region in the vicinity
of the grain boundaries.
[0008] According to the disclosure by Hiraga, et al. in Japanese Journal of Applied Physics,
volume 24, L30 (1985), an electron microscopic examination of a neodymium-based permanent
magnet revealed that the magnet had a structure in which the crystallite grains of
Nd
2Fe
14B were, so to say, enveloped by a magnetically soft, thin b.c.c. phase and the interface
therebetween is in a very clean condition without distortion. This fact suggests that
the large coercive force of the magnet is produced as a result of the fact that the
magnetic domain walls are constrained to the outermost layer formed of the magnetically
soft b.c.c. phase. Accordingly, it is presumable that the coercive force of the neodymium-based
magnet is increased by the addition of the above mentioned additive elements such
as the heavy rare earth elements, aluminium, niobium and the like because these additive
elements have an effect to increase the anisotropic magnetic field of the Nd
2Fe
14B compound and to influence on the morphology at the proximity of the grain boundaries
of the crystallites.
[0009] The above described information and consideration have provided the inventors with
a guide principle that the key factor for the improvement in tha coercive force of
a neodymium-based permanent magnet is to control the condition on and around the grain
boundaries alone of the crystallites leading to the completion of the present invention.
Summary of the invention
[0010] Thus, the present invention provides a rare earth-based permanent magnet which is
a sintered body of a powdery mixture comprising or, rather, essentially composed of:
a) from 90 to 99.9 parts by weight of a first alloy containing from 25 to 35% by weight
of a light rare earth element selected from the group consisting of the elements of
the atomic number from 57 to 62, of which at least a half by weight is neodymium,
praseodymium or a combination thereof, and from 0.7 to 1.5% by weight of boron, the
balance being iron, cobalt or a combination of iron and cobalt; and
b) from 10 to 0.1 part by weight of a second alloy containing from 30 to 86% by weight
of a heavy rare earth element selected from the group consisting of the elements of
the atomic number from 64 to 71, of which at least a half by weight is terbium, dysprosium,
holmium or a combination thereof, the balance being an element selected from the group
consisting of aluminium, niobium, zirconium, vanadium, tantalum and molybdenum.
[0011] The powdery mixture should preferably have a particle size distribution in the range
from 2 to 811m.
Detailed description of the preferred embodiments
[0012] As is understood from the above given summary of the invention, the rare earth-based
permanent magnet of the invention is a magnet prepared by the powder metallurgical
process from a magnetic alloy powder which is characteristically a mixture of two
kinds of alloys defined above. Different from the conventional method in which the
additive elements contributing to the increase of the coercive force are uniformly
admixed beforehand with the principal magnet alloy of a light rare earth element,
e.g. neodymium, iron and boron, the invention proposes that the alloying elements
are divided into two groups which are separately converted into the first alloy for
the principal magnetic constituent and the second alloy for the additive elements
and these two alloys are concurrently pulverized or separately pulverized followed
by mixing of the powders together to give a powdery mixture to be subjected to shaping
and sintering.
[0013] In the conventional method in which all of the alloying elements are melted together
into a single alloy for the powder metallurgical process, the coercive force of the
resultant permanent magnet cannot be sufficiently improved unless the amounts of the
effective additive elements are considerably large to affect the residual magnetization
in order to have a sufficient influence on or in the proximity of the grain boundaries
of the crystallites. In contrast thereto, the additive elements in the invention form
the second alloy separately from the first alloy for the matrix phase of the magnet
and the powdery mixture for the powder metallurgical process is formed of the particles
of these two types of alloys. In the sintering procedure, accordingly, the additive
elements diffuse into the particles of the matrix phase from the surface of the particles
but never reach the core portions of the particles. Therefore, the concentration of
the additive elements is inhomogeneous in the inventive magnet as sintered. Namely,
the concentration is high only at the surface of the matrix particles while the additive
elements are substantially absent in the core portion of the matrix particles exhibiting
a great influence on the anisotropic magnetic field and morphology at or in the vicinity
of the grain boundaries even when the overall amount of the additive elements is so
low that the residual magnetization of the magnet is little affected and consequently
the magnet has a high maximum energy product (BH)
max. The above mentioned inhomogeneous distribution of the additive elements could be
confirmed by the X-ray microprobe analysis.
[0014] The first alloy, which is pulverized and mixed with a powder of the second alloy,
is a ternary alloy composed of a light rare earth element, iron and/or cobalt and
boron. The light rare earth element here implied as the first component of the first
alloy includes the rare earth elements having an atomic number of 57 to 62, i.e. lanthanum
to samarium, but it is preferably neodymium or praseodymium although combinations
of these two elements without or with a minor amount of the other light rare earth
elements can be used equally. In particular, at least 50% by weight of the light rare
earth component should be neodymium, praseodymium or a combination of the two. Neodymium
is preferred. The amount of the light rare earth element or elements in the first
alloy should be in the range from 25 to 35% by weight.
[0015] The second component in the first alloy is boron, of which the content in the first
alloy should be in the range from 0.7 to 1.5% by weight. The balance of the above
mentioned light rare earth elements and boron in the first alloy is iron, cobalt or
a combination thereof although iron is preferred mainly for the economical reason
while replacement of a part of iron with cobalt has an effect of increasing the Curie
point of the magnet contributing to the improvement of the reversible temperature
coefficient. The amount of this third component, i.e. iron and/or cobalt, in the first
alloy should accordingly be in the range from 63.5 to 74.3% by weight including unavoidable
impurity elements, the amount of which should be as small as possible.
[0016] The second alloy, which is pulverized and mixed with the powder of the first alloy,
is a binary alloy composed of a heavy rare earth element and an alloying element selected
from the group consisting of aluminium, niobium, zirconium, vanadium, tantalum and
molybdenum. The heavy rare earth element here implied is an element having an atomic
number of 64 to 71, i.e. gadolinium to lutetium, and terbium, dysprosium and holmium
are preferred, of which dysprosium is more preferable. These heavy rare earth elements
are preferred to the light rare earth elements, e.g. neodymium, forthe reason that
these heavy rare earth elements give a R
2Fe
14B type compound (R: a rare earth element) having a larger anisotropic magnetic field
than Nd
2Fe
14B so that the improvement on the coercive force of the magnetic could be obtained
with addition of a smaller amount thereof. The above mentioned six kinds of alloying
elements can exhibit an effect of increasing the coercive force of the magnet even
in an unalloyed condition while alloying thereof with a heavy rare earth element may
have a synergistic effect. It is noteworthy that the alloy is more resistant against
oxidation than the heavy rare earth element alone. The amount of the heavy rare earth
element or elements in the second alloy should be in the range from 30to 86% by weight,
the balance, i.e. from 70 to 14% by weight, being one or a combination of the above
mentioned alloying elements including unavoidable impurity elements, the amount of
which should be as small as possible. When the amount of the heavy rare earth element
or elements is too small, the alloy can be pulverized with great difficulties due
to the increased tenacity of the alloy. When the amount of the heavy rare earth element
is too large, on the other hand, the alloy would be more susceptible to oxidation.
[0017] Among the many possible combinations of the heavy rare earth elements and the six
kinds of the alloying elements, the most preferred is an alloy of dysprosium and aluminium,
which should have a composition of DyA1
2 in the so-called Laves phase. This is because the Laves phase of the DyA1
2 alloy is brittle and can be easily pulverized and the powder thereof is little susceptible
to oxidation in addition to the relatively large effect on the magnet properties by
the addition thereof.
[0018] The elementary materials forming the first or the second alloy should be melted together
to prepare the first and second alloys separately. The method for the preparation
of the alloy can be conventional without particular limitations. The two alloys may
be separately pulverized into powders which are weighed and mixed together subsequently.
It is, however, a convenient way that each of the alloys in the form of an ingot is
crushed into coarse granules having a particle size distribution of, for example,
10 to 500
11m which should be mixed with the granules of the other alloy in a calculated proportion
followed by concurrent fine pulverization so that the pulverization and mixing can
be performed in one step. The fine powder of the two alloys should have a particle
size distribution in the range from 1 to 10 µm or, preferably, from 2 to 8 µm.
[0019] The thus prepared mixed powder should be composed of from 90 to 99.9 parts by weight
of the first alloy and from 10 to 0.1 part by weight of the second alloy. When the
amount of the second alloy is smaller than 0.1 part by weight in 100 parts by weight
of the mixed powder, no sufficient improvement can be obtained in the coercive force
of the resultant sintered magnet. When the amount of the second alloy is too large,
on the other hand, the residual magnetization of the sintered magnet would be unduly
decreased.
[0020] In the following, the sintered rare earth-based permanent magnet of the invention
is described in more detail by way of examples. The values of percentage appearing
below are all in % by weight.
Example 1
[0021] A first alloy ingot was prepared by melting together, in a high frequency induction
furnace under an inert atmosphere, metallic neodymium having a purity of 99.4%, iron
having a purity of 99.5% and boron having a purity of 99.5% in such a proportion that
the alloy was composed of 34.0% of neodymium, 64.9% of iron and 1.1 % of boron.
[0022] Separately, a second alloy ingot was prepared from metallic dysprosium having a purity
of 99.4% and aluminium having a purity of 99.9% in a weight proportion of 75.1% dysprosium
and 24.9% aluminium.
[0023] Each of the alloy ingots was crushed in a disc mill separately from the other into
granules having a fineness to pass a screen of 20 meshes by the Tyler standard. The
granules of the first alloy were admixed with the granules of the second alloy in
four different weight proportions as indicated in Table 1 below and each of the mixtures
as well as the granules of the first alloy alone for comparative purpose was finely
pulverized in a jet mill using nitrogen as the ject gas into a powder having an average
particle diameter of 3.0 µm.
[0024] The powder was molded into a shaped body in a magnetic field of 10 kOe under a compressive
pressure of 1.5 tons/cm
2 into a green body which was subjected to sintering at 1050°Cfor 1 hour in an atmosphere
of argon followed by aging at 550°C for 1 hour and then quenching with a cold inert
gas. Table 1 below shows the residual magnetization B
r and coercive force
iH
c of the prepared sintered magnets. It is understood from these results that the addition
of the second alloy to the first alloy was very effective in increasing the coercive
force of the magnets with little adverse influence on the residual magnetization of
the magnets.
[0025]

Example 2
[0026] The experimental procedure in each of the experiments (Experiments No. 1 to No. 5)
was substantially the same as in Example 1 excepting modifications in the compositions
of the first and second alloys and the mixing ratio thereof. Namely, the first alloy
was composed of of 31 % neodymium, 68% iron and 1 % boron as prepared using the same
materials as used in Example 1. The second alloy was one of the four alloys having
compositions of:
(1) 46% dysprosium and 54% niobium (Experiment No. 1);
(2) 61 % dysprosium and 39% vanadium (Experiment No. 2);
(3) 45% dysprosium and 55% molybdenum (Experiment No. 3); and
(4) 74.7% terbium and 25.3% aluminium (Experiment No. 4),
each prepared from materials having a purity of 99.9%. The mixing ratio of the first
and second alloys was 99:1 by weight in each of Experiments No. 1 to No. 4. For comparison
in Experiment No. 5, the first alloy alone was processed into a sintered magnet in
the same manner by omitting the second alloy. Table 2 below shows the residual magnetization
B, and coercive force
iH
c of the thus obtained sintered magnets. It is clear from these results that the addition
of the second alloy is very effective in increasing the coercive force with little
decrease in the residual magnetization.

1. A rare earth-based permanent magnet which is a sintered body of a powdery mixture
comprising:
a) from 90 to 99.9 parts by weight of a first alloy containing from 25 to 35% by weight
of a light rare earth element and from 0.7 to 1.5% by weight of boron, the balance
being iron, cobalt or a combination of iron and cobalt; and
b) from 10 to 0.1 part by weight of a second alloy containing from 30 to 86% by weight
of a heavy rare earth element, the balance being an element selected from the group
consisting of aluminium, niobium, zirconium, vanadium, tantalum and molybdenum.
2. The rare earth-based permanent magnet as claimed in claim 1 wherein the light rare
earth element is selected from the group consisting of lanthanum, cerium, praseodymium,
neodymium and samarium.
3. The rare earth-based permanent magnet as claimed in claim 1 wherein the heavy rare
earth element is selected from the group consisting of gadolinium, terbium, dysprosium,
holmium, erbium, thulium, ytterbium and lutetium.
4. The rare earth-based permanent magnet as claimed in claim 1 wherein at least 50%
by weight of the light rare earth element in the first alloy is neodymium, praseodymium
or a combination thereof.
5. The rare earth-based permanent magnet as claimed in claim 1 wherein at least 50%
by weight of the heavy rare earth element in the second alloy is terbium, dysprosium,
holmium or a combination thereof.
6. The rare earth-based permanent magnet as claimed in claim 1 wherein the second
alloy is an alloy of dysprosium and aluminium.
7. The rare earth-based permanent magnet as claimed in claim 1 wherein the powdery
mixture has a particle size distribution in the range from 2 to 8 µm.
1. Permanentmagnet auf Basis seltener Erdmetalle in Form eines aus einer pulverigen
Mischung gesinterten Körpers, wobei die Mischung
a) 90 bis 99,9 Gew.-Teile einer ersten Legierung, die 25 bis 35 Gew.-% eines leichten
seltenen Erdmetallelements und 0,7 bis 1,5 Gew.-% Bor enthält, wobei der Rest aus
Eisen, Kobalt oder einer Eisen/Kobalt-Kombination besteht; und
b) 10 bis 0,1 Gew.-Teile einer zweiten Legierung umfaßt, die 30 bis 86 Gew.-% eines
schweren seltenen Erdmetallelements enthält, wobei der Rest aus einem aus der Reihe
Aluminium, Niob, Zirkonium, Vanadium, Tantal und Molybdän ausgewählten Element besteht.
2. Permanentmagnet auf Basis seltener Erdmetalle nach Anspruch 1, worin das leichte
seltene Erdmetallelement aus der Reihe bestehend aus Lanthan, Cer, Praseodym, Neodym
und Samarium ausgewählt ist.
3. PermanentmagnetaufBasisseltenerErdmetalle nach Anspruch 1, worin das schwere seltene
Erdmetallelement aus der Reihe bestehend aus Gadolinium, Terbium, Dysprosium, Holmium,
Erbium, Thulium, Ytterbium und Lutetium ausgewählt ist.
4. Permanentmagnet auf Basis seltener Erdmetalle nach Anspruch 1, worin mindestens
50 Gew.-% des leichten seltenen Erdmetallelements der ersten Legierung aus Neodym,
Praseodym oder einer Kombination daraus besteht.
5. Permanentmagnet auf Basis seltener Erdmetalle nach Anspruch 1, worin mindestens
50 Gew.-% des schweren seltenen Erdmetallelements der zweiten Legierung aus Terbium,
Dysprosium, Holmium oder einer Kombination daraus besteht.
6. PermanentmagnetaufBasisseltenerErdmetalle nach Anspruch 1, worin die zweite Legierung
eine Dysprosium-Aluminium-Legierung ist.
7. PermanentmagnetaufBasisseltenerErdmetalle nach Anspruch 1, worin die pulverige
Mischung eine Teilchengröße-Verteilung im Bereich von 2 bis 8 µm besitzt.
1. Aimant permanent à base de terres rares, formé d'un corps fritté qui est constitué
d'un mélange pulvérulent comprenant:
a) 90 à 99,9 parties en poids d'un premier alliage contenant 25 à 35% en poids d'un
élément léger des terres rares et 0,7 à 1,5% en poids de bore, le reste étant du fer,
du cobalt ou une combinaison de fer et de cobalt; et
b) 10 à 0,1 partie en poids d'un second alliage contenant de 30 à 86% en poids d'un
élément lourd des terres rares, le reste étant un élément choisi dans le groupe constitué
par l'aluminium, le niobium, le zirconium, le vanadium, le tantale et le molybdène.
2. Aimant permanent à base de terres rares selon la revendication 1, dans lequel l'élément
léger des terres rares est choisi dans le groupe constitué par le lanthane, le cérium,
le praséodyme, le néodyme et le samarium.
3. Aimant permanent à base de terres rares selon la revendication 1, dans lequel l'élément
lourd des terres rares est choisi dans le groupe constitué par le gadolinium, le terbium,
le dysprosium, l'holmium, l'erbium, le thulium, l'ytterbium et le lutétium.
4. Aimant permanent à base de terres rares selon la revendication 1, dans lequel au
moins 50% en poids de l'élément léger des terres rares compris dans le premier alliage
est le néodyme, le praséodyme ou une combinaison de ces éléments.
5. Aimant permanent à base de terres rares selon la revendication 1, dans lequel au
moins 50% en poids de l'élément lourd des terres rares compris dans le second alliage
est le terbium, le dysprosium, l'holmium ou une combinaison de ces éléments.
6. Aimant permanent à base de terres rares selon la revendication 1, dans lequel le
second alliage est un alliage de dysprosium et d'aluminium.
7. Aimant permanent à base de terres rares selon la revendication 1, dans lequel le
mélange pulvérulent présente une répartition granulométrique dans la gamme de 2 à
8 µm.