Field of the Invention
[0001] The present invention relates to permanent magnet materials composed mainly of R
(where R represents at least one rare earth element), Fe and B, and a process of producing
the same, particularly, it relates to R-Fe-B permanent magnet materials and to processes
of producing the same. Such materials are typically powdered and then molded into
shape and sintered to form magnets.
Description of Prior Art
[0002] Nowadays, an R-Fe-B permanent magnet (Japanese Patent Application Laid Open No. Sho
59-46008), is typically used as a high performance permanent magnet. A high magnetic
characteristic is obtained by a magnet material structure having a main phase of ternary
tetragonal compounds and an R-rich phase, and such magnets are used in a broad field
from general domestic electric appliance to peripheral equipment of large-sized computers.
Thus R-Fe-B permanent magnets having various structures have been proposed so as to
exhibit various magnetic characteristics depending on their proposed uses.
[0003] However, in response to recent stringent requirements in the manufacture of small-sized,
light and highly functional electric and electronic equipment, inexpensive R-Fe-B
permanent magnets with a higher performance are required.
[0004] In general, the residual magnetic flux density (Br) of an Fe-B sintered magnet can
be expressed as the following Equation (1).

where,
Is : saturation magnetization
β : temperature dependence of Is
f: Degree of orientation
ρ : density of sintered body
ρ0 : theoretical maximum density
α : volume fraction of grain boundary phase
(volume fraction of non-magnetic phase)
[0005] Thus, in order to raise the residual magnetic flux density (Br) of an R-Fe-B sintered
magnet, (1) the volume fraction of the R
2Fe
14B matrix phase may be increased, (2) the density of the magnet may be raised to the
theoretical maximum density, and further, 3) the degree of orientation of the main
phase crystal grains in a easily magnetizing axial direction may be enhanced.
[0006] Thus it is important to bring a magnet composition close to the stoichiometrical
composition of the above-mentioned R
2Fe
14B to achieve the item 1). When the R-Fe-B sintered magnet is produced using as a starting
material, an alloy ingot which is prepared by melting the alloy having the aforementioned
composition and casting in a mold, since α-Fe crystallizes in the alloy ingot and
the R-rich phase becomes segregated locally, it is difficult to pulverize the ingot
to fine powders and the composition changes during pulverizing due to oxidation.
[0007] In the case of mechanically pulverizing the alloy ingot after hydrogenation and dehydrogenation
(as particularly described in Japanese Patent Application Laid Open Nos. Sho 60-63304
and Sho 63-33505) α-Fe crystallized in the alloy ingot remains as it is at the time
of pulverization and thus hinders the pulverization because of its ductility, and
an R-rich phase which is throughout locally present becomes fine due to hydrogenation
producing hydrides. Thus oxidation is accelerated at the time of mechanical pulverization,
or pulverization by a jet mill, causing discrepancies in the composition due to dispersion.
[0008] When producing the sintered body by using an alloy powder which is brought close
to the stoichiometric composition of R
2Fe
14B to achieve the item 1), in the sintering process, the presence of a Nd-rich phase
for causing liquid phase sintering produces oxides and it is consumed by the inevitable
oxidation whereby the sintering is hindered, and since the Nd-rich phase and B-rich
phase are inevitably decreased by increase of the R
2Fe
14B phase, the production of the sintered body becomes more difficult. Furthermore,
the coercive force (iHc) which is one of indexes showing stability of the permanent
magnet material and one of its important properties is degraded.
[0009] Furthermore, as to the item 3), it is usual in a process of producing an R-Fe-B permanent
magnet, to adopt a process of press molding in the magnetic field in order to make
the direction of the easy magnetization axes of the main phase crystal grains uniform.
In such a case, it is known that the residual magnetic flux density (Br) value and
the value of the squareness of the demagnetization curve {(Br2/4(BH)max} change depending
on the direction of magnetic field application and the pressing direction, and are
influenced by the applied magnetic field intensity.
[0010] Recently, a production process has been proposed (Japanese Patent Application Laid
Open No. Sho 63-317643) for preventing coarsening of the crystal grains, and residue
and segregation of a-Fe which are disadvantages in the production of R-Fe-B alloy
powders by an ingot pulverizing process. In that process, a cast piece having a specific
thickness is formed from an R-Fe-B molten alloy by the double roll casting method,
and according to a common powder metallurgical process, the cast piece is ground coarsely
by means of a stamp mill, a jaw crusher or the like, and then comminuted into powders
having a mean grain size of 3 to 5 µm by a mechanical pulverizing process in a disk
mill a ball mill, grinder, a jet mill or the like, and thereafter pressed in a magnetic
field, sintered, and annealed.
[0011] However, in this process, as compared with the conventional case of pulverizing an
ingot cast in a mold, the pulverizing efficiency at the time of pulverization can
not be improved significantly., Also magnetic characteristics can not be greatly improved
at the time of pulverization, because not only grain boundary pulverization but also
intergranular pulverization occurs, and since the R-rich phase is not in a RH
2 phase stable against oxidation, or since the R-rich phase is fine and has a large
surface area, it is poor in oxidation resistance, with the result that oxidation proceeds
during the process and high magnetic characteristics can not be obtained.
[0012] Recently, demands for cost reduction of the R-Fe-B permanent magnet materials are
becoming greater, thus it is very important to manufacture high performance permanent
magnet materials efficiently. And hence, manufacturing conditions for drawing out
the very best characteristics need to be improved.
[0013] We have conducted various studies on processes of producing R-Fe-B permanent magnet
materials efficiently and improving their magnetic characteristics.
[0014] Enhancement of the residual magnetic flux density (Br) of an R-Fe-B sintered magnet
can be achieved by increasing a content of the R
2Fe
14B phase of the main phase which is the ferro-magnetic phase. That is, it is important
to make the magnet composition close to the stoichiometric composition of R
2Fe
14B.
[0015] However, when producing the R
2Fe
14B sintered magnet from the alloy ingot, prepared by melting the alloy having the aforementioned
composition and casting in the mold, as the starting material, particularly as α-Fe
crystallized in the alloy ingot and the R-rich phase is locally present throughout,
the alloy is difficult to pulverize and has discrepancies in composition.
[0016] Also, when producing the alloy powder having the aforementioned composition by a
direct reducing and diffusing process, un-reacted Fe grains appear. When raising the
reduction temperature to eliminate this, then the grains grow by sintering to one
another: if Ca is added as a reducing agent and its oxides are taken in, impurities
are thereby increased.
[0017] Therefore, as the result of various studies made for the reduction of the various
problems related to the production of magnetic alloy materials, we have found out
that, by using a strip casting process for rapid cooling and solidifying of the molten
alloy, crystallization of an α-Fe phase can be suppressed and a cast alloy piece having
a fine grain structure and an homogeneous composition can be produced.
[0018] When an R-Fe-B sintered magnet is sintered, a liquid-phase sintering reaction takes
place. That is, in the magnet, besides the main R
2Fe
14B phase which is the ferromagnetic phase, a B-rich phase and an R-rich phase are present
as grain boundary phases, which react with one another during sintering to generate
a liquid phase, thereby causing densification of the alloy.
[0019] Thus, the B-rich phase and the R-rich phase are indispensable phases for producing
a dense R-Fe-B sintered magnet. However, in order to optimise the magnetic characteristics,
it is necessary to maximise the R
2Fe
14B phase which is the main ferromagnetic phase, and for this purpose, it is necessary
to densify an alloy powder which is close to the stoichiometric composition of the
R
2Fe
14B phase.
SUMMARY OF THE INVENTION
[0020] It is an object of the present invention to provide high performance R-Fe-B permanent
magnet materials having magnetic properties such that when the maximum energy product
value (BH)max is expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

[this being equivalent to the expression of a total value A + B ≥ 59 wherein (A)
is a (BH) max value expressed in megaGaussOersted (1 MGOe = 10
5ö4π kJ/m
3); and (B) is the coercive force iHc value expressed in kilo-Oersted (1 KOe = 10
6ö4π kA/m)]; and such that when the residual magnetic flux density (Br) is expressed
in tenths of one Tesla, (kiloGauss) the squareness of the demagnetization curve {(Br
2×1.99)/(BH) max} has a value of between 1.01 and 1.045, [this being equivalent to
the expression {(Br
2/4)/A} having a value between 1.01 and 1.045 where (A) is again a (BH) max value,
but expressed in megaGaussOersted], wherein problems in a process of producing the
R-Fe-B materials are solved, efficient pulverization is made possible, oxidation resistance
is high, a high iHc is realized by fining crystal grains of a magnet, and orientation
of the easy magnetization axis of the crystal grains is improved.
[0021] It is another object of the present invention to provide processes of producing such
R-Fe-B permanent magnet materials.
[0022] According to the present invention, there is provided an R-Fe-B permanent magnet
material as defined in Claim 1 hereof.
[0023] By the hydrogenation of the strip cast R-Fe-B alloy having a specific composition
and thickness, an R-rich phase which is finely dispersed produces hydrides to cause
volume expansion and eventual spontaneous decay of the alloy, thereafter the main
phase crystal grains constituting the alloy can be comminuted and the powder having
a uniform grain distribution can be produced. At this time, the R-rich phase is finely
dispersed and the R
2Fe
14B phase is also comminuted, thus when the alloy powder which is dehydrogenated and
stabilized is comminuted production efficiency is greatly improved, and by orientation
using a pulsed magnetic field and pressing, the R-Fe-B permanent magnet of excellent
magnetic properties can be obtained.
[0024] The present invention also provide various processes for the production of such a
magnet material. These processes are defined in Claims 9, 11 and 18 hereof. According
to the process of claim 9, an alloy of the desired final composition is directly strip
cast and further processed by hydrogenation, dehydrogenation, comminution, magnetic
orientation, molding, sintering and annealing. According to the processes of claims
11 and 18, a main phase base alloy and an adjusting alloy are produced separately,
and then after hydrogenation, dehydrogenation and comminution the resulting powders
are blended together prior to magnetic orientation, molding, sintering and annealing.
[0025] For example, by adding and blending an adjusting alloy powder containing a Nd
2Fe
17 phase obtained by the strip casting process with the R-Fe-B alloy powder containing
the R
2Fe
14B phase as the main phase also obtained by the strip casting process, due to the reaction
between the Nd
2Fe
17 phase in the adjusting alloy powder and the B-rich and Nd-rich phase in the main
phase of R-Fe-B alloy powder, the B-rich phase and Nd-rich phase which are deleterious
for permanent magnetic characteristics can be adjusted and decreased, the resulting
magnet performance can be improved, and further, oxygen content in the alloy powder
can be reduced, and an alloy powder having a composition responsive to various magnetic
characteristics is provided easily.
[0026] Alternatively, by adding and blending an adjusting alloy powder containing an R-Co
intermetallic compound phase obtained by the strip casting process with an R-Fe-B
alloy powder containing the R
2Fe
14B phase as the main phase obtained by the strip casting process, even when the liquid-phase
sintering can not be effected only by the main phase of R-Fe-B alloy powder due to
the shortage of R-rich and B-rich phases, the R-Co intermetallic compound phase of
the adjusting alloy powder is melted to supply a liquid phase for high densification
thus the resulting magnet performance can be improved, and further, oxygen content
in the alloy powder can be decreased and an alloy powder having a composition responsive
to various magnetic characteristics is again provided easily.
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] Fig. 1 is an explanatory view of a press machine, in which a pulse magnetic field
and a static magnetic field can be applied together.
[0028] Fig. 2 is a graph showing the relationship between time and magnetic field intensity
of a pulse magnetic field.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0029] We have found out that, in the production of an R-Fe-B cast piece having a fine and
homogeneous structure by a strip casting process, and comminuting alloy powders which
are stabilized by dehydrogenation after hydrogenation, as the result of various studies
carried out on a grinding process for the purpose of improving pulverizing efficiency,
oxidation resistance and magnetic characteristics of an R-Fe-B sintered magnet, and
in particular, the coercive force iHc of an R-Fe-B alloy, pulverizing efficiency is
improved about twice as much as conventional pulverizing efficiency, and by molding,
sintering and annealing the fine powder which has been oriented by applying a pulse
magnetic field, the excellent magnetic properties required by this invention can be
achieved.
[0030] Thus, when an R-Fe-B alloy which is strip cast and has a specific composition having
a structure in which an R-rich phase of specific thickness is finely dispersed, is
subjected to hydrogenation of such R-rich phase produces hydrides and causes expansion
so that, the alloy can be spontaneously decayed, and as a result, crystal grains constituting
the alloy can be comminuted and a powder having a uniform grain distribution can be
produced.
[0031] It is important that, at this time, the R-rich phase is finely dispersed and the
R
2Fe
14B phase is also fine. Furthermore, in a process of making the alloy ingot by using
a usual mold, when the alloy composition is brought close to the stoichiometric composition
of the R
2Fe
14B phase, crystallization of α-Fe primary crystals is unavoidable, causing a large
deterioration of the pulverizing efficiency in the following process. And hence, though
means for providing heat treatment and eliminating α-Fe is taken to homogenize the
alloy ingot, since the main phase crystal grains become coarse and segregation of
the R-rich phase proceeds, iHc of the sintered magnet is only improved with difficulty.
[0032] It is also necessary to make uniform the easily magnetizing axial direction or to
improve the degree of orientation of the main phase crystal grains, for achieving
high magnetization, and the improvement of the squareness of the demagnetzation curve:
and hence, a process of compacting the powder in a magnetic field is adopted.
[0033] However, in a coil or a power source disposed on a usual press machine (a hydraulic
press or a mechanical press) for generating the magnetic field, a magnetic field of
only 10 kOe to 20 kOe (796 to 1592 kA/m) is generated at the most, and the squareness
ofthe demagnetization curve {(Br
2×1.99)/(BH)ma} also assumes a value of 1.05 or more, thus it is difficult to achieve
the theoretical (BH)max value (when the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} is 1.00) expected from a given Br value. Therefore, attempts have
been made to mold in a higher magnetic field, but for generating such higher magnetic
field, the number of turns of the coil must be increased and also the apparatus requires
a high power source and must be made larger.
[0034] By analyzing the relationship between the magnetic field intensity at the time of
pressing and Br of the sintered body, we have found out that, the more the magnetic
field intensity is increased, the higher the magnetization and the more the squareness
of the demagnetization curve is improved, thus by using a pulse magnetic field capable
of generating a strong magnetic field instantaneously, a higher magnetization and
a higher the squareness of the demagnetization curve are made possible.
[0035] Meanwhile, we have found out that, in the process of using a pulse magnetic field,
it is important instantaneously to orient once by the pulse magnetic field, and it
is possible to mold the powder using an isostatic press, and by combining the pulse
magnetic field with a static magnetic field generated by an electromagnet, press molding
in the magnetic field is also possible.
[0036] Thus, according to one aspect of the invention, after strip casting a molten alloy
consisting of 12 atomic % to 16 atomic % R (where, R represents at least one rare
earth element), 4 atomic % to 8 atomic % B, 5000 ppm or less O
2, Fe (of which a part is optionally replaced by one or both of Co and Ni) and unavoidable
impurities, into a cast piece whose main phase is an R
2Fe
14B phase, the cast piece is contained in a pressure vessel which can take in and discharge
air, the air in the pressure vessel is replaced by hydrogen for hydrogenation of the
cast piece. The cast material is then dehydrogenated, and is thereafter comminuted
into a fine powder of 1 µm to 10 µm mean particle size under an inert gas, the fine
powder is packed into a mold and oriented by applying the pulse magnetic field of
10 kOe (796 kA/m) or more instantaneously, then molded, sintered and annealed, thereby
to obtain a permanent magnet material which has magnetic properties such that when
the maximum energy product value is expressed in kJ/m
3 and the coercive force iHc is measured in kA/m, the total value [(BH)max ö 7.96]+
[iHc ö 79.6] is 59 or more, and such that when the residual magnetic flux density
(Br) is measured in tenths of one Tesla (kiloGauss), the squareness of the demagnetization
curve {(Br
2×1.99)/(BH)max} is 1.01 to 1.045
[0037] Whereas an R
2Fe
17 phase in an R-Fe alloy such as a Nd-Fe alloy is an intermetallic compound having
an easily magnetizing direction in a C phase when its Curie point is in the vicinity
of room temperature, and conventionally, in an R-Fe-B sintered permanent magnet, when
the amount of B is less than 6 atomic %, for example, an R
2Fe
17 phase is produced in the magnet and this weakens its coercivity.
[0038] However, as the results of various studies, we have found that, in material powders
in which a specific amount of R-Fe alloy powder containing the R
2Fe
17 phase such as the Nd
2Fe
17 phase is added to and blended with the R-Fe-B alloy powder containing the R
2Fe
14B phase as the main phase, near a eutectic temperature of 690°C ofNd in the Nd-rich
phase and the Nd
2Fe
17 phase in the R-Fe alloy powder in the grain boundary phase, for example, a reaction
of Nd + Nd
2Fe
17 phase ↔ liquid phase takes place, and this low melting point liquid phase accelerates
the sintering of the R-Fe-B alloy powder.
[0039] Meanwhile, an adjusting alloy powder containing the Nd
2Fe
17 phase and the R-Fe-B alloy powder containing the R
2Fe
14B phase as the main phase react as follows during the sintering, and act to increase
the R
2Fe
14B phase as the main phase.

[0040] That is, we have found that since the Nd
2Fe
14B phase is newly produced by a reaction between the Nd
2Fe
17 phase in the adjusting alloy powder and the B-rich phase and Nd-rich phase in the
main phase R-Fe-B alloy powder, in a permanent magnet obtained by using only the alloy
powder containing the R
2Fe
14B phase as the main phase of the conventional process, the amount of the B-rich phase
and Nd-rich phase (which is one of the factors deleterious for magnetic characteristics)
can be reduced at the time of the sintering reaction.
[0041] Furthermore, from the fact that it is a large advantage from a production point of
view to obtain material alloy powders which are easily comminuted when producing the
R-Fe-B magnet by a powder metallurgical process, as the result of various studies
into a process of producing the R-Fe-B permanent magnet material powders, we have
found that R-Fe-B permanent magnet material powders may be obtained by mixing a necessary
amount of main phase alloy powder containing the R
2Fe
14B phase as its main phase and an adjusting alloy powder containing the R
2Fe
17 phase also obtained by rapid cooling and solidifying of a molten alloy formed by
the strip casting process.
[0042] Thus, reasons for producing the main phase alloy powder and adjusting alloy powder
from the alloy obtained by the strip casting process in the present invention are
that, by strip casting, a main phase alloy powder can be obtained from an alloy cast
piece, in which the R
2Fe
14B main phase is fine and the B-rich phase and Nd-rich phases are sufficiently dispersed,
and in which crystallization of Fe primary crystals is suppressed, and furthermore,
an adjusting alloy powder in which the R
2Fe
17 phase is dispersed uniformly can be obtained from a strip cast alloy piece.
[0043] In particular, when the R
2Fe
14B phase is fine and the B-rich phase and R-rich phase are uniformly dispersed in the
main phase material powders, pulverizing is improved considerably, and a powder having
a uniform particle distribution can be obtained. Furthermore, when producing the magnet,
since the crystal structure is fine, a high coercive force is obtained.
[0044] Meanwhile, an advantage of producing the adjusting alloy powder containing the R
2Fe
17 phase by the strip casting process is that, since the R
2Fe
17 phase can be made fine and dispersed sufficiently at the time of mixing with the
main phase alloy powder, the reaction takes place uniformly. In the usual alloy melting
process using a mold, since α-Fe and the other R-Fe (Co) compound phase are crystallized
on the resulting alloy ingot, in order to obtain stable material alloy powders, the
alloy ingot must be heated and homogenized, causing the production cost ofthe alloy
powder to increase and the R
2Fe
17 phase to grow. Furthermore, when producing the adjusting alloy powder by a direct
reducing and diffusing process, such problems are encountered that, unreacted Fe grains
remain or individual grain compositions differ from each other, and it is very difficult
to homogenize the mixture of alloy powders.
[0045] As the result of various studies on the above-mentioned findings, we have also found
out that, in the material powders prepared by adding and blending a specific amount
of R-Co alloy powder containing the R-Co intermetallic compound phase, for example,
a Nd
3Co phase or a NdCo
2 phase as the main phase, to an R-Fe-B alloy powder containing the R
2Fe
14B phase as the main phase, by the reactions of Nd + Nd
3Co phase ↔ liquid phase in the vicinity of eutectic temperature 625°C ofNd of the
Nd-rich phase in the main phase alloy powder and Nd
3Co in the R-Co alloy powder, the low melting point liquid phase accelerates the sintering
of the R-Fe-B alloy.
[0046] Thus, according to the present invention, it is possible to supply the amount of
liquid phase necessary for sintering, as a result, an alloy powder made close to the
stoichiometric composition of the R
2Fe
14B phase can be liquid-phase sintered. In this way, the magnet composition can be made
close to the stoichiometric composition of the R
2Fe
14B phase. In other words, when producing the magnet only by the conventional alloy
powder containing the R
2Fe
14B phase as the main phase, the Nd-rich phase serving as a supply source of the liquid
phase produces Nd-oxides during the process by unavoidable material oxidation, so
that the amount of liquid phase necessary for sintering can not be secured. As a result,
a high sufficiently densification can not be achieved, so that the composition must
be set in advance with some tolerance margins. Any such deviations from the optimum
composition can be reduced or even eliminated by the present invention.
[0047] In particular, when the R
2Fe
14B phase in the main phase material powders is fine and the B-rich phase and Nd-rich
phase are dispersed uniformly, the comminution is considerably improved at the time
of producing the magnet, and a powder having a uniform grain distribution can be produced.
Furthermore, since the crystal structure is fine, a high coercivity can be obtained
when producing the magnet. Particularly, even when the alloy powder composition is
made close to the stoichiometric composition of the R
2Fe
14B phase, crystallization of the α-Fe primary crystal is eliminated and a uniform structure
is obtained.
[0048] Furthermore, advantages of producing the adjusting alloy powder containing the R-Co
intermetallic compound phase by the strip casting process are that, such problems
as follow can be solved. In the usual alloy melting process using a mold, the Co(Fe)
phase and the other R-Co(Fe) compound phase are crystallized in the resulting alloy
ingot, and the phases are locally present throughout, therefore, in order to obtain
stable material alloy powders, the alloy ingot must be heated and homogenized, causing
increase in the production cost of the alloy powder. Also, when producing the adjusting
alloy powder by the direct reducing and diffusing process, un-reacted Co and Fe grains
remain or individual grain compositions differ from each other, thus it is very difficult
to homogenize that whole alloy powder.
[0049] It is an object of the present invention to provide high performance R-Fe-B permanent
magnet materials having magnetic properties such that
[0050] Magnetic characteristics of the R-Fe-B permanent magnet according to the present
invention are achieved as follows: when the maximum energy product value (BH)max is
expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

and also, when the residual magnetic flux density (Br) is expressed in tenths of
one Tesla, (kiloGauss) the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} has a value of between 1.01 and 1.045.
[0051] This is equivalent to stating that a total value A + B is 59 or more, in which A
is a maximum energy product value (BH) max expressed in MGOe and B is a coercive force
iHc expressed in kOe, and that the squareness of demagnetization curve {(Br
2/4A} value is 1.01 to 1.045 (Br being expressed in tenths of one Tesla [kG]), and
A again being a maximum energy product value (BH) max expressed in MGOe.
[0052] By selecting the composition and production conditions suitably, the necessary magnetic
characteristics are obtained.
[0053] In the present invention, a cast piece of the magnet materials having a structure
in which the main R
2Fe
14B phase and the R-rich phase are finely separated, is produced by strip casting a
molten alloy having a specific composition by a single roll process or a double roll
process. The resulting cast piece is a sheet whose thickness is 0.03 mm to 10 mm.
Though the single roll process and the double roll process may both be used depending
on the desired thickness of the cast piece, the double roll process is preferably
adopted when the plate thickness is thick, and the single roll process is preferably
used when the plate thickness is thin.
[0054] Reasons for limiting the thickness of the cast piece within 0.03 mm to 10 mm are
that, when the thickness is below 0.03 mm, a rapid cooling effect increases and the
crystal grain size becomes smaller than 1 µm, and thus too easily oxidized when comminuted,
resulting in deterioration of the magnetic characteristics, and when the thickness
exceeds 10 mm, the cooling rate becomes slower, α-Fe is easily crystallized, the crystal
grain size becomes larger and also the Nd-rich phase becomes present throughout, and
thus the magnetic characteristics deteriorate.
[0055] In the present invention, a sectional structure of the R-Fe-B alloy having a given
composition obtained by the strip casting process is such that, the main phase R
2Fe
14B crystal size is finer than about one tenth or more as compared with that of a conventional
ingot obtained by casting in a mold. For example, crystal sizes are 0.1 µm to 50 µm
in a short axial direction and 5 µm to 200 µm in a long axial direction, and the R-rich
phase is finely dispersed surrounding the main phase crystal grain, and even in local
regions, the size is below 20 µm. Crystal grains of the main phase alloy powder and
the adjusting alloy powder obtained by the strip casting process have the same properties.
[0056] By dispersing the R-rich phase finely below 5 µm, when the R-rich phase produces
hydrides at the time of hydrogenation processing, volume expansion occurs uniformly
for fracturing, so that the main phase crystal grain is fractured and pulverized and
a fine powder having a uniform grain distribution is obtained.
[0057] In the following paragraphs, reasons for limiting the compositions of the R-Fe-B
permanent magnet and the alloy in the present invention are described.
[0058] Rare earth elements which may constitute R contained in the permanent magnet alloy
ingot of the present invention may contain yttrium (Y), and are the rare earth elements
including light rare earths and heavy rare earths.
[0059] As R, the light rare earths are sufficient, and particularly, Nd and Pr are preferable.
Though, usually, one kind of R is sufficient, in practice, mixtures (such as mischmetal,
didymium, etc.) of two or more rare earth elements will often be used for the reason
of availability, and Sm, Y, La, Ce, Gd etc. can be used as a mixture with other R,
particularly, Nd, Pr and the like. The R is not necessarily made up of pure rare earth
element(s), and those containing unavoidable impurities in production may be used
according to what is commercially available.
[0060] R is an indispensable element of the alloy for producing the R-Fe-B permanent magnet,
in that sufficiently high magnetic characteristics cannot be obtained below 12 atomic
%, particularly, a high coercive force can not be obtained, and when exceeding 16
atomic %, the residual magnetic flux density (Br) is lowered and a permanent magnet
having the best characteristics can not be obtained. And hence, R is within the range
of 12 atomic % to 16 atomic %, the optimum range being 12.5 atomic % to 14 atomic
%.
[0061] B is an indispensable element of the alloy for producing the R-Fe-B permanent magnet,
whereby the high coercive force (iHc) cannot be obtained below 4 atomic %, and when
exceeding 8 atomic %, the residual magnetic flux density (Br) is lowered, so that
the best permanent magnet cannot be obtained. And hence, the B is 4 atomic % to 8
atomic %, the optimum range being 5.8 atomic % to 7 atomic %.
[0062] In the case of Fe, the residual magnetic flux density (Br) is lowered below 76 atomic
%, and when exceeding 84 atomic %, the high coercive force cannot be obtained, so
that Fe is restricted to 76 to 84 atomic %.
[0063] Also, though the reason for substituting a part of Fe with one or both of Co and
Ni is to obtain the effect of improved temperature characteristics and corrosion resistance
of the permanent magnet, when one or both of Co and Ni exceed 50% of Fe, the highest
coercivity cannot be obtained and the best permanent magnet cannot be obtained. And
hence, the preferred upper limit of Co and Ni is 50% of Fe.
[0064] The reason for restricting O
2 below 5000 ppm is that, when exceeding 5000 ppm, the R-rich phase is oxidized and
insufficient liquid phase is produced at sintering, resulting in lowered density,
so that a high magnetic flux density cannot be obtained and weathering resistance
is also reduced. An optimum range of O
2 is between 200 to 3000 ppm.
[0065] When the apparent density of the permanent magnet material is below 7.45 g/cm
3, a high magnetic flux density cannot be obtained, and the magnet materials cannot
be obtained with a total value [(BH)max ö 7.96]+[iHc ö 79.6] of 59 or more,, which
is a feature of the present invention.
[0066] Also, as the starting material powders in the present invention, as well as powders
of the magnet material composition, it is also possible to blending an R-Fe-B alloy
powder containing an R
2Fe
14B main phase in which the amount of R, to be described later, is 11 atomic % to 20
atomic %, and an R-Fe-B alloy powder containing the R
2Fe
17 phase, in which the amount of R is below 20 atomic % in order to adjust the total
amounts of R, B and Fe to the required magnet composition,.
[0067] As to the amount of B, the magnet composition can be adjusted by blending the main
phase R-Fe-B alloy powder, in which the amount of B is 4 atomic % to 12 atomic % or
more, and an adjusting R-Fe-B alloy powder containing the R
2Fe
17 phase, in which the amount ofB is below 6 atomic %, or an adjusting R-Fe alloy powder
containing the R
2Fe
17 phase, in which B is not contained.
[0068] Furthermore, the magnet composition can be adjusted by blending an adjusting R-Co
(can be substituted by Fe) alloy powder containing an R-Co intermetallic compound
(Nd
3-Co, Nd-Co
2 and the like).
[0069] Though the presence of unavoidable impurities in industrial production is permissible,
besides R, B and Fe in the alloy cast piece of the present invention, by substituting
a part of B by a total amount of 4.0 atomic % or less of at least one of 4.0 atomic
% or less C, 3.5 atomic % or less P, 2.5 atomic % or less S and 3.5 atomic % or less
C, improvements in productivity and reductions in the cost of the magnet alloy are
possible.
[0070] Meanwhile, by adding at least one of
| Al―9.5 atomic % or less, |
Ti―4.5 atomic % or less, |
| V―9.5 atomic % or less, |
Cr―8.5 atomic % or less, |
| Mn―8.0 atomic % or less, |
Bi―5 atomic % or less, |
| Nb―12.5 atomic % or less, |
Ta―10.5 atomic % or less, |
| Mo―9.5 atomic % or less, |
W―9.5 atomic % or less, |
| Sb―2.5 atomic % or less, |
Ge―7 atomic % or less, |
| Sn―3.5 atomic % or less, |
Zr―5.5 atomic % or less and |
| Hf―5.5 atomic % or less, |
|
to the alloy powder containing the R, B, Fe alloys or the R-Fe-B alloy containing
Co or the blended R
2Fe
14B phase as the main phase, or to the adjusting alloy powder containing the R
2Fe
17 phase and the adjusting alloy powder containing the R-Co intermetallic compound phase,
a high coercivity of the permanent magnet alloy is promoted.
[0071] In the R-B-Fe permanent magnet of the present invention, it is necessary that the
R
2Fe
14B phase of the main phase of a crystal phase presents above 90%, preferably, above
94%. R-Fe-B sintered magnets, which are produced in large numbers at present, has
the R
2Fe
14B phase of up to 90%. The high magnetic characteristics of the present invention,
in which the value [(BH)max ö 7.96]+[iHc ö 79.6] is above 59, can not be obtained
below 90%.
[0072] A degree of orientation of the magnet of the present invention is calculated from
the aforementioned equation 1, it is necessary that the degree of orientation of the
magnet is above 85% to hold the value [(BH)max ö 7.96]+[iHc ö 79.6] above 59. When
the degree of orientation is below 85%, the squareness of demagnetization curve is
poor and the high residual magnetic flux density (Br) is lowered, resulting in a low
(BH) max value. The degree of orientation is preferably above 92%.
[0073] Though the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} theoretically shows a value of 1.00, since the above-mentioned degree
of orientation is inevitably disturbed in the practical permanent magnet material,
it has been limited to 1.05 even after many improvement in the past: in the permanent
magnet materials of the present invention obtained by the aforementioned specific
process, the value of the squareness of demagnetization curve is 1.01 to 1.045.
[0074] In the following paragraphs, reasons for the preferred composition ranges of the
main phase alloy and the adjusting alloy for the R-Fe-B permanent magnet materials
are described.
[0075] For obtaining a main phase alloy powder containing the R
2Fe
14B phase as the main phase to which an adjusting alloy powder containing the R
2Fe
17 phase is added and blended, when R is below 11 atomic %, residual iron where R and
B do not diffuse increases, and when exceeding 20 atomic %, the R-rich phase increases
and the oxygen content increases at pulverization. Accordingly, R is preferably 11
atomic % to 20 atomic %, more preferably, 13 atomic % to 16 atomic %.
[0076] A high coercive force (iHc) can not be obtained when B is below 4 atomic %, and since
the residual magnetic flux density (Br) is lowered when exceeding 12 atomic %, the
best permanent magnet can not be obtained, so B is preferably 4 atomic % to 12 atomic
%, more preferably, 6 atomic % to 10 atomic %.
[0077] The rest is composed of Fe and unavoidable impurities, Fe is preferably within the
range of 65 atomic % to 82 atomic %. When Fe is below 65 atomic %, the rare earth
element(s) and B become relatively abundant, and the R-rich phase and the B-rich phase
increase; when exceeding 82 atomic %, the rare earth elements and B decrease relatively,
and the residual Fe increases, resulting in a non-uniform alloy powder. Fe is preferably
74 atomic % to 81 atomic %.
[0078] When one or both of Co and Ni in the main phase alloy powder are substituted for
Fe in the R
2Fe
14B main phase this lowers the coercive force, Co is preferably below 10 atomic % and
Ni is preferably below 3 atomic %. When replacing a part of Fe with the above-mentioned
Co or Ni, Fe is preferably in the range of 55 atomic % to 72 atomic %.
[0079] When obtaining an adjusting alloy powder containing the R
2Fe
17 phase, the R-rich phase increases in production of the alloy powder and causes oxidation
when R exceeds 20 atomic %, thus R is preferably 5 to 15 atomic %. When B is below
6 atomic %, since only the R
2Fe
14B phase is present and the amount of B in the main phase alloy powder can be adjusted,
B is preferably below 6 atomic %.
[0080] Meanwhile, the balance of the main phase powder is composed of Fe and unavoidable
impurities, Fe is preferably 85 atomic % to 95 atomic %.
[0081] For obtaining an alloy powder containing the R
2Fe
14B phase as the main phase, to which the R-Fe adjusting alloy powder containing the
R-Co intermetallic compound phase is added and blended, since the residual iron, when
R and B do not diffuse, increases when R is below 11 atomic %, and the R-rich phase
increases and the oxygen content increases at pulverization when exceeding 15 atomic
%, R is preferably 11 atomic % to 15 atomic %, more preferably, 12 atomic % to 14
atomic %.
[0082] Since high coercive force (iHc) is not obtained when B is below atomic %, and the
residual magnetic flux density (Br) is lowered when exceeding 12 atomic %, B is preferably
4 atomic % to 12 atomic %, more preferably, 6 atomic % to 10 atomic %.
[0083] Meanwhile, the balance is composed of Fe and unavoidable impurities, Fe is preferably
73 atomic % to 85 atomic %. When Fe is below 73 atomic %, the rare earth elements
and B become abundant relatively and the R-rich phase and the B-rich phase increase,
when exceeding 85 atomic %, the rare earth elements and B decrease relatively and
the residual Fe increases, results in the non-uniform alloy powder, thus Fe is, more
preferably, 76 atomic % to 82 atomic %.
[0084] Substituting one or both of Co and Ni in the main phase alloy powder for Fe in the
R
2Fe
14B main phase tends to reduce the coercive force, so Co is preferably below 10 atomic
% and Ni below 3 atomic %. When a part of Fe is replaced with the above-mentioned
Co or Ni, Fe is preferably 63 atomic % to 82 atomic %.
[0085] For obtaining the adjusting alloy powder containing the R-Co intermetallic compound
phase, the R-rich phase increases and tends to cause oxidation in production of the
alloy powder when R exceeds 45 atomic %: R is preferably 10 to 20 atomic %.
[0086] When the balance is composed of Co and unavoidable impurities, Co is preferably 55
atomic % to 95 atomic %.
[0087] One or both of Fe and Ni may be substituted for Co in the adjusting alloy powder.
Since the oxidation resistance of the adjusting alloy powder is reduced when the amount
of Fe is increased, and the coercive force of the magnet is lowered when the amount
ofNi is increased, Fe is preferably below 50 atomic % and Ni below 10 atomic %. When
replacing a part of Co with Fe or Ni, Co is preferably 5 atomic % to 45 atomic %.
[0088] In the present invention, the magnet composition alloy powder, the main phase alloy
powder containing the R
2Fe
14B phase as the main phase, and the adjusting alloy powder containing the R
2Fe
17 phase or the R-Co intermetallic compound phase, are produced by, for example, a known
strip casting process by a single roll process or a double roll process.
[0089] Hydrogenation processing is that, for example, a cast piece cut into a predetermined
size and having the thickness of 0.03 mm to 10 mm is inserted into a material case,
which is covered and charged into a pressure vessel which can be closed tightly, after
closing the pressure vessel tightly, the pressure therein is reduced sufficiently,
whereafter H
2 gas at 200 Torr (26.6 kPa) to 50 kg/cm
2 (4.9 MPa) pressure is introduced so that hydrogen is occluded by the cast piece.
[0090] Since the hydrogenation reaction is an exothermic reaction, the H
2 gas having a predetermined pressure is supplied for a fixed time, while providing
a piping around the pressure vessel for supplying cooling water to suppress the temperature
rise in the pressure vessel, so that the H
2 gas is absorbed and the cast piece decays spontaneously and is pulverized. The pulverized
alloy is then cooled and dehydrogenated in vacuum.
[0091] Since fine cracks are produced in the processed alloy powder grains, it can be comminuted
by a ball mill, a jet mill and the like, and the alloy powder having the necessary
grain size of 1 µm to 80 µm can be obtained.
[0092] In the present invention, air in the processing pressure vessel may be replaced by
inert gas beforehand, and with the inert gas being later replaced by the H
2 gas.
[0093] The smaller the cut size of the cast piece the lower the H
2 gas pressure required, and though the cut cast piece absorbs H
2 and is comminuted even at low pressures, the higher the hydrogenation pressure, the
easier the pulverization. However, the pulverization is reduced when the hydrogen
pressure is below 200 Torr (26.6 kPa), and though it may be preferable from a viewpoint
of hydrogenation and pulverization to exceed 50 kg/cm
2 (4.9 MPa), it is not so from the viewpoint of the apparatus and safety, so that the
H
2 gas pressure is preferably 200 Torr to 50 kg/cm
2. For convenience in mass production, it is preferably 2 kg/cm
2 to 10 kg/cm
2.
[0094] In the present invention, though the pulverization time due to the Hydrogenation
varies depending on the closed pressure vessel size, the size of the cut piece and
the H
2 gas pressure, it takes more than 5 minutes.
[0095] The alloy powder pulverized by hydrogenation is subjected to a primary dehydrogenation
in vacuum after cooling. Then, when the pulverized alloy is heated at 100°C to 750°C
in vacuum or in argon gas, and subjected to a secondary dehydrogenation for 0.5 hours
or longer, the H
2 gas in the pulverized alloy can be completely removed, and oxidation of the powder
or a molded body due to prolonged storage is prevented, so that deterioration of the
magnetic characteristics of the resulting permanent magnet can be prevented.
[0096] Since heating up to 100°C or higher has a good dehydrogenating effect during the
dehydrogenation processing, the above-mentioned primary dehydrogenation in vacuum
may be omitted, and the decayed powder may be directly dehydrogenated in vacuum or
in an argon gas atmosphere at 100°C or higher.
[0097] That is, after the hydrogenation and decaying reactions in the aforesaid pressure
vessel, the resulting decayed powder may be, subsequently, subjected to dehydrogenation
in the pressure vessel atmosphere at 100°C or higher.
[0098] Alternatively, after dehydrogenation in vacuum, the decayed powder may be taken out
from the pressure vessel for pulverization, whereafter dehydrogenation processing
including heating to 100°C or higher in the pressure vessel may be effected again.
[0099] When the heating temperature in the above-mentioned dehydrogenation is below 100°C,
it takes longer to remove H
2 remaining in the decayed alloy powder thus it is not conducive to mass production.
When the temperature exceeds 750°C, a liquid phase is produced and the powder is agglomerated,
making pulverization difficult and lessening the moldability at pressing, thus it
is not preferable when producing sintered magnets.
[0100] When considering the sinterability of the sintered magnet, the preferable dehydrogenation
temperature is 200°C to 600°C. Though the processing time varies depending on the
processing amount, it usually takes 0.5 hours or longer.
[0101] Comminution is suitably effected by a jet mill under an inert gas (e.g. N
2, Ar). It goes without saying that a ball mill or a grinder may be used for comminuting
the powder using an organic solvent (e.g. benzene, toluene and the like).
[0102] Mean grain sizes ofthe powder at comminution is preferably 1 µm to 10 µm. When below
1 µm, the comminuted powder becomes very active and susceptible to oxidation, with
the possibility of spontaneous ignition. When exceeding 10 µm, uncomminuted coarse
grains remain to cause deterioration of the coercive force and a slow sintering rate,
resulting in a low density. The mean grain size of the fine powder is, more preferably,
2 to 4 µm.
[0103] For pressing using the magnetic field, the following process is proposed.
[0104] Comminuted powders are packed into a mold in an inert gas atmosphere. The mold may
be made of, besides non-magnetic metals and oxides, organic compounds such as plastics,
rubber and the like.
[0105] The charging density of the powder is from a bulk density (charging density 1.4 g/cm
3) in a quiescent state of the powder, up to the solidifying bulk density (charging
density 3.0 g/cm
3) after tapping. Thus, the charging density is restricted to 1.4 to 3.0 g/cm
3.
[0106] A pulse magnetic field by an air-core coil and a capacitor power source is applied
for orientation of the powder. At the time of orientation, the pulse magnetic field
may be applied repeatedly, while compressing the powder by upper and lower punches.
The larger the pulse magnetic field intensity, the better, at least 10 kOe (796 kA/m)
is necessary, preferably, 30 kOe to 80 kOe (2387 to 6366 kA/m}.
[0107] As shown in the graph of Fig. 2 showing the time and the magnetic field intensity,
the pulse magnetic field duration is preferably 1 µsec to 10 sec, more preferably
5 µsec to 100 msec, and an applying frequency of the magnetic field is preferably
1 to 10 times, more preferably, 1 to 5 times.
[0108] The oriented powder may be solidified by a hydrostatic press. At this time, in the
case of using the plastic mold, hydrostatic pressing can be effected as it is. Pressure
by the hydrostatic pressing process is preferably 0.5 ton/cm
2 to 5 ton/cm
2 (49 to 490 MPa), more preferably, 1 ton/cm
2 to 3 ton/cm
2 (98 to 294 MPa).
[0109] For continuously performing the orientation by the magnetic field and pressing, it
is possible to mold by a magnetic field pressing process, after embedding a coil generating
the pulse magnetic field in a die, and using the magnetic field for orientation. Pressure
by the magnetic field pressing process is likewise preferably 0.5 ton/cm
2 to 5 ton/cm
2 (49 to 490 MPa), more preferably, 1 ton/cm
2 to 3 ton/cm
2 (98 to 294 MPa).
EXAMPLES
Embodiment 1
[0110] A sheet cast piece having a thickness of about 1 mm is prepared from a molten alloy
having compositions of Nd 13.0 - B 6.0- Fe 81 obtained by melting in a high frequency
melting furnace, by using a double-roll type strip caster including two copper rolls
of 200 mm diameter. Crystal grain sizes of the cast piece are 0.5 µm to 15 µm in a
short axial direction and 5 µm to 80 µm in a long axial direction. An R-rich phase
which is finely separated into about 3 µm is present surrounding a main phase. The
oxygen content is 300 ppm.
[0111] The cast piece of 1000 g cut into a 50 mm square or smaller is placed in a closed
pressure vessel which can take in and discharge air, and N
2 gas is introduced into the pressure vessel for 30 minutes. After flushing out the
air, H
2 gas at 3 kg/cm
2 (about 300 kPa) pressure is fed into the pressure vessel for 2 hours to cause the
cast piece to decay spontaneously by hydrogenation. The decayed cast is retained in
vacuum at 500°C for 5 hours for dehydrogenation, and thereafter it is cooled to room
temperature and ground into 100 mesh.
[0112] Next, 800 g of this coarse grain is comminuted in a jet mill to obtain an alloy powder
of 3.5 µm mean grain size. The resulting alloy powder is packed into a rubber mold
and a pulse magnetic field of 60 kOe (4775 kA/m) is applied instantaneously for orientation.
The mold is then subjected to hydrostatic pressing at 2.5 T/cm
2 (245 MPa) by a hydrostatic press.
[0113] The molded body taken out from the mold is sintered at 1090°C for 3 hours to obtain
a permanent magnet after one hour annealing at 600°C. Magnetic characteristics and
density, crystal grain size, degree of orientation, the squareness of demagnetization
curve main phase amount and oxygen content are shown in Table 1.
Embodiment 2
[0114] A molten alloy having the same composition as that of Embodiment 1 is strip cast
to obtain a sheet cast piece having the sheet thickness of about 0.5 µm
[0115] Crystal grain sizes in the cast piece are 0.3 µm to 12 µm in a short axial direction
and 5 µm to 70 µm in a long axial direction, and an R-rich phase finely separated
into about 3 µm is present surrounding the main phase. The cast piece is comminuted
by a jet mill under the same condition as Embodiment 1 to obtain an alloy powder of
about 3.4 µm mean grain size. The powder is molded in a magnetic field of about 12
kOe (955 kA/m), after, first, having been oriented in a pulse magnetic field of about
30 kOe (2387 kA/m), by a press machine, in which, as shown in Fig. 1, static magnetic
field coils 3,4 are disposed around upper and lower punches 1,2, and a pulse magnetic
field coil 6 is provided in a die 5 so as to generate the pulse magnetic field and
the usual magnetic field commonly applied to magnet material powders 7. Thereafter,
the molded body is sintered and annealed under the same conditions as Embodiment 1.
[0116] Magnetic characteristics and density, crystal grain size, degree of orientation,
the squareness of demagnetization curve, main phase amount and O
2 content of the resulting permanent magnet are shown in Table 1.
Embodiment 3
[0117] An alloy ofNd 13.5 - Dy 0.5 - B 6.5 - Co 1.0 - Fe 78.5 is formed and strip cast as
in Embodiment 1 to obtain a sheet cast piece. The cast piece of 100 g cut into a 50
mm square or smaller is decayed spontaneously by hydrogenation as in Embodiment 1,
and dehydrogenated in vacuum for 6 hours. Then, after coarse grinding, it is comminuted
in a jet mill to obtain powder of 3.5 µm mean grain size.
[0118] The resulting powder is oriented in a pulse magnetic field as in Embodiment 1, and
a molded body obtained by hydrostatic pressing is sintered similarly. Magnetic characteristics
and density, crystal grain size, degree of orientation, the squareness of demagnetization
curve, main phase amount and O
2 content are shown in Table 1.
Comparative Example 1
[0119] The powder obtained at the same condition as the Embodiment 1 is pressed and molded
in the magnetic field of about 12 kOe (955 kA/m) by the usual magnetic field press
machine in dried state, then sintered and annealed at the same condition as in Embodiment
1. However, oxidation occurred during the pressing, thus densification to a sufficient
sinter density was impossible, and the magnetic characteristics could not be measured
and only the density and O
2 content are measured (Table 1).
Comparative Example 2
[0120] Coarse powder obtained under the same conditions as Embodiment 1 is comminuted in
a ball mill, using toluene as a solvent, to obtain the fine powder of 3.5 µm mean
grain size, which is pressed and molded in the magnetic field of about 12 kOe (955
kA/m) by the usual magnetic field press machine in a wet state, then sintered and
annealed under the same conditions as Embodiment 1.
[0121] Magnetic characteristics and density, crystal grain size, degree of orientation,
the squareness of the demagnetization curve, main phase amount O
2 content of the resulting permanent magnet are shown in Table 1.
Comparative Example 3
[0122] A molten alloy having the composition of Nd 14- B 6.0-Fe 80 obtained by melting in
a high-frequency melting furnace is cast in an iron mold. When the structure of the
resulting alloy ingot was observed, crystallization of a-Fe primary crystals is seen,
so it was heated at 1050°C for 10 hours in a homogenizing process.
[0123] Crystal grain sizes of the resulting ingot are 30 to 150 µm in a short axial direction
and 100 µm to several mm in a long axial direction, and an R-rich phase is segregated
with grain sizes of about 150 µm locally.
[0124] After coarsely grinding the alloy ingot, the coarse powder is obtained by the hydrogenation
and dehydrogenation processes of Embodiment 1. Furthermore, the coarse powder is comminuted
by a jet mill under the same conditions as Embodiment 1, and the resulting alloy powder
of about 3.7 µm mean grain size is pressed and molded in the magnet field of about
12 kOe (955 kA/m) for sintering and heat treatment at the same conditions as the Embodiment
1. Magnetic characteristics and density, crystal grain size, degree orientation, the
squareness of demagnetization curve, main phase amount and O
2 content of the resulting permanent magnet are shown in Table 1.
Comparative Example 4
[0125] After coarsely grinding a strip cast piece having the same composition and thickness
as the Embodiment 1, 1000 g of the resulting coarse powder is ground, for one hour
in a stamp mill, into coarse powders of 100 mesh, without the hydrogenation and dehydrogenation
processing, and is then comminuted in the jet mill to obtain the alloy powder of 3.8
µm mean grain size.
[0126] The alloy powder is pressed in the magnetic field of about 12 kOe (955 kA/m), sintered
and annealed to obtain the permanent magnet. Magnetic characteristics and density,
crystal grain size, degree of orientation, the squareness of demagnetization curve,
main phase amount and O
2 content of the resulting permanent magnet are shown in Table 1.
Comparative Example 5
[0127] An alloy having the composition ofNd 13.5- Dy 0.5- B 6.5 - Co 1.0 - Fe 78.5 is cast
by the same method as the Comparative Example 3. Since α-Fe primary crystals are present
in the resulting alloy ingot, it is subjected to heat treatment at 1050°C for 6 hours.
After coarsely grinding the alloy ingot, it is subjected to hydrogenation as in Embodiment
1, and then dehydrogenated in vacuum. The coarse powder is ground coarsely and comminuted
in a jet mill to obtain a powder of 3.7 µm mean grain size.
[0128] The powder is pressed in the magnetic field of about 12 kOe (955 kA/m), then sintered
and heated under the same condition as the Embodiment 1. Magnetic characteristics
and density, crystal grain size, degree of orientation, the squareness of demagnetization
curve, main phase amount and O
2 content of the resulting permanent magnet are shown in Table 1.
Comparative Example 6
[0129] After casting an alloy having the composition ofNd 16.5 - B 7- Fe 76.5 into an ingot
as in Comparative Example 3, without liquefaction, the ingot is ground coarsely, and
as in Comparative Example 4, coarsely ground in a stamp mill, thereafter comminuted
in a jet mill to obtain a fine powder of 3.7 µm mean grain size.
[0130] Furthermore, the fine powder is pressed in the magnetic field of about 12 kOe (955
kA/m), then sintered and annealed at the same condition as the Embodiment 1. Magnetic
characteristics and density, crystal grain size, degree of orientation the squareness
of the demagnetization curve, main phase amount and O
2 content of the resulting permanent magnet are shown in Table 1.
Table 1-1
| |
Br (kG) |
Hc |
(BH)max |
iHc |
| |
10-1T |
kOe |
kA/m |
MGOe |
kJ/m3 |
kOe |
kA/m |
| Embodiment 1 |
14.8 |
10.50 |
835.6 |
53.1 |
422.6 |
10.58 |
841.9 |
| Embodiment 2 |
14.5 |
11.0 |
875.4 |
50.8 |
404.3 |
11.50 |
915.1 |
| Embodiment 3 |
13.8 |
12.9 |
1026.5 |
45.9 |
365.3 |
15.00 |
1193.7 |
| Comparative Example 1 |
_ |
_ |
_ |
_ |
_ |
_ |
_ |
| Comparative Example 2 |
13.3 |
9.9 |
787.8 |
42.0 |
334.2 |
9.98 |
794.2 |
| Comparative Example 3 |
13.4 |
10.3 |
819.6 |
42.7 |
339.8 |
10.70 |
851.5 |
| Comparative Example 4 |
13.1 |
10.0 |
795.8 |
40.5 |
322.3 |
10.30 |
819.6 |
| Comparative Example 5 |
12.9 |
11.3 |
899.2 |
39.3 |
312.7 |
13.50 |
1074.3 |
| Comparative Example 6 |
12.2 |
10.5 |
835.6 |
34.4 |
273.7 |
11.50 |
915.1 |
Table 1-2
| |
density ρ (g/cm3) |
crystal grain size (µm) |
degree of orientation f(%) |
angularity (squareness) See Note 1 |
main phase amount (1-a)(%) |
oxygen content (ppm) |
| Embodiment 1 |
7.55 |
average 6 |
96 |
1.031 |
96.5 |
1500 |
| Embodiment 2 |
7.57 |
average 6 |
95.5 |
1.035 |
94.0 |
2500 |
| Embodiment 3 |
7.59 |
average 6 |
93.2 |
1.038 |
92.7 |
2000 |
| Comparative Example 1 |
6.8 |
_ |
_ |
_ |
_ |
6500 |
| Comparative Example 2 |
7.40 |
average 11 |
87.5 |
1.053 |
96.5 |
4200 |
| Comparative Example 3 |
7.44 |
average 15 |
88.4 |
1.052 |
95.5 |
5000 |
| Comparative Example 4 |
7.43 |
average 12 |
86.5 |
1.060 |
95.5 |
5500 |
| Comparative Example 5 |
7.44 |
average 14 |
87.2 |
1.058 |
92.7 |
5000 |
| Comparative Example 6 |
7.50 |
average 15 |
85.8 |
1.081 |
86.0 |
6500 |
| Note 1: The angularity or squareness is calculated as the function {(Br2×1.99)/(BH)max} when Br is measured in tenths of a Tesla and (BH)max is measured in
kJ/m3, or as the function {(Br2/4)/(BH)max} when (BH)max is measured in MGOe. These two functions give the same numerical
result. |
Embodiment 4
[0131] The following are used as materials for a main phase alloy powder by a strip casting
process,
340 g a Nd metal of 99% purity,
8 g of a Dy metal of 99% purity,
65.5 g of a Fe-B alloy containing 20% B, and
600 g of an electrolytic iron of 99% purity
[0132] These materials are melted in an Ar atmosphere so as to obtain an alloy having a
predetermined composition, then cast by a strip casting process using copper rolls
to obtain a cast piece having a plate thickness of about 2 mm. The cast piece is coarsely
ground by a hydrogenation processing, and comminuted by a jaw crusher, a disk mill
or the like to obtain 800 g of powder of about 10 µm mean grain size.
[0133] The resulting powder consisting of 14.9 atomic % Nd, 0.1 atomic % Pr, 0.3 atomic
% Dy, 8.0 atomic % B and Fe, is observed by an x-ray diffraction EPMA, as a result,
it is confirmed that O
2 content is about 800 ppm. As the result of EPMA observation on the cast piece structure,
the R
2Fe
14B main phase is about 5 µm in a short axial direction and 20 to 80 µm in a long axial
direction, and the R-rich phase is finely dispersed surrounding the main phase.
[0134] As materials of adjusting alloy powders containing an R
2Fe
17 phase by the strip casting process,
250 g of a Nd metal of 99% purity,
11 g of a Dy metal of 99% purity,
730 g of an electrolytic iron of 99% purity and
20 g of a Fe-B alloy containing 20.0% B
are used, to obtain a cast piece having a plate thickness of about 2 mm, the same
as the main phase alloy. Furthermore, the powder is prepared by the same processing
as the main phase alloy. A composition of the resulting powder is a 0.8 atomic % Nd,
0.1 atomic % Pr, 0.4 atomic % Dy, 2.4 atomic % B and Fe.
[0135] As noted from EPMA observation on the cast piece structure, it consists of the R
2Fe
17 phase, partly R
2Fe
14B and the Nd-rich phase: α-Fe is not confirmed. The oxygen content is 850 ppm.
[0136] Using the above-mentioned two kinds of material powders, 30% adjusting alloy powder
is blended with the main phase alloy powder. The material powders are fed into a grinder
such as a jet mill or the like to pulverize into about 3 'Lm, the resulting fine powder
is filled into a rubber mold, and is subjected to hydrostatic pressing at 2.5 T/cm
2 (245MPa)by a hydrostatic press machine, after applying a pulse magnetic field of
60 kOe(4775 kA/m) instantaneously for orientation, thereby to obtain a molded body
of 8 mm × 15 mm × 10 mm,
[0137] The molded body is sintered at 1100°C in an Ar atmosphere for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics ofthe resulting magnet are shown in
table 2.
Comparative Example 7
[0138] As materials for the main phase alloy powder, as in Embodiment 4,
340 g of a Nd metal of 99% purity,
8 g of a Dy metal of 99% purity,
600 g of an electrolytic iron of 99% purity and
65.5 g of a FE-B alloy containing 20% B
are used:, these are molten in an Ar atmosphere and cast in an iron mold. The resulting
alloy ingot is comminuted into the powder of 10 µm mean grain size by the same method
as the Embodiment 1. Following composition analysis, it is found to consist of 14.9
atomic % Nd, 0.1 atomic % Pr, 0.3 atomic % Dy, 8.0 atomic % B and Fe (balance). The
oxygen content is about 900 ppm.
[0139] As the result of EPMA observation on the alloy ingot structure, the R
2Fe
14B main phase is about 50 µm in a short axial direction and about 500 µm in a long
axial direction, the R-rich phase having grain sizes of 50 µm is locally present throughout.
Also, α-Fe of 5 to 10 µm is seen in the main phase.
[0140] As adjusting materials containing the R
2Fe
17 phase,
200 g Md2O3 (98% purity),
12 g of Dy2O3 (99% purity),
65 g of a Fe-B alloy containing 20% B and
600 g of iron powders of 99% purity
are used, to which 150 g of metal Ca of 99% purity and 25 g of CaCl
2 anhydride are mixed, and charged into a stainless steel pressure vessel to obtain
the adjusting alloy powder by a direct reducing and diffusing process at 950°C for
8 hours in the Ar atmosphere. Component analysis of the resulting alloy powder shows
of 10.8 atomic % Nd, 0.1 atomic % Pr, 0.4 atomic percent Dy, 2.4 atomic % B and Fe
(balance). The oxygen content is 1500 ppm. Using the aforementioned two kinds of material
powders, 30% adjusting alloy powder is blended with the main phase alloy powder and
comminuted into about 3 µm in a grinder such as a jet mill or the like. The resulting
fine powder is oriented in a magnetic field of about 10 kOe (796 kA/m), and molded
at about 1.5 T/cm
2 (about 150 MPa) pressure at right angles to the magnetic field to obtain a molded
body of 8 mm × 15 mm × 10 mm.
[0141] The molded body is sintered in an Ar atmosphere at 1100°C for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics of the resulting magnet are also shown
in Table 2.
Comparative Example 8
[0142] The main phase alloy powder of Comparative Example 1 is used, and as materials for
the adjusting alloy powder,
250 g of a Nd metal of 99% purity,
11 g of Dy metal of 99% purity,
730 g of an electrolytic iron of 99% purity and 20 g of a Fe-B alloy containing 20.0
g B-are used, melted in an Ar atmosphere and cast in an iron mold. By observation
on the structure of the resulting alloy ingot, it is confirmed that a large amount
of α-Fe is crystallized, so a homogenizing process is performed at 1000°C for 12 hours.
[0143] Component analysis made by the same method as Embodiment 4, shows 10.8 atomic % Nd,
0.1 atomic % Pr, 0.4 atomic % Dy, 2.4 atomic % B and Fe (balance).
[0144] Using the above-mentioned two kinds of material powders, 30% adjusting alloy powder
is blended with the main phase alloy powder to prepare a magnetic as in Comparative
Example 7. Magnetic characteristics of the resulting magnet are shown in Table 2.
Comparative Example 9
[0145] As materials,
315 g of a Nd metal of 99% purity,
8.5 g of a Dy metal of 99% purity,
52 g of a Fe-B alloy containing 20 % B and
636 g of an electrolytic iron of 99% purity
are used, melted in an Ar atmosphere so as to obtain an alloy having a predetermined
composition, then a cast piece having a plate thickness of about 2 mm is obtained
by the strip casting process using copper rolls. The cast piece is coarsely ground
by hydrogenation processing ,then comminuted in a jaw crusher, disk mill or the like
to obtain 800 g of powders of 10 µm mean grain size.
[0146] EPMA observation on the resulting powder, shows 13.8 atomic % Nd, 0.1 atomic % Pr,
0.3 atomic % Dy, 6.3 atomic % B and Fe Balance). The oxygen content is about 800 ppm.
As the result EPMA observation also on the cast piece structure, the crystal size
ofthe R
2Fe
14B main phase is about 6 µm in a short axial direction and 20 to 80 µm in a long axial
direction, and the R-rich phase is present as a fine phase surrounding the main phase.
[0147] Using the alloy powder by the strip casting process, a magnet is produced as described
in Comparative Example 7. Magnetic characteristics of the resulting magnet are also
shown in Table 2.
Table 2-1
| |
composition |
magnetic characteristics |
| |
|
Br (kG) |
Hc |
(BH)max |
iHc |
| |
|
10-1T |
kOe |
kA/m |
MGOe |
kJ/m3 |
kOe |
kA/m |
| Embodiment 4 |
13.8Nd - 0.1Pr - 0.3Dy - 6.3B - bal. Fe |
14.0 |
12.5 |
994.7 |
47.5 |
378.0 |
13.5 |
1074.3 |
| Comparative Example 7 |
13.8Nd - 0.1Pr - 0.3Dy - 6.3B - bal. Fe |
13.2 |
12.0 |
954.9 |
40.7 |
323.9 |
12.5 |
994.7 |
| Comparative Example 8 |
13.8Nd - 0.1Pr - 0.3Dy - 6.3B - bal. Fe |
13.2 |
11.9 |
947.0 |
40.8 |
324.7 |
12.0 |
954.9 |
| Comparative Example 9 |
13.8Nd - 0.1Pr - 0.3Dy - 6.3B - bal. Fe |
13.3 |
12.3 |
978.8 |
42.3 |
336.6 |
12.9 |
1026.5 |
Table 2-2
| |
density ρ (g/cm3) |
crystal grain size (µm) |
degree of orientation f% |
angularity (squareness) See Note 1 |
main phase amount (1-α)(%) |
oxygen content (ppm) |
| Embodiment 4 |
7.56 |
average 8 |
94.5 |
1.32 |
92.8 |
3000 |
| Comparative Example 7 |
7.53 |
average 15 |
89.2 |
1.07 |
92.8 |
5000 |
| Comparative Example 8 |
7.53 |
average 16 |
89.2 |
1.068 |
92.8 |
5500 |
| Comparative Example 9 |
7.54 |
average 8 |
89.9 |
1.053 |
92.8 |
4000 |
| Note 1: The angularity or squareness is calculated as the function {(Br2×1.99)/(BH)max} when Br is measured in tenths of a Tesla and (BH)max is measured in
kJ/m3, or as the function {(Br2/4)/(BH)max} when (BH)max is measured in MGOe. These two functions give the same numerical
result. |
Embodiment 5
[0148] 800 g of main phase alloy powder of 10 µm mean grain size having a composition different
from the Embodiment 4 is obtained by the process of that Embodiment. The resulting
powder consists of 14 atomic % Nd, 0.1 atomic % Pr, 0.5 atomic % Dy, 8 atomic % B
and Fe. As the result of observation by the x-ray diffraction EPMA, it is mostly the
R
2Fe
14B phase. The oxygen content is about 80 ppm. As the result of EPMA observation on
the cast piece structure, the R
2Fe
14B main phase has a grain size of about 0.5 to 15 µm in a short axial direction and
5 to 90 µm in a long axial direction, and the R-rich phase is dispersed finely to
surround the main phase.
[0149] As materials ofthe adjusting alloy powder containing an R
2Fe
17 phase, 125 g of Nd metal of 99% purity, 5 g of Dy metal of 99% purity and 275 g of
an electrolytic iron of 99% purity are used, and a cast piece having a plate thickness
of about 2 mm is obtained by the same strip casting process as the main phase alloy.
This, powder is prepared by the same process as the main phase alloy. The composition
of the resulting powder is 11.0 atomic % Nd, 0.05 atomic % Pr, 0.4 atomic % Dy and
Fe.
[0150] EPMA observation on the cast piece structure shows it to consist of an R
2Fe
17 phase, partly R
2Fe
14B, and an R-rich phase: α-Fe is not seen. The oxygen content at 10 µm mean grain size
is 700 ppm.
[0151] Using the two above-mentioned kinds of material powders, 25 % adjusting alloy powder
is blended with the main phase alloy powder. The material powders are charged into
a grinder such as a jet mill to comminute it into about 3 µm, then packed into a rubber
mold, and the resulting fine powder is subjected to hydrostatic pressing at 2.5 T/cm
2 (245 MPa) pressure by an isostatic press machine to obtain a molded body of 8 mm
x 15 mm x 10 mm, after applying a pulse magnet field of 60 kOe (4775 kA/m) instantaneously
for orientation.
[0152] The molded body is sintered in an Ar atmosphere at 1100°C for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics of the resulting magnet are shown
in Table 3.
Comparative Example 10
[0153] As the main phase alloy powder, an alloy having the same composition as the Embodiment
5 is cast in an iron mold to obtain powder of about 10 µm mean grain size by the same
method as Embodiment 4. Composition is 14 atomic % Nd, 0.1 atomic % Pr, 0.5 atomic
% Dy, 8 atomic % B and Fe (balance), the oxygen content is about 900 ppm. As a result,
the crystal grain size is about 50 µm in a short axial direction and about 500 µm
in a long axial direction, and an R-rich phase (50 µm) is locally present throughout.
Also, 5 to 10 µm crystals of α-Fe are present in the main phase.
[0154] The adjusting alloy powder containing the R
2Fe
17 phase is produced by the same direct reducing and diffusing process as Comparative
Example 7, by using 280 g of Nd
2O
3 (purity 98%), 12 g of Dy
2O
3 (purity 99%) and 750 g of iron powder (purity 99%). Components are 11.0 atomic %
Nd, 0.05 atomic % Pr, 0.9 atomic % Dy and Fe. The oxygen content is 1500 ppm.
[0155] Using the above-mentioned two kinds of material powder, 25% adjusting alloy powder
is blended with the main phase alloy powder, and charged into a jet mill or the like
to comminute it to about 3 µm The resulting fine powder is oriented in the magnet
field of about 10 kOe (796 kA/m), and molded at about 1.5 T/cm
2 (about 150 MPa) pressure at right angles to the magnetic field to obtain a molded
body of 8 mm × 15 mm × 10 mm.
[0156] The molded body is sintered in an Ar atmosphere at 1100°C for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics ofthe resulting magnet are also shown
in Table 3.
Comparative Example 11
[0157] Using the main phase alloy powder of Comparative Example 10, an adjusting alloy powder
is prepared by melting 350 g of a Nd metal, 10 g of a Dy metal and 750 g of an electrolytic
iron of 99% purity in the Ar atmosphere, and cast in the iron mold. As the result
of observation on the resulting alloy ingot, since a large amount of α-Fe is crystallized,
homogenizing is effected at 1000°C for 12 hours. As shown by component analysis, it
consists of 11.0 atomic % Nd, 0.05 atomic % Pr, 0.4 atomic % Dy and Fe (balance).
[0158] Using the above-mentioned two material powders, 25% adjusting alloy powder is blended
with the main phase alloy powder to produce a magnet as in Comparative Example 10.
Magnetic characteristics of the resulting magnet are also shown in Table 3.
Comparative Example 12
[0159] As starting materials, 300 g of a Nd metal, 13 g of a Dy metal, 50 g of a Fe-B alloy
containing 20% B and 645 g of an electrolytic iron of 99% purity are used, and melted
in an Ar atmosphere so as to obtain an alloy having a predetermined composition, then,
by the strip casting process using copper rolls, a cast piece having a plate thickness
of about 2 mm is obtained. Furthermore, the cast piece is pulverized by hydrogenation,
and jaw crusher, disk mill and the like to obtain 800 g of powder of about 10 µm mean
grain size.
[0160] The resulting powder consists of 13.3 atomic % Nd, 0.1 atomic % Pr, 0.5 atomic %
Dy, 6 atomic % B and Fe (balance). The oxygen content is about 800 ppm. As shown by
EPMA observation on the cast piece structure, the R
2Fe
14B main phase crystal size is about 0.3 to 15 µm in a short axial direction and about
5 to 90 µm in a long axial direction, and an R-rich phase is present as a fine phase
surrounding the main phase.
[0161] Using the alloy powder by the strip casting process, a magnet is produced in the
same way as Comparative Example 10. Magnetic characteristics of the resulting magnet
are also shown in Table 3.
Table 3-1
| |
composition |
magnetic characteristics |
| |
|
Br (kG) |
Hc |
(BH)max |
iHc |
| |
|
10-1T |
kOe |
kA/m |
MGOe |
kJ/m3 |
kOe |
kA/m |
| Embodiment 5 |
13.3Nd - 0.1Pr - 0.5Dy - 6B - bal. Fe |
14.2 |
12.8 |
1018.6 |
48.5 |
386.0 |
14.5 |
1153.9 |
| Comparative Example 10 |
13.3Nd - 0.1Pr - 0.5Dy - 68 - bal. Fe |
13.3 |
11.5 |
915.1 |
41.5 |
330.2 |
13.5 |
1074.3 |
| Comparative Example 11 |
13.3Nd - 0.1Pr - O.5Dy -6B-bal. Fe |
13.3 |
11.8 |
939.0 |
41.7 |
331.8 |
13.6 |
1082.3 |
| Comparative Example 12 |
13.3Nd -0.1Fr - 0.5Dy - 68 - bal. Fe |
13.4 |
11.6 |
923.1 |
42.6 |
339.0 |
14.0 |
1114.1 |
Table 3[sim ]2
| |
density ρ (g/cm3) |
crystal grain size (µm) |
degree of orientation f% |
angularity (squareness) See Note 1 |
main phase amount (1-α)(%) |
oxygen content (ppm) |
| Embodiment 5 |
7.57 |
average 6 |
95.9 |
1.039 |
94.0 |
2000 |
| Comparative Example 10 |
7.56 |
average 14 |
89.8 |
1.066 |
94.0 |
5000 |
| Comparative Example 11 |
7.55 |
average 15 |
89.8 |
1.060 |
94.0 |
5500 |
| Comparative Example 12 |
7.56 |
average 8 |
90.5 |
1.054 |
94.0 |
3800 |
| Note 1: The angularity or squareness is calculated as the function {(Br2×1.99)/(BH)max} when Br is measured in tenths of a Tesla and (BH)max is measured in
kJ/m3, or as the function {(Br2/4)/(BH)max} when (BH)max is measured in MGOe. These two functions give the same numerical
result. |
Embodiment 6
[0162] As materials of the main phase alloy powder produced by the strip casting process,
260 g of a Nd metal of 99% purity,
23 g of a Dy metal of 99% purity,
68.5 g of a Fe-B alloy containing 20% B and
655 g of an electrolytic iron of 99% purity
are used. These are melted in an Ar atmosphere so as to obtain an alloy having predetermined
composition, then cast by the strip casting process using copper rolls to obtain a
cast piece having the plate thickness of about 2 mm. The cast piece is coarsely ground
by hydrogenation processing, and pulverized by a jaw crusher, a disk mill or the like
to obtain 800 g of powder of about 10 µm mean grain size.
[0163] The resulting powder consists of 11 atomic % Nd, 0.1 atomic % Pr, 1.0 atomic % Dy,
8 atomic % B and Fe (balance), as is observed by x-ray diffraction EPMA, and it is
confirmed that it mostly consists of a R
2Fe
14B phase. The oxygen content is about 800 ppm. As the result of EPMA observation on
the cast piece structure, the R
2Fe
14B main phase crystal size is about 0.5 to 1.5 µm in a short axial direction and 5
to 90 µm in a long axial direction, and the R-rich phase is finely dispersed surrounding
the main phase.
[0164] As materials of an adjusting alloy powder containing an R-Co intermetallic compound
phase produced by the strip casting process,
490 g of a Nd metal,
2∼6 g of a Dy metal and
500 g of Co of 99% purity
are used, to obtain a cast piece having the plate thickness of about 2 mm, the same
as the main phase alloy. Also, adjusting alloy powder is prepared by the same processing
as the main phase alloy. The composition of the resulting powder is 27.0 atomic %
Nd, 0.5 atomic % Pr, 1.3 atomic % Dy and Co (balance).
[0165] Following EPMA observation of the cast piece structure, it consists of the R
3Co phase and partly the R
2Co
17 phase, and the R
3Co phase is finely dispersed. The oxygen content in the powder, which has a 10 µm
mean grain size, is 700 ppm.
[0166] Using the above-mentioned two powders, 20% adjusting alloy powder is blended with
the main phase alloy powder. The material powders are charged into a grinder such
as a jet mill or the like to comminute them into about 3 µm grain sizes, and the resulting
powder is filled into a rubber mold and is subjected to hydrostatic pressing at 2.5
T/cm
2 (245 MPa) by a hydrostatic press machine, after applying a pulse magnetic field of
60 kOe (4775 kA/m) instantaneously for orientation, thereby to obtain a molded body
of 8 mm × 15mm × 10 mm.
[0167] The molded body is sintered at 1100°C in an Ar atmosphere for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics of the resulting magnet are shown
in Table 4.
Embodiment 7
[0168] Magnetic characteristics of the magnet obtained by blending 10 % adjusting alloy
powder with the main phase alloy powder prepared in the Embodiment 1, and magnetizing
by the same process as the Embodiment 6 are shown in Table 4.
Comparative Example 13
[0169] For the main phase alloy powder, as in Embodiment 6,
260 g of a Nd metal of 99% purity,
26 g of a Dy metal of 99% purity,
665 g of an electrolytic iron of 99% purity and
68.5 g of a Fe-B alloy containing 20.0% B
are used, melted in an Ar atmosphere and cast in an iron mold. The resulting alloy
ingot is comminuted into powder of about 10 µm mean grain size by the same method
as the Embodiment 1. Component analysis shows the powder to consist of 11 atomic %
Nd, 0.1 atomic % Pr, 1.0 atomic % Dy, 8 atomic % B and Fe (balance), the oxygen content
is about 900 ppm.
[0170] EPMA observation on the alloy ingot structure indicates that the R
2Fe
14B main phase crystal size is about 50 µm in a short axial direction and about 500
µm in a long axial direction, the R-rich phase (50 µm) is locally present throughout.
Some α-Fe of 5 to 10 µm grain size is present in the main phase.
[0171] As adjusting materials containing an R-Co intermetallic compound phase, by the direct
reducing and diffusing process,
550 g of Nd2O3 (98% purity),
29 g of Dy2O3 (99% purity) and
500 g of Co powder of 99% purity
are used, to which 350 g of metal Ca of 99% purity and 60 g of CaCl
2 anhydride are mixed, and charged into a stainless steel pressure vessel to obtain
an alloy powder in an Ar atmosphere at 750°C for 8 hours. Component analysis shows
the resulting alloy powder to consist of 27.0 atomic % Nd, 0.6 atomic % Pr, 1.3 atomic
% Dy and Co, the oxygen content is 1500 ppm.
[0172] Using the above-mentioned two kinds of material powders, 20 % adjusting alloy powder
is blended with the main phase alloy powder, and charged into a grinder such as a
jet mill or the like to pulverize into about 3 µm. The resulting fine powder is oriented
in the magnetic field of about 10 kOe (796 kA/m), and molded at about 1.5 T/cm
2 (about 150 MPa) pressure to obtain a molded body of 8 mm × 15 mm × 10 mm.
[0173] The molded body is sintered in an Ar atmosphere at 1100°C for 3 hours, and annealed
at 550°C for one hour. Magnetic characteristics of the resulting magnet are also shown
in Table 4.
Comparative Example 14
[0174] Using the main phase alloy of Embodiment 13, the adjusting alloy powder is prepared
by melting.
490 g of a Nd metal,
26 g of Dy metal and
500 g of Co of 99% purity
in an Ar atmosphere, and casting in an iron mold. As shown by observation on the
resulting alloy ingot structure, a large amount of Co is crystallized, so homogenizing
is effected at 800°C for 12 hours. Component analysis, shows it to consist of 11.0
atomic % Nd, 0.6 atomic % Pr, 1.3 atomic % Dy and Co.
[0175] Using the above-mentioned two material powders, 20% adjusting alloy powder is blended
with the main phase alloy powder to produce a magnet as in Comparative Example 13.
Magnetic characteristics of the resulting magnet are also shown in Table 4.
Comparative Example 15
[0176]
305 g of a Nd metal,
26 g of a Dy metal,
55 g of a Fe-B alloy containing 20% B,
100 g of Co of 99% purity, and
525 g of an electrolytic iron of 99% purity are melted in an Ar atmosphere so as to
obtain an alloy having a predetermined composition, and by the strip casting process
using copper rolls, a cast piece having a plate thickness of about 2 mm is obtained.
The cast piece is coarsely ground by hydrogenation processing and comminuted by a
jaw crusher, disk mill or the like to obtain 800 g of powder of about 10 µm grain
size.
[0177] The resulting powder consists of 13.5 atomic % Nd, 0.1 atomic % Pr, 1.0 atomic %
Dy, 6.7 atomic % B, 11.3 atomic % Co and Fe. The oxygen content is about 800 ppm.
As the result of EPMA observation on the cast piece structure, the crystal size of
the R
2(Fe, Co
14)B phase is about 0.3 to 1.5 µm in a short axial direction and about 5 to 90 µm in
a long axial direction, the R-rich phase and the R-Co phase being present finely surrounding
the main phase.
[0178] Using the alloy powder by the strip casting process, a magnet is produced as in Comparative
Example 3.
[0179] Magnetic characteristics of the resulting magnet are also shown in Table 4.
Table 4-1
| |
composition |
magnetic characteristics |
Density |
| |
|
Br |
Hc |
(BH)max |
iHc |
|
| |
|
10-1T |
kOe |
kA/m |
MGOe |
kJ/m3 |
kOe |
kA/m |
g/cm3 |
| Embodiment 6 |
13.5Nd - 0.1Pr - 1.ODy 6.7B - 6.5Co - bal. Fe |
13.3 |
12.4 |
986.8 |
42.5 |
338.2 |
17.0 |
1352.8 |
7.62 |
| Embodiment 7 |
12.3Nd-0.1Pr - 1ODy 7.3B - 11.3Co - bal. Fe |
13.5 |
12.5 |
994.7 |
44.0 |
350.1 |
16.8 |
1336.9 |
7.61 |
| Comparative Example 13 |
13.SNd - 0.1Pr - 1ODy 6.7B - 11.3Co - bal. Fe |
12.0 |
11.0 |
875.4 |
34.0 |
270.6 |
15.8 |
1257.3 |
7.56 |
| Comparative Example 14 |
13.5Nd - 0.1Fr - 1ODy 6.7B - 11.3Co - bal. Fe |
12.2 |
11.1 |
883.3 |
35.0 |
278.5 |
15.5 |
1233.5 |
7.55 |
| Comparative Example 15 |
13.5Nd - 0.1Pr - 1ODy 6.7B - 11.3Co - bal. Fe |
12.2 |
11.2 |
891.3 |
35.2 |
280.1 |
16.5 |
1313.0 |
7.58 |
Table 4-2
| |
density ρ (g/cm3) |
crystal grain size (µm) |
degree of orientation f% |
angularity (squareness) See Note 1 |
main phase amount (1-α)(%) |
oxygen content (ppm) |
| Embodiment 6 |
7.62 |
average 5 |
94 |
1.04 |
91 |
2800 |
| Embodiment 7 |
7.61 |
average 6 |
95.5 |
1.036 |
94 |
2200 |
| Comparative Example 13 |
7.56 |
average 14 |
85.7 |
1.056 |
91 |
4800 |
| Comparative Example 14 |
7.55 |
average 15 |
87.1 |
1.063 |
91 |
5000 |
| Comparative Example 15 |
7.58 |
average 6 |
87.1 |
1.057 |
91 |
3500 |
| Note 1: The angularity or squareness is calculated as the function {(Br2×1.99)/(BH)max} when Br is measured in tenths of a Tesla and (BH)max is measured in
kJ/m3, or as the function {(Br2/4)/(BH)max} when (BH)max is measured in MGOe. These two functions give the same numerical
result. |
1. An R-Fe-B permanent magnet material characterised in that such material is of a substantially
homogeneous composition consisting of:
R 12 atomic % to 16 atomic %, where R represents at least one rare earth element,
B 4 atomic % to 8 atomic %,
O2 5000 ppm or less,
and which optionally contains one or more additives selected from:
| 0 to 9.5 atomic % of Al, |
0 to 4.5 atomic % of Ti, |
0 to 9.5 atomic % of V, |
| 0 to 8.5 atomic % of Cr, |
0 to 8.0 atomic % of Mn, |
0 to 5 atomic % of Bi, |
| 0 to 12.5 atomic % of Nb, |
0 to 10.5 atomic % of Ta, |
0 to 9.5 atomic % of Mo, |
| 0 to 9.5 atomic % of W, |
0 to 2.5 atomic % of Sb, |
0 to 7 atomic % of Ge, |
| 0 to 3.5 atomic % of Sn, |
0 to 5.5 atomic % of Zr, |
and |
| 0 to 5.5 atomic % of Hf, |
|
|
the balance being Fe, of which a part is optionally replaced by one or both of Co
and Ni, and unavoidable impurities,
and which contains 90% or more of a main phase of R
2Fe
14B, of which a part of the Fe is optionally replaced by one or both of Co and Ni, and
has a mean grain size of 10 µm or less, an apparent density of 7.45 g/cm
3 or more, a degree of orientation of 85% or more, and which has magnetic properties
such that when the maximum energy product value (BH)max is expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

and such that when the residual magnetic flux density, Br is expressed in tenths
of one Tesla (10
-1T=1kG), the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} is between 1.01 and 1.045.
2. An R-Fe-B permanent magnet material in accordance with claim 1, and containing:
R 12.5 atomic % to 14 atomic %, where R represents at least one rare earth element
B 5.8 atomic % to 7 atomic %,
O2 200 ppm to 3000 ppm.
3. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
less than 50% of Fe is replaced by one or both of Co and Ni.
4. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
a main phase of R2Fe14B of which a part of the Fe is optionally replaced by one or both of Co and Ni constitutes
94% or more of the material.
5. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
a maximum frequency of crystal grain sizes is between 5 µm and 6 µm.
6. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
the degree of orientation is 92% or more.
7. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
when the (BH)max value is above 50 MGOe (398 kJ/m3), and the iHc value is 9 kOe (716 kA/m) or more.
8. An R-Fe-B permanent magnet material in accordance with claim 1 or claim 2, wherein
when the (BH)max value above 45 MGOe (3581 kJ/m3), and the iHc value is 14 kOe (827 kA/m) or more.
9. A process of producing R-Fe-B permanent magnet material characterized by the steps
of: strip casting a molten alloy composed of
R 12 atomic % to 16 atomic % where R represents at least one rare earth element,
B 4 atomic % to 8 atomic %,
O2 5000 ppm or less,
and which optionally contains one or more of:
| 0 to 9.5 atomic % of Al, |
0 to 4.5 atomic % of Ti, |
0 to 9.5 atomic % of V, |
| 0 to 8.5 atomic % of Cr, |
0 to 8.0 atomic % of Mn, |
0 to 5 atomic % of Bi, |
| 0 to 12.5 atomic % of Nb, |
0 to 10.5 atomic % of Ta, |
0 to 9.5 atomic % of Mo, |
| 0 to 9.5 atomic % of W, |
0 to 2.5 atomic % of Sb, |
0 to 7 atomic % of Ge, |
| 0 to 3.5 atomic % of Sn, |
0 to 5.5 atomic % of Zr, |
and |
| 0 to 5.5 atomic % of Hf, |
|
|
the balance being Fe of which a part is optionally replaced by one or both of Co
and Ni, and unavoidable impurities, to form a cast strip containing 90% or more of
a main phase of R
2Fe
14B of which a part of the Fe is optionally replaced by one or both of Co and Ni, placing
the cast strip in a pressure vessel, discharging air therefrom and substituting hydrogen
in order to cause the cast strip to decay by hydrogenation,
dehydrogenating the cast strip
comminuting the cast strip under an inert gas into a powder having a mean grain size
between 1 µm and 10µm,
packing the powder into a mold and orienting the packed powder by momentarily applying
a pulsed magnetic field having a strength of at least 10kOe (796 kA/m), and then molding,
sintering and annealing the material, thereby to form a permanent magnet material
which has magnetic properties such that when the maximum energy product value (BH)max
is expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

and such that when the residual magnetic flux density (Br) is expressed in tenths
of one Tesla (10
-1T=1kG), the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} is between 1.01 and 1.045
10. A process of producing R-Fe-B permanent magnet material in accordance with claim 9,
wherein the molten alloy contains:
R 12.5 atomic % to 14 atomic %, where R represent at least one rare earth element
B 5.8 atomic % to 7 atomic %,
O2 200 ppm to 3000 ppm,
11. A process of producing R-Fe-B permanent magnet material characterized by the steps
of strip casting a molten main phase alloy and strip casting an adjusting alloy, placing
the cast strip of each alloy in a pressure vessel, discharging air therefrom and substituting
hydrogen in order to cause each cast alloy strip to decay by hydrogenation, dehydrogenating
the cast alloys
comminuting the cast alloys under an inert gas into powders each having a mean grain
size between 1 µm and 10µm,
blending the powders to form a mixture containing 90% or more of R
2Fe
14B of which a part of the Fe is optionally replaced by one or both of Co and Ni, and
packing the powder mixture into a mold and orienting the packed powder by momentarily
applying a pulsed magnetic field having a strength of at least 10kOe (796 kA/m), and
then molding, sintering and annealing the material, thereby to form a permanent magnet
material which has magnetic properties such that when the maximum energy product value
(BH)max is expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

and such that when the residual magnetic flux density (Br) is expressed in tenths
of one Tesla (10
-1T=1kG), the squareness of the demagnetization curve {(Br
2×1.99)/(HB)max} {(Br
2/4)/(BH)max} is between 1.01 and 1.045., wherein said main phase alloy contains:
R 11 atomic % to 20 atomic % where R represents at least one rare earth element,
B 4 atomic % to 12 atomic %,
and said adjusting alloy contains:
R 20 atomic % or less where R again represents at least one rare earth element,
and wherein the balances of said main phase alloy and said adjusting alloy are so
made up that said powder blend optionally contains one or more of:
| 0 to 9.5 atomic % of Al, |
0 to 4.5 atomic % of Ti, |
0 to 9.5 atomic % of V, |
| 0 to 8.5 atomic % of Cr, |
0 to 8.0 atomic % of Mn, |
0 to 5 atomic % of Bi, |
| 0 to 12.5 atomic % of Nb, |
0 to 10.5 atomic % of Ta, |
0 to 9.5 atomic % of Mo, |
| 0 to 9.5 atomic % of W, |
0 to 2.5 atomic % of Sb, |
0 to 7 atomic % of Ge, |
| 0 to 3.5 atomic % of Sn, |
0 to 5.5 atomic % of Zr, |
and |
| 0 to 5.5 atomic % of Hf, |
|
|
and so that the balance of said powder blend is Fe of which a part is optionally
replaced by one or both of Co and Ni, and unavoidable impurities.
12. A process of producing R-Fe-B permanent magnet material in accordance with claim 11,
wherein the main phase molten alloy contains 13 atomic % to 16 atomic % R and 6 atomic
% to 10 atomic % B.
13. A process of producing R-Fe-B permanent magnet material in accordance with claim 11,
wherein said adjusting alloy contains 20 atomic % or less of R and 6 atomic % or less
of B
14. A process of producing R-Fe-B permanent magnet materials in accordance with claim
13, wherein said adjusting alloy contains 5 atomic % to 15 atomic % of R.
15. A process of producing R-Fe-B permanent magnet materials in accordance with claim
11 and claim 13, wherein said main phase alloy contains:
R 13 atomic % to 16 atomic %, and
B 6 atomic % to 10 atomic %.
16. A process in accordance with claim 11 for producing R-Fe-B permanent magnet material
in accordance with claim 1, wherein Fe in the main phase alloy is partially replaced
by of 10 atomic % or less of Co and/or 3 atomic % or less of Ni.
17. A process in accordance with claim 11 for producing R-Fe-B permanent magnet material
in accordance with claim 1, wherein the adjusting alloy powder contains 5 atomic %
to 15 atomic % of R.
18. A process of producing R-Fe-B permanent magnet material characterized by the steps
of strip casting a molten main phase alloy and strip casting an adjusting alloy, placing
the cast strip of each alloy in a pressure vessel, discharging air therefrom and substituting
hydrogen in order to cause each cast alloy strip to decay by hydrogenation,
dehydrogenating the cast alloys
comminuting the cast alloys under an inert gas into powders each having a mean grain
size between 1 µm and 10µm,
blending the powders to form a mixture containing 90% or more of R
2Fe
14B of which a part of the Fe is optionally replaced by one or both of Co and Ni, and
packing the powder mixture into a mold and orienting the packed powder by momentarily
applying a pulsed magnetic field having a strength of at least 10kOe (796 kA/m),
and then molding, sintering and annealing the material, thereby to form a permanent
magnet material which has magnetic properties such that when the maximum energy product
value (BH)max is expressed in kJ/m
3, and the coercive force iHc is expressed in kA/m, the total value

and such that when the residual magnetic flux density (Br) is expressed in tenths
of one Tesla (10
-1T=1kG), the squareness of the demagnetization curve {(Br
2×1.99)/(BH)max} is between 1.01 and 1.045, wherein said main phase alloy contains:
R 11 atomic % to 15 atomic % where R represents at least one rare earth element,
B 4 atomic % to 12 atomic %,
the balance being Fe of which a part is optionally replaced by one or both of Co
and Ni, an optional additive and unavoidable impurities, so that such main phase alloy
contains an R
2Fe
14B phase as its main phase,
and said adjusting alloy contains:
R 45 atomic % or less where R again represents at least one rare earth element,
the balance being Co of which a part is optionally replaced by one or both of Fe and
Ni, an optional additive and unavoidable impurities, whereby such adjusting alloy
contains an R-Co intermetallic compound phase
and wherein the optional additive which may be added to either or both of said main
phase alloy and said adjusting alloy is of such nature and amount that said powder
blend optionally contains one or more of:
| 0 to 9.5 atomic % of Al, |
0 to 4.5 atomic % of Ti, |
0 to 9.5 atomic % of V, |
| 0 to 8.5 atomic % of Cr, |
0 to 8.0 atomic % of Mn, |
0 to 5 atomic % of Bi, |
| 0 to 12.5 atomic % of Nb, |
0 to 10.5 atomic % of Ta, |
0 to 9.5 atomic % of Mo, |
| 0 to 9.5 atomic % of W, |
0 to 2.5 atomic % of Sb, |
0 to 7 atomic % of Ge, |
| 0 to 3.5 atomic % of Sn, |
0 to 5.5 atomic % of Zr, |
and |
| 0 to 5.5 atomic % of Hf. |
|
|
19. A process of producing R-Fe-B permanent magnet material in accordance with claim 18,
wherein said main phase alloy contains:
R 12 atomic % to 14 atomic % where R represents at least one rare earth element,
B 6 atomic % to 10 atomic %.
20. A process of producing R-Fe-B permanent magnet materials in accordance with claim
18, wherein Fe in the main phase alloy containing an R2Fe14B phase as a main phase is replaced by one or both of 10 atomic % or less Co and 3
atomic % or less Ni.
21. A process of producing R-Fe-B permanent magnet materials in accordance with claim
18, wherein the adjusting alloy contains R in an amount of 10 atomic % to 20 atomic
%.
22. A process of producing R-Fe-B permanent magnet materials in accordance with claim
18, wherein part of the Co in the adjusting alloy is replaced by one or both of 50
atomic % or less Fe and/or 10 atomic % or less Ni.
23. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 11, 13 and 18, wherein the amount of adjusting alloy powder used is less than
60% of the weight of the main phase alloy powder.
24. A process of producing R-Fe-B permanent magnet materials in accordance with claim
23, wherein the amount of adjusting alloy powder used is between 0.1% and 40% of the
weight of the main phase alloy powder.
25. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 24, wherein said strip casting process is a single roll process or a double
roll process.
26. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 25, wherein the thickness of the cast strip(s) is between 0.03 mm and
10 mm.
27. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 26, wherein the cast strip has a crystal grain size which is between 0.1
µm and 50 µm in a short axial direction and between 5 µm and 200 µm in a long axial
direction, and contains an R-rich phase is finely dispersed below 5 µm.
28. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 27, wherein hydrogenation proceeds under a H2 gas pressure 200 Torr (26.6k Pa) to 50 kg/cm2 (4.9 MPa).
29. A process of producing R-Fe-B permanent magnet material in accordance with claim 28,
wherein the H2 gas pressure during hydrogenation is 2 kg/cm2 (0.2 MPa) to 10 kg/cm2 (1 MPa).
30. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 29, wherein dehydrogenation of the decayed alloy powder is carried out
at a temperature between 100°C and 750°C for 0.5 hours or longer.
31. A process of producing R-Fe-B permanent magnet material in accordance with claim 30,
wherein a dehydrogenation proceeds at a temperature between 200°C and 600°C.
32. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 31, wherein the mean grain size of the comminuted powder is between 2
µm and 4 µm.
33. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 32, wherein the mold is formed of one or more non-magnetic metals, oxides
or organic compounds such as plastics and rubber.
34. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 33, wherein the packing density of powder packed into the mold is 1.4
g/cm3 to 3.0 g/cm3.
35. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 34, wherein the powder is oriented by applying a pulse magnetic field
using an air-core coil and a capacitor power source.
36. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 35, wherein the pulse magnetic field intensity is 10 kOe (796 kA/m) or
more.
37. A process of producing R-Fe-B permanent magnet material in accordance with claim 36,
wherein the pulse magnetic field intensity is between 30 kOe and 80 kOe (2387 and
6366 kA/m).
38. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 37, wherein a single magnetic field pulse lasts between 1 µsec, and 10
sec.
39. A process of producing R-Fe-B permanent magnet material in accordance with claim 38,
wherein a single magnetic field pulse lasts between 5 µsec and 100 msec.
40. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 39, wherein a magnetic field pulse is applied from 1 to 10 times.
41. A process of producing R-Fe-B permanent magnet material in accordance with claim 40,
wherein a magnetic field pulse is applied from 1 to 5 times.
42. A process of producing R-Fe-B permanent magnet material in accordance with any of
claims 9 to 41, wherein molding after orientation is effected by a hydrostatic pressing
process.
43. A process of producing R-Fe-B permanent magnet materials in accordance with any of
claims 9 to 41, wherein molding after orientation is effected by a magnetic field
pressing process.
44. A process of producing R-Fe-B permanent magnet material in accordance with claim 42
or 43, wherein the pressure exerted during pressing is between 0.5 ton/cm2 and 5 ton/cm2 (49 MPa and 490 MPa).
45. A process of producing R-Fe-B permanent magnet materials in accordance with claim
44, wherein the pressure exerted during pressing is between 1 ton/cm2 and 3 ton/cm2 (98 MPa and 294 MPa)..
1. R-Fe-B-Permanentmagnetmaterial, dadurch gekennzeichnet, daß das Material eine im wesentlichen
homogene Zusammensetzung aufweist, die aus den Komponenten:
R: 12 At.% bis 16 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B: 4 At.% bis 8 At.%
O2: 5000 ppm oder weniger
besteht und die wahlweise einen oder mehrere Zusätze enthält, die aus den Anteilen:
| 0 bis 9,5 At.% Al, |
0 bis 4,5 At.% Ti, |
0 bis 9,5 At.% V, |
| 0 bis 8,5 At.% Cr, |
0 bis 8,0 At.% Mn, |
0 bis 5 At.% Bi, |
| 0 bis 12,5 At.% Nb, |
0 bis 10,5 At.% Ta, |
0 bis 9,5 At.% Mo, |
| 0 bis 9,5 At.% W, |
0 bis 2,5 At.% Sb, |
0 bis 7 At.% Ge, |
| 0 bis 3,5 At.% Sn, |
0 bis 5,5 At.% Zr, |
und |
| 0 bis 5,5 At.% Hf |
|
|
ausgewählt sind, wobei der Rest Fe ist, von dem ein Teil wahlweise durch Co und/oder
Ni ersetzt ist, sowie unvermeidbare Verunreinigungen,
und die 90% oder mehr einer Hauptphase aus R
2Fe
14B enthält, bei der ein Teil des Fe wahlweise durch Co und/oder Ni ersetzt ist, und
eine mittlere Korngröße von 10µm oder weniger, eine Rohdichte von 7,45 g/cm
3 oder mehr und einen Orientierungsgrad von 85% oder mehr aufweist und die solche magnetischen
Eigenschaften besitzt, daß, wenn der maximale Energieprodukt-Wert (BH)max in kJ/m
3 und die Koerzitivkraft iHc in kA/m ausgedrückt werden,
der Gesamtwert

ist
und daß, wenn die magnetische Restflußdichte Br in Zehnteln von einem Tesla (10
-1T=1kG) ausgedrückt wird, die Rechteckigkeit der Entmagnetisierungskurve {(Br
2x1,99)/(BH)max} zwischen 1,01 und 1,045 liegt.
2. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1, welches
R zu 12,5 At.% bis 14 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B zu 5,8 At.% bis 7 At.% und
O2 zu 200 ppm bis 3000 ppm enthält.
3. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem weniger
als 50% an Fe durch Co und/oder Ni ersetzt ist.
4. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem eine Hauptphase
aus R2Fe14B, bei welcher ein Teil des Fe wahlweise durch Co und/oder Ni ersetzt ist, 94% oder
mehr des Materials bildet.
5. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem ein Häufigkeitsmaximum
der Kristallkorngrößen zwischen 5µm und 6µm liegt.
6. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem der Orientierungsgrad
92% oder mehr beträgt.
7. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem, wenn
der (BH)max-Wert über 50 MGOe (398 kJ/m3) liegt, der iHc-Wert 9 kOe (716 kA/m) oder mehr beträgt.
8. R-Fe-B-Permanentmagnetmaterial nach Anspruch 1 oder Anspruch 2, bei welchem, wenn
der (BH)max-Wert über 45 MGOe (358,1 kJ/m3) liegt, der iHc-Wert 14 kOe (827 kA/m) oder mehr beträgt.
9. Verfahren zur Herstellung eines R-Fe-B-Permanentmagnetmaterials, gekennzeichnet durch
die Verfahrensschritte: Streifengießen einer geschmolzenen Legierung, bestehend aus
R: 12 At.% bis 16 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B: 4 At.% bis 8 At.%
O2: 5000 ppm oder weniger,
die wahlweise einen oder mehrere Zusätze enthält, ausgewählt aus:
| 0 bis 9,5 At.% Al, |
0 bis 4,5 At.% Ti, |
0 bis 9,5 At.% V, |
| 0 bis 8,5 At.% Cr, |
0 bis 8,0 At.% Mn, |
0 bis 5 At.% Bi, |
| 0 bis 12,5 At.% Nb, |
0 bis 10,5 At.% Ta, |
0 bis 9,5 At.% Mo, |
| 0 bis 9,5 At.% W, |
0 bis 2,5 At.% Sb, |
0 bis 7 At.% Ge, |
| 0 bis 3,5 At.% Sn, |
0 bis 5,5 At.% Zr, |
und |
| 0 bis 5,5 At.% Hf, |
|
|
wobei der Rest Fe ist, von dem ein Teil wahlweise durch Co und/oder Ni ersetzt ist,
sowie unvermeidbare Verunreinigungen;
Bilden eines Gußstreifens, der 90% oder mehr einer Hauptphase aus R
2Fe
14B enthält, bei der ein Teil des Fe wahlweise durch Co und/oder Ni ersetzt ist;
Einbringen des Gußstreifens in ein Druckgefäß;
Entfernen der Luft aus dem Druckgefäß und ihr Ersetzen durch Wasserstoff um zu bewirken,
daß der Gußstreifen aufgrund von Hydrierung zerfällt;
Dehydrieren des Gußstreifens;
Zerkleinern des Gußstreifens in einem inerten Gas zu einem Pulver mit einer mittleren
Korngröße zwischen 1µm und 10µm;
Einpacken des Pulvers in eine Form und Orientieren des eingepackten Pulvers durch
kurzzeitiges Anlegen eines gepulsten Magnetfeldes mit einer Stärke von mindestens
10kOe (796 kA/m) und dann Formen, Sintern und Glühen des Materials zur Bildung eines
Permanentmagnetmaterials, welches solche magnetischen Eigenschaften besitzt, daß,
wenn der maximale Energieprodukt-Wert (BH)max in kJ/m
3 und die Koerzitivkraft iHc in kA/m ausgedrückt werden, der Gesamtwert

ist
und daß, wenn die magnetische Restflußdichte (Br) in Zehnteln von einem Tesla (10
-1T=1kG) ausgedrückt wird, die Rechteckigkeit der Entmagnetisierungskurve {(Br
2x1,99)/(BH)max} zwischen 1,01 und 1,045 liegt.
10. Verfahren zur Herstellung eines R-Fe-B-Permanentmagnetmaterials nach Anspruch 9, bei
welchem die geschmolzene Legierung
R zu 12,5 At.% bis 14 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B zu 5,8 At.% bis 7 At.%,
O2 zu 200 ppm bis 3000 ppm enthält.
11. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial, gekennzeichnet durch
die Verfahrensschritte:
Streifengießen einer geschmolzenen Hauptphasen-Legierung und Streifengießen einer
Einstell-Legierung;
Einbringen des Gußstreifens jeder Legierung in ein Druckgefäß;
Entfernen der Luft aus dem Druckgefäß und ihr Ersetzen durch Wasserstoff um zu bewirken,
daß jeder Gußlegierungsstreifen aufgrund von Hydrierung zerfällt;
Dehydrieren der Gußlegierungen;
Zerkleinern der Gußlegierungen in einem inerten Gas zu Pulvern, von denen jedes eine
mittlere Korngröße zwischen 1µm und 10µm aufweist;
Mischen der Pulver zur Bildung eines Gemisches, das 90% oder mehr an R
2Fe
14B enthält, bei welchem ein Teil des Fe wahlweise durch Co und/oder Ni ersetzt ist;
Einpacken des Pulvergemisches in eine Form und Orientieren des eingepackten Pulvers
durch kurzzeitiges Anlegen eines gepulsten Magnetfeldes mit einer Stärke von mindestens
10kOe (796kA/m); und dann
Formen, Sintern und Glühen des Materials zur Bildung eines Permanentmagnetmaterials,
welches solche magnetische Eigenschaften besitzt, daß, wenn der maximale Energieprodukt-Wert
(BH)max in kJ/m
3 und die Koerzitivkraft iHc in kA/m ausgedrückt werden, der Gesamtwert

ist
und daß, wenn die magnetische Restflußdichte (Br) in Zehnteln von einem Tesla (10
-1T=1kG) ausgedrückt wird, die Rechteckigkeit der Entmagnetisierungskurve {(Br2xl,99)/(BH)max}
{(Br
2/4)/(BH)max} zwischen 1,01 und 1,045 liegt; wobei die besagte Hauptphasen-Legierung
R zu 11 At.% bis 20 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B zu 4 At.% bis 12 At.% enthält, und die besagte Einstellegierung
R zu 20 At.% oder weniger, wobei R wiederum mindestens ein Seltenerdelement darstellt,
enthält,und wobei die Gleichgewichte der besagten Hauptphasen-Legierung und der besagten
Einstell-Legierung so eingestellt sind, daß das besagte Pulvergemisch wahlweise einen
oder mehrere Zusätze enthält, die aus:
| 0 bis 9,5 At.% Al, |
0 bis 4,5 At.% Ti, |
0 bis 9,5 At.% V, |
| 0 bis 8,5 At.% Cr, |
0 bis 8,0 At.% Mn, |
0 bis 5 At.% Bi |
| 0 bis 12,5 At.% Nb, |
0 bis 10,5 At.% Ta, |
0 bis 9,5 At.% Mo |
| 0 bis 9,5 At.% W, |
0 bis 2,5 At.% Sb, |
0 bis 7 At.% Ge |
| 0 bis 3,5 At.% Sn, |
0 bis 5,5 At.% Zr, |
und |
| 0 bis 5,5 At.% Hf, |
|
|
ausgewählt sind und der Rest des besagten Pulvergemisches Fe ist, von dem ein Teil
wahlweise durch Co und/oder Ni ersetzt ist, sowie unvermeidbare Verunreinigungen.
12. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 11, bei
welchem die Hauptphase der geschmolzenen Legierung 13 At.% bis 16 At.% R und 6 At.%
bis 10 At.% B enthält.
13. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 11, bei
welchem die besagte Einstell-Legierung 20 At.% oder weniger R und 6 At.% oder weniger
B enthält.
14. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 13,
bei welchem die besagte Einstell-Legierung 5 At.% bis 15 At.% R enthält.
15. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach den Ansprüchen
11 und 13, bei welchem die besagte Hauptphase
R zu 13 At.% bis 16 At.% und
B zu 6 At.% bis 10 At.%
enthält.
16. Verfahren nach Anspruch 11 zur Herstellung von R-Fe-B-Permanentmagnetmaterial gemäß
Anspruch 1, bei welchem Fe in der Hauptphase teilweise durch 10 At.% oder weniger
an Co und/oder 3 At.% oder weniger an Ni ersetzt ist.
17. Verfahren nach Anspruch 11 zur Herstellung von R-Fe-B-Permanentmagnetmaterial gemäß
Anspruch 1, bei welchem das Einstell-Legierungspulver 5 At.% bis 15 At.% R enthält.
18. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial gekennzeichnet durch
die Verfahrensschritte:
Streifengießen einer geschmolzenen Hauptphasen-Legierung und Streifengießen einer
Einstell-Legierung;
Einbringen des Gußstreifens jeder Legierung in ein Druckgefäß;
Entfernen der Luft aus dem Druckgefäß und ihrer Ersetzung durch Wasserstoff, um zu
bewirken, daß jeder Gußlegierungsstreifen aufgrund von Hydrierung zerfällt;
Dehydrieren der Gußlegierungen;
Zerkleinern der Gußlegierungen in einem inerten Gas zu Pulvern, von denen jedes eine
mittlere Korngröße zwischen 1µm und 10µm aufweist;
Mischen der Pulver zur Bildung eines Gemisches, das 90% oder mehr an R
2Fe
14B enthält, bei welchem ein Teil des Fe wahlweise durch Co und/oder Ni ersetzt ist;
Einpacken des Pulvergemisches in eine Form und Orientieren des eingepackten Pulvers
durch kurzzeitiges Anlegen eines gepulsten Magnetfeldes mit einer Stärke von mindestens
10kOe (796kA/m); und dann
Formen, Sintern und Glühen des Materials zur Bildung eines Permanentmagnetmaterials,
welches solche magnetischen Eigenschaften besitzt, daß, wenn der maximale Energieprodukt-Wert
(BH)max in kJ/m
3 und die Koerzitivkraft iHc in kA/m ausgedrückt werden, der Gesamtwert

ist
und daß, wenn die magnetische Restflußdichte (Br) in Zehnteln von einem Tesla (10
-1T=1kG) ausgedrückt wird, die Rechteckigkeit der Entmagnetisierungskurve {(Br
2x1,99) /(BH)max} zwischen 1,01 und 1,045 liegt;
wobei die besagte Hauptphasen-Legierung
R zu 11 At.% bis 15 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B zu 4 At.% bis 12 At.%
und als Rest Fe, von dem ein Teil wahlweise durch Co und/oder Ni ersetzt ist, enthält,
sowie wahlweise einen Zusatz und unvermeidbare Verunreinigungen derart, daß diese
Hauptphasen-Legierung eine R
2Fe
14B-Phase als ihre Hauptphase enthält; und
die besagte Einstell-Legierung
R zu 45 At.% oder weniger, wobei R wiederum mindestens ein Seltenerdelement darstellt,
und als Rest Co, von dem wahlweise ein Teil durch Fe und/oder Ni ersetzt ist, und
wahlweise einen Zusatz und unvermeidbare Verunreinigungen enthält,
wobei diese Einstell-Legierung eine R-Co-intermetallische Verbindungsphase enthält
und wobei der wahlweise Zusatz, welcher der besagten Hauptphasen-Legierung und/oder
der besagten Einstell-Legierung zugesetzt werden kann, eine solche Art und einen solchen
Anteil aufweist, daß das Pulvergemisch wahlweise ein oder mehrere Zusätze enthält,
die aus:
| 0 bis 9,5 At.% Al, |
0 bis 4,5 At.% Ti, |
0 bis 9,5 At.% V, |
| 0 bis 8,5 At.% Cr, |
0 bis 8,0 At.% Mn, |
0 bis 5 At.% Bi |
| 0 bis 12,5 At.% Nb, |
0 bis 10,5 At.% Ta, |
0 bis 9,5 At.% Mo |
| 0 bis 9,5 At.% W, |
0 bis 2,5 At.% Sb, |
0 bis 7 At.% Ge |
| 0 bis 3,5 At.% Sn, |
0 bis 5,5 At.% Zr, |
und |
| 0 bis 5,5 At.% Hf, |
|
|
ausgewählt sind.
19. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 18, bei
welchem die besagte Hauptphase
R zu 12 At.% bis 14 At.%, wobei R mindestens ein Seltenerdelement darstellt,
B zu 6 At.% bis 10 At.%
enthält.
20. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 18,
bei welchem in der Hauptphasen-Legierung, die eine R2Fe14B-Phase als Hauptphase enthält, Fe durch 10 At.% oder weniger Co und/oder 3 At.% oder
weniger Ni ersetzt ist.
21. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 18,
bei welchem die Einstell-Legierung einen Anteil von 10 At.% bis 20 At.% R enthält.
22. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 18,
bei welchem in der Einstell-Legierung ein Teil des Co durch 50 At.% oder weniger Fe
und/oder 10 At.% oder weniger Ni ersetzt ist.
23. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
11, 13 und 18, bei welchem der Anteil des verwendeten Einstell-Legierungspulvers weniger
als 60% des Gewichts des Hauptphasen-Legierungspulvers beträgt.
24. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 23,
bei welchem der Anteil des verwendeten Einstell-Legierungspulvers zwischen 0,1% und
40% des Gewichts des Hauptphasen-Legierungspulvers liegt.
25. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 24, bei welchem das besagte Streifengußverfahren ein Einfachwalzverfahren oder
ein Doppelwalzverfahren ist.
26. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 25, bei welchem die Dicke der Gußstreifen zwischen 0,03 mm und 10 mm liegt.
27. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 26, bei welchem der Gußstreifen eine Kristallkorngröße aufweist, die in Richtung
einer kurzen Achse zwischen 0,1µm und 50µm und in Richtung einer langen Achse zwischen
5µm und 200µm liegt und eine R-reiche Phase enthält, die eine Feinverteilung unterhalb
5µm aufweist.
28. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 27, bei welcher die Hydrierung unter einem H2-Gasdruck von 200 Torr (26,6kPa) bis 50kg/cm2 (4,9 MPa) stattfindet.
29. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial, bei welchem der H2-Gasdruck während der Hydrierung 2 kg/cm2 (0,2 MPa) bis 10 kg/cm2 (1 MPa) beträgt.
30. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 29, bei welchem die Dehydrierung des zerfallenen Legierungspulvers bei einer
Temperatur zwischen 100°C und 750°C 0,5 Stunden lang oder länger durchgeführt wird.
31. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 30, bei
welchem eine Dehydrierung bei einer Temperatur zwischen 200°C und 600°C durchgeführt
wird.
32. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 31, bei welchem die mittlere Korngröße des zerkleinerten Pulvers zwischen 2µm
und 4µm liegt.
33. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 32, bei welchem die Form aus einem oder mehreren nichtmagnetischen Metallen,
Oxiden oder organischen Verbindungen wie Kunststoffen oder Gummi gebildet wird.
34. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 33, bei welchem die Packungsdichte des in die Form eingepackten Pulvers 1,4
g/cm3 bis 3,0 g/cm3 beträgt.
35. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 34, bei welchem das Pulver durch Anlegen eines gepulsten Magnetfeldes unter
Verwendung einer Luftkern-Spule und einer kapazitiven Stromquelle orientiert wird.
36. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 35, bei welchem die Intensität des gepulsten Magnetfeldes 10 kOe (796 kA/m)
oder mehr beträgt.
37. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 36, bei
welchem die Intensität des gepulsten Magnetfeldes zwischen 30 kOe und 80 kOe (2387
und 6366 kA/m) liegt.
38. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 37, bei welchem ein einzelner Impuls des Magnetfeldes zwischen 1 µsec und 10
sec dauert.
39. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 38, bei
welchem ein einzelner Impuls des Magnetfeldes zwischen 5 µsec und 100 msec dauert.
40. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 39, bei welchem ein Magnetfeldimpuls 1 bis 10 mal angelegt wird.
41. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach Anspruch 40, bei
welchem ein Magnetfeldimpuls 1 bis 5 mal angelegt wird.
42. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach einem der Ansprüche
9 bis 41, bei welchem das Formen nach dem Orientieren durch ein hydrostatisches Preßverfahren
bewirkt wird.
43. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach einem der Ansprüche
9 bis 41, bei welchem das Formen nach dem Orientieren durch ein Magnetfeld-Preßverfahren
bewirkt wird.
44. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterial nach den Ansprüchen 42
oder 43, bei welchem der während des Pressens ausgeübte Druck zwischen 0,5 t/cm2 und 5 t/cm2 (49 MPa und 490 MPa) liegt.
45. Verfahren zur Herstellung von R-Fe-B-Permanentmagnetmaterialien nach Anspruch 44,
bei welchem der während des Pressens ausgeübte Druck zwischen 1 t/cm2 und 3 t/cm2 (98 MPa und 294 MPa) liegt.
1. Un matériau pour aimants permanents de type R-Fe-B caractérisé en ce qu'il présente
une composition sensiblement homogène constituée de
R 12 à 16 % atomiques, R représentant au moins un élément des terres rares,
B 4 à 8 % atomiques,
O2 5000 ppm ou moins,
et contient facultativement un ou plusieurs additifs choisis parmi :
0 à 9,5 % atomiques d'Al, 0 à 4,5 % atomiques de Ti, 0 à 9,5 % atomiques de V, 0 à
8,5 % atomiques de Cr, 0 à 8,0 % atomiques de Mn, 0 à 5 % atomiques de Bi, 0 à 12,5
% atomiques de Nb, 0 à 10,5 % atomiques de Ta, 0 à 9,5 % atomiques de Mo, 0 à 9,5
% atomiques de W, 0 à 2,5 % atomiques de Sb, 0 à 7 % atomiques de Ge, 0 à 3,5 % atomiques
de Sn, 0 à 5,5 % atomiques de Zr et 0 à 5,5 % atomiques de Hf,
le complément étant formé de Fe dont une partie est facultativement remplacée par
du cobalt et/ou par du nickel, et des impuretés inévitables,
et qui renferme 90 % ou plus d'une phase principale de R
2Fe
14B dont une partie du fer est facultativement remplacée par du cobalt et/ou du nickel,
et qui présente une grosseur de grain de 10 µm ou moins, une masse volumique apparente
de 7,45 g/cm
3 ou plus, un degré d'orientation de 85 % ou plus, et qui a des propriétés magnétiques
telles que, lorsque la valeur du produit d'énergie maximum (BH)
max est exprimée en kJ/m
3 et le champ coercitif iHc en kA/m, on ait (BH)
max/7,96+iHc/79,6 ≥ 59, et que, lorsque la densité de flux magnétique résiduelle Br est
exprimée en dixièmes de tesla (10
-1T = 1 kG), la rectangularité de la courbe de désaimantation, Br
2x1,99/(BH)
max, soit comprise entre 1,01 et 1,045.
2. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1, contenant
:
R 12,5 à 14 % atomiques, R représentant au moins un élément des terres rares,
B 5,8 à 7 % atomiques,
O2 200 à 3000 ppm.
3. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel moins de 50 % du fer sont remplacés par du cobalt et/ou
du nickel.
4. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel la phase principale de R2Fe14B dont une partie du fer est facultativement remplacée par du cobalt et/ou du nickel
constitue 94 % ou plus du matériau.
5. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel la fréquence maximum des grosseurs de grain cristallin
est celle des grosseurs comprises entre 5 et 6 µm.
6. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel le degré d'orientation est de 92 % ou plus.
7. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel la valeur de (BH)max est supérieure à 50 MG.Oe (398 kJ/m3) et la valeur de iHc est de 9 kOe (716 kA/m) ou plus.
8. Un matériau pour aimants permanents de type R-Fe-B selon la revendication 1 ou la
revendication 2, dans lequel la valeur de (BH)max, est supérieure à 45 MG.Oe (358 kJ/m3) et la valeur de iHc est de 14 kOe (1114 kA/m) ou plus.
9. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B caractérisé
par les opérations consistant: à couler en bande un alliage fondu composé de
R 12 à 16 % atomiques, R représentant au moins un élément des terres rares,
B 4 à 8 % atomiques,
O2 5000 ppm ou moins,
et qui contient facultativement un ou plusieurs éléments choisis parmi :
0 à 9,5 % atomiques d'Al, 0 à 4,5 % atomiques de Ti, 0 à 9,5 % atomiques de V, 0 à
8,5 % atomiques de Cr, 0 à 8,0 % atomiques de Mn, 0 à 5 % atomiques de Bi, 0 à 12,5
% atomiques de Nb, 0 à 10,5 % atomiques de Ta, 0 à 9,5 % atomiques de Mo, 0 à 9,5
% atomiques de W, 0 à 2,5 % atomiques de Sb, 0 à 7 % atomiques de Ge, 0 à 3,5 % atomiques
de Sn, 0 à 5,5 % atomiques de Zr et 0 à 5,5 % atomiques de Hf,
le complément étant formé de Fe dont une partie est facultativement remplacée par
du cobalt et/ou par du nickel, et des impuretés inévitables, pour former une bande
coulée renfermant 90 % ou plus d'une phase principale de R
2Fe
14B dont une partie du fer est facultativement remplacée par du cobalt et/ou du nickel,
à placer la bande coulée dans une enceinte tenant la pression, à en évacuer l'air
et à y substituer de l'hydrogène pour provoquer une décomposition de la bande coulée
par hydrogénation,
à déshydrogéner la bande coulée,
à broyer la bande coulée sous un gaz inerte en une poudre ayant une grosseur de grain
moyenne comprise entre 1 et 10 µm,
à comprimer la poudre dans un moule et à orienter la poudre comprimée par application
momentanée d'un champ magnétique pulsé ayant une intensité d'au moins 10 kOe (796
kA/m),
puis à mouler, fritter et recuire le matériau, pour former ainsi un matériau pour
aimants permanents qui a des propriétés magnétiques telles que, lorsque la valeur
du produit d'énergie maximum (BH)
max est exprimée en kJ/m
3 et que le champ coercitif iHc est exprimé en kA/m, on ait (BH)
max/7,96+iHc/79,6 ≥ 59,
et que, lorsque la densité de flux magnétique résiduelle (Br) est exprimée en dixièmes
de tesla (10
-1T = 1kG), la rectangularité de la courbe de désaimantation, {Br
2x1,99/(BH)
max}, soit comprise entre 1,01 et 1,045.
10. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 9, dans lequel l'alliage fondu contient :
R 12,5 à 14 % atomiques, R représentant au moins un élément des terres rares,
B 5,8 à 7 % atomiques,
O2 200 à 3000 ppm.
11. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B, caractérisé
par les opérations consistant à couler en bande un alliage de phase principale fondu
et à couler en bande un alliage d'ajustement, à placer la bande coulée de chaque alliage
dans une enceinte tenant la pression, à en évacuer l'air et à y substituer de l'hydrogène
pour provoquer une décomposition par hydrogénation de chaque bande d'alliage coulé,
à déshydrogéner les alliages coulés
à broyer les alliages coulés sous un gaz inerte en des poudres ayant chacune une grosseur
de grain moyenne comprise entre 1 et 10 µm,
à mélanger les poudres pour former un mélange renfermant 90 % ou plus de R
2Fe
14B dont une partie du fer est facultativement remplacée par du cobalt et/ou du nickel,
et à comprimer le mélange de poudres dans un moule et à orienter la poudre comprimée
par application momentanée d'un champ magnétique pulsé ayant une intensité d'au moins
10 kOe (796 kA/m),
puis à mouler, à fritter et à recuire le matériau, pour former ainsi un matériau pour
aimants permanents qui a des propriétés magnétiques telles que, lorsque la valeur
du produit d'énergie maximum (BH)
max est exprimée en kJ/m
3 et que le champ coercitif iHc est exprimé en kA/m, on ait (BH)
max/7,96+iHc/79,6 ≥ 59,
et que, lorsque la densité de flux magnétique résiduelle (Br) est exprimée en dixièmes
de tesla (10
-1T = 1 kG), la rectangularité de la courbe de désaimantation, {Br
2x1,99/(BH)
max} {(Br
2/4)/(BH)
max}, soit comprise entre 1,01 et 1,045, ledit alliage de phase principale contenant
:
R 11 à 20 % atomiques, R représentant au moins un élément des terres rares,
B 4 à 12 % atomiques,
et ledit alliage d'ajustement contenant :
R 20 % atomiques ou moins, R représentant ici encore au moins un élément des terres
rares,
et les compléments à 100 % dudit alliage de phase principale et dudit alliage d'ajustement
étant dosés en sorte que ledit mélange de poudres renferme facultativement un ou plusieurs
des composants suivants :
0 à 9,5 % atomiques d'Al, 0 à 4,5 % atomiques de Ti, 0 à 9,5 % atomiques de V, 0 à
8,5 % atomiques de Cr, 0 à 8,0 % atomiques de Mn, 0 à 5 % atomiques de Bi, 0 à 12,5
% atomiques de Nb, 0 à 10,5 % atomiques de Ta, 0 à 9,5 % atomiques de Mo, 0 à 9,5
% atomiques de W, 0 à 2,5 % atomiques de Sb, 0 à 7 % atomiques de Ge, 0 à 3,5 % atomiques
de Sn, 0 à 5,5 % atomiques de Zr et 0 à 5,5 % atomiques de Hf,
et que le complément à 100 % dudit mélange de poudres soit formé de Fe dont une partie
est facultativement remplacée par du cobalt et/ou par du nickel, et des impuretés
inévitables.
12. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 11, dans lequel l'alliage fondu de phase principale renferme 13 à
16 % atomiques de R et 6 à 10 % atomiques de B.
13. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 11, dans lequel ledit alliage d'ajustement renferme 20 % atomiques
ou moins de R et 6 % atomiques ou moins de B.
14. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 13, dans lequel ledit alliage d'ajustement renferme 5 à 15 % atomiques
de R.
15. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 11 et la revendication 13, dans lequel ledit alliage de phase principale
renferme 13 à 16 % atomiques de R et 6 à 10 % atomiques de B.
16. Un procédé selon la revendication 11 pour la production d'un matériau pour aimants
permanents de type R-Fe-B selon la revendication 1, dans lequel le fer de l'alliage
de phase principale est partiellement remplacé par 10 % atomiques ou moins de cobalt
et/ou 3 % atomiques ou moins de nickel.
17. Un procédé selon la revendication 11 pour la production d'un matériau pour aimants
permanents de type R-Fe-B selon la revendication 1, dans lequel la poudre d'alliage
d'ajustement contient 5 à 15 % atomiques de R.
18. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B, caractérisé
par les opérations consistant à couler en bande un alliage de phase principale fondu
et à couler en bande un alliage d'ajustement, à placer la bande coulée de chaque alliage
dans une enceinte tenant la pression, à en évacuer l'air et à y substituer de l'hydrogène
pour provoquer une décomposition par hydrogénation de chaque bande d'alliage coulé,
à déshydrogéner les alliages coulés,
à broyer les alliages coulés sous un gaz inerte en des poudres ayant chacune une grosseur
de grain moyenne comprise entre 1 et 10 µm,
à mélanger les poudres pour former un mélange renfermant 90 % ou plus de R
2Fe
14B dont une partie du fer est facultativement remplacée par du cobalt et/ou du nickel,
et à comprimer le mélange de poudres dans un moule et à orienter la poudre comprimée
par application momentanée d'un champ magnétique pulsé ayant une intensité d'au moins
10 kOe (796 kA/m),
puis à mouler, fritter et recuire le matériau, pour former ainsi un matériau pour
aimants permanents qui a des propriétés magnétiques telles que, lorsque la valeur
du produit d'énergie maximum (BH)
max est exprimée en kJ/m
3 et que le champ coercitif iHc est exprimé en kA/m, on ait (BH)
max/7,96+iHc/79,6 ≥ 59,
et que, lorsque la densité de flux magnétique résiduelle (Br) est exprimée en dixièmes
de tesla (10
-1T = 1kG), la rectangularité de la courbe de désaimantation, Br
2x1,99/(BH)
max, soit comprise entre 1,01 et 1,045, ledit alliage de phase principale contenant :
R 11 à 15 % atomiques, R représentant au moins un élément des terres rares,
B 4 à 12 % atomiques,
le complément étant formé de fer dont une partie est facultativement remplacée par
du cobalt et/ou par du nickel, d'un additif facultatif et des impuretés inévitables,
de sorte que ledit alliage de phase principale renferme une phase de R
2Fe
14B en tant que phase principale,
et ledit alliage d'ajustement contenant :
R 45 % atomiques ou moins, R représentant ici encore au moins un élément des terres
rares,
le complément étant formé de cobalt dont une partie est facultativement remplacée
par du fer et/ou du nickel, d'un additif facultatif et des impuretés inévitables,
de sorte que ledit alliage d'ajustement renferme une phase de composé intermétallique
R-Co,
et l'additif facultatif susceptible d'être ajouté à l'un et/ou l'autre desdits alliages
de phase principale et d'ajustement étant de nature et d'abondance telles que ledit
mélange de poudres contienne l'un ou plusieurs des composants suivants : 0 à 9,5 %
atomiques d'Al, 0 à 4,5 % atomiques de Ti, 0 à 9,5 % atomiques de V, 0 à 8,5 % atomiques
de Cr, 0 à 8,0 % atomiques de Mn, 0 à 5 % atomiques de Bi, 0 à 12,5 % atomiques de
Nb, 0 à 10,5 % atomiques de Ta, 0 à 9,5 % atomiques de Mo, 0 à 9,5 % atomiques de
W, 0 à 2,5 % atomiques de Sb, 0 à 7 % atomiques de Ge, 0 à 3,5 % atomiques de Sn,
0 à 5,5 % atomiques de Zr et 0 à 5,5 % atomiques de Hf.
19. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 18, dans lequel ledit alliage de phase principale contient :
R 12 à 14 % atomiques, R représentant au moins un élément des terres rares,
B 6 à 10 % atomiques.
20. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 18, dans lequel du fer de l'alliage de phase principale contenant
une phase de R2Fe14B en tant que phase principale est remplacé par 10 % atomiques ou moins de cobalt
et/ou 3 % atomiques ou moins de nickel.
21. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 18, dans lequel l'alliage d'ajustement contient R en une proportion
de 10 à 20 % atomiques.
22. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 18, dans lequel une partie du cobalt de l'alliage d'ajustement est
remplacée par 50 % atomiques ou moins de fer et/ou 10% atomiques ou moins de nickel.
23. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 11, 13 et 18, dans lequel la quantité de poudre
d'alliage d'ajustement utilisée est inférieure à 60 % du poids de la poudre d'alliage
de phase principale.
24. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 23, dans lequel la quantité de poudre d'alliage d'ajustement utilisée
est comprise entre 0,1 et 40 % du poids de la poudre d'alliage de phase principale.
25. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 24, dans lequel ledit processus de coulage
en bande est un processus à cylindre unique ou un processus à double cylindre.
26. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 25, dans lequel l'épaisseur de la ou des bandes
coulées est comprise entre 0,03 et 10 mm.
27. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 26, dans lequel la bande coulée présente une
grosseur de grains cristallins comprise entre 0,1 et 50 µm dans une direction de petit
axe et entre 5 et 200 µm dans une direction de grand axe, et renferme une phase riche
en R finement divisée de granulométrie inférieure à 5 µm.
28. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 27, dans lequel l'hydrogénation a lieu sous
une pression gazeuse d'hydrogène de 200 torr (26,6 kPa) à 50 kg/cm2 (4,9 MPa).
29. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendications 28, dans lequel la pression gazeuse d'hydrogène pendant l'hydrogénation
est de 2 kg/cm2 (0,2 MPa) à 10 kg/cm2 (1 MPa).
30. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 29, dans lequel la déshydrogénation de la
poudre d'alliage décomposée est opérée à une température comprise entre 100 et 750°C
pendant 0,5 heure ou plus.
31. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 30, dans lequel une déshydrogénation se déroule à une température
comprise entre 200 et 600°C.
32. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 31, dans lequel la grosseur de grain moyenne
de la poudre broyée est comprise entre 2 et 4 µm.
33. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 32, dans lequel le moule est formé d'un ou
plusieurs métaux, oxydes ou composés organiques non magnétiques tels que des matières
plastiques et du caoutchouc.
34. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 33, dans lequel la masse volumique à l'état
comprimé de la poudre comprimée dans le moule est de 1,4 à 3,0 g/cm3.
35. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 34, dans lequel la poudre est orientée par
application d'un champ magnétique pulsé au moyen d'une bobine sans fer et d'une source
d'énergie à condensateur.
36. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 35, dans lequel l'intensité du champ magnétique
pulsé est de 10 kOe (796 kA/m) ou plus.
37. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendication 36, dans lequel l'intensité du champ magnétique pulsé est comprise
ente 30 et 80 kOe (2387 et 6366 kA/m).
38. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 37, dans lequel une impulsion de champ magnétique
unique dure entre 1 microseconde et 10 secondes.
39. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendications 38, dans lequel une impulsion de champ magnétique unique dure entre
5 µs et 100 ms.
40. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 39, dans lequel une impulsion de champ magnétique
est appliquée 1 à 10 fois.
41. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
la revendications 40, dans lequel une impulsion de champ magnétique est appliquée
1 à 5 fois.
42. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 41, dans lequel le moulage opéré après orientation
est effectué par un processus de compression hydrostatique.
43. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 9 à 41, dans lequel le moulage opéré après orientation
est effectué par un processus de compression par champ magnétique.
44. Un procédé de production d'un matériau pour aimants permanents de type R-Fe-B selon
l'une quelconque des revendications 42 et 43, dans lequel la pression exercée lors
de la compression est comprise entre 0,5 t/cm2 (49 MPa) et 5 t/cm2 (490 MPa).
45. Un procédé de production de matériaux pour aimants permanents de type R-Fe-B selon
la revendication 44, dans lequel la pression exercée lors de la compression est comprise
entre 1 t/cm2 (98 MPa) et 3 t/cm2 (294 MPa).