BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to a magnesium alloy having both high strength and
high ductility; and a production process thereof.
Description of the Related Art
[0002] Since magnesium is lighter in weight than iron or aluminum, its use as a light-weight
substitute for members made of an iron steel material or aluminum alloy material is
under investigation. Ordinary magnesium alloys have, however, lower strength than
the other metal structure materials such as iron steel, aluminum alloy and titanium
alloy. An AZ91 material for die casting, which is said to have relatively high strength,
has strength as low as 160 MPa. In addition, industrial parts are required to have,
at a moving part thereof, a percent elongation of at least 4 to 5%, but ordinary magnesium
alloys do not have sufficient ductility. Even the above-described AZ91 material has
a percent elongation of only about 3%.
[0003] A variety of magnesium alloys equipped with both high strength and high ductility
have so far been proposed.
[0004] For example, known is a magnesium alloy having a composition represented by the formula:
Mg
100-
a-b-cCa
aZn
bX
c (wherein, X represents one or more than one elements selected from the group consisting
of Y, Ce, La, Nd, Pr, Sm and Mm (misch metal); and 0.5 ≤ a ≤5 atomic %, 0 < b ≤ 5
atomic %, and 0 < c ≤ 3 atomic % with the proviso that 1 ≤ a+b+c ≤ 11 atomic %), and
having a structure in which one or more of Mg-Ca, Mg-Zn and Mg-X intermetallic compounds
have been finely dispersed in a Mg mother phase composed of a fine crystalline material.
The above-described magnesium alloy having intermetallic compound(s) can be obtained
as a high strength magnesium alloy in the powder form by rapid solidification of a
molten alloy having the above-described composition by atomization or the like method.
It can be molded or formed into even complex shaped products by hot plastic processing
(refer to Japanese Patent Laid-Open No. 41065/1997).
[0005] Also known is a magnesium alloy having a composition represented by the formula:
Mg
100-a-bLn
aM
b (wherein, M is one or more elements selected from Al and Zn; Ln is one or more elements
selected from Y, Ce, La, Nd, Pr, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb, Lu and Mm
(misch metal), or a mixture of rare earth elements; and 0.5 ≤a ≤ 5 atomic %, and 0.2
≤ b ≤ 4 atomic %, with the proviso that 1.5 ≤ a+b ≤ 7 atomic %); having a crystal
grain size less than 2,000 nm; and having a long period hexagonal structure in a part
or whole region of the crystals. The above-described magnesium alloy having a long
period hexagonal structure can be prepared as a high strength and high ductility magnesium
alloy in the powder form by rapid solidification of a molten alloy having the above-described
composition by atomization or the like method. By subjecting the resulting powder
to plastic processing at an extrusion ratio of from 3 to 20, extrusion goods made
of the magnesium alloy can be obtained (refer to Japanese Patent Laid-Open No. 2002-256370).
[0006] The above-described magnesium alloys however have a drawback: a yield at the time
of rapid solidification of the molten alloy is low, which inevitably leads to a cost
rise when the powder obtained by rapid solidification is molded or formed.
[0007] The above-described magnesium alloys each has a percent elongation not greater than
5%, which is almost a limit value when they are used for moving portions of industrial
parts. Thus, they do not have sufficient ductility. The industrial parts using the
above-described magnesium alloys therefore have a drawback: design freedom is greatly
limited and they are not suited for practical use.
[0008] The magnesium alloy having a long period hexagonal structure, on the other hand,
is said so that it could be formed into a molded product by casting using a copper
mold with a large cooling rate. When the copper mold is used, however, molded products
thus obtained must be relatively small in order to raise its cooling rate. Thus, this
magnesium alloy has a drawback that any size of a molded product cannot be produced
freely.
SUMMARY OF THE INVENTION
[0009] An object of the present invention is to overcome the above-described drawbacks and
provide a magnesium alloy which is inexpensive, has a good yield, can be molded or
formed into any size, and has both high strength and high ductility; and a production
method of the magnesium alloy.
[0010] With a view to attaining the above-described object, the magnesium alloy of the present
invention comprises from 1 to 4 atomic % of Zn and from 1 to 4.5 atomic % of Y, each
based on the total amount, at a Zn/Y composition ratio falling within a range of from
0.6 to 1.3, and further comprises Mg
3Y
2Zn
3 which is an intermetallic compound and Mg
12YZn having a long period structure.
[0011] Since the magnesium alloy according to the present invention has, as well as the
above-described composition, both the intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure, it is able to have both high strength and high
ductility. Either one of or both of strength and ductility become insufficient when
the content of Zn is less than 1 atomic % or exceeds 4 atomic % and that of Y is less
than 1 atomic % or exceeds 4.5 atomic %, based on the total amount of the magnesium
alloy.
[0012] Even if Zn and Y both satisfy the above-described ranges based on the total amount
of the magnesium alloy, either one or both of strength and ductility becomes insufficient
when the magnesium alloy is free of either one or both of the intermetallic compound
Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure.
[0013] In addition, the magnesium alloy of the present invention is required to satisfy
the Zn/Y composition ratio which falls within a range of from 0.6 to 1.3 in order
to incorporate both the intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure in the alloy without failure. When the Zn/Y composition
ratio is less than 0.6 or exceeds 1.3, the magnesium alloy does not always contain
either one or both of the intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure.
[0014] It is known in a rapidly solidified Mg-Zn-Y alloy that an alloy of MgZ
nY
x (X=2 to 4) in which the concentration of Y > the concentration of Zn has an increased
long period structure as the concentration of Y becomes greater; in the case of an
alloy of MgZn
xY (X=2 to 4) in which the concentration of Zn > the concentration of Y, heat treatment
of it causes precipitation of the intermetallic compound Mg
3Y
zZn
3; and an alloy of MgZn
xY
x (X=1 to 4) in which the concentration of Y = the concentration of Zn, that is, an
equiatomic alloy is heat treated to generate the long period structure (refer to:
Masayuki Nagano, Minoru Nishida, and Yoshihito Kawamura, "Influences of concentrations
of Zn and Y and heat treatment on the structure formation of rapidly solidified Mg-Zn-Y
alloy",
Collected Abstracts of the 2003 meeting of the Japan Institute of Metals, The Japan Institute of Metals, p187).
[0015] According to the investigation by the present inventors, however, no intermetallic
compound Mg
3Y
2Zn
3 exists in each of the alloy in which the concentration of Y > the concentration of
Z and the equiatomic alloy in which the concentration of Y = the concentration of
Zn, while no long period structure exists in the alloy in which the concentration
of Zn > the concentration of Y. Accordingly, the long period structure and intermetallic
compound Mg
3Y
2Zn
3 do not exist simultaneously in the rapidly solidified Mg-Zn-Y alloy.
[0016] The magnesium alloy of the present invention preferably contains from 2 to 3.5 atomic
% of Zn and from 2 to 4.5 atomic % of Y, each based on the total amount, at a Zn/Y
composition ratio falling within a range of from 0.8 to 1.2, in order to have both
higher strength and higher ductility.
[0017] The magnesium alloy of the present invention may contain from 1 to 4 atomic % of
Zn and from 1 to 4.5 atomic % of Y, based on the total amount, and contain, as a remaining
portion, Mg and inevitable impurities. Alternatively, it may contain from 0.1 to 0.5
atomic % of Zr, based on the total amount, and contain as a remaining portion Mg and
inevitable impurities.
[0018] Incorporation of Zr in the magnesium alloy of the present invention within the above-descried
range enables to impart a miniaturized alloy structure to the magnesium alloy. Miniaturization
effect of the alloy structure cannot be attained when the content of Zr is less than
0.1 atomic % based on the total alloy amount. On the other hand, when the content
of Zr exceeds 0.5 atomic % based on the total alloy amount, formation of the intermetallic
compound Mg
3Y
2Zn
3 is sometimes disturbed.
[0019] The magnesium alloy of the present invention is able to have higher strength by the
addition, to the above-described composition, of a small amount of at least one element
selected from the group consisting of La, Ce, Nd, Sm and Yb. Moreover, the magnesium
alloy of the present invention can be obtained as a composite by adding a reinforcing
material such as fibers and particles.
[0020] The magnesium alloy of the present invention can be produced by a process comprising
casting an Mg alloy containing from 1 to 4 atomic % of Zn and from 1 to 4.5 atomic
% of Y, each based on the total amount, at a Zn/Y composition ratio falling within
a range of from 0.6 to 1.3; and plastic processing of the cast product obtained in
the above-described step into an alloy structure containing an intermetallic compound
Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0021] Embodiments of the present invention will hereinafter be described more specifically.
[0022] In this Embodiment, a material containing from 1 to 4 atomic % of Zn and from 1 to
4.5 atomic % of Y, each based on the total alloy amount, at a Zn/Y composition ratio
falling within a range of from 0.6 to 1.3, preferably further containing from 0.1
to 0.5 atomic % of Zr and, as a remaining portion, Mg and inevitable impurities is
charged in a carbon crucible. In an argon atmosphere, the material is melted in a
high-frequency melting furnace, for example, at 700°C to yield a molten alloy.
[0023] The molten alloy is poured into a mold, followed by casting. A cooling rate during
the casting is preferably 10 K/sec or less. This cooling rate is much lower than that
of atomization method or twin-roll method employed for rapid solidification, that
is, 10
4 K/sec or greater. It is also much lower than that of roll casting method or quenched
copper mold method, that is, 10
3 to 10
2 K/sec. In this Embodiment, ordinarily employed molds such as metal mold, graphite
mold and sand mold can be used for casting and a copper mold or water-cooled copper
mold is not necessary, which leads to a reduction in the production cost.
[0024] The cast product thus obtained is subjected to plastic processing, whereby a molded
or formed product can be obtained. The molded or formed product is a magnesium alloy
containing from 1 to 4 atomic % of Zn and from 1 to 4.5% of Y, based on the total
alloy amount, at a Zn/Y composition ratio falling within a range of from 0.6 to 1.3.
Preferably, it further contains from 0.1 to 0.5 atomic % of Zr and as a remaining
portion Mg and inevitable impurities. It contains both an intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure. As a result, the molded or formed product is able
to have both high strength and high ductility.
[0025] Examples, Comparative examples and Referential Examples of the present invention
will next be described.
[Examples]
[0026] In Examples, materials containing, based on the total alloy amount, from 1 to 4 atomic
% of Zn and from 1 to 4.5 atomic % of Y at a Zn/Y composition ratio falling within
a range of from 0.6 to 1.3, preferably further containing from 0.1 to 0.5 atomic %
of Zr, and, as a remaining portion, Mg and inevitable impurities, which materials
were however different from each other with their amounts of Zn, Y and Zr varied within
the above-described ranges were charged in a carbon crucible. In an argon atmosphere,
the materials were melted in a high-frequency melting furnace, for example, at 700°C.
The molten alloys thus obtained were poured into metal molds, followed by casting
at a cooling rate not greater than 10K/sec, whereby rod materials were obtained. The
rod materials were heated to a temperature range of from 350 to 450°C in an electric
furnace, and then extruded at an extrusion ratio of 10, whereby extrusion goods were
obtained.
[0027] The metal structure of each of the resulting extrusion goods was identified by X-ray
diffraction and transmission electron microscope, whereby the presence or absence
of an intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure was confirmed. Test pieces were cut from the extrusion
goods. Their 0.2% proof stress, tensile strength and elongation were measured by conducting
a tensile test on them at normal temperature. The results are shown in Table 1.
[Comparative Examples]
[0028] In Comparative Examples, in a similar manner to that employed for the above-described
Examples except that materials containing, each based on the total alloy amount, from
0.5 to 5 atomic % of Zn and from 0.5 to 5 atomic % of Y and containing, as a remaining
portion, Mg and inevitable impurities, which materials were however different from
each other with their amounts of Zn and Y varied within the above-described ranges
were used, rod materials were obtained. The rod materials were extruded as in the
above-described Examples, whereby extrusion goods were obtained.
[0029] The metal structure of each of the resulting extrusion goods was identified by X-ray
diffraction and transmission electron microscope, whereby the presence or absence
of an intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure was confirmed. Test pieces were cut from the extrusion
goods. Their 0.2% proof stress, tensile strength and elongation were measured by conducting
a tensile test on them at normal temperature. The results are shown in Table 1.
[Referential Examples]
[0030] In Referential Examples, a metal structure of known magnesium alloys, that is, WE54-T6
material and AZ91 material was identified by X-ray diffraction and a transmission
electron microscope, whereby the presence or absence of an intermetallic compound
Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure was confirmed. Test pieces were cut from the WE54-T6
material and AZ91 material, respectively. Their 0.2% proof stress, tensile strength
and elongation were measured by conducting a tensile test on them at normal temperature.
The results are shown in Table 1.

[0031] From Table 1, it is apparent that the magnesium alloys obtained in Examples 1 to
14 containing, based on the total alloy amount, from 1 to 4 atomic % of Zn and from
1 to 4.5 atomic % of Y at a Zn/Y composition ratio falling within a range of from
0.6 to 1.3, and containing both an intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure have both high strength and high ductility, because
they are markedly superior to known WE54-T6 material and AZ91 material in each of
strength (0.2% proof stress, tensile strength) and ductility (elongation).
[0032] Compared with the magnesium alloys obtained in Examples, those obtained in Comparative
Examples 1 to 5 containing Zn and Y at a Zn/Y composition ratio outside the range
of from 0.6 to 1.3 have only either one of the intermetallic compound Mg
3Y
2Zn
3 or Mg
12YZn having a long period structure, suggesting that they are not equipped sufficiently
with either one or both of strength and ductility. It is apparent that the magnesium
alloy obtained in Comparative Example 6 which contained Y in an amount exceeding the
invention range of from 1 to 4.5 atomic % does not have the intermetallic compound
Mg
3Y
2Zn
3 so that it does not have sufficient ductility. It is also apparent that the magnesium
alloy obtained in Comparative Example 7 containing Zn in an amount less than the invention
range of from 1 to 4 atomic % and Y in an amount less than the invention range of
from 1 to 4.5 atomic % does not have the intermetallic compound Mg
3Y
2Zn
3 so that it does not have sufficient strength. It is also apparent that the magnesium
alloy obtained in Comparative Example 8 containing Zn in an amount exceeding the invention
range of from 1 to 4 atomic % and Y in an amount exceeding the invention range of
from 1 to 4.5 atomic % contains both the intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure but it does not have sufficient ductility.
[0033] Provided are a magnesium alloy which is inexpensive, can be produced at a high yield,
and has both high strength and high ductility; and a production process of the magnesium
alloy. The magnesium alloy contains from 1 to 4 atomic % of Zn and from 1 to 4.5 atomic
% of Y at a Zn/Y composition ratio ranging from 0.6 to 1.3, and contains both an intermetallic
compound Mg
3Y
2Zn
3, and Mg
12YZn having a long period structure. It may contain from 2 to 3.5 atomic % of Zn and
from 2 to 4.5 atomic % of Y at a Zn/Y composition ratio falling within a range of
from 0.8 to 1.2. It may contain from 1 to 4 atomic % of Zn, from 1 to 4.5 atomic %
of Y and from 0.1 to 0.5 atomic % of Zr and contains, as a remaining portion, Mg and
inevitable impurities. An alloy structure having both an intermetallic compound Mg
3Y
2Zn
3 and Mg
12YZn having a long period structure is available by casting an Mg alloy containing
from 1 to 4 atomic % of Zn and from 1 to 4.5 atomic % of Y at a Zn/Y composition ratio
ranging from 0.6 to 1.3, followed by plastic processing.
1. A magnesium alloy, which comprises, based on a total alloy amount, from 1 to 4 atomic
% of Zn and from 1 to 4.5 atomic % of Y at a Zn/Y composition ratio falling within
a range of from 0.6 to 1.3, and includesv an intermetallic compound Mg3Y2Zn3 and Mg12YZn having a long period structure.
2. A magnesium alloy according to Claim 1, which comprises at least 3 atomic % of Zn
and at least 3 atomic % of Y, each based on a total alloy amount, and as a remaining
portion Mg and inevitable impurities.
3. A magnesium alloy according to Claim 1, which comprises from 2 to 3.5 atomic % of
Zn and from 2 to 4.5 atomic % of Y, each based on a total alloy amount, at a Zn/Y
composition ratio falling within a range of from 0.8 to 1.2.
4. A magnesium alloy according to Claim 3, which comprises at least 3 atomic % of Zn
and at least 3 atomic % of Y, each based on a total alloy amount, and as a remaining
portion Mg and inevitable impurities.
5. A magnesium alloy according to Claim 1, which comprises from 1 to 4 atomic % of Zn,
from 1 to 4.5 atomic % of Y, and from 0.1 to 0.5 atomic % of Zr, each based on a total
alloy amount, and as a remaining portion Mg and inevitable impurities.
6. A production process of a magnesium alloy, which comprises casting an Mg alloy comprising
from 1 to 4 atomic % of Zn and from 1 to 4.5 atomic % of Y at a Zn/Y composition ratio
falling within a range of from 0.6 to 1.3; and plastic processing of the cast product
obtained in the above-described step into an alloy structure containing an intermetallic
compound Mg3Y2Zn3 and Mg12YZn having a long period structure.
7. A production process of a magnesium alloy according to Claim 6, which comprises at
least 3 atomic % of Zn and at least 3 atomic % of Y, each based on a total alloy amount,
and as a remaining portion Mg and inevitable impurities.
8. A production process of a magnesium alloy according to Claim 6, which comprises from
2 to 3.5 atomic % of Zn and from 2 to 4.5 atomic % of Y, each based on a total alloy
amount, at a Zn/Y composition ratio falling within a range of from 0.8 to 1.2.
9. A production process of a magnesium alloy according to Claim 8, wherein the magnesium
alloy contains at least 3 atomic % of Zn and at least 3 atomic % of Y, each based
on a total alloy amount and contains as a remaining portion Mg and inevitable impurities.
10. A production process of a magnesium alloy according to Claim 6, wherein the magnesium
alloy contains from 1 to 4 atomic % of Zn, from 1 to 4.5 atomic % of Y and from 0.1
to 0.5 atomic % of Zr, each based on a total alloy amount and contains as a remaining
portion Mg and inevitable impurities.
11. A production process of a magnesium alloy according to Claim 6, wherein the casting
is performed at a cooling rate of 10 K/sec or less.
12. A production process of a magnesium alloy according to Claim 6, wherein the plastic
processing is carried out by extrusion of the cast product.