TECHNICAL FIELD
[0001] The present invention relates to a magnesium alloy case comprising a superplastically
formed body of a magnesium alloy sheet or plate material, and more particularly to
a high-quality magnesium alloy case having a complex shape, which comprises a superplastically
formed body and in which the formation of cavities during the superplastic forming
is inhibited by highly accurately controlling the material composition and oxygen
concentration in the magnesium alloy sheet material, and also to a technology for
manufacturing the magnesium alloy case. The present invention provides a novel magnesium
alloy case which has such properties as high resistance to fracture and a high strength
and which can be used in a wide variety of fields including aerospace material, materials
for electronic devices, automobile parts and the like.
BACKGROUND ART
[0002] Magnesium alloy materials have the lowest density (= 1.7 g/cm
3) among the practical structural metallic materials, and the magnesium alloy materials
have attracted attention as next-generation lightweight structural materials because
they have good recyclability inherent to metal materials and because natural resources
therefor are abundant. Presently, most magnesium products in Japan are fabricated
by a casting process such as die casting and thixocasting. The possibility of forming
thin products by such methods is the main reason for successful industrial utilization
of magnesium alloy materials. In particular, in household electronic products, cast
magnesium alloy materials have been used for cases, for example, cases of personal
computers, cellular phones, and digital cameras. However, the problems associated
with the industrial manufacture of magnesium alloy materials by the existing casting
methods include the necessity of conducting the after-treatment to repair the casting
defects, a low yield, and problematic strength and rigidity of the products.
[0003] Plastic processing can be considered as an effective method and the demand therefor
is growing because it has a high yield and provides for increased strength and toughness
simultaneously with forming. In particular, the possibility of fabricating formed
bodies from magnesium alloy sheet materials by a deep drawing, stretch forming, and
blow forming would enable the manufacture of thin-wall and high-strength formed bodies
by an inexpensive process, and strong demand, e.g., for cases of household electronic
products manufactured by such a process can be expected. However, there are only very
few examples of magnesium alloy members fabricated by plastic processing.
[0004] A critical decomposition shear stress of non-base sliding of a magnesium alloy is
much larger than that of other sliding systems at normal temperature, and the formability
of the magnesium alloy at normal temperature is low. Furthermore, a specific feature
of rolled magnesium alloy materials is that a texture in which a {0001} plane is oriented
parallel to the sheet surface is formed therein and strains in the sheet thickness
direction during plastic deformation cannot be expected, this being a factor inhibiting
formability of the magnesium alloy at normal temperature. Because of the above-described
problems, it is essentially difficult to implement cold press forming, which is a
major reason why magnesium alloy members cannot be fabricated by plastic processing.
[0005] A forming method that uses superplastic deformation has attracted attention as a
method for forming magnesium alloys, which have poor cold formability, by plastic
processing. A superplastic phenomenon is developed in metal materials when crystal
grains are refined. In accordance with the present invention, superplastic deformation
is understood as "a phenomenon in which a deformation stress demonstrates strong dependence
on a strain rate in tensile deformation of a polycrystalline material, and a gigantic
elongation in excess of several hundreds of percents is demonstrated without causing
local shrinkage". In such a superplastic deformation, the shape of the crystal itself
is basically not changed and deformation is attained by sliding at the crystallite
interfaces. This phenomenon is called as grain boundary sliding. Superplastic deformation
generally occurs when crystal grain diameter of a material is decreased and a sample
is heated to a temperature of about 50% the liquidus temperature or to a higher temperature.
DISCLOSURE OF THE INVENTION
[0007] Grain boundary sliding is the main superplastic deformation mechanism of magnesium
alloys. A principle diagram of grain boundary sliding is shown in FIG. 1. Grain boundary
sliding indicates a mechanism by which deformation is attained by crystals moving
along grain boundaries, without intragranular deformation. When ideal grain boundary
sliding occurs between crystals, the crystals move along grain boundaries, without
intragranular deformation. Therefore, a cavity unavoidably appears in the vicinity
of a triple point of the grain boundary. FIG. 2 shows a temperature dependence of
grain boundary diffusion coefficients of various alloys (
M. Mabuchi et al.: "Tensile Properties at Room Temperature to 823 K of Mg-4Y-3RE Alloy",
Mater. Trans. 43 (2002), pp. 2063-2068). In FIG. 2, a dimensionless temperature normalized by melting point is plotted against
the abscissa. A dimensionless grain boundary diffusion coefficient is plotted against
the ordinate. A grain boundary diffusion coefficient of magnesium can be confirmed
to be much higher than that of aluminum and iron over the entire temperature range.
Even if a cavity appears in the vicinity of a triple point of grain boundaries during
superplastic deformation in magnesium, which has a high grain boundary diffusion coefficient,
the formation of cavities apparently can be moderated by diffusion. This is why superplastic
forming can be actively used as a method for forming magnesium alloys.
[0008] On the other hand, when a commercial magnesium alloy sheet material is subjected
to superplastic forming, an error in the forming conditions causes the formation of
cavities and the material is ruptured during forming. FIG. 3 shows the pattern of
internal cavities occurring when a rolled material of an AZ31 magnesium alloy (Mg
- 3 mass% Al - 1 mass% Zn - 0.5 mass% Mn) is subjected to tensile deformation at a
temperature of 623 K and a strain rate of 1 x 10
-3 sec
-1 to a true strain of 0.9. Further, in this case, the initial grain diameter was 10
µm. According to FIG. 3, the presence of fine cavities with a size of less than 1
µm and comparatively coarse cavities with a size of 5 µm or more can be confirmed.
The cavities observed in FIG. 3 occur when the formation of cavities in the vicinity
of grain boundaries cannot be moderated by the diffusion of material. Thus, control
of deformation temperature that affects the diffusion rate and control of strain rate
that affects the cavity formation rate are extremely important elements in superplastic
forming.
[0009] Not only the grain boundaries, but also internal impurities can be considered as
origination points for the formation of cavities during superplastic deformation.
However, as an alloy specifications, magnesium alloys have no standards on impurities
that originate in formability, and no measures designed to eliminate the effect of
impurities on superplastic deformation can be found therein. The present invention
has been created with the foregoing in view based on the discovery made by the inventors
that a process of fabricating and providing a magnetism alloy case which is ensuring
formability as a superplastically formed body and having a complex shape can be realized
by specifying the composition of the magnesium alloy sheet material and reducing the
amount of internal impurities to an appropriate value or below. It is an object of
the present invention to provide a high-quality magnesium alloy case that has a complex
shape and ensures formability as a superplastically formed body.
[0010] The present invention that resolves the above-described problems and provides a magnesium
alloy case comprising a superplastically formed body of a magnesium alloy sheet material
that comprises 1.0 to 10.0 mass% of aluminum, 0.5 to 3.0 mass% of zinc, and 0.1 to
0.8 mass% of manganese as a part of added alloying elements and has an oxygen concentration
of 300 mass ppm or less, this superplastically formed body having a structure in which
the formation of cavities during the superplastic forming is inhibited. The preferred
aspects of the magnesium alloy case are as follows: (1) the case comprises a superplastically
formed body of a magnesium alloy sheet material with an oxygen concentration of 100
mass ppm or less, (2) some zones of the magnesium alloy sheet material are formed
by the superplastic forming, (3) the superplastic forming is a deep drawing, (4) the
superplastic forming is a stretch forming, (5) the superplastic forming is a blow
forming, and (6) crystal grains in part of the magnesium alloy case have a size of
20 µm or less. The present invention also relates to a structural lightweight member
comprising the magnesium alloy case.
[0011] The present invention will be described below in greater detail.
[0012] The inventors have focused their attention on oxides present inside a magnesium alloy
sheet material as means for ensuring formability as a superplastically formed body
and making it possible to provide a high-quality magnesium alloy case having a complex
shape. From amongst practical metals, magnesium has the highest affinity to oxygen
and it has been used as a deoxidizing agent in iron and steel refining and the like.
In the alloy preparation and casting of magnesium alloys, the operations are performed
under a cover gas such as a gas mixture of SF
6 and CO
2 so that molten magnesium does not come into contact with the air, but due to process
restrictions it is difficult to avoid oxidation of molten magnesium occurring before
the solidification stage. Oxides (MgO or Al
2O
3) that are nonmetallic inclusions are presently separated by aggregation, flotation
and precipitation induced by blowing argon into magnesium in a molten state.
[0013] When the oxides are admixed in excess to a magnesium alloy sheet material that will
be subjected to superplastic forming, the cavity formation starts from the oxides.
A mechanism of cavity formation is shown in FIG. 4. Because stress concentration occurs
close to the oxides during superplastic forming and also because dislocations are
accumulated around the oxides, cavity formation that starts from oxides is initiated.
When cavity formation shown in FIG. 4 occurs frequently in a material, the cavities
are associated together, thereby causing fracture. Based on the results of comprehensive
research and development, the inventors have gained new insights, namely, that superplastic
deformation can be achieved, while inhibiting the formation of cavities, and a high-quality
case made of a magnesium alloy sheet material and having a complex shape can be created
by controlling the concentration of oxygen in the material to an appropriate value
and further adding appropriately additional elements to magnesium.
[0014] More specifically, it was experimentally confirmed that a magnesium alloy can be
provided with a complex shape by using superplastic forming by controlling the concentration
of oxygen in a magnesium alloy sheet material to 300 mass ppm or less, preferably
100 mass ppm or less. Thus, it was found that by controlling the oxides present inside
a magnesium alloy sheet material to a predetermined amount, even if cavity formation
starts from the oxides during superplastic forming, the cavities do not expand and
are moderated by diffusion. On the other hand, the increase in the concentration of
oxygen in the magnesium alloy sheet material raises the probability of the oxides
being present as impurities in the grain boundary triple points. When oxides are present
in the grain boundary triple points, the oxides become barriers for grain boundary
diffusion and inhibit the moderation of cavity formation, thereby greatly degrading
the formability. For this reason, the oxides should be prevented as thoroughly as
possible from being incorporated into the magnesium alloy sheet material. Thus, the
inventors have confirmed that a phenomenon according to which the oxides enhance the
formation of cavities can be inhibited by suppressing the concentration of oxygen
to 300 ppm or less, preferably to 100 ppm. If the concentration of oxygen in the magnesium
alloy sheet material exceeds 300 ppm, the aforementioned cavity formation and expansion
of cavities cannot be inhibited. In accordance with the present invention, it is especially
important that the superplastically formed body be manufactured by using a magnesium
alloy sheet material in which the concentration of oxygen is highly accurately controlled
to a predetermined range so that the concentration of oxygen does not exceed 300 mass
ppm.
[0015] In accordance with the present invention, where a magnesium alloy has fine crystal
grains of 20 µm or less, preferably fine crystal grains of 15 µm or less, the superplastic
phenomenon can be easily demonstrated in a temperature range of 473 K or higher to
723 K or lower and strain rate region of 1 x 10
-5 1/sec or more to 1 x 10
-1 1/sec or less. Here, a process in which a strain in part of a magnesium alloy sheet
material is 1.0 or more or part of the sheet material is deformed by grain boundary
sliding is defined as superplastic deformation. When a sheet material is deformed
by grain boundary sliding, crystal grains of the sheet material do not grow during
forming or the crystal grains are refined following the dynamic recrystallization.
Thus, in accordance with the present invention, when the crystal grains in the zone
of the formed body where the largest deformation has occurred are 20 µm or less, preferably
15 µm, it can serve as evidence of superplastic forming.
[0016] Theoretically, it is necessary that the crystal grain diameter of a magnesium alloy
sheet material supplied to superplastic forming be decreased to 20 µm or less. On
the other hand, a magnesium alloy sheet material having comparatively coarse grains
with a diameter of about 40 µm also can be supplied to superplastic forming. Even
when a magnesium alloy sheet material having coarse grains of about 40 µm in diameter
is supplied to superplastic forming, the crystal grains of the sheet material can
be refined and effective superplastic forming can be provided to the magnesium alloy
sheet material by using dynamic recrystallization that accompanies the processing.
[0017] In order to inhibit the growth of crystal grains during forming and also to ensure
strength and corrosion characteristics of the magnesium alloy sheet material after
forming, it is necessary to regulate accurately other components of the magnesium
alloy. More specifically, it is preferred that the alloy comprise 1.0 to 10.0 mass%
of aluminum, 0.5 to 3.0 mass% of zinc, and 0.1 to 0.8 mass% of manganese as a part
of added alloy elements.
[0018] Thus, in accordance with the present invention, it is preferred that 1.0 to 10.0
mass% or aluminum be added as an additional alloying element. By adding 1 mass% or
more of aluminum, solid solution strengthening of the magnesium alloy can be expected.
If 6 mass% or more of aluminum is added, then a network-like β phase (Mg
17Al
12) can precipitate on grain boundaries, thereby further increasing the strength of
the material. On the other hand, if 10 mass% or more of aluminum is added, then ductility
of the magnesium alloy after forming might be greatly degraded. Therefore, it is preferred
that the amount of aluminum added to the alloy is 1.0 mass% or more to 10 mass% or
less.
[0019] Further, in accordance with the present invention, the addition of zinc is necessary
to maintain the strength of recycled material. On the other hand, the addition of
3.0 mass% or more of zinc sometimes causes undesirable degradation of corrosion characteristic.
Manganese can moderate the influence of iron that is an impurity element degrading
corrosion resistance, and this effect is demonstrated most effectively when manganese
is added within the above-described range.
[0020] Further, in accordance with the present invention, the addition of manganese is indispensable
for controlling the crystal grain size of the magnesium alloy sheet material. Thus,
crystal grains inside the material grow during superplastic forming and fine crystal
grains that can initiate grain boundary sliding are difficult to maintain unless an
appropriate amount of manganese is added. More specifically, it is preferred that
0.1 mass% or more of manganese be added. On the other hand, if 0.8 mass% or more of
manganese is added, then coarse intermetallic compounds of manganese and aluminum
are formed inside the material and an adverse effect is produced on ductility and
strength of the material. Accordingly, the addition of 0.8 mass% or more of manganese
is undesirable.
[0021] The magnesium alloy case in accordance with the present invention that is obtained
by subjecting the magnesium alloy sheet material to a superplastic forming does not
depend on the type of the superplastic forming. Examples of processes suitable for
forming the magnesium alloy sheet material by the superplastic forming include a deep
drawing, stretch forming, and blow forming. In accordance with the present invention,
formability as a superplastically formed body can be ensured and a high-quality case
having a complex shape can be manufactured essentially by highly accurately controlling
the material quality of the magnesium alloy sheet material, and a magnesium alloy
case manufactured by using any method can be the object of the present invention.
[0022] Where specific amounts of aluminum, zinc, and manganese are added as part of additional
elements to a magnesium alloy sheet material in order to manufacture the magnesium
alloy case in accordance with the present invention through superplastic forming,
fine crystal grains can be maintained by the superplastic forming. More specifically,
by highly accurately controlling the amount of these additional elements and the concentration
of oxygen, it is possible to manufacture a magnesium alloy case comprising a superplastically
formed body in which crystal grains in part of the magnesium alloy case have a size
of 20 µm or less. The yield strength (hardness) of a magnesium alloy has strong correlation
with a crystal grain size, and the manufacture of a high-strength case can be realized
by refining the crystal grains to 20 µm or less. With the conventional technology,
the formation of cavities in superplastic forming was difficult to prevent and the
crystal grains were difficult to refine to a size of 20 µm or less, but in the magnesium
alloy case manufactured in accordance with the present invention, the formation of
cavities caused by superplastic forming is inhibited to a degree larger than that
in the case manufactured through other processes, the crystal grains are refined to
a size of 20 µm or less, and a product with high fracture resistance and high strength
is therefore obtained. By analyzing these properties, the two products can be clearly
distinguished (identified).
[0023] The present invention demonstrates the following noticeable effects: (1) a magnesium
alloy case having a complex shape can be manufactured by a superplastic forming by
controlling the material composition and oxygen concentration of a magnesium alloy
sheet material; (2) a magnesium alloy case comprising a superplastically formed body
having a high fracture resistance and a high strength and having a structure in which
the cavities to be formed during the superplastic forming is inhibited can thereby
be provided; (3) an ultra-lightweight magnesium alloy case that is expected to serve
as a next-generation structural lightweight material can be provided.
BRIEF DESCRIPTION FO THE DRAWINGS
[0024]
FIG. 1 shows a principle of grain boundary sliding. This figure shows how a material
is deformed when crystals move along grain boundaries, without causing deformation
inside the crystal grains.
FIG. 2 shows a temperature dependence of grain boundary diffusion coefficients of
magnesium, iron, and aluminum. The grain boundary diffusion coefficient of magnesium
is shown to be much higher than those of aluminum and iron over the entire temperature
range. A dimensionless temperature normalized by a melting point is plotted against
the abscissa, and a normalized grain boundary diffusion coefficient is plotted against
the ordinate.
FIG. 3 shows the pattern of internal cavities occurring when a rolled material of
an AZ31 magnesium alloy (Mg - 3 mass% Al - 1 mass% Zn - 0.5 mass% Mn) is subjected
to tensile deformation at a temperature of 623 K and a strain rate of 1 x 10-3 sec-1 to a true strain of 0.9. This figure shows the formation of fine cavities with a
size of less than 1 µm and comparatively coarse cavities with a size of 5 µm or more.
The initial crystal grain size is 10 µm.
FIG. 4 illustrates the principle of cavity formation during superplastic forming when
impurities are present inside the material. Because stress concentration occurs in
the vicinity of oxides during superplastic forming and also because dislocations are
accumulated around the oxides, cavity formation that starts from oxides is initiated.
FIG. 5 shows the shape of a die used for blow forming in the embodiments.
FIG. 6 shows the external appearance of the magnesium alloy sheet material after blow
forming as viewed from a side surface. The results are obtained when the applied gas
pressure is 0.5 MPa and 0.2 MPa. The results indicate that formability of the sheet
material is degraded with the increase in internal oxygen concentration of the magnesium
alloy sheet materials.
FIG. 7 shows sheet thickness strain distribution of the sample subjected to blow forming
in Embodiment (Example) 3 and Embodiment (Example) 11. The figure shows that a sheet
thickness strain of 1.0 or more is demonstrated in some zones of the sample. The X
axis shows the measurement zones of strains and shows a sheet thickness strain distribution
on concentric circles, wherein the central portion of the sheet material is assumed
to be at 0 mm. The Y axis shows the sheet thickness strain distribution in various
measurement points.
BEST MODE FOR CARRYING OUT THE INVENTION
[0025] The present invention will be described below in greater detail based on embodiments
(working examples) thereof. However, the present invention is not limited to these
embodiments.
[0026] Rolled materials of an AZ31 magnesium alloy having different oxygen concentrations
were prepared and superplastic formability thereof was evaluated. The AZ31 magnesium
alloy has a composition of Mg - 3 mass% Al - 1 mass% Zn - 0.5 mass% Mn and is a typical
magnesium alloy to be used for wrought material. AZ31 magnesium alloy sheet materials
with a width of 50 mm and a thickness of 5 mm that had different internal oxygen concentrations
were prepared. These magnesium alloy sheet materials were subjected to hot rolling
at a sample temperature of 673 K to manufacture rolled materials of magnesium alloys
with a thickness of 1 mm. No roll heating was performed during hot rolling, and the
draft ratio per 1 pass was 12%. The concentration of oxygen in the samples obtained
and the average crystal grain size of the samples are presented together in Table
1. The concentration of oxygen was measured with a glow discharge mass spectrometer
(GDMS), and the crystal grain size was measured by a section method by observing the
structure of the plane parallel to the rolling direction under an optical microscope.
[Table 1]
| Material |
Oxygen concentration (mass ppm) |
Grain size prior to forming (µm) |
| Sample 1 |
14 |
14.8 |
| Sample 2 |
15 |
17.8 |
| Sample 3 |
52 |
16.8 |
| Sample 4 |
73 |
19.5 |
| Sample 5 |
173 |
16.3 |
| Sample 6 |
248 |
14.6 |
| Sample 7 |
350 |
14.9 |
| Sample 8 |
500 |
14.6 |
[0027] A rectangular magnesium alloy sheet material with a length of 70 mm, a width of 70
mm, and a thickness of 1 mm was cut out from the rolled material and subjected to
superplastic blow forming. In the blow forming, a pressure die and a forming die shown
in FIG. 5 were used. The magnesium alloy sheet material was fixed between two dies,
the dies and the sample piece were heated to 673 K, and blow forming was implemented
by blowing N
2 gas under a pressure of 0.2 MPa or 0.5 MPa on the magnesium alloy sheet material
from the pressure die. The strain rate of the material under an applied pressure of
0.2 MPa is equivalent to about 1 x 10
-5 sec
-1, and the strain rate of the material under an applied pressure of 0.5 MPa is equivalent
to about 1 x 10
-4 sec
-1. The forming was completed when part of the sheet material was ruptured.
[0028] The results obtained in blow forming the AZ31 magnesium alloy sheet materials of
various types are shown in Table 2. A typical outer shape of the sheet material after
blow forming is shown in FIG. 6. Observations of the outer shapes obtained in Embodiment
(Example) 1 and Embodiment 7 shown in FIG. 6 confirm that a perfect cup shape could
be formed in Embodiment 1. On the other hand, in Embodiment 7, although the cup shape
could not be formed, a dome-like shape could be formed. The results obtained in Embodiment
1 and Embodiment 7 relate to a sheet material with the lowest internal oxygen concentration
(14 mass ppm). According to the embodiments, the formability tended to degraded with
the increase in oxygen concentration. The reference symbols shown in the "Formability"
column of Table 2 represent the results obtained by visually comparing the results
of the respective embodiments with the result obtained in Embodiment 1 or Embodiment
7. Thus, symbol o indicates conditions under which practically no difference could
be visually observed. Symbol Δ indicates conditions under which the formability was
visually found to degrade locally. Symbol × indicates conditions under which degradation
of formability was clearly confirmed by multiple forming under the same conditions.
As shown in Embodiment 3 and Embodiment 11, in portions with O and Δ, the formability
could not be visually confirmed to degrade. On the other hand, as shown in Embodiment
7 and Embodiment 15, obvious degradation of formability was confirmed when the concentration
of oxygen was more than 300 mass ppm.
[0029] Table 2 also shows the crystal grain size of samples after blow forming. The measurement
location was a central portion of the sheet material that is the portion with the
highest level of deformation of the sheet material. The table demonstrates that a
state with fine crystal grains (20 µm or less) was maintained in all the samples and
the samples were deformed by superplastic forming.
[Table 2]
| |
Material |
Pressure (MPa) |
Oxygen concentration (mass ppm) |
Grain size prior to forming (µm) |
Formability |
Grain size after forming (µm) |
| Embodiment 1 |
Sample 1 |
0.2 |
14 |
14.2 |
O |
14.8 |
| Embodiment 2 |
Sample 2 |
0.2 |
15 |
17.9 |
O |
17.8 |
| Embodiment 3 |
Sample 3 |
0.2 |
52 |
17.6 |
O |
16.8 |
| Embodiment 4 |
Sample 4 |
0.2 |
73 |
18.2 |
O |
19.5 |
| Embodiment 5 |
Sample 5 |
0.2 |
173 |
15.3 |
Δ |
16.3 |
| Embodiment 6 |
Sample 6 |
0.2 |
248 |
14.3 |
Δ |
14.6 |
| Embodiment 7 |
Sample 7 |
0.2 |
350 |
14.6 |
× |
14.9 |
| Embodiment 8 |
Sample 8 |
0.2 |
500 |
14.3 |
× |
14.6 |
| Embodiment 9 |
Sample 1 |
0.5 |
14 |
14.2 |
O |
14.3 |
| Embodiment 10 |
Sample 2 |
0.5 |
15 |
17.9 |
O |
18.2 |
| Embodiment 11 |
Sample 3 |
0.5 |
52 |
17.6 |
O |
18 |
| Embodiment 12 |
Sample 4 |
0.5 |
73 |
18.2 |
O |
18.8 |
| Embodiment 13 |
Sample 5 |
0.5 |
173 |
15.3 |
Δ |
16.4 |
| Embodiment 14 |
Sample 6 |
0.5 |
248 |
14.3 |
Δ |
14.6 |
| Embodiment 15 |
Sample 7 |
0.5 |
350 |
14.6 |
× |
14.9 |
| Embodiment 16 |
Sample 8 |
0.5 |
500 |
14.3 |
× |
15.1 |
[0030] FIG. 7 shows the results obtained in observing cross sections of the samples subjected
to blow forming in Embodiment 3 and Embodiment 11 and measuring the sheet thickness
strains in various zones. The X axis shows the measurement zones of strains and shows
a sheet thickness strain distribution on concentric circles, wherein the central portion
of the sheet material is assumed to be at 0 mm. The Y axis shows the sheet thickness
strain distribution in various measurement points. According to FIG. 7, a sheet thickness
strain of 1.0 or more was confirmed in some measurement locations at any strain rate,
thereby indicating that superplastic forming has been reached. Thus, it was confirmed
that superplastic forming was developed in samples with highly accurately controlled
oxygen concentration.
INDUSTRIAL APPLICABILITY
[0031] As described hereinabove, the present invention relates to a magnesium alloy case,
and the invention can provide a magnesium alloy case having a complex shape, high
fracture resistance and a high strength, and a structure in which cavity formation
is inhibited even in superplastic forming by accurately specifying the composition
and impurities of the magnesium alloy sheet material. The present invention is useful
because it enables mass production and practical use of ultra-lightweight magnesium
alloy cases that can be actively applied to cases of household electronic products,
for example, digital cameras, notebook personal computers, and PDA.
1. A magnesium alloy case characterized by comprising a superplastic body formed through the superplastic forming of a magnesium
alloy sheet material, which is containing 1.0 to 10.0 mass% of aluminum, 0.5 to 3.0
mass% of zinc, and 0.1 to 0.8 mass% of manganese as a part of added alloy elements
and has an oxygen concentration of 300 mass ppm or less, and the case having a structure
being inhibited in cavity formation during the superplastic forming is inhibited.
2. The magnesium alloy case according to claim 1, wherein the case comprises a superplastically
formed body of the magnesium alloy sheet material having an oxygen concentration of
100 mass ppm or less.
3. The magnesium alloy case according to claim 1 or 2, wherein some portions of the magnesium
alloy sheet material are formed through the superplastic forming.
4. The magnesium alloy case according to claim 3, wherein the superplastic forming is
a deep drawing.
5. The magnesium alloy case according to claim 3, wherein the superplastic forming is
a stretch forming.
6. The magnesium alloy case according to claim 3, wherein the superplastic forming is
a blow forming.
7. The magnesium alloy case according to any one of claims 1 to 6, wherein some crystal
grains of the magnesium alloy case have a size of 20 µm or less.
8. A lightweight structural member characterized by comprising the magnesium alloy case defined in any one of claims 1 to 7.