[TECHNICAL FIELD]
[0001] The present invention relates to a surface-treated aluminum material, a method of
manufacturing the same, a metal casing, and a kitchen appliance.
[BACKGROUND ART]
[0002] Aluminum materials composed of aluminum or an aluminum alloy are utilized in various
applications. An anodic oxide film can be provided on the surface(s) of these aluminum
materials for purposes such as surface protection. In addition, a sealing treatment
is sometimes performed for the purpose of closing up the pores formed in the anodic
oxide film and increasing the corrosion resistance of the aluminum material.
[0003] For example, a method of surface-treating aluminum or an aluminum alloy is described
in Patent Document 1, characterized by having: a step of forming an anodic oxide film
on a surface of aluminum or an aluminum alloy; a first sealing treatment step of immersion
in an aqueous solution, which contains nickel fluoride, at 20-35°C; and a second sealing
treatment step of immersion in an aqueous solution, which contains nickel acetate,
at 80-93°C.
[PRIOR ART LITERATURE]
[Patent Documents]
[SUMMARY OF THE INVENTION]
[PROBLEMS TO BE SOLVED BY THE INVENTION]
[0005] However, with regard to aluminum materials obtained by the manufacturing method of
Patent Document 1, cracks are more likely to form in the anodic oxide film when the
temperature has risen, and there is a risk that debris composed of small pieces of
the anodic oxide film might be formed. To curtail the formation of such debris, there
is a demand to further increase the heat resistance of aluminum materials having anodic
oxide films on their surfaces.
[0006] The present invention was conceived in view of this background, and it is an object
to provide: a surface-treated aluminum material that is capable of curtailing the
formation of cracks even when the temperature has risen; a method of manufacturing
the same; a metal casing; and a kitchen appliance.
[MEANS FOR SOLVING THE PROBLEMS]
[0007] One aspect of the present invention is a surface-treated aluminum material comprising:
a base material, which is composed of aluminum or an aluminum alloy; and a protective
film, which is formed on the base material; wherein:
the protective film is composed of an oxide or oxides of aluminum, and has:
an oxide layer, which covers the base material; and
a hydrated oxide layer, which covers the oxide layer;
the hydrated oxide layer contains:
a hydrated oxide or hydrated oxides of aluminum; and
a metal oxide or metal oxides and/or a metal hydroxide or metal hydroxides containing
one or two or more metal elements selected from the group consisting of Ni (nickel),
Cr (chromium), Zr (zirconium), Si (silicon), Ti (titanium), Au (gold), Ag (solver),
Co (cobalt), Mo (molybdenum), Mn (manganese), Nb (niobium), Ta (tantalum), W (tungsten),
Zn (zinc), Fe (iron), Ir (iridium), and Sc (scandium); and
in the situation in which cathode polarization measurements are performed-using a
measurement solution obtained by mixing a solution of NaCl having a concentration
of 5 mass% and acetic acid having a concentration of 99.7% such that the volumetric
ratio of the NaCl solution to the acetic acid = 1000:1-on the base material and on
the surface-treated aluminum material after it had been heated for 4 hours at a temperature
of 200°C, and the current density at the electric potential at the center of an electric-potential
region of the base material that exhibits the diffusion-limited current of hydrogen
ions was measured, the ratio J1/J2 of the current density J1 of the surface-treated
aluminum material to the current density J2 of the base material is 90 × 10-5 or less.
[0008] A second aspect of the present invention is a surface-treated aluminum material having
a base material, which is composed of aluminum or an aluminum alloy, and a protective
film, which is formed on the base material, wherein:
the protective film is composed of an oxide or oxides of aluminum, and has:
an oxide layer, which covers the base material; and
a hydrated oxide layer, which covers the oxide layer;
the hydrated oxide layer contains:
a hydrated oxide or hydrated oxides of aluminum; and
a metal oxide or metal oxides and/or a metal hydroxide or metal hydroxides containing
one or two or more metal elements selected from the group consisting of Ni, Cr, Zr,
Si, Ti, Au, Ag, Co, Mo, Mn, Nb, Ta, W, Zn, Fe, Ir, and Sc; and
a sample having the protective film on one surface of the base material was prepared
from the surface-treated aluminum material and measured in a state in which a strain
gauge is mounted on the sample on a rear surface of the surface having the protective
film, the difference ε1 - ε2 between the amount ε1 of strain of the sample at a temperature
of 200°C and the amount ε2 of strain of the base material at a temperature of 200°C
is 100 × 10-6 or less.
[0009] A third aspect of the present invention is a metal casing composed of the surface-treated
aluminum material according to the above-mentioned aspects.
[0010] A fourth aspect of the present invention is a kitchen appliance comprising the metal
casing.
[0011] A fifth aspect of the present invention is a method of manufacturing the surface-treated
aluminum material according to the aforementioned aspects, comprising:
forming the oxide layer, which has pores, on the base material by performing an anodizing
treatment on the base material;
thereafter, heating the base material and the oxide layer at a temperature of 200°C
or higher and 400°C or lower; and
thereafter, contacting the oxide layer with a sealing agent that contains the metal
element(s), thereby forming the hydrated oxide layer on the oxide layer and sealing
the pores.
[EFFECTS OF THE INVENTION]
[0012] A surface-treated aluminum material (referred to as "aluminum material" below) according
to the first aspect has a protective film having the oxide layer and the hydrated
oxide layer on a surface or surfaces of the base material. In addition, in the situation
in which cathodic polarization measurements have been performed according to the above-mentioned
specific method on the base material and on the surface-treated aluminum material
after it was heated for 4 hours at a temperature of 200°C, the ratio J1/J2 of the
current density J1 of the surface-treated aluminum material to the current density
J2 of the base material is 90 × 10
-5 or less. Aluminum materials having such a characteristic excel in heat resistance,
and can curtail the formation of cracks even in situations in which the temperature
has risen.
[0013] A surface-treated aluminum material according to the second aspect has a protective
film, which comprises the oxide layer and the hydrated oxide layer on a surface of
the base material. In addition, the difference ε1 - ε2 between the amount ε1 of strain
of the sample at a temperature of 200°C and the amount ε2 of strain of the base material
at a temperature of 200°C, measured using the above-mentioned specific method, is
100 × 10
-6 or less. Aluminum materials having such a characteristic excel in heat resistance,
and can curtail the formation of cracks even in situations in which the temperature
has risen.
[0014] Because the metal casing according to the third aspect is constituted from the above-mentioned
aluminum material, it excels in heat resistance and can curtail the formation of cracks
even in situations in which the temperature has risen.
[0015] The metal casing on the kitchen appliance according to the fourth aspect is constituted
from the above-mentioned aluminum material. As described above, because the above-mentioned
aluminum material excels in heat resistance, it can curtail the formation of cracks
in a metal casing on a kitchen appliance, even in situations in which the temperature
has risen.
[0016] In addition, in the method of manufacturing the aluminum material according to the
fifth aspect, after an anodizing treatment has been performed on the base material,
the oxide layer, which had formed owing to the anodizing treatment, is heated at a
temperature within the above-mentioned specific range. Thus, by heating the oxide
layer before sealing the pores in the oxide layer, internal stresses created when
the oxide layer was formed can be relaxed. Then, after the internal stresses in the
oxide layer have been relaxed, by contacting the oxide layer with a sealing agent
and forming the hydrated oxide layer on the oxide layer while sealing the pores, heat
resistance increases, and the formation of cracks can be curtailed even in situations
in which the temperature has risen.
[0017] As described above, according to the above-mentioned aspects, a surface-treated aluminum
material that excels in heat resistance and is capable of curtailing the formation
of cracks even in situations in which the temperature has risen, a method of manufacturing
the same, a metal casing, and a kitchen appliance can be provided.
[BRIEF DESCRIPTION OF THE DRAWINGS]
[0018]
[FIG. 1] FIG. 1 is a cross-sectional view of a surface-treated aluminum material of
Working Example 1.
[FIG. 2] FIG. 2 is a cross-sectional view of a base material on which an oxide layer
is formed during a process of manufacturing the surface-treated aluminum material
of Working Example 1.
[FIG. 3] FIG. 3 is an explanatory graph showing a cathodic polarization curve of the
base material of Working Example 1.
[FIG. 4] FIG. 4 is an enlarged view of a step portion in the cathodic polarization
curve of the base material.
[FIG. 5] FIG. 5 is an explanatory diagram for describing a method of measuring the
amount of strain in the surface-treated aluminum material according to a reference
example.
[FIG. 6] FIG. 6 is an explanatory graph showing results of measuring the amount of
strain in the surface-treated aluminum material according to the reference example.
[MODES FOR CARRYING OUT THE INVENTION]
(Aluminum Material)
[0019] The base material of the aluminum material is constituted from aluminum or an aluminum
alloy. The shape of the base material is not particularly limited, and various shapes
may be used in accordance with the application of the aluminum material. In addition,
the material of the base material can be selected, as appropriate, from the group
consisting of aluminum and aluminum alloys in accordance with the application of the
aluminum material. More specifically, for example, a 1000-series aluminum can be used
as the aluminum constituting the base material. In addition, for example, a 2000-series
aluminum alloy, a 3000-series aluminum alloy, a 4000-series aluminum alloy, a 5000-series
aluminum alloy, a 6000-series aluminum alloy, a 7000-series aluminum alloy, and an
8000-series aluminum alloy can be used as the aluminum alloy constituting the base
material.
[0020] A protective film that contains an oxide layer, which is composed of an oxide or
oxides of aluminum and has been laminated on the base material, and a hydrated oxide
layer, which has been laminated on the oxide layer, is provided on the base material.
The hydrated oxide layer contains a hydrated oxide or hydrated oxides of aluminum,
and one or more metal compounds selected from the group consisting of a metal oxide
or metal oxides and a metal hydroxide or metal hydroxides, which contain(s) the metal
element(s). After having formed the oxide layer, which has numerous pores, on the
surface of the base material by performing an anodizing treatment on the base material,
the protective film can be obtained, for example, by performing a sealing treatment
and thereby closing up the pores in the oxide layer with the hydrated oxide layer.
Such a protective film excels in corrosion resistance with respect to corrosive gas.
For this reason, the corrosion resistance of the aluminum material can be increased
by forming the protective film on the base material.
[0021] The thickness of the protective film preferably is 2 µm or more. Thereby, the corrosion
resistance of the aluminum material can be further increased. From the viewpoint of
corrosion resistance, the upper limit of the thickness of the protective film is not
particularly limited; the thicker the protective film is made, the more the corrosion
resistance of the aluminum material can be increased. From this viewpoint, the thickness
of the protective film is more preferably 5 µm or more and yet more preferably 10
µm or more. It is noted that, from the viewpoint of manufacturing, the upper limit
of the thickness of the protective film is, for example, 200 µm. From the viewpoint
of reducing manufacturing time, the thickness of the protective film preferably is
100 µm or less.
[0022] A ratio A
M/A
H of the integrated value A
M of light-emission intensities of the metal element(s) to the integrated value A
H of the light-emission intensities of hydrogen measured in a range from the surface
of the aluminum material to a depth of 500 nm by glow-discharge optical emission spectroscopy
(referred to below as "GDOES") is preferably 0.1 or more and 5.0 or less. The light-emission
intensities of elements measured by GDOES indicate the content of said element(s),
and a higher light-emission intensity signifies that a larger amount of said element(s)
is included. In addition, a majority of the hydrated oxide layer is constituted by
a hydroxide or hydroxides of aluminum. Accordingly, the value of the ratio A
M/A
H indicates the content of the metal element(s), which has been normalized in accordance
with the amount of the hydroxide(s) of aluminum. Furthermore, by making the value
of the ratio A
M/A
H for the aluminum material to be within the above-mentioned specific range, the effect
of improving the corrosion resistance can be more reliably obtained.
[0023] The value of the ratio A
M/A
H can be calculated by the following method. First, using a depth-direction profile
of the light-emission intensities acquired by GDOES for hydrogen in the aluminum material,
the light-emission intensities of hydrogen at each measurement point present within
a range from the surface of the aluminum material to a depth of 500 nm are added together,
and this value is taken as the integrated value A
H of the light-emission intensities of hydrogen. Similarly, using a depth-direction
profile of the light-emission intensities of the metal element(s) in the aluminum
material, the light-emission intensity of the metal element(s) at each of the measurement
points present within the range from the surface to the depth of 500 nm are added
together, and this value is taken as the integrated value A
M of the light-emission intensities of the metal element(s). By dividing the integrated
value A
M of the light-emission intensities of the metal element(s) by the integrated value
A
H of the light-emission intensities of the hydrogen obtained in this manner, the value
of the ratio A
M/A
H can be obtained.
[0024] In a situation in which a sealing test has been performed according to the method
stipulated in JIS H8683-2:2013, the mass loss per unit of area of the aluminum material
is preferably 0.3 g/dm
2 or less. In such an aluminum material, the pores in the oxide layer are sufficiently
sealed by the hydrated oxide layer. Consequently, by making the mass loss per unit
of area of the aluminum material to be within the above-mentioned specific range,
the corrosion resistance of the aluminum material can be more reliably increased.
[0025] It is noted that a specific method of the sealing test is as follows. First, 35 mL
of phosphoric acid and 20 g of anhydrous chromic acid are dissolved in water to prepare
1 L of a test solution. Next, a test piece, which includes the protective film, is
extracted from the aluminum material, and the surface area of the protective film
on the test piece is measured. After contamination on the surface of this test piece
has been removed, the mass of the test piece is measured. Subsequently, the test piece
is immersed for 15 min ±5 s in the test solution, which is held at a temperature of
38°C ±1°C.
[0026] After immersion of the test piece in the test solution has been completed, the test
piece is rinsed with running water and then further rinsed with deionized water or
distilled water. Following the rinsing and after the test piece has been thoroughly
dried, the mass of the test piece is measured.
[0027] The surface area S (unit: dm
2) of the protective film of the test piece obtained as described above, the mass m
1 (unit: g) of the test piece before immersion in the test solution, and the mass m
2 (unit: g) of the test piece after immersion in the test solution can be used to calculate
the mass loss δ
S per unit of area (unit: g/dm
2) based on Equation (1) below.

[0028] Surface-treated aluminum materials according to the first aspect have the characteristic
that, in the situation in which cathodic polarization measurements are performed-using
a measurement solution obtained by mixing a solution of NaCl having a concentration
of 5 mass% and acetic acid having a concentration of 99.7% such that the volumetric
ratio of NaCl solution:acetic acid = 1000:1-on the base material and on the surface-treated
aluminum material after it had been heated at a temperature of 200°C for 4 hours,
and the current density at the electric potential at the center of an electric-potential
region of the base material that exhibits the diffusion-limited current of hydrogen
ions was measured, the ratio J1/J2 of the current density J1 of the surface-treated
aluminum material to the current density J2 of the base material is 90 × 10
-5 or less. Aluminum materials having a ratio J1/J2 of the current density J1 within
the above-mentioned specific range have the characteristic that cracks form less readily
when the temperature has risen and they excel in heat resistance.
[0029] From the same viewpoint of further improving the heat resistance of aluminum materials,
the current-density ratio J1/J2 is preferably 70 × 10
-5 or less, more preferably 50 × 10
-5 or less, and yet more preferably 30× 10
-5 or less. From the viewpoint of increasing the heat resistance of the aluminum material,
there is no lower limit for the current-density ratio J1/J2; thus, given that definition,
the current-density ratio J1/J2 is definitely a value greater than 0.
[0030] In addition, surface-treated aluminum materials according to the second aspect have
the characteristic that the difference ε1 - ε2 between the amount ε1 of strain of
a sample, which has the protective film on one surface of the base material and was
prepared from the surface-treated aluminum material and measured in a state in which
a strain gauge is mounted on the sample on a rear surface of the protective film-at
a temperature of 200°C and the amount ε2 of strain of the base material at a temperature
of 200°C is 100 × 10
-6 or less. Aluminum materials, in which the difference ε1 - ε2 of the amounts of strain
is within the above-mentioned specific range, have the characteristic that cracks
form less readily when the temperature has risen and they excel in heat resistance.
It is noted that the lower limit of the difference ε1 - ε2 in the amounts of strain
of the sample, which was prepared from the aluminum material, usually becomes -100
× 10
-6 or more.
[0031] The method of preparing the sample from the surface-treated aluminum material is
not particularly limited, and various methods can be employed as long as the method
chosen does not affect the amount of strain in the sample. In the situation in which
the surface-treated aluminum material is, for example, a sheet having the protective
film on only one surface of the base material, a small piece of the surface-treated
aluminum material that is cut to an appropriate size can be used as the sample. In
addition, in the situation in which the surface-treated aluminum material is, for
example, a sheet having the protective film on both surfaces of the base material,
the sample can be obtained by cutting the surface-treated aluminum material to an
appropriate size to prepare a small piece and then removing one of the two protective
films from the small piece. A method of, for example, dissolving the protective film
using an acid or an alkali, or the like can be employed as a method of removing the
protective film.
[0032] As described above, the aluminum materials can curtail the formation of cracks in
the protective film even in the situation in which the temperature has risen. For
this reason, the aluminum materials are suitable for applications such as a casing
for an appliance that becomes a high temperature while in use, such as a kitchen appliance,
or the like. More specifically, the aluminum materials are suited for use, for example,
as a metal casing, such as for a kitchen appliance. For example, heating and cooking
equipment, such as an oven, a microwave oven, a gas range, or a fryer, and a hot food
showcase can be given as examples of kitchen appliances.
(Method of Manufacturing the Aluminum Material)
[0033] To manufacture the surface-treated aluminum material, first, a base material composed
of aluminum or an aluminum alloy is prepared. The method of manufacturing the base
material is not particularly limited, and known methods can be employed. The base
material may be manufactured, for example, by a method in which casting, rolling,
and heat treatment(s) are combined as appropriate. In addition, after the base material
has been manufactured and before performing the anodizing treatment, pretreatments
of the anodizing treatment, such as degreasing, acid cleaning, and grinding, may be
performed, as necessary. Next, the oxide layer, which has pores, is formed on the
base material by performing the anodizing treatment on the base material. The oxide
layer can be formed on the surface(s) of the base material during the anodizing treatment
by flowing a direct current between the base material and a counter electrode in a
state in which the base material and the counter electrode are immersed in an electrolyte
solution. The oxide layer thus formed is constituted from an oxide or oxides of aluminum,
such as alumina, and has numerous pores.
[0034] The electrolyte solution employed in the anodizing treatment may be, for example,
an acidic electrolyte solution containing an electrolyte, such as sulfuric acid, phosphoric
acid, or the like, or may be an alkaline electrolyte solution containing an electrolyte,
such as sodium metaborate. The electrolyte solution employed in the anodizing treatment
preferably contains an inorganic electrolyte composed of an inorganic cation, such
as a metal ion or an ammonium ion, and one or two or more anions selected from the
group consisting of a sulfate ion, a phosphate ion, and a borate ion. An oxide layer
having a desired structure can be more easily formed by performing the anodizing treatment
using an electrolyte solution that contains an inorganic electrolyte.
[0035] The current density of the direct current in the anodizing treatment can be set,
for example, in a range of 1 mA/cm
2 or more and 100 mA/cm
2 or less, as appropriate. In addition, the temperature of the electrolyte solution
in the anodizing treatment can be set, for example, in a range of 0°C or higher and
40°C or lower, as appropriate.
[0036] The thickness of the oxide layer formed in the anodizing treatment is preferably
2 µm or more. By making the thickness of the oxide layer 2 µm or more, the thickness
of the protective film obtained after sealing can be made sufficiently thick, and
an aluminum material that excels in corrosion resistance and in heat resistance can
be more easily obtained.
[0037] In the above-mentioned method of manufacturing, after the anodizing treatment has
been performed, the base material and the oxide layer are heated at a temperature
of 200°C or higher and 400°C or lower. By heating the oxide layer at a temperature
within the above-mentioned specific range after the anodizing treatment has been performed
and before sealing the pores in the oxide layer, internal stresses in the oxide layer
can be relaxed. Then, by sealing the pores after the internal stresses of the oxide
layer were relaxed, the internal stresses in the protective film after sealing can
be reduced. As a result, the formation of cracks in the protective film when heated
can be curtailed, and the heat resistance of the aluminum material can be improved.
[0038] In the situation in which the heating temperature of the oxide layer is too low,
there is a risk that the relaxation of the internal stresses in the oxide layer might
be insufficient, and cracks might form in the protective layer more readily when the
temperature of the aluminum material has risen. From the viewpoint of easily avoiding
such a problem, the heating temperature of the oxide layer is set to 200°C or more.
On the other hand, in the situation in which the heating temperature of the oxide
layer is too high, there is a risk that the oxide layer might be unable to follow
the thermal expansion of the base material, and cracks might form in the protective
film. From the viewpoint of easily avoiding such a problem, the heating temperature
of the oxide layer is set to 400°C or less.
[0039] When heating the oxide layer, the heating may be ended immediately after the temperature
of the oxide layer has reached a desired temperature, or that temperature may be maintained
for a certain extent of time after the desired temperature of the oxide layer has
been reached. From the viewpoint of sufficiently relaxing the internal stresses in
the oxide layer and more reliably increasing the heat resistance of the aluminum material,
the heating time from when heating of the oxide layer is started to when heating is
ended is preferably 1 min or more and less than 12 hours.
[0040] After the oxide layer has been heated, the oxide layer is contacted with a sealing
agent. Thereby, a hydrated oxide layer is formed on the oxide layer, and the pores
in the oxide layer are sealed by the hydrated oxide layer. For example, an aqueous
solution containing one or two or more metal elements selected from the group consisting
of Ni, Cr, Zr, Si, Ti, Au, Ag, Co, Mo, Mn, Nb, Ta, W, Zn, Fe, Ir, and Sc can be used
as the sealing agent. When an aqueous solution containing the above-mentioned metal
element(s) is used as the sealing agent and is contacted with the oxide layer, the
hydration reaction of the oxide or oxides of aluminum and the precipitation reaction
of the metal element(s) progress in parallel. As a result, a hydrated oxide layer
containing a hydrated oxide or hydrated oxides of aluminum, and an oxide or oxides
and/or a hydrated oxide or hydrated oxides of the above-mentioned metal element(s)
can be formed on the oxide layer.
[0041] The sealing agent is preferably an aqueous solution that contains ions of the metal
element(s). By using such a sealing agent, the hydrated oxide layer can be more reliably
formed. The metal element(s) in the sealing agent may be present as metal ions or
may be present as complex ions. For example, an aqueous solution of a metal salt or
metal salts that contains the above-mentioned metal element(s), such as aqueous nickel
acetate, aqueous cobalt acetate, aqueous chromate, and aqueous silicate, can be used
as the sealing agent.
[Working Examples]
(Working Example 1)
[0042] Working examples of a surface-treated aluminum material and a method of manufacturing
the same will be described with reference to FIG. 1 to FIG. 2. As shown in FIG. 1,
the surface-treated aluminum material 1 of the present example comprises: a base material
2, which is composed of aluminum or an aluminum alloy; and a protective film 3, which
is formed on the base material. The protective film 3 comprises: an oxide layer 31,
which is composed of an oxide or oxides of aluminum and covers the base material 2;
and a hydrated oxide layer 32, which covers the oxide layer 31. The hydrated oxide
layer 32 contains a hydrated oxide or hydrated oxides of aluminum, and a metal oxide
or metal oxides and/or a metal hydroxide or metal hydroxides containing one or two
or more metal elements selected from the group consisting of Ni, Cr, Zr, Si, Ti, Au,
Ag, Co, Mo, Mn, Nb, Ta, W, Zn, Fe, Ir, and Sc. In the situation in which cathodic
polarization measurements are performed-using a measurement solution obtained by mixing
a solution of NaCl having a concentration of 5 mass% and acetic acid having a concentration
of 99.7% such that the volumetric ratio of the NaCl solution:acetic acid = 1000:1-on
the base material 2 and on the surface-treated aluminum material 1 after it had been
heated for 4 hours at a temperature of 200°C, and the current density at the electric
potential at the center of an electric-potential region of the base material 2 that
exhibits the diffusion-limited current of hydrogen ions was measured, the ratio J1/J2
of the current density J1 of the surface-treated aluminum material 1 to the current
density J2 of the base material 2 is 90 × 10
-5 or less.
[0043] To manufacture the aluminum material 1 of the present example, an oxide layer 31,
which has pores 311, is first formed on the base material 2, as shown in FIG. 2, by
performing an anodizing treatment on the base material 2. Thereafter, the base material
2 and the oxide layer 31 are heated at a temperature of 200°C or higher and 400°C
or lower and internal stresses in the oxide layer 31 are relaxed. Thereafter, the
aluminum material 1 can be obtained by contacting the oxide layer 31 with the sealing
agent, and forming a hydrated oxide layer 32 on the oxide layer 31 while sealing the
pores 311.
[0044] Specific examples of the aluminum material 1 (Test Materials A1-A12) are shown in
Table 1. The method of manufacturing Test Materials A1-A12 is, for example, as follows.
First, aluminum sheets having the chemical compositions indicated by each of the alloy
numbers listed in Table 1 and having a thickness of 1.1 mm are prepared as the base
material 2. Pretreatments of the anodizing treatment are performed on these base materials
2. Specifically, as the pretreatments, an alkaline etching treatment is first performed
in which the base material 2 is immersed in an aqueous solution of sodium hydroxide
having a concentration of 5 mass% and a temperature of 55°C. Subsequently, a desmutting
treatment is performed by immersing the base material 2 in nitric acid having a concentration
of 30 mass%.
[0045] After the pretreatments have been performed on the base material 2 as described above,
an anodizing treatment is performed on the base material 2, and the oxide layer 31
forms on the surface of the base material 2. The electrolyte solution used in the
anodizing treatment is an aqueous solution of sulfuric acid having a concentration
of 15 mass%, and the temperature of the electrolyte solution is 5°C. In addition,
the current density in the anodizing treatment is 10 mA/cm
2, and the treatment time is 60 min. The oxide layer 31 thus formed is a so-called
porous-type alumite film and, as shown in FIG. 2, has numerous pores 311. It is noted
that the thickness of the oxide layer 31 formed by performing the anodizing treatment
under the conditions described above is approximately 19 µm.
[0046] After having performed the anodizing treatment, the base material 2 is heated inside
a heating furnace and the internal stresses in the oxide layer 31 are relaxed. The
set temperature of the heating furnace is the value shown in the "Heating Temperature"
column in Table 1, the residence time of the base material inside the furnace, that
is, the time from the start of heating to the end of heating, is the value shown in
the "Heating Time" column in Table 1.
[0047] Thereafter, by immersing the base material 2, which has the oxide layer 31, in the
sealing agent for 60 min, the hydrated oxide layer 32, which is composed of the hydrated
oxide(s) of aluminum, forms on the oxide layer 31, and the pores 311 in the oxide
layer 31 are sealed by the hydrated oxide layer 32. The sealing agent used in the
present example is, specifically, either of an aqueous solution, in which "Top Seal
(registered trademark) H-298" manufactured by Okuno Chemical Industries Co., Ltd.
has been diluted with water to a concentration of 40 mL/L, or an aqueous solution,
in which "Top Seal L-100" manufactured by Okuno Chemical Industries Co., Ltd. has
been dissolved in water at a concentration of 5 g/L. It is noted that "Top Seal H-298"
is an aqueous solution in which nickel acetate serves as the main component. In addition,
"Top Seal L-100" is a solid in which nickel fluoride serves as the main component.
In Table 1, "Top Seal H-298" is recorded as "H-298" and "Top Seal L-100" is recorded
as "L-100."
[0048] Test Materials A1-A12 shown in Table 1 could thereby be obtained based on the above.
It is noted that Test Materials B1-B7 shown in Table 1 are test materials for comparison
with Test Materials A1-A12. The method of manufacturing Test Materials B1-B2, B5-B7
was the same as the method of manufacturing Test Material A1 except that, after the
oxide layer 31 was formed on the base material 2, the oxide layer 31 was brought into
contact with a sealing agent without being heated. In addition, the method of manufacturing
Test Materials B3-B4 is the same as the method of manufacturing Test Material A1 except
that the heating conditions in the heating furnace were modified as shown in Table
1.
[0049] Next, the method of measuring the cathodic polarization of Test Materials A1-A12
and Test Materials B1-B7 will be explained.
(Cathodic Polarization Measurement)
[0050] Using the following method, cathodic polarization measurements are performed on the
base material and on the test material that had been heated for 4 hours at a temperature
of 200°C; based on the resulting cathodic polarization curves, the ratio J1/J2 of
the current density J1 of the surface-treated aluminum material to the current density
J2 of the base material is calculated. First, the test material is heated for 4 hours
in an oven set to a temperature of 200°C. After removing the test material from the
oven and cooling to room temperature, an evaluation region is established on the protective
film, and portions other than the evaluation region on the surface of the test material
are covered with silicone resin.
[0051] Next, an aqueous solution of NaCl having a concentration of 5 mass% and acetic acid
having a concentration of 99.7% are prepared, and a measurement solution is prepared
by adding the acetic acid to the aqueous solution of NaCl such that the volumetric
ratio of aqueous solution of NaCl to the acetic acid is an aqueous solution of NaCl:acetic
acid = 1000:1. A test piece, a counter electrode, and a reference electrode, which
are electrically connected to a potentiostat, are immersed in this measurement solution
and left standing for 30 min to stabilize the electric potential of the measurement
area. It is noted that degassing of the measurement solution is not performed. In
addition, for example, an Ag/AgCl electrode can be used as the reference electrode.
[0052] After the electric potential of the measurement area had stabilized, a voltage is
applied between the test piece and the counter electrode using the potentiostat, and
the electric potentials of the measurement area are swept at a sweep rate of 20 mV/min
until the electric potentials of the measurement area reached -2,000 mV relative to
the reference electrode. A cathodic polarization curve for the post-heated test material
is obtained by measuring the current density flowing in the measurement area at this
time. In addition, a cathodic polarization curve for the base material is obtained
by performing a similar measurement using the base material after the pretreatment
of the anodizing treatment had been performed using the method described above. It
is noted that the cathodic polarization measurements of both the test materials and
the base materials are performed in the state in which the temperature of the measurement
solution was maintained at 25°C in ambient atmosphere. In addition, the cathodic polarization
measurements of the test materials and the base materials are performed in the state
in which the measurement solution was not agitated and the measurement solution was
substantially not flowing.
[0053] One example of the cathodic polarization curve of the base material is shown in FIG.
3. It is noted that, in FIG. 3, the ordinate is the electric potential of the measurement
area (unit: V), and the abscissa is the current density (unit: µA/cm
2). In addition, the scale of the abscissa in FIG. 3 is a logarithmic scale. As shown
in FIG. 3, the cathodic polarization curve of the base material has a step shape.
During the cathodic polarization measurements, the change in the electric current
becomes smaller relative to the change in the electric potential of the measurement
areas as the electric current approaches the state in which it becomes rate limited
owing to the diffusion of hydrogen ions. Accordingly, as shown in FIG. 3, in the cathodic
polarization curve in which the electric potential is represented by the ordinate
and the current density is represented by the abscissa, the electric-potential region
that exhibits the diffusion-limited current of the hydrogen ions contains a portion
in which the slope of the curve is steep at a step portion of the cathodic polarization
curve.
[0054] An enlarged view of the step portion in the cathodic polarization curve in FIG. 3
is shown in FIG. 4. The following is the method of determining the electric-potential
region that exhibited the diffusion-limited current of the hydrogen ions in the cathodic
polarization curve of the base material. First, a tangent L is drawn at the step portion
of the cathodic polarization curve at which the absolute value of the slope is the
largest as shown in FIG. 4. Then, region R where this tangent L and the cathodic polarization
curve overlap is taken as the electric-potential region that represents the diffusion-limited
current of the hydrogen ions. Current density J2 is calculated at the electric potential
at the center of region R determined in this manner. In addition, in the cathodic
polarization curve of the post-heated test material, current density J1 is calculated
at the electric potential the same as the electric potential at the center of the
electric-potential region in the cathodic polarization curve of the base material
as described above.
[0055] Current density J1 calculated based on the cathodic polarization curve of the post-heated
test material can be used as an indicator of the contact-surface area between the
base material of the post-heated test material and the measurement solution; the higher
the current density value, the greater the contact-surface area between the base material
and the measurement solution. Accordingly, the ratio J1/J2 of the current density
J1, calculated using the post-heated test piece, to the current density J2, calculated
using the base material, can be used as an indicator of the percentage of increase
in the surface area of the base material that was exposed by heating. More specifically,
in the situation in which, for example, defects, such as cracks, are formed in the
protective film of the post-heated test material, then the base material is sometimes
exposed by the cracks. Accordingly, the current-density ratio J1/J2 becomes large
in this situation. In Table 1, the current-density ratio J1/J2 for each test material
is shown.
[Table 1]
[0056]
(Table 1)
| |
Base Material |
Sealing Agent |
Heating of Oxide Layer |
Current-Density Ratio J1/J2 |
| Heating Temperature (°C) |
Heating Time (Minutes) |
| Test Material A1 |
AA6016 |
H-298 |
250 |
30 |
1 × 10-5 |
| Test Material A2 |
AA6016 |
H-298 |
250 |
3 |
3 × 10-5 |
| Test Material A3 |
AA6016 |
H-298 |
250 |
5 |
5 × 10-5 |
| Test Material A4 |
AA6016 |
H-298 |
250 |
10 |
6 × 10-5 |
| Test Material A5 |
AA6016 |
H-298 |
250 |
120 |
6 × 10-5 |
| Test Material A6 |
AA6016 |
H-298 |
300 |
10 |
2 × 10-5 |
| Test Material A7 |
AA6016 |
H-298 |
350 |
10 |
9 × 10-5 |
| Test Material A8 |
AA6016 |
H-298 |
400 |
10 |
12 × 10-5 |
| Test Material A9 |
AA6016 |
L-100 |
250 |
30 |
20 × 10-5 |
| Test Material A10 |
AA1050 |
H-298 |
250 |
30 |
4 × 10-5 |
| Test Material A11 |
AA3003 |
H-298 |
250 |
30 |
2 × 10-5 |
| Test Material A12 |
AA5052 |
H-298 |
250 |
30 |
3 × 10-5 |
| Test Material B1 |
AA6016 |
H-298 |
No heating |
308 × 10-5 |
| Test Material B2 |
AA6016 |
L-100 |
No heating |
734 × 10-5 |
| Test Material B3 |
AA6016 |
H-298 |
150 |
10 |
333 × 10-5 |
| Test Material B4 |
AA6016 |
H-298 |
500 |
10 |
322 × 10-5 |
| Test Material B5 |
AA1050 |
H-298 |
No heating |
120 × 10-5 |
| Test Material B6 |
AA3003 |
H-298 |
No heating |
91 × 10-5 |
| Test Material B7 |
AA5052 |
H-298 |
No heating |
396 × 10-5 |
[0057] As shown in Table 1, when Test Materials A1-A12 are being manufactured, after the
oxide layer had formed on the base material, the oxide layer is heated at a temperature
within the above-mentioned specific range before sealing the pores in the oxide layer.
Consequently, the current-density ratio J1/J2 of each of these test materials is in
the above-mentioned specific range, and the formation of cracks in the protective
film could be curtailed even in the situation in which the temperature had risen.
In addition, these test materials excelled in corrosion resistance because the oxide
layer of the protective film was sealed by the hydrated oxide layer.
[0058] In contrast, when Test Materials B1-B2, B5-B7 are being manufactured, after the oxide
layer had formed on the base material, the pores are sealed without heating the oxide
layer. Consequently, the current-density ratio J1/J2 of each of these test materials
is higher than the above-mentioned specific range, and therefore cracks tend to form
in the situation in which the temperature has risen.
[0059] When Test Material B3 was being manufactured, the heating temperature when the oxide
layer was heated was too low. Consequently, the current-density ratio J1/J2 of Test
Material B3 is higher than the above-mentioned specific range, and cracks tend to
form in the situation in which the temperature has risen.
[0060] When Test Material B4 was being manufactured, the heating temperature when the oxide
layer was heated was too high. Consequently, the current-density ratio J1/J2 of Test
Material B4 is higher than the above-mentioned specific range, and cracks tend to
form in the situation in which the temperature has risen.
[0061] The mass loss per unit of area obtained by the sealing test stipulated in JIS H8683-2:2013
and the values of the ratio A
Ni/A
H of the integrated value A
Ni of the light-emission intensities of Ni to the integrated value A
H of the light-emission intensities of hydrogen obtained by glow-discharge optical
emission spectroscopy for Test Material A1 and Test Material A10, from among Test
Materials A1-A12 of the present example, are shown in Table 2. The specific method
of the sealing test is as described above.
[0062] The measurement apparatus used for the glow-discharge optical emission spectroscopy
is the "GDA750" manufactured by SPECTRUMA GmbH. Argon gas is used in the sputtering
during GDOES, and, with regard to the sputtering conditions, the anode diameter is
set to 2.5 mm, the output is set to 25 W, and the gas pressure is set to 350 Pa. The
sputtering speed of the test materials during such conditions is approximately 40
nm/s. In addition, during GDOES, the depth-direction profile of the light-emission
intensities of each of the elements is created by acquiring the light-emission intensities
of hydrogen and Ni at 0.005-second intervals during the sputtering.
[0063] Then, using the depth-direction profile of the light-emission intensities for hydrogen,
the light-emission intensities of hydrogen at each measurement point present within
the range from the surface to the depth of 500 nm are added together, and this value
is taken as the integrated value A
H of the light-emission intensities of hydrogen. Similarly, using a depth-direction
profile of the light-emission intensities of nickel, the light-emission intensities
of nickel at each of the measurement points present within the range from the surface
to the depth of 500 nm are added together, and this value is taken as the integrated
value A
Ni of the light-emission intensities of nickel. By dividing the integrated value A
Ni of the light-emission intensities of the above-mentioned metal elements by the integrated
value A
H of the light-emission intensities of the hydrogen obtained in this manner, the value
of the ratio A
Ni/A
H can be obtained.
[0064] It is noted that Test Materials C1-C2 in Table 2 are test materials for comparison
with Test Material A1 and Test Material A10. The method of manufacturing Test Material
C1 is the same as the method of manufacturing Test Material A1 except for the point
that no sealing agent is used. The method of manufacturing Test Material C2 is the
same as the method of manufacturing Test Material A1 except for the point that boiling
water is used as the sealing agent.
[Table 2]
[0065]
(Table 2)
| |
Base Material |
Sealing Agent |
Heating of Oxide Layer |
Integrated Value of Light-Emission Intensities |
Sealing Test |
| Heating Temperature (°C) |
Heating Time (Minutes) |
ANi |
AH |
ANi/AH |
Mass-Loss Amount (g/dm2) |
| Test Material A1 |
AA6016 |
H-298 |
250 |
30 |
420 |
870 |
0.5 |
0.0031 |
| Test Material A10 |
AA6016 |
L-100 |
250 |
30 |
660 |
597 |
1.1 |
0.0124 |
| Test Material C1 |
AA6016 |
None |
250 |
30 |
- |
- |
- |
0.3819 |
| Test Material C2 |
AA6016 |
Boiling water |
250 |
30 |
0 |
1505 |
0.0 |
- |
[0066] As shown in Table 2, in the situation in which the sealing test was performed, the
mass loss per unit of area of Test Material A1 and Test Material A10 is 0.3 g/dm
2 or less. In contrast, the mass loss per unit of area of Test Material C1, for which
no sealing treatment is performed, is greater than 0.3 g/dm
2. Accordingly, it can be understood from comparing Test Material A1 and Test Material
A10 with Test Material C1 that the pores in the oxide layer of Test Material A1 and
Test Material A10 are sufficiently closed up. In addition, because the sealing treatment
is performed for Test Materials A2-A9, A11-A12 under the same conditions as those
of Test Material A1 and Test Material A10, it can be presumed that the pores in the
oxide layer of these test materials as well are also sufficiently closed up.
[0067] In addition, the values of ratio A
Ni/A
H in Test Material A1 and Test Material A10 are within the range of 0.1 or more and
5.0 or less. In contrast, the value of ratio A
Ni/A
H for Test Material C2, which uses a sealing agent that does not contain nickel, is
0. Accordingly, it can be understood from comparing Test Material A1 and Test Material
A10 with Test Material C2 that the protective film, which includes the above-mentioned
metal element, can be formed by contacting the oxide layer with the sealing agent,
which includes the above-mentioned metal element.
(Working Example 2)
[0068] In the present example, an example is explained in which heat resistance was evaluated
for the situation in which heating was performed at temperatures higher than those
in Working Example 1. In the present example, Test Materials A1-A2 and Test Materials
B1-B2 are prepared by the same method as that in Working Example 1, and these test
materials are heated for 4 hours in an oven set to a temperature of 250°C. Thereafter,
the cathodic polarization measurements are performed using the same method as that
in Working Example 1, and the current-density ratios J1/J2 are computed. In Table
3, current-density ratios J1/J2 of Test Materials A1-A2 and Test Materials B1-B2 are
shown.
[Table 3]
[0069]
(Table 3)
| |
Base Material |
Sealing Agent |
Heating of Oxide Layer |
Current-Density Ratio J1/J2 |
| Heating Temperature (°C) |
Heating Time (Minutes) |
| Test Material A1 |
AA6016 |
H-298 |
250 |
30 |
53 × 10-5 |
| Test Material A2 |
AA6016 |
H-298 |
250 |
3 |
79 × 10-5 |
| Test Material B1 |
AA6016 |
H-298 |
No heating |
280 × 10-5 |
| Test Material B2 |
AA6016 |
L-100 |
No heating |
1162 × 10-5 |
[0070] As shown in Table 3, current-density ratios J1/J2 of Test Materials A1-A2, in which
the sealing treatment is performed after the oxide layer has been heated, become lower
than current-density ratios J1/J2 of Test Materials B1-B2, in which heating of the
oxide layer is not performed, even in the situation in which heating is performed
at a temperature of 250°C. Accordingly, from these results as well, it can be understood
that the heat resistance of the above-mentioned aluminum material can be increased
by performing the sealing treatment after heating of the oxide layer has been performed.
(Reference Example)
[0071] In the present example, measurements of the amounts of strain in aluminum materials
having the protective film on the base material will be explained. It is noted that,
among the symbols used in the present example, unless particularly explained, the
symbols that are the same as the symbols used in previously discussed examples indicate
structural elements, etc. the same as structural elements, etc. in the previously
discussed examples.
[0072] The method of manufacturing the test materials in the present example is as follows.
First, an aluminum sheet having the chemical composition indicated by the alloy number
AA6016 and having a thickness of 1.1 mm is prepared as the base material 2. Pretreatments
of the anodizing treatment are performed on this base material 2 using methods similar
to those in the working example, and next the anodizing treatment is performed. After
having performed the anodizing treatment, the base material 2 is heated inside a heating
furnace and the internal stresses in the oxide layer 31 are relaxed. The set temperature
of the heating furnace is the value shown in the "Heating Temperature" column in Table
4, the residence time of the base material inside the furnace, that is, the time from
the start of heating to the end of heating, is the value shown in the "Heating Time"
column in Table 4.
[0073] Thereafter, by immersing the base material 2, which has the oxide layer 31, in boiling
water as the sealing agent for 60 min, the hydrated oxide layer 32 forms on the oxide
layer 31, and the pores 311 in the oxide layer 31 are sealed by the hydrated oxide
layer 32. Based on the above, Test Material D1 shown in Table 1 could be obtained.
[0074] It is noted that Test Material E1 shown in Table 4 is a test material for comparison
with Test Material D1, The method of manufacturing Test Material E1 is the same as
the method of manufacturing Test Materials D1 except that, after the oxide layer 31
was formed on the base material 2, the oxide layer 31 is contacted with the sealing
agent without being heated. In addition, the base materials shown in Table 4 are obtained
by performing pretreatments of the anodizing treatment, using the methods described
above, on a sheet material composed of an aluminum alloy having the chemical composition
indicated by the alloy number AA6016.
[0075] To measure the amount of strain in the aluminum materials 1 that comprise Test Material
D1 and Test Material E1, the base material 2 of the aluminum material 1 is exposed
on the rear surface of the surface having the protective film 3, as shown in FIG.
5. Then, a strain gauge 4 is mounted on the exposed base material 2. The strain during
heating of the base material 2 and the protective film 3 can be measured by heating
the aluminum material 1 on which the strain gauge 4 was mounted in the aforementioned
manner. It is noted that the structure of the protective film 3 is simplified in FIG.
5 for the sake of convenience of explanation.
[0076] Although not shown in the drawing, to measure the amount of strain in the base material
2, after the strain gauge has been mounted on one of the surfaces in the thickness
direction of the base material 2, the base material 2 should be heated.
[0077] In FIG. 6, changes in the amounts of strain are shown in the situation in which Test
Material D1, Test Material E1, and the base material were heated for 30 min using
the heating furnace, which was set to a temperature of 200°C. In FIG. 6, the ordinate
is the amount of strain and the abscissa is the time elapsed since the start of heating.
Because the test materials immediately after the start of heating underwent thermal
expansion commensurate with the temperature rise, as shown in FIG. 6, the respective
amounts of strain increased sharply from the point in time when the test started up
until several minutes elapsed thereafter. Thereafter, when the temperatures of the
test material and the base material reached a roughly constant temperature, the respective
amounts of strain of the test material and the base material became roughly constant
values.
[0078] In Table 4, the maximum value of the amounts of strain while the test materials and
the base material were being heated is shown. In addition, value ε1 - ε2 resulting
from subtracting the maximum value ε2 of the amount of strain of the base material
from the maximum value ε1 of the amount of strain of the corresponding test material
is shown in Table 4. The difference ε1 - ε2 between the amount ε1 of strain of the
corresponding test material and the amount ε2 of strain of the base material indicates
the magnitude of the internal stresses in the protective film released by the heating
during the test; this means that the smaller the difference ε1 - ε2 of the amounts
of strain, the smaller the internal stresses in the protective film.
[Table 4]
[0079]
(Table 4)
| |
Base Material |
Sealing Agent |
Protective Film |
Heating of Oxide Layer |
Maximum Value of Strain Amount |
Difference Between Strain Amounts ε1-ε2 |
| Heating Temperature (°C) |
Heating Time (Minutes) |
| Test Material D1 |
A6016 |
Boiling water |
Present |
250 |
60 |
2298 × 10-6 |
-11 × 10-6 |
| Test Material E1 |
A6016 |
Boiling water |
Present |
No heating |
2461 × 10-6 |
152 × 10-6 |
| Base Material |
A6016 |
None |
Not present |
No heating |
2309 × 10-6 |
- |
[0080] As shown in Table 4, the amount of strain of Test Material D1, on which the hydrated
oxide layer is formed after the oxide layer is heated during the process of manufacturing
the test material, is smaller than the amount of strain of Test Material E1, on which
the hydrated oxide layer is formed without heating the oxide layer. It is conceivable
that this is because the internal stresses of the oxide layer were relaxed by the
heating of the oxide layer. In addition, it is conceivable that the internal stresses
of the protective film are substantially unchanged during the sealing treatment performed
after the heating of the oxide layer. Accordingly, from these results, it is presumed
that, even for Test Materials A1-A12 of Working Example 1, the difference ε1 - ε2
between the amount ε1 of strain of each of the test materials and the amount ε2 of
strain of the base material will become within the above-mentioned specific range,
and the internal stresses of the protective film will be relaxed.
[0081] Aspects of the surface-treated aluminum material and the method of manufacturing
the same according to the present invention were described above based on the working
examples; however, the specific aspects of the surface-treated aluminum material and
the method of manufacturing the same according to the present invention are not limited
to the aspects in the working examples, and the constitutions thereof can be modified,
as appropriate, within a scope that does not depart from the gist of the present invention.
[0082] For example, the surface-treated aluminum material according to the present invention
can obtain the aspects according to [1]-[4] below.
- [1] A surface-treated aluminum material comprising: a base material, which is composed
of aluminum or an aluminum alloy; and a protective film, which is formed on the base
material; wherein:
the protective film is composed of an oxide or oxides of aluminum, and has:
an oxide layer, which covers the base material; and
a hydrated oxide layer, which covers the oxide layer;
the hydrated oxide layer contains:
a hydrated oxide or hydrated oxides of aluminum; and
a metal oxide or metal oxides and/or a metal hydroxide or metal hydroxides containing
one or two or more metal elements selected from the group consisting of Ni, Cr, Zr,
Si, Ti, Au, Ag, Co, Mo, Mn, Nb, Ta, W, Zn, Fe, Ir, and Sc; and
in the situation in which cathode polarization measurements are performed-using a
measurement solution obtained by mixing a solution of NaCl having a concentration
of 5 mass% and acetic acid having a concentration of 99.7% such that the volumetric
ratio of the NaCl solution to the acetic acid = 1000:1-on the base material and on
the surface-treated aluminum material after it had been heated for 4 hours at a temperature
of 200°C, and the current density at the electric potential at the center of an electric-potential
region of the base material that exhibits the diffusion-limited current of hydrogen
ions was measured, the ratio J1/J2 of the current density J1 of the surface-treated
aluminum material to the current density J2 of the base material is 90 × 10-5 or less.
- [2] A surface-treated aluminum material comprising: a base material, which is composed
of aluminum or an aluminum alloy; and a protective film, which is formed on the base
material; wherein:
the protective film is composed of an oxide or oxides of aluminum, and has:
an oxide layer, which covers the base material; and
a hydrated oxide layer, which covers the oxide layer;
the hydrated oxide layer contains:
a hydrated oxide or hydrated oxides of aluminum; and
a metal oxide or metal oxides and/or a metal hydroxide or metal hydroxides containing
one or two or more metal elements selected from the group consisting of Ni, Cr, Zr,
Si, Ti, Au, Ag, Co, Mo, Mn, Nb, Ta, W, Zn, Fe, Ir, and Sc; and
a sample having the protective film on one surface of the base material was prepared
from the surface-treated aluminum material and measured in a state in which a strain
gauge is mounted on the sample on a rear surface having the protective film, the difference
ε1 - ε2 between the amount ε1 of strain of the sample at a temperature of 200°C and
the amount ε2 of strain of the base material at a temperature of 200°C is 100 × 10-6 or less.
- [3] The surface-treated aluminum material according to [1] or [2], wherein the mass
loss per unit of area is 0.3 g/dm2 or less in the situation in which a sealing degree test has been performed using
the method stipulated in JIS H8683-2:2013.
- [4] The surface-treated aluminum material according to any one of [1] to [3], wherein
a ratio AM/AH of the integrated value AM of light-emission intensities of the metal element(s) to the integrated value AH of the light-emission intensities of hydrogen measured in a range from a surface
of the aluminum material to a depth of 500 nm by glow-discharge optical emission spectroscopy
is 0.1 or more and 5.0 or less.
A metal casing according to the present invention may take the form according to [5]
below.
- [5] A metal casing composed of the surface-treated aluminum material according to
any one of [1] to [4].
A kitchen appliance according to the present invention may take the form according
to [6] below.
- [6] A kitchen appliance comprising the metal casing according to [5].
A method of manufacturing the surface-treated aluminum material according to the present
invention can obtain the aspects according to [7]-[10] below.
- [7] A method of manufacturing the surface-treated aluminum material according to any
one of [1]-[4], comprising:
forming the oxide layer, which has pores, on the base material by performing an anodizing
treatment on the base material;
thereafter, heating the base material and the oxide layer at a temperature of 200°C
or higher and 400°C or lower; and
thereafter, contacting the oxide layer with a sealing agent that contains the metal
element(s), thereby forming the hydrated oxide layer on the oxide layer and sealing
the pores.
- [8] The method of manufacturing the surface-treated aluminum material according to
[7], wherein, during the heating, the heating time from the start of heating the oxide
layer to the end of heating is 1 min or more and less than 12 hours.
- [9] The method of manufacturing the surface-treated aluminum material according to
[7] or [8], wherein the electrolyte solution employed in the anodizing treatment contains
an inorganic electrolyte composed of an inorganic cation and one or two or more anions
selected from the group consisting of a sulfate ion, a phosphate ion, and a borate
ion.
- [10] The method of manufacturing the surface-treated aluminum material according to
any one of [7] to [9], wherein the sealing agent is an aqueous solution that contains
ions of the metal element(s).