Technical Field
[0001] The present disclosure relates to a coated steel material and a method for manufacturing
a coated steel material.
Background Art
[0002] A wide variety of coated steel materials are used, for example, in the field of construction
materials. Many of them are Zn-coated steel materials. Due to the need for having
a long life for construction materials, research on improving the corrosion resistance
of Zn-coated steel materials has been conducted over a long time, and various coated
steel materials have been developed. The first high corrosion resistant coated steel
material for construction materials was a Zn-5% Al coated steel material (Galfan coated
steel material), in which Al was added to a Zn-based coating layer to improve the
corrosion resistance. It is a well-known fact that the corrosion resistance is improved
by addition of Al into a coating layer, and by addition of 5% of Al, Al phase are
formed in the coating layer (specifically Zn phase) and the corrosion resistance is
improved. A Zn-55% Al-1.6% Si coated steel material (Galvalume steel product) is also
a coated steel material, in which corrosion resistance is basically improved for the
same reason.
[0003] The attractive feature of a Zn-based coated steel material is the sacrificial corrosion
protection effect on a base steel. In other words, in a cut edge of a coated steel
material, a cracked portion of a coating layer generated at the time of forming, and
an exposed portion of a base steel which appears, for example, by exfoliation of a
coating layer, the coating layer in the vicinity of such portions dissolves out before
corrosion of the base steel, and the dissolved coating component forms a protective
film. This makes it possible to prevent rusting in the base steel to some extent.
[0004] In general, such effects are preferable in a case of a lower Al concentration and
a higher Zn concentration. Accordingly, a high corrosion-resistant coated steel material
in which the Al concentration is reduced to a relatively low concentration of about
from 5% to 25% has been available for practical use in recent years. In particular,
a coated steel material, in which the Al concentration is suppressed at a low level
and Mg is contained at about from 1% to 3%, has superior corrosion resistance with
respect to the Galfan coated steel material. Therefore, this has become a market trend
in coated steel materials, and widely known in the market at present.
[0005] As such a coated steel material containing a certain amount of Al and Mg, for example,
a coated steel material disclosed in Patent Literature 1 has been also developed.
[0006] Specifically, Patent Literature 1 discloses "a hot dip Zn-Al-Mg-Si coated steel material
in which 200 or more Al phases exist per 1 mm
2 on the surface of a coated steel material having a coating layer composed of from
5% to 18% by mass of Al, from 1% to 10% by mass of Mg, from 0.01% to 2% by mass of
Si, and the balance of Zn and unavoidable impurities".
[0007] In addition, Patent Literature 2 discloses "a coated steel material including a steel
product, and a coating layer including a Zn-Al-Mg alloy layer provided on a surface
of the steel product, in which the coatcoating layer has a chemical composition composed
of Zn at more than 65.0%, Al at more than 5.0% and less than 25.0%, Mg at more than
3.0% and less than 12.5%, and Sn at from 0.1% to 20.0%, and in a backscattered electron
image of the Zn-Al-Mg alloy layer, obtained by polishing a surface of the Zn-Al-Mg
alloy layer to 1/2 of a layer thickness, and observing the surface at a magnification
of 100 x with a scanning electron microscope, Al phase are present, and an average
value of a cumulative circumferential length of the Al phase is from 88 to 195 mm/mm
2".
Citation List
Patent Literature
SUMMARY OF INVENTION
Technical Problem
[0009] In a Zn-Al-Mg-based alloy coated steel material having a high Al concentration and
a high Mg concentration, corrosion resistance is superior to that of a Zn-based coated
steel material in a heavy salt damage region in which the amount of airborne chlorides
is large and the corrosion environment is severe, but white rust tends to be generated
soon after construction. In addition, since coating with a high Mg concentration is
likely to cause oxidative discoloration and the coating is hard, formability may be
poor.
[0010] Therefore, an object of the disclosure is to provide a coated steel material which
is excellent in corrosion resistance even in a heavy salt damage region and can achieve
both formability and discoloration resistance, and a method for manufacturing the
coated steel material.
Solution to Problem
[0011] The above object is achieved by the following means.
<1> A coated steel material including a base steel and a coating layer including a
Zn-Al-Mg alloy layer provided on a surface of the base steel and a Mg enrichment layer
provided on a surface of the Zn-Al-Mg alloy layer,
in which the coating layer has a chemical composition composed of, in terms of % by
mass:
Zn at more than 65.00%,
Al at more than 5.00% and less than 25.00%,
Mg at more than 3.00% and less than 12.50%,
Sn at from 0% to 3.0%,
Bi at from 0% to less than 5.00%,
In at from 0% to less than 2.00%,
Ca at from 0% to 3.00%,
Y at from 0% to 0.50%,
La at from 0% to less than 0.50%,
Ce at from 0% to less than 0.50%,
Si at from 0% to less than 2.5%,
Cr at from 0% to less than 0.25%,
Ti at from 0% to less than 0.25%,
Zr at from 0% to less than 0.25%,
Mo at from 0% to less than 0.25%,
W at from 0% to less than 0.25%,
Ag at from 0% to less than 0.25%,
P at from 0% to less than 0.25%,
Ni at from 0% to less than 0.25%,
Co at from 0% to less than 0.25%
V at from 0% to less than 0.25%,
Nb at from 0% to less than 0.25%,
Cu at from 0% to less than 0.25%,
Mn at from 0% to less than 0.25%,
Li at from 0% to less than 0.25%,
Na at from 0% to less than 0.25%,
K at from 0% to less than 0.25%,
Fe at from 0% to 5.0%,
Sr at from 0% to less than 0.5%
Sb at from 0% to less than 0.5%
Pb at from 0% to less than 0.5%,
B at from 0% to less than 0.5%, and
impurities,
in the Zn-Al-Mg alloy layer, a total area ratio of Al phase, MgZn2, phase, and Zn/Al/MgZn2 ternary eutectics is 90% or more, and
a thickness of the Mg enrichment layer is 0.8 µm or more and (thickness of coating
layer × 1/2) or less.
<2> The coated steel material according to <1>, in which the coating layer has an
Al-Fe alloy layer between the base steel and the Zn-Al-Mg alloy layer.
<3> A method for manufacturing the coated steel material according to <1> or <2>,
in which a base steel is immersed in a hot-dip coating bath and pulled up from the
hot-dip coating bath, and then cooled down in a temperature range of from 450°C to
395°C at an average cooling rate of 15°C/s or less, cooled down in a temperature range
of from 395°C to 340°C at an average cooling rate of 3°C/s or less, and cooled down
in a temperature range of from 340°C to 280°C at an average cooling rate of from 10
to 20°C/s or more, and
after the cooling, subjected to skin pass rolling under conditions that a surface
roughness Ra of a skin pass roll is from 1 to 5 µm and a skin pass rolling force is
from 100 to 500 ton.
Advantageous Effects of Invention
[0012] Therefore, according to the disclosure, it is possible to provide a coated steel
material which is excellent in corrosion resistance even in a heavy salt damage region
and can achieve both formability and discoloration resistance, and a method for manufacturing
the coated steel material.
BRIEF DESCRIPTION OF DRAWINGS
[0013] Fig. 1 is a graph for explaining a method for measuring a thickness of a Mg enrichment
layer.
DESCRIPTION OF EMBODIMENTS
[0014] An example of the disclosure will be described below.
[0015] In the disclosure, the expression of "%" with respect to the content of each element
of a chemical composition means "% by mass".
[0016] A numerical range expressed using "to" means a range including the numerical values
stated before and after "to" as the upper limit and lower limit.
[0017] In a case where the numerical values stated before and after "to" are denoted with
the term "more than" or "less than", the numerical range means a range not including
the numerical value as the upper limit or lower limit.
[0018] The content of an element of a chemical composition may be expressed as an element
concentration (for example, Zn concentration and Mg concentration).
[0019] A coated steel material according to the disclosure includes a base steel and a coating
layer including a Zn-Al-Mg alloy layer provided on a surface of the base steel and
a Mg enrichment layer provided on a surface of the Zn-Al-Mg alloy layer.
[0020] In the Zn-Al-Mg alloy layer, a total area ratio of Al phase, MgZn
2 phase, and Zn/Al/MgZn
2 ternary eutectics is 90% or more.
[0021] Also, a thickness of the Mg enrichment layer is 0.8 µm or more and (thickness of
coating layer × 1/2) or less.
[0022] Since the coated steel material of the disclosure has the Mg enrichment layer of
the Zn-Al-Mg alloy layer on the surface of the Zn-Al-Mg alloy layer, a dense corrosion
product film containing Mg is formed soon in the early stage of corrosion. The dense
corrosion product film reduces a corrosion rate. Therefore, corrosion resistance is
excellent even in a heavy salt damage region in which the amount of airborne chlorides
is large and the corrosion environment is severe. When setting a chemical composition
of a coating layer and a range of the Mg enrichment layer to appropriate ranges, both
formability and discoloration resistance can be achieved.
[0023] In addition, when the Zn-Al-Mg alloy layer having the above structure is present
below the Mg enrichment layer, Mg ions and Al ions are supplied to the corrosion environment
from the middle to the late stage of corrosion while securing formability. Accordingly,
a dense corrosion product film is maintained, and therefore corrosion resistance is
improved.
[0024] The coated steel material of the disclosure will be described in detail below.
(Base Steel)
[0025] There is no particular restriction on the shape of the base steel. Examples of the
base steel include besides a steel sheet, shape formed base steel, such as a steel
pipe, a civil engineering and building material (such as fence conduit, corrugated
pipe, drain ditch cover, wind-blown sand preventing coate, bolt, wire mesh, guardrail,
and cut-off wall), a home electrical appliance component (such as housing for an air
conditioner outdoor unit), and an automobile part (such as a suspension system component).
For shape forming, for example, various plastic working methods, such as press working,
roll forming, and bending, can be used.
[0026] There is no particular restriction on the material of the base steel. As the base
steel, there are various applicable base steels, and examples thereof include general
steel, precoated steel, Al killed steel, ultra-low carbon steel, high carbon steel,
various high tensile strength steels, and some high alloy steels (for example, steel
containing a strengthening element such as Ni and Cr).
[0027] With respect to the base steel, there is also no particular restriction on the method
for manufacturing a base steel, or the conditions of a method for manufacturing a
base steel sheet (such as a hot rolling method, a pickling method, and a cold rolling
method).
[0028] In addition, as the base steel, a hot-rolled steel sheet, a hot-rolled steel strip,
a cold rolled steel sheet, and a cold rolled steel strip described in JIS G 3302 (2010)
are also applicable.
[0029] The base steel may be a precoated steel material which has been precoated. A precoated
steel material is obtained, for example, by an electrolytic treatment method or a
displacement coating method. In the electrolytic treatment method, a base steel is
immersed in a sulfate bath or chloride bath containing various metal ions corresponding
to precoating components, and an electrolytic treatment is performed to obtain a precoated
steel material. In the displacement coating method, a base steel is immersed in an
aqueous solution, which contains various metal ions corresponding to precoating components,
and of which a pH has been adjusted with sulfuric acid, for causing displacement deposition
of a metal to obtain a precoated steel material.
[0030] Typical examples of a precoated steel material include a Ni precoated steel material.
(Coating Layer)
[0031] The coating layer includes a Zn-Al-Mg alloy layer and a Mg enrichment layer provided
on a surface of the Zn-Al-Mg alloy layer. The coating layer may include an Al-Fe alloy
layer in addition to the Zn-Al-Mg alloy layer and the Mg enrichment layer. The Al-Fe
alloy layer is provided between the base steel and the Zn-Al-Mg alloy layer.
[0032] That is, the coating layer may have a laminated structure including the Zn-Al-Mg
alloy layer, the Mg enrichment layer, and the Al-Fe alloy layer.
[0033] Although there are some cases where an oxide film of a constituent element of the
coating layer is formed on the surface of the coating layer in a thickness of about
50 nm, a thickness thereof is thin relative to the thickness of the entire coating
layer (about from 8 to 60 µm) such that the oxide film is deemed not to constitute
a main part of the coating layer.
[0034] A deposited amount of the coating layer is preferably from 40 to 300 g/m
2 per one surface.
[0035] When the deposited amount of the coating layer is 40 g/m
2 or more, corrosion resistance can be ensured more reliably. Also, when the deposited
amount of the coating layer is 300 g/m
2 or less, appearance defects such as sagging patterns of the coating layer can be
suppressed.
[0036] Next, the chemical composition of the coating layer will be described.
[0037] The chemical composition of the coating layer is a chemical composition composed
of, in terms of % by mass:
Zn at more than 65.00%,
Al at more than 5.00% and less than 25.00%,
Mg at more than 3.00% and less than 12.50%,
Sn at from 0% to 3.00%,
Bi at from 0% to less than 5.00%,
In at from 0% to less than 2.00%,
Ca at from 0% to 3.00%,
Y at from 0% to 0.50%,
La at from 0% to less than 0.50%,
Ce at from 0% to less than 0.50%,
Si at from 0% to less than 2.5%,
Cr at from 0% to less than 0.25%,
Ti at from 0% to less than 0.25%,
Zr at from 0% to less than 0.25%,
Mo at from 0% to less than 0.25%,
W at from 0% to less than 0.25%,
Ag at from 0% to less than 0.25%,
P at from 0% to less than 0.25%,
Ni at from 0% to less than 0.25%,
Co at from 0% to less than 0.25%
V at from 0% to less than 0.25%,
Nb at from 0% to less than 0.25%,
Cu at from 0% to less than 0.25%,
Mn at from 0% to less than 0.25%,
Li at from 0% to less than 0.25%,
Na at from 0% to less than 0.25%,
K at from 0% to less than 0.25%,
Fe at from 0% to 5.00%,
Sr at from 0% to less than 0.50%
Sb at from 0% to less than 0.50%
Pb at from 0% to less than 0.50%,
B at from 0% to less than 0.50%, and
impurities.
[0038] In the chemical composition of the coating layer, Sn, Bi, In, Ca, Y, La, Ce, Si,
Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu, Mn, Li, Na, K, Fe, Sr, Sb, Pb, and B
are optional components. In other words, these elements need not be contained in the
coating layer. When any of these optional components is contained, the content of
each optional element is preferably in the range described below.
[0039] Here, the chemical composition of the coating layer is an average chemical composition
of the entire coating layer (an average chemical composition of all of the Zn-Al-Mg
alloy layer and the Mg enrichment layer or an average chemical composition of all
of the Al-Fe alloy layer, the Zn-Al-Mg alloy layer, and the Mg enrichment layer).
[0040] Each element of a coating layer will be described below.
Zn at More Than 65.00%
[0041] Zn is an element necessary for obtaining corrosion resistance. As for Zn concentration
in terms of the atomic composition ratio, since the coating layer is composed together
with elements having a low specific gravity such as Al and Mg, Zn is required to occupy
the main portion also in the atomic composition ratio.
[0042] Therefore, the Zn concentration is set above 65.00%. The Zn concentration is preferably
70.00% or more. In this regard, the upper limit of the Zn concentration is a remnant
concentration excluding elements other than Zn, and impurities.
Al at More Than 5.00% and Less Than 25.00%
[0043] Al is an essential element for forming Al phase and ensuring corrosion resistance.
Also, Al is an essential element for enhancing the adhesion of a coating layer and
ensuring the formability. Therefore, the lower limit of the Al concentration is set
above 5.00% (preferably at 10.00% or more).
[0044] Meanwhile, when the Al concentration increases too much, the corrosion resistance
tends to deteriorate. Therefore, the upper limit of the Al concentration is set below
25.00% (preferably at 23.00% or less).
Mg at More Than 3.00% and Less Than 12.50%
[0045] Mg is an essential element for ensuring corrosion resistance. Therefore, the lower
limit of the Mg concentration is set above 3.00% (preferably above 4.00%).
[0046] Meanwhile, when the Mg concentration increases too much, the formability tends to
deteriorate. Therefore, the upper limit of the Mg concentration is set at lower than
12.50% (preferably at 10.00% or less).
Sn at from 0% to 3.00%
[0047] Sn is an element that contributes to corrosion resistance and initial discoloration
resistance. Therefore, the lower limit of the Sn concentration is preferably more
than 0.00% (preferably 0.05% or more, and more preferably 0.10% or more).
[0048] Meanwhile, when the Sn concentration increases too much, corrosion resistance and
initial discoloration resistance tend to deteriorate. Therefore, the upper limit of
the Sn concentration is set at 3.00% or less.
Bi at from 0% to Less Than 5.00%
[0049] Bi is an element that contributes to corrosion resistance. Therefore, the lower limit
of the Bi concentration is preferably more than 0.00% (preferably 0.10% or more, and
more preferably 3.00% or more).
[0050] Meanwhile, when the Bi concentration increases too much, the corrosion resistance
tends to deteriorate. Therefore, the upper limit of the Bi concentration is set below
5.00% (preferably at 4.80% or less).
In at from 0% to Less Than 2.00%
[0051] In is an element that contributes to corrosion resistance. Therefore, the lower limit
of the In concentration is preferably more than 0.00% (preferably 0.10% or more, and
more preferably 1.00% or more).
[0052] Meanwhile, when the In concentration increases too much, the corrosion resistance
tends to deteriorate. Therefore, the upper limit of the In concentration is set below
2.00% (preferably at 1.80% or less).
Ca at from 0% to 3.00%
[0053] Ca is an element capable of adjusting the dissolution amount of Mg to a level optimal
for imparting corrosion resistance. Therefore, the lower limit of the Ca concentration
is preferably more than 0.00% (preferably 0.05% or more).
[0054] Meanwhile, when the Ca concentration increases too much, the corrosion resistance
and formability tend to deteriorate. Therefore, the upper limit of the Ca concentration
is set at 3.00% or less (preferably at 1.00% or less).
Y at from 0% to 0.50%
[0055] Y is an element that contributes to corrosion resistance. Therefore, the lower limit
of the Y concentration is preferably more than 0.00% (preferably 0.10% or more).
[0056] Meanwhile, when the Y concentration increases too much, the corrosion resistance
tends to deteriorate. Therefore, the upper limit of the Y concentration is set at
0.50% or less (preferably at 0.30% or less).
La And Ce at from 0% to Less Than 0.50%
[0057] La and Ce are elements that contribute to corrosion resistance. Therefore, the lower
limit of each of the La concentration and Ce concentration is preferably more than
0.00% (preferably 0.10% or more).
[0058] Meanwhile, when the La concentration or the Ce concentration increases too much,
the corrosion resistance tends to deteriorate. Therefore, the upper limit of each
of the La concentration and the Ce concentration is set below 0.50% (preferably at
0.40% or less).
Si at from 0% to Less Than 2.50%
[0059] Si is an element that contributes to improvement of the corrosion resistance by suppressing
growth of an Al-Fe alloy layer. Therefore, the Si concentration is preferably more
than 0.00% (preferably 0.05% or more, and more preferably 0.10% or more). In particular,
when Sn is not contained (that is, when the Sn concentration is 0%), the Si concentration
is preferably 0.10% or more (preferably 0.20% or more) from the viewpoint of ensuring
corrosion resistance.
[0060] Meanwhile, when the Si concentration increases too much, the corrosion resistance
and formability tend to deteriorate. Therefore, the upper limit of the Si concentration
is set below 2.50%. In particular, from the viewpoint of corrosion resistance, the
Si concentration is preferably 2.40% or less, more preferably 1.80% or less, and further
preferably 1.20% or less.
[0061] Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu, Mn, Li, Na, and K at from 0% to Less
Than 0.25%
[0062] Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu, Mn, Li, Na, and K are elements that
contribute to corrosion resistance. Therefore, the lower limit of the concentration
of each of Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu, Mn, Li, Na and K is preferably
more than 0% (preferably 0.05% or more, and more preferably 0.10% or more).
[0063] Meanwhile, when the concentration of Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu,
Mn, Li, Na, or K increases too much, corrosion resistance tends to deteriorate. Therefore,
the upper limit of the concentration of each of Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co,
V, Nb, Cu, Mn, Li, Na, and K is set below 0.25%. The upper limit of the concentration
of Cr, Ti, Zr, Mo, W, Ag, P, Ni, Co, V, Nb, Cu, Mn, Li, Na, or K is preferably 0.22%
or less.
Fe at from 0% to 5.00%
[0064] When a coating layer is formed by a hot dip metal coating method, Fe is contained
in a Zn-Al-Mg alloy layer and an Al-Fe alloy layer at certain concentrations.
[0065] It has been confirmed that there is no adverse effect on the performance, even when
Fe is contained in a coating layer (particularly a Zn-Al-Mg alloy layer), up to a
concentration of 5.00%. Since most of the Fe is contained in an Al-Fe alloy layer
in many cases, when the thickness of this layer is large, the Fe concentration generally
increases.
Sr, Sb, Pb, and B at from 0% to Less Than 0.50%
[0066] Sr, Sb, Pb, and B are elements that contribute to corrosion resistance. Therefore,
the lower limit of the concentration of each of Sr, Sb, Pb, and B is preferably more
than 0% (preferably 0.05% or more, and more preferably 0.10% or more).
[0067] Meanwhile, when the concentration of Sr, Sb, Pb, or B increases too much, the corrosion
resistance tends to deteriorate. Therefore, the upper limit of the concentration of
each of Sr, Sb, Pb, and B is set below 0.50%.
Impurities
[0068] Impurities refer to components contained in raw materials, or components to be mixed
in in the manufacturing process, which are not intentionally added. For example, in
a coating layer, trace amounts of components other than Fe may be mixed in as impurities
in a coating layer by mutual atomic diffusion between a base steel and a hot-dip coating
bath.
[0069] The chemical components of a coating layer are measured by the following method.
[0070] First, an acid solution in which a coating layer is separated and dissolved with
an acid containing an inhibitor that inhibits the corrosion of a base steel is prepared.
Next, the chemical composition of the coating layer can be obtained by measuring the
obtained acid solution by ICP analysis. There is no particular restriction on the
acid species, insofar as it is an acid capable of dissolving the coating layer. The
chemical composition is measured as an average chemical composition. In the ICP analysis,
the Zn concentration is determined from "Formula: Zn concentration = 100% - Concentration
(%) of other elements".
[0071] Here, when a precoated steel material is used as a base steel, a component of the
precoating is also detected.
[0072] For example, when a Ni precoated steel material is used, not only Ni in the coating
layer but also Ni in the Ni precoating is detected in the ICP analysis. Specifically,
for example, when a precoated steel material having a Ni deposited amount of from
1 g/m
2 to 3 g/m
2 (thickness of about 0.1 to 0.3 µm) is used as a base steel, even if the concentration
of Ni contained in the coating layer is 0%, the Ni concentration is detected as from
0.1% to 15% when measured by the ICP analysis.
[0073] Here, a method for determining whether a base steel is a Ni precoated steel material
is as follows.
[0074] A sample in which a cross section cut along the thickness direction of the coating
layer serves as a measurement surface is collected from a target steel product.
[0075] The vicinity of the interface between the coating layer and the base steel in the
steel product is linearly analyzed by an electron probe microanalyzer (FE-EPMA) on
the measurement surface of the sample to measure the Ni concentration. The measurement
conditions are an acceleration voltage of 15 kV, a beam diameter of about 100 nm,
irradiation time per point of 1000 ms, and a measurement pitch of 60 nm. A measurement
distance may be any distance insofar as it is possible to confirm whether or not the
Ni concentration is concentrated at the interface between a coating layer and a base
steel in a steel product.
[0076] When the Ni concentration is concentrated at the interface between a coating layer
and a base steel in the steel product, the base steel is discriminated as a Ni precoated
steel material.
[0077] When a Ni precoated steel material is used as a base steel, the Ni concentration
of the coating layer is defined as a value measured as follows.
[0078] First, with a high frequency glow discharge emission surface analyzer (GDS: manufactured
by HORIBA, Ltd., model number: GD-Profiler2), the emission intensity of Ni is measured
for three or more kinds of standard samples (Zn alloy standard samples IMN ZH1, ZH2,
and ZH4 manufactured by BAS) having different Ni concentrations. A calibration curve
is prepared from the relationship between the obtained emission intensity of Ni and
the Ni concentration in the standard test.
[0079] Next, the surface of the coating layer of the sample is polished in the thickness
direction of the coating layer (hereinafter also referred to as "Z-axis direction").
[0080] Specifically, the surface of the coating layer is dry-polished with a #1200 abrasive
sheet, and then finish-polishing is carried out successively using a finishing liquid
containing alumina having an average particle diameter of 3 µm, a finishing liquid
containing alumina having an average particle diameter of 1 µm, and a finishing liquid
containing colloidal silica in the mentioned order.
[0081] In doing so, the Zn intensity in the surface of the coating layer is measured by
XRF (X-ray fluorescence analysis) before and after the polishing, and when the Zn
intensity after the polishing reduces to 1/2 the Zn intensity before the polishing,
the then thickness of the coating layer is deemed as the 1/2 layer thickness.
[0082] Next, the emission intensity of Ni at a position where a film thickness of a coating
layer of a coated steel material to be measured is 1/2 is measured by the high frequency
glow discharge emission surface analyzer (GDS: manufactured by HORIBA, model number:
GD-Profiler2). The Ni concentration at the position of 1/2 of the coating layer is
determined from the obtained emission intensity of Ni and the prepared calibration
curve.
[0083] When a Ni precoated steel material is used as a base steel, the Zn concentration
of the coating layer is defined as a Zn concentration calculated from the following
formula.
Zn concentration = 100 - (Concentration of elements other than Zn and Ni determined
by ICP analysis + Ni concentration determined by GDS)
[0084] Measurement conditions of the high frequency glow discharge emission surface analyzer
are as follows.
· H.V.: 630 V
· Anode diameter: φ 4 mm
· Gas: Ar
· Gas pressure: 600 Pa
· Output: 35 W
[0085] Next, the structure of the Zn-Al-Mg alloy layer will be described.
[0086] In the Zn-Al-Mg alloy layer, a total area ratio of Al phase, MgZn
2 phase, and Zn/Al/MgZn
2 ternary eutectics is 90% or more.
[0087] From the viewpoint of improving corrosion resistance, the lower limit of the area
ratio is preferably 92%, 95%, or 98%. Ideally, the area ratio is particularly preferably
100%.
[0088] In addition, the area ratio of the structure excluding the Al phase, the MgZn
2 phase, and the Zn/Al/MgZn
2 ternary eutectics, as that of Zn phase is preferably from 0% to 10%, more preferably
from 0% to 8% or from 0% to 5%, and still more preferably from 0% to 2%. Ideally,
the area ratio of Zn phase is particularly preferably 0% (that is, it is particularly
preferable not to contain Zn phase.).
[0089] Here, the Al crystal and the Zn crystal each mean phase crystallized independently.
[0090] The structure of the Zn-Al-Mg alloy layer is measured as follows.
[0091] First, a sample is taken from a coated steel material to be measured. In this regard,
the sample is taken from a portion which is not in the vicinity (within 2 mm from
the end face) of the punched end face of the coated steel material, and is free from
a defect of the coating layer.
[0092] Next, the surface of the coating layer of the sample is polished in the thickness
direction of the coating layer (hereinafter also referred to as "Z-axis direction").
[0093] Specifically, the surface of the coating layer is dry-polished with a #1200 abrasive
sheet, and then finish-polishing is carried out successively using a finishing liquid
containing alumina having an average particle diameter of 3 µm, a finishing liquid
containing alumina having an average particle diameter of 1 µm, and a finishing liquid
containing colloidal silica in the mentioned order.
[0094] In doing so, the Zn intensity in the surface of the coating layer is measured by
XRF (X-ray fluorescence analysis) before and after the polishing, and when the Zn
intensity after the polishing reduces to 1/2 the Zn intensity before the polishing,
the then thickness of the coating layer is deemed as the 1/2 layer thickness. Since
the Zn-Al-Mg alloy layer occupies 1/2 or more of the layer thickness of the coating
layer, the polished surface obtained by polishing the surface of the coating layer
to 1/2 of the layer thickness is the polished surface of the Zn-Al-Mg alloy layer.
Therefore, the metal structure contained in the Zn-Al-Mg alloy layer can be grasped
by analyzing the polished surface.
[0095] Next, the polished surface is observed with a scanning electron microscope (SEM)
at a magnification of 500 x to obtain a backscattered electron image (hereinafter
also referred to as "SEM backscattered electron image"). The SEM observation conditions
are: acceleration voltage at 15 kV, probe-current at 10 nA, and visual field size
of 244 µm × 198 µm.
[0096] Further, using an electron probe microanalyzer (FE-EPMA), mapping analysis is performed
at a magnification of 500 x at an acceleration voltage of 15 kV, an irradiation current
of 30 nA, a beam diameter of about 100 nm, an irradiation time per point of 5 ms,
and a measurement pitch of 300 nm. Then, regions can be roughly divided into a region
in which the detection points of Mg and Zn overlap, a region in which the detection
points of Al and Zn overlap, and a region in which Zn is detected alone. In this case,
the region in which the detection points of Mg and Zn overlap is defined as MgZn
2, and a region in which the detection points of Al and Zn overlap is defined as Al
phase. Further, in the region in which Zn is detected alone, FE-EPMA line analysis
is performed at a magnification of 2000 x for a length of 10 µm. In this case, in
the measurement region, a region in which Mg or Al is detected by 1% or more can be
discriminated as Zn/Al/MgZn
2 ternary eutectics, and a region in which both Mg and Al are detected by less than
1% can be discriminated as Zn phase.
[0097] Computer image processing is performed on these regions to obtain the area ratio
(area (pixel) of each phase in the visual field is calculated).
[0098] Next, the Mg enrichment layer will be described.
[0099] The Mg enrichment layer is a layer in which a Mg-containing phase such as a Zn/Al/MgZn
2 ternary eutectics existing in a surface layer of the Zn-Al-Mg alloy layer is densified
and a Mg concentration is enriched.
[0100] When the Mg enrichment layer is thin, corrosion resistance becomes poor. On the other
hand, when the Mg enrichment layer is too thick, discoloration resistance deteriorates.
[0101] Therefore, a thickness of the Mg enrichment layer is set to 0.8 µm or more and (thickness
of coating layer × 1/2) or less. The thickness of the Mg enrichment layer is preferably
0.9 µm or more and 25 µm or less, and more preferably 1.0 µm or more and 22.5 µm or
less.
[0102] The thickness of the coating layer is preferably 5 µm or more and 50 µm or less,
and more preferably 10 µm or more and 45 µm or less.
[0103] The Mg enrichment layer is a layer defined as follows.
[0104] First, sputtering is performed in a depth direction from a surface side of the coating
layer by glow discharge optical emission spectrometry (quantitative GDS), and the
depth direction distribution of the intensity of each element (such as Zn, Al, Mg,
or Fe) contained in the coating layer is measured (see Fig. 1) (measurement device:
manufactured by HORIBA, Ltd., model number: GD-Profiler2, measurement conditions:
DC mode, voltage: 900 V, current: 20 mA). In this case, in a case where a chemical
conversion film or the like is present on the coating layer, the depth direction distribution
of the intensity of an element as a main component of a film (for example, carbon
(C) in the case of an organic film, and an element as a main component of a film in
the case of an inorganic film) is also measured. In the case of the inorganic film,
the element as a main component is, for example, zirconium (Zr) in a case of a zirconium
oxide film, and silicon (Si) in a case of a film containing a silane coupling agent.
[0105] The measurement is performed to a depth at which the coating layer disappears and
a base iron is sufficiently exposed. In this case, the depth [µm] of a hole after
the measurement is measured, and the sputtering rate [µm/s] is obtained by dividing
the measured value by the GDS measurement time [s]. By multiplying this sputtering
rate by the elapsed time from the start of measurement at the target measurement position,
the depth [µm] from the surface of the target measurement position is obtained.
[0106] Here, a point at which the amount of increase in intensity of Fe per 0.1 µm exceeds
0.003 when the change in intensity of Fe is viewed from the coating surface direction
is defined as (A). The intensity of Mg at the point (A) is defined as 1, and a point
(B) at which the relative intensity of Mg is 1.03 when the Mg intensity is viewed
from the base iron (that is, the base steel) side to the coating layer surface side
is defined as an interface between the Mg enrichment layer and the Zn-Al-Mg alloy
layer. A point (C) at which the intensity of Mg and the intensity of carbon (C) become
the same when the coating layer surface side is viewed from the point (B) is defined
as the top of the Mg enrichment layer. The intensity of carbon (C) that determines
the point (C) (the intensity of the carbon (C) in a case where no chemical conversion
film or the like is present on the coating layer) is the intensity of the carbon (C)
derived from dust or oil attached to the surface of the coating layer.
[0107] However, in a case where a chemical conversion film or the like is present on the
coating layer, the point at which the intensity of the chemical conversion film or
the like is the same as the intensity of the element as the main component of the
film is defined as the point (C), and the point (C) is defined as the top of the Mg
enrichment layer.
[0108] The Mg enrichment layer is defined as a layer between the point (B) and the point
(C), and the thickness of the Mg enrichment layer is defined as an average value of
differences in depth between the point (B) and the point (C) measured at three points.
[0109] Next, the Al-Fe alloy layer will be described.
[0110] The Al-Fe alloy layer is a layer that is formed on the surface of a base steel (specifically,
between a base steel and a Zn-Al-Mg alloy layer), and has a structure constituted
mainly with an Al
5Fe phase. The Al-Fe alloy layer is formed by mutual atomic diffusion of a base steel
and a hot-dip coating bath. Since, in the steel product of the disclosure, a coating
layer is formed by using a hot dip metal coating method, an Al-Fe alloy layer is easily
formed in a coating layer containing an Al element. Since Al is contained in a hot-dip
coating bath at a certain concentration or higher, an Al
5Fe phase is formed at the highest content. However, it takes time for atomic diffusion,
and there is a portion where the Fe concentration is high in the vicinity of the base
steel. Therefore, the Al-Fe alloy layer may partially contain a small amount of an
AlFe phase, an Al
3Fe phase, an Al
5Fe
2 phase, or the like. Also, since Zn is also contained in the hot-dip coating bath
at a certain concentration, the Al-Fe alloy layer also contains a small amount of
Zn.
[0111] Regarding the corrosion resistance, there is no significant difference among any
of an Al
5Fe phase, an Al
3Fe phase, an AlFe phase, and an Al
5Fe
2 phase. The referred corrosion resistance is the corrosion resistance at a portion
not affected by welding.
[0112] When Si is contained in a coating layer, Si is particularly apt to be incorporated
into an Al-Fe alloy layer and an Al-Fe-Si intermetallic compound phase may be formed.
The intermetallic compound phase to be identified includes an AlFeSi phase, and there
are α, β, q1, q2-AlFeSi phases, or the like as isomers. Therefore, these AlFeSi phases
or the like may be detected in the Al-Fe alloy layer in some cases. Such an Al-Fe
alloy layer including the AlFeSi phases or the like is also referred to as an Al-Fe-Si
alloy layer.
[0113] Since the thickness of the Al-Fe-Si alloy layer is also small relative to the Zn-Al-Mg
alloy layer, the effect on the corrosion resistance of the entire coating layer is
small.
[0114] Also, when various precoated steel materials are used for a base steel, the structure
of the Al-Fe alloy layer may be changed in some cases depending on the deposited amount
of the precoating. Specifically, there are a case where a layer of a pure metal used
for precoating remains in the vicinity of the Al-Fe alloy layer, a case where an intermetallic
compound phase (for example, an Al
3Ni phase), in which a constituent component of the Zn-Al-Mg alloy layer is bonded
to a precoating component, constitutes an alloy layer, a case where some of Al atoms
and Fe atoms are displaced to form an Al-Fe alloy layer, a case where some of Al atoms,
Fe atoms, and Si atoms are displaced to form an Al-Fe-Si alloy layer, and the like.
[0115] That is, the Al-Fe alloy layer means a layer that includes the above various modes
of alloy layers in addition to the alloy layer mainly composed of the Al
5Fe phase.
[0116] When a coating layer is formed on a Ni precoated steel material among various precoated
steel materials, an Al-Ni-Fe alloy layer is formed as the Al-Fe alloy layer.
[0117] The thickness of the Al-Fe alloy layer is, for example, 0 µm or more and 7 µm or
less.
[0118] The thickness of the Al-Fe alloy layer is preferably 0.05 µm or more and 5 µm or
less from the viewpoints of increasing the adhesion of the coating layer (specifically,
Zn-Al-Mg alloy layer), and ensuring the corrosion resistance and formability.
[0119] Since the thickness of a Zn-Al-Mg alloy layer is normally larger than that of an
Al-Fe alloy layer, the contribution of an Al-Fe alloy layer as a coated steel material
to the corrosion resistance is small as compared with a Zn-Al-Mg alloy layer. However,
an Al-Fe alloy layer contains Al and Zn, which are corrosion-resistant elements, at
a certain concentration or more, as inferred from the results of a component analysis.
Therefore, the Al-Fe alloy layer has a certain degree of corrosion resistance for
a base steel.
[0120] Also, when a coating layer having the chemical composition specified in the disclosure
is formed by a hot dip metal coating method, an Al-Fe alloy layer having a thickness
of 100 nm or more is apt to be formed between the base steel and the Zn-Al-Mg alloy
layer.
[0121] From the viewpoint of corrosion resistance, it is more preferable that the Al-Fe
alloy layer is thicker. Therefore, the thickness of the Al-Fe alloy layer is preferably
0.05 µm or more. However, since a thick Al-Fe alloy layer causes significant deterioration
in formability, the thickness of the Al-Fe alloy layer is preferably 7 µm or less.
When the thickness of the Al-Fe alloy layer is 7 µm or less, cracks generated from
the Al-Fe alloy layer and the amount of powdering are reduced and the formability
is improved. The thickness of the Al-Fe alloy layer is more preferably 5 µm or less
and still more preferably 2 µm or less.
[0122] The thickness of the Al-Fe alloy layer is measured as follows.
[0123] The thickness of an identified Al-Fe alloy layer is measured at optional 5 positions
in an SEM backscattered electron image (magnification: 10000 x, visual field size:
50 µm in width × 200 µm in length, provided that an Al-Fe alloy layer is visible in
the visual field) of a cross section of a coating layer (a cross section cut along
the coate thickness direction of the coating layer) prepared by embedding a sample
in a resin and then polishing the same. The arithmetic average of the five positions
is defined as the thickness of the Al-Fe alloy layer.
[0124] Regarding the thickness of the coating layer, the thickness thereof is also measured
at optional five positions in the SEM backscattered electron image (magnification:
500 x, visual field size: 198 µm in width × 244 µm in length, provided that the entire
coating layer is visible in the visual field) of the cross section. The arithmetic
average of the five positions is defined as the thickness of the coating layer.
(method for Manufacturing coated steel material)
[0125] Hereinafter, an example of a method for manufacturing a coated steel material according
to the disclosure will be described.
[0126] A coated steel material of the disclosure is obtained by forming a coating layer
having the above-specified chemical composition and metal structure on the surface(s)
(namely, on one side, or both sides) of a base steel (such as a base steel sheet)
by a hot dip metal coating method.
[0127] Specifically, for example, hot dip metal coating is performed under the following
conditions. Hereinafter, a method for manufacturing a coated steel sheet will be described
as an example of the method for manufacturing a coated steel material of the disclosure.
[0128] First, a base steel sheet as the base steel is immersed in a hot-dip coating bath
and pulled up from the hot-dip coating bath, and then cooled down in a temperature
range of from 450°C to 395°C at an average cooling rate of 15°C/s or less.
[0129] Next, cooling down is performed in a temperature range of from 395°C to 340°C at
an average cooling rate of 3°C/s or less.
[0130] Next, cooling down is performed in a temperature range of from 340°C to 280°C at
an average cooling rate of from 10°C/s to 20°C/s or more.
[0131] Here, for coating, for example, a continuous hot dip metal coating method such as
a Sendzimir method is carried out.
[0132] Then, after cooling, skin pass rolling is performed under conditions that a surface
roughness Ra of a skin pass roll is from 1 to 5 µm and a skin pass rolling force is
from 100 to 500 ton.
[0133] Here, the coating layer solidifies in the order of Al phase, a MgZn
2 phase crystallized around Al phase, and a Zn/Al/MgZn
2 ternary eutectic.
[0134] Therefore, Al phase are grown by performing cooling down in a temperature range of
from 450°C to 395°C at an average cooling rate of 15°C/s or less. When cooling down
is performed in the temperature range of from 395°C to 340°C at an average cooling
rate of 3°C/s or less, MgZn
2 phase are reliably crystallized around the Al phase. By doing so, the Zn/Al/MgZn
2 ternary eutectics can be refined.
[0135] The upper limit of the average cooling rate in the temperature range of from 450°C
to 395°C is 15°C/s, preferably 13°C/s, and more preferably 11°C/s.
[0136] The lower limit is not particularly limited, and is preferably 1°C/s, more preferably
2°C/s or more from the viewpoint of productivity.
[0137] When the average cooling rate in the temperature range of from 450°C to 395°C is
more than 15°C/s, the Al phase are excessively finely crystallized, and the Zn/Al/MgZn
2 ternary eutectics are also excessively refined. This makes it difficult to form a
Mg enrichment layer by skin pass rolling described below.
[0138] The upper limit of the average cooling rate in the temperature range of from 395°C
to 340°C is 3°C/s, and preferably 2.5°C/s.
[0139] The lower limit is not particularly limited, and is preferably 0.5°C/s, more preferably
1°C/s or more from the viewpoint of productivity.
[0140] When the average cooling rate in the temperature range of 395°C to 340°C is more
than 3°C/s, MgZn
2 phase around the Al crystal cannot be sufficiently grown, and the refinement of the
Zn/Al/MgZn
2 ternary eutectics becomes insufficient.
[0141] As a result, it is difficult to form a Mg enrichment layer by skin pass rolling described
below.
[0142] Next, when cooling down is performed in the temperature range of from 340°C to 280°C
at an average cooling rate of 10°C/s or more, the Zn/Al/MgZn
2 ternary eutectics are refined. This makes it easier to form a Mg enrichment layer
by skin pass rolling described below.
[0143] However, when the average cooling rate in the temperature range of from 340°C to
280°C is more than 20°C/s, the Zn/Al/MgZn
2 ternary eutectics is excessively refined, and it is difficult to form a Mg enrichment
layer by skin pass rolling described below.
[0144] The average cooling rate in the temperature range of lower than 280°C is not limited.
For example, furnace cooling may be used, or heat retention may be performed by adjusting
the properties of a steel material. In addition, water cooling may be performed by
mist cooling or the like. The average cooling rate in the method as exemplified here
is, for example, 50°C/sec or less.
[0145] Next, after cooling, when skin pass rolling is performed under the conditions that
the surface roughness Ra of the skin pass roll is 1 µm or more and the skin pass rolling
force is 100 ton or more, soft Mg-containing phase (such as Zn/Al/MgZn
2 ternary eutectics) present on a surface layer of the Zn-Al-Mg alloy layer are extended,
and the Mg enrichment layer is formed.
[0146] However, when the surface roughness Ra of the skin pass roll is more than 5 µm, a
surface area of the coating layer surface increases, and therefore, the Mg enrichment
layer is excessively thickened, and discoloration resistance deteriorates. Meanwhile,
when the surface roughness Ra of the skin pass roll is less than 1 µm, the base steel
sheet slips during the skin pass rolling, and uniform rolling cannot be performed,
and corrosion resistance and discoloration resistance cannot be secured.
[0147] In addition, when the skin pass rolling force is more than 500 ton, soft Mg-containing
phase (such as Zn/Al/MgZn
2 ternary eutectics) excessively extend, and therefore, the Mg enrichment layer is
difficult to be thickened, and corrosion resistance deteriorates. However, even when
the skin pass rolling force is less than 100 ton, the Mg enrichment layer is difficult
to be thickened, and corrosion resistance deteriorates.
[0148] When the surface roughness Ra of the skin pass roll increases within an appropriate
range of the skin pass rolling force, the point (B) in Fig. 1 tends to move to the
right side, and the thickness of the Mg enrichment layer increases.
[0149] The surface roughness Ra of the skin pass roll is measured as follows. Roughness
is measured at three positions on the surface of the skin pass roll in the width direction
of the roll with a stylus-type portable roughness meter, and an average value thereof
is obtained.
[0150] A post-treatment applicable to a coated steel material of this disclosure will be
described below.
[0151] A film may be formed on the coating layer of a coated steel material of this disclosure.
The film may be constituted with a single layer, or two or more layers. Examples of
the kind of the film directly on the coating layer include a chromate film, a phosphate
film, and a chromate-free film. A chromate treatment, a phosphate treatment, or a
chromate-free treatment for forming the film may be performed by a known method.
[0152] The chromate treatment includes an electrolytic chromate treatment, by which a chromate
film is formed by electrolysis; a reactive chromate treatment, by which a film is
formed utilizing a reaction with a material, and then an excess treatment solution
is washed out; and a painting type chromate treatment, by which a treatment solution
is applied to an object, and then dried without washing with water to form a film.
Any treatment may be adopted.
[0153] Examples of the electrolytic chromate treatment include those using chromic acid,
silica sol, a resin (such as an acrylic resin, a vinyl ester resin, a vinyl acetate/acrylic
emulsion, a carboxylated styrene butadiene latex, a diisopropanolamine-modified epoxy
resin), or hard silica.
[0154] Examples of the phosphate treatment include a zinc phosphate treatment, a zinc calcium
phosphate treatment, and a manganese phosphate treatment.
[0155] The chromate-free treatment is particularly preferable because it does not impose
a burden on an environment. The chromate-free treatment includes an electrolytic chromate-free
treatment, by which a chromate-free film is formed by electrolysis; a reactive chromate-free
treatment, by which a film is formed utilizing a reaction with a material, and then
an excess treatment solution is washed out; and a painting type chromate-free treatment,
by which a treatment solution is applied to an object, and then dried without washing
with water to form a film. Any treatment may be adopted.
[0156] Furthermore, one layer, or two or more layers of an organic resin film may be provided
on the film directly on the coating layer. There is no particular restriction on the
kind of the organic resin, and examples thereof include a polyester resin, a polyurethane
resin, an epoxy resin, an acrylic resin, and a polyolefin resin, as well as modified
products of these resins. In this regard, the modified product refers to a resin in
which a reactive functional group included in the structure of these resins is reacted
with another compound (such as a monomer, or a crosslinking agent) having in its structure
a functional group capable of reacting with the former functional group.
[0157] As such an organic resin, one kind, or a mixture of two or more kinds of (unmodified)
organic resins may be used; or one kind, or a mixture of two or more kinds of organic
resins obtained by modifying at least one kind of organic resin in the presence of
at least one kind of another organic resin may be used. Further, the organic resin
film may contain an optional color pigment or rust preventive pigment. A water-based
form prepared through dissolution or dispersion in water may also be used.
Examples
(Examples)
[0158] In order to obtain a coating layer having a chemical composition shown in Tables
1 and 2, an ingot was melted in a vacuum melting furnace using a predetermined amount
of pure metal ingot, and then a hot-dip coating bath was prepared in the air. A hot
dip metal coating simulator was used for preparing the coated steel sheet.
[0159] As the base steel material, a general hot-rolled steel sheet (C concentration < 0.1%)
having a sheet thickness of 2.3 mm was used. After a surface to be coated of the base
steel was brush-polished, degreasing and pickling were performed immediately before
a coating step.
[0160] In addition, in some examples, as the base steel, a Ni precoated steel material prepared
by applying Ni precoating to general hot-rolled steel sheet having a sheet thickness
of 2.3 mm was used. The deposited amount of Ni was set at from 1 g/m
2 to 3 g/m
2. In this regard, with respect to an example in which a Ni precoated steel material
was used as the base steel, a remark of "Ni precoated" was entered in the column of
"Base steel" in the Tables.
[0161] A contact type K thermocouple was attached to a back surface of the surface to be
coated of the base steel in order to monitor the temperature of the steel product
in a coated steel sheet preparing process.
[0162] In any sample preparation, the same reduction treatment method was applied to the
base steel up to a step of immersion in the hot-dip coating bath. In other words,
the base steel was heated from room temperature to 800°C by electric heating in a
N
2-H
2 (5%) environment (dew point of -40°C or less, oxygen concentration of less than 25
ppm), retained there for 60 sec, cooled to the hot-dip coating bath temperature +10°C
by N
2 gas blow, and then immediately immersed in the hot-dip coating bath.
[0163] In any of the coated steel sheets, the immersion time in the hot-dip coating bath
was set to the time in the table. The N
2 gas wiping pressure was adjusted and a coated steel sheet was prepared such that
a coating thickness was 30 µm (±1 µm).
[0164] The hot-dip coating bath temperature was 500°C. The immersion time in the hot-dip
coating bath was 2 seconds.
[0165] The base steel was pulled up from the hot-dip coating bath, and then subjected to
a cooling process under the conditions set forth in Table 1 or 2 with respect to the
following average cooling rates at the first to third stages as itemized in Table
1 or 2 to obtain a coating layer.
· Average cooling rate at first stage: Average cooling rate in the temperature range
of from 450°C to 395°C
· Average cooling rate at second stage: Average cooling rate in the temperature range
of from 395°C to 340°C
· Average cooling rate at third stage: Average cooling rate in the temperature range
of from 340°C to 280°C
In the cooling process, the steel product was cooled down by spraying N2 gas onto the steel product after being coated. In this case, cooling was performed
while adjusting a spraying amount of the N2 gas so as to achieve a predetermined cooling rate in the above temperature range.
-Various Measurements-
[0166] A sample was cut out from an obtained coated steel sheet. The following items were
measured according to the method described above.
· Thickness of coating layer
· Thickness of Mg enrichment layer
· Thickness of Al-Fe alloy layer (thickness of Al-Ni-Fe alloy layer, in an example
in which a Ni precoated steel sheet was used as the base steel)
· A total area ratio of Al phase, MgZn2 phase, and Zn/Al/MgZn2 ternary eutectics in Zn-Al-Mg alloy layer (in Tables, referred to as specific structure
area ratio)
-Corrosion Resistance-
[0167] A sample was cut out from an obtained coated steel sheet. Then, the samples were
placed vertically, and 21 cycles of a combined cycle corrosion test (CCT) in accordance
with the corrosion acceleration test (JASO M609-91) were conducted. After performing
the corrosion test, the case where the corrosion loss was 20 g/m
2 or less was evaluated as "A", and the case where the corrosion loss was more than
20 g/m
2 was evaluated as "NG".
-Formability -
[0168] A sample was cut out from an obtained coated steel sheet. After bending the sample
by 1 T, tape was exfoliated from the processed portion, and an area ratio of the coating
layer attached to the tape was evaluated. An area ratio of the deposited coating layer
of 5% or less was evaluated as "A", and an area ratio of more than 5% was evaluated
as "NG".
-Discoloration Resistance -
[0169] A sample was cut out from an obtained coated steel sheet. Then, the sample was placed
at an angle of 60° with respect to the horizontal direction on a constant temperature
and humidity tester (KCL-2000 manufactured by EYELA) at 50°C and 80%RH, and a color
difference ΔE after 3 days was evaluated. With respect to the color difference, before
and after the test, the L value, a* value, and b* value of the sample in a SCE (specular
light removal) method were measured with a colorimeter (CR-400 manufactured by Konica
Minolta Optics), and the color difference ΔE was investigated at 4 points to determine
an average value thereof.
[0170] A case where the average value of the color differences ΔE after three days was 10
or less was evaluated as "A", and a case where the average value was more than 10
was evaluated as "NG".
[0171] Examples are listed in Tables 1 and 2.
[Table 1-1]
[0172]
Table 1-1
No. |
Class |
Base steel |
Coating cooling |
Skin pass rolling |
Average cooling rate at first stage |
Average cooling rate at second stage |
Average cooling rate at third stage |
Roll surface roughness Ra |
Rolling force |
- |
(°C/s) |
(°C/s) |
(°C/s) |
(µm) |
(ton) |
1 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
2 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
3 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
4 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
5 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
6 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
7 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
8 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
9 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
10 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
11 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
12 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
13 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
14 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
15 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
16 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
17 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
18 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
19 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
20 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
21 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
22 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
23 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
24 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
25 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
26 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
27 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
28 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
29 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
30 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
31 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
32 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
33 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
34 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
35 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
36 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
37 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
38 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
39 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
40 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
41 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
42 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
43 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
44 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
45 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
46 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
47 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
48 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
49 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
50 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
51 |
Example |
- |
15 |
2 |
15 |
3 |
300 |
52 |
Example |
- |
9 |
3 |
15 |
3 |
300 |
53 |
Example |
- |
9 |
2 |
10 |
3 |
300 |
54 |
Example |
- |
9 |
2 |
20 |
3 |
300 |
55 |
Example |
- |
9 |
2 |
15 |
1 |
300 |
56 |
Example |
- |
9 |
2 |
15 |
5 |
300 |
57 |
Example |
- |
9 |
2 |
15 |
3 |
100 |
58 |
Example |
- |
9 |
2 |
15 |
3 |
500 |
59 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
60 |
Example |
- |
9 |
2 |
15 |
3 |
300 |
61 |
Example |
Pre-Ni |
9 |
2 |
15 |
3 |
300 |
62 |
Example |
Pre-Ni |
9 |
2 |
15 |
3 |
300 |
63 |
Example |
Pre-Ni |
9 |
2 |
15 |
3 |
300 |
64 |
Example |
Pre-Ni |
9 |
2 |
15 |
3 |
300 |
[Table 1-2]
[0173]
Table 1-2
No. |
Class |
Composition of coating layer (mass%) |
Zn |
Al |
Mg |
Sn |
Bi |
In |
Ca |
Y |
La |
Ce |
Si |
Cr |
Ti |
Zr |
Mo |
W |
Ag |
P |
1 |
Example |
88.40 |
5.50 |
6.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
2 |
Example |
88.32 |
5.50 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
3 |
Example |
69.32 |
24.50 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
4 |
Example |
76.32 |
20.00 |
3.50 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
5 |
Example |
67.82 |
20.00 |
12.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
6 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
7 |
Example |
73.50 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
8 |
Example |
73.70 |
20.00 |
6.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
9 |
Example |
73.50 |
20.00 |
6.00 |
0.20 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
10 |
Example |
73.50 |
20.00 |
6.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
11 |
Example |
73.40 |
20.00 |
6.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
12 |
Example |
72.87 |
20.00 |
6.00 |
0.03 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
1.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
13 |
Example |
72.04 |
20.00 |
6.00 |
0.06 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
1.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
14 |
Example |
73.75 |
20.00 |
6.00 |
0.15 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
15 |
Example |
73.62 |
20.00 |
6.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
16 |
Example |
73.30 |
20.00 |
6.00 |
0.60 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
17 |
Example |
72.90 |
20.00 |
6.00 |
1.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
18 |
Example |
83.93 |
10.00 |
4.00 |
2.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
19 |
Example |
69.30 |
20.00 |
6.00 |
0.10 |
4.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
20 |
Example |
72.30 |
20.00 |
6.00 |
0.10 |
0.00 |
1.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
21 |
Example |
73.70 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
22 |
Example |
73.30 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
23 |
Example |
72.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
1.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
24 |
Example |
70.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
3.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
25 |
Example |
73.30 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
26 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.40 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
27 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.40 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
28 |
Example |
71.50 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
2.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
29 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
30 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
31 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
32 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
33 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
34 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
35 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
36 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
37 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
38 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
39 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
40 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
41 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
42 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
43 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
44 |
Example |
73.60 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
45 |
Example |
68.90 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
46 |
Example |
68.90 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
47 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
48 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
49 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
50 |
Example |
73.40 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
51 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
52 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
53 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
54 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
55 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
56 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
57 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
58 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
59 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
60 |
Example |
73.80 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
61 |
Example |
73.76 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
62 |
Example |
73.77 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
63 |
Example |
73.76 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
64 |
Example |
73.77 |
20.00 |
6.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
[Table 1-3]
[0174]
Table 1-3
No. |
Class |
Composition of coating layer (mass%) |
Ni |
Co |
v |
Nb |
Cu |
Mn |
Li |
Na |
K |
Fe |
Sr |
Sb |
Pb |
B |
1 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
2 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
3 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
4 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
5 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
6 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
7 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
8 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
9 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
10 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
11 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
12 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
13 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
14 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
15 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
16 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
17 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
18 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.07 |
0.00 |
0.00 |
0.00 |
0.00 |
19 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
20 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
21 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
22 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
23 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
24 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
25 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
26 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
27 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
28 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
29 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
30 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
31 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
32 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
33 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
34 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
35 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
36 |
Example |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
37 |
Example |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
38 |
Example |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
39 |
Example |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
40 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
41 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
42 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
43 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
44 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.20 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
45 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
5.00 |
0.00 |
0.00 |
0.00 |
0.00 |
46 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
5.00 |
0.00 |
0.00 |
0.00 |
0.00 |
47 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.40 |
0.00 |
0.00 |
0.00 |
48 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.40 |
0.00 |
0.00 |
49 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.40 |
0.00 |
50 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.40 |
51 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
52 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
53 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
54 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
55 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
56 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
57 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
58 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
59 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
60 |
Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
61 |
Example |
0.04 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
62 |
Example |
0.03 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
63 |
Example |
0.04 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
64 |
Example |
0.03 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
[Table 1-4]
[0175]
Table 1-4
No. |
Class |
Thickness of coating layer |
Thickness of Mg enrichment layer |
Thickness of Al-Fe alloy layer |
Specific structure area ratio |
Corrosion resistance |
formability |
Discoloration resistance |
(µm) |
(µm) |
(µm) |
(%) |
1 |
Example |
20 |
5 |
1 |
99 |
A |
A |
A |
2 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
3 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
4 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
5 |
Example |
20 |
5 |
1 |
98 |
A |
A |
A |
6 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
7 |
Example |
20 |
5 |
1 |
95 |
A |
A |
A |
8 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
9 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
10 |
Example |
20 |
5 |
1 |
95 |
A |
A |
A |
11 |
Example |
20 |
5 |
1 |
94 |
A |
A |
A |
12 |
Example |
20 |
5 |
1 |
92 |
A |
A |
A |
13 |
Example |
20 |
5 |
1 |
93 |
A |
A |
A |
14 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
15 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
16 |
Example |
20 |
5 |
1 |
95 |
A |
A |
A |
17 |
Example |
20 |
5 |
1 |
94 |
A |
A |
A |
18 |
Example |
20 |
5 |
1 |
94 |
A |
A |
A |
19 |
Example |
20 |
5 |
1 |
92 |
A |
A |
A |
20 |
Example |
20 |
5 |
1 |
93 |
A |
A |
A |
21 |
Example |
20 |
5 |
1 |
95 |
A |
A |
A |
22 |
Example |
20 |
5 |
1 |
93 |
A |
A |
A |
23 |
Example |
20 |
5 |
1 |
92 |
A |
A |
A |
24 |
Example |
20 |
5 |
1 |
90 |
A |
A |
A |
25 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
26 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
27 |
Example |
20 |
5 |
1 |
95 |
A |
A |
A |
28 |
Example |
20 |
5 |
1 |
91 |
A |
A |
A |
29 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
30 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
31 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
32 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
33 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
34 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
35 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
36 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
37 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
38 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
39 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
40 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
41 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
42 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
43 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
44 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
45 |
Example |
20 |
5 |
5 |
97 |
A |
A |
A |
46 |
Example |
20 |
5 |
4 |
97 |
A |
A |
A |
47 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
48 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
49 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
50 |
Example |
20 |
5 |
1 |
96 |
A |
A |
A |
51 |
Example |
20 |
0.8 |
1 |
97 |
A |
A |
A |
52 |
Example |
20 |
4 |
1 |
97 |
A |
A |
A |
53 |
Example |
20 |
4 |
1 |
97 |
A |
A |
A |
54 |
Example |
20 |
2 |
1 |
97 |
A |
A |
A |
55 |
Example |
20 |
1.5 |
1 |
97 |
A |
A |
A |
56 |
Example |
20 |
6 |
1 |
97 |
A |
A |
A |
57 |
Example |
20 |
6 |
1 |
97 |
A |
A |
A |
58 |
Example |
20 |
2 |
1 |
97 |
A |
A |
A |
59 |
Example |
50 |
5 |
1 |
97 |
A |
A |
A |
60 |
Example |
10 |
5 |
1 |
97 |
A |
A |
A |
61 |
Example |
30 |
5 |
1 |
97 |
A |
A |
A |
62 |
Example |
10 |
5 |
1 |
97 |
A |
A |
A |
63 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
64 |
Example |
20 |
5 |
1 |
97 |
A |
A |
A |
[Table 2-1]
[0176]
Table 2-1
No. |
Class |
Base steel |
Coating cooling |
Skin pass rolling |
Average cooling rate at first stage |
Average cooling rate at second stage |
Average cooling rate at third stage |
Roll surface roughness Ra |
Rolling force |
- |
(°C/s) |
(°C/s) |
(°C/s) |
(µm) |
(ton) |
65 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
66 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
67 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
68 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
69 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
70 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
71 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
72 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
73 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
74 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
75 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
76 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
77 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
78 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
79 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
80 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
81 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
82 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
83 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
84 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
85 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
86 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
87 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
88 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
89 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
90 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
91 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
92 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
93 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
94 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
95 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
96 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
97 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
98 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
99 |
Comparative Example |
- |
18 |
2 |
15 |
3 |
300 |
100 |
Comparative Example |
- |
9 |
5 |
15 |
3 |
300 |
101 |
Comparative Example |
- |
9 |
2 |
25 |
3 |
300 |
102 |
Comparative Example |
- |
9 |
2 |
15 |
8 |
300 |
103 |
Comparative Example |
- |
9 |
2 |
15 |
0.5 |
300 |
104 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
50 |
105 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
700 |
106 |
Comparative Example |
- |
9 |
2 |
7 |
3 |
300 |
107 |
Comparative Example |
- |
9 |
2 |
15 |
3 |
300 |
[Table 2-2]
[0177]
Table 2-2
No. |
Class |
Composition of coating layer (mass%) |
Zn |
Al |
Mg |
Sn |
Bi |
In |
Ca |
Y |
La |
Ce |
Si |
Cr |
Ti |
Zr |
Mo |
W |
Ag |
P |
65 |
Comparative Example |
63.90 |
24.00 |
12.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
66 |
Comparative Example |
89.40 |
4.50 |
6.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
67 |
Comparative Example |
67.90 |
26.00 |
6.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
68 |
Comparative Example |
77.40 |
20.00 |
2.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
69 |
Comparative Example |
66.90 |
20.00 |
13.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
70 |
Comparative Example |
70.40 |
20.00 |
6.00 |
3.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
71 |
Comparative Example |
68.82 |
20.00 |
6.00 |
0.08 |
5.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
72 |
Comparative Example |
71.82 |
20.00 |
6.00 |
0.08 |
0.00 |
2.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
73 |
Comparative Example |
70.32 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
3.50 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
74 |
Comparative Example |
73.22 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
75 |
Comparative Example |
73.22 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
76 |
Comparative Example |
73.22 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
77 |
Comparative Example |
71.12 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
2.70 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
78 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
79 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
80 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
81 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
82 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
83 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
84 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
85 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
86 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
87 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
88 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
89 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
90 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
91 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
92 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
93 |
Comparative Example |
73.52 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
94 |
Comparative Example |
66.92 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
95 |
Comparative Example |
73.32 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
96 |
Comparative Example |
73.32 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
97 |
Comparative Example |
73.32 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
98 |
Comparative Example |
73.22 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
99 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
100 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
101 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
102 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
103 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
104 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
105 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
106 |
Comparative Example |
73.82 |
20.00 |
6.00 |
0.08 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
107 |
Comparative Example |
95.00 |
2.00 |
2.90 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
[Table 2-3]
[0178]
Table 2-3
No. |
Class |
Composition of coating layer (mass%) |
Ni |
Co |
v |
Nb |
Cu |
Mn |
Li |
Na |
K |
Fe |
Sr |
Sb |
Pb |
B |
65 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
66 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
67 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
68 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
69 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
70 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
71 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
72 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
73 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
74 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
75 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
76 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
77 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
78 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
79 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
80 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
81 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
82 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
83 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
84 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
85 |
Comparative Example |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
86 |
Comparative Example |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
87 |
Comparative Example |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
88 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
89 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
90 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
91 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
92 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
93 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.30 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
94 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
7.00 |
0.00 |
0.00 |
0.00 |
0.00 |
95 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
0.00 |
0.00 |
96 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
0.00 |
97 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.60 |
0.00 |
98 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.60 |
99 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
100 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
101 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
102 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
103 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
104 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
105 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
106 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
107 |
Comparative Example |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.00 |
0.10 |
0.00 |
0.00 |
0.00 |
0.00 |
[Table 2-4]
[0179]
Table 2-4
No. |
Class |
Thickness of coating layer |
Thickness of Mg enrichment layer |
Thickness of Al-Fe alloy layer |
Specific structure area ratio |
Corrosion resistance |
Formability |
Discoloration resistance |
(µm) |
(µm) |
(µm) |
(%) |
65 |
Comparative Example |
20 |
5 |
1 |
92 |
NG |
A |
A |
66 |
Comparative Example |
20 |
5 |
1 |
60 |
NG |
NG |
A |
67 |
Comparative Example |
20 |
5 |
1 |
97 |
NG |
A |
A |
68 |
Comparative Example |
20 |
0 |
1 |
91 |
NG |
A |
A |
69 |
Comparative Example |
20 |
5 |
1 |
96 |
A |
NG |
A |
70 |
Comparative Example |
20 |
5 |
1 |
89 |
NG |
A |
NG |
71 |
Comparative Example |
20 |
5 |
1 |
88 |
NG |
A |
A |
72 |
Comparative Example |
20 |
5 |
1 |
92 |
NG |
A |
A |
73 |
Comparative Example |
20 |
5 |
1 |
89 |
NG |
NG |
A |
74 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
75 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
76 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
77 |
Comparative Example |
20 |
5 |
1 |
87 |
NG |
NG |
A |
78 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
79 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
80 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
81 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
82 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
83 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
84 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
85 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
86 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
87 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
88 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
89 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
90 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
91 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
92 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
93 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
94 |
Comparative Example |
20 |
5 |
8 |
94 |
NG |
NG |
A |
95 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
96 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
97 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
98 |
Comparative Example |
20 |
5 |
1 |
94 |
NG |
A |
A |
99 |
Comparative Example |
20 |
0 |
1 |
97 |
NG |
A |
A |
100 |
Comparative Example |
20 |
0.5 |
1 |
97 |
NG |
A |
A |
101 |
Comparative Example |
20 |
0 |
1 |
97 |
NG |
A |
A |
102 |
Comparative Example |
20 |
11 |
1 |
97 |
A |
A |
NG |
103 |
Comparative Example |
- |
- |
- |
97 |
NG |
A |
NG |
104 |
Comparative Example |
20 |
0.3 |
1 |
97 |
NG |
A |
A |
105 |
Comparative Example |
20 |
0.6 |
1 |
97 |
NG |
A |
A |
106 |
Comparative Example |
20 |
0.6 |
1 |
97 |
NG |
A |
A |
107 |
Comparative Example |
20 |
0.8 |
1 |
55 |
NG |
A |
A |
[0180] From the above results, Examples corresponding to a coated steel material of the
disclosure exhibit more excellent corrosion resistance as compared to Comparative
Examples, even in a coastal region in which the amount of airborne chlorides is large
and the corrosion environment is severe. In addition, it can also be seen that formability
and discoloration resistance are excellent.
[0181] In Test No. 103, since uniform rolling could not be performed and the variation in
appearance was large, the thickness of various coating layers was not measured.
[0182] The preferred embodiments of the disclosure have been described in detail with reference
to the accompanying drawings, but the disclosure is not limited to such examples.
It is obvious that those skilled in the art to which this disclosure belongs can conceive
of various changes or modifications within the scope of the technical concept described
in the claims. It is obviously understood that these changes or modifications also
fall within the technical scope of the disclosure.
[0184] All the literature, patent application, and technical standards cited herein are
also herein incorporated to the same extent as provided for specifically and severally
with respect to an individual literature, patent application, and technical standard
to the effect that the same should be so incorporated by reference.