Technical Field
[0001] The present disclosure relates to a cold rolled steel sheet having excellent weldability,
strength and formability and a method of manufacturing the same.
Background Art
[0002] Recently, in order reduce the weight of automobiles and enhance safety thereof, a
technology for manufacturing a steel sheet having high strength is being promoted,
and in particular, demand for a high-strength steel material having a tensile strength
of 980 MPa or higher is increasing. However, when simply improving strength, since
it is a common phenomenon that ductility and formability decrease, a high-strength
steel sheet for cold forming overcoming this to have formability are highly utilized
in terms of improving fuel efficiency through weight reduction, improving manufacturing
parts/forming productivity, and ensuring safety of final parts.
[0003] In order to improve the formability of a steel material, a method of using a Transformation
Induced Plasticity (TRIP) phenomenon by introducing retained austenite as in Patent
Document 1 is widely used as a method to increase elongation. However, in the case
of such a TRIP steel sheet, it is necessary to add a large amount of Si and Al to
introduce retained austenite, which causes Liquid Metal Embrittlement (LME) to occur
during spot welding of the steel sheet, thereby limiting the use of a plated steel
sheet and a cold-rolled steel sheet welded with a plating material. In addition, as
the strength of the steel sheet increases, a problem of hydrogen embrittlement, in
which assembled parts suddenly fracture during use, may occur, so it is necessary
to ensure that the steel sheet does not corrode severely, even when exposed to a corrosive
environment.
[Prior art document]
Summary of Invention
Technical Problem
[0005] An aspect of the present disclosure is to provide a cold-rolled steel sheet having
excellent weldability, strength, and formability, and a method of manufacturing the
same.
Solution to Problem
[0006] According to an aspect of the present disclosure, provided is a cold-rolled steel
sheet having excellent weldability, strength, and formability, the cold-rolled steel
sheet including by weight: C: 0.14 to 0.16%, Si: 0.3 to 0.6%, Al: 0.01 to 0.3%, Mn:
2.6 to 3.0%, Cr: 0.01 to 0.25%, Mo: 0.15 to 0.4%, B: 0.0001 to 0.005%, Nb: 0.001 to
0.05%, Ti: 0.001 to 0.05%, P: 0.04% or less (excluding 0%), S: 0.01% or less (excluding
0%), N: 0.01% or less (excluding 0%), with a remainder of Fe and other unavoidable
impurities, wherein the following Relational Expressions 1 and 2 are satisfied, wherein
a microstructure consists of retained austenite: more than 1% and 5% or less, fresh
martensite: 10% or more and less than 25%, bainite: less than 20% (excluding 0%),
tempered martensite: 55% or more and less than 80%, and ferrite: 5% or less (including
0%).
234× [C] - 29×[Si] - 128×[Al] + 29×[Mn] + 10×[Cr] - 17×[Mo] -37×[Nb] - 49×[Ti] + 100×[B]
≥ 80
5× [C] + [Si] + 0.5× [Al] ≤ 1.5
where a content of each element in the above Relational Expressions 1 and 2 refers
to % by weight.
[0007] According to another aspect of the present disclosure, provided is a method of manufacturing
a cold-rolled steel sheet having excellent weldability, strength, and formability,
the method including: heating a slab including by weight: C: 0.14 to 0.16%, Si: 0.3
to 0.6%, Al: 0.01 to 0.3%, Mn: 2.6 to 3.0%, Cr: 0.01 to 0.25%, Mo: 0.15 to 0.4%, B:
0.0001 to 0.005%, Nb: 0.001 to 0.05%, Ti: 0.001 to 0.05%, P: 0.04% or less (excluding
0%), S: 0.01% or less (excluding 0%), N: 0.01% or less (excluding 0%), with a remainder
of Fe and other unavoidable impurities, wherein the following Relational Expressions
1 and 2 are satisfied; finish hot rolling the heated slab at a temperature within
a range of 830 to 980°C to obtain a hot-rolled steel sheet; coiling the hot-rolled
steel sheet at a temperature within a range of 450 to 700°C; cold rolling the coiled
hot-rolled steel sheet to obtain a cold-rolled steel sheet; continuously annealing
the cold-rolled steel sheet at a temperature within a range of 800 to 840°C; primarily
cooling the continuously annealed steel sheet at an average cooling rate of less than
10°C/s to a primary cooling end temperature of 550 to 650°C; secondarily cooling the
primarily cooled steel sheet at an average cooling rate of 10°C/s or more to a secondary
cooling end temperature of 320 to 360°C; and reheating the secondarily cooled steel
sheet to a temperature within a range of 380 to 480°C.
234×[C] - 29×[Si] - 128×[Al] + 29×[Mn] + 10×[Cr] - 17×[Mo] -37×[Nb] - 49×[Ti] + 100×[B]
≥ 80
5× [C] + [Si] + 0.5× [Al] ≤ 1.5
where a content of each element in the above Relational Expressions 1 and 2 refers
to % by weight.
Advantageous Effects of Invention
[0008] As set forth above, according to an aspect of the present disclosure, a cold-rolled
steel sheet having excellent weldability, strength, and formability and a method of
manufacturing the same may be provided.
Best Mode for Invention
[0009] Hereinafter, a cold-rolled steel sheet having excellent weldability, strength, and
formability according to an embodiment of the present disclosure will be described.
[0010] First, an alloy composition of the present disclosure will be described. A content
of the alloy composition described below refers to % by weight.
Carbon (C): 0.14 to 0.16%
[0011] Carbon (C) is an element to secure strength of a steel material, through solid solution
strengthening and precipitation strengthening. When the C content is less than 0.14%,
it is difficult to secure a tensile strength (TS) of 1180 MPa. On the other hand,
when the C content is more than 0.16%, arc weldability and laser weldability deteriorate,
and a risk of occurrence of LME cracks increases. Therefore, the C content is preferably
in a range of 0.14 to 0.16%. A lower limit of the C content is more preferably 0.145%.
An upper limit of the C content is more preferably 0.155%.
Silicon (Si): 0.3 to 0.6%
[0012] Silicon (Si) is a key element in Transformation Induced Plasticity (TRIP) steel increasing
a fraction and elongation of retained austenite by inhibiting precipitation of cementite.
When the Si content is less than 0.3%, almost no retained austenite remains, resulting
in excessively low elongation. On the other hand, when the Si content is more than
0.6%, it is impossible to prevent deterioration of properties of a weld zone due to
the formation of LME cracks, and surface properties and plating properties of a steel
material deteriorate. Therefore, the Si content is preferably in a range of 0.3 to
0.6%. A lower limit of the Si content is more preferably 0.35%. An upper limit of
the Si content is more preferably 0.55%, even more preferably 0.5%, and most preferably
0.45%.
Aluminum (Al): 0.01 to 0.3%
[0013] Aluminum (Al) is not only an element included for deoxidation of a steel material,
but also an element which is effective in stabilizing retained austenite by suppressing
precipitation of cementite. When the Al content is less than 0.01%, the deoxidation
of the steel material is not sufficiently achieved, and cleanliness of the steel material
is impaired. On the other hand, when the Al content is more than 0.3%, a temperature
required for single-phase region heating during annealing increases, and castability
of the steel material is impaired. Therefore, the Al content is preferably in a range
of 0.01 to 0.3%. A lower limit of the Al content is more preferably 0.02%. An upper
limit of the Al content is more preferably 0.25%, and even more preferably 0.2%.
Manganese (Mn): 2.6 to 3.0%
[0014] Manganese (Mn) is an element added to secure strength. When the Mn content is less
than 2.6%, it is difficult to secure strength therewith. On the other hand, when the
Mn content is more than 3.0%, a bainite transformation rate is slowed and too much
fresh martensite is formed, making it difficult to obtain high hole expandability.
In addition, a band structure may be formed due to segregation of Mn, which impairs
the material uniformity and formability of the material. Therefore, the Mn content
is preferably in a range of 2.6 to 3.0%. A lower limit of the Mn content is more preferably
2.7%. An upper limit of the Mn content is more preferably 2.9%.
Chromium (Cr): 0.01 to 0.25%
[0015] Chromium (Cr) is an element added to secure strength and hardenability. When Mn is
added alone, a very large amount of Mn should be added, exceeding the range of the
Mn content of the present disclosure. This problem can be solved by adding 0.01% or
more of Cr. On the other hand, when the Cr content is more than 0.25%, local corrosion
properties may deteriorate, hydrogen embrittlement cracks may occur, and oxides may
be formed on the surface, impairing phosphate treatment properties. Therefore, the
Cr content is preferably in a range of 0.01 to 0.25%. A lower limit of the Cr content
is more preferably 0.05%, and even more preferably 0.1%. An upper limit of the Cr
content is more preferably 0.2%, and even more preferably 0.15%.
Molybdenum (Mo): 0.15 to 0.4%
[0016] Molybdenum (Mo) is an element added to secure strength and hardenability. When the
Mo content is less than 0.15%, it is difficult to secure strength and hardenability.
On the other hand, when the Mo content is more than 0.4%, phase transformation is
suppressed, making it difficult to obtain a bainite structure, and as an expensive
element, economic feasibility in manufacturing a steel sheet deteriorates. Therefore,
the Mo content is preferably in a range of 0.15 to 0.4%. A lower limit of the Mo content
is more preferably 0.17%. An upper limit of the Mo content is more preferably 0.3%,
and even more preferably 0.23%.
Boron (B): 0.0001 to 0.005%
[0017] Boron (B) is an element added to secure hardenability. When Mn is added alone, a
very large amount of Mn should be added exceeding the range of the Mn content of the
present disclosure, but this problem can be solved by adding 0.0001% or more of B.
However, when the B content is more than 0.005%, B is excessively accumulated on the
surface, impairing plating adhesion of a plating material. Therefore, the B content
is preferably in a range of 0.0001 to 0.005%. A lower limit of the B content is more
preferably 0.0005%. An upper limit of the B content is more preferably 0.002%, and
even more preferably 0.0015%.
Niobium (Nb): 0.001 to 0.05%
[0018] Niobium (Nb) is an element added to secure strength of a steel sheet and refine a
microstructure thereof. When Nb is added in an amount of less than 0.001%, it is difficult
to obtain an effect of improving the strength and refining the microstructure. On
the other hand, when the Nb content is more than 0.05%, recrystallization is delayed
due to local grain fixation, thereby impairing the uniformity of the microstructure.
Therefore, the Nb content is preferably in a range of 0.001 to 0.05%. A lower limit
of the Nb content is more preferably 0.02%, and even more preferably 0.025%. An upper
limit of the Nb content is more preferably 0.04%, and even more preferably 0.035%.
Titanium (Ti): 0.001 to 0.05%
[0019] Titanium (Ti) is an element added to secure strength of a steel sheet and refine
a microstructure thereof. When Ti is added in an amount of less than 0.001%, it is
difficult to obtain an effect of improving the strength and refining the microstructure.
On the other hand, when the Ti content is more than 0.05%, castability is impaired
due to excessive formation of TiN, and recrystallization is delayed due to local grain
fixation, thereby impairing the uniformity of the microstructure. Therefore, the Ti
content is preferably in a range of 0.001 to 0.05%. A lower limit of the Ti content
is more preferably 0.01%, and even more preferably 0.015%. An upper limit of the Ti
content is more preferably 0.03%, and even more preferably 0.02%.
Phosphorus (P): 0.04% or less (excluding 0%)
[0020] Phosphorus (P) exists as an impurity in steel, which is advantageous to control the
P content as low as possible. However, considering the case in which P is inevitably
included, 0% is excluded (i.e., more than 0%). Meanwhile, P may be intentionally added
to increase the strength of a steel material, but when P is added excessively, toughness
of the steel material deteriorates. Therefore, in the present disclosure, an upper
limit of the P content is preferably limited to 0.04% to prevent this. The P content
is more preferably 0.02% or less, and even more preferably 0.01% or less.
Sulfur (S): 0.01% or less (excluding 0%)
[0021] Sulfur (S), like P, exists as an impurity in steel, and it is advantageous to control
the S content as low as possible. In addition, since S deteriorates ductility and
impact properties of steel, an upper limit of the S content is preferably limited
to 0.01%. The S content is more preferably 0.003% or less, and even more preferably
0.001% or less. However, considering the case in which S is inevitably included, 0%
is excluded (i.e., more than 0%).
Nitrogen (N): 0.01% or less (excluding 0%)
[0022] Nitrogen (N)is an impurity element, which is included in a steel material, and when
a large amount of N is contained, there is a risk that a large amount of nitrides
such as TiN and AlN, so it is advantageous that the N content be as low as possible.
Therefore, an upper limit of the N content is preferably to limit to 0.01%. The N
content is more preferably 0.05% or less, and even more preferably 0.03% or less.
However, considering the case in which N is inevitably included, 0% is excluded (i.e.,
more than 0%).
[0023] The remaining component of the present disclosure is iron (Fe). However, since in
the common manufacturing process, unintended impurities may be inevitably incorporated
from raw materials or the surrounding environment, the component may not be excluded.
Since these impurities are known to any person skilled in the common manufacturing
process, the entire contents thereof are not particularly mentioned in the present
specification.
[0024] Meanwhile, the cold-rolled steel sheet of the present disclosure may further include
one or two of Cu: 0.1% or less (excluding 0%) and Ni: 0.1% or less (excluding 0%).
Copper (Cu): 0.1% or less (excluding 0%) and Nickel (Ni): 0.1% or less (excluding
0%)
[0025] Copper (Cu) and nickel (Ni) are elements increasing strength of a steel material.
The above-described elements are elements of increasing the strength and hardenability
of the steel material. However, when an excessive amount of copper (Cu) and nickel
(Ni) are added, a target strength grade may be exceeded, and since copper (Cu) and
nickel (Ni) are expensive elements, which is disadvantageous from an economic perspective,
an upper limit of each of the contents of copper (Cu) and nickel (Ni) is preferably
0.1% or less. Meanwhile, in order to obtain better solid solution strengthening, a
lower limit of each of the contents of Cu and Ni may be 0.03%.
[0026] In addition, the cold-rolled steel sheet of the present disclosure may optionally
further include V: 0.05% or less (excluding 0%).
Vanadium (V): 0.05% or less (excluding 0%)
[0027] Vanadium (V) may increase strength of a steel material even with addition of a small
amount thereof, but the action thereof on improving elongation is not significant,
so the V content is preferably to be controlled to be 0.05% or less.
[0028] In addition, the cold-rolled steel sheet of the present disclosure is preferably
to satisfy the alloy composition described above, and at the same time, to satisfy
the Relational Expressions 1 and 2 below.
234 × [C] - 29 × [Si] - 128 × [Al] + 29 × [Mn] + 10 × [Cr] - 17 [Mo] - 37 × [Nb] -
49 × [Ti] + 100 [B] ≥ 80
[0029] When the above-described Relational Expression 1 is not satisfied, a fraction of
ferrite desired by the present disclosure is formed excessively during annealing conditions,
deteriorating not only yield strength but also hole expandability. In the above Relational
Expression 1, a value of a left side is more preferably 90 or more, and even more
preferably, 100 or more.
5× [C] + [Si] + 0.5 × [Al] ≤ 1.5
[0030] Meanwhile, according to an embodiment of the present disclosure, when a large amount
of alloying elements such as C, Si, and Al are added, spot weldability deteriorates,
and in particular, when spot welding is performed on a galvanized steel sheet, Liquid
Metal Embrittlement (LME) is caused. In general, spot welding of a steel material
is performed below a minimum current value at which expulsion occurs, and a minimum
current value at which expulsion occurs may be seen as the condition that can provide
the highest amount of heat input when performing actual spot welding. When LME resistance
is high, LME may not occur even at a welding current value above the minimum current
value at which expulsion occurs, and in this case, an AE value defined as a difference
obtained by subtracting the minimum current value at which expulsion occurs from the
minimum current value minimum current at which LME occurs has a positive value. That
is, welding is performed below the minimum current value at which expulsion occurs
during actual spot welding, and at this time, if LME does not occur, it can be determined
that the AE value is 0 or more. Meanwhile, the AE value has a unit of kA.
[0031] Relational Expression 2 is a component Relational Expression which derives a condition
for excellent LME resistance, that is, the AE value is 0 or more. When the Relational
Expression 2 is not satisfied, there is a problem that the LME resistance is reduced.
In the above Relational Expression 2, the value of the left side is more preferably
1.25 or less, and even more preferably 1.05 or less.
[0032] The microstructure of the cold-rolled steel sheet according to an embodiment of the
present disclosure preferably consists of: retained austenite: more than 1% and 5%
or less, fresh martensite: 10% or more and less than 25% (excluding 0%), bainite:
less than 20%, tempered martensite: 55% or more and less than 80%, and ferrite: 5%
or less (including 0%). A fraction of the microstructure described below refers to
% by area.
Retained austenite: more than 1% and less than 5%
[0033] Retained austenite is a structure increasing elongation of a steel material through
a TRIP effect. The higher the fraction, the higher the elongation may be obtained.
In the present disclosure, in order to obtain the required level of elongation, it
is preferable that the fraction is more than 1%. However, to obtain more than 5% of
austenite, a large amount of C and Si should be added, and in this case, spot welding
LME resistance deteriorates.
Fresh martensite: 10% or more and less than 25%
[0034] Fresh martensite is a structure advantageous for securing strength. When the fraction
of fresh martensite is less than 10%, tensile strength of a steel material may be
insufficient, but yield strength may be excessively high. When the fraction of fresh
martensite is 25% or more, the strength may be excessively high and hole expandability
may be low.
Bainite: less than 20% (excluding 0%)
[0035] Bainite is a structure having lower strength than martensite, but which is advantageous
for stabilizing retained austenite. However, when the bainite fraction is 20% or more,
the martensite fraction may be relatively low, which may cause a problem of insufficient
overall strength.
Tempered martensite: 55% or more and less than 80%
[0036] Tempered martensite is a structure advantageous for securing strength and hole expandability.
Tempered martensite is formed when the steel sheet is cooled below a martensite transformation
start point (Ms) during secondary cooling after annealing and then subjected to a
tempering heat treatment in the process of being reheated. When a fraction of tempered
martensite is less than 55%, which means that there is too much fresh martensite formed
during final cooling, and thus the strength becomes excessively high and hole expandability
becomes poor. In addition, when the fraction of tempered martensite is 80% or more,
a fraction of fresh martensite decreases and strength cannot be obtained.
Ferrite: 5% or less (including 0%)
[0037] Ferrite is a structure that has an adverse effect on yield strength and hole expandability,
and theoretically, a fraction of ferrite is preferably 0%. However, ferrite may inevitably
be formed during the manufacturing process, and when the fraction of ferrite is more
than 5%, the yield strength may be lowered and the hole expandability may also be
poor, so in the present disclosure, an upper limit of the fraction of ferrite is limited
to be 5%.
[0038] The cold-rolled steel sheet of the present disclosure provided as described above
may have a tensile strength of 1180 to 1350 MPa, a yield strength of 740 to 980 MPa,
an elongation of 8% or more, a hole expandability of 20% or more, and an AE value
of 0 kA or more, and thus excellent strength, ductility. hole expandability, and weldability
may be secured at the same time.
[0039] In addition, the cold-rolled steel sheet of the present disclosure may have a hot-dip
galvanized layer or an alloyed hot-dip galvanized layer formed on at least one surface
thereof. In the present disclosure, there is no particular limitation on the composition
of the hot-dip galvanized layer, and any hot-dip galvanized layer commonly applied
in the technical field may be preferably applied to the present disclosure. In addition,
the hot-dip galvanized layer may be an alloyed hot-dip galvanized layer alloyed with
some alloy components of the steel sheet.
[0040] Hereinafter, a method of manufacturing a cold-rolled steel sheet having excellent
weldability, strength, and formability according to an embodiment of the present disclosure
will be described.
[0041] First, a slab satisfying the above-described alloy composition and Relational Expressions
1 and 2 is heated. Although not particularly limited, a heating temperature when heating
the slab may be 1150 to 1250°C. When the slab heating temperature is lower than 1150°C,
it may not be possible to perform hot rolling, a subsequent operation. On the other
hand, when the slab heating temperature is more than 1250°C, a lot of energy is unnecessarily
consumed to increase the slab temperature. Therefore, it is preferable that the slab
heating temperature has a range from 1150 to 1250°C. A lower limit of the slab heating
temperature is more preferably 1170°C, and even more preferably 1180°C. An upper limit
of the slab heating temperature is more preferably 1230°C, and even more preferably
1220°C.
[0042] Thereafter, the heated slab is subjected to finish hot rolling at a temperature within
a range of 830 to 980°C to obtain a hot-rolled steel sheet. When the finishing hot
rolling temperature (hereinafter also referred to as 'FDT') is lower than 830°C, a
rolling load is increased and shape defects increase, thereby deteriorating productivity.
On the other hand, when the finishing hot rolling temperature is more than 980°C,
surface quality deteriorates due to an increase in oxides due to excessively high
temperature work. Therefore, it is preferable that the finish hot rolling temperature
has a range from 830 to 980°C. A lower limit of the finish hot rolling temperature
is more preferably 850°C, and even more preferably 880°C. An upper limit of the finish
hot rolling temperature is more preferably 950°C, and even more preferably 930°C.
[0043] Thereafter, the hot-rolled steel sheet is coiled at a temperature within a range
of 450 to 700°C. When the coiling temperature (hereinafter also referred to as 'CT')
is more than 700°C, coarse internal oxidation in hot rolling occurs, which may cause
a disadvantage of deteriorating surface properties. On the other hand, when the coiling
temperature is lower than 450°C, it corresponds to a transition boiling region, which
may cause a disadvantage of deteriorating controllability of the coiling temperature
and deteriorating the shape of the steel sheet. Therefore, it is preferable that the
coiling temperature has a range of 450 to 700°C. A lower limit of the coiling temperature
is 500°C. An upper limit of the coiling temperature is more preferably 650°C, and
even more preferably 620°C.
[0044] Meanwhile, although not particularly limited, after the finish hot rolling, cooling
may be performed at an average cooling rate of 10 to 110°C/s to the coiling temperature.
When the average cooling rate is less than 10°C/s, there is a disadvantage in that
hot rolling productivity is low and a cooling medium with low cooling capacity should
be deliberately adopted during actual production. When the average cooling rate is
more than 100°C/s, there is a disadvantage in that the temperature deviation inside
the steel sheet becomes uneven, causing the shape to deteriorate and the strength
of the steel sheet to become excessively high.
[0045] Thereafter, the coiled hot-rolled steel sheet is cold rolled to obtain a cold-rolled
steel sheet. During the cold rolling, a cold rolling reduction rate may be 30 to 60%.
When the cold rolling reduction rate is less than 30%, it may be difficult to secure
target thickness accuracy and correction of the shape of the steel plate may become
difficult. On the other hand, when the cold rolling reduction rate is more than 60%,
the possibility of cracks occurring at an edge of the steel sheet increases, and a
cold rolling load may become excessively large.
[0046] Thereafter, the cold-rolled steel sheet is continuously annealed at a temperature
within a range of 800 to 840°C. The continuous annealing is performed to heat a steel
sheet to an austenite single phase region to form austenite close to 100% and be used
for subsequent phase transformation. If the continuous annealing temperature (hereinafter
also referred to as 'SS') is lower than 800°C, sufficient recrystallization and austenite
transformation may not occur and ferrite at a level which is more than 5 % by area
may be generated. On the other hand, if the continuous annealing temperature is higher
than 840°C, productivity may decrease, coarse austenite may be formed and the material
may deteriorate, and surface quality such as peeling of a plating material may deteriorate.
Meanwhile, the continuous annealing may be performed in a continuous alloying hot
dip plating furnace.
[0047] Meanwhile, although not particularly limited, during the continuous annealing, an
atmosphere in a continuous annealing furnace may be controlled with a gas comprising,
by volume, 95% or more of nitrogen and a remainder of hydrogen. When the nitrogen
fraction is less than 95% and a ratio of hydrogen is not increased accordingly, an
oxidizing atmosphere is formed in the furnace and oxides are formed on a surface of
the steel sheet, deteriorating the surface quality. When the ratio of hydrogen increases,
process difficulties such as explosion prevention increase.
[0048] Thereafter, the continuously annealed steel sheet is primarily cooled at an average
cooling rate of less than 10°C/s to a primary cooling end temperature of 550 to 650°C
(hereinafter referred to as 'SCS'). The primary cooling end temperature may be defined
as a point in time at which secondary cooling (rapid cooling) is initiated by additionally
applying a quenching equipment that was not applied in primary cooling. When the cooling
process is divided into primary and secondary cooling and performed in stages, a temperature
distribution of the steel sheet may be made uniform in a slow cooling stage, a final
temperature and material deviation may be reduced, and a necessary phase composition
may be obtained. When the primary cooling end temperature is higher than 650°C, a
cooling amount of cooling to the secondary cooling end temperature may increase and
the shape of the steel sheet may deteriorate, and when the primary cooling end temperature
is lower than 550°C, a load of a slow cooling process increases. When the primary
cooling rate is 10°C/s or more, the amount of cooling in the secondary cooling increases,
resulting in an increase in the final temperature deviation and material deviation.
Meanwhile, when the primary cooling rate is less than 1°C/s, a large amount of ferrite
phases are formed during cooling, so that it may be difficult to obtain the target
microstructure and material. A lower limit of the primary cooling end temperature
is more preferably 570°C. An upper limit of the primary cooling end temperature is
more preferably 630°C. The primary cooling rate is even more preferably in the range
of 1°C/s or more and less than 10°C/s.
[0049] Thereafter, the primarily cooled steel sheet is secondarily cooled at an average
cooling rate of 10°C/s or more to a secondary cooling end temperature of 320 to 360°C
(hereinafter referred to as 'RCS'). The secondary cooling end temperature is set to
be a Ms temperature of the steel sheet or lower, so that martensite transformation
occurs during cooling, and this martensite ultimately becomes tempered martensite
through a reheating operation, which is a post-process. Since the Ms temperature of
1180MPa of a high-elongated steel sheet is mostly 400°C or lower, in the present disclosure,
the secondary cooling end temperature was controlled to be in a range of 320 to 360°C.
When the secondary cooling end temperature is lower than 320°C, an amount of initial
martensite transformation increases too much and the yield strength increases, resulting
in poor formability. On the other hand, when the secondary cooling end temperature
is more than 360°C, tempered martensite is not generated and a fraction of vulnerable
fresh martensite increases, resulting in poor yield strength and hole expandability.
When the secondary cooling rate is less than 10°C/s, even if the target secondary
cooling end temperature is reached, high-temperature phase transformation occurs during
cooling, so that it may not obtain the target martensite fraction and high strength.
A lower limit of the second cooling stop temperature is more preferably 330°C. An
upper limit of the secondary cooling stop temperature is more preferably 350°C.
[0050] Meanwhile, as mentioned above, the secondary cooling may be performed by additionally
using a quenching equipment which was not applied in the primary cooling, and in the
present disclosure, the type of the quenching equipment is not particularly limited,
but a hydrogen quenching equipment may be used as a preferred example. More specifically,
the hydrogen quenching equipment may use a gas consisting of 5 to 80% hydrogen and
a remainder of nitrogen by volume. When the hydrogen fraction is more than 80%, there
may be a disadvantage in that it becomes difficult to manage equipment such as explosion
control of the equipment, and when the hydrogen fraction is less than 5%, there may
be a disadvantage in that it becomes difficult to utilize the efficient heat transfer
characteristics of hydrogen, which is a light element.
[0051] Thereafter, the secondarily cooled steel sheet is reheated to a temperature range
of 380 to 480°C. Through the above-described process, carbon distribution between
phases and additional bainite phase transformation required for stabilization of retained
austenite are obtained. In the present disclosure, an end point temperature of the
heating section is referred to as a reheating temperature (hereinafter also referred
to as 'RHS') for convenience. When the reheating temperature is lower than 380°C,
the strength becomes excessively high and the elongation deteriorates. On the other
hand, when the reheating temperature is more than 480°C, an austenite phase remains
untransformed and a rate of fresh martensite, which is transformed during final cooling,
increases, thereby impairing hole expandability and elongation. Meanwhile, a temperature
at which bainite transformation is performed most actively, the so-called nose temperature,
is about 400 to 420°C. In consideration thereof, it is more preferable to maintain
the reheating temperature in a range of 400 to 420°C.
[0052] Meanwhile, although not particularly limited, during the reheating, an average temperature
increase rate may be 0.5 to 2.5°C/s. When the average temperature increase rate is
less than 0.5°C/s, an overall process time may become too long, which may cause a
problem of an excessive heat treatment, and when the average temperature increase
rate is more than 2.5°C/s, it may be difficult to secure the target physical properties
in the present disclosure.
[0053] According to an embodiment of the present disclosure, after the reheating operation,
if necessary, the cold-rolled steel sheet may be additionally subjected to a hot-dip
galvanizing, alloyed hot-dip galvanizing, or temper rolling process.
[0054] Specifically, an operation of hot dip galvanizing the reheated cold-rolled steel
sheet in a plating bath at a temperature within a range of 450 to 470°C may be further
included. In addition, if necessary, an operation of performing an alloying heat treatment
of the hot-dip galvanized cold-rolled steel sheet may be further included bath at
a temperature within a range of 470 to 550°C. The alloying heat treatment is performed
to obtain an appropriate alloying level, the temperature may be determined by a surface
condition of the steel sheet. By controlling the surface condition of a steel material,
an alloying heat treatment temperature should not exceed 550°C to prevent softening
of the steel sheet and loss of retained austenite due to excessive temperature. Meanwhile,
in order to quickly proceed with alloying, the alloying heat treatment temperature
is preferably higher than the hot-dip galvanizing temperature, so the lower limit
may be controlled to a temperature of 470°C. In addition, after performing the alloying
heat treatment, in order to correct the shape of the steel sheet and adjust the yield
strength, an operation in which the alloyed heat treated cold-rolled steel sheet is
cooled to room temperature and then temper rolled at a reduction rate of less than
1% may be further included.
Mode for Invention
[0055] Hereinafter, the present disclosure will be specifically described through the following
Examples. However, it should be noted that the following examples are only for describing
the present disclosure by illustration, and not intended to limit the right scope
of the present disclosure. The reason is that the right scope of the present disclosure
is determined by the matters described in the claims and reasonably inferred therefrom.
(Example)
[0056] A slab having the alloy composition shown in Table 1 below was prepared and then
reheated at a temperature within a range of 1180 to 1220°C, and was subjected to hot
rolling, coiling, primary cooling, secondary cooling, and reheating processes under
the conditions shown in Table 2 below to manufacture a cold-rolled steel sheet. In
this case, after finishing hot rolling, the cooling rate was 30 to 50°C/s, the cold
rolling reduction rate was 33 to 55%, and the gas used during continuous annealing
was 95% N by volume to 5% H by volume, and the gas used during secondary cooling was
75% H by volume to 25% N by volume.
[0057] A microstructure and mechanical properties of the cold-rolled steel sheet prepared
as described above were measured, and the results thereof were shown in Table 3 below.
[0058] The microstructure was measured using a Point Counting method from a photograph using
a scanning electron microscope (SEM), and a fraction of retained austenite was measured
using XRD.
[0059] Among the mechanical properties, yield strength YS, tensile strength TS, and elongation
EL were measured through a tensile test in a direction perpendicular to rolling. A
test specimen having a gauge length of 50 mm and a width of a tensile specimen of
25 mm was used.
[0060] Among the mechanical properties, hole expandability (HER) was measured according
to ISO 16330 standards, and a hole was sheared with a clearance of 12% using a 10mm
diameter punch.
[0061] Meanwhile, hot-dip galvanizing (GI) was performed on the cold-rolled steel sheet
under the conditions shown in Table 2 below, an alloying heat treatment (GA) was performed
on some steel types, and spot welding was performed to measure an AE value, and the
results there of were shown in Table 3 below. The AE value refers to a value obtained
by subtracting a minimum current value at which expulsion occurs from a minimum current
value at which LME occurs. In the spot welding test, a current was increased in a
unit of 0.5 kA from a low current value, but a short cooling time was given between
each current value to prevent excessive heat input to the material. As the current
value is increased in this manner, a minimum current value at which a nugget in a
weld zone expulsions was measured, and at the same time, a minimum current value at
which LME occurs is measured from observation of a surface and cross-section of the
weld zone, and then the results thereof were shown in Table 3 below. Regarding whether
LME occurs, when the surface of the weld zone was observed at 10x magnification and
the cross-section thereof was observed at 100x magnification, a case in which no cracks
due to LME were observed were evaluated as pass, and a case in which cracks were observed
were evaluated as fail.
[0062] In addition, a hole with a diameter of 10 mm was drilled in the cold-rolled steel
sheet using a punch with a clearance of 12%, immersed in a hydrochloric acid solution
of 0.1 normal concentration and corroded for 100 hours, and then whether hydrogen
embrittlement cracks occur in the punched region was evaluated.
[Table 1]
Ste el typ e No. |
Alloy composition(weight %) |
C |
Si |
Al |
Mn |
Cr |
Mo |
B |
Nb |
Ti |
P |
S |
N |
Relat ion 1 |
Relati on2 |
A |
0.1 49 |
0. 41 |
0.0 85 |
2. 85 |
0. 18 |
0. 21 |
0.00 18 |
0.0 31 |
0.01 8 |
0.00 66 |
0.00 08 |
0.00 41 |
91.1 |
1.20 |
B |
0.1 |
0. 57 |
0.0 9 |
2. 62 |
0. 03 |
0. 12 |
0.00 1 |
0.0 22 |
0.02 1 |
0.00 95 |
0.00 15 |
0.00 34 |
67.8 |
1.12 |
C |
0.1 2 |
0. 42 |
0.3 15 |
2. 42 |
0. 41 |
0. 05 |
0.00 02 |
0.0 15 |
0.01 7 |
0.00 72 |
0.00 24 |
0.00 45 |
47.6 |
1.18 |
D |
0.1 8 |
0. 72 |
0.0 34 |
2. 57 |
0. 67 |
0. 19 |
0.00 12 |
0.0 33 |
0.01 2 |
0.00 53 |
0.00 19 |
0.00 42 |
93.2 |
1.64 |
E |
0.1 |
1. |
0.0 |
2. |
0. |
0. |
0.00 |
0.0 |
0.01 |
0.00 |
0.00 |
0.00 |
83.6 |
2.17 |
|
9 |
21 |
23 |
63 |
52 |
15 |
04 |
26 |
7 |
58 |
21 |
57 |
|
|
F |
0.1 55 |
0. 39 |
0.0 33 |
2. 72 |
0. 21 |
0. 26 |
0.00 08 |
0.0 29 |
0.02 1 |
0.00 82 |
0.00 14 |
0.00 33 |
95.3 |
1.18 |
G |
0.1 54 |
0. 51 |
0.0 52 |
2. 61 |
0. 24 |
0. 22 |
0.00 02 |
0.0 42 |
0.00 23 |
0.00 74 |
0.00 12 |
0.00 43 |
87.3 |
1.31 |
[Relation 1] 234×[C] - 29×[Si] - 128×[Al] + 29×[Mn] + 10×[Cr] - 17×[Mo] -37×[Nb] -
49×[Ti] + 100×[B] ≥ 80 |
[Relation 2] 5× [C] + [Si] + 0.5× [Al] ≤ 1.5 |
[Table 2]
Division |
Ste el typ e |
Thickn ess of hot-rolled materi al (mm) |
FD T (° C) |
CT (° C) |
Thickn ess of cold-rolled materi al (mm) |
SS (° C) |
Prima ry avera ge cooli ng rate (°C/s ) |
SC S (° C) |
Second ary averag e coolin g rate (°C/s) |
RC S (° C) |
RH S (° C) |
GI PO T (° C) |
GA (° C) |
Comparat ive Example 1 |
A |
2.7 |
93 8 |
58 2 |
1.6 |
83 2 |
4.1 |
60 5 |
13.9 |
31 2 |
44 3 |
45 8 |
51 7 |
Inventiv e Example 1 |
A |
2.1 |
92 5 |
59 3 |
1.2 |
83 3 |
4.0 |
59 2 |
11.6 |
33 2 |
44 0 |
46 0 |
50 9 |
Inventiv e Example 2 |
A |
2.4 |
94 1 |
60 5 |
1.4 |
82 9 |
3.6 |
61 2 |
11.7 |
34 9 |
43 3 |
46 3 |
51 1 |
Comparat ive Example 2 |
A |
2.6 |
91 2 |
59 6 |
1.6 |
83 2 |
4.4 |
58 8 |
10.4 |
36 8 |
43 2 |
46 0 |
- |
Comparat ive Example 3 |
B |
2.4 |
92 1 |
63 2 |
1.2 |
81 1 |
4.1 |
58 2 |
12.3 |
32 2 |
43 3 |
46 2 |
- |
Comparat ive Example 4 |
C |
2.4 |
89 9 |
56 5 |
1.2 |
82 5 |
3.3 |
63 3 |
14.0 |
32 6 |
45 1 |
45 8 |
51 9 |
Comparat ive Example 5 |
D |
2.5 |
91 6 |
61 7 |
1.3 |
82 1 |
4.3 |
57 2 |
11.4 |
32 3 |
44 8 |
46 3 |
- |
Comparat ive Example 6 |
E |
2.2 |
88 2 |
66 4 |
1.1 |
81 2 |
3.6 |
62 2 |
15.2 |
32 1 |
43 5 |
46 1 |
50 4 |
Inventiv e Example 3 |
F |
2.7 |
88 7 |
55 4 |
1.6 |
83 3 |
3.9 |
59 3 |
11.3 |
32 8 |
42 1 |
45 9 |
- |
Inventiv e Example 4 |
G |
2.1 |
91 1 |
61 1 |
1.1 |
82 7 |
4.1 |
60 4 |
13.2 |
33 6 |
43 6 |
46 1 |
51 1 |
[Table 3]
Divisio n |
Microstructure (area) |
Mechanical properties |
LME properties |
Whether hydrogen embrittle ment cracks occur |
RA |
FM |
B |
TM |
F |
YS (MP a) |
TS (MP a) |
EL (% ) |
HE R (% ) |
AE val ue (kA ) |
Minimu m curren t value at which expuls ion occurs (kA) |
Mini mum curr ent valu e at whic h LME occu rs (kA) |
Whet her LME occu rs |
Compara tive Example 1 |
3 |
8 |
10 |
77 |
2 |
101 1 |
119 8 |
11 |
40 |
1.5 |
10.5 |
12 |
Pass |
Not occur |
Inventi ve Example 1 |
3 |
14 |
10 |
71 |
2 |
868 |
126 0 |
10 |
33 |
1 |
11 |
12 |
Pass |
Not occur |
Inventi ve Example 2 |
2 |
21 |
12 |
62 |
3 |
843 |
132 3 |
9 |
26 |
1.5 |
10.5 |
12 |
Pass |
Not occur |
Compara tive Example 2 |
3 |
33 |
25 |
36 |
3 |
912 |
137 2 |
8 |
18 |
1 |
10.5 |
11.5 |
Pass |
Not occur |
Compara tive Example 3 |
3 |
15 |
21 |
36 |
25 |
721 |
112 3 |
13 |
12 |
1.5 |
10 |
11.5 |
Pass |
Not occur |
Compara tive Example 4 |
3 |
14 |
11 |
38 |
34 |
689 |
110 7 |
12 |
13 |
1.5 |
10 |
11.5 |
Pass |
Occur |
Compara tive Example 5 |
4 |
15 |
11 |
68 |
2 |
878 |
119 5 |
11 |
28 |
- 0.5 |
11.5 |
11 |
Fail |
Occur |
Compara tive Example 6 |
7 |
12 |
13 |
65 |
3 |
923 |
122 7 |
13 |
35 |
-1 |
12 |
11 |
Fail |
Occur |
Inventi ve Example 3 |
2 |
17 |
11 |
68 |
2 |
921 |
123 3 |
10 |
31 |
1 |
10.5 |
11.5 |
Pass |
Not occur |
Inventi ve Example 4 |
3 |
19 |
12 |
64 |
2 |
888 |
122 5 |
9 |
29 |
0.5 |
11 |
11.5 |
Pass |
Not occur |
RA: Retained Austenite, FM: Fresh Martensite, B: Bainite, TM: Tempered Martensite,
F: Ferrite |
[0063] As can be seen from Tables 1 to 3, in Inventive Examples 1 to 4 satisfying the alloy
composition, Relational Expressions 1 and 2, and manufacturing conditions, proposed
by the present disclosure, it can be seen that the cold-rolled steel sheet not only
has a tensile strength of 1180 to 1350MPa, a yield strength of 740 to 980MPa, an elongation
of 8% or more, and hole expandability of 20% or more, but also has excellent LME properties.
[0064] On the other hand, in Comparative Examples 1 and 2 in which the alloy composition
and Relational Expressions 1 and 2 of the present disclosure were satisfied, but a
secondary cooling end temperature was outside the range of the present disclosure,
it can be seen that the microstructure desired by the present disclosure was not secured,
and the yield strength was too high or the hole expandability was lowered to less
than 20%, resulting in poor formability.
[0065] In Comparative Examples 3 and 4, the manufacturing conditions of the present disclosure
were satisfied, but the alloy composition and Relational Expression1 of the present
disclosure were not satisfied, so it can be seen that the microstructure desired by
the present disclosure cannot be secured and the mechanical properties are inferior.
[0066] In Comparative Examples 5 and 6, the manufacturing conditions of the present disclosure
were satisfied, but the alloy composition and Relational Expression2 of the present
disclosure were not satisfied, so it can be seen that the LME properties were inferior.
[0067] In particular, in Comparative Examples 4, 5, and 6, it can be seen that hydrogen
embrittlement cracks occurred due to excessive addition of Cr.
1. A cold-rolled steel sheet, comprising by weight:
C: 0.14 to 0.16%, Si: 0.3 to 0.6%, Al: 0.01 to 0.3%, Mn: 2.6 to 3.0%, Cr: 0.01 to
0.25%, Mo: 0.15 to 0.4%, B: 0.0001 to 0.005%, Nb: 0.001 to 0.05%, Ti: 0.001 to 0.05%,
P: 0.04% or less (excluding 0%), S: 0.01% or less (excluding 0%), N: 0.01% or less
(excluding 0%), with a remainder of Fe and other unavoidable impurities, wherein the
following Relational Expressions 1 and 2 are satisfied,
wherein a microstructure consists of retained austenite: more than 1% and 5% or less,
fresh martensite: 10% or more and less than 25%, bainite: less than 20% (excluding
0%), tempered martensite: 55% or more and less than 80%, and ferrite: 5% or less (including
0%),
234 × [C] - 29 × [Si] - 128 × [Al] + 29 × [Mn] + 10 × [Cr] - 17 [Mo] - 37 × [Nb] -
49 × [Ti] + 100 [B] ≥ 80
5× [C] + [Si] + 0.5 × [Al] ≤ 1.5
where a content of each element in the above Relational Expressions 1 and 2 refers
to % by weight.
2. The cold-rolled steel sheet of claim 1, wherein the cold-rolled steel sheet further
comprises one or two of Cu: 0.1% or less (excluding 0%) and Ni: 0.1% or less (excluding
0%).
3. The cold-rolled steel sheet of claim 1, wherein the cold-rolled steel sheet further
comprises V: 0.05% or less (excluding 0%).
4. The cold-rolled steel sheet of claim 1, wherein the cold-rolled steel sheet has a
tensile strength of 1180 to 1350 MPa, a yield strength of 740 to 980 MPa, an elongation
of 8% or more, hole expandability of 20% or more, and an AE value of 0 kA or more,
where the AE value refers to a difference obtained by subtracting a minimum current
value at which expulsion occurs from a minimum current value at which LME occurs.
5. The cold-rolled steel sheet of claim 1, wherein the cold-rolled steel sheet has a
hot-dip galvanized layer or alloyed hot-dip galvanized layer formed on at least one
surface of the cold-rolled steel sheet.
6. A method for manufacturing a cold-rolled steel sheet, comprising:
heating a slab including by weight: C: 0.14 to 0.16%, Si: 0.3 to 0.6%, Al: 0.01 to
0.3%, Mn: 2.6 to 3.0%, Cr: 0.01 to 0.25%, Mo: 0.15 to 0.4%, B: 0.0001 to 0.005%, Nb:
0.001 to 0.05%, Ti: 0.001 to 0.05%, P: 0.04% or less (excluding 0%), S: 0.01% or less
(excluding 0%), N: 0.01% or less (excluding 0%), with a remainder of Fe and other
unavoidable impurities, wherein the following Relational Expressions 1 and 2 are satisfied;
finish hot rolling the heated slab at a temperature within a range of 830 to 980°C
to obtain a hot-rolled steel sheet;
coiling the hot-rolled steel sheet at a temperature within a range of 450 to 700°C;
cold rolling the coiled hot-rolled steel sheet to obtain a cold-rolled steel sheet;
continuously annealing the cold-rolled steel sheet at a temperature within a range
of 800 to 840°C;
primarily cooling the continuously annealed steel sheet at an average cooling rate
of less than 10°C/s to a primary cooling end temperature of 550 to 650°C;
secondarily cooling the primarily cooled steel sheet at an average cooling rate of
10°C/s or more to a secondary cooling end temperature of 320 to 360°C; and
reheating the secondarily cooled steel sheet to a temperature within a range of 380
to 480°C,
234 × [C] - 29 × [Si] - 128 × [Al] + 29 × [Mn] + 10 × [Cr] - 17 [Mo] - 37 × [Nb] -
49 × [Ti] + 100 [B] ≥ 80
5× [C] + [Si] + 0.5 × [Al] ≤ 1.5
where a content of each element in the above Relational Expressions 1 and 2 refers
to % by weight.
7. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein the slab
further comprises one or two of Cu: 0.1% or less (excluding 0%) and Ni: 0.1% or less
(excluding 0%).
8. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein the slab
further comprises V: 0.05% or less (excluding 0%).
9. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein when the
slab is heated, a heating temperature is 1150 to 1250°C.
10. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein after the
finish hot rolling is performed, cooling is performed at an average cooling rate of
10 to 100°C/s to a coiling temperature.
11. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein during
the cold rolling, a cold rolling reduction rate is 30 to 60%.
12. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein during
the continuous annealing, an atmosphere in a continuous annealing furnace is controlled
with a gas consisting of by volume, 95% or more of nitrogen and a remainder of hydrogen.
13. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein during
the secondary cooling, a gas consisting of by volume, 5 to 80% of hydrogen and a remainder
of nitrogen is used.
14. The method for manufacturing a cold-rolled steel sheet of claim 6, wherein during
the reheating, an average temperature increase rate is 0.5 to 2.5°C/s.
15. The method for manufacturing a cold-rolled steel sheet of claim 6, further comprising,
after the reheating:
hot-dip galvanizing the cold-rolled steel sheet in a plating bath at a temperature
within a range of 450 to 470 °C.
16. The method for manufacturing a cold-rolled steel sheet of claim 15, further comprising,
after the hot-dip galvanizing:
performing an alloying heat treatment of the cold-rolled steel sheet at a temperature
within a range of 470 to 550°C.
17. The method for manufacturing a cold-rolled steel sheet of claim 16, further comprising,
after performing the alloying heat treatment:
in which the cold-rolled steel sheet is cooled to room temperature, and then temper
rolled at a reduction rate of less than 1%.