Title of the invention: Steel sheet and its manufacturing method
Technical field
[0001]
The present invention relates to a steel sheet and a method for manufacturing the same. The present application claims priority based on Japanese Patent Application No. 2020-001531 filed in Japan on January 8, 2020, the contents of which are incorporated herein by reference.
Background technology
[0002]
In recent years, automobiles have high strength in order to reduce the weight of the vehicle body, improve fuel efficiency, reduce carbon dioxide emissions, and to absorb collision energy in the event of a collision to ensure the protection and safety of passengers. Steel plates are often used. However, in general, when the strength of the steel sheet is increased, the deformability (ductility, bendability, etc.) decreases. If the deformability of the steel sheet is reduced, the dimensional accuracy during press forming may not be excellent.
[0003]
For example, Patent Document 1 discloses a high-strength steel plate having a tensile strength of 900 MPa or more that can achieve both high strength and excellent formability. In Patent Document 1, in the steel structure, ferrite is 5% or more and 80% or less, autotempered martensite is 15% or more, bainite is 10% or less, retained austenite is 5% or less, and as hardened. Martensite is 40% or less, the average hardness of autotempered martensite is HV ≤ 700, and the average number of iron-based carbides deposited in autotempered martensite of 5 nm or more and 0.5 μm or less is 5 per 1 mm 2. × 10 4 or more.
[0004]
Patent Document 2 discloses a thin steel sheet having a tensile strength of 900 MPa or more, good weldability, and good elongation. In the thin steel sheet of Patent Document 2, ferrite is 25% or more and 65% or less in area ratio, martensite in which iron-based carbides are precipitated in martensite grains is 35% or more and 75% or less in area ratio, and the ferrite and the remaining structure are The total area ratio other than the martensite is 20% or less (including 0%), the average particle size of the ferrite and the martensite is 5 μm or less, respectively, and Si on the interface between the ferrite and the martensite. And have a steel structure in which the sum of Mn is 5% or more in atomic concentration.
[0005]
Patent Document 3 contains a total of 60 area% or more of ferrite and bainite, and 3 area% or more and 20 area% or less of retained austenite, and the average particle size of the ferrite and bainite is 0.5 μm or more and 6.0 μm. Hereinafter, the Mn-enriched portion having a steel structure in which the C concentration in the retained austenite is 0.5% by mass or more and 1.2% by mass or less and extending in the rolling direction at a depth of 50 μm from the surface of the steel sheet and the Mn-concentrated portion. It has an element concentration distribution in which the average spacing of the Si-enriched portions in the direction perpendicular to rolling is 1000 μm or less, the maximum depth of cracks on the surface of the steel sheet is 4.5 μm or less, and the width is 6 μm or less and the depth is 2 μm or more. It has a surface texture with a crack number density of 10 pieces / 50 μm or less, and a work hardening index (n 3-8) in a plastic strain region with a tensile strength (TS) of 800 MPa or more and 1200 MPa or less, 3% or more, and 8% or less. ) Is 0.10 or more, and a cold-rolled steel sheet having mechanical properties in which the bendability satisfies the formula (R / t ≦ 1.5) is disclosed.
[0006]
Patent Document 4 describes in terms of mass%, C: 0.03% or more and 0.15% or less, Si: 1.5% or less, Mn: 0.6% or less, P: 0.05% or less, S: 0. It has a composition containing 0.01% or less, Al: 0.08% or less, N: 0.0080% or less, Ti: 0.04% or more and 0.18% or less, and the area ratio of the ferrite phase is 90% or more. The variation in the area ratio of the ferrite phase in the coil surface is 3% or less, the area ratio of the processed ferrite with respect to the ferrite phase is 15% or less, and the average particle diameter of the carbide containing Ti in the crystal grains of the ferrite phase is 10 nm. Hereinafter, a high-strength cold-rolled steel plate in which the ratio of the amount of Ti present in the matrix as a solid solution to the amount of Ti contained is less than 10% is disclosed.
[0007]
However, as a result of the examination by the present inventors, it was found that the dimensional accuracy at the time of press molding may not be sufficient in Patent Documents 1 to 4.
Prior art literature
Patent documents
[0008]
Patent Document 1: International Publication No. 2009/096596
Patent Document 2: International Publication No. 2018/03503
Patent Document 3: Japanese Patent No. 5569929
Patent Document 4: Japanese Patent Application Laid-Open No. 2015-147967
Outline of the invention
Problems to be solved by the invention
[0009]
As described above, the present invention has been made in view of the fact that high-strength steel sheets are required to improve dimensional accuracy during press forming in addition to improving formability and strength. The present invention relates to high-strength steel sheets (including galvanized steel sheets, zinc alloy plated steel sheets, alloyed zinc plated steel sheets, and alloyed zinc alloy plated steel sheets), which are excellent in formability, strength, and dimensional accuracy during press molding. It is an object of the present invention to provide a manufacturing method.
Means to solve problems
[0010]
As a result of studies by the present inventors in order to solve the above problems, the present inventors obtained the following findings.
In order to obtain a steel sheet with excellent formability, strength and dimensional accuracy during press forming, it is necessary to suppress fluctuations in the characteristics of the steel sheet in the plate width direction, which increases the variation in dimensional accuracy during press forming. Specifically, it is important to suppress fluctuations in the area ratio of ferrite, the average crystal grain size of ferrite, the area ratio of unrecrystallized ferrite, and the average diameter of carbonitride in the plate width direction of the steel sheet.
[0011]
The gist of the present invention made based on the above findings is as follows.
[1] The steel sheet according to one aspect of the present invention is
Ingredient composition is mass%,
C: 0.035 to 0.150%,
Si: 0.010 to 1.500%,
Mn: 0.10 to 3.00%,
Al: 0.005 to 1.000%,
P: 0.100% or less,
S: 0.0200% or less,
N: 0.0150% or less,
O: 0.0100% or less,
V: 0 to 0.50%,
Cr: 0 to 1.00%,
Ni: 0 to 1.00%,
Cu: 0 to 1.00%,
Mo: 0 to 1.00%,
W: 0 to 1.00%,
B: 0 to 0.0100%,
Sn: 0 to 1.00%,
Sb: 0 to 0.20%,
Nb: 0 to 0.060%,
Ti: 0 to 0.100%,
Ca: 0-0.0100%,
Mg: 0 to 0.0100%,
Zr: 0-0.0100%,
REM: 0-0.0100%, and
Remaining: Fe and impurities,
Satisfy the following formulas (1-1) to (1-3)
The microstructure in the 1/4 width portion, which is 1/4 of the plate width in the plate width direction from the end in the plate width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, and the plate from the end in the plate width direction. The microstructure in the 1/2 width portion, which is 1/2 of the plate width in the width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, and 3 of the plate width in the plate width direction from the end in the plate width direction. The microstructure in the 3/4 width portion, which is the / 4 position and the 1/4 position of the plate thickness in the plate thickness direction from the surface,
Area%, ferrite: 80% or more, martensite: 2% or less, retained austenite: 2% or less, and residual structure.
The ratio of unrecrystallized ferrite to the ferrite is 5 to 60%.
The average diameter of the carbonitride is 6.0 to 30.0 nm,
Satisfy the following formulas (2) to (5)
0.2% proof stress is 280-600MPa,
Tensile strength is 450-800 MPa,
The yield ratio is 0.50 to 0.90, and
Uniform elongation is 10.0% or more
A steel plate characterized by that.
1.5 x Nb + Ti ≧ 0.015 ... (1-1)
0.03 ≤ {(Ti / 48-N / 14) + Nb / 93} / (C / 12) ≤ 0.40 ... (1-2)
Ca + Mg + Zr + REM ≤ 0.0100 ... (1-3)
Δ SF / μ SF ≤ 0.10 ... (2)
Δ dF / μ dF ≦ 0.20… (3)
Δ SUF ≤ 20 ... (4)
Δ dC / μ dC ≦ 0.50 ... (5)
Ti, N, Nb, C, Ca, Mg, Zr and REM in the above formulas (1-1) to (1-3) indicate the content of each element in mass% and do not contain the element. In the case, 0% is substituted, and when the value of (Ti / 48-N / 14) becomes negative, 0 is substituted as the value of (Ti / 48-N / 14).
The μ SF in the formula (2) is the area ratio of ferrite in the microstructure in the 1/4 width portion, the area ratio of ferrite in the microstructure in the 1/2 width portion, and the 3/4 width portion. It is the average value of the area ratio of ferrite in the microstructure in the width portion, and ΔSF is the area of ​​ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. The difference between the maximum and minimum rates
The μdF in the formula (3) is the average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the average crystal grain size of ferrite in the microstructure in the 1/2 width portion, and It is the average value of the average crystal grain size of ferrite in the microstructure in the 3/4 width portion, and Δ dF is the micro in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. It is the difference between the maximum and minimum values ​​of the average crystal grain size of ferrite in the structure.
ΔSUF in the formula (4) is the maximum and minimum values ​​of the area ratio of unrecrystallized ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. Is the difference between
The μdC in the formula (5) is the average diameter of the carbonitride in the microstructure in the 1/4 width portion, the average diameter of the carbonitride in the microstructure in the 1/2 width portion, and It is the average value of the average diameters of the carbonitrides in the microstructure in the 3/4 width portion, and Δ dC is the micro in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. It is the difference between the maximum value and the minimum value of the average diameter of the carbonitride in the structure.
[2] The steel sheet according to the above [1] may have a component composition of Mn: 0.70 to 3.00% in mass%.
[3] The steel sheet according to [1] or [2] has an average crystal grain size of 5.0 to the ferrite in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. It may be 15.0 μm.
[4] The steel sheet according to any one of the above [1] to [3] may have a zinc-plated layer on the surface.
[5] The steel sheet according to any one of the above [1] to [3] may have a zinc alloy plating layer on the surface thereof.
[6] The steel sheet according to the above [4] or [5] has an Fe content of 7.0 to 13.0% in mass% in the zinc plating layer or the zinc alloy plating layer. good.
[7] The method for producing a steel sheet according to another aspect of the present invention is the method for producing a steel sheet according to any one of the above [1] to [3].
The steel piece having the component composition described in the above [1] is heated to 1150 to 1320 ° C., hot rolling is completed so that the hot rolling completion temperature becomes 850 to 930 ° C., and the steel piece is cooled after 1.5 s or more. The hot rolling process of cooling to a temperature range of less than 450 ° C. to obtain a hot-rolled steel sheet so that the average cooling rate in the temperature range of 800 to 450 ° C. is 20 ° C./s or more.
A reheating process that heats the hot-rolled steel sheet to a temperature range of 450 to 700 ° C.
A cooling process that cools the hot-rolled steel sheet to room temperature,
A cold rolling process in which the hot-rolled steel sheet is cold-rolled so that the total reduction ratio is 30 to 80% and the cold-rolling completion temperature is 120 ° C. or higher to obtain a cold-rolled steel sheet.
It has an annealing step of heating the cold-rolled steel sheet to an annealing temperature of 720 to 850 ° C. and cooling it to a temperature range of 500 ° C. or lower.
In the hot rolling process,
Satisfy the following formula (6) in the temperature range of 1000 ° C or less,
In the reheating process,
In the temperature range of 450 to 700 ° C, the following formula (7-1) and the following formula (8) are satisfied.
In the annealing process,
In the heating process to the annealing temperature
Satisfy the following formula (9) in the temperature range of 550 to 720 ° C.
In the temperature range from 720 ° C to the annealing temperature, a tension of 15 MPa or more is applied, and the following formula (10) is satisfied.
In the cooling process from the annealing temperature
Satisfy the following formula (11) in the temperature range of 720 to 500 ° C.
A method for manufacturing a steel sheet, which is characterized in that.
[Number 1]

In the above formula (6), f n is in the temperature range of 1000 ° C. or lower in the hot rolling process. It is an index showing the progress of precipitation of fine carbides. Each reference numeral in the above equation (6) represents the following.
N: Number of rolling passes at 1000 ° C or lower
H: Plate thickness [mm] before rolling on the nth pass
H *: Plate thickness [mm] after rolling on the nth pass
Nb and Ti: Nb and Ti content [mass%]
T n: Average steel sheet temperature from rolling in the nth pass to rolling in the n + 1th pass [° C]
T n: The shorter time [s] from the rolling of the nth pass to the rolling of the n + 1th pass, or the time [s] from the rolling of the nth pass to the decrease of the steel sheet temperature to reach 800 ° C.
a 1 to 11: Constants (a 1 = 2.28 × 100, a 2 = 1.25 × 100, a 3 = 7.86 × 10 -4, a 4 = 1.36 × 10 -3, a 5 = 6.76 × 10 -4, a 6 = 7.86 × 10 -4, a 7 = 2.13 × 10 -3, a 8 = 1.14 × 10 -3, a 9 = 6.70 × 10- 2, a 10 = 1.11 × 100, a 11 = 5.27 × 10 -1)
[Number 2]

In the above formula (7-1), each reference numeral represents the following.
b 1-7: Constants (b 1 = 6.82 × 10 6, b 2 = 1.00 × 10 3, b 3 = 8.70 × 10 1, b 4 = 1.25 × 10 2, b 5 = 1.00 × 10 2, b 6 = -1.50 × 10 1, b 7 = -2.50 × 10 1)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T max: Maximum heating temperature (° C)
T 20: Effective heat treatment time (s) in the 20th section when the staying time in the temperature range of 450 to 700 ° C. is divided into 20 equal parts.
D 20: An index showing the effective diffusion rate in the 20th section when the staying time in the temperature range of 450 to 700 ° C is divided into 20 equal parts.
However, the m-th effective heat treatment time tm and the m-th effective diffusion rate index D m are expressed by the following formula (7-2).
[Number 3]

In the above formula (7-2), each reference numeral represents the following.
M: Integer from 1 to 20
B 9-11: Constants (b 8 = 6.81 × 10 1, b 9 = 2.61 × 10 5, b 10 = 5.60 × 100, b 11 = 2.86 × 105)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T m: Average steel plate temperature [° C] in the m-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
T m: Effective heat treatment time in the m-th section when the staying time in the temperature range of 450 ° C to 700 ° C is divided into 20 equal parts [s]
However, let t 1 = t'
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
[Number 4]

In the above formula (8), K 20 is an index showing the degree of stabilization of cementite in the 20th section when the temperature history in the temperature range of 450 to 700 ° C. in the reheating step is divided into 20 equal parts with respect to time. Is. Each reference numeral in the above formula (8) represents the following.
J: An integer from 1 to 20
Si, Mn, Cr and Mo: Content of each element [mass%]
T j: Average steel sheet temperature [° C] in the j-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
S j: Effective heat treatment time in the j-th section when the staying time in the temperature range of 450 ° C to 700 ° C is divided into 20 equal parts [s]
However, s 1 = t'.
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
[Number 5]

In the above formula (9), p10 is an index showing the degree of recrystallization in the tenth section when the residence time in the temperature range of 550 to 720 ° C. in the heating process of the annealing step is divided into 10 equal parts. .. Each reference numeral in the above equation (9) represents the following.
D 1 to 4: Constants (d 1 = 4.24 × 10 2, d 2 = 2.10 × 100, d 3 = 1.31 × 10 3, d 4 = 7.63 × 10 3)
H: Plate thickness before cold rolling [mm]
H *: Plate thickness after cold rolling [mm]
TR: Cold rolling completion temperature [° C]
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 2: Value obtained by equation (7-1)
N: An integer from 1 to 10
T n': Average temperature [° C.] in the nth section when the staying time in the temperature range of 550 to 720 ° C. is divided into 10.
Δ t: Time obtained by dividing the elapsed time from when the steel sheet temperature reached 550 ° C to when it reached 720 ° C into 10 [s]
However, t 1 = Δt.
[Number 6]

In the above formula (10), ym is an index indicating the degree of progress of reverse transformation in the m-th section when the staying time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 equal parts. Each reference numeral in the above formula (10) represents the following.
E1 to 4: Constants (e1 = 4.50 × 10 2, e2 = 2.85 × 10 4, e3 = 2.24 × 100, e4 = 8.56 × 10-8)
K 2: Value on the left side of equation (7-1)
K 3: Value of K 20 obtained by equation (8)
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T m: Average temperature [° C] in the m-th section when the residence time in the temperature range from 720 ° C to the annealing temperature is divided into 10.
T m: Effective heat treatment time in the m-th section when the residence time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 [s]
[Number 7]

In the above formula (11), each reference numeral indicates the following.
I: Integer from 1 to 10
Δ i: 750-18 x Si-17 x Mn-10 x Cr-8 x Ni + 15 x Al-T i
However, each element indicates the content in% by mass, and if the element is not contained, 0 is substituted. If the calculated value of Δ i is a negative value, Δ i is set to 0.
g 1 to 6: Constants (g 1 = 1.00 × 10 -1, g 2 = 1.46 × 10 -1, g 3 = 1.14 × 10 -1, g 4 = 2.24 × 100, g 5 = 4.53 × 100, g 6 = 4.83 × 10 3)
Nb, Mo, Si, Mn, Cr, Ni and Al: Content of each element [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T max: Annealing temperature [° C]
Ti: Average temperature [° C] in the i-th section when the staying time in the temperature range of 720 to 500 ° C is divided into 10 equal parts.
Δt: Time obtained by dividing the total staying time in the temperature range of 720 to 500 ° C. into 10 equal parts [s]
[8] In the method for producing a steel sheet according to the above [7], the cold-rolled steel sheet may be subjected to hot-dip galvanizing treatment in the cooling process of the annealing step.
[9] In the method for producing a steel sheet according to the above [7], the cold-rolled steel sheet may be subjected to a hot-dip zinc alloy plating treatment in the cooling process of the annealing step.
[10] The method for producing a steel sheet according to the above [8] or [9] may be an alloying treatment after the hot-dip galvanizing treatment or after the hot-dip galvanizing treatment in the cooling process of the annealing step. good.
Effect of the invention
[0012]
According to the above aspect according to the present invention, it is possible to provide a steel sheet having excellent formability, strength and dimensional accuracy at the time of press molding, and a method for producing the same.
Mode for carrying out the invention
[0013]
Hereinafter, the steel sheet and its manufacturing conditions according to this embodiment will be sequentially described. First, the reason for limiting the component composition (chemical composition) of the steel sheet according to the present embodiment will be described. The numerical limit range described below with "to" in between includes the lower limit value and the upper limit value. Numerical values ​​indicated as "less than" and "greater than" do not include the values ​​in the numerical range. All% of the component composition indicates mass%.
[0014]
The steel plate according to the present embodiment has a component composition of mass%, C: 0.035 to 0.150%, Si: 0.010 to 1.500%, Mn: 0.10 to 3.00%, Al. : 0.005 to 1.000%, P: 0.100% or less, S: 0.0200% or less, N: 0.0150% or less, O: 0.0100% or less, V: 0 to 0.50% , Cr: 0 to 1.00%, Ni: 0 to 1.00%, Cu: 0 to 1.00%, Mo: 0 to 1.00%, W: 0 to 1.00%, B: 0 to 0.0100%, Sn: 0 to 1.00%, Sb: 0 to 0.20%, Nb: 0 to 0.060%, Ti: 0 to 0.100%, Ca: 0 to 0.0100%, Mg: 0 to 0.0100%, Zr: 0 to 0.0100%, REM: 0 to 0.0100%, and the balance: Fe and impurities, satisfying the formulas (1-1) to (1-3). ..
1.5 x Nb + Ti ≧ 0.015 ... (1-1)
(0.03 ≤ {(Ti / 48-N / 14) + Nb / 93} / (C / 12) ≤ 0.40) ... (1-2)
Ca + Mg + Zr + REM ≤ 0.0100 ... (1-3)
Hereinafter, each element will be described.
[0015]
C: 0.035 to 0.150%
C is an element that greatly increases the strength of the steel sheet. When the C content is 0.035% or more, sufficient tensile strength can be obtained, so the C content is 0.035% or more. In order to further increase the tensile strength of the steel sheet, the C content is preferably 0.040% or more, more preferably 0.050% or more.
On the other hand, when the C content is 0.150% or less, it is possible to suppress the formation of a large amount of retained austenite after heat treatment (annealing), and a desired microstructure can be obtained. Therefore, the C content is set to 0.150% or less. The C content is preferably 0.130% or less, more preferably 0.110% or less or 0.090% or less.
[0016]
Si: 0.010 to 1.500%
Si is an element that refines iron-based carbides and contributes to improving the strength-formability balance of steel sheets. In order to improve the strength-formability balance of the steel sheet, the Si content is 0.010% or more. It is preferably 0.050% or more, and preferably 0.100% or more for increasing the strength.
Further, when the Si content is 1.500% or less, the formation of coarse Si oxide that acts as a starting point of fracture can be suppressed, cracks are less likely to occur, and embrittlement of steel can be suppressed. Therefore, the Si content is set to 1.500% or less. The Si content is preferably 1.300% or less or 1.000% or less, and more preferably 0.800% or less, 0.600% or less or 0.400% or less.
[0017]
Mn: 0.10 to 3.00%
Mn is an element that enhances the hardenability of steel and contributes to the improvement of strength. In order to obtain the desired strength, the Mn content is 0.10% or more. Preferably, it is 0.50% or more. In addition to strength, it is more preferably greater than 0.60% in order to obtain a higher degree of post-press molding dimensional accuracy. More preferably, it is 0.70% or more or 1.00% or more.
Further, when the Mn content is 3.00% or less, it is possible to prevent the macro-homogeneity in the steel sheet from being impaired due to the uneven distribution of Mn during casting, and the formability of the steel sheet can be ensured. Therefore, the Mn content is set to 3.00% or less. In order to obtain better moldability, the Mn content is preferably 2.80% or less or 2.60% or less, and more preferably 2.30% or less, 2.00% or less or 1.70% or less.
[0018]
Al: 0.005 to 1.000%
Al is an element that functions as a deoxidizing material. Al content When it is 0.005% or more, a sufficient deoxidizing effect can be obtained, so the Al content is set to 0.005% or more. It is preferably 0.010% or more, and more preferably 0.020% or more.
Al is also an element that forms a coarse oxide that is the starting point of fracture and embrittles steel. When the Al content is 1.000% or less, the formation of coarse oxides that act as the starting point of fracture can be suppressed, and the slabs can be suppressed from being easily cracked. Therefore, the Al content is set to 1.000% or less. The Al content is preferably 0.800% or less or 0.6000% or less, and more preferably 0.300% or less, 0.150% or less or 0.080% or less.
[0019]
P: 0.100% or less
P is an element that embrittles steel and also embrittles the molten part generated by spot welding. When the P content is 0.100% or less, it is possible to prevent the steel sheet from becoming brittle and easily cracking in the production process. Therefore, the P content is set to 0.100% or less. From the viewpoint of productivity, the P content is preferably 0.050% or less, more preferably 0.030% or less.
The lower limit of the P content, which is an impurity, is 0%. The P content is rarely less than 0.001%, and 0.001% may be the lower limit.
[0020]
S: 0.0200% or less
S is an element that forms Mn sulfide and deteriorates moldability such as ductility, hole expandability, stretch flangeability and bendability. When the S content is 0.0200% or less, it is possible to suppress a significant decrease in the moldability of the steel sheet, so the S content is 0.0200% or less. The S content is preferably 0.0100% or less, more preferably 0.0080% or less.
The lower limit of the S content, which is an impurity, is 0%. The S content is rarely less than 0.0001%, and 0.0001% may be the lower limit.
[0021]
Nb: 0 to 0.060%,
Ti: 0 to 0.100% and
1.5 x Nb + Ti ≧ 0.015 ... (1-1)
The chemical composition of the steel sheet according to this embodiment satisfies Nb: 0 to 0.060% Ti: 0 to 0.100% and the above formula (1-1). Nb is an element that contributes to the improvement of steel sheet strength by strengthening with precipitates, strengthening fine granulation by suppressing the growth of ferrite crystal grains, and strengthening dislocations by suppressing recrystallization. Ti is an element having the effect of reducing S, N and O that generate coarse inclusions that act as the starting point of fracture. In addition, Ti has the effect of refining the structure and enhancing the strength-formability balance of the steel sheet. In order to obtain these effects, the chemical composition of the steel sheet according to the present embodiment satisfies the above formula (1-1). That is, 1.5 × Nb + Ti ≧ 0.015. If necessary, the right side of the above formula (1-1), that is, the lower limit of "1.5 x Nb + Ti" may be set to 0.020% or 0.025%.
[0022]
When the Nb content is 0.060% or less, recrystallization can be promoted and unrecrystallized ferrite can be suppressed from remaining, and the formability of the steel sheet can be ensured. Therefore, the Nb content is set to 0.060% or less. The Nb content is preferably 0.050% or less, more preferably 0.040% or less. When the Ti content is 0.100% or less, the formation of coarse Ti sulfide, Ti nitride, and Ti oxide can be suppressed, and the formability of the steel sheet can be ensured. Therefore, the Ti content is set to 0.100% or less. The Ti content is preferably 0.075% or less, more preferably 0.060% or less. As long as the above formula (1-1) is satisfied, the lower limit of the Nb content or the Ti content is 0%. Even if the above formula (1-1) is deleted, the lower limit of the Nb content is 0.010%, the lower limit of the Ti content is 0.015%, and either Nb or Ti is equal to or higher than this lower limit. good. Nb and Ti in the above formula (1-3) indicate the content of each element in mass%, and 0 is substituted when the element is not contained.
[0023]
0.03 ≤ {(Ti / 48-N / 14) + Nb / 93} / (C / 12) ≤ 0.40 ... (1-2)
The chemical composition of the steel sheet according to this embodiment satisfies the above formula (1-2). By satisfying the above formula (1-2), it is possible to suppress an increase in the amount of cementite in the microstructure and deterioration of the formability of the steel sheet.
Note that Ti, N, Nb and C in the above formula (1-2) indicate the content of each element in mass%, and when the element is not contained, 0 is substituted. If the value in parentheses (Ti / 48-N / 14) including Ti and N is negative, 0 is substituted as the value in the parentheses.
[0024]
N: 0.0150% or less
N is an element that forms a nitride and deteriorates moldability such as ductility, hole expansion, stretch flangeability, and bendability. When the N content is 0.0150% or less, it is possible to suppress the deterioration of the moldability of the steel sheet, so the N content is set to 0.0150% or less. In addition, N is also an element that causes welding defects during welding and hinders productivity. Therefore, the N content is preferably 0.0120% or less, more preferably 0.0100% or less or 0.0070% or less.
The lower limit of the N content, which is an impurity, is 0%. The N content is rarely less than 0.0005%, and 0.0005% may be the lower limit.
[0025]
O: 0.0100% or less
O is an element that forms an oxide and inhibits moldability such as ductility, hole expansion, stretch flangeability and bendability. When the O content is 0.0100% or less, it is possible to suppress a significant decrease in the moldability of the steel sheet, so the O content is 0.0100% or less. It is preferably 0.0080% or less, more preferably 0.0050% or less or 0.0030% or less.
The lower limit of the O content, which is an impurity, is 0%. The O content is rarely less than 0.0001%, and 0.0001% may be the lower limit.
[0026]
The steel sheet according to this embodiment may contain the following elements as optional elements. The lower limit of the content when the following optional elements are not contained, that is, the content of the following elements is 0%.
[0027]
V: 0 to 0.50%
V is an element that contributes to the improvement of steel sheet strength by strengthening with precipitates, strengthening fine granulation by suppressing the growth of ferrite crystal grains, and strengthening dislocations by suppressing recrystallization. Since V does not necessarily have to be contained, the lower limit of the V content includes 0%. In order to sufficiently obtain the strength improving effect by V, the V content is preferably 0.01% or more, more preferably 0.03% or more.
Further, when the V content is 0.50% or less, it is possible to suppress the precipitation of a large amount of carbonitride and deterioration of the moldability of the steel sheet. Therefore, the V content is set to 0.50% or less.
[0028]
Cr: 0 to 1.00%
Cr is an element that enhances the hardenability of steel and contributes to the improvement of steel sheet strength, and is an element that can replace a part of Mn. Since Cr does not necessarily have to be contained, the lower limit of the Cr content includes 0%. In order to sufficiently obtain the strength improving effect of Cr, the Cr content is preferably 0.05% or more, more preferably 0.20% or more.
Further, when the Cr content is 1.00% or less, it is possible to suppress the formation of coarse Cr carbides that can be the starting point of fracture. Therefore, the Cr content is set to 1.00% or less.
[0029]
Ni: 0 to 1.00%
Ni is an element that suppresses phase transformation at high temperatures and contributes to the improvement of steel sheet strength, and is an element that can replace a part of Mn. Since Ni does not necessarily have to be contained, the lower limit of the Ni content includes 0%. In order to sufficiently obtain the strength improving effect of Ni, the Ni content is preferably 0.05% or more, more preferably 0.20% or more.
Further, when the Ni content is 1.00% or less, it is possible to suppress the deterioration of the weldability of the steel sheet, so the Ni content is set to 1.00% or less.
[0030]
Cu: 0 to 1.00%
Cu is an element that is present in steel as fine particles and contributes to the improvement of steel sheet strength, and is an element that can replace a part of C and / or Mn. Since Cu does not necessarily have to be contained, the lower limit of the Cu content includes 0%. In order to sufficiently obtain the strength improving effect of Cu, the Cu content is preferably 0.05% or more, more preferably 0.15% or more.
Further, when the Cu content is 1.00% or less, it is possible to suppress the deterioration of the weldability of the steel sheet, so the Cu content is set to 1.00% or less.
[0031]
Mo: 0 to 1.00%
Mo is an element that suppresses phase transformation at high temperatures and contributes to the improvement of steel sheet strength, or is an element that can replace a part of Mn. Since Mo does not necessarily have to be contained, the lower limit of the Mo content includes 0%. In order to sufficiently obtain the strength improving effect of Mo, the Mo content is preferably 0.03% or more, more preferably 0.06% or more.
Further, when the Mo content is 1.00% or less, it is possible to suppress a decrease in hot workability and a decrease in productivity. Therefore, the Mo content is set to 1.00% or less.
[0032]
W: 0 to 1.00%
W is an element that suppresses phase transformation at high temperatures and contributes to the improvement of steel sheet strength, and is an element that can replace a part of C and / or Mn. Since W does not necessarily have to be contained, the lower limit of the W content includes 0%. In order to sufficiently obtain the strength improving effect by W, the W content is preferably 0.03% or more, more preferably 0.10% or more.
Further, when the W content is 1.00% or less, it is possible to suppress the decrease in hot workability and the decrease in productivity, so the W content is set to 1.00% or less.
[0033]
B: 0-0.0100%
B is an element that suppresses phase transformation at high temperatures and contributes to the improvement of steel sheet strength, and is an element that can replace a part of Mn. Since B does not necessarily have to be contained, the lower limit of the B content includes 0%. In order to sufficiently obtain the strength improving effect of B, the B content is preferably 0.0005% or more, more preferably 0.0010% or more.
Further, when the B content is 0.0100% or less, it is possible to suppress the formation of B precipitates and the decrease in the strength of the steel sheet, so the B content is set to 0.0100% or less.
[0034]
Sn: 0 to 1.00%
Sn is an element that suppresses the coarsening of crystal grains and contributes to the improvement of steel sheet strength. Since Sn does not necessarily have to be contained, the lower limit of the Sn content includes 0%. In order to sufficiently obtain the effect of Sn, the Sn content is more preferably 0.01% or more.
Further, when the Sn content is 1.00% or less, it is possible to prevent the steel sheet from becoming brittle and breaking during rolling, so the Sn content is set to 1.00% or less.
[0035]
Sb: 0 to 0.20%
Sb is an element that suppresses the coarsening of crystal grains and contributes to the improvement of steel sheet strength. Since Sb does not necessarily have to be contained, the lower limit of the Sb content includes 0%. In order to obtain the above effect sufficiently, the Sb content is preferably 0.005% or more.
Further, when the Sb content is 0.20% or less, it is possible to prevent the steel sheet from becoming brittle and breaking during rolling, so the Sb content is set to 0.20% or less.
The composition of the steel sheet according to the present embodiment may contain one or more of Ca, Ce, Mg, Zr, La and REM, if necessary.
One or more of Ca, Ce, Mg, Zr, La and REM: 0 to 0.0100% in total
Ca, Ce, Mg, Zr, La and REM are elements that contribute to the improvement of moldability of the steel sheet. The lower limit of the total of one or more of Ca, Ce, Mg, Zr, La and REM includes 0%, but in order to sufficiently obtain the effect of improving moldability, a total of 0.0001% or more is preferable. More preferably 0.0010% or more.
Further, when the total content of one or more of Ca, Ce, Mg, Zr, La, and REM is 0.0100% or less, it is possible to suppress the decrease in ductility of the steel sheet. Therefore, the total content of the above elements is 0.0100% or less. It is preferably 0.0050% or less.
REM (Rare Earth Metal) means an element group excluding La and Ce, which are individually specified, among the element groups belonging to the lanthanoid series. These are often added in the form of mischmetal, but in addition to La and Ce, lanthanoid series elements are inevitable.It may be contained in.
[0036]
Ca: 0-0.0100%,
Mg: 0-0.0100%,
Zr: 0-0.0100%,
REM: 0 to 0.0100%, and
Ca + Mg + Zr + REM ≤ 0.0100 ... (1-3)
Ca, Mg, Zr, and REM are elements that contribute to the improvement of moldability of the steel sheet and can be contained. If the content of each of these elements exceeds 0.0100%, there is a concern that the moldability will deteriorate, and the content of each of these elements shall be 0.0100% or less.
The chemical composition of the steel sheet according to this embodiment satisfies the above formula (1-3). Since Ca, Mg, Zr and REM do not necessarily have to be contained, the lower limit of the total of one or more of Ca, Mg, Zr and REM includes 0%. On the other hand, Ca, Mg, Zr and REM are elements that contribute to the improvement of moldability of the steel sheet. Therefore, the lower limit of "Ca + Mg + Zr + REM" may be 0.0001%. In order to sufficiently obtain the effect of improving moldability, the lower limit of "Ca + Mg + Zr + REM" is preferably 0.0005% or more, more preferably 0.0010% or more.
Further, by satisfying the above formula (1-3), that is, "Ca + Mg + Zr + REM ≦ 0.0100", it is possible to suppress the decrease in ductility of the steel sheet. Preferably, the upper limit of "Ca + Mg + Zr + REM" is 0.0070% or 0.0050%.
REM (Rare Earth Metal) means a group of elements belonging to the lanthanoid series. These are often added in the form of mischmetal, but may inevitably contain elements of the lanthanide series. Examples of REM include Ce and La.
Note that Ca, Mg, Zr and REM in the above formula (1-3) indicate the content of each element in mass%, and 0 is substituted when the element is not contained.
[0037]
The balance of the component composition of the steel sheet according to the present embodiment may be Fe and impurities. Examples of impurities include elements that are unavoidably mixed from steel raw materials or scrap and / or in the steelmaking process and are allowed as long as they do not impair the characteristics of the steel sheet according to the present embodiment. As impurities, H, Na, Cl, Co, Zn, Ga, Ge, As, Se, Y, Tc, Ru, Rh, Pd, Ag, Cd, In, Te, Cs, Ta, Re, Os, Ir, Pt. , Au, Pb, Bi, Po. Impurities may contain 0.100% or less in total.
[0038]
Next, the microstructure of the steel sheet according to this embodiment will be described.
The steel plate according to the present embodiment has a microstructure in a 1/4 width portion which is a 1/4 position of the plate width in the plate width direction from the end portion in the plate width direction and a 1/4 position of the plate thickness in the plate thickness direction from the surface. , From the microstructure in the 1/2 width portion, which is 1/2 of the plate width in the plate width direction from the end in the plate width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, and from the end in the plate width direction. In the microstructure in the 3/4 width portion, which is 3/4 of the plate width in the plate width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, in area%, ferrite: 80% or more, martensite. : 2% or less, retained austenite: 2% or less, and residual structure, the ratio of unrecrystallized ferrite to the ferrite is 5 to 60%, and the average diameter of carbon nitride is 6.0 to 30.0 nm. It is characterized in that it satisfies the following equations (2) to (5).
In the present embodiment, the microstructure at a position 1/4 of the plate thickness in the plate thickness direction from the surface is defined because the microstructure at this position shows a typical microstructure of the steel sheet and correlates with the mechanical properties of the steel sheet. Is strong. The ratio of the following structures in the microstructure is the area ratio (area%).
[0039]
Δ SF / μ SF ≤ 0.10 ... (2)
Δ dF / μ dF ≦ 0.20… (3)
Δ SUF ≤ 20 ... (4)
Δ dC / μ dC ≦ 0.50 ... (5)
[0040]
The μ SF in the above formula (2) is the area ratio of ferrite in the microstructure in the 1/4 width portion, the area ratio of ferrite in the microstructure in the 1/2 width portion, and the 3/4 width portion. It is the average value of the area ratio of ferrite in the microstructure in the width portion (the average value of the three area ratios), and ΔSF is the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. It is the difference between the maximum value and the minimum value of the area ratio of ferrite in the microstructure in the above.
The μdF in the above formula (3) is the average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the average crystal grain size of ferrite in the microstructure in the 1/2 width portion, and It is the average value of the average crystal grain size of ferrite in the microstructure in the 3/4 width portion (the average value of the three average values), and Δ dF is the 1/4 width portion, the 1/2 width portion, and the above-mentioned 1/2 width portion. It is the difference between the maximum value and the minimum value of the average crystal grain size of ferrite in the microstructure in the 3/4 width portion.
ΔSUF in the above formula (4) is the maximum value and the minimum value of the area ratio of unrecrystallized ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. Is the difference.
The μdC in the above formula (5) is the average diameter of the carbon nitride containing Ti and / or Nb in the microstructure in the 1/4 width portion, and the μdC in the microstructure in the 1/2 width portion. It is the average value of the average diameter of the carbon nitride and the average diameter of the carbon nitride in the microstructure in the 3/4 width portion (the average value of the three average values), and ΔdC is the 1/4 width. It is the difference between the maximum value and the minimum value of the average diameter of the carbonitride in the microstructure in the portion, the 1/2 width portion and the 3/4 width portion.
[0041]
Ferrite: 80% or more
Ferrite has a structure with excellent moldability. When the area ratio of ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion is 80% or more, desired moldability can be obtained. Therefore, the area ratio of ferrite is set to 80% or more. The area ratio of ferrite is preferably 85% or more, more preferably 90% or more. Since it is preferable that the amount of ferrite is large, the area ratio of ferrite may be 100%.
[0042]
Percentage of unrecrystallized ferrite in ferrite: 5-60%
Unrecrystallized ferrite is a ferrite in which strain introduced by cold rolling or the like remains inside, and has higher strength but inferior ductility than ordinary ferrite. Sufficient strength can be obtained when the area ratio of unrecrystallized ferrite in the ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion is 5% or more, respectively. Therefore, the area ratio of unrecrystallized ferrite to ferrite is set to 5% or more. It is preferably 10% or more. Further, when the area ratio of the unrecrystallized ferrite in the ferrite is 60% or less, the moldability can be ensured, so that the area ratio of the unrecrystallized ferrite in the ferrite is 60% or less. It is preferably 50% or less.
[0043]
Martensite: 2% or less
Martensite is a structure that increases strength, but it is the starting point for the generation of fine voids during molding. If fine voids are generated during molding, the desired impact fracture resistance cannot be obtained. In order to suppress the generation of fine voids during molding, the area ratio of martensite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion is 2% or less, respectively. And. The area ratio of martensite is preferably 1% or less, more preferably 0%.
[0044]
Residual austenite: 2% or less
Residual austenite is a structure that improves the strength-ductility balance of steel sheets, but it is the starting point for the generation of fine voids during molding. In order to suppress the generation of fine voids during molding, the area ratio of retained austenite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion is 2% or less, respectively. And. The area ratio of retained austenite is preferably 1% or less, more preferably 0%.
[0045]
Remaining organization
Remaining tissues in the microstructure include pearlite, cementite and bainite. By setting the total area ratio of these tissues to 20% or less, desired impact resistance fracture characteristics can be obtained. Therefore, the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion Among the microstructures in the above, the total area ratio of these tissues is preferably 20% or less, more preferably 15% or less, still more preferably 10% or less. The lower limit of the area ratio of pearlite is originally 0%, but it may be 2% or 5%, and the upper limit may be 15%, 10% or 5%, if necessary. The lower limit of the area ratio of cementite (excluding cementite existing in pearlite; the same applies hereinafter) is originally 0%, but the lower limit may be 0.5% or 1%, if necessary. The upper limit may be 3%, 2.2% or 1%. The lower limit of the area ratio of bainite is originally 0%, but it may be 2% or 5%, and the upper limit may be 15%, 10% or 5%, if necessary. If necessary, the area ratio of pearlite may be set to 0%, and the area ratio of cementite may be set to 0%.
[0046]
The method of measuring the area ratio of the microstructure will be described below.
Test pieces (three in total) whose observation surface is a cross section parallel to the rolling direction of the steel sheet and perpendicular to the surface of the steel sheet from the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion of the steel sheet. ) Is collected. After polishing the observation surface of the test piece, night tar etching is performed at a position near 1/4 of the plate thickness in the plate thickness direction from the surface (however, the observation range is 1/8 to 3/8 t from the surface of the plate thickness (however, the observation range is 1/8 to 3/8 t from the surface of the plate thickness). t is limited to the area of ​​plate thickness).) With an observation magnification of 1000 to 3000 times in a field of 1 or more, a total area of ​​2.0 × 10-9 m 2 or more is covered by an electric field radiation scanning electron microscope (t). FE-SEM: Field Measurement Scanning Electron Microscope) is observed, each structure is identified based on the structure morphology (crystal grain shape, subgrain boundary in crystal grain, carbonized product formation state, etc.), and the area ratio (area ratio). Area%) is measured. This gives the area ratios of ferrite, unrecrystallized ferrite, martensite, MA (a region consisting of both martensite and retained austenite), pearlite, cementite and bainite. When observing a plurality of fields of view, the area to be analyzed in each field of view shall be 4.0 × 10 -10 m 2 or more.
[0047]
The area ratio is analyzed by the point counting method in each field of view, 15 lines are drawn parallel to the rolling direction and 15 lines are drawn perpendicular to the rolling direction, and the structure is discriminated at 225 intersections consisting of these lines. Specifically, the method for discriminating each structure is to discriminate the massive region without cementite and subgrain boundaries as ferrite, and unrecrystallize the massive region without cementite and having subgranular boundaries inside. Determined to be ferrite. In addition, martensite and MA containing a large amount of solute carbon are brighter and appear whiter than other tissues, and thus can be distinguished from other tissues. By the above method, the total of the area ratio of ferrite, the area ratio of unrecrystallized ferrite, and the area ratio of "martensite and MA (region consisting of both martensite and retained austenite)" is obtained. By dividing the area ratio of unrecrystallized ferrite by the area ratio of ferrite, the ratio of unrecrystallized ferrite to ferrite is obtained. The field of view used in the point counting method may be two or more.
[0048]
The area ratio of retained austenite is analyzed by X-ray diffraction method. 1 / of the plate thickness in the plate thickness direction from the surface of the plate thickness of the test pieces (however, a total of three test pieces from the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion). In the vicinity of 4 positions (however, the measurement range is limited to the region of 1 / 8t to 3 / 8t (t is the plate thickness)), the surface parallel to the steel plate surface is mirror-finished, and the FCC iron is subjected to X-ray diffraction. Analyze the volume fraction. The obtained volume fraction is regarded as the area ratio of retained austenite. In addition, the area ratio of the obtained retained austenite was the sum of the area ratios of "martensite and MA" obtained by the above observation by FE-SEM. By subtracting from, the area ratio of martensite can be obtained.
Further, the area ratio of the residual structure is obtained by subtracting the area ratio of ferrite, the area ratio of martensite, and the area ratio of retained austenite from 100%.
The above measurement is performed at the 1/4 position, 1/2 position and 3/4 position of the plate width in the plate width direction from the end in the rolling direction.
[0049]
Average diameter of carbonitride: 6.0-30.0 nm
The average diameter of the carbonitride is 6.0 to 30.0 nm in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. When the average diameter of the carbonitride is 6.0 nm or more, excessive precipitation strengthening can be suppressed and moldability can be ensured. The average diameter of the carbonitride is preferably 8.0 nm or more, more preferably 10.0 μm or more. On the other hand, when the average diameter of the carbonitride is 30.0 nm or less, sufficient strength can be obtained. The average diameter of the carbonitride is preferably 25.0 nm or less or 20.0 nm or less, more preferably 17.0 nm or less, 15.0 nm or less, 12.5 nm or less or 11.0 nm or less.
[0050]
The average diameter of the carbonitride is measured by the following method.
Similar to the case where the area ratio of the microstructure was obtained, the test piece (however, the 1/4 width portion, the 1/2 width portion, and the 3 /) from the vicinity of the 1/4 position of the plate thickness in the plate thickness direction from the surface. Collect (a total of 3 test pieces from the 4 widths) (however, the plate thickness range for collecting the test pieces is 1/8 t to 3/8 t (t is the plate thickness) from the surface of the plate thickness of the test piece). Limited to the area of.). From the collected test pieces, needle-shaped test pieces are prepared by cutting and electropolishing, and if necessary, by utilizing the focused ion beam processing method in combination with electropolishing, and three-dimensional atom probe measurement is performed. With respect to the obtained three-dimensional atomic map containing Ti and / or Nb carbonitrides, the major axis of 30 or more Ti and / or Nb carbonitrides is arbitrarily obtained, and the average value thereof is calculated. The average diameter of the carbonitride containing Ti and / or Nb is obtained for each of a total of three test pieces from the / 4 width portion, the 1/2 width portion, and the 3/4 width portion.
[0051]
The steel sheets in the present embodiment include Δ SF / μ SF ≦ 0.10… (2), Δ dF / μ dF ≦ 0.20… (3), Δ SUF ≦ 20… (4) and Δ dC / μ dC ≦. 0.50 ... (5) is satisfied.
Satisfying the above formulas (2) to (5) means that the area ratio of ferrite in the plate width direction of the steel plate, the average crystal grain size of ferrite, the area ratio of unrecrystallized ferrite, and carbonitride containing Ti and / or Nb. It shows that the fluctuation of the average diameter of the object is suppressed. By satisfying the above formulas (2) to (5), it is possible to suppress fluctuations in the characteristics of the steel sheet in the plate width direction, which increases the variation in dimensional accuracy during press forming, and as a result, formability, strength and press. A steel sheet having excellent dimensional accuracy during molding can be obtained.
[0052]
For μ SF in the above formula (2), the area ratio of ferrite in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion was measured by the above method, and these Obtained by calculating the average value of the area ratio. Further, for ΔSF in the above formula (2), the area ratio of ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion is measured by the above method. , Obtained by calculating the difference between the maximum value and the minimum value of the obtained ferrite area ratio.
[0053]
ΔSUF in the above formula (4) is the difference between the maximum value and the minimum value of unrecrystallized ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. be. By the above method, the area ratio of unrecrystallized ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion was measured, and the area of ​​the obtained unrecrystallized ferrite was obtained. It is obtained by calculating the difference between the maximum value and the minimum value of the rates.
[0054]
For μ dF in the above formula (3), the average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion was measured by the method described later. , Obtained by calculating the average value of these average crystal grain sizes. Further, ΔdF in the above formula (3) is the average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion by the method described later. It is obtained by measuring and calculating the difference between the maximum value and the minimum value of the obtained average crystal grain size of ferrite.
[0055]
The μdC in the above formula (5) is the average value of the major axis of the carbonitride in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion by the method described later. It is obtained by measuring (average diameter) and calculating the average value of these average diameters. Further, ΔdC in the above formula (5) measures the average diameter of the carbonitride in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion by the above method. Then, it is obtained by calculating the difference between the maximum value and the minimum value of the average diameter of the obtained carbonitride.
[0056]
The average crystal grain size of ferrite is measured by the following method.
The average crystal grain size of ferrite is calculated by the line segment method. In the field of measurement of the area ratio of the microstructure described above, draw one or more straight lines having a total length of 200 μm or more in the rolling direction, and add 1 to the number of intersections between the straight line and the ferrite grain boundary to obtain the length of the straight line. The average crystal grain size of ferrite is obtained by calculating the value obtained by dividing.
[0057]
Average crystal grain size of ferrite: 5.0 to 15.0 μm
The average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the microstructure in the 1/2 width portion, and the microstructure in the 3/4 width portion is 5.0 to 15.0 μm. Is preferable. By setting the average crystal grain size of ferrite to 5.0 to 15.0 μm, the strength-formability balance can be further improved. In order to improve the strength, the upper limit may be set to 13.0 μm, 11.0 μm or 9.5 μm.
The average crystal grain size of ferrite is measured by the above method.
[0058]
The steel sheet according to the present embodiment may be a steel sheet having a zinc plating layer or a zinc alloy plating layer on one side or both sides of the steel sheet. Further, the steel sheet according to the present embodiment may be a steel sheet having an alloyed zinc plating layer or an alloyed zinc alloy plating layer obtained by subjecting a zinc plating layer or a zinc alloy plating layer to an alloying treatment.
The plating layer formed on one side or both sides of the steel sheet according to the present embodiment is preferably a zinc plating layer or a zinc alloy plating layer containing zinc as a main component. The zinc alloy plating layer preferably contains Ni as an alloy component.
[0059]
The zinc plating layer and the zinc alloy plating layer are formed by a hot-dip plating method, an electroplating method, or a vapor deposition plating method. When the Al content of the galvanized layer is 0.5% by mass or less, the adhesion between the steel sheet surface and the zinc plating layer can be ensured, so that the Al content of the galvanized layer is 0.5% by mass or less. preferable. When the zinc-plated layer is a hot-dip galvanized layer, the Fe amount of the hot-dip galvanized layer is preferably 3.0% by mass or less in order to improve the adhesion between the steel sheet surface and the zinc-plated layer.
When the zinc plating layer is an electrozinc plating layer, the Fe amount of the plating layer is preferably 0.5% by mass or less in terms of improving corrosion resistance.
[0060]
The zinc plating layer and the zinc alloy plating layer include Al, Ag, B, Be, Bi, Ca, Cd, Co, Cr, Cs, Cu, Ge, Hf, Zr, I, K, La, Li, Mg, Mn, One or more of Mo, Na, Nb, Ni, Pb, Rb, Sb, Si, Sn, Sr, Ta, Ti, V, W, Zr, and REM in a range that does not impair the corrosion resistance and formability of the steel plate. And may be contained. In particular, Ni, Al, and Mg are effective in improving corrosion resistance.
[0061]
The zinc plating layer or zinc alloy plating layer on the surface of the steel sheet according to the present embodiment may be an alloyed zinc plating layer or an alloyed zinc alloy plating layer that has been alloyed. When the hot-dip zinc plating layer or the hot-dip zinc alloy plating layer is alloyed, the hot-dip zinc plating layer after the alloying treatment (alloyed zinc plating layer) is used from the viewpoint of improving the adhesion between the steel plate surface and the alloyed plating layer. Alternatively, the Fe content of the molten zinc alloy plating layer (alloyed zinc alloy plating layer) is preferably 7.0 to 13.0% by mass. By alloying a steel plate having a hot-dip galvanizing layer or a hot-dip zinc alloy plating layer, Fe is incorporated into the plating layer and the Fe content is increased. Thereby, the Fe content can be set to 7.0% by mass or more. That is, the zinc plating layer having an Fe content of 7.0% by mass or more is an alloyed zinc plating layer or an alloyed zinc alloy plating layer.
[0062]
The Fe content of the hot-dip zinc plating layer (alloyed zinc plating layer) or the hot-dip zinc alloy plating layer (alloyed zinc alloy plating layer) after the alloying treatment can be obtained by the following method. Only the plating layer is dissolved and removed using a 5% HCl aqueous solution containing an inhibitor. The Fe content (% by mass) in the zinc plating layer is obtained by measuring the Fe content in the obtained solution using ICP-AES (Inductively Coupled Plasma-Atomic Measurement Spectrometry).
[0063]
The thickness of the steel sheet according to the present embodiment is not limited to a specific range, but is preferably 0.2 to 5.0 mm in consideration of versatility and manufacturability. By setting the plate thickness to 0.2 mm or more, it becomes easy to maintain the shape of the steel plate flat, and the dimensional accuracy and the shape accuracy can be improved. Therefore, the plate thickness is preferably 0.2 mm or more. More preferably, it is 0.4 mm or more.
On the other hand, when the plate thickness is 5.0 mm or less, it becomes easy to apply appropriate strain and control the temperature in the manufacturing process, and a homogeneous structure can be obtained. Therefore, the plate thickness is preferably 5.0 mm or less. More preferably, it is 4.5 mm or less or 3.2 mm or less.
[0064]
0.2% proof stress: 280 to 600 MPa, tensile strength: 450 to 800 MPa, yield ratio: 0.50 to 0.90, uniform elongation: 10.0% or more
The target values ​​of the tensile properties of the steel plate according to the present embodiment are 0.2% proof stress of 280 to 600 MPa, tensile strength of 450 to 600 MPa, and a yield ratio of 0.2% proof stress / tensile strength. It is 0.50 to 0.90, and the uniform elongation, which is the plastic elongation at the maximum load, is 10.0% or more. Thereby, the moldability and strength of the steel sheet can be improved. In addition, "uniform elongation" is also called "uniform elongation", and both uniform elongation and uniform elongation are translated as uniform elongation in English.
[0065]
0.2% proof stress, tensile strength, yield ratio and uniform elongation are measured by the following methods.
0.2% proof stress, tensile strength, yield ratio and uniform elongation can be obtained by performing a tensile test. In accordance with JIS Z 2241: 2011, a No. 13B test piece is prepared, and a tensile test is performed with the tensile axis as the rolling direction of the steel sheet. With the tension axis as the rolling direction of the steel plate, 1/4 position of the plate width in the plate width direction from the end in the plate width direction, 1/2 position in the plate width direction from the end in the plate width direction, and plate width from the end in the plate width direction. Take a tensile test piece from the 3/4 position in the direction. By calculating the average values ​​of 0.2% proof stress, tensile strength and uniform elongation obtained from these three tensile test pieces, 0.2% proof stress, tensile strength and uniform elongation are obtained. The yield ratio is obtained by dividing the 0.2% proof stress by the tensile strength.
[0066]
Next, the method for manufacturing the steel sheet according to the present embodiment will be described.
The steel sheet according to the present embodiment can obtain the effect if it has the above characteristics regardless of the manufacturing method, but it is preferable because it can be stably manufactured by the manufacturing method including the following steps.
(I) A steel piece having a predetermined composition is heated to 1150 to 1320 ° C., hot rolling is completed so that the hot rolling completion temperature becomes 850 to 930 ° C., and cooling is started after 1.5 s or more have passed. Then, a hot rolling process of cooling to a temperature range of less than 450 ° C. to obtain a hot-rolled steel sheet so that the average cooling rate in the temperature range of 800 to 450 ° C. is 20 ° C./s or more.
(II) A reheating step of heating the hot-rolled steel sheet to a temperature range of 450 to 700 ° C.
(III) A cooling step of cooling the hot-rolled steel sheet to room temperature.
(IV) Cold pressure of the hot-rolled steel sheet so that the total reduction rate is 30 to 80% and the cold rolling completion temperature is 120 ° C. or higher.Cold rolling process to roll into cold-rolled steel sheets,
(V) An annealing step of heating the cold-rolled steel sheet to an annealing temperature of 720 to 850 ° C. and cooling it to a temperature range of 500 ° C. or lower.
Hereinafter, preferable conditions for each process will be described.
[0067]

First, the steel piece having the composition of the steel sheet according to the present embodiment described above is heated to 1150 to 1320 ° C. When the heating temperature is 1150 ° C. or higher, coarse carbides of Ti and / or Nb generated during casting can be sufficiently dissolved, and it is possible to suppress that the state of the carbonitride is likely to vary. Further, when the heating temperature of the steel piece is 1320 ° C. or lower, it is possible to suppress the generation of excessively coarse matrix austenite grains, and the recrystallization behavior in the hot rolling step can be made uniform. The steel piece to be heated is preferably produced by continuous casting from the viewpoint of manufacturing cost, but may be produced by another casting method (for example, ingot forming method).
[0068]
After heating the steel pieces, hot rolling is performed so that the hot rolling completion temperature is 850 to 930 ° C. When the hot rolling completion temperature is 850 ° C. or higher, rolling is performed in the single-phase region, so that the anisotropy of the metal structure can be suppressed. Therefore, the hot rolling completion temperature is set to 850 ° C. or higher. Further, when the hot rolling completion temperature is 930 ° C. or lower, it is possible to suppress the excessive growth of the recrystallized grains and make the particle size of the matrix phase uniform. Therefore, the hot rolling completion temperature is set to 930 ° C. or lower.
[0069]
In the hot rolling process, it is necessary to satisfy the following formula (6) in a temperature range of 1000 ° C or lower. By controlling the path schedule so as to satisfy the following formula (6) in a temperature range of 1000 ° C. or lower, recrystallization proceeds uniformly, and carbides are finely and homogeneously precipitated in the steel. As a result, segregation of carbides can be suppressed, and fluctuations in the characteristics of the steel sheet in the plate width direction can be suppressed.
[0070]
[Number 8]

[0071]
F n in the above formula (6) is an index indicating the degree of progress of precipitation of fine carbides in the temperature range of 1000 ° C. or lower in the hot rolling process. Each reference numeral in the above equation (6) represents the following.
N: Number of rolling passes at 1000 ° C or lower
H: Plate thickness [mm] before rolling on the nth pass
H *: Plate thickness [mm] after rolling on the nth pass
Nb and Ti: Nb and Ti content [mass%]
T n: Average steel sheet temperature from rolling in the nth pass to rolling in the n + 1th pass [° C]
T n: The shorter time [s] from the rolling of the nth pass to the rolling of the n + 1th pass, or the time [s] from the rolling of the nth pass to the decrease of the steel sheet temperature to reach 800 ° C.
a 1 to 11: Constants (a 1 = 2.28 × 100, a 2 = 1.25 × 100, a 3 = 7.86 × 10 -4, a 4 = 1.36 × 10 -3, a 5 = 6.76 × 10 -4, a 6 = 7.86 × 10 -4, a 7 = 2.13 × 10 -3, a 8 = 1.14 × 10 -3, a 9 = 6.70 × 10- 2, a 10 = 1.11 × 100, a 11 = 5.27 × 10 -1)
However, f n can be obtained by setting f 0 to 0 and calculating from f 1 to f n in order.
[0072]
The average steel plate temperature in the present application is, for example, the width direction of a steel strip whose temperature distribution in the width direction is controlled to be within ± 15 ° C. with respect to the average temperature when manufacturing a steel strip having a width of about 600 mm to about 2500 mm. At 1/4 position in the plate width direction from the end in the plate width direction, 1/2 position in the plate width direction from the end in the plate width direction, and 3/4 position in the plate width direction from the end in the plate width direction. The average temperature. When the temperature control range exceeds the above-mentioned ± 15 ° C., a slight difference in structure may occur in the temperature control range by the so-called conventional method, which may cause deterioration of the dimensional accuracy of the press-formed product. In other words, according to the manufacturing method according to the embodiment of the present invention, only the temperature distribution in the width direction is controlled to be within ± 15 ° C. with respect to the average temperature at the time of manufacturing, and the tissue variation in the width direction is reduced. can. As a result, steel plates and steel strips with little dimensional variation during press forming can be obtained.
[0073]
After the completion of hot rolling, cooling is started after 1.5 s or more, and the temperature is cooled to less than 450 ° C so that the average cooling rate in the temperature range of 800 to 450 ° C is 20 ° C / s or more. As a result, a hot-rolled steel sheet is obtained.
By securing 1.5 s or more of time from the completion of hot rolling to the start of cooling, recrystallization occurs and a homogeneous structure is obtained.
[0074]
By setting the average cooling rate in the temperature range of 800 to 450 ° C to 20 ° C / s or more, stabilization of cementite is suppressed and coarse cementite is suppressed. When the average cooling rate in the above temperature range is 20 ° C./s or more, stabilization of cementite can be suppressed, and a desired microstructure can be obtained in the finally obtained steel sheet.
The upper limit of the average cooling rate is not particularly set, but since a special refrigerant is required to obtain a cooling rate exceeding 200 ° C./s, the average cooling rate is preferably 200 ° C./s or less from the viewpoint of production cost. ..
[0075]
The average cooling rate in the present embodiment is a value obtained by dividing the temperature difference between the start point and the end point of the set range by the elapsed time from the start point to the end point.
[0076]

In the reheating step, the obtained hot-rolled steel sheet is heated to a temperature range of 450 to 700 ° C. Further, in the reheating step, the temperature history in the temperature range of 450 to 700 ° C. needs to satisfy the following formula (7-1) and the following formula (8). By satisfying the following formula (7-1), carbonitride is precipitated in the steel. Further, by satisfying the following formula (8), it is possible to prevent cementite from being excessively stabilized. As a result, the desired microstructure can be finally obtained.
[0077]
When the maximum reheating temperature (maximum heating temperature in the reheating step) is 450 ° C. or higher, the carbonitride can be sufficiently precipitated in the steel, and a desired microstructure is finally obtained. Can be done. Further, when the maximum reheating temperature is 700 ° C. or lower, it is possible to suppress the start of melting of a part of the carbonitride and cementite, and it is possible to ensure the homogeneity of the steel sheet.
[0078]
[Number 9]

[0079]
Each code in the above formula (7-1) represents the following.
b 1-7: Constants (b 1 = 6.82 × 10 6, b 2 = 1.00 × 10 3, b 3 = 8.70 × 10 1, b 4 = 1.25 × 10 2, b 5 = 1.00 × 10 2, b 6 = -1.50 × 10 1, b 7 = -2.50 × 10 1)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T max: Maximum heating temperature [° C]
T 20: Effective heat treatment time in the 20th section when the staying time in the temperature range of 450 to 700 ° C. is divided into 20 equal parts [s]
D 20: An index showing the effective diffusion rate in the 20th section when the staying time in the temperature range of 450 to 700 ° C is divided into 20 equal parts.
However, the m-th effective heat treatment time tm and the m-th effective diffusion rate index D m are expressed by the following formula (7-2).
[0080]
[Number 10]

[0081]
In the above formula (7-2), each reference numeral represents the following.
M: Integer from 1 to 20
B 9-11: Constants (b 8 = 6.81 × 10 1, b 9 = 2.61 × 10 5, b 10 = 5.60 × 100, b 11 = 2.86 × 105)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T m: Average steel plate temperature [° C] in the m-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
T m: Effective heat treatment time in the m-th section when the staying time in the temperature range of 450 ° C to 700 ° C is divided into 20 equal parts [s]
However, t 1 = t'.
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
[0082]
[Number 11]

[0083]
K20 in the above formula (8) indicates the degree of stabilization of cementite in the 20th section when the temperature history in the temperature range of 450 to 700 ° C. in the reheating step is divided into 20 equal parts with respect to time. It is an index. Each reference numeral in the above formula (8) represents the following.
J: An integer from 1 to 20
Si, Mn, Cr and Mo: Content of each element [mass%]
T j: Average steel sheet temperature [° C] in the j-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
S j: Effective heat treatment time in the j-th section when the staying time in the temperature range of 450 ° C to 700 ° C is divided into 20 equal parts [s]
However, s 1 = t'.
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
However, t 1 = Δt.
[0084]
K 20 is an index showing the degree of stabilization of cementite, and the larger this value is, the more stable cementite is. By satisfying the above formula (8), it is possible to suppress the formation of excessively stable cementite in the reheating step. As a result, the formation of austenite having a high carbon concentration can be suppressed. Therefore, the formation of martensite can be suppressed in the cooling process after heating. As a result, the homogeneity of the steel sheet can be ensured. Preferably K 20 ≦ 18500. This makes it possible to further suppress the formation of martensite in the cooling process after heating.
[0085]

After the reheating process, cool the hot-rolled steel sheet to room temperature. The cooling rate at this time is not particularly limited, and examples of the cooling method include air cooling.
[0086]

Next, the cooled hot-rolled steel sheet is cold-rolled so that the total reduction ratio is 30 to 80% and the cold-rolling completion temperature is 120 ° C. or higher. As a result, a cold-rolled steel sheet is obtained. When the total reduction ratio is 30% or more, recrystallization in the subsequent heat treatment can be sufficiently proceeded, unrecrystallized ferrite can be suppressed from remaining, and a desired microstructure can be finally obtained. .. Therefore, the total rolling reduction during cold rolling is set to 30% or more. From the viewpoint of refining the structure and enhancing the strength-formability balance, the total reduction ratio is preferably 45% or more, and more preferably 60% or more. Further, when the total rolling reduction in cold rolling is 80% or less, it is possible to suppress the increase in anisotropy of the steel sheet and secure the formability. Therefore, the total rolling reduction during cold rolling is set to 80% or less. The total reduction rate is preferably 75% or less in order to further improve the moldability.
[0087]
When the cold rolling completion temperature is 120 ° C. or higher, it is possible to suppress the remaining of unrecrystallized ferrite, and finally a desired microstructure can be obtained. Therefore, the cold rolling completion temperature is set to 120 ° C. or higher. It is preferably 150 ° C. or higher, and more preferably 170 ° C. or higher. From the viewpoint of moldability, the cold rolling completion temperature is preferably 250 ° C. or lower in order to efficiently proceed with recrystallization.
[0088]

[Heating process]
Subsequently, heat treatment (annealing) is performed on the cold-rolled steel sheet (cold-rolled steel sheet). First, the cold-rolled steel sheet is heated to an annealing temperature of 720 to 850 ° C. At the time of this heating, it is necessary to satisfy the following formula (9) in the temperature range of 550 to 720 ° C., and in the temperature range of 720 ° C. to the annealing temperature (720 to 850 ° C.), a tension of 15 MPa or more is applied and a tension of 15 MPa or more is applied. The temperature history must satisfy the following equation (10).
[0089]
Recrystallization is promoted by controlling the temperature history so as to satisfy the formula (9) in the temperature range of 550 to 720 ° C. As a result, the desired microstructure can be finally obtained.
[0090]
By applying a tension of 15 MPa or more in the temperature range of 720 ° C. to annealing temperature, nucleation of austenite is promoted and a homogeneous reverse transformation structure is formed. In order to sufficiently promote the nucleation of austenite and homogenize the tissue, the tension is preferably 20 MPa or more, more preferably 25 MPa or more... If the tension is less than 15 MPa, the behavior of the reverse transformation varies and the homogeneity of the structure is impaired.
[0091]
Further, in the temperature range from 720 ° C. to the annealing temperature, cementite is dissolved by controlling the temperature history so as to satisfy the following formula (10). In the temperature history, when e4 · ym · (K3 · K4) -2/1 obtained by the following formula (10) is 0.10 or more, the dissolution of cementite can be sufficiently promoted. It is possible to suppress the remaining of coarse cementite. If coarse cementite remains, the amount of solute carbon in the austenite around it increases, making it difficult to proceed with the phase transformation in the cooling process after heating, and martensite is likely to be generated. Further, in the temperature history, when e4 · ym · (K3 · K4) -2/1 obtained by the formula (10) is 1.00 or less, the nucleation and growth of the austenite transformation are well-balanced. As it progresses, the degree of progress becomes uniform, and the homogeneity of the steel sheet can be ensured.
[0092]
[Number 12]

[0093]
P10 in the above formula (9) is an index showing the degree of progress of recrystallization in the tenth section when the residence time in the temperature range of 550 to 720 ° C. in the heating process of the annealing step is divided into 10 equal parts. .. Each reference numeral in the above equation (9) represents the following.
D 1 to 4: Constants (d 1 = 4.24 × 10 2, d 2 = 2.10 × 100, d 3 = 1.31 × 10 3, d 4 = 7.63 × 10 3)
H: Plate thickness before cold rolling [mm]
H *: Plate thickness after cold rolling [mm]
TR: Cold rolling completion temperature [° C]
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 2: Value obtained by equation (7-1)
N: An integer from 1 to 10
T n': Average temperature [° C.] in the nth section when the staying time in the temperature range of 550 to 720 ° C. is divided into 10.
Δ t: Time obtained by dividing the elapsed time from when the steel sheet temperature reached 550 ° C to when it reached 720 ° C into 10 [s]
However, t 1 = Δt.
[0094]
[Number 13]

[0095]
In the above formula (10), ym is an index indicating the degree of progress of reverse transformation in the m-th section when the staying time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 equal parts. Each reference numeral in the above formula (10) represents the following.
E1 to 4: Constants (e1 = 4.50 × 10 2, e2 = 2.85 × 10 4, e3 = 2.24 × 100, e4 = 8.56 × 10-8)
K 2: Value on the left side of equation (7-1)
K 3: Value of K 20 obtained by equation (8)
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T m: Average temperature [° C] in the m-th section when the residence time in the temperature range from 720 ° C to the annealing temperature is divided into 10.
T m: Effective heat treatment time in the m-th section when the residence time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 [s]
[0096]
The annealing temperature in the annealing process shall be 720 ° C or higher. When the annealing temperature is 720 ° C. or higher, it is possible to suppress the undissolved coarse cementite and the excessive progress of recrystallization, and a desired microstructure can be obtained. The annealing temperature is preferably 750 ° C. or higher, more preferably 780 ° C. or higher. Further, when the annealing temperature is 850 ° C. or lower, excessive progress of reverse transformation can be suppressed, and a desired amount of unrecrystallized ferrite can be left. Therefore, the annealing temperature is set to 850 ° C. or lower. When the area ratio of ferrite is increased to further enhance the moldability, the annealing temperature is preferably 830 ° C. or lower, more preferably 810 ° C. or lower.
[0097]
[Holding process]
The holding time at the annealing temperature, that is, the time from reaching the annealing temperature of 720 ° C. or higher in the heating process to reaching 720 ° C. again through the annealing temperature of 720 to 850 ° C. is preferably 3 s or more. When the holding time is 3 s or more, the change of the microstructure is stabilized and the homogeneity can be ensured. The holding time is preferably 10 s or more, and more preferably 25 s or more. The upper limit of the holding time is not particularly set, but holding for more than 200 s does not affect the characteristics of the steel sheet, so it is preferably 200 s or less in consideration of the production cost.
[0098]
[Cooling process]
Heat to the annealing temperature, secure the holding time, and then cool.
In the cooling process of cooling to a temperature range of 500 ° C. or lower, the temperature history must satisfy the following formula (11) in the temperature range of 720 to 500 ° C. By performing cooling in which the temperature history in the temperature range of 720 to 500 ° C. satisfies the following formula (11), the formation of a hard phase (martensite and retained austenite) is suppressed. As a result, the desired microstructure can be finally obtained.
[0099]
[Number 14]

[0100]
Each reference numeral in the above formula (11) represents the following.
I: Integer from 1 to 10
Δ i: 750-18 x Si-17 x Mn-10 x Cr-8 x Ni + 15 x Al-T i
However, each element indicates the content in% by mass, and if the element is not contained, 0 is substituted. If the calculated value of Δ i is a negative value, Δ i is set to 0.
g 1 to 6: Constants (g 1 = 1.00 × 10 -1, g 2 = 1.46 × 10 -1, g 3 = 1.14 × 10 -1, g 4 = 2.24 × 100, g 5 = 4.53 × 100, g 6 = 4.83 × 10 3)
Nb, Mo, Si, Mn, Cr, Ni and Al: Content of each element [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T max: Annealing temperature [° C]
Ti: Average temperature [° C] in the i-th section when the staying time in the temperature range of 720 to 500 ° C is divided into 10 equal parts.
Δt: Time obtained by dividing the total staying time in the temperature range of 720 to 500 ° C. into 10 equal parts [s]
[0101]
After the annealing step, the steel sheet may be subjected to hot-dip galvanizing treatment or hot-dip zinc alloy plating treatment in a temperature range of 500 ° C. or lower. At this time, the steel sheet may be reheated before being immersed in the plating bath. Further, the steel sheet after the plating treatment may be heated to alloy the plating layer.
[0102]
The steel sheet after the annealing step may be electroplated or vapor-deposited to form a zinc-plated layer on one or both sides of the steel sheet to produce a zinc-plated steel sheet having a zinc-plated layer.
The atmosphere in the annealing process may be controlled to modify the surface of the steel sheet. For example, by heat-treating in a decarburized atmosphere, a steel sheet having an appropriately decarburized surface layer portion of the steel sheet and having excellent bendability can be obtained.
[0103]

After the annealing step, temper rolling may be performed so that the total rolling reduction is 0.05 to 2.00%. By performing such temper rolling, it is possible to flatten the surface shape and adjust the surface roughness.
Example
[0104]
Next, an example of the present invention will be described. The conditions in the examples are one condition example adopted for confirming the feasibility and effect of the present invention. The present invention is not limited to this one-condition example. The present invention may adopt various conditions as long as the gist of the present invention is not deviated and the object of the present invention is achieved.
[0105]
Steel pieces were manufactured by casting molten steel with the chemical composition shown in Table 1-1 and Table 1-2. Next, hot-rolled steel sheets were obtained by hot-rolling the steel pieces under the conditions shown in Table 2-1 and Table 2-2. Tables 2-1 and 2-2 show the temperature history of the hot rolling step at 1000 ° C. or lower and f n obtained from the above formula (6).
Next, reheating was performed under the conditions shown in Table 2-1 and Table 2-2. Tables 2-1 and 2-2 show the temperature history of the reheating step in the temperature range of 450 to 700 ° C. and the formulas (7-) obtained from the above formulas (7-1) and (7-2). The left side of 1) is shown, and K20 obtained from the temperature history of the reheating step in the temperature range of 450 to 700 ° C. and the above formula (8) is shown.
[0106]
After that, the hot-rolled steel sheet was cold-rolled, heat-treated (annealed), and, if necessary, temper-rolled under the conditions shown in Tables 3-1 to 3-3 to obtain a steel sheet. The annealing was carried out by heating to the annealing temperatures shown in Tables 3-1 to 3-3, holding for 3 to 200 seconds, and then cooling.
Tables 3-1 to 3-3 show the temperature history of the heating process in the annealing step in the temperature range of 550 to 720 ° C. and p10 obtained from the above equation (9). The e4 · ym · (K3 · K4) -2/1 obtained from the temperature history in the temperature range of 720 ° C. to the annealing temperature and the above equation (10) is shown.
[0107]
The plating treatments in Tables 3-1 to 3-3 are as follows.
Zn alloy: A process in which a zinc alloy plated steel sheet is obtained by cooling the steel sheet to a temperature range of 500 ° C. or lower in the annealing step, immersing it in a molten zinc alloy bath, and cooling it to room temperature.
Alloyed Zn alloy: In the annealing process, the steel plate is cooled to a temperature range of 500 ° C. or lower, then immersed in a molten zinc alloy bath, further alloyed by reheating to 580 ° C., and then alloyed by cooling to room temperature. This is a process for obtaining a zinc alloy plated steel sheet.
GA: In the annealing step, the steel sheet is cooled to a temperature range of 500 ° C. or lower, immersed in a hot-dip galvanized bath, further alloyed by reheating to 560 ° C., and then cooled to room temperature to form an alloyed hot-dip galvanized steel sheet. This is a process for obtaining (GA).
GI: A process for obtaining a hot-dip galvanized steel sheet (GI) by cooling the steel sheet to a temperature range of 500 ° C. or lower in the annealing step, immersing it in a hot-dip zinc bath, and cooling it to room temperature.
Thin-film deposition: A process in which a galvanized steel sheet is obtained by performing a vapor deposition plating process after the annealing process.
EG: A process of obtaining an electrogalvanized steel sheet (EG) by subjecting it to an electrogalvanized steel sheet (EG) after the annealing process.
[0108]
Tables 4-1 to 4-6 show the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion of the steel sheet obtained under the manufacturing conditions shown in Tables 1-1 to 3-3. From the part, test pieces (three in total) having a cross section parallel to the rolling direction of the steel sheet and perpendicular to the surface of the steel sheet were collected and the microstructure was observed. As a result of the microstructure observation performed by the above method, Tables 4-1 to 4-6 show the area ratio of ferrite, the ratio of unrecrystallized ferrite to ferrite, the area ratio of martensite, the volume ratio of retained austenite, and carbon. The average diameter of the nitride, the average crystal grain size of ferrite, and the left side of the formulas (2) to (4) are shown. The thickness of the steel sheet was the same as the thickness after rolling in Table 3-1 and Table 3-3.
For the alloyed steel plate, the Fe content of the hot-dip zinc plating layer (alloyed zinc plating layer) or the hot-dip zinc alloy plating layer (alloyed zinc alloy plating layer) after the alloying treatment is measured by the above method. did.
[0109]
The plating layers in Tables 4-1 to 4-6 are as follows.
Zn alloy: Zinc alloy plating layer
Alloyed Zn alloy: Alloyed zinc alloy plating layer
GA: An alloyed hot-dip galvanized layer formed by soaking in a hot-dip zinc bath and then performing an alloying treatment.
GI: Hot-dip galvanized layer formed by immersing in a hot-dip zinc bath
Thin-film deposition: A zinc-plated layer formed by a vapor-deposit plating process
EG: Galvanized layer formed by electrozinc plating
[0110]
Tables 5-1 to 5-3 show the characteristics of the steel sheets obtained under the manufacturing conditions of Tables 1-1 to 3-3. The tensile properties are 0.2% proof stress (YS: Yield Strength), tensile strength (TS: Tensile Strength), yield ratio (YR: Yield Ratio).And uniform elongation (uEl: uniform Elongation) were evaluated. 0.2% proof stress, tensile strength, yield ratio and uniform elongation were obtained by performing a tensile test. A No. 13B test piece was prepared in accordance with JIS Z 2241: 2011, and a tensile test was performed with the tensile axis as the rolling direction of the steel sheet. With the tension axis as the rolling direction of the steel plate, 1/4 position of the plate width in the plate width direction from the end in the plate width direction, 1/2 position in the plate width direction from the end in the plate width direction, and plate width from the end in the plate width direction. A tensile test piece was taken from the 3/4 position in the direction. By calculating the average values ​​of 0.2% proof stress, tensile strength and uniform elongation obtained from these three tensile test pieces, 0.2% proof stress, tensile strength and uniform elongation were obtained. The yield ratio was obtained by dividing the average value of tensile strength by the average value of 0.2% proof stress.
[0111]
A steel sheet having a 0.2% proof stress of 280 to 600 MPa, a yield ratio of 0.50 to 0.90, and a uniform elongation of 10.0% or more was judged to be acceptable as having excellent formability. .. On the other hand, a steel sheet having a 0.2% proof stress of less than 280 MPa or more than 600 MPa, a yield ratio of less than 0.50 or more than 0.90, or a uniform elongation of less than 10.0% can be used for formability. It was judged to be inferior and rejected.
A steel sheet with a tensile strength of 450 to 800 MPa was judged to be acceptable as having excellent strength. On the other hand, when the tensile strength was less than 450 MPa, it was judged to be inferior in strength and rejected.
[0112]
The homogeneity of the steel sheet was evaluated by the following formulas (12), (13) and (14). Steel sheets satisfying the following formulas (12), (13) and (14) were judged to be acceptable because the steel sheets were homogeneous and had excellent dimensional accuracy during press forming. On the other hand, a steel sheet that does not satisfy any one of the following formulas (12), (13) and (14) was judged to be unacceptable because the steel sheet was inhomogeneous and the dimensional accuracy at the time of press molding was inferior.
[0113]
The YS in the following formula (12) is a 1/4 position of the plate width in the plate width direction from the end portion in the plate width direction and a 1/2 position in the plate width direction from the end portion in the plate width direction obtained by the above method. And it is the average value of 0.2% proof stress at the 3/4 position in the plate width direction from the end in the plate width direction. Further, ΔYS in the following formula (12) is obtained by the above method, 1/4 position in the plate width direction from the end portion in the plate width direction, 1/2 position in the plate width direction from the end portion in the plate width direction, and It was obtained by calculating the difference between the maximum value and the minimum value of the 0.2% proof stress at the 3/4 position in the plate width direction from the end in the plate width direction.
[0114]
The uEl in the following formula (13) is a quarter position of the plate width in the plate width direction from the end portion in the plate width direction and a 1/2 position in the plate width direction from the end portion in the plate width direction obtained by the above method. It is the average value of uniform elongation at the 3/4 position in the plate width direction from the end in the plate width direction. Further, Δ uEl in the following formula (13) is obtained by the above-mentioned method, 1/4 position in the plate width direction from the end portion in the plate width direction, 1/2 position in the plate width direction from the end portion in the plate width direction, and It was obtained by calculating the difference between the maximum value and the minimum value of the uniform elongation at the 3/4 position in the plate width direction from the end in the plate width direction.
[0115]
Α M in the following equation (14) is 1/4 position in the plate width direction from the end in the plate width direction, 1/2 position in the plate width direction from the end in the plate width direction, and the plate width direction from the end in the plate width direction. A total of three test pieces were collected from each of the 3/4 positions, and the bending angle was measured in a bending test conforming to the standard 238-100 of the December 2010 edition of the German Automobile Manufacturers Association (Verband der Automobilindustrie: VDA). This is the angle of the test piece having the largest difference with respect to 90 ° among the measured values ​​of the plastic bending angle α of the test piece after applying the deformation of 90 ° and then unloading the load. That is, α M is the maximum value of the absolute value of “α-90 °”, and α M / 90 is an index showing the magnitude of dimensional variation after press molding in which the plastic bending angle α M is made dimensionless at 90 °. Is. In addition, the following conditions were set in the bending test of the VDA standard. Roll diameter: φ30 mm, distance between rolls: 2 x plate thickness + 0.5 ± 0.05 mm, punch shape: tip R = 0.4 mm, punch pushing speed: 20 mm / min, test piece dimensions: plate thickness x 60 mm x 60 mm, Bending direction: A direction perpendicular to the rolling direction. The plastic bending angle is a measured value of the angle inside the bending among the angles formed by the extension lines of the two flat surfaces of the test piece deformed into a "V" shape by the bending test.
[0116]
Δ YS / YS ≤ 0.20 ... (12)
Δ uEl / uEl ≦ 0.25 ... (13)
0.90 ≤ α M / 90 ≤ 1.10 ... (14)
[0117]
[Table 1-1]

[0118]
[Table 1-2]

[0119]
[Table 2-1]

[0120]
[Table 2-2]

[0121]
[Table 3-1]

[0122]
[Table 3-2]

[0123]
[Table 3-3]

[0124]
[Table 4-1]

[0125]
[Table 4-2]

[0126]
[Table 4-3]

[0127]
[Table 4-4]

[0128]
[Table 4-5]

[0129]
[Table 4-6]

[0130]
[Table 5-1]

[0131]
[Table 5-2]

[0132]
[Table 5-3]

[0133]
Of the steels A to AH shown in Table 1-1 and Table 1-2, the steels AA to AG are comparative examples that deviate from the range of the component composition defined in the present invention.
[0134]
AA steel did not satisfy equation (1-2). The steel sheet of Experimental Example 77 obtained using this steel had a low 0.2% proof stress, tensile strength and yield ratio because of the small amount of unrecrystallized ferrite.
[0135]
AB steel did not satisfy equation (1-2). The steel sheet of Experimental Example 78 obtained using this steel contained a large amount of unrecrystallized ferrite and did not satisfy the formula (4), so that the 0.2% proof stress and the yield ratio were high, and the formulas (12) and the formula (12) and the formula (4) were not satisfied. (13) was not satisfied.
[0136]
The AC steel had a Ti content higher than the range of the present invention. The steel sheet of Experimental Example 79 obtained using this steel contained a large amount of unrecrystallized ferrite, so that it had a high proof stress and yield ratio of 0.2% and a low uniform elongation.
[0137]
The Nb content of AD steel was higher than the range of the present invention. The steel sheet of Experimental Example 80 obtained using this steel contained a large amount of unrecrystallized ferrite, and therefore had a high proof stress of 0.2% and a high yield ratio.
[0138]
The C content of AE steel was lower than the range of the present invention. The steel sheet of Experimental Example 81 obtained using this steel had a low tensile strength.
[0139]
The AF steel had a C content and an S content higher than the range of the present invention. The steel sheet of Experimental Example 82 obtained using this steel had a low uniform elongation because the amount of ferrite was small.
[0140]
AG steel did not contain both Ti and Nb. The steel sheet of Experimental Example 83 obtained using this steel had a small amount of unrecrystallized ferrite, did not contain carbonitride, and did not satisfy the formula (5). Therefore, 0.2% proof stress, tensile strength and yield were obtained. The ratio was low.
[0141]
Experimental Examples 4, 7, 12, 21, 34, 41 and 61 are comparative examples in which the conditions of the hot rolling process deviate from the scope of the present invention.
[0142]
Experimental example 4 is a comparative example in which the formulas (2) and (3) were not satisfied and the formulas (12) and (13) were not satisfied because the hot rolling completion temperature was low.
[0143]
Experimental example 7 is a comparative example in which the average diameter of the carbonitride became large, the proof stress decreased by 0.2%, and the formula (12) was not satisfied because the heating temperature of the steel piece was low.
[0144]
Experimental example 12 is a comparative example in which the formula (2) was not satisfied and the formula (13) was not satisfied because the average cooling rate in the temperature range of 800 to 450 ° C. was low.
[0145]
Experimental Example 21 is a comparative example in which the formula (3) and the formula (5) were not satisfied and the formula (12) was not satisfied because the fn was large and the formula (6) was not satisfied in the temperature range of 1000 ° C. or lower. be.
[0146]
Experimental example 34 is a comparative example in which the formula (3) was not satisfied and the formula (12) was not satisfied because the time from the hot rolling to the start of cooling was short.
[0147]
Experimental example 41 is a comparative example in which the formula (3) was not satisfied and the formula (12) was not satisfied because the heating temperature of the steel piece was high.
[0148]
Experimental example 61 is a comparative example in which the formula (3) was not satisfied and the formula (12) was not satisfied because the hot rolling completion temperature was high.
[0149]
Experimental examples 38, 47, 71 and 76 are comparative examples in which the conditions of the reheating step deviate from the scope of the present invention.
[0150]
Experimental example 38 is a comparative example in which the maximum reheating temperature was high, so that the formulas (2), (4) and (5) were not satisfied, and the formulas (12) and (13) were not satisfied.
[0151]
In Experimental Example 47, since the maximum reheating temperature was low, the amount of unrecrystallized ferrite was large, the average diameter of the carbonitride was small, and the formulas (4) and (5) were not satisfied. This is a comparative example in which the yield ratio is high, the uniform elongation is low, and the formulas (12) and (13) are not satisfied.
[0152]
In Experimental Example 71, since K20 was high and the formula (8) was not satisfied in the temperature range of 450 to 700 ° C., the amount of martensite was large and the formula (5) was not satisfied, and the formulas (12) and (13) were not satisfied. It is a comparative example that did not satisfy.
[0153]
In Experimental Example 76, since the formula (7-1) was not satisfied, the average diameter of the carbonitride was small, the formula (5) was not satisfied, the 0.2% proof stress and the yield ratio were high, and the formula (13) was used. This is a comparative example that did not meet the requirements.
[0154]
Experimental Examples 2, 18 and 69 are comparative examples in which the conditions of the cold rolling process deviate from the scope of the present invention.
[0155]
In Experimental Example 2, since the cold rolling completion temperature was low, the amount of unrecrystallized ferrite was large, the formula (4) was not satisfied, the 0.2% proof stress was high, the uniform elongation was low, and the formula (12) and This is a comparative example in which the formula (13) was not satisfied.
[0156]
Experimental example 18 is a comparative example in which the formula (3) was not satisfied and the formula (12) was not satisfied because the total reduction rate was high.
[0157]
In Experimental Example 69, since the total reduction rate was low, the amount of unrecrystallized ferrite was large, the 0.2% proof stress and yield ratio were high, the uniform elongation was low, and the formulas (12) and (13) were not satisfied. This is a comparative example.
[0158]
Experimental Examples 9, 10, 19, 32, 37, 46, 49 and 50 are comparative examples in which the conditions of the annealing step deviate from the scope of the present invention.
[0159]
Experimental example 9 is a comparative example in which P10 was low and the formula (9) was not satisfied, so that the amount of unrecrystallized ferrite was large and the yield strength was high by 0.2%.
[0160]
Experimental example 10 is a comparative example in which the formula (10) was not satisfied, so the formula (2) was not satisfied, and the formulas (12) and (13) were not satisfied.
[0161]
Experimental example 19 is a comparative example in which the amount of retained austenite was large and the 0.2% proof stress and yield ratio were low because the formula (11) was not satisfied.
[0162]
Experimental example 32 is a comparative example in which the formula (2) was not satisfied and the formula (13) was not satisfied because tension was not applied in the temperature range from 720 ° C. to the annealing temperature.
[0163]
Experimental example 37 is a comparative example in which the amount of martensite was large and the 0.2% proof stress and yield ratio were low because the formula (10) was not satisfied.
[0164]
Experimental example 46 is a comparative example in which the amount of ferrite and the amount of unrecrystallized ferrite were small because the annealing temperature was high, and the uniform elongation was low.
[0165]
Experimental example 49 is a comparative example in which the amount of unrecrystallized ferrite was small because the annealing temperature was low, and the 0.2% proof stress and yield ratio were low.
[0166]
Experimental example 50 is a comparative example in which the amount of martensite was large and the 0.2% proof stress and yield ratio were low because the formula (10) was not satisfied.
[0167]
Experimental Example 84 does not satisfy the formula (6), the time until the start of cooling in the hot rolling step is short, and the rolling completion temperature is low in the cold rolling step, so that the formulas (2) to (5) are not satisfied. This is a comparative example.
[0168]
Experimental examples excluding the above comparative examples are examples in the present invention. It can be seen that the steel sheet described as an example has excellent formability, strength, and dimensional accuracy after press molding by manufacturing by a manufacturing method that satisfies the manufacturing conditions of the present invention.Karu.
[0169]
Experimental Examples 5, 11, 13, 15, 20, 24, 30, 39, 40, 43, 45, 48, 52, 54, 57, 62, 67 and 70 are plated steel sheets of the present invention. Is the example obtained.
[0170]
In Experimental Examples 15, 24, 43, 45 and 62, a hot-dip galvanized steel sheet (GI) was obtained by cooling the steel sheet to 500 ° C. in the annealing step, immersing it in a hot-dip zinc bath, and cooling it to room temperature. Is.
[0171]
In Experimental Examples 5, 11, 13, 30, 39 and 40, the steel sheet was cooled to 500 ° C. in the annealing step, immersed in a hot-dip zinc bath, further alloyed by reheating to 560 ° C., and then cooled to room temperature. This is an example in which an alloyed hot-dip galvanized steel sheet (GA) was obtained.
[0172]
Experimental examples 20 and 70 are examples in which a zinc alloy plated steel sheet was obtained by cooling the steel sheet to 500 ° C. in the annealing step, immersing it in a molten zinc alloy bath, and cooling it to room temperature.
[0173]
In Experimental Examples 48 and 52, the steel sheet was cooled to 500 ° C. in the annealing step, then immersed in a hot-dip zinc alloy bath, further alloyed by reheating to 580 ° C., and then alloyed by cooling to room temperature. This is an example obtained by obtaining a zinc alloy plated steel sheet.
[0174]
Experimental example 57 is an example in which a galvanized steel sheet was obtained by subjecting a vapor deposition plating treatment after temper rolling.
[0175]
Experimental examples 54 and 67 are examples in which an electrogalvanized steel sheet (EG) was obtained by subjecting an electrogalvanized steel sheet (EG) after an annealing step.
Industrial applicability
[0176]
According to the above aspect according to the present invention, it is possible to provide a steel sheet having excellent formability, strength and dimensional accuracy at the time of press molding, and a method for producing the same. The steel sheet according to the above aspect is a steel sheet suitable for significantly reducing the weight of an automobile and ensuring the protection and safety of passengers. Therefore, the present invention is highly applicable in the steel sheet manufacturing industry and the automobile industry.
The scope of the claims
[Claim 1]
Ingredient composition is mass%,
C: 0.035 to 0.150%,
Si: 0.010 to 1.500%,
Mn: 0.10 to 3.00%,
Al: 0.005 to 1.000%,
P: 0.100% or less,
S: 0.0200% or less,
N: 0.0150% or less,
O: 0.0100% or less,
V: 0 to 0.50%,
Cr: 0 to 1.00%,
Ni: 0 to 1.00%,
Cu: 0 to 1.00%,
Mo: 0 to 1.00%,
W: 0 to 1.00%,
B: 0 to 0.0100%,
Sn: 0 to 1.00%,
Sb: 0 to 0.20%,
Nb: 0 to 0.060%,
Ti: 0 to 0.100%,
Ca: 0-0.0100%,
Mg: 0 to 0.0100%,
Zr: 0-0.0100%,
REM: 0-0.0100%, and
Remaining: Fe and impurities,
Satisfy the following formulas (1-1) to (1-3)
The microstructure in the 1/4 width portion, which is 1/4 of the plate width in the plate width direction from the end in the plate width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, and the plate from the end in the plate width direction. The microstructure in the 1/2 width portion, which is 1/2 of the plate width in the width direction and 1/4 of the plate thickness in the plate thickness direction from the surface, and 3 of the plate width in the plate width direction from the end in the plate width direction. The microstructure in the 3/4 width portion, which is the / 4 position and the 1/4 position of the plate thickness in the plate thickness direction from the surface,
Area%, ferrite: 80% or more, martensite: 2% or less, retained austenite: 2% or less, and residual structure.
The ratio of unrecrystallized ferrite to the ferrite is 5 to 60%.
The average diameter of the carbonitride is 6.0 to 30.0 nm,
Satisfy the following formulas (2) to (5)
0.2% proof stress is 280-600MPa,
Tensile strength is 450-800 MPa,
The yield ratio is 0.50 to 0.90, and
Uniform elongation is 10.0% or more
A steel plate characterized by that.
1.5 x Nb + Ti ≧ 0.015 ... (1-1)
0.03 ≤ {(Ti / 48-N / 14) + Nb / 93} / (C / 12) ≤ 0.40 ... (1-2)
Ca + Mg + Zr + REM ≤ 0.0100 ... (1-3)
Δ SF / μ SF ≤ 0.10 ... (2)
Δ dF / μ dF ≦ 0.20… (3)
Δ SUF ≤ 20 ... (4)
Δ dC / μ dC ≦ 0.50 ... (5)
Ti, N, Nb, C, Ca, Mg, Zr and REM in the above formulas (1-1) to (1-3) indicate the content of each element in mass% and do not contain the element. In the case, 0% is substituted, and when the value of (Ti / 48-N / 14) becomes negative, 0 is substituted as the value of (Ti / 48-N / 14).
The μ SF in the formula (2) is the area ratio of ferrite in the microstructure in the 1/4 width portion, the area ratio of ferrite in the microstructure in the 1/2 width portion, and the 3/4 width portion. It is the average value of the area ratio of ferrite in the microstructure in the width portion, and ΔSF is the area of ​​ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. The difference between the maximum and minimum rates
The μdF in the formula (3) is the average crystal grain size of ferrite in the microstructure in the 1/4 width portion, the average crystal grain size of ferrite in the microstructure in the 1/2 width portion, and It is the average value of the average crystal grain size of ferrite in the microstructure in the 3/4 width portion, and Δ dF is the micro in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion. It is the difference between the maximum and minimum values ​​of the average crystal grain size of ferrite in the structure.
ΔSUF in the formula (4) is the maximum and minimum values ​​of the area ratio of unrecrystallized ferrite in the microstructure in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. Is the difference between
The μdC in the formula (5) is the average diameter of the carbonitride in the microstructure in the 1/4 width portion, the average diameter of the carbonitride in the microstructure in the 1/2 width portion, and It is the average value of the average diameters of the carbonitrides in the microstructure in the 3/4 width portion, and Δ dC is the micro in the 1/4 width portion, the 1/2 width portion and the 3/4 width portion. It is the difference between the maximum value and the minimum value of the average diameter of the carbonitride in the structure.
[Claim 2]
The component composition is mass%,
The steel sheet according to claim 1, wherein the Mn: 0.70 to 3.00%.
[Claim 3]
1 or 2 according to claim 1, wherein the average crystal grain size of the ferrite in the 1/4 width portion, the 1/2 width portion, and the 3/4 width portion is 5.0 to 15.0 μm. The steel plate described in.
[Claim 4]
The steel sheet according to any one of claims 1 to 3, which has a zinc-plated layer on the surface.
[Claim 5]
The steel sheet according to any one of claims 1 to 3, which has a zinc alloy plating layer on the surface.
[Claim 6]
The steel sheet according to claim 4 or 5, wherein the Fe content in the zinc plating layer or the zinc alloy plating layer is 7.0 to 13.0% in mass%.
[Claim 7]
The method for manufacturing the steel sheet according to any one of claims 1 to 3.
The steel piece having the component composition according to claim 1 is heated to 1150 to 1320 ° C., hot rolling is completed so that the hot rolling completion temperature becomes 850 to 930 ° C., and cooling is performed after 1.5 s or more have elapsed. A hot rolling process that starts and cools to a temperature range of less than 450 ° C so that the average cooling rate in the temperature range of 800 to 450 ° C is 20 ° C / s or more to form a hot-rolled steel sheet.
A reheating process that heats the hot-rolled steel sheet to a temperature range of 450 to 700 ° C.
A cooling process that cools the hot-rolled steel sheet to room temperature,
A cold rolling process in which the hot-rolled steel sheet is cold-rolled so that the total reduction ratio is 30 to 80% and the cold-rolling completion temperature is 120 ° C. or higher to obtain a cold-rolled steel sheet.
It has an annealing step of heating the cold-rolled steel sheet to an annealing temperature of 720 to 850 ° C. and cooling it to a temperature range of 500 ° C. or lower.
In the hot rolling process,
Satisfy the following formula (6) in the temperature range of 1000 ° C or less,
In the reheating process,
In the temperature range of 450 to 700 ° C, the following formula (7-1) and the following formula (8) are satisfied.
In the annealing process,
In the heating process to the annealing temperature
Satisfy the following formula (9) in the temperature range of 550 to 720 ° C.
In the temperature range from 720 ° C to the annealing temperature, a tension of 15 MPa or more is applied, and the following formula (10) is satisfied.
In the cooling process from the annealing temperature
Satisfy the following formula (11) in the temperature range of 720 to 500 ° C.
A method for manufacturing a steel sheet, which is characterized in that.
[Number 1]

In the above formula (6), f n is an index indicating the degree of progress of precipitation of fine carbides in the temperature range of 1000 ° C. or lower in the hot rolling process. Each reference numeral in the above equation (6) represents the following.
N: Number of rolling passes at 1000 ° C or lower
H: Plate thickness [mm] before rolling on the nth pass
H *: Plate thickness [mm] after rolling on the nth pass
Nb and Ti: Nb and Ti content [mass%]
T n: Average steel sheet temperature from rolling in the nth pass to rolling in the n + 1th pass [° C]
T n: The shorter time [s] from the rolling of the nth pass to the rolling of the n + 1th pass, or the time [s] from the rolling of the nth pass to the decrease of the steel sheet temperature to reach 800 ° C.
a 1 to 11: Constants (a 1 = 2.28 × 100, a 2 = 1.25 × 100, a 3 = 7.86 × 10 -4, a 4 = 1.36 × 10 -3, a 5 = 6.76 × 10 -4, a 6 = 7.86 × 10 -4, a 7 = 2.13 × 10 -3, a 8 = 1.14 × 10 -3, a 9 = 6.70 × 10- 2, a 10 = 1.11 × 100, a 11 = 5.27 × 10 -1)
[Number 2]

In the above formula (7-1), each reference numeral represents the following.
b 1-7: Constants (b 1 = 6.82 × 10 6, b 2 = 1.00 × 10 3, b 3 = 8.70 × 10 1, b 4 = 1.25 × 10 2, b 5 = 1.00 × 10 2, b 6 = -1.50 × 10 1, b 7 = -2.50 × 10 1)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T max: Maximum heating temperature [° C]
T 20: Effective heat treatment time in the 20th section when the staying time in the temperature range of 450 to 700 ° C. is divided into 20 equal parts [s]
D 20: An index showing the effective diffusion rate in the 20th section when the staying time in the temperature range of 450 to 700 ° C is divided into 20 equal parts.
However, the m-th effective heat treatment time tm and the m-th effective diffusion rate index D m are expressed by the following formula (7-2).
[Number 3]

In the above formula (7-2), each reference numeral represents the following.
M: Integer from 1 to 20
B 9-11: Constants (b 8 = 6.81 × 10 1, b 9 = 2.61 × 10 5, b 10 = 5.60 × 100, b 11 = 2.86 × 105)
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
T m: Average steel plate temperature [° C] in the m-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
T m: Effective heat treatment time in the m-th section when the staying time in the temperature range of 450 ° C to 700 ° C is divided into 20 equal parts [s]
However, let t 1 = t'
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
[Number 4]

In the above formula (8), K 20 is an index showing the degree of stabilization of cementite in the 20th section when the temperature history in the temperature range of 450 to 700 ° C. in the reheating step is divided into 20 equal parts with respect to time. Is. Each reference numeral in the above formula (8) represents the following.
J: An integer from 1 to 20
Si, Mn, Cr and Mo: Content of each element [mass%]
T j: Average steel sheet temperature [° C] in the j-th section when the staying time in the above temperature range of 450 ° C to 700 ° C is divided into 20 equal parts.
S j: Effective heat treatment time in the j-th section when the staying time in the temperature range of 450 ° C. to 700 ° C. is divided into 20 equal parts [s]
However, s 1 = t'.
T': 1/20 [s] of the total staying time in the temperature range of 450 ° C to 700 ° C
[Number 5]

In the above formula (9), p10 is an index showing the degree of recrystallization in the tenth section when the residence time in the temperature range of 550 to 720 ° C. in the heating process of the annealing step is divided into 10 equal parts. .. Each reference numeral in the above equation (9) represents the following.
D 1 to 4: Constants (d 1 = 4.24 × 10 2, d 2 = 2.10 × 100, d 3 = 1.31 × 10 3, d 4 = 7.63 × 10 3)
H: Plate thickness before cold rolling [mm]
H *: Plate thickness after cold rolling [mm]
TR: Cold rolling completion temperature [° C]
Nb: Nb content [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 2: Value obtained by equation (7-1)
N: An integer from 1 to 10
T n': Average temperature [° C.] in the nth section when the staying time in the temperature range of 550 to 720 ° C. is divided into 10.
Δ t: Time obtained by dividing the elapsed time from when the steel sheet temperature reached 550 ° C to when it reached 720 ° C into 10 [s]
However, t 1 = Δt.
[Number 6]

In the above formula (10), ym is an index indicating the degree of progress of reverse transformation in the m-th section when the staying time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 equal parts. Each reference numeral in the above formula (10) represents the following.
E1 to 4: Constants (e1 = 4.50 × 10 2, e2 = 2.85 × 10 4, e3 = 2.24 × 100, e4 = 8.56 × 10-8)
K 2: Value on the left side of equation (7-1)
K 3: Value of K 20 obtained by equation (8)
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T m: Average temperature [° C] in the m-th section when the residence time in the temperature range from 720 ° C to the annealing temperature is divided into 10.
T m: Effective heat treatment time in the m-th section when the residence time in the temperature range from 720 ° C. to the annealing temperature is divided into 10 [s]
[Number 7]

In the above formula (11), each reference numeral indicates the following.
I: Integer from 1 to 10
Δ i: 750-18 x Si-17 x Mn-10 x Cr-8 x Ni + 15 x Al-T i
However, each element indicates the content in% by mass, and if the element is not contained, 0 is substituted. If the calculated value of Δ i is a negative value, Δ i is set to 0.
g 1 to 6: Constants (g 1 = 1.00 × 10 -1, g 2 = 1.46 × 10 -1, g 3 = 1.14 × 10 -1, g 4 = 2.24 × 100, g 5 = 4.53 × 100, g 6 = 4.83 × 10 3)
Nb, Mo, Si, Mn, Cr, Ni and Al: Content of each element [mass%]
Ti *: Effective Ti amount represented by Ti-42 / 14 × N
However, Ti and N indicate the content of the element in mass%, and if the element is not contained, 0 is substituted.
K 4: Value of p10 obtained by equation (9)
Ac 1: Austenite transformation start temperature during heating [° C]
Ac 3: Austenite transformation completion temperature during heating [° C]
T max: Annealing temperature [° C]
Ti: Average temperature [° C] in the i-th section when the staying time in the temperature range of 720 to 500 ° C is divided into 10 equal parts.
Δt: Time obtained by dividing the total staying time in the temperature range of 720 to 500 ° C. into 10 equal parts [s]
[Claim 8]
The method for manufacturing a steel sheet according to claim 7, wherein the cold-rolled steel sheet is subjected to a hot-dip galvanizing treatment in the cooling process of the annealing step.
[Claim 9]
The method for manufacturing a steel sheet according to claim 7, wherein the cold-rolled steel sheet is subjected to a hot-dip zinc alloy plating treatment in the cooling process of the annealing step.
[Claim 10]
The method for producing a steel sheet according to claim 8 or 9, wherein in the cooling process of the annealing step, an alloying treatment is performed after the hot-dip galvanizing treatment or the hot-dip zinc alloy plating treatment.