Hot stamped steel and method for producing the same

Abstract

In a hot stamped steel, when [C] represents an amount of C (mass %), [Si] represents an amount of Si (mass %), and [Mn] represents an amount of Mn (mass %), an expression of 5×[Si]+[Mn])/[C]>10 is satisfied, a metallographic structure includes 80% or more of a martensite in an area fraction, and optionally, further includes one or more of 10% or less of a pearlite in an area fraction, 5% or less of a retained austenite in a volume ratio, 20% or less of a ferrite in an area fraction, and less than 20% of a bainite in an area fraction, TS×λ, which is a product of TS that is a tensile strength and λ that is a hole expansion ratio is 50000 MPa.Math.% or more, and a hardness of the martensite measured with a nanoindenter satisfies H2/H1<1.10 and σHM<20.

Claims

1. A hot stamped steel comprising, by mass %: C: more than 0.150% to 0.300%; Si: 0.010% to 1.000%; Mn: 1.50% to 2.70%; P: 0.001% to 0.060%; S: 0.001% to 0.010%; N: 0.0005% to 0.0100%; and Al: 0.010% to 0.050%; and optionally one or more of B: 0.0005% to 0.0020%; Mo: 0.01% to 0.50%; Cr: 0.01% to 0.50%; V: 0.001% to 0.100%; Ti: 0.001% to 0.100%; Nb: 0.001% to 0.050%; Ni: 0.01% to 1.00%; Cu: 0.01% to 1.00%; Ca: 0.0005% to 0.0050%; and REM: 0.0005% to 0.0050%; and a balance including Fe and unavoidable impurities, wherein, when [C] represents an amount of C by mass %, [Si] represents an amount of Si by mass %, and [Mn] represents an amount of Mn by mass %, a following expression a is satisfied, a metallographic structure includes 80% or more of a martensite in an area fraction, and optionally, further includes one or more of 10% or less of a pearlite in an area fraction, 5% or less of a retained austenite in a volume ratio, 20% or less of a ferrite in an area fraction, and less than 20% of a bainite in an area fraction, TS×λ which is a product of TS that is a tensile strength and λ that is a hole expansion ratio is 50000 MPa.Math.% or more, and a hardness of the martensite measured with a nanoindenter satisfies a following expression b and a following expression c,
(5×[Si]+[Mn])/[C]>10   (a)
1.005≦H2/H1<1.10   (b)
σHM<20   (c) here, the H1 represents an average hardness of the martensite in a surface portion, the H2 represents the average hardness of the martensite in a center part of a sheet thickness that is an area having a width of ±100 μm in a thickness direction from a center of the sheet thickness, and the σHM represents a variance of the hardness of the martensite existing in the central part of the sheet thickness.

2. The hot stamped steel according to claim 1, wherein an area fraction of a MnS existing in the metallographic structure and having an equivalent circle diameter of 0.1 μm to 10 μm is 0.01% or less, and a following expression d is satisfied,
n2/n1<1.5  (d) here, the n1 represents an average number density per 10000 μm.sup.2 of the MnS in a ¼ part of the sheet thickness, and the n2 represents an average number density per 10000 μm.sup.2 of the MnS in the central part of the sheet thickness.

3. The hot stamped steel according to claim 1 or 2, wherein a hot dip galvanized layer is formed on a surface thereof.

4. The hot stamped steel according to claim 3, wherein the hot dip galvanized layer includes a galvannealed layer.

5. The hot stamped steel according to claim 1 or 2, wherein an electrogalvanized layer is formed on a surface thereof.

6. The hot stamped steel according to claim 1 or 2, wherein an aluminized layer is formed on a surface thereof.

7. A method for producing a hot stamped steel comprising: casting a molten steel having a chemical composition according to claim 1 and obtain a steel; heating the steel; hot-rolling the steel with a hot-rolling facility having a plurality of stands; coiling the steel after the hot-rolling; pickling the steel after the coiling; cold-rolling the steel after the pickling with a cold rolling mill having a plurality of stands under a condition satisfying a following expression e; annealing in which the steel is heated under 700° C. to 850° C. and cooled after the cold-rolling; temper-rolling the steel after the annealing; and hot stamping in which the steel is heated to a temperature range of 750° C. or more at a temperature-increase rate of 5° C./second or more, formed within the temperature range, and cooled to 20° C. to 300° C. at a cooling rate of 10° C./second or more after the temper-rolling,
1.5×r1/r+1.2×r2/r+r3/r>1  (e) wherein ri (i=1, 2 or 3) represents an individual target cold-rolling reduction in unit % at an i.sup.th stand (i=1, 2 or 3) based on an uppermost stand among the plurality of the stands in the cold-rolling, and r represents a total cold-rolling reduction in unit % in the cold-rolling, and wherein an area fraction of a pearlite of the steel before the cold-rolling is 15% or more and the area fraction of the pearlite of the steel after the temper-rolling is 10% or less.

8. The method for producing a hot stamped steel according to claim 7, wherein, when CT in unit ° C. represents a coiling temperature in the coiling; [C] represents an amount of C by mass %, [Mn] represents an amount of Mn by mass %, [Cr] represents an amount of Cr by mass %, and [Mo] represents an amount of Mo by mass % in the steel; a following expression f is satisfied;
560−474×[C]−90×[Mn]−20×[Cr]−20×[Mo]<CT<830−270×[C]−90×[Mn]−70×[Cr]−80×[Mo]  (f).

9. The method for producing a hot stamped steel according to claim 7 or 8, wherein, when T in unit ° C. represents a heating temperature in the heating, t in unit minutes represents an in-furnace time; and [Mn] represents an amount of Mn by mass %, and [S] represents an amount of S by mass % in the steel, a following expression g is satisfied,
T×ln(t)/(1.7×[Mn]+[S])>1500  (g).

10. The method for producing a hot stamped steel according to claim 7 or 8, further comprising: galvanizing the steel between the annealing and the temper-rolling.

11. The method for producing a hot stamped steel according to claim 10, further comprising: alloying the steel between the hot dip galvanizing and the temper-rolling.

12. The method for producing a hot stamped steel according to claim 7 or 8, further comprising: electrogalvanizing the steel between the temper-rolling and the hot stamping.

13. The method for producing a hot stamped steel according to claim 7 or 8, further comprising: aluminizing the steel between the annealing and the temper-rolling.

Description

BRIEF DESCRIPTION OF THE DRAWING

(1) FIG. 1 is a graph illustrating a relationship between (5×[Si]+[Mn])/[C] and TS×λ.

(2) FIG. 2A is a graph illustrating a foundation of an expression b and an expression c, and is a graph illustrating a relationship between H2/H1 and σHM of a hot stamped steel.

(3) FIG. 2B is a graph illustrating a foundation of the expression c, and is a graph illustrating a relationship between the σHM and TS×λ.

(4) FIG. 3 is a graph illustrating a relationship between n2/n1 and TS×λ before and after hot stamping, and illustrating a foundation of expression d.

(5) FIG. 4 is a graph illustrating a relationship between 1.5×r1/r+1.2×r2/r+r3/r, and the H2/H1, and illustrating a foundation of an expression e.

(6) FIG. 5A is a graph illustrating a relationship between an expression f and a fraction of a martensite.

(7) FIG. 5B is a graph illustrating a relationship between the expression f and a fraction of a pearlite.

(8) FIG. 6 is a graph illustrating a relationship between T×ln(t)/(1.7×[Mn]+[S]) and TS×λ, and illustrating a foundation of expression g.

(9) FIG. 7 is a perspective view of a hot stamped steel used in an example.

(10) FIG. 8 is a flowchart illustrating a method for producing the hot stamped steel according to an embodiment of the present invention.

EMBODIMENTS OF THE INVENTION

(11) As described above, it is important to establish an appropriate relationship among an amount of Si, an amount of Mn and an amount of C, and furthermore, to set an appropriate hardness of a martensite at a predetermined position to improve a formability (hole expansibility) of a hot stamped steel. Thus far, there have been no studies regarding a relationship between the formability of the hot stamped steel and the hardness of the martensite.

(12) Hereinafter, an embodiment of the present invention will be described in detail.

(13) First, reasons for limiting a chemical composition of a cold rolled steel sheet for hot stamping (including a hot dip galvanized cold rolled steel sheet or an aluminized cold rolled steel sheet and, in some cases, referred to as a cold rolled steel sheet according to the embodiment or simply as a cold rolled steel sheet for hot stamping) used for a hot stamped steel according to an embodiment of the present invention (the hot stamped steel according to the present embodiment or, in some cases, referred to simply as the hot stamped steel) will be described. Hereinafter, “%” that is a unit of an amount of an individual component indicates “mass %”. Since a component amount of a chemical composition of the steel sheet does not change in the hot stamping, the chemical composition is identical in both the cold rolled steel sheet and the hot stamped steel for which the cold rolled steel sheet is used.

(14) C: more than 0.150% to 0.300%

(15) C is an important element to strengthen a ferrite and the martensite and increase a strength of a steel. However, when an amount of the C is 0.150% or less, a sufficient amount of a martensite cannot be obtained, and it is not possible to sufficiently increase the strength. On the other hand, when the amount of the C exceeds 0.300%, an elongation and the hole expansibility significantly degrades. Therefore, a range of the amount of the C is set to more than 0.150% and 0.300% or less.

(16) Si: 0.010% to 1.000%

(17) Si is an important element to suppress a generation of a harmful carbide and to obtain multi-phases mainly including the ferrite and the martensite. However, when an amount of the Si exceeds 1.000%, elongation or hole expansibility degrades, and a chemical conversion property also degrades. Therefore, the amount of the Si is set to 1.000% or less. In addition, the Si is added for deoxidation, but a deoxidation effect is not sufficient at the amount of the Si of less than 0.010%. Therefore, the amount of the Si is set to 0.010% or more.

(18) Al: 0.010% to 0.050%

(19) Al is an important element as a deoxidizing agent. To obtain the deoxidation effect, an amount of the Al is set to 0.010% or more. On the other hand, even when the Al is excessively added, the above-described effect is saturated, and conversely, the steel becomes brittle, and TS×λ is decreased. Therefore, the amount of the Al is set in a range of 0.010% to 0.050%.

(20) Mn: 1.50% to 2.70%

(21) Mn is an important element to improve a hardenability and strengthen the steel. However, when an amount of the Mn is less than 1.50%, it is not possible to sufficiently increase the strength. On the other hand, when the amount of the Mn exceeds 2.70%, the hardenability becomes excessive, and the elongation or the hole expansibility degrades. Therefore, the amount of the Mn is set to 1.50% to 2.70%. In a case in which higher elongation is required, the amount of the Mn is desirably set to 2.00% or less.

(22) P: 0.001% to 0.060%

(23) At a large amount, P segregates at grain boundaries, and deteriorates a local elongation and a weldability. Therefore, an amount of the P is set to 0.060% or less. The amount of the P is desirably smaller, but an extreme decrease in the amount of the P leads to a cost increase for refining, and therefore the amount of the P is desirably set to 0.001% or more.

(24) S: 0.001% to 0.010%

(25) S is an element that forms MnS and significantly deteriorates the local elongation or the weldability. Therefore, an upper limit of an amount of the S is set to 0.010%. In addition, the amount of the S is desirably smaller; however, due to a problem of a refining cost, a lower limit of the amount of the S is desirably set to 0.001%.

(26) N: 0.0005% to 0.0100%

(27) N is an important element to precipitate AlN and the like and miniaturize crystal grains. However, when an amount of the N exceeds 0.0100%, a nitrogen solid solution remains and elongation or hole expansibility is degraded. Therefore, an amount of the N is set to 0.0100% or less. The amount of the N is desirably smaller; however, due to a problem of a refining cost, a lower limit of the amount of the N is desirably set to 0.0005%.

(28) The cold rolled steel sheet according to the embodiment has a basic composition including the above-described elements and a balance including iron and unavoidable impurities, however, in some cases, includes at least one element of Nb, Ti, V, Mo, Cr, Ca, REM (rare earth metal), Cu, Ni and B as elements that have thus far been used in an amount that is equal to or less than an upper limit described below to improve the strength, to control a shape of a sulfide or an oxide, and the like. The above-described chemical elements are not necessarily added to the steel sheet, and therefore a lower limit thereof is 0%.

(29) Nb, Ti and V are elements that precipitate a fine carbonitride and strengthen the steel. In addition, Mo and Cr are elements that increase the hardenability and strengthen the steel. To obtain the above-described effects, it is desirable to include Nb: 0.001% or more, Ti: 0.001% or more, V: 0.001% or more, Mo: 0.01% or more and Cr: 0.01% or more. However, even when Nb: more than 0.050%, Ti: more than 0.100%, V: more than 0.100%, Mo: more than 0.50%, and Cr: more than 0.50% are contained, a strength-increasing effect is saturated, and the degradation of the elongation or the hole expansibility is caused. Therefore, upper limits of Nb, Ti, V, Mo and Cr are set to 0.050%, 0.100%, 0.100%, 0.50% and 0.50%, respectively.

(30) Ca controls the shape of the sulfide or the oxide and improves the local elongation or the hole expansibility. To obtain the above-described effect, it is desirable to contain 0.0005% or more of the Ca. However, since an excessive addition deteriorates a workability, an upper limit of an amount of the Ca is set to 0.0050%.

(31) Similarly to Ca, rare earth metal (REM) controls the shape of the sulfide and the oxide and improves the local elongation or the hole expansibility. To obtain the above-described effect, it is desirable to contain 0.0005% or more of the REM. However, since an excessive addition deteriorates the workability, an upper limit of an amount of the REM is set to 0.0050%.

(32) The steel can further include Cu: 0.01% to 1.00%, Ni: 0.01% to 1.00% and B: 0.0005% to 0.0020%. The above-described elements also can improve the hardenability and increase the strength of the steel. However, to obtain the above-described effect, it is desirable to contain Cu: 0.01% or more, Ni: 0.01% or more and B: 0.0005% or more. In amounts that are equal to or less than the above-described amounts, the effect that strengthens the steel is small. On the other hand, even when Cu: more than 1.00%, Ni: more than 1.00% and B: more than 0.0020% are added, the strength-increasing effect is saturated, and the elongation or the hole expansibility degrades. Therefore, an upper limit of an amount of the Cu is set to 1.00%, an upper limit of an amount of the Ni is set to 1.00%, and an upper limit of an amount of B is set to 0.0020%.

(33) In a case in which B, Mo, Cr, V, Ti, Nb, Ni, Cu, Ca and REM are included, at least one element is included. The balance of the steel includes Fe and unavoidable impurities. As the unavoidable impurities, elements other than the above-described elements (for example, Sn, As and the like) may be further included as long as characteristics are not impaired. When B, Mo, Cr, V, Ti, Nb, Ni, Cu, Ca and REM are included in amounts that is less than the above-described lower limits, the elements are treated as the unavoidable impurities.

(34) Furthermore, in the hot stamped steel according to the embodiment, when [C] represents the amount of the C (mass %), [Si] represents the amount of Si (mass %) and [Mn] represents the amount of Mn (mass %), it is important to satisfy the following expression a to obtain the sufficient hole expansibility as illustrated in FIG. 1.
(5×[Si]+[Mn])/[C]>10   (a)

(35) When a value of (5×[Si]+[Mn])/[C] is 10 or less, TS×λ becomes less than 50000 MPa.Math.%, and it is not possible to obtain the sufficient hole expansibility. This is because, when the amount of the C is high, a hardness of a hard phase becomes too high and a difference between a hardness of a hard phase and a hardness of a soft phase becomes great, and thereby, a value of λ is deteriorated, and, when the amount of the Si or the amount of the Mn is small, TS becomes low. Therefore, it is necessary to set the each element in the above-described ranges, and furthermore, to control a balance among the amounts thereof Since the value of (5×[Si]+[Mn])/[C] does not change even after hot stamping as described above, the value is preferably satisfied when producing the cold rolled steel sheet. However, even when (5×[Si]+[Mn])/[C]>10 is satisfied, in a case in which the H2/H1 or the σHM described below does not satisfy the conditions, the sufficient hole expansibility cannot be obtained. In FIG. 1, a reference sign for after the hot stamping indicates the hot stamped steel, and a reference sign for before the hot stamping indicates the cold rolled steel sheet for hot stamping.

(36) Generally, it is the martensite rather than the ferrite to dominate the formability (hole expansibility) in the cold rolled steel sheet having the metallographic structure mainly including the ferrite and the martensite. The inventors carried out intensive studies regarding a relationship between the hardness and the formability such as the elongation or the hole expansibility of the martensite. As a result, it was found that, when a hardness ratio (a difference of the hardness) of the martensite between a surface portion of a sheet thickness and a central part of the sheet thickness, and a hardness distribution of the martensite in the central part of the sheet thickness are in a predetermined state regarding a hot stamp formability according to the embodiment as illustrated in FIGS. 2A and 2B, the formability such as the elongation or the hole expansibility becomes favorable. In addition, it was clarified that, when the hardness ratio and the hardness distribution are in a predetermined range in the cold rolled steel sheet for hot stamping used for the hot stamp formability according to the embodiment, the hardness ratio and the hardness distribution are almost maintained in the hot stamped steel as well, and the formability such as the elongation or the hole expansibility becomes favorable. This is because the hardness distribution of the martensite formed in the cold rolled steel sheet for hot stamping also has a significant effect on the hot stamped steel after the hot stamping. Specifically, this is considered to be because alloy elements condensed in the central part of the sheet thickness still hold a state of being condensed in the central part even after the hot stamping is carried out. That is, in the cold rolled steel sheet for hot stamping, in a case in which the hardness difference of the martensite between the surface portion of the sheet thickness and the central part of the sheet thickness is great or a case in which a variance of the hardness of the martensite is great in the central part of the sheet thickness, the similar hardness ratio and the similar variance are obtained in the hot stamped steel as well. In FIGS. 2A and 2B, a reference sign for after the hot stamping indicates the hot stamped steel, and a reference sign for before the hot stamping indicates the cold rolled steel sheet for hot stamping.

(37) The inventors also found that, regarding a hardness measurement of the martensite measured with a nanoindenter manufactured by Hysitron Corporation at 1000 times, when the following expression b and the following expression c are satisfied, the formability of the hot stamped steel improves. Here, an “H1” is the hardness of the martensite in the surface portion of the sheet thickness that is within an area having a width of 200 μm in a thickness direction from an outermost layer of the hot stamped steel. An “H2” is the hardness of the martensite in the central part of the sheet thickness of the hot stamped steel, that is, in an area having a width of ±100 μm in the thickness direction from the central part of the sheet thickness. A “σHM” is the variance of the hardness of the martensite existing in an area having a width of 200 μm in the thickness direction in the central part of the sheet thickness of the hot stamped steel. The H1, the H2 and the σHM are each obtained from 300-point measurements. The area having a width of 200 μm in the thickness direction in the central part of the sheet thickness refers to an area having a center at a center of the sheet thickness and having a dimension of 200 μm in the thickness direction.
H2/H1<1.10   (b)
σHM<20   (c)

(38) In addition, here, the variance is a value obtained using the following expression h and indicating a distribution of the hardness of the martensite.

(39) $\left[\mathrm{Expression}1\right]$$\begin{array}{cc}\sigma \mathrm{HM}=\frac{1}{n}\underset{i=1}{\overset{n}{.Math.}}{\left(x_{\mathrm{ave}}-x_i\right)}^2& \left(h\right)\end{array}$

(40) An X.sub.ave represents an average value of the measured hardness of the martensite, and X.sub.i represents the hardness of an i.sup.th martensite.

(41) FIG. 2A illustrates the ratios between the hardness of the martensite in the surface portion and the hardness of the martensite in the central part of the sheet thickness of the hot stamped steel and the cold rolled steel sheet for hot stamping. In addition, FIG. 2B collectively illustrates the variance of the hardness of the martensite existing in the width of ±100 μm in the sheet thickness direction from the center of the sheet thickness of the hot stamped steel and the cold rolled steel sheet for hot stamping. As illustrated in FIGS. 2A and 2B, the hardness ratio of the cold rolled steel sheet before the hot stamping and the hardness ratio of the cold rolled steel sheet after the hot stamping are almost the same. In addition, the variances of the hardness of the martensite in the central part of the sheet thickness are also almost the same both in the cold rolled steel sheet before the hot stamping and in the cold rolled steel sheet after the hot stamping.

(42) In the hot stamped steel, a value of the H2/H1 being 1.10 or more represents that the hardness of the martensite in the central part of the sheet thickness is 1.10 or more times the hardness of the martensite in the surface portion of the sheet thickness. That is, this indicates that the hardness in the central part of the sheet thickness becomes too high. As illustrated in FIG. 2A, when the H2/H1 is 1.10 or more, the σHM reaches 20 or more. In this case, TS×λ becomes less than 50000 MPa.Math.%, and a sufficient formability cannot be obtained after quenching, that is, in the hot stamped steel. Theoretically, there is a case in which a lower limit of the H2/H1 becomes the same in the central part of the sheet thickness and in the surface portion of the sheet thickness unless a special thermal treatment is carried out; however, in an actual production process in consideration of a productivity, the lower limit is, for example, up to approximately 1.005.

(43) The variance σHM of the hot stamped steel being 20 or more indicates that a variation of the hardness of the martensite is large, and parts in which the hardness is too high locally exist. In this case, TS×λ becomes less than 50000 MPa.Math.%. That is, a sufficient formability cannot be obtained in the hot stamped steel.

(44) Next, the metallographic structure of the hot stamped steel according to the embodiment will be described. An area fraction of the martensite is 80% or more in the hot stamped steel according to the embodiment. When the area fraction of the martensite is less than 80%, a sufficient strength that has been recently required for the hot stamped steel (for example, 1.5 GPA) cannot be obtained. Therefore, the area fraction of the martensite is set to 80% or more. All or principal parts of the metallographic structure of the hot stamped steel are occupied by the martensite, and may further include one or more of 0% to 10% of a pearlite in an area fraction, 0% to 5% of a retained austenite in a volume ratio, 0% to 20% of the ferrite in an area fraction, and 0% to less than 20% of a bainite in an area fraction. While there is a case in which 0% to 20% of the ferrite exists depending on a hot stamping condition, there is no problem with the strength after the hot stamping within the above-described range. When the retained austenite remains in the metallographic structure, a secondary working brittleness and a delayed fracture characteristic are likely to degrade. Therefore, it is preferable that the residual austenite is substantially not included; however, unavoidably, 5% or less of the residual austenite in a volume ratio may be included. Since the pearlite is a hard and brittle structure, it is preferable not to include the pearlite; however, unavoidably, up to 10% of the pearlite in an area fraction may be included. The bainite is a structure that can be formed as a residual structure, and is an intermediate structure in terms of the strength or the formability, may be included. The bainite may be included up to less than 20% in terms of an area fraction. In the embodiment, the metallographic structures of the ferrite, the bainite and the pearlite were observed through Nital etching, and the metallographic structure of the martensite was observed through Le pera etching. All the metallographic structures were observed in a ¼ part of the sheet thickness with an optical microscope at 1000 times. The volume ratio of the retained austenite was measured with an X-ray diffraction apparatus after polishing the steel sheet up to the ¼ part of the sheet thickness.

(45) Next, the desirable metallographic structure of the cold rolled steel sheet for hot stamping for which the hot stamped steel according to the embodiment is used will be described. The metallographic structure of the hot stamped steel is affected by the metallographic structure of the cold rolled steel sheet for hot stamping. Therefore, when the metallographic structure of the cold rolled steel sheet for hot stamping is controlled, it becomes easy to obtain the above-described metallographic structure in the hot stamped steel. In the cold rolled steel sheet according to the embodiment, the area fraction of the ferrite is desirably 40% to 90%. When the area fraction of the ferrite is less than 40%, the strength becomes too high even before the hot stamping and there is a case in which the shape of the hot stamped steel deteriorates or cutting becomes difficult. Therefore, the area fraction of the ferrite before the hot stamping is desirably set to 40% or more. In addition, in the cold rolled steel sheet according to the embodiment, since an amount of alloy elements is great, it is difficult to set the area fraction of the ferrite to more than 90%. In the metallographic structure, in addition to the ferrite, the martensite is included, and the area fraction thereof is desirably 10% to 60%. A total of the area fraction of the ferrite and the area fraction of the martensite is desirably 60% or more before the hot stamping. The metallographic structure may further include one or more of the pearlite, the bainite and the retained austenite. However, when the retained austenite remains in the metallographic structure, the secondary working brittleness and the delayed fracture characteristics are likely to degrade, and therefore it is preferable that the retained austenite be substantially not included. However, unavoidably, 5% or less of the retained austenite may be included in a volume ratio. Since the pearlite is a hard and brittle structure, the pearlite is preferably not included; however, unavoidably, up to 10% of the pearlite may be included in an area fraction. Up to 20% or less of the bainite as the residual structure can be included in an area fraction for the same reason as described above. Similarly to the cold rolled steel sheet before the hot stamping, the metallographic structures of the ferrite, the bainite and the pearlite were observed through Nital etching, and the metallographic structure of the martensite was observed through Le pera etching. All the metallographic structures were observed in a ¼ part of the sheet thickness with an optical microscope at 1000 times. The volume ratio of the retained austenite was measured with an X-ray diffraction apparatus after polishing the steel sheet up to the ¼ part of the sheet thickness.

(46) In addition, in the hot stamped steel according to the embodiment, the hardness of the martensite measured with a nanoindenter at 1000 times (indentation hardness (GPa or N/mm.sup.2) or a value obtained by converting the indentation hardness to a Vickers hardness (Hv)) is specified. In an ordinary Vickers hardness test, a formed indentation becomes larger than the martensite. Therefore, a macroscopic hardness of the martensite and peripheral structures thereof (the ferrite and the like) can be obtained, but it is not possible to obtain the hardness of the martensite itself. Since the formability such as the hole expansibility is significantly affected by the hardness of the martensite itself, it is difficult to sufficiently evaluate the formability only with the Vickers hardness. On the contrary, in the hot stamped steel according to the embodiment, since the hardness ratio of the hardness of the martensite measured with the nanoindenter and a dispersion state are controlled in an appropriate range, it is possible to obtain an extremely favorable formability.

(47) The MnS was observed at a location of ¼ of the sheet thickness (a location that is ¼ of the sheet thickness deep from the surface) and the central part of the sheet thickness of the hot stamped steel. As a result, it was found that an area fraction of the MnS having an equivalent circle diameter of 0.1 μm to 10 μm of 0.01% or less and, as illustrated in FIG. 3, the following expression d being satisfied are preferable for favorably and stably obtaining TS×λ≧50000 MPa.Math.%.
n2/n1<1.5   (d)

(48) Here, the n1 represents a number density (average number density) (grains/10000 μm.sup.2) of the MnS having the equivalent circle diameter of 0.1 μm to 10 μm per unit area in the ¼ part of the sheet thickness of the hot stamped steel, and the n2 represents a number density (average number density) (grains/10000 μm.sup.2) of the MnS having the equivalent circle diameter of 0.1 μm to 10 μm per unit area in the central part of the sheet thickness of the hot stamped steel.

(49) A reason for the formability improving in a case in which the area fraction of MnS of 0.1 μm to 10 μm is 0.01% or less is considered that, when a hole expansion test is carried out, if there is MnS having the equivalent circle diameter of 0.1 μm or more, since stress concentrates in a vicinity thereof, cracking is likely to occur. A reason for not counting the MnS having the equivalent circle diameter of less than 0.1 μm is that an effect on the stress concentration is small, and a reason for not counting the MnS having the equivalent circle diameter of more than 10 μm is that the MnS having the equivalent circle diameter of more than 10 μm is originally not suitable for working. Furthermore, when the area fraction of the MnS having the equivalent circle diameter of 0.1 μm to 10 μm exceeds 0.01%, since it becomes easy for fine cracks generated due to the stress concentration to propagate. Therefore, there is a case in which the hole expansibility degrades. Furthermore, a lower limit of the area fraction of the MnS is not particularly specified, but it is reasonable to set the lower limit to 0.0001% or more since setting the lower limit to less than 0.0001% in consideration of a measurement method described below, limitations of a magnification and a visual field, the amount of the Mn or the S, and a desulfurization treatment capability has an effect on a productivity and a cost.

(50) When the area fraction of MnS having the equivalent circle diameter of 0.1 μm to 10 μm in the hot stamped steel is more than 0.01%, as described above, the formability is likely to degrade due to the stress concentration. A value of the n2/n1 being 1.5 or more in the hot stamped steel indicates that the number density of the MnS in the central part of the sheet thickness of the hot stamped steel is 1.5 or more times the number density of the MnS in the ¼ part of the sheet thickness of the hot stamped steel. In this case, the formability is likely to degrade due to a segregation of the MnS in the central part of the sheet thickness. In the embodiment, the equivalent circle diameter and the number density of the MnS were measured with a field emission scanning electron microscope (Fe-SEM) manufactured by JEOL Ltd. The magnification was 1000 times, and a measurement area of the visual field was set to 0.12×0.09 mm.sup.2 (=10800 μm.sup.2≈10000 μm.sup.2). 10 visual fields were observed at the location of ¼ of the sheet thickness from the surface (the ¼ part of the sheet thickness), and 10 visual fields were observed in the central part of the sheet thickness. The area fraction of the MnS was computed with particle analysis software. In the embodiment, the MnS was observed in the cold rolled steel sheet for hot stamping in addition to the hot stamped steel. As a result, it was found that a form of the MnS formed before the hot stamping (in the cold rolled steel sheet for hot stamping) did not change even in the hot stamped steel (after the hot stamping). FIG. 3 is a view illustrating a relationship between the n2/n1 and TS×λ of the hot stamped steel, and also illustrates an evaluation of measurement results of the number density of the MnS in the ¼ part of the sheet thickness and in the central part of the sheet thickness of the cold rolled steel sheet for hot stamping using the same index as for the hot stamped steel. In FIG. 3, a reference sign for after the hot stamping indicates the hot stamped steel, and a reference sign for before the hot stamping indicates the cold rolled steel sheet for hot stamping. As illustrated in FIG. 3, the n2/n1 (a ratio of the MnS between the ¼ part of the sheet thickness and the central part of the sheet thickness) of the cold rolled steel sheet for hot stamping and the hot stamped steel is almost the same. This is because the form of the MnS does not change at a heating temperature of the hot stamping.

(51) The hot stamped steel according to the embodiment is obtained, for example, by heating the cold rolled steel sheet according to the embodiment to 750° C. to 1000° C. at a temperature-increase rate of, 5° C./second to 500° C./second, forming (working) the steel sheet for 1 second to 120 seconds, and cooling the steel sheet to a temperature range of 20° C. to 300° C. at a cooling rate of 10° C./second to 1000° C./second. An obtained hot stamped steel has a tensile strength of 1500 MPa to 2200 MPa, and can obtain a significant formability-improving effect, particularly, in a steel sheet having a high strength of approximately 1800 MPa to 2000 MPa.

(52) It is preferable to form a galvanizing, for example, a hot dip galvanizing, a galvannealing, an electrogalvanizing, or an aluminizing on the hot stamped steel according to the embodiment in terms of rust prevention. In a case in which a plating is formed on the hot stamped steel, a plated layer does not change under the above-described hot stamping condition, and therefore a plating may be formed on the cold rolled steel sheet for hot stamping. Even when the above-described plating is formed on the hot stamped steel, the effects of the embodiment are not impaired. The above-described platings can be formed with a well-known method.

(53) Hereinafter, a method for producing the cold rolled steel sheet according to the embodiment and the hot stamped steel according to the embodiment obtained by hot-stamping the cold rolled steel sheet will be described.

(54) When producing the cold rolled steel sheet according to the embodiment, as an ordinary condition, a molten steel melted so as to have the above-described chemical composition is continuously cast after a converter, thereby producing a slab. In the continuous casting, when a casting rate is fast, a precipitate of Ti and the like becomes too fine. On the other hand, when the casting rate is slow, productivity deteriorates, and consequently, the above-described precipitate coarsens so as to decrease the number of particles, and there is a case in which other characteristics such as a delayed fracture cannot be controlled appears. Therefore, the casting rate is desirably 1.0 m/minute to 2.5 m/minute.

(55) The slab after the melting and the casting can be subjected to hot-rolling as cast. Alternatively, in a case in which the slab is cooled to less than 1100° C., it is possible to reheat the slab to 1100° C. to 1300° C. in a tunnel furnace or the like and subject the slab to the hot-rolling. When a temperature of the slab during the hot-rolling is less than 1100° C., it is difficult to ensure a finishing temperature in the hot-rolling, which causes a degradation of the elongation. In addition, in the steel sheet to which Ti or Nb is added, a dissolution of the precipitate becomes insufficient during the heating, which causes a decrease in the strength. On the other hand, when the temperature of the slab is more than 1300° C., a generation of a scale becomes great, and there is a concern that it may be impossible to make the surface quality of the steel sheet favorable.

(56) In addition, to decrease the area fraction of the MnS, when [Mn] represents the amount of the Mn (mass %) and [S] represent the amount of the S (mass %) in the steel, it is preferable for a temperature T (° C.) of a heating furnace before carrying out the hot-rolling, an in-furnace time t (minutes), [Mn] and [S] to satisfy the following expression g as illustrated in FIG. 6.
T×ln(t)/(1.7×[Mn]+[S])>1500   (g)

(57) When a value of T×ln(t)/(1.7×[Mn]+[S]) is equal to or less than 1500, the area fraction of the MnS becomes large, and there is a case in which a difference between the number of the MnS in the ¼ part of the sheet thickness and the number of the MnS in the central part of the sheet thickness becomes large. The temperature of the heating furnace before carrying out the hot-rolling refers to an extraction temperature at an outlet side of the heating furnace, and the in-furnace time refers to a time elapsed from an insertion of the slab into the hot heating furnace to an extraction of the slab from the heating furnace. Since the MnS does not change with the hot-rolling or the hot stamping as described above, it is preferable to satisfy the expression g during heating of the slab. The above-described In represents a natural logarithm.

(58) Next, the hot-rolling is carried out according to a conventional method. At this time, it is desirable to set the finishing temperature (a hot-rolling end temperature) to an Ar3 temperature to 970° C. and carry out the hot-rolling on the slab. When the finishing temperature is less than the Ar3 temperature, there is a concern that the rolling may become a two-phase region rolling of the ferrite (α) and the austenite (γ), and the elongation may degrade. On the other hand, when the finishing temperature is more than 970° C., an austenite grain size coarsens, a fraction of the ferrite becomes small, and there is a concern that the elongation may degrade.

(59) The Ar3 temperature can be estimated from an inflection point after carrying out a formastor test and measuring a change in a length of a test specimen in response to a temperature change.

(60) After the hot-rolling, the steel is cooled at an average cooling rate of 20° C./second to 500° C./second, and is coiled at the predetermined coiling temperature CT° C. In a case in which the cooling rate is less than 20° C./second, the pearlite causing the degradation of the elongation is likely to be formed, which is not preferable.

(61) On the other hand, an upper limit of the cooling rate is not particularly specified, but the upper limit of the cooling rate is desirably set to approximately 500° C./second from a viewpoint of a facility specification, but is not limited thereto.

(62) After the coiling, pickling is carried out, and cold-rolling is carried out. At this time, as illustrated in FIG. 4, the cold-rolling is carried out under a condition in which the following expression e is satisfied to obtain a range satisfying the above-described expression b. When the above-described rolling is carried out, and then annealing, cooling and the like are performed in below-described conditions, TS×λ>50000 MPa.Math.% can be obtained in the cold rolled steel sheet before hot stamping, and furthermore, it is possible to ensure TS×λ>50000 MPa.Math.% in the hot stamped steel for which the cold rolled steel sheet is used. Meanwhile, the cold-rolling is desirably carried out with a tandem rolling mill in which a plurality of rolling mills is linearly disposed, and the steel sheet is continuously rolled in a single direction, thereby obtaining a predetermined thickness.
1.5×r1/r+1.2×r2/r+r3/r>1.0   (e)

(63) Here, the “ri (i=1, 2 or 3)” represents an individual target cold-rolling reduction (%) at an i.sup.th stand (i=1, 2, 3) based on an uppermost stand in the cold-rolling, and the “r” represents a total target cold-rolling reduction (%) in the cold-rolling.

(64) The total cold-rolling reduction is a so-called cumulative reduction, is based on the sheet thickness at an inlet of a first stand, and is a percentage of the cumulative reduction (a difference between the sheet thickness at the inlet of a first pass and the sheet thickness at an outlet after a final pass) with respect to the above-described basis.

(65) When the cold-rolling is carried out under a condition in which the above-described expression e is satisfied, it is possible to sufficiently divide the pearlite in the cold-rolling even when the large pearlite exists before the cold-rolling. As a result, it is possible to burn the pearlite or suppress the area fraction of the pearlite to the minimum extent through annealing carried out after the cold-rolling. Therefore, it becomes easy to obtain a structure satisfying the expression b and the expression c. On the other hand, in a case in which the expression e is not satisfied, the cold-rolling reductions in the upper stream stands are not sufficient, and the large pearlite is likely to remain. As a result, it is not possible to form the martensite having a desired form in an annealing process.

(66) In addition, the inventors found that, in the cold rolled steel sheet that had been subjected to a rolling satisfying the expression e, it was possible to maintain the form of the martensite structure obtained after the annealing in almost the same state even when the hot stamping is carried out afterwards, and the elongation or the hole expansibility became advantageous. In a case in which the cold rolled steel sheet for hot stamping according to the embodiment is heated up to an austenite region through the hot stamping, the hard phase including the martensite turns into an austenite having a high C concentration, and the ferrite phase turns into the austenite having a low C concentration. When the austenite is cooled afterwards, the austenite forms a hard phase including martensite. That is, when the hot stamping is carried out on the steel sheet for hot stamping having the hardness of the martensite so as to satisfy the expression e (so as to make the above-described H2/H1 in a predetermined range), the above-described H2/H1 reaches in a predetermined range even after the hot stamping, and the formability after the hot stamping becomes excellent.

(67) In the embodiment, the r, the r1, the r2 and the r3 are the target cold-rolling reductions. Generally, the target cold-rolling reduction and an actual cold-rolling reduction are controlled so as to become substantially the same value, and the cold-rolling is carried out. It is not preferable to carry out the target cold-rolling after unnecessarily making the actual cold-rolling reduction different from the cold-rolling reduction. In a case in which there is a large difference between a target rolling reduction and an actual rolling reduction, it is possible to consider that the embodiment is carried out when the actual cold-rolling reduction satisfies the expression e. The actual cold-rolling reduction is preferably converged within ±10% of the cold-rolling reduction.

(68) After the cold-rolling, the annealing is carried out. When the annealing is carried out, a recrystallization is caused in the steel sheet, and the desired martensite is formed. Regarding an annealing temperature, it is preferable to carry out the annealing by heating the steel sheet to a range of 700° C. to 850° C. according to a conventional method, and to cool the steel sheet to 20° C. or a temperature at which a surface treatment such as the hot dip galvanizing is carried out. When the annealing is carried out in the above-described range, it is possible to ensure a desirable fraction of the ferrite and a desirable area fraction of the martensite and to obtain a total of the area fraction of the ferrite and the area fraction of the martensite of 60% or more, TS×λ, improves.

(69) Conditions other than the annealing temperature are not particularly specified, but a lower limit of a holding time at 700° C. to 850° C. is preferably set to 1 second or more to reliably obtain a predetermined structure, for example, approximately 10 minutes as long as the productivity is not impaired. It is preferable to appropriately determine the temperature-increase rate to 1° C./second to an upper limit of a facility capacity, for example, 1000° C./second, and to appropriately determine the cooling rate to 1° C./second to the upper limit of the facility capacity, for example, 500° C./second. Temper-rolling may be carried out with a conventional method. An elongation ratio of the temper-rolling is, generally, approximately 0.2% to 5%, and is preferable when a yield point elongation is avoided and the shape of the steel sheet can be corrected.

(70) As a still more preferable condition of the present invention, when [C] represents the amount of the C (mass %), [Mn] represents the amount of Mn (mass %), [Si] represents the amount of Si (mass %), and [Mo] represents the amount of Mo (mass %) in steel, the coiling temperature CT in a coiling process preferably satisfies the following expression f.
560−474×[C]−90×[Mn]−20×[Cr]−20×[Mo]<CT <830−270×[C]−90×[Mn]−70×[Cr]−80×[Mo]  (f)

(71) When the coiling temperature CT is less than 560−474×[C]−90×[Mn]−20×[Cr]−20×[Mo], that is, CT−(560−474×[C]−90×[Mn]−20×[Cr]−20×[Mo]) is less than zero as illustrated in FIG. 5A, the martensite is excessively formed, and the steel sheet becomes too hard such that there is a case in which the subsequent cold-rolling becomes difficult. On the other hand, when the coiling temperature CT is more than 830−270×[C]−90×[Mn]−70×[Cr]−80×[Mo], that is, CT−(830−270×[C]−90×[Mn]−70×[Cr]−80×[Mo]) is more than zero as illustrated in FIG. 5B, a banded structure including the ferrite and the pearlite is likely to be formed. In addition, a fraction of the pearlite in the central part of the sheet thickness is likely to become high. Therefore, a uniformity of a distribution of the martensite being formed in the subsequent annealing process degrades, and it becomes difficult to satisfy the above-described expression b. In addition, there is a case in which it becomes difficult for a sufficient amount of the martensite to be formed.

(72) When the expression f is satisfied, the ferrite and the hard phase have an ideal distribution form before the hot stamping as described above. Furthermore, in this case, the C and the like are likely to diffuse in a uniform manner after heating is carried out in the hot stamping. Therefore, the distribution form of the hardness of the martensite in the hot stamped steel becomes approximately ideal. When it is possible to more reliably ensure the above-described metallographic structure by satisfying the expression f, the formability of the hot stamped steel becomes excellent.

(73) Furthermore, to improve a rust-preventing capability, it is also preferable to include a hot dip galvanizing process in which a hot dip galvanizing is formed between the annealing process and the temper-rolling process and to form the hot dip galvanizing on a surface of the cold rolled steel sheet. Furthermore, it is also preferable to include an alloying process in which an alloying is formed between the hot dip galvanizing process and the temper-rolling process to obtain a galvannealing by alloying the hot dip galvanizing. In a case in which the alloying is carried out, a treatment in which a galvannealed surface is brought into contact with a substance oxidizing a plated surface such as water vapor, thereby thickening an oxidized film may be further carried out on the surface.

(74) It is also preferable to include, for example, an electrogalvanizing process in which an electrogalvanizing is formed on the surface of the cold rolled steel sheet after the temper-rolling process other than the hot dip galvanizing process and the galvannealing process. In addition, it is also preferable to include, instead of the hot dip galvanizing, an aluminizing process in which an aluminizing is formed between the annealing process and the temper-rolling process, and to form the aluminizing on the surface of the cold rolled steel sheet. The aluminizing is generally hot dip aluminizing, which is preferable.

(75) After a series of the above-described treatments, the hot stamping is carried out on the obtained cold rolled steel sheet for hot stamping, thereby producing a hot stamped steel. In a hot stamping process, the hot stamping is desirably carried out under, for example, the following conditions. First, the steel sheet is heated up to 750° C. to 1000° C. at the temperature-increase rate of 5° C./second to 500° C./second. After the heating, working (forming) is carried out for 1 second to 120 seconds. To obtain a high strength, the heating temperature is preferably more than an Ac3 temperature. The Ac3 temperature was estimated from the inflection point of the length of the test specimen after carrying out the formastor test.

(76) Subsequently, it is preferable to cool the steel sheet to 20° C. to 300° C. at the cooling rate of, for example, 10° C./second to 1000° C./second. When the heating temperature is less than 750° C., in the hot stamped steel, the fraction of the martensite is not sufficient, and the strength cannot be ensured. When the heating temperature is more than 1000° C., the steel sheet becomes too soft, and, in a case in which a plating is formed on the surface of the steel sheet, particularly, in a case in which zinc is plated, there is a concern that the zinc may be evaporated and burned, which is not preferable. Therefore, the heating temperature in the hot stamping process is preferably 750° C. to 1000° C. When the temperature-increase rate is less than 5° C./second, since a control thereof is difficult, and the productivity significantly degrades, it is preferable to heat the steel sheet at the temperature-increase rate of 5° C./second or more. On the other hand, an upper limit of the temperature-increase rate of 500° C./second is from a current heating capability, but is not limited thereto. At the cooling rate of less than 10° C./second, since the rate control thereof is difficult, and the productivity also significantly degrades, it is preferable to cool the steel sheet at the cooling rate of 10° C./second or more. An upper limit of the cooling rate is not particularly specified, but becomes 1000° C./second or less in consideration of a current cooling capability. A reason for carrying out the temperature increasing and the forming working within 1 second to 120 seconds is to avoid the evaporation of the zinc and the like in a case in which the hot dip galvanizing and the like are formed on the surface of the steel sheet. A reason for setting the cooling temperature to 20° C. (the room temperature) to 300° C. is to sufficiently ensure the martensite so as to ensure the strength after the hot stamping.

(77) According to what has been described above, when the above-described conditions are satisfied, it is possible to produce the hot stamped steel in which the hardness distribution or the structure is almost maintained even after the hot stamping, and consequently the strength is ensured and the more favorable hole expansibility can be obtained.

(78) FIG. 8 illustrates a flowchart (processes Si to S14) of an example of the production method described above.

EXAMPLE

(79) A steel having a composition described in Table 1 was continuously cast at a casting rate of 1.0 m/minute to 2.5 m/minute, then, a slab was heated in a heating furnace under a condition of Table 2 according to a conventional method as cast or after cooling the steel once, and hot rolling was carried out at a finishing temperature of 910° C. to 930° C., thereby producing a hot rolled steel sheet. After that, the hot rolled steel sheet was coiled at a coiling temperature CT described in Table 2. After that, scales on a surface of the steel sheet were removed by carrying out pickling, and a sheet thickness was set to 1.2 mm to 1.4 mm through cold-rolling. At this time, the cold rolling was carried out so that the value of the expression e became the value described in Table 2. After the cold-rolling, annealing was carried out in a continuous annealing furnace at an annealing temperature described in Tables 3 and 4. On a part of the steel sheets, a hot dip galvanizing was formed in the middle of cooling after soaking in the continuous annealing furnace, and then alloying was further carried out on the part thereof, thereby forming a galvannealing. In addition, an electrogalvanizing or an aluminizing was formed on the part of the steel sheets. Temper rolling was carried out at an elongation ratio of 1% according to a conventional method. In this state, a sample was taken to evaluate material qualities and the like of the cold rolled steel sheet for hot stamping, and a material quality test or the like was carried out. After that, to obtain a hot stamped steel having a form illustrated in FIG. 7, hot stamping in which a temperature was increased at a temperature-increase of 10° C./second, the steel sheet was held at a heating temperature of 850° C. for 10 seconds, and cooled to 200° C. or less at a cooling rate of 100° C./second was carried out. A sample was cut out from a location of FIG. 7 in an obtained molded article, a material quality test and a structure observation were carried out, and fractions of individual structures, a number density of MnS, a hardness, a tensile strength (TS), an elongation (El), a hole expansion ratio (2) and the like were obtained. The results are described in Tables 3 to 8. The hole expansion ratios λ in Tables 3 to 6 are obtained with the following expression i.
λ(%)={(d′−d)/d}×100   (i)

(80) d′: a hole diameter when a crack penetrates a sheet thickness

(81) d: an initial hole diameter

(82) Regarding plating types in Tables 5 and 6, CR represents a non-plated cold rolled steel sheet, GI represents a formation of the hot dip galvanizing, GA represents a formation of the galvannealing, EG represents a formation of the electrogalvanizing, and Al represents a formation of the aluminizing.

(83) An amount of “0” in Table 1 indicates that an amount is equal to or less than a measurement lower limit.

(84) Determinations G and B in Tables 2, 7 and 8 are defined as follows.

(85) G: a target condition expression is satisfied.

(86) B: the target condition expression is not satisfied.

(87) TABLE-US-00001 TABLE 1 (mass %) Steel Type Reference symbol C Si Mn P S N Al Cr Mo V Ti A 0.151 0.145 2.01 0.003 0.008 0.0035 0.035 0 0 0 0 B 0.158 0.231 1.61 0.023 0.006 0.0064 0.021 0 0 0 0 C 0.167 0.950 2.12 0.008 0.009 0.0034 0.042 0.12 0 0 0 D 0.178 0.342 1.62 0.007 0.007 0.0035 0.042 0.42 0.15 0 0 E 0.186 0.251 1.89 0.008 0.008 0.0045 0.034 0.21 0 0 0 F 0.191 0.256 1.71 0.006 0.009 0.0087 0.041 0 0 0 0 G 0.197 0.321 1.51 0.012 0.008 0.0041 0.038 0 0 0 0 H 0.206 0.465 1.52 0.051 0.001 0.0035 0.032 0.32 0.05 0 0 I 0.214 0.512 2.05 0.008 0.002 0.0035 0.041 0 0 0.03 0 J 0.216 0.785 1.62 0.007 0.009 0.0014 0.045 0 0.00 0 0 K 0.222 0.412 1.74 0.006 0.008 0.0026 0.034 0 0 0 0 L 0.227 0.624 2.11 0.012 0.006 0.0015 0.012 0 0.21 0 0.05 M 0.231 0.325 1.58 0.011 0.005 0.0032 0.025 0 0 0 0 N 0.236 0.265 2.61 0.009 0.008 0.0035 0.041 0 0.31 0 0 O 0.241 0.955 1.74 0.007 0.007 0.0041 0.037 0 0.25 0 0 P 0.245 0.210 2.45 0.005 0.008 0.0022 0.012 0.42 0 0 0 Q 0.251 0.325 1.84 0.011 0.003 0.0041 0.035 0 0.11 0 0 R 0.256 0.120 2.06 0.008 0.004 0.0047 0.035 0 0 0 0 S 0.264 0.562 1.86 0.013 0.007 0.0034 0.015 0 0.12 0 0 T 0.271 0.150 2.01 0.018 0.003 0.0031 0.031 0 0.21 0 0.03 U 0.278 0.115 2.41 0.011 0.003 0.0060 0.021 0 0.31 0 0 W 0.281 0.562 2.03 0.012 0.007 0.0012 0.036 0 0 0 0 X 0.289 0.921 1.54 0.013 0.003 0.0087 0.026 0.15 0.11 0 0.05 Y 0.293 0.150 2.44 0.009 0.007 0.0074 0.034 0.32 0 0 0 Z 0.298 0.352 2.00 0.008 0.004 0.0069 0.035 0 0.15 0.05 0 AA 0.175 0.210 1.85 0.010 0.005 0.0025 0.025 0 0 0 0 AB 0.185 0.210 1.84 0.011 0.005 0.0032 0.032 0 0 0 0 AC 0.192 0.150 1.95 0.008 0.003 0.0035 0.035 0 0 0 0 AD 0.175 0.325 1.95 0.008 0.004 0.0034 0.031 0 0.15 0 0 AE 0.187 0.256 1.99 0.008 0.002 0.0030 0.031 0 0 0 0 AF 0.192 0.263 1.85 0.008 0.002 0.0030 0.031 0 0 0 0 AG 0.154 0.526 1.85 0.007 0.003 0.0034 0.030 0 0 0 0 AH 0.120 0.320 1.65 0.007 0.003 0.0035 0.035 0 0 0 0 AI 0.321 0.489 2.04 0.003 0.006 0.0009 0.041 0 0 0 0 AJ 0.174 0.005 2.22 0.007 0.009 0.0035 0.035 0 0.15 0 0 AK 0.189 1.151 1.50 0.008 0.005 0.0034 0.026 0.280 0.32 0 0 AL 0.210 0.660 1.21 0.009 0.003 0.0032 0.029 0 0 0 0 AM 0.254 0.050 2.91 0.007 0.004 0.0034 0.036 0 0 0 0 AN 0.263 0.321 2.05 0.091 0.003 0.0021 0.034 0.256 0.15 0 0 AO 0.275 0.154 2.50 0.002 0.025 0.0059 0.034 0 0 0 0 AP 0.245 0.256 1.52 0.011 0.009 0.0145 0.026 0 0 0 0 AQ 0.174 0.012 2.25 0.006 0.004 0.0058 0.003 0 0.20 0 0 AR 0.281 0.150 2.35 0.005 0.003 0.0035 0.074 0 0.22 0 0 AS 0.291 0.020 1.54 0.007 0.003 0.0032 0.031 0 0 0 0 AT 0.294 0.315 1.95 0.005 0.003 0.0020 0.025 0 0 0 0 AU 0.274 0.220 1.84 0.005 0.003 0.0020 0.025 0 0 0 0.01 AV 0.277 0.201 1.61 0.018 0.003 0.0031 0.031 0 0 0 0.01 Steel Type Reference Expres- symbol Nb Ni Cu Ca B REM sion a Note A 0 0 0 0 0 0 18 Invention components B 0 0.3 0 0 0 0 18 Invention components C 0 0 0 0 0 0 41 Invention components D 0 0 0 0 0 0 19 Invention components E 0 0 0 0 0 0 17 Invention components F 0 0 0.4 0.004 0 0 16 Invention components G 0 0 0 0 0 0 16 Invention components H 0 0 0 0.003 0 0 19 Invention components I 0 0 0 0 0 0 22 Invention components J 0 0 0 0 0.0008 0 26 Invention components K 0 0 0 0 0 0 18 Invention components L 0 0 0 0 0 0 24 Invention components M 0 0 0 0 0 0 14 Invention components N 0 0 0 0 0.0012 0 17 Invention components O 0 0 0 0 0 0 28 Invention components P 0 0 0 0 0 0 15 Invention components Q 0.01 0 0 0 0.0010 0 14 Invention components R 0.03 0 0 0 0 0 11 Invention components S 0 0 0 0 0 0 18 Invention components T 0 0 0 0 0 0 10 Invention components U 0 0 0 0 0.0008 0 11 Invention components W 0 0 0 0.002 0 0 17 Invention components X 0 0 0 0 0.0014 0.0005 22 Invention components Y 0 0 0 0 0.0015 0 11 Invention components Z 0 0 0 0 0 0 13 Invention components AA 0 0 0 0 0 0 17 Invention components AB 0 0 0 0 0.0008 0 16 Invention components AC 0 0 0 0 0.0011 0 14 Invention components AD 0 0 0 0 0 0 20 Invention components AE 0.01 0 0 0 0.0015 0 17 Invention components AF 0 0 0 0 0 0 16 Invention components AG 0 0 0 0 0 0 29 Invention components AH 0 0 0 0 0 0.0006 27 Comparative components AI 0 0 0 0 0 0 14 Comparative components AJ 0 0 0 0 0.0012 0 13 Comparative components AK 0 0 0 0 0.0015 0 38 Comparative components AL 0 0 0 0 0.0000 0 21 Comparative components AM 0 0 0 0 0 0 12 Comparative components AN 0.03 0 0 0 0 0 14 Comparative components AO 0 0.2 0 0 0 0 12 Comparative components AP 0.02 0 0 0.003 0 0 11 Comparative components AQ 0 0 0 0 0 0 13 Comparative components AR 0 0 0 0 0 0 11 Comparative components AS 0 0 0 0 0.001 0  6 Comparative components AT 0.01 0 0 0 0 0 12 Invention components AU 0 0 0 0 0 0 11 Invention components AV 0 0 0 0 0 0  9 Comparative components

(88) TABLE-US-00002 TABLE 2 Heating Heating furnace Right Test furnace in-furnace side of Left side of Left side of Right side of reference temperature time expression expression expression CT expression symbol (° C.) (minutes) (g) Determination (e) Determination (f) (° C.) (f) Determination 1 1200 121 1616 G 1.4 G 308 550 608 G 2 1111 39 1371 B 1.2 G 340 615 642 G 3 1285 205 1502 G 1.1 G 288 555 586 G 4 1156 124 1800 G 1.4 G 318 495 595 G 5 1222 136 1733 G 1.4 G 298 574 595 G 6 1232 127 1887 G 1.2 G 316 631 625 B 7 1256 111 2048 G 1.3 G 331 623 641 G 8 1256 106 1921 G 1.2 G 318 601 611 G 9 1250 205 1665 G 1.6 G 278 554 590 G 10 1206 87 1522 G 1.4 G 313 440 626 G 11 1214 152 1810 G 1.1 G 301 627 615 B 12 1233 182 1524 G 1.2 5 261 550 563 G 13 1198 132 1943 G 1.3 G 310 457 627 G 14 1287 252 1513 G 1.2 G 209 389 508 G 15 1105 201 1498 B 1.5 G 287 541 590 G 16 1285 222 1587 G 1.7 G 217 487 515 G 17 1156 135 1642 G 1.9 G 276 501 589 G 18 1200 185 1730 G 1.6 G 256 244 577 B 19 1232 122 1589 G 1.3 G 269 520 584 G 20 1256 152 1769 G 1.1 G 250 512 561 G 21 1256 155 1506 G 1.2 G 209 489 515 G 22 1250 145 1550 G 1.3 G 246 501 572 G 23 1150 138 1600 G 1.2 G 283 253 596 B 24 1260 182 1526 G 1.4 G 197 485 510 G 25 1146 114 1447 B 1.5 G 236 504 558 G 26 1200 132 1746 G 0.7 B 311 602 616 G 27 1194 71 1525 G 0.8 B 307 514 614 G 28 1163 96 1532 G 0.6 B 293 506 603 G 29 1200 145 1641 G 0.8 B 299 451 595 G 30 1155 152 1595 G 0.9 B 292 554 600 G 31 1187 75 1504 G 0.7 B 302 521 612 G 32 1215 152 1663 G 0.8 B 321 555 622 G 33 1241 132 1939 G 1.2 G 355 511 649 G 34 1250 178 1637 G 1.1 G 224 545 560 G 35 1205 111 1502 G 1.2 G 275 520 571 G 36 1156 127 1513 G 1.2 G 323 510 599 G 37 1109 45 1554 G 1.2 G 352 602 664 G 38 1295 336 1508 G 1.3 G 178 485 500 G 39 1212 124 1535 G 1.2 G 243 540 544 G 40 1297 164 1504 G 1.3 G 202 501 521 G 41 1312 132 2256 G 1.1 G 307 582 627 G 42 1241 162 1645 G 1.1 G 271 389 565 G 43 1254 222 1634 G 1.5 G 211 471 525 G 45 1278 205 2579 G 1.4 G 283 600 613 G 46 1199 210 1766 G 1.3 G 245 502 575 G 47 1185 202 1879 G 1.6 G 265 552 590 G 48 1194 202 2157 G 1.6 G 284 502 610 G

(89) TABLE-US-00003 TABLE 3 After annealing and temper rolling and before hot stamping Pearlite Annealing (cold rolled steel sheet for hot stamping) area condition Mar- Ferrite + Retained fraction Test Annealing Ferrite tensite martensite austenite Bainite Pearlite before Steel type refer- temper- TS × λ area area area area area area cold reference ence ature TS EL λ TS × EL (MPa .Math. fraction fraction fraction fraction fraction fraction rolling symbol symbol (° C.) (MPa) (%) (%) (MPa .Math. %) %) (%) (%) (%) (%) (%) (%) (%) A 1 774 584 32.5 111 18980 64824 88 11 99 1 0 0 31 B 2 778 578 28.5 100 16473 57800 74 15 89 3 4 4 25 C 3 784 524 30.5 99 15982 51876 75 12 87 4 5 4 32 D 4 825 562 33.2 95 18658 53390 77 12 89 3 8 0 24 E 5 815 591 29.8 90 17612 53190 70 15 85 4 11 0 51 F 6 780 622 27.4 81 17043 50382 58 10 68 3 20 9 62 G 7 841 603 31.2 83 18814 50049 74 12 86 2 6 6 48 H 8 784 612 30.5 85 18666 52020 70 15 85 3 8 4 35 I 9 778 614 28.1 82 17253 50348 75 12 87 4 5 4 71 J 10 825 665 30.5 76 20283 50540 76 12 88 3 7 2 25 K 11 841 709 23.1 71 16378 50339 61 10 71 4 17 8 35 L 12 815 705 25.6 72 18048 50760 79 12 91 2 5 2 15 M 13 805 712 24.2 80 17230 56960 66 26 92 3 5 0 10 N 14 789 755 28.6 81 21593 61155 50 34 84 2 5 9 42 O 15 785 762 29.8 74 22708 56388 72 19 91 3 6 0 9 P 16 785 748 25.5 68 19074 50864 59 28 87 3 1 9 25 Q 17 841 780 20.1 71 15678 55380 78 18 96 0 4 0 31 R 18 845 783 20.1 65 15738 50895 41 44 85 4 5 6 51 S 19 789 805 20.4 74 16422 59570 42 38 80 4 10 6 46 T 20 785 789 22.2 71 17516 56019 44 40 84 3 12 1 18 U 21 805 845 20.2 62 17069 52390 41 38 79 5 12 4 22 W 22 778 922 17.4 61 16043 56242 41 39 80 4 12 4 15 X 23 804 988 15.5 51 15314 50388 42 46 88 2 4 6 45 Y 24 820 1012 17.4 51 17609 51612 45 37 82 2 16 0 42 Z 25 836 1252 13.5 45 16902 56340 41 48 89 2 9 0 10

(90) TABLE-US-00004 TABLE 4 After annealing and temper rolling and before hot stamping Pearlite Annealing (cold rolled steel sheet for hot stamping) area condition Mar- Ferrite + Retained fraction Test Annealing Ferrite tensite martensite austenite Bainite Pearlite before Steel type refer- temper- TS × λ area area area area area area cold reference ence ature TS EL λ TS × EL (MPa .Math. fraction fraction fraction fraction fraction fraction rolling symbol symbol (° C.) (MPa) (%) (%) (MPa .Math. %) %) (%) (%) (%) (%) (%) (%) (%) AA 26 804 577 27.2 77 15694 44429 59 10 69 2 12 17 35 AB 27 775 601 26.8 69 16107 41469 64 15 79 0 6 15 32 AC 28 754 513 28.9 74 14826 37962 62 12 74 2 5 19 25 AD 29 778 588 23.1 72 13583 42336 36 15 51 1 45 3 5 AE 30 780 595 27.9 69 16601 41055 73 10 83 2 3 12 66 AF 31 805 616 28.5 64 17556 39424 70 9 79 2 10 9 22 AG 32 812 632 28.6 52 18075 32864 58 20 78 2 9 11 25 AH 33 768 326 41.9 112 13659 36512 95 0 95 3 2 0 2 AI 34 781 1512 8.9 25 13457 37800 5 90 95 4 1 0 3 AJ 35 805 635 22.5 72 14288 45720 74 22 96 2 2 0 42 AK 36 789 625 31.2 55 19500 34375 75 22 97 2 1 0 15 AL 37 784 705 26.0 48 18330 33840 42 25 67 1 25 7 2 AM 38 841 795 15.6 36 12402 28620 30 52 82 3 10 5 14 AN 39 845 784 19.1 42 14974 32928 51 37 88 3 9 0 16 AO 40 826 602 30.5 35 18361 21070 68 21 89 4 7 0 22 AP 41 807 586 27.4 66 16056 38676 69 21 90 4 6 0 32 AQ 42 845 1254 7.5 25 9405 31350 11 68 79 4 11 6 22 AR 43 775 1480 9.6 26 14208 38480 12 69 81 3 16 0 5 AS 45 845 1152 12.0 42 13824 48384 41 35 76 0 23 1 5 AT 46 684 852 16.0 52 13632 44304 80 0 80 1 2 17 5 AU 47 912 1355 6.0 33 8130 44715 5 50 55 1 40 4 5 AV 48 805 1355 6.0 33 8130 44715 41 48 89 1 10 0 5

(91) TABLE-US-00005 TABLE 5 Hot After hot stamping(hot stamped steel) stamping Re- Test condition tained Pearl- ref- Thermal Mar- Ferrite + aus- ite er- treatment TS × Ferrite tensite martensite tenite Bainite area ence temper- EL TS × λ area area area area area frac- sym- ature TS EL λ (MPa .Math. (MPa .Math. fraction fraction fraction fraction fraction tion Plating bol (° C.) (MPa) (%) (%) %) %) (%) (%) (%) (%) (%) (%) type *) Note 1 871 1512 8.5 41 12852 61992 10 82 92 1 7 0 CR Invention example 2 861 1514 7.6 38 11506 57532 12 84 96 0 4 0 GA Invention example 3 825 1612 8.1 37 13057 59644 8 81 89 1 5 5 GI Invention example 4 816 1658 7.4 40 12269 66320 11 86 97 3 0 0 EG Invention example 5 901 1689 8.4 36 14188 60804 9 84 93 1 0 6 AI Invention example 6 778 1745 8.2 37 14309 64565 10 82 92 3 5 0 CR Invention example 7 885 1784 7.6 38 13558 67792 5 81 86 0 6 8 CR Invention example 8 925 1795 9.2 40 16514 71800 0 89 89 3 8 0 GA Invention example 9 955 1812 8.6 35 15583 63420 0 94 94 0 6 0 GA Invention example 10 875 1815 9.1 34 16517 61710 0 100 100 0 0 0 GA Invention example 11 851 1823 8.4 31 15313 56513 0 100 100 0 0 0 GA Invention example 12 864 1855 8.2 36 15211 66780 0 97 97 2 0 1 GI Invention example 13 865 1894 7.6 37 14394 70078 0 100 100 0 0 0 GA Invention example 14 897 1912 9.2 35 17590 66920 5 90 95 0 5 0 GA Invention example 15 880 1894 8.6 36 16288 68184 0 100 100 0 0 0 GI Invention example 16 888 1912 8.4 37 16061 70744 0 94 94 0 6 0 GA Invention example 17 955 1925 8.2 38 15785 73150 3 92 95 3 2 0 GA Invention example 18 856 1945 7.6 40 14782 77800 0 100 100 0 0 0 CR Invention example 19 841 1962 9.2 35 18050 68670 0 94 94 0 0 6 GA Invention example 20 874 2012 8.6 34 17303 68408 0 100 100 0 0 0 GI Invention example 21 884 2015 9.1 31 18337 62465 4 95 99 0 0 1 EG Invention example 22 908 2025 7.8 36 15795 72900 0 100 100 0 0 0 GA Invention example 23 925 2035 8.6 37 17501 75295 10 90 100 0 0 0 AI Invention example 24 901 2145 8.7 35 18662 75075 0 87 87 1 10 2 GA Invention example 25 865 2215 8.2 40 18163 88600 0 100 100 0 0 0 CR Invention example

(92) TABLE-US-00006 TABLE 6 Hot After hot stamping(hot stamped steel) stamping Fer- Re- Test condition rite + tained Pearl- ref- Thermal Mar- mar- aus- ite er- treatment TS × Ferrite tensite tensite tenite Bainite area ence temper- EL TS × λ area area area area area frac- sym- ature TS EL λ (MPa .Math. (MPa .Math. fraction fraction fraction fraction fraction tion Plating bol (° C.) (MPa) (%) (%) %) %) (%) (%) (%) (%) (%) (%) type *) Note 26 849 1754 20.1 26 35255 45604 8 77 85 0 5 10  GA Comparative example 27 878 1792 16.1 26 28851 46592 5 74 79 0 12  9 CR Comparative example 28 865 1817 15.4 26 27982 47242 3 81 84 0 3 13  GA Comparative example 29 825 1823 16.5 27 30080 49221 8 76 84 3 11  2 EG Comparative example 30 869 1988 14.9 25 29621 49700 6 78 84 0 7 9 GI Comparative example 31 848 1965 13.6 25 26724 49125 8 77 85 0 11 4 AI Comparative example 32 876 1512 18.5 25 27972 37800 7 74 81 4 7 8 CR Comparative example 33 835 1524 42.5 24 64770 36576 32  52 84 10  2 4 GA Comparative example 34 895 2012 8.5 21 17102 42252 30  62 92 4 1 3 GA Comparative example 35 888 1812 18.5 26 33522 47112 5 85 90 2 5 3 GA Comparative example 36 846 1842 17.2 20 31682 36840 0 95 95 2 3 0 GA Comparative example 37 805 1785 16.5 25 29453 44625 7 78 85 3 10  2 GI Comparative example 38 863 1812 15.0 26 27180 47112 3 92 95 3 2 0 GI Comparative example 39 878 1845 18.2 24 33579 44280 0 100  100  0 0 0 GI Comparative example 40 899 2012 17.0 21 34204 42252 0 95 95 0 0 5 GI Comparative example 41 905 1744 31.0 22 54064 38368 0 100  100  0 0 0 EG Comparative example 42 923 2012 11.1 21 22333 42252 11  68 79 4 11  6 AI Comparative example 43 907 2022 10.2 21 20624 42462 12  69 81 3 16  0 GA Comparative example 45 845 2014 10.0 20 20140 40280 4 78 82 3 13  2 GA Comparative example 46 879 2033 13.0 21 26429 42693 4 72 76 0 22  2 GA Comparative example 47 886 2122 9.0 20 19098 42440 19  55 74 3 14  9 GA Comparative example 48 914 2066 11.0 24 22726 49584 7 86 93 0 5 2 GA Comparative example

(93) TABLE-US-00007 TABLE 7 Cold rolled Cold rolled Hot Cold rolled Hot steel sheet for steel sheet for Stamped steel sheet for Stamped hot stamping hot stamping steel hot stamping steel Area Steel Left Left Left Left fraction of type Test side of side of side of side of MnS of reference reference expression Determina- expression Determina- expression expression 0.1 μm or symbol symbol (b) tion (b) tion (c) Determination (c) Determination more (%) A 1 1.02 G 1.02 G 15 G 16 G 0.005 B 2 1.03 G 1.03 G 18 G 17 G 0.011 C 3 1.04 G 1.04 G 12 G 10 G 0.005 D 4 1.01 G 1.01 G 14 G 18 G 0.006 E 5 1.06 G 1.06 G 11 G 14 G 0.007 F 6 1.06 G 1.06 G 10 G 10 G 0.008 G 7 1.06 G 1.06 G 11 G 10 G 0.004 H 8 1.03 G 1.03 G 16 G 17 G 0.008 I 9 1.07 G 1.07 G 18 G 16 G 0.006 J 10 1.08 G 1.08 G 10 G 11 G 0.007 K 11 1.09 G 1.09 G 6 G 6 G 0.006 L 12 1.08 G 1.08 G 6 G 8 G 0.008 M 13 1.06 G 1.06 G 8 G 7 G 0.009 N 14 1.07 G 1.07 G 13 G 14 G 0.003 O 15 1.06 G 1.06 G 3 G 5 G 0.011 P 16 1.08 G 1.08 G 18 G 17 G 0.007 Q 17 1.06 G 1.06 G 14 G 13 G 0.006 R 18 1.04 G 1.04 G 13 G 13 G 0.008 S 19 1.02 G 1.02 G 9 G 8 G 0.003 T 20 1.03 G 1.03 G 8 G 8 G 0.008 U 21 1.03 G 1.03 G 8 G 6 G 0.005 W 22 1.05 G 1.05 G 11 G 10 G 0.006 X 23 1.07 G 1.07 G 16 G 16 G 0.007 Y 24 1.06 G 1.06 G 16 G 17 G 0.006 Z 25 1.04 G 1.04 G 15 G 17 G 0.012 Hot Stamped Cold rolled Hot steel steel sheet for Stamped Area hot stamping steel Steel fraction of Left Left type Test MnS of side of side of reference reference 0.1 μm or expression expression symbol symbol more (%) n1 n2 (d) Determination n1 n2 (d) Determination A 1 0.005 10 12 1.2 G 9 12 1.3 G B 2 0.011 7 12 1.7 B 8 12 1.5 B C 3 0.007 5 7 1.4 G 5 6 1.2 G D 4 0.006 9 11 1.2 G 9 10 1.1 G E 5 0.008 17 18 1.1 G 18 19 1.1 G F 6 0.003 14 16 1.1 G 12 15 1.3 G G 7 0.008 7 10 1.4 G 7 10 1.4 G H 8 0.005 9 10 1.1 G 9 10 1.1 G I 9 0.006 19 20 1.1 G 20 21 1.1 G J 10 0.007 26 29 1.1 G 25 26 1.0 G K 11 0.006 7 8 1.1 G 7 8 1.1 G L 12 0.008 5 6 1.2 G 5 6 1.2 G M 13 0.008 12 15 1.3 G 11 15 1.4 G N 14 0.003 6 8 1.3 G 6 8 1.3 G O 15 0.011 2 3 1.5 B 2 3 1.5 B P 16 0.005 4 5 1.3 G 4 5 1.3 G Q 17 0.006 7 9 1.3 G 7 9 1.3 G R 18 0.007 16 18 1.1 G 15 18 1.2 G S 19 0.008 10 12 1.2 G 10 12 1.2 G T 20 0.004 6 7 1.2 G 6 7 1.2 G U 21 0.008 8 10 1.3 G 7 9 1.3 G W 22 0.006 16 20 1.3 G 15 20 1.3 G X 23 0.007 23 26 1.1 G 22 25 1.1 G Y 24 0.005 22 28 1.3 G 20 28 1.4 G Z 25 0.012 20 31 1.6 B 22 32 1.5 B

(94) TABLE-US-00008 TABLE 8 Cold rolled Cold rolled Hot Cold rolled Hot steel sheet for steel sheet for Stamped steel sheet for Stamped hot stamping hot stamping steel hot stamping steel Area Steel Left Left Left Left fraction of type Test side of side of side of side of MnS of reference reference expression Determina- expression Determina- expression expression 0.1 μm or symbol symbol (b) tion (b) tion (c) Determination (c) Determination more (%) AA 26 1.18 B 1.18 B 22 B 23 B 0.009 AB 27 1.15 B 1.15 B 21 B 19 G 0.008 AC 28 1.2  B 1.19 B 24 B 22 B 0.006 AD 29 1.14 B 1.13 B 22 B 25 B 0.007 AE 30 1.11 B 1.12 B 20 B 18 G 0.009 AF 31 1.12 B 1.14 B 22 B 21 B 0.002 AG 32 1.13 B 1.13 B 23 B 22 B 0.003 AH 33 1.16 B 1.16 B 21 B 21 B 0.004 AI 34 1.23 B 1.18 B 25 B 25 B 0.006 AJ 35 1.21 B 1.21 B 24 B 24 B 0.007 AK 36 1.16 B 1.15 B 21 B 21 B 0.006 AL 37 1.35 B 1.37 B 31 B 30 B 0.006 AM 38 1.32 B 1.32 B 30 B 31 B 0.006 AN 39 1.23 B 1.25 B 25 B 28 B 0.008 AO 40 1.34 B 1.33 B 30 B 32 B 0.004 AP 41 1.05 G 1.04 G 12 G 11 G 0.002 AQ 42 1.04 G 1.05 G 18 G 15 G 0.003 AR 43 1.13 B 1.14 B 26 B 26 B 0.002 AS 45 1.11 B 1.15 B 26 B 25 B 0.007 AT 46 1.25 B 1.27 B 26 B 27 B 0.004 AU 47 1.05 G 1.06 G 17 G 16 G 0.003 AV 48 1.12 B 1.13 B 21 B 23 B 0.005 Hot Stamped Cold rolled Hot steel steel sheet for Stamped Area hot stamping steel Steel fraction of Left Left type Test MnS of side of side of reference reference 0.1 μm or expression expression symbol symbol more (%) n1 n2 (d) Determination n1 n2 (d) Determination AA 26 0.009 13 15 1.2 G 12 15 1.3 G AB 27 0.008 7 10 1.4 G 8 11 1.4 G AC 28 0.006 14 19 1.4 G 13 18 1.4 G AD 29 0.007 6 7 1.2 G 6 7 1.2 G AE 30 0.009 12 15 1.3 G 12 15 1.3 G AF 31 0.002 18 23 1.3 G 17 22 1.3 G AG 32 0.003 6 7 1.2 G 6 7 1.2 G AH 33 0.004 4 5 1.3 G 4 5 1.3 G AI 34 0.006 12 14 1.2 G 12 13 1.1 G AJ 35 0.007 15 17 1.1 G 15 17 1.1 G AK 36 0.007 11 12 1.1 G 11 12 1.1 G AL 37 0.006 12 17 1.4 G 12 17 1.4 G AM 38 0.006 15 21 1.4 G 16 21 1.3 G AN 39 0.008 10 12 1.2 G 10 11 1.1 G AO 40 0.004 8 11 1.4 G 8 11 1.4 G AP 41 0.006 6 8 1.3 G 6 8 1.3 G AQ 42 0.003 12 15 1.3 G 12 15 1.3 G AR 43 0.002 23 26 1.1 G 23 25 1.1 G AS 45 0.007 16 18 1.1 G 15 18 1.2 G AT 46 0.005 17 19 1.1 G 16 17 1.1 G AU 47 0.003 18 20 1.1 G 16 18 1.1 G AV 48 0.005 18 19 1.1 G 17 18 1.1 G

(95) It is found from Tables 1 to 8 that, when the conditions of the present invention are satisfied, it is possible to obtain the hot stamped steel for which the high-strength cold rolled steel sheet satisfying TS×λ≧50000 MPa.Math.% is used.

INDUSTRIAL APPLICABILITY

(96) According to the present invention, since an appropriate relationship is established among the amount of the C, the amount of the Mn and the amount of the Si, and an appropriate hardness measured with a nanoindenter is provided to the martensite, it is possible to provide the hot stamped steel which ensures the strength of 1.5 GPa or more, and has a more favorable hole expansibility.

BRIEF DESCRIPTION OF THE REFERENCE SYMBOLS

(97) S1: MELTING PROCESS

(98) S2: CASTING PROCESS

(99) S3: HEATING PROCESS

(100) S4: HOT-ROLLING PROCESS

(101) S5: COILING PROCESS

(102) S6: PICKLING PROCESS

(103) S7: COLD-ROLLING PROCESS

(104) S8: ANNEALING PROCESS

(105) S9: TEMPER-ROLLING PROCESS

(106) S10: HOT STAMPING PROCESS

(107) S11: GALVANIZING PROCESS

(108) S12: ALLOYING PROCESS

(109) S13: ALUMINIZING PROCESS

(110) S14: ELECTROGALVANIZING PROCESS