HOT STAMPED BODY

Abstract
There is provided a hot stamped body including a middle part in sheet thickness and a surface layer arranged at both sides or one side of the middle part in sheet thickness, further including an intermediate layer formed between the middle part in sheet thickness and each surface layer so as to adjoin them, wherein the middle part in sheet thickness has a predetermined composition, the middle part in sheet thickness has a hardness of 500 Hv or more and 800 Hv or less, the surface layer has a hardness change ΔH1 in the sheet thickness direction of 10 Hv or more and less than 200 Hv, and the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 50 Hv or more and less than 200 Hv.
Description
FIELD

The present invention relates to high strength steel sheet used for structural members or reinforcing members of automobiles or structures where strength is required, in particular a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance.


BACKGROUND

In recent years, from the viewpoints of environmental protection and resource saving, lighter weight of automobile bodies is being sought. For this reason, application of high strength steel sheet to automobile members has been accelerating. However, along with the increase in strength of steel sheets, the formability deteriorates, and therefore in high strength steel sheets, formability into members with complicated shapes is a problem.


To solve this problem, hot stamping, where the steel sheet is heated to a high temperature of the austenite region, then press formed, is increasingly being applied. Since hot stamping performs press forming and simultaneously quenching in the die, it is possible to obtain a strength corresponding to the C amount of the steel sheet. This is being taken note of as a technique achieving both formation of a material into an automobile member and securing strength.


However, since in conventional hot pressed parts which were produced by press quenching, the entire sheet thickness is formed by hard structures (mainly martensite), if bending deformation occurs at the time of collision of the automobile, the largest strain will be applied to the bent portion of the part, cracks will advance starting from the vicinity of the surface layer of the steel sheet, and finally fracture will easily be caused. Further, since the density of lattice defects at the surface layer of the steel sheet is high, there is the problem that penetration by hydrogen is promoted and the member becomes poor in hydrogen embrittlement resistance. Due to this reason, hot pressed parts produced by press quenching have been limited in locations of auto parts applied to.


To deal with this problem, art has been proposed for raising the deformability of hot pressed parts to suppress cracking. PTL 1 discloses making the hardness of the middle in sheet thickness of a hot pressed part 400 Hv or more and forming a soft layer with a thickness of 20 μm to 200 μm and a hardness of 300 Hv or less on a surface layer so as to secure a strength of a tensile strength of 1300 MPa or more while suppressing cracking at the time of automobile collision. Furthermore, PTL 1 discloses that the above soft layer has a tempered structure.


PTL 2 discloses controlling the concentration of carbon at a surface layer of a high strength automobile member to ⅕ or less of the concentration of carbon of the inner layer steel so as to reduce the density of lattice defects of the surface layer and improve the hydrogen embrittlement resistance.


PTL 3 discloses to make the steel structure a dual phase structure of ferrite and martensite and raise the area rate of ferrite of a surface layer portion compared with an inner layer portion so as to obtain a hot pressed steel sheet member having high tensile strength and excellent ductility and bendability.


However, in the members described in PTLs 1 and 2, by making a surface layer portion in sheet thickness by soft structures and making a middle part in sheet thickness by hard structures, a sharp gradient in hardness ends up being formed in the sheet thickness direction. For this reason, when subjected to bending deformation, there is the issue that cracking easily occurs near the boundary between the soft structures and hard structures where this sharp gradient of hardness occurs. Further, in the member described in PTL 3, a surface layer portion in sheet thickness is made by soft structures and the middle part in sheet thickness is made a dual phase structure of hard structures and soft structures so as to reduce the sharp gradient in hardness in the sheet thickness direction. However, since making the middle part in sheet thickness a dual phase structure, the upper limit of tensile strength ends up becoming 1300 MPa or so. It is difficult to secure the tensile strength of 1500 MPa or more sought for hot pressed parts.


CITATION LIST
Patent Literature
[PTL 1] Japanese Unexamined Patent Publication No. 2015-30890
[PTL 2] Japanese Unexamined Patent Publication No. 2006-104546
[PTL 3] WO 2015/097882
SUMMARY
Technical Problem

In consideration of the technical issues in the prior art, an object of the present invention is to provide a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance.


Solution to Problem

The inventors engaged in an in-depth study of a method for solving the above technical issues. First, to improve the hydrogen embrittlement resistance, it is effective to reduce the density of lattice defects at the surface layer of sheet thickness. For this reason, it is necessary to form soft structures at the surface layer. On the other hand, to secure a 1500 MPa or more tensile strength, it is necessary to form the middle part in sheet thickness by only hard structures. Therefore, the inventors thought that if forming the surface layer of sheet thickness by soft structures and forming the middle part in sheet thickness by hard structures, if it were possible to reduce the rapid gradient of hardness in the sheet thickness direction occurring near the boundary of the hard structures and soft structures, a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance could be ensured while excellent bendability could be obtained. Specifically, they caused the formation of structures (intermediate layer) having hardnesses between the hard structures and soft structures at the boundary of the same so as to reduce the gradient of hardness in the sheet thickness direction and ease the concentration of stress at the time of bending deformation. As a result, they were able to suppress the occurrence of cracking at the time of bending deformation and able to secure a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance while obtaining excellent bendability and thereby were able to obtain hot stamped bodies excellent in impact resistance and hydrogen embrittlement resistance.


Further, the inventors discovered that by controlling the addition amount of Mn at the middle part in sheet thickness to a relatively high value, more specifically to 1.50% to less than 3.00%, it is possible to raise the hardenability and reduce the variation in hardness at the stamped body, i.e., to stably secure a high strength. As a result, it was possible to secure a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance while obtaining a hot stamped body excellent in impact resistance from the viewpoint of not only bendability, but also strength stability (variation in hardness).


Furthermore, the inventors discovered that by controlling the addition amount of Si at the middle part in sheet thickness to a relatively high value, more specifically to more than 0.50% and less than 3.00% to secure structures contributing to improvement of deformability, it is possible to raise the ductility. As a result, they were able to secure a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance while obtaining a hot stamped body excellent in impact resistance from the viewpoint of not only bendability, but also ductility.


In addition, the inventors discovered that by controlling the addition amounts of Mn and Si in the middle part in sheet thickness to relatively high values, more specifically respectively to 1.50% or more and less than 3.00% and to more than 0.50% and less than 3.00%, it is possible to improve the ductility and raise the hardenability to reduce the variation in hardness at the stamped body, i.e., to stably secure a high strength. As a result, they were able to obtain a hot stamped body securing a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance while being excellent in impact resistance from the viewpoint of not only bendability, but also of strength stability (variation of hardness) and ductility.


The present invention was completed based on the above discovery and has as its gist the following:


(1) A hot stamped body comprising a middle part in sheet thickness and a surface layer arranged at both sides or one side of the middle part in sheet thickness, wherein


the hot stamped body further comprises an intermediate layer formed between the middle part in sheet thickness and each surface layer so as to adjoin them,


the middle part in sheet thickness comprises, by mass %,


C: 0.20% or more and less than 0.70%


Si: less than 3.00%,


Mn: 0.20% or more and less than 3.00%,


P: 0.10% or less,


S: 0.10% or less,


sol. Al: 0.0002% or more and 3.0000% or less,


N: 0.01% or less, and


a balance of Fe and unavoidable impurities,


the middle part in sheet thickness has a hardness of 500 Hv or more and 800 Hv or less,


the surface layer has a hardness change ΔH1 in the sheet thickness direction of 10 Hv or more and less than 200 Hv, and


the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 50 Hv or more and less than 200 Hv.


(2) The hot stamped body according to the above (1), wherein the Si content of the middle part in sheet thickness is 0.50% or less and the Mn content of the middle part in sheet thickness is 0.20% or more and less than 1.50%.


(3) The hot stamped body according to the above (1), wherein the Si content of the middle part in sheet thickness is 0.50% or less and the Mn content of the middle part in sheet thickness is 1.50% or more and less than 3.00%.


(4) The hot stamped body according to the above (1), wherein the Si content of the middle part in sheet thickness is more than 0.50% and less than 3.00%, the Mn content of the middle part in sheet thickness is 0.20% or more and less than 1.50%, and the middle part in sheet thickness comprises, by area percent, 1.0% or more and less than 5.0% of residual austenite.


(5) The hot stamped body according to the above (1), wherein the Si content of the middle part in sheet thickness is more than 0.50% and less than 3.00%, the Mn content of the middle part in sheet thickness is 1.50% or more and less than 3.00%, and the middle part in sheet thickness comprises, by area percent, 1.0% or more and less than 5.0% of residual austenite.


(6) The hot stamped body according to any one of the above (1) to (5), wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.


(7) The hot stamped body according to any one of the above (1) to (6), wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.


(8) The hot stamped body according to any one of the above (1) to (7), further comprising a plated layer at the surface of the each surface layer.


Advantageous Effects of Invention

According to the present invention, it is possible to realize excellent bendability and possible to provide a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance. Further, according to the present invention, by controlling the addition amount of Mn at the middle part in sheet thickness to a relatively high value, it is possible to further improve the impact resistance from the viewpoint of not only bendability, but also strength stability (variation of hardness). Furthermore, according to the present invention, by controlling the addition amount of Si at the middle part in sheet thickness to a relatively high value, it is possible to further improve the impact resistance from the viewpoint of not only bendability, but also ductility. In addition, according to the present invention, by controlling the addition amounts of Mn and Si at the middle part in sheet thickness to relatively high values, it is possible to further improve the impact resistance from the viewpoints of not only bendability, but also of strength stability (variation of hardness) and ductility.





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1 is a schematic view for explaining the diffusion of C atoms when producing the high strength steel sheet of the present invention.



FIG. 2 is a graph showing the change in dislocation density after a rolling pass relating to rough rolling used in the method for producing the high strength steel sheet of the present invention.





DESCRIPTION OF EMBODIMENTS

Below, a hot stamped body of the present invention and a method for producing the same will be explained.


First, the reasons for limitation of the chemical constituents of the middle part in sheet thickness forming the hot stamped body of the present invention will be explained. Below, the % relating to the chemical constituents means mass %.


“C: 0.20% or More and Less than 0.70%”


C is an important element for obtaining a 500 Hv to 800 Hv hardness at the middle part in sheet thickness. With less than 0.20%, it is difficult to secure 500 Hv or more at the middle part in sheet thickness, so C is 0.20% or more. Preferably it is 0.30% or more. On the other hand, with 0.70% or more, the hardness of the middle part in sheet thickness exceeds 800 Hv and the bendability falls, so C is less than 0.70%. Preferably, it is 0.50% or less.


“Si: Less than 3.00%”


Si is an element contributing to improvement of strength by solution strengthening, so may be added up to 0.50% as an upper limit from the viewpoint of improvement of strength. On the other hand, even if added in more than 0.50%, the effect of improvement of strength becomes saturated, so 0.50% is the upper limit. Preferably it is 0.30% or less. Si further is an element having the effect of raising the ductility without impairing the hydrogen embrittlement resistance and bendability manifested by control of the structures of the surface layer. In particular, if bending deformation occurs at the time of collision of an automobile, buckling of the hat shaped member causes the deformation to become localized and the load resistance of the member to drop. That is, the member and the maximum load affect not only the strength of the member, but also the ease of buckling. In the state of the member, if the ductility of the steel sheet is high, the deformation region becomes harder to localize. That is, the sheet becomes hard to buckle. Therefore, in a hot stamped member as well, while the ductility is important, in general the ductility of martensite is low. From such a viewpoint, by adding Si in more than 0.50%, it is possible to secure residual austenite in an area percent of 1.0% or more. To improve the ductility, Si is preferably added in more than 0.50%. More preferably, the content is 1.00% or more. On the other hand, if adding 3.00% or more, the residual austenite becomes present in an area rate of 5.0% or more and deterioration of the bendability is invited, so the upper limit is less than 3.00%. Preferably, the content is less than 2.00%.


“Mn: 0.20% or More and Less than 3.00%”


Mn is an element contributing to improvement of strength by solution strengthening. From the viewpoint of improvement of strength, with less than 0.20%, the effect is not obtained, so 0.20% or more is added. Preferably the content is 0.70% or more. On the other hand, even if adding 1.50% or more, the effect of improvement of the strength becomes saturated, so less than 1.50% is the upper limit. Mn, further, is an element having the effect of raising the hardenability without impairing the hydrogen embrittlement resistance and bendability manifested by control of the structures of the surface layer. In a hot stamped body, the way of contact with the die is not necessarily uniform. For example, at the vertical wall parts of a hat member etc., the cooling rate easily falls. For this reason, steel sheet is sometimes locally formed with regions with low hardnesses. Deformation concentrates in a local soft part at the time of collision and becomes a cause of cracking, so in securing impact resistance, it is important that the hardenability be raised and the variation in hardness in the stamped body be reduced, i.e., that stable strength be secured. From such a viewpoint, by adding Mn in 1.50% or more, it is possible to raise the hardenability and stably obtain high strength, so Mn is preferably added in 1.50% or more. More preferably, it is 1.70% or more. On the other hand, even if adding 3.00% or more, the effect of strength stability becomes saturated, so the upper limit is less than 3.00%. Preferably, the content is less than 2.00%.


“P: 0.10% or Less”

P is an element segregating at the grain boundaries and impairing the strength of the grain boundaries. If more than 0.10%, the strength of the grain boundaries remarkably falls and the hydrogen embrittlement resistance and bendability fall, so P is 0.10% or less. Preferably, it is 0.05% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0001%, the dephosphorization cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% is the substantive lower limit.


“S: 0.10% or Less”

S is an element forming inclusions. If more than 0.10%, inclusions are formed and the hydrogen embrittlement resistance and bendability fall, so S is 0.10% or less. Preferably, it is 0.005% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0015%, the desulfurization cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0015% is the substantive lower limit.


“Sol. Al: 0.0002% or More and 3.0000% or Less”


Al is an element acting to deoxidize the molten steel and make the steel sounder. With less than 0.0002%, the deoxidation is insufficient, so sol. Al is 0.0002% or more. Preferably the content is 0.0010% or more. On the other hand, even if adding more than 3.0000%, the effect becomes saturated, so the content is 3.0000% or less.


“N: 0.01% or Less”

N is an impurity element and is an element which forms nitrides and impairs bendability. If more than 0.01%, coarse nitrides are formed and the bendability remarkably falls, so N is 0.01% or less. Preferably the content is 0.0075% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0001%, the denitridation cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% is the substantive lower limit.


“Ni: 0.01% or More and 3.00% or Less”

Ni is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.01%, the effect is not obtained, so the content is 0.01% or more. Preferably, the content is 0.50% or more. On the other hand, even if added in more than 3.00%, the effect becomes saturated, so the content is 3.00% or less. Preferably, the content is 2.50% or less.


“Nb: 0.010% or More and 0.150% or Less”

Nb is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.010%, the effect is not obtained, so the content is 0.010% or more. Preferably, the content is 0.035% or more. On the other hand, even if added in more than 0.150%, the effect becomes saturated, so the content is 0.150% or less. Preferably, the content is 0.120% or less.


“Ti: 0.010% or More and 0.150% or Less”

Ti is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.010%, the effect is not obtained, so the content is 0.010% or more. Preferably, the content is 0.020% or more. On the other hand, even if added in more than 0.150%, the effect becomes saturated, so the content is 0.150% or less. Preferably, the content is 0.120% or less.


“Mo: 0.005% or More and 1.000% or Less”

Mo is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.005%, the effect is not obtained, so the content is 0.005% or more. Preferably, the content is 0.010% or more. On the other hand, even if added in more than 1.000%, the effect becomes saturated, so the content is 1.000% or less. Preferably, the content is 0.800% or less.


“B: 0.0005% or More and 0.0100% or Less”

B is an element segregating at the grain boundaries and improving the strength of the grain boundaries, so may be added as needed. With less than 0.0005%, the effect of addition is not sufficiently obtained, so 0.0005% or more is added. Preferably, the content is 0.0010% or more. On the other hand, even if added in more than 0.0100%, the effect becomes saturated, so the content is 0.0100% or less. Preferably, the content is 0.0075% or less.


The balance of the chemical constituents of the middle part in sheet thickness consists of Fe and unavoidable impurities. The unavoidable impurities are elements which unavoidably enter from the steel raw materials and/or in the steelmaking process and are allowed in ranges not impairing the characteristics of the hot stamped body of the present invention.


Next, the chemical constituents of the surface layer forming the hot stamped body of the present invention will be explained.


Regarding the constituents of the surface layer, it is preferable that one or more of the C content, Si content, and Mn content be 0.6 time or less the corresponding contents of the elements at the middle part in sheet thickness. In that case, the preferable ranges of the constituents are as follows:


“C: 0.05% or More and Less than 0.42%”


C is added to raise the strength. If less than 0.05%, the effect is not obtained, so 0.05% or more is added. From the viewpoint of raising the load resistance as a member and improving the impact characteristics, preferably the content is 0.10% or more. On the other hand, to make the hardness of a surface layer lower than the hardness of the middle part in sheet thickness, it is preferable to make the content smaller than the middle part in sheet thickness. For this reason, the preferable C content of the surface layer is less than 0.42%. Preferably the C content is 0.35% or less.


“Si: Less than 2.00%”


Si is an element contributing to improvement of strength by solution strengthening, so is added for raising the strength. To make the hardness of the surface layer lower than the hardness of the middle part in sheet thickness, it is preferable to make this smaller in content than the middle part in sheet thickness. For this reason, the preferable S content of the surface layer is less than 2.00%, preferably 1.50% or less, more preferably 0.30% or less, still more preferably 0.20% or less.


“Mn: 0.01% or More and Less than 1.80%”


Mn is an element contributing to improvement of strength by solution strengthening, so is added for raising the strength. To make the hardness of the surface layer lower than the hardness of the middle part in sheet thickness, it is preferably smaller in content than the middle part in sheet thickness. For this reason, the preferable Mn content of the surface layer is less than 1.80%, preferably 1.40% or less, more preferably less than 0.90%, still more preferably 0.70% or less.


The other constituents of the surface layer are not particularly limited. In general, a surface layer may optionally contain one or more of the following constituents in addition to C, Si, and Mn.


“P: 0.10% or Less”

P is an element segregating at the grain boundaries and impairing the strength of the grain boundaries. If more than 0.10%, the strength of the grain boundaries remarkably falls and the hydrogen embrittlement resistance and bendability fall, so P is 0.10% or less. Preferably, it is 0.05% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0001%, the dephosphorization cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% is the substantive lower limit.


“S: 0.10% or Less”

S is an element forming inclusions. If more than 0.10%, inclusions are formed and the hydrogen embrittlement resistance and bendability fall, so S is 0.10% or less. Preferably, it is 0.005% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0015%, the desulfurization cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0015% is the substantive lower limit.


“Sol. Al: 0.0002% or More and 3.0000% or Less”


Al is an element acting to deoxidize the molten steel and make the steel sounder. With less than 0.0002%, the deoxidation is insufficient, so the sol. Al is 0.0002% or more. Preferably the content is 0.0010% or more. On the other hand, even if adding more than 3.0000%, the effect becomes saturated, so the content is 3.0000% or less.


“N: 0.01% or Less”

N is an impurity element and is an element which forms nitrides and impairs bendability. If more than 0.01%, coarse nitrides are formed and the bendability remarkably falls, so N is 0.01% or less. Preferably the content is 0.0075% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0001%, the denitridation cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% is the substantive lower limit.


“Ni: 0.01% or More and 3.00% or Less”

Ni is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.01%, the effect is not obtained, so the content is 0.01% or more. Preferably, the content is 0.50% or more. On the other hand, even if added in more than 3.00%, the effect becomes saturated, so the content is 3.00% or less. Preferably, the content is 2.50% or less.


“Nb: 0.010% or More and 0.150% or Less”

Nb is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.010%, the effect is not obtained, so the content is 0.010% or more. Preferably, the content is 0.035% or more. On the other hand, even if added in more than 0.150%, the effect becomes saturated, so the content is 0.150% or less. Preferably, the content is 0.120% or less.


“Ti: 0.010% or More and 0.150% or Less”

Ti is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.010%, the effect is not obtained, so the content is 0.010% or more. Preferably, the content is 0.020% or more. On the other hand, even if added in more than 0.150%, the effect becomes saturated, so the content is 0.150% or less. Preferably, the content is 0.120% or less.


“Mo: 0.005% or More and 1.000% or Less”

Mo is an element contributing to improvement of strength by solution strengthening, so may be added as needed. With less than 0.005%, the effect is not obtained, so the content is 0.005% or more. Preferably, the content is 0.010% or more. On the other hand, even if added in more than 1.000%, the effect becomes saturated, so the content is 1.000% or less. Preferably, the content is 0.800% or less.


“B: 0.0005% or More and 0.0100% or Less”

B is an element segregating at the grain boundaries and improving the strength of the grain boundaries, so may be added as needed. With less than 0.0005%, the effect of addition is not sufficiently obtained, so 0.0005% or more is added. Preferably, the content is 0.0010% or more. On the other hand, even if added in more than 0.0100%, the effect becomes saturated, so the content is 0.0100% or less. Preferably, the content is 0.0075% or less.


The balance of the chemical constituents of the surface part consists of Fe and unavoidable impurities. The unavoidable impurities are elements which unavoidably enter from the steel raw materials and/or in the steelmaking process and are allowed in ranges not impairing the characteristics of the hot stamped body of the present invention.


Next, the microstructure of the hot stamped body of the present invention will be explained.


“Middle Part in Sheet Thickness has a Hardness of 500 Hv or More and 800 Hv or Less”

If the hardness of the middle part in sheet thickness is 500 Hv or more, as the tensile strength of the hot stamped body, 1500 MPa or more can be secured. Preferably, it is 600 Hv or more. On the other hand, if the hardness of the middle part in sheet thickness is more than 800 Hv, the difference in hardness between the surface layer and the intermediate layer becomes too large and deterioration of the bendability is invited, and therefore 800 Hv is the upper limit. Preferably the hardness is 720 Hv or less.


“Middle Part in Sheet Thickness Comprises, by Area Percent, 1.0% or More and Less than 5.0% of Residual Austenite”


By controlling the Si content at the middle part in sheet thickness to more than 0.50% and less than 3.00% to make the middle part in sheet thickness contain residual austenite as a metal structure in an area percent of 1.0% or more and less than 5.0%, it is possible improve the ductility of the obtained hot stamped body. Preferably the content is 2.0% or more. On the other hand, if the area percent of the residual austenite becomes 5.0% or more, deterioration of the bendability is invited, so the upper limit is less than 5.0%. Preferably, the content is less than 4.5%.


In the present invention, the area percent of the residual austenite is measured by the following method. A sample is taken from a hot stamped member and ground down at its surface to a sheet thickness ¼ depth from the normal direction of the rolling surface for use for X-ray diffraction measurement. From the image obtained by the X-ray diffraction method using Kα rays of Mo, the area percent Vγ of residual austenite was determined using the following formula:






Vγ=(⅔){100/(0.7×α(211)/γ(220)+1)}+(⅓){100/(0.78×α(211)/γ(311)+1)}


Here, α(211) is the reflection surface intensity at the (211) face of ferrite, γ(220) is the reflection surface intensity at the (220) face of austenite, and γ(311) is the reflection surface intensity at the (311) face of austenite.


“The surface layer has a hardness change ΔH1 in the sheet thickness direction of 10 Hv or more and less than 200 Hv, and the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 50 Hv or more and less than 200 Hv”


In the present invention, the “surface layer” means the region from both sides or one side of the hot stamped body to 8% of the thickness of the hot stamped body, i.e., each surface layer has a thickness of 8% of the thickness of the hot stamped body. Similarly, in the present invention, the “intermediate layer” means the part from both sides or one side of the hot stamped body to 20% of the thickness of the hot stamped body except for the above surface layer, i.e., each intermediate layer has a thickness of 12% of the thickness of the hot stamped body. In the present invention, the “middle part in sheet thickness” means the part other than the surface layer and intermediate layer of the hot stamped body, i.e., the middle part in sheet thickness has a thickness of 60% of the thickness of the hot stamped body in the case of a hot stamped body with a surface layer and intermediate layer arranged at both sides of the middle part in sheet thickness and has a thickness of 80% of the thickness of the hot stamped body in the case of a hot stamped body with a surface layer and intermediate layer arranged at only one side of the middle part in sheet thickness. Here, ΔH1 shows the hardness change in sheet thickness direction at the surface layer, while ΔH2 shows the hardness change in sheet thickness direction at the intermediate layer. The inventors studied this in depth and as a result learned that from the viewpoint of the effects on the bendability, etc., the hardness change in this region (ΔH1, ΔH2) is important. It was learned that if ΔH1 is 10 Hv or more and less than 200 Hv, a good bendability and hydrogen embrittlement resistance are obtained. Because of such a good bendability, it is possible to ease the stress occurring due to bending deformation, etc., at the time of impact and suppress fracture and cracking, and therefore it is possible to achieve excellent impact resistance at the hot stamped body. On the other hand, if ΔH1 becomes less than 10 Hv, the effect of easing the stress at the time of bending deformation cannot be obtained and cracks easily progress from the surface layer. Therefore, the lower limit is 10 Hv. Preferably ΔH1 is 20 Hv or more, more preferably 30 Hv or more. Further, if ΔH1 becomes less than 200 Hv, the effect of easing the concentration of stress at the time of bending deformation is raised and good bendability is obtained. Therefore, the upper limit is less than 200 Hv. Preferably, ΔH1 is less than 150 Hv, more preferably less than 100 Hv or 95 Hv or less, most preferably 90 Hv or less.


Similarly, it was learned that if ΔH2 is 50 Hv or more and less than 200 Hv, excellent bendability was obtained. With an ΔH2 of 200 Hv or more, the gradient of hardness at the intermediate layer becomes sharp, it becomes difficult to ease the stress concentration at the time of bending deformation, and the bendability deteriorates. Therefore, less than 200 Hv is the upper limit. Preferably, this is 190 Hv or less, more preferably 180 Hv or less. Further, the lower limit is preferably 60 Hv or more, more preferably 70 Hv or more.


The method of measurement of the hardness of the middle part in sheet thickness is as follows: The cross-section vertical to the sheet surface of the hot stamped body was taken to prepare a sample of the measurement surface which was supplied to a hardness test. The method of preparing the measurement surface may be based on JIS Z 2244. For example, #600 to #1500 silicon carbide paper may be used to polish the measurement surface, then a solution of particle size 1 μm to 6 μm diamond powder dispersed in alcohol or another diluent or pure water may be used to finish the sample to a mirror surface. The hardness test may be performed by the method described in JIS Z 2244. A micro-Vickers hardness tester is used to measure 10 points at the ½ position of thickness of the hot stamped body by a load of 1 kgf and intervals of 3 times or more of the dents. The average value was defined as the hardness of the middle part in sheet thickness.


Next, the method of measurement of the hardness of the surface layer and intermediate layer will be explained. The cross-section vertical to the sheet surface of the hot stamped body is taken to prepare a sample of the measurement surface which is then supplied to a hardness test. The measurement surface is prepared so that there is extremely little unevenness and there is no drooping near the surface so as to enable accurate measurement of the hardness near the surface of the hot stamped body. For example, a cross section polisher made by JEOL is used for sputtering the measurement surface by an argon ion beam. At this time, to keep striation-like unevenness from occurring at the measurement surface, a sample rotation holder made by JEOL may be used so as to irradiate the measurement surface by the argon ion beam from 360 degree directions.


In the case of a hot stamped body with a surface layer and intermediate layer arranged at both sides of the middle part in sheet thickness, the sample with the prepared measurement surface is measured two times using a micro-Vickers hardness tester. The first time, the region from the first surface of the hot stamped body to 20% of the thickness of the hot stamped body is measured in a direction perpendicular to the sheet surface (sheet thickness direction) by a load of 1 kgf and intervals of 3 times or more the dents. At this time, the total of the measurement points differs depending on the thickness of the hot stamped body, but to calculate the later explained ΔH1 and ΔH2, it is sufficient to perform measurement for at least two points or more. The measurement position at the surfacemost side of the hot stamped body is made in the region within 20 μm from the sheet surface (if there is a plated layer, directly under the plated layer or directly under the alloy layer between the plated layer and the matrix material). The second measurement is performed from the surface of the hot stamped body at the opposite side to the first time. That is, the region from the second surface of the hot stamped body to 20% of the thickness is measured in a direction vertical to the sheet surface (sheet thickness direction) by a load of 1 kgf and intervals of 3 times or more the dents. The measurement position at the surfacemost side of the hot stamped body is made the region from the sheet surface (if there is a plated layer, directly under the plated layer or directly under the alloy layer between the plated layer and the matrix material) to within 20 μm.


In the case of a hot stamped body with a surface layer and intermediate layer arranged at only one side of the middle part in sheet thickness, the sample with the prepared measurement surface is measured using a micro-Vickers hardness tester in the region from the surface layer of the hot stamped body to 20% of the thickness of the hot stamped body in a direction perpendicular to the sheet surface (sheet thickness direction) by a load of 1 kgf and intervals of 3 times or more the dents. At this time, the total of the measurement points differs depending on the thickness of the hot stamped body, but to calculate the later explained ΔH1 and ΔH2, it is sufficient to perform measurement for at least two points or more. The measurement position at the surfacemost side of the hot stamped body is made the region from the sheet surface (if there is a plated layer, directly under the plated layer or directly under the alloy layer between the plated layer and the matrix material) to within 20 μm.


Next, the method of calculation of ΔH1 in the case of a hot stamped body with a surface layer and intermediate layer arranged at both sides of the middle part in sheet thickness will be explained. First, the formula (1) is used to calculate the gradient Δa of hardness of the first surface side surface layer from all of the measurement points included in the region from the first surface to thickness 8% of the hot stamped body. Here, ai is the distance from the first surface at the i-th measurement point (μm), ci is the Vickers hardness at ai (Hv), and “n” is the total of all measurement points included in the region from the first surface to thickness 8%. Next, all measurement points included in the region from the second surface to the thickness 8% of the hot stamped body were used to calculate the gradient Δb of the hardness of the second surface side surface layer by the formula (2). Here, bi is the distance from the second surface at the i-th measurement point (μm), di is the Vickers hardness at bi (Hv), and “m” is the total of all measurement points included in the region from the second surface to thickness 8%. After calculating Δa and Δb, formula (3-1) is used to calculate the hardness change ΔH1 in the sheet thickness direction of the surface layer. Here, “t” is the sheet thickness of the hot stamped body (μm).


On the other hand, in the case of a hot stamped body with a surface layer and intermediate layer arranged at only one side of the middle part in sheet thickness, formula (3-2) may be used to calculate the hardness change ΔH1 in the sheet thickness direction of the surface layer.


Next, the method of calculation of ΔH2 in the case of a hot stamped body with a surface layer and intermediate layer arranged at both sides of the middle part in sheet thickness will be explained. First, the formula (4) is used to calculate the gradient ΔA of hardness of the first surface side intermediate layer from all of the measurement points included in the region from the position of thickness 8% to the position of thickness 20% at the first surface side of the hot stamped body. Here, Ai is the distance from the first surface at the i-th measurement point (μm), Ci is the Vickers hardness at Ai (Hv), and N is the total of all measurement points included at the region from the position of the thickness 8% to the position of the 20% thickness at the first surface side. Next, the formula (5) is used to calculate the gradient ΔB of hardness of the second surface side intermediate layer from all of the measurement points included in the region from the position of thickness 8% to the position of thickness 20% at the second surface side of the hot stamped body. Here, Bi is the distance from second surface at the i-th measurement point (μm), Di is the Vickers hardness at Bi (Hv), and M is the total of all measurement points included at the region from the thickness 8% to 20% at the second surface side. After calculating ΔA and ΔB, formula (6-1) is used to calculate the hardness change ΔH2 in the sheet thickness direction of the intermediate layer.


On the other hand, in the case of a hot stamped body with a surface layer and intermediate layer arranged at only one side of the middle part in sheet thickness, formula (6-2) may be used to calculate the hardness change ΔH2 in the sheet thickness direction of the surface layer.









[

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where,


ΔH1: Hardness change in sheet thickness direction at surface layer (Hv)


Δa: Gradient of hardness of first surface side surface layer (Hv/μm)


ai: Distance from first surface at i-th measurement point (μm)


ci: Vickers hardness at ai (Hv)


n: Total of all measurement points included at first surface side surface layer


Δb: Gradient of hardness of second surface side surface layer (Hv/μm)


bi: Distance from second surface at i-th measurement point (μm)


di: Vickers hardness at bi (Hv)


m: Total of all measurement points included at second surface side surface layer


ΔH2: Hardness change in sheet thickness direction at intermediate layer (Hv)


ΔA: Gradient of hardness of first surface side intermediate layer (Hv/μm)


Ai: Distance from first surface at i-th measurement point (μm)


Ci: Vickers hardness at Ai (Hv)


N: Total of all measurement points included at first surface side intermediate layer


ΔB: Gradient of hardness at second surface side intermediate layer (Hv/μm)


Bi: Distance from second surface at i-th measurement point (μm)


Di: Vickers hardness at Bi (Hv)


M: Total of all measurement points included at second surface side intermediate layer


t: Sheet thickness (μm)


The surface of each surface layer of the hot stamped body may be formed with a plated layer for the purpose of improving the corrosion resistance. The plated layer may be either an electroplated layer or a hot dip plated layer. An electroplated layer includes, for example, an electrogalvanized layer, electro Zn—Ni alloy plated layer, etc.


A “hot dip plated layer”, for example, includes a hot dip galvanized layer, a hot dip galvannealed layer, a hot dip aluminum plated layer, a hot dip Zn—Al alloy plated layer, a hot dip Zn—Al—Mg alloy plated layer, a hot dip Zn—Al—Mg—Si alloy plated layer, etc. The amount of deposition of the plated layer is not particularly limited and may be a general amount of deposition.


Next, the mode of the method for obtaining the hot stamped body of the present invention will be explained. The following explanation is intended to simply illustrate the method for obtaining the hot stamped body of the present invention and is not meant to limit the hot stamped body of the present invention to one obtained from a double-layer steel sheet obtained by stacking two steel sheets as explained below. For example, it is also possible to decarburize a single layer steel sheet to soften its surface layer part to obtain high strength steel sheet comprised of a surface layer and middle part in sheet thickness and to heat treat this in the same way as a double-layer steel sheet to produce the body.


A matrix steel sheet satisfying the above constituents in middle part in sheet thickness was produced, ground at both or one surface to remove the surface oxides, then welded with surface layer steel sheet at both surfaces or one surface of the matrix steel sheet by arc welding. It is preferable to superpose a surface layer steel sheet with one or more of the C content, Si content, and Mn content of the surface layer steel sheet of 0.6 time or less the content of the corresponding element of the matrix steel sheet. The reason is not necessarily clear, but the inventors investigated hot stamped bodies exhibiting excellent bendability and as a result one or more of the C content, Si content, and Mn content of the surface layer steel sheet was 0.6 time or less the content of the corresponding element of the matrix steel sheet.


The above multilayer member (double-layer steel sheet) may be hot rolled, cold rolled, hot stamped, continuously hot dip plated, etc., to obtain the high strength steel sheet according to the present invention, more specifically the hot stamped body.


For example, in the case of obtaining hot rolled steel sheet, the double-layer steel sheet prepared by the above method is preferably held at a 1100° C. to 1350° C. temperature for 20 minutes or more and less than 60 minutes. By performing such heat treatment, it is possible to control the hardness change ΔH1 in the sheet thickness direction at the surface layer after hot pressing to 10 Hv or more and less than 200 Hv, in particular to less than 100 Hv. Further, due to the above heat treatment, it is possible to cause elements to diffuse between the matrix steel sheet and the surface layer steel sheet to form an intermediate layer between the two and, furthermore, to control the hardness change ΔH2 in the sheet thickness direction at the intermediate layer after hot pressing to 50 Hv or more and less than 200 Hv. In contrast, with a heating temperature of less than 1100° C., the hardness change ΔH1 in the sheet thickness direction at the surface layer after hot pressing becomes more than 200 Hv and the hardness change ΔH2 in the sheet thickness direction at the intermediate layer after hot pressing becomes less than 10 Hv. In this case, penetration of hydrogen from the hot stamped body surface is aggravated, deterioration of the hydrogen embrittlement resistance is invited, and, furthermore, good bendability cannot be obtained. Therefore, the lower limit is 1100° C. On the other hand, if the heating temperature exceeds 1350° C., ΔH1 becomes less than 10 Hv and, furthermore, ΔH2 ends up exceeding 200 Hv and a good bendability cannot be obtained. Therefore, the upper limit is 1350° C. The heating holding operation is preferably performed for 20 minutes or more and less than 60 minutes. The inventors studied this in depth and as a result learned that if the holding time is 20 minutes or more and less than 60 minutes, a good hydrogen embrittlement resistance and bendability can be obtained and that the microstructure obtained at that time becomes one with a ΔH2 of 50 Hv or more and less than 200 Hv. For this reason, the holding time is 20 minutes or more and less than 60 minutes.


Further, to promote more the formation of the intermediate layer in the present invention, the hot rolling after the above heat treatment of the double-layer steel sheet preferably includes rough rolling and finish rolling with the rough rolling being performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a reduction rate of sheet thickness per pass of 5% or more and less than 50%, and a time between passes of 3 seconds or more.


Specifically, to promote more the formation of the intermediate layer in the present invention, the concentrations of alloy elements, in particular C atoms, have to be controlled to become more moderately distributed. The distribution of concentration of C is obtained by diffusion of C atoms. The diffusion frequency of C atoms increases the higher the temperature. Therefore, to control the C concentration, control in the rough rolling from the hot rolling heating becomes important. In hot rolling heating, to promote the diffusion of C atoms, the heating temperature has to be high. Preferably, it is 1100° C. or more and 1350° C. or less, more preferably more than 1150° C. and 1350° C. or less. With hot rolled heating, the changes of (i) and (ii) shown in FIG. 1 occur. (i) shows the diffusion of C atoms from the middle part in sheet thickness to the surface layer, while (ii) shows the decarburization reaction of C being desorbed from the surface layer to the outside. A distribution occurs in the concentration of C due to the balance between this diffusion of C atoms and the desorption reaction of (i) and (ii). With less than 1100° C., the reaction of (i) is insufficient, so the preferable distribution of the concentration of C cannot be obtained. On the other hand, with more than 1350° C., the reaction of (ii) excessively occurs, so similarly a preferable distribution of concentration cannot be obtained.


After adjusting the hot rolling heating temperature to obtain the preferable distribution of concentration of C, to obtain a further optimum distribution of concentration of C, pass control in rough rolling becomes extremely important. Rough rolling is performed two times or more under conditions of a rough rolling temperature of 1100° C. or more, a reduction rate of sheet thickness per pass of 5% or more and less than 50%, and a time between passes of 3 seconds or more. This is so as to promote the diffusion of C atoms of (i) in FIG. 1 by the strain introduced in the rough rolling. Even if using an ordinary method to rough roll and finish roll a slab controlled in concentration of C to a preferable state by hot rolling heating, the sheet thickness will be reduced without the C atoms sufficiently diffusing in the surface layer. Therefore, if manufacturing hot rolled steel sheet of a thickness of several mm from a slab having a thickness more than 200 mm by an ordinary hot rolling, the result will be a steel sheet changing rapidly in concentration of C at the surface layer. A moderate hardness change will no longer be able to be obtained. The method discovered to solve this is the above pass control of the rough rolling. The diffusion of C atoms is greatly affected by not only the temperature, but also the strain (dislocation density). In particular, compared with lattice diffusion, with dislocation diffusion, the diffusion frequency becomes 10 times or more higher, so steps have to be taken to leave the dislocation density while rolling to reduce the sheet thickness. Curve 1 of FIG. 2 shows the change in the dislocation density after a rolling pass in the case where the reduction rate of sheet thickness per pass in the rough rolling is small. It will be understood that strain remains over a long time period. By causing strain to remain at the surface layer over a long time period in this way, C atoms sufficiently disperse in the surface layer and the optimum distribution of concentration of C can be obtained. On the other hand, curve 2 shows the change in dislocation density in the case where the reduction rate of sheet thickness is large. If the amount of strain introduced by the rolling rises, recovery is easily promoted and the dislocation density rapidly falls. For this reason, to obtain the optimal distribution of concentration of C, it is necessary to prevent the occurrence of a change in dislocation density like the curve 2. From such a viewpoint, the upper limit of the reduction rate of sheet thickness per pass becomes less than 50%. To promote the diffusion of C atoms at the surface layer, certain amounts of dislocation density and holding time have to be secured, so the lower limit of the reduction rate of sheet thickness becomes 5%. As the time between passes, 3 seconds or more has to be secured.


The finish rolling may be finish rolling performed under usual conditions. For example, it may be performed with a finish temperature of 810° C. or more in temperature region. The subsequent following cooling conditions also do not have to be prescribed. The sheet is coiled at the 750° C. or less temperature region. Further, the hot rolled steel sheet may also be heat treated again for the purpose of softening it.


The heating, shaping, and cooling steps at the time of hot stamping may also be performed under usual conditions. For example, hot rolled steel sheet obtained by uncoiling hot rolled steel sheet coiled in the hot rolling step, cold rolled steel sheet obtained by uncoiling and cold rolling coiled hot rolled steel sheet, or steel sheet obtained by plating cold rolled steel sheet, heating this by a 0.1° C./s to 200° C./s heating rate up to 810° C. or more and 1000° C. or less in temperature, and holding it at this temperature is formed into the required shape by the usual hot stamping. The holding time may be set according to the mode of forming. Therefore, although this is not particularly limited, the holding time may be 30 seconds or more and 600 seconds or less. Hot stamped body is cooled to room temperature. The cooling rate may also be set to a usual condition. For example, the average cooling rate in the temperature region from the heating temperature to 400° C. may be 50° C./s or more. In the case of steel sheet with an Si content at the middle part in sheet thickness of more than 0.50% and less than 3.00% and an Mn content at the middle part in sheet thickness of 0.20% or more and less than 1.50% and steel sheet with an Si content at the middle part in sheet thickness of more than 0.50% and less than 3.00% and an Mn content at the middle part in sheet thickness of 1.50% or more and less than 3.00%, for the purpose of increasing the amount of formation of residual austenite to improve the ductility, it is preferable to control the average cooling rate at the cooling after heating and holding at the 200° C. to 400° C. temperature region to less than 50° C./s. Further, for the purpose of adjusting the strength etc., it is possible to temper the stamped body cooled down to room temperature in the range of 150° C. to 600° C.


The cold rolling may be cold rolling performed by a usual rolling reduction, for example, 30 to 90%. The hot rolled steel sheet and the cold rolled steel sheet include sheets as hot rolled and cold rolled and also steel sheets obtained by recrystallization annealing hot rolled steel sheet or cold rolled steel sheet under usual conditions and steel sheets obtained by skin pass rolling under usual conditions. The plating conditions are not particularly limited and may be usual conditions. Hot rolled steel sheet, cold rolled steel sheet, or steel sheet obtained by recrystallization annealing and/or skin pass rolling cold rolled steel sheet are plated under usual plating conditions according to need.


EXAMPLES

Next, examples of the present invention will be explained, but the conditions in the examples are just illustrations of conditions employed for confirming the workability and advantageous effects of the present invention. The present invention is not limited to the illustration of examples. The present invention can employ various conditions so long as not departing from the gist of the present invention and achieving the object of the present invention.


In the examples, the hardness of a hot stamped steel sheet was measured by the method explained above and the hardness of the middle part in sheet thickness, the hardness change ΔH1 in the sheet thickness direction of the surface layer, and the hardness change ΔH2 in the sheet thickness direction of the intermediate layer were calculated.


Further, a tensile test of the hot stamped steel sheet was performed. The tensile test was performed by preparing a No. 5 test piece described in ES Z 2201 and following the test method described in JIS Z 2241.


The hydrogen embrittlement resistance of the hot stamped body was evaluated using a test piece cut out from the stamped body. In general, a hot stamped body is joined with other parts using spot welding or another joining method. Depending upon the precision of the shape of the part, the hot stamped body will be subjected to twisting and stress will be applied. The stress differs depending on the position of the part. Accurately calculating this is difficult, but if there is no delayed fracture at the yield stress, it is believed there is no problem in practical use. Therefore, a sheet thickness 1.2 mm×width 6 mm×length 68 mm test piece was cut out from the stamped body, a strain corresponding to the yield stress was imparted in a four-point bending test, then the test piece was immersed in pH3 hydrochloric acid for 100 hours. The presence of any cracking was used to evaluate the hydrogen embrittlement resistance. A case of no cracking was marked as passing (“good”) and a case with cracking was marked as failing (“poor”).


The impact resistance of the hot stamped body was evaluated by the bendability of the hot stamped body based on the VDA standard (VDA238-100) prescribed by the German Association of the Automotive Industry under the following measurement conditions. In the present invention, the displacement at the time of maximum load obtained in the bending test was converted to angle by the VDA standard to find maximum bending angle.


Test piece dimensions: 60 mm (rolling direction)×60 mm (direction vertical to rolling) or 30 mm (rolling direction)×60 mm (direction vertical to rolling)


Bending ridgeline: direction perpendicular to rolling


Test method: roll support, punch pressing


Roll diameter: φ30 mm


Punch shape: tip R=0.4 mm


Distance between rolls: 2.0×sheet thickness (mm)+0.5 mm


Pressing rate: 20 mm/min


Tester: SHIMAZU AUTOGRAPH 20 kN


Example A

A matrix steel sheet having the chemical constituents shown in Table 1 was ground on its surface to remove surface oxides, then a surface layer steel sheet having the chemical constituents shown in Table 2 was welded with both surfaces or one surface by arc welding. The total thickness of the surface layer steel sheet and the matrix steel sheet after arc welding is 200 mm to 300 mm and the thickness of the surface layer steel sheet is ⅓ or so the thickness of the matrix steel sheet (in the case of a single side, ¼ or so). Manufacturing Nos. 1 to 36 and 38 to 40 are steels with surface layer steel sheets welded to both surfaces, while Manufacturing No. 37 is steel with a surface layer steel sheet welded to only one surface. These multilayer steel sheets are hot rolled and/or cold rolled as shown in Table 3. The obtained steel sheets are heat treated as shown in Table 3 and hot stamped to produce stamped bodies. Table 4 shows the microstructures and mechanical characteristics of the hot stamped steel sheets (hot stamped bodies). The chemical constituents analyzed at sheet thickness ½ positions of samples taken from the hot stamped steel sheets and at positions of 20 μm from the surfaces (positions within surface layers) are equivalent to the chemical constituents of the matrix steel sheets and surface layer steel sheets shown in Tables 1 and 2.










TABLE 1







Matrix steel
Chemical constituents of matrix steel sheet (mass %)



















sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B






















1
0.21
0.20
1.24
0.012
0.0018
0.043
0.0032
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


3
0.35
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


4
0.45
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


5
0.12
0.15
1.24
0.014
0.0004
0.040
0.0036
0
0
0
0
0


6
0.25
0.14
1.22
0.008
0.0007
0.041
0.0035
0
0
0
0
0


7
0.28
0.14
1.28
0.007
0.0007
0.041
0.0031
0
0
0
0
0


8
0.32
0.14
1.29
0.010
0.0013
0.041
0.0030
0
0
0
0
0


9
0.76
0.13
1.27
0.013
0.0007
0.041
0.0031
0
0
0
0
0


10
0.31
0.41
1.29
0.012
0.0017
0.044
0.0030
0
0
0
0
0


11
0.32
0.16
0.11
0.008
0.0008
0.040
0.0036
0
0
0
0
0


12
0.30
0.16
0.80
0.007
0.0003
0.043
0.0030
0
0
0
0
0


13
0.29
0.17
1.25
0.008
0.0010
0.045
0.0032
0.40
0
0
0
0


14
0.33
0.16
1.31
0.013
0.0003
0.046
0.0033
0
0.047
0
0
0


15
0.31
0.16
1.25
0.014
0.0013
0.043
0.0029
0
0
0.023
0
0


16
0.29
0.13
1.35
0.009
0.0007
0.045
0.0034
0
0
0
0.01
0


17
0.29
0.13
1.31
0.013
0.0010
0.046
0.0033
0
0
0
0
0.0017


1
0.21
0.20
1.24
0.012
0.0018
0.043
0.0032
0
0
0
0
0


1
0.21
0.20
1.24
0.012
0.0018
0.043
0.0032
0
0
0
0
0


1
0.21
0.20
1.24
0.012
0.0018
0.043
0.0032
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


3
0.35
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


3
0.35
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


3
0.35
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


4
0.45
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


4
0.45
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


4
0.45
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


18
0.67
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


18
0.67
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.











TABLE 2







Man.
Matrix steel
Chemical constituents of surface layer steel sheet (mass %)




















no.
sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B























1
1
0.099
0.094
0.595
0.011
0.0011
0.039
0.0030
0
0
0
0
0


2
2
0.150
0.086
0.576
0.012
0.0016
0.041
0.0030
0
0
0
0
0


3
3
0.158
0.085
0.622
0.010
0.0010
0.041
0.0032
0
0
0
0
0


4
4
0.225
0.082
0.627
0.011
0.0016
0.039
0.0032
0
0
0
0
0


5
5
0.054
0.072
0.608
0.009
0.0008
0.040
0.0033
0
0
0
0
0


6
6
0.118
0.067
0.598
0.009
0.0016
0.043
0.0032
0
0
0
0
0


7
7
0.143
0.071
0.602
0.013
0.0013
0.041
0.0031
0
0
0
0
0


8
8
0.170
0.071
0.593
0.007
0.0011
0.043
0.0030
0
0
0
0
0


9
9
0.365
0.059
0.635
0.009
0.0017
0.043
0.0031
0
0
0
0
0


10
10
0.140
0.226
0.684
0.012
0.0017
0.043
0.0032
0
0
0
0
0


11
11
0.173
0.086
0.056
0.014
0.0012
0.039
0.0030
0
0
0
0
0


12
12
0.150
0.086
0.360
0.009
0.0008
0.039
0.0032
0
0
0
0
0


13
13
0.160
0.090
0.650
0.010
0.0008
0.042
0.0030
0.39
0
0
0
0


14
14
0.182
0.074
0.655
0.007
0.0018
0.043
0.0033
0
0.042
0
0
0


15
15
0.158
0.082
0.613
0.009
0.0009
0.043
0.0033
0
0
0.021
0
0


16
16
0.154
0.070
0.621
0.011
0.0008
0.043
0.0033
0
0
0
0.02
0


17
17
0.136
0.070
0.642
0.009
0.0017
0.041
0.0030
0
0
0
0
0.0020


18
1
0.095
0.182
1.190
0.009
0.0008
0.042
0.0031
0
0
0
0
0


19
1
0.092
0.182
0.645
0.012
0.0015
0.043
0.0033
0
0
0
0
0


20
1
0.116
0.100
1.128
0.010
0.0009
0.039
0.0032
0
0
0
0
0


21
2
0.276
0.072
0.678
0.012
0.0010
0.039
0.0031
0
0
0
0
0


22
2
0.273
0.088
1.139
0.013
0.0013
0.042
0.0030
0
0
0
0
0


23
2
0.267
0.146
0.614
0.011
0.0011
0.041
0.0031
0
0
0
0
0


24
3
0.277
0.072
0.610
0.011
0.0014
0.043
0.0033
0
0
0
0
0


25
3
0.182
0.154
0.648
0.012
0.0016
0.040
0.0031
0
0
0
0
0


26
3
0.165
0.077
0.991
0.014
0.0018
0.043
0.0033
0
0
0
0
0


27
4
0.405
0.088
0.691
0.009
0.0012
0.039
0.0033
0
0
0
0
0


28
4
0.212
0.146
0.602
0.011
0.0018
0.042
0.0033
0
0
0
0
0


29
4
0.207
0.072
1.126
0.012
0.0012
0.043
0.0030
0
0
0
0
0


30
2
0.150
0.086
0.576
0.008
0.0011
0.040
0.0031
0
0
0
0
0


31
2
0.150
0.086
0.576
0.008
0.0007
0.042
0.0031
0
0
0
0
0


32
2
0.150
0.086
0.576
0.010
0.0018
0.043
0.0030
0
0
0
0
0


33
2
0.150
0.086
0.576
0.013
0.0013
0.041
0.0033
0
0
0
0
0


34
18
0.335
0.086
0.576
0.013
0.0011
0.043
0.0032
0
0
0
0
0


35
18
0.335
0.086
0.576
0.011
0.0008
0.040
0.0031
0
0
0
0
0


36
2
0.150
0.086
0.576
0.008
0.0014
0.042
0.0030
0
0
0
0
0


37
2
0.150
0.086
0.576
0.012
0.0016
0.041
0.0030
0
0
0
0
0


38
2
0.150
0.086
0.576
0.012
0.0016
0.041
0.0030
0.00
0.000
0.000
0.00
0.00


39
2
0.150
0.086
0.576
0.012
0.0016
0.041
0.0030
0.00
0.000
0.000
0.00
0.00


40
2
0.150
0.086
0.576
0.012
0.0016
0.041
0.0030
0.00
0.000
0.000
0.00
0.00










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


















Hot rolling
Cold




















No. of rolling


rolling





Rough

operations with
Finish
Coiling
Cold



Heating
Holding
rolling
Thickness
time between
temp.
temp.
rolling


Man.
temp.
time
temp.
reduction
passes of
temp.
temp.
rate


no.
(° C.)
(min)
(° C.)
rate (%)
3 sec or more
(° C.)
(° C.)
(%)





1
1130
50
1116
35
3
838
591
55


2
1247
51
1159
40
3
844
545
54


3
1255
49
1137
28
3
911
594
49


4
1128
47
1116
39
3
845
565
47


5
1138
47
1135
32
3
848
700
53


6
1197
49
1151
30
3
860
588
60


7
1246
44
1193
33
3
880
676
51


8
1100
48
1100
44
3
847
688
43


9
1199
46
1145
30
3
872
710
57


10
1100
45
1100
36
3
830
614
45


11
1172
57
1136
28
3
891
619
57


12
1247
50
1198
40
3
844
545
54


13
1187
51
1165
34
3
868
738
45


14
1181
52
1125
44
3
919
542
54


15
1217
59
1174
33
3
915
562
44


16
1215
52
1132
31
3
850
715
45


17
1234
55
1123
44
3
855
576
40


18
1176
54
1141
42
3
864
583
41


19
1160
45
1143
41
3
853
641
57


20
1233
46
1130
42
3
865
666
42


21
1137
53
1125
42
3
837
589
57


22
1270
51
1173
30
3
850
551
48


23
1105
55
1102
37
3
851
697
52


24
1213
58
1150
39
3
856
587
48


25
1174
55
1160
37
3
884
698
51


26
1153
56
1139
27
3
888
579
43


27
1154
55
1144
27
3
867
661
41


28
1236
51
1178
26
3
892
700
51


29
1171
54
1147
33
3
886
626
59


30
 980
54
 971
34
3
834
607
43


31
1167
12
1131
45
3
911
730
46


32
1380
54
1141
38
3
862
590
55


33
1141
45
1136
26
3
896
613
0


34
1152
55
1132
31
3
831
676
57


35
1247
51
1138
40
3
840
630
45


36
1122
54
1117
37
3
850
736
45


37
1241
50
1120
35
3
839
559
54


38
1199
52
1009
44
3
837
607
48


39
1187
45
1186
 3
2
856
613
51


40
1234
55
1145
27
1
867
736
43













Heat treatment step at hot stamping


















Average
Average








cooling rate
cooling rate


Thickness



Heating
Heating
from heating
from 400° C.
Tempering

after hot


Man.
rate
temp.
temp. to
to 200° C.
temp.

stamping


no.
(° C./s)
(° C.)
400° C. (° C./s)
(° C./s)
(° C.)
Plating
(mm)





1
39
906
78
60
None
None
1.3


2
33
873
104
96
None
None
1.3


3
51
848
79
59
None
None
1.4


4
58
890
96
83
None
None
1.5


5
48
878
87
79
None
None
1.3


6
63
828
76
62
None
None
1.1


7
70
924
88
74
None
None
1.4


8
53
822
70
59
None
None
1.6


9
28
854
79
62
None
None
1.2


10
48
924
73
55
None
None
1.5


11
56
847
94
80
None
None
1.2


12
62
873
88
73
None
None
1.3


13
27
827
93
76
None
None
1.5


14
43
897
84
62
None
None
1.3


15
24
913
83
71
None
None
1.6


16
34
904
102
85
None
None
1.5


17
59
842
107
96
None
None
1.7


18
46
913
96
78
None
None
1.7


19
20
838
83
72
None
None
1.2


20
26
904
91
72
None
None
1.6


21
21
842
89
73
None
None
1.2


22
19
820
94
84
None
None
1.5


23
67
836
100
85
None
None
1.3


24
71
928
89
70
None
None
1.5


25
63
911
99
87
None
None
1.4


26
19
860
91
78
None
None
1.6


27
73
899
86
78
None
None
1.7


28
27
889
107
91
None
None
1.4


29
39
876
93
85
None
None
1.1


30
45
925
88
85
None
None
1.6


31
74
907
70
54
None
None
1.5


32
65
833
78
66
None
None
1.3


33
69
850
75
58
None
None
2.8


34
55
899
82
67
250
None
1.2


35
55
917
89
69
257
Yes
1.5


36
45
837
97
73
None
Yes
1.5


37
25
882
86
74
None
None
1.3


38
32
820
95
74
None
None
1.7


39
62
911
74
72
None
None
1.2


40
31
876
108
96
None
None
1.3




















TABLE 4









Microstructure
Mechanical properties
















Hardness of middle




Hydrogen



Man.
part in sheet thickness


Tensile strength
Max. bending
embrittlement


no.
(Hv)
ΔH1 (Hv)
ΔH2 (Hv)
(MPa)
angle (°)
resistance
Remarks

















1
503
73
135
1661
88.6
Good
Inv. ex.


2
633
65
124
2088
80.8
Good
Inv. ex.


3
705
78
144
2326
76.1
Good
Inv. ex.


4
767
39
72
2531
73.2
Good
Inv. ex.


5
374
63
144
1118
98.1
Good
Comp. ex.


6
561
51
124
1851
85.2
Good
Inv. ex.


7
604
49
97
1993
82.9
Good
Inv. ex.


8
662
38
77
2183
79.6
Good
Inv. ex.


9
971
63
120
3204
62.1
Good
Comp. ex.


10
647
51
92
2136
82.5
Good
Inv. ex.


11
487
93
176
1456
81.2
Good
Comp. ex.


12
631
65
124
2082
86.6
Good
Inv. ex.


13
637
63
121
2102
85.4
Good
Inv. ex.


14
652
79
143
2152
86.1
Good
Inv. ex.


15
643
83
184
2122
85.5
Good
Inv. ex.


16
642
80
146
2119
82.5
Good
Inv. ex.


17
655
57
140
2162
84.1
Good
Inv. ex.


18
511
71
131
1644
86.1
Good
Inv. ex.


19
514
73
141
1644
88.9
Good
Inv. ex.


20
505
75
135
1668
89.4
Good
Inv. ex.


21
638
61
121
2105
80.1
Good
Inv. ex.


22
634
68
137
2092
81.3
Good
Inv. ex.


23
636
65
131
2098
82.1
Good
Inv. ex.


24
710
74
144
2342
77.6
Good
Inv. ex.


25
701
78
148
2313
75.9
Good
Inv. ex.


26
704
77
139
2322
77.4
Good
Inv. ex.


27
771
41
71
2544
72.9
Good
Inv. ex.


28
765
39
72
2525
74.2
Good
Inv. ex.


29
771
38
74
2544
73.9
Good
Inv. ex.


30
629
221
7
2075
61.2
Poor
Comp. ex.


31
636
210
4
2098
62.3
Poor
Comp. ex.


32
635
5
211
2095
66.9
Good
Comp. ex.


33
631
66
125
2082
80.8
Good
Inv. ex.


34
723
71
131
2386
75.3
Good
Inv. ex.


35
720
61
124
2376
75.6
Good
Inv. ex.


36
636
66
138
2098
80.6
Good
Inv. ex.


37
631
65
124
2082
76.1
Good
Inv. ex.


38
642
207
6
2115
59.1
Poor
Comp. ex.


39
640
210
7
2122
62.2
Poor
Comp. ex.


40
654
211
8
2150
62.5
Poor
Comp. ex.









A case where the tensile strength is 1500 MPa or more, the maximum bending angle)(° is 70)(° or more, and the hydrogen embrittlement resistance is of the passing level was evaluated as a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance (invention examples in Table 4). On the other hand, a case where even one of the above three performances failed to be satisfied was designated as a comparative example.


Example B (Mn: 1.50% or More and Less than 3.00%)

A matrix steel sheet having the chemical constituents shown in Table 5 was ground on its surface to remove surface oxides, then a surface layer steel sheet having the chemical constituents shown in Table 6 was welded with both surfaces or one surface by arc welding. The total thickness of the surface layer steel sheet and the matrix steel sheet after arc welding is 200 mm to 300 mm and the thickness of the surface layer steel sheet is ⅓ or so the thickness of the matrix steel sheet (in the case of a single side, ¼ or so). Manufacturing Nos. 101 to 135 and 137 to 139 are steels with surface layer steel sheets welded to both surfaces, Manufacturing No. 136 is steel with a surface layer steel sheet welded to only one surface. These multilayer steel sheets are hot rolled and/or cold rolled as shown in Table 7. The obtained steel sheets are heat treated as shown in Table 7 and hot stamped to produce stamped bodies. Table 8 shows the microstructures and mechanical characteristics of the hot stamped steel sheets (hot stamped bodies). The chemical constituents analyzed at sheet thickness ½ positions of samples taken from the hot stamped steel sheets and at positions of 20 μm from the surfaces (positions within surface layers) are equivalent to the chemical constituents of the matrix steel sheets and surface layer steel sheets shown in Tables 5 and 6.










TABLE 5







Matrix steel
Chemical constituents of matrix steel sheet (mass %)



















sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B






















101
0.22
0.21
1.55
0.013
0.0010
0.039
0.0032
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


104
0.45
0.05
1.78
0.010
0.0008
0.041
0.0037
0
0
0
0
0


105
0.19
0.10
1.70
0.010
0.0015
0.037
0.0035
0
0
0
0
0


106
0.25
0.02
1.95
0.010
0.0010
0.035
0.0029
0
0
0
0
0


107
0.28
0.15
1.66
0.010
0.0008
0.035
0.0028
0
0
0
0
0


108
0.37
0.10
1.77
0.005
0.0010
0.035
0.0030
0
0
0
0
0


109
0.73
0.05
1.85
0.020
0.0008
0.040
0.0034
0
0
0
0
0


110
0.22
0.20
0.40
0.010
0.0008
0.033
0.0035
0
0
0
0
0


111
0.32
0.25
1.00
0.012
0.0013
0.038
0.0020
0
0
0
0
0


112
0.33
0.30
1.54
0.010
0.0008
0.030
0.0030
0.20
0
0
0
0


113
0.32
0.22
1.75
0.008
0.0005
0.040
0.0035
0
0.080
0.02
0.01
0.0018


114
0.35
0.20
1.70
0.015
0.0004
0.040
0.0028
0
0.05
0.022
0
0.0018


115
0.35
0.21
1.65
0.010
0.0008
0.040
0.0030
0
0
0
0.10
0


116
0.34
0.22
1.65
0.009
0.0010
0.040
0.0030
0
0
0
0
0.0020


101
0.22
0.21
1.55
0.012
0.0010
0.039
0.0032
0
0
0
0
0


101
0.22
0.21
1.55
0.012
0.0010
0.039
0.0032
0
0
0
0
0


101
0.22
0.21
1.55
0.012
0.0010
0.039
0.0032
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


104
0.45
0.05
1.78
0.010
0.0008
0.041
0.0037
0
0
0
0
0


104
0.45
0.05
1.78
0.010
0.0008
0.041
0.0037
0
0
0
0
0


104
0.45
0.05
1.78
0.010
0.0008
0.041
0.0037
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


103
0.36
0.20
1.50
0.010
0.0011
0.030
0.0035
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0


102
0.31
0.22
1.73
0.008
0.0004
0.040
0.0034
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.











TABLE 6







Man.
Matrix steel
Chemical constituents of surface layer steel sheet (mass %)




















no.
sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B























101
101
0.10
0.09
0.85
0.009
0.0013
0.034
0.0034
0
0
0
0
0


102
102
0.16
0.10
0.78
0.007
0.0008
0.032
0.0035
0
0
0
0
0


103
103
0.17
0.10
0.75
0.010
0.0009
0.038
0.0037
0
0
0
0
0


104
104
0.22
0.02
0.71
0.007
0.0010
0.042
0.0032
0
0
0
0
0


105
105
0.09
0.05
0.88
0.009
0.0007
0.040
0.0032
0
0
0
0
0


106
106
0.13
0.01
0.78
0.013
0.0015
0.030
0.0035
0
0
0
0
0


107
107
0.14
0.08
0.78
0.008
0.0013
0.036
0.0035
0
0
0
0
0


108
108
0.19
0.06
0.89
0.010
0.0011
0.031
0.0031
0
0
0
0
0


109
109
0.37
0.03
0.87
0.013
0.0013
0.042
0.0031
0
0
0
0
0


110
110
0.12
0.11
0.24
0.007
0.0009
0.039
0.0035
0
0
0
0
0


111
111
0.16
0.14
0.57
0.007
0.0006
0.030
0.0034
0
0
0
0
0


112
112
0.15
0.14
0.77
0.008
0.0008
0.036
0.0037
0.22
0
0
0
0


113
113
0.14
0.10
0.89
0.009
0.0015
0.038
0.0036
0
0.055
0
0
0


114
114
0.20
0.10
0.85
0.007
0.0011
0.039
0.0037
0
0
0.023
0
0


115
115
0.19
0.10
0.79
0.008
0.0011
0.036
0.0032
0
0
0
0.030
0


116
116
0.18
0.10
0.81
0.013
0.0008
0.040
0.0030
0
0
0
0
0.0018


117
101
0.16
0.16
0.74
0.010
0.0013
0.030
0.0032
0
0
0
0
0


118
101
0.10
0.19
0.85
0.008
0.0012
0.039
0.0034
0
0
0
0
0


119
101
0.10
0.11
1.32
0.009
0.0010
0.037
0.0031
0
0
0
0
0


120
102
0.25
0.10
0.78
0.008
0.0008
0.041
0.0037
0
0
0
0
0


121
102
0.16
0.17
1.14
0.007
0.0007
0.042
0.0035
0
0
0
0
0


122
102
0.16
0.10
1.56
0.013
0.0008
0.031
0.0036
0
0
0
0
0


123
103
0.31
0.10
0.75
0.008
0.0014
0.030
0.0031
0
0
0
0
0


124
103
0.24
0.13
0.75
0.011
0.0013
0.037
0.0036
0
0
0
0
0


125
103
0.17
0.10
1.20
0.007
0.0014
0.042
0.0033
0
0
0
0
0


126
104
0.28
0.02
0.71
0.011
0.0008
0.034
0.0031
0
0
0
0
0


127
104
0.22
0.03
0.71
0.012
0.0012
0.036
0.0038
0
0
0
0
0


128
104
0.22
0.02
1.51
0.010
0.0007
0.031
0.0030
0
0
0
0
0


129
102
0.12
0.11
0.87
0.008
0.0010
0.041
0.0031
0
0
0
0
0


130
102
0.14
0.10
0.88
0.009
0.0015
0.030
0.0036
0
0
0
0
0


131
102
0.19
0.11
0.88
0.010
0.0007
0.034
0.0034
0
0
0
0
0


132
102
0.16
0.10
0.78
0.011
0.0006
0.038
0.0030
0
0
0
0
0


133
103
0.19
0.11
0.75
0.013
0.0007
0.036
0.0035
0
0
0
0
0


134
103
0.19
0.10
0.69
0.009
0.0014
0.036
0.0034
0
0
0
0
0


135
102
0.17
0.10
0.87
0.009
0.0015
0.039
0.0037
0
0
0
0
0


136
102
0.17
0.10
0.87
0.010
0.0016
0.038
0.0035
0
0
0
0
0


137
102
0.16
0.10
0.78
0.007
0.0008
0.032
0.0035
0
0
0
0
0


138
102
0.16
0.10
0.78
0.007
0.0008
0.032
0.0035
0
0
0
0
0


139
102
0.16
0.10
0.78
0.007
0.0008
0.032
0.0035
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.












TABLE 7









Hot rolling
Cold




















No. of rolling


rolling





Rough

operations with
Finish
Coiling
Cold



Heating
Holding
rolling
Thickness
time between
temp.
temp.
rolling


Man.
temp.
time
temp.
reduction
passes of
temp.
temp.
rate


no.
(° C.)
(min)
(° C.)
rate (%)
3 sec or more
(° C.)
(° C.)
(%)





101
1250
59
1160
34
3
917
618
50


102
1260
55
1143
38
3
910
622
43


103
1255
58
1140
21
3
900
570
42


104
1200
57
1158
35
3
890
600
50


105
1253
55
1132
35
3
863
631
42


106
1250
55
1150
39
3
886
560
50


107
1250
56
1206
39
3
881
570
50


108
1250
57
1137
43
3
887
572
50


109
1200
59
1165
25
3
890
700
40


110
1260
53
1146
37
3
925
610
50


111
1280
45
1124
40
3
900
570
50


112
1250
48
1190
39
3
890
620
50


113
1190
59
1176
22
3
920
620
43


114
1260
57
1146
37
3
900
575
40


115
1250
59
1162
39
3
900
600
45


116
1255
58
1151
36
3
890
620
50


117
1250
57
1126
42
3
920
600
50


118
1245
58
1150
37
3
925
605
50


119
1252
58
1164
34
3
910
615
50


120
1260
55
1130
50
3
905
620
43


121
1255
54
1145
43
3
913
625
43


122
1250
57
1172
31
3
907
611
43


123
1250
55
1124
43
3
900
580
42


124
1260
45
1161
34
3
910
575
42


125
1255
48
1157
41
3
905
581
42


126
1210
57
1132
34
3
895
640
50


127
1250
55
1177
32
3
900
645
50


128
1260
60
1168
19
3
914
655
50


129
1070
55
1004
33
3
825
580
43


130
1390
60
1162
30
3
930
630
43


131
1150
5
1125
44
3
905
600
43


132
1250
60
1134
24
3
863
595
0


133
1250
60
1124
42
3
916
581
42


134
1255
50
1145
44
3
920
590
42


135
1264
50
1168
38
3
907
690
43


136
1250
55
1135
36
3
912
650
43


137
1252
54
1006
42
3
910
615
43


138
1255
55
1160
2
2
895
625
43


139
1250
57
1174
39
1
914
581
50













Heat treatment step at hot stamping


















Average
Average








cooling rate
cooling rate


Thickness



Heating
Heating
from heating
from 400° C.
Tempering

after hot


Man.
rate
temp.
temp. to
to 200° C.
temp.

stamping


no.
(° C./s)
(° C.)
400° C. (° C./s)
(° C./s)
(° C.)
Plating
(mm)





101
34
897
68
69
None
None
1.4


102
37
895
103
90
None
None
1.6


103
48
900
69
68
None
None
1.6


104
51
900
91
82
None
None
1.4


105
51
898
89
78
None
None
1.6


106
66
900
86
70
None
None
1.4


107
68
900
95
97
None
None
1.4


108
56
900
88
82
None
None
1.4


109
31
905
86
68
None
None
1.7


110
39
900
86
76
None
None
1.4


111
58
900
94
85
None
None
1.4


112
56
890
97
84
None
None
1.4


113
28
905
79
73
None
None
1.6


114
37
900
73
66
None
None
1.7


115
17
900
86
80
None
None
1.5


116
33
900
94
82
None
None
1.4


117
56
900
94
89
None
None
1.4


118
48
900
86
83
None
None
1.4


119
25
900
72
66
None
None
1.4


120
26
895
98
96
None
None
1.6


121
17
895
90
82
None
None
1.6


122
26
895
89
82
None
None
1.6


123
64
891
107
97
None
None
1.6


124
72
904
97
83
None
None
1.6


125
52
888
110
95
None
None
1.6


126
19
900
84
68
None
None
1.4


127
64
900
91
79
None
None
1.4


128
33
900
93
91
None
None
1.4


129
30
900
93
84
None
None
1.6


130
53
900
88
85
None
None
1.6


131
68
900
74
60
None
None
1.6


132
56
906
72
57
None
None
2.8


133
46
903
78
70
200
None
1.6


134
55
902
101
89
250
Yes
1.6


135
50
905
105
97
None
Yes
1.6


136
32
900
95
77
None
None
1.6


137
28
900
91
87
None
None
1.6


138
68
904
86
76
None
None
1.6


139
23
900
116
102
None
None
1.4



















TABLE 8









Mechanical properties













Microstructure

Average



















Hardness of


Tensile
Average

cross-sectional
Max.
Hydrogen



Man.
middle part in
ΔH1
ΔH2
strength
cross-sectional
Minimum
hardness − Minimum
bending
embrittlement


no.
sheet thickness (Hv)
(Hv)
(Hv)
(MPa)
hardness (Hv)
hardness (Hv)
hardness (Hv)
angle (°)
resistance
Remarks




















101
518
50
100
1548
500
475
25
88.1
Good
Inv. ex.


102
647
30
64
1935
625
614
11
80.7
Good
Inv. ex.


103
719
93
198
2150
698
665
33
74.5
Good
Inv. ex.


104
795
45
100
2377
784
771
13
71.1
Good
Inv. ex.


105
475
73
171
1419
446
401
45
89.5
Good
Comp. ex.


106
561
72
128
1677
545
522
23
85.1
Good
Inv. ex.


107
604
51
104
1806
579
557
22
82.8
Good
Inv. ex.


108
734
41
81
2193
718
712
6
75.2
Good
Inv. ex.


109
1252
55
116
3742
1235
1230
5
43.0
Poor
Comp. ex.


110
478
69
105
1429
437
298
139
89.0
Good
Comp. ex.


111
662
69
109
1978
631
522
109
79.2
Good
Inv. ex.


112
676
77
198
2021
654
613
41
77.2
Good
Inv. ex.


113
662
73
190
1978
648
632
16
77.9
Good
Inv. ex.


114
705
93
77
2107
687
674
13
77.0
Good
Inv. ex.


115
705
79
57
2110
695
690
5
77.2
Good
Inv. ex.


116
690
61
88
2064
676
657
19
77.7
Good
Inv. ex.


117
518
48
115
1548
504
476
28
78.5
Good
Inv. ex.


118
521
37
94
1558
501
482
19
82.1
Good
Inv. ex.


119
522
54
100
1561
502
475
27
80.7
Good
Inv. ex.


120
647
39
75
1935
627
618
9
74.2
Good
Inv. ex.


121
642
25
91
1920
631
620
11
73.8
Good
Inv. ex.


122
651
27
106
1946
632
624
8
72.7
Good
Inv. ex.


123
719
85
191
2150
701
681
20
72.1
Good
Inv. ex.


124
724
70
160
2165
705
686
19
73.6
Good
Inv. ex.


125
722
77
153
2159
714
699
15
72.8
Good
Inv. ex.


126
790
40
120
2362
767
745
22
71.2
Good
Inv. ex.


127
791
48
111
2365
760
749
11
72.4
Good
Inv. ex.


128
799
45
136
2389
771
761
10
71.0
Good
Inv. ex.


129
645
207
5
1929
617
602
15
59.0
Poor
Comp. ex.


130
648
5
220
1938
625
615
10
55.6
Good
Comp. ex.


131
651
210
1
1946
631
603
28
59.7
Poor
Comp. ex.


132
652
82
122
1949
635
621
14
79.6
Good
Inv. ex.


133
715
67
123
2120
689
652
37
82.7
Good
Inv. ex.


134
704
63
123
2101
684
650
34
77.1
Good
Inv. ex.


135
650
74
147
1944
631
607
24
79.0
Good
Inv. ex.


136
647
72
140
1935
635
609
26
78.2
Good
Inv. ex.


137
654
203
4
2158
654
625
29
59.1
Poor
Comp. ex.


138
661
208
7
2181
661
628
33
63.0
Poor
Comp. ex.


139
649
201
5
2142
649
631
18
62.1
Poor
Comp. ex.









Deformation concentrates in a local soft part at the time of collision and becomes a cause of cracking, so in securing impact resistance, it is important that the variation in hardness in the stamped body be small, i.e., that stable strength be secured. Therefore, in the examples, the impact resistance of the hot stamped body was evaluated from the viewpoint of variation of hardness as well. A cross-section of a long shaped hot stamped body vertical to the long direction was taken at any position in that long direction and measured for hardness of the middle position in sheet thickness in the entire cross-sectional region including the vertical walls. For the measurement, a Vickers tester was used. The measurement load was 1 kgf and the measurement intervals were 1 mm. A case where there were no measurement points of below 100 Hv from the average value of all measurement points was evaluated as being small in variation of hardness, i.e., being excellent in strength stability, and as a result being excellent in impact resistance and marked as a passing level (good), while a case where there were measurement points of below 100 Hv was marked as a failing level (poor). More specifically, a case where a difference from an average value of hardness of all measurement points (average cross-sectional hardness in Table 8) and the value of the smallest hardness among all measurement points is 100 Hv was marked as passing and a case of more than 100 Hv was marked as failing.


In the same way as the case of Example A, a case where the tensile strength is 1500 MPa or more, the maximum bending angle (°) is 70(°) or more, and the hydrogen embrittlement resistance is of the passing level was evaluated as a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance (invention examples in Table 8). Further, a case where the average cross-sectional hardness-minimum hardness is 100 Hv or less was evaluated as improved in impact resistance even from the viewpoint of strength stability in addition to bendability (invention examples other than Example 111 in Table 8). On the other hand, a case where even one of the requirements of “tensile strength”, “maximum bending angle”, and “hydrogen embrittlement resistance” failed to be satisfied was designated as a comparative example.


Example C (Si: More than 0.50% and Less than 3.00%)

A matrix steel sheet having the chemical constituents shown in Table 9 was ground on its surface to remove surface oxides, then a surface layer steel sheet having the chemical constituents shown in Table 10 was welded with both surfaces or one surface by arc welding. The total thickness of the surface layer steel sheet and the matrix steel sheet after arc welding is 200 mm to 300 mm and the thickness of the surface layer steel sheet is ⅓ or so the thickness of the matrix steel sheet (in the case of a single side, ¼ or so). Manufacturing Nos. 201 to 236 and 238 to 240 are steels with surface layer steel sheets welded to both surfaces, Manufacturing No. 237 is steel with a surface layer steel sheet welded to only one surface. These multilayer steel sheets are hot rolled and/or cold rolled as shown in Table 11. The obtained steel sheets are heat treated as shown in Table 11 and hot stamped to produce stamped bodies. Table 12 shows the microstructures and mechanical characteristics of the hot stamped steel sheets (hot stamped bodies). The chemical constituents analyzed at sheet thickness ½ positions of samples taken from the hot stamped steel sheets and at positions of 20 μm from the surfaces (positions within surface layers) are equivalent to the chemical constituents of the matrix steel sheets and surface layer steel sheets shown in Tables 9 and 10.










TABLE 9







Matrix steel
Chemical constituents of matrix steel sheet (mass %)



















sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B






















201
0.26
1.42
1.49
0.009
0.0019
0.047
0.0035
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


203
0.38
1.62
1.03
0.011
0.0005
0.044
0.0036
0
0
0
0
0


204
0.44
1.07
1.10
0.004
0.0002
0.034
0.0034
0
0
0
0
0


205
0.17
1.71
1.09
0.013
0.0004
0.033
0.0034
0
0
0
0
0


206
0.21
1.45
1.08
0.004
0.0010
0.034
0.0032
0
0
0
0
0


207
0.31
1.64
1.32
0.012
0.0008
0.044
0.0027
0
0
0
0
0


208
0.29
1.21
1.48
0.008
0.0016
0.041
0.0030
0
0
0
0
0


209
0.81
1.64
1.44
0.015
0.0006
0.044
0.0033
0
0
0
0
0


210
0.28
0.23
1.44
0.012
0.0017
0.040
0.0027
0
0
0
0
0


211
0.33
0.45
1.32
0.006
0.0002
0.045
0.0033
0
0
0
0
0


212
0.36
1.37
0.07
0.013
0.0013
0.036
0.0033
0
0
0
0
0


213
0.35
1.37
1.18
0.006
0.0009
0.050
0.0029
0.36
0
0
0
0


214
0.38
1.35
1.36
0.012
0.0004
0.042
0.0029
0
0.068
0
0
0


215
0.27
1.46
1.49
0.015
0.0016
0.046
0.0030
0
0
0.078
0
0


216
0.25
1.44
1.41
0.006
0.0012
0.052
0.0031
0
0
0
0.06
0


217
0.30
1.63
1.19
0.009
0.0013
0.041
0.0032
0
0
0
0
0.0025


201
0.26
1.42
1.49
0.009
0.0019
0.047
0.0035
0
0
0
0
0


201
0.26
1.42
1.49
0.009
0.0019
0.047
0.0035
0
0
0
0
0


201
0.26
1.42
1.49
0.009
0.0019
0.047
0.0035
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


203
0.38
1.62
1.03
0.011
0.0005
0.044
0.0036
0
0
0
0
0


203
0.38
1.62
1.03
0.011
0.0005
0.044
0.0036
0
0
0
0
0


203
0.38
1.62
1.03
0.011
0.0005
0.044
0.0036
0
0
0
0
0


204
0.44
1.07
1.10
0.004
0.0002
0.034
0.0034
0
0
0
0
0


204
0.44
1.07
1.10
0.004
0.0002
0.034
0.0034
0
0
0
0
0


204
0.44
1.07
1.10
0.004
0.0002
0.034
0.0034
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


218
0.66
1.79
1.29
0.012
0.0007
0.041
0.0030
0
0
0
0
0


218
0.66
1.79
1.29
0.012
0.0007
0.041
0.0030
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0


202
0.28
1.43
1.16
0.012
0.0004
0.041
0.0026
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.











TABLE 10







Man.
Matrix steel
Chemical constituents of surface layer steel sheet (mass %)




















no.
sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B























201
201
0.12
0.81
0.86
0.015
0.0020
0.046
0.0030
0
0
0
0
0


202
202
0.13
0.69
0.56
0.011
0.0017
0.033
0.0033
0
0
0
0
0


203
203
0.18
0.87
0.50
0.018
0.0017
0.039
0.0038
0
0
0
0
0


204
204
0.20
0.58
0.58
0.014
0.0006
0.042
0.0030
0
0
0
0
0


205
205
0.08
0.96
0.50
0.009
0.0012
0.042
0.0029
0
0
0
0
0


206
206
0.10
0.74
0.60
0.009
0.0022
0.043
0.0026
0
0
0
0
0


207
207
0.14
0.85
0.61
0.016
0.0007
0.036
0.0035
0
0
0
0
0


208
208
0.14
0.67
0.70
0.013
0.0007
0.037
0.0032
0
0
0
0
0


209
209
0.38
0.89
0.66
0.017
0.0007
0.035
0.0030
0
0
0
0
0


210
210
0.13
0.11
0.76
0.017
0.0019
0.037
0.0022
0
0
0
0
0


211
211
0.15
0.20
0.59
0.011
0.0026
0.039
0.0034
0
0
0
0
0


212
212
0.16
0.73
0.03
0.012
0.0018
0.039
0.0025
0
0
0
0
0


213
213
0.17
0.70
0.60
0.015
0.0011
0.034
0.0032
0.03
0
0
0
0


214
214
0.17
0.73
0.68
0.009
0.0005
0.041
0.0035
0
0.017
0
0
0


215
215
0.13
0.70
0.73
0.016
0.0022
0.046
0.0031
0
0
0.012
0
0


216
216
0.12
0.72
0.78
0.013
0.0016
0.039
0.0038
0
0
0
0.02
0


217
217
0.14
0.86
0.68
0.016
0.0010
0.050
0.0033
0
0
0
0
0.0016


218
201
0.10
1.15
1.10
0.008
0.0016
0.044
0.0025
0
0
0
0
0


219
201
0.12
1.33
0.69
0.007
0.0004
0.041
0.0027
0
0
0
0
0


220
201
0.16
0.65
1.30
0.012
0.0017
0.046
0.0036
0
0
0
0
0


221
202
0.24
0.77
0.45
0.003
0.0009
0.035
0.0031
0
0
0
0
0


222
202
0.26
0.79
1.03
0.007
0.0019
0.033
0.0027
0
0
0
0
0


223
202
0.26
1.26
0.36
0.013
0.0007
0.040
0.0029
0
0
0
0
0


224
203
0.29
0.52
0.53
0.008
0.0005
0.042
0.0032
0
0
0
0
0


225
203
0.17
1.47
0.52
0.016
0.0020
0.041
0.0026
0
0
0
0
0


226
203
0.17
0.91
0.85
0.006
0.0012
0.039
0.0025
0
0
0
0
0


227
204
0.40
0.60
0.50
0.015
0.0015
0.038
0.0034
0
0
0
0
0


228
204
0.22
0.85
0.51
0.021
0.0012
0.032
0.0031
0
0
0
0
0


229
204
0.32
0.57
1.05
0.011
0.0003
0.040
0.0030
0
0
0
0
0


230
202
0.13
0.76
0.55
0.013
0.0017
0.041
0.0031
0
0
0
0
0


231
202
0.13
0.80
0.67
0.011
0.0006
0.040
0.0028
0
0
0
0
0


232
202
0.13
0.77
0.57
0.010
0.0020
0.037
0.0032
0
0
0
0
0


233
202
0.13
0.74
0.67
0.013
0.0011
0.042
0.0033
0
0
0
0
0


234
202
0.13
0.79
0.66
0.015
0.0012
0.033
0.0030
0
0
0
0
0


235
218
0.31
0.84
0.72
0.013
0.0018
0.040
0.0031
0
0
0
0
0


236
218
0.32
1.02
0.72
0.009
0.0025
0.035
0.0029
0
0
0
0
0


237
202
0.13
0.76
0.59
0.012
0.0016
0.032
0.0037
0
0
0
0
0


238
202
0.13
0.69
0.56
0.011
0.0017
0.033
0.0033
0
0
0
0
0


239
202
0.13
0.69
0.56
0.011
0.0017
0.033
0.0033
0
0
0
0
0


240
202
0.13
0.69
0.56
0.011
0.0017
0.033
0.0033
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.












TABLE 11









Hot rolling
Cold




















No. of rolling


rolling





Rough

operations with
Finish
Coiling
Cold



Heating
Holding
rolling
Thickness
time between
temp.
temp.
rolling


Man.
temp.
time
temp.
reduction
passes of
temp.
temp.
rate


no.
(° C.)
(min)
(° C.)
rate (%)
3 sec or more
(° C.)
(° C.)
(%)





201
1252
34
1169
42
3
828
595
48


202
1284
57
1156
31
3
840
549
42


203
1234
52
1139
29
3
901
584
46


204
1257
35
1172
30
3
842
565
43


205
1274
53
1140
31
3
836
703
49


206
1263
52
1149
30
3
863
574
45


207
1225
44
1191
43
3
892
681
46


208
1261
38
1127
41
3
851
698
47


209
1274
52
1139
30
3
873
709
46


210
1238
28
1141
39
3
833
629
46


211
1241
28
1136
33
3
851
556
48


212
1276
26
1197
38
3
892
619
49


213
1264
48
1185
31
3
869
739
48


214
1256
50
1141
38
3
922
535
47


215
1267
46
1178
36
3
907
564
47


216
1238
34
1145
35
3
863
714
45


217
1274
35
1120
48
3
846
580
45


218
1232
27
1141
39
3
867
574
47


219
1232
52
1163
42
3
865
653
42


220
1275
25
1125
42
3
872
668
45


221
1246
52
1162
48
3
848
580
47


222
1227
39
1165
29
3
844
538
44


223
1263
26
1132
37
3
856
691
44


224
1265
35
1155
36
3
850
600
47


225
1239
33
1140
39
3
885
688
44


226
1259
36
1132
21
3
899
569
43


227
1240
31
1191
34
3
855
662
43


228
1276
37
1166
24
3
903
710
44


229
1258
28
1138
42
3
876
639
46


230
965
47
955
43
3
823
593
49


231
1368
35
1141
43
3
863
603
44


232
1261
6
1147
42
3
916
716
45


233
1275
56
1139
32
3
902
745
46


234
1240
33
1126
33
3
906
603
0


235
1254
47
1150
40
3
834
683
46


236
1231
32
1152
34
3
830
621
49


237
1270
29
1113
43
3
850
734
49


238
1238
35
1017
43
3
865
580
47


239
1267
52
1151
3
2
856
688
44


240
1232
35
1134
38
1
885
710
44













Heat treatment step at hot stamping


















Average
Average








cooling rate
cooling rate


Thickness



Heating
Heating
from heating
from 400° C.
Tempering

after hot


Man.
rate
temp.
temp. to
to 200° C.
temp.

stamping


no.
(° C./s)
(° C.)
400° C. (° C./s)
(° C./s)
(° C.)
Plating
(mm)





201
36
898
73
27
None
None
1.7


202
29
865
121
16
None
None
1.5


203
39
854
69
16
None
None
1.6


204
54
900
103
28
None
None
1.5


205
52
868
73
28
None
None
1.7


206
67
832
58
27
None
None
1.6


207
59
929
77
25
None
None
1.6


208
49
821
74
16
None
None
1.7


209
31
864
77
8
None
None
1.6


210
45
933
78
17
None
None
1.6


211
52
872
88
40
None
None
1.7


212
64
850
91
16
None
None
1.7


213
25
820
70
25
None
None
1.7


214
36
899
83
27
None
None
1.7


215
29
906
74
14
None
None
1.7


216
28
900
92
18
None
None
1.6


217
65
837
94
13
None
None
1.6


218
51
918
83
17
None
None
1.7


219
19
846
75
38
None
None
1.5


220
23
904
104
14
None
None
1.6


221
18
836
108
10
None
None
1.7


222
25
826
85
27
None
None
1.5


223
68
846
108
32
None
None
1.5


224
63
925
87
21
None
None
1.7


225
49
901
116
22
None
None
1.5


226
31
866
90
6
None
None
1.5


227
75
899
84
17
None
None
1.5


228
35
894
115
14
None
None
1.5


229
42
878
77
29
None
None
1.6


230
54
928
96
25
None
None
1.7


231
79
839
75
30
None
None
1.5


232
61
905
72
24
None
None
1.6


233
57
905
58
14
None
None
1.6


234
49
852
67
27
None
None
2.8


235
56
890
74
25
266
None
1.6


236
54
922
97
30
278
Yes
1.7


237
32
828
86
21
None
Yes
1.7


238
31
846
85
29
None
None
1.5


239
68
899
72
29
None
None
1.5


240
25
928
106
33
None
None
1.6




















TABLE 12









Microstructure
Mechanical properties


















Hardness of


Area rate of
Tensile
Uniform
Max.
Hydrogen



Man.
middle part in


residual
strength
elongation
bending
embrittlement


no.
sheet thickness (Hv)
ΔH1 (Hv)
ΔH2 (Hv)
austenite (%)
(MPa)
(%)
angle (°)
resistance
Remarks



















201
511
71
129
3.6
1529
6.6
88.9
Good
Inv. ex.


202
640
63
134
3.2
1913
6.4
81.1
Good
Inv. ex.


203
712
81
142
2.7
2128
5.8
76.5
Good
Inv. ex.


204
775
36
70
2.3
2503
5.2
73.9
Good
Inv. ex.


205
384
66
140
1.9
1148
5.1
89.1
Good
Comp. ex.


206
565
46
134
2.3
1689
6.2
85.1
Good
Inv. ex.


207
605
45
94
3.5
1809
6.5
83.1
Good
Inv. ex.


208
665
37
78
2.1
1987
5.2
79.7
Good
Inv. ex.


209
1001
60
115
1.1
2993
5.3
62.4
Good
Comp. ex.


210
644
53
97
0.5
1926
3.6
83.2
Good
Inv. ex.


211
626
60
128
0.8
1872
4.2
88.1
Good
Inv. ex.


212
495
91
177
2.1
1480
5.2
81.6
Good
Comp. ex.


213
645
66
125
4.1
1929
6.4
85.5
Good
Inv. ex.


214
666
83
147
3.8
1991
5.9
86.4
Good
Inv. ex.


215
653
87
189
3.3
1952
6.6
85.8
Good
Inv. ex.


216
653
80
154
1.5
1952
6.7
83.0
Good
Inv. ex.


217
656
59
141
3.3
1961
5.8
84.8
Good
Inv. ex.


218
504
39
120
4.5
1508
6.2
82.6
Good
Inv. ex.


219
508
56
95
2.4
1520
6.4
80.6
Good
Inv. ex.


220
512
84
90
2.4
1532
5.3
79.4
Good
Inv. ex.


221
635
66
118
1.1
1898
5.3
83.6
Good
Inv. ex.


222
637
46
135
3.2
1904
6.8
79.6
Good
Inv. ex.


223
638
86
119
2.4
1907
5.5
84.6
Good
Inv. ex.


224
706
56
106
2.7
2110
5.2
86.6
Good
Inv. ex.


225
714
55
87
2.7
2134
6.6
81.4
Good
Inv. ex.


226
709
84
104
3.5
2119
6.7
79.3
Good
Inv. ex.


227
775
87
86
1.5
2317
5.3
78.8
Good
Inv. ex.


228
767
44
128
2.5
2293
5.5
83.9
Good
Inv. ex.


229
772
59
116
2.7
2308
5.4
82.5
Good
Inv. ex.


230
637
215
4
2.9
1904
6.6
65.1
Poor
Comp. ex.


231
635
8
210
3.4
1898
5.4
67.0
Good
Comp. ex.


232
634
223
6
3.8
1895
6.4
63.6
Poor
Comp. ex.


233
638
97
101
4.1
1907
5.5
85.9
Good
Inv. ex.


234
641
68
124
2.9
1916
5.8
80.5
Good
Inv. ex.


235
730
74
127
1.5
2183
5.0
75.5
Good
Inv. ex.


236
718
61
127
2.7
2147
5.7
76.0
Good
Inv. ex.


237
634
62
141
2.3
1895
5.5
81.5
Good
Inv. ex.


238
630
200
5
2.7
2079
6.1
60.6
Poor
Comp. ex.


239
629
206
8
2.8
2076
6.4
62.1
Poor
Comp. ex.


240
624
201
7
3.0
2059
6.4
60.5
Poor
Comp. ex.









In the examples, the impact resistance of the hot stamped body was evaluated from the viewpoint of ductility as well. Specifically, a tensile test of the hot stamped steel sheet was performed to find the uniform elongation of the steel sheet and evaluate the impact resistance. The tensile test was performed by preparing a No. 5 test piece described in JIS Z 2201 and following the test method described in JIS Z 2241. The elongation at which the greatest tensile load was obtained was defined as the “uniform elongation”.


In the same way as the case of Example A, a case where the tensile strength is 1500 MPa or more, the maximum bending angle (°) is 70(°) or more, and the hydrogen embrittlement resistance is of the passing level was evaluated as a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance (examples in Table 12). Further, a case where the uniform elongation is 5% or more was evaluated as improved in impact resistance even from the viewpoint of ductility in addition to bendability (invention examples other than Examples 210 and 211 in Table 12). On the other hand, a case where even one of the requirements of “tensile strength”, “maximum bending angle”, and “hydrogen embrittlement resistance” failed to be satisfied was designated as a comparative example.


Example D (Mn: 1.50% or More and Less than 3.00% and Si: More than 0.50% and Less than 3.00%)

A matrix steel sheet having the chemical constituents shown in Table 13 was ground on its surface to remove surface oxides, then a surface layer steel sheet having the chemical constituents shown in Table 14 was welded with both surfaces or one surface by arc welding. The total thickness of the surface layer steel sheet and the matrix steel sheet after arc welding is 200 mm to 300 mm and the thickness of the surface layer steel sheet is ⅓ or so the thickness of the matrix steel sheet (in the case of a single side, ¼ or so). Manufacturing Nos. 301 to 339 and 341 to 343 are steels with surface layer steel sheets welded to both surfaces, Manufacturing No. 340 is steel with a surface layer steel sheet welded to only one surface. These multilayer steel sheets are hot rolled and/or cold rolled as shown in Table 15. The obtained steel sheets are heat treated as shown in Table 15 and hot stamped to produce stamped bodies. Table 16 shows the microstructures and mechanical characteristics of the hot stamped steel sheets (hot stamped bodies). The chemical constituents analyzed at sheet thickness ½ positions of samples taken from the hot stamped steel sheets and at positions of 20 μm from the surfaces (positions within surface layers) are equivalent to the chemical constituents of the matrix steel sheets and surface layer steel sheets shown in Tables 13 and 14.










TABLE 13







Matrix steel
Chemical constituents of matrix steel sheet (mass %)



















sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B






















301
0.25
1.34
1.85
0.011
0.0020
0.039
0.0032
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


303
0.37
1.54
1.66
0.012
0.0011
0.043
0.0031
0
0
0
0
0


304
0.46
1.52
2.06
0.007
0.0010
0.041
0.0037
0
0
0
0
0


305
0.19
1.21
1.77
0.011
0.0006
0.039
0.0030
0
0
0
0
0


306
0.24
1.46
1.94
0.004
0.0009
0.035
0.0029
0
0
0
0
0


307
0.27
1.78
1.88
0.017
0.0014
0.047
0.0020
0
0
0
0
0


308
0.32
1.78
1.89
0.007
0.0025
0.043
0.0025
0
0
0
0
0


309
0.82
1.61
1.86
0.019
0.0011
0.048
0.0034
0
0
0
0
0


310
0.25
0.15
1.91
0.012
0.0021
0.045
0.0020
0
0
0
0
0


311
0.31
0.44
1.88
0.004
0.0009
0.036
0.0035
0
0
0
0
0


312
0.35
1.23
0.16
0.015
0.0016
0.033
0.0034
0
0
0
0
0


313
0.30
1.25
0.71
0.016
0.0016
0.041
0.0018
0
0
0
0
0


314
0.35
0.36
0.29
0.005
0.0006
0.041
0.0028
0
0
0
0
0


315
0.34
0.22
0.81
0.016
0.0022
0.045
0.0026
0
0
0
0
0


316
0.33
1.57
1.77
0.006
0.0014
0.051
0.0030
0.41
0
0
0
0


317
0.34
0.98
1.78
0.016
0.0005
0.043
0.0026
0
0.082
0
0
0


318
0.25
1.61
1.98
0.016
0.0021
0.039
0.0031
0
0
0.036
0
0


319
0.24
1.26
1.99
0.009
0.0013
0.051
0.0023
0
0
0
0.05
0


320
0.26
1.47
1.70
0.009
0.0019
0.044
0.0027
0
0
0
0
0.0018


301
0.25
1.34
1.85
0.011
0.0020
0.039
0.0032
0
0
0
0
0


301
0.25
1.34
1.85
0.011
0.0020
0.039
0.0032
0
0
0
0
0


301
0.25
1.34
1.85
0.011
0.0020
0.039
0.0032
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


303
0.37
1.54
1.66
0.012
0.0011
0.043
0.0031
0
0
0
0
0


303
0.37
1.54
1.66
0.012
0.0011
0.043
0.0031
0
0
0
0
0


303
0.37
1.54
1.66
0.012
0.0011
0.043
0.0031
0
0
0
0
0


304
0.46
1.52
2.06
0.007
0.0010
0.041
0.0037
0
0
0
0
0


304
0.46
1.52
2.06
0.007
0.0010
0.041
0.0037
0
0
0
0
0


304
0.46
1.52
2.06
0.007
0.0010
0.041
0.0037
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


321
0.64
1.35
1.89
0.015
0.0014
0.044
0.0025
0
0
0
0
0


321
0.64
1.35
1.89
0.015
0.0014
0.044
0.0025
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0


302
0.29
1.31
1.86
0.012
0.0010
0.034
0.0020
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.











TABLE 14







Man.
Matrix steel
Chemical constituents of surface layer steel sheet (mass %)




















no.
sheet no.
C
Si
Mn
P
S
sol. Al
N
Ni
Nb
Ti
Mo
B























301
301
0.14
0.72
1.05
0.011
0.0020
0.047
0.0027
0
0
0
0
0


302
302
0.13
0.58
1.06
0.016
0.0015
0.040
0.0038
0
0
0
0
0


303
303
0.17
0.83
0.90
0.012
0.0017
0.043
0.0041
0
0
0
0
0


304
304
0.23
0.64
0.89
0.015
0.0007
0.041
0.0032
0
0
0
0
0


305
305
0.09
0.59
0.92
0.010
0.0008
0.039
0.0031
0
0
0
0
0


306
306
0.12
0.76
1.01
0.008
0.0021
0.041
0.0027
0
0
0
0
0


307
307
0.13
0.87
0.88
0.019
0.0011
0.038
0.0034
0
0
0
0
0


308
308
0.17
0.94
1.04
0.011
0.0007
0.036
0.0034
0
0
0
0
0


309
309
0.36
0.89
0.78
0.015
0.0006
0.035
0.0020
0
0
0
0
0


310
310
0.14
0.08
1.07
0.018
0.0022
0.035
0.0029
0
0
0
0
0


311
311
0.14
0.23
0.83
0.016
0.0026
0.043
0.0032
0
0
0
0
0


312
312
0.20
0.70
0.08
0.011
0.0029
0.040
0.0026
0
0
0
0
0


313
313
0.15
0.68
0.40
0.013
0.0027
0.036
0.0028
0
0
0
0
0


314
314
0.15
0.17
0.12
0.010
0.0024
0.042
0.0035
0
0
0
0
0


315
315
0.16
0.11
0.36
0.011
0.0019
0.041
0.0022
0
0
0
0
0


316
316
0.14
0.77
0.80
0.014
0.0016
0.034
0.0029
0.05
0
0
0
0


317
317
0.14
0.44
0.89
0.010
0.0006
0.043
0.0029
0
0.018
0
0
0


318
318
0.15
0.84
0.97
0.019
0.0020
0.051
0.0028
0
0
0.005
0
0


319
319
0.13
0.59
0.88
0.009
0.0022
0.037
0.0038
0
0
0
0.02
0


320
320
0.14
0.69
0.85
0.019
0.0005
0.041
0.0030
0
0
0
0
0.0014


321
301
0.11
1.05
1.33
0.007
0.0017
0.039
0.0029
0
0
0
0
0


322
301
0.12
1.26
0.96
0.005
0.0006
0.038
0.0020
0
0
0
0
0


323
301
0.16
0.66
1.61
0.013
0.0019
0.048
0.0036
0
0
0
0
0


324
302
0.24
0.72
0.84
0.011
0.0008
0.041
0.0036
0
0
0
0
0


325
302
0.26
0.79
1.77
0.008
0.0017
0.036
0.0029
0
0
0
0
0


326
302
0.27
1.11
0.60
0.016
0.0008
0.035
0.0027
0
0
0
0
0


327
303
0.28
0.42
0.78
0.010
0.0008
0.048
0.0029
0
0
0
0
0


328
303
0.18
1.36
0.78
0.019
0.0019
0.046
0.0025
0
0
0
0
0


329
303
0.17
0.80
1.43
0.006
0.0013
0.039
0.0028
0
0
0
0
0


330
304
0.41
0.94
1.03
0.013
0.0017
0.037
0.0032
0
0
0
0
0


331
304
0.21
1.29
0.93
0.018
0.0012
0.029
0.0032
0
0
0
0
0


332
304
0.34
0.90
1.77
0.011
0.0006
0.039
0.0028
0
0
0
0
0


333
302
0.12
0.64
0.99
0.012
0.0019
0.035
0.0031
0
0
0
0
0


334
302
0.16
0.71
0.78
0.012
0.0013
0.036
0.0033
0
0
0
0
0


335
302
0.17
0.73
1.04
0.011
0.0004
0.033
0.0030
0
0
0
0
0


336
302
0.14
0.66
0.89
0.014
0.0015
0.049
0.0034
0
0
0
0
0


337
302
0.14
0.62
0.82
0.010
0.0011
0.038
0.0034
0
0
0
0
0


338
321
0.33
0.76
1.10
0.015
0.0024
0.039
0.0036
0
0
0
0
0


339
321
0.34
0.73
0.79
0.012
0.0021
0.032
0.0028
0
0
0
0
0


340
302
0.16
0.72
0.93
0.010
0.0013
0.039
0.0037
0
0
0
0
0


341
302
0.13
0.58
1.06
0.016
0.0015
0.040
0.0038
0
0
0
0
0


342
302
0.13
0.58
1.06
0.016
0.0015
0.040
0.0038
0
0
0
0
0


343
302
0.13
0.58
1.06
0.016
0.0015
0.040
0.0038
0
0
0
0
0










In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.


In the table, fields in which chemical constituent is “0” indicate corresponding constituent is not intentionally added.












TABLE 15









Hot rolling
Cold




















No. of rolling


rolling





Rough

operations with
Finish
Coiling
Cold



Heating
Holding
rolling
Thickness
time between
temp.
temp.
rolling


Man.
temp.
time
temp.
reduction
passes of
temp.
temp.
rate


no.
(° C.)
(min)
(° C.)
rate (%)
3 sec or more
(° C.)
(° C.)
(%)





301
1282
47
1173
36
3
873
718
48


302
1236
44
1155
36
3
876
630
47


303
1257
41
1126
29
3
865
639
43


304
1274
28
1175
31
3
856
526
38


305
1252
36
1131
30
3
863
631
42


306
1280
32
1153
38
3
886
557
49


307
1260
46
1195
34
3
881
599
55


308
1239
54
1131
41
3
862
538
54


309
1278
46
1151
31
3
885
695
42


310
1249
40
1146
33
3
877
550
41


311
1273
49
1144
38
3
867
651
47


312
1256
47
1202
44
3
869
640
41


313
1281
45
1168
30
3
875
555
48


314
1278
38
1150
40
3
886
706
56


315
1256
42
1175
37
3
896
562
41


316
1265
55
1135
36
3
888
703
43


317
1237
30
1127
40
3
856
527
51


318
1246
50
1155
39
3
877
599
44


319
1245
32
1149
43
3
900
591
56


320
1279
28
1110
38
3
855
616
49


321
1270
49
1157
41
3
843
522
56


322
1253
52
1165
32
3
863
652
44


323
1261
30
1120
36
3
880
669
42


324
1272
34
1162
43
3
874
619
54


325
1275
54
1144
43
3
885
558
43


326
1258
47
1124
21
3
863
559
49


327
1253
54
1189
36
3
874
672
45


328
1285
50
1181
21
3
854
623
50


329
1260
41
1135
42
3
855
685
49


330
1265
37
1154
33
3
879
546
39


331
1241
36
1144
37
3
894
691
39


332
1266
55
1132
40
3
882
626
44


333
1080
45
1065
28
3
846
665
56


334
1399
33
1120
29
3
858
7
48


335
1281
4
1131
43
3
903
544
52


336
1242
38
1162
32
3
885
587
50


337
1268
53
1117
45
3
863
595
0


338
1251
35
1113
41
3
897
654
48


339
1237
51
1133
40
3
900
707
43


340
1242
51
1140
33
3
900
712
45


341
1281
45
1016
39
3
854
591
44


342
1237
30
1155
4
2
882
619
45


343
1270
30
1139
35
1
858
672
39













Heat treatment step at hot stamping


















Average
Average








cooling rate
cooling rate


Thickness



Heating
Heating
from heating
from 400° C.
Tempering

after hot


Man.
rate
temp.
temp. to
to 200° C.
temp.

stamping


no.
(° C./s)
(° C.)
400° C. (° C./s)
(° C./s)
(° C.)
Plating
(mm)





301
37
895
75
30
None
None
1.5


302
31
892
116
15
None
None
1.5


303
43
878
74
18
None
None
1.6


304
59
878
100
30
None
None
1.7


305
49
898
77
23
None
None
1.6


306
65
907
54
29
None
None
1.4


307
64
889
72
27
None
None
1.3


308
50
904
75
12
None
None
1.3


309
29
906
82
11
None
None
1.6


310
47
903
75
19
None
None
1.7


311
56
879
88
35
None
None
1.5


312
60
901
87
14
None
None
1.7


313
23
876
71
28
None
None
1.5


314
39
879
80
27
None
None
1.2


315
24
898
72
18
None
None
1.7


316
32
881
91
19
None
None
1.6


317
66
899
99
12
None
None
1.4


318
49
904
88
18
None
None
1.6


319
21
900
77
34
None
None
1.2


320
24
899
100
19
None
None
1.4


321
20
905
104
15
None
None
1.2


322
20
900
89
28
None
None
1.6


323
63
898
109
28
None
None
1.6


324
64
871
92
26
None
None
1.3


325
53
870
112
25
None
None
1.6


326
28
909
85
9
None
None
1.4


327
73
891
83
13
None
None
1.5


328
31
904
113
13
None
None
1.4


329
42
888
79
27
None
None
1.4


330
49
900
96
25
None
None
1.7


331
74
879
73
25
None
None
1.7


332
62
875
75
27
None
None
1.6


333
61
905
60
14
None
None
1.2


334
53
900
70
26
None
None
1.5


335
61
878
74
20
None
None
1.3


336
53
873
96
32
None
None
1.4


337
30
906
84
21
None
None
2.8


338
73
903
99
19
259
None
1.5


339
49
902
100
19
282
Yes
1.6


340
53
898
92
26
None
Yes
1.5


341
28
898
85
29
None
None
1.5


342
68
891
76
26
None
None
1.7


343
26
879
106
35
None
None
1.5




















TABLE 16









Microstructure
Mechanical properties





















Hardness of





Average

Average






middle part


Area rate


cross-

cross-sectional



in sheet


of residual
Tensile
Uniform
sectional
Minimum
hardness −
Max.
Hydrogen


Man.
thickness
ΔH1
ΔH2
austenite
strength
elongation
hardness
hardness
Minimum
bending
embrittlement


no.
(Hv)
(Hv)
(Hv)
(%)
(MPa)
(%)
(Hv)
(Hv)
hardness (Hv)
angle (°)
resistance
Remarks






















301
598
69
128
3.5
1788
6.2
598
534
64
87.2
Good
Inv. ex.


302
668
70
132
2.8
1997
5.4
668
635
33
82.1
Good
Inv. ex.


303
751
79
152
3.1
2245
5.9
751
686
65
78.1
Good
Inv. ex.


304
789
21
63
2.2
2509
5.7
789
753
36
71.4
Good
Inv. ex.


305
464
71
135
1.9
1387
5.2
464
434
30
89.1
Good
Comp. ex.


306
775
34
143
2.0
2316
5.3
775
710
65
75.8
Good
Inv. ex.


307
767
42
81
3.5
2292
6.6
767
742
25
74.7
Good
Inv. ex.


308
791
33
74
2.3
2365
5.8
791
733
58
75.7
Good
Inv. ex.


309
1457
63
103
1.4
4356
5.5
1457
1385
72
61.0
Good
Comp. ex.


310
702
52
97
0.2
2099
2.9
702
651
51
89.1
Good
Inv. ex.


311
786
56
133
0.8
2351
4.4
786
757
29
88.7
Good
Inv. ex.


312
478
88
187
2.2
1429
5.1
478
292
186
88.0
Good
Comp. ex.


313
747
69
68
3.4
2234
6.2
747
579
168
78.2
Good
Inv. ex.


314
733
48
171
0.5
2193
3.9
733
592
141
78.3
Good
Inv. ex.


315
726
32
98
0.4
2172
3.2
726
582
144
80.6
Good
Inv. ex.


316
787
77
118
4.3
2353
6.9
787
746
41
84.4
Good
Inv. ex.


317
773
73
161
3.7
2310
6.6
773
704
69
84.1
Good
Inv. ex.


318
782
93
186
3.2
2338
6.2
782
709
73
80.9
Good
Inv. ex.


319
711
79
152
1.2
2126
5.2
711
672
39
86.8
Good
Inv. ex.


320
709
61
128
3.6
2120
6.9
709
666
43
88.8
Good
Inv. ex.


321
627
63
91
4.9
1876
6.7
627
585
42
86.0
Good
Inv. ex.


322
618
62
134
2.4
1849
5.9
618
556
62
84.2
Good
Inv. ex.


323
616
69
126
2.2
1843
5.4
616
577
39
86.0
Good
Inv. ex.


324
730
84
91
1.2
2184
5.1
730
695
35
80.0
Good
Inv. ex.


325
720
60
128
3.3
2154
6.2
720
648
72
80.6
Good
Inv. ex.


326
722
69
129
2.6
2160
5.9
722
658
64
82.2
Good
Inv. ex.


327
773
68
112
2.4
2311
5.8
773
733
40
84.5
Good
Inv. ex.


328
790
74
87
2.7
2362
5.4
790
758
32
84.5
Good
Inv. ex.


329
776
71
90
3.4
2320
6.2
776
751
25
84.0
Good
Inv. ex.


330
791
77
121
1.8
2365
5.1
791
750
41
82.0
Good
Inv. ex.


331
788
81
90
2.7
2356
6.5
788
731
57
82.9
Good
Inv. ex.


332
795
72
96
2.4
2377
5.3
795
763
32
84.2
Good
Inv. ex.


333
725
210
3
3.0
2169
5.2
725
677
48
58.5
Poor
Comp. ex.


334
730
7
217
3.9
2184
6.9
730
673
57
66.9
Good
Comp. ex.


335
732
209
8
3.4
2190
5.6
732
710
22
69.1
Poor
Comp. ex.


336
745
88
95
4.3
2229
6.7
745
688
57
85.9
Good
Inv. ex.


337
727
82
122
2.9
2175
6.1
727
673
54
82.2
Good
Inv. ex.


338
787
67
123
1.5
2353
5.2
787
735
52
72.8
Good
Inv. ex.


339
759
63
123
3.1
2269
5.2
759
728
31
77.1
Good
Inv. ex.


340
730
74
147
2.1
2184
5.7
730
665
65
84.5
Good
Inv. ex.


341
644
206
5
2.8
2125
6.4
644
598
46
60.5
Poor
Comp. ex.


342
630
201
8
3.0
2079
6.6
630
590
40
61.5
Poor
Comp. ex.


343
649
202
6
2.9
2142
6.2
649
622
27
60.9
Poor
Comp. ex.









In the examples, in the same way as the case of Example B, the impact resistance of the hot stamped body was evaluated from the viewpoint of variation in hardness as well. A cross-section of a long shaped hot stamped body vertical to the long direction was taken at any position in that long direction and measured for hardness of the middle position in sheet thickness in the entire cross-sectional region including the vertical walls. For the measurement, a Vickers tester was used. The measurement load was 1 kgf and the measurement intervals were 1 mm. A case where there were no measurement points of below 100 Hv from the average value of all measurement points was evaluated as being small in variation of hardness, i.e., being excellent in strength stability, and as a result being excellent in impact resistance and marked as a passing level (good), while a case where there were measurement points of below 100 Hv was marked as a failing level (poor). More specifically, a case where a difference from an average value of hardness of all measurement points (average cross-sectional hardness in Table 16) and the value of the smallest hardness among all measurement points is 100 Hv was marked as passing and a case of more than 100 Hv was marked as failing.


Furthermore, in the examples, in the same way as the case of Example C, the impact resistance of the hot stamped body was evaluated from the viewpoint of ductility as well. Specifically, a tensile test of the hot stamped steel sheet was performed to find the uniform elongation of the steel sheet and evaluate the impact resistance. The tensile test was performed by preparing a No. 5 test piece described in JIS Z 2201 and following the test method described in JIS Z 2241. The elongation at which the greatest tensile load was obtained was defined as the “uniform elongation”.


In the same way as the case of Example A, a case where the tensile strength is 1500 MPa or more, the maximum bending angle)(° is 70)(° or more, and the hydrogen embrittlement resistance is of the passing level was evaluated as a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance (examples in Table 16). Further, a case where the uniform elongation is 5% or more and the average cross-sectional hardness-minimum hardness is 100 Hv or less was evaluated as improved in impact resistance even from the viewpoint of ductility and strength stability in addition to bendability (invention examples other than Examples 310, 311, and 313 to 315 in Table 16). On the other hand, a case where even one of the requirements of “tensile strength”, “maximum bending angle”, and “hydrogen embrittlement resistance” failed to be satisfied was designated as a comparative example.

Claims
  • 1. A hot stamped body comprising: a middle part in sheet thickness; an intermediate layer; and a surface layer, the intermediate layer adjoining the middle part in sheet thickness and the surface layer, wherein the middle part in sheet thickness comprises, by mass %,C: 0.20% or more and less than 0.70%Si: less than 3.00%,Mn: 0.20% or more and less than 3.00%,P: 0.10% or less,S: 0.10% or less,sol. Al: 0.0002% or more and 3.0000% or less,N: 0.01% or less, anda balance of Fe and unavoidable impurities,the middle part in sheet thickness has a hardness of 500 Hv or more and 800 Hv or less,the surface layer has a hardness change ΔH1 in the sheet thickness direction of 10 Hv or more and less than 200 Hv, andthe intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 50 Hv or more and less than 200 Hv.
  • 2. The hot stamped body according to claim 1, wherein the Si content of the middle part in sheet thickness is 0.50% or less and the Mn content of the middle part in sheet thickness is 0.20% or more and less than 1.50%.
  • 3. The hot stamped body according to claim 1, wherein the Si content of the middle part in sheet thickness is 0.50% or less and the Mn content of the middle part in sheet thickness is 1.50% or more and less than 3.00%.
  • 4. The hot stamped body according to claim 1, wherein the Si content of the middle part in sheet thickness is more than 0.50% and less than 3.00%, the Mn content of the middle part in sheet thickness is 0.20% or more and less than 1.50%, andthe middle part in sheet thickness comprises, by area percent, 1.0% or more and less than 5.0% of residual austenite.
  • 5. The hot stamped body according to claim 1, wherein the Si content of the middle part in sheet thickness is more than 0.50% and less than 3.00%, the Mn content of the middle part in sheet thickness is 1.50% or more and less than 3.00%, andthe middle part in sheet thickness comprises, by area percent, 1.0% or more and less than 5.0% of residual austenite.
  • 6. The hot stamped body according to claim 1, wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.
  • 7. The hot stamped body according to claim 1, wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.
  • 8. The hot stamped body according to claim 1, further comprising a plated layer at the surface of the each surface layer.
  • 9. The hot stamped body according to claim 2, wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.
  • 10. The hot stamped body according to claim 3, wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.
  • 11. The hot stamped body according to claim 4, wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.
  • 12. The hot stamped body according to claim 5, wherein the middle part in sheet thickness further comprises, by mass %, Ni: 0.01% or more and 3.00% or less.
  • 13. The hot stamped body according to claim 2, wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.
  • 14. The hot stamped body according to claim 3, wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.
  • 15. The hot stamped body according to claim 4, wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.
  • 16. The hot stamped body according to claim 5, wherein the middle part in sheet thickness further comprises, by mass %, one or more of Nb: 0.010% or more and 0.150% or less, Ti: 0.010% or more and 0.150% or less, Mo: 0.005% or more and 1.000% or less, and B: 0.0005% or more and 0.0100% or less.
  • 17. The hot stamped body according to claim 2, further comprising a plated layer at the surface of the surface layer.
  • 18. The hot stamped body according to claim 3, further comprising a plated layer at the surface of the surface layer.
  • 19. The hot stamped body according to claim 4, further comprising a plated layer at the surface of the surface layer.
  • 20. The hot stamped body according to claim 5, further comprising a plated layer at the surface of the surface layer.
Priority Claims (1)
Number Date Country Kind
2017-029300 Feb 2017 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2018/006078 2/20/2018 WO 00