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 100 Hv or more and less than 200 Hv, and the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 10 Hv or more and less than 50 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 ease the concentration of stress at the time of bending deformation and suppress the occurrence of cracking. Furthermore, they discovered that by controlling the gradient of hardness inside the intermediate layer, even if cracks occur, the effect of suppressing their progression can be obtained. As a result, they succeeded in securing a 1500 MPa or more tensile strength and excellent hydrogen embrittlement resistance while realizing 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 raise the hardenability to reduce the variation in hardness at the stamped body, i.e., to stably secure a high strength and, furthermore, it is possible to secure structures contributing to improvement of deformability and thereby 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 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 100 Hv or more and less than 200 Hv, and


the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 10Hv or more and less than 50 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% to 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 0.50% may be added 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 100 Hv or more and less than 200 Hv, and the intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 10 Hv or more and less than 50 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 100 Hv or more and less than 200 Hv, an excellent hydrogen embrittlement resistance is secured while an excellent bendability is 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 100 Hv or more, the effect of easing the stress at the time of bending deformation is obtained. Therefore, the lower limit is 100 Hv, preferably 110 Hv or more, more preferably 120 Hv or more. Further, if is 200 Hv or more, penetration of hydrogen from the hot stamped body surface is aggravated and deterioration of the hydrogen embrittlement resistance is invited. Therefore, the upper limit is less than 200 Hv. Preferably, it is 190 Hv, more preferably 180 Hv or less.


Similarly, if ΔH2 is 10 Hv or more and less than 50 Hv, excellent bendability can be obtained. With an ΔH2 of less than 50 Hv, the effect of easing the concentration of stress at the time of bending deformation was raised and excellent bendability could be obtained. Therefore, the upper limit is less than 50 Hv. Preferably it is 45 Hv or less, more preferably 40 Hv or less. On the other hand, if ΔH2 is less than 10 Hv, it becomes difficult to ease the concentration of stress at the time of bending deformation and the bendability remarkably deteriorates. Therefore, the lower limit is 10 Hv. Preferably, it is 15 Hv or more, more preferably 20 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.









[

Mathematical





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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 60 minutes or more. 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 100 Hv or more and less than 200 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 10 Hv or more and less than 50 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 60 minutes or more. The upper limit is not particularly limited, but if holding for more than 300 minutes, the heating cost greatly rises and the result becomes economically disadvantageous. Therefore, in actual operation, 300 minutes is the substantive upper limit.


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 ΔHI 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 JIS 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
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


3
0.32
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


4
0.43
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


5
0.11
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


6
0.22
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


7
0.27
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


8
0.30
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


9
0.74
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


10
0.28
0.41
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


11
0.26
0.16
0.11
0.007
0.0003
0.043
0.0030
0
0
0
0
0


12
0.29
0.16
0.80
0.007
0.0003
0.043
0.0030
0
0
0
0
0


13
0.27
0.16
1.28
0.007
0.0003
0.043
0.0030
0.02
0
0
0
0


14
0.27
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0.047
0
0
0


15
0.27
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0.023
0
0


16
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0.01
0


17
0.27
0.16
1.28
0.007
0.0003
0.043
0.0030
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
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


3
0.32
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


3
0.32
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


3
0.32
0.16
1.27
0.009
0.0003
0.041
0.0035
0
0
0
0
0


4
0.43
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


4
0.43
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


4
0.43
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


18
0.66
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


18
0.64
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
0.16
1.28
0.007
0.0003
0.043
0.0030
0
0
0
0
0


2
0.28
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.















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
0.084
0.094
0.595
0.010
0.0014
0.041
0.0031
0
0
0
0
0


2
2
0.140
0.086
0.576
0.012
0.0015
0.040
0.0030
0
0
0
0
0


3
3
0.142
0.085
0.622
0.008
0.0015
0.042
0.0033
0
0
0
0
0


4
4
0.214
0.082
0.627
0.012
0.0004
0.041
0.0030
0
0
0
0
0


5
5
0.049
0.077
0.627
0.012
0.0007
0.040
0.0029
0
0
0
0
0


6
6
0.104
0.077
0.627
0.007
0.0017
0.043
0.0029
0
0
0
0
0


7
7
0.135
0.082
0.602
0.011
0.0009
0.042
0.0034
0
0
0
0
0


8
8
0.160
0.082
0.589
0.012
0.0005
0.042
0.0032
0
0
0
0
0


9
9
0.354
0.072
0.640
0.007
0.0006
0.043
0.0031
0
0
0
0
0


10
10
0.127
0.226
0.678
0.012
0.0016
0.040
0.0029
0
0
0
0
0


11
11
0.143
0.086
0.056
0.007
0.0017
0.041
0.0032
0
0
0
0
0


12
12
0.143
0.086
0.360
0.007
0.0016
0.041
0.0032
0
0
0
0
0


13
13
0.149
0.085
0.666
0.009
0.0012
0.041
0.0033
0.03
0
0
0
0


14
14
0.149
0.074
0.640
0.008
0.0005
0.040
0.0030
0
0.049
0
0
0


15
15
0.139
0.082
0.627
0.008
0.0018
0.043
0.0029
0
0
0.018
0
0


16
16
0.146
0.086
0.589
0.009
0.0018
0.040
0.0033
0
0
0
0.03
0


17
17
0.128
0.086
0.627
0.012
0.0004
0.042
0.0032
0
0
0
0
0.0018


18
1
0.092
0.180
1.178
0.008
0.0015
0.041
0.0030
0
0
0
0
0


19
1
0.086
0.178
0.608
0.008
0.0004
0.043
0.0029
0
0
0
0
0


20
1
0.107
0.098
1.104
0.008
0.0011
0.043
0.0029
0
0
0
0
0


21
2
0.246
0.066
0.653
0.007
0.0008
0.042
0.0033
0
0
0
0
0


22
2
0.244
0.085
1.101
0.008
0.0015
0.039
0.0032
0
0
0
0
0


23
2
0.244
0.144
0.576
0.009
0.0005
0.043
0.0029
0
0
0
0
0


24
3
0.243
0.070
0.597
0.009
0.0005
0.042
0.0033
0
0
0
0
0


25
3
0.158
0.152
0.622
0.012
0.0016
0.040
0.0029
0
0
0
0
0


26
3
0.139
0.075
1.118
0.009
0.0009
0.043
0.0030
0
0
0
0
0


27
4
0.389
0.086
0.678
0.011
0.0010
0.042
0.0033
0
0
0
0
0


28
4
0.231
0.149
0.563
0.012
0.0006
0.040
0.0031
0
0
0
0
0


29
4
0.231
0.070
1.165
0.008
0.0007
0.040
0.0029
0
0
0
0
0


30
2
0.140
0.086
0.576
0.009
0.0009
0.040
0.0033
0
0
0
0
0


31
2
0.140
0.086
0.576
0.010
0.0014
0.040
0.0032
0
0
0
0
0


32
2
0.140
0.086
0.576
0.007
0.0003
0.042
0.0029
0
0
0
0
0


33
2
0.140
0.086
0.576
0.008
0.0016
0.042
0.0034
0
0
0
0
0


34
18
0.329
0.086
0.576
0.009
0.0012
0.041
0.0034
0
0
0
0
0


35
18
0.321
0.086
0.576
0.010
0.0018
0.043
0.0034
0
0
0
0
0


36
2
0.138
0.086
0.576
0.009
0.0015
0.041
0.0033
0
0
0
0
0


37
2
0.140
0.086
0.576
0.008
0.0011
0.041
0.0034
0
0
0
0
0


38
2
0.140
0.086
0.576
0.009
0.0009
0.040
0.0033
0
0
0
0
0


39
2
0.140
0.086
0.576
0.010
0.0014
0.040
0.0032
0
0
0
0
0


40
2
0.140
0.086
0.576
0.007
0.0003
0.042
0.0029
0
0
0
0
0





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


















TABLE 3









Hot rolling

Heat treatment step at hot stamping


























Rough
Thickness
No. of rolling
Finish
Coiling
Cold rolling


Average cooling rate



Thickness



Heating
Holding
rolling
reduction
operations with
temp.
temp.
Cold rolling
Heating
Heating
from heating temp,
Average cooling rate
Tempering

after hot


Man.
temp.
time
temp.
rate
time between passes
temp.
temp.
rate
rate
temp.
to 400° C.
from 400° C. to 200° C.
temp.

stamping


no.
(° C.)
(min)
(° C.)
(%)
of 3 sec or more
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
(° C./s)
(° C./s)
(° C.)
Plating
(mm)

























1
1236
102
1169
38
3
878
704
55
34
841
73
57
None
None
1.3


2
1193
99
1154
35
3
838
706
54
36
841
108
96
None
None
1.3


3
1256
95
1133
28
3
894
661
49
46
887
78
63
None
None
1.4


4
1187
99
1160
34
3
917
653
47
54
920
95
81
None
None
1.5


5
1118
129
1140
32
3
878
574
53
53
845
89
77
None
None
1.3


6
1235
129
1153
34
3
882
682
60
68
887
74
57
None
None
1.1


7
1199
85
1190
38
3
880
684
51
66
823
91
79
None
None
1.4


8
1228
119
1134
44
3
890
715
43
53
832
75
56
None
None
1.6


9
1114
109
1102
29
3
896
714
57
31
878
75
65
None
None
1.2


10
1115
112
1109
34
3
842
567
45
46
836
76
57
None
None
1.5


11
1175
116
1135
33
3
881
710
57
55
904
94
79
None
None
1.2


12
1247
88
1189
39
3
844
545
54
57
873
87
69
None
None
1.3


13
1135
92
1117
30
3
868
652
45
27
894
89
79
None
None
1.5


14
1122
95
1118
40
3
915
619
54
40
828
80
60
None
None
1.3


15
1179
78
1166
36
3
847
692
44
22
872
80
66
None
None
1.6


16
1239
126
1139
36
3
845
692
45
34
890
99
85
None
None
1.5


17
1156
112
1125
44
3
843
721
40
64
871
106
95
None
None
1.7


18
1257
122
1150
39
3
837
660
41
48
924
93
75
None
None
1.7


19
1108
99
1105
39
3
862
556
57
25
903
80
70
None
None
1.2


20
1187
109
1123
41
3
910
666
42
21
847
91
71
None
None
1.6


21
1269
71
1163
45
3
834
687
57
23
826
94
77
None
None
1.2


22
1155
102
1135
34
3
851
645
48
24
901
91
79
None
None
1.5


23
1130
92
1120
40
3
894
582
52
65
923
100
88
None
None
1.3


24
1118
105
1107
38
3
916
633
48
69
889
85
66
None
None
1.5


25
1230
102
1150
40
3
900
647
51
58
929
103
92
None
None
1.4


26
1163
122
1138
25
3
898
712
43
23
885
89
77
None
None
1.6


27
1117
119
1109
31
3
845
697
41
68
891
90
75
None
None
1.7


28
1189
85
1180
25
3
841
635
51
31
892
104
88
None
None
1.4


29
1228
102
1142
37
3
888
703
59
37
859
92
80
None
None
1.1


30
982
119
955
38
3
903
665
43
45
895
93
80
None
None
1.6


31
1390
88
1139
41
3
842
644
55
70
901
70
52
None
None
1.3


32
1113
17
1109
39
3
862
616
46
66
900
78
61
None
None
1.5


33
1151
95
1137
27
3
881
671
0
66
908
73
59
None
None
2.8


34
1131
126
1128
32
3
841
554
57
51
921
82
68
250
None
1.2


35
1154
78
1144
42
3
874
546
45
57
920
90
74
257
Yes
1.5


36
1150
85
1134
35
3
852
557
45
50
842
94
76
None
Yes
1.5


37
1121
105
1112
40
3
835
699
53
28
839
88
75
None
None
1.3


38
1135
126
1004
45
3
896
545
45
28
826
95
78
None
None
1.7


39
1108
71
1102
3
2
845
556
42
67
891
79
68
None
None
1.5


40
1189
92
1155
35
1
851
665
51
31
895
107
94
None
None
1.7




















TABLE 4









Microstructure
Mechanical properties
















Hardness of middle



Max. bending
Hydrogen



Man.
part in sheet thickness
ΔH1
ΔH2
Tensile strength
angle
embrittlement


no.
(Hv)
(Hv)
(Hv)
(MPa)
(°)
resistance
Remarks

















1
514
187
48
1697
106.7
Good
Inv. ex.


2
644
171
32
2124
103.4
Good
Inv. ex.


3
716
166
47
2362
101.3
Good
Inv. ex.


4
786
128
34
2594
99.6
Good
Inv. ex.


5
385
197
42
1150
109.8
Good
Comp. ex.


6
572
188
49
1887
104.8
Good
Inv. ex.


7
615
114
15
2029
104.4
Good
Inv. ex.


8
672
187
46
2219
102.2
Good
Inv. ex.


9
897
188
41
2960
61.7
Good
Comp. ex.


10
644
177
43
2124
103.0
Good
Inv. ex.


11
471
174
45
1443
103.3
Good
Comp. ex.


12
652
113
27
2151
103.5
Good
Inv. ex.


13
640
136
35
2111
103.4
Good
Inv. ex.


14
648
141
23
2137
103.6
Good
Inv. ex.


15
643
144
27
2121
103.5
Good
Inv. ex.


16
649
187
46
2141
102.9
Good
Inv. ex.


17
643
177
49
2121
103.0
Good
Inv. ex.


18
517
181
46
1707
108.1
Good
Inv. ex.


19
518
185
47
1710
107.9
Good
Inv. ex.


20
512
187
43
1690
105.4
Good
Inv. ex.


21
641
168
31
2114
101.9
Good
Inv. ex.


22
640
165
32
2111
102.8
Good
Inv. ex.


23
643
172
29
2121
100.4
Good
Inv. ex.


24
720
158
45
2375
97.1
Good
Inv. ex.


25
720
161
44
2375
98.5
Good
Inv. ex.


26
718
160
47
2368
99.4
Good
Inv. ex.


27
782
154
32
2830
96.8
Good
Inv. ex.


28
791
121
34
2840
97.4
Good
Inv. ex.


29
788
137
31
2840
99.9
Good
Inv. ex.


30
642
212
4
2118
69.1
Poor
Comp. ex.


31
637
7
259
2101
62.8
Good
Comp. ex.


32
642
245
3
2118
66.1
Poor
Comp. ex.


33
640
168
43
2111
103.3
Good
Inv. ex.


34
643
145
31
2156
101.4
Good
Inv. ex.


35
652
158
26
2144
101.5
Good
Inv. ex.


36
651
171
32
2147
107.7
Good
Inv. ex.


37
635
178
31
2096
99.8
Good
Inv. ex.


38
644
209
5
2114
60.1
Poor
Comp. ex.


39
642
214
7
2121
62.6
Poor
Comp. ex.


40
652
210
8
2147
62.0
Poor
Comp. ex.









A case where the tensile strength is 1500 MPa or more, the maximum bending angle (°) is 90(°) 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 136 and 138 to 140 are steels with surface layer steel sheets welded to both surfaces, Manufacturing No. 137 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
0.21
0.18
1.74
0.014
0.0029
0.045
0.0036
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


103
0.33
0.12
1.80
0.009
0.0013
0.042
0.0035
0
0
0
0
0


104
0.43
0.15
1.73
0.013
0.0018
0.045
0.0035
0
0
0
0
0


105
0.10
0.16
1.70
0.010
0.0013
0.042
0.0034
0
0
0
0
0


106
0.32
0.12
1.84
0.007
0.0013
0.039
0.0035
0
0
0
0
0


107
0.32
0.19
1.77
0.005
0.0033
0.046
0.0031
0
0
0
0
0


108
0.37
0.16
1.88
0.003
0.0003
0.043
0.0027
0
0
0
0
0


109
0.78
0.12
1.85
0.005
0.0023
0.043
0.0036
0
0
0
0
0


110
0.28
0.39
1.81
0.008
0.0013
0.046
0.0029
0
0
0
0
0


111
0.34
0.12
0.11
0.008
0.0023
0.039
0.0028
0
0
0
0
0


112
0.36
0.12
0.80
0.008
0.0013
0.047
0.0034
0
0
0
0
0


113
0.37
0.16
1.71
0.008
0.0023
0.046
0.0031
1.70
0
0
0
0


114
0.32
0.17
1.69
0.013
0.0033
0.044
0.0028
0
0.082
0
0
0


115
0.38
0.13
1.81
0.009
0.0033
0.043
0.0032
0
0
0.078
0
0


116
0.28
0.18
1.84
0.012
0.0013
0.045
0.0036
0
0
0
0.06
0


117
0.28
0.12
1.80
0.011
0.0013
0.045
0.0033
0
0
0
0
0.0025


101
0.21
0.18
1.74
0.014
0.0029
0.045
0.0036
0
0
0
0
0


101
0.21
0.18
1.74
0.014
0.0029
0.045
0.0036
0
0
0
0
0


101
0.21
0.18
1.74
0.014
0.0029
0.045
0.0036
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


103
0.33
0.12
1.80
0.009
0.0013
0.042
0.0035
0
0
0
0
0


103
0.33
0.12
1.80
0.009
0.0013
0.042
0.0035
0
0
0
0
0


103
0.33
0.12
1.80
0.009
0.0013
0.042
0.0035
0
0
0
0
0


104
0.43
0.15
1.73
0.013
0.0018
0.045
0.0035
0
0
0
0
0


104
0.43
0.15
1.73
0.013
0.0018
0.045
0.0035
0
0
0
0
0


104
0.43
0.15
1.73
0.013
0.0018
0.045
0.0035
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


118
0.68
0.19
1.80
0.012
0.0032
0.039
0.0029
0
0
0
0
0


118
0.68
0.19
1.80
0.012
0.0032
0.039
0.0029
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0


102
0.29
0.14
1.82
0.003
0.0023
0.044
0.0032
0
0
0
0
0





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
0.09
0.08
0.80
0.011
0.0014
0.043
0.0029
0
0
0
0
0


102
102
0.14
0.08
0.75
0.010
0.0015
0.041
0.0030
0
0
0
0
0


103
103
0.15
0.06
0.86
0.010
0.0013
0.041
0.0035
0
0
0
0
0


104
104
0.22
0.07
0.90
0.009
0.0005
0.042
0.0030
0
0
0
0
0


105
105
0.04
0.07
0.88
0.012
0.0008
0.040
0.0031
0
0
0
0
0


106
106
0.14
0.06
0.88
0.004
0.0017
0.045
0.0031
0
0
0
0
0


107
107
0.17
0.09
0.89
0.014
0.0007
0.042
0.0035
0
0
0
0
0


108
108
0.18
0.08
0.85
0.009
0.0005
0.042
0.0033
0
0
0
0
0


109
109
0.34
0.05
0.93
0.009
0.0004
0.044
0.0030
0
0
0
0
0


110
110
0.05
0.22
0.91
0.011
0.0018
0.041
0.0027
0
0
0
0
0


111
111
0.19
0.06
0.05
0.008
0.0019
0.042
0.0033
0
0
0
0
0


112
112
0.17
0.06
0.36
0.006
0.0015
0.041
0.0030
0
0
0
0
0


113
113
0.20
0.09
0.91
0.011
0.0010
0.039
0.0034
0.01
0
0
0
0


114
114
0.16
0.07
0.81
0.010
0.0003
0.042
0.0032
0
0.038
0
0
0


115
115
0.19
0.06
0.80
0.010
0.0019
0.044
0.0030
0
0
0.011
0
0


116
116
0.14
0.10
0.83
0.009
0.0020
0.042
0.0034
0
0
0
0.02
0


117
117
0.14
0.06
0.79
0.013
0.0003
0.044
0.0034
0
0
0
0
0.0012


118
101
0.08
0.17
1.57
0.007
0.0016
0.041
0.0029
0
0
0
0
0


119
101
0.08
0.16
0.82
0.010
0.0002
0.042
0.0029
0
0
0
0
0


120
101
0.10
0.09
1.60
0.008
0.0012
0.041
0.0031
0
0
0
0
0


121
102
0.24
0.06
0.87
0.004
0.0007
0.040
0.0033
0
0
0
0
0


122
102
0.24
0.07
1.58
0.009
0.0017
0.039
0.0033
0
0
0
0
0


123
102
0.26
0.12
0.86
0.011
0.0003
0.045
0.0028
0
0
0
0
0


124
103
0.26
0.05
0.88
0.007
0.0005
0.044
0.0031
0
0
0
0
0


125
103
0.17
0.12
0.86
0.015
0.0018
0.042
0.0029
0
0
0
0
0


126
103
0.14
0.06
1.49
0.007
0.0007
0.042
0.0030
0
0
0
0
0


127
104
0.39
0.08
0.83
0.010
0.0012
0.041
0.0033
0
0
0
0
0


128
104
0.22
0.14
0.81
0.015
0.0005
0.041
0.0032
0
0
0
0
0


129
104
0.25
0.06
1.51
0.006
0.0007
0.038
0.0031
0
0
0
0
0


130
102
0.14
0.08
0.86
0.007
0.0011
0.042
0.0034
0
0
0
0
0


131
102
0.14
0.07
0.80
0.012
0.0014
0.041
0.0032
0
0
0
0
0


132
102
0.14
0.08
0.86
0.005
0.0001
0.040
0.0030
0
0
0
0
0


133
102
0.15
0.07
0.86
0.011
0.0014
0.041
0.0034
0
0
0
0
0


134
102
0.15
0.07
0.86
0.012
0.0013
0.039
0.0035
0
0
0
0
0


135
118
0.31
0.10
0.81
0.010
0.0018
0.044
0.0032
0
0
0
0
0


136
118
0.32
0.10
0.76
0.010
0.0017
0.039
0.0031
0
0
0
0
0


137
102
0.13
0.08
0.76
0.005
0.0013
0.041
0.0035
0
0
0
0
0


138
102
0.14
0.08
0.75
0.010
0.0015
0.041
0.0030
0
0
0
0
0


139
102
0.14
0.08
0.75
0.010
0.0015
0.041
0.0030
0
0
0
0
0


140
102
0.14
0.08
0.75
0.010
0.0015
0.041
0.0030
0
0
0
0
0





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


















TABLE 7









Hot rolling

Heat treatment step at hot stamping


























Rough
Thickness
No. of rolling
Finish
Coiling
Cold rolling


Average cooling rate



Thickness



Heating
Holding
rolling
reduction
operations with
temp.
temp.
Cold rolling
Heating
Heating
from heating temp.
Average cooling rate
Tempering

after hot


Man.
temp.
time
temp.
rate
time between passes
temp.
temp.
rate
rate
temp.
to 400° C.
from 400° C. to 200° C.
temp.

stamping


no.
(° C.)
(min)
(° C.)
(%)
of 3 sec or more
(° C.)
(° C.)
(%)
(° C/s)
(° C.)
(° C./s)
(° C./s)
(° C.)
Plating
(mm)

























101
1263
97
1159
36
3
888
604
53
35
904
72
67
None
None
1.3


102
1235
94
1149
33
3
881
629
47
41
868
103
93
None
None
1.5


103
1244
90
1143
24
3
842
660
53
51
845
72
67
None
None
1.3


104
1272
98
1163
31
3
909
656
53
56
915
95
87
None
None
1.3


105
1286
129
1138
32
3
887
620
44
50
853
84
78
None
None
1.6


106
1268
133
1149
39
3
833
556
52
69
901
83
75
None
None
1.3


107
1274
89
1200
36
3
833
621
50
69
926
97
92
None
None
1.4


108
1266
111
1134
45
3
855
686
46
54
827
85
78
None
None
1.5


109
1282
117
1160
28
3
869
637
44
27
919
81
72
None
None
1.6


110
1293
107
1143
33
3
887
720
54
44
907
85
79
None
None
1.3


111
1253
119
1128
37
3
836
662
46
58
823
93
88
None
None
1.5


112
1278
90
1186
42
3
844
545
49
54
873
94
88
None
None
1.4


113
1245
94
1187
25
3
876
614
45
29
881
81
73
None
None
1.5


114
1293
101
1144
37
3
837
557
57
38
843
72
63
None
None
1.2


115
1250
82
1160
35
3
891
566
49
21
830
87
78
None
None
1.4


116
1268
125
1141
37
3
892
590
50
38
872
93
85
None
None
1.4


117
1279
103
1126
40
3
915
556
48
59
908
99
89
None
None
1.5


118
1256
126
1155
35
3
880
679
46
44
831
87
82
None
None
1.5


119
1242
99
1162
36
3
865
708
49
21
872
71
61
None
None
1.4


120
1276
103
1124
45
3
892
703
46
26
839
98
91
None
None
1.5


121
1284
71
1153
48
3
891
684
48
22
870
88
83
None
None
1.5


122
1266
104
1163
34
3
831
632
46
25
856
90
83
None
None
1.5


123
1265
85
1125
38
3
903
734
57
64
900
107
100
None
None
1.2


124
1258
95
1155
36
3
873
641
46
72
900
93
84
None
None
1.5


125
1266
97
1159
45
3
874
641
52
56
870
110
100
None
None
1.3


126
1273
125
1129
29
3
911
546
49
18
891
80
71
None
None
1.4


127
1255
121
1186
32
3
880
697
52
67
865
88
79
None
None
1.3


128
1251
76
1173
23
3
862
698
50
28
889
95
86
None
None
1.4


129
1295
109
1133
32
3
892
706
50
34
846
89
80
None
None
1.4


130
971
125
951
34
3
855
588
46
48
900
85
80
None
None
1.5


131
1364
81
1131
46
3
870
663
51
68
921
70
61
None
None
1.4


132
1284
18
1150
36
3
862
686
57
62
870
74
64
None
None
1.2


133
1281
96
1140
29
3
835
612
46
61
857
71
62
None
None
1.5


134
1280
128
1129
37
3
857
619
0
48
883
74
66
None
None
2.8


135
1290
74
1142
43
3
853
654
55
60
825
96
86
269
None
1.3


136
1277
83
1172
39
3
864
576
49
46
915
103
94
251
Yes
1.4


137
1281
115
1128
41
3
847
709
46
31
893
91
81
None
Yes
1.5


138
1276
119
1002
42
3
892
590
53
29
870
95
86
None
None
1.4


139
1266
82
1162
4
2
873
708
45
68
900
86
76
None
None
1.4


140
1251
103
1168
38
1
880
684
57
28
846
113
104
None
None
2.8




















TABLE 8









Microstructure
Mechanical properties



















Hardness of





Average cross-
Max.





middle part in


Tensile
Average cross-
Minimum
sectional hardness-
bending
Hydrogen


Man.
sheet thickness
ΔH1
ΔH2
strength
sectional hardness
hardness
Minimum hardness
angle
embrittlement


no.
(Hv)
(Hv)
(Hv)
(MPa)
(Hv)
(Hv)
(Hv)
(°)
resistance
Remarks




















101
539
192
45
1613
539
475
64
99.7
Good
Inv. ex.


102
651
173
38
1948
651
612
39
96.4
Good
Inv. ex.


103
715
169
46
2138
715
651
64
95.3
Good
Inv. ex.


104
790
131
28
2362
790
745
45
91.6
Good
Inv. ex.


105
401
196
39
1199
401
354
47
103.2
Good
Comp. ex.


106
697
190
44
2083
697
663
34
97.8
Good
Inv. ex.


107
695
110
11
2077
695
631
64
101.4
Good
Inv. ex.


108
769
181
41
2298
769
735
34
101.2
Good
Inv. ex.


109
906
184
40
2990
906
862
44
54.2
Good
Comp. ex.


110
644
178
37
1926
644
601
43
95.0
Good
Inv. ex.


111
462
169
49
1401
462
304
158
103.5
Good
Comp. ex.


112
715
110
26
2138
715
579
136
98.5
Good
Inv. ex.


113
768
137
32
2295
768
702
66
102.4
Good
Inv. ex.


114
701
142
27
2095
701
672
29
100.6
Good
Inv. ex.


115
781
140
27
2335
781
737
44
97.5
Good
Inv. ex.


116
645
190
33
1929
645
589
56
94.9
Good
Inv. ex.


117
643
173
39
1923
643
598
45
101.6
Good
Inv. ex.


118
543
179
47
1625
543
478
65
97.1
Good
Inv. ex.


119
538
187
45
1610
538
504
34
97.9
Good
Inv. ex.


120
543
185
41
1625
543
517
26
97.7
Good
Inv. ex.


121
651
164
28
1948
651
594
57
97.7
Good
Inv. ex.


122
655
160
30
1960
655
581
74
98.0
Good
Inv. ex.


123
658
167
32
1969
658
598
60
96.5
Good
Inv. ex.


124
710
154
42
2123
710
683
27
96.6
Good
Inv. ex.


125
707
163
48
2114
707
676
31
96.6
Good
Inv. ex.


126
712
158
43
2129
712
675
37
97.3
Good
Inv. ex.


127
781
155
34
2335
781
741
40
96.9
Good
Inv. ex.


128
788
121
34
2356
788
751
37
97.2
Good
Inv. ex.


129
779
132
27
2329
779
728
51
98.1
Good
Inv. ex.


130
656
210
9
1963
656
611
45
61.1
Poor
Comp. ex.


131
655
5
219
1960
655
600
55
62.8
Good
Comp. ex.


132
650
221
5
1945
650
601
49
69.1
Poor
Comp. ex.


133
659
117
41
1972
659
599
60
90.2
Good
Inv. ex.


134
657
168
49
1966
657
581
76
96.3
Good
Inv. ex.


135
721
140
31
2156
721
660
61
92.4
Good
Inv. ex.


136
718
157
32
2147
718
653
65
92.5
Good
Inv. ex.


137
659
171
27
1972
659
584
75
102.1
Good
Inv. ex.


138
655
201
6
2162
655
622
33
59.5
Poor
Comp. ex.


139
662
211
7
2185
662
627
35
63.8
Poor
Comp. ex.


140
641
204
4
2115
641
612
29
60.9
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 90(°) 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 112 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
0.22
1.63
1.33
0.011
0.0020
0.046
0.0027
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


203
0.31
1.45
1.25
0.006
0.0007
0.040
0.0040
0
0
0
0
0


204
0.49
1.50
1.34
0.010
0.0005
0.057
0.0028
0
0
0
0
0


205
0.07
1.48
1.23
0.008
0.0002
0.029
0.0033
0
0
0
0
0


206
0.23
1.19
1.23
0.004
0.0006
0.055
0.0035
0
0
0
0
0


207
0.29
1.06
1.31
0.009
0.0004
0.037
0.0025
0
0
0
0
0


208
0.31
1.44
1.20
0.003
0.0003
0.053
0.0027
0
0
0
0
0


209
0.79
1.11
1.31
0.005
0.0003
0.040
0.0028
0
0
0
0
0


210
0.34
0.21
1.25
0.007
0.0004
0.041
0.0031
0
0
0
0
0


211
0.29
0.44
0.84
0.007
0.0006
0.057
0.0033
0
0
0
0
0


212
0.27
1.27
0.09
0.009
0.0002
0.057
0.0028
0
0
0
0
0


213
0.29
1.41
1.31
0.006
0.0007
0.057
0.0034
1.14
0
0
0
0


214
0.23
1.47
1.21
0.004
0.0007
0.035
0.0026
0
0.032
0
0
0


215
0.33
1.67
1.22
0.006
0.0003
0.062
0.0033
0
0
0.078
0
0


216
0.27
1.48
1.34
0.007
0.0006
0.042
0.0033
0
0
0
0.04
0


217
0.33
1.26
1.28
0.011
0.0007
0.055
0.0026
0
0
0
0
0.0023


201
0.22
1.63
1.33
0.011
0.0020
0.046
0.0027
0
0
0
0
0


201
0.22
1.63
1.33
0.011
0.0020
0.046
0.0027
0
0
0
0
0


201
0.22
1.63
1.33
0.011
0.0020
0.046
0.0027
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


203
0.31
1.45
1.25
0.006
0.0007
0.040
0.0040
0
0
0
0
0


203
0.31
1.45
1.25
0.006
0.0007
0.040
0.0040
0
0
0
0
0


203
0.31
1.45
1.25
0.006
0.0007
0.040
0.0040
0
0
0
0
0


204
0.49
1.50
1.34
0.010
0.0005
0.057
0.0028
0
0
0
0
0


204
0.49
1.50
1.34
0.010
0.0005
0.057
0.0028
0
0
0
0
0


204
0.49
1.50
1.34
0.010
0.0005
0.057
0.0028
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


218
0.69
1.21
1.34
0.011
0.0005
0.057
0.0027
0
0
0
0
0


218
0.69
1.21
1.34
0.011
0.0005
0.057
0.0027
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0


202
0.24
1.56
1.23
0.010
0.0005
0.054
0.0029
0
0
0
0
0





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
0.13
0.86
0.67
0.015
0.0017
0.046
0.0028
0
0
0
0
0


202
202
0.12
0.83
0.65
0.012
0.0016
0.036
0.0033
0
0
0
0
0


203
203
0.15
0.80
0.60
0.015
0.0018
0.041
0.0037
0
0
0
0
0


204
204
0.28
0.78
0.75
0.011
0.0006
0.040
0.0033
0
0
0
0
0


205
205
0.03
0.86
0.63
0.011
0.0010
0.039
0.0032
0
0
0
0
0


206
206
0.10
0.58
0.64
0.006
0.0021
0.039
0.0028
0
0
0
0
0


207
207
0.12
0.61
0.63
0.017
0.0007
0.038
0.0032
0
0
0
0
0


208
208
0.15
0.72
0.65
0.011
0.0005
0.041
0.0035
0
0
0
0
0


209
209
0.40
0.60
0.69
0.014
0.0009
0.039
0.0027
0
0
0
0
0


210
210
0.16
0.12
0.68
0.016
0.0018
0.039
0.0025
0
0
0
0
0


211
211
0.13
0.24
0.42
0.012
0.0024
0.040
0.0031
0
0
0
0
0


212
212
0.12
0.65
0.04
0.011
0.0017
0.043
0.0026
0
0
0
0
0


213
213
0.15
0.78
0.72
0.015
0.0012
0.035
0.0031
0.05
0
0
0
0


214
214
0.12
0.76
0.59
0.009
0.0002
0.042
0.0033
0
0.028
0
0
0


215
215
0.19
0.97
0.67
0.014
0.0019
0.045
0.0029
0
0
0.018
0
0


216
216
0.15
0.78
0.72
0.010
0.0019
0.037
0.0036
0
0
0
0.03
0


217
217
0.14
0.67
0.60
0.018
0.0007
0.046
0.0032
0
0
0
0
0.0018


218
201
0.07
1.40
1.09
0.007
0.0018
0.042
0.0026
0
0
0
0
0


219
201
0.10
1.60
0.70
0.009
0.0005
0.039
0.0026
0
0
0
0
0


220
201
0.12
0.67
1.24
0.010
0.0017
0.044
0.0034
0
0
0
0
0


221
202
0.19
0.73
0.57
0.005
0.0007
0.036
0.0031
0
0
0
0
0


222
202
0.21
0.76
1.02
0.010
0.0016
0.033
0.0029
0
0
0
0
0


223
202
0.21
1.47
0.47
0.010
0.0007
0.042
0.0032
0
0
0
0
0


224
203
0.21
0.55
0.71
0.010
0.0007
0.044
0.0030
0
0
0
0
0


225
203
0.17
1.42
0.61
0.017
0.0022
0.042
0.0027
0
0
0
0
0


226
203
0.14
0.73
1.04
0.006
0.0010
0.041
0.0027
0
0
0
0
0


227
204
0.42
0.72
0.66
0.012
0.0017
0.034
0.0034
0
0
0
0
0


228
204
0.21
1.22
0.63
0.019
0.0010
0.034
0.0031
0
0
0
0
0


229
204
0.32
0.77
1.29
0.009
0.0006
0.039
0.0028
0
0
0
0
0


230
202
0.10
0.76
0.59
0.012
0.0015
0.041
0.0032
0
0
0
0
0


231
202
0.11
0.87
0.70
0.012
0.0018
0.040
0.0034
0
0
0
0
0


232
202
0.11
0.84
0.70
0.010
0.0006
0.039
0.0028
0
0
0
0
0


233
202
0.10
0.80
0.65
0.014
0.0014
0.043
0.0036
0
0
0
0
0


234
202
0.10
0.87
0.63
0.014
0.0012
0.035
0.0033
0
0
0
0
0


235
218
0.28
0.64
0.74
0.013
0.0020
0.038
0.0031
0
0
0
0
0


236
218
0.32
0.65
0.70
0.009
0.0022
0.038
0.0029
0
0
0
0
0


237
202
0.12
0.87
0.69
0.009
0.0015
0.036
0.0036
0
0
0
0
0


238
202
0.12
0.83
0.65
0.012
0.0016
0.036
0.0033
0
0
0
0
0


239
202
0.12
0.83
0.65
0.012
0.0016
0.036
0.0033
0
0
0
0
0


240
202
0.12
0.83
0.65
0.012
0.0016
0.036
0.0033
0
0
0
0
0





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


















TABLE 11









Hot rolling

Heat treatment step at hot stamping


























Rough
Thickness
No. of rolling
Finish
Coiling
Cold rolling


Average cooling rate



Thickness



Heating
Holding
rolling
reduction
operations with
temp.
temp.
Cold rolling
Heating
Heating
from heating temp.
Average cooling rate
Tempering

after hot


Man.
temp.
time
temp.
rate
time between passes
temp.
temp.
rate
rate
temp.
to 400° C.
from 400° C. to 200° C.
temp.

stamping


no.
(° C.)
(min)
(° C.)
(%)
of 3 sec or more
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
(° C./s)
(° C./s)
(° C.)
Plating
(mm)

























201
1260
101
1164
38
3
892
694
46
37
835
75
30
None
None
1.5


202
1237
91
1150
35
3
843
709
57
31
860
116
15
None
None
1.2


203
1239
104
1130
28
3
889
673
46
43
875
74
18
None
None
1.5


204
1279
98
1170
34
3
922
648
55
59
911
100
30
None
None
1.3


205
1286
122
1138
32
3
869
568
54
49
838
77
23
None
None
1.3


206
1274
127
1144
34
3
895
677
45
65
893
54
29
None
None
1.5


207
1282
101
1199
38
3
887
685
51
64
817
72
27
None
None
1.4


208
1262
112
1136
44
3
898
710
56
50
821
75
12
None
None
1.2


209
1291
112
1148
29
3
908
719
47
29
884
82
11
None
None
1.5


210
1296
101
1146
34
3
850
583
48
47
852
75
19
None
None
1.5


211
1259
124
1141
33
3
854
527
53
56
864
88
35
None
None
1.3


212
1273
89
1196
39
3
888
697
51
60
904
87
14
None
None
1.4


213
1249
89
1177
30
3
861
648
53
23
885
71
28
None
None
1.3


214
1288
104
1144
40
3
898
600
55
39
818
80
27
None
None
1.3


215
1246
80
1172
36
3
847
679
57
24
859
72
18
None
None
1.2


216
1269
120
1135
36
3
841
684
57
32
904
91
19
None
None
1.2


217
1280
105
1125
44
3
847
734
46
66
879
99
12
None
None
1.5


218
1261
117
1149
39
3
824
647
56
49
911
88
18
None
None
1.2


219
1245
93
1156
39
3
846
563
47
21
916
77
34
None
None
1.5


220
1282
117
1118
41
3
898
664
57
24
862
100
19
None
None
1.2


221
1281
73
1167
45
3
818
674
46
20
812
104
15
None
None
1.5


222
1262
111
1170
34
3
841
655
48
20
893
89
28
None
None
1.5


223
1269
96
1128
40
3
876
587
46
63
913
109
28
None
None
1.5


224
1263
95
1161
38
3
916
629
54
64
890
92
26
None
None
1.3


225
1275
97
1143
40
3
894
664
54
53
943
112
25
None
None
1.3


226
1268
119
1134
25
3
898
713
47
28
885
85
9
None
None
1.5


227
1259
131
1184
31
3
827
679
55
73
893
83
13
None
None
1.3


228
1247
80
1173
25
3
835
650
54
31
890
113
13
None
None
1.3


229
1305
102
1140
37
3
900
705
48
42
845
79
27
None
None
1.5


230
891
125
881
38
3
901
646
46
49
887
96
25
None
None
1.5


231
1392
79
1137
41
3
826
636
57
74
918
73
25
None
None
1.2


232
1290
16
1141
39
3
861
625
56
62
886
75
27
None
None
1.2


233
1278
97
1129
27
3
842
550
45
61
914
60
14
None
None
1.5


234
1276
128
1129
32
3
870
678
0
53
899
70
26
None
None
2.8


235
1291
83
1140
42
3
841
560
48
61
940
74
20
262
None
1.5


236
1274
89
1161
35
3
882
545
57
53
921
96
32
278
Yes
1.2


237
1283
110
1112
40
3
836
554
46
30
842
84
21
None
Yes
1.5


238
1282
117
1009
38
3
841
629
57
28
890
85
29
None
None
1.5


239
1275
95
1161
3
2
894
713
47
68
890
76
26
None
None
1.2


240
1247
119
1140
40
1
835
550
54
26
918
106
35
None
None
1.5




















TABLE 12









Microstructure
Mechanical properties


















Hardness of


Area rate of


Max.





middle part in


residual
Tensile
Uniform
bending
Hydrogen


Man.
sheet thickness
ΔH1
ΔH2
austenite
strength
elongation
angle
embrittlement


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



















201
529
191
48
3.3
1535
6.5
102.9
Good
Inv. ex.


202
654
175
35
4.0
1896
6.8
105.0
Good
Inv. ex.


203
725
175
48
3.4
2101
6.5
103.7
Good
Inv. ex.


204
792
132
35
2.0
2297
5.0
100.9
Good
Inv. ex.


205
411
187
44
2.7
1192
5.8
104.3
Good
Comp. ex.


206
588
192
45
2.7
1704
6.2
103.8
Good
Inv. ex.


207
622
122
14
3.4
1803
6.6
103.1
Good
Inv. ex.


208
687
195
39
2.3
1994
5.5
101.6
Good
Inv. ex.


209
908
197
41
1.8
2633
5.3
58.5
Good
Comp. ex.


210
664
181
48
0.4
1925
3.9
104.9
Good
Inv. ex.


211
665
117
28
0.8
1928
4.6
101.8
Good
Inv. ex.


212
397
182
48
2.1
1310
5.6
100.9
Good
Comp. ex.


213
663
144
39
3.9
1922
6.6
102.0
Good
Inv. ex.


214
664
148
20
4.1
1925
6.5
103.4
Good
Inv. ex.


215
648
152
29
4.1
1878
6.9
101.3
Good
Inv. ex.


216
653
193
48
1.9
1893
7.0
103.0
Good
Inv. ex.


217
661
181
45
3.0
1917
5.9
102.9
Good
Inv. ex.


218
518
184
40
4.4
1503
6.6
103.5
Good
Inv. ex.


219
522
172
43
3.0
1514
6.5
106.8
Good
Inv. ex.


220
521
197
36
2.7
1511
6.1
107.6
Good
Inv. ex.


221
662
157
21
2.0
1919
5.0
102.2
Good
Inv. ex.


222
660
163
31
3.7
1913
6.8
112.0
Good
Inv. ex.


223
651
164
27
2.8
1887
6.0
99.7
Good
Inv. ex.


224
730
167
40
2.6
2116
6.0
107.4
Good
Inv. ex.


225
721
154
48
3.2
2090
6.5
103.8
Good
Inv. ex.


226
734
148
44
4.1
2127
7.0
96.1
Good
Inv. ex.


227
777
152
28
2.3
2253
5.3
108.6
Good
Inv. ex.


228
780
122
31
2.3
2262
5.4
101.7
Good
Inv. ex.


229
791
138
24
2.6
2294
5.6
108.8
Good
Inv. ex.


230
651
218
3
3.3
1887
6.6
68.5
Poor
Comp. ex.


231
650
5
218
3.9
1884
6.9
62.7
Good
Comp. ex.


232
658
221
2
4.2
1908
5.7
66.6
Poor
Comp. ex.


233
651
128
23
3.8
1887
5.9
102.5
Good
Inv. ex.


234
652
177
47
3.5
1890
6.7
101.0
Good
Inv. ex.


235
735
152
31
2.4
2132
5.7
98.1
Good
Inv. ex.


236
744
162
30
2.5
2158
5.9
98.5
Good
Inv. ex.


237
650
175
30
2.3
1884
5.6
104.4
Good
Inv. ex.


238
635
201
4
2.8
2096
6.0
60.9
Poor
Comp. ex.


239
640
209
9
2.9
2112
6.5
62.8
Poor
Comp. ex.


240
655
207
6
3.2
2162
6.6
60.7
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 90(°) 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 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 sheet
Chemical constituents of matrix steel sheet (mass %)



















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






















301
0.21
1.42
1.77
0.021
0.0032
0.055
0.0031
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


303
0.35
1.58
1.71
0.014
0.0011
0.040
0.0027
0
0
0
0
0


304
0.44
1.44
1.98
0.019
0.0017
0.041
0.0041
0
0
0
0
0


305
0.10
1.27
1.86
0.014
0.0022
0.038
0.0043
0
0
0
0
0


306
0.29
1.43
1.88
0.007
0.0021
0.046
0.0044
0
0
0
0
0


307
0.33
1.78
1.79
0.008
0.0031
0.048
0.0036
0
0
0
0
0


308
0.39
1.73
1.97
0.004
0.0001
0.051
0.0032
0
0
0
0
0


309
0.82
1.69
1.83
0.012
0.0032
0.044
0.0029
0
0
0
0
0


310
0.31
0.24
2.00
0.010
0.0021
0.044
0.0019
0
0
0
0
0


311
0.26
0.39
1.92
0.010
0.0006
0.043
0.0032
0
0
0
0
0


312
0.34
1.23
0.11
0.007
0.0027
0.047
0.0038
0
0
0
0
0


313
0.35
1.18
0.80
0.009
0.0014
0.048
0.0040
0
0
0
0
0


314
0.29
0.32
0.22
0.010
0.0010
0.045
0.0029
0
0
0
0
0


315
0.26
0.41
0.76
0.009
0.0007
0.056
0.0026
0
0
0
0
0


316
0.40
1.58
1.78
0.010
0.0032
0.055
0.0032
2.21
0
0
0
0


317
0.36
1.07
1.75
0.014
0.0033
0.047
0.0022
0
0.078
0
0
0


318
0.36
1.64
1.98
0.015
0.0033
0.046
0.0025
0
0
0.046
0
0


319
0.31
1.29
1.90
0.016
0.0013
0.054
0.0031
0
0
0
0.05
0


320
0.31
1.40
1.72
0.018
0.0011
0.042
0.0041
0
0
0
0
0.0025


301
0.21
1.42
1.77
0.021
0.0032
0.055
0.0031
0
0
0
0
0


301
0.21
1.42
1.77
0.021
0.0032
0.055
0.0031
0
0
0
0
0


301
0.21
1.42
1.77
0.021
0.0032
0.055
0.0031
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


303
0.35
1.58
1.71
0.014
0.0011
0.040
0.0027
0
0
0
0
0


303
0.35
1.58
1.71
0.014
0.0011
0.040
0.0027
0
0
0
0
0


303
0.35
1.58
1.71
0.014
0.0011
0.040
0.0027
0
0
0
0
0


304
0.44
1.44
1.98
0.019
0.0017
0.041
0.0041
0
0
0
0
0


304
0.44
1.44
1.98
0.019
0.0017
0.041
0.0041
0
0
0
0
0


304
0.44
1.44
1.98
0.019
0.0017
0.041
0.0041
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


321
0.69
1.32
1.83
0.011
0.0035
0.032
0.0024
0
0
0
0
0


321
0.69
1.32
1.83
0.011
0.0035
0.032
0.0024
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0


302
0.29
1.35
1.95
0.008
0.0026
0.049
0.0025
0
0
0
0
0





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
















TABLE 14









Matrix










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




















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























301
301
0.10
0.75
0.90
0.012
0.0019
0.043
0.0029
0
0
0
0
0


302
302
0.15
0.66
0.98
0.013
0.0018
0.039
0.0037
0
0
0
0
0


303
303
0.20
0.65
0.75
0.014
0.0016
0.043
0.0040
0
0
0
0
0


304
304
0.23
0.78
0.99
0.013
0.0005
0.037
0.0030
0
0
0
0
0


305
305
0.05
0.56
0.95
0.010
0.0009
0.037
0.0031
0
0
0
0
0


306
306
0.17
0.72
0.83
0.007
0.0021
0.038
0.0029
0
0
0
0
0


307
307
0.15
0.71
0.84
0.016
0.0009
0.040
0.0033
0
0
0
0
0


308
308
0.16
0.81
1.02
0.010
0.0004
0.040
0.0033
0
0
0
0
0


309
309
0.42
0.73
0.95
0.014
0.0006
0.039
0.0023
0
0
0
0
0


310
310
0.13
0.11
0.96
0.017
0.0021
0.036
0.0029
0
0
0
0
0


311
311
0.12
0.20
1.00
0.015
0.0024
0.042
0.0032
0
0
0
0
0


312
312
0.14
0.57
0.06
0.011
0.0026
0.037
0.0028
0
0
0
0
0


313
313
0.20
0.57
0.37
0.010
0.0025
0.039
0.0028
0
0
0
0
0


314
314
0.14
0.16
0.10
0.013
0.0025
0.038
0.0035
0
0
0
0
0


315
315
0.11
0.21
0.37
0.008
0.0016
0.041
0.0022
0
0
0
0
0


316
316
0.23
0.68
0.89
0.014
0.0015
0.032
0.0032
0.07
0
0
0
0


317
317
0.20
0.47
0.84
0.011
0.0003
0.043
0.0029
0
0.021
0
0
0


318
318
0.14
0.87
0.91
0.016
0.0018
0.047
0.0028
0
0
0.001
0
0


319
319
0.18
0.61
0.95
0.007
0.0020
0.039
0.0039
0
0
0
0.03
0


320
320
0.15
0.71
0.81
0.021
0.0007
0.044
0.0033
0
0
0
0
0.0018


321
301
0.08
1.25
1.43
0.008
0.0017
0.040
0.0029
0
0
0
0
0


322
301
0.11
1.29
0.99
0.006
0.0006
0.040
0.0022
0
0
0
0
0


323
301
0.11
0.51
1.50
0.012
0.0016
0.045
0.0036
0
0
0
0
0


324
302
0.26
0.69
0.98
0.008
0.0010
0.038
0.0034
0
0
0
0
0


325
302
0.28
0.77
1.58
0.008
0.0014
0.033
0.0031
0
0
0
0
0


326
302
0.23
1.38
0.60
0.013
0.0010
0.039
0.0029
0
0
0
0
0


327
303
0.22
0.68
0.89
0.011
0.0008
0.046
0.0028
0
0
0
0
0


328
303
0.16
1.53
0.77
0.018
0.0021
0.044
0.0024
0
0
0
0
0


329
303
0.15
0.87
1.30
0.009
0.0011
0.042
0.0030
0
0
0
0
0


330
304
0.39
0.65
0.99
0.010
0.0018
0.037
0.0035
0
0
0
0
0


331
304
0.18
1.15
1.03
0.021
0.0013
0.032
0.0032
0
0
0
0
0


332
304
0.28
0.72
1.70
0.009
0.0007
0.037
0.0026
0
0
0
0
0


333
302
0.15
0.61
1.01
0.010
0.0016
0.039
0.0030
0
0
0
0
0


334
302
0.16
0.63
0.96
0.015
0.0016
0.039
0.0034
0
0
0
0
0


335
302
0.15
0.66
0.88
0.012
0.0007
0.036
0.0031
0
0
0
0
0


336
302
0.15
0.74
0.94
0.011
0.0016
0.045
0.0034
0
0
0
0
0


337
302
0.13
0.65
0.92
0.013
0.0010
0.034
0.0037
0
0
0
0
0


338
321
0.28
0.66
0.95
0.015
0.0023
0.037
0.0033
0
0
0
0
0


339
321
0.32
0.66
0.84
0.011
0.0024
0.035
0.0025
0
0
0
0
0


340
302
0.15
0.62
0.94
0.012
0.0016
0.035
0.0040
0
0
0
0
0


341
302
0.15
0.66
0.98
0.013
0.0018
0.039
0.0037
0
0
0
0
0


342
302
0.15
0.66
0.98
0.013
0.0018
0.039
0.0037
0
0
0
0
0


343
302
0.15
0.66
0.98
0.013
0.0018
0.039
0.0037
0
0
0
0
0





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


















TABLE 15









Hot rolling

Heat treatment step at hot stamping


























Rough
Thickness
No. of rolling
Finish
Coiling
Cold rolling


Average cooling rate



Thickness



Heating
Holding
rolling
reduction
operations with
temp.
temp.
Cold rolling
Heating
Heating
from heating temp.
Average cooling rate
Tempering

after hot


Man.
temp.
time
temp.
rate
time between passes
temp.
temp.
rate
rate
temp.
to 400° Ce.
from 400° C. to 200° C.
temp.

stamping


no.
(° C.)
(min)
(° C.)
(%)
of 3 sec or more
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
(° C./s)
(° C./s)
(° C.)
Plating
(mm)

























301
1252
91
1164
38
3
908
651
58
37
896
75
30
None
None
1.2


302
1235
101
1150
35
3
896
618
47
31
826
116
15
None
None
1.5


303
1238
100
1130
28
3
904
581
46
43
856
74
18
None
None
1.5


304
1271
92
1170
34
3
910
607
55
59
873
100
30
None
None
1.3


305
1284
127
1138
32
3
901
642
52
49
820
77
23
None
None
1.3


306
1275
127
1144
34
3
883
722
52
65
899
54
29
None
None
1.3


307
1277
102
1199
38
3
856
618
57
64
821
72
27
None
None
1.2


308
1250
121
1136
44
3
886
740
46
50
859
75
12
None
None
1.5


309
1281
105
1148
29
3
841
635
56
29
896
82
11
None
None
1.2


310
1292
99
1146
34
3
892
723
49
47
899
75
19
None
None
1.4


311
1262
127
1141
33
3
919
625
54
56
829
88
35
None
None
1.3


312
1263
99
1196
39
3
910
654
57
60
907
87
14
None
None
1.2


313
1247
87
1177
30
3
830
728
50
23
863
71
28
None
None
1.4


314
1288
113
1144
40
3
857
563
45
39
885
80
27
None
None
1.5


315
1243
78
1172
36
3
872
701
49
24
910
72
18
None
None
1.4


316
1257
126
1135
36
3
914
725
56
32
896
91
19
None
None
1.2


317
1273
98
1125
44
3
871
645
53
66
876
99
12
None
None
1.3


318
1257
113
1149
39
3
868
738
51
49
924
88
18
None
None
1.4


319
1234
94
1156
39
3
882
654
48
21
829
77
34
None
None
1.5


320
1268
126
1118
41
3
851
713
53
24
858
100
19
None
None
1.3


321
1281
71
1167
45
3
859
700
54
20
862
104
15
None
None
1.3


322
1251
102
1170
34
3
853
636
53
20
899
89
28
None
None
1.3


323
1272
94
1128
40
3
904
555
46
63
866
109
28
None
None
1.5


324
1250
91
1161
38
3
920
727
58
64
852
92
26
None
None
1.2


325
1272
102
1143
40
3
905
637
57
53
828
112
25
None
None
1.2


326
1255
118
1134
25
3
873
628
53
28
842
85
9
None
None
1.3


327
1246
133
1184
31
3
886
619
45
73
901
83
13
None
None
1.5


328
1237
88
1173
25
3
846
589
53
31
891
113
13
None
None
1.3


329
1241
110
1140
37
3
908
696
45
42
888
79
27
None
None
1.5


330
1232
133
1149
38
3
841
564
48
49
885
96
25
None
None
1.5


331
1248
71
1137
41
3
859
592
50
74
918
73
25
None
None
1.4


332
1247
72
1141
39
3
838
665
53
62
896
75
27
None
None
1.3


333
965
98
955
27
3
880
640
47
61
841
60
14
None
None
1.5


334
1388
120
1129
32
3
868
577
56
53
833
70
26
None
None
1.2


335
1244
13
1140
42
3
843
559
58
61
837
74
20
None
None
1.2


336
1235
95
1161
35
3
843
675
45
53
880
96
32
None
None
1.5


337
1243
105
1112
40
3
890
728
0
30
927
84
21
None
None
2.8


338
1242
91
1118
40
3
864
575
57
73
863
99
19
277
None
1.2


339
1234
83
1128
41
3
893
615
57
49
863
100
19
260
Yes
1.2


340
1247
87
1134
34
3
911
591
54
53
925
92
26
None
Yes
1.3


341
1281
113
1021
38
3
851
628
53
28
885
85
29
None
None
1.3


342
1250
71
1161
4
2
905
592
53
68
841
76
26
None
None
1.5


343
1242
118
1140
40
1
846
577
45
26
880
106
35
None
None
1.5



















TABLE 16









Mechanical properties













Average






cross-














Microstructure

Average

sectional





















Hardness of


Area rate


cross-

hardness-
Max.





middle part in


of residual
Tensile
Uniform
sectional
Minimum
Minimum
bending
Hydrogen


Man.
sheet thickness
ΔH1
ΔH2
austenite
strength
elongation
hardness
hardness
hardness
angle
embrittlement


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






















301
574
187
44
2.5
1717
5.5
574
505
69
94.8
Good
Inv. ex.


302
686
163
34
3.4
2052
5.9
686
656
30
96.9
Good
Inv. ex.


303
760
172
40
3.9
2272
6.5
760
699
61
92.4
Good
Inv. ex.


304
789
131
30
4.5
2510
6.7
789
753
36
94.6
Good
Inv. ex.


305
436
190
29
2.2
1304
5.1
436
401
35
101.7
Good
Comp. ex.


306
742
177
44
3.7
2217
6.1
742
674
68
94.7
Good
Inv. ex.


307
737
111
14
3.1
2202
6.8
737
712
25
96.4
Good
Inv. ex.


308
778
181
37
4.4
2326
6.9
778
723
55
104.9
Good
Inv. ex.


309
901
173
37
3.8
2973
6.8
1428
1354
74
45.8
Good
Comp. ex.


310
667
167
29
0.2
1994
2.9
667
619
48
98.3
Good
Inv. ex.


311
757
164
36
0.7
2265
3.3
757
730
27
92.5
Good
Inv. ex.


312
442
154
46
2.1
1459
5.2
442
261
181
103.0
Good
Comp. ex.


313
717
105
24
2.8
2144
6.2
717
552
165
92.1
Good
Inv. ex.


314
738
178
33
0.4
2208
3.2
738
594
144
96.6
Good
Inv. ex.


315
724
178
45
0.8
2166
3.8
724
575
149
98.7
Good
Inv. ex.


316
769
128
39
2.9
2299
6.4
769
726
43
96.5
Good
Inv. ex.


317
741
137
28
2.0
2214
5.4
741
673
68
95.6
Good
Inv. ex.


318
754
152
30
2.6
2254
5.7
754
683
71
93.2
Good
Inv. ex.


319
680
181
28
3.3
2033
6.7
680
640
40
94.5
Good
Inv. ex.


320
675
170
45
2.7
2018
5.9
675
636
39
97.7
Good
Inv. ex.


321
592
174
48
2.5
1771
5.5
592
552
40
96.2
Good
Inv. ex.


322
584
130
48
3.3
1747
6.8
584
526
58
103.3
Good
Inv. ex.


323
580
156
34
2.7
1735
5.9
580
538
42
99.1
Good
Inv. ex.


324
698
155
32
4.3
2088
6.9
698
667
31
92.0
Good
Inv. ex.


325
691
138
30
2.7
2067
5.9
691
622
69
98.3
Good
Inv. ex.


326
689
150
40
3.4
2061
6.9
689
628
61
95.7
Good
Inv. ex.


327
742
178
49
2.0
2219
5.3
742
701
41
99.1
Good
Inv. ex.


328
753
155
30
3.4
2251
6.1
753
721
32
101.8
Good
Inv. ex.


329
745
150
48
3.7
2228
6.8
745
715
30
97.1
Good
Inv. ex.


330
788
157
47
4.1
2514
6.7
788
749
39
94.1
Good
Inv. ex.


331
791
142
44
4.1
2519
6.9
791
734
57
96.6
Good
Inv. ex.


332
789
161
36
2.4
2510
5.3
789
761
28
101.4
Good
Inv. ex.


333
691
209
5
4.5
2067
6.6
691
638
53
53.8
Poor
Comp. ex.


334
695
6
221
4.5
2079
6.8
695
639
56
66.5
Good
Comp. ex.


335
698
219
5
3.0
2088
6.6
698
672
26
62.9
Poor
Comp. ex.


336
708
106
45
4.5
2118
6.8
708
654
54
94.2
Good
Inv. ex.


337
695
174
42
4.0
2079
6.9
695
640
55
99.6
Good
Inv. ex.


338
751
141
33
4.6
2245
6.9
751
699
52
97.1
Good
Inv. ex.


339
762
143
37
4.1
2278
6.5
762
729
33
95.8
Good
Inv. ex.


340
700
160
26
3.4
2094
6.8
700
638
62
101.9
Good
Inv. ex.


341
640
200
6
2.9
2112
6.5
640
598
42
61.8
Poor
Comp. ex.


342
629
202
7
2.8
2076
6.5
629
591
38
63.0
Poor
Comp. ex.


343
651
204
5
3.0
2148
6.6
651
620
31
61.2
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 90(°) 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 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 100 Hv or more and less than 200 Hv, andthe intermediate layer has a hardness change ΔH2 in the sheet thickness direction of 10 Hv or more and less than 50 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%, 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 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%, 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 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 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
2017-029311 Feb 2017 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2018/006057 2/20/2018 WO 00