HOT STAMPED BODY

Information

  • Patent Application
  • 20200230681
  • Publication Number
    20200230681
  • Date Filed
    February 20, 2018
    6 years ago
  • Date Published
    July 23, 2020
    4 years ago
Abstract
The present invention, in consideration of the problems in the prior art, provides a hot stamped body simultaneously achieving the high bendability and high ductility for realizing impact resistance and also hydrogen embrittlement resistance and kept down in scattering in hardness. The hot stamped body according to the present invention is provided with a middle part in sheet thickness and a softened layer arranged at both sides or one side of the middle part in sheet thickness. The middle part in sheet thickness has a hardness of 500Hv to 800Hv and has metal structures from a depth of 20 μm below the surface of the softened layer to a depth of ½ of the thickness of the softened layer with an area rate of a total of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and 15° or less of 50% or more and less than 85%, when a region surrounded by grain boundaries having an orientation difference of 15° or more in a cross-section parallel to the sheet thickness direction is defined as a “crystal grain”.
Description
FIELD

The present invention relates to a hot stamped body used for structural members or reinforcing members of automobiles or structures where strength is required, in particular a hot stamped body excellent in strength, impact resistance, ductility, and hydrogen embrittlement resistance after hot stamping and small in scattering in hardness.


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 is 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 hardening, 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.


For example, in a conventional hat-shaped member or other hot stamped body produced by press hardening, if bending deformation occurs at the time of collision of an automobile, the hat-shaped member will buckle and thereby deformation will become localized and the load resistance of the member will fall. That is, the maximum load of a member of a hot stamped body is affected not only by the strength of the member, but also the ease of buckling. If the ductility of the steel sheet is high, in the state of a member formed into a certain shape, it becomes harder for localization of the deformation region to occur. That is, the member becomes resistant to buckling.


Further, 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-shaped 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 a small scattering in hardness of the body, that is, securing stable strength, is important in securing impact resistance.


Therefore, in a hot stamped part as well, ductility is important, but in general the ductility of martensite is low. Further, the density of lattice defects of the surface layer of the steel sheet is high, so there is the problem that penetration by hydrogen is promoted and the part becomes poor in hydrogen embrittlement resistance. Due to such reasons, hot stamped parts produced by press hardening have been limited in locations of use in auto parts.


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 softened 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. PTL 2 discloses controlling the concentration of carbon at a surface layer in sheet thickness to ⅕ or less of the concentration of carbon of the middle part in sheet thickness 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 middle part in sheet thickness a dual phase structure of ferrite and martensite and raise the structural fraction of ferrite of a surface layer portion so as to ease the stress even if the surface layer part receives severe bending deformation.


However, in the members described in PTL 1 and PTL 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 PTL 3, a surface layer portion in sheet thickness is made by soft structures and the middle part in sheet thickness is made by 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

The present invention, in consideration of the technical issues in the prior art, has as its object to provide a hot stamped body achieving both a high bendability and high ductility for realizing impact resistance and hydrogen embrittlement resistance and keeping down the scattering in hardness.


Solution to Problem

The inventors engaged in an in-depth study of a method for solving the above technical issues. As a result, to improve the hydrogen embrittlement resistance, it is effective to reduce the density of lattice defects at the surface layer in 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. In this way, the inventors thought that if forming the surface layer in sheet thickness by soft structures and forming the middle part in sheet thickness by hard structures, if it were possible to reduce the sharp gradient of hardness in the sheet thickness direction occurring near the boundary of the hard structures and soft structures, a strength of a tensile strength of 1500 MPa or more and excellent hydrogen embrittlement resistance could be secured while excellent bendability could be obtained.


Therefore, the inventors investigated and engaged in intensive studies on metal structures of steel sheets where good bendability was obtained by controlling the structures of a surface layer of soft structures. As a result, it was discovered that the metal structures forming the surface layer should be comprised of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° when a region surrounded by grain boundaries having an orientation difference of 15° or more in the sheet thickness cross-section is defined as a “crystal grain”. These measurements were performed in the region from a position of a depth of 20 μm below the surface of the surface layer to a position of a depth of ½ of the thickness of the surface layer (center of surface layer). It was discovered that the effects of the surface properties of the hot stamped body and the effects of the transitional part from the middle part in sheet thickness to the surface layer can be eliminated by such metal structures.


Further, by controlling the amounts of addition of Mn and Si at the middle part in sheet thickness, the inventors raised the ductility and raised the hardenability to stably secure high strength. As a result, it is possible to keep down the occurrence of cracking at the time of bending deformation. The inventors succeeded in securing a 1500 MPa or more tensile strength and good hydrogen embrittlement resistance while realizing excellent bendability, ductility, and stability of strength and were able to obtain a hot stamped body excellent in impact resistance and hydrogen embrittlement resistance.


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 softened layer arranged at both sides or one side of the middle part in sheet thickness, 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, and


a balance of Fe and unavoidable impurities, and has a hardness of 500 Hv or more and 800 Hv or less,


in the metal structures from a depth of 20 μm below the surface of the softened layer to a depth of ½ of the thickness of the softened layer, when defining a region surrounded by grain boundaries having a 15° or higher orientation difference in a cross-section parallel to the sheet thickness direction as a “crystal grain”, the area rate of the total of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° is 50% or more and less than 85%,


the tensile strength is 1500 MPa or more.


(2) The hot stamped body according to (1), wherein the Si content is 0.50% or less and the Mn content is 0.20% or more and less than 1.50%.


(3) The hot stamped body according to (1), wherein the Si content is 0.50% or less and the Mn content is 1.50% or more and less than 3.00%.


(4) The hot stamped body according to (1), wherein the Si content is more than 0.50% and less than 3.00%, the Mn content 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 (1), wherein the Si content is more than 0.50% and less than 3.00%, the Mn content 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 (1) to (5), where 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 (1) to (6), where 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 (1) to (7), where a plated layer is formed on the softened layer.


Advantageous Effects of Invention

According to the present invention, it is possible to provide a hot stamped body excellent in bendability, ductility, impact resistance, and hydrogen embrittlement resistance and with small scattering in hardness.





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1 is a schematic view for explaining the diffusion of C atoms when producing a hot stamped body 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 hot stamped body of the present invention.





DESCRIPTION OF EMBODIMENTS
(Structure of Hot Stamped Body According to Present Invention)

The hot stamped body according to the present invention is a structure with a softened layer arranged on the surface at both sides or one side. The softened layer has a region having a hardness 10 Hv or more lower than the hardness of the middle part in sheet thickness.


(Middle Part in Sheet Thickness)

The middle part in sheet thickness of the hot stamped body according to the present invention must have a hardness of 500 Hv to 800 Hv. The reasons for limiting the composition of constituents at the middle part in sheet thickness to make the hardness of the middle part in sheet thickness the above-mentioned range are explained below. Below, the % relating to the component of constituents means mass %.


(C: 0.20% or More and Less than 0.70%))


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


(Si: Less than 3.00%)


Si is an element contributing to improvement of strength by solution strengthening. The amount of addition of Si for obtaining the effect of improvement of strength of the steel sheet by formation of a solid solution of Si in the metal structures is preferably 0.30% or more, but even if adding more than 0.5% of Si, the effect becomes saturated.


Si also has the effect of causing the formation of residual austenite and raising the ductility. To obtain this effect, addition of more than 0.50% is at least necessary. On the other hand, even if adding more than 3.00%, the effect becomes saturated, and therefore the amount of addition of Si is one with an upper limit of less than 3.00%. Preferably, the amount is less than 2.0%.


(Mn: 0.20% or More and Less than 3.00%)


Mn is an element contributing to improvement of strength by solution strengthening. The effect of improving the strength of the steel sheet by solid solution of Mn in the metal structures cannot be obtained with an amount of addition of less than 0.20%, 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 becomes saturated.


Mn, further, has the effect of raising the hardenability. By adding 1.50% or more, it is possible to raise the hardenability and stably obtain high strength. The preferable amount of addition for obtaining the effect of raising the hardenability is 1.70% or more. Even if adding 3.00% or more, the effect becomes saturated, and therefore the upper limit of the amount of addition of Mn is 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, and therefore 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 dephosphorizing 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, and therefore S is 0.10% or less. Preferably, it is 0.0025% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0015%, the desulfurizing cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% 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. In the present invention, to obtain the deoxidizing action, the range of content of not all of the Al contained in the steel, but the content of so-called “acid soluble aluminum” (sol. Al) is prescribed. With a sol. Al content of less than 0.0002%, the deoxidizing is insufficient, and therefore sol. Al is 0.0002% or more. Preferably the content is 0.0010% or more. On the other hand, even if adding more than 3.0%, the effect becomes saturated, and therefore 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, and therefore 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 denitriding 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 0.010%, the effect is not obtained, so 0.010% or more is added. Preferably, the content is 0.5% or more. On the other hand, even if added in more than 3.00%, the effect becomes saturated, and therefore 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 0.010% or more is added. Preferably, the content is 0.035% or more. On the other hand, even if added in more than 0.150%, the effect becomes saturated, and therefore 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, and therefore the content is 0.010% or more. Preferably, the content is 0.020%. On the other hand, even if added in more than 0.150%, the effect becomes saturated, and therefore the content is 0.150% or less. Preferably, the content is 0.120% or less.


(Mo: 0.005% or More and 1.0% 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, and therefore the content is 0.005% or more. Preferably, the content is 0.0100% or more. On the other hand, even if added in more than 1.000%, the effect becomes saturated, and therefore 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, and therefore the content is 0.0100% or less. Preferably, the content is 0.0075% or less.


The balance of the composition of 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.


(Hardness of Middle Part in Sheet Thickness is 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 of the present invention, 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, since the difference in hardness with the softened layer becomes too large and deterioration of the bendability is invited, 800 Hv is the upper limit. Preferably the hardness is 720 Hv or less.


The method of measurement of the hardness of the middle part in sheet thickness is as follows: A cross-section vertical to the sheet surface of the hot stamped body is taken to prepare a sample of the measurement surface. This is 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.


(Metal Structures at Middle Part in Sheet Thickness)

The middle part in sheet thickness can be improved in ductility by including residual austenite in an area percent of 1% or more. The area percent of residual austenite at the middle part in sheet thickness is preferably 2% or more. However, if making the area percent of the residual austenite 5% or more, since deterioration of the bendability is invited, the upper limit is less than 5.0%. Preferably, the fraction is less than 4.5%.


The area percent of the residual austenite can be measured by the following method. A sample is taken from a hot stamped member and ground down at its surface to a depth of ½ of the sheet thickness from the normal direction of the rolling surface. The ground down surface is used for X-ray diffraction measurement. From the image obtained by the X-ray diffraction method using Kα rays of Mo, the area rate Vγ of residual austenite can be 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 X-ray diffraction intensity at the (211) face of ferrite, γ(220) is the X-ray diffraction intensity at the (220) face of austenite, and γ(311) is the X-ray diffraction intensity at the (311) face of austenite.


(Softened Layer)

As explained above, in the present invention, the “softened layer” is the region in the sheet thickness direction of the cross-section of sheet thickness of the hot stamped body from the position where the hardness falls by 10 Hv or more from hardness of the middle part in sheet thickness (hardness at position of ½ of sheet thickness) to the surface of the stamped body.


(Metal Structures of Softened Layer)

The inventors investigated the metal structures of steel sheets where good bendability was obtained and as a result discovered that the metal structures forming the softened layer should be comprised of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° when defining a region surrounded by grain boundaries having a 15° or higher orientation difference in a cross-section of sheet thickness as a “crystal grain”. These measurements were performed in the region from a position of a depth of 20 μm below the surface of the softened layer to a position of a depth of ½ of the thickness of the softened layer (center of softened layer). The inventors engaged in intensive studies and as a result discovered that from the viewpoint of the bendability and other effects, the fractions of structures from a position of 20 μm from the surface of the softened layer to a position of a depth of ½ of the thickness of the softened layer are important. The effects of the surface properties of the hot stamped body and the effects of the transitional part from the middle part in sheet thickness to the softened layer can be eliminated by such metal structures.


In the above-mentioned metal structures of the softened layer, the area rate of the total of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° should be 50% or more, more preferably 55% or more. On the other hand, with an area rate of the total of the metal structures of the softened layer of 85% or more, the difference in hardness of the softened layer and the middle part in sheet thickness becomes too great and the effect of reduction of the sharp gradient of hardness in the sheet thickness direction occurring at the time of bending deformation cannot be obtained, and therefore the area rate is less than 85%. More preferably, it is 80% or less.


Between the position of a depth of ½ of the thickness of the softened layer (center of softened layer) to the middle part in sheet thickness, if the hardness at the sheet thickness middle part side of the softened layer (boundary with middle part in sheet thickness) is HvA and the hardness of the center of the softened layer is HvB, they are in the relationship of HvA−HvB≥10 Hv.


The method of determining the region from 20 μm below the surface of the softened layer to a position of ½ of the thickness of the softened layer will be explained below. A cross-section vertical to the surface of the hot stamped body being measured (cross-section of sheet thickness) is taken to prepare a sample of the measurement surface. This is used for 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 sample with the prepared measurement surface is measured two times based on the method described in JIS Z 2244 using a micro Vickers hardness tester. The first time measures the hardness from the region within 20 μm from the surface of the hot stamped body in the sheet thickness direction to the middle part in sheet thickness (position of ½ of sheet thickness) in the direction vertical to the surface (sheet thickness direction) by a load of 0.3 kgf at intervals of 3 times or more the dents. However, if there is a plated layer, this is measured from the region within 20 μm right under the plating or coating or the alloy layer of the plating or coating and material of the softened layer. The position where the hardness starts to drop by 10 Hv or more from the hardness of the middle part in sheet thickness (hardness at position of ½ of sheet thickness) is determined and the layer from that sheet thickness position to the surface of the hot stamped body is defined as the “softened layer”. If the softened layer is present at both surfaces, the second measurement is performed at the surface at the opposite side to the first one (back surface) by a similar method to determine the position where the hardness starts to drop by 10 Hv or more from the hardness of the middle part in sheet thickness.


Next, the method of calculating the area rates of metal structures of the softened layer will be explained. A sample is cut out from a hot stamped body to enable examination of a cross-section vertical to its surface (sheet thickness direction). The length of the sample depends on the measuring device, but may be about 50 μm. The region in the sheet thickness direction of the sample from the surface of the softened layer to the position of ½ of the thickness of the softened layer (center of softened layer) is analyzed at 0.2 μm measurement intervals by EBSD to obtain information on the crystal orientation. Here, this EBSD analysis is performed using an apparatus comprised of a thermal field emission type scan electron microscope (JSM-7001F made by JEOL) and EBSD detector (DVCS type detector made by TSL) at an analysis speed of 200 to 300 points/second.


Next, based on the obtained crystal orientation information, a region surrounded by grain boundaries having an orientation difference of 15° or more is defined as one crystal grain and a crystal orientation map in the sheet surface direction is prepared. The obtained crystal orientation map is used to find the crossing points of the long axis of one crystal grain and the crystal grain boundaries. Among the two crossing points, one is designated as the starting point and the other is designated as the end point and the difference in orientation among all measurement points contained on the long axis of the crystal grain is calculated. The maximum value of the orientation difference obtained was defined as the maximum crystal orientation difference at that crystal grain. The above analysis was performed for all crystal grains included in the measurement region, then the average of these values was defined as the maximum crystal orientation difference inside a region surrounded by grain boundaries of 15° or more.


The above-defined maximum crystal orientation difference can be simply calculated, for example, if using the “Inverse Pole Figure Map” and “Profile Vector” functions included in the software (OIM Analysis®) attached to the EBSD analysis system. With the “Inverse Pole Figure Map” function, it is possible to draw grain boundaries having slants of 15° or more as large angle grain boundaries and further possible to prepare a crystal orientation map in the sheet surface direction. With the “Profile Vector” function, it is possible to calculate the misorientation angle (difference in crystal orientations) between all measurement points included on any line. All crystal grains contained in the measurement region (crystal grains at end parts of measurement region not included) are analyzed as explained above and the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° is calculated. If the softened layer is formed on both surfaces, the above procedure is performed at the back surface side of the hot stamped body as well and the average value of the area rates obtained from the front surface side and the back surface side is employed.


(Composition of Softened Layer)

The composition of the softened layer is not particularly limited other than regarding the unavoidable impurity elements of P, S, and N impairing the strength and/or bendability, but the layer is preferably the following composition so as to secure the strength of the hot stamped body and steel exhibiting excellent bendability.


In the composition of the softened layer, one or more of the C content, Si content, and Mn content are preferably respectively 0.6 time the corresponding contents of elements of the middle part in sheet thickness. The preferable ranges of the constituents in this case are as follows:


(C: 0.05% or More and Less than 0.42%)


C may be added in 0.05% or more so as to raise the strength. From the viewpoint of raising the load resistance as a member and improving the impact characteristics, preferably the content is 0.10% or more. To make the hardness of the softened 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 softened layer is less than 0.42%. Preferably the 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. However, to make the hardness of the softened 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.


If the Si content of the middle part in sheet thickness is 0.50% or less, the preferable Si content of the softened layer is 0.30% or less, more preferably 0.20% or less. Further, if the Si content of the middle part in sheet thickness is more than 0.50% and less than 3.00%, the preferable Si content of the softened layer is less than 2.00%, more preferably 1.50% or less.


(Mn: 0.12% or More and Less than 1.80%)


Mn is an element contributing to improvement of strength by solution strengthening, so may be added in 0.12% or more for raising the strength. However, to make the hardness of the softened 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.


If the Mn content at the middle part in sheet thickness is 0.20% to less than 1.50%, the preferable Mn content of the softened layer is less than 0.90%, more preferably is 0.70% or less. Further, if the Mn content of the middle part in sheet thickness is 1.50% to less than 3.00%, the preferable Mn content of the softened layer is less than 1.80%, preferably 1.40% or less.


(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, and therefore P is 0.1% 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 dephosphorizing 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, and therefore S is 0.10% or less. Preferably, it is 0.0025% or less. The lower limit is not particularly prescribed, but if reducing this to less than 0.0015%, the desulfurizing cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% 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. In the present invention, to obtain this deoxidizing action, the range of content of not all of the Al contained in the steel, but the so-called “acid soluble aluminum” (sol. Al) is prescribed. With a sol. Al content of less than 0.0002%, the deoxidizing is insufficient, and therefore the sol. Al is preferably 0.0002% or more. More preferably the content is 0.0010% or more. On the other hand, even if adding more than 3.0000%, the effect becomes saturated, and therefore 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, and therefore 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 denitriding cost greatly rises and the result becomes economically disadvantageous, so in practical steel sheet, 0.0001% is the substantive lower limit.


Regarding the constituents of the softened layer, one or more of the C content, Si content, and Mn content are preferably respectively 0.6 time or less the C content, Si content, and Mn content of the middle part in sheet thickness. Other than the upper limits of the unavoidable impurity elements of P, S, and N impairing the strength and/or bendability being prescribed, the other constituents are not particularly limited. In general, the softened layer may optionally and selectively include one or more of the following constituents besides C, Si, and Mn.


(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, and therefore preferably 0.01% or more is added. 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, and therefore 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 preferably 0.010% or more is added. 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, and therefore 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, and therefore preferably the content is 0.010% or more. More preferably, the content is 0.020%. On the other hand, even if added in more than 0.150%, the effect becomes saturated, and therefore 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, and therefore preferably the content is 0.005% or more. 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, and therefore 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, and therefore preferably 0.0005% or more is added. More preferably, the content is 0.0010% or more. On the other hand, even if added in more than 0.0100%, since the effect becomes saturated, the content is 0.0100% or less. Preferably, the content is 0.0075% or less.


(Cross-Sectional Distribution of Hardness of Hot Stamped Body)

At the cross-section vertical to the surface of the hot stamped body, the distribution of hardness at the middle part in sheet thickness is preferably uniform with no scattering. In a hat-shaped structure, at the vertical wall parts, contact with the die is difficult and the cooling rate becomes low, so sometimes the hardness falls. If there is a region where the hardness falls by 100 Hv or more from the average hardness of the cross-section vertical to the longitudinal direction of the hat-shaped member, at the time of impact, the deformation will concentrate at the softened part and the part will fracture early, so a high impact resistance cannot be obtained. For this reason, there must not be a point with a hardness more than 100 HV below the average value of the distribution of hardness in the cross-section vertical to the surface of the hot stamped body (below, referred to as the “average hardness of cross-section”). The distribution of hardness at the cross-section and the average hardness of the cross-section are obtained by obtaining a cross-section vertical to the longitudinal direction of a long hot stamped body at any position in the longitudinal direction and measuring the Vickers hardness between the end parts of the cross-section at equal intervals of 1 mm pitch or less at the middle position of sheet thickness of the entire cross-sectional region including the vertical walls using a Vickers hardness tester (load of 1 kgf).


(Formation of Plated Layer)

The surface of the softened layer 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 coated layer. An electroplated layer includes, for example, an electrogalvanized layer, electro Zn—Ni alloy plated layer, etc. As a hot dip coated layer, a hot dip galvanized layer, a hot dip galvannealed layer, a hot dip aluminum coated layer, a hot dip Zn—Al alloy coated layer, a hot dip Zn—Al—Mg alloy coated layer, a hot dip Zn—Al—Mg—Si alloy coated layer, etc., may be mentioned. The amount of deposition of the layer is not particularly limited and may be a general amount of deposition.


(Method of Production of Hot Stamped Body According to Present Invention)

Next, the method of production for obtaining the hot stamped body according to the present invention will be explained, but the present invention is not limited to the form of the double layer steel sheet explained below.


As one embodiment of the method of production of the present invention, first, a steel sheet satisfying the requirements of the composition of constituents of the middle part in sheet thickness explained above is ground down at its front surface and/or back surface to remove surface oxides, then a steel sheet for softened layer formation use (below, referred to as a “steel sheet for surface layer”) is superposed on each ground down surface side. The method of joining the steel sheet for surface layer and the steel sheet for sheet thickness middle part is not particularly limited, but they may be joined by arc welding. A steel sheet for surface layer wherein one or more of the C content, Si content, and Mn content are 0.6 time or less the content of the corresponding element of the steel sheet for sheet thickness middle part is preferably superposed.


Further, by controlling the casting rate to ton/min or more in the continuous casting process of the steel sheet for surface layer, it is possible to keep down microsegregation of Mn in the steel sheet for surface layer and possible to make the distribution of concentration of Mn at the steel sheet for surface layer uniform. Mn raises the yield strength of austenite to thereby affect the behavior in formation of grain boundaries in the transformed structures, so when defining a region surrounded with grain boundaries having orientation differences of 15° or more as a “crystal grain”, it has the effect of promoting the formation of crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15°. For this reason, it is also possible to control the casting rate to 6 ton/min or more in the continuous casting process of steel sheet for surface layer for the purpose of promoting the formation of the above microstructures.


Further, a double layer steel sheet fabricated by the above method is preferably held at 1100° C. or more and 1350° C. or less in temperature for 20 minutes to less than 60 minutes. The held sheet is preferably used as the steel sheet for hot stamped body according to the present invention. The inventors studied this and as a result learned that by performing heat treatment holding the steel sheet at 1100° C. or more and 1350° C. or less for 20 minutes to less than 60 minutes, in the metal structures in the region from a position of a depth of 20 μm below the surface of the softened layer to the center of the softened layer, the area rate of the total of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° becomes 50% to less than 85% when a region surrounded by grain boundaries having an orientation difference of 15° or more is defined as a “crystal grain” and that excellent bendability and hydrogen embrittlement resistance can be obtained.


The multilayer member produced by the above method of production (double layer steel sheet) can be treated by hot rolling, cold rolling, hot stamping, continuous hot dip coating, etc., to obtain the hot stamped body according to the present invention.


The hot rolling may be hot rolling performed under usual conditions. For example, the finishing temperature may also be in the temperature range of 810° C. or more. The subsequent following cooling conditions also do not have to be particularly prescribed. The steel sheet is coiled in the temperature region of 750° C. or less. Further, it may be reheated for the purpose of softening the double layer steel sheet after hot rolling.


Further, to promote more the formation of the middle part in sheet thickness, 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 twice under conditions of a temperature of 1100° C. or more, a sheet thickness reduction rate 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 middle part in sheet thickness 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 sheet thickness reduction rate 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 through a general hot rolling process, 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 sheet thickness reduction rate 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 diffuse 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 sheet thickness reduction rate 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 sheet thickness reduction rate 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 sheet thickness reduction rate becomes 5%. As the time between passes, 3 seconds or more has to be secured.


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 steel 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 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 or coating 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, so is not particularly limited. For example, if 30 seconds or more and 600 seconds or less, a good 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 more than 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 body cooled down to room temperature in the range of 150° C. to 600° C.


In the method of production of the hot stamped body of the above-mentioned embodiment, the middle part in sheet thickness and the softened layer were configured by separate steel sheets. However, the hot stamped body of the present invention is not limited to double layer steel sheet comprised of two of the above-mentioned steel sheets superposed. The middle part in sheet thickness and the softened layer may be formed inside a single material steel sheet. For example, it is possible to treat a single layer steel sheet to decarburize it and soften the surface layer part to thereby produce high strength steel sheet comprised of a softened layer and a middle part in sheet thickness.


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 conditions. 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.


Manufacturing Example A

The Nos. 1 to 18 steel sheets for sheet thickness middle part having the chemical compositions shown in Table A-1-1 (in the table, “Steel Nos. 1 to 18”) were ground down at their surfaces to remove the surface oxides. After that, the respective steel sheets for sheet thickness middle part were welded with steel sheets for surface layer having the chemical compositions shown in Table A-1-2 at both surfaces or single surfaces by arc welding to fabricate the Nos. 1 to 43 multilayer steel sheets for hot stamped body. The total of the sheet thicknesses of the steel sheet for surface layer and the steel sheet for sheet thickness middle part after arc welding is 200 mm to 300 mm and the thickness of the steel sheet for surface layer is ⅓ or so of the thickness of the steel sheet for sheet thickness middle part (¼ or so in case of single side). The No. 37 multilayer steel sheet is steel with the steel sheet for surface layer welded to only one surface. In the Nos. 1 to 43 multilayer steel sheets of Table A-1-1 to Table A-1-2, ones with a steel sheet for sheet thickness middle part not satisfying the requirement for composition of the middle part in sheet thickness of the hot stamped body according to the present invention are indicated as “comparative steel” in the remarks column.


The Nos. 1 to 43 multilayer steel sheets were respectively treated under the conditions of the Nos. 1 to 43 manufacturing conditions shown in Table A-2-1 to Table A-2-2 by heat treatment before hot rolling, rough rolling, hot rolling, and cold rolling to obtain steel sheets. Next, the steel sheets were heat treated as shown in Table A-2-1 and Table A-2-2 (in the tables, “heat treatment of hot stamped body”) for hot stamping to manufacture the Nos. 1A to 43A hot stamped bodies (“stamped bodies” of Table A-3). Further, the Nos. 35A and 36A hot stamped bodies were coated on a hot dip coating line at the surfaces with 120 to 160 g/m2 amounts of aluminum.


In the tables, the item “sheet thickness reduction rate” of the “rough rolling” means the sheet thickness reduction rate per pass of the rough rolling. The item “number of rolling operations” means the number of rolling operations under the conditions of a time between passes of 3 seconds or more. Further, the item in the tables of “heating rate (° C./s)” means the rate of temperature rise until reaching the heating temperature of the “heat treatment at the time of hot stamping” after the cold rolling process. Further, in the tables, the item “heating temperature (° C.)” of the “heat treatment at the time of hot stamping” is the temperature at the time of hot stamping, the “average cooling rate (° C./s) (more than 400° C.)” means the average cooling rate (° C./s) in the temperature region from the heating temperature to more than 400° C., and the “average cooling rate (° C./s) (400° C. or less)” means the average cooling rate (° C./s) in the temperature region from 200° C. to 400° C. Further, in the tables, the fields with the notations “-” indicate no corresponding treatment performed.


Table A-3 shows the metal structures and characteristics of the Nos. 1A to 43A hot stamped bodies. The constituents obtained by analyzing the positions of ½ of the sheet thicknesses of the samples taken from the hot stamped bodies and positions of 20 μm from the surfaces of the softened layers were equivalent to the constituents of the steel sheets for sheet thickness middle part and steel sheets for surface layer of the Nos. 1 to 43 multilayer steel sheets of Table A-1-1 to Table A-1-2.


The metal structures of the hot stamped steel sheets were measured by the above-mentioned method. The hardness of the steel sheet for sheet thickness middle part forming the middle part in sheet thickness and the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer forming the softened layer to ½ of the thickness were calculated. The calculated values of the area rate are shown in the item “area rate (%) of total of crystal grains with maximum crystal orientation difference inside large angle grain boundaries of 1° or less and crystal grains with maximum crystal orientation difference of 8° or more and less than 15°” of Table A-3.


Further, a tensile test of the hot stamped body was performed. The results are shown in Table A-3. 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 body 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 indicated as passing (“good”) and a case with cracking was indicated as failing (“poor”).


For the purpose of evaluating the impact resistance of the hot stamped body, the body was evaluated 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 and thereby evaluate the impact resistance of the hot stamped body.


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


Indentation rate: 20 mm/min


Tester: SHIMAZU AUTOGRAPH 20 kN


If the tensile strength is 1500 MPa or more, the maximum bending angle (°) was 70(°) or more, and the hydrogen embrittlement resistance was a passing level, it was judged that the impact resistance and hydrogen embrittlement resistance were excellent and the case was indicated as an “invention example”. If even one of the three aspects of performance is not satisfied, the case was indicated as a “comparative example”.


In each hot stamped body of the invention examples, the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness was 50% to less than 85%. Further, each hot stamped body of the invention examples was excellent in tensile strength, bendability, and hydrogen embrittlement resistance.


As opposed to this, the No. 5A hot stamped body was low in carbon content of the steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness became insufficient and the tensile strength became insufficient. The No. 9A hot stamped body was excessive in carbon content of the steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness became excessive and the targeted bendability could not be obtained. Further, the No. 11A hot stamped body was low in Mn content at the steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness became insufficient and the tensile strength became insufficient.


The Nos. 30A to 32A hot stamped bodies are comparative examples produced using the multilayer steel sheets for hot stamped body to which the desirable heat treatment had not been applied before the hot stamping process. The No. 30A hot stamped body was low in heat treatment temperature before the hot stamping process, while the No. 31A hot stamped body was short in heat treatment time before the hot stamping process, so in the metal structures from the surface of the softened layer to ½ of the thickness, the soft structures and metal structures with intermediate hardnesses insufficiently grew and the target bendability could not be obtained. Further, the No. 32A hot stamped body was excessively high in heat treatment temperature before the hot stamping process, so the effect of reduction of the sharp gradient in hardness in the sheet thickness direction occurring at the time of bending deformation could not be obtained.


The No. 40A hot stamped body was low in rolling temperature of the rough rolling. Further, the No. 41A hot stamped body was low in sheet thickness reduction rate of the rough rolling. Further, the No. 42A hot stamped body was low in number of rolling operations under conditions of a time between passes of 3 seconds or more. These hot stamped bodies were not manufactured under the suitable rough rolling conditions, so the soft structures and metal structures with intermediate hardnesses insufficiently grew, it was not possible to ease the strain occurring due to bending deformation, and the targeted bendability could not be obtained.


The No. 43A hot stamped body is a steel sheet controlled in casting rate to 6 ton/min or more in the continuous casting process of steel sheet for surface layer. It can raise the area rate (%) of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness and is excellent in bendability.











TABLE A-1-1







Multilayer
Chemical constituents of steel sheet for sheet thickness middle part (mass %)






















steel sheet
Steel















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
























 1
1
0.25
0.24
1.22
0.016
0.0025
0.047
0.0037
0
0
0
0
0



 2
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



 3
3
0.38
0.13
1.31
0.011
0.0010
0.045
0.0033
0
0
0
0
0



 4
4
0.45
0.17
1.35
0.009
0.0001
0.040
0.0028
0
0
0
0
0



 5
5
0.12
0.17
1.31
0.016
0.0011
0.037
0.0039
0
0
0
0
0
Comp. steel


 6
6
0.23
0.17
1.28
0.015
0.0012
0.043
0.0037
0
0
0
0
0



 7
7
0.33
0.12
1.27
0.006
0.0014
0.037
0.0032
0
0
0
0
0



 8
8
0.32
0.11
1.34
0.007
0.0016
0.049
0.0033
0
0
0
0
0



 9
9
0.82
0.14
1.26
0.015
0.0007
0.043
0.0027
0
0
0
0
0
Comp. steel


10
10
0.35
0.43
1.29
0.010
0.0020
0.049
0.0028
0
0
0
0
0



11
11
0.30
0.22
0.07
0.016
0.0016
0.042
0.0041
0
0
0
0
0
Comp. steel


12
12
0.29
0.22
0.76
0.015
0.0011
0.044
0.0027
0
0
0
0
0



13
13
0.27
0.24
1.29
0.005
0.0014
0.045
0.0028
0.37
0
0
0
0



14
14
0.35
0.18
1.29
0.018
0.0003
0.044
0.0034
0
0.042
0
0
0



15
15
0.29
0.14
1.23
0.014
0.0013
0.050
0.0031
0
0
0.018
0
0



16
16
0.32
0.12
1.40
0.010
0.0011
0.049
0.0032
0
0
0
0.06
0



17
17
0.34
0.20
1.38
0.013
0.0018
0.047
0.0033
0
0
0
0
0.0021



18
1
0.25
0.24
1.22
0.016
0.0025
0.047
0.0037
0
0
0
0
0



19
1
0.25
0.24
1.22
0.016
0.0025
0.047
0.0037
0
0
0
0
0



20
1
0.25
0.24
1.22
0.016
0.0025
0.047
0.0037
0
0
0
0
0



21
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



22
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



23
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



24
3
0.38
0.13
1.31
0.011
0.0010
0.045
0.0033
0
0
0
0
0



25
3
0.38
0.13
1.31
0.011
0.0010
0.045
0.0033
0
0
0
0
0



26
3
0.38
0.13
1.31
0.011
0.0010
0.045
0.0033
0
0
0
0
0



27
4
0.45
0.17
1.35
0.009
0.0001
0.040
0.0028
0
0
0
0
0



28
4
0.45
0.17
1.35
0.009
0.0001
0.040
0.0028
0
0
0
0
0



29
4
0.45
0.17
1.35
0.009
0.0001
0.040
0.0028
0
0
0
0
0



30
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



31
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



32
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



33
2
0.30
0.23
1.25
0.015
0.0007
0.039
0.0036
0
0
0
0
0



34
18
0.69
0.22
1.34
0.005
0.0004
0.051
0.0027
0
0
0
0
0



35
18
0.69
0.22
1.34
0.005
0.0004
0.051
0.0027
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.














TABLE A-1-2







Multilayer










steel sheet
Composition of constituents of steel sheet for surface layer (mass %)





















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























 1
0.095
0.098
0.476
0.017
0.0034
0.049
0.0036
0
0
0
0
0



 2
0.141
0.104
0.613
0.014
0.0012
0.037
0.0034
0
0
0
0
0



 3
0.175
0.069
0.655
0.011
0.0014
0.046
0.0033
0
0
0
0
0



 4
0.230
0.090
0.702
0.009
0.0001
0.040
0.0028
0
0
0
0
0



 5
0.043
0.071
0.655
0.015
0.0017
0.039
0.0041
0
0
0
0
0
Comp. steel


 6
0.104
0.082
0.563
0.015
0.0018
0.044
0.0035
0
0
0
0
0



 7
0.162
0.052
0.584
0.004
0.0019
0.039
0.0032
0
0
0
0
0



 8
0.176
0.056
0.509
0.007
0.0024
0.051
0.0033
0
0
0
0
0



 9
0.328
0.064
0.517
0.016
0.0017
0.042
0.0028
0
0
0
0
0
Comp. steel


10
0.158
0.224
0.697
0.008
0.0029
0.051
0.0027
0
0
0
0
0



11
0.147
0.119
0.029
0.014
0.0026
0.040
0.0042
0
0
0
0
0
Comp. steel


12
0.145
0.119
0.365
0.015
0.0016
0.045
0.0025
0
0
0
0
0



13
0.124
0.127
0.684
0.003
0.002
0.045
0.0027
0.34
0
0
0
0



14
0.172
0.085
0.555
0.018
0.0006
0.044
0.0033
0
0.0038
0
0
0



15
0.136
0.064
0.492
0.016
0.0022
0.05
0.0032
0
0
0.0025
0
0



16
0.166
0.061
0.63
0.008
0.0015
0.048
0.0031
0
0
0
0.05
0



17
0.153
0.102
0.607
0.012
0.0021
0.047
0.0031
0
0
0
0
0.0018



18
0.110
0.211
1.183
0.016
0.0029
0.045
0.0036
0
0
0
0
0



19
0.105
0.214
0.622
0.016
0.0031
0.049
0.0038
0
0
0
0
0



20
0.143
0.11
1.049
0.016
0.0031
0.048
0.0036
0
0
0
0
0



21
0.273
0.101
0.638
0.014
0.0013
0.038
0.0038
0
0
0
0
0



22
0.270
0.124
1.088
0.013
0.0014
0.041
0.0038
0
0
0
0
0



23
0.264
0.205
0.575
0.015
0.0014
0.038
0.0038
0
0
0
0
0



24
0.296
0.057
0.616
0.009
0.0018
0.044
0.0033
0
0
0
0
0



25
0.190
0.124
0.655
0.009
0.0018
0.047
0.0034
0
0
0
0
0



26
0.175
0.061
1.009
0.010
0.0017
0.044
0.0032
0
0
0
0
0



27
0.401
0.092
0.689
0.011
0.0004
0.038
0.0027
0
0
0
0
0



28
0.207
0.153
0.594
0.007
0.0007
0.041
0.0028
0
0
0
0
0



29
0.203
0.075
1.175
0.009
0.0007
0.040
0.0027
0
0
0
0
0



30
0.144
0.127
0.550
0.014
0.0014
0.039
0.0036
0
0
0
0
0



31
0.144
0.113
0.588
0.013
0.0009
0.038
0.0037
0
0
0
0
0



32
0.135
0.113
0.563
0.017
0.0012
0.039
0.0036
0
0
0
0
0



33
0.156
0.110
0.513
0.015
0.0016
0.039
0.0036
0
0
0
0
0



34
0.290
0.125
0.63
0.004
0.0009
0.052
0.0025
0
0
0
0
0



35
0.352
0.112
0.63
0.006
0.0004
0.053
0.0028
0
0
0
0
0



36
0.132
0.12
0.575
0.017
0.0015
0.039
0.0036
0
0
0
0
0



37
0.150
0.124
0.563
0.013
0.0010
0.038
0.0035
0
0
0
0
0



38
0.221
0.092
0.689
0.011
0.0004
0.038
0.0027
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indeicate corresponding constituents not intentionally added.
























TABLE A-2-1









Heat






Heat treatment at hot stamping
























treatment






Average

























before hot
Rough rolling




cooling
Average
























Multi-

rolling

Rate of

Hot rolling
Cold
Heat-

rate
cooling


























layer
Manu-
Heat-
Hold-
Roll-
reduction
No. of
Finish
Coil-
rolling
ing
Heat-
(° C./s)
rate
Temper-

Sheet


steel
facturing
ing
ing
ing
of sheet
rolling
rolling
ing
Rolling
rate
ing
(more
(° C./s)
ing

thick-


sheet
condition
temp.
time
temp.
thickness
operations
temp.
temp.
rate
(° C./
temp.
than
(400° C.
temp.
Plat-
ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
s)
(° C.)
400° C.)
or less)
(° C.)
ing
(mm)


























 1
 1
1320
35
1149
34
3
838
586
53
32
903
70
53

None
1.3


 2
 2
1293
31
1171
32
3
840
538
58
34
872
97
94

None
1.2


 3
 3
1257
41
1138
20
3
917
604
53
51
859
73
66

None
1.3


 4
 4
1285
36
1157
42
3
840
567
48
61
885
100
86

None
1.5


 5
 5
1318
36
1133
38
3
856
712
60
54
884
96
84

None
1.1


 6
 6
1275
35
1165
30
3
865
578
57
74
822
70
62

None
1.2


 7
 7
1275
32
1184
47
3
872
685
49
61
909
82
77

None
1.4


 8
 8
1268
41
1130
42
3
847
680
37
51
817
81
79

None
1.8


 9
 9
1338
50
1167
29
3
865
693
58
29
843
69
60

None
1.2


10
10
1270
39
1132
37
3
838
602
51
40
913
77
69

None
1.4


11
11
1272
45
1130
34
3
900
620
62
57
831
99
98

None
1.1


12
12
1301
49
1174
37
3
844
536
61
59
880
75
77

None
1.1


13
13
1297
52
1176
28
3
860
744
38
26
823
100
93

None
1.7


14
14
1287
42
1143
42
3
927
536
53
42
905
73
63

None
1.3


15
15
1341
58
1154
43
3
915
545
40
28
912
89
77

None
1.7


16
16
1268
54
1142
35
3
845
722
50
34
887
104
95

None
1.4


17
17
1321
43
1141
43
3
865
569
34
63
849
113
109

None
1.8


18
18
1315
55
1146
34
3
868
570
49
49
902
96
83

None
1.4


19
19
1306
47
1157
42
3
862
624
63
20
844
73
63

None
1


20
20
1322
34
1126
42
3
867
652
40
22
887
106
86

None
1.7


21
21
1316
58
1159
48
3
847
589
57
19
845
102
93

None
1.2


22
22
1287
56
1171
34
3
856
562
44
29
812
99
92

None
1.6


23
23
1333
58
1132
40
3
856
707
47
61
834
97
80

None
1.5


24
24
1306
47
1167
34
3
861
574
42
70
940
79
67

None
1.6


25
25
1339
54
1143
40
3
882
697
48
63
899
91
83

None
1.5



























TABLE A-2-2









Heat






Heat treatment at hot stamping
























treatment






Average








before hot
Rough rolling





cooling
Average
























Multi-

rolling

Rate of

Hot rolling
Cold


rate
cooling


























layer
Manu-
Heat-
Hold-
Roll-
reduction
No. of
Finish
Coil-
rolling
Heat-
Heat-
(° C./s)
rate
Temper-

Sheet


steel
facturing
ing
ing
ing
of sheet
rolling
rolling
ing
Rolling
ing
ing
(more
(° C./s)
ing

thick-


sheet
condition
temp.
time
temp.
thickness
operations
temp
temp.
rate
rate
temp.
than
(400° C.
temp.
Plat-
ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
ing
(mm)


























26
26
1267
58
1131
24
3
884
587
40
21
869
91
84

None
1.7


27
27
1251
46
1176
22
3
861
659
47
70
893
97
93

None
1.5


28
28
1267
53
1183
22
3
893
699
59
28
877
105
100

None
1.1


29
29
1270
49
1140
35
3
896
634
61
44
877
87
69

None
1.1


30
30
981
58
 970
30
3
841
612
44
52
933
83
82

None
1.6


31
31
1320
 7
1141
47
3
906
713
42
73
893
71
62

None
1.6


32
32
1387
48
1135
29
3
858
578
50
69
843
85
69

None
1.4


33
33
1298
42
1127
20
3
899
604
 0
69
839
84
67

None
2.8


34
34
1281
55
1122
22
3
835
667
56
50
903
70
71
267
None
1.2


35
35
1289
49
1132
46
3
831
641
51
58
927
95
87
274
Yes
1.4


36
36
1318
49
1171
38
3
844
745
53
53
864
101
88

Yes
1.3


37
37
1239
48
1138
42
3
829
551
51
24
879
80
67
None
None
1.3


38
38
1250
44
1127
39
3
885
661
47
30
856
103
90

None
1.5


39
39
1251
49
1170
39
3
891
700
59
68
871
85
72

None
1.1


40
40
1322
52
1008
44
3
882
697
40
69
917
104
103

None
1.6


41
41
1333
43
1152
 3
2
893
634
59
31
934
74
76

None
1.4


42
42
1267
58
1141
40
1
906
713
50
65
903
83
78

None
1.2


43
43
1339
22
1111
38
3
899
667
51
63
892
102
93

None
1.3























TABLE A-3










Metal structures























Area rate (%)










of total of crystal










grains with










maximum difference










of crystal










orientation inside










large angle grain










boundaries of 1° or









Hardness
less and crystal




















of middle
grains with
Mechanical properties



















part in
maximum difference

Max.





Multilayer

sheet
of crystal orientation
Tensile
bending
Hydrogen



Stamped
steel sheet
Manufacturing
thickness
of 8° or more and
strength
angle
embrittlement



body no.
no.
condition no.
(Hv)
less than 15°
(MPa)
(°)
resistance
Remarks


















 1A
 1
 1
564
80
1674
87.5
Good
Inv. ex.


 2A
 2
 2
632
72
1884
79.1
Good
Inv. ex.


 3A
 3
 3
751
65
2259
72.6
Good
Inv. ex.


 4A
 4
 4
771
57
2309
75.8
Good
Inv. ex.


 5A
 5
 5
377
82
1119
89.9
Good
Comp. ex.


 6A
 6
 6
528
76
1586
86.8
Good
Inv. ex.


 7A
 7
 7
678
73
2034
79.4
Good
Inv. ex.


 8A
 8
 8
663
68
1994
75.7
Good
Inv. ex.


 9A
 9
 9
973
52
2915
63.4
Good
Comp. ex.


10A
10
10
700
69
2100
80.8
Good
Inv. ex.


11A
11
11
490
83
1467
81.7
Good
Comp. ex.


12A
12
12
630
71
1883
89.5
Good
Inv. ex.


13A
13
13
640
70
1927
88.4
Good
Inv. ex.


14A
14
14
653
68
1940
84.4
Good
Inv. ex.


15A
15
15
640
69
1918
89.3
Good
Inv. ex.


16A
16
16
642
69
1905
85.5
Good
Inv. ex.


17A
17
17
657
68
1963
83.7
Good
Inv. ex.


18A
18
18
505
80
1511
86.9
Good
Inv. ex.


19A
19
19
504
80
1502
87.4
Good
Inv. ex.


20A
20
20
500
80
1532
88.1
Good
Inv. ex.


21A
21
21
634
72
1909
78.9
Good
Inv. ex.


22A
22
22
631
72
1900
79
Good
Inv. ex.


23A
23
23
633
72
1905
77.1
Good
Inv. ex.


24A
24
24
710
65
2132
72.4
Good
Inv. ex.


25A
25
25
702
65
2084
71.9
Good
Inv. ex.


26A
26
26
703
65
2110
70.9
Good
Inv. ex.


27A
27
27
768
57
2290
74.3
Good
Inv. ex.


28A
28
28
767
57
2297
76.8
Good
Inv. ex.


29A
29
29
770
57
2308
76.2
Good
Inv. ex.


30A
30
30
631
16
1895
68.1
Poor
Comp. ex.


31A
31
31
630
18
1880
61.7
Poor
Comp. ex.


32A
32
32
632
95
1885
68.8
Good
Comp. ex.


33A
33
33
628
70
1878
83.1
Good
Inv. ex.


34A
34
34
721
63
2168
73
Good
Inv. ex.


35A
35
35
715
63
2145
78.3
Good
Inv. ex.


36A
36
36
631
70
1892
84
Good
Inv. ex.


37A
37
37
641
72
2153
72.6
Good
Inv. ex.


38A
38
38
776
56
2297
73.9
Good
Inv. ex.


39A
39
39
781
55
2381
70.2
Good
Inv. ex.


40A
40
40
627
10
2069
60.2
Poor
Comp. ex.


41A
41
41
635
11
2096
60.1
Poor
Comp. ex.


42A
42
42
625
13
2063
59.2
Poor
Comp. ex.


43A
43
43
634
46
2092
109.5
Good
Inv. ex.









Manufacturing Example B

The Nos. 1 to 18 steel sheets for sheet thickness middle part having the chemical compositions shown in Table B-1-1 (“Steel Nos. 1 to 18” in Table B-1-1) were ground down at their surfaces to remove the surface oxides. After that, the respective steel sheets for sheet thickness middle part were welded with steel sheets for surface layer having the chemical compositions shown in Table B-1-2 at both surfaces or single surfaces by arc welding to fabricate the Nos. 1 to 41 multilayer steel sheets for hot stamped body. The sheet thickness of the total of the steel sheet for surface layer and the steel sheet for sheet thickness middle part after arc welding was 200 mm to 300 mm and the thickness of the steel sheet for surface layer was ⅓ or so of the thickness of the steel sheet for sheet thickness middle part (in case of single side, ¼ or so). The No. 37 multilayer steel sheet was steel with steel sheet for surface layer welded to only one side. The multilayer steel sheets other than No. 37 respectively had steel sheets for surface layer welded to both sides of the steel sheet for sheet thickness middle part. Among the Nos. 1 to 41 multilayer steel sheets of Table B-1-3, ones where the steel sheet for sheet thickness middle part did not satisfy the requirements of composition of the middle part in sheet thickness of the hot stamped body according to the present invention are indicated as “comparative steels” in the remarks columns.


The Nos. 1 to 41 multilayer steel sheets were respectively treated under the conditions of the Nos. 1 to 41 manufacturing conditions shown in Table B-2-1 to Table B-2-2 by heat treatment before hot rolling, rough rolling, hot rolling, and cold rolling to obtain steel sheets. Next, the steel sheets were heat treated as shown in Table B-2-1 and Table B-2-2 (in the tables, “heat treatment of hot stamped body”) for hot stamping to manufacture the Nos. 1B to 41B hot stamped bodies (“stamped bodies” of Table B-3-1 and Table B-3-2). Further, the Nos. 35B and 36B hot stamped bodies were coated on a hot dip coating line at their surfaces with 120 to 160 g/m2 amounts of aluminum. Further, the items in Table B-2-1 to Table B-2-2 correspond to the items in Table A-2-1 to Table A-2-2. Further, in the tables, the fields with the notations “-” indicate no corresponding treatment performed.


Table B-3-1 and Table B-3-2 show the metal structures and characteristics of the Nos. 1B to 41B hot stamped bodies. The constituents obtained by analyzing the positions of ½ of the sheet thicknesses of the samples taken from the hot stamped bodies (middle parts in sheet thickness) and positions of 20 μm from the surfaces of the softened layers were equivalent to the constituents of the steel sheets for sheet thickness middle part and steel sheets for surface layer of the Nos. 1 to 41 multilayer steel sheets of Table B-1-1 to Table B-1-3.


The metal structures of the hot stamped steel sheets were measured by the above-mentioned method. The hardness of the steel sheet for sheet thickness middle part forming the middle part in sheet thickness and the area rate (%) of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer forming the softened layer to ½ of the thickness of that softened layer were calculated. The calculated values of the area rate are shown in the items “area rate (%) of total of crystal grains with maximum crystal orientation difference inside large angle grain boundaries of 1° or less and crystal grains with maximum crystal orientation difference of 8° or more and less than 15°” of Tables B-3-1 to Table B-3-2.


Further, the Nos. 1B to 41B hot stamped bodies were respectively measured for average hardness (HV) and minimum hardness (HV) at the middle part in sheet thickness (position of ½ of sheet thickness) by the above method. The measurement results are shown in Table B-3-1 to Table B-3-2. The Nos. 1B to 41B hot stamped bodies had differences of the average hardness (HV) and minimum hardness (HV) shown in the “scattering in cross-sectional hardness” of Table B-3-1 to Table B-3-2. Further, cases with a scattering in cross-sectional hardness of 100 HV or more were indicated as failing.


The hot stamped bodies were subjected to tensile tests. The results are shown in Table B-3-1 to Table B-3-2. The tensile tests were performed by fabricating No. 5 test pieces described in JIS Z 2201 and testing them by the method described in JIS Z 2241.


The hydrogen embrittlement resistance of the hot stamped body, in the same way as Manufacturing Example A, was evaluated using a test piece cut out from the stamped body. That is, a test piece of a sheet thickness of 1.2 mm×width 6 mm×length 68 mm was cut out from the stamped body, given a strain corresponding to the yield stress in a four-point bending test, then immersed in pH3 hydrochloric acid for 100 hours and evaluated for hydrogen embrittlement resistance by the presence of any cracks. The case of no cracks was indicated as passing (“Good”) and the case of cracks was evaluated as failing (“Poor”).


For the purpose of evaluating the impact resistance of the hot stamped body, the body was evaluated based on the VDA standard (VDA238-100) prescribed by the German Association of the Automotive Industry under the same measurement conditions as Manufacturing Example A. 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 and thereby evaluate the impact resistance of the hot stamped body.


If the tensile strength is 1500 MPa or more, the maximum bending angle (°) was 70(°) or more, and the hydrogen embrittlement resistance was a passing level, it was judged that the impact resistance and hydrogen embrittlement resistance were excellent and the case was indicated as an “invention example”. If even one of the three aspects of performance is not satisfied, the case was indicated as a “comparative example”.


In each hot stamped body of the invention examples, the area rate (%) of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness was 50% to less than 85%. Further, each hot stamped body of the invention examples was excellent in tensile strength, bendability, and hydrogen embrittlement resistance.


As opposed to this, the No. 5B hot stamped body was low in carbon content at the steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness became insufficient and the tensile strength became insufficient. The No. 9B hot stamped body was excessive in carbon content of steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness also became excessive and the targeted bendability could not be obtained. Further, the No. 11B hot stamped body was sparse in Mn content at the steel sheet for sheet thickness middle part, so the hardness of the middle part in sheet thickness became insufficient and the tensile strength became insufficient.


The Nos. 30B to 32B hot stamped bodies are comparative examples produced using the multilayer steel sheets for hot stamped body to which the desirable heat treatment had not been applied before the hot stamping process. The No. 30B hot stamped body was low in heat treatment temperature before the hot stamping process, while the No. 31B hot stamped body was short in heat treatment time before the hot stamping process, so in the metal structures of the softened layer from the surface of the softened layer to ½ of the thickness, the soft structures and metal structures with intermediate hardnesses insufficiently grew and the target bendability could not be obtained. Further, the No. 32B hot stamped body was excessively high in heat treatment temperature before the hot stamping process, so the effect of reduction of the sharp gradient in hardness in the sheet thickness direction occurring at the time of bending deformation could not be obtained.


The No. 38B hot stamped body was low in rolling temperature of the rough rolling. Further, the No. 39B hot stamped body was low in sheet thickness reduction rate of the rough rolling. Further, the No. 40B hot stamped body was low in number of rolling operations under conditions of a time between passes of 3 seconds or more. These hot stamped bodies were not manufactured under the suitable rough rolling conditions, so the soft structures and metal structures with intermediate hardnesses insufficiently grew, it was not possible to ease the strain occurring due to bending deformation, and the targeted bendability could not be obtained.


The No. 41B hot stamped body is a steel sheet controlled in casting rate to 6 ton/min or more in the continuous casting process of steel sheet for surface layer. It can raise the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness and is excellent in bendability.










TABLE B-1-1







Multilayer
Composition of constituents of steel sheet for sheet thickness middle part (mass %)




















steel sheet
Steel














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























 1
1
0.24
0.25
1.57
0.012
0.0005
0.042
0.0037







 2
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







 3
3
0.38
0.13
1.79
0.006
0.0018
0.045
0.004







 4
4
0.45
0.21
1.69
0.009
0.0015
0.025
0.0044







 5
5
0.17
0.17
1.51
0.006
0.0018
0.025
0.0035







 6
6
0.24
0.20
1.64
0.014
0.0014
0.043
0.0027







 7
7
0.33
0.15
1.75
0.016
0.0014
0.031
0.0027







 8
8
0.32
0.11
1.57
0.012
0.0020
0.045
0.0031







 9
9
0.81
0.14
1.96
0.013
0.0016
0.034
0.003







10
10
0.35
0.27
1.75
0.008
0.0013
0.033
0.003







11
11
0.3
0.22
1.05
0.014
0.0013
0.026
0.003







12
12
0.29
0.22
1.74
0.016
0.0007
0.032
0.004







13
13
0.27
0.24
1.63
0.01
0.0007
0.045
0.0043
0.20






14
14
0.35
0.20
1.55
0.012
0.0014
0.043
0.004

0.050





15
15
0.29
0.15
2.05
0.006
0.0015
0.033
0.0039


0.015




16
16
0.32
0.12
1.84
0.012
0.0007
0.032
0.0044



0.050



17
17
0.34
0.20
1.79
0.009
0.0007
0.033
0.0043




0.0019


18
1
0.24
0.25
1.57
0.012
0.0005
0.042
0.0037







19
1
0.24
0.25
1.57
0.012
0.0005
0.042
0.0037







20
1
0.24
0.25
1.57
0.012
0.0005
0.042
0.0037







21
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







22
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







23
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







24
3
0.38
0.13
1.79
0.006
0.0018
0.045
0.0040







25
3
0.38
0.13
1.79
0.006
0.0018
0.045
0.0040







26
3
0.38
0.13
1.79
0.006
0.0018
0.045
0.0040







27
4
0.45
0.21
1.69
0.009
0.0015
0.025
0.0044







28
4
0.45
0.21
1.69
0.009
0.0015
0.025
0.0044







29
4
0.45
0.21
1.69
0.009
0.0015
0.025
0.0044







30
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







31
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







32
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







33
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







34
18
0.68
0.23
1.81
0.008
0.0019
0.041
0.0036







35
18
0.68
0.23
1.81
0.008
0.0019
0.041
0.0036







36
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







37
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







38
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







39
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







40
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031







41
2
0.31
0.25
1.78
0.015
0.0009
0.032
0.0031





In the table, blanks indicate corresponding constituents not intentionally added.














TABLE B-1-2







Multilayer



steel sheet
Composition of constituents of steel sheet for surface layer (mass %)



















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





 1
0.10
0.10
0.48
0.005
0.0018
0.030
0.0036







 2
0.13
0.10
0.60
0.016
0.0008
0.033
0.0030







 3
0.11
0.07
0.75
0.015
0.0010
0.041
0.0029







 4
0.22
0.09
0.70
0.006
0.0020
0.029
0.0031







 5
0.10
0.07
0.66
0.006
0.0019
0.028
0.0041







 6
0.14
0.08
0.56
0.014
0.0019
0.033
0.0028







 7
0.11
0.05
0.58
0.008
0.0016
0.030
0.0040







 8
0.12
0.06
0.51
0.006
0.0012
0.033
0.0027







 9
0.36
0.06
0.52
0.018
0.0017
0.036
0.0032







10
0.15
0.22
0.70
0.018
0.0005
0.033
0.0042







11
0.15
0.12
0.03
0.013
0.0008
0.027
0.0044







12
0.11
0.12
0.36
0.008
0.0017
0.038
0.0041







13
0.12
0.13
0.68
0.010
0.0013
0.032
0.0027
0.15






14
0.14
0.08
0.55
0.018
0.0009
0.038
0.0040

0.010





15
0.11
0.06
0.49
0.013
0.0008
0.034
0.0032


0.010




16
0.10
0.06
0.63
0.018
0.0008
0.028
0.0039



0.050



17
0.25
0.10
0.61
0.017
0.0010
0.035
0.0039




0.0018


18
0.12
0.21
1.18
0.012
0.0008
0.029
0.0030







19
0.10
0.21
0.62
0.012
0.0007
0.037
0.0042







20
0.10
0.11
1.05
0.016
0.0011
0.033
0.0039







21
0.20
0.10
1.25
0.007
0.0007
0.029
0.0030







22
0.13
0.16
1.09
0.009
0.0014
0.033
0.0036







23
0.15
0.20
0.58
0.018
0.0019
0.027
0.0033







24
0.11
0.06
0.62
0.007
0.0005
0.041
0.0032







25
0.10
0.12
0.66
0.011
0.0017
0.030
0.0042







26
0.14
0.06
1.01
0.008
0.0016
0.027
0.0040







27
0.30
0.09
0.69
0.014
0.0011
0.041
0.0029







28
0.23
0.15
0.59
0.005
0.0013
0.040
0.0033







29
0.23
0.07
1.17
0.007
0.0010
0.030
0.0031







30
0.26
0.20
0.55
0.018
0.0020
0.043
0.0044







31
0.17
0.11
0.59
0.017
0.0011
0.035
0.0029







32
0.17
0.11
0.56
0.008
0.0014
0.032
0.0039







33
0.17
0.11
0.51
0.008
0.0018
0.036
0.0027







34
0.36
0.13
0.63
0.007
0.0005
0.042
0.0035







35
0.37
0.11
0.63
0.007
0.0011
0.029
0.0031







36
0.16
0.12
0.58
0.015
0.0005
0.033
0.0032







37
0.17
0.12
0.56
0.008
0.0009
0.030
0.0044







38
0.13
0.10
0.60
0.016
0.0008
0.033
0.0030







39
0.13
0.10
0.60
0.016
0.0008
0.033
0.0030







40
0.13
0.10
0.60
0.016
0.0008
0.033
0.0030







41
0.13
0.10
0.60
0.016
0.0008
0.033
0.0030





In the table, blanks indicate corresponding constituents not intentionally added.


















TABLE B-1-3








Steel sheet for
Sheet thickness




Multilayer
sheet thickness
of steel sheet




steel sheet
middle part
for surface




no.
Steel no.
layer (mm)
Remarks









 1
 1
85




 2
 2
83




 3
 3
84




 4
 4
97




 5
 5
94
Comp. steel



 6
 6
82




 7
 7
88




 8
 8
94




 9
 9
83
Comp. steel



10
10
88




11
11
83
Comp. steel



12
12
92




13
13
82




14
14
86




15
15
95




16
16
96




17
17
96




18
 1
95




19
 1
99




20
 1
98




21
 2
88




22
 2
84




23
 2
85




24
 3
83




25
 3
91




26
 3
88




27
 4
96




28
 4
82




29
 4
91




30
 2
93




31
 2
92




32
 2
94




33
 2
84




34
18
92




35
18
92




36
 2
84




37
 2
93




38
 2
95




39
 2
98




40
 2
85




41
 2
88



























TABLE B-2-1









Heat






Heat treatment at hot stamping























treatment






Average








before hot
Rough rolling





cooling
Average
























Multi-

rolling

Rate of

Hot rolling
Cold


rate
cooling


























layer
Manu-
Heat-
Hold-
Roll-
reduction
No. of
Finish
Coil-
rolling
Heat-
Heat-
(° C./s)
rate
Temper-

Sheet


steel
facturing
ing
ing
ing
of sheet
rolling
rolling
ing
Rolling
ing
ing
(more
(° C./s)
ing

thick-


sheet
condition
temp.
time
temp.
thickness
operations
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.
Plat-
ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
ing
(mm)


























 1
 1
1290
35
1151
33
3
917
565
50
35
858
72
49
None
None
1.4


 2
 2
1280
50
1167
31
3
911
688
44
35
849
96
89
None
None
1.6


 3
 3
1255
40
1141
22
3
915
515
57
46
861
77
65
None
None
1.2


 4
 4
1285
40
1153
39
3
887
661
40
64
896
96
86
None
None
1.7


 5
 5
1318
35
1129
40
3
895
513
55
57
916
101
81
None
None
1.3


 6
 6
1275
35
1162
33
3
885
527
57
70
880
72
61
None
None
1.2


 7
 7
1275
35
1180
51
3
896
591
49
56
912
82
78
None
None
1.4


 8
 8
1250
40
1135
47
3
895
628
35
47
902
76
76
None
None
1.8


 9
 9
1350
55
1168
30
3
920
701
35
25
863
65
60
None
None
1.8


10
10
1290
35
1136
35
3
899
611
51
35
854
73
71
None
None
1.4


11
11
1250
40
1125
38
3
894
688
50
52
871
100
102
None
None
1.4


12
12
1300
40
1171
41
3
907
652
50
63
884
78
77
None
None
1.4


13
13
1250
50
1175
26
3
896
687
38
30
895
101
93
None
None
1.7


14
14
1300
55
1142
41
3
900
714
53
43
910
68
67
None
None
1.3


15
15
1330
50
1157
46
3
906
559
40
27
909
87
78
None
None
1.7


16
16
1270
60
1146
34
3
895
710
50
31
891
107
97
None
None
1.4


17
17
1310
45
1137
45
3
899
672
34
65
901
111
114
None
None
1.8


18
18
1300
55
1151
34
3
888
664
50
50
855
95
83
None
None
1.4


19
19
1300
40
1156
40
3
917
564
50
15
915
75
66
None
None
1.4


20
20
1290
50
1122
44
3
903
666
50
23
871
108
88
None
None
1.4


21
21
1280
55
1163
46
3
907
614
57
22
868
101
89
None
None
1.2


22
22
1280
40
1171
30
3
914
514
44
34
855
96
93
None
None
1.6


23
23
1300
40
1136
42
3
888
562
47
66
878
93
79
None
None
1.5


24
24
1255
40
1164
32
3
893
524
57
70
857
75
71
None
None
1.2


25
25
1255
55
1143
39
3
910
520
57
67
899
91
83
None
None
1.2



























TABLE B-2-2









Heat






Heat treatment at hot stamping
























treatment






Average








before hot
Rough rolling





cooling
Average
























Multi-

rolling

Rate of

Hot rolling
Cold


rate
cooling


























layer
Manu-
Heat-
Hold-
Roll-
reduction
No. of
Finish
Coil-
rolling
Heat
Heat-
(° C./s)
rate
Temper-

Sheet


steel
facturing
ing
ing
ing
of sheet
rolling
rolling
ing
Rolling
ing
ing
(more
(° C./s)
ing

thick-


sheet
condition
temp.
time
temp.
thickness
operations
temp.
temp.
rate
rate
temp.
than
(400 C.
temp.
Plat-
ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
ing
(mm)


























26
26
1300
35
1127
20
3
893
527
57
23
901
88
81
None
None
1.2


27
27
1285
40
1174
27
3
901
533
40
71
869
92
90
None
None
1.7


28
28
1285
40
1178
24
3
913
522
40
31
879
102
100
None
None
1.7


29
29
1350
55
1142
33
3
905
551
40
40
912
92
66
None
None
1.7


30
30
1070
50
1010
32
3
908
638
44
55
847
88
83
None
None
1.6


31
31
1300
10
1137
48
3
892
587
44
74
862
76
66
None
None
1.6


32
32
1400
50
1140
26
3
911
642
44
68
871
82
71
None
None
1.6


33
33
1300
40
1123
16
3
916
534
 0
66
891
80
63
None
None
2.8


34
34
1280
55
1124
18
3
881
665
56
45
900
67
76
267
None
1.2


35
35
1300
40
1127
41
3
883
650
51
63
874
91
85
274
Yes
1.4


36
36
1290
50
1166
43
3
909
541
44
52
891
101
86
None
Yes
1.6


37
37
1280
50
1143
47
3
910
704
44
29
863
80
72
None
None
1.6


38
38
1330
40
1005
48
3
882
697
40
67
917
103
108

None
1.2


39
39
1310
45
1157
 3
2
893
634
59
26
934
69
74

None
1.2


40
40
1290
40
1137
41
1
906
713
50
62
903
84
82

None
1.6


41
41
1280
23
1112
41
3
899
667
51
65
892
100
90

None
1.6


























TABLE B-3-1










Metal structures





























Area rate (%)













of total of













crystal grains













with maximum













difference of













crystal orientation













inside large angle













grain boundaries













of 1° or less and
























crystal grains







Hardness
with maximum
Mechanical properties






















of middle
difference



Average

Scattering






part in
of crystal

Maximum

cross-

in cross-




Multilayer

sheet
orientation of
Tensile
bending
Hydrogen
sectional
Minimum
sectional



Stamped
steel sheet
Manufacturing
thickness
8° or more and
strength
angle
embrittlement
hardness
hardness
hardness



body no.
no.
condition no.
(Hv)
less than 15°
(MPa)
(°)
resistance
(Hv)
(Hv)
(Hv)
Remarks





















 1B
 1
 1
546
75
1621
89
Good
519
480
39
Inv. ex.


 2B
 2
 2
647
64
1836
78.6
Good
607
575
32
Inv. ex.


 3B
 3
 3
748
65
2187
72.4
Good
714
705
9
Inv. ex.


 4B
 4
 4
785
57
2328
70.7
Good
742
724
18
Inv. ex.


 5B
 5
 5
446
80
1210
89.7
Good
450
357
93
Comp. ex.


 6B
 6
 6
528
66
1579
88.1
Good
499
469
30
Inv. ex.


 7B
 7
 7
678
53
2027
79.6
Good
643
628
15
Inv. ex.


 8B
 8
 8
663
71
1982
77.3
Good
615
581
34
Inv. ex.


 9B
 9
 9
973
56
2746
57.8
Good
915
899
16
Comp. ex.


10B
10
10
700
65
2093
75.1
Good
668
655
13
Inv. ex.


11B
11
11
490
57
1362
88.5
Good
458
327
131
Comp. ex.


12B
12
12
618
54
1847
81.3
Good
588
562
26
Inv. ex.


13B
13
13
590
65
1760
82.5
Good
568
540
28
Inv. ex.


14B
14
14
705
77
2085
73.5
Good
655
631
24
Inv. ex.


15B
15
15
618
60
1832
80.2
Good
591
580
11
Inv. ex.


16B
16
16
662
65
1975
81.7
Good
625
618
7
Inv. ex.


17B
17
17
683
71
2034
74.3
Good
649
638
11
Inv. ex.


18B
18
18
534
80
1564
86.1
Good
504
461
43
Inv. ex.


19B
19
19
537
78
1596
89.2
Good
522
473
49
Inv. ex.


20B
20
20
541
60
1621
89.5
Good
518
497
21
Inv. ex.


21B
21
21
639
82
1901
77.4
Good
598
588
10
Inv. ex.


22B
22
22
630
75
1874
79.2
Good
581
567
14
Inv. ex.


23B
23
23
625
68
1850
80.8
Good
578
559
19
Inv. ex.


24B
24
24
740
60
2105
73.5
Good
691
681
10
Inv. ex.


25B
25
25
735
76
2195
71.1
Good
667
656
11
Inv. ex.


























TABLE B-3-2










Metal structures





























Area rate (%)













of total of













crystal 1 grains













with maximum













difference of













crystal orientation













inside large angle













grain boundaries













of 1° or less























Hardness
and crystal grains
Mechanical properties






















of middle
with maximum



Average

Scattering






part in
difference of

Maximum

cross-

in cross-




Multilayer

sheet
crystal orientation
Tensile
bending
Hydrogen
sectional
Minimum
sectional



Stamped
steel sheet
Manufacturing
thickness
of 8° or more and
strength
angle
embrittlement
hardness
hardness
hardness



body no.
no.
condition no.
(Hv)
less than 15°
(MPa)
(°)
resistance
(Hv)
(Hv)
(Hv)
Remarks





















26B
26
26
731
78
2187
70.8
Good
671
654
17
Inv. ex.


27B
27
27
791
70
2387
72.5
Good
754
737
17
Inv. ex.


28B
28
28
775
63
2317
73
Good
739
717
22
Inv. ex.


29B
29
29
780
78
2271
74.5
Good
734
721
13
Inv. ex.


30B
30
30
657
15
1975
61.6
Poor
627
605
22
Comp. ex.


31B
31
31
647
18
1931
62.4
Poor
620
600
20
Comp. ex.


32B
32
32
644
90
1957
65.1
Good
611
599
12
Comp. ex.


33B
33
33
645
84
1930
75.8
Good
605
551
54
Inv. ex.


34B
34
34
745
64
2180
78.5
Good
717
702
15
Inv. ex.


35B
35
35
740
75
2260
79.3
Good
726
707
19
Inv. ex.


36B
36
36
647
71
1941
77.7
Good
611
581
30
Inv. ex.


37B
37
37
647
65
1920
78.1
Good
614
587
27
Inv. ex.


38B
38
38
643
 9
2122
59.9
Poor
643
614
29
Comp. ex.


39B
39
39
637
10
2102
59.8
Poor
637
608
29
Comp. ex.


40B
40
40
645
12
2129
60.1
Poor
645
615
30
Comp. ex.


41B
41
41
641
45
2115
111.2
Good
641
611
30
Inv. ex.









Manufacturing Example C

Steel sheets for sheet thickness middle part having the chemical compositions shown in Table C-1-1 to Table C-1-2 were ground down at their surfaces to remove the surface oxides. After that, the respective steel sheets for sheet thickness middle part were welded with steel sheets for surface layer having the chemical compositions shown in Table C-1-3 to Table C-1-4 at both surfaces or single surfaces by arc welding to fabricate the Nos. 1 to 49 multilayer steel sheets for hot stamped body. The sheet thickness of the total of the steel sheet for surface layer and the steel sheet for sheet thickness middle part after arc welding was 200 mm to 300 mm and the thickness of the steel sheet for surface layer was ⅓ or so of the thickness of the steel sheet for sheet thickness middle part (in case of single side, ¼ or so). The No. 31 multilayer steel sheet was steel with steel sheet for surface layer welded to only one side. Among the Nos. 1 to 53 multilayer steel sheets of Table C-1-1 to Table C-1-4, ones where the steel sheet for sheet thickness middle part did not satisfy the requirements of composition of the middle part in sheet thickness of the hot stamped body according to the present invention are indicated as “comparative steels” in the remarks columns.


The “ratio of C, Si, and Mn contents of steel sheet for surface layer to steel sheet for sheet thickness middle part” of Table C-1-3 to Table C-1-4 show the ratios of C, Si, and Mn contents of steel sheet for surface layer to the C, Si, and Mn contents of steel sheet for sheet thickness middle part in the Nos. 1 to 53 multilayer steel sheets for hot stamped body.


The Nos. 1 to 53 multilayer steel sheets were respectively treated under the conditions of the Nos. 1 to 53 manufacturing conditions shown in Table C-2-1 to Table C-2-2 by heat treatment before hot rolling, rough rolling, hot rolling, and cold rolling to obtain steel sheets. Next, the steel sheets were heat treated as shown in Table C-2-1 to Table C-2-2 (in the tables, “heat treatment of hot stamped body”) for hot stamping to manufacture the Nos. 1C to 53C hot stamped bodies (“stamped bodies” of Table C-3-1 to Table C-3-2). Further, the No. 30C hot stamped body was coated on a hot dip coating line at the surface with a 120 to 160 g/m2 amount of aluminum. Further, the items in Table C-2-1 to Table C-2-2 correspond to the items in Table A-2-1 to Table A-2-2. Further, in the tables, the fields with the notations “-” indicate no corresponding treatment performed.


Table C-3-1 to Table C-3-2 show the metal structures and characteristics of the Nos. 1C to 53C hot stamped bodies. The constituents obtained by analyzing the positions of ½ of the sheet thicknesses of the samples taken from the hot stamped bodies (middle parts in sheet thickness) and positions of 20 μm from the surfaces of the softened layers were equivalent to the constituents of the steel sheets for sheet thickness middle part and the steel sheets for surface layer of the Nos. 1 to 53 multilayer steel sheets of Table C-1-1 to Table C-1-4.


The metal structures of the hot stamped steel sheets were measured by the above-mentioned method. The hardness of the steel sheet for sheet thickness middle part forming the middle part in sheet thickness and the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer forming the softened layer to ½ of the thickness of that softened layer were calculated. The calculated values of the area rate are shown in the items “area rate (%) of total of crystal grains with maximum crystal orientation difference inside large angle grain boundaries of 1° or less and crystal grains with maximum crystal orientation difference of 8° or more and less than 15°” of Tables C-3-1 to C-3-2.


The hot stamped bodies were subjected to tensile tests. The results are shown in Table C-3-1 to Table C-3-2. The tensile tests were performed by fabricating No. 5 test pieces described in JIS Z 2201 and testing them by the method described in JIS Z 2241.


The hydrogen embrittlement resistance of the hot stamped body, in the same way as Manufacturing Example A, was evaluated using a test piece cut out from the stamped body. That is, a test piece of a sheet thickness of 1.2 mm×width 6 mm×length 68 mm was cut out from the stamped body, given a strain corresponding to the yield stress in a four-point bending test, then immersed in pH3 hydrochloric acid for 100 hours and evaluated for hydrogen embrittlement resistance by the presence of any cracks. The case of no cracks was indicated as passing (“Good”) and the case of cracks was evaluated as failing (“Poor”).


For the purpose of evaluating the impact resistance of the hot stamped body, the body was evaluated based on the VDA standard (VDA238-100) prescribed by the German Association of the Automotive Industry under the same measurement conditions as Manufacturing Example A. 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 and thereby evaluate the impact resistance of the hot stamped body.


If the tensile strength is 1500 MPa or more, the maximum bending angle (°) was 70(°) or more, the uniform elongation was 5% or more, and the hydrogen embrittlement resistance was a passing level, it was judged that the impact resistance, hydrogen embrittlement resistance, and ductility were excellent and the case was indicated as an “invention example”. If even one of the three aspects of performance is not satisfied, the case was indicated as a “comparative example”.


In each hot stamped body of the invention examples, the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness of the steel sheet for surface layer was 50% to less than 85%. Further, each hot stamped body of the invention examples was excellent in tensile strength, bendability, and hydrogen embrittlement resistance.


As opposed to this, the No. 5C hot stamped body was low in carbon content of the steel sheet for sheet thickness middle part, so became insufficient in hardness of the middle part in sheet thickness and became insufficient in tensile strength. The No. 9C hot stamped body was excessive in carbon content of the steel sheet for sheet thickness middle part, so also became excessive in hardness of the middle part in sheet thickness and could not be given the targeted bendability. Further, the No. 11C hot stamped body was low in Si content of the steel sheet for sheet thickness middle part, so the area percent of the residual austenite of the metal structures at the middle part in sheet thickness was less than 1.0% and the uniform elongation was low.


The Nos. 25C to 27C and 49C hot stamped bodies are comparative examples manufactured using the multilayer steel sheets for hot stamped body to which the preferable heat treatment is not applied before the hot stamping process. The No. 25C hot stamped body is too low in heat treatment temperature before the hot stamping process, so the soft structures and metal structures with intermediate hardnesses insufficiently grew, the effect of surface properties of the hot stamped body and effect of the transitional part from the middle part in sheet thickness to the softened layer could not be eliminated, and excellent bendability could not be obtained.


Further, the No. 26C hot stamped body was excessively high in heat treatment time before the hot stamping process, so the soft structures and metal structures with intermediate hardnesses excessively grew, the difference in hardness between the softened layer and the middle part in sheet thickness became too large, and the effect of reducing the sharp gradient of hardness in the sheet thickness direction occurring at the time of bending deformation could not be obtained. For this reason, the No. 26C hot stamped body could not be given the targeted bendability.


Further, the Nos. 27C and 49C hot stamped bodies were too long in heat treatment time before the hot stamping process, the difference in hardness between the softened layer and the middle part in sheet thickness become too great. Further, the heat treatment temperature was excessively high, so the effect of reducing the sharp gradient of hardness in the sheet thickness direction occurring at the time of bending deformation could not be obtained. For this reason, the Nos. 27C and 49C hot stamped bodies could not be given excellent bendability.


The No. 50C hot stamped body was low in rolling temperature of the rough rolling. Further, the No. 51C hot stamped body was low in sheet thickness reduction rate of the rough rolling. Further, the No. 52C hot stamped body was low in number of rolling operations under conditions of a time between passes of 3 seconds or more. These hot stamped bodies were not manufactured under the suitable rough rolling conditions, so the soft structures and metal structures with intermediate hardnesses insufficiently grew, it was not possible to ease the strain occurring due to bending deformation, and the targeted bendability could not be obtained.


The No. 53C hot stamped body is a steel sheet controlled in casting rate to 6 ton/min or more in the continuous casting process of steel sheet for surface layer. It can raise the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness and is excellent in bendability.










TABLE C-1-1







Multilayer



steel sheet
Composition of constituents of steel sheet for sheet thickness middle part (mass %)




















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























 1
0.22
1.67
1.23
0.007
0.0025
0.036
0.0041
0
0
0
0
0



 2
0.36
1.84
0.68
0.011
0.0028
0.027
0.0053
0
0
0
0
0



 3
0.28
2.29
1.33
0.012
0.0015
0.056
0.0030
0
0
0
0
0



 4
0.50
1.33
1.15
0.006
0.0043
0.032
0.0068
0
0
0
0
0



 5
0.19
2.23
1.48
0.006
0.0033
0.059
0.0044
0
0
0
0
0
Comp. steel


 6
0.20
0.71
1.21
0.005
0.0029
0.025
0.0053
0
0
0
0
0



 7
0.22
2.70
1.21
0.010
0.0045
0.046
0.0055
0
0
0
0
0



 8
0.24
1.14
0.65
0.009
0.0049
0.036
0.0032
0
0
0
0
0



 9
0.72
1.45
0.68
0.007
0.0007
0.038
0.0060
0
0
0
0
0
Comp. steel


10
0.22
1.50
0.58
0.006
0.0059
0.052
0.0036
0
0
0
0
0



11
0.34
0.42
1.18
0.010
0.0020
0.030
0.0038
0
0
0
0
0
Comp. steel


12
0.36
1.29
1.25
0.010
0.0016
0.041
0.0019
0
0
0
0
0



13
0.25
0.85
0.80
0.006
0.0004
0.034
0.0023
0.10
0
0
0
0



14
0.27
1.12
1.49
0.005
0.0007
0.031
0.0011
0
0
0
0
0.0015



15
0.26
1.71
1.34
0.010
0.0051
0.034
0.0047
0
0.045
0.025
0
0.0020



16
0.22
0.72
1.42
0.010
0.0041
0.047
0.0066
0
0
0
0
0



17
0.23
0.58
1.13
0.012
0.0001
0.041
0.0062
0
0
0
0
0



18
0.37
2.64
0.58
0.004
0.006
0.035
0.0044
0
0
0
0
0



19
0.32
1.03
1.21
0.008
0.0038
0.030
0.0021
0
0
0
0
0



20
0.37
2.35
0.56
0.007
0.0036
0.059
0.0053
0
0
0
0
0



21
0.30
0.95
0.89
0.011
0.0035
0.054
0.0031
0
0
0
0
0



22
0.55
1.03
1.00
0.004
0.0004
0.028
0.0055
0
0.020
0.025
0
0.0015



23
0.56
1.80
1.04
0.009
0.0060
0.023
0.0053
0
0
0
0
0



24
0.51
0.65
0.76
0.008
0.0028
0.036
0.0028
0
0
0
0
0



25
0.36
2.06
1.42
0.005
0.0020
0.041
0.0013
0
0
0
0
0



26
0.33
1.01
1.27
0.011
0.0027
0.049
0.0041
0
0
0
0
0



29
0.61
2.88
0.60
0.011
0.0047
0.058
0.0047
0
0
0
0
0



30
0.64
2.41
1.34
0.004
0.0006
0.038
0.0064
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.














TABLE C-1-2







Multilayer



steel sheet
Chemical consttuents of steel sheet for sheet thickness middle part (mass %)




















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























31
0.32
1.13
0.84
0.006
0.0032
0.043
0.0014
0
0
0
0
0



32
0.31
2.44
0.81
0.100
0.0060
2.600
0.0052
0
0
0
0
0



33
0.28
2.08
0.67
0.083
0.0040
0.057
0.0030
2.50
0
0
0
0



34
0.25
1.81
0.82
0.108
0.0030
0.053
0.0053
0.05
0
0
0
0



35
0.34
2.48
1.08
0.072
0.0020
0.042
0.0033
0
0.120
0
0
0



36
0.40
2.78
1.33
0.112
0.0030
0.059
0.0034
0
0
0.130
0
0



37
0.28
1.89
0.80
0.088
0.0020
0.046
0.0034
0
0
0
0.600
0



38
0.36
2.04
0.96
0.066
0.0050
0.059
0.0031
0
0
0
0.100
0



39
0.38
2.48
1.05
0.084
0.0060
0.054
0.0057
0
0
0
0
0.0070



40
0.31
2.43
1.11
0.100
0.0020
0.039
0.0036
0
0
0
0
0



41
0.36
2.37
1.36
0.066
0.0040
0.035
0.0034
0
0
0
0
0



42
0.32
1.93
1.08
0.119
0.0060
0.055
0.0055
0
0
0
0
0



43
0.31
1.93
0.63
0.082
0.0040
0.053
0.0038
0
0
0
0
0



44
0.27
2.13
1.09
0.103
0.0040
0.049
0.0034
0
0
0
0
0



45
0.37
1.96
0.64
0.074
0.0050
0.055
0.0044
0
0
0
0
0



46
0.25
2.80
0.60
0.080
0.0030
0.053
0.0037
0
0
0
0
0



47
0.34
2.00
1.38
0.095
0.0040
0.034
0.0054
0
0
0
0
0



48
0.33
2.41
1.26
0.071
0.0060
0.055
0.0032
0
0
0
0
0



49
0.35
2.55
1.32
0.066
0.0050
0.037
0.0038
0
0
0
0
0



50
0.36
1.84
0.68
0.011
0.0028
0.027
0.0053
0
0
0
0
0



51
0.36
1.84
0.68
0.011
0.0028
0.027
0.0053
0
0
0
0
0



52
0.36
1.84
0.68
0.011
0.0028
0.027
0.0053
0
0
0
0
0



53
0.36
1.84
0.68
0.011
0.0028
0.027
0.0053
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.



























TABLE C-1-3




















Thickness
















of steel
















sheet for



Multilayer












surface











steel sheet
Composition of constituents of steel sheet for surface layer (mass %)
layer






















no.
C
Si
Mn
P
S
sol.Al
N
Ni
Nb
Ti
Mo
B
(mm)
Remarks
























 1
0.106
0.735
0.517
0.006
0.0024
0.048
0.0046
0
0
0
0
0
96



 2
0.173
1.030
0.360
0.006
0.0065
0.036
0.0016
0
0
0
0
0
91



 3
0.099
0.847
0.399
0.006
0.0032
0.036
0.0035
0
0
0
0
0
95



 4
0.294
0.479
0.414
0.006
0.0056
0.039
0.0070
0
0
0
0
0
96



 5
0.082
1.115
0.592
0.003
0.0070
0.034
0.0020
0
0
0
0
0
78
Comp. steel


 6
0.075
0.355
0.520
0.006
0.0018
0.034
0.0031
0
0
0
0
0
82



 7
0.100
1.485
0.387
0.009
0.0025
0.034
0.0068
0
0
0
0
0
84



 8
0.143
0.684
0.390
0.009
0.0038
0.027
0.0027
0
0
0
0
0
106



 9
0.310
0.827
0.252
0.009
0.0078
0.035
0.0059
0
0
0
0
0
85
Comp. steel


10
0.106
0.795
0.313
0.006
0.0080
0.029
0.0058
0
0
0
0
0
85



11
0.174
0.151
0.578
0.004
0.0062
0.049
0.0048
0
0
0
0
0
103
Comp. steel


12
0.182
0.606
0.713
0.011
0.0039
0.032
0.0031
0
0
0
0
0
75



13
0.095
0.357
0.408
0.005
0.0019
0.043
0.0010
0
0
0
0
0
94



14
0.155
0.437
0.760
0.006
0.0023
0.031
0.0024
0
0
0
0
0.0017
89



15
0.153
1.163
0.965
0.012
0.0071
0.040
0.0035
0
0.045
0.025
0
0.0015
83



16
0.096
0.518
0.809
0.009
0.0025
0.050
0.0034
0
0
0
0
0
87



17
0.086
0.197
0.848
0.005
0.0071
0.032
0.0017
0
0
0
0
0
86



18
0.260
1.320
0.209
0.003
0.0027
0.032
0.0070
0
0
0
0
0
90



19
0.287
0.453
1.041
0.006
0.0062
0.035
0.0020
0
0
0
0
0
102



20
0.296
2.021
0.235
0.008
0.0056
0.026
0.0054
0
0
0
0
0
101



21
0.189
0.352
0.472
0.004
0.0045
0.040
0.0036
0
0
0
0
0
105



22
0.456
0.474
0.570
0.004
0.0069
0.034
0.0054
0
0
0
0
0
84



23
0.373
1.278
0.530
0.004
0.0051
0.043
0.0051
0
0
0
0
0
102



24
0.224
0.371
0.631
0.010
0.0028
0.029
0.0038
0.10
0
0
0
0
88



25
0.155
1.030
0.667
0.011
0.0049
0.021
0.0061
0
0
0
0
0
84



26
0.184
0.313
0.762
0.011
0.0075
0.031
0.0044
0
0
0
0
0
89





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.
















TABLE C-1-4









Thickness





of steel



Multilayer

sheet for



steel
Composition of constituents of steel sheet for surface layer (mass %)
surface






















sheet no.
C
Si
Mn
P
S
sol.Al
N
Ni
Nb
Ti
Mo
B
layer (mm)
Remarks
























29
0.262
1.699
0.180
0.009
0.0045
0.038
0.0027
0
0
0
0
0
86



30
0.230
0.940
0.590
0.007
0.0076
0.034
0.0046
0
0
0
0
0
81



31
0.188
0.350
0.454
0.007
0.0048
0.049
0.0064
0
0
0
0
0
162



32
0.146
0.625
1.127
0.006
0.0040
0.040
0.0045
0
0
0
0
0
103



33
0.118
0.545
1.120
0.007
0.0050
0.039
0.0088
0
0
0
0
0
88



34
0.130
0.484
1.128
0.010
0.0030
0.033
0.0077
0
0
0
0
0
107



35
0.136
0.588
0.893
0.012
0.0020
0.021
0.0073
0
0
0
0
0
81



36
0.200
0.673
0.680
0.012
0.0060
0.043
0.0051
0
0
0
0
0
102



37
0.120
0.530
0.966
0.012
0.0050
0.023
0.0056
0
0
0
0
0
96



38
0.180
0.650
1.680
0.007
0.0020
0.050
0.0099
0
0
0
0
0
100



39
0.163
0.383
1.250
0.007
0.0030
0.036
0.0053
0
0
0
0
0
92



40
0.177
0.519
0.800
0.009
0.0030
0.047
0.0097
2.20
0
0
0
0
91



41
0.209
0.573
1.081
0.009
0.0060
0.042
0.0041
0.05
0
0
0
0
86



42
0.157
0.522
1.368
0.011
0.0040
0.023
0.0067
0
0.110
0
0
0
103



43
0.183
0.447
1.566
0.012
0.0040
0.046
0.0064
0
0
0.110
0
0
89



44
0.130
0.423
1.260
0.010
0.0020
0.048
0.0065
0
0
0
0.600
0
92



45
0.215
0.567
1.120
0.013
0.0050
0.045
0.0052
0
0
0
0.100
0
109



46
0.130
0.672
1.653
0.009
0.0050
0.036
0.0059
0
0
0
0
0.010
82



47
0.160
0.452
1.276
0.007
0.0050
0.028
0.0049
0
0
0
0
0.001
88



48
0.211
0.595
1.612
0.011
0.0030
0.020
0.0070
0
0
0
0
0
97



49
0.172
0.656
0.846
0.010
0.0030
0.029
0.0094
0
0
0
0
0
91



50
0.173
1.030
0.360
0.006
0.0065
0.036
0.0016
0
0
0
0
0
91



51
0.173
1.030
0.360
0.006
0.0065
0.036
0.0016
0
0
0
0
0
91



52
0.173
1.030
0.360
0.006
0.0065
0.036
0.0016
0
0
0
0
0
91



53
0.173
1.030
0.360
0.006
0.0065
0.036
0.0016
0
0
0
0
0
91





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.




















TABLE C-2-1












Heat treatment at hot stamping



























Average







Heat treatment
Rough rolling




cooling
Average
























before hot

Rate of
No. of
Hot rolling
Cold


rate
cooling
























Manu-
rolling
Roll-
reduction
rolling
Finish
Coil-
rolling
Heat-
Heat-
(° C./s)
rate
Tem-

Sheet






















facturing
Heating
Holding
ing
of sheet
opera-
rolling
ing
Rolling
ing
ing
(more
(° C./s)
pering

thick-


condition
temp.
time
temp.
thickness
tions
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.

ness


no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
Plating
(mm)

























1
1275
45
1144
36
3
948
609
69
39
847
70
44

None
1.6


2
1274
21
1166
31
3
872
510
66
39
848
98
42

None
1.4


3
1300
23
1145
26
3
924
665
63
41
882
79
29

None
1.4


4
1278
31
1162
39
3
869
741
50
68
916
94
30

None
1.2


5
1333
26
1129
45
3
925
635
41
61
849
100
29

None
1.0


6
1315
55
1161
32
3
915
581
50
68
891
75
25

None
1.2


7
1193
40
1180
52
3
920
678
51
55
822
87
28

None
1.2


8
1239
27
1137
52
3
919
606
61
48
838
80
37

None
1.4


9
1329
53
1169
28
3
905
550
52
23
872
63
30

None
1.1


10
1191
52
1145
39
3
909
686
45
32
836
76
27

None
1.0


11
1143
56
1135
43
3
921
747
66
50
903
96
30

None
1.4


12
1171
50
1150
36
3
942
546
49
62
873
74
38

None
1.1


13
1108
33
1102
23
3
883
619
45
35
898
101
33

None
1.0


14
1323
44
1149
37
3
886
633
46
41
869
69
25

None
1.0


15
1169
35
1150
46
3
856
500
50
24
925
88
27

None
1.0


16
1127
43
1112
31
3
863
500
69
36
904
104
25

None
1.6


17
1135
38
1128
49
3
881
590
60
64
850
113
44

None
1.4


18
1111
50
1103
38
3
948
541
60
49
826
100
32

None
1.4


19
1194
39
1159
43
3
939
606
55
15
900
71
28

None
1.2


20
1277
23
1131
40
3
920
563
49
25
917
104
32

None
1.0


21
1131
31
1121
48
3
867
693
42
25
889
97
41

None
1.0


22
1204
32
1167
33
3
938
514
57
35
886
98
44

None
1.2


23
1231
22
1129
44
3
876
668
60
71
896
90
32

None
1.4


24
1160
23
1142
32
3
936
657
53
75
855
74
26

None
1.2


25

1070

20

1020

40
3
943
523
53
65
892
96
27

None
1.2


26

1370

43
1123
16
3
912
666
49
20
907
86
43

None
1.1





In the table, fields with notations — indicate corresponding treatment not performed.




















TABLE C-2-2












Heat treatment at hot stamping



























Average







Heat treatment
Rough rolling




cooling
Average
























before hot

Rate of
No. of
Hot rolling
Cold


rate
cooling
























Manu-
rolling
Roll-
reduction
rolling
Finish
Coil-
rolling
Heat-
Heat-
(° C./s)
rate
Tem-

Sheet






















facturing
Heating
Holding
ing
of sheet
opera-
rolling
ing
Rolling
ing
ing
(more
(° C./s)
pering

thick-


condition
temp.
time
temp.
thickness
tions
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.

ness


no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
Plating
(mm)

























29
1192
21
1145
35
3
941
659
57
35
919
89
33
322
None
1.2


30
1336
54
1136
37
3
864
649
60
55
926
92
27
395
Yes
1.4


31
1178
25
1135
50
3
861
708
44
74
852
72
38

None
1


32
1258
37
1137
23
3
900
630
45
65
947
80
34

None
1.7


33
1246
47
1128
13
3
868
576
45
62
841
85
44

None
1.2


34
1226
32
1121
22
3
868
576
56
41
891
67
27

None
1.1


35
1208
23
1123
38
3
895
588
47
62
937
88
41

None
1.5


36
1256
46
1160
46
3
879
616
52
53
906
100
29

None
1.1


37
1196
50
1152
52
3
881
621
56
33
895
81
43

None
1.3


38
1191
58
1152
44
3
894
563
53
33
856
104
38

None
1.1


39
1245
34
1121
22
3
893
618
52
69
848
72
37

None
1.6


40
1236
51
1166
22
3
937
622
45
67
873
83
30

None
1.6


41
1217
32
1170
29
3
945
628
45
70
913
98
30

None
1.7


42
1248
23
1143
35
3
864
554
46
28
861
70
35

None
1.7


43
1237
24
1150
35
3
918
620
57
67
842
93
42

None
1.2


44
1188
33
1132
51
3
924
621
55
28
925
97
35

None
1.7


45
1183
23
1131
21
3
909
621
48
39
835
82
36

None
1


46
1236
24
1126
14
3
910
590
52
56
846
102
39

None
1.1


47
1239
42
1125
22
3
917
595
50
67
838
72
37

None
1.4


48
1195
56
1124
39
3
896
642
57
67
893
88
39

None
1.8


49
1214

15

1182
22
3
853
583
51
66
910
99
33

None
1.1


50
1208
32

1013

48
3
882
697
40
71
917
107
26

None
1.7


51
1191
50
1161

4

2
893
634
59
28
934
71
36

None
1


52
1236
34
1137
46

1

906
713
50
63
903
84
32

None
1


53
1248
22
1103
46
3
899
667
51
60
892
96
34

None
1.4





In the table, fields with notations — indicate corresponding treatment not performed.

















TABLE C-3-1










Metal






structure


















Any rate








(%) of








total of








crystal








grains








with








maximum








difference








of








crystal








orientation








inside








large








angle








grain








boundaries








of 1° or








less and








crystal








grains with







Hard-
maximum







ness
difference







of
of







middle
crystal





Multi-
Manu-
part in
orientation
Mechanical properties



















layer
facturing
sheet
of 8°


Maximum

Residual



Stamped
steel
condi-
thick-
or more
Tensile
Uniform
bending
Hydrogen
γ area



body
sheet
tion
ness
and less
strength
elongation
angle
embrittlement
rate



no.
no.
no.
(Hv)
than 15°
(MPa)
(%)
(°)
resistance
(%)
Remarks




















 1C
1
1
576
70
1547
5.2
87.5
Good
4.5
Inv. ex.


 2C
2
2
738
50
2083
7.5
95.6
Good
2.6
Inv. ex.


 3C
3
3
639
58
2156
5.6
95.6
Good
3
Inv. ex.


 4C
4
4
785
68
2212
6
71.1
Good
1.7
Inv. ex.


 5C
5
5

402

55

1116

6.5
91.9
Good
4

Comp. ex.



 6C
6
6
554
54
1770
6.2
88.5
Good
3.8
Inv. ex.


 7C
7
7
567
65
1644
7.2
85.5
Good
2.9
Inv. ex.


 8C
8
8
592
79
1963
6.6
82.2
Good
4.4
Inv. ex.


 9C
9
9

823

64
2442
5.6

39.4

Good
1

Comp. ex.



10C
10
10
694
71
1805
7.5
80.4
Good
2.5
Inv. ex.


11C
11
11
664
55
2145

4.2

97.7
Good

0.8


Comp. ex.



12C
12
12
727
82
2062
6.3
88.2
Good
3.1
Inv. ex.


13C
13
13
622
84
1901
5.7
89.8
Good
2
Inv. ex.


14C
14
14
667
85
1969
7.4
84.7
Good
4.8
Inv. ex.


15C
15
15
542
54
1545
5.2
81
Good
2
Inv. ex.


16C
16
16
590
80
1536
7.5
83.9
Good
2.6
Inv. ex.


17C
17
17
513
80
1549
6.8
92.8
Good
2.6
Inv. ex.


18C
18
18
759
59
2024
6.1
88
Good
2.3
Inv. ex.


19C
19
19
603
77
2006
6.4
87
Good
2.9
Inv. ex.


20C
20
20
578
81
1895
6.3
92.3
Good
4.6
Inv. ex.


21C
21
21
713
79
2035
5.8
87.6
Good
4.9
Inv. ex.


22C
22
22
683
74
2690
7.2
75.6
Good
3.6
Inv. ex.


23C
23
23
726
69
2475
6.4
78.1
Good
4.3
Inv. ex.


24C
24
24
771
55
2450
5.5
73.2
Good
1.9
Inv. ex.


25C
25
25
700

15

1964
7.5

54.3


Poor

1

Comp. ex.



26C
26
26
728

92

1832
7.1

54.2

Good
3

Comp. ex.






















TABLE C-3-2










Metal







structure



















Any rate








(%) of








total of








crystal








grains








with








maximum








difference








of








crystal








orientation








inside








large








angle








grain








boundaries








of 1° or








less and








crystal








grains with







Hard-
maximum







ness
difference







of
of







middle
crystal





Multi-
Manu-
part in
orientation
Mechanical properties



















layer
facturing
sheet
of 8°


Maximum

Residual



Stamped
steel
condi-
thick-
or more
Tensile
Uniform
bending
Hydrogen
γ area



body
sheet
tion
ness
and less
strength
elongation
angle
embrittlement
rate



no.
no.
no.
(Hv)
than 15°
(MPa)
(%)
(°)
resistance
(%)
Remarks




















29C
29
29
792
51
2102
5.8
89.1
Good
4.7
Inv. ex.


30C
30
30
698
70
2317
5.1
81.8
Good
3.5
Inv. ex.


31C
31
31
695
56
2139
6.6
82
Good
3
Inv. ex.


32C
32
32
633
72
2018
5.5
74
Good
3.7
Inv. ex.


33C
33
33
671
62
2261
6.9
90
Good
2.6
Inv. ex.


34C
34
34
612
64
2240
6.2
73
Good
3.3
Inv. ex.


35C
35
35
682
71
2055
7.5
82
Good
4.3
Inv. ex.


36C
36
36
622
61
2118
5.8
86
Good
2.5
Inv. ex.


37C
37
37
659
50
2003
5.7
75
Good
2.4
Inv. ex.


38C
38
38
647
72
2253
6.5
87
Good
2.9
Inv. ex.


39C
39
39
614
73
2072
7.4
75
Good
3.4
Inv. ex.


40C
40
40
649
56
2115
5.8
83
Good
2.6
Inv. ex.


41C
41
41
606
62
2167
6.6
90
Good
2.9
Inv. ex.


42C
42
42
639
61
2032
6.4
83
Good
4.5
Inv. ex.


43C
43
43
670
53
2140
8
75
Good
4.1
Inv. ex.


44C
44
44
669
67
2055
7
88
Good
2.9
Inv. ex.


45C
45
45
692
53
2246
6.5
78
Good
4.4
Inv. ex.


46C
46
46
673
62
2222
6.5
90
Good
2.1
Inv. ex.


47C
47
47
659
56
2156
6.5
90
Good
2.7
Inv. ex.


48C
48
48
625
52
2177
7.8
85
Good
2.3
Inv. ex.


49C
49
49
656

13

2222
6.5

62


Poor

2.8

Comp. ex.



50C
50
50
630

9

2079
6.7

59.1


Poor

3.1

Comp. ex.



51C
51
51
644

10

2125
6.2

59.8


Poor

3.1

Comp. ex.



52C
52
52
635

13

2096
6.3

60.4


Poor

3.2

Comp. ex.



53C
53
53
638
47
2105
6.3
112.5
Good
3.1
Inv. ex.









Manufacturing Example D

Steel sheets for sheet thickness middle part having the Nos. 1 to 37 chemical compositions shown in Table D-1-1 to Table D-1-2 (in the tables, “Steel Nos. 1 to 37”) were ground down at their surfaces to remove the surface oxides. After that, the respective steel sheets for sheet thickness middle part were welded with steel sheets for surface layer having the chemical compositions shown in Table D-1-3 to Table D-1-4 at both surfaces or single surfaces by arc welding to fabricate the Nos. 1 to 60 multilayer steel sheets for hot stamped body. The sheet thickness of the total of the steel sheet for surface layer and the steel sheet for sheet thickness middle part after arc welding was 200 mm to 300 mm and the thickness of the steel sheet for surface layer was ⅓ or so of the thickness of the steel sheet for sheet thickness middle part (in case of single side, ¼ or so). The No. 37 multilayer steel sheet is steel with the steel sheet for surface layer welded to only one surface. The multilayer steel sheets other than No. 37 have steel sheets for surface layer welded to both surfaces of the steel sheet for sheet thickness middle part. In the Nos. 1 to 60 multilayer steel sheets of Table D-1-1 to Table D-1-4, cases where the steel sheet for sheet thickness middle part does not satisfy the requirement of the composition of the middle part in sheet thickness of the hot stamped body according to the present invention are indicated as “comparative steels” in the remarks column.


The Nos. 1 to 60 multilayer steel sheets were treated under the conditions of the Nos. 1 to 60 manufacturing conditions shown in Table D-2-1 to Table D-2-3 by heat treatment before hot rolling, rough rolling, hot rolling, and cold rolling to obtain steel sheets. Next, the steel sheets were heat treated as shown in Table D-2-1 to Table D-2-3 (in the tables, “heat treatment of hot stamped bodies”) for hot stamping to produce the Nos. 1D to 60D hot stamped bodies (“stamped bodies” of Tables D-3-1 to D-3-3). Further, the Nos. 38D and 39D hot stamped bodies were coated on a hot dip coating line at the surfaces with 120 to 160 g/m2 amounts of aluminum. Further, the items of Table D-2-1 to Table D-2-3 correspond to the items of Table A-2-1 to Table A-2-2. Further, in the tables, the fields with the notations “-” indicate no corresponding treatment performed.


Tables D-3-1 to D-3-3 show the metal structures and characteristics of the Nos. 1D to 60D hot stamped bodies. The constituents obtained by analyzing the positions of ½ of the sheet thicknesses of the samples taken from hot stamped bodies (middle parts in sheet thickness) and positions of 20 μm from the surfaces of the softened layers were equivalent to the constituents of the steel sheets for sheet thickness middle part and the steel sheets for surface layer of the Nos. 1 to 60 multilayer steel sheets of Table D-1-1 to Table D-1-3.


The metal structures of the hot stamped steel sheets were measured by the above-mentioned method. The hardness of the steel sheet for sheet thickness middle part forming the middle part in sheet thickness and the area rate of the total of the crystal grains with a maximum crystal orientation difference inside the regions surrounded by grain boundaries of 15° or more of 1° or less and the crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer forming the softened layer to ½ of the thickness of that softened layer were calculated. The calculated values of the area rate are shown in the items “area rate (%) of total of crystal grains with maximum crystal orientation difference inside large angle grain boundaries of 1° or less and crystal grains with maximum crystal orientation difference of 8° or more and less than 15°” of Tables D-3-1 to D-3-3.


The Nos. 1D to 60D hot stamped bodies were subjected to tensile tests. The results are shown in Tables D-3-1 to D-3-3. The tensile tests were performed by fabricating No. 5 test pieces described in JIS Z 2201 and testing them by the method described in JIS Z 2241.


The hot stamped bodies were evaluated for hydrogen embrittlement resistance in the same way as Manufacturing Example A using test pieces cut out from the stamped bodies. That is, test pieces of a sheet thickness of 1.2 mm×width 6 mm×length 68 mm were cut out from the stamped bodies, given strain corresponding to the yield stress in four-point bending tests, then immersed in pH3 hydrochloric acid for 100 hours and evaluated for hydrogen embrittlement resistance by the presence of any cracks. Cases of no fracture were evaluated as passing (“good”) and cases of fracture were evaluated as failing (“Poor”).


For the purpose of evaluating the impact resistance of the hot stamped body, the body was evaluated based on the VDA standard (VDA238-100) prescribed by the German Association of the Automotive Industry under the same measurement conditions as Manufacturing Example A. 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 and thereby evaluate the impact resistance of the hot stamped body.


The hot stamped bodies were also evaluated for impact resistance from the viewpoint of ductility. Specifically, the hot stamped steel sheets were subjected to tensile tests to find the uniform elongations of the steel sheet to evaluate the impact resistance. The tensile tests were performed by fabricating No. 5 test pieces described in JIS Z 2201 and testing them by the method described in JIS Z 2241. The elongations where the maximum tensile loads were obtained were defined as the uniform elongations.


Deformation concentrates at a local softened part at the time of collision and becomes a cause of cracking, so a small scattering in hardness at the stamped body, that is, securing stable strength, is important in securing impact resistance. Therefore, the impact resistance of a hot stamped body was also evaluated from the viewpoint of the scattering in hardness. A cross-section vertical to the longitudinal direction of a long hot stamped body was taken at any position in that longitudinal direction and measured for hardness at the middle position in sheet thickness at the entire cross-sectional region including the vertical walls. For the measurement, use was made of a Vickers hardness tester. The measurement load was 1 kgf, 10 points were measured, and the measurement interval was 1 mm. The difference between the average cross-sectional hardness and the minimum hardness is shown in Table D-3-1 to Table D-3-3. Cases with no measurement points of below 100 Hv from the average value of all measurement points were evaluated as being small in scattering in hardness, that is, excellent in stability of strength and, as a result, were evaluated as excellent in impact resistance and therefore passing, while cases with measurement points below 100 Hv were evaluated as failing.


Cases where the tensile strength was 1500 MPa or more, the uniform elongation was 5% or more, the scattering in hardness was a passing level, the maximum bending angle (°) was 70.0(°) or more, and the hydrogen embrittlement resistance was passing were evaluated as hot stamped bodies excellent in impact resistance and hydrogen embrittlement resistance (“invention examples” in Table D-3-1 to Table D-3-3). On the other hand, cases where even one of the above five aspects of performance was not satisfied are indicated as “comparative examples”.


In each of the hot stamped bodies of the invention examples, the area rate of the total of crystal grains with a maximum crystal orientation difference inside regions surrounded by grain boundaries of 15° or higher of 1° or less and crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness was 50% to less than 85%. Further, in each of the hot stamped bodies of the invention examples, the tensile strength, bendability, and hydrogen embrittlement resistance were excellent.


As opposed to this, the No. 5D hot stamped body was low in carbon content of the steel sheet for sheet thickness middle part, so became insufficient in hardness of the middle part in sheet thickness and became insufficient in tensile strength. The No. 9D hot stamped body was excessive in carbon content of the steel sheet for sheet thickness middle part, so became excessive in hardness of the middle part in sheet thickness as well and could not be given the targeted bendability. Further, the Nos. 10D and 11D hot stamped bodies were sparse in Si content of the steel sheet for sheet thickness middle part, so were insufficient in uniform elongation. Further, the No. 12D hot stamped body was insufficient in Mn content, so became insufficient in hardness of the middle part in sheet thickness and were insufficient in tensile strength. The No. 14D and the No. 15D hot stamped bodies were sparse in Si content and Mn content, so had an area percent of residual austenite of less than 1.0% and an insufficient uniform elongation. Further, the No. 12D to No. 15D hot stamped bodies were large in scattering in hardness and deemed failing.


The Nos. 33D to 35D hot stamped bodies are comparative examples produced using multilayer steel sheets for hot stamped body which were not subjected to the desirable heat treatment before the hot stamping process. The No. 33D hot stamped body was low in heat treatment temperature before the hot stamping process, so became insufficient in growth of soft structures and metal structures of intermediate hardnesses in the metal structures of the softened layer from the surface of the softened layer to ½ of the thickness and was not able to be given the targeted bendability. The No. 34D hot stamped body was excessively high in heat treatment temperature before the hot stamping process, so the fraction of structures from a position of 20 μm from the surface of the softened layer to a position of a depth of ½ of the thickness of the softened layer exceeded 85%. For this reason, in the No. 34D hot stamped body, the difference in hardness between the softened layer and the middle part in sheet thickness became too large, and the effect of reduction of the sharp gradient in hardness in the sheet thickness direction occurring at the time of bending deformation could not be obtained. Further, the No. 35D hot stamped body was short in heat treatment time before the hot stamping process, so in the metal structures from the surface of the softened layer to ½ of the thickness, the soft structures and metal structures with intermediate hardnesses insufficiently grew and the target bendability could not be obtained.


The No. 40D hot stamped body was excessive in Si content, so residual austenite was excessively produced exceeding an area percent of 5%. For this reason, the No. 40D hot stamped body was inferior in bendability. The No. 41D hot stamped body was excessive in Mn content, so became the greatest in tensile strength among the Nos. 1D to 56D hot stamped bodies and was inferior in bendability. The No. 42D hot stamped body was poor in content of acid soluble aluminum, so inclusions containing oxygen were excessively produced and bendability was inferior. Further, the No. 45D hot stamped body included excessive aluminum, so oxides mainly comprised of aluminum were excessively produced and bendability was inferior.


The No. 57D hot stamped body was low in rolling temperature of the rough rolling. Further, the No. 58D hot stamped body was low in sheet thickness reduction rate of the rough rolling. Further, the No. 59D hot stamped body was low in number of rolling operations under conditions of a time between passes of 3 seconds or more. These hot stamped bodies were not produced under optimal rough rolling conditions, so were insufficient in growth of soft structures and metal structures of intermediate hardnesses, were not able to be eased in strain caused by bending deformation, and were not able to be given the targeted bendability.


The No. 60D hot stamped body is steel sheet with a casting rate controlled to 6 ton/min or more in a continuous casting process of steel sheet for surface layer. It can raise the area rate of the total of crystal grains with a maximum crystal orientation difference inside regions surrounded by grain boundaries of 15° or higher of 1° or less and crystal grains with a crystal orientation difference of 8° or more and less than 15° in the metal structures from the surface of the steel sheet for surface layer to ½ of the thickness and is excellent in bendability.











TABLE D-1-1







Multi-




layer




steel
Chemical constituents of steel sheet for sheet thickness middle part (mass %)






















sheet
Steel















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
























1
1
0.26
1.32
1.82
0.013
0.0028
0.049
0.0036
0
0
0
0
0



2
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



3
3
0.35
1.54
1.68
0.013
0.0011
0.043
0.0036
0
0
0
0
0



4
4
0.48
1.5
2.08
0.005
0.0002
0.035
0.0026
0
0
0
0
0



5
5

0.08

1.25
1.77
0.016
0.0010
0.029
0.0036
0
0
0
0
0

Comp. steel



6
6
0.23
1.45
1.98
0.016
0.0014
0.035
0.0037
0
0
0
0
0



7
7
0.36
1.81
1.89
0.010
0.0018
0.044
0.0032
0
0
0
0
0



8
8
0.28
1.75
1.90
0.011
0.0017
0.054
0.0029
0
0
0
0
0



9
9

0.83

1.65
1.84
0.017
0.0008
0.034
0.0027
0
0
0
0
0

Comp. steel



10
10
0.38

0.13

1.87
0.009
0.0022
0.058
0.003
0
0
0
0
0

Comp. steel



11
11
0.32

0.41

1.90
0.020
0.0016
0.048
0.0038
0
0
0
0
0

Comp. steel



12
12
0.25
1.21

0.19

0.012
0.0009
0.046
0.0023
0
0
0
0
0

Comp. steel



13
13
0.31
1.27

0.90

0.006
0.0021
0.052
0.0028
0
0
0
0
0

Comp. steel



14
14
0.34

0.48


1.34

0.018
0.0016
0.051
0.0041
0
0
0
0
0

Comp. steel



15
15
0.27

0.27


1.18

0.016
0.0008
0.053
0.0031
0
0
0
0
0

Comp. steel



16
16
0.30
1.59
1.75
0.004
0.0012
0.052
0.0030
0.33
0
0
0
0



17
17
0.36
1.00
1.78
0.022
0.0007
0.045
0.0032
0
0.078
0
0
0



18
18
0.27
1.63
1.97
0.016
0.0012
0.051
0.0029
0
0
0.032
0
0



19
19
0.29
1.27
2.01
0.013
0.0013
0.057
0.0030
0
0
0
0.040
0



20
20
0.30
1.45
1.72
0.014
0.0016
0.043
0.0032
0
0
0
0
0.0020



21
1
0.26
1.32
1.82
0.013
0.0028
0.049
0.0036
0
0
0
0
0



22
1
0.26
1.32
1.82
0.013
0.0028
0.049
0.0036
0
0
0
0
0



23
1
0.26
1.32
1.82
0.013
0.0028
0.049
0.0036
0
0
0
0
0



24
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



25
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



26
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



27
3
0.35
1.54
1.68
0.013
0.0011
0.043
0.0036
0
0
0
0
0



28
3
0.35
1.54
1.68
0.013
0.0011
0.043
0.0036
0
0
0
0
0



29
3
0.35
1.54
1.68
0.013
0.0011
0.043
0.0036
0
0
0
0
0



30
4
0.48
1.5
2.08
0.005
0.0002
0.035
0.0026
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.















TABLE D-1-2







Multi-




layer




steel
Chemical constituents of steel sheet for sheet thickness middle part (mass %)






















sheet
Steel















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
























31
4
0.48
1.50
2.08
0.005
0.0002
0.035
0.0026
0
0
0
0
0



32
4
0.48
1.50
2.08
0.005
0.0002
0.035
0.0026
0
0
0
0
0



33
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



34
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



35
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



36
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



37
21
0.65
1.29
1.84
0.008
0.0005
0.058
0.003
0
0
0
0
0



38
21
0.65
1.29
1.84
0.008
0.0005
0.058
0.003
0
0
0
0
0



39
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



40
22
0.38

5.30

1.87
0.009
0.0022
0.058
0.003
0
0
0
0
0

Comp. steel



41
23
0.25
1.21

4.90

0.012
0.0009
0.046
0.0023
0
0
0
0
0

Comp. steel



42
24
0.26
1.32
1.82
0.013
0.0028

0.0001

0.0036
0
0
0
0
0

Comp. steel



43
25
0.26
1.32
1.82
0.013
0.0028
0.001
0.0036
0
0
0
0
0



44
26
0.26
1.32
1.82
0.013
0.0028
2.600
0.0036
0
0
0
0
0



45
27
0.26
1.32
1.82
0.013
0.0028

4.200

0.0036
0
0
0
0
0

Comp. steel



46
28
0.30
1.59
1.75
0.004
0.0012
0.052
0.0030
0.03
0
0
0
0



47
29
0.30
1.59
1.75
0.004
0.0012
0.052
0.0030
2.70
0
0
0
0



48
30
0.36
1.00
1.78
0.022
0.0007
0.045
0.0032
0
0.020
0
0
0



49
31
0.36
1.00
1.78
0.022
0.0007
0.045
0.0032
0
0.130
0
0
0



50
32
0.27
1.63
1.97
0.016
0.0012
0.051
0.0029
0
0
0.040
0
0



51
33
0.27
1.63
1.97
0.016
0.0012
0.051
0.0029
0
0
0.120
0
0



52
34
0.29
1.27
2.01
0.013
0.0013
0.057
0.003
0
0
0
0.009
0



53
35
0.29
1.27
2.01
0.013
0.0013
0.057
0.003
0
0
0
0.900
0



54
36
0.30
1.45
1.72
0.014
0.0016
0.043
0.0032
0
0
0
0
0.0009



55
37
0.30
1.45
1.72
0.014
0.0016
0.043
0.0032
0
0
0
0
0.0070



56
4
0.48
1.50
2.08
0.005
0.0002
0.035
0.0026
0
0
0
0
0



57
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



58
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



59
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0



60
2
0.27
1.29
1.84
0.012
0.0011
0.045
0.0035
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.















TABLE D-1-3







Multi-




layer




steel




sheet
Chemical constituents of steel sheet for sheet thickness middle part (mass %)





















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























1
0.15
0.66
0.91
0.011
0.0026
0.045
0.0031
0
0
0
0
0



2
0.12
0.72
0.94
0.01
0.0008
0.041
0.003
0
0
0
0
0



3
0.19
0.88
0.96
0.009
0.0008
0.038
0.0031
0
0
0
0
0



4
0.28
0.78
1.14
0.004
0.0001
0.029
0.0021
0
0
0
0
0



5
0.05
0.60
0.90
0.014
0.0006
0.024
0.0034
0
0
0
0
0

Comp. steel



6
0.11
0.80
1.09
0.013
0.0011
0.029
0.0035
0
0
0
0
0



7
0.17
0.81
0.91
0.009
0.0015
0.041
0.0029
0
0
0
0
0



8
0.15
0.86
0.86
0.007
0.0014
0.050
0.0027
0
0
0
0
0



9
0.39
0.79
0.92
0.015
0.0005
0.029
0.0024
0
0
0
0
0

Comp. steel



10
0.21
0.06
0.94
0.004
0.0021
0.053
0.0027
0
0
0
0
0

Comp. steel



11
0.16
0.24
0.93
0.019
0.0015
0.042
0.0035
0
0
0
0
0

Comp. steel



12
0.14
0.64
0.11
0.009
0.0005
0.041
0.0021
0
0
0
0
0

Comp. steel



13
0.17
0.64
0.41
0.002
0.0017
0.046
0.0024
0
0
0
0
0

Comp. steel



14
0.16
0.24
0.72
0.014
0.0015
0.046
0.0036
0
0
0
0
0

Comp. steel



15
0.14
0.15
0.58
0.013
0.0006
0.047
0.0029
0
0
0
0
0

Comp. steel



16
0.15
0.78
0.95
0.003
0.0008
0.046
0.0028
0.21
0
0
0
0



17
0.17
0.55
0.91
0.020
0.0003
0.040
0.0027
0
0.036
0
0
0



18
0.15
0.85
1.04
0.013
0.0009
0.046
0.0026
0
0
0.028
0
0



19
0.15
0.74
1.13
0.008
0.0012
0.054
0.0027
0
0
0
0.030
0



20
0.17
0.78
0.81
0.013
0.0012
0.039
0.0027
0
0
0
0
0.0020



21
0.21
0.59
0.87
0.009
0.0027
0.044
0.0031
0
0
0
0
0



22
0.12
0.91
0.82
0.009
0.0027
0.043
0.0032
0
0
0
0
0



23
0.14
0.73
1.55
0.010
0.0025
0.044
0.0032
0
0
0
0
0



24
0.21
0.59
1.03
0.009
0.0009
0.041
0.0033
0
0
0
0
0



25
0.14
0.95
0.83
0.009
0.0007
0.039
0.0031
0
0
0
0
0



26
0.15
0.66
1.69
0.011
0.0008
0.041
0.0032
0
0
0
0
0



27
0.28
0.75
0.81
0.010
0.001
0.039
0.0032
0
0
0
0
0



28
0.20
1.40
0.96
0.008
0.0009
0.037
0.0032
0
0
0
0
0



29
0.17
0.89
1.46
0.009
0.0009
0.037
0.0031
0
0
0
0
0



30
0.41
0.75
1.1
0.002
0.0009
0.032
0.0021
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.















TABLE D-1-4







Multi-




layer




steel




sheet
Chemical constituents of steel sheet for sheet thickness middle part (mass %)





















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























31
0.24
1.26
1.02
0.003
0.0009
0.029
0.0021
0
0
0
0
0



32
0.27
0.84
1.68
0.003
0.0009
0.030
0.0024
0
0
0
0
0



33
0.13
0.62
1.01
0.010
0.0009
0.039
0.0032
0
0
0
0
0



34
0.16
0.62
0.83
0.007
0.0010
0.041
0.0031
0
0
0
0
0



35
0.12
0.63
0.96
0.007
0.0010
0.040
0.0033
0
0
0
0
0



36
0.15
0.66
0.85
0.011
0.0009
0.040
0.0031
0
0
0
0
0



37
0.3
0.59
1.03
0.006
0.0003
0.053
0.0027
0
0
0
0
0



38
0.32
0.74
0.98
0.007
0.0003
0.054
0.0028
0
0
0
0
0



39
0.14
0.58
0.86
0.008
0.0008
0.042
0.0033
0
0
0
0
0



40
0.21
0.06
0.94
0.007
0.002
0.054
0.0026
0
0
0
0
0

Comp. steel



41
0.14
0.64
0.11
0.011
0.0006
0.043
0.0018
0
0
0
0
0

Comp. steel



42
0.15
0.66
0.91
0.01
0.0026
0.042
0.0032
0
0
0
0
0

Comp. steel



43
0.15
0.66
0.91
0.01
0.0026
0.043
0.0032
0
0
0
0
0



44
0.15
0.66
0.91
0.011
0.0026
2.595
0.0032
0
0
0
0
0



45
0.15
0.66
0.91
0.009
0.0026
2.819
0.0031
0
0
0
0
0

Comp. steel



46
0.15
0.78
0.95
0.002
0.0011
0.047
0.0027
0.04
0
0
0
0



47
0.15
0.78
0.95
0.002
0.0008
0.049
0.0025
2.60
0
0
0
0



48
0.17
0.55
0.91
0.021
0.0004
0.041
0.0028
0
0.030
0
0
0



49
0.17
0.55
0.91
0.019
0.0006
0.042
0.0030
0
0.120
0
0
0



50
0.15
0.85
1.04
0.011
0.0010
0.046
0.0027
0
0
0.060
0
0



51
0.15
0.85
1.04
0.012
0.0009
0.046
0.0025
0
0
0.110
0
0



52
0.15
0.74
1.13
0.009
0.0011
0.052
0.0025
0
0
0
0.010
0



53
0.15
0.74
1.13
0.008
0.0011
0.054
0.0027
0
0
0
0.800
0



54
0.17
0.78
0.81
0.009
0.0015
0.037
0.0027
0
0
0
0
0.001



55
0.17
0.78
0.81
0.009
0.0014
0.037
0.0029
0
0
0
0
0.006



56
0.2
0.98
1.44
0.003
0.0009
0.030
0.0024
0
0
0
0
0



57
0.12
0.72
0.94
0.01
0.0008
0.041
0.003
0
0
0
0
0



58
0.12
0.72
0.94
0.01
0.0008
0.041
0.003
0
0
0
0
0



59
0.12
0.72
0.94
0.01
0.0008
0.041
0.003
0
0
0
0
0



60
0.12
0.72
0.94
0.01
0.0008
0.041
0.003
0
0
0
0
0





In the table, fields with compositions of constituents of 0 indicate corresponding constituents not intentionally added.





















TABLE D-2-1









Heat
Rough rolling


Heat treatment at hot stamping

























treatment

Rate of


Cold


Average








before hot

reduc-

Hot rolling
roll-


cooling
Average

























Multi-
Manu-
rolling

tion of
No. of
Finish

ing


rate
cooling


























layer
facturing
Heat-
Hold-
Roll-
sheet
rolling
roll-
Coil-
Roll-
Heat-
Heat-
(° C./s)
rate
Temper-

Sheet


steel
condi-
ing
ing
ing
thick-
opera-
ing
ing
ing
ing
ing
(more
(° C./s)
ing

thick-


sheet
tion
temp.
time
temp.
ness
tions
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.

ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
Plating
(mm)


























1
1
1220
47
1147
33
3
854
556
45
39
895
69
41
None
None
1.5


2
2
1205
43
1156
26
3
855
674
54
35
899
94
42
None
None
1.3


3
3
1218
43
1141
24
3
840
602
48
37
910
78
28
None
None
1.5


4
4
1254
38
1164
35
3
834
601
50
69
898
99
33
None
None
1.4


5
5
1268
23
1123
44
3
831
675
53
61
886
97
27
None
None
1.3


6
6
1260
23
1153
31
3
856
614
42
70
904
76
21
None
None
1.6


7
7
1264
46
1170
47
3
862
553
54
57
891
88
32
None
None
1.3


8
8
1224
32
1141
52
3
870
680
49
52
908
83
37
None
None
1.4


9
9
1153
38
1123
23
3
843
600
46
28
893
68
31
None
None
1.5


10
10
1263
23
1140
36
3
845
564
50
37
891
72
22
None
None
1.4


11
11
1239
38
1132
42
3
865
627
54
55
910
101
30
None
None
1.3


12
12
1249
45
1180
31
3
831
582
48
58
883
69
41
None
None
1.5


13
13
1177
57
1155
18
3
840
684
54
30
910
100
38
None
None
1.3


14
14
1223
36
1150
36
3
856
578
43
39
898
65
22
None
None
1.6


15
15
1240
34
1149
45
3
853
714
49
20
884
90
31
None
None
1.4


16
16
1229
25
1154
27
3
849
637
52
36
897
101
22
None
None
1.3


17
17
1151
39
1127
46
3
868
582
54
64
883
111
41
None
None
1.3


18
18
1192
28
1162
36
3
857
643
49
52
884
95
35
None
None
1.4


19
19
1316
32
1159
43
3
832
677
47
14
892
66
26
None
None
1.5


20
20
1264
44
1140
39
3
859
628
45
29
904
107
37
None
None
1.5
























TABLE D-2-2









Heat
Rough rolling


Heat treatment at hot stamping

























treatment

Rate of


Cold


Average








before hot

reduc-


roll-


cooling
Average





Multi-
Manu-
rolling

tion of
No. of
Hot rolling
ing


rate
cooling


























layer
facturing
Heat-
Hold-
Roll-
sheet
rolling
Finish
Coil-
Roll-
Heat-
Heat-
(° C./s)
rate
Temper-

Sheet


steel
condi-
ing
ing
ing
thick-
opera-
rolling
ing
ing
ing
ing
(more
(° C./s)
ing

thick-


sheet
tion
temp.
time
temp.
ness
tions
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.

ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
Plating
(mm)


























21
21
1217
23
1170
46
3
858
601
47
21
890
99
38
None
None
1.5


22
22
1165
40
1158
31
3
840
621
48
36
895
95
40
None
None
1.5


23
23
1259
39
1127
44
3
854
552
51
66
881
85
33
None
None
1.4


24
24
1176
32
1171
28
3
849
643
42
78
909
77
25
None
None
1.6


25
25
1153
29
1137
40
3
834
597
51
62
883
92
30
None
None
1.4


26
26
1193
39
1128
11
3
856
608
45
20
898
83
47
None
None
1.5


27
27
1250
54
1181
23
3
861
651
42
72
909
95
41
None
None
1.6


28
28
1304
32
1169
23
3
842
707
43
40
910
108
26
None
None
1.6


29
29
1226
27
1153
31
3
864
633
43
33
894
89
29
None
None
1.6


30
30
1188
38
1141
33
3
861
566
49
50
897
91
28
None
None
1.4


31
31
1267
36
1144
47
3
853
597
44
77
893
69
40
None
None
1.6


32
32
1262
36
1128
20
3
859
687
51
64
885
83
37
None
None
1.4


33
33

1084

37

1052

12
3
836
647
43
59
892
87
43
None
None
1.6


34
34

1372

50
1118
17
3
861
623
52
40
899
63
31
None
None
1.3


35
35
1204

14

1127
34
3
850
555
49
57
910
84
43
None
None
1.4


36
36
1274
29
1153
44
3
865
713
0
53
892
105
26
None
None
2.8


37
37
1294
51
1145
52
3
868
671
54
35
897
78
43
258
None
1.3


38
38
1211
43
1160
43
3
855
562
48
34
890
99
33
271
Yes
1.5


39
39
1305
51
1111
17
3
840
679
46
72
901
71
37
None
Yes
1.5


40
40
1229
47
1159
21
3
847
555
50
62
892
85
26
None
None
1.4
























TABLE D-2-3









Heat
Rough rolling


Heat treatment at hot stamping

























treatment

Rate of


Cold


Average








before hot

reduc-


roll-


cooling
Average





Multi-

rolling

tion of
No. of
Hot rolling
ing


rate
cooling


























layer
Manu-
Heat-
Hold-
Roll-
sheet
rolling
Finish
Coil-
Roll-
Heat-
Heat-
(° C./s)
rate
Temper-

Sheet


steel
facturing
ing
ing
ing
thick-
opera-
rolling
ing
ing
ing
ing
(more
(° C./s)
ing

thick-


sheet
condition
temp.
time
temp.
ness
tions
temp.
temp.
rate
rate
temp.
than
(400° C.
temp.

ness


no.
no.
(° C.)
(min)
(° C.)
(%)
(times)
(° C.)
(° C.)
(%)
(° C./s)
(° C.)
400° C.)
or less)
(° C.)
Plating
(mm)


























41
41
1270
30
1161
29
3
848
596
48
70
897
100
29
None
None
1.5


42
42
1233
56
1145
33
3
839
608
45
32
879
66
34
None
None
1.5


43
43
1247
40
1158
35
3
850
576
45
69
888
88
40
None
None
1.5


44
44
1237
36
1141
47
3
841
583
45
31
885
98
40
None
None
1.5


45
45
1246
54
1134
17
3
851
591
45
36
894
80
38
None
None
1.5


46
46
1257
51
1136
9
3
838
636
52
59
887
105
36
None
None
1.3


47
47
1239
33
1126
21
3
847
565
52
72
875
70
35
None
None
1.3


48
48
1265
57
1130
37
3
852
565
54
65
876
83
42
None
None
1.3


49
49
1235
56
1183
19
3
849
638
54
66
877
98
34
None
None
1.3


50
50
1276
45
1155
31
3
842
624
49
72
883
107
27
None
None
1.4


51
51
1232
38
1138
50
3
846
565
49
25
889
69
37
None
None
1.4


52
52
1257
26
1128
18
3
848
564
47
66
890
89
36
None
None
1.5


53
53
1220
31
1132
12
3
845
628
47
64
893
94
31
None
None
1.5


54
54
1215
38
1130
17
3
842
555
45
29
877
81
31
None
None
1.5


55
55
1264
33
1132
39
3
843
644
45
68
890
93
29
None
None
1.5


56
56
1261
37
1192
18
3
856
681
51
59
855
91
35
None
None
1.4


57
57
1246
40

1019

47
3
841
596
48
69
885
106
28
None
None
1.5


58
58
1265
54
1163
1
2
852
591
45
32
875
75
39
None
None
1.5


59
59
1232
56
1143
41
1
842
565
54
61
877
88
36
None
None
1.3


60
60
1215
21
1102
43
3
848
638
49
57
893
96
32
None
None
1.5





















TABLE D-3-1










Metal structure




















Any rate









(%) of









total of









crystal









grains









with









maximum









difference









of









crystal









orientation









inside









large









angle









grain









boundaries









of 1° or









less and









crystal

Mechanical properties























grains with



Average








Hard-
maximum



cross








ness
difference



sec-








of
of



tional








middle
crystal



hard-






Multi-
Manu-
part in
orientation



ness






layer
facturing
sheet
of 8°
Residual


mini-
Maximum




Stamped
steel
condi-
thick-
or more
γ area
Tensile
Uniform
mum
bending
Hydrogen



body
sheet
tion
ness
and less
rate
strength
elongation
hard-
angle
embrittlement



no.
no.
no.
(Hv)
than 15°
(%)
(MPa)
(%)
ness
(°)
resistance
Remarks





















 1D
1
1
600
82
2.5
1740
5.2
43
84.8
Good
Inv. ex.


 2D
2
2
671
78
2.2
1945
5.1
26
75.6
Good
Inv. ex.


 3D
3
3
768
71
3.3
2227
6.3
44
73.4
Good
Inv. ex.


 4D
4
4
793
63
4.7
2300
6.8
68
74.9
Good
Inv. ex.


 5D
5
5

420

84
3.2

1218

6.1
53
88.9
Good

Comp. ex.



 6D
6
6
570
66
4.4
1653
6.8
44
86.6
Good
Inv. ex.


 7D
7
7
720
83
4
2088
6.4
60
76.2
Good
Inv. ex.


 8D
8
8
699
78
2.3
2026
5.8
61
76.2
Good
Inv. ex.


 9D
9
9

1014

52
2.8
2941
5.8
58

61.2

Good

Comp. ex.



10D
10
10
741
71

0.2

2148

2.6

35
80
Good

Comp. ex.



11D
11
11
751
81

0.5

2478

4.3

43
83.6
Good

Comp. ex.



12D
12
12

443

84
3.5

1285

6.4

167

89.2
Good

Comp. ex.



13D
13
13

492

53
4.6

1427

6.8

155

86.8
Good

Comp. ex.



14D
14
14
632
63

0.7

1832

4.8


115

76.8
Good

Comp. ex.



15D
15
15
629
83

0.3

1824

3.7


127

74.1
Good

Comp. ex.



16D
16
16
681
78
4.3
1975
6.9
41
89.6
Good
Inv. ex.


17D
17
17
688
65
2.6
1995
5
49
88.3
Good
Inv. ex.


18D
18
18
685
63
3.2
1987
6.1
72
86.2
Good
Inv. ex.


19D
19
19
678
79
3.8
1966
6.9
38
82.9
Good
Inv. ex.


20D
20
20
697
67
2.7
2021
5.4
64
84.5
Good
Inv. ex.





















TABLE D-3-2










Metal structure




















Any rate









(%) of









total of









crystal









grains









with









maximum









difference









of









crystal









orientation









inside









large









angle









grain









boundaries









of 1° or









less and









crystal

Mechanical properties























grains with



Average








Hard-
maximum



cross








ness
difference



sec-








of
of



tional








middle
crystal



hard-






Multi-
Manu-
part in
orientation



ness






layer
facturing
sheet
of 8°
Residual


mini-
Maximum




Stamped
steel
condi-
thick-
or more
γ area
Tensile
Uniform
mum
bending
Hydrogen



body
sheet
tion
ness
and less
rate
strength
elongation
hard-
angle
embrittlement



no.
no.
no.
(Hv)
than 15°
(%)
(MPa)
(%)
ness
(°)
resistance
Remarks





















21D
21
21
542
72
2.5
1573
5.6
57
79.5
Good
Inv. ex.


22D
22
22
546
80
4.5
1584
6.8
56
78.6
Good
Inv. ex.


23D
23
23
540
64
4.5
1567
6.9
27
87.6
Good
Inv. ex.


24D
24
24
669
68
3.1
1940
6.1
32
75.3
Good
Inv. ex.


25D
25
25
671
73
3
1945
5.9
69
80.5
Good
Inv. ex.


26D
26
26
676
82
3
1960
5.3
39
74.6
Good
Inv. ex.


27D
27
27
749
66
4.3
2171
6.6
32
82.3
Good
Inv. ex.


28D
28
28
747
80
3.6
2166
5.7
36
81.2
Good
Inv. ex.


29D
29
29
742
72
2.4
2151
5.7
56
76.7
Good
Inv. ex.


30D
30
30
781
67
3.9
2265
5.4
27
83.7
Good
Inv. ex.


31D
31
31
792
79
2.8
2297
5.5
69
75.7
Good
Inv. ex.


32D
32
32
788
77
4.1
2285
6.7
64
84.9
Good
Inv. ex.


33D
33
33
668

14

4.6
1937
6.9
44

66.8


Poor


Comp. ex.



34D
34
34
667

95

4.6
1934
6.9
52

67.4

Good

Comp. ex.



35D
35
35
673

17

4.2
1951
6.8
26

61.9


Poor


Comp. ex.



36D
36
36
671
61
3.1
1945
6.1
28
82.4
Good
Inv. ex.


37D
37
37
763
69
4.4
2213
6.6
44
71.2
Good
Inv. ex.


38D
38
38
753
71
4.2
2184
5.9
26
78.5
Good
Inv. ex.


39D
39
39
669
77
2.9
1940
5.8
54
82.5
Good
Inv. ex.


40D
40
40
743
71

12.5

2148
8
67

61.8

Good

Comp. ex.






















TABLE D-3-3










Metal structure




















Any rate









(%) of









total of









crystal









grains









with









maximum









difference









of









crystal









orientation









inside









large









angle









grain









boundaries









of 1° or









less and









crystal

Mechanical properties























grains with



Average








Hard-
maximum



cross








ness
difference



sec-








of
of



tional








middle
crystal



hard-






Multi-
Manu-
part in
orientation



ness






layer
facturing
sheet
of 8°
Residual


mini-
Maximum




Stamped
steel
condi-
thick-
or more
γ area
Tensile
Uniform
mum
bending
Hydrogen



body
sheet
tion
ness
and less
rate
strength
elongation
hard-
angle
embrittlement



no.
no.
no.
(Hv)
than 15°
(%)
(MPa)
(%)
ness
(°)
resistance
Remarks





















41D
41
41
792
84
3.5
2610
6.3
26
51.2
Good

Comp. ex.



42D
42
42
605
83
2.1
1997
5.2
42

64.1

Good

Comp. ex.



43D
43
43
612
75
2.5
2020
5.4
71
84.5
Good
Inv. ex.


44D
44
44
608
76
2.2
2006
5.5
65
84.4
Good
Inv. ex.


45D
45
45
605
84
2.3
1997
5.3
40

56.1

Good

Comp. ex.



46D
46
46
651
76
4.3
2148
6.8
39
88.7
Good
Inv. ex.


47D
47
47
701
79
4.4
2313
6.9
60
89.8
Good
Inv. ex.


48D
48
48
661
63
2.5
2181
5.1
57
88.1
Good
Inv. ex.


49D
49
49
703
65
2.6
2320
5.3
41
88.7
Good
Inv. ex.


50D
50
50
658
61
3
2171
5.9
34
86.7
Good
Inv. ex.


51D
51
51
709
64
3.3
2340
6.2
60
85.1
Good
Inv. ex.


52D
52
52
661
77
3.7
2181
6.7
65
81.6
Good
Inv. ex.


53D
53
53
682
80
3.8
2251
7
61
82.5
Good
Inv. ex.


54D
54
54
683
65
2.4
2254
5.3
25
81.8
Good
Inv. ex.


55D
55
55
705
67
2.8
2327
5.5
68
84.4
Good
Inv. ex.


56D
56
56
781
76
4
2577
6.6
61
85.3
Good
Inv. ex.


57D
57
57
642

10

2.9
2119
6.3
30

59.2


Poor


Comp. ex.



58D
58
58
634

11

3.0
2092
6.7
26

61.4


Poor


Comp. ex.



59D
59
59
637

12

3.0
2102
6.6
22

61.9


Poor


Comp. ex.



60D
60
60
636
46
3.0
2099
6.7
27
111.8
Good
Inv. ex.









INDUSTRIAL APPLICABILITY

The hot stamped body of the present invention is excellent in strength, ductility, bendability, impact resistance, and hydrogen embrittlement resistance and is small in scattering in hardness, so can be suitably used for structural members or reinforcing members for automobiles or structures requiring strength.

Claims
  • 1-8. (canceled)
  • 9. A hot stamped body comprising a middle part in sheet thickness and a softened layer arranged at both sides or one side of the middle part in sheet thickness, 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, and has a hardness of 500 Hv or more and 800 Hv or less,in the metal structures from a depth of 20 μm below the surface of the softened layer to a depth of ½ of the thickness of the softened layer, when defining a region surrounded by grain boundaries having a 15° or higher orientation difference in a cross-section parallel to the sheet thickness direction as a “crystal grain”, the area rate of the total of crystal grains with a maximum crystal orientation difference inside the crystal grains of 1° or less and crystal grains with a maximum crystal orientation difference inside the crystal grains of 8° or more and less than 15° is 50% or more and less than 85%,the tensile strength is 1500 MPa or more.
  • 10. The hot stamped body according to claim 9, wherein the Si content is 0.50% or less and the Mn content is 0.20% or more and less than 1.50%.
  • 11. The hot stamped body according to claim 9, wherein the Si content is 0.50% or less and the Mn content is 1.50% or more and less than 3.00%.
  • 12. The hot stamped body according to claim 9, wherein the Si content is more than 0.50% and less than 3.00%, the Mn content 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.
  • 13. The hot stamped body according to claim 9, wherein the Si content is more than 0.50% and less than 3.00%, the Mn content 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.
  • 14. The hot stamped body according to claim 9, where the middle part in sheet thickness further comprises, by mass %, one or more of Ni: 0.01% or more and 3.00% or less, 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 10, where the middle part in sheet thickness further comprises, by mass %, one or more of Ni: 0.01% or more and 3.00% or less, 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 11, where the middle part in sheet thickness further comprises, by mass %, one or more of Ni: 0.01% or more and 3.00% or less, 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 12, where the middle part in sheet thickness further comprises, by mass %, one or more of Ni: 0.01% or more and 3.00% or less, 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.
  • 18. The hot stamped body according to claim 13, where the middle part in sheet thickness further comprises, by mass %, one or more of Ni: 0.01% or more and 3.00% or less, 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.
  • 19. The hot stamped body according to claim 9, where a plated layer is formed on the softened layer.
  • 20. The hot stamped body according to claim 10, where a plated layer is formed on the softened layer.
  • 21. The hot stamped body according to claim 11, where a plated layer is formed on the softened layer.
  • 22. The hot stamped body according to claim 12, where a plated layer is formed on the softened layer.
  • 23. The hot stamped body according to claim 13, where a plated layer is formed on the softened layer.
  • 24. The hot stamped body according to claim 14, where a plated layer is formed on the softened layer.
  • 25. The hot stamped body according to claim 15, where a plated layer is formed on the softened layer.
  • 26. The hot stamped body according to claim 16, where a plated layer is formed on the softened layer.
  • 27. The hot stamped body according to claim 17, where a plated layer is formed on the softened layer.
  • 28. The hot stamped body according to claim 18, where a plated layer is formed on the softened layer.
Priority Claims (1)
Number Date Country Kind
2017-029318 Feb 2017 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2018/006086 2/20/2018 WO 00