HOT-STAMPING FORMED BODY

Abstract
This hot-stamping formed body has a predetermined chemical composition, in a surface layer region, an area ratio of bainite of more than 10%, a maximum value of pole density of a texture of 4.0 or less, and a deboronization index of 0.05 or more.
Description
TECHNICAL FIELD OF THE INVENTION

The present invention relates to a hot-stamping formed body.


Priority is claimed on Japanese Patent Application No. 2022-067023, filed Apr. 14, 2022, the content of which is incorporated herein by reference.


BACKGROUND ART

In recent years, there has been a demand for a reduction in a weight of a vehicle body for a vehicle in terms of environmental protection and resource saving, and a high-strength steel sheet has been applied to vehicle members. Vehicle members are manufactured by press forming, but not only a forming load is increased but also the formability deteriorates as the strength of a steel sheet is increased. For this reason, the formability of a high-strength steel sheet into a member having a complicated shape becomes an issue.


In order to solve this issue, the application of a hot stamping technique in which press forming is performed after a steel sheet is heated up to a high temperature of an austenite range where the steel sheet softens is in progress. Hot stamping is attracting attention as a technique that achieves both the formability of a steel sheet into a vehicle member and strength of a vehicle member by performing hardening of the steel sheet in a die at the same time as press working.


For example, Patent Document 1 discloses an electrolytic zinc-based plated steel sheet having a high yield ratio and excellent bendability, in which the critical hydrogen amount in the steel is 0.20 mass ppm or less.


PRIOR ART DOCUMENT
Patent Document



  • [Patent Document 1] PCT International Publication No. WO2020/079925



DISCLOSURE OF THE INVENTION
Problems to be Solved by the Invention

In order to make vehicle members lighter, it is effective to make the microstructure of steel sheets a microstructure in which martensite with a high dislocation density is a main phase. However, in a microstructure whose main phase is martensite with a high dislocation density, since a trap amount of hydrogen irrupting from the outside increases, hydrogen embrittlement cracking more likely to be occurred in vehicle members.


Hydrogen embrittlement cracking is a phenomenon in which a steel member, to which high stress is applied in use, suddenly fractures due to hydrogen which is irrupted into the steel from an external environment. This phenomenon is also called delayed fracture due to the mode of the occurrence of fracture. It is generally known that hydrogen embrittlement cracking is more likely to occur in the steel sheet as tensile strength of the steel sheet increases. It is considered that this is because the higher tensile strength of the steel sheet, the greater residual stress in the steel sheet after a component is formed. This susceptibility to hydrogen embrittlement cracking (delayed fracture) is called hydrogen embrittlement resistance.


In Patent Document 1, bendability is considered, but hydrogen embrittlement resistance are not considered.


The present invention has been made in view of the above-mentioned problem.


An object of the present invention is to provide a hot-stamping formed body having high strength and excellent hydrogen embrittlement resistance.


Means for Solving the Problem

The gist of the present invention is as follows.


[1]A hot-stamping formed body according to an aspect of the present invention comprising, as a chemical composition, by mass %:

    • C: more than 0.40% and 0.70% or less;
    • Si: 0.010% to 3.000%;
    • Mn: 0.10% or more and less than 0.60%;
    • P: 0.100% or less;
    • S: 0.0100% or less:
    • N: 0.0200% or less;
    • 0: 0.0200% or less;
    • Al: 0.0010% to 0.5000%;
    • Nb: 0.0010% to 0.1000%;
    • Ti: 0.010% to 0.200%;
    • Cr: 0.010% to 0.800%;
    • Mo: 0.0010% to 1.0000%;
    • B: 0.0005% to 0.0200%;
    • Co: 0% to 4.00%;
    • Ni: 0% to 3.00%;
    • Cu: 0% to 3.00%;
    • V: 0% to 3.00%;
    • W: 0% to 3.00%;
    • Ca: 0% to 1.0000%;
    • Mg: 0% to 1.0000%;
    • REM: 0% to 1.0000%;
    • Sb: 0% to 1.000%:
    • Sn: 0% to 1.000%;
    • Zr: 0% to 1.000%;
    • As: 0% to 0.100%; and


a remainder: Fe and impurities,


in a surface layer region, which is a region from a surface of the hot-stamping formed body to 1/25 depth of a sheet thickness from the surface,


an area ratio of bainite is more than 10%,


a maximum value of pole density of a texture is 4.0 or less, and


a deboronization index is 0.05 or more.


[2] The hot-stamping formed body according to [1] may comprise, as the chemical composition, by mass %, one or more selected from the group consisting of:

    • Co: 0.01% to 4.00%;
    • Ni: 0.01% to 3.00%;
    • Cu: 0.01% to 3.00%;
    • V: 0.01% to 3.00%;
    • W: 0.01% to 3.00%;
      • Ca: 0.0001% to 1.0000%;
      • Mg: 0.0001% to 1.0000%;
      • REM: 0.0001% to 1.0000%;
      • Sb: 0.001% to 1.000%;
      • Sn: 0.001% to 1.000%;
      • Zr: 0.001% to 1.000%; and
      • As: 0.001% to 0.100%.


Effects of the Invention

According to the above-described aspects of the present invention, it is possible to provide a hot-stamping formed body having high strength and excellent hydrogen embrittlement resistance.





BRIEF DESCRIPTION OF THE DRAWINGS

[FIG. 1]A figure explaining the method to obtain a deboronization index.





EMBODIMENTS OF THE INVENTION

The present inventors found that in a surface layer region, by generating a desired amount of bainite, creating a texture with a desired crystal orientation, and achieving a desired deboronization index, hydrogen embrittlement resistance of the hot-stamping formed body can be improved.


The present inventors found that in order to obtain a hot-stamping formed body having the above features, it is particularly effective to perform annealing under a desired condition during manufacturing a steel sheet for hot stamping.


Hereinafter, the hot-stamping formed body according to the present embodiment will be described in detail. First, the reason the chemical composition of the hot-stamping formed body according to the present embodiment is limited will be described.


A limited numerical range described using “to” described below includes a lower limit and an upper limit. Numerical values represented using “less than” or “more than” are not included in a numerical range. All percentages (%) related to the chemical composition mean mass %.


The hot-stamped formed body according to the present embodiment comprises, as a chemical composition, by mass %, C: more than 0.40% and 0.70% or less, Si: 0.010% to 3.000%, Mn: 0.10% or more and less than 0.60%, P: 0.100% or less, S: 0.0100% or less, N: 0.0200% or less, 0: 0.0200% or less, Al: 0.0010% to 0.5000%, Nb: 0.0010% to 0.1000% c, Ti: 0.010% to 0.200%, Cr: 0.010% to 0.800%, Mo: 0.0010% to 1.0000%, B: 0.0005% to 0.0200%, and a remainder: Fe and impurities. Each element will be described below.


C: more than 0.40% and 0.70% or less


C is an element that improves the strength of the hot-stamping formed body. When the C content is 0.40% or less, a desired strength of the hot-stamping formed body cannot be obtained. For this reason, the C content is set to more than 0.40%. The C content is preferably 0.42% or more or 0.44% or more.


Meanwhile, when the C content is more than 0.70%, since an amount of hydrogen trapped in martensite increases, a desired hydrogen embrittlement resistance cannot be obtained. For this reason, the C content is set to 0.70% or less. The C content is preferably 0.65% or less or 0.60% or less.


Si: 0.010% to 3.000%


Si is an element that improves strength of the hot-stamping formed body by solid-solution strengthening. When the Si content is less than 0.010%, a desired strength cannot be obtained. For this reason, the Si content is set to 0.010% or more. The Si content is preferably 0.050% or more, 0.100% or more or 0.150% or more.


Meanwhile, when the Si content is more than 3.000%, the amount of ferrite increases and a desired microstructure cannot be obtained. For this reason, the Si content is set to 3.000% or less. The Si content is preferably 2.000% or less, 1.000% or less or 0.600% or less.


Mn: 0.10% or more and less than 0.60%


Mn is an element that increases strength of the hot-stamping formed body by increasing the hardenability of steel. In order to obtain a desired strength, the Mn content is set to 0.10% or more. The Mn content is preferably 0.20% or more or 0.25% or more.


Meanwhile, when the Mn content is 0.60% or more, a desired texture cannot be obtained. For this reason, the Mn content is set to less than 0.60%. The Mn content is preferably 0.55% or less, 0.50% or less or 0.45% or less.


P: 0.100% or less


P is an impurity element, and decreases strength of the grain boundaries by segregating in the grain boundaries. This deteriorates hydrogen embrittlement resistance of the hot-stamping formed body. When the P content is more than 0.100%, the above effects become significant. For this reason, the P content is set to 0.100% or less. The P content is preferably 0.050% or less or 0.010% or less.


The lower limit of the P content is not particularly limited, but may be 0%. However, when the P content is reduced to less than 0.0001%, the dephosphorization cost increases significantly, which is not preferable economically. For this reason, the P content may be set to 0.0001% or more, 0.001% or more or 0.005% or more.


S: 0.0100% or less


S is an impurity element, and forms inclusions in steel. The inclusions trap a large amount of hydrogen and form a region with locally high hydrogen concentration, and thereby deteriorate hydrogen embrittlement resistance of the hot-stamping formed body. When the S content is more than 0.100%, the above effects become significant. For this reason, the S content is set to 0.0100% or less. The S content is preferably 0.0080% or less, 0.0050% or less or 0.0030% or less.


The lower limit of the S content is not particularly limited, but may be 0%. However, when the S content is reduced to less than 0.0001%, the desulfurization cost increases significantly, which is not preferable economically. For this reason, the S content may be set to 0.0001% or more, 0.0002% or more, 0.0003% or more or 0.0010% or more.


N: 0.0200% or less


N is an impurity element, and forms nitrides in steel. The nitrides trap a large amount of hydrogen and form a region with locally high hydrogen concentration, and thereby deteriorate hydrogen embrittlement resistance of the hot-stamping formed body. When the N content is more than 0.0200%, the above effects become significant. For this reason, the N content is set to 0.0200% or less. The N content is preferably 0.0150% or less, 0.0100% or less, 0.0060% or less or 0.0040% or less.


The lower limit of the N content is not particularly limited, but may be 0%. However, when the N content is reduced to less than 0.0001%, the denitrification cost increases significantly, which is not preferable economically. For this reason, the N content may be set to 0.0001% or more or 0.0010% or more.


O: 0.0200% or less


O forms coarse oxides when a large amount of O is comprised in steel. The oxides trap a large amount of hydrogen and form a region with locally high hydrogen concentration, and thereby deteriorate hydrogen embrittlement resistance of the hot-stamping formed body. When the O content is more than 0.0200%, the above effects become significant. For this reason, the O content is set to 0.0200% or less. The O content is preferably 0.0100% or less, 0.0070% or less or 0.0040% or less.


The O content may be 0%, in order to disperse many oxides during deoxidizing of molten steel, the O content may be set to 0.0005% or more or 0.0010% or more.


Al: 0.0010% to 0.5000%


Al is an element having an effect of deoxidizing molten steel and achieving soundness of the steel. When the Al content is less than 0.0010%, deoxidation is not sufficiently performed, and coarse oxides are generated. The oxides trap a large amount of hydrogen and form a region with locally high hydrogen concentration, and thereby deteriorate hydrogen embrittlement resistance of the hot-stamping formed body. For these reasons, the Al content is set to 0.0010% or more. The Al content is preferably 0.0050% or more, 0.0100% or more or 0.0300% or more.


Meanwhile, when the Al content is more than 0.5000%, coarse oxides are generated in steel. The oxides trap a large amount of hydrogen and form a region with locally high hydrogen concentration, and thereby deteriorate hydrogen embrittlement resistance of the hot-stamping formed body. For this reason, the Al content is set to 0.5000% or less. The Al content is preferably 0.4000% or less, 0.3000% or less, or 0.2000% or less or 0.1000% or less.


Nb: 0.0010% to 0.1000%


Nb is an element that forms carbonitride in steel and improves strength of the hot-stamping formed body by precipitation strengthening. When the Nb content is less than 0.0010%, a desired strength cannot be obtained. For this reason, the Nb content is set to 0.0010% or more. The Nb content is preferably 0.0050% or more, 0.0090% v or more or 0.0150% or more.


Meanwhile, when the Nb content is more than 0.1000%, many carbonitrides are generated in steel, and hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the Nb content is set to 0.1000% or less. The Nb content is preferably 0.0800% or less or 0.0600% or less.


Ti: 0.010% to 0.200%


Ti is an element that forms carbonitride in steel and improves strength of the hot-stamping formed body by precipitation strengthening. When the Ti content is less than 0.010%, a desired strength cannot be obtained. For this reason, the Ti content is set to 0.010% or more. The Ti content is preferably 0.020% or more or 0.025% or more.


Meanwhile, when the Ti content is more than 0.200%, many coarse carbonitrides are generated in steel, the carbonitrides become sites with local increase of hydrogen concentration, and thereby hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the Ti content is set to 0.200% or less. The Ti content is preferably 0.150% or less, 0.090% or less, 0.080% or less, 0.070% or less, 0.060% or less or 0.050% or less.


Cr: 0.010% to 0.800%


Cr is an element that increases strength of the hot-stamping formed body by dissolving in prior austenite grains during heating before hot stamping. When the Cr content is less than 0.010%, a desired strength cannot be obtained. For this reason, the Cr content is set to 0.010% or more. The Cr content is preferably 0.100% or more, 0.150% or more or 0.200% or more.


Meanwhile, when the Cr content is more than 0.800%, a desired texture cannot be obtained in the hot-stamping formed body and hydrogen embrittlement resistance deteriorates. For this reason, the Cr content is set to 0.800% or less. The Cr content is preferably 0.700% or less, 0.500% or less or 0.400% or less.


Mo: 0.0010% to 1.0000%


Mo is an element that increases strength of the hot-stamping formed body by dissolving in prior austenite grains during heating before hot stamping. When the Mo content is less than 0.0010%, a desired strength cannot be obtained. For this reason, the Mo content is set to 0.0010% or more. The Mo content is preferably 0.0100% or more, 0.0500% or more or 0.1000% or more.


Meanwhile, when the Mo content is more than 1.0000%, a desired texture cannot be obtained in the hot-stamping formed body and hydrogen embrittlement resistance deteriorates. For this reason, the Mo content is set to 1.0000% or less. The Mo content is preferably 0.8000% or less, 0.6000% or less or 0.4000% or less.


B: 0.0005% to 0.0200%


B is an element that improves the hardenability of steel. When the B content is less than 0.0005%, a desired strength cannot be obtained. For this reason, the B content is set to 0.0005% or more. The B content is preferably 0.0010% or more or 0.0015% or more.


Meanwhile, when the B content is more than 0.0200%, coarse intermetallic compounds are generated in the hot-stamping formed body, the intermetallic compounds become sites with local increase of hydrogen concentration, and thereby hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the B content is set to 0.0200% or less. The B content is preferably 0.0150% or less, 0.0100% or less, 0.0080% or less, 0.0040% or less or 0.0030% or less.


The remainder of the chemical composition of the hot-stamping formed body may be Fe and impurities. Elements which are unavoidably mixed from a steel raw material or scrap and/or during the manufacture of steel and are allowed in a range where the properties of the hot-stamping formed body according to the present embodiment do not deteriorate are exemplary examples of the impurities.


The hot-stamping formed body may comprise the following elements as optional elements. The content of the following optional elements obtained in a case where the following optional elements are not contained is 0%.


Co: 0% to 4.00%


Co is an element that improves strength of the hot-stamping formed body by solid-solution strengthening. In order to reliably obtain the effect, it is preferable that the Co content be set to 0.01% or more. The Co content is more preferably set to 0.05% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Co content is set to 4.00% or less. If necessary, the upper limit of Co content may be set to 1.00%, 0.50%, 0.10%, 0.05% or 0.02%.


Ni: 0% to 3.00%


Ni has an effect of increasing strength of the hot-stamping formed body by dissolving in prior austenite grains during heating before hot stamping. In order to reliably obtain the effect, the Ni content is preferably set to 0.01% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Ni content is preferably set to 3.00% or less. If necessary, the upper limit of Ni content may be set to 1.50%, 1.00%, 0.50%, 0.10%, 0.05% or 0.02%.


Cu: 0% to 3.00%


Cu has an effect of increasing strength of the hot-stamping formed body by dissolving in prior austenite grains during heating before hot stamping. In order to reliably obtain the effect, the Cu content is preferably set to 0.01% or more. The Cu content is more preferably set to 0.05% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Cu content is preferably set to 3.00% or less. If necessary, the upper limit of Cu content may be set to 1.50%, 1.00%, 0.50%, 0.10%, 0.05% or 0.02%.


V: 0% to 3.00%


V has an effect of forming carbonitride in steel and improves strength of the hot-stamping formed body by precipitation strengthening. In order to reliably obtain the effect, the V content is preferably set to 0.01% or more. The V content is more preferably set to 0.05% or more.


Meanwhile, when the V content is more than 3.00%, many coarse carbonitrides are generated in steel. The carbonitrides become sites with local increase in hydrogen concentration, and thereby hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the V content is set to 3.00% or less. If necessary, the upper limit of V content may be set to 1.50%, 1.00%, 0.50%, 0.10%, 0.05% or 0.02%.


W: 0% to 3.00%


W has an effect of improving strength of the hot-stamping formed body. In order to reliably obtain the effects, the W content is preferably set to 0.01% or more. The W content is preferably set to 0.05% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the W content is preferably set to 3.00% or less. If necessary, the upper limit of W content may be set to 1.50%, 1.00%, 0.50%, 0.10%, 0.05% or 0.02%.


Ca: 0% to 1.0000%


Ca is an element that suppresses generation of carbides that become starting points for fracture, and contributes to improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the Ca content is preferably set to 0.0001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Ca content is set to 1.0000% or less. If necessary, the upper limit of Ca content may be set to 0.1000%, 0.0100%, 0.0050%, 0.0010%, 0.0005% or 0.0002%.


Mg: 0% to 1.000%


Mg forms oxides and sulfides in molten steel, suppresses formation of a coarse MnS, disperses a lot of fine oxides, miniaturizes the microstructure. This contributes to improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain these effects, the Mg content is preferably set to 0.0001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Mg content is set to 1.0000% or less. If necessary, the upper limit of Mg content may be set to 0.1000%, 0.0100%, 0.0050%, 0.0010%, 0.0005% or 0.0002%.


REM: 0% to 1.000%


REM suppresses generation of coarse oxides that become sites with local increase of hydrogen concentration. This contributes improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the REM content is preferably set to 0.0001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the REM content is set to 1.0000% or less. If necessary, the upper limit of REM content may be set to 0.1000%, 0.0100%, 0.0050%, 0.0010%, 0.0005% or 0.0002%.


In the present embodiment, REM refers to a total of 17 elements that are composed of Sc, Y and lanthanoid, and the REM content refers to the total content of these elements.


Sb: 0% to 1.000%


Sb suppresses generation of coarse oxides that become sites with local increase of hydrogen concentration. This contributes improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the Sb content is preferably set to 0.001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Sb content is set to 1.000% or less. If necessary, the upper limit of Sb content may be set to 0.100%, 0.050%, 0.020%, 0.010%, 0.005% or 0.002%.


Sn: 0% to 1.000%


Sn suppresses generation of coarse oxides that become sites with local increase of hydrogen concentration. This contributes improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the Sn content is preferably set to 0.001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Sn content is set to 1.000% or less. If necessary, the upper limit of Sn content may be set to 0.100%, 0.050%, 0.020%, 0.010%, 0.005% or 0.002%.


Zr: 0% to 1.000%


Zr suppresses generation of coarse oxides that become sites with local increase of hydrogen concentration. This contributes improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the Zr content is preferably set to 0.001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the Zr content is set to 1.000% or less. If necessary, the upper limit of Zr content may be set to 0.100%, 0.050%, 0.020%, 0.010%, 0.005% or 0.002%.


As: 0% to 0.100%


As refines the prior austenite grains by lowering an austenite single-phase transformation temperature. This contributes improvement of hydrogen embrittlement resistance of the hot-stamping formed body. In order to reliably obtain the effect, the As content is preferably set to 0.001% or more.


Meanwhile, since the above effect will be saturated even if a large amount is comprised, the As content is set to 0.100% or less. If necessary, the upper limit of As content may be set to 0.100%, 0.050%, 0.020%, 0.010%, 0.005% or 0.002%.


The above-mentioned chemical composition of the hot-stamping formed body may be measured by a standard analysis method. For example, the chemical composition may be measured using inductively coupled plasma-atomic emission spectrometry (ICP-AES). C and S may be measured using a combustion-infrared absorption method, N may be measured using an inert gas fusion-thermal conductivity method, and O may be measured using an inert gas fusion-nondispersive infrared absorption method.


When a plating layer or a coating film is provided on the surface of the hot-stamping formed body, the chemical composition is analyzed after the plating layer or the coating film is removed by mechanical grinding.


Next, the microstructure of the hot-stamping formed body according to the present embodiment will be described.


In the hot-stamping formed body according to the present embodiment, in a surface layer region, which is a region from a surface of the hot-stamping formed body to 1/25 depth of a sheet thickness (thickness of the hot-stamping formed body) from the surface, the area ratio of bainite is more than 10%, the maximum value of pole density of the texture is 4.0 or less, and the deboronization index is 0.05 or more.


The surface layer region in the present embodiment refers to a region between the surface of the hot-stamping formed body and 1/25 depth of the sheet thickness (thickness of the hot-stamping formed body) from the surface.


When the hot-stamping formed body has the plating layer or the coating film on the surface thereof, the “surface” refers to the interface of the plating layer or the coating film and the base steel sheet, and for convenience, the plating layer or the coating film is excluded from the hot-stamping formed body. Specifically, when the hot-stamping formed body has the plating layer or the coating film on the surface thereof, as described below, for convenience, a region where the Fe concentration is less than 90% by mass in GD-OES measurement, that is, the plating layer or the coating film is excluded from the hot-stamping formed body, the measuring point where the Fe concentration is 90% by mass (the interface of the base steel sheet and the plating layer) is regarded as the surface of the hot-stamping formed body. As described above, the plating layer or the coating film is excluded from the hot-stamping formed body, when the thickness of the plating layer or the coating film is very small compared to the sheet thickness (thickness) of the hot-stamping formed body and can be ignored (however, when only the plating layer is formed, the thickness of the plating layer is often very small and can be ignored in most cases), when measuring the sheet thickness (thickness) of the hot-stamping formed body, the sheet thickness (thickness) of the hot-stamping formed body may be regarded as the sheet thickness (thickness) including the plating layer or the coating film.


“Surface Layer Region”

Area ratio of bainite: more than 10%


By generating bainite in the surface layer region, dislocation density of the surface layer region can be decreased. As a result, irruption of hydrogen from the external environment can be suppressed, and hydrogen embrittlement resistance of the hot-stamping formed body can be improved. Furthermore, by generating bainite in the surface layer region, since excessive softening of the surface layer can be suppressed, hydrogen embrittlement resistance can be further improved while maintaining a load bearing of the member. When the area ratio of bainite in the surface layer region is 10% or less, hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the area ratio of bainite is set to more than 10%, preferably 20% or more, 40% or more or 60% or more.


The upper limit of the area ratio of bainite is not particularly limited, but may be set to 100%, 90% or 80%.


In the microstructure of the surface layer region, except for bainite, martensite of 0% to 90% (0% or more and 90% or less), ferrite and residual austenite of 0% to 65% (0% or more and 65% or less) may be included. Martensite in the present embodiment includes untempered martensite (fresh martensite) and tempered martensite.


The area ratio of the microstructure is calculated for the surface layer region (the region from the surface to 1/25 depth of the sheet thickness from the surface) by the following method.


A sample is cut out from an arbitrary position away from an end surface of the hot-stamping formed body by a distance of 50 mm or more (a position that avoids an end portion in a case where a sample cannot be collected at this position) so that a sheet thickness cross section parallel to the rolling direction can be observed. The size of the sample depends on a measurement device, but is set to a size that can be observed by about 10 mm in the rolling direction.


After polishing the cross section of the sample using silicon carbide paper of #600 to #1500, the cross section is mirror-finished using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in a diluted solution of alcohol or the like or pure water. Next, the observation surface is finished by electrolytic polishing. At an arbitrary position on the cross section of the sample in a longitudinal direction, a region which has a length of 50 μm and is present between the surface of the hot-stamping formed body and 1/25 depth of the sheet thickness from the surface is measured at a measurement interval of 0.1 μm by an electron backscatter diffraction method, and thus, crystal orientation information is obtained. An EBSD analyzer composed of a Schottky emission scanning electron microscope and an EBSD detector may be used for measurement, for example, an EBSD analyzer composed of JSM-7001F manufactured by JEOL Ltd. and DVC 5-type detector manufactured by TSL Solutions may be used for measurement. In this case, the degree of vacuum in the EBSD analyzer may be set to 9.6×105 Pa or less, an accelerating voltage may be set to 15 kV, and an irradiation current level may be set to 13.


In the obtained crystal structure information, using the “Phase Map” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer, a region where a crystal structure is fcc is determined as residual austenite. The ratio of the residual austenite is calculated, thereby the area ratio of the residual austenite is obtained. Next, in the regions where the crystal structure is bcc, under the condition that boundary with 5° is regarded as the grain boundary, using the “Grain Average Misorientation” function installed in the software “OTIM Analysis (registered trademark)” attached to the EBSD analyzer, regions where a grain average misorientation is more than 0.50° and 0.75° or lower are extracted as bainite. By calculating the area ratio of the extracted bainite, the area ratio of bainite is obtained.


Subsequently, the region where “Grain Average Misorientation” is 0.5° or lower is extracted as ferrite. By calculating the area ratio of the extracted ferrite, the area ratio of ferrite is obtained. The remaining region (the region where “Grain Average Misorientation” is more than 0.75°) is extracted as martensite, and the area ratio thereof is calculated, thereby the area ratio of martensite is obtained.


In addition, in the present embodiment, the rolling direction of the hot-stamping formed body is determined by the following method.


First, a sample is cut out from an arbitrary position away from an end surface of the hot-stamping formed body by a distance of 50 mm or more so that a sheet thickness cross section parallel to a rolling direction can be observed. After finishing the cross section of the collected sample by mirror polishing, observations with an optical microscope at 100, 200, 500, and 1000 magnifications are performed respectively. Depending on the size of the inclusion, an observation result with an appropriate magnification that the size of the inclusion can be measured is selected. The observation area is width of 500 μm or more and full of the sheet thickness, and the areas with low brightness are determined to be inclusions. The observation may be performed at multiple fields when observing. Next, using the sheet thickness cross section initially observed by the above method as a reference, in the range of 0° to 180° with the sheet thickness direction as the axis, the cross-sectional observation of the plane parallel to the plane rotated in 5° increments is performed in the same way as the above method. The average values of the lengths of the long axes of the plurality of inclusions in each cross section are calculated respectively. The cross section in which the obtained average value of the length of the long axes of the inclusions is maximum is specified. A direction parallel to the longitudinal direction of the inclusion in the cross section is determined as the rolling direction.


“Surface Layer Region”

Crystal orientation in surface layer region: Maximum value of pole density of texture is 4.0 or less


By controlling the texture in the surface layer region, irruption of hydrogen from the external environment can be suppressed, and hydrogen embrittlement resistance of the hot-stamping formed body can be improved. When the maximum value of pole density of the texture in the surface layer region is more than 4.0, hydrogen embrittlement resistance of the hot-stamping formed body deteriorates. For this reason, the maximum value of pole density of the texture in the surface layer region is set to 4.0 or less, preferably 3.5 or less, 3.0 or less or 2.5 or less.


The lower limit of the pole density of the texture in the surface layer region is not particularly limited, but may be set to 1.0 or 1.2.


In the surface layer region (the region between the surface and 1/25 depth of the sheet thickness from the surface), the texture in the surface layer region is obtained by the following method.


A sample is cut out from an arbitrary position away from an end surface of the hot-stamping formed body by a distance of 50 mm or more (a position that avoids an end portion in a case where the sample cannot be collected at this position) so that a sheet thickness cross section parallel to a rolling direction can be observed. The size of the sample depends on a measurement device, but is set to a size that can be observed by about 10 mm in the rolling direction.


After polishing the cross section of the sample using silicon carbide paper of #600 to #1500, the cross section of the sample is mirror-finished using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in a diluted solution of alcohol or the like or pure water. Next, the observation surface is finished by electrolytic polishing. At an arbitrary position on the cross section of the sample in a longitudinal direction, a region which has a length of 1000 μm and is present between the surface and 1/25 depth of the sheet thickness from the surface is measured at a measurement interval of 5.0 μm by an electron backscatter diffraction method, and thus, crystal orientation information is obtained. An EBSD analyzer composed of a Schottky emission scanning electron microscope and an EBSD detector may be used for measurement, for example, an EBSD analyzer composed of JSM-7001F manufactured by JEOL Ltd. and DVC 5-type detector manufactured by TSL Solutions may be used for measurement. In this case, the degree of vacuum in the EBSD analyzer may be set to 9.6×105 Pa or less, an accelerating voltage may be set to 15 kV, and an irradiation current level may be set to 13.


By using the obtained crystal orientation information, using the “Texture” function installed in the software “OIM Analysis (registered trademark)” which is attached to the EBSD analyzer, intensity calculation is performed using a Harmonic Series Expansion for grains whose crystal structure is bcc. At this time, the expansion order is set to 16, and a half width when applied to a Gaussian distribution is set to 5°. Next, the “Texture Plot” function is used for the output file after the intensity calculation to output a φ2=45° cross section in the orientation distribution function (ODF). The maximum value of the pole density in the φ2=45° cross section is regarded as the maximum value of pole density of the texture in the surface layer region.


“Surface Layer Region”

Deboronization index: 0.05 or more


The deboronization index is an index that quantitatively represents the amount of decrease of the B concentration in the surface layer region. By decreasing the B concentration in the surface layer region, deformability of prior austenite grain is improved by reducing strength of prior austenite before transformation, and the generation of grains having random orientation is facilitated in the surface layer region. When the deboronization index in the surface layer region is less than 0.05, grains having a desired texture cannot be obtained in the surface layer region. For this reason, the deboronization index is set to 0.05 or more, preferably 0.20 or more, 0.30 or more or 0.35 or more.


The upper limit of the deboronization index is not particularly limited, but may be set to 1.00, 0.80 or 0.60.


The deboronization index in the surface layer region is obtained by the following method.


An element concentration distribution in the sheet thickness direction in the hot-stamping formed body is measured using glow discharge optical emission spectrometry (GD-OES: Manufactured by Horiba, Ltd., Marcus type high-frequency glow discharge optical emission spectrometer, GD-PROFILER-HR). The measurement conditions are an analysis diameter of 4 mmφ, a sputtering rate of 4 μm/min, an argon pressure of 600 Pa, an RF output of 35 W, and a measurement interval of 0.02 μm or less. All elements that are comprised in the hot-stamping formed body are measured.


In a case where the hot-stamping formed body has the plating layer on the surface, the “surface” refers to the interface of the plating layer and the base steel sheet. In a case where the hot-stamping formed body has the plating layer or the coating film on the surface, GD-OES measurement is performed after removing a part or all of the plating layer or the coating film by mechanical polishing or chemical polishing such that measurement to 200 μm depth from the surface of the base steel sheet (the interface of the plating layer and the base steel sheet) can be performed. In the GD-OES measurement, a measuring point where the Fe concentration becomes 90 mass % is regarded as the surface of the hot-stamping formed body. In addition, in the following description, for ease of explanation, the hot-stamping formed body may be referred to as a base steel sheet.


Next, B concentrations from the surface of the hot-stamping formed body to at least 100 μm depth from the surface are measured. After measuring the B concentration at a position of 100 μm depth from the surface, in a case where the absolute value of the difference between the average value of the B concentration in a region from 80 μm to 100 μm and the maximum value of the measured value of the B concentration in the region from 80 μm to 100 μm is 0.0006% by mass or less, and, in a case where the absolute value of the difference between the average value of the B concentration in the region from 80 μm to 100 μm and the minimum value of the measured value of the B concentration in the region from 80 μm to 100 μm is 0.0006% by mass or less, the measurement in the depth direction of the B concentration is finished at the position of 100 μm depth from the surface.


In a case where the requirements for ending the measurement are not satisfied, the measurement of the B concentration in the depth direction is continued. Then, each time a new B concentration measurement value is obtained in the depth direction, the average value of the B concentration in the region between the deepest part and 20 μm from the deepest part to the surface side is calculated. In a case where the absolute value of the difference between the average value of the B concentration in the region between the deepest part and 20 μm from the deepest part to the surface side and the maximum value of the measured value of the B concentration in the region between the deepest part and 20 μm from the deepest part to the surface side is 0.0006 mass % or less, and, in a case where the absolute value of the difference between the average value of the B concentration in the region between the deepest part and 20 μm from the deepest part to the surface side and the minimum value of the measured value of the B concentration in the region between the deepest part and 20 μm from the deepest part to the surface side is 0.0006 mass % or less, the measurement of the B concentration in the depth direction is finished at the position. For example, when the measured value of the B concentration at 150 μm depth from the surface is obtained, in a case where the absolute value of the difference between the average value of the B concentration in the region between 130 μm depth from the surface and 150 μm depth from the surface and the maximum value of the measured value of the B concentration in the region between 130 μm depth from the surface and 150 μm depth from the surface is 0.0006 mass % or less, and, in a case where the absolute value of the difference between the average value of the B concentration in the region between 130 μm depth from the surface and 150 μm depth from the surface and the minimum value of the measured value of the B concentration in the region between 130 μm depth from the surface and 150 μm depth from the surface is 0.0006 mass % or less, the measurement of the B concentration in the depth direction is finished at the position of 150 μm depth from the surface.


Even if the requirements for ending the measurement described above are not satisfied and the measurement of the B concentration in the depth direction cannot be finished, the measurement of the B concentration in the depth direction is finished when the measurement of the B concentration at the position of 200 μm depth from the surface is completed. Then, at the time when the measurement of the B concentration in the depth direction is finished, the average value of the B concentration in the region between the deepest part (the deepest position where the B concentration used for calculating the deboronization index was obtained) and the position of 20 μm from the deepest part to the surface side is used for the below calculation of the deboronization index (hereinafter, the average value of the B concentration in the region will be referred to as the average B concentration at the deepest part of 20 μm).


For convenience of measurement, for example, after measuring the B concentration to 200 μm depth from the surface, in a region between 100 μm and 200 μm from the surface, the shallowest depth position that satisfies the ending condition for the B concentration measurement in the depth direction is searched for, and in a case where the depth position is found, the deboronization index may be calculated without using the measurement results of the B concentration at the position deeper than the shallowest depth position. For example, the B concentration may be measured from the surface to 200 μm depth from the surface, in this case, in a case where a shallowest depth position that satisfies the ending condition for B concentration measurement in the depth direction exists in a region of 100 μm or more depth from the surface, the measurement is regarded as ending at the depth position, and the deboronization index is calculated.


In the region between the deepest part and 20 μm from the deepest part to the surface side of the hot-stamping formed body, the amount of decrease in the B concentration per unit depth (the value obtained by subtracting the B concentration at each measurement point from the average B concentration at the deepest part of 20 μm) is calculated, the integrated value of the product of the unit depth and the amount of decrease in the B concentration is calculated and determined as the area of the B-depletion region (area of region A in FIG. 1). However, when the value obtained by subtracting the B concentration at each measurement point from the average B concentration at the deepest part of 20 μm is negative, it is integrated as 0 (due to the B removal phenomenon near the surface, the B concentration at each measurement point is in most cases lower than the average B concentration at the deepest part of 20 μm, and the integrated value becomes positive). Next, the product of the average B concentration at the deepest part of 20 μm and the length of 200 μm is calculated as a reference area (area of rectangular region B in FIG. 1). The value obtained by dividing a B-depletion area (area of region A) by the reference area (area of region B) is defined as the deboronization index (area of region A/area of region B). Even in a case where the above-mentioned requirement for ending the measurement is satisfied in a region from the surface to 200 μm, the reference area (area of region B) is calculated by assuming that the length by which the average B concentration at the deepest part of 20 μm is multiplied is 200 μm.


The microstructure of a region other than the surface layer region (for example, the region between 4/16 depth of the sheet thickness from the surface of the hot-stamping formed body and 5/16 depth of the sheet thickness from the surface) is not particularly limited as long as a desired strength and hydrogen embrittlement resistance can be obtained, for example, in area %, the microstructure may consist of martensite and bainite of 90% to 100% (90% or more and 100% or less) in total, and ferrite and residual austenite of 0% to 10% (0% or more and 10% or less) in total.


The microstructure of a region other than the surface layer region is measured by the following method. Note that the microstructure in the region other than the surface layer region is measured from ⅛ depth of the sheet thickness from the surface to ⅜ depth of the sheet thickness from the surface. The reason is that the microstructure in this region shows a typical microstructure of the hot-stamping formed body.


A sample is cut out from an arbitrary position away from an end surface of the hot-stamping formed body by a distance of 50 mm or more (a position that avoids an end portion in a case where the sample cannot be collected at this position) so that a sheet thickness cross section parallel to the rolling direction can be observed. The size of the sample depends on a measurement device, but is set to a size that can be observed by about 10 mm in the rolling direction.


After polishing the cross section of the sample using silicon carbide paper of #600 to #1500, the cross section is mirror-finished using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in a diluted solution of alcohol or the like or pure water. Next, the observation surface is finished by electrolytic polishing. At an arbitrary position on the cross section of the sample in a longitudinal direction, a region which has a length of 50 μm and is present between ⅛ depth of the sheet thickness from the surface and ⅜ depth of the sheet thickness from the surface is measured at a measurement interval of 0.1 μm by an electron backscatter diffraction method, and thus, crystal orientation information is obtained. An EBSD analyzer composed of a Schottky emission scanning electron microscope and an EBSD detector may be used for measurement, for example, an EBSD analyzer composed of JSM-7001F manufactured by JEOLLtd. and DVC 5-type detector manufactured by TSL Solutions may be used for measurement. In this case, the degree of vacuum in the EBSD analyzer may be set to 9.6×10 Pa or less, an accelerating voltage may be set to 15 kV, and an irradiation current level may be set to 13.


In the obtained crystal structure information, using “Phase Map” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer, a region where a crystal structure is fcc is determined as residual austenite. The area ratio of the residual austenite is calculated, thereby the area ratio of the residual austenite is obtained. Next, regions where the crystal structure is bcc is determined as bainite, martensite, and ferrite. In these regions, under the condition that boundary with 5° is regarded as the grain boundary, using “Grain Average Misorientation” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer, regions where a grain average misorientation is 0.50 or lower are extracted as ferrite. By calculating the area ratio of the extracted ferrite, the area ratio of ferrite is obtained.


Subsequently, the area ratio of the remaining region (the region where “Grain Average Misorientation” is more than 0.5°) is calculated, and this area ratio is determined as the total area ratio of martensite and bainite.


The hot-stamping formed body may have a plating layer on the surface. By having the plating layer on the surface, corrosion resistance can be improved after hot stamping. Examples of the plating layer include an aluminum plating layer, aluminum-galvanized layer, aluminum-silicon plating layer, hot-dip galvanized layer, electrogalvanized layer, galvannealed layer, zinc-nickel plating layer, aluminum-magnesium-zinc-based plating layer.


Next, a steel sheet for hot stamping for obtaining the hot-stamping formed body according to the present embodiment will be described.


The steel sheet for hot stamping has the above-described chemical composition. The microstructure of the steel sheet for hot stamping is not particularly limited as long as a desired strength and hydrogen embrittlement resistance are obtained after hot stamping, for example, in area %, the microstructure may consist of ferrite: 5% to 90%, bainite and martensite: 0% to 100%, pearlite: 10% to 95%, and residual austenite: 0% to 5%. In addition to these, iron carbides, alloy carbides, intermetallic compounds, and inclusions may be included,


Further, the steel sheet for hot stamping may have a plating layer on the surface. By having the plating layer on the surface, corrosion resistance can be improved after hot stamping. Examples of the plating layer include an aluminum plating layer, aluminum-galvanized layer, aluminum-silicon plating layer, hot-dip galvanized layer, electrogalvanized layer, galvannealed layer, zinc-nickel plating layer, aluminum-magnesium-zinc-based plating layer.


Manufacturing method of steel sheet for hot stamping


A manufacturing method to obtain the steel sheet for hot stamping for obtaining the hot-stamping formed body according to the present embodiment will be described. In order to obtain the above-described hot-stamping formed body, it is particularly effective to control the annealing condition in the manufacturing method of the steel sheet for hot stamping.


The casting method of molten steel, the conditions of heating before hot rolling, rough rolling, finish rolling, coiling, and cold rolling are not particularly limited, and may be standard conditions.


Furthermore, for the purpose of softening the hot-rolled steel sheet, a softening heat treatment may be performed on the coil after coiling. The softening heat treatment method is not particularly limited, and standard conditions may be adopted.


Annealing

After cold rolling, it is preferable to perform annealing to heat for 15 seconds or more in an oxidizing atmosphere. Generally, it is preferable to perform annealing in a reducing atmosphere in order to suppress formation of scale. However, in the present embodiment, formation of scale on the steel sheet surface is promoted by performing annealing in the oxidizing atmosphere. During heating of hot stamping, the scale formed on the steel sheet surface becomes an oxidation source, and C and B in the surface layer region are oxidized. Since oxidized C and B leave the surface layer of the steel sheet, the amounts of C and B are reduced in the surface layer region. As a result, the strength of the prior austenite grains decreases and they become easily deformed, and grains having random orientation are likely to be generated. Thereby, grains having a desired texture can be generated in the surface layer region.


The heating temperature during annealing may be set to a temperature range of 730° C. to 900° C., and by staying in this heating temperature range for 15 seconds or more, formation of scale can be promoted while suppressing peeling of scale. The time for annealing is preferably 100 seconds or more, more preferably 200 seconds or more, and even more preferably 300 seconds or more. On the other hand, annealing for more than 3600 seconds is not preferable since the prior austenite grain sizes become coarser, the grain boundary diffusion rate of B decreases, removal of B does not proceed, and the deboronization index cannot be 0.05 or more. For this reason, the annealing time is preferably 3600 seconds or less.


After annealing in the oxidizing atmosphere, the annealing step may be performed again in an oxidizing atmosphere or a non-oxidizing atmosphere unless a treatment for removing oxide scale (for example, pickling) is performed.


In the present embodiment, the oxidizing atmosphere may be any heating atmosphere that generates oxide scale on the surface layer of the steel sheet, and may be a standard condition. For example, in a gas combustion atmosphere, it is preferable to create an atmosphere in which the mixture ratio of air and fuel (air-fuel ratio) is controlled to 1.00 or more, and more preferably controlled to 1.10 or more. It is preferable to generate an oxide scale of 15 μm or more on the steel sheet surface by annealing in the oxidizing atmosphere.


It is preferable that the oxide scale on the steel sheet surface remain in subsequent processes. That is, it is preferable to perform hot stamping, which will be described later, with the oxide scale remaining. Oxide scale is removed by shot blasting after hot stamping.


Furthermore, even when the plating layer is formed on the surface of the steel sheet for hot stamping, oxide scale remains at the interface between the base steel sheet and the plating layer. When the plating layer is formed, the oxide scale disappears after hot stamping due to an alloying reaction during heating before hot stamping.


Hot Stamping

A hot-stamping formed body according to the present embodiment is obtained by hot stamping the steel sheet for hot stamping manufactured by the above-described method. The hot stamping conditions are not particularly limited. However, for example, it is preferable to heat the steel sheet for hot stamping to a temperature range of 800° C. to 1000° C. and hold in this temperature range for 60 to 1200 seconds.


When the heating temperature is lower than 800° C., austenitization becomes insufficient, and hydrogen embrittlement resistance may deteriorate or a desired strength may not be obtained in the hot-stamping formed body. On the other hand, when the heating temperature is higher than 1000° C., the grains of prior austenite grow excessively, and hydrogen embrittlement resistance may deteriorate or a desired strength may not be obtained in the hot-stamping formed body. When the holding time is shorter than 60 seconds, austenitization becomes insufficient, and hydrogen embrittlement resistance may deteriorate or a desired strength may not be obtained in the hot-stamping formed body. When the holding time is longer than 1200 seconds, grains of prior austenite grow excessively, and hydrogen embrittlement resistance may deteriorate or a desired strength may not be obtained in the hot-stamping formed body.


A heating atmosphere is not particularly limited, and may be standard conditions, for example, such as the atmosphere, a gas combustion atmosphere with a controlled ratio of air and fuel, or a nitrogen atmosphere, and the dew point of these gases may be controlled.


After holding in the temperature range, hot stamping is performed. After hot stamping, cooling may be performed to a temperature range of 250° C. or lower at an average cooling rate of 20° C./s or faster.


Examples of heating methods before hot stamping include heating using an electric furnace and gas furnace, flame heating, electrical heating, high-frequency heating, and induction heating.


By the above methods, the hot-stamping formed body according to the present embodiment is obtained. A tempering treatment at 130° C. to 600° C. may be performed for softening after hot stamping, or a baking hardening treatment after painting may be performed. In addition, a portion of the hot-stamping formed body may be tempered by laser irradiation or the like to provide a partially softened region.


Example

Next, examples of the present invention will be described. Conditions in the examples are one example of conditions employed to confirm the feasibility and effects of the present invention, but the present invention is not limited to these examples. The present invention may employ various conditions to achieve the object of the present invention without departing from the scope of the present invention.


Slabs manufactured by casting molten steel having a chemical composition shown in Tables 1A to 2C were heated, held in a temperature range of 1200° C. or higher for 20 minutes or longer, and then subjected to rough rolling, finish rolling, cold rolling and coiling under standard conditions. And then, annealing was performed under the conditions shown in Tables 3A to 3C. Annealing was performed in an oxidizing atmosphere. In annealing in the oxidizing atmosphere, the mixture ratio of air and fuel (air-fuel ratio) was controlled to 1.05 in the gas combustion atmosphere.


The obtained steel sheets for hot stamping were heated to a temperature range shown in Tables 3A to 3C in a furnace continuously supplied with nitrogen gas (hot stamp heating), held in the temperature range, subjected to hot stamping, and then cooled to 250° C. or lower at an average cooling rate of 20° C./s or faster. As a result, the hot-stamping formed bodies shown in Tables 4A to 4C were obtained.


However, for some examples, as described in the tables, re-annealing, plating, or heating treatment for softening were performed.


The underlines in the tables indicate that it is outside the scope of the present invention, falls outside the preferable manufacturing conditions, or the characteristic value is not preferable. In addition, other than bainite, the microstructure of the surface layer region of the hot-stamping formed bodies according to the present invention examples included, in area %, martensite of 90% or more, and ferrite and residual austenite of 65% or less in total. Furthermore, the microstructure in the region other than the surface layer region of the hot-stamping formed body according to the present invention examples consisted of, in area %, martensite and bainite of 90% or more in total, and ferrite and residual austenite of 10% or less in total.


Measurements of the microstructure, deboronization index, and pole density of the texture of the hot-stamping formed body were performed by the above-described methods. In addition, the mechanical properties of the hot-stamping formed body were evaluated by the following methods.


Tensile Strength

The tensile (maximum) strength TS of the hot-stamping formed body was obtained, in accordance with JIS Z 2241:2011, by preparing a No. 5 test piece from an arbitrary position of the hot-stamping formed body and conducting a tensile test. The crosshead speed was set to 1 mm/min. When the tensile strength TS was 2200 MPa or more, it was determined as having high strength and successful, and when the tensile strength TS was less than 2200 MPa, it was determined as not having high strength and not successful.


Hydrogen Embrittlement Resistance

Hydrogen embrittlement resistance of the hot-stamping formed body was evaluated by the following method. A test piece with a length of 68 mm and a width of 6 mm was taken from an arbitrary position of the hot-stamping formed body, and the edges of the test piece were polished using silicon carbide paper of #200 to #1500, and then mirror finishing was performed using a liquid in which diamond powder with a particle size of 1 μm to 6 μm was dispersed in a diluent such as alcohol and pure water. Furthermore, the corners of the test piece were chamfered using silicon carbide paper of #200 to #1500. A stress of 800 MPa or more was applied to the test piece, the test piece was immersed in a liter of hydrochloric acid adjusted to pH 4 at room temperature for 48 hours, and the presence or absence of cracks was determined.


When no crack occurred under the load stress of 800 MPa or more, it was determined as successful. When no crack occurred at 800 MPa, an evaluation of “Fair” was used in the tables, when no crack occurred at 900 MPa, an evaluation of “Good” was used in the tables, when no crack occurred at 1000 MPa, an evaluation of “Very Good” was used in the tables, and when no crack occurred at 1100 MPa or higher, an evaluation of “Excellent” was used in the tables. On the other hand, when a crack occurred at a load stress of 800 MPa, it was determined as not successful and “Bad” was described in the tables.











TABLE 1A








Chemical composition (mass %) remainder being Fe and impurities






















Steel
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Notes
























1
0.46
0.430
0.42
0.009
0.0003
0.0035
0.0016
0.0440
0.0180
0.020
0.270
0.1900
0.0025
Steel of present invention


2
0.47
0.330
0.40
0.009
0.0008
0.0031
0.0017
0.0290
0.0470
0.020
0.410
0.1000
0.0019
Steel of present invention


3
0.41
0.282
0.46
0.013
0.0003
0.0030
0.0017
0.0424
0.0600
0.019
0.500
0.0500
0.0020
Steel of present invention


4
0.55
0.322
0.44
0.013
0.0002
0.0023
0.0020
0.0330
0.0286
0.015
0.500
0.0200
0.0025
Steel of present invention


5
0.69
0.400
0.46
0.012
0.0002
0.0030
0.0015
0.0600
0.0500
0.025
0.461
0.1500
0.0020
Steel of present invention


6

0.39

0.361
0.40
0.013
0.0005
0.0026
0.0019
0.0365
0.0600
0.025
0.230
0.1800
0.0027
Steel of present invention


7

0.72

0.200
0.42
0.013
0.0004
0.0024
0.0025
0.0600
0.0290
0.020
0.300
0.0500
0.0028
Comparative steel


8
0.47
0.015
0.50
0.012
0.0003
0.0024
0.0019
0.0424
0.0500
0.025
0.422
0.0950
0.0019
Comparative steel


9
0.47
1.290
0.50
0.010
0.0003
0.0026
0.0016
0.0482
0.0450
0.018
0.460
0.1000
0.0018
Steel of present invention


10
0.47
2.980
0.40
0.013
0.0004
0.0022
0.0017
0.0600
0.0290
0.015
0.304
0.0980
0.0021
Steel of present invention


11
0.41

0.004

0.42
0.013
0.0004
0.0034
0.0010
0.0380
0.0330
0.021
0.200
0.0200
0.0014
Comparative steel


12
0.47

3.050

0.40
0.011
0.0003
0.0024
0.0021
0.0420
0.0450
0.015
0.200
0.1000
0.0027
Comparative steel


13
0.47
0.322
0.10
0.014
0.0004
0.0024
0.0025
0.0365
0.0300
0.019
0.400
0.3000
0.0026
Steel of present invention


14
0.46
0.361
0.59
0.013
0.0003
0.0024
0.0021
0.0541
0.0208
0.023
0.500
0.1000
0.0024
Steel of present invention


15
0.42
0.420

0.05

0.008
0.0005
0.0037
0.0015
0.0330
0.0200
0.024
0.100
0.0300
0.0020
Comparative steel


16
0.45
0.280

0.65

0.013
0.0003
0.0030
0.0017
0.0420
0.0600
0.019
0.300
0.1500
0.0030
Comparative steel


17
0.46
0.361
0.42
0.095
0.0003
0.0028
0.0017
0.0365
0.0300
0.019
0.500
0.1900
0.0015
Steel of present invention


18
0.46
0.420
0.41

0.115

0.0004
0.0035
0.0014
0.0400
0.0200
0.020
0.280
0.1900
0.0025
Comparative steel


19
0.47
0.282
0.42
0.014
0.0098
0.0022
0.0023
0.0365
0.0290
0.023
0.200
0.1900
0.0020
Steel of present invention


20
0.46
0.430
0.40
0.010

0.0135

0.0033
0.0015
0.0400
0.0210
0.020
0.300
0.1900
0.0024
Comparative steel


21
0.45
0.400
0.44
0.014
0.0003
0.0193
0.0017
0.0541
0.0340
0.021
0.300
0.2000
0.0025
Steel of present invention


22
0.45
0.240
0.44
0.010
0.0003

0.0210

0.0015
0.0600
0.0520
0.021
0.460
0.1900
0.0027
Comparative steel


23
0.46
0.361
0.48
0.012
0.0003
0.0022
0.0194
0.0541
0.0522
0.019
0.500
0.2100
0.0021
Steel of present invention


24
0.46
0.400
0.46
0.010
0.0003
0.0020

0.0210

0.0300
0.0200
0.015
0.420
0.2000
0.0015
Comparative steel


25
0.45
0.322
0.40
0.013
0.0004
0.0020
0.0021
0.0018
0.0365
0.020
0.304
0.1900
0.0019
Steel of present invention





The underline indicates that it is outside the scope of the present invention.















TABLE 1B








Chemical composition (mass %) remainder being Fe and impurities






















Steel
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Notes





26
0.46
0.330
0.50
0.012
0.0004
0.0033
0.0017
0.2950
0.0440
0.019
0.290
0.2000
0.0020
Steel of present invention


27
0.47
0.204
0.50
0.011
0.0005
0.0026
0.0021
0.4910
0.0350
0.020
0.300
0.2000
0.0023
Steel of present invention


28
0.46
0.330
0.48
0.011
0.0004
0.0035
0.0050

0.0006

0.0450
0.021
0.270
0.1900
0.0024
Comparative steel


29
0.45
0.280
0.48
0.011
0.0003
0.0022
0.0021

0.5200

0.0280
0.020
0.380
0.1950
0.0021
Comparative steel


30
0.45
0.282
0.44
0.013
0.0003
0.0028
0.0025
0.0424
0.0050
0.023
0.100
0.2000
0.0018
Steel of present invention


31
0.46
0.420
0.40
0.010
0.0004
0.0034
0.0018
0.0450
0.0950
0.020
0.290
0.1900
0.0027
Steel of present invention


32
0.41
0.300
0.40
0.011
0.0003
0.0028
0.0020
0.0330

0.0006

0.021
0.270
0.0600
0.0019
Comparative steel


33
0.46
0.400
0.42
0.011
0.0004
0.0027
0.0020
0.0330

0.1200

0.020
0.300
0.1000
0.0024
Comparative steel


34
0.46
0.282
0.48
0.014
0.0002
0.0020
0.0019
0.0541
0.0350
0.011
0.300
0.2000
0.0019
Steel of present invention


35
0.46
0.400
0.42
0.011
0.0004
0.0028
0.0020
0.0390
0.0190
0.064
0.270
0.1900
0.0028
Steel of present invention


36
0.45
0.361
0.48
0.012
0.0002
0.0026
0.0023
0.0310
0.0290
0.180
0.340
0.1800
0.0015
Steel of present invention


37
0.41
0.300
0.39
0.012
0.0005
0.0030
0.0025
0.0320
0.0200

0.006

0.300
0.0500
0.0023
Comparative steel


38
0.46
0.390
0.41
0.012
0.0006
0.0031
0.0018
0.0300
0.0410

0.210

0.300
0.2000
0.0027
Comparative steel


39
0.47
0.243
0.48
0.015
0.0004
0.0030
0.0017
0.0482
0.0500
0.020
0.015
0.2000
0.0025
Steel of present invention


40
0.46
0.361
0.44
0.012
0.0004
0.0030
0.0021
0.0430
0.0300
0.023
0.780
0.1900
0.0018
Steel of present invention


41
0.41
0.400
0.42
0.012
0.0005
0.0030
0.0023
0.0320
0.0190
0.020

0.004

0.0500
0.0019
Comparative steel


42
0.45
0.280
0.46
0.014
0.0002
0.0024
0.0025
0.0420
0.0200
0.020

0.870

0.1800
0.0025
Comparative steel


43
0.46
0.400
0.42
0.010
0.0003
0.0035
0.0016
0.0400
0.0220
0.022
0.400
0.0040
0.0020
Steel of present invention


44
0.46
0.400
0.43
0.011
0.0004
0.0034
0.0020
0.0380
0.0210
0.022
0.370
0.5000
0.0021
Steel of present invention


45
0.46
0.410
0.40
0.011
0.0003
0.0018
0.0019
0.0380
0.0210
0.022
0.380
0.9700
0.0015
Steel of present invention


46
0.42
0.350
0.42
0.010
0.0004
0.0026
0.0020
0.0330
0.0200
0.021
0.100

0.0008

0.0024
Comparative steel


47
0.46
0.420
0.40
0.010
0.0005
0.0023
0.0019
0.0300
0.0200
0.020
0.350

1.1000

0.0025
Comparative steel


48
0.46
0.322
0.40
0.012
0.0003
0.0026
0.0015
0.0482
0.0360
0.017
0.460
0.2000
0.0005
Steel of present invention


49
0.46
0.300
0.41
0.010
0.0003
0.0030
0.0017
0.0350
0.0270
0.020
0.400
0.1900
0.0105
Steel of present invention


50
0.46
0.300
0.42
0.010
0.0004
0.0031
0.0018
0.0340
0.0280
0.020
0.400
0.1900
0.0198
Steel of present invention





The underline indicates that it is outside the scope of the present invention.















TABLE 1C








Chemical composition (mass %) remainder being Fe and impurities






















Steel
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Notes
























51
0.42
0.240
0.30
0.011
0.0005
0.0029
0.0018
0.0300
0.0290
0.020
0.100
0.1000

0.0002

Comparative steel


52
0.46
0.250
0.42
0.012
0.0005
0.0036
0.0019
0.0310
0.0300
0.021
0.300
0.2000

0.0210

Comparative steel


53
0.46
0.420
0.43
0.010
0.0003
0.0035
0.0016
0.0440
0.0180
0.020
0.270
0.1900
0.0029
Steel of present invention


54
0.46
0.420
0.43
0.011
0.0004
0.0034
0.0018
0.0400
0.0190
0.020
0.280
0.1900
0.0028
Steel of present invention


55
0.46
0.420
0.43
0.010
0.0003
0.0034
0.0019
0.0410
0.0200
0.020
0.280
0.1900
0.0027
Steel of present invention


56
0.46
0.430
0.43
0.010
0.0003
0.0034
0.0018
0.0400
0.0190
0.020
0.280
0.1900
0.0025
Steel of present invention


57
0.46
0.420
0.41
0.011
0.0004
0.0030
0.0020
0.0320
0.0200
0.020
0.290
0.1950
0.0023
Steel of present invention


58
0.46
0.420
0.41
0.011
0.0004
0.0030
0.0020
0.0330
0.0200
0.020
0.290
0.2000
0.0023
Steel of present invention


59
0.46
0.420
0.41
0.011
0.0004
0.0025
0.0020
0.0320
0.0200
0.020
0.290
0.2000
0.0024
Steel of present invention


60
0.46
0.420
0.41
0.011
0.0005
0.0024
0.0023
0.0330
0.0200
0.020
0.290
0.2000
0.0023
Steel of present invention


61
0.46
0.420
0.42
0.010
0.0004
0.0030
0.0020
0.0320
0.0200
0.020
0.290
0.2000
0.0025
Steel of present invention


62
0.46
0.400
0.41
0.010
0.0004
0.0030
0.0021
0.0330
0.0210
0.021
0.300
0.2000
0.0023
Steel of present invention


63
0.46
0.400
0.41
0.011
0.0003
0.0032
0.0020
0.0320
0.0200
0.020
0.290
0.1950
0.0027
Steel of present invention


64
0.46
0.420
0.41
0.011
0.0004
0.0029
0.0020
0.0320
0.0200
0.020
0.290
0.1950
0.0023
Steel of present invention





The underline indicates that it is outside the scope of the present invention.















TABLE 2A








Chemical composition (mass %) remainder being Fe and impurities





















Steel
Co
Ni
Cu
V
W
Ca
Mg
REM
Sb
Sn
Zr
As
Notes























1












Steel of present invention


2












Steel of present invention


3












Steel of present invention


4












Steel of present invention


5












Steel of present invention


6












Comparative steel


7












Comparative steel


8












Steel of present invention


9












Steel of present invention


10












Steel of present invention


11












Comparative steel


12












Comparative steel


13












Steel of present invention


14












Steel of present invention


15












Comparative steel


16












Comparative steel


17












Steel of present invention


18












Comparative steel


19












Steel of present invention


20












Comparative steel


21












Steel of present invention


22












Comparative steel


23












Steel of present invention


24












Comparative steel


25












Steel of present invention


















TABLE 2B








Chemical composition (mass %) remainder being Fe and impurities





















Steel
Co
Ni
Cu
V
W
Ca
Mg
REM
Sb
Sn
Zr
As
Notes





26












Steel of present invention


27












Steel of present invention


28












Comparative steel


29












Comparative steel


30












Steel of present invention


31












Steel of present invention


32












Comparative steel


33












Comparative steel


34












Steel of present invention


35












Steel of present invention


36












Steel of present invention


37












Comparative steel


38












Comparative steel


39












Steel of present invention


40












Steel of present invention


41












Comparative steel


42












Comparative steel


43












Steel of present invention


44












Steel of present invention


45












Steel of present invention


46












Comparative steel


47












Comparative steel


48












Steel of present invention


49












Steel of present invention


50












Steel of present invention


















TABLE 2C








Chemical composition (mass %) remainder being Fe and impurities





















Steel
Co
Ni
Cu
V
W
Ca
Mg
REM
Sb
Sn
Zr
As
Notes





51












Comparative steel


52












Comparative steel


53
3.00











Steel of present invention


54

0.20










Steel of present invention


55


0.30









Steel of present invention


56



0.09








Steel of present invention


57




0.50







Steel of present invention


58





0.0055






Steel of present invention


59






0.0032





Steel of present invention


60







0.0046




Steel of present invention


61








0.050



Steel of present invention


62









0.051


Steel of present invention


63










0.080

Steel of present invention


64











0.004
Steel of present invention





















TABLE 3A









Annealing
Hot stamping


















Annealing
Annealing
Heating
Holding




Examination

temperature
time
temperature
time




No.
Steel
° C.
s
° C.
s
Notes
Notes

















1
 1
800
600
900
120

Present invention example


2
 2
800
600
900
120

Present invention example


3
 3
800
600
900
120

Present invention example


4
 4
800
600
900
120
Softening heat treatment
Present invention example








on coil after coiling



5
 5
780
200
850
120
Softening heat treatment
Present invention example








on coil after coiling



6
6
800
650
900
150

Comparative example


7
7
780
200
850
120

Comparative example


8
 8
800
600
900
120
Galvannealed plating
Present invention example


9
 9
800
600
900
120

Present invention example


10
10
840
600
990
200

Present invention example


11

11

800
600
900
120

Comparative example


12

12

800
600
900
120

Comparative example


13
13
800
600
900
120

Present invention example


14
14
800
600
900
120
Re-annealing
Present invention example


15

15

800
600
900
120

Comparative example


16

16

800
600
900
120

Comparative example


17
17
800
600
900
120

Present invention example


18

18

800
600
900
120

Comparative example


19
19
800
600
900
120

Present invention example


20

20

800
600
900
120

Comparative example


21
21
800
600
900
120

Present invention example


22

22

800
600
900
120

Comparative example


23
23
800
600
900
120
Electrogalvanized plating
Present invention example


24

24

800
600
900
120

Comparative example


25
25
800
600
900
120

Present invention example





The underline indicates that it falls outside the preferable manufacturing conditions.


















TABLE 3B









Annealing
Hot stamping


















Annealing
Annealing
Heating
Holding




Examination

temperature
time
temperature
time




No.
Steel
° C.
s
° C.
s
Notes
Notes

















26
26
800
600
900
120

Present invention example


27
27
800
600
900
120

Present invention example


28

28

800
600
900
120

Comparative example


29

29

800
300
900
120

Comparative example


30
30
800
600
900
120

Present invention example


31
31
800
600
900
120

Present invention example


32

32

800
600
900
120

Comparative example


33

33

800
600
900
120

Comparative example


34
34
800
600
900
120

Present invention example


35
35
800
600
900
120

Present invention example


36
36
800
600
900
120

Present invention example


37

37

800
600
900
120

Comparative example


38

38

800
600
900
120

Comparative example


39
39
800
600
900
120

Present invention example


40
40
800
600
900
120
Softening heat treatment
Present invention example








on coil after coiling



41

41

800
600
900
120

Comparative example


42

42

800
600
900
120

Comparative example


43
43
800
600
900
120

Present invention example


44
44
800
600
900
120

Present invention example


45
45
800
600
900
120
Softening heat treatment
Present invention example








on coil after coiling



46

46

800
600
900
120

Comparative example


47

47

800
600
900
120

Comparative example


48
48
800
600
900
120

Present invention example


49
49
800
600
900
120
Aluminum-galvanized
Present invention example








plating



50
50
800
600
900
120

Present invention example





The underline indicates that it falls outside the preferable manufacturing conditions.


















TABLE 3C









Annealing
Hot stamping


















Annealing
Annealing
Heating
Holding




Examination

temperature
time
temperature
time




No.
Steel
° C.
s
° C.
s
Notes
Notes

















51

51

800
600
900
120

Comparative example


52

52

800
600
900
120

Comparative example


53
53
800
600
900
120

Present invention example


54
54
800
600
900
120
Aluminum-silicon
Present invention example








plating



55
55
800
600
900
120
Aluminum plating
Present invention example


56
56
800
600
900
120

Present invention example


57
57
800
600
900
120
Aluminum-magnesium-
Present invention example








zinc plating



58
58
800
600
900
120

Present invention example


59
59
800
600
900
120

Present invention example


60
60
800
600
900
120

Present invention example


61
61
800
600
900
120
Galvannealed plating
Present invention example


62
62
800
600
900
120

Present invention example


63
63
800
600
900
120
Zinc-nickel plating
Present invention example


64
64
800
600
900
120

Present invention example


65
 1
750
600
900
120

Present invention example


66
 1
900
600
900
120

Present invention example


67
 1

680

600
900
120

Comparative example


68
 1

1000

600
900
120

Comparative example


69
 1
800
 20
900
120

Present invention example


70
 1
780
10
900
120

Comparative example


71
 1
800
300
820
120

Present invention example


72
 1
800
600
1000 
120

Present invention example


73
 1
800
600

750

120

Comparative example


74
 1
800
600

1100

120

Comparative example


75
 1
800
600
900
 60

Present invention example


76
 1
800
600
900
1100 

Present invention example


77
 1
800
300
900
30

Comparative example


78
 1
800
600
900

1300


Comparative example


79
 1
800
600
900
120

Annealing in reducing

Comparative example









atmosphere, Hot-stamping










in atmosphere



80
56
800
600
900
120

Annealing in reducing

Comparative example









atmosphere, Hot-stamping










in atmosphere



81
 1
800
600
900
120
Hot-stamping in
Present invention example








atmosphere



82
56
800
600
900
120
Hot-stamping in
Present invention example








atmosphere



83
 1
800

3700

900
120

Comparative example





The underline indicates that it falls outside the preferable manufacturing conditions.


















TABLE 4A









Surface layer region




















Maximum









value of


Evaluation





Bainite
pole

Tensile
of hydrogen



Examination

area
density of
Deboronization
strength
embrittlement



No.
Steel
%
texture-
index-
MPa
resistance
Notes





 1
 1
22
2.6
0.45
2412
Excellent
Present invention example


 2
 2
30
2.4
0.47
2426
Excellent
Present invention example


 3
 3
68
1.7
0.47
2245
Excellent
Present invention example


 4
 4
72
2.7
0.45
2705
Good
Present invention example


 5
 5
85
3.2
0.40
3136
Fair
Present invention example


6
6
35
1.6
0.48

2124

Excellent
Comparative example


7
7
90

4.1

0.30
2458

Bad

Comparative example


 8
 8
25
2.2
0.46
2374
Excellent
Present invention example


 9
 9
45
2.4
0.44
2463
Excellent
Present invention example


10
10
60
1.2
0.64
2404
Excellent
Present invention example



11


11

9
2.0
0.45

2098

Excellent
Comparative example



12


12

5
1.9
0.48

2178


Bad

Comparative example


13
13
50
2.0
0.48
2228
Excellent
Present invention example


14
14
65
3.8
0.47
2478
Good
Present invention example



15


15

15
1.5
0.48

2011

Excellent
Comparative example



16


16

70

4.8

0.45
2407

Bad

Comparative example


17
17
38
3.2
0.44
2439
Fair
Present invention example



18


18

35
3.0
0.44
2412

Bad

Comparative example


19
19
47
2.5
0.46
2451
Fair
Present invention example



20


20

45
2.4
0.46
2430

Bad

Comparative example


21
21
42
2.3
0.47
2409
Good
Present invention example



22


22

40
2.5
0.45
2387

Bad

Comparative example


23
23
38
2.9
0.44
2439
Fair
Present invention example



24


24

35
2.7
0.45
2411

Bad

Comparative example


25
25
40
3.0
0.42
2451
Good
Present invention example





The underline indicates that it is outside the scope of the present invention, or the characteristic value is not preferable.


















TABLE 4B









Surface layer region




















Maximum


Evaluation






value


of






of pole

Tensile
hydrogen



Examination

Bainite
density of
Deboronization
strength
embrittlement



No.
Steel
area %
texture-
index-
MPa
resistance
Notes





26
26
29
2.8
0.46
2426
Excellent
Present invention example


27
27
30
3.0
0.45
2437
Very Good
Present invention example



28


28

41
3.1
0.40
2460

Bad

Comparative example



29


29

25
3.1
0.35
2444

Bad

Comparative example


30
30
38
2.0
0.34
2380
Good
Present invention example


31
31
25
2.9
0.48
2452
Very Good
Present invention example



32


32

60
1.6
0.45

2155

Excellent
Comparative example



33


33

32
3.2
0.49
2478

Bad

Comparative example


34
34
28
2.8
0.45
2440
Excellent
Present invention example


35
35
31
2.9
0.45
2456
Excellent
Present invention example


36
36
30
2.7
0.46
2418
Very Good
Present invention example



37


37

60
1.5
0.46

2178

Excellent
Comparative example



38


38

45
3.2
0.45
2432

Bad

Comparative example


39
39
40
2.8
0.47
2450
Excellent
Present invention example


40
40
60
3.7
0.44
2479
Good
Present invention example



41


41

8
1.6
0.45

2021

Excellent
Comparative example



42


42

65

4.3

0.44
2490

Bad

Comparative example


43
43
14
1.9
0.46
2325
Excellent
Present invention example


44
44
48
2.8
0.45
2468
Very Good
Present invention example


45
45
70
3.9
0.44
2508
Fair
Present invention example



46


46


10

1.5
0.45

2048

Excellent
Comparative example



47


47

75

4.2

0.44
2522

Bad

Comparative example


48
48
19
2.5
0.32
2419
Excellent
Present invention example


49
49
28
2.7
0.46
2434
Excellent
Present invention example


50
50
35
2.9
0.48
2452
Good
Present invention example





The underline indicates that it is outside the scope of the present invention, or the characteristic value is not preferable.


















TABLE 4C









Surface layer region




















Maximum









value of


Evaluation of






pole

Tensile
hydrogen



Examination

Bainite
density of
Deboronization
strength
embrittlement



No.
Steel
area %
texture-
index-
MPa
resistance
Notes






51


51

11
2.2
0.19

2189

Excellent
Comparative example



52


52

40
3.4
0.46
2421

Bad

Comparative example


53
53
24
2.6
0.46
2425
Excellent
Present invention example


54
54
28
2.4
0.46
2439
Very Good
Present invention example


55
55
26
2.5
0.47
2418
Very Good
Present invention example


56
56
27
2.7
0.45
2449
Excellent
Present invention example


58
58
25
2.8
0.45
2426
Very Good
Present invention example


59
59
23
2.5
0.45
2408
Excellent
Present invention example


60
60
20
2.3
0.46
2403
Excellent
Present invention example


61
61
22
2.5
0.44
2415
Excellent
Present invention example


62
62
25
2.5
0.45
2422
Excellent
Present invention example


63
63
26
2.4
0.44
2420
Excellent
Present invention example


64
64
26
2.4
0.45
2421
Excellent
Present invention example


65
65
28
2.5
0.46
2437
Excellent
Present invention example


65
 1
20
2.7
0.28
2423
Very Good
Present invention example


66
 1
15
2.4
0.54
2355
Excellent
Present invention example



67

 1
6

5.4

0.10
2427

Bad

Comparative example



68

 1
5
2.4
0.60

2179


Bad

Comparative example


69
 1
15
3.7
0.11
2439
Good
Present invention example



70

 1
9

4.2


0.03

2450

Bad

Comparative example


71
 1
13
2.8
0.12
2473
Very Good
Present invention example


72
 1
14
2.7
0.48
2258
Very Good
Present invention example



73

 1
8

4.5


0.04


2185


Bad

Comparative example



74

 1
7
2.7
0.49

2193


Bad

Comparative example


75
 1
20
2.7
0.43
2459
Very Good
Present invention example


76
 1
16
2.4
0.49
2238
Excellent
Present invention example



77

 1
5

4.1


0.04


2178


Bad

Comparative example



78

 1
6
2.6
0.48

2164


Bad

Comparative example



79

 1
15

4.3


0.03

2455

Bad

Comparative example



80

56
20

4.5


0.04

2461

Bad

Comparative example


81
 1
19
3.1
0.30
2426
Excellent
Present invention example


82
56
29
2.9
0.47
2463
Excellent
Present invention example



83

 1
11

4.5


0.03

2302

Bad

Comparative example





The underline indicates that it is outside the scope of the present invention, or the characteristic value is not preferable.






From Tables 4A to 4C, it can be seen that the hot-stamping formed bodies according to the present invention examples had high strength and excellent hydrogen embrittlement resistance. On the other hand, it can be seen that in the hot-stamping formed bodies according to comparative examples, one of the properties deteriorated.


INDUSTRIAL APPLICABILITY

According to the above-described aspects of the present invention, it is possible to provide a hot-stamping formed body having high strength and excellent hydrogen embrittlement resistance.

Claims
  • 1. A hot-stamping formed body comprising, as a chemical composition, by mass %: C: more than 0.40% and 0.70% or less;Si: 0.010% to 3.000%;Mn: 0.10% or more and less than 0.60%;P: 0.100% or less;S: 0.0100% or less;N: 0.0200% or less;0: 0.0200% or less;Al: 0.0010% to 0.5000%;Nb: 0.0010% to 0.1000%;Ti: 0.010% to 0.200%;Cr: 0.010% to 0.800%;Mo: 0.0010% to 1.0000%;B: 0.0005% to 0.0200%;Co: 0% to 40.00%;Ni: 0% to 3.00%;Cu: 0% to 30.00%;V: 0% to 3.00%;W: 0% to 3.00%;Ca: 0% to 1.0000%;Mg: 0% to 1.0000%;REM: 0% to 1.0000%;Sb: 0% to 1.000%;Sn: 0% to 1.000%;Zr: 0% to 1.000%;As: 0% to 0.100%; anda remainder: Fe and impurities,in a surface layer region, which is a region from a surface of the hot-stamping formed body to 1/25 depth of a sheet thickness from the surface,an area ratio of bainite is more than 10%,a maximum value of pole density of a texture is 4.0 or less, anda deboronization index is 0.05 or more.
  • 2. The hot-stamping formed body according to claim 1 comprising, as the chemical composition, by mass %, one or more of: Co: 0.01% to 4.00%;Ni: 0.01% to 3.00%;Cu: 0.01% to 3.00%;V: 0.01% to 3.00%;W: 0.01% to 3.00%;Ca: 0.0001% to 1.0000%;Mg: 0.0001% to 1.0000%;REM: 0.0001% to 1.0000%;Sb: 0.001% to 1.000%;Sn: 0.001% to 1.000%;Zr: 0.001% to 1.000%; andAs: 0.001% to 0.100%.
Priority Claims (1)
Number Date Country Kind
2022-067023 Apr 2022 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2023/007780 3/2/2023 WO