HOT-STAMPING FORMED BODY

Information

  • Patent Application
  • 20250101557
  • Publication Number
    20250101557
  • Date Filed
    March 02, 2023
    2 years ago
  • Date Published
    March 27, 2025
    15 days ago
Abstract
This hot-stamping formed body has a predetermined chemical composition, in an interior region, a standard deviation of grain sizes of prior austenite grains of 5.0 μm or less, 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. 2022-067020, 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



Non-Patent Document



  • Non-Patent Document 1: Acta Materialia, 58 (2010), 6393-6403



DISCLOSURE OF THE INVENTION
Problems to be Solved by the Invention

In order to make vehicle members lighter, it is effective to increase the strength of steel sheets. In order to increase the strength of the steel sheets, there is a method of increasing the Mn content in order to improve hardenability of the steel sheet. However, increasing the Mn content poses problems such as hydrogen embrittlement cracking and early fracture.


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.


Early fracture is a phenomenon in which fracture occurs at a stress lower than tensile strength estimated from the hardness of the steel member. This susceptibility to early fracture is called early fracture resistance:


In Patent Document 1, bendability is considered, but hydrogen embrittlement resistance and early fracture 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 and early fracture 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 3.00%;
    • Mn: 0.60% to 3.00%;
    • P: 0.100% or less;
    • S: 0.0100% or less;
    • N: 0.0200% or less;
    • O: 0.0200% or less;
    • Al: 0.0010% to 0.5000%;
    • Nb: 0.0010% to 0.100%;
    • Ti: 0.010% to 0.200%;
    • Cr: 0.01% to 0.80%;
    • Mo: 0.0010% to 1.000%;
    • 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 1.000%;
    • Mg: 0% to 1.000%;
    • REM: 0% to: 1.000%;
    • 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 an interior region, which is a region between 4/16 depth of a sheet thickness from a surface of the hot-stamping formed body and 5/16 depth of the sheet thickness from the surface,
    • a standard deviation of grain sizes of prior austenite grains is 5.0 μm or less,
    • in a surface layer region, which is a region between the surface and 1/25 depth of the 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: 0.001% to 1.000%;
    • Mg: 0.001% to 1.000%;
    • REM: 0.001% to 1.000%;
    • 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, excellent hydrogen embrittlement resistance and early fracture 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 by reducing the standard deviation of grain sizes of prior austenite grains in the interior region, hydrogen embrittlement resistance and early fracture resistance of the hot-stamping formed body can be improved. In addition, the present inventors found that in the surface layer region, by generating a desired amount of bainite, by creating the texture with a desired crystal orientation, and by achieving a desired deboronization index, hydrogen embrittlement resistance can be further 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 finish rolling and annealing under desired conditions during manufacturing of 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 3.00%, Mn: 0.60% to 3.00%, P: 0.100% or less, S: 0.0100% or less, N: 0.0200% or less, O: 0.0200% or less, Al: 0.0010% to 0.5000%, Nb: 0.0010% to 0.100%, Ti: 0.010% to 0.200%, Cr: 0.01% to 0.80%, Mo: 0.0010% to 1.000%, 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%, toughness of martensite deteriorates and excellent 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 3.00%

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 0.05% or more, 0.10% or more or 0.15% or more.


Meanwhile, when the Si content is more than 3.00%, the amount of ferrite increases and a desired microstructure cannot be obtained. For this reason, the Si content is set to 3.00% or less. The Si content is preferably 2.00% or less, 1.00% or less or 0.70% or less.


Mn: 0.60% to 3.00%

Mn promotes the transformation from prior austenite to pearlite in a hot-rolled steel sheet having the chemical composition of the present embodiment, and contributes to control of grain size distribution of prior austenite of the hot-stamping formed body. In order to set the standard deviation of grain sizes of prior austenite grains, the Mn content is set to 0.60% or more. The Mn content is preferably 0.70% or more or 1.00% or more.


Meanwhile, when the Mn content is more than 3.00%, transformation from prior austenite to pearlite in a hot-rolled steel sheet having the chemical composition of the present embodiment is excessively promoted, and the standard deviation of grain sizes of prior austenite grains in the hot-stamping formed body cannot be set to a desired range. For this reason, the Mn content is set to 3.00% or less. The Mn content is preferably 2.50% or less or 2.30% or less.


P: 0.100% or Less.

P is an impurity element, and by segregating in the grain boundaries, it becomes a starting point for fracture and deteriorates early fracture resistance. 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 become starting points for fracture and deteriorate early fracture resistance. 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 become starting points for fracture and deteriorate early fracture resistance. 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 a coarse oxide that becomes a starting point for fracture in steel when a large amount of O is comprised, and deteriorates early fracture resistance of the hot-stamping formed body. 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 and early fracture resistance deteriorates. 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, and early fracture resistance of the hot-stamping formed body deteriorates. 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 0.100%

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 0.005% or more, 0.009% or more or 0.015% or more.


Meanwhile, when the Nb content is more than 0.100%, many carbonitrides are generated in steel, and early fracture resistance of the hot-stamping formed body deteriorates. For this reason, the Nb content is set to 0.100% or less. The Nb content is preferably 0.080% or less or 0.060% 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 carbonitrides are generated in steel, and early fracture 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, 0.100% or less, 0.080% or less, 0.060% or less or 0.050% or less.


Cr: 0.01% to 0.80%

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 0.01%, a desired strength cannot be obtained. For this reason, the Cr content is set to 0.01% or more. The Cr content is preferably 0.10% or more, 0.15% or more or 0.20% or more.


Meanwhile, when the Cr content is more than 0.80%, coarse intermetallic compounds are formed in the hot-stamping formed body and early fracture resistance deteriorates. For this reason, the Cr content is set to 0.80% or less. The Cr content is preferably 0.70% or less, 0.50% or less or 0.40% or less.


Mo: 0.0010% to 1.000%

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 0.010% or more, 0.050% or more or 0.100% or more.


Meanwhile, when the Mo content is more than 1.000%, coarse intermetallic compounds are formed in the hot-stamping formed body and early fracture resistance deteriorates. For this reason, the Mo content is set to 1.000% or less. The Mo content is preferably 0.800% or less, 0.600% or less or 0.400% 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 formed in the hot-stamping formed body and early fracture resistance 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 carbonitrides are generated in steel, and early fracture 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 1.000%

Ca is an element that suppresses generation of carbides that become starting points for fracture, and contributes to improvement of early fracture resistance. In order to reliably obtain the effect, the Ca 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 Ca content is set to 1.000% or less. If necessary, the upper limit of Ca content may be set to 0.100%, 0.010%, 0.005%, 0.001%, 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, and contributes to improvement of early fracture resistance. In order to reliably obtain these effects, the Mg 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 Mg content is set to 1.000% or less. If necessary, the upper limit of Mg content may be set to 0.100%, 0.010%, 0.005%, 0.001%, 0.0005% or 0.0002%.


REM: 0% to 1.000%

REM suppresses generation of oxides that become starting points of fracture and contributes to improvement of early fracture resistance. In order to reliably obtain the effect, the REM 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 REM content is set to 1.000% or less. If necessary, the upper limit of REM content may be set to 0.100%, 0.010%, 0.005%, 0.001%, 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 oxides that become starting points of fracture and contributes to improvement of early fracture resistance. 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 oxides that become starting points of fracture and contributes to improvement of early fracture resistance. 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 oxides that become starting points of fracture and contributes to improvement of early fracture resistance. 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, and contributes to improvement of early fracture resistance. 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 the interior region, which is a region between 4/16 depth of the sheet thickness (thickness of the hot-stamping formed body) from the surface of the hot-stamping formed body and 5/16 depth of the sheet thickness from the surface, the standard deviation of grain sizes of prior austenite grains is 5.0 μm or less; in the surface layer region, which is a region between the surface and 1/25 depth of the sheet thickness 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 interior region in the present embodiment refers to a 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.


In addition, the surface layer region refers to a region between the surface of the hot-stamping formed body and 1/25 depth of the sheet thickness 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.


“Interior Region”
Standard Deviation of Grain Sizes of Prior Austenite Grains: 5.0 μm or Less

By reducing the dispersion of grain sizes of prior austenite grains in the interior region, that is, by reducing the standard deviation, an increase of local residual stress can be suppressed. As a result, hydrogen embrittlement resistance and early fracture resistance of the hot-stamping formed body can be improved. When the standard deviation of grain sizes of prior austenite grains is more than 5.0 μm, hydrogen embrittlement resistance and early fracture resistance deteriorate. For this reason, the standard deviation of grain sizes of prior austenite grains is set to 5.0 μm or less, preferably 4.0 μm or less, 3.0 μm or less or 2.5 μm or less.


The lower limit of the standard deviation of grain sizes of prior austenite grains is not particularly limited, but may be set to 0.1 μm. 0.5 μm, 1.0 μm or 1.5 μm.


The standard deviation of grain sizes of prior austenite grains 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 50 μm and is present between 4/16 depth of the sheet thickness from the surface and 5/16 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 9.6×10−5 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, the crystal orientation of prior austenite grains is calculated from the crystal orientation relationship between general prior austenite grains and grains having a body-centered structure after transformation, and after calculating the average grain size of prior austenite grains using the crystal orientation, the standard deviation is calculated.


The method for calculating the crystal orientation of prior austenite grains is the following method. First, the crystal orientation map of the prior austenite grains is created by the method described in Non-Patent Document 1. For one of prior austenite grain included in the observed visual field, an average value of a shortest diameter and a longest diameter is calculated, and the average value is regarded as the grain size of the prior austenite grain. The above operation is performed on all prior austenite grains except for the prior austenite grains which are not entirely included in the photographed visual fields, such as grains in an end portion of the photographed visual field, and the grain sizes of all the prior austenite grains in the photographed visual fields are obtained. By calculating the standard deviation from the obtained grain sizes of all austenite grains, the standard deviation of grain sizes of austenite grains 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.


The microstructure of the interior region is not particularly limited as long as the desired strength, hydrogen embrittlement resistance and early fracture 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. Martensite in the present embodiment includes untempered martensite (fresh martensite) and tempered martensite.


The microstructure of the hot-stamping formed body is measured 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 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 4/16 depth of the sheet thickness from the surface and 5/16 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 9.6×10:5 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 fec 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 0.5° 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.


“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 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 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.


The area ratio of the microstructure is calculated for the surface layer region (the region between the surface and 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 9.6×10−5 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 “OIM 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.


“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 9.6×10−5 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 @2=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 mm, 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 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, hydrogen embrittlement resistance and early fracture 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 finish rolling condition and the annealing condition in the manufacturing method of the steel sheet for hot stamping.


Finish Rolling

In finish rolling, it is preferable to set the rolling reduction of the final pass (final rolling reduction) to 20% or more. The final rolling reduction can be expressed as {(t0−t1)/t0}×100(%), where to is the sheet thickness before rolling of the final pass, and t1 is the sheet thickness after rolling of the final pass. By increasing the final rolling reduction, pearlite is uniformly dispersed in the hot-rolled steel sheet after rolling. This pearlite becomes a reverse transformation site of prior austenite during heating of hot stamping. For this reason, when pearlite is uniformly dispersed, the standard deviation of grain sizes of prior austenite grains in the hot-stamping formed body becomes small. As a result, the early fracture resistance of the hot-stamping formed body can be improved. More preferably, the final rolling reduction is 30% or more, 40% or more or 45% or more.


In the chemical composition of the hot-stamping formed body according to the present embodiment, when the Mn content is 0.60% or more, in order to preferably control the texture of the surface layer region of the hot-stamping formed body, it is important to increase the final rolling reduction of final rolling as described above.


The casting method of molten steel, the conditions of heating before hot rolling, rough rolling, coiling, and cold rolling are not particularly limited, and may be standard conditions. The coiling temperature may be set to 750° C. or lower. By setting the coiling temperature to 750° C. or lower, it is possible to suppress ferrite from being connected and arranged in the hot-rolled steel sheet after rolling, and pearlite is uniformly dispersed. This pearlite becomes a reverse transformation site of prior austenite during heating of hot stamping. For this reason, when pearlite is uniformly dispersed, the standard deviation of the grain sizes of prior austenite grains in the hot-stamping formed body becomes small. As a result, early fracture resistance of the hot-stamping formed body can be improved.


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 0.80 or more, and more preferably controlled to exceed 1.00. 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.


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 600 seconds. When the heating temperature is lower than 800° C., austenitization becomes insufficient, a desired distribution of prior austenite grain sizes cannot be obtained, and early fracture resistance may deteriorate. On the other hand, when the heating temperature is higher than 1000° C., the grains of prior austenite grow excessively, a desired distribution of prior austenite grain sizes cannot be obtained, and early fracture resistance may deteriorate. When the holding time is shorter than 60 seconds, austenitization becomes insufficient, a desired distribution of prior austenite grain sizes cannot be obtained, and early fracture resistance may deteriorate. When the holding time is longer than 600 seconds, grains of prior austenite grow excessively, a desired distribution of prior austenite grain sizes cannot be obtained, and early fracture resistance may deteriorate.


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 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 IT were heated, held in a temperature range of 1200° C. or higher for 20 minutes or longer, and then subjected to finish rolling, coiling, and annealing under conditions shown in Tables 2A to 2H. Except for some examples, annealing was performed in an oxidizing atmosphere. For examples not specifically described in the notes in the tables, 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. For some examples, as described in the tables, annealing was performed in the reducing atmosphere, and the coils after coiling were subjected to softening heat treatment.


The obtained steel sheets for hot stamping were heated to a temperature range of higher than 800° C. 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 3A to 3H were obtained. In addition, for the examples not specifically described in the notes in the tables, a gas combustion atmosphere was used in which the mixture ratio of air and fuel (air-fuel ratio) was controlled to 0.85.


However, for some examples, as described in the tables, heating in a furnace adjusted to a different atmosphere, re-annealing, plating, tempering, heating of hot stamping, or the like 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.


Measurements of the microstructure (including the standard deviation of the grain sizes of austenite grains), 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.


In addition, for examples in which early fracture resistance described below was determined as not successful, the value obtained by multiplying the Vickers hardness, which is measured by the method for early fracture resistance evaluation described below, by 3.3 (=Vickers hardness×3.3) was regarded as the tensile strength.


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.


Early Fracture Resistance

The early fracture resistance was evaluated by the value calculated by dividing the tensile strength of the hot-stamping formed body, which was obtained by the above method, by the value obtained by multiplying the Vickers hardness, which was obtained by the following method, by 3.3 (tensile strength/(Vickers hardness×3.3)). When the value was 0.60 or more, it was determined as having excellent early fracture resistance and successful, and when the value was less than 0.60, it was determined as not successful. The value obtained by multiplying the Vickers hardness by 3.3 is the tensile strength estimated from the hardness, and when the measured value of the tensile strength is 0.60 times or more of the estimated tensile strength, then it can be determined as having excellent early fracture resistance.


The Vickers hardness used for evaluation of early fracture resistance was obtained by the following method. First, from an arbitrary position 50 mm or more away from the end surface of the hot-stamping formed body, a sample was cut out so that a cross section perpendicular to the surface (sheet thickness cross section) could be observed. The size of the sample depended on the measuring device, but was set to a size that could be observed by 10 mm in the rolling direction. A cross section of the sample was polished using silicon carbide paper of #600 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. For a mirror-finished cross section, using a micro Vickers hardness tester at any position in the area between a position of 4/16 depth of the sheet thickness from the surface and a position of 5/16 depth of the sheet thickness from the surface, hardness was measured in a direction parallel to the sheet surface (rolling direction) under a load of 1 kgf at intervals of three times or more the indentations. The Vickers hardness was obtained by measuring a total of 20 points and calculating the average value.











TABLE 1A









Chemical composition (mass %) remainder being Fe and impurities




















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























A1

0.36

0.39
1.34
0.004
0.0020
0.0028
0.0019
0.0580
0.028
0.043
0.24
0.202
0.0033


A2
0.41
0.45
1.33
0.005
0.0019
0.0031
0.0019
0.0450
0.021
0.045
0.25
0.190
0.0018


A3
0.43
0.43
1.22
0.005
0.0005
0.0028
0.0025
0.0430
0.038
0.040
0.34
0.134
0.0028


A4
0.44
0.39
1.33
0.006
0.0013
0.0022
0.0017
0.0540
0.023
0.028
0.26
0.179
0.0018


A5
0.45
0.39
1.34
0.007
0.0018
0.0028
0.0029
0.0450
0.038
0.039
0.26
0.217
0.0029


A6
0.46
0.44
1.33
0.007
0.0007
0.0025
0.0029
0.0440
0.034
0.027
0.25
0.153
0.0027


A7
0.47
0.45
1.25
0.007
0.0006
0.0032
0.0031
0.0610
0.035
0.036
0.31
0.165
0.0033


A8
0.49
0.39
1.28
0.009
0.0005
0.0025
0.0033
0.0520
0.030
0.046
0.24
0.181
0.0025


A9
0.52
0.41
1.27
0.004
0.0016
0.0024
0.0015
0.0610
0.037
0.037
0.32
0.159
0.0021


A10
0.55
0.42
1.35
0.005
0.0006
0.0023
0.0016
0.0510
0.025
0.038
0.24
0.219
0.0033


A11
0.58
0.41
1.31
0.008
0.0006
0.0032
0.0026
0.0470
0.034
0.035
0.28
0.219
0.0029


A12
0.63
0.43
1.23
0.004
0.0009
0.0021
0.0025
0.0530
0.028
0.027
0.31
0.176
0.0021


A13
0.68
0.42
1.21
0.006
0.0022
0.0024
0.0022
0.0540
0.032
0.031
0.29
0.134
0.0021


A14

0.72

0.40
1.22
0.005
0.0016
0.0019
0.0023
0.0570
0.022
0.039
0.25
0.157
0.0026


B1
0.47
0.005
1.26
0.009
0.0021
0.0030
0.0024
0.0520
0.030
0.038
0.30
0.218
0.0033


B2
0.47
 0.013
1.26
0.006
0.0020
0.0026
0.0018
0.0450
0.025
0.040
0.33
0.166
0.0027


B3
0.46
0.03
1.32
0.009
0.0005
0.0022
0.0030
0.0460
0.042
0.038
0.32
0.213
0.0026


B4
0.47
0.07
1.23
0.009
0.0006
0.0020
0.0023
0.0600
0.041
0.032
0.24
0.191
0.0028


B5
0.47
0.13
1.35
0.006
0.0004
0.0031
0.0017
0.0400
0.038
0.044
0.26
0.140
0.0021


B6
0.47
0.21
1.32
0.009
0.0013
0.0025
0.0024
0.0560
0.021
0.033
0.34
0.176
0.0031


B7
0.45
0.27
1.33
0.006
0.0007
0.0030
0.0019
0.0550
0.030
0.042
0.27
0.215
0.0021


B8
0.45
0.35
1.26
0.007
0.0022
0.0032
0.0032
0.0430
0.025
0.030
0.24
0.210
0.0020


B9
0.45
0.43
1.27
0.007
0.0017
0.0029
0.0024
0.0480
0.028
0.037
0.28
0.152
0.0023


B10
0.46
0.62
1.23
0.005
0.0015
0.0031
0.0028
0.0510
0.038
0.027
0.26
0.130
0.0031


B11
0.45
0.85
1.21
0.009
0.0018
0.0021
0.0024
0.0590
0.026
0.031
0.27
0.221
0.0027


B12
0.45
1.61
1.34
0.005
0.0014
0.0030
0.0029
0.0460
0.021
0.043
0.24
0.216
0.0022


B13
0.47
2.41
1.34
0.005
0.0010
0.0031
0.0026
0.0580
0.020
0.026
0.27
0.154
0.0029


B14
0.47
2.89
1.35
0.005
0.0006
0.0022
0.0035
0.0520
0.035
0.038
0.25
0.157
0.0028


B15
0.45

3.10

1.35
0.006
0.0006
0.0031
0.0024
0.0480
0.026
0.046
0.29
0.147
0.0026





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
















TABLE 1B









Chemical composition (mass %) remainder being Fe and impurities





















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











A1
Comparative steel


A2
Steel of present invention


A3
Steel of present invention


A4
Steel of present invention


A5
Steel of present invention


A6
Steel of present invention


A7
Steel of present invention


A8
Steel of present invention


A9
Steel of present invention


A10
Steel of present invention


A11
Steel of present invention


A12
Steel of present invention


A13
Steel of present invention


A14
Comparative steel


B1
Comparative steel


B2
Steel of present invention


B3
Steel of present invention


B4
Steel of present invention


B5
Steel of present invention


B6
Steel of present invention


B7
Steel of present invention


B8
Steel of present invention


B9
Steel of present invention


B10
Steel of present invention


B11
Steel of present invention


B12
Steel of present invention


B13
Steel of present invention


B14
Steel of present invention


B15
Comparative steel


















TABLE 1C









Chemical composition (mass %) remainder being Fe and impurities.




















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























C1
0.47
0.41

0.56

0.008
0.0012
0.0030
0.0020
0.0390
0.025
0.045
0.34
0.163
0.0025


C2
0.47
0.39
0.62
0.008
0.0011
0.0023
0.0029
0.0480
0.039
0.035
0.26
0.170
0.0025


C3
0.47
0.45
0.72
0.007
0.0007
0.0028
0.0034
0.0440
0.030
0.036
0.26
0.196
0.0031


C4
0.45
0.40
0.91
0.007
0.0016
0.0026
0.0020
0.0540
0.026
0.035
0.23
0.193
0.0022


C5
0.47
0.41
1.21
0.006
0.0004
0.0030
0.0014
0.0500
0.033
0.030
0.29
0.212
0.0022


C6
0.46
0.44
1.32
0.006
0.0017
0.0019
0.0031
0.0530
0.027
0.029
0.33
0.218
0.0022


C7
0.45
0.43
1.59
0.005
0.0009
0.0033
0.0018
0.0410
0.022
0.035
0.26
0.193
0.0018


C8
0.45
0.43
1.82
0.008
0.0004
0.0025
0.0032
0.0580
0.038
0.038
0.34
0.171
0.0024


C9
0.45
0.43
2.10
0.009
0.0016
0.0025
0.0024
0.0570
0.036
0.031
0.29
0.134
0.0020


C10
0.47
0.40
2.29
0.006
0.0017
0.0032
0.0021
0.0530
0.030
0.041
0.28
0.226
0.0019


C11
0.46
0.40
2.42
0.004
0.0011
0.0030
0.0030
0.0390
0.019
0.045
0.25
0.133
0.0026


C12
0.47
0.44
2.67
0.004
0.0015
0.0026
0.0016
0.0550
0.023
0.033
0.30
0.174
0.0033


C13
0.47
0.42
2.91
0.005
0.0011
0.0032
0.0021
0.0410
0.027
0.033
0.23
0.211
0.0033


C14
0.46
0.45

3.12

0.005
0.0012
0.0020
0.0023
0.0590
0.035
0.035
0.25
0.182
0.0029


D1
0.46
0.39
1.22
 0.0007
0.0021
0.0024
0.0019
0.0500
0.039
0.029
0.32
0.133
0.0028


D2
0.45
0.45
1.33
0.004
0.0014
0.0030
0.0017
0.0420
0.040
0.025
0.27
0.144
0.0032


D3
0.45
0.45
1.32
0.007
0.0006
0.0025
0.0028
0.0400
0.026
0.039
0.33
0.175
0.0025


D4
0.47
0.43
1.27
0.009
0.0020
0.0023
0.0020
0.0520
0.034
0.042
0.32
0.217
0.0027


D5
0.47
0.45
1.29
0.013
0.0017
0.0033
0.0035
0.0510
0.030
0.037
0.33
0.142
0.0027


D6
0.46
0.40
1.33
0.041
0.0021
0.0030
0.0019
0.0500
0.025
0.042
0.33
0.211
0.0027


D7
0.47
0.45
1.24
0.068
0.0010
0.0034
0.0031
0.0410
0.020
0.037
0.24
0.161
0.0033


D8
0.47
0.39
1.35
0.089
0.0011
0.0033
0.0015
0.0530
0.040
0.032
0.27
0.229
0.0032


D9
0.45
0.42
1.24

0.130

0.0013
0.0033
0.0027
0.0500
0.033
0.029
0.27
0.159
0.0020


EL
0.46
0.43
1.27
0.008
0.0001
0.0030
0.0027
0.0450
0.039
0.035
0.30
0.208
0.0020


E2
0.46
0.41
1.35
0.009
0.0003
0.0032
0.0024
0.0540
0.020
0.037
0.28
0.142
0.0030


E3
0.47
0.43
1.24
0.009
0.0008
0.0029
0.0017
0.0570
0.039
0.031
0.30
0.214
0.0030


E4
0.46
0.45
1.34
0.004
0.0011
0.0027
0.0024
0.0560
0.035
0.041
0.26
0.148
0.0029


E5
0.45
0.40
1.27
0.007
0.0022
0.0032
0.0019
0.0610
0.023
0.027
0.26
0.195
0.0022


E6
0.46
0.42
1.21
0.005
0.0042
0.0026
0.0025
0.0470
0.039
0.032
0.24
0.215
0.0033


E7
0.47
0.41
1.31
0.008
0.0068
0.0022
0.0027
0.0570
0.036
0.031
0.31
0.224
0.0020


E8
0.46
0.39
1.26
0.005
0.0094
0.0023
0.0017
0.0410
0.038
0.045
0.32
0.217
0.0027


E9
0.47
0.45
1.32
0.004

0.0170

0.0029
0.0024
0.0550
0.037
0.040
0.25
0.144
0.0018





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
















TABLE 1D









Chemical composition (mass %) remainder being Fe and impurities





















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











C1
Comparative steel


C2
Steel of present invention


C3
Steel of present invention


C4
Steel of present invention


C5
Steel of present invention


C6
Steel of present invention


C7
Steel of present invention


C8
Steel of present invention


C9
Steel of present invention


C10
Steel of present invention


C11
Steel of present invention


C12
Steel of present invention


C13
Steel of present invention


C14
Comparative steel


D1
Steel of present invention


D2
Steel of present invention


D3
Steel of present invention


D4
Steel of present invention


D5
Steel of present invention


D6
Steel of present invention


D7
Steel of present invention


D8
Steel of present invention


D9
Comparative steel


E1
Steel of present invention


E2
Steel of present invention


E3
Steel of present invention


E4
Steel of present invention


E5
Steel of present invention


E6
Steel of present invention


E7
Steel of present invention


E8
Steel of present invention


E9
Comparative steel


















TABLE 1E









Chemical composition (mass %) remainder being Fe and impurities




















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























F1
0.47
0.39
1.25
0.006
0.0004
0.0002
0.0031
0.0450
0.035
0.042
0.31
0.130
0.0032


F2
0.47
0.39
1.21
0.004
0.0013
0.0008
0.0035
0.0430
0.024
0.042
0.34
0.188
0.0025


F3
0.45
0.44
1.21
0.004
0.0010
0.0019
0.0029
0.0420
0.039
0.031
0.27
0.209
0.0026


F4
0.47
0.39
1.31
0.006
0.0018
0.0031
0.0032
0.0560
0.032
0.033
0.26
0.157
0.0023


F5
0.45
0.41
1.27
0.009
0.0011
0.0049
0.0029
0.0540
0.040
0.034
0.30
0.161
0.0022


F6
0.46
0.45
1.34
0.006
0.0018
0.0066
0.0018
0.0540
0.033
0.029
0.28
0.161
0.0030


F7
0.46
0.44
1.26
0.004
0.0012
0.0106
0.0023
0.0600
0.026
0.039
0.26
0.174
0.0019


F8
0.45
0.45
1.31
0.006
0.0018
0.0185
0.0032
0.0540
0.033
0.034
0.28
0.161
0.0030


F9
0.45
0.39
1.30
0.007
0.0017

0.0240

0.0027
0.0560
0.032
0.035
0.26
0.228
0.0028


G1
0.47
0.45
1.32
0.009
0.0009
0.0030
0.0007
0.0410
0.039
0.036
0.25
0.179
0.0028


G2
0.46
0.41
1.28
0.004
0.0006
0.0026
0.0014
0.0510
0.027
0.026
0.34
0.229
0.0028


G3
0.47
0.45
1.23
0.004
0.0012
0.0028
0.0021
0.0470
0.031
0.034
0.27
0.154
0.0032


G4
0.47
0.42
1.32
0.006
0.0015
0.0021
0.0035
0.0520
0.033
0.033
0.25
0.139
0.0023


G5
0.45
0.43
1.24
0.008
0.0020
0.0023
0.0052
0.0590
0.029
0.028
0.30
0.187
0.0019


G6
0.45
0.44
1.28
0.004
0.0008
0.0031
0.0081
0.0410
0.041
0.026
0.28
0.228
0.0027


G7
0.46
0.40
1.22
0.009
0.0015
0.0024
0.0191
0.0610
0.023
0.030
0.33
0.160
0.0023


G8
0.46
0.43
1.28
0.004
0.0016
0.0027

0.0241

0.0590
0.037
0.035
0.30
0.201
0.0033


H1
0.47
0.44
1.31
0.006
0.0013
0.0034
0.0025

0.0008

0.028
0.034
0.26
0.157
0.0019


H2
0.47
0.45
1.27
0.009
0.0018
0.0028
0.0017
0.0014
0.025
0.040
0.32
0.181
0.0018


H3
0.47
0.40
1.34
0.006
0.0004
0.0029
0.0015
0.0052
0.027
0.045
0.23
0.200
0.0021


H4
0.46
0.43
1.35
0.006
0.0020
0.0033
0.0015
0.0161
0.025
0.034
0.32
0.228
0.0018


H5
0.47
0.41
1.29
0.006
0.0009
0.0020
0.0025
0.0252
0.029
0.030
0.26
0.206
0.0028


H6
0.46
0.39
1.24
0.004
0.0019
0.0034
0.0032
0.0392
0.033
0.027
0.23
0.165
0.0032


H7
0.46
0.43
1.35
0.005
0.0011
0.0034
0.0035
0.0491
0.029
0.045
0.29
0.212
0.0021


H8
0.46
0.42
1.34
0.008
0.0011
0.0034
0.0021
0.0689
0.032
0.035
0.34
0.196
0.0030


H9
0.46
0.42
1.33
0.009
0.0014
0.0029
0.0018
0.0812
0.032
0.036
0.23
0.171
0.0020


H10
0.47
0.45
1.26
0.005
0.0019
0.0024
0.0022
0.1277
0.037
0.041
0.29
0.136
0.0029


H11
0.46
0.39
1.34
0.006
0.0003
0.0032
0.0034
0.2655
0.040
0.039
0.29
0.221
0.0032


H12
0.45
0.40
1.23
0.008
0.0010
0.0034
0.0014
0.3691
0.036
0.028
0.29
0.196
0.0019


H13
0.46
0.40
1.23
0.008
0.0017
0.0019
0.0034
0.4915
0.020
0.032
0.24
0.167
0.0029


H14
0.46
0.44
1.32
0.004
0.0020
0.0022
0.0027

0.5214

0.038
0.042
0.30
0.146
0.0021





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
















TABLE 1F









Chemical composition (mass %) remainder being Fe and impurities





















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











F1
Steel of present invention


F2
Steel of present invention


F3
Steel of present invention


F4
Steel of present invention


F5
Steel of present invention


F6
Steel of present invention


F7
Steel of present invention


F8
Steel of present invention


F9
Comparative steel


G1
Steel of present invention


G2
Steel of present invention


G3
Steel of present invention


G4
Steel of present invention


G5
Steel of present invention


G6
Steel of present invention


G7
Steel of present invention


G8
Comparative steel


H1
Comparative steel


H2
Steel of present invention


H3
Steel of present invention


H4
Steel of present invention


H5
Steel of present invention


H6
Steel of present invention


H7
Steel of present invention


H8
Steel of present invention


H9
Steel of present invention


H10
Steel of present invention


H11
Steel of present invention


H12
Steel of present invention


H13
Steel of present invention


H14
Comparative steel


















TABLE 1G









Chemical composition (mass %) remainder being Fe and impurities




















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





I1
0.47
0.40
1.23
0.007
0.0010
0.0026
0.0035
0.0490

0.0007

0.035
0.28
0.177
0.0023


I2
0.45
0.40
1.22
0.004
0.0022
0.0029
0.0034
0.0410
0.0013
0.028
0.31
0.135
0.0033


I3
0.45
0.45
1.28
0.007
0.0006
0.0027
0.0020
0.0410
0.003
0.034
0.23
0.195
0.0031


I4
0.47
0.44
1.28
0.007
0.0017
0.0022
0.0025
0.0560
0.007
0.032
0.28
0.163
0.0029


I5
0.45
0.40
1.24
0.009
0.0010
0.0020
0.0021
0.0520
0.011
0.036
0.25
0.181
0.0031


I6
0.46
0.39
1.30
0.009
0.0005
0.0028
0.0015
0.0410
0.019
0.035
0.24
0.185
0.0025


I7
0.46
0.39
1.35
0.009
0.0012
0.0032
0.0029
0.0390
0.024
0.044
0.27
0.170
0.0023


I8
0.47
0.45
1.35
0.008
0.0017
0.0033
0.0030
0.0590
0.036
0.040
0.32
0.158
0.0026


I9
0.46
0.39
1.25
0.007
0.0016
0.0026
0.0031
0.0450
0.042
0.025
0.33
0.160
0.0023


I10
0.46
0.44
1.29
0.009
0.0003
0.0022
0.0035
0.0480
0.054
0.045
0.31
0.148
0.0021


I11
0.45
0.41
1.25
0.007
0.0022
0.0030
0.0025
0.0390
0.068
0.043
0.28
0.153
0.0030


I12
0.47
0.39
1.25
0.005
0.0019
0.0034
0.0026
0.0530
0.083
0.040
0.25
0.172
0.0021


I13
0.46
0.39
1.25
0.008
0.0007
0.0022
0.0019
0.0420
0.092
0.041
0.31
0.161
0.0030


I14
0.45
0.45
1.28
0.006
0.0015
0.0023
0.0017
0.0460

0.121

0.043
0.30
0.200
0.0029


J1
0.45
0.41
1.25
0.008
0.0013
0.0020
0.0035
0.0580
0.037

0.008

0.25
0.149
0.0021


J2
0.45
0.44
1.27
0.009
0.0010
0.0027
0.0015
0.0460
0.034
0.012
0.28
0.141
0.0031


J3
0.46
0.45
1.27
0.005
0.0011
0.0027
0.0024
0.0430
0.028
0.018
0.30
0.172
0.0028


J4
0.46
0.45
1.35
0.005
0.0021
0.0023
0.0026
0.0400
0.030
0.022
0.33
0.171
0.0029


J5
0.46
0.45
1.31
0.009
0.0004
0.0026
0.0016
0.0520
0.034
0.028
0.32
0.220
0.0028


J6
0.47
0.40
1.28
0.009
0.0017
0.0026
0.0030
0.0550
0.040
0.034
0.28
0.162
0.0028


J7
0.47
0.44
1.28
0.004
0.0016
0.0023
0.0034
0.0530
0.026
0.046
0.28
0.199
0.0030


J8
0.47
0.43
1.23
0.007
0.0010
0.0025
0.0017
0.0610
0.034
0.058
0.33
0.229
0.0022


J9
0.47
0.44
1.24
0.005
0.0012
0.0021
0.0019
0.0590
0.022
0.076
0.25
0.168
0.0028


J10
0.46
0.45
1.32
0.004
0.0015
0.0027
0.0026
0.0410
0.030
0.112
0.32
0.158
0.0028


J11
0.47
0.44
1.24
0.007
0.0012
0.0025
0.0019
0.0530
0.034
0.187
0.25
0.229
0.0028


J12
0.46
0.39
1.28
0.004
0.0003
0.0024
0.0035
0.0520
0.019

0.209

0.30
0.204
0.0030





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
















TABLE 1H









Chemical composition (mass %) remainder being Fe and impurities





















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





I1












Comparative steel


I2












Steel of present invention


I3












Steel of present invention


I4












Steel of present invention


I5












Steel of present invention


I6












Steel of present invention


I7












Steel of present invention


I8












Steel of present invention


I9












Steel of present invention


I10












Steel of present invention


I11












Steel of present invention


I12












Steel of present invention


I13












Steel of present invention


I14












Comparative steel


J1












Comparative steel


J2












Steel of present invention


J3












Steel of present invention


J4












Steel of present invention


J5












Steel of present invention


J6












Steel of present invention


J7












Steel of present invention


J8












Steel of present invention


19












Steel of present invention


J10












Steel of present invention


J11












Steel of present invention


J12












Comparative steel


















TABLE 1I









Chemical composition (mass %) remainder being Fe and impurities




















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





K1
0.45
0.43
1.29
0.008
0.0022
0.0028
0.0033
0.0480
0.031
0.031

0.009

0.139
0.0021


K2
0.47
0.41
1.27
0.005
0.0006
0.0026
0.0030
0.0480
0.021
0.043
0.013
0.193
0.0026


K3
0.47
0.41
1.25
0.006
0.0009
0.0031
0.0034
0.0610
0.021
0.037
0.051
0.150
0.0032


K4
0.45
0.39
1.31
0.007
0.0016
0.0023
0.0032
0.0510
0.025
0.026
0.087
0.196
0.0032


K5
0.47
0.45
1.25
0.005
0.0013
0.0025
0.0018
0.0460
0.037
0.027
0.12
0.205
0.0031


K6
0.45
0.41
1.35
0.005
0.0021
0.0027
0.0035
0.0420
0.029
0.036
0.18
0.219
0.0030


K7
0.45
0.43
1.30
0.007
0.0015
0.0024
0.0031
0.0540
0.025
0.025
0.23
0.215
0.0028


K8
0.47
0.42
1.22
0.008
0.0005
0.0028
0.0026
0.0440
0.029
0.032
0.27
0.211
0.0025


K9
0.46
0.45
1.22
0.006
0.0004
0.0033
0.0014
0.0580
0.021
0.046
0.34
0.194
0.0019


K10
0.47
0.43
1.28
0.004
0.0020
0.0020
0.0019
0.0440
0.018
0.027
0.43
0.173
0.0019


K11
0.46
0.41
1.35
0.005
0.0020
0.0027
0.0030
0.0500
0.031
0.026
0.61
0.178
0.0021


K12
0.47
0.44
1.26
0.008
0.0020
0.0028
0.0026
0.0530
0.020
0.034
0.77
0.159
0.0032


K13
0.47
0.41
1.31
0.004
0.0006
0.0023
0.0034
0.0400
0.032
0.034

0.84

0.214
0.0027


L1
0.45
0.44
1.29
0.004
0.0004
0.0032
0.0028
0.0500
0.027
0.045
0.27

0.0008

0.0028


L2
0.47
0.45
1.28
0.005
0.0018
0.0024
0.0026
0.0510
0.020
0.043
0.32
0.0013
0.0024


L3
0.47
0.43
1.35
0.004
0.0009
0.0028
0.0016
0.0390
0.018
0.046
0.29
0.0053
0.0024


L4
0.46
0.45
1.23
0.004
0.0013
0.0029
0.0029
0.0570
0.026
0.035
0.24
0.022
0.0018


L5
0.46
0.45
1.33
0.007
0.0021
0.0026
0.0024
0.0580
0.030
0.044
0.33
0.075
0.0033


L6
0.46
0.39
1.30
0.005
0.0015
0.0032
0.0026
0.0490
0.027
0.028
0.26
0.132
0.0031


L7
0.47
0.40
1.26
0.006
0.0010
0.0032
0.0028
0.0450
0.039
0.027
0.28
0.191
0.0025


L8
0.46
0.42
1.24
0.008
0.0015
0.0023
0.0023
0.0500
0.020
0.043
0.23
0.237
0.0019


L9
0.47
0.39
1.33
0.005
0.0017
0.0033
0.0019
0.0560
0.033
0.035
0.30
0.354
0.0018


L10
0.46
0.45
1.25
0.008
0.0011
0.0030
0.0032
0.0440
0.038
0.046
0.30
0.494
0.0022


L11
0.47
0.39
1.32
0.007
0.0010
0.0030
0.0030
0.0390
0.033
0.042
0.23
0.671
0.0021


L12
0.45
0.43
1.24
0.009
0.0015
0.0030
0.0025
0.0600
0.020
0.035
0.26
0.889
0.0022


L13
0.47
0.41
1.24
0.008
0.0017
0.0019
0.0016
0.0470
0.028
0.040
0.24

1.241

0.0033





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
















TABLE 1J









Chemical composition (mass %) remainder being Fe and impurities





















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





K1












Comparative steel


K2












Steel of present invention


K3












Steel of present invention


K4












Steel of present invention


K5












Steel of present invention


K6












Steel of present invention


K7












Steel of present invention


K8












Steel of present invention


K9












Steel of present invention


K10












Steel of present invention


K11












Steel of present invention


K12












Steel of present invention


K13












Comparative steel


L1












Comparative steel


L2












Steel of present invention


L3












Steel of present invention


L4












Steel of present invention


L5












Steel of present invention


L6












Steel of present invention


L7












Steel of present invention


L8












Steel of present invention


L9












Steel of present invention


L10












Steel of present invention


L11












Steel of present invention


L12












Steel of present invention


L13












Comparative steel


















TABLE 1K









Chemical composition (mass %) remainder being Fe and impurities




















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





M1
0.46
0.39
1.31
0.006
0.0016
0.0021
0.0033
0.0530
0.037
0.026
0.29
0.136

0.0002



M2
0.45
0.43
1.35
0.004
0.0018
0.0030
0.0033
0.0400
0.040
0.033
0.26
0.209
0.0007


M3
0.45
0.44
1.35
0.009
0.0005
0.0020
0.0025
0.0610
0.041
0.043
0.34
0.188
0.0012


M4
0.45
0.40
1.27
0.006
0.0018
0.0033
0.0025
0.0580
0.032
0.043
0.34
0.192
0.0018


M5
0.46
0.45
1.27
0.005
0.0007
0.0034
0.0016
0.0490
0.021
0.046
0.33
0.198
0.0021


M6
0.46
0.43
1.24
0.004
0.0018
0.0022
0.0026
0.0470
0.019
0.029
0.34
0.148
0.0033


M7
0.46
0.41
1.28
0.005
0.0016
0.0024
0.0019
0.0440
0.038
0.041
0.23
0.189
0.0047


M8
0.47
0.43
1.34
0.004
0.0017
0.0022
0.0022
0.0580
0.042
0.043
0.25
0.146
0.0071


M9
0.47
0.45
1.34
0.007
0.0003
0.0034
0.0033
0.0450
0.020
0.033
0.24
0.140
0.0122


M10
0.47
0.43
1.28
0.004
0.0017
0.0022
0.0019
0.0580
0.042
0.041
0.25
0.189
0.0182


M11
0.45
0.39
1.32
0.007
0.0012
0.0032
0.0033
0.0610
0.032
0.027
0.28
0.184

0.0216



N1
0.45
0.44
1.31
0.005
0.0013
0.0027
0.0018
0.0560
0.027
0.038
0.27
0.148
0.0022


N2
0.47
0.40
1.21
0.007
0.0014
0.0020
0.0026
0.0600
0.035
0.030
0.34
0.207
0.0031


N3
0.46
0.40
1.26
0.009
0.0013
0.0025
0.0023
0.0500
0.040
0.028
0.23
0.187
0.0024


N4
0.47
0.43
1.30
0.007
0.0011
0.0023
0.0017
0.0460
0.033
0.029
0.34
0.171
0.0019


N5
0.47
0.43
1.26
0.005
0.0016
0.0019
0.0029
0.0500
0.042
0.033
0.31
0.228
0.0031


N6
0.45
0.44
1.28
0.007
0.0013
0.0021
0.0021
0.0420
0.036
0.029
0.27
0.156
0.0024


N7
0.47
0.43
1.23
0.007
0.0021
0.0032
0.0031
0.0490
0.029
0.031
0.32
0.209
0.0023


N8
0.45
0.39
1.28
0.006
0.0020
0.0034
0.0035
0.0490
0.026
0.034
0.25
0.148
0.0022


N9
0.47
0.45
1.32
0.007
0.0007
0.0020
0.0020
0.0520
0.039
0.030
0.23
0.168
0.0024


N10
0.45
0.41
1.29
0.007
0.0003
0.0026
0.0017
0.0470
0.021
0.033
0.28
0.191
0.0023


N11
0.45
0.41
1.22
0.005
0.0022
0.0019
0.0027
0.0520
0.024
0.043
0.27
0.192
0.0027


N12
0.47
0.43
1.29
0.005
0.0005
0.0022
0.0017
0.0480
0.019
0.032
0.31
0.229
0.0026


N13
0.45
0.43
1.34
0.006
0.0009
0.0020
0.0031
0.0600
0.023
0.028
0.26
0.147
0.0033





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
















TABLE 1L









Chemical composition (mass %) remainder being Fe and impurities





















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





M1












Comparative steel


M2












Steel of present invention


M3












Steel of present invention


M4












Steel of present invention


M5












Steel of present invention


M6












Steel of present invention


M7












Steel of present invention


M8












Steel of present invention


M9












Steel of present invention


M10












Steel of present invention


M11












Comparative steel


N1
0.06











Steel of present invention


N2
0.11











Steel of present invention


N3
0.24











Steel of present invention


N4
0.41











Steel of present invention


N5
0.62











Steel of present invention


N6
0.87











Steel of present invention


N7
1.12











Steel of present invention


N8
1.34











Steel of present invention


N9
1.59











Steel of present invention


N10
1.71











Steel of present invention


N11
1.92











Steel of present invention


N12
2.51











Steel of present invention


N13
3.67











Steel of present invention


















TABLE 1M









Chemical composition (mass %) remainder being Fe and impurities




















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





O1
0.47
0.42
1.28
0.004
0.0018
0.0029
0.0019
0.0560
0.040
0.043
0.33
0.176
0.0020


O2
0.46
0.41
1.26
0.009
0.0009
0.0023
0.0015
0.0530
0.030
0.027
0.30
0.217
0.0023


O3
0.47
0.44
1.25
0.004
0.0011
0.0034
0.0017
0.0390
0.018
0.038
0.29
0.185
0.0024


O4
0.47
0.39
1.33
0.005
0.0011
0.0027
0.0018
0.0560
0.029
0.029
0.29
0.204
0.0029


O5
0.46
0.43
1.31
0.004
0.0022
0.0034
0.0021
0.0450
0.025
0.027
0.26
0.177
0.0027


O6
0.47
0.39
1.31
0.004
0.0004
0.0034
0.0015
0.0450
0.019
0.029
0.33
0.153
0.0026


O7
0.47
0.45
1.27
0.008
0.0016
0.0030
0.0027
0.0540
0.025
0.025
0.25
0.195
0.0024


O8
0.46
0.41
1.28
0.004
0.0019
0.0026
0.0016
0.0420
0.022
0.032
0.34
0.144
0.0022


O9
0.46
0.41
1.33
0.006
0.0006
0.0021
0.0018
0.0390
0.025
0.028
0.33
0.181
0.0028


O10
0.47
0.42
1.32
0.006
0.0012
0.0029
0.0015
0.0490
0.020
0.026
0.30
0.184
0.0031


O11
0.47
0.42
1.32
0.007
0.0010
0.0033
0.0033
0.0550
0.039
0.029
0.25
0.208
0.0021


O12
0.46
0.44
1.24
0.006
0.0015
0.0022
0.0027
0.0560
0.038
0.035
0.24
0.213
0.0022


P1
0.47
0.42
1.23
0.007
0.0013
0.0021
0.0032
0.0420
0.021
0.028
0.26
0.132
0.0027


P2
0.47
0.42
1.29
0.008
0.0016
0.0024
0.0014
0.0450
0.031
0.030
0.28
0.194
0.0020


P3
0.46
0.45
1.24
0.005
0.0007
0.0030
0.0015
0.0590
0.042
0.041
0.26
0.199
0.0021


P4
0.46
0.44
1.33
0.008
0.0012
0.0033
0.0030
0.0570
0.040
0.046
0.28
0.182
0.0019


P5
0.45
0.39
1.35
0.005
0.0013
0.0027
0.0016
0.0490
0.029
0.030
0.31
0.163
0.0031


P6
0.45
0.39
1.26
0.006
0.0019
0.0032
0.0018
0.0440
0.023
0.046
0.30
0.223
0.0025


P7
0.47
0.39
1.21
0.007
0.0005
0.0027
0.0015
0.0390
0.023
0.032
0.29
0.226
0.0024


P8
0.47
0.39
1.30
0.008
0.0021
0.0020
0.0015
0.0610
0.024
0.026
0.27
0.198
0.0019


P9
0.45
0.45
1.33
0.009
0.0014
0.0019
0.0021
0.0600
0.031
0.028
0.26
0.143
0.0022


P10
0.45
0.42
1.29
0.009
0.0008
0.0020
0.0021
0.0600
0.026
0.035
0.25
0.219
0.0032


P11
0.47
0.42
1.23
0.007
0.0007
0.0021
0.0019
0.0450
0.019
0.025
0.32
0.222
0.0020


P12
0.45
0.44
1.24
0.006
0.0003
0.0030
0.0018
0.0570
0.019
0.040
0.29
0.171
0.0028



















TABLE 1N









Chemical composition (mass %) remainder being Fe and impurities





















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





O1

0.03










Steel of present invention


O2

0.11










Steel of present invention


O3

0.26










Steel of present invention


O4

0.42










Steel of present invention


O5

0.87










Steel of present invention


O6

1.23










Steel of present invention


O7

1.65










Steel of present invention


O8

1.91










Steel of present invention


O9

2.14










Steel of present invention


O10

2.55










Steel of present invention


O11

2.77










Steel of present invention


O12

2.96










Steel of present invention


P1


0.06









Steel of present invention


P2


0.13









Steel of present invention


P3


0.25









Steel of present invention


P4


0.41









Steel of present invention


P5


0.85









Steel of present invention


P6


1.31









Steel of present invention


P7


1.61









Steel of present invention


P8


1.89









Steel of present invention


P9


2.22









Steel of present invention


P10


2.49









Steel of present invention


P11


2.71









Steel of present invention


P12


2.92









Steel of present invention


















TABLE 1O









Chemical composition (mass %) remainder being Fe and impurities




















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





Q1
0.46
0.43
1.35
0.005
0.0008
0.0030
0.0020
0.0470
0.036
0.026
0.28
0.164
0.0031


Q2
0.47
0.39
1.30
0.008
0.0019
0.0030
0.0035
0.0570
0.025
0.029
0.25
0.141
0.0032


Q3
0.46
0.39
1.33
0.004
0.0008
0.0019
0.0022
0.0390
0.037
0.036
0.26
0.201
0.0032


Q4
0.46
0.39
1.33
0.006
0.0010
0.0031
0.0028
0.0490
0.024
0.045
0.30
0.182
0.0024


Q1
0.45
0.41
1.28
0.007
0.0021
0.0025
0.0034
0.0540
0.039
0.046
0.29
0.220
0.0028


Q2
0.47
0.40
1.30
0.007
0.0013
0.0019
0.0015
0.0420
0.021
0.042
0.29
0.174
0.0032


Q3
0.46
0.42
1.34
0.008
0.0006
0.0021
0.0029
0.0430
0.035
0.043
0.34
0.170
0.0020


Q4
0.47
0.43
1.24
0.008
0.0021
0.0029
0.0029
0.0540
0.042
0.025
0.24
0.203
0.0033


Q1
0.46
0.45
1.33
0.004
0.0018
0.0022
0.0030
0.0410
0.032
0.036
0.25
0.227
0.0018


Q2
0.46
0.44
1.27
0.007
0.0006
0.0031
0.0023
0.0440
0.032
0.027
0.28
0.196
0.0019


Q3
0.47
0.44
1.29
0.009
0.0008
0.0025
0.0026
0.0450
0.034
0.025
0.30
0.171
0.0019


Q4
0.46
0.45
1.27
0.005
0.0014
0.0021
0.0033
0.0540
0.028
0.040
0.23
0.221
0.0019


R1
0.46
0.41
1.34
0.007
0.0018
0.0030
0.0033
0.0570
0.023
0.028
0.23
0.225
0.0032


R2
0.45
0.39
1.29
0.005
0.0019
0.0021
0.0033
0.0470
0.023
0.032
0.32
0.188
0.0021


R3
0.46
0.44
1.22
0.007
0.0020
0.0028
0.0028
0.0580
0.036
0.043
0.29
0.205
0.0020


R4
0.47
0.44
1.27
0.007
0.0020
0.0024
0.0034
0.0400
0.039
0.046
0.24
0.162
0.0024


R5
0.45
0.40
1.29
0.005
0.0004
0.0023
0.0019
0.0420
0.035
0.030
0.32
0.198
0.0029


R6
0.46
0.45
1.22
0.007
0.0018
0.0029
0.0021
0.0480
0.029
0.032
0.24
0.198
0.0032


R7
0.47
0.45
1.28
0.009
0.0015
0.0022
0.0024
0.0400
0.025
0.025
0.30
0.143
0.0027


R8
0.46
0.40
1.22
0.004
0.0013
0.0026
0.0033
0.0420
0.036
0.044
0.26
0.222
0.0022


R9
0.45
0.44
1.30
0.009
0.0003
0.0028
0.0024
0.0510
0.023
0.033
0.25
0.132
0.0022


R10
0.46
0.40
1.32
0.008
0.0012
0.0023
0.0018
0.0500
0.018
0.039
0.29
0.193
0.0022


R11
0.47
0.40
1.35
0.008
0.0020
0.0020
0.0018
0.0510
0.032
0.035
0.34
0.148
0.0027


R12
0.46
0.41
1.31
0.004
0.0009
0.0022
0.0020
0.0430
0.036
0.029
0.33
0.155
0.0028



















TABLE 1P









Chemical composition (mass %) remainder being Fe and impurities





















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





Q1



0.06








Steel of present invention


Q2



0.12








Steel of present invention


Q3



0.23








Steel of present invention


Q4



0.42








Steel of present invention


Q1



0.81








Steel of present invention


Q2



1.34








Steel of present invention


Q3



1.63








Steel of present invention


Q4



1.86








Steel of present invention


Q1



2.20








Steel of present invention


Q2



2.51








Steel of present invention


Q3



2.68








Steel of present invention


Q4



2.90








Steel of present invention


R1




0.07







Steel of present invention


R2




0.14







Steel of present invention


R3




0.25







Steel of present invention


R4




0.46







Steel of present invention


R5




0.84







Steel of present invention


R6




1.37







Steel of present invention


R7




1.59







Steel of present invention


R8




1.81







Steel of present invention


R9




2.23







Steel of present invention


R10




2.52







Steel of present invention


R11




2.67







Steel of present invention


R12




2.91







Steel of present invention


















TABLE 1Q









Chemical composition (mass %) remainder being Fe and impurities




















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





S1
0.47
0.40
1.26
0.007
0.0021
0.0029
0.0016
0.0510
0.023
0.044
0.26
0.164
0.0033


S2
0.46
0.41
1.25
0.008
0.0017
0.0024
0.0032
0.0470
0.041
0.033
0.26
0.206
0.0027


S3
0.46
0.39
1.25
0.005
0.0008
0.0029
0.0032
0.0460
0.028
0.045
0.32
0.156
0.0025


S4
0.47
0.40
1.30
0.004
0.0005
0.0022
0.0035
0.0600
0.019
0.043
0.23
0.195
0.0033


S5
0.47
0.43
1.23
0.006
0.0003
0.0025
0.0020
0.0450
0.033
0.036
0.27
0.154
0.0023


S6
0.46
0.41
1.30
0.008
0.0012
0.0024
0.0031
0.0570
0.022
0.038
0.33
0.165
0.0026


S7
0.45
0.41
1.34
0.009
0.0004
0.0019
0.0026
0.0440
0.023
0.039
0.29
0.213
0.0021


S8
0.46
0.42
1.34
0.006
0.0020
0.0025
0.0029
0.0470
0.025
0.033
0.33
0.135
0.0029


T1
0.46
0.40
1.29
0.005
0.0005
0.0030
0.0014
0.0420
0.026
0.029
0.27
0.186
0.0024


T2
0.46
0.45
1.27
0.008
0.0022
0.0025
0.0028
0.0590
0.037
0.039
0.34
0.205
0.0028


T3
0.45
0.44
1.32
0.008
0.0006
0.0032
0.0033
0.0460
0.033
0.026
0.25
0.140
0.0021


T4
0.46
0.45
1.32
0.006
0.0003
0.0029
0.0030
0.0430
0.019
0.040
0.27
0.193
0.0020


T5
0.47
0.39
1.27
0.008
0.0005
0.0027
0.0021
0.0400
0.029
0.037
0.32
0.220
0.0032


T6
0.47
0.44
1.31
0.004
0.0004
0.0020
0.0018
0.0470
0.041
0.032
0.29
0.168
0.0026


T7
0.47
0.41
1.22
0.004
0.0013
0.0026
0.0035
0.0580
0.028
0.031
0.26
0.212
0.0020


T8
0.45
0.41
1.34
0.004
0.0003
0.0025
0.0035
0.0550
0.025
0.035
0.23
0.187
0.0023


U1
0.47
0.43
1.34
0.008
0.0015
0.0030
0.0018
0.0560
0.040
0.032
0.26
0.160
0.0031


U2
0.47
0.44
1.23
0.008
0.0014
0.0027
0.0020
0.0450
0.022
0.029
0.31
0.135
0.0020


U3
0.45
0.41
1.28
0.005
0.0020
0.0032
0.0026
0.0580
0.025
0.037
0.34
0.146
0.0019


U4
0.45
0.45
1.27
0.008
0.0022
0.0020
0.0016
0.0430
0.029
0.045
0.23
0.154
0.0025


U5
0.45
0.41
1.27
0.007
0.0009
0.0021
0.0028
0.0440
0.024
0.046
0.26
0.141
0.0028


U6
0.46
0.41
1.22
0.004
0.0010
0.0022
0.0018
0.0540
0.027
0.025
0.26
0.194
0.0022


U7
0.46
0.44
1.23
0.007
0.0007
0.0030
0.0025
0.0550
0.021
0.030
0.30
0.172
0.0033


U8
0.46
0.39
1.29
0.005
0.0019
0.0029
0.0015
0.0560
0.030
0.025
0.33
0.215
0.0028


V1
0.47
0.40
1.24
0.008
0.0018
0.0022
0.0017
0.0520
0.018
0.025
0.33
0.221
0.0028


V2
0.46
0.40
1.31
0.008
0.0015
0.0026
0.0032
0.0430
0.040
0.046
0.26
0.141
0.0028


V3
0.45
0.39
1.22
0.005
0.0009
0.0025
0.0034
0.0390
0.038
0.035
0.26
0.131
0.0025


V4
0.46
0.39
1.26
0.006
0.0011
0.0034
0.0025
0.0470
0.020
0.026
0.24
0.217
0.0018


V5
0.46
0.42
1.23
0.007
0.0013
0.0025
0.0021
0.0610
0.021
0.034
0.34
0.131
0.0022


V6
0.47
0.44
1.24
0.007
0.0010
0.0023
0.0030
0.0580
0.041
0.030
0.31
0.156
0.0031


V7
0.45
0.43
1.31
0.007
0.0009
0.0020
0.0023
0.0570
0.033
0.033
0.25
0.147
0.0031


V8
0.45
0.41
1.33
0.006
0.0005
0.0024
0.0023
0.0590
0.034
0.045
0.30
0.134
0.0030



















TABLE 1R









Chemical composition (mass %) remainder being Fe and impurities





















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





S1





0.002






Steel of present invention


S2





0.010






Steel of present invention


S3





0.120






Steel of present invention


S4





0.290






Steel of present invention


S5





0.440






Steel of present invention


S6





0.620






Steel of present invention


S7





0.770






Steel of present invention


S8





0.920






Steel of present invention


T1






0.002





Steel of present invention


T2






0.020





Steel of present invention


T3






0.110





Steel of present invention


T4






0.280





Steel of present invention


T5






0.430





Steel of present invention


T6






0.610





Steel of present invention


T7






0.790





Steel of present invention


T8






0.930





Steel of present invention


U1







0.002




Steel of present invention


U2







0.030




Steel of present invention


U3







0.100




Steel of present invention


U4







0.270




Steel of present invention


U5







0.410




Steel of present invention


U6







0.620




Steel of present invention


U7







0.780




Steel of present invention


U8







0.920




Steel of present invention


V1








0.002



Steel of present invention


V2








0.020



Steel of present invention


V3








0.110



Steel of present invention


V4








0.290



Steel of present invention


V5








0.430



Steel of present invention


V6








0.600



Steel of present invention


V7








0.750



Steel of present invention


V8








0.910



Steel of present invention


















TABLE 1S









Chemical composition (mass %) remainder being Fe and impurities




















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





W1
0.46
0.39
1.25
0.004
0.0007
0.0022
0.0015
0.0550
0.021
0.037
0.31
0.168
0.0024


W2
0.47
0.39
1.21
0.005
0.0021
0.0021
0.0031
0.0440
0.032
0.025
0.26
0.226
0.0018


W3
0.46
0.44
1.25
0.007
0.0020
0.0034
0.0028
0.0480
0.021
0.032
0.23
0.149
0.0029


W4
0.47
0.44
1.21
0.008
0.0017
0.0023
0.0026
0.0600
0.042
0.029
0.31
0.223
0.0018


W5
0.47
0.45
1.21
0.007
0.0017
0.0022
0.0015
0.0390
0.019
0.032
0.26
0.167
0.0019


W6
0.46
0.42
1.22
0.009
0.0018
0.0033
0.0026
0.0540
0.034
0.032
0.31
0.140
0.0018


W7
0.47
0.43
1.28
0.009
0.0004
0.0021
0.0028
0.0570
0.032
0.037
0.28
0.219
0.0024


W8
0.47
0.40
1.23
0.004
0.0016
0.0031
0.0024
0.0520
0.033
0.029
0.30
0.183
0.0026


X1
0.46
0.42
1.24
0.005
0.0016
0.0034
0.0021
0.0610
0.029
0.031
0.30
0.219
0.0027


X2
0.47
0.43
1.31
0.009
0.0014
0.0028
0.0033
0.0390
0.024
0.037
0.23
0.167
0.0026


X3
0.45
0.43
1.33
0.007
0.0007
0.0020
0.0020
0.0600
0.029
0.025
0.28
0.158
0.0026


X4
0.47
0.42
1.24
0.004
0.0009
0.0031
0.0022
0.0460
0.022
0.038
0.32
0.199
0.0027


X5
0.45
0.40
1.30
0.008
0.0006
0.0023
0.0021
0.0530
0.041
0.026
0.25
0.218
0.0033


X6
0.47
0.41
1.21
0.005
0.0011
0.0024
0.0031
0.0500
0.025
0.030
0.28
0.221
0.0027


X7
0.47
0.42
1.34
0.005
0.0006
0.0029
0.0025
0.0460
0.028
0.042
0.25
0.166
0.0033


X8
0.47
0.45
1.34
0.008
0.0009
0.0020
0.0029
0.0390
0.037
0.044
0.33
0.145
0.0027


AA1
0.45
0.43
1.31
0.009
0.0007
0.0031
0.0021
0.0600
0.029
0.037
0.23
0.219
0.0026


AA2
0.45
0.40
1.24
0.007
0.0011
0.0024
0.0022
0.0500
0.041
0.038
0.25
0.199
0.0033


AA3
0.47
0.42
1.30
0.005
0.0006
0.0029
0.0031
0.0460
0.028
0.030
0.25
0.221
0.0033


Y1
0.45
0.39
1.21
0.006
0.0021
0.0030
0.0028
0.0560
0.023
0.038
0.32
0.159
0.0029


Y2
0.47
0.41
1.21
0.004
0.0022
0.0019
0.0024
0.0460
0.031
0.045
0.34
0.135
0.0024


Y3
0.47
0.39
1.28
0.004
0.0009
0.0031
0.0018
0.0580
0.035
0.043
0.31
0.223
0.0020


Y4
0.46
0.44
1.31
0.009
0.0020
0.0024
0.0018
0.0510
0.032
0.034
0.34
0.204
0.0033


Z1
0.47
0.43
0.81
0.007
0.0010
0.0019
0.0019
0.0430
0.030
0.044
0.25
0.214
0.0033


Z2
0.46
0.43
1.31
0.007
0.0003
0.0031
0.0014
0.0490
0.019
0.028
0.27
0.190
0.0021


Z3
0.45
0.43
2.04
0.005
0.0013
0.0020
0.0029
0.0460
0.040
0.029
0.29
0.161
0.0029


Z4
0.46
0.43
2.23
0.004
0.0004
0.0031
0.0033
0.0400
0.021
0.031
0.33
0.210
0.0024



















TABLE 1T









Chemical composition (mass %) remainder being Fe and impurities





















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





W1










0.002

Steel of present invention


W2










0.030

Steel of present invention


W3










0.130

Steel of present invention


W4










0.260

Steel of present invention


W5










0.410

Steel of present invention


W6










0.590

Steel of present invention


W7










0.730

Steel of present invention


W8










0.920

Steel of present invention


X1









0.002


Steel of present invention


X2









0.020


Steel of present invention


X3









0.110


Steel of present invention


X4









0.260


Steel of present invention


X5









0.420


Steel of present invention


X6









0.620


Steel of present invention


X7









0.760


Steel of present invention


X8









0.910


Steel of present invention


AA1











0.002
Steel of present invention


AA2











0.025
Steel of present invention


AA3











0.081
Steel of present invention


Y1

0.07
0.25









Steel of present invention


Y2




0.10







Steel of present invention


Y3
1.00











Steel of present invention


Y4

0.05
0.26






0.120


Steel of present invention


Z1












Steel of present invention


Z2












Steel of present invention


Z3












Steel of present invention


Z4












Steel of present invention

























TABLE 2A







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























1

A1

56
554
786
120
895
368

Comparative example


2
A2
52
554
755
127
897
358

Present invention example


3
A3
54
549
783
118
896
360

Present invention example


4
A4
56
552
762
119
909
353

Present invention example


5
A5
56
551
780
106
903
354

Present invention example


6
A6
52
546
764
105
896
365

Present invention example


7
A7
53
553
764
110
915
365

Present invention example


8
A8
54
556
787
123
896
360

Present invention example


9
A9
56
544
766
122
901
375

Present invention example


10
A10
54
544
782
105
915
365

Present invention example


11
A11
55
545
769
114
895
348

Present invention example


12
A12
53
551
758
116
898
368

Present invention example


13
A13
52
550
790
102
908
357

Present invention example


14

A14

51
543
792
127
903
364

Comparative example


15

B1

51
541
784
107
909
345

Comparative example


16
B2
54
559
793
112
902
345

Present invention example


17
B3
53
544
762
128
924
352

Present invention example


18
B4
56
554
757
100
923
367

Present invention example


19
B5
54
542
773
108
912
353

Present invention example


20
B6
55
560
772
115
911
353

Present invention example


21
B7
55
544
792
115
923
364

Present invention example


22
B8
51
552
759
101
905
351

Present invention example


23
B9
56
560
794
117
924
362

Present invention example


24
B10
55
548
774
101
924
369

Present invention example


25
B11
55
550
775
124
914
367

Present invention example


26
B12
51
547
778
111
918
359

Present invention example


27
B13
56
548
771
123
923
355

Present invention example


28
B14
54
545
792
102
910
364

Present invention example


29

B15

52
556
776
118
908
362

Comparative example


30

C1

53
545
765
104
896
372

Comparative example


31
C2
55
546
761
114
925
365

Present invention example


32
C3
52
551
771
123
900
362

Present invention example


33
C4
53
557
785
106
895
371

Present invention example


34
C5
51
556
771
116
895
354

Present invention example


35
C6
54
556
787
120
902
366

Present invention example


36
C7
53
554
768
122
902
363

Present invention example


37
C8
51
555
778
119
905
358

Present invention example


38
C9
52
551
786
127
900
367

Present invention example


39
C10
56
552
781
108
919
365

Present invention example


40
C11
56
549
761
109
898
346

Present invention example


41
C12
53
558
756
117
908
359

Present invention example


42
C13
52
552
773
113
905
364

Present invention example


43

C14

54
553
788
120
898
368

Comparative example


44
D1
56
557
761
129
920
367

Present invention example


45
D2
56
555
769
105
920
362

Present invention example


46
D3
56
555
784
107
907
355

Present invention example


47
D4
52
554
780
121
910
345

Present invention example





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






















TABLE 2B







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























48
D5
56
540
776
127
910
355

Present invention example


49
D6
52
541
782
101
896
352

Present invention example


50
D7
53
558
760
106
911
353

Present invention example


51
D8
53
550
759
124
895
359

Present invention example


52

D9

52
555
758
100
915
370

Comparative example


53
E1
53
540
787
101
904
353

Present invention example


54
E2
53
552
779
106
917
345

Present invention example


55
E3
56
549
793
120
917
364

Present invention example


56
E4
54
548
758
109
904
373

Present invention example


57
E5
51
551
779
118
895
345

Present invention example


58
E6
51
550
755
109
905
362

Present invention example


59
E7
56
559
773
126
909
362

Present invention example


60
E8
51
559
791
100
908
345

Present invention example


61

E9

53
540
783
108
904
350

Comparative example


62
F1
56
550
768
106
914
371

Present invention example


63
F2
54
549
780
112
919
374

Present invention example


64
F3
56
540
756
116
914
362

Present invention example


65
F4
53
542
787
127
907
370

Present invention example


66
F5
51
555
778
107
915
375

Present invention example


67
F6
56
555
790
127
900
371

Present invention example


68
F7
51
543
760
100
922
372

Present invention example


69
F8
51
542
778
116
900
370

Present invention example


70

F9

56
548
763
104
913
365

Comparative example


71
G1
54
555
786
123
897
357

Present invention example


72
G2
53
558
795
129
909
373

Present invention example


73
G3
53
557
789
125
914
359

Present invention example


74
G4
52
540
755
112
924
365

Present invention example


75
G5
54
555
790
101
896
357

Present invention example


76
G6
56
557
794
123
908
350

Present invention example


77
G7
54
558
788
115
910
372

Present invention example


78

G8

55
550
789
102
915
354

Comparative example


79

H1

52
549
779
121
910
369

Comparative example


80
H2
56
543
771
104
923
369

Present invention example


81
H3
55
558
788
113
911
348

Present invention example


82
H4
54
551
768
100
904
347

Present invention example


83
H5
51
548
755
119
902
363

Present invention example


84
H6
52
546
766
111
916
362

Present invention example


85
H7
55
549
760
112
903
355

Present invention example


86
H8
53
554
766
115
912
347

Present invention example


87
H9
55
555
773
119
914
370

Present invention example


88
H10
51
544
775
111
914
355

Present invention example


89
H11
51
554
791
128
911
369

Present invention example


90
H12
52
543
782
124
899
353

Present invention example


91
H13
53
556
787
111
924
362

Present invention example


92

H14

53
544
775
125
905
348

Comparative example


93

I1

55
555
763
119
916
375

Comparative example


94
I2
51
552
760
128
900
365

Present invention example





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






















TABLE 2C







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























95
I3
56
542
787
114
896
362

Present invention example


96
I4
56
542
755
129
915
363

Present invention example


97
I5
56
560
768
124
905
354

Present invention example


98
I6
51
550
757
100
900
370

Present invention example


99
I7
53
541
763
102
912
354

Present invention example


100
I8
52
551
778
120
914
360

Present invention example


101
I9
51
551
781
111
918
359

Present invention example


102
I10
56
549
771
124
907
368

Present invention example


103
I11
54
557
785
119
920
355

Present invention example


104
I12
54
548
781
108
922
351

Present invention example


105
I13
51
545
764
108
922
348

Present invention example


106

I14

55
548
769
114
899
360

Comparative example


107

J1

56
552
774
107
919
367

Comparative example


108
J2
51
552
792
111
914
357

Present invention example


109
J3
53
550
789
127
899
369

Present invention example


110
J4
55
559
784
111
910
348

Present invention example


111
J5
56
559
759
109
898
366

Present invention example


112
J6
54
545
783
112
903
374

Present invention example


113
J7
53
558
781
119
899
347

Present invention example


114
J8
52
540
791
112
900
368

Present invention example


115
J9
53
540
771
117
907
374

Present invention example


116
J10
53
546
776
121
923
373

Present invention example


117
J11
53
540
771
119
900
374

Present invention example


118

J12

54
556
790
124
911
351

Comparative example


119

K1

54
557
792
130
901
369

Comparative example


120
K2
51
546
791
117
908
371

Present invention example


121
K3
52
540
772
116
917
349

Present invention example


122
K4
53
544
785
119
907
375

Present invention example


123
K5
52
547
766
116
909
362

Present invention example


124
K6
53
545
794
111
910
364

Present invention example


125
K7
55
556
771
106
903
369

Present invention example


126
K8
56
558
765
107
900
373

Present invention example


127
K9
55
542
774
117
912
358

Present invention example


128
K10
56
542
776
125
914
373

Present invention example


129
K11
56
554
767
123
899
346

Present invention example


130
K12
54
556
774
101
907
372

Present invention example


131

K13

52
553
776
117
920
353

Comparative example


132

L1

54
555
757
130
897
368

Comparative example


133
L2
56
545
779
129
898
361

Present invention example


134
L3
54
555
775
100
915
372

Present invention example


135
L4
52
547
776
120
898
354

Present invention example


136
L5
52
545
768
127
914
357

Present invention example


137
L6
55
545
763
119
925
365

Present invention example


138
L7
53
540
792
103
911
358

Present invention example


139
L8
56
541
793
100
909
350

Present invention example


140
L9
56
541
779
125
917
375

Present invention example


141
L10
52
558
776
121
920
366

Present invention example





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






















TABLE 2D







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























142
L11
53
547
767
117
917
349

Present invention example


143
L12
53
547
783
102
908
368

Present invention example


144

L13

56
559
786
112
917
346

Present invention example


145

M1

54
550
793
118
914
351

Comparative example


146
M2
56
550
784
126
907
360

Comparative example


147
M3
51
552
785
124
922
375

Present invention example


148
M4
53
559
773
129
919
357

Present invention example


149
M5
52
559
768
111
897
361

Present invention example


150
M6
56
551
778
124
924
346

Present invention example


151
M7
55
556
788
121
924
368

Present invention example


152
M8
51
554
755
106
914
361

Present invention example


153
M9
54
551
787
120
902
364

Present invention example


154
M10
51
556
755
129
924
346

Present invention example


155

M11

56
559
772
115
921
353

Comparative example


156
N1
51
549
777
129
917
352

Present invention example


157
N2
51
544
758
128
914
364

Present invention example


158
N3
56
542
765
113
907
373

Present invention example


159
N4
51
544
761
112
911
365

Present invention example


160
N5
52
557
785
112
899
350

Present invention example


161
N6
53
543
784
123
903
353

Present invention example


162
N7
54
560
767
103
899
366

Present invention example


163
N8
53
544
785
100
896
366

Present invention example


164
N9
53
544
757
114
922
367

Present invention example


165
N10
51
557
770
106
916
355

Present invention example


166
N11
55
553
764
101
906
358

Present invention example


167
N12
52
549
785
126
904
356

Present invention example


168
N13
53
555
779
101
910
361

Present invention example


169
O1
54
550
793
111
921
370

Present invention example


170
O2
51
557
787
105
907
348

Present invention example


171
O3
52
548
783
104
925
353

Present invention example


172
O4
52
552
761
130
920
360

Present invention example


173
O5
53
554
775
130
914
353

Present invention example


174
O6
53
546
779
108
908
356

Present invention example


175
O7
51
558
782
128
897
365

Present invention example


176
O8
56
560
780
121
900
354

Present invention example


177
O9
56
545
787
109
918
372

Present invention example


178
O10
53
548
770
110
905
346

Present invention example


179
O11
53
551
766
109
907
375

Present invention example


180
O12
51
559
767
108
902
355

Present invention example


181
P1
53
546
769
125
924
366

Present invention example


182
P2
51
542
766
112
919
363

Present invention example


183
P3
52
560
764
103
915
357

Present invention example


184
P4
56
560
785
121
902
347

Present invention example


185
P5
52
545
773
104
910
367

Present invention example


186
P6
53
552
775
122
910
352

Present invention example


187
P7
52
549
780
112
897
355

Present invention example


188
P8
51
553
783
119
911
366

Present invention example





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






















TABLE 2E







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























189
P9
55
549
770
110
900
368

Present invention example


190
P10
52
548
788
108
900
356

Present invention example


191
P11
54
560
792
113
924
351

Present invention example


192
P12
53
552
775
113
910
345

Present invention example


193
Q1
51
553
787
126
910
359

Present invention example


194
Q2
54
547
795
115
904
357

Present invention example


195
Q3
56
560
795
106
897
360

Present invention example


196
Q4
54
553
766
103
917
358

Present invention example


197
Q1
52
545
794
107
919
359

Present invention example


198
Q2
55
540
763
110
917
370

Present invention example


199
Q3
54
541
759
119
923
352

Present invention example


200
Q4
53
554
774
106
910
347

Present invention example


201
Q1
53
551
776
128
925
347

Present invention example


202
Q2
54
548
773
130
905
354

Present invention example


203
Q3
53
555
761
109
925
355

Present invention example


204
Q4
53
558
759
122
913
348

Present invention example


205
R1
54
552
765
125
915
369

Present invention example


206
R2
54
555
758
114
896
354

Present invention example


207
R3
53
560
767
100
905
349

Present invention example


208
R4
53
542
775
129
917
364

Present invention example


209
RS
51
542
779
108
909
371

Present invention example


210
R6
54
545
755
100
901
356

Present invention example


211
R7
51
555
772
104
914
359

Present invention example


212
R8
56
559
758
102
897
350

Present invention example


213
R9
55
546
787
121
901
355

Present invention example


214
R10
53
547
756
121
903
347

Present invention example


215
R11
51
551
786
105
916
355

Present invention example


216
R12
53
555
765
100
924
347

Present invention example


217
S1
52
544
770
104
923
363

Present invention example


218
S2
53
551
755
101
908
375

Present invention example


219
S3
55
544
769
109
919
351

Present invention example


220
S4
54
545
793
116
907
354

Present invention example


221
S5
56
550
795
118
912
359

Present invention example


222
S6
52
549
756
102
905
363

Present invention example


223
S7
54
554
795
102
909
352

Present invention example


224
S8
53
541
791
111
912
357

Present invention example


225
T1
54
558
765
130
914
361

Present invention example


226
T2
51
552
764
112
897
371

Present invention example


227
T3
51
558
791
106
915
373

Present invention example


228
T4
56
543
775
122
909
352

Present invention example


229
T5
54
547
757
103
916
358

Present invention example


230
T6
55
543
755
107
921
372

Present invention example


231
T7
51
542
784
124
923
346

Present invention example


232
T8
51
541
790
105
898
348

Present invention example


233
U1
54
548
795
122
904
368

Present invention example


234
U2
52
546
369
128
915
357

Present invention example


235
U3
56
554
783
118
911
359

Present invention example

























TABLE 2F







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























236
U4
56
558
769
114
919
346

Present invention example


237
U5
55
545
769
101
923
358

Present invention example


238
U6
56
550
774
114
917
361

Present invention example


239
U7
54
543
789
115
923
360

Present invention example


240
U8
51
552
760
121
905
367

Present invention example


241
V1
52
556
790
128
908
374

Present invention example


242
V2
55
552
763
124
909
358

Present invention example


243
V3
54
548
771
128
903
368

Present invention example


244
V4
55
552
773
109
901
361

Present invention example


245
V5
53
553
776
105
904
349

Present invention example


246
V6
52
541
768
114
897
360

Present invention example


247
V7
54
542
757
100
906
371

Present invention example


248
V8
55
542
766
125
900
354

Present invention example


249
W1
51
544
764
101
920
370

Present invention example


250
W2
56
545
758
110
895
361

Present invention example


251
W3
56
560
771
117
912
359

Present invention example


252
W4
54
546
765
129
902
374

Present invention example


253
W5
53
542
793
128
896
360

Present invention example


254
W6
55
556
785
112
898
368

Present invention example


255
W7
51
542
767
128
900
350

Present invention example


256
W8
56
556
763
100
916
352

Present invention example


257
X1
56
553
771
104
919
353

Present invention example


258
X2
51
556
765
104
922
374

Present invention example


259
X3
51
550
770
128
919
345

Present invention example


260
X4
51
551
791
119
907
353

Present invention example


261
X5
53
550
765
108
906
349

Present invention example


262
X6
52
556
788
118
896
356

Present invention example


263
X7
56
557
779
111
917
345

Present invention example


264
X8
56
543
764
127
896
347

Present invention example


265
AA1
56
556
770
104
907
349

Present invention example


266
AA2
51
550
779
118
896
356

Present invention example


267
AA3
51
556
771
115
903
364

Present invention example


268
Y1
51
556
794
111
900
358

Present invention example


269
Y2
52
560
770
124
920
373

Present invention example


270
Y3
56
555
777
110
903
364

Present invention example


271
Y4
56
548
770
104
919
374

Present invention example


272
Z1
54
554
788
115
896
356

Present invention example


273
Z2
54
553
771
102
912
354

Present invention example


274
Z3
56
548
765
127
918
371

Present invention example


275
Z4
55
557
779
124
899
365

Present invention example


276
Z2

15

554
761
117
896
350

Comparative example


277
Z2
22
560
766
127
921
348

Present invention example


278
Z2
33
551
776
102
897
359

Present invention example


279
Z2
42
547
765
117
896
360

Present invention example


280
Z2
50
552
755
119
908
350

Present invention example


281
Z2
52
552
778
101
909
363

Present invention example


282
Z2
51
604
778
101
911
362

Present invention example





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






















TABLE 2G







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























283
Z2
56
655
781
115
903
368

Present invention example


284
Z2
56
708
783
115
905
362

Present invention example


285
Z2
53
721
793
124
919
357

Present invention example


286
Z2
55

774

777
106
907
362
Softening heat
Comparative example










treatment on coil










after coiling


287
Z2
56
 25
761
120
896
351
Softening heat
Present invention example










treatment on coil










after coiling


288
Z2
52
252
772
106
902
360
Softening heat
Present invention example










treatment on coil










after coiling


289
Z2
53
405
780
109
918
374
Softening heat
Present invention example










treatment on coil










after coiling


290
Z2
55
553
765
11
920
357

Comparative example


291
Z2
52
557
777
 16
898
349

Present invention example


292
Z2
51
543
783
 24
895
347

Present invention example


293
Z2
53
542
763
 41
909
370

Present invention example


294
Z2
52
550
782
 60
899
354

Present invention example


295
Z2
51
540
761
107
899
369

Present invention example


296
Z2
51
558
779
170
920
366

Present invention example


297
Z2
56
543
772
232
925
357

Present invention example


298
Z2
56
558
772
367
904
346

Present invention example


299
Z2
51
548
788
480
905
366

Present invention example


300
Z2
56
543
771
603
903
365

Present invention example


301
Z2
55
541
780
1213 
902
349

Present invention example


302
Z2
55
560
760
1809 
913
375

Present invention example


303
Z2
52
552

720

106
903
345

Comparative example


304
Z2
52
542
739
112
900
355

Present invention example


305
Z2
51
540
750
127
895
347

Present invention example


306
Z2
52
555
765
106
916
355

Present invention example


307
Z2
54
546
772
124
905
347

Present invention example


308
Z2
55
541
781
128
904
353

Present invention example


309
Z2
55
540
799
111
897
371

Present invention example


310
Z2
55
547
820
100
898
348

Present invention example


311
Z2
55
556
842
116
895
355

Present invention example


312
Z2
56
555
861
117
895
351

Present invention example


313
Z2
51
552
885
111
896
355

Present invention example


314
Z2
54
543

919

121
909
361

Comparative example


315
Z2
54
558
764
117
898
353
Annealing in reducing
Comparative example










atmosphere


316
Z2
52
559
767
108
905
375
Annealing in reducing
Comparative example










atmosphere


317
Z2
52
547
775
118
906
372
Re-annealing after
Present invention example










annealing in










oxidizing atmosphere


318
Z2
55
558
778
114
920
347
Aluminum plating
Present invention example


319
Z2
54
545
757
130
915
364
Aluminum galvanized
Present invention example










plating


320
Z2
52
540
787
115
896
368
Aluminum-silicon
Present invention example










plating


321
Z2
54
559
771
123
907
357
Hot-dip galvanized
Present invention example










plating


322
Z2
56
555
783
102
897
362
Electrogalvanized
Present invention example










plating


323
Z2
56
554
781
126
923
354
Galvannealed plating
Present invention example


324
Z2
53
552
756
120
899
357
Zinc-nickel plating
Present invention example


325
Z2
55
544
765
108
915
358
Aluminum-
Present invention example










magnesium-zinc










plating


326
Z2
51
560
784
127

772

366

Comparative example


327
Z2
56
557
766
130
804
364

Present invention example


328
Z2
56
550
787
120
821
361

Present invention example





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






















TABLE 2H







Final











rolling
Coiling
Annealing
Annealing
Heating
Holding


Examination

reduction
temperature
temperature
time
temperature
time


No.
Steel
%
° C.
° C.
s
° C.
s
Notes
Notes
























329
Z2
55
552
784
111
843
357

Present invention example


330
Z2
55
547
790
112
858
359

Present invention example


331
Z2
56
558
762
101
870
364

Present invention example


332
Z2
52
540
761
123
870
369

Present invention example


333
Z2
53
541
760
120
887
366

Present invention example


334
Z2
51
560
765
115
903
363

Present invention example


335
Z2
53
556
792
121
920
346

Present invention example


336
Z2
56
542
769
106
937
354

Present invention example


337
Z2
56
541
771
115
951
366

Present invention example


338
Z2
55
546
761
127
972
368

Present invention example


339
Z2
56
558
781
129
988
346

Present invention example


340
Z2
51
556
789
106

1021

364

Comparative example


341
Z2
55
559
767
104
906
53

Comparative example


342
Z2
52
543
760
117
901
 64

Present invention example


343
Z2
55
555
789
123
908
 81

Present invention example


344
Z2
55
548
765
102
916
106

Present invention example


345
Z2
51
543
758
100
908
126

Present invention example


346
Z2
56
547
767
128
895
187

Present invention example


347
Z2
55
558
780
129
898
245

Present invention example


348
Z2
56
540
774
108
919
293

Present invention example


349
Z2
56
556
773
110
919
332

Present invention example


350
Z2
54
544
760
119
903
368

Present invention example


351
Z2
51
552
766
114
924
398

Present invention example


352
Z2
53
543
773
111
913
436

Present invention example


353
Z2
53
542
770
107
895
499

Present invention example


354
Z2
51
552
781
100
910
524

Present invention example


355
Z2
51
558
787
123
899
568

Present invention example


356
Z2
53
541
780
125
909
588

Present invention example


357
Z2
56
553
792
125
905

623


Comparative example


358
Z2
54
552
781
100
897
353
Annealing in
Present invention example










gas combustion










atmosphere (air-










fuel ratio: 0.80)


359
Z2
55
549
757
113
914
363
Annealing in
Present invention example










gas combustion










atmosphere (air-










fuel ratio: 0.85)


360
Z2
56
555
761
112
909
369
Annealing in
Present invention example










gas combustion










atmosphere (air-










fuel ratio: 1.10)


361
Z2
55
560
778
129
925
375
Hot-stamping
Present invention example










heating: atmosphere










(furnace heating)


362
Z2
54
549
758
103
918
359
Hot-stamping heating:
Present invention example










nitrogen gas (dew










point of −30° C.)


363
Z2
54
545
758
118
905
361
Hot-stamping heating:
Present invention example










nitrogen gas (dew










point of 0° C.)


364
Z2
56
552
769
104
899
353
Hot-stamping heating:
Present invention example










nitrogen gas (dew










point of +10° C.)


365
Z2
51
559
786
116
906
354
Hot-stamping heating:
Present invention example










electrical heating


366
Z2
55
556
769
105
905
368
Tempering
Present invention example










temperature: 150° C.


367
Z2
51
550
764
117
896
359
Tempering
Present invention example










temperature: 170° C.


368
Z2
56
552
783
125
917
355
Tempering
Present invention example










temperature: 200° C.


369
Z2
51
543
787
111
897
352
Tempering
Present invention example










temperature: 310° C.


370
Z2
55
547
771
109
900
348
Tempering
Present invention example










temperature: 429° C.


371
Z2
54
547
761
100
911
345
Tempering
Present invention example










temperature: 513° C.


372
Z2
56
559
782
121
901
357
Tempering
Present invention example










temperature: 588° C.


373
Z2
52
554
782
125
903
348
Partial softening
Present invention example










treatment was










performed


374
Z2
51
585
785
100
900
325
Hot-stamping
Present invention example










heating atmosphere










(furnace heating)


375
Z2
52
548
790
110
897
340
Annealing in
Comparative example










reducing atmosphere,










Hot-stamping










heating atmosphere










(furnace heating)


376
Z2
53
557
840

3700

900
330

Comparative example





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



















TABLE 3A









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















1

A1

2.4
97
1.5
0.41

2171

0.98
Excellent
Comparative example


 2
A2
2.4
64
1.8
0.37
2253
0.98
Excellent
Present invention example


 3
A3
2.1
78
1.7
0.44
2352
0.94
Excellent
Present invention example


 4
A4
2.4
86
1.5
0.43
2426
0.97
Excellent
Present invention example


 5
A5
1.9
79
1.5
0.37
2475
0.97
Excellent
Present invention example


 6
A6
2.5
60
2.1
0.47
2504
0.97
Excellent
Present invention example


 7
A7
2.0
69
1.6
0.48
2525
0.95
Excellent
Present invention example


 8
A8
2.5
84
2.5
0.45
2601
0.81
Very Good
Present invention example


 9
A9
2.1
96
2.1
0.44
2702
0.84
Very Good
Present invention example


10
A10
2.2
71
2.2
0.37
2806
0.85
Very Good
Present invention example


11
A11
2.0
63
2.1
0.46
3001
0.84
Very Good
Present invention example


12
A12
2.0
64
1.7
0.45
3102
0.64
Fair
Present invention example


13
A13
2.0
90
2.1
0.38
3206
0.66
Fair
Present invention example



14


A14

2.1
94
2.0
0.48
2526

0.47

Fair
Comparative example



15


B1

1.9
63
1.8
0.49

2173

0.91
Excellent
Comparative example


16
B2
2.5
70
1.7
0.38
2255
0.99
Excellent
Present invention example


17
B3
2.1
72
2.2
0.50
2292
0.90
Excellent
Present invention example


18
B4
2.3
81
2.1
0.46
2354
0.94
Excellent
Present invention example


19
B5
2.4
60
2.1
0.37
2395
0.98
Excellent
Present invention example


20
B6
2.4
77
1.5
0.43
2421
0.96
Excellent
Present invention example


21
B7
2.2
66
2.2
0.44
2476
0.94
Excellent
Present invention example


22
B8
2.5
77
2.4
0.50
2506
0.96
Excellent
Present invention example


23
B9
2.4
64
2.1
0.38
2525
0.94
Excellent
Present invention example


24
B10
2.1
74
2.3
0.45
2544
0.93
Excellent
Present invention example


25
B11
2.4
53
1.7
0.43
2544
0.93
Very Good
Present invention example


26
B12
2.0
52
2.0
0.36
2546
0.99
Very Good
Present invention example


27
B13
2.2
25
2.3
0.37
2541
0.98
Good
Present invention example


28
B14
2.4
12
2.2
0.36
2546
0.96
Fair
Present invention example



29


B15

2.4
5
1.6
0.50
2544
0.98

Bad

Comparative example



30


C1


5.8

78
2.2
0.50
2451

0.46

Fair
Comparative example


31
C2
4.9
62
1.9
0.48
2550
0.66
Excellent
Present invention example


32
C3
3.5
90
2.4
0.49
2498
0.73
Excellent
Present invention example


33
C4
2.9
62
2.2
0.48
2423
0.82
Excellent
Present invention example


34
C5
2.5
74
2.0
0.39
2482
0.92
Excellent
Present invention example


35
C6
1.9
81
2.1
0.48
2431
0.92
Excellent
Present invention example


36
C7
2.1
73
2.5
0.46
2458
0.94
Excellent
Present invention example


37
C8
2.5
88
2.2
0.45
2424
0.99
Excellent
Present invention example


38
C9
2.2
86
2.5
0.47
2443
0.94
Excellent
Present invention example


39
C10
2.1
86
2.3
0.43
2467
0.97
Excellent
Present invention example


40
C11
2.8
77
2.5
0.41
2430
0.84
Excellent
Present invention example


41
C12
3.7
93
1.7
0.44
2425
0.72
Excellent
Present invention example


42
C13
4.9
74
2.1
0.43
2484
0.62
Excellent
Present invention example



43


C14


5.6

94
1.5
0.35
2458

0.56

Fair
Comparative example


44
D1
2.5
99
1.6
0.39
2526
0.93
Excellent
Present invention example


45
D2
1.9
82
1.8
0.42
2491
0.99
Excellent
Present invention example


46
D3
2.0
99
2.5
0.50
2416
0.91
Excellent
Present invention example


47
D4
2.0
61
2.4
0.40
2419
0.93
Excellent
Present invention example





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



















TABLE 3B









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















48
D5
2.0
68
2.4
0.44
2415
0.88
Excellent
Present invention example


49
D6
2.1
99
1.8
0.44
2501
0.76
Excellent
Present invention example


50
D7
2.4
61
2.2
0.46
2488
0.73
Excellent
Present invention example


51
D8
2.5
86
1.7
0.43
2427
0.65
Excellent
Present invention example



52


D9

2.5
82
2.4
0.47
2407

0.39

Fair
Comparative example


53
E1
2.3
75
1.8
0.46
2458
0.95
Excellent
Present invention example


54
E2
2.2
85
2.0
0.44
2452
0.98
Excellent
Present invention example


55
E3
2.2
79
2.5
0.37
2482
0.97
Excellent
Present invention example


56
E4
1.9
92
1.6
0.47
2537
0.91
Excellent
Present invention example


57
E5
2.3
61
2.4
0.35
2424
0.96
Excellent
Present invention example


58
E6
2.4
65
2.5
0.50
2510
0.80
Excellent
Present invention example


59
E7
2.4
76
2.2
0.46
2463
0.74
Excellent
Present invention example


60
E8
2.0
94
2.3
0.50
2433
0.65
Excellent
Present invention example



61


E9

2.3
62
1.8
0.43
2435

0.32

Fair
Comparative example


62
F1
2.3
91
2.3
0.44
2404
0.92
Excellent
Present invention example


63
F2
2.5
66
1.7
0.40
2492
0.90
Excellent
Present invention example


64
F3
2.0
71
2.2
0.38
2546
0.94
Excellent
Present invention example


65
F4
2.3
89
1.5
0.36
2544
0.94
Excellent
Present invention example


66
F5
2.2
62
2.5
0.37
2413
0.84
Excellent
Present invention example


67
F6
2.2
88
2.4
0.37
2437
0.71
Excellent
Present invention example


68
F7
2.4
69
2.5
0.38
2504
0.61
Excellent
Present invention example


69
F8
2.2
89
2.4
0.37
2417
0.62
Excellent
Present invention example



70


F9

1.9
60
2.3
0.44
2532

0.31

Fair
Comparative example


71
G1
2.2
80
1.6
0.48
2459
0.98
Excellent
Present invention example


72
G2
2.5
94
2.4
0.50
2473
0.97
Excellent
Present invention example


73
G3
2.4
65
2.3
0.47
2449
0.97
Excellent
Present invention example


74
G4
2.1
90
1.7
0.35
2528
0.96
Excellent
Present invention example


75
G5
2.1
81
2.1
0.44
2443
0.86
Excellent
Present invention example


76
G6
2.4
64
2.4
0.44
2414
0.72
Excellent
Present invention example


77
G7
2.3
91
2.4
0.45
2521
0.67
Excellent
Present invention example



78


G8

2.4
60
2.3
0.48
2428

0.34

Fair
Comparative example



79


H1

1.9
88
1.8
0.35
2476

0.31

Fair
Comparative example


80
H2
2.4
95
1.8
0.40
2431
0.67
Excellent
Present invention example


81
H3
2.4
91
1.5
0.38
2471
0.70
Excellent
Present invention example


82
H4
2.3
68
2.1
0.46
2449
0.86
Excellent
Present invention example


83
H5
2.2
78
2.3
0.48
2401
0.81
Excellent
Present invention example


84
H6
2.4
83
1.7
0.44
2516
0.94
Excellent
Present invention example


85
H7
2.5
85
2.2
0.40
2416
0.90
Excellent
Present invention example


86
H8
2.1
81
2.1
0.37
2474
0.91
Excellent
Present invention example


87
H9
2.5
83
1.6
0.48
2450
0.92
Excellent
Present invention example


88
H10
1.9
92
2.4
0.37
2532
0.86
Excellent
Present invention example


89
H11
1.9
73
1.8
0.43
2435
0.81
Excellent
Present invention example


90
H12
2.5
95
1.8
0.48
2550
0.65
Excellent
Present invention example


91
H13
2.2
87
1.5
0.49
2461
0.68
Excellent
Present invention example



92


H14

2.0
67
1.6
0.40
2476

0.37

Fair
Comparative example



93


I1

2.4
71
1.5
0.40
2030
0.97
Excellent
Comparative example


94
I2
2.4
93
1.8
0.49
2274
0.97
Excellent
Present invention example





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



















TABLE 3C









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















 95
I3
2.3
76
2.0
0.44
2368
0.97
Excellent
Present invention example


 96
I4
2.2
96
1.7
0.50
2330
0.99
Excellent
Present invention example


 97
I5
2.0
76
2.1
0.45
2354
0.92
Excellent
Present invention example


 98
I6
2.3
81
2.4
0.44
2488
0.97
Excellent
Present invention example


 99
I7
2.5
77
2.3
0.49
2474
0.91
Excellent
Present invention example


100
I8
2.0
93
2.5
0.47
2466
0.98
Excellent
Present invention example


101
I9
2.5
61
2.3
0.39
2431
0.95
Excellent
Present invention example


102
I10
2.1
76
1.9
0.41
2435
0.95
Excellent
Present invention example


103
I11
1.9
80
1.6
0.48
2445
0.84
Excellent
Present invention example


104
I12
2.1
92
2.3
0.48
2546
0.76
Excellent
Present invention example


105
I13
2.5
64
1.8
0.41
2441
0.69
Excellent
Present invention example



106


I14

2.5
93
1.6
0.45
2521

0.38

Fair
Comparative example



107


J1

2.5
78
1.8
0.39

1951

0.91
Excellent
Comparative example


108
J2
2.1
61
1.5
0.47
2283
0.99
Excellent
Present invention example


109
J3
1.9
91
2.4
0.47
2390
0.93
Excellent
Present invention example


110
J4
2.3
61
2.0
0.48
2381
0.91
Excellent
Present invention example


111
J5
2.2
94
1.8
0.40
2447
0.97
Excellent
Present invention example


112
J6
2.2
76
2.0
0.37
2441
0.92
Excellent
Present invention example


113
J7
2.5
92
1.7
0.45
2475
0.97
Excellent
Present invention example


114
J8
2.3
76
1.5
0.40
2478
0.88
Excellent
Present invention example


115
J9
2.3
71
1.8
0.49
2546
0.77
Excellent
Present invention example


116
J10
2.0
85
2.5
0.44
2435
0.63
Excellent
Present invention example


117
J11
2.3
76
1.7
0.40
2425
0.62
Excellent
Present invention example



118


J12

2.0
95
1.9
0.40
2528

0.53

Fair
Comparative example



119


K1

2.3
91
1.7
0.50

2034

0.95
Excellent
Comparative example


120
K2
2.5
90
2.2
0.45
2300
0.91
Excellent
Present invention example


121
K3
1.9
79
1.7
0.35
2321
0.94
Excellent
Present invention example


122
K4
2.5
67
2.5
0.40
2386
0.98
Excellent
Present invention example


123
K5
2.3
72
1.5
0.38
2356
0.91
Excellent
Present invention example


124
K6
2.2
77
2.5
0.49
2372
0.93
Excellent
Present invention example


125
K7
2.4
68
2.0
0.39
2417
0.92
Excellent
Present invention example


126
K8
2.1
64
2.3
0.45
2494
0.98
Excellent
Present invention example


127
K9
2.3
97
2.2
0.37
2518
0.93
Excellent
Present invention example


128
K10
2.0
97
2.2
0.49
2437
0.85
Excellent
Present invention example


129
K11
2.4
85
2.2
0.37
2414
0.77
Excellent
Present invention example


130
K12
2.3
62
2.1
0.39
2476
0.65
Excellent
Present invention example



131


K13

2.3
78
2.1
0.37
2529

0.39

Fair
Comparative example



132


L1

2.3
68
2.4
0.42

2009

0.97
Excellent
Comparative example


133
L2
2.2
75
2.5
0.48
2292
0.98
Excellent
Present invention example


134
L3
2.0
70
1.8
0.46
2346
0.99
Excellent
Present invention example


135
L4
2.2
73
2.3
0.41
2321
0.94
Excellent
Present invention example


136
L5
2.5
94
1.7
0.49
2356
0.94
Excellent
Present invention example


137
L6
2.1
97
1.7
0.37
2461
0.92
Excellent
Present invention example


138
L7
2.3
74
1.8
0.43
2488
0.92
Excellent
Present invention example


139
L8
2.3
67
2.2
0.43
2453
0.96
Excellent
Present invention example


140
L9
2.3
66
1.8
0.43
2486
0.99
Excellent
Present invention example


141
L10
2.5
94
2.3
0.39
2492
0.88
Excellent
Present invention example





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



















TABLE 3D









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















142
L11
1.9
98
2.3
0.40
2435
0.74
Excellent
Present invention example


143
L12
2.5
88
1.5
0.38
2545
0.67
Excellent
Present invention example



144


L13

2.0
93
1.7
0.35
2523

0.36

Fair
Comparative example



145


M1

2.0
96
1.9
0.40

2095

0.91
Excellent
Comparative example


146
M2
2.1
81
2.0
0.47
2228
0.90
Excellent
Present invention example


147
M3
2.5
77
1.9
0.49
2335
0.92
Excellent
Present invention example


148
M4
1.9
93
2.3
0.41
2547
0.92
Excellent
Present invention example


149
M5
2.3
73
2.4
0.47
2547
0.95
Excellent
Present invention example


150
M6
2.3
84
2.4
0.46
2548
0.94
Excellent
Present invention example


151
M7
2.0
96
2.2
0.38
2504
0.82
Excellent
Present invention example


152
M8
2.1
94
1.6
0.41
2547
0.74
Excellent
Present invention example


153
M9
2.2
98
1.7
0.49
2461
0.64
Excellent
Present invention example


154
M10
2.1
98
1.6
0.45
2455
0.62
Excellent
Present invention example



155


M11

1.9
64
2.2
0.50
2528

0.35

Fair
Comparative example


156
N1
2.3
80
2.5
0.41
2623
0.91
Excellent
Present invention example


157
N2
2.4
97
1.7
0.43
2704
0.95
Excellent
Present invention example


158
N3
2.3
67
1.6
0.48
2654
0.99
Excellent
Present invention example


159
N4
2.5
77
2.1
0.36
2601
0.91
Excellent
Present invention example;


160
N5
2.1
75
2.1
0.45
2676
0.95
Excellent
Present invention example


161
N6
2.5
95
2.5
0.39
2727
0.90
Excellent
Present invention example


162
N7
2.2
89
2.1
0.37
2691
0.92
Excellent
Present invention example


163
N8
2.0
97
1.6
0.44
2746
0.98
Excellent
Present invention example


164
N9
2.0
79
2.1
0.41
2853
0.91
Excellent
Present invention example


165
N10
2.0
85
1.5
0.40
2746
0.91
Excellent
Present invention example


166
N11
2.1
70
1.8
0.46
2896
0.98
Excellent
Present invention example


167
N12
2.4
86
1.5
0.50
2675
0.97
Excellent
Present invention example


168
N13
2.5
94
2.1
0.36
2646
0.97
Excellent
Present invention example


169
O1
1.9
69
2.2
0.36
2595
0.95
Excellent
Present invention example


170
O2
2.3
75
2.2
0.44
2932
0.91
Excellent
Present invention example


171
O3
2.0
63
2.3
0.44
2733
0.92
Excellent
Present invention example


172
O4
2.3
77
1.9
0.37
2552
0.92
Excellent
Present invention example


173
O5
2.3
61
1.6
0.39
2802
0.99
Excellent
Present invention example


174
O6
1.9
73
2.5
0.39
2658
0.93
Excellent
Present invention example


175
O7
2.3
71
2.5
0.49
2953
0.95
Excellent
Present invention example


176
O8
2.3
96
1.9
0.44
2948
0.98
Excellent
Present invention example


177
O9
2.2
70
2.1
0.36
2655
0.96
Excellent
Present invention example


178
O10
2.1
94
2.3
0.37
2640
0.97
Excellent
Present invention example


179
O11
2.2
77
2.2
0.42
2797
0.96
Excellent
Present invention example


180
O12
2.5
88
1.8
0.45
2692
0.97
Excellent
Present invention example


181
P1
2.0
69
1.6
0.48
2993
0.97
Excellent
Present invention example


182
P2
2.2
91
1.7
0.43
2947
0.91
Excellent
Present invention example


183
P3
2.1
98
1.9
0.36
2591
0.94
Excellent
Present invention example


184
P4
2.0
85
2.0
0.49
2768
0.96
Excellent
Present invention example


185
P5
2.0
84
2.1
0.47
2984
0.91
Excellent
Present invention example


186
P6
2.2
76
1.5
0.45
2866
0.90
Excellent
Present invention example


187
P7
2.3
62
2.0
0.50
2896
0.92
Excellent
Present invention example


188
P8
2.3
66
1.8
0.42
2922
0.98
Excellent
Present invention example





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



















TABLE 3E









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















189
P9
1.9
95
2.5
0.37
2581
0.99
Excellent
Present invention example


190
P10
2.2
64
1.9
0.45
2592
0.93
Excellent
Present invention example


191
P11
2.0
86
2.4
0.47
2578
0.91
Excellent
Present invention example


192
P12
2.4
99
1.5
0.44
2730
0.98
Excellent
Present invention example


193
Q1
1.9
96
2.1
0.49
2863
0.94
Excellent
Present invention example


194
Q2
2.5
81
2.2
0.35
2860
0.96
Excellent
Present invention example


195
Q3
1.9
78
1.7
0.47
2800
0.95
Excellent
Present invention example


196
Q4
2.2
64
1.9
0.45
2915
0.96
Excellent
Present invention example


197
Q1
1.9
64
1.5
0.43
2598
0.99
Excellent
Present invention example


198
Q2
2.1
91
2.3
0.49
2558
0.97
Excellent
Present invention example


199
Q3
2.0
62
2.0
0.47
2853
0.94
Excellent
Present invention example


200
Q4
2.4
82
1.6
0.35
2958
0.93
Excellent
Present invention example


201
Q1
1.9
90
1.9
0.42
2971
0.91
Excellent
Present invention example


202
Q2
2.0
85
1.8
0.37
2659
0.94
Excellent
Present invention example


203
Q3
2.5
83
1.6
0.37
2569
0.99
Excellent
Present invention example


204
Q4
2.1
64
2.2
0.37
2720
0.95
Excellent
Present invention example


205
R1
2.1
92
1.6
0.35
2804
0.93
Excellent
Present invention example


206
R2
1.9
80
2.5
0.41
2985
0.99
Excellent
Present invention example


207
R3
1.9
67
1.5
0.41
2708
0.92
Excellent
Present invention example


208
R4
2.2
76
2.2
0.36
2905
0.99
Excellent
Present invention example


209
R5
2.1
85
1.8
0.45
2799
0.90
Excellent
Present invention example


210
R6
2.2
98
2.0
0.36
2962
0.92
Excellent
Present invention example


211
R7
2.4
73
2.2
0.38
2787
0.92
Excellent
Present invention example


212
R8
2.0
73
1.9
0.41
2734
0.94
Excellent
Present invention example


213
R9
2.5
88
1.6
0.37
2887
0.94
Excellent
Present invention example


214
R10
2.0
71
2.5
0.49
2936
0.90
Excellent
Present invention example


215
R11
2.2
87
1.5
0.40
2920
0.95
Excellent
Present invention example


216
R12
2.0
80
1.8
0.47
2709
0.95
Excellent
Present invention example


217
S1
2.3
67
2.5
0.36
2469
0.94
Excellent
Present invention example


218
S2
2.0
68
2.2
0.48
2542
0.90
Excellent
Present invention example


219
S3
2.3
72
2.4
0.39
2528
0.90
Excellent
Present invention example


220
S4
2.4
94
1.9
0.41
2529
0.95
Excellent
Present invention example


221
S5
1.9
60
1.9
0.42
2469
0.98
Excellent
Present invention example


222
S6
1.9
77
2.3
0.50
2513
0.97
Excellent
Present invention example


223
S7
2.2
92
1.6
0.45
2407
0.99
Excellent
Present invention example


224
S8
2.5
75
2.2
0.40
2550
0.99
Excellent
Present invention example


225
T1
2.3
77
2.1
0.39
2502
0.95
Excellent
Present invention example


226
T2
2.5
70
1.9
0.39
2447
0.93
Excellent
Present invention example


227
T3
2.3
75
2.0
0.41
2481
0.98
Excellent
Present invention example


228
T4
2.4
88
1.5
0.44
2523
0.91
Excellent
Present invention example


229
T5
1.9
97
1.8
0.42
2433
0.98
Excellent
Present invention example


230
T6
1.9
63
1.9
0.38
2475
0.96
Excellent
Present invention example


231
T7
2.2
80
1.7
0.38
2410
0.93
Excellent
Present invention example


232
T8
2.2
79
2.5
0.39
2531
0.93
Excellent
Present invention example


233
U1
2.5
68
2.3
0.41
2412
0.94
Excellent
Present invention example


234
U2
2.3
67
1.5
0.40
2465
0.98
Excellent
Present invention example


235
U3
2.5
93
2.4
0.45
2536
0.96
Excellent
Present invention example






















TABLE 3F









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















236
U4
2.5
83
2.4
0.41
2424
0.98
Excellent
Present invention example


237
U5
2.4
88
1.7
0.36
2499
0.95
Excellent
Present invention example


238
U6
2.5
69
2.3
0.38
2503
0.99
Excellent
Present invention example


239
U7
2.4
78
2.4
0.42
2415
0.97
Excellent
Present invention example


240
U8
1.9
60
2.0
0.43
2454
0.92
Excellent
Present invention example


241
V1
2.0
84
1.8
0.47
2515
0.97
Excellent
Present invention example


242
V2
2.4
78
1.6
0.40
2478
0.93
Excellent
Present invention example


243
V3
2.0
64
2.4
0.41
2521
0.96
Excellent
Present invention example


244
V4
2.4
73
2.4
0.47
2548
0.96
Excellent
Present invention example


245
V5
2.4
78
2.5
0.47
2423
0.93
Excellent
Present invention example


246
V6
2.3
87
2.2
0.44
2520
0.98
Excellent
Present invention example


247
V7
2.2
94
1.5
0.42
2531
0.93
Excellent
Present invention example


248
V8
2.3
80
2.5
0.39
2514
0.99
Excellent
Present invention example


249
W1
2.0
73
2.4
0.39
2444
0.99
Excellent
Present invention example


250
W2
2.3
83
1.6
0.44
2403
0.92
Excellent
Present invention example


251
W3
2.1
72
1.8
0.47
2514
0.91
Excellent
Present invention example


252
W4
2.5
89
1.6
0.39
2496
0.99
Excellent
Present invention example


253
W5
1.9
87
1.3
0.37
2498
0.95
Excellent
Present invention example


254
W6
2.5
64
2.2
0.37
2437
0.94
Excellent
Present invention example


255
W7
2.0
85
1.6
0.48
2412
0.96
Excellent
Present invention example


256
W8
2.4
69
1.8
0.39
2453
0.92
Excellent
Present invention example


257
X1
2.0
93
2.1
0.50
2460
0.95
Excellent
Present invention example


258
X2
2.1
69
1.8
0.38
2543
0.93
Excellent
Present invention example


259
X3
2.4
96
1.9
0.38
2531
0.90
Excellent
Present invention example


260
X4
2.5
69
1.6
0.48
2524
0.93
Excellent
Present invention example


261
X5
1.9
80
2.5
0.47
2464
0.97
Excellent
Present invention example


262
X6
2.0
92
2.0
0.43
2480
0.90
Excellent
Present invention example


263
X7
2.1
71
1.7
0.43
2500
0.93
Excellent
Present invention example


264
X8
2.3
79
1.8
0.35
2444
0.90
Excellent
Present invention example


265
AA1
2.1
72
2.1
0.44
2489
0.90
Excellent
Present invention example


266
AA2
2.2
79
1.8
0.43
2502
0.90
Excellent
Present invention example


267
AA3
2.3
79
1.8
0.38
2448
0.93
Excellent
Present invention example


268
Y1
1.9
70
1.6
0.39
2436
0.97
Excellent
Present invention example


269
Y2
2.2
82
2.0
0.48
2446
0.97
Excellent
Present invention example


270
Y3
2.4
64
1.9
0.47
2436
0.99
Excellent
Present invention example


271
Y4
2.4
78
2.2
0.47
2536
0.94
Excellent
Present invention example


272
Z1
2.3
78
2.5
0.37
2540
0.99
Excellent
Present invention example


273
Z2
2.1
74
1.6
0.37
2423
0.93
Excellent
Present invention example


274
Z3
2.5
97
2.1
0.40
2544
0.97
Excellent
Present invention example


275
Z4
2.0
77
2.0
0.43
2449
0.96
Excellent
Present invention example



276

Z2

5.6

90

4.2

0.35
2524

0.40


Bad

Comparative example


277
Z2
2.3
69
2.0
0.46
2427
0.61
Excellent
Present invention example


278
Z2
2.3
78
2.2
0.43
2418
0.70
Excellent
Present invention example


279
Z2
2.4
74
2.1
0.42
2526
0.87
Excellent
Present invention example


280
Z2
2.4
86
1.6
0.40
2434
0.90
Excellent
Present invention example


281
Z2
2.5
65
1.7
0.35
2496
0.96
Excellent
Present invention example


282
Z2
2.0
93
1.7
0.36
2444
0.91
Excellent
Present invention example





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



















TABLE 3G









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















283
Z2
2.5
68
2.5
0.42
2479
0.84
Excellent
Present invention example


284
Z2
2.5
66
2.4
0.41
2453
0.75
Excellent
Present invention example


285
Z2
2.1
73
2.1
0.45
2438
0.67
Excellent
Present invention example



286

Z2

5.5

73
2.2
0.47
2463

0.33

Fair
Comparative example


287
Z2
2.4
91
1.9
0.35
2484
0.91
Excellent
Present invention example


288
Z2
2.0
80
1.7
0.39
2468
0.97
Excellent
Present invention example


289
Z2
2.1
67
2.5
0.48
2525
0.93
Excellent
Present invention example



290

Z2
2.0
3

4.9


0.03

2532
0.97

Bad

Comparative example


291
Z2
2.2
15
3.7
0.12
2440
0.99
Fair
Present invention example


292
Z2
2.2
28
3.2
0.23
2545
0.98
Good
Present invention example


293
Z2
2.5
46
2.7
0.34
2463
0.99
Very Good
Present invention example


294
Z2
2.0
94
2.5
0.50
2529
0.94
Excellent
Present invention example


295
Z2
2.3
86
1.6
0.42
2450
0.93
Excellent
Present invention example


296
Z2
2.4
97
1.6
0.42
2413
0.93
Excellent
Present invention example


297
Z2
2.4
74
2.3
0.41
2447
0.96
Excellent
Present invention example


298
Z2
2.4
79
2.2
0.40
2430
0.96
Excellent
Present invention example


299
Z2
2.0
90
2.0
0.36
2415
0.96
Excellent
Present invention example


300
Z2
2.5
92
2.5
0.42
2543
0.92
Excellent
Present invention example


301
Z2
2.4
98
2.5
0.45
2404
0.91
Excellent
Present invention example


302
Z2
2.3
98
2.4
0.44
2502
0.99
Excellent
Present invention example



303

Z2
2.1
7

5.1


0.02

2521
0.92

Bad

Comparative example


304
Z2
2.4
11
3.3
0.07
2504
0.90
Fair
Present invention example


305
Z2
2.0
30
3.4
0.22
2463
0.96
Good
Present invention example


306
Z2
2.0
53
2.7
0.30
2438
0.92
Very Good
Present invention example


307
Z2
2.1
94
1.7
0.47
2519
0.97
Excellent
Present invention example


308
Z2
2.3
93
2.4
0.42
2535
0.93
Excellent
Present invention example


309
Z2
2.2
60
2.2
0.43
2471
0.97
Excellent
Present invention example


310
Z2
2.3
62
1.7
0.45
2431
0.99
Excellent
Present invention example


311
Z2
1.9
53
2.9
0.32
2441
0.97
Very Good
Present invention example


312
Z2
2.1
22
3.5
0.24
2434
0.91
Good
Present invention example


313
Z2
2.0
11
3.6
0.09
2527
0.99
Fair
Present invention example



314

Z2
2.4
3

4.6


0.01

2428
0.92

Bad

Comparative example



315

Z2
2.4
5

5.1


0.02

2448
0.91

Bad

Comparative example



316

Z2
2.3
3

4.4


0.02

2446
0.99

Bad

Comparative example


317
Z2
1.9
64
1.9
0.42
2544
0.99
Excellent
Present invention example


318
Z2
2.2
81
1.9
0.44
2498
0.95
Excellent
Present invention example


319
Z2
2.0
97
1.7
0.44
2505
0.96
Excellent
Present invention example


320
Z2
2.0
78
2.5
0.38
2478
0.94
Excellent
Present invention example


321
Z2
2.2
75
1.9
0.43
2535
0.94
Excellent
Present invention example


322
Z2
2.1
76
2.5
0.46
2507
0.98
Excellent
Present invention example


323
Z2
2.0
88
1.7
0.39
2534
0.94
Excellent
Present invention example


324
Z2
2.4
90
1.5
0.50
2537
0.90
Excellent
Present invention example


325
Z2
2.5
69
2.2
0.35
2473
0.99
Excellent
Present invention example



326

Z2

5.4

82
2.1
0.43
2422

0.36

Fair
Comparative example


327
Z2
1.9
67
2.1
0.36
2481
0.94
Excellent
Present invention example


328
Z2
2.0
79
1.5
0.41
2522
0.90
Excellent
Present invention example


329
Z2
2.5
89
2.2
0.38
2496
0.95
Excellent
Present invention example





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



















TABLE 3H









Interior region







Standard
Surface layer region


















deviation of

Maximum value


Evaluation
Evaluation





grain sizes of

of pole density
Deboronization
Tensile
of early
of hydrogen


Examination

prior γ grains
Bainite
of texture
index
strength
fracture
embrittlement


No.
Steel
μm
area %


MPa
resistance
resistance
Notes



















330
Z2
2.3
89
2.3
0.41
2486
0.92
Excellent
Present invention example


331
Z2
2.4
84
2.3
0.48
2523
0.98
Excellent
Present invention example


332
Z2
2.3
99
1.6
0.47
2545
0.90
Excellent
Present invention example


333
Z2
2.5
64
1.7
0.49
2439
0.99
Excellent
Present invention example


334
Z2
2.1
95
1.7
0.41
2453
0.94
Excellent
Present invention example


335
Z2
2.2
71
2.2
0.39
2515
0.92
Excellent
Present invention example


336
Z2
3.0
65
2.0
0.46
2421
0.83
Excellent
Present invention example


337
Z2
2.7
67
2.1
0.37
2460
0.80
Excellent
Present invention example


338
Z2
3.9
61
2.0
0.48
2405
0.79
Excellent
Present invention example


339
Z2
4.6
86
1.5
0.37
2518
0.69
Excellent
Present invention example



340

Z2

5.6

69
1.6
0.42
2493

0.39

Fair
Comparative example



341

Z2

5.8

91
2.4
0.42
2484

0.58

Fair
Comparative example


342
Z2
4.8
74
2.2
0.44
2530
0.63
Excellent
Present invention example


343
Z2
3.7
89
1.8
0.42
2442
0.73
Excellent
Present invention example


344
Z2
3.0
79
2.2
0.50
2437
0.88
Excellent
Present invention example


345
Z2
2.1
66
1.5
0.50
2445
0.99
Excellent
Present invention example


346
Z2
2.0
77
1.7
0.37
2462
0.92
Excellent
Present invention example


347
Z2
1.9
88
1.8
0.36
2422
0.92
Excellent
Present invention example


348
Z2
2.0
61
1.9
0.49
2549
0.92
Excellent
Present invention example


349
Z2
2.4
73
2.3
0.48
2507
0.94
Excellent
Present invention example


350
Z2
1.9
99
2.0
0.40
2517
0.92
Excellent
Present invention example


351
Z2
1.9
73
2.5
0.38
2437
0.96
Excellent
Present invention example


352
Z2
2.2
77
1.7
0.43
2449
0.98
Excellent
Present invention example


353
Z2
1.9
80
2.2
0.49
2489
0.95
Excellent
Present invention example


354
Z2
3.0
99
2.5
0.50
2430
0.86
Excellent
Present invention example


355
Z2
3.2
67
1.8
0.50
2476
0.71
Excellent
Present invention example


356
Z2
4.4
68
2.3
0.43
2462
0.61
Excellent
Present invention example



357

Z2

5.3

74
1.7
0.35
2451

0.39

Fair
Comparative example


358
Z2
2.1
97
1.8
0.37
2469
0.95
Excellent
Present invention example


359
Z2
2.1
76
1.8
0.38
2437
0.95
Excellent
Present invention example


360
Z2
2.2
66
1.9
0.46
2411
0.99
Excellent
Present invention example


361
Z2
2.1
82
1.9
0.38
2433
0.99
Excellent
Present invention example


362
Z2
2.3
88
2.3
0.35
2451
0.92
Excellent
Present invention example


363
Z2
2.3
82
1.5
0.39
2424
0.92
Excellent
Present invention example


364
Z2
2.2
66
1.8
0.46
2403
0.97
Excellent
Present invention example


365
Z2
2.5
74
2.5
0.41
2518
0.97
Excellent
Present invention example


366
Z2
2.1
94
2.1
0.37
2425
0.98
Excellent
Present invention example


367
Z2
2.3
74
1.8
0.48
2423
0.96
Excellent
Present invention example


368
Z2
2.4
75
1.8
0.44
2398
0.98
Excellent
Present invention example


369
Z2
2.3
65
1.8
0.43
2319
0.93
Excellent
Present invention example


370
Z2
2.5
69
1.8
0.39
2207
0.96
Excellent
Present invention example


371
Z2
2.1
74
1.7
0.41
2274
0.95
Excellent
Present invention example;


372
Z2
2.2
73
2.5
0.36
2233
0.99
Excellent
Present invention example


373
Z2
2.5
93
2.5
0.45
2424
0.93
Excellent
Present invention example


374
Z2
2.4
78
1.5
0.43
2398
0.91
Excellent
Present invention example



375

Z2
2.3
76

4.2


0.02

2481
0.90

Bad

Comparative example



376

Z2
2.6
74
2.8

0.03

2467
0.92

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 3A to 3H, it can be seen that the hot-stamping formed bodies according to the present invention examples had high strength and excellent hydrogen embrittlement resistance and early fracture 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 and early fracture 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 3.00%;Mn: 0.60% to 3.00%;P: 0.100% or less;S: 0.0100% or less;N: 0.0200% or less;O: 0.0200% or less;Al: 0.0010% to 0.5000%;Nb: 0.0010% to 0.100%;Ti: 0.010% to 0.200%;Cr: 0.01% to 0.80%;Mo: 0.0010% to 1.000%;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 1.000%;Mg: 0% to 1.000%;REM: 0% to 1.000%;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 an interior region, which is a region between 4/16 depth of a sheet thickness from a surface of the hot-stamping formed body and 5/16 depth of the sheet thickness from the surface,a standard deviation of grain sizes of prior austenite grains is 5.0 μm or less,in a surface layer region, which is a region between the surface and 1/25 depth of the 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: 0.001% to 1.000%;Mg: 0.001% to 1.000%;REM: 0.001% to 1.000%;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
2022-067020 Apr 2022 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2023/007855 3/2/2023 WO