HOT STAMPED COMPONENT

Abstract
This hot stamped component has a predetermined chemical composition, in a position at ¼ of a sheet thickness from a surface, in a texture of prior austenite, a maximum value of pole densities of an orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=45° is 3.0 or more, an average value of block sizes of martensite, tempered martensite and bainite is 1.20 μm or less.
Description
TECHNICAL FIELD OF INVENTION

The present invention relates to a hot stamped component.


Priority is claimed on Japanese Patent Application No. 2022-090847, filed Jun. 3, 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 from the perspective 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 a hardenable steel having excellent cold formability that can obtain excellent impact strength and hardness by reheating and quenching the steel.


PRIOR ART DOCUMENT
Patent Document
Patent Document 1



  • Japanese Unexamined Patent Application Publication No. 2020-508393



Non-Patent Document
Non-Patent Document 1



  • Acta Materialia, 58 (2010), 6393-6403



DISCLOSURE OF INVENTION
Problems to be Solved by Invention

When a hot stamped component with further improved tensile strength is used as a vehicle member, a greater effect of vehicle weight reduction can be achieved. However, since it is a vehicle member, it may be subjected to bending deformation due to a collision or the like, and therefore the hot stamped component needs to have high bendability. However, Patent Document 1 does not consider bendability.


The present invention has been made in view of the above-mentioned problem, and an object of the present invention is to provide a hot stamped component having high strength and excellent bendability.


Means for Solving the Problem

The gist of the present invention is as follows.


[1]A hot stamped component according to an aspect of the present invention comprising, as a chemical composition, by mass %:

    • C: 0.40% to 0.70%;
    • Si: 0.010% to 3.000%;
    • Mn: 0.10% or more and less than 0.60%;
    • P: 0.100% or less;
    • S: 0.0100% or less;
    • N: 0.0100% or less;
    • O: 0.0200% or less;
    • Al: 0.0010% to 0.5000%;
    • Nb: 0.0010% to 0.1000%;
    • Ti: 0.010% to 0.100%;
    • Cr: 0.010% to 1.000%;
    • Mo: 0.050% to 1.000%;
    • B: 0.0005% to 0.0100%;
    • Co: 0% to 3.00%;
    • Ni: 0% to 3.00%;
    • Cu: 0% to 3.00%;
    • V: 0% to 3.00%;
    • W: 0% to 3.00%;
    • Ca: 0% to 0.1000%;
    • Mg: 0% to 1.0000%;
    • REM: 0% to 1.0000%;
    • Sb: 0% to 1.000%;
    • Sn: 0% to 1.000%;
    • Zr: 0% to 1.000%;
    • As: 0% to 0.100%; and
    • a remainder: Fe and impurities,
    • in a position at ¼ of a sheet thickness from a surface,
    • in a texture of prior austenite, a maximum value of pole densities of an orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=45° is 3.0 or more,
    • an average value of block sizes of martensite, tempered martensite and bainite is 1.20 μm or less.


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

    • Co: 0.01% to 3.00%;
    • Ni: 0.01% to 3.00%;
    • Cu: 0.01% to 3.00%;
    • V: 0.01% to 3.00%;
    • W: 0.01% to 3.00%;
    • Ca: 0.0001% to 0.1000%;
    • Mg: 0.0001% to 1.0000%;
    • REM: 0.0001% to 1.0000%;
    • Sb: 0.001% to 1.000%;
    • Sn: 0.001% to 1.000%;
    • Zr: 0.001% to 1.000%; and
    • As: 0.001% to 0.100%.


Effects of Invention

According to the above-described aspects of the present invention, it is possible to provide a hot stamped component having high strength and excellent bendability.


EMBODIMENTS OF INVENTION

The present inventors found that by controlling a texture of prior austenite and an average value of block sizes of martensite, tempered martensite and bainite in a position at ¼ of a sheet thickness from a surface of a hot stamped component, the bendability of the hot stamped component can be improved. In particularly, the present inventors found that the bendability of a hot stamped component can be improved by controlling not a texture of martensite, tempered martensite, bainite, or the like, which are a microstructure of the hot stamped component but a texture of prior austenite before transformation to martensite, bainite, or the like (i.e., state of austenite at a high temperature of Ar3 point or higher) to be within a specific range.


In addition, the present inventors found that in order to obtain the hot stamped component having the above features, it is particularly effective to strictly control final rolling conditions during hot rolling.


Hereinafter, the hot stamped component according to the present embodiment will be described in detail. First, the reason the chemical composition of the hot stamped component 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 component according to the present embodiment comprises, as a chemical composition, by mass %, C: 0.40% to 0.70%, Si: 0.010% to 3.000%, Mn: 0.10% or more and less than 0.60%, P: 0.100% or less, S: 0.0100% or less, N: 0.0100% or less, O: 0.0200% or less, Al: 0.0010% to 0.5000%, Nb: 0.0010% to 0.1000%, Ti: 0.010% to 0.100%, Cr: 0.010% to 1.000%, Mo: 0.050% to 1.000%, B: 0.0005% to 0.0100%, and a remainder: Fe and impurities.


Each element will be described below.


C: 0.40% to 0.70%

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


On the other hand, when the C content is more than 0.70%, the strength excessively increases and the bendability of the hot stamped component deteriorates. For this reason, the C content is set to 0.70% or less. The C content is preferably 0.65% or less or 0.60% or less.


Si: 0.010% to 3.000%

Si is an element that improves the strength of the hot stamped component by solid-solution strengthening. When the Si content is less than 0.010%, a desired strength of the hot stamped component cannot be obtained. For this reason, the Si content is set to 0.010% or more. The Si content is preferably 0.100% or more, 0.300% or more or 0.500% or more.


On the other hand, when the Si content is more than 3.000%, the amount of ferrite increases and a desired strength of the hot stamped component cannot be obtained. For this reason, the Si content is set to 3.000% or less. The Si content is preferably 2.000% or less, 1.000% or less or 0.800% or less.


Mn: 0.10% or More and Less than 0.60%


Mn is an element that increases hardenability of steel and increases the strength of the hot stamped component. When the Mn content is less than 0.10%, a desired strength of the hot stamped component cannot be obtained. For this reason, the Mn content is set to 0.10% or more. The Mn content is preferably 0.20% or more or 0.35% or more.


On the other hand, when the Mn content is 0.60% or more, a desired texture of prior austenite cannot be obtained. For this reason, the Mn content is set to less than 0.60%. The Mn content is preferably 0.55% or less or 0.50% or less.


P: 0.100% or Less

P decreases the strength of the grain boundaries by segregating in the grain boundaries. As a result, P deteriorates the bendability of the hot stamped component. When the P content is more than 0.100%, the bendability of the hot stamped component deteriorates significantly. 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 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.


S: 0.0100% or Less

S forms inclusions in steel. When the S content is more than 0.0100%, the bendability of the hot stamped component deteriorates significantly. 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 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.


N: 0.0100% or Less

N forms nitrides in steel. When the N content is more than 0.0100%, the bendability of the hot stamped component deteriorates significantly. For this reason, the N content is set to 0.0100% or less. The N content is preferably 0.0080% or less, 0.0060% or less or 0.0040% or less.


The lower limit of the N content 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.


O: 0.0200% or Less

O forms coarse oxides when a large amount of O is comprised in steel. When the O content is more than 0.0200%, the bendability of the hot stamped component deteriorates significantly. 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, 0.0040% or less or 0.0030% or less.


The O content may be 0%. However, in order to disperse many oxides during deoxidizing of molten steel, the O content may be set to 0.0005% 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 (minimizing the occurrence of defects such as blowholes in steel). When the Al content is less than 0.0010%, deoxidation is not sufficiently performed, and coarse oxides are generated. As a result, the bendability of the hot stamped component 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.


On the other hand, when the Al content is more than 0.5000%, coarse oxides are generated in steel. As a result, the bendability of the hot stamped component deteriorates significantly. For this reason, the Al content is set to 0.5000% or less. The Al content is preferably 0.4000% or less, 0.3000% or less, or 0.2000% or less or 0.1000% or less.


Nb: 0.0010% to 0.1000%

Nb is an element that forms carbonitrides in steel and improves the strength of the hot stamped component by precipitation strengthening. When the Nb content is less than 0.0010%, a desired strength of the hot stamped component cannot be obtained. For this reason, the Nb content is set to 0.0010% or more. The Nb content is preferably 0.0050% or more, 0.0100% or more or 0.0200% or more.


On the other hand, when the Nb content is more than 0.1000%, many carbonitrides are generated in steel, and the bendability of the hot stamped component deteriorates. For this reason, the Nb content is set to 0.1000% or less. The Nb content is preferably 0.0800% or less or 0.0600% or less.


Ti: 0.010% to 0.100%

Ti is an element that forms carbonitrides in steel and improves the strength of the hot stamped component by precipitation strengthening. When the Ti content is less than 0.010%, a desired strength of the hot stamped component 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.


On the other hand, when the Ti content is more than 0.100%, many carbonitrides are generated in steel, and the bendability of the hot stamped component deteriorates. For this reason, the Ti content is set to 0.100% or less. The Ti content is preferably 0.080% or less, 0.060% or less or 0.050% or less.


Cr: 0.010% to 1.000%

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


On the other hand, when the Cr content is more than 1.000%, a desired texture of prior austenite cannot be obtained. For this reason, the Cr content is set to 1.000% or less. The Cr content is preferably 0.700% or less, 0.500% or less or 0.400% or less.


Mo: 0.050% to 1.000%

Mo is an element that increases the strength of the hot stamped component by dissolving in prior austenite grains during heating before hot stamping. When the Mo content is less than 0.050%, a desired strength of the hot stamped component cannot be obtained. For this reason, the Mo content is set to 0.050% or more. The Mo content is preferably 0.100% or more or 0.150% or more.


On the other hand, when the Mo content is more than 1.000%, a desired texture of prior austenite cannot be obtained. 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 0.0100%

B is an element that improves the hardenability of steel. When the B content is less than 0.0005%, a desired strength of the hot stamped component cannot be obtained. For this reason, the B content is set to 0.0005% or more. The B content is preferably 0.0020% or more or 0.0030% or more.


On the other hand, when the B content is more than 0.0100%, coarse intermetallic compounds are formed in the hot stamped component. As a result, the bendability of the hot stamped component deteriorates. For this reason, the B content is set to 0.0100% or less. The B content is preferably 0.0080% or less, 0.0060% or less or 0.0040% or less.


The hot stamped component may comprise the following elements as optional elements in place of a part of Fe. The content of the following optional elements obtained when the following optional elements are not contained is 0%.


Co: 0.01% to 3.00%

Co is an element that improves strength of the hot stamped component by solid-solution strengthening. In order to reliably obtain the effect, the Co content is preferably set to 0.01% or more, and more preferably set to 0.05% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the Co content is set to 3.00% or less. If necessary, the Co content may be limited to 2.00% or less, 1.50% or less, 1.00% or less or 0.50% or less.


Ni: 0.01% to 3.00%

Ni has an effect of increasing strength of the hot stamped component 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.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the Ni content is set to 3.00% or less. If necessary, the Ni content may be limited to 2.00% or less, 1.50% or less, 1.00% or less or 0.50% or less.


Cu: 0.01% to 3.00%

Cu has an effect that increases the strength of the hot stamped component 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, and more preferably set to 0.05% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the Cu content is set to 3.00% or less. If necessary, the Cu content may be limited to 2.00% or less, 1.50% or less, 1.00% or less or 0.50% or less.


V: 0.01% to 3.00%

V has an effect that forms carbonitrides in steel and improves the strength of the hot stamped component by precipitation strengthening. In order to reliably obtain the effect, the V content is preferably set to 0.01% or more, and more preferably set to 0.05% or more.


On the other hand, when the V content is more than 3.00%, a lot of coarse carbonitrides is generated in steel. As a result, the bendability of the hot stamped component deteriorates. For this reason, the V content is set to 3.00% or less. If necessary, the V content may be limited to 2.00% or less, 1.50% or less, 1.00% or less or 0.50% or less.


W: 0.01% to 3.00%

W has an effect of improving the strength of the hot stamped component. In order to reliably obtain the effects, the W content is preferably set to 0.01% or more, and more preferably set to 0.05% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the W content is set to 3.00% or less. If necessary, the W content may be limited to 2.00% or less, 1.50% or less, 1.00% or less or 0.50% or less.


Ca: 0.0001% to 0.1000%

Ca is an element that suppresses generation of carbides that become starting points for fracture, and contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the Ca content is preferably set to 0.0001% or more, and more preferably set to 0.0010% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the Ca content is set to 0.1000% or less. If necessary, the Ca content may be limited to 0.0500% or less, 0.0200% or less, 0.0100% or less or 0.0060% or less.


Mg: 0.0001% to 1.0000%

Mg refines the microstructure due to formation of oxides and sulfides in molten steel, suppressing formation of a coarse MnS, and dispersing a lot of fine oxides. As a result, Mg contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain these effects, the Mg content is preferably set to 0.0001% or more, and more preferably set to 0.0010% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the Mg content is set to 1.0000% or less. If necessary, the Mg content may be limited to 0.0500% or less, 0.0200% or less, 0.0100% or less or 0.0060% or less.


REM: 0.0001% to 1.000%

REM suppresses generation of coarse oxides. As a result, REM contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the REM content is preferably set to 0.0001% or more, and more preferably set to 0.0010% or more.


On the other hand, since the above effect will be saturated even if a large amount is comprised, the REM content is set to 1.0000% or less. If necessary, the REM content may be limited to 0.0500% or less, 0.0200% or less, 0.0100% or less or 0.0060% or less.


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: 0.001% to 1.000%

Sb suppresses generation of coarse oxides. As a result, Sb contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the Sb content is preferably set to 0.001% or more.


On the other hand, 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 Sb content may be limited to 0.500% or less, 0.200% or less, 0.100% or less or 0.050% or less.


Sn: 0.001% to 1.000%

Sn suppresses generation of coarse oxides. As a result, Sn contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the Sn content is preferably set to 0.001% or more.


On the other hand, 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 Sn content may be limited to 0.500% or less, 0.200% or less, 0.100% or less or 0.050% or less.


Zr: 0.001% to 1.000%

Zr suppresses generation of coarse oxides. As a result, Zr contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the Zr content is preferably set to 0.001% or more.


On the other hand, 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 Zr content may be limited to 0.500% or less, 0.200% or less, 0.100% or less or 0.050% or less.


As: 0.001% to 0.100%

As refines the prior austenite grains by lowering an austenite single-phase transformation temperature. As a result, As contributes for improvement of the bendability of the hot stamped component. In order to reliably obtain the effect, the As content is preferably set to 0.001% or more.


On the other hand, 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 As content may be limited to 0.500% or less, 0.200% or less, 0.100% or less or 0.050% or less.


The remainder of the chemical composition of the hot stamped component 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 stamped component according to the present embodiment do not deteriorate are exemplary examples of the impurities.


The above-mentioned chemical composition of the hot stamped component may be measured by an ordinary 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 stamped component, the chemical composition is analyzed after the plating layer or the coating film is removed by mechanical grinding.


Next, the microstructure of the hot stamped component according to the present embodiment will be described.


In the hot stamped component according to the present embodiment, in a position at ¼ of a sheet thickness from a surface, in a texture of prior austenite, a maximum value of pole densities of an orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=450 is 3.0 or more, an average value of block sizes of martensite, tempered martensite and bainite is 1.20 μm or less.


In the present embodiment, the microstructure is specified in the position at ¼ of the sheet thickness from the surface of the hot stamped component (in a region from a depth of ⅛ of the sheet thickness from the surface to a depth of ⅜ of the sheet thickness from the surface). The reason therefor is that the microstructure at this position indicates a typical microstructure of the hot stamped component.


Note that when the hot stamped component 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.


In texture of prior austenite, maximum value of pole densities of orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=45°: 3.0 or more


The present inventors obtained the following findings about a texture of prior austenite.


By developing the texture of prior austenite, it is possible to alleviate a strain concentration introduced by bending deformation. As a result, an increase of a load in an initial stage of the bending deformation is reduced and the bendability of the hot stamped component can be increased.


In the texture of prior austenite, when the maximum value of pole densities of the orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=45° (hereinafter, it may be referred as the pole density in the texture of prior austenite) is less than 3.0, a desired bendability of the hot stamped component cannot be obtained. For this reason, the maximum value of the pole densities of the orientation group in the texture of prior austenite is set to 3.0 or more. It is preferably 5.0 or more.


The upper limit is not particularly limited, but the maximum value of the pole densities of the orientation group in the texture of prior austenite may be set to 50.0 or less, 20.0 or less, 15.0 or less or 10.0 or less.


The pole density in the texture of prior austenite is measured by the following method.


The pole density of the texture of prior austenite is measured using an EBSD analyzer including a thermal field emission type scanning electron microscope and an EBSD detector, and the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer. The pole density of the texture of prior austenite can be obtained by using the orientation data measured by the EBSD (Electron Back Scattering Diffraction) method and an orientation distribution function (ODF) that displays the three-dimensional texture calculated by computing, using spherical harmonics.


For a sample to be subjected to analysis by the EBSD method, a cross section parallel to a rolling direction and perpendicular to a sheet surface is mechanically polished, and strain is removed by chemical polishing or electrolytic polishing. Using this sample, EBSD measurement is performed at the position at ¼ of the sheet thickness from the surface (in the region from the depth of ⅛ of the sheet thickness from the surface to the depth of ⅜ of the sheet thickness from the surface), with a measurement range of 150 μm in length and a region of 50 μm in the sheet thickness direction and measurement intervals of 0.2 μm. For the measurement, an EBSD analyzer including a thermal field emission type scanning electron microscope and an EBSD detector may be used, for example, an EBSD analyzer including JSM-7001F manufactured by JEOL Ltd. and DVC5-type detector manufactured by TSL Solutions may be used. In this case, the degree of vacuum in the EBSD analyzer may be set to 9.6×10−5 Pa or less, the acceleration voltage may be set to 15 kV and the irradiation current level may be set to 13.


The orientation of prior austenite is measured by the following method. The orientation of prior austenite is calculated by the method described in Non-Patent Document 1, and the orientation of the prior austenite in each coordinate of the EBSD-measured region is specified. Next, an orientation map of prior austenite is created using the “Inverse Pole Figure” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer. Based on the orientation map, the maximum value of pole densitis of an orientation group within the ranges of Φ=60° to 90°, φ1=60° to 90° in section of φ2=45° is calculated. As a result, the maximum value of the pole densitis of the orientation group expressed by Euler angles of 0=60° to 90°, φ1=60° to 90°, and φ2=450 is obtained.


Analyses of a texture using the Euler angles (φ1, Φ, φ2) are widely performed. For example, the definition of the Euler angles (φ1, Φ, φ2) is described in Hiroshi Inoue: “Lecture (Easy Material Analysis Techniques)—Three-dimensional Orientation Analysis of Texture”, Light Metals, Vol. 41, No. 6 (1992), 358. By performing analysis using the above-mentioned software, even a person who does not fully understand the definition of the Euler angles (φ1, Φ, φ2) can easily calculate the maximum value of the pole densitis of the orientation group within the ranges of Φ=60° to 90°, φ1=60° to 90° in section of φ2=45°.


Average value of block sizes of martensite, tempered martensite and bainite: 1.20 μm or less


When the average value of block sizes of martensite, tempered martensite and bainite is more than 1.20 μm, a desired bendability of the hot stamped component cannot be obtained. For this reason, the average value of block sizes of martensite, tempered martensite and bainite is set to 1.20 μm or less. It is preferably 1.00 μm or less, and more preferably 0.90 μm or less.


The lower limit is not particularly limited, but it may be set to 0.30 μm or more, 0.40 μm or more or 0.50 μm or more.


The average value of block sizes of martensite, tempered martensite and bainite is measured by the following method.


A sample is cut out from an arbitrary position away from an end surface of the hot stamped component by a distance of 50 mm or more (a position that possibly 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 at least about 10 mm in the rolling direction.


After polishing the cross section of the above 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 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. Using this sample, in a position at ¼ of the sheet thickness from the surface (a region from a depth of ⅛ of the sheet thickness from the surface to a depth of ⅜ of the sheet thickness from the surface), an orientation information is obtained by measurement using an electron backscatter diffraction method with a measurement range of 150 μm in length and a region of 50 μm in the sheet thickness direction and measurement intervals of 0.2 μm. For the measurement, an EBSD analyzer including a thermal field emission type scanning electron microscope and an EBSD detector may be used, for example, an EBSD analyzer including JSM-7001F manufactured by JEOL Ltd. and DVC5-type detector manufactured by TSL Solutions may be used. In this case, the degree of vacuum in the EBSD analyzer may be set to 9.6×10−5 Pa or less, the acceleration voltage may be set to 15 kV and the irradiation current level may be set to 13.


In the obtained orientation information, using “Phase Map” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer, a region where a crystal structure is fcc is extracted. In these regions, using “Grain Average Misorientation” function installed in the software “OIM Analysis (registered trademark)” attached to the EBSD analyzer, under the condition that boundary with a crystal misorientation of 5° or more is regarded as the grain boundary, regions where the grain average misorientation is more than 0.5° are extracted as martensite, tempered martensite and bainite. For the obtained region, under the condition that boundary with a crystal misorientation of 150 or more is regarded as the grain boundary, the average value of block sizes of martensite, tempered martensite and bainite is obtained by obtaining the value calculated by the Number method using the “Grain Size (diameter)” function.


Note that the rolling direction of the hot stamped component is determined by the following method.


First, a sample is collected so that a sheet thickness cross section of the hot stamped component can be observed. The sheet thickness cross section of the collected sample is finished by mirror polishing, and then observed with an optical microscope. The observation area is width of 500 μm and full of the sheet thickness, and the areas with low brightness are determined as inclusions. 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 observations of the plane parallel to the plane rotated in 5° increments are performed in the same way as the above method. The average values of the lengths of the long axes of inclusions in each cross section are calculated respectively, and a direction parallel to the long axes of the inclusions in the cross section in which the average value of the length of the long axes of the inclusions is maximum is determined as the rolling direction.


Note that when the rolling direction of the hot stamped component is known in advance, the rolling direction of the hot stamped component may be determined without using the above-mentioned determination method.


The microstructure of the hot stamped component is not particularly limited as long as a desired strength and bendability can be obtained. For example, the microstructure may consist of, by area %, a total of 90% or more of martensite, bainite and tempered martensite, and 10% or less of ferrite and residual austenite.


The area ratios of each structure are measured by the following method.


A sample is cut out from an arbitrary position away from an end surface of the hot stamped component by a distance of 50 mm or more (a position that possibly 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 at least 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 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, for a region which has a length of 50 μm and is present in a region from the depth of ⅛ of the sheet thickness from the surface to the depth of ⅜ of the sheet thickness from the surface, an orientation information is obtained by measurement using the electron backscatter diffraction method with measurement intervals of 0.1 μm. For the measurement, an EBSD analyzer including a thermal field emission type scanning electron microscope and an EBSD detector may be used, for example, an EBSD analyzer including JSM-7001F manufactured by JEOL Ltd. and DVC5-type detector manufactured by TSL Solutions may be used. In this case, a degree of vacuum in the EBSD analyzer may be set to 9.6×10−5 Pa or less, the acceleration voltage may be set to 15 kV and the irradiation current level may be set to 13.


Using the obtained crystal structure information and 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 obtaining the area ratio of the residual austenite. Next, in the regions where the crystal structure is bcc is determined as bainite, tempered martensite, martensite and ferrite. For these regions, using the “Grain Average Misorientation” function installed in the software “OM Analysis (registered trademark)” attached to the EBSD analyzer, under the condition that boundary with a crystal misorientation of 5° or more is regarded as the grain boundary, regions where the grain average misorientation is 0.50 or less are extracted as ferrite. The area ratio of the extracted ferrite is calculated, thereby obtaining the area ratio of ferrite.


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


The hot stamped component may have a plating layer or a coating film on the surface. By having the plating layer or the coating film 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.


The sheet thickness of the hot stamped component according to the present embodiment is not particularly limited, but it is preferably set to 0.5 to 3.5 mm from the perspective of reducing the weight of a vehicle body or the like.


It is not specifically necessary to limit the shape of the hot stamped component. For example, the hot stamped component may have a flat sheet shape, a curved shape, or a three-dimensional shape such as a hat shape.


The hot stamped component according to the present embodiment preferably have a tensile strength of 2300 MPa or more. The tensile strength is more preferably 2400 MPa or more, and even more preferably 2500 MPa or more. It is not necessary to limit the upper limit of the tensile strength, if necessary, the tensile strength may be set to 3000 MPa or less or 2800 MPa or less.


The tensile strength is obtained according to the test method described in JIS Z 2241:2011 by producing a No. 5 test piece described in JIS Z 2241:2011 from a flat position of the hot stamped component. A crosshead speed is set to 1 mm/min.


When the hot stamped component according to the present embodiment has a flat sheet shape (has no curved portion, etc.), a load at a ½ stroke of a stroke at the maximum load is preferably 8050 N or more. It is more preferably 8100 N or more, and even more preferably 8150 N or more. However, these standards are based on the case where the sheet thickness of the hot stamped component is 1.6 mm.


The load at the ½ stroke is obtained by performing a bending test under the following conditions based on the VDA standard (VDA238-100: 2017-04) specified by the Verband der Automobilindustrie and obtaining the load at the ½ stroke of the stroke at the maximum load.


When the sheet thickness of the hot stamped component is more than 1.6 mm, the bending test is performed after reducing the sheet thickness to 1.6 mm.


When the sheet thickness of the hot stamped component is less than 1.6 mm, where t is the sheet thickness of the hot stamped component, the load at the ½ stroke of the stroke at the maximum load is preferably 8050×t/1.6 (N) or more.


Note that the load at the ½ stroke of the stroke at the maximum load (however, when the sheet thickness of the hot stamped component is less than 1.6 mm, the value obtained by multiplying the load at the ½ stroke by 1.6/t (t is the sheet thickness in mm)) rarely exceeds 8500 N, 8300 N or 8200 N.

    • Dimensions of test piece: 60 mm (rolling direction)×30 mm (direction parallel to sheet width direction)
    • Bending ridge: direction parallel to sheet width direction
    • Test method: roll support and punch pressing
    • Roll diameter: φ30 mm
    • Punch shape: tip end R=0.4 mm
    • Distance between rolls: 2.0×sheet thickness (mm)+0.5 mm
    • Pressing speed: 20 mm/min
    • Tester: for example, SHIMADZU AUTOGRAPH 20 kN


Next, a steel sheet for hot stamping for obtaining the hot stamped component according to the present embodiment will be described.


The steel sheet for hot stamping has the above-described chemical composition. The microstructure of the steel sheet for hot stamping is not particularly limited as long as a desired strength and bendability are obtained after hot stamping. For example, the microstructure may consist of, by area %, ferrite: 0% to 90%, bainite and martensite: 0% to 100%, pearlite: 0% to 80%, and residual austenite: 0% to 5%.


Further, the steel sheet for hot stamping may have a plating layer or a coating film on the surface. By having the plating layer or the coating film 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 stamped component according to the present embodiment will be described. In order to obtain the above-described hot stamped component, it is particularly effective to control the finish rolling conditions during hot rolling in the manufacturing method of the steel sheet for hot stamping.


Finish Rolling

In the finish rolling, it is preferable to perform a rolling at one stand before a final stand and a rolling at the final stand with a rolling reduction of 50% or more respectively. By performing the rolling at one stand before the final stand and the rolling at the final stand with the rolling reduction of 50% or more, it is possible to control prior austenite with a desired texture.


Note that the rolling reduction here can be expressed as (1−t1/t0)×100(%), where t0 is an inlet sheet thickness and t1 is an outlet sheet thickness of each stand.


After the completion of the finish rolling (after the rolling of the final stand), it is preferable to start cooling after a lapse of 5.0 seconds or more. By elapsing 5.0 seconds or more before starting cooling, granular austenite grains can be generated. As a result, austenite grains with a flat shape are reduced, and granular austenite grains can be sufficiently secured.


Note that the cooling here does not include air cooling (cooling at an average cooling rate of slower than 10° C./s), but includes, for example, such as water cooling at an average cooling rate of 10° C./s or faster. The cooling stop temperature is preferably 550° C. to 650° C.


By the cooling after the finish rolling, austenite transforms into ferrite and pearlite. At this time, pearlite transformation progresses from the grain boundaries of the prior austenite grains. Pearlite having a specific texture is generated by transformation from austenite grains having a specific texture.


In addition, in order to soften the hot-rolled steel sheet, a coil after coiling may be subjected to softening heat treatment. The method of the softening heat treatment is not particularly limited, and an ordinary conditions may be used.


The total reduction during cold rolling is preferably set to 50% or less. The total reduction here can be expressed as (1−t3/t2)×100(%), where t3 is the sheet thickness after the cold rolling and t2 is the sheet thickness before the cold rolling.


Hot Stamping

A hot stamped component according to the present embodiment is obtained by hot stamping the steel sheet for hot stamping manufactured by the above-described method. As the hot stamping conditions, for example, it is preferable to heat the steel sheet for hot stamping to a temperature range of 800° C. to 1000° C. and hold in this temperature range for 60 to 1200 seconds.


By heating during hot stamping, a reverse transformation from pearlite to austenite is caused. Because pearlite has a specific texture, the texture of the austenite generated by the reverse transformation develops. By cooling after hot stamping, a transformation from austenite to martensite is caused. When the final structure becomes martensite, the texture of austenite is preserved. Therefore, the texture of the prior austenite remains developed in the structure after hot stamping.


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


A heating atmosphere is, 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 a gas furnace, a flame heating, an electrical heating, a high-frequency heating, and an induction heating.


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







EXAMPLES

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 1F were held in a temperature range of 1200° C. or higher for 20 minutes or longer, and then subjected to hot rolling, coiling, and cold rolling. The final rolling was performed under conditions shown in Tables 2A to 2E.


Note that after the completion of the finish rolling, the average cooling rate of cooling after a lapse of 5.0 seconds or more was 10° C./s or faster, and the cooling stop temperature was 550° C. to 650° C. In addition, the total reduction of cold rolling was 50% or less.


The obtained steel sheets for hot stamping were subjected to hot stamping under the conditions shown in Tables 2A to 2E, and then cooled to the temperature range of 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 3G were obtained.


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


The underlines in the tables indicate that it is outside the scope of the present invention, falls outside the preferable manufacturing conditions, or the characteristic value is not preferable.


The microstructure of the hot stamped component according to the present invention consisted of, by area %, a total of 90% or more of martensite, bainite and tempered martensite, and 10% or less of ferrite and residual austenite. In addition, the sheet thickness of the hot stamped component according to the present invention was 0.5 to 3.5 mm.


Measurements of the microstructure of the hot stamped component and the measurement of the mechanical properties of the hot stamped component were performed by the above-described methods.


The bending test according to the VDA standard (VDA238-100: 2017-04) is widely performed on components for vehicle, but the bending test targets only flat sheet. Therefore, this VDA standard cannot evaluate the bendability of the hot stamped component with shapes other than flat sheet shape. On the other hand, when the hot stamped component has a bent portion, the bend portion is affected by such as the curvature of the bent portion. For this reason, the inventors considered that it is appropriate to evaluate the bendability according to this VDA standard using a hot stamped component with a flat sheet shape as a test material. Therefore, the bending test was performed on a hot stamped component with a flat sheet shape obtained by hot stamping without bending (using a die that can obtain a hot stamped component without a bent portion). In addition, since the rolling direction of the hot stamped component was known in advance, the rolling direction of the hot stamped component was determined without determining of the rolling direction by evaluation using the above-mentioned determination method. For the bending test machine, a SHIMADZU AUTOGRAPH 20 kN was used.


When the tensile strength TS was 2300 MPa or more, it was determined as having high strength and acceptable, and when the tensile strength TS was less than 2300 MPa, it was determined as not having high strength and unacceptable.


When the load at the ½ stroke of the stroke at the maximum load was 8050 N or more, it was determined as having excellent bendability and acceptable. On the other hand, when the load at the ½ stroke of the stroke at the maximum load was less than 8050 N, it was determined as not having excellent bendability and unacceptable. However, in a case where the sheet thickness of the hot stamped component was less than 1.6 mm, where t was the sheet thickness of the hot stamped component, when the load at the ½ stroke of the stroke at the maximum load was 8050×t/1.6 (N) or more, it was determined as having excellent bendability and acceptable. On the other hand, when the load at the ½ stroke of the stroke at the maximum load was less than 8050×t/1.6 (N), it was determined as not having excellent bendability and unacceptable. Note that in a case where the sheet thickness of the hot stamped component was less than 1.6 mm, the value obtained by multiplying the load at the ½ stroke by 1.6/t (t is the sheet thickness in mm) was mentioned in the “Load at ½ stroke” in Tables 3 A to 3G.











TABLE 1A







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes

























1

0.38

0.550
0.57
0.005
0.0005
0.0016
0.0016
0.0460
0.0360
0.020
0.350
0.230
0.0021

Comparative steel


2
0.41
0.330
0.30
0.004
0.0021
0.0046
0.0027
0.0520
0.0260
0.037
0.140
0.150
0.0034

Steel of present invention


3
0.43
0.580
0.49
0.005
0.0006
0.0040
0.0012
0.0590
0.0410
0.047
0.430
0.210
0.0033

Steel of present invention


4
0.47
0.440
0.45
0.009
0.0013
0.0018
0.0012
0.0450
0.0230
0.043
0.190
0.200
0.0018

Steel of present invention


5
0.55
0.380
0.57
0.011
0.0020
0.0028
0.0017
0.0420
0.0330
0.030
0.430
0.190
0.0026

Steel of present invention


6
0.66
0.270
0.56
0.005
0.0020
0.0024
0.0015
0.0440
0.0330
0.022
0.230
0.230
0.0026

Steel of present invention


7

0.72

0.500
0.29
0.009
0.0004
0.0022
0.0033
0.0520
0.0360
0.020
0.170
0.240
0.0030

Comparative steel


8
0.46

0.008

0.57
0.006
0.0004
0.0046
0.0017
0.0400
0.0150
0.030
0.320
0.170
0.0031

Comparative steel


9
0.46
0.020
0.35
0.009
0.0017
0.0042
0.0029
0.0610
0.0290
0.039
0.230
0.180
0.0021

Steel of present invention


10
0.44
0.070
0.35
0.008
0.0013
0.0029
0.0025
0.0470
0.0270
0.034
0.110
0.180
0.0023

Steel of present invention


11
0.44
0.140
0.24
0.008
0.0018
0.0021
0.0014
0.0560
0.0410
0.025
0.170
0.180
0.0025

Steel of present invention


12
0.46
0.260
0.47
0.009
0.0015
0.0038
0.0010
0.0580
0.0310
0.036
0.160
0.190
0.0022

Steel of present invention


13
0.45
0.440
0.39
0.004
0.0018
0.0023
0.0010
0.0610
0.0380
0.039
0.380
0.180
0.0019

Steel of present invention


14
0.47
0.870
0.32
0.006
0.0020
0.0046
0.0016
0.0550
0.0190
0.019
0.200
0.220
0.0025

Steel of present invention


15
0.47
1.600
0.49
0.004
0.0007
0.0037
0.0025
0.0410
0.0340
0.035
0.310
0.210
0.0024

Steel of present invention


16
0.45
2.700
0.36
0.007
0.0018
0.0022
0.0030
0.0450
0.0200
0.027
0.230
0.140
0.0032

Steel of present invention


17
0.47

3.200

0.33
0.005
0.0018
0.0040
0.0020
0.0450
0.0180
0.040
0.300
0.210
0.0030

Comparative steel


18
0.45
0.250

0.05

0.007
0.0012
0.0033
0.0025
0.0550
0.0360
0.047
0.330
0.230
0.0032

Comparative steel


19
0.44
0.660
0.16
0.004
0.0008
0.0037
0.0015
0.0440
0.0150
0.038
0.320
0.180
0.0034

Steel of present invention


20
0.46
0.480
0.24
0.006
0.0020
0.0029
0.0033
0.0570
0.0390
0.033
0.220
0.130
0.0029

Steel of present invention


21
0.45
0.630
0.39
0.007
0.0015
0.0021
0.0019
0.0500
0.0360
0.048
0.350
0.150
0.0022

Steel of present invention


22
0.45
0.510
0.46
0.011
0.0009
0.0016
0.0023
0.0490
0.0220
0.025
0.410
0.200
0.0028

Steel of present invention


23
0.44
0.480
0.55
0.007
0.0020
0.0039
0.0012
0.0500
0.0280
0.031
0.340
0.190
0.0027

Steel of present invention


24
0.45
0.450

0.84

0.004
0.0007
0.0019
0.0024
0.0390
0.0210
0.033
0.240
0.160
0.0034

Comparative steel


25
0.47
0.220
0.35
0.006
0.0013
0.0017
0.0033
0.0490
0.0210
0.037
0.380
0.180
0.0016

Steel of present invention


26
0.47
0.570
0.29
0.012
0.0013
0.0037
0.0011
0.0400
0.0290
0.029
0.340
0.230
0.0032

Steel of present invention





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















TABLE 1B







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes

























27
0.46
0.450
0.24
0.025
0.0021
0.0032
0.0019
0.0580
0.0240
0.037
0.110
0.240
0.0022

Steel of present invention


28
0.45
0.270
0.35
0.046
0.0008
0.0020
0.0017
0.0390
0.0310
0.041
0.140
0.120
0.0029

Steel of present invention


29
0.44
0.590
0.39
0.083
0.0019
0.0023
0.0031
0.0470
0.0130
0.026
0.150
0.200
0.0027

Steel of present invention


30
0.45
0.210
0.55

0.120

0.0021
0.0030
0.0010
0.0430
0.0230
0.029
0.330
0.220
0.0030

Comparative steel


31
0.44
0.580
0.28
0.010
0.0012
0.0024
0.0026
0.0610
0.0280
0.020
0.110
0.240
0.0023

Steel of present invention


32
0.44
0.250
0.49
0.011
0.0028
0.0028
0.0023
0.0490
0.0210
0.047
0.190
0.140
0.0030

Steel of present invention


33
0.47
0.400
0.26
0.008
0.0043
0.0041
0.0011
0.0590
0.0240
0.048
0.260
0.230
0.0028

Steel of present invention


34
0.47
0.640
0.47
0.005
0.0075
0.0039
0.0022
0.0530
0.0200
0.028
0.260
0.130
0.0029

Steel of present invention


35
0.46
0.350
0.55
0.004
0.0092
0.0041
0.0011
0.0580
0.0160
0.035
0.140
0.190
0.0029

Steel of present invention


36
0.44
0.280
0.39
0.012

0.0134

0.0042
0.0016
0.0550
0.0140
0.035
0.430
0.170
0.0032

Comparative steel


37
0.47
0.410
0.38
0.010
0.0003
0.0012
0.0014
0.0420
0.0230
0.035
0.140
0.140
0.0030

Steel of present invention


38
0.47
0.590
0.55
0.010
0.0012
0.0022
0.0013
0.0530
0.0200
0.022
0.180
0.200
0.0023

Steel of present invention


39
0.44
0.530
0.55
0.006
0.0011
0.0047
0.0013
0.0490
0.0190
0.043
0.410
0.160
0.0033

Steel of present invention


40
0.46
0.520
0.48
0.008
0.0015
0.0065
0.0022
0.0490
0.0360
0.025
0.280
0.220
0.0034

Steel of present invention


41
0.47
0.660
0.25
0.006
0.0020
0.0089
0.0019
0.0460
0.0280
0.021
0.280
0.150
0.0034

Steel of present invention


42
0.44
0.310
0.57
0.009
0.0012

0.0121

0.0016
0.0400
0.0150
0.026
0.200
0.230
0.0026

Comparative steel


43
0.46
0.480
0.57
0.006
0.0015
0.0034
0.0017
0.0440
0.0170
0.037
0.190
0.150
0.0017

Steel of present invention


44
0.45
0.530
0.49
0.010
0.0013
0.0016
0.0038
0.0580
0.0130
0.032
0.250
0.130
0.0025

Steel of present invention


45
0.45
0.280
0.49
0.006
0.0012
0.0019
0.0058
0.0410
0.0290
0.038
0.250
0.200
0.0034

Steel of present invention


46
0.46
0.420
0.53
0.011
0.0004
0.0019
0.0084
0.0510
0.0240
0.046
0.270
0.220
0.0028

Steel of present invention


47
0.44
0.240
0.25
0.008
0.0011
0.0043
0.0176
0.0590
0.0220
0.028
0.410
0.180
0.0022

Steel of present invention


48
0.46
0.290
0.55
0.008
0.0012
0.0026

0.0240

0.0570
0.0340
0.025
0.260
0.220
0.0031

Comparative steel


49
0.45
0.470
0.28
0.009
0.0009
0.0040
0.0024

0.0006

0.0150
0.037
0.430
0.230
0.0022

Comparative steel


50
0.46
0.210
0.37
0.012
0.0011
0.0038
0.0009
0.0019
0.0200
0.035
0.290
0.190
0.0022

Steel of present invention


51
0.47
0.560
0.53
0.006
0.0018
0.0026
0.0020
0.0052
0.0340
0.041
0.130
0.160
0.0017

Steel of present invention


52
0.44
0.420
0.26
0.009
0.0015
0.0026
0.0026
0.0130
0.0270
0.040
0.290
0.150
0.0018

Steel of present invention





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















TABLE 1C







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes

























53
0.45
0.500
0.27
0.007
0.0021
0.0019
0.0016
0.0390
0.0130
0.041
0.260
0.170
0.0017

Steel of present invention


54
0.45
0.320
0.32
0.010
0.0005
0.0041
0.0018
0.0820
0.0270
0.020
0.120
0.180
0.0032

Steel of present invention


55
0.47
0.670
0.53
0.010
0.0020
0.0023
0.0023
0.1800
0.0400
0.019
0.380
0.210
0.0021

Steel of present invention


56
0.47
0.600
0.30
0.009
0.0021
0.0035
0.0033
0.2500
0.0320
0.021
0.110
0.150
0.0029

Steel of present invention


57
0.45
0.550
0.53
0.011
0.0014
0.0032
0.0028
0.3200
0.0400
0.029
0.240
0.200
0.0029

Steel of present invention


58
0.46
0.470
0.55
0.010
0.0019
0.0038
0.0009
0.4800
0.0410
0.041
0.110
0.170
0.0023

Steel of present invention


59
0.45
0.560
0.31
0.006
0.0012
0.0025
0.0031

0.6200

0.0150
0.042
0.360
0.170
0.0023

Comparative steel


60
0.46
0.560
0.33
0.009
0.0020
0.0042
0.0015
0.0520

0.0008

0.031
0.230
0.190
0.0018

Comparative steel


61
0.44
0.620
0.44
0.010
0.0007
0.0032
0.0021
0.0500
0.0012
0.034
0.370
0.220
0.0026

Steel of present invention


62
0.45
0.570
0.38
0.009
0.0006
0.0016
0.0032
0.0600
0.0039
0.048
0.170
0.170
0.0026

Steel of present invention


63
0.45
0.400
0.35
0.012
0.0003
0.0023
0.0011
0.0490
0.0076
0.020
0.160
0.240
0.0034

Steel of present invention


64
0.46
0.300
0.55
0.009
0.0014
0.0040
0.0028
0.0510
0.0120
0.038
0.430
0.140
0.0022

Steel of present invention


65
0.45
0.280
0.49
0.007
0.0004
0.0040
0.0013
0.0450
0.0180
0.034
0.190
0.170
0.0033

Steel of present invention


66
0.45
0.400
0.27
0.011
0.0011
0.0042
0.0013
0.0420
0.0340
0.025
0.200
0.240
0.0020

Steel of present invention


67
0.45
0.220
0.44
0.012
0.0003
0.0027
0.0014
0.0510
0.0560
0.039
0.190
0.120
0.0023

Steel of present invention


68
0.45
0.620
0.44
0.007
0.0009
0.0036
0.0030
0.0570
0.0880
0.044
0.160
0.190
0.0030

Steel of present invention


69
0.47
0.470
0.55
0.007
0.0002
0.0018
0.0009
0.0580

0.1330

0.029
0.170
0.140
0.0026

Comparative steel


70
0.46
0.620
0.35
0.011
0.0018
0.0028
0.0030
0.0390
0.0220

0.007

0.260
0.120
0.0024

Comparative steel


71
0.46
0.560
0.32
0.005
0.0003
0.0015
0.0029
0.0610
0.0140
0.013
0.350
0.240
0.0019

Steel of present invention


72
0.44
0.440
0.42
0.004
0.0020
0.0016
0.0009
0.0440
0.0280
0.022
0.220
0.120
0.0019

Steel of present invention


73
0.46
0.330
0.27
0.005
0.0013
0.0039
0.0029
0.0530
0.0380
0.038
0.140
0.120
0.0023

Steel of present invention


74
0.45
0.540
0.34
0.007
0.0018
0.0042
0.0025
0.0540
0.0160
0.047
0.420
0.220
0.0018

Steel of present invention


75
0.45
0.590
0.33
0.005
0.0008
0.0024
0.0017
0.0500
0.0260
0.062
0.280
0.150
0.0031

Steel of present invention


76
0.45
0.330
0.28
0.012
0.0014
0.0022
0.0019
0.0590
0.0310
0.075
0.290
0.230
0.0032

Steel of present invention


77
0.47
0.570
0.28
0.012
0.0002
0.0016
0.0015
0.0500
0.0210
0.087
0.180
0.150
0.0026

Steel of present invention


78
0.46
0.310
0.39
0.008
0.0012
0.0038
0.0020
0.0410
0.0230

0.121

0.230
0.230
0.0018

Comparative steel


79
0.45
0.290
0.52
0.007
0.0019
0.0033
0.0027
0.0520
0.0320
0.040

0.007

0.150
0.0018

Comparative steel





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















TABLE 1D







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes





 80
0.45
0.250
0.52
0.010
0.0009
0.0034
0.0013
0.0610
0.0140
0.032
0.018
0.230
0.0022

Steel of

















present invention


 81
0.45
0.670
0.35
0.007
0.0007
0.0024
0.0014
0.0550
0.0130
0.034
0.110
0.180
0.0024

Steel of

















present invention


 82
0.44
0.550
0.50
0.010
0.0009
0.0025
0.0016
0.0480
0.0210
0.027
0.280
0.170
0.0025

Steel of

















present invention


 83
0.44
0.250
0.33
0.009
0.0021
0.0041
0.0021
0.0530
0.0370
0.020
0.350
0.180
0.0033

Steel of

















present invention


 84
0.44
0.450
0.33
0.006
0.0019
0.0037
0.0021
0.0520
0.0190
0.037
0.480
0.240
0.0028

Steel of

















present invention


 85
0.46
0.280
0.43
0.008
0.0010
0.0027
0.0022
0.0460
0.0210
0.031
0.650
0.170
0.0017

Steel of

















present invention


 86
0.44
0.330
0.25
0.007
0.0005
0.0017
0.0016
0.0460
0.0170
0.048
0.880
0.160
0.0018

Steel of

















present invention


 87
0.46
0.410
0.32
0.012
0.0008
0.0027
0.0018
0.0550
0.0200
0.019

1.220

0.180
0.0018

Comparative steel


 88
0.46
0.530
0.41
0.011
0.0005
0.0046
0.0020
0.0460
0.0170
0.019
0.140

0.020

0.0018

Comparative steel


 89
0.44
0.600
0.29
0.008
0.0006
0.0021
0.0015
0.0430
0.0160
0.043
0.190
0.070
0.0019

Steel of

















present invention


 90
0.44
0.630
0.33
0.008
0.0021
0.0019
0.0024
0.0580
0.0360
0.030
0.410
0.110
0.0023

Steel of

















present invention


 91
0.46
0.560
0.50
0.005
0.0013
0.0028
0.0026
0.0420
0.0320
0.047
0.310
0.190
0.0027

Steel of

















present invention


 92
0.44
0.660
0.49
0.008
0.0014
0.0036
0.0026
0.0470
0.0310
0.034
0.320
0.330
0.0021

Steel of

















present invention


 93
0.46
0.580
0.24
0.005
0.0016
0.0019
0.0016
0.0610
0.0310
0.046
0.330
0.560
0.0022

Steel of

















present invention


 94
0.46
0.480
0.53
0.007
0.0002
0.0035
0.0026
0.0500
0.0350
0.042
0.220
0.780
0.0029

Steel of

















present invention


 95
0.46
0.250
0.39
0.006
0.0003
0.0044
0.0012
0.0430
0.0240
0.028
0.390
0.930
0.0024

Steel of

















present invention


 96
0.44
0.420
0.27
0.004
0.0005
0.0024
0.0015
0.0540
0.0250
0.022
0.230

1.230

0.0024

Comparative steel


 97
0.44
0.460
0.38
0.007
0.0003
0.0045
0.0012
0.0540
0.0300
0.029
0.260
0.230

0.0004


Comparative steel


 98
0.45
0.300
0.34
0.011
0.0017
0.0029
0.0031
0.0510
0.0270
0.021
0.110
0.140
0.0007

Steel of

















present invention


 99
0.44
0.250
0.37
0.009
0.0019
0.0033
0.0032
0.0460
0.0190
0.033
0.170
0.220
0.0012

Steel of

















present invention


100
0.45
0.610
0.57
0.010
0.0011
0.0040
0.0012
0.0410
0.0400
0.032
0.130
0.170
0.0019

Steel of

















present invention


101
0.45
0.580
0.40
0.007
0.0008
0.0024
0.0016
0.0610
0.0130
0.033
0.290
0.190
0.0032

Steel of

















present invention


102
0.46
0.220
0.42
0.005
0.0005
0.0031
0.0023
0.0450
0.0300
0.039
0.410
0.210
0.0055

Steel of

















present invention


103
0.44
0.620
0.46
0.005
0.0004
0.0036
0.0029
0.0600
0.0260
0.035
0.380
0.210
0.0072

Steel of

















present invention


104
0.46
0.350
0.54
0.012
0.0006
0.0020
0.0033
0.0430
0.0260
0.032
0.120
0.210
0.0086

Steel of

















present invention


105
0.46
0.230
0.37
0.005
0.0015
0.0031
0.0033
0.0530
0.0250
0.026
0.180
0.210

0.0115


Comparative steel





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















TABLE 1E







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes





106
0.45
0.530
0.30
0.007
0.0003
0.0024
0.0011
0.0520
0.0410
0.047
0.210
0.210
0.0024
Co = 0.06
Steel of

















present invention


107
0.47
0.270
0.42
0.006
0.0021
0.0032
0.0030
0.0420
0.0240
0.024
0.190
0.200
0.0016
Co = 1.30
Steel of

















present invention


108
0.47
0.390
0.40
0.012
0.0004
0.0020
0.0009
0.0410
0.0330
0.032
0.280
0.130
0.0021
Co = 2.50
Steel of

















present invention


109
0.45
0.660
0.33
0.006
0.0005
0.0040
0.0029
0.0530
0.0260
0.033
0.390
0.150
0.0029
Ni = 0.03
Steel of

















present invention


110
0.47
0.390
0.44
0.009
0.0019
0.0025
0.0015
0.0520
0.0270
0.032
0.260
0.120
0.0032
Ni = 1.10
Steel of

















present invention


111
0.46
0.220
0.48
0.011
0.0018
0.0021
0.0010
0.0390
0.0370
0.036
0.380
0.120
0.0020
Ni = 2.60
Steel of

















present invention


112
0.47
0.330
0.52
0.007
0.0008
0.0022
0.0012
0.0470
0.0250
0.031
0.220
0.140
0.0034
Cu = 0.07
Steel of

















present invention


113
0.46
0.440
0.57
0.009
0.0018
0.0046
0.0017
0.0400
0.0160
0.031
0.370
0.190
0.0019
Cu = 1.20
Steel of

















present invention


114
0.46
0.660
0.43
0.005
0.0002
0.0020
0.0032
0.0390
0.0290
0.038
0.290
0.230
0.0017
Cu = 2.70
Steel of

















present invention


115
0.46
0.260
0.56
0.004
0.0006
0.0037
0.0015
0.0570
0.0270
0.028
0.390
0.190
0.0017
V = 0.06
Steel of

















present invention


116
0.44
0.230
0.26
0.012
0.0006
0.0031
0.0014
0.0580
0.0150
0.033
0.120
0.160
0.0019
V = 0.90
Steel of

















present invention


117
0.44
0.610
0.39
0.007
0.0021
0.0028
0.0030
0.0610
0.0230
0.029
0.420
0.150
0.0031
V = 2.20
Steel of

















present invention


118
0.46
0.220
0.28
0.006
0.0003
0.0030
0.0029
0.0460
0.0400
0.021
0.140
0.130
0.0025
W = 0.09
Steel of

















present invention


119
0.45
0.620
0.44
0.005
0.0010
0.0035
0.0010
0.0500
0.0140
0.019
0.410
0.210
0.0033
W = 1.50
Steel of

















present invention


120
0.47
0.620
0.38
0.011
0.0010
0.0024
0.0030
0.0570
0.0310
0.020
0.320
0.150
0.0029
W = 2.60
Steel of

















present invention


121
0.44
0.620
0.45
0.012
0.0019
0.0028
0.0026
0.0410
0.0230
0.034
0.120
0.220
0.0032
  Ca = 0.0016
Steel of

















present invention


122
0.46
0.250
0.47
0.007
0.0013
0.0026
0.0014
0.0410
0.0350
0.023
0.160
0.160
0.0017
  Ca = 0.0120
Steel of

















present invention


123
0.44
0.620
0.32
0.012
0.0002
0.0036
0.0032
0.0460
0.0210
0.029
0.400
0.170
0.0020
  Ca = 0.0860
Steel of

















present invention


124
0.45
0.470
0.41
0.007
0.0018
0.0027
0.0025
0.0410
0.0400
0.037
0.340
0.150
0.0034
 Mg = 0.0018
Steel of

















present invention


125
0.46
0.640
0.53
0.008
0.0018
0.0023
0.0021
0.0520
0.0230
0.025
0.430
0.230
0.0034
 Mg = 0.2100
Steel of

















present invention


126
0.45
0.640
0.39
0.006
0.0005
0.0027
0.0017
0.0390
0.0260
0.041
0.190
0.240
0.0026
 Mg = 0.9200
Steel of

















present invention


127
0.46
0.660
0.37
0.012
0.0021
0.0017
0.0016
0.0590
0.0180
0.033
0.390
0.150
0.0023
REM = 0.0016
Steel of

















present invention


128
0.44
0.370
0.36
0.011
0.0004
0.0038
0.0022
0.0500
0.0300
0.034
0.110
0.120
0.0022
REM = 0.1300
Steel of

















present invention


129
0.45
0.650
0.51
0.012
0.0013
0.0027
0.0033
0.0440
0.0160
0.024
0.330
0.220
0.0019
REM = 0.6700
Steel of

















present invention


















TABLE 1F







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























No.
C
Si
Mn
P
S
N
O
Al
Nb
Ti
Cr
Mo
B
Others
Notes





130
0.45
0.620
0.38
0.007
0.0006
0.0026
0.0019
0.0420
0.0220
0.037
0.160
0.160
0.0020
Sb = 0.006
Steel of

















present invention


131
0.45
0.630
0.39
0.005
0.0017
0.0037
0.0010
0.0440
0.0340
0.027
0.140
0.140
0.0020
Sb = 0.140
Steel of

















present invention


132
0.45
0.470
0.47
0.009
0.0009
0.0031
0.0011
0.0400
0.0150
0.042
0.190
0.170
0.0030
Sb = 0.850
Steel of

















present invention


133
0.46
0.220
0.47
0.005
0.0013
0.0026
0.0013
0.0540
0.0400
0.031
0.200
0.230
0.0034
Sn = 0.003
Steel of

















present invention


134
0.47
0.660
0.31
0.005
0.0010
0.0030
0.0015
0.0550
0.0210
0.036
0.160
0.140
0.0033
Sn = 0.120
Steel of

















present invention


135
0.44
0.670
0.33
0.006
0.0019
0.0040
0.0017
0.0500
0.0280
0.036
0.350
0.240
0.0033
Sn = 0.790
Steel of

















present invention


136
0.44
0.410
0.50
0.009
0.0004
0.0038
0.0017
0.0400
0.0210
0.020
0.120
0.240
0.0031
Zr = 0.005
Steel of

















present invention


137
0.45
0.550
0.32
0.007
0.0012
0.0028
0.0013
0.0480
0.0400
0.040
0.210
0.150
0.0017
Zr = 0.090
Steel of

















present invention


138
0.46
0.360
0.26
0.005
0.0021
0.0020
0.0015
0.0520
0.0270
0.035
0.140
0.120
0.0018
Zr = 0.720
Steel of

















present invention


139
0.47
0.510
0.39
0.010
0.0014
0.0015
0.0025
0.0580
0.0320
0.022
0.170
0.170
0.0032
As = 0.003
Steel of

















present invention


140
0.46
0.260
0.53
0.008
0.0016
0.0025
0.0012
0.0520
0.0220
0.028
0.340
0.180
0.0025
As = 0.042
Steel of

















present invention


141
0.46
0.580
0.50
0.007
0.0020
0.0037
0.0033
0.0550
0.0140
0.045
0.340
0.160
0.0019
As = 0.093
Steel of

















present invention


142
0.45
0.420
0.48
0.012
0.0003
0.0033
0.0022
0.0470
0.0370
0.036
0.410
0.150
0.0020
Co = 1.40,
Steel of
















Ni = 1.20
present invention


143
0.44
0.430
0.27
0.010
0.0010
0.0036
0.0027
0.0590
0.0370
0.022
0.410
0.220
0.0022
Co = 1.30,
Steel of
















Cu = 1.40
present invention


144
0.45
0.550
0.27
0.010
0.0010
0.0046
0.0030
0.0410
0.0200
0.033
0.200
0.170
0.0025
Co = 1.40,
Steel of
















W = 1.60
present invention


145
0.45
0.270
0.43
0.007
0.0013
0.0025
0.0024
0.0580
0.0400
0.034
0.230
0.200
0.0018
Co = 1.50,
Steel of
















Mg = 0.1900
present invention


146
0.44
0.490
0.42
0.010
0.0019
0.0023
0.0033
0.0390
0.0160
0.044
0.180
0.200
0.0033
Ni = 1.30,
Steel of
















Cu = 1.20
present invention


147
0.46
0.540
0.34
0.006
0.0004
0.0029
0.0017
0.0580
0.0250
0.048
0.200
0.150
0.0034
Ni = 1.20,
Steel of
















W = 1.40
present invention


148
0.46
0.300
0.48
0.005
0.0007
0.0016
0.0027
0.0610
0.0250
0.034
0.310
0.220
0.0027
Ni = 1.10,
Steel of
















Mg = 0.1800
present invention


149
0.47
0.280
0.31
0.008
0.0013
0.0028
0.0016
0.0450
0.0210
0.046
0.260
0.180
0.0017
Cu = 1.10,
Steel of
















W = 1.30
present invention


150
0.44
0.210
0.56
0.011
0.0017
0.0040
0.0033
0.0540
0.0400
0.041
0.290
0.190
0.0018
Cu = 1.20,
Steel of
















Mg = 0.2200
present invention


151
0.44
0.260
0.54
0.005
0.0004
0.0025
0.0026
0.0580
0.0170
0.042
0.260
0.190
0.0026
W = 1.40,
Steel of
















Mg = 0.2100
present invention






















TABLE 2A









Final rolling



















Rolling

Cooling
Hot stamping

















reduction
Rolling
Time
Heating




Manu-

at one stand
reduction at
until
tem-




facturing
Steel
before final
final stand
starting
perature
Holding



No.
No.
stand %
%
coolings
° C.
times
Notes





 1
1
54
51
6.9
920
478
Comparative example


 2
 2
53
51
6.4
882
481
Present invention example


 3
 3
51
51
6.6
919
495
Present invention example


 4
 4
53
55
6.2
892
465
Present invention example


 5
 5
55
56
6.3
881
466
Present invention example


 6
 6
52
54
5.2
914
495
Present invention example


 7
7
53
51
6.3
906
479
Comparative example


 8
8
50
54
7.1
911
481
Comparative example


 9
 9
54
55
5.9
885
477
Present invention example


10
10
50
52
5.4
882
481
Present invention example


11
11
53
52
5.7
896
478
Present invention example


12
12
52
55
7.4
894
478
Present invention example


13
13
53
53
5.3
892
495
Present invention example


14
14
54
56
5.9
904
465
Present invention example


15
15
52
55
6.5
896
478
Present invention example


16
16
54
54
7.2
916
477
Present invention example


17

17

52
50
5.4
905
492
Comparative example


18

18

52
51
6.7
903
489
Comparative example


19
19
54
52
6.7
912
493
Present invention example


20
20
55
50
7.4
882
474
Present invention example


21
21
51
51
6.6
896
474
Present invention example


22
22
50
56
6.5
882
480
Present invention example


23
23
52
51
7.0
889
485
Present invention example


24

24

51
53
5.0
911
487
Comparative example


25
25
51
54
6.3
894
479
Present invention example


26
26
54
50
6.6
915
472
Present invention example


27
27
55
50
6.0
898
479
Present invention example


28
28
50
53
6.2
881
473
Present invention example


29
29
53
55
7.4
899
470
Present invention example


30

30

51
52
5.4
885
468
Comparative example


31
31
50
55
6.8
918
484
Present invention example


32
32
52
55
6.5
897
475
Present invention example


33
33
52
50
6.0
894
473
Present invention example


34
34
52
56
5.1
903
491
Present invention example


35
35
53
50
5.6
918
465
Present invention example


36

36

55
52
5.6
888
482
Comparative example


37
37
54
50
6.7
909
466
Present invention example





The underline indicates that the manufacturing condition is not preferable.



















TABLE 2B









Final rolling
Cooling


















Rolling reduction
Rolling
Time
Hot stamping















Manu-

at one stand
reduction
until
Heating




facturing
Steel
before final
at final
starting
temperature
Holding



No.
No.
stand %
stand %
coolings
° C.
times
Notes





38
38
55
52
6.6
904
472
Present invention example


39
39
54
51
7.1
916
477
Present invention example


40
40
52
52
7.3
918
486
Present invention example


41
41
51
54
6.8
887
471
Present invention example


42

42

51
50
7.2
906
484
Comparative example


43
43
54
52
5.3
893
476
Present invention example


44
44
51
55
5.7
903
491
Present invention example


45
45
51
52
5.6
914
489
Present invention example


46
46
52
53
6.5
900
469
Present invention example


47
47
53
52
6.0
917
470
Present invention example


48

48

55
50
6.6
906
482
Comparative example


49

49

52
52
5.3
919
490
Comparative example


50
50
55
56
6.9
887
495
Present invention example


51
51
52
54
7.1
897
467
Present invention example


52
52
54
53
6.1
882
471
Present invention example


53
53
55
54
6.2
910
467
Present invention example


54
54
53
50
6.8
900
488
Present invention example


55
55
55
51
6.2
881
468
Present invention example


56
56
53
51
7.2
902
495
Present invention example


57
57
52
54
5.7
911
483
Present invention example


58
58
52
55
6.4
918
494
Present invention example


59

59

50
52
5.7
882
473
Comparative example


60

60

52
52
5.1
882
482
Comparative example


61
61
53
55
5.3
900
491
Present invention example


62
62
53
52
5.1
908
478
Present invention example


63
63
53
53
6.2
895
492
Present invention example


64
64
53
50
6.1
912
480
Present invention example


65
65
54
54
5.2
912
479
Present invention example


66
66
52
51
5.4
891
484
Present invention example


67
67
51
56
5.5
909
478
Present invention example


68
68
52
52
7.3
909
484
Present invention example


69

69

55
52
6.6
889
483
Comparative example


70

70

50
56
5.3
897
493
Comparative example


71
71
55
52
5.9
897
477
Present invention example


72
72
50
55
5.3
910
478
Present invention example


73
73
51
54
6.8
891
493
Present invention example


74
74
53
54
6.4
898
485
Present invention example


75
75
52
50
5.9
915
485
Present invention example





The underline indicates that the manufacturing condition is not preferable.



















TABLE 2C









Final rolling
Cooling


















Rolling reduction
Rolling
Time
Hot stamping















Manu-

at one stand
reduction at
until
Heating




facturing
Steel
before final
final stand
starting
temperature
Holding



No.
No.
stand %
%
coolings
° C.
times
Notes





 76
 76
54
52
7.4
897
493
Present invention example


 77
 77
51
50
5.5
905
465
Present invention example


 78
78
53
56
6.3
886
494
Comparative example


 79
79
55
50
6.2
881
482
Comparative example


 80
 80
54
55
6.4
894
491
Present invention example


 81
 81
50
52
5.8
894
488
Present invention example


 82
 82
55
54
5.1
897
467
Present invention example


 83
 83
52
53
6.4
903
483
Present invention example


 84
 84
54
50
7.0
911
483
Present invention example


 85
 85
54
55
7.4
907
487
Present invention example


 86
 86
55
51
5.2
888
476
Present invention example.


 87
87
54
54
6.4
898
488
Comparative example


 88
88
54
50
5.8
910
478
Comparative example


 89
 89
50
50
7.0
884
478
Present invention example


 90
 90
54
53
6.7
902
474
Present invention example


 91
 91
55
52
5.0
900
476
Present invention example


 92
 92
54
51
5.2
907
495
Present invention example


 93
 93
53
54
6.0
881
480
Present invention example


 94
 94
55
50
6.6
901
471
Present invention example


 95
 95
54
55
5.1
911
478
Present invention example


 96
96
52
52
5.0
905
494
Comparative example


 97
97
54
52
7.0
894
484
Comparative example


 98
 98
54
52
5.5
905
495
Present invention example


 99
 99
51
56
5.6
917
487
Present invention example


100
100
55
55
5.9
914
485
Present invention example


101
101
52
50
5.0
899
470
Present invention example


102
102
51
51
6.8
915
483
Present invention example


103
103
55
56
7.1
887
477
Present invention example


104
104
50
51
5.3
919
466
Present invention example


105

105

54
50
5.0
882
466
Comparative example


106
106
52
53
5.5
905
484
Present invention example


107
107
51
50
6.2
902
477
Present invention example


108
108
50
54
5.2
894
472
Present invention example


109
109
53
51
7.2
916
482
Present invention example


110
110
53
50
7.1
915
492
Present invention example


111
111
51
52
6.1
903
479
Present invention example





The underline indicates that the manufacturing condition is not preferable.


















TABLE 2D









Final rolling
Cooling
Hot stamping

















Rolling reduction
Rolling
Time
Heating




Manu-

at one stand
reduction
until
temper-




facturing
Steel
before final
at final
starting
ature
Holding



No.
No.
stand %
stand %
coolings
° C.
times
Notes





112
112
50
55
6.9
880
489
Present invention example


113
113
53
56
5.3
886
472
Present invention example


114
114
52
55
5.9
915
492
Present invention example


115
115
52
56
6.6
899
466
Present invention example


116
116
54
55
7.4
898
495
Present invention example


117
117
55
51
7.3
904
466
Present invention example


118
118
55
52
5.3
884
484
Present invention example


119
119
51
50
7.0
918
493
Present invention example


120
120
53
50
6.6
903
492
Present invention example


121
121
53
52
5.1
887
488
Present invention example


122
122
53
52
7.2
881
470
Present invention example


123
123
52
53
5.0
882
494
Present invention example


124
124
53
55
5.8
886
478
Present invention example


125
125
50
55
6.2
914
488
Present invention example


126
126
53
51
7.0
896
473
Present invention example


127
127
54
53
6.9
892
477
Present invention example


128
128
50
50
6.2
880
481
Present invention example


129
129
50
54
6.0
900
480
Present invention example


130
130
51
52
6.4
898
481
Present invention example


131
131
55
53
7.2
901
465
Present invention example


132
132
53
50
7.3
903
491
Present invention example


133
133
51
55
6.2
910
494
Present invention example


134
134
53
52
6.8
889
472
Present invention example


135
135
53
53
7.0
900
472
Present invention example


136
136
54
51
7.3
900
480
Present invention example


137
137
55
55
6.2
920
485
Present invention example


138
138
50
54
5.4
918
480
Present invention example


139
139
55
56
6.5
890
494
Present invention example.


140
140
52
56
5.3
907
476
Present invention example


141
141
54
52
7.2
915
494
Present invention example


142
142
55
56
5.5
887
489
Present invention example


143
143
55
52
6.3
885
465
Present invention example


144
144
53
52
6.3
882
488
Present invention example


145
145
53
53
5.5
916
470
Present invention example


146
146
54
55
5.8
885
486
Present invention example


147
147
55
50
6.5
918
480
Present invention example


148
148
55
50
6.1
910
485
Present invention example


149
149
54
52
5.2
904
486
Present invention example


150
150
53
50
5.4
895
482
Present invention example





















TABLE 2E









Final rolling
Cooling
Hot stamping

















Rolling reduction
Rolling
Time
Heating




Manu-

at one stand
reduction
until
temper-




facturing
Steel
before final
at final
starting
ature
Holding



No.
No.
stand %
stand %
coolings
° C.
time
Notes





151
151
52
52
7.0
889
482
Present invention example


152
 11

20


10

6.4
880
494
Comparative example


153
 11

20


20

7.4
920
481
Comparative example


154
 14

30


30

5.2
910
465
Comparative example


155
 22

40


30

6.1
881
466
Comparative example


156
 14

30


40

6.3
899
478
Comparative example


157
 20

40


40

5.1
919
470
Comparative example


158
 20

20

50
5.8
890
477
Comparative example


159
 14
50

20

5.8
909
471
Comparative example


160
 12
55
50

0.4

913
478
Comparative example


161
 22
52
54

2.2

919
475
Comparative example


162
 14
51
51

4.1

904
485
Comparative example


163
 21
54
54
6.1
895
470
Present invention example


164
 12
51
56
6.7
911
471
Present invention example


165
 13
51
54
5.5
892
487
Present invention example


166
 11
50
53
5.3
886
466
Present invention example


167
 22
50
56
7.0
909
475
Present invention example


168
 21
55
53
5.1
903
468
Present invention example


169
 11
55
50
7.1
897
470
Present invention example


170
 14
51
52
5.5
881
489
Present invention example


171
 22
52
54
6.3

745

478
Comparative example


172
 22
50
52
6.3
843
490
Present invention example


173
 14
53
54
5.2
895
482
Present invention example


174
 20
53
52
5.6
952
483
Present invention example


175
 22
53
53
5.0

1023

489
Comparative example


176
 14
51
51
6.0
890
 38
Comparative example


177
 22
51
51
7.0
899
 62
Present invention example


178
 14
51
51
6.7
885
481
Present invention example


179
 14
51
52
6.7
908
955
Present invention example


180
 13
52
53
5.2
891

1258

Comparative example


181
 11
53
50
6.6
907
466
Present invention example


182
 12
50
52
6.8
881
476
Present invention example


183
 21
54
53
6.5
880
478
Present invention example


184
 14
51
56
7.4
895
486
Present invention example


185
 12
50
53
6.4
883
489
Present invention example


186
 20
54
52
5.2
911
482
Present invention example


187
 13
50
50
6.2
883
492
Present invention example


188
 13
53
50
5.3
899
488
Present invention example





The underline indicates that the manufacturing condition is not preferable.
















TABLE 3A









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value
Tensile
Load at



facturing
Steel


softened
densitis of texture of prior
of block
strength
½ stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





1
1



6.6
0.69

2083

8149
Comparative example


 2
 2



4.4
0.81
2306
8131
Present invention example


 3
 3



9.0
0.74
2445
8090
Present invention example


 4
 4



4.7
0.70
2521
8073
Present invention example


 5
 5



4.0
0.76
2762
8129
Present invention example


 6
 6



4.4
0.68
2855
8151
Present invention example


7
7



9.0
0.74
2937

7826

Comparative example


8
8



8.8
0.70

2214

8146
Comparative example


 9
 9



8.6
0.80
2325
8127
Present invention example


10
10



4.0
0.85
2436
8152
Present invention example


11
11



9.7
0.75
2463
8120
Present invention example


12
12



5.6
0.85
2387
8137
Present invention example


13
13



10.1 
0.77
2361
8153
Present invention example


14
14



3.4
0.71
2385
8089
Present invention example


15
15



4.9
0.84
2468
8091
Present invention example


16
16



8.3
0.70
2317
8119
Present invention example



17


17




9.8
0.78

2216

8076
Comparative example



18


18




6.0
0.82

2187

8072
Comparative example


19
19



3.9
0.74
2341
8128
Present invention example


20
20



4.4
0.81
2460
8148
Present invention example


21
21



9.4
0.79
2418
8080
Present invention example


22
22



8.2
0.78
2372
8081
Present invention example


23
23



4.6
0.73
2520
8093
Present invention example



24


24





2.1

0.85
2377

8004

Comparative example


25
25



4.0
0.79
2400
8093
Present invention example


26
26



9.6
0.85
2392
8148
Present invention example


27
27



9.3
0.72
2451
8093
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









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value
Tensile
Load at



facturing
Steel


softened
densitis of texture of prior
of block
strength
½ stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





28
28



7.4
0.81
2469
8130
Present invention example


29
29



4.6
0.71
2478
8053
Present invention example



30


30





2.7

0.69
2420

7832

Comparative example


31
31



4.1
0.85
2496
8141
Present invention example


32
32



9.8
0.73
2367
8102
Present invention example


33
33



7.1
0.84
2493
8139
Present invention example


34
34



10.3 
0.79
2527
8077
Present invention example


35
35



6.1
0.75
2377
8067
Present invention example



36


36





2.8

0.83
2416

7838

Comparative example


37
37



6.7
0.81
2385
8099
Present invention example


38
38



6.9
0.70
2374
8116
Present invention example


39
39



3.5
0.83
2384
8134
Present invention example


40
40



3.8
0.72
2353
8150
Present invention example


41
41



4.2
0.68
2525
8077
Present invention example



42


42





1.7

0.72
2418

7972

Comparative example


43
43



5.2
0.73
2549
8125
Present invention example


44
44



9.0
0.69
2500
8076
Present invention example


45
45



9.1
0.73
2546
8146
Present invention example


46
46



9.2
0.82
2389
8096
Present invention example


47
47



4.1
0.72
2460
8056
Present invention example



48


48





2.2

0.77
2369

7885

Comparative example



49


49





2.4

0.85
2526

7913

Comparative example


50
50



6.9
0.79
2430
8065
Present invention example


51
51



8.8
0.84
2547
8125
Present invention example


52
52



8.0
0.79
2379
8096
Present invention example


53
53



9.1
0.78
2394
8143
Present invention example


54
54



9.7
0.69
2476
8075
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









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value
Tensile
Load at



facturing
Steel


softened
densities of texture of prior
of block
strength
½ stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





55
55



6.0
0.77
2473
8134
Present invention example


56
56



6.1
0.81
2417
8086
Present invention example


57
57



6.8
0.76
2437
8144
Present invention example


58
58



6.8
0.85
2447
8058
Present invention example



59


59





2.6

0.76
2547

7838

Comparative example



60


60




8.0
0.68

2175

8124
Comparative example


61
61



9.2
0.72
2311
8085
Present invention example


62
62



9.8
0.79
2363
8128
Present invention example


63
63



5.5
0.79
2355
8103
Present invention example


64
64



6.2
0.68
2375
8081
Present invention example


65
65



4.7
0.80
2484
8120
Present invention example


66
66



5.8
0.81
2352
8148
Present invention example


67
67



6.1
0.75
2454
8091
Present invention example


68
68



3.9
0.83
2547
8066
Present invention example



69


69





1.9

0.76
2375

7962

Comparative example



70


70




3.7
0.77

2226

8120
Comparative example


71
71



7.4
0.79
2374
8117
Present invention example


72
72



4.1
0.83
2534
8097
Present invention example


73
73



3.5
0.68
2366
8092
Present invention example


74
74



7.3
0.76
2440
8121
Present invention example


75
75



6.0
0.74
2355
8089
Present invention example


76
76



6.6
0.72
2533
8146
Present invention example


77
77



7.2
0.75
2486
8070
Present invention example



78


78





2.3

0.71
2465

7953

Comparative example



79


79




8.3
0.80

2298

8149
Comparative example


80
80



7.9
0.78
2336
8130
Present invention example


81
81



7.0
0.82
2375
8129
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









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value of
Tensile
Load at



facturing
Steel


softened
densities of texture of prior
block sizes
strength
½ stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





 82
 82



5.9
0.80
2388
8095
Present invention example


 83
 83



8.0
0.73
2481
8126
Present invention example


 84
 84



4.5
0.81
2509
8077
Present invention example


 85
 85



10.3 
0.77
2444
8116
Present invention example


 86
 86



3.8
0.73
2441
8128
Present invention example


87
87




2.6

0.80
2457

7963

Comparative example


88
88



6.4
0.79

2244

8117
Comparative example


 89
 89



6.7
0.81
2328
8119
Present invention example


 90
 90



3.5
0.81
2451
8154
Present invention example


 91
 91



8.4
0.82
2390
8104
Present invention example


 92
 92



3.5
0.77
2442
8117
Present invention example


 93
 93



4.0
0.84
2489
8112
Present invention example


 94
 94



7.1
0.80
2414
8136
Present invention example


 95
 95



4.2
0.82
2426
8091
Present invention example


96
96




2.2

0.68
2403

7889

Comparative example


97
97



3.9
0.81

2209

8108
Comparative example


 98
 98



3.3
0.71
2348
8089
Present invention example


 99
 99



7.8
0.80
2528
8148
Present invention example


100
100



3.7
0.71
2542
8102
Present invention example


101
101



7.0
0.80
2400
8143
Present invention example


102
102



6.9
0.77
2438
8120
Present invention example


103
103



6.7
0.78
2394
8114
Present invention example


104
104



5.5
0.80
2414
8055
Present invention example



105


105





2.1

0.77
2426

7859

Comparative example


106
106



10.3 
0.82
2451
8074
Present invention example


107
107



7.4
0.78
2479
8138
Present invention example


108
108



7.8
0.85
2470
8106
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









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value
Tensile
Load at



facturing
Steel


softened
densities of texture of prior
of block
strength
½ stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





109
109



8.3
0.70
2492
8115
Present invention example


110
110



6.8
0.72
2424
8140
Present invention example


111
111



8.2
0.69
2354
8078
Present invention example


112
112



6.9
0.78
2530
8074
Present invention example


113
113



8.1
0.78
2400
8152
Present invention example


114
114



10.2 
0.83
2419
8131
Present invention example


115
115



3.3
0.80
2529
8093
Present invention example


116
116



7.8
0.77
2414
8103
Present invention example


117
117



9.2
0.72
2484
8121
Present invention example


118
118



9.3
0.82
2541
8084
Present invention example


119
119



6.7
0.84
2390
8090
Present invention example


120
120



7.7
0.69
2415
8138
Present invention example


121
121



3.2
0.70
2502
8154
Present invention example


122
122



10.1 
0.69
2512
8147
Present invention example


123
123



6.7
0.73
2465
8112
Present invention example


124
124



7.7
0.71
2362
8112
Present invention example


125
125



9.2
0.72
2434
8126
Present invention example


126
126



6.5
0.83
2524
8119
Present invention example


127
127



7.5
0.68
2508
8136
Present invention example


128
128



5.8
0.81
2409
8137
Present invention example


129
129



5.3
0.79
2478
8093
Present invention example


130
130



3.4
0.80
2464
8128
Present invention example


131
131



9.7
0.75
2383
8118
Present invention example


132
132



9.5
0.85
2545
8117
Present invention example


133
133



5.5
0,83
2464
8081
Present invention example


134
134



3.4
0.77
2396
8107
Present invention example


135
135



3.6
0.85
2429
8141
Present invention example



















TABLE 3F









Hot stamped component

















Manu-



Partially
Maximum value of pole
Average value
Tensile
Load at



facturing
Steel


softened
densities of texture of prior
of block
strength
1/2 stroke



No.
No.
Plating
Tempering
region
austenite -
sizes μm
MPa
N
Notes





136
136



8.1
0.80
2458
8081
Present invention example


137
137



10.3 
0.78
2460
8146
Present invention example


138
138



7.8
0.79
2527
8126
Present invention example


139
139



7.6
0.73
2494
8134
Present invention example


140
140



8.7
0.85
2501
8074
Present invention example


141
141



4.6
0.77
2531
8092
Present invention example


142
142



7.7
0.73
2372
8106
Present invention example


143
143



4.4
0.83
2396
8078
Present invention example


144
144



9.1
0.85
2464
8128
Present invention example


145
145



9.9
0.68
2510
8122
Present invention example


146
146



9.4
0.79
2376
8073
Present invention example


147
147



3.7
0.68
2527
8107
Present invention example


148
148



6.5
0.85
2457
8111
Present invention example


149
149



4.3
0.79
2396
8137
Present invention example


150
150



9.2
0.79
2398
8132
Present invention example


151
151



9.9
0.73
2509
8134
Present invention example



152

 11




1.9

0.75
2425

7964

Comparative example



153

 11




1.8

0.72
2549

7965

Comparative example



154

 14




2.2

0.79
2441

7982

Comparative example



155

 22




2.4

0.84
2502

8002

Comparative example



156

 14




2.7

0.80
2491

8011

Comparative example



157

 20




2.8

0.72
2466

8039

Comparative example



158

 20




2.2

0.84
2424

7995

Comparative example



159

 14




2.5

0.81
2501

8011

Comparative example



160

 12




2.3

0.78
2372

7896

Comparative example



161

 22




2.1

0.71
2359

7923

Comparative example



162

 14




2.4

0.71
2451

7984

Comparative example





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
















TABLE 3G









Hot stamped component






















Maximum value of
Average

Load



Manu-



Partially
pole densities of
value of
Tensile
at ½



facturing
Steel


softened
texture of prior
block sizes
strength
stroke



No.
No.
Plating
Tempering
region
austenite -
μm
MPa
N
Notes





163
21
aluminum plating


9.4
0.78
2547
8104
Present invention example


164
12
aluminum-galvanized


9.5
0.73
2512
8117
Present invention example


165
13
aluminum-silicon


5.1
0.71
2540
8132
Present invention example




plating









166
11
hot-dip galvanized


6.1
0.74
2399
8116
Present invention example


167
22
electrogalvanized


6.7
0.73
2487
8147
Present invention example


168
21
galvannealed


6.6
0.80
2490
8098
Present invention example


169
11
zinc-nickel plating


7.5
0.75
2387
8073
Present invention example


170
14
aluminum-


5.8
0.72
2540
8090
Present invention example




magnesium-zinc-











based plating










171

22




2.5

0.91

2265


7898

Comparative example


172
22



7.9
0.88
2334
8056
Present invention example


173
14



9.2
0.78
2418
8075
Present invention example


174
20



8.3
0.93
2386
8062
Present invention example



175

22




1.9


1.31


2156


7762

Comparative example


176
14




2.4

0.87

2259


7930

Comparative example


177
22



8.2
0.75
2346
8067
Present invention example


178
14



9.6
0.79
2481
8111
Present invention example


179
14



7.6
0.85
2335
8056
Present invention example



180

13




2.2


1.27


2203


7991

Comparative example


181
11

Tempering

8.9
0.76
2456
8097
Present invention example





temperature 153° C.








182
12

Tempering

9.3
0.84
2363
8140
Present invention example





temperature 172° C.








183
21

Tempering

9.5
0.71
2531
8104
Present invention example





temperature 205° C.








184
14

Tempering

6.5
0.79
2434
8092
Present invention example





temperature 339° C.








185
12

Tempering

7.2
0.73
2354
8121
Present invention example





temperature 432° C.








186
20

Tempering

10.2 
0.71
2369
8151
Present invention example





temperature 515° C.








187
13

Tempering

5.8
0.81
2459
8137
Present invention example





temperature 588° C.








188
13


Partially
4.1
0.78
2448
8126
Present invention example






softened











treatment





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






From Tables 3A to 3G, it can be seen that the hot-stamping formed bodies according to the present invention examples had high strength and excellent bendability.


On the other hand, it can be seen that in the hot-stamping formed bodies according to comparative examples, one or more of the properties deteriorated.


INDUSTRIAL APPLICABILITY

According to the above-described aspects of the present invention, it is possible to provide a hot stamped component having high strength and excellent bendability.

Claims
  • 1. A hot stamped component comprising, as a chemical composition, by mass %: C: 0.40% to 0.70%;Si: 0.010% to 3.000%;Mn: 0.10% or more and less than 0.60%;P: 0.100% or less;S: 0.0100% or less;N: 0.0100% or less;O: 0.0200% or less;Al: 0.0010% to 0.5000%;Nb: 0.0010% to 0.1000%;Ti: 0.010% to 0.100%;Cr: 0.010% to 1.000%;Mo: 0.050% to 1.000%;B: 0.0005% to 0.0100%;Co: 0% to 3.00%;Ni: 0% to 3.00%;Cu: 0% to 3.00%;V: 0% to 3.00%;W: 0% to 3.00%;Ca: 0% to 0.1000%;Mg: 0% to 1.0000%;REM: 0% to 1.0000%;Sb: 0% to 1.000%;Sn: 0% to 1.000%;Zr: 0% to 1.000%;As: 0% to 0.100%; anda remainder: Fe and impurities,in a position at ¼ of a sheet thickness from a surface,in a texture of prior austenite, a maximum value of pole densities of an orientation group expressed by Euler angles of Φ=60° to 90°, φ1=60° to 90°, and φ2=450 is 3.0 or more,an average value of block sizes of martensite, tempered martensite and bainite is 1.20 m or less.
  • 2. The hot stamped component according to claim 1 comprising, as the chemical composition, by mass %, one or more of: Co: 0.01% to 3.00%;Ni: 0.01% to 3.00%;Cu: 0.01% to 3.00%;V: 0.01% to 3.00%;W: 0.01% to 3.00%;Ca: 0.0001% to 0.1000%;Mg: 0.0001% to 1.0000%;REM: 0.0001% to 1.0000%;Sb: 0.001% to 1.000%;Sn: 0.001% to 1.000%;Zr: 0.001% to 1.000%; andAs: 0.001% to 0.100%.
Priority Claims (1)
Number Date Country Kind
2022-090847 Jun 2022 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2023/020238 5/31/2023 WO