Hot-stamping formed body

Abstract
This hot-stamping formed body has a predetermined chemical composition and has a metallographic structure consisting of, by area ratio, a total of 10% to 30% of ferrite and granular bainite and a remainder in microstructure consisting of one or more of martensite, bainite, and tempered martensite, and, in textures of a surface layer region and an inside region, ratios between a pole density of an orientation group consisting of {001}<1-10> to {001}<−1-10> and a pole density of an orientation group consisting of {111}<1-10> to {111}<−1-12> are controlled.
Description
TECHNICAL FIELD OF THE INVENTION

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


Priority is claimed on Japanese Patent Application No. 2020-084591, filed May 13, 2020, the content of which is incorporated herein by reference.


BACKGROUND ART

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


In order to solve this issue, the application of 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 technique that achieves both the formability of a steel sheet into a vehicle member and the strength of the vehicle, member by performing the hardening of the steel sheet in a die at the same time as press working.


In order to obtain a higher effect of reducing the weight of a vehicle body from a vehicle member into which a steel sheet is formed by hot stamping, it is necessary to obtain a member that has high strength and is also excellent in collision characteristics. As a technique for improving the collision characteristics of a vehicle member, particularly, a technique for improving the bendability of the vehicle member is being studied.


Patent Document 1 discloses a high strength pressed component having excellent impact absorption characteristics, in which the hardness of the pressed component in the sheet thickness center is Hv400 or more, a soft layer having a hardness of Hv300 or less is provided in a surface layer of the pressed component, and the thickness of the soft layer is 20 to 200 μm.


Patent Document 2 discloses a high strength cold-rolled steel sheet having excellent uniform elongation and hole expansibility, in which the texture in the center portion of the steel sheet is controlled.


At the time of bending distortion, distortion starts from the surface of a vehicle member, and the distortion gradually progresses toward the inside of the vehicle member. Therefore, in order to further improve the bendability of the vehicle member, it is effective to enhance the bending distortion capability of the surface layer of the vehicle member and then enhance the bending distortion capability of the inside of the vehicle member. In Patent Documents 1 and 2, improvement in the bending distortion capabilities of both the surface layer area and the inside of the vehicle member are not taken into account.


In addition, when the surface layer of a vehicle member is softened in order to improve the bendability of the vehicle member, there is a problem of the deterioration of the ductility.


PRIOR ART DOCUMENT
Patent Document





    • [Patent Document 1] Japanese Unexamined Patent Application, First Publication No. 2015-30890

    • [Patent Document 2] PCT International Publication No. WO2012/144567





DISCLOSURE OF THE INVENTION
Problems to be Solved by the Invention

The present invention has been made in view of the above-mentioned problem. An object of the present invention is to provide a hot-stamping formed body having excellent strength, bendability, and ductility.


Means for Solving the Problem

The gist of the present invention is as follows.


(1) A hot-stamping formed body according to an aspect of the present invention contains, as a chemical composition, by mass %,

    • C: 0.15 to 0.50%,
    • Si: 0.0010% to 3.000%,
    • Mn: 0.30% to 3.00%,
    • Al: 0.0002% to 2.000%,
    • P: 0.100% or less,
    • S: 0.1000% or less,
    • N: 0.0100% or less,
    • Nb: 0% to 0.15%,
    • Ti: 0% to 0.15%,
    • V: 0% to 0.15%,
    • Mo: 0% to 1.0%,
    • Cr: 0% to 1.0%,
    • Cu: 0% to 1.0%,
    • Ni: 0% to 1.0%,
    • B: 0% to 0.0100%,
    • Ca: 0% to 0.010%,
    • REM: 0% to 0.30%, and
    • a remainder consisting of Fe and an impurity,
    • in which the hot-stamping formed body has a metallographic structure consisting of, by area ratio, a total of 10% to 30% of ferrite and granular bainite and a remainder in microstructure consisting of one or more of martensite, bainite, and tempered martensite,
    • in a texture between a surface and a sheet thickness ¼ position from the surface, a ratio between a pole density of an orientation group consisting of {001}<1-10> to {001}<−1-10> and a pole density of an orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 1.8, and
    • in a texture between the sheet thickness ¼ position from the surface and a sheet thickness ½ position from the surface, a ratio between a pole density of an orientation group consisting of {001}<1-10> to {001}<−1-10> and a pole density of an orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 2.3.


(2) The hot-stamping formed body according to (1) may further contain, as the chemical composition, by mass %, one or more of the group consisting of

    • Nb: 0.05% to 0.15%,
    • Ti: 0.05% to 0.15%,
    • V: 0.05% to 0.15%,
    • Mo: 0.05% to 1.0%,
    • Cr: 0.05% to 1.0%,
    • Cu: 0.05% to 1.0%,
    • Ni: 0.05% to 1.0%,
    • B: 0.0001% to 0.0100%,
    • Ca: 0.001% to 0.010%, and
    • REM: 0.001% to 0.30%.


(3) The hot-stamping formed body according to (1) or (2), in which a decarburization index may be 0.085 or more.


Effects of the Invention

According to the above-mentioned aspect of the present invention, it is possible to provide a hot-stamping formed body having excellent strength, bendability, and ductility.







EMBODIMENTS OF THE INVENTION

The present inventors studied a method enabling not only for a tensile (maximum) strength of 1.5 to 2.5 GPa and excellent bendability to be obtained but also for the deterioration of ductility to be suppressed after hot stamping. As a result, the present inventors found that, in a hot-stamping formed body, when the surface layer of the steel sheet is softened, and furthermore, the texture at a predetermined position in the sheet thickness direction is controlled, it is possible to, obtain a high strength and superior bendability than ever and to suppress the deterioration of ductility.


The texture is affected by the texture and the carbon concentration of the metallographic structure before hot stamping. Therefore, the present inventors found that, in order to obtain a desired texture in the hot-stamping formed body, it is effective to control the texture in the steel sheet after hot rolling and, furthermore, to reduce the amount of carbon in the surface layer of the steel sheet during the subsequent annealing.


Hereinafter, a steel sheet for hot stamping for manufacturing a hot-stamping formed body according to the present embodiment by hot stamping will be described in detail. First, the reasons for limiting the chemical composition of the steel sheet for hot stamping will be described.


Numerical limiting ranges expressed below using “to” include the lower limit and the upper limit in the ranges. Numerical values expressed with ‘more than’ and ‘less than’ are not included in numerical ranges. Regarding the chemical composition, “%” indicates “mass %” in all cases.


The steel sheet for hot stamping for manufacturing the hot-stamping formed body according to the present embodiment by hot stamping contains, as a chemical composition, mass %, C: 0.15% to 0.50%. Si: 0.0010% to 3.000%, Mn: 0.30% to 3.00%, Al: 0.0002% to 2.000% P: 0.100% or less S: 0.1000% or less, N: 0.0100% or less, Nb: 0% to 0.15%, Ti: 0% to 0.15%, V: 0% to 0.15%, Mo: 0% to 1.0%, Cr: 0% to 1.0%, Cu: 0% to 1.0%. Ni: 0% to 1.0%. B: 0% to 0.0100%, Ca: 0% to 0.010%, REM: 0% to 0.30%, and a remainder consisting of Fe and an impurity.


Hereinafter, each element will be described.


C: 0.15% to 0.50%


C is an element that improves the strength of the hot-stamping formed body. In a case where the C content is less than 0.15%, the desired strength of the hot-stamping formed body cannot be obtained. For this reason, the C content is set to 0.15% or more. The C content is preferably 0.17% or more, 0.20% or more, or 0.23% or more. On the other hand, when the C content is more than 0.50%, it is not possible to obtain excellent bendability. For this reason, the C content is set to 0.50% or less. The C content is preferably 0.46% or less or 0.43% or less.


Si: 0.0010% to 3.000%


Si is an element that improves the strength of the hot-stamping formed body by solid solution strengthening. When the Si content is less than 0.0010%, it is not possible to obtain a desired strength. For this reason, the Si content is set to 0.0010% or more. The Si content is preferably 0.050% or more, 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 it is not possible to obtain a desired metallographic structure. For this reason, the Si content is set to 3.000% or less. The Si content is preferably 2.700% or less or 2.500% or less.


Mn: 0.30% to 3.00%


Mn is an element that improves the hardenability of steel. In order to improve the hardenability and thereby obtain a desired amount of martensite after hot stamping, the Mn content is set to 0.30% or more. The Mn content is preferably 0.50% or more, 0.70% or more, or 1.00% or more. On the other hand, when the Mn content is more than 3.00%, cracking attributed to Mn segregation is likely to occur, and it is not possible to obtain excellent bendability. For this reason, the Mn content is set to 3.00% or less. The Mn content is preferably 2.70% or less, 2.50% or less, or 2.30% or less.


Al: 0.0002% to 2.000%


Al is an element that improves the distortion capability by deoxidizing molten steel to suppress the formation of oxide serving as the origin of fracture and improves the bendability of the hot-stamping formed body. When the Al content is less than 0.0002%, deoxidation is not sufficiently performed, and a coarse oxide is formed, which makes it impossible to obtain the above-mentioned effect. For this reason, the Al content is set to 0.0002% or more. The Al content is preferably 0.001% or more. On the other hand, when the Al content exceeds 2.000%, a coarse oxide is formed in steel, and the bendability of the hot-stamping formed body deteriorates. For this reason, the Al content is set to 2.000% or less. The Al content is preferably 1.700% or less or 1.500% or less.


P: 0.100% or Less


P is an impurity element and serves as the origin of fracture by being segregated at a grain boundary. For this reason, the P content is limited to 0.100% or less. The P content is preferably 0.050% or less. The lower limit of the P content is not particularly limited, but reduction of the P content to less than 0.0001% significantly increases the dephosphorization cost, which is not preferable economically. For this reason, the P content may be set to 0.0001% or more.


S: 0.1000% or Less


S is an impurity element and forms an inclusion in steel. Since this inclusion serves as the origin of fracture, the S content is limited to 0.1000% or less. The S content is preferably 0.0500% or less or 0.0300% or less. The lower limit of the S content is not particularly limited, but reduction of the S content to less than 0.0001% significantly increases the desulfurization cost, 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 is an impurity element and forms nitride in steel. Since this nitride serves as the origin of fracture, the N content is limited to 0.0100% or less. The N content is preferably 0.0050% or less. The lower limit of the N content is not particularly limited, but reduction of the N content to less than 0.0001% significantly increases the denitrification cost, which is not preferable economically. For this reason, the N content may be set to 0.0001% or more.


The remainder of the chemical composition of the steel sheet for hot stamping 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 characteristics of the hot-stamping formed body according to this embodiment do not deteriorate, are exemplary examples of the impurities.


The steel sheet for hot stamping may contain the following elements as arbitrary elements instead of a part of Fe. The contents of the following arbitrary elements, which are obtained in a case where the following arbitrary elements are not contained, are 0%.


Nb: 0% to 0.15%


Ti: 0% to 0.15%


V: 0% to 0.15%


Nb and Ti have an effect on improvement in the strength of the hot-stamping formed body by precipitation hardening by forming a carbonitride in steel. In order to reliably exhibit this effect, the content of even one of Nb, Ti, and V is preferably set to 0.05% or more. On the other hand, in a case where the content of even one of Nb, Ti, and V is set to more than 0.15%, a large amount of a carbonitride is formed in steel, and the ductility of the hot-stamping formed body deteriorates. Therefore, the Nb content, Ti content, and V content are each set to 0.15% or less.


Mo: 0% to 1.0%


Cr: 0% to 1.0%


Cu: 0% to 1.0%


Ni: 0% to 1.0%


Mo and Cr have an action of increasing the strength of the hot-stamping formed body by forming a solid solution in prior austenite grains during heating before hot stamping. In order to reliably obtain this effect, the content of even one of Mo, Cr, Cu, and Ni is preferably set to 0.05% or more. On the other hand, since the effect is saturated even when a large amount of Mo, Cr Cu, and Ni are contained, the Mo content, the Cr content, the Cu content, and the Ni content are each preferably set to 1.0% or less.


B: 0% to 0.0100%


B is an element that improves the hardenability of steel. In order to reliably obtain this effect, the B content is preferably set to 0.0001% or more. On the other hand, even when the B content is set to more than 0.0100%, the effect on improvement in the hardenability is saturated. For this reason, the B content is set to 0.0100% or less.


Ca: 0% to 0.010%


REM: 0% to 0.30%


Ca and REM are elements that improve the distortion capability by suppressing the formation of an oxide serving as the origin of fracture and improve the bendability of the hot-stamping formed body. In order to reliably obtain this effect, the content of even one of Ca and REM is preferably set to 0.001% or more. On the other hand, since the effect is saturated even when a large amount of Ca and REM are contained, the Ca content is set to 0.010% or less, and the REM content is set to 0.30% or less.


In this 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.


The above-mentioned chemical composition of the steel sheet for hot stamping may be measured by an ordinary analysis method. For example, the chemical composition of the above-mentioned hot-stamping formed body may be measured using inductively coupled plasma-atomic emission spectrometry (ICP-AES). C and S may be measured using a combustion-infrared absorption method and N may be measured using an inert gas fusion-thermal conductivity method. In a case where a plating layer is provided on the surface of the steel sheet for hot stamping, the chemical composition may be analyzed after the plating layer is removed by mechanical grinding.


Next, the metallographic structure of the steel sheet for hot stamping for manufacturing the hot-stamping formed body according to the present embodiment by hot stamping will be described.


The steel sheet for hot stamping has a metallographic structure consisting of, by area ratio, a total of 20% to 80% of ferrite, granular bainite, bainite, and martensite and the remainder in microstructure consisting of pearlite and a carbide. Regarding the metallographic structure to be described below, “%” indicates “area %” in all cases.


Ferrite, Granular Bainite, Bainite, and Martensite: 20% to 80%


Ferrite, granular bainite, bainite, and martensite are necessary structures to obtain a desired texture in a hot-stamping formed body. When the total area ratio of these structures is less than 20%, it is not possible to obtain a desired texture in the hot-stamping formed body. For this reason, the area ratio of the ferrite is set to 20% or more. The area ratio of the ferrite is preferably 30% or more or 40% or more. On the other hand, when the area ratio of these structures is more than 80%, carbon is concentrated in pearlite, which is the remainder it becomes difficult for a carbide to dissolve during hot stamp heating, and the carbide serves as the origin of cracking during distortion. Therefore, the area ratio is set to 80% or less. The area ratio is preferably 70% or less or 60% or less.


Remainder in Microstructure: Pearlite and Carbide


The remainder in microstructure of the metallographic structure of the steel sheet for hot stamping consists of pearlite and a carbide. In the metallographic structure of the steel sheet for hot stamping, structures other than the above-mentioned structure, pearlite, and the carbide are not contained, the area ratio of the remainder in microstructure may be set to 20% to 80%.


Measurement Method of Metallographic Structure of Steel Sheet for Hot Stamping


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


After being polished using silicon carbide paper having a grit of #600 to #1500, the cross section of the sample is finished as a mirror surface using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in diluted solution of alcohol or the like or pure water and finish-polished using a colloidal silica solution. Next, analysis is performed in a region that has a length of 50 μm and is present between a depth corresponding to ⅛ of the sheet thickness from the surface and a depth corresponding to ⅜ of the sheet thickness from the surface at an arbitrary position on the cross section of the sample in a longitudinal direction at an analysis rate of 200 to 300 points/second using an EBSD analyzer including a schottky emission scanning electron microscope (JSM-7001F manufactured by JEOL Ltd.) and an EBSD detector (DVC 5-type detector manufactured by TSL Solutions). The area ratio of a region where the crystal structure is bcc is calculated using a “Phase Map” function installed in software “OIM Analysis (registered trademark)” included in an EBSD analyzer, whereby the total area ratio of the ferrite, the granular bainite, the bainite, and the martensite can be obtained.


The pearlite and the carbide can be identified by the following method. After being polished using silicon carbide paper having a grit of #600 to #1500, the cross section of the sample is finished as a mirror surface using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in diluted solution of alcohol or the like or pure water and Nital etching is performed. Then, photographs having a plurality of visual fields are taken using a schottky emission scanning electron microscope (JSM-7001F manufactured by JEOL Ltd.) in a region that has a length of 50 μm and is present between a depth corresponding to ⅛ of the sheet thickness from the surface and a depth corresponding to ⅜ of the sheet thickness from the surface at an arbitrary position on the cross section of the sample in a longitudinal direction. Evenly spaced grids are drawn in the taken photographs, and structures at grid points are identified. The number of grid points corresponding to each structure is obtained and is divided by the total number of grid points, so that the area ratio of each structure is obtained. The area ratio can be more accurately obtained as the total number of grid points is larger. In this embodiment, grid spacings are set to 2 μm×2 μm and the total number of grid points is set to 1500. Particles with bright brightness are regarded as the carbide, and a region where regions with bright brightness are disposed in a granular or sheet shape and in a lamellar shape is regarded as the pearlite.


Next, the texture of the steel sheet for hot stamping for manufacturing the hot-stamping formed body according to the present embodiment by hot stamping will be described.


In the steel sheet for hot stamping, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 1.5 in the texture between the surface and the sheet thickness ¼ position from the surface, and the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 2.0 in the texture between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from the surface.


The orientation group consisting of {001}<1-10> to {001}<−1-10> includes crystal orientations of {001}<1-10>, {001}<1-20>, {001}<0-10>, and {001}<−1-10>. The orientation group consisting of {111}<1-10> to {111}<−1-12> includes crystal orientations of {111}<1-10>, {111}<1-21>, {111}<0-11>, and {111}<−1-12>.


Texture between surface and sheet thickness ¼ position from surface: Ratio between pole density of orientation group consisting of {001}<1-10> to {001}<−1-10> and pole density of orientation group consisting of {111}<1-10> to {111}<−1-12< being less than 1.5


In the texture between the surface and the sheet thickness ¼ position from the surface (hereinafter, referred to as the surface layer region in some cases), the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12< is set to less than 1.5.


When the texture in the surface layer region of the steel sheet for hot stamping is preferably controlled, it is possible to suppress carbon recuperation in the surface layer region (diffusion of carbon from the inside region into the surface layer region having a low C concentration) during heating for hot stamping, and, when a texture that easily relaxes strain introduced by bending distortion in the surface layer region where energy attributed to distortion is absorbed such as a vicinity of the surface of the steel sheet is, developed, it, is possible to obtain a steel sheet for hot stamping having excellent bendability after hot stamping.


When the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12< of the texture in the surface layer region is 1.5 or more, the above-mentioned effect cannot be obtained. Therefore, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12< of the texture in the surface layer region is set to, less than 1.5. The ratio is preferably less than 1.2.


The ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture in the surface layer region may be set to 0.4 or more from the viewpoint of ensuring the strength of the hot-stamping formed body.


Texture between sheet thickness ¼ position from surface and sheet thickness ½ position from surface: Ratio between pole density of orientation group consisting of {001}<1-10> to {001}<−1-10> and pole density of orientation group consisting of {111}<1-10> to {111}<−1-12> being less than 2.0


In the texture between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from surface (hereinafter, referred to as the inside region in some cases), the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is set to less than 2.0.


When the texture in the inside region of the steel sheet for hot stamping is preferably controlled, it is possible to develop a texture including grain boundaries that do not easily fracture in a region that withstands a load such as the vicinity of the inside of the steel sheet and also to improve the load capacity while maintaining excellent bendability. When the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-120> of the texture in the inside region is 2.0 or more, the above-mentioned effect cannot be obtained. Therefore, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture in the inside region is set to less than 2.0. The ratio is preferably less than 1.6.


The ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture in the inside region may be set to 0.4 or more from the viewpoint of ensuring the toughness.


Measurement Method of Pole Density


The pole densities of the surface layer region and the inside region are measured by the following method.


The pole densities of the surface layer region and the inside region can be obtained from an orientation distribution function (ODF) that displays a three-dimensional texture calculated by computing, using spherical harmonics, an orientation data measured by an electron back scattering diffraction (EBSD) method using a device in which a scanning electron microscope and an EBSD analyzer are combined and OIM Analysis (registered trademark) manufactured by TSL Solutions.


The measurement ranges are a region between the surface and the sheet thickness ¼ position from the surface (a region between the surface as the start point and the sheet thickness ¼ position in the sheet thickness direction from the surface as the end point) for the surface layer region and a region between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from the surface (a region between the sheet thickness ¼ position in the sheet thickness direction from the surface as the start point and the sheet thickness ½ position in the sheet thickness direction from the surface as the end point) for the inside region. The measurement pitches are set to 5 μm/step.


A value obtained by dividing the average value of the pole densities of the orientation group consisting of {001}<1-10> to {001}<−1-10> by the average value of the pole densities of the orientation group consisting of {111}<1-10> to {111}<−1-12> is regarded as the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12>.


It should be noted that {hkl} indicates a crystal plane parallel to a rolled surface and <uvw> indicates a crystal direction parallel to a rolling direction. That is, {hkl}<uvw> indicates a crystal in which {hkl} is oriented in the sheet surface normal direction and <uvw> is oriented in the rolling direction.


The above-mentioned steel sheet for hot stamping may have a plating layer on the surface. The plating layer provided on the surface makes it possible to improve the corrosion resistance after hot stamping. As the plating layer, an aluminum plating layer, an aluminum-zinc plating layer, an aluminum-silicon plating layer, a hot-dip galvanized layer, an electrogalvanized layer, a hot-dip galvannealed layer, or the like is an exemplary example.


Decarburization Index of Steel Sheet for Hot Stamping Being 0.085 or More


When the decarburization index of the steel sheet for hot stamping is preferably controlled, it is possible to promote the development of the texture including grain boundaries that do not easily fracture in a region that withstands a load such as the vicinity of the inside of the steel sheet and also to improve the load capacity while maintaining excellent bendability. The decarburization index is preferably 0.140 or more and more preferably 0.180 or more. Due to the calculation method of the decarburization index, the upper limit becomes 1.000.


Measurement Method of Decarburization Index


The decarburization index is an index that quantifies the amount of carbon reduced in the surface layer of the steel sheet and can be calculated by the following method. An element concentration distribution in the sheet thickness direction in the steel sheet for hot stamping is measured using a glow discharge optical emission spectrometry (GD-OES). Here, the measurement range is set to a depth of 200 μm from the outermost surface of the steel sheet, and the measurement intervals are set to 0.02 μm or less. All elements that are contained in the steel sheet for hot stamping are measured.


For steel sheets having a plating layer, a coating film, or the like on the surface, a part or all of the plating layer, coating, or the like is removed by mechanical polishing or chemical polishing such that measurement becomes possible up to a position 200 μm deep from the outermost surface of the steel sheet, and GD-OES measurement is performed. In the GD-OES measurement, a region where the iron concentration becomes 90 mass % or more is determined as the steel sheet, and a measurement point where the iron concentration becomes 90 mass % is defined as the outermost surface position of the steel sheet.


Next, the average value of the measurement values (1000 points or more) of the carbon concentration from the outermost surface position of the steel sheet to a depth of 180 μm to a depth of 200 μm is calculated, and this average value is regarded as the carbon concentration of the steel sheet base metal.


Alternatively, regarding the measurement value of the carbon concentration in a 20 μm region from the deepest portion toward the surface layer, in a case where the absolute value of the difference between the average value of the carbon concentrations in the 20 μm regions from the deepest portion toward the surface layer and the maximum value of the measurement values of the carbon concentrations in the 20 μm regions from the deepest portion toward the surface layer is 0.1% or less, and the absolute value of the difference between the average value of the carbon concentrations in the 20 μm regions from the deepest portion toward the surface layer and the minimum value of the measurement values of the carbon concentrations in the 20 μm regions from the deepest portion toward the surface layer is 0.1% or less, the average value of the carbon concentrations in the 20 μm regions from the deepest portion toward the surface layer may be regarded as the carbon concentration of the steel sheet base metal.


The unit depth is 20 μm, and the deepest portion refers to each deep position in a case where positions are marked every unit depth from the outermost surface position of the steel sheet to a depth position of 200 μm. For example, in a case where the deepest portion is 120 μm, “the measurement value of the carbon concentration in the 20 μm region from the deepest portion toward the surface layer” means the carbon concentration at a measurement point that is included between the 100 μm position and the 120 μm position.


The amount of the carbon concentration decreased per unit depth (a value obtained by subtracting the carbon concentration at each measurement point, from the carbon concentration of the base metal) is calculated from the outermost surface position of the steel sheet to the depth position of 200 μm, and the integrated value of the product of the unit depth and the amount of the carbon concentration decreased is obtained and regarded as the area of a carbon deficient region (area A). Next, the product of the carbon concentration of the base metal and 200 μm is regarded as a reference area (area B), and a value obtained by dividing the carbon deficient area (area A) by the reference area (area B) is regarded as the decarburization index.


Next, the hot-stamping formed body according to the present embodiment will be described. The hot-stamping formed body according to the present embodiment can be obtained by applying a manufacturing method to be described below to the above-described steel sheet for hot stamping. In the hot-stamping formed body according to the present embodiment, the texture is changed between the surface layer region and the inside region, whereby the bendability of the metallographic structure in the surface layer region is improved, and one or more of ferrite and granular bainite are formed to increase the ductility of the surface layer region. Specifically, in the surface layer region where energy attributed to bending distortion is absorbed, a texture where strain introduced due to bending distortion is easily relaxed is developed, and, in the inside region that has an influence on the load capacity, a texture including grain boundaries that do not easily fracture is developed. The chemical composition of the hot-stamping formed body according to the present embodiment is the same as the chemical composition of the above-described steel sheet for hot stamping and thus will not be described again.


The hot-stamping formed body according to the present embodiment has a metallographic structure consisting of, by area ratio, a total of 10% to 30% of ferrite and granular bainite and the remainder in microstructure consisting of one or more of martensite, bainite and tempered martensite, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 1.8 in the texture between the surface and the sheet thickness ¼ position from the surface, and the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 2.3 in the texture between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from the surface. Regarding the metallographic structure to be described below, “%” indicates “area %” in all cases.


Ferrite and Granular Bainite: Total of 10% to 30%


Ferrite and, granular bainite are soft structures having excellent ductility. When the area ratio of ferrite and granular bainite is less than 10% in total, desired ductility cannot be obtained. Therefore, in the hot-stamping formed body according to the present embodiment, the area ratio of ferrite and granular bainite is set to 10% or more in total. The area ratio is preferably 15% or more or 20% or more.


On the other hand, when the area ratio of ferrite and granular bainite is more than 30% in total, a desired strength cannot be obtained. Therefore, the area ratio of ferrite and granular bainite is set to 30% or less in total. The area ratio is preferably 27% or less or 25% or less.


In the present embodiment, a total of 10% to 30% of ferrite and granular bainite may be contained or 10% to 30% of one of ferrite or granular bainite may be contained.


Remainder in Microstructure: One or More of Martensite, Bainite, and Tempered Martensite


The hot-stamping formed body according to the present embodiment has a remainder in microstructure consisting of one or more of martensite, bainite, and tempered martensite. The area ratio of these remainder in microstructure is preferably set to 70% or more in order to obtain a desired strength. The area ratio is preferably 73% or more or 75% or more. In addition, in order to obtain desired ductility, the area ratio of these remainder in microstructure may be set to 90% or less, 85% or less, or 80% or less.


Measurement Method of Area Ratio of Metallographic Structure


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


After being polished using silicon carbide paper having a grit of #600 to #1500, the cross section of the sample is finished as a mirror surface using liquid in which diamond powder having a grain size in the range of 1 μm to 6 μm is dispersed in diluted solution of alcohol or the like or pure water. Then, the sample is polished for 8 minutes using colloidal silica not containing alkaline solution at a room temperature, and thus, strain introduced into the surface layer of the sample is removed. A region, which has a length of 50 μm and is present between a depth corresponding to ⅛ of the sheet thickness from the surface and a depth corresponding to ⅜ of the sheet thickness from the surface, is measured at a measurement interval of 0.1 μm at an arbitrary position on the cross section of the sample in a longitudinal direction by an electron back scatter diffraction method, and thus, crystal orientation information is obtained. An EBSD analyzer formed of a schottky emission scanning electron microscope (JSM-7001F manufactured by JEOL Ltd.) and an EBSD detector (DVC 5-type detector manufactured by TSL Solutions) is used for measurement. In this case, the degree of vacuum in the EBSD analyzer is set to 9.6×10−5 Pa or less, an accelerating voltage is set to 15 kV, an irradiation current level is set to 13, and the irradiation level of an electron beam is set to 62.


A region where the crystal structure is bcc is specified using the obtained crystal orientation information and “Phase Map” function of software “OIM Analysis (registered trademark)” included in an EBSD analyzer. Regions where the crystal structure is bcc are determined as martensite, bainite, tempered martensite, granular bainite, and ferrite. In these regions, regions where a grain average image misorientation value is more than 3.0° are determined as martensite, bainite, and tempered martensite using “Grain Average Misorientation” function of software “OIM Analysis (registered trademark)” included in the EBSD analyzer, and the total of these area ratios is calculated, thereby obtaining the total area ratio of “martensite, bainite, and tempered martensite”. Regions where a grain average misorientation value is 3.0° or less are determined as ferrite and granular bainite, and the total of these area ratios is calculated, thereby obtaining the total area ratio of “ferrite and granular bainite”.


Texture between surface and sheet thickness ¼ position from surface: Ratio between pole density of orientation group consisting of {001}<1-10> to {001}<−1-10> and pole density of orientation group consisting of {111}<1-10> to {111}<−1-12> being less than 1.8


In the texture between the surface and the sheet thickness ¼ position from the surface (surface layer region), when, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is set to less than 1.8, the bendability can be improved. Therefore, in the texture of the surface layer region, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is set to less than 1.8. The ratio is preferably less than 1.7 or less than 1.6.


The ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture of the surface layer region may be set to 0.4 or more from the viewpoint of ensuring the strength.


Texture between sheet thickness ¼ position from surface and sheet thickness ½ position from surface: Ratio between pole density of orientation group consisting of {001}<1-10> to {001}<−1-10> and pole density of orientation group consisting of {111}<1-10> to {111}<−1-12> being less than 2.3


In the texture between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from the surface (inside region), when the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-<10> to {111}<−1-12> is set to less than 2.3, the ductility can be improved. Therefore, in the texture of the inside region, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> is set to less than 2.3. The ratio is preferably less than 2.2 or less than 2.1.


The ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture of the inside region may be set to 0.4 or more from the viewpoint of ensuring the toughness.


The pole densities of the surface layer region and the inside region may be measured by the same method as that for the steel sheet for hot stamping. However, the rolling direction in the hot-stamping formed body may be determined by the following method.


First, a test piece is collected such that the sheet, thickness cross section of the hot-stamping formed body can be observed.


The sheet thickness cross section of the collected test piece is finished by mirror polishing and then observed using an optical microscope. The observation range is set to the overall thickness of the sheet thickness, and a region where the brightness is dark is determined as an inclusion. Among inclusions, in inclusions having a major axis length of 40 μm or more, a direction parallel to a direction where the inclusion extends is determined as the rolling direction.


The hot-stamping formed body according to the present embodiment may have a plating layer on a surface. The plating layer provided on the surface makes it possible to improve the corrosion resistance after hot stamping. As the plating layer, an aluminum plating layer, an aluminum-zinc plating layer, an aluminum-silicon plating layer, a hot-dip galvanized layer, an electrogalvanized layer, a hot-dip galvannealed layer, or the like is an exemplary example.


Decarburization Index of Hot-Stamping Formed Body being 0.085 or More


When the decarburization index of the hot-stamping formed body is preferably controlled, it is possible to promote the development of the texture including grain boundaries that do not easily fracture in a region that withstands a load such as the vicinity of the inside of the steel sheet and also to improve the load capacity while maintaining excellent bendability. The decarburization index is preferably 0.140 or more and more preferably 0.180 or more. Due to the calculation method of the decarburization index, the upper limit of the decarburization index becomes 1.000; however, in order to improve the load capacity as well while maintaining excellent bendability, the upper, limit is preferably 0.500 or less and more preferably 0.040 or less.


The decarburization index of the hot stamping formed body may be measured by the same method as that for the steel sheet for hot stamping.


Manufacturing Method of Steel Sheet for Hot Stamping


Hereinafter, a preferable manufacturing method of the steel sheet for hot stamping for manufacturing the hot-stamping formed body according to the present embodiment by hot stamping will be described.


First, it is preferable that a cast piece is heated to 1200° C. or higher and held for 20 minutes or longer and then, in a hot rolling process, a rolling which is 1 pass before a final rolling is performed in a temperature range of 850° C. to 900° C. at a rolling reduction of 8% to 30%. Next, the hot rolling is preferably completed in a temperature range of 800° C. or higher and lower than 850° C. at a rolling reduction of 6% to 12%. That is, the final rolling of the hot rolling is preferably performed in a temperature range of 800° C. or higher and lower than 850° C. at a rolling reduction of 6% to 12%.


It is preferable that, after 2.5 seconds or longer elapses from the end of the hot rolling, cooling is performed at an average cooling rate in a temperature range from the hot rolling end temperature to 450° C. of slower than 10° C./s. After that, the hot-rolled steel sheet is preferably coiled in a temperature range of 700° C., or lower. Furthermore, it is preferable that decarburization annealing is performed, thereby manufacturing a steel sheet for hot stamping having the above-described chemical composition.


The present inventors found that a texture that improves the bending distortion capability and the load capacity after hot stamping develops by transformation from austenite including a small amount of dislocation into ferrite or granular bainite. Therefore, when the rolling one pass before the final rolling is performed at lower than 850° C. or performed at a rolling reduction of larger than 30%, there is a case where the cast piece is finally rolled while the dislocation of austenite before transformation remains unrecovered, transformation from austenite including the dislocation to ferrite occurs, and the development of a desired texture is impaired.


On the other hand, when the rolling one pass before the final rolling is performed at higher than 900° C. or performed at a rolling reduction of smaller than 8%, there is a case where the recovery of dislocation is excessively promoted, the dislocation density in austenite becomes too low, and a desired texture cannot be obtained.


Therefore, the rolling one pass before the final rolling in the hot rolling is preferably performed in a temperature range of 850° C. to 900° C. at a rolling reduction of 8% to 30%.


When the final rolling is performed at lower than 800° C. or performed at a rolling reduction of larger than 12%, there is a case where the cast piece is finally rolled while the dislocation of austenite before transformation remains unrecovered, transformation from austenite including the dislocation to ferrite occurs, and the development of a desired texture is impaired.


On the other hand, when the final rolling is performed at 850° C. or higher or performed at a rolling reduction of smaller than 6%, there is a case where the recovery of dislocation is excessively promoted, and thus the dislocation density in austenite becomes too low, and a desired texture cannot be obtained.


Therefore, the final rolling of the hot rolling is preferably performed in a temperature range of 800° C. or higher and lower than 850° C. at a rolling reduction of 6% to 12%.


It is preferable to start cooling after 2.5 seconds or longer elapses from the end of the hot rolling. When a time of 2.5 seconds or longer is ensured before the start of the cooling, phase transformation to ferrite or granular bainite is promoted, and a desired texture can be sufficiently developed. When the elapsed time is shorter than 2.5 seconds, there is a case where a desired texture cannot be obtained.


After 2.5 seconds or longer elapses from the completion of the hot rolling, when the average cooling rate in a temperature range from the hot rolling end temperature to 450° C. is set to slower than 10° C./s, phase transformation to ferrite or granular bainite is promoted, and a desired texture can be sufficiently developed. When, the average cooling rate in the above-described temperature range is 10° C./s or faster, there is a case where a desired texture cannot be obtained.


The average cooling rate mentioned herein is defined as a value obtained by dividing a temperature difference between the start point and the end point of a set range by the elapsed time from the start point to the end point.


When the coiling temperature is higher than 700° C., there is a case where the recovery of dislocation is excessively promoted and a desired texture does not develop. Therefore, the coiling temperature is preferably set to 700° C. or lower.


The steel sheet for hot stamping is obtained by the above method.


It is preferable to perform decarburization annealing on the steel sheet for hot stamping obtained by the above method. Before the decarburization annealing, a heat treatment for the purpose of softening may be performed as necessary and furthermore, cold rolling may be performed at a cumulative rolling reduction (={1−(sheet thickness after cold rolling/sheet thickness before cold rolling)}×100) of 30% to 70%. Plating may be performed in a decarburization annealing line or an annealing line for plating may be threaded again after the end of the decarburization annealing. As a plating layer that is imparted to the surface of the steel sheet for hot stamping, an aluminum plating layer, an aluminum-zinc plating layer, an aluminum-silicon plating layer, a hot-dip galvanized layer, an electrogalvanized layer, a hot-dip galvannealed layer, or the like is an exemplary example.


The decarburization annealing reduces the amount of C in the surface layer region of the steel sheet for hot stamping. As the conditions of the decarburization annealing, it is preferable that the atmosphere is set to a moist atmosphere contain hydrogen, nitrogen, or oxygen, the decarburization annealing temperature (the maximum attainment temperature of the steel sheet) is set to 700° C. to 950° C., and the residence time in the temperature range of 700° C. to 950° C. is set to 5 seconds to 1200 seconds. The residence time mentioned herein refer to a time from when the steel sheet temperature rises and reaches 700° C. to when the steel sheet temperature is held at 700° C. to 950° C., decreases and reaches 700° C.


When the maximum attainment temperature is lower than 700° C. and the residence time in the temperature range of 700° C. to 950° C. is shorter than 5 seconds, since the diffusion of C is not sufficiently promoted, there is a case where decarburization does not proceed, and the texture of the surface layer region cannot be controlled. On the other hand, when the maximum attainment temperature is higher than 950° C. and the residence time in the temperature range of 700° C. to 950° C. is longer than 1200 seconds, there is a case where decarburization excessively proceeds and, in the texture of the surface layer region of the steel sheet for hot stamping, the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> cannot be controlled to less than 1.5.


Next, a preferable manufacturing method of the hot-stamping formed body according to the present embodiment using the above-described steel sheet for hot stamping will be described.


First, it is preferable that the steel sheet for hot stamping is heated and held in a temperature range of 800° C. to 1000° C. for 60 to 600 seconds. The average heating rate during the heating may be set to 0.1° C./s or faster or 200° C./s or slower. The average heating rate mentioned herein is a value that is obtained in a case where a temperature difference between the surface temperature of a steel sheet at the time of start of the heating and a holding temperature is divided by a time difference from the start of the heating to a time when a temperature reaches a holding temperature. In addition, during the holding, the temperature of a steel sheet may be fluctuated in the temperature range of 800° C. to 1000° C. or may be constant.


When the heating temperature is lower than 800° C. and the holding time is shorter than 60 seconds, there is a case where the dissolution of a carbide becomes impure and the remaining carbide acts as a starting point of cracking to degrade the bendability. When the heating temperature is higher than 1000° C. and the holding time is longer than 600 seconds, there is a case where the diffusion of C is excessively promoted and the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> of the texture of the inside region cannot be set to less than 2.3.


Exemplary examples of a heating method to be performed before the hot stamping include heating using an electric furnace, a gas furnace, or the like, flame heating, energization heating, high-frequency heating, induction heating, and the like.


After the steel sheet is held in the above-described temperature range, hot stamping is performed. In the manufacturing method of the hot-stamping formed body according to the present embodiment, forming is preferably performed at 300° C. or higher and lower than 650° C. After the hot stamping, it is preferable to cool the steel sheet to a temperature range of 300° C. or lower at 10° C./s or faster.


In the manufacturing method of the hot-stamping formed body according to the present embodiment, when the forming temperature is 650° C. or higher, the total area ratio of ferrite and granular bainite becomes less than 10%, and desired ductility cannot be obtained. When the forming temperature is lower than 300° C., the forming load becomes too high, and there is a case where a die breaks.


The hot-stamping formed body is obtained by the above method. After the hot stamping, a tempering treatment may be performed at 150° C. to 600° C. In addition, a part of the hot-stamping formed body may be tempered by laser irradiation or the like to partially provide a softened region.


Examples

Next, examples of the present invention will be described. Conditions in the examples are examples of conditions adopted to confirm the feasibility and effect of the present invention, and the present invention is not limited to the examples of conditions. The present, invention is capable of adopting a variety of conditions as long as the object of the present invention is achieved without departing from the gist of the present invention.


Steel pieces manufactured by casting molten steel having a chemical composition shown in Table 1-1 and Table 1-2 were held in a temperature range of 1200° C. or higher for 20 minutes or longer, and then hot rolling, cold rolling, and decarburization annealing were performed under conditions shown in Table 2-1 to Table 2-6. A softening heat treatment was performed before the decarburization annealing as necessary. In addition, plating and plating annealing were performed as necessary. Therefore, steel sheets for hot stamping, shown in Table 3-1 to Table 3-3 were obtained.


Hot stamping was performed on the obtained steel sheet for hot stamping under conditions shown in Table 4-B-1 to Table 4-B-3, thereby obtaining hot-stamping formed bodies. On some of the hot-stamping formed bodies, a tempering treatment was performed at 150° C. to 600° C. after the hot stamping. In addition, for some of the hot-stamping formed bodies, the hot-stamping formed bodies were partially irradiated with a laser, thereby forming partially softened regions. Table 5-B-1 to Table 5-B-3 show the microstructures and mechanical properties of the obtained hot-stamping formed bodies.


Underlined values in the tables indicate that the values are outside the scope of the present invention, the preferred manufacturing conditions are not satisfied, or property values are not preferable. In addition, “pole density ratio in texture of surface layer region” in Table 5-B-1 to Table 5-B-3 indicates the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> in the texture between the surface and the sheet thickness ¼ position from the surface, and “pole density ratio in texture of inside region” indicates the ratio between the pole density of the orientation group consisting of {001}<1-10> to {001}<−1-10> and the pole density of the orientation group consisting of {111}<1-10> to {111}<−1-12> in the texture between the sheet thickness ¼ position from the surface and the sheet thickness ½ position from the surface.


The metallographic structures and the textures of the steel sheet for hot stamping and the hot-stamping formed bodies were measured by the above-described measurement method. In addition, the mechanical properties of the hot-stamping formed body were evaluated by the following methods.


Tensile Strength and Uniform Elongation


The tensile (maximum) strength TS and uniform elongation uEl of the hot-stamping formed body were obtained by producing a No. 5 test piece from an arbitrary position of the hot-stamping formed body in accordance with JIS Z 2241: 2011 and performing a tensile test. The speed of a cross-head was set to 3 mm/min.


In a case where the tensile strength TS was 1500 MPa or more, the hot-stamping formed body was determined as acceptable for being excellent in terms of strength, and, in a case where the tensile strength TS was less than 1500 MPa, the hot-stamping formed body was determined as unacceptable for being poor in strength. In addition, in a case where the product of the tensile strength TS and the uniform elongation uEl (TS×UuEl) was 6000 MPa·% or more, the hot-stamping formed body was determined as acceptable for being excellent in terms of ductility, and, in a case where the product was less than 6000 MPa·%, the hot-stamping formed body was determined as unacceptable for being poor in ductility.


Bending Angle


The bending angle was evaluated by the following method based on the VDA standard (VDA238-100) specified by Verband der Automobilindustrie. In the present examples, displacement under the maximum load that was obtained in a bending test was converted to an angle based on VDA standard, thereby obtaining the maximum bending angle α (°). In a case where the product (TS×α) of the tensile strength TS and the maximum bending angle α obtained by the above-described method was 75000 MPa·° or more, the hot-stamping formed body was determined as acceptable for being excellent in terms of bendability, and, in a case where the product was less than 75000 MPa·°, the hot-stamping formed body was determined as unacceptable for being poor in bendability.


The conditions in the bending test were as described below.

    • Dimensions of test piece: 60 mm (rolling direction)×30 mm (a direction parallel to a sheet width direction)
    • Test piece sheet thickness: 1.6 mm
    • Bending ridge: A direction parallel to a sheet width direction
    • Testing method: Supported by rolls and pressed by a punch
    • Roll diameter: φ30 mm
    • Punch shape: Tip R=0.4 mm
    • Distance between rolls: 2.0×sheet thickness (mm)+0.5 mm
    • Pressing speed: 20 mm/min
    • Tester: SHIMADZU AUTOGRAPH 20 kN


From Table 5-B-1 to Table 5-B-3, it is found that the hot-stamping formed bodies that were the present invention examples had excellent strength, bendability, and ductility. On the other hand, it is found that the hot-stamping formed bodies that were the comparative examples were poor in one or more properties.











TABLE 1-1







Steel
Chemical composition (mass %), remainder: Fe and impurity


























No.
C
Si
Mn
Al
P
S
N
Nb
Ti
V
Mo
Cr
Cu
Ni
B
Ca
REM
Note




























1

0.12

0.200
1.60
0.026
0.010
0.0012
0.0056










Comparative Steel


2
0.21
0.130
1.20
0.026
0.012
0.0010
0.0081










Present Invention Steel


3
0.31
0.300
1.30
0.031
0.009
0.0036
0.0030










Present Invention Steel


4
0.36
0.200
1.40
0.030
0.015
0.0029
0.0047










Present Invention Steel


5
0.45
0.120
1.60
0.031
0.015
0.0025
0.0059










Present Invention Steel


6

0.51

0.210
1.70
0.040
0.013
0.0031
0.0086










Comparative Steel


7
0.18
0.0005
1.30
0.038
0.015
0.0026
0.0044










Comparative Steel


8
0.35
0.005
1.20
0.029
0.009
0.0011
0.0044










Present Invention Steel


9
0.35
0.200
1.00
0.027
0.011
0.0037
0.0094










Present Invention Steel


10
0.35
1.000
1.40
0.029
0.015
0.0019
0.0032










Present Invention Steel


11
0.35

3.200

1.60
0.033
0.015
0.0018
0.0095










Comparative Steel


12
0.35
0.240

0.20

0.028
0.014
0.0015
0.0098










Comparative Steel


13
0.35
0.220
0.50
0.039
0.012
0.0015
0.0086










Present Invention Steel


14
0.35
0.180
1.30
0.044
0.014
0.0008
0.0065










Present Invention Steel


15
0.35
0.290
2.00
0.037
0.013
0.0026
0.0047










Present Invention Steel


16
0.35
0.280

3.20

0.027
0.010
0.0014
0.0030










Comparative Steel


17
0.35
0.260
1.50

0.000

0.012
0.0030
0.0069










Comparative Steel


18
0.35
0.220
1.70
0.001
0.009
0.0040
0.0047










Present Invention Steel


19
0.35
0.280
1.00
0.030
0.014
0.0040
0.0070










Present Invention Steel


20
0.35
0.230
1.50
1.700
0.013
0.0023
0.0060










Present Invention Steel


21
0.35
0.120
1.90

2.200

0.014
0.0007
0.0038










Comparative Steel


22
0.35
0.190
1.70
0.045
0.001
0.0018
0.0073










Present Invention Steel





Underlines indicate that the corresponding values are outside the scope of the present invention.















TABLE 1-2







Steel
Chemical composition (mass %), remainder: Fe and impurity


























No.
C
Si
Mn
Al
P
S
N
Nb
Ti
V
Mo
Cr
Cu
Ni
B
Ca
REM
Note




























23
0.35
0.120
1.30
0.035
0.008
0.0020
0.0094










Present Invention Steel


24
0.35
0.220
2.00
0.039

0.150

0.0035
0.0036










Comparative Steel


25
0.35
0.110
1.30
0.043
0.014
0.0003
0.0070










Present Invention Steel


26
0.35
0.150
1.30
0.041
0.008
0.0030
0.0065










Present Invention Steel


27
0.35
0.250
1.10
0.030
0.011

0.1500

0.0057










Comparative Steel


28
0.35
0.270
1.50
0.035
0.013
0.0013
0.0008










Present Invention Steel


29
0.35
0.280
1.40
0.030
0.009
0.0016
0.0040










Present Invention Steel


30
0.35
0.240
1.70
0.035
0.012
0.0032

0.1200











Comparative Steel


31
0.37
0.240
1.00
0.028
0.011
0.0038
0.0093
0.05









Present Invention Steel


32
0.37
0.110
2.00
0.036
0.009
0.0015
0.0072

0.05








Present Invention Steel


33
0.37
0.190
1.30
0.038
0.015
0.0034
0.0031


0.05







Present Invention Steel


34
0.37
0.220
1.20
0.025
0.009
0.0017
0.0076



0.2






Present Invention Steel


35
0.37
0.140
1.20
0.030
0.015
0.0033
0.0083




0.4





Present Invention Steel


36
0.37
0.110
1.40
0.041
0.009
0.0020
0.0089





0.3




Present Invention Steel


37
0.37
0.270
1.30
0.045
0.012
0.0020
0.0082






0.4



Present Invention Steel


38
0.35
0.100
1.10
0.045
0.013
0.0033
0.0038







0.0025


Present Invention Steel


39
0.35
0.150
1.30
0.028
0.011
0.0026
0.0061








0.006

Present Invention Steel


40
0.35
0.170
1.40
0.028
0.012
0.0036
0.0067









0.20
Present Invention Steel


41
0.35
2.890
1.42
0.030
0.014
0.0022
0.0039










Present Invention Steel


42
0.35
0.297
2.78
0.031
0.012
0.0024
0.0044










Present Invention Steel


43
0.35
0.124
1.31
0.037
0.091
0.0025
0.0097










Present Invention Steel


44
0.35
0.147
1.29
0.045
0.008
0.0870
0.0059










Present Invention Steel





Underlines indicate that the corresponding values are outside the scope of the present invention.















TABLE 2-1









Hot rolling

















Rolling










temperature
Rolling

Rolling
Elapsed time
Average cooling rate




one pass
reduction one
Final
reduction
from end of hot
in temperature range


Steel

before final
pass before
rolling
of final
rolling to start
from hot rolling end
Coiling


sheet
Steel
rolling
final rolling
temperature
rolling
of cooling
temperature to 450° C.
temperature


No.
No.
(° C.)
(%)
(° C.)
(%)
(sec)
(° C./s)
(° C.)


















1
1
856
23
831
10
4.2
7
691


2
 2
858
19
807
8
2.5
5
675


3
 3
857
21
807
6
3.6
8
686


4
 4
873
17
819
12
4.0
9
682


5
 5
875
17
825
6
3.6
9
634


6
6
867
17
813
6
4.3
9
609


7
7
872
18
824
10
3.3
8
604


8
 8
875
22
835
10
4.4
5
614


9
 9
853
23
819
6
3.0
6
682


10
10
860
18
805
11
3.3
6
694


11

11

876
20
832
9
4.4
6
614


12

12

867
22
810
12
4.3
6
680


13
13
855
17
807
8
4.5
7
658


14
14
870
22
820
6
4.0
9
647


15
15
862
21
831
10
3.1
8
609


16

16

854
23
828
6
3.6
7
633


17

17

875
19
808
10
4.1
6
623


18
18
872
23
825
10
4.2
6
680


19
19
858
18
807
8
2.9
9
642


20
20
862
18
810
12
4.1
6
651


21

21

860
20
824
9
3.7
5
645


22
22
852
23
812
10
3.2
6
699


23
23
872
21
818
7
3.0
5
646


24

24

875
19
831
12
3.9
5
622


25
25
864
22
811
9
2.8
5
625


26
26
869
19
820
10
4.1
7
695


27

27

866
22
810
7
3.9
9
603


28
28
857
22
808
12
4.5
6
641


29
29
862
23
824
11
4.5
5
699


30

30

868
23
829
10
3.6
6
696





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.















TABLE 2-2









Hot rolling

















Rolling










temperature
Rolling

Rolling
Elapsed time
Average cooling rate




one pass
reduction one
Final
reduction
from end of hot
in temperature range


Steel

before final
pass before
rolling
of final
rolling to start
from hot rolling end
Coiling


sheet
Steel
rolling
final rolling
temperature
rolling
of cooling
temperature to 450° C.
temperature


No.
No.
(° C.)
(%)
(° C.)
(%)
(sec)
(° C./s)
(° C.)


















31
31
867
19
817
11 
4.3
6
689


32
32
866
21
822
9
3.0
6
679


33
33
868
23
819
11 
4.1
7
629


34
34
867
19
808
10 
3.2
5
671


35
35
876
19
826
7
2.5
7
625


36
36
859
18
816
9
2.7
7
638


37
37
851
19
815
6
3.6
6
689


38
38
868
22
822
8
2.6
9
685


39
39
854
22
822
7
2.7
6
618


40
40
864
19
808
9
3.8
8
699


41
4

800

22
820
9
3.7
9
616


42
4
860
19
820
8
3.0
9
689


43
4

950

21
825
7
3.7
9
684


44
4
873
7
828
8
3.9
6
679


45
4
872
20
825
9
3.2
7
671


46
4
854

35

810
8
3.0
6
615


47
4
850
23

770

9
3.0
5
682


48
4
873
21
820
10 
2.5
8
632


49
4
853
23

870

12 
4.4
5
672


50
4
853
21
818

4

2.8
7
639


51
4
873
23
823
8
4.3
7
603


52
4
861
22
831

18

2.8
5
689


53
4
862
18
825
6

1.5

9
694


54
4
856
18
827
11 
3.5
5
692


55
4
875
21
830
8
6.7
6
611


56
4
875
18
832
10 
2.8
7
690


57
4
869
20
813
8
2.5
9
665


58
4
866
22
808
6
3.0

15

617


59
4
872
23
810
7
4.4
5
550


60
4
887
19
808
11 
4.2
8
650





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.















TABLE 2-3









Hot rolling

















Rolling










temperature
Rolling

Rolling
Elapsed time
Average cooling rate




one pass
reduction one
Final
reduction
from end of hot
in temperature range


Steel

before final
pass before
rolling
of final
rolling to start
from hot rolling end
Coiling


sheet
Steel
rolling
final rolling
temperature
rolling
of cooling
temperature to 450° C.
temperature


No.
No.
(° C.)
(%)
(° C.)
(%)
(sec)
(° C./s)
(° C.)


















61
4
866
20
823
7
2.5
9

750



62
4
856
21
834
10
2.5
5
630


63
4
860
20
834
8
4.5
9
681


64
4
855
20
817
9
4.1
7
603


65
4
850
17
812
11
2.9
7
685


66
4
856
23
832
11
4.5
6
699


67
4
870
23
832
8
4.4
6
685


68
4
855
21
821
12
4.1
6
676


69
4
867
23
814
9
3.6
6
638


70
4
867
22
831
7
4.4
8
657


71
4
875
18
832
8
4.4
9
663


72
4
864
17
805
11
3.0
7
653


73
4
866
21
809
12
3.0
9
628


74
4
871
22
812
7
3.6
5
636


75
4
857
22
807
8
4.0
9
602


76
4
873
18
822
8
3.8
5
691


77
4
873
22
830
9
3.1
8
674


78
4
866
21
822
11
3.3
6
660


79
4
865
19
826
6
4.2
8
693


80
4
865
17
811
12
3.0
8
631


81
4
858
21
811
7
3.2
9
642


82
4
854
22
820
11
3.8
7
668


83
4
868
20
827
8
4.2
9
686


84
4
875
19
833
9
3.2
7
669


85
4
860
22
821
6
3.0
7
686


86
4
859
19
821
9
4.4
6
616


87
41
856
18
811
10
2.9
6
698


88
42
855
23
821
11
2.7
8
609


89
43
875
22
814
8
3.4
4
651


90
44
879
20
828
9
4.2
7
697





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.


















TABLE 2-4









Cold rolling
Decarburization annealing
Plating


















Presence or
Cumulative
Maximum
Residence time in

Plating



Steel

absence of
rolling
attainment
temperature range
Presence
annealing after


sheet
Steel
softening heat
reduction
temperature
of 700° C. to 950° C.
or absence
decarburization


No.
No.
treatment
(%)
(° C.)
(sec)
of plating
annealing
Note


















1
1
Absent
69
830
151


Comparative Example


2
 2
Absent
66
818
166


Present Invention Example


3
 3
Absent
36
784
172


Present Invention Example


4
 4
Absent
30
773
135


Present Invention Example


5
 5
Absent
41
808
216


Present Invention Example


6
6
Absent
39
811
268


Comparative Example


7
7
Absent
45
789
231


Comparative Example


8
 8
Absent
45
818
273


Present Invention Example


9
 9
Absent
33
801
237


Present Invention Example


10
10
Absent
64
818
228


Present Invention Example


11

11

Absent
44
801
277


Comparative Example


12

12

Absent
66
775
209


Comparative Example


13
13
Absent
65
795
219


Present Invention Example


14
14
Absent
63
776
197


Present Invention Example


15
15
Absent
40
803
183


Present Invention Example


16

16

Absent
54
805
250


Comparative Example


17

17

Absent
64
810
177


Comparative Example


18
18
Absent
66
828
216


Present Invention Example


19
19
Absent
33
826
248


Present Invention Example


20
20
Absent
54
824
280


Present Invention Example


21

21

Absent
32
822
179


Comparative Example


22
22
Absent
31
827
167


Present Invention Example


23
23
Absent
40
786
197


Present Invention Example


24

24

Absent
32
823
167


Comparative Example


25
25
Absent
49
787
258


Present Invention Example


26
26
Absent
70
800
150


Present Invention Example


27

27

Absent
52
787
187


Comparative Example


28
28
Absent
43
817
140


Present Invention Example


29
29
Absent
49
808
148


Present Invention Example


30

30

Absent
46
813
265


Comparative Example





Underlines indicate that the oorresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.


















TABLE 2-5









Cold rolling
Decarburization annealing
Plating


















Presence or
Cumulative
Maximum
Residence time in

Plating



Steel

absence of
rolling
attainment
temperature range
Presence
annealing after


sheet
Steel
softening heat
reduction
temperature
of 700° C. to 950° C.
or absence
decarburization


No.
No.
treatment
(%)
(° C.)
(sec)
of plating
annealing
Note


















31
31
Absent
51
808
209


Present Invention Example


32
32
Absent
55
778
270


Present Invention Example


33
33
Absent
46
792
167


Present Invention Example


34
34
Absent
57
819
246


Present Invention Example


35
35
Absent
54
815
267


Present Invention Example


36
36
Absent
69
774
275


Present Invention Example


37
37
Absent
43
804
240


Present Invention Example


38
38
Absent
65
822
238


Present Invention Example


39
39
Absent
56
784
209


Present Invention Example


40
40
Absent
58
824
130


Present Invention Example


41
4
Absent
41
775
251


Comparative Example


42
4
Absent
39
828
151


Present Invention Example


43
4
Absent
61
814
241


Comparative Example


44
4
Absent
37
828
173


Comparative Example


45
4
Absent
62
789
166


Present Invention Example


46
4
Absent
48
775
211


Comparative Example


47
4
Absent
40
806
265


Comparative Example


48
4
Absent
70
817
165


Present Invention Example


49
4
Absent
45
798
130


Comparative Example


50
4
Absent
44
811
232


Comparative Example


51
4
Absent
37
775
225


Present Invention Example


52
4
Absent
42
812
262


Comparative Example


53
4
Absent
33
817
255


Comparative Example


54
4
Absent
48
814
275


Present Invention Example


55
4
Absent
61
792
137


Present Invention Example


56
4
Absent
58
800
273


Present Invention Example


57
4
Absent
62
792
197


Present Invention Example


58
4
Absent
52
814
149


Comparative Example


59
4
Absent
37
812
215


Present Invention Example


60
4
Absent
67
779
276


Present Invention Example





Underlines indicate that the corresponding valuesare outside the scope of the present invention and manufacturing conditions are not preferable.


















TABLE 2-6









Cold rolling
Decarburization annealing
Plating


















Presence or
Cumulative
Maximum
Residence time in

Plating



Steel

absence of
rolling
attainment
temperature range
Presence
annealing after


sheet
Steel
softening heat
reduction
temperature
of 700° C. to 950° C.
or absence
decarburization


No.
No.
treatment
(%)
(° C.)
(sec)
of plating
annealing
Note


















61
4
Absent
44
785
234


Comparative Example


62
4
Present
59
809
267


Present Invention Example


63
4
Absent
40
814
272


Present Invention Example


64
4
Absent
55

660

155


Comparative Example


65
4
Absent
31
720
269


Present Invention Example


66
4
Absent
64
800
263


Present Invention Example


67
4
Absent
61
900
247


Present Invention Exampie


68
4
Absent
50

970

263


Comparative Example


69
4
Absent
56
806
3


Comparative Example


70
4
Absent
62
770
 60


Present Invention Exampie


71
4
Absent
54
770
180


Present Invention Example


72
4
Absent
45
812
900


Present Invention Example


73
4
Absent
54
793

1300



Comparative Example


74
4
Absent
44
803
234
Present

Present Invention Example


75
4
Absent
56
773
189

Present
Present Invention Example


76
4
Absent
67
777
268


Present Invention Exampie


77
4
Absent
58
798
138


Present Invention Example


78
4
Absent
35
829
246


Present Invention Example


79
4
Absent
52
799
211


Present Invention Exampie


80
4
Absent
33
801
151


Present Invention Example


81
4
Absent
37
805
203


Present Invention Example


82
4
Absent
49
823
179


Present Invention Exampie


83
4
Absent
31
821
276


Present Invention Example


84
4
Absent
64
802
163


Present Invention Example


85
4
Absent
46
801
176


Present Invention Exampie


86
4
Absent
67
801
146


Present Invention Example


87
41
Absent
66
828
216


Present Invention Example


88
42
Absent
42
794
189


Present Invention Example


89
43
Absent
38
782
188


Present Invention Example


90
44
Absent
64
802
135


Present Invention Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 3-1









Steel sheet for hot stamping




















Ratio between










pole density of
Ratio between






orientation group
pole density of






consisting of
orientation group






{001} <1-10> to
consisting of






{001} <−1-10> and
{001} <1-10> to




Ferrite,

pole density of
{001} <−1-10> and




granular

orientation group
pole density of




bainite,

consisting of {111}
orientation group




bainite,
Pearlite
<1-10> to {111}
consisting of {111}


Steel

and
and
<−1-12> in texture
<1-10> to {111}
Decarbu-
Sheet


sheet
Steel
martensite
carbide
of surface
<−1-12> in texture
rization
thickness


No.
No.
(area %)
(area %)
layer region
of inside region
index
(mm)
Note


















1
1
28
72
1.3
1.9
0.174
1.6
Comparative Example


 2
 2
52
48
1.2
1.6
0.198
1.6
Present Invention Example


 3
 3
74
26
1.3
1.8
0.244
1.6
Present Invention Example


 4
 4
22
78
1.3
1.7
0.270
1.6
Present Invention Example


 5
 5
37
63
1.2
1.7
0.320
1.6
Present Invention Example


6
6
68
32
1.3
1.9
0.376
1.6
Comparative Example


7
7
22
78
1.3
1.7
0.283
1.6
Comparative Example


 8
 8
43
57
1.3
1.6
0.267
1.6
Present Invention Example


 9
 9
41
59
1.2
1.7
0.250
1.6
Present Invention Example


10
10
56
44
1.2
1.8
0.236
1.6
Present Invention Example



11


11

60
40
1.2
1.9
0.243
1.6
Comparative Example



12


12

43
57
1.3
1.8
0.241
1.6
Comparative Example


13
13
60
40
1.3
1.6
0.266
1.6
Present Invention Example


14
14
77
23
1.2
1.8
0.285
1.6
Present Invention Example


15
15
30
70
1.2
1.8
0.279
1.6
Present Invention Example



16


16

50
50
1.2
1.6
0.279
1.6
Comparative Example



17


17

21
79
1.3
1.7
0.261
1.6
Comparative Example


18
18
31
69
1.3
1.9
0.280
1.6
Present Invention Example


19
19
51
49
1.3
1.8
0.279
1.6
Present Invention Example


20
20
34
66
1.2
1.9
0.277
1.6
Present Invention Example



21


21

60
40
1.2
1.6
0.248
1.6
Comparative Example


22
22
28
72
1.3
1.6
0.268
1.6
Present Invention Example


23
23
66
34
1.2
1.7
0.280
1.6
Present Invention Example



24


24

25
75
1.2
1.7
0.257
1.6
Comparative Example


25
25
54
46
1.2
1.7
0.260
1.6
Present Invention Example


26
26
75
25
1.2
1.6
0.261
1.6
Present Invention Example



27


27

52
48
1.2
1.8
0.273
1.6
Comparative Example


28
28
39
61
1.3
1.8
0.261
1.6
Present Invention Example


29
29
55
45
1.3
1.7
0.260
1.6
Present Invention Example



30


30

71
29
1.2
1.7
0.236
1.6
Comparative Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 3-2









Steel sheet for hot stamping




















Ratio between










pole density of
Ratio between






orientation group
pole density of






consisting of
orientation group






{001} <1-10> to
consisting of






{001} <−1-10> and
{001} <1-10> to




Ferrite,

pole density of
{001} <−1-10> and




granular

orientation group
pole density of




bainite,

consisting of {111}
orientation group




bainite,
Pearlite
<1-10> to {111}
consisting of {111}


Steel

and
and
<−1-12> in texture
<1-10> to {111}
Decarbu-
Sheet


sheet
Steel
martensite
carbide
of surface
<−1-12> in texture
rization
thickness


No.
No.
(area %)
(area %)
layer region
of inside region
index
(mm)
Note


















31
31
70
30
1.2
1.6
0.271
1.6
Present Invention Example


32
32
24
76
1.3
1.6
0.280
1.6
Present Invention Example


33
33
23
77
1.2
1.6
0.259
1.6
Present Invention Example


34
34
76
24
1.2
1.8
0.249
1.6
Present Invention Example


35
35
28
72
1.3
1.7
0.251
1.6
Present Invention Example


36
36
76
24
1.3
1.9
0.284
1.6
Present Invention Example


37
37
55
45
1.3
1.8
0.241
1.6
Present Invention Example


38
38
28
72
1.2
1.7
0.231
1.6
Present Invention Example


39
39
57
43
1.2
1.7
0.261
1.6
Present Invention Example


40
40
38
62
1.2
1.6
0.236
1.6
Present Invention Exampie



41

4
40
60

1.8


2.4

0.254
1.6
Comparative Example


42
4
58
42
1.2
1.5
0.275
1.6
Present Invention Example



43

4
37
63

1.8


2.2

0.277
1.6
Comparative Example



44

4
26
74

1.9


2.6

0.248
1.6
Comparative Example


45
4
49
51
0.8
1.1
0.239
1.6
Present Invention Example



46

4
40
60

1.9


2.4

0.239
1.6
Comparative Example



47

4
51
49

1.9


2.6

0.243
1.6
Comparative Example


48
4
72
28
1.1
1.1
0.268
1.6
Present Invention Example



49

4
57
43

1.9


2.3

0.243
1.6
Comparative Example



50

4
23
77

1.7


2.4

0.239
1.6
Comparative Example


51
4
69
31
1.1
1.5
0.263
1.6
Present Invention Example



52

4
21
79

1.9


2.3

0.251
1.6
Comparative Example



53

4
68
32

1.7


2.4

0.232
1.6
Comparative Example


54
4
43
57
1.3
1.7
0.274
1.6
Present Invention Example


55
4
27
73
1.2
1.4
0.260
1.6
Present Invention Example


56
4
69
31
0.9
1.2
0.246
1.6
Present Invention Example


57
4
31
69
1.3
1.8
0.230
1.6
Present Invention Example



58

4
33
67

1.8


2.6

0.213
1.6
Comparative Example


59
4
42
58
1.2
1.5
0.239
1.6
Present Invention Example


60
4
45
55
1.2
1.8
0.234
1.6
Present Invention Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 3-3









Steel sheet for hot stamping




















Ratio between










pole density of
Ratio between






orientation group
pole density of






consisting of
orientation group






{001} <1-10> to
consisting of






{001} <−1-10> and
{001} <1-10> to




Ferrite,

pole density of
{001} <−1-10> and




granular

orientation group
pole density of




bainite,

consisting of {111}
orientation group




bainite,
Pearlite
<1-10> to {111}
consisting of {111}


Steel

and
and
<−1-12> in texture
<1-10> to {111}
Decarbu-
Sheet


sheet
Steel
martensite
carbide
of surface
<−1-12> in texture
rization
thickness


No.
No.
(area %)
(area %)
layer region
of inside region
index
(mm)
Note



















61

4
69
31

1.9


2.2

0.271
1.6
Comparative Example


62
4
26
74
1.2
1.6
0.260
1.6
Present Invention Example


63
4
71
29
1.2
1.7
0.270
1.6
Present Invention Example



64

4
55
45

1.7

1.9
0.078
1.6
Comparative Example


65
4
25
75
1.2
1.7
0.459
1.6
Present Invention Example


66
4
57
43
0.9
1.2
0.221
1.6
Present Invention Example


67
4
80
20
1.2
1.7
0.342
1.6
Present Invention Example



68

4
35
65

1.9

1.6
0.520
1.6
Comparative Example



69

4
64
36

1.8

1.7
0.016
1.6
Comparative Example


70
4
72
28
1.3
1.8
0.097
1.6
Present Invention Example


71
4
36
64
0.9
1.3
0.261
1.6
Present Invention Example


72
4
75
25
1.3
1.7
0.423
1.6
Present Invention Example



73

4
72
28

1.6

1.8
0.514
1.6
Comparative Example


74
4
28
72
1.2
1.8
0.244
1.6
Present Invention Example


75
4
77
23
1.3
1.8
0.289
1.6
Present Invention Example


76
4
70
30
1.2
1.6
0.273
1.6
Present Invention Example


77
4
24
76
1.2
1.9
0.265
1.6
Present Invention Example


78
4
74
26
1.2
1.6
0.264
1.6
Present Invention Example


79
4
21
79
1.3
1.8
0.275
1.6
Present Invention Example


80
4
43
57
1.2
1.6
0.281
1.6
Present Invention Example


81
4
21
79
1.2
1.8
0.271
1.6
Present Invention Example


82
4
47
53
1.3
1.8
0.247
1.6
Present Invention Example


83
4
50
50
1.2
1.8
0.246
1.6
Present Invention Example


84
4
59
41
1.3
1.9
0.282
1.6
Present Invention Example


85
4
39
61
1.3
1.6
0.246
1.6
Present Invention Example


86
4
76
24
1.2
1.8
0.235
1.6
Present Invention Example


87
41
55
40
1.2
1.7
0.275
1.6
Present Invention Example


88
42
29
66
1.1
1.7
0.291
1.6
Present Invention Example


89
43
64
36
1.1
1.6
0.254
1.6
Present Invention Example


90
44
75
28
1.1
1.5
0.270
1.6
Present Invention Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 4-B-1









Hot stamping conditions























Cooling rate to






Steel

Heating

Forming
temperature range

Partially


Manufacturing
sheet
Steel
temperature
Holding
temperature
of 300° C. or lower
Tempering
softened


No.
No.
No.
(° C.)
time
(° C.)
(° C./s)
treatment
region
Note



















1
1
1
880
306
585
21


Comparative Example


2
 2
 2
890
325
602
31


Present Invention Example


3
 3
 3
960
231
600
42


Present Invention Example


4
 4
 4
930
330
605
48
Present

Present Invention Example


5
 5
 5
880
295
625
25


Present Invention Example


6
6
6
970
322
576
35


Comparative Example


7
7
7
870
315
571
38


Comparative Example


8
 8
 8
870
324
569
27


Present Invention Example


9
 9
 9
920
237
600
37


Present Invention Example


10
10
10
870
192
544
28


Present Invention Example


11

11


11

940
293
596
44


Comparative Example


12

12


12

940
190
547
40


Comparative Example


13
13
13
970
251
634
34

Present
Present Invention Example


14
14
14
900
225
630
37


Present Invention Example


15
15
15
910
294
633
25


Present Invention Example


16

16


16

870
316
600
37


Comparative Example


17

17


17

960
322
548
42


Comparative Example


18
18
18
940
293
543
43


Present Invention Example


19
19
19
930
192
616
35
Present

Present Invention Example


20
20
20
940
282
588
42


Present Invention Example


21

21


21

960
270
582
49


Comparative Example


22
22
22
900
291
547
48


Present Invention Example


23
23
23
900
232
592
36


Present Invention Example


24

24


24

960
292
542
24


Comparative Example


25
25
25
960
238
547
18


Present Invention Example


26
26
26
920
214
626
17


Present Invention Example


27

27


27

890
206
579
19


Comparative Example


28
28
28
920
243
593
21


Present Invention Example


29
29
29
900
193
540
32


Present Invention Example


30

30


30

920
263
616
47


Comparative Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 4-B-2









Hot stamping conditions























Cooling rate to






Steel

Heating

Forming
temperature range

Partially


Manufacturing
sheet
Steel
temperature
Holding
temperature
of 300° C. or lower
Tempering
softened


No.
No.
No.
(° C.)
time
(° C.)
(° C./s)
treatment
region
Note



















31
31
31
910
311
551
22


Present Invention Example


32
32
32
940
307
623
35


Present Invention Example


33
33
33
890
301
568
26


Present Invention Example


34
34
34
950
338
608
45


Present Invention Example


35
35
35
970
233
542
16


Present Invention Example


36
36
36
890
313
580
49


Present Invention Example


37
37
37
930
251
559
30


Present Invention Example


38
38
38
920
301
615
32


Present Invention Example


39
39
39
890
329
606
36


Present Invention Example


40
40
40
880
324
598
38


Present Invention Example


41

41

4
910
291
600
34


Comparative Example


42
42
4
970
330
581
29


Present Invention Example


43

43

4
950
280
620
17


Comparative Example


44

44

4
920
323
599
46


Comparative Example


45
45
4
900
221
556
49


Present Invention Example


46

46

4
890
339
532
23


Comparative Example


47

47

4
920
228
603
20


Comparative Example


48
48
4
870
227
612
35


Present Invention Example


49

49

4
940
258
563
27


Comparative Example


50

50

4
960
204
637
34


Comparative Example


51
51
4
920
253
538
20


Present Invention Example


52

52

4
870
262
534
30


Comparative Example


53

53

4
870
299
599
28


Comparative Example


54
54
4
920
192
543
15


Present Invention Example


55
55
4
930
339
593
19


Present Invention Example


56
56
4
960
302
596
50
Present

Present Invention Example


57
57
4
920
273
637
48


Present Invention Example


58

58

4
900
259
591
21


Comparative Example


59
59
4
920
227
561
20


Present Invention Example


60
60
4
920
309
587
30


Present Invention Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 4-B-3









Hot stamping conditions























Cooling rate to






Steel

Heating

Forming
temperature range

Partially


Manufacturing
sheet
Steel
temperature
Holding
temperature
of 300° C. or lower
Tempering
softened


No.
No.
No.
(° C.)
time
(° C.)
(° C./s)
treatment
region
Note



















61

61

4
960
312
574
28


Comparative Example


62
62
4
880
249
612
26


Present Invention Example


63
63
4
940
237
637
41


Present Invention Example


64

64

4
960
197
629
34


Comparative Example


65
65
4
960
304
576
23


Present Invention Example


66
66
4
910
322
597
19


Present Invention Example


67
67
4
890
336
534
20


Present Invention Example


68

68

4
920
308
534
39


Comparative Example


69

69

4
940
227
556
21


Compaiative Example


70
70
4
960
240
588
15


Present Invention Example


71
71
4
960
280
556
35

Present
Present Invention Example


72
72
4
910
225
544
27


Present Invention Example


73

73

4
970
207
532
47


Comparative Example


74
74
4
900
331
605
43


Present Invention Example


75
75
4
920
261
576
34


Present Invention Example


76
76
4

770

303
538
40


Comparative Example


77
77
4
920
238
531
21


Present Invention Example


78
78
4

1030

339
604
48


Comparative Example


79
79
4
910
45
534
49


Comparative Example


80
80
4
920
240
621
23


Present Invention Example


81
81
4
880

630

606
36


Comparative Example


82
82
4
960
290
538
32


Present Invention Example


83
83
4
870
316
569
16


Present Invention Example


84
84
4
970
316
535
47


Present Invention Example


85
85
4
890
212
630
22


Present Invention Example


86
86
4
880
331

710

20


Comparative Example


87
87
41
877
185
535
23


Present Invention Example


88
88
42
920
296
638
22


Present Invention Example


89
89
43
908
240
593
32


Present Invention Example


90
90
44
925
212
622
16


Present Invention Example





Underlines indicate that the corresponding values are outside the scope of the present invention and manufacturing conditions are not preferable.
















TABLE 5-B-1









Textures




















Ratio between









pole density of
Ratio between







orientation group
pole density of







consisting of
orientation group







{001} <1-10> to
consisting of







{001} <−1-10> and
{001} <1-10> to







pole density of
{001} <−1-10> and












Microstructures
orientation group
pole density of
Decarbu-

















Ferrite
Martensite,
consisting of {111}
orientation group
rization





and
bainite,
<1-10> to {111}
consisting of {111}
amount



Steel

granular
and tempered
<−1-12> in texture
<1-10> to {111}
Decarbu-


Manufacturing
sheet
Steel
bainite
martensite
of surface
<−1-12> in texture
rization


No.
No.
No.
(area %)
(area %)
layer region
of inside region
index





1
1
1
12
88
1.7
2.2
0.220


 2
 2
 2
21
79
1.7
2.0
0.260


 3
 3
 3
25
75
1.7
2.1
0.306


 4
 4
 4
25
75
1.6
2.2
0.329


 5
 5
 5
17
83
1.5
2.2
0.375


6
6
6
26
74
1.6
2.1
0.428


7
7
7
10
90
1.6
2.1
0.341


 8
 8
 8
15
85
1.7
2.0
0.322


 9
 9
 9
17
83
1.7
2.2
0.299


10
10
10
18
82
1.6
1.9
0.299



11


11


11

22
78
1.5
2.0
0.291



12


12


12

20
80
1.7

2.3

0.300


13
13
13
25
75
1.7
2.1
0.323


14
14
14
22
78
1.7
1.9
0.333


15
15
13
24
76
1.7
1.9
0.331



16


16


16

23
77
1.7
2.1
0.334



17


17


17

14
86
1.5
2.0
0.309


18
18
18
22
78
1.7
1.9
0.326


19
19
19
15
85
1.7
2.2
0.328


20
20
20
19
81
1.5
2.1
0.340



21


21


21

20
80
1.6
2.2
0.311


22
22
22
14
86
1.5
2.2
0.313


23
23
23
24
76
1.6
1.9
0.342



24


24


24

22
78
1.6
1.9
0.310


25
25
25
27
73
1.7
2.2
0.323


26
26
26
15
85
1.6
1.9
0.316



27


27


27

17
83
1.7
2.2
0.329


28
28
28
23
77
1.7
2.2
0.311


29
29
29
24
76
1.6
1.9
0.315



30


30


30

25
75
1.7
2.2
0.293













Mechanical properties

















Tensile
Maximum

Uniform






strength
Bending

elongation



Manufacturing
TS
angle α
TS × α
uEL
TS × uEL



No.
(MPa)
(°)
(MPa · °)
(%)
(MPa · %)
Note







1

1313

97
127361
4.8
 6115
Comparative Example



 2
1533
75
114975
4.6
 6831
Present Invention Example



 3
1821
53
 96513
5.4
 9331
Present Invention Example



 4
2033
57
115881
5.0
 9600
Present Invention Example



 5
2486
51
126786
5.4
12960
Present Invention Example



6
2617
2
70659
2.2
5757
Comparative Example



7

1289

99
127611
5.7
 7347
Comparative Example



 8
2200
54
118800
5.1
10659
Present Invention Example



 9
2215
72
159480
6.4
13286
Present Invention Example



10
2221
51
113271
5.4
11405
Present Invention Example




11


1334

85
113390
6.4
 8538
Comparative Example




12


1308

98
128184
6.6
 8633
Comparative Example



13
2042
55
112310
5.0
10000
Present Invention Example



14
2243
81
181683
6.1
12749
Present Invention Example



15
2025
55
111375
5.0
 9900
Present Invention Example




16

2020
33
66660
5.8
11252
Comparative Example




17

2019
33
66627
5.5
10450
Comparative Example



18
2036
56
114016
5.2
10192
Present Invention Example



19
2049
50
102450
5.8
11484
Present Invention Example



20
2039
54
110106
5.4
10584
Present Invention Example




21

1996
33
65868
6.9
13524
Comparative Example



22
1986
89
176754
5.7
11172
Present Invention Example



23
2032
57
115824
5.2
10296
Present Invention Example




24

2032
27
54864
5.0
10000
Comparative Example



25
1985
89
176665
6.8
13192
Present Invention Example



26
1996
54
107784
5.0
 9600
Present Invention Example




27

2005
33
66165
5.3
10282
Comparative Example



28
2017
79
159343
6.6
12540
Present Invention Example



29
2014
51
102714
5.1
 9996
Present Invention Example




30

2002
35
70070
5.4
10800
Comparative Example







Underlines indicate that the corresponding values are outside the scope of the present invention and characteristics are not preferable.
















TABLE 5-B-2









Textures




















Ratio between









pole density of
Ratio between







orientation group
pole density of







consisting of
orientation group







{001} <1-10> to
consisting of







{001} <−1-10> and
{001} <1-10> to







pole density of
{001} <−1-10> and












Microstructures
orientation group
pole density of
Decarbu-

















Ferrite
Martensite,
consisting of {111}
orientation group
rization





and
bainite,
<1-10> to {111}
consisting of {111}
amount



Steel

granular
and tempered
<−1-12> in texture
<1-10> to {111}
Decarbu-


Manufacturing
sheet
Steel
bainite
martensite
of surface
<−1-12> in texture
rization


No.
No.
No.
(area %)
(area %)
layer region
of inside region
index





31
31
31
15
85
1.5
2.0
0.317


32
32
32
12
88
1.5
2.0
0.335


33
33
33
26
74
1.5
2.1
0.304


34
34
34
17
83
1.6
1.9
0.304


35
35
35
20
80
1.6
2.2
0.303


36
36
36
27
73
1.5
2.2
0.345


37
37
37
28
72
1.5
2.1
0.286


38
38
38
11
89
1.7
2.2
0.286


39
39
39
24
76
1.5
2.0
0.306


40
40
40
25
75
1.7
2.1
0.295



41


41

4
15
85

2.2


2.5

0.310


42
42
4
28
72
0.9
1.7
0.337



43


43

4
22
78

2.0


2.5

0.324



44


44

4
10
90

2.3


2.7

0.310


45
45
4
28
72
0.9
1.5
0.303



46


46

4
11
89

2.0


2.6

0.284



47


47

4
16
84

2.1


2.5

0.299


48
48
4
22
78
1.4
1.8
0.325



49


49

4
10
90

2.4


2.6

0.288



50


50

4
10
80

2.2


2.6

0.297


51
51
4
18
82
1.4
1.5
0.311



52


52

4
21
79

2.2


2.8

0.306



53


53

4
19
81

2.2


2.6

0.294


54
54
4
24
76
1.6
2.1
0.326


55
55
4
15
85
0.8
1.8
0.308


56
56
4
14
86
1.4
1.5
0.309


57
57
4
24
76
1.6
2.2
0.281



58


58

4
14
86

2.0


2.7

0.290


59
59
4
17
83
0.8
1.7
0.291


60
60
4
18
82
1.6
2.0
0.283













Mechanical properties

















Tensile
Maximum

Uniform






strength
Bending

elongation



Manufacturing
TS
angle α
TS × α
uEL
TS × uEL



No.
(MPa)
(°)
(MPa · °)
(%)
(MPa · %)
Note







31
2306
65
149890
6.6
14573
Present Invention Example



32
2318
78
180804
6.1
13469
Present Invention Example



33
2323
83
192809
6.9
15553
Present Invention Example



34
2313
80
185040
6.3
14055
Present Invention Example



35
2330
73
170090
6.3
13910
Present Invention Example



36
2349
65
152685
6.4
14426
Present Invention Example



37
2299
67
151033
7.0
15617
Present Invention Example



38
2207
59
130213
5.2
10868
Present Invention Example



39
2040
72
146880
6.9
13386
Present Invention Example



40
2018
63
127134
6.4
12160
Present Invention Example




41

2033
27
54891
5.4
10692
Comparative Example



42
2041
78
159432
7.0
13720
Present Invention Example




43

2028
35
70980
5.3
10388
Comparative Example




44

1969
36
70884
5.0
9600
Comparative Example



45
2040
66
134640
5.8
11020
Present Invention Example




46

2033
30
60990
5.4
10368
Comparative Example




47

1989
31
61659
5.4
10692
Comparative Example



48
2010
65
130650
6.7
12864
Present Invention Example




49

1994
26
51844
5.3
10070
Comparative Example




50

2025
27
54675
5.2
10400
Comparative Example



51
2033
77
156541
5.5
11000
Present Invention Example




52

2035
31
63085
5.0
9900
Comparative Example




53

2017
35
70595
5.2
10088
Comparative Example



54
2048
50
102400
5.0
9900
Present Invention Example



55
2015
77
155155
6.6
12936
Present Invention Example



56
1996
88
175648
6.5
12740
Present Invention Example



57
2023
59
119357
5.1
9792
Present Invention Example




58

2015
36
72540
5.2
9984
Comparative Example



59
2025
89
180225
6.1
11712
Present Invention Example



60
2032
51
103632
5.3
10282
Present Invention Example







Underlines indicate that the corresponding values are outside the scope of the present invention and characteristics are not preferable.
















TABLE 5-B-3









Textures




















Ratio between









pole density of
Ratio between







orientation group
pole density of







consisting of
orientation group







{001} <1-10> to
consisting of







{001} <−1-10> and
{001} <1-10> to







pole density of
{001} <−1-10> and












Microstructures
orientation group
pole density of
Decarbu-

















Ferrite
Martensite,
consisting of {111}
orientation group
rization





and
bainite,
<1-10> to {111}
consisting of {111}
amount



Steel

granular
and tempered
<−1-12> in texture
<1-10> to {111}
Decarbu-


Manufacturing
sheet
Steel
bainite
martensite
of surface
<−1-12> in texture
rization


No.
No.
No.
(area %)
(area %)
layer region
of inside region
index






61


61

4
19
81

2.0


2.8

0.330


62
62
4
12
88
1.7
2.2
0.321


63
63
4
14
86
1.7
2.2
0.324



64


64

4
18
82

2.3

2.0
0.080


65
65
4
10
90
1.7
2.0
0.206


66
66
4
14
86
1.1
1.4
0.269


67
67
4
14
86
1.6
2.1
0.381



68


68

4
17
83

2.0

1.9
0.568



69


69

4
26
74

2.1

2.0
0.060


70
70
4
23
77
1.7
2.2
0.147


71
71
4
25
75
1.3
1.8
0.299


72
72
4
13
87
1.5
1.9
0.481



73


73

4
21
79

2.3


2.3

0.565


74
74
4
25
75
1.7
1.9
0.295


75
75
4
24
76
1.5
2.2
0.348



76

76
4
21
79

2.0


2.7

0.318


77
77
4
14
86
1.7
2.0
0.322



78

78
4
27
73
1.6

2.9

0.314



79

79
4
23:
77

1.9


2.6

0.335


80
80
4
25
75
1.7
2.2
0.329



81

81
4
21
79
1.6

2.7

0.324


82
82
4
20
80
1.7
1.9
0.301


83
83
4
14
86
1.7
2.1
0.303


84
84
4
18
82
1.5
2.2
0.342


85
85
4
15
85
1.5
2.0
0.306



86

86
4
5

95

1.6
2.0
0.281


87
87
41
19
81
1.6
1.9
0.320


88
88
42
24
76
1.6
2.0
0.352


89
89
43
23
77
1.6
1.8
0.301


90
90
44
14
86
1.5
2.0
0.322













Mechanical properties

















Tensile
Maximum

Uniform






strength
Bending

elongation



Manufacturing
TS
angle α
TS × α
uEL
TS × uEL



No.
(MPa)
(°)
(MPa · °)
(%)
(MPa · %)
Note








61

2000
28
56000
5.1
 9894
Comparative Example



62
1992
53
105576
5.4
10368
Present Invention Example



63
2039
50
101950
5.2
10088
Present Invention Example




64

1988
36
71568
5.3
10070
Comparative Example



65
2037
57
116109
5.3
10282
Present Invention Example



66
2029
83
168407
6.7
13132
Present Invention Example



67
2043
54
110322
5.0
 9500
Present Invention Example




68

2011
36
73210
4.9
 6115
Comparative Example




69

2000
32
64000
5.4
10692
Comparative Example



70
2011
52
104572
5.4
10800
Present Invention Example



71
2009
75
150675
6.0
11880
Present Invention Example



72
2022
53
107166
5.1
 9690
Present Invention Example




73

2014
37
74520
6.7
13494
Cornparative Example



74
2028
50
101400
5.3
10388
Present Invention Example



75
2050
58
118900
5.0
 9900
Present Invention Example




76

2001
33
66033
5.2
10296
Cornparative Example



77
2047
56
114632
5.1
 9690
Present Invention Example




78

2009
28
56252
5.4
10692
Comparative Example




79

2036
28
57008
5.0
 9800
Comparative Example



80
1996
52
103792
5.0
 9700
Present Invention Example




81

1988
36
71568
5.4
10692
Comparative Example



82
1988
50
 99400
5.2
10192
Present Invention Example



83
2050
55
112750
5.4
10692
Present Invention Example



84
2020
52
105040
5.2
 9984
Present Invention Example



85
2024
52
105248
5.4
10368
Present Invention Example




86

1990
57
113430
2.9
5771
Comparative Example



87
2057
51
104907
5.5
11314
Present Invention Example



88
2025
55
111375
5.1
10328
Present Invention Example



89
2037
54
109998
5.3
10796
Present Invention Example



90
1990
52
103480
4.9
 9751
Present Invention Example







Underlines indicate that the corresponding values are outside the scope of the present invention and characteristics are not preferable.






INDUSTRIAL APPLICABILITY

According to the above-mentioned aspect of the present invention, it is possible to provide a hot-stamping formed body having excellent strength, bendability, and ductility.

Claims
  • 1. A hot-stamping formed body comprising, as a chemical composition, by mass %: C: 0.15 to 0.50%;Si: 0.0010% to 3.000%;Mn: 0.30% to 3.00%;Al: 0.0002% to 2.000%;P: 0.100% or less;S: 0.1000% or less;N: 0.0100% or less;Nb: 0% to 0.15%;Ti: 0% to 0.15%;V: 0% to 0.15%;Mo: 0% to 1.0%;Cr: 0% to 1.0%;Cu: 0% to 1.0%;Ni: 0% to 1.0%;B: 0% to 0.0100%;Ca: 0% to 0.010%;REM: 0% to 0.30%; anda remainder consisting of Fe and an impurity,wherein the hot-stamping formed body has a metallographic structure consisting of, by area ratio, a total of 10% to 30% of ferrite and granular bainite and a remainder in microstructure consisting of one or more of martensite, bainite, and tempered martensite,in a texture between a surface and a sheet thickness ¼ position from the surface, a ratio between a pole density of an orientation group consisting of {001}<1-10> to {001}<−1-10> and a pole density of an orientation group consisting of {111}<1-10> to {111}<−1-12> is less than 1.8, andin a texture between the sheet thickness ¼ position from the surface and a sheet thickness ½ position from the surface, a ratio between a pole density of an orientation group consisting of {001}<1-10> to {001}<−1-10> and a pole density of an orientation group consisting of {111} <1-10> to {111}<−1-12> is less than 2.3.
  • 2. The hot-stamping formed body according to claim 1, further comprising, as the chemical composition, by mass %, one or more of the group: Nb: 0.05% to 0.15%,Ti: 0.05% to 0.15%,V: 0.05% to 0.15%,Mo: 0.05% to 1.0%,Cr: 0.05% to 1.0%,Cu: 0.05% to 1.0%,Ni: 0.05% to 1.0%,B: 0.0001% to 0.0100%,Ca: 0.001% to 0.010%, andREM: 0.001% to 0.30%.
  • 3. The hot-stamping formed body according to claim 1, wherein a decarburization index is 0.085 or more.
  • 4. The hot-stamping formed body according to claim 2, wherein a decarburization index is 0.085 or more.
  • 5. A hot-stamping formed body comprising, as a chemical composition, by mass %: C: 0.15 to 0.50%;Si: 0.0010% to 3.000%;Mn: 0.30% to 3.00%;Al: 0.0002% to 2.000%;P: 0.100% or less;S: 0.1000% or less;N: 0.0100% or less;Nb: 0% to 0.15%;Ti: 0% to 0.15%;V: 0% to 0.15%;Mo: 0% to 1.0%;Cr: 0% to 1.0%;Cu: 0% to 1.0%;Ni: 0% to 1.0%;B: 0% to 0.0100%;Ca: 0% to 0.010%;REM: 0% to 0.30%; anda remainder comprising Fe and an impurity,wherein the hot-stamping formed body has a metallographic structure comprising, by area ratio, a total of 10% to 30% of ferrite and granular bainite and a remainder in microstructure comprising one or more of martensite, bainite, and tempered martensite,in a texture between a surface and a sheet thickness ¼ position from the surface, a ratio between a pole density of an orientation group comprising {001}<1-10> to {001}<−1-10> and a pole density of an orientation group comprising {111}<1-10> to {111}<−1-12> is less than 1.8, andin a texture between the sheet thickness ¼ position from the surface and a sheet thickness ½ position from the surface, a ratio between a pole density of an orientation group comprising {001}<1-10> to {001}<−1-10> and a pole density of an orientation group comprising {111}<1-10> to {111}<−1-12> is less than 2.3.
Priority Claims (1)
Number Date Country Kind
2020-084591 May 2020 JP national
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2021/017506 5/7/2021 WO
Publishing Document Publishing Date Country Kind
WO2021/230149 11/18/2021 WO A
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Entry
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Related Publications (1)
Number Date Country
20230091784 A1 Mar 2023 US