STEEL SHEET

Abstract
A steel sheet has a predetermined chemical composition and a metal structure represented by, in area fraction, polygonal ferrite: 40% or less, martensite: 20% or less, bainitic ferrite: 50% to 95%, and retained austenite: 5% to 50%. In area fraction, 80% or more of the bainitic ferrite is composed of bainitic ferrite grains that have an aspect ratio of 0.1 to 1.0 and have a dislocation density of 8×102 (cm/cm3) or less in a region surrounded by a grain boundary with a misorientation angle of 15° or more. In area fraction, 80% or more of the retained austenite is composed of retained austenite grains that have an aspect ratio of 0.1 to 1.0, have a major axis length of 1.0 μm to 28.0 μm, and have a minor axis length of 0.1 μm to 2.8 μm.
Description
TECHNICAL FIELD

The present invention relates to a steel sheet suitable for automotive parts.


BACKGROUND ART

In order to reduce the amount of carbon dioxide gas emissions from automobiles, the reduction in weight of automobile bodies using high-strength steel sheets has been in progress. For example, in order to secure the safety of a passenger, the high-strength steel sheet has come to be often used for framework system parts of a vehicle body. Examples of mechanical properties that have a significant impact on collision safety include a tensile strength, ductility, a ductile-brittle transition temperature, and a 0.2% proof stress. For example, a steel sheet used for a front side member is required to have excellent ductility.


On the other hand, the framework system part has a complex shape, and the high-strength steel sheet for framework system parts is required to have excellent hole expandability and bendability. For example, a steel sheet used for a side sill is required to have excellent hole expandability.


However, it is difficult to achieve both the improvement in collision safety and the improvement in formability. Conventionally, there have been proposed arts relating to the improvement in collision safety or the improvement in formability (Patent Literatures 1 and 2), but even these arts have difficulty in achieving both the improvement in collision safety and the improvement in formability.


CITATION LIST
Patent Literature

Patent Literature 1: Japanese Patent No. 5589893


Patent Literature 2: Japanese Laid-open Patent Publication No. 2013-185196


Patent Literature 3: Japanese Laid-open Patent Publication No. 2005-171319


Patent Literature 4: International Publication Pamphlet No. WO 2012/133563


SUMMARY OF INVENTION
Technical Problem

An object of the present invention is to provide a steel sheet capable of obtaining excellent collision safety and formability.


Solution to Problem

The present inventors conducted earnest examinations in order to solve the above-described problem. As a result, excellent elongation of a steel sheet with a tensile strength of 980 MPa or more was found to be exhibited by setting the area fractions and the forms of retained austenite and bainitic ferrite to predetermined area fractions and forms. Further, it became clear that when the area fraction of polygonal ferrite is low, the hardness difference is small in the steel sheet, and not only excellent elongation but also excellent hole expandability and bendability are obtained, and embrittlement resistance at sufficiently low temperatures and a 0.2% proof stress are also obtained.


As a result of further repeated earnest examinations based on such findings, the present inventor came to an idea of various aspects of the invention described below.


(1)


A steel sheet includes:


a chemical composition represented by,


in mass %,


C: 0.10% to 0.5%,


Si: 0.5% to 4.0%,


Mn: 1.0% to 4.0%,


P: 0.015% or less,


S: 0.050% or less,


N: 0.01% or less,


Al: 2.0% or less,


Si and Al: 0.5% to 6.0% in total,


Ti: 0.00% to 0.20%,


Nb: 0.00% to 0.20%,


B: 0.0000% to 0.0030%,


Mo: 0.00% to 0.50%,


Cr: 0.0% to 2.0%,


V: 0.00% to 0.50%,


Mg: 0.000% to 0.040%,


REM: 0.000% to 0.040%,


Ca: 0.000% to 0.040%, and


the balance: Fe and impurities; and


a metal structure represented by,


in area fraction,


polygonal ferrite: 40% or less,


martensite: 20% or less,


bainitic ferrite: 50% to 95%, and


retained austenite: 5% to 50%, in which


in area fraction, 80% or more of the bainitic ferrite is composed of bainitic ferrite grains that have an aspect ratio of 0.1 to 1.0 and have a dislocation density of 8×102 (cm/cm3) or less in a region surrounded by a grain boundary with a misorientation angle of 15° or more, and


in area fraction, 80% or more of the retained austenite is composed of retained austenite grains that have an aspect ratio of 0.1 to 1.0, have a major axis length of 1.0 ,μm to 28.0 μm, and have a minor axis length of 0.1 μm to 2.8 μm.


(2)


The steel sheet according to (1), in which


the metal structure is represented by, in area fraction,


polygonal ferrite: 5% to 20%,


martensite: 20% or less,


bainitic ferrite: 75% to 90%, and


retained austenite: 5% to 20%.


(3)


The steel sheet according to (1), in which


the metal structure is represented by, in area fraction,


polygonal ferrite: greater than 20% and 40% or less,


martensite: 20% or less,


bainitic ferrite: 50% to 75%, and


retained austenite: 5% to 30%.


(4)


The steel sheet according to any one of (1) to (3), in which


in the chemical composition, in mass %,


Ti: 0.01% to 0.20%,


Nb: 0.005% to 0.20%,


B: 0.0001% to 0.0030%,


Mo: 0.01% to 0.50%,


Cr: 0.01% to 2.0%,


V: 0.01% to 0.50%,


Mg: 0.0005% to 0.040%,


REM: 0.0005% to 0.040%, or


Ca: 0.0005% to 0.040%,


or an arbitrary combination of the above is established.


(5)


The steel sheet according to any one of (1) to (4), further includes:


a plating layer formed on a surface thereof.


Advantageous Effects of Invention

According to the present invention, it is possible to obtain excellent collision safety and formability because the area fractions, the forms, and the like of retained austenite and bainitic ferrite are proper.





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1 is a view illustrating an example of an equivalent ellipse of a retained austenite grain.





DESCRIPTION OF EMBODIMENTS

There will be explained an embodiment of the present invention below.


First, there will be explained a metal structure of a steel sheet according to the embodiment of the present invention. The steel sheet according to this embodiment has a metal structure represented by, in area fraction, polygonal ferrite: 40% or less, martensite: 20% or less, bainitic ferrite: 50% to 95%, and retained austenite: 5% to 50%. In area fraction, 80% or more of the bainitic ferrite is composed of bainitic ferrite grains that have an aspect ratio of 0.1 to 1.0 and have a dislocation density of 8×102 (cm/cm3) or less in a region surrounded by a grain boundary with a misorientation angle of 15° or more. In area fraction, 80% or more of the retained austenite is composed of retained austenite grains that have an aspect ratio of 0.1 to 1.0, have a major axis length of 1.0 μm to 28.0 μm, and have a minor axis length of 0.1 μm to 2.8 μm.


(Area Fraction of Polygonal Ferrite: 40% or Less)


Polygonal ferrite is a soft structure. Therefore, the difference in hardness between polygonal ferrite and martensite being a hard structure is large, and at the time of forming, cracking is likely to occur at an interface between them. The cracking also extends along this interface in some cases. When the area fraction of the polygonal ferrite is greater than 40%, such cracking and extension tend to occur, making it difficult to obtain sufficient hole expandability, bendability, embrittlement resistance at low temperatures, and 0.2% proof stress. Accordingly, the area fraction of the polygonal ferrite is set to 40% or less.


The lower the area fraction of the polygonal ferrite is, the less C is concentrated in the retained austenite, and the hole expandability improves, but the ductility decreases. Therefore, when the hole expandability is more important than the ductility, the area fraction of the polygonal ferrite is preferably set to 20% or less, and when the ductility is more important than the hole expandability, the area fraction of the polygonal ferrite is preferably set to greater than 20% and 40% or less. When the hole expandability is more important than the ductility as well, the area fraction of the polygonal ferrite is preferably set to 5% or more in order to ensure ductility.


(Area Fraction of Bainitic Ferrite: 50% to 95%)


Bainitic ferrite is denser and contains more dislocations than polygonal ferrite, which contributes to the increase in tensile strength. The hardness of bainitic ferrite is higher than that of polygonal ferrite and is lower than that of martensite, and thus, the difference in hardness between bainitic ferrite and martensite is smaller than that between polygonal ferrite and martensite. Accordingly, the bainitic ferrite contributes also to the improvement in hole expandability and bendability. When the area fraction of the bainitic ferrite is less than 50%, it is impossible to obtain a sufficient tensile strength. Therefore, the area fraction of the bainitic ferrite is set to 50% or more. When the hole expandability is more important than the ductility, the area fraction of the bainitic ferrite is preferably set to 75% or more. On the other hand, when the area fraction of the bainitic ferrite is greater than 95%, the retained austenite becomes short, failing to obtain sufficient formability. Accordingly, the area fraction of the bainitic ferrite is set to 95% or less.


(Area Fraction of Martensite: 20% or Less)


Martensite includes fresh martensite (untempered martensite) and tempered martensite. As described above, the difference in hardness between polygonal ferrite and martensite is large, and at the time of forming, cracking is likely to occur at an interface between them. The cracking also extends along this interface in some cases. When the area fraction of the martensite is greater than 20%, such cracking and extension tend to occur, making it difficult to obtain sufficient hole expandability, bendability, embrittlement resistance at low temperatures, and 0.2% proof stress. Accordingly, the area fraction of the martensite is set to 20% or less.


(Area Fraction of Retained Austenite: 5% to 50%)


Retained austenite contributes to the improvement in formability. When the area fraction of the retained austenite is less than 5%, it is impossible to obtain sufficient formability. On the other hand, when the area fraction of the retained austenite is greater than 50%, bainitic ferrite becomes short, failing to obtain a sufficient tensile strength. Accordingly, the area fraction of the retained austenite is set to 50% or less.


Identification of polygonal ferrite, bainitic ferrite, retained austenite, and martensite and determination of their area fractions can be performed, for example, by a scanning electron microscope (SEM) observation or transmission electron microscope (TEM) observation. When a SEM or TEM is used, for example, a sample is corroded using a nital solution and a LePera solution, and a cross section parallel to the rolling direction and the thickness direction (cross section vertical to the width direction) and/or a cross section vertical to the rolling direction are/is observed at 1000-fold to 100000-fold magnification.


Polygonal ferrite, bainitic ferrite, retained austenite, and martensite can also be distinguished by a crystal orientation analysis by crystal orientation diffraction (FE-SEM-EBSD) using an electron back scattering diffraction (EBSD) function attached to a field emission scanning electron microscope (FE-SEM), or by a hardness measurement in a small region such as a micro Vickers hardness measurement.


For example, in determining the area fractions of the polygonal ferrite and the bainitic ferrite, a cross section parallel to the rolling direction and the thickness direction of the steel sheet (a cross section vertical to the width direction) is polished and etched with a nital solution. Then, the area fraction is measured by observing a region where the depth from the surface of the steel sheet is ⅛ to ⅜ of the thickness of the steel sheet using a FE-SEM. Such an observation is made at a magnification of 5000 times for 10 visual fields, and from the average value of the 10 visual fields, the area fraction of each of the polygonal ferrite and the bainitic ferrite is obtained.


The area fraction of the retained austenite can be determined, for example, by an X-ray measurement. In this method, for example, a portion of the steel sheet from the surface up to a ¼ thickness of the steel sheet is removed by mechanical polishing and chemical polishing, and as characteristic X-rays, MoK α rays are used. Then, from integrated intensity ratios of diffraction peaks of (200) and (211) of a body-centered cubic lattice (bcc) phase and (200), (220), and (311) of a face-centered cubic lattice (fcc) phase, the area fraction of the retained austenite is calculated by using the following equation. Such an observation is made for 10 visual fields, and from the average value of the 10 visual fields, the area fraction of the retained austenite is obtained.






Sγ=(I200f+I220f+I311f)/(I200b+I211b)×100


(Sγ indicates the area fraction of the retained austenite, I200f, I220f, and I311f indicate intensities of the diffraction peaks of (200), (220), and (311) of the fcc phase respectively, and I200b and I211b indicate intensities of the diffraction peaks of (200) and (211) of the bcc phase respectively.)


The area fraction of the martensite can be determined by a field emission-scanning electron microscope (FE-SEM) observation and an X-ray measurement, for example. In this method, for example, a region where the depth from the surface of the steel sheet is ⅛ to ⅜ of the thickness of the steel sheet is set as an object to be observed and a LePera solution is used for corrosion. Since the structure that is not corroded by the LePera solution is martensite and retained austenite, it is possible to determine the area fraction of the martensite by subtracting the area fraction Sγ of the retained austenite determined by the X-ray measurement from an area fraction of a region that is not corroded by the LePera solution. The area fraction of the martensite can also be determined by using an electron channeling contrast image to be obtained by the SEM observation, for example. In the electron channeling contrast image, a region that has a high dislocation density and has a substructure such as a block or packet in a grain is the martensite. Such an observation is made for 10 visual fields, and from the average value of the 10 visual fields, the area fraction of the martensite is obtained.


(Area Fraction of Bainitic Ferrite Grains in a Predetermined Form: 80% or More of the Entire Bainitic Ferrite)


Bainitic ferrite grains with a high dislocation density do not contribute to the improvement in elongation as much as polygonal ferrite, and thus, as the area fraction of the bainitic ferrite grains with a high dislocation density is higher, the elongation tends to be lower. Then, it is difficult to obtain sufficient elongation when the area fraction of bainitic ferrite grains that have an aspect ratio of 0.1 to 1.0 and have a dislocation density of 8×102 (cm/cm3) or less in a region surrounded by a grain boundary with a misorientation angle of 15° or more is less than 80%. Accordingly, the area fraction of the bainitic ferrite grains in such a form is set to 80% or more of the entire bainitic ferrite, and is preferably set to 85% or more.


The dislocation density of the bainitic ferrite can be determined by a structure observation using a transmission electron microscope (TEM). For example, by dividing the number of dislocation lines present in a crystal grain surrounded by a grain boundary with a misorientation angle of 15° by the area of this crystal grain, the dislocation density of the bainitic ferrite can be determined.


(Area Fraction of Retained Austenite Grains in a Predetermined Form: 80% or More of the Entire Retained Austenite)


Retained austenite is transformed into martensite during forming by strain-induced transformation. When the retained austenite is transformed into martensite, in the case where this martensite is adjacent to polygonal ferrite or untransformed retained austenite, there is caused a large difference in hardness between them. The large hardness difference leads to the occurrence of cracking as described above. Such cracking is prone to occur particularly in a place where stresses concentrate, and the stresses tend to concentrate in the vicinity of the martensite transformed from the retained austenite with an aspect ratio of less than 0.1. Then, when the area fraction of the retained austenite grains that have an aspect ratio of 0.1 to 1.0, have a major axis length of 1.0 μm to 28.0 μm, and have a minor axis length of 0.1 μm to 2.8 μm is less than 80%, the cracking due to stress concentration occurs easily, making it difficult to obtain sufficient elongation. Accordingly, the area fraction of the retained austenite grains in such a form is set to 80% or more of the entire retained austenite, and preferably set to 85% or more. Here, the aspect ratio of the retained austenite grain is the value obtained by dividing the length of a minor axis of an equivalent ellipse of the retained austenite grain by the length of its major axis. FIG. 1 illustrates one example of the equivalent ellipse. Even when a retained austenite grain 1 has a complex shape, an aspect ratio (L2/L1) of this retained austenite grain can be obtained from, of an equivalent ellipse 2, a length L1 of a major axis and a length L2 of a minor axis.


Next, there will be explained a chemical composition of the steel sheet according to the embodiment of the present invention and a slab to be used for manufacturing the steel sheet. As described above, the steel sheet according to the embodiment of the present invention is manufactured by undergoing hot rolling, pickling, cold rolling, first annealing, second annealing, and so on. Thus, the chemical composition of the steel sheet and the slab is one considering not only properties of the steel sheet but also these treatments. In the following explanation, “%” being the unit of a content of each element contained in the steel sheet and the slab means “mass %” unless otherwise stated. The steel sheet according to this embodiment and the slab used for manufacturing the steel sheet has a chemical composition represented by, in mass %, C: 0.1% to 0.5%, Si: 0.5% to 4.0%, Mn: 1.0% to 4.0%, P: 0.015% or less, S: 0.050% or less, N: 0.01% or less, Al: 2.0% or less, Si and Al: 0.5% to 6.0% in total, Ti: 0.00% to 0.20%, Nb: 0.00% to 0.20%, B: 0.0000% to 0.0030%, Mo: 0.00% to 0.50%, Cr: 0.0% to 2.0%, V: 0.00% to 0.50%, Mg: 0.000% to 0.040%, REM (rare earth metal): 0.000% to 0.040%, Ca: 0.000% to 0.040%, and the balance: Fe and impurities.


(C: 0.10% to 0.5%)


Carbon (C) contributes to the improvement in strength of the steel sheet and to the improvement in elongation through the improvement in stability of retained austenite. When the C content is less than 0.10%, it is difficult to obtain a sufficient strength, for example, a tensile strength of 980 MPa or more, and it is impossible to obtain sufficient elongation because the stability of retained austenite is insufficient. Thus, the C content is set to 0.10% or more and preferably set to 0.15% or more. On the other hand, when the C content is greater than 0.5%, the transformation from austenite into bainitic ferrite is delayed, and therefore, the bainitic ferrite grains in a predetermined form become short, failing to obtain sufficient elongation. Thus, the C content is set to 0.5% or less and preferably set to 0.25% or less.


(Si: 0.5% to 4.0%)


Silicon (Si) contributes to the improvement in strength of steel and to the improvement in elongation through the improvement in stability of retained austenite. When the Si content is less than 0.5%, it is impossible to sufficiently obtain these effects. Thus, the Si content is set to 0.5% or more and preferably set to 1.0% or more. On the other hand, when the Si content is greater than 4.0%, the strength of the steel increases too much, leading to a decrease in elongation. Thus, the Si content is set to 4.0% or less and preferably set to 2.0% or less.


(Mn: 1.0% to 4.0%)


Manganese (Mn) contributes to the improvement in strength of steel and suppresses a polygonal ferrite transformation that occurs in the middle of cooling of first annealing or second annealing. In the case where a hot-dip galvanizing treatment is performed, the polygonal ferrite transformation that occurs in the middle of cooling of this treatment is also suppressed. When the Mn content is less than 1.0%, it is impossible to sufficiently obtain these effects and polygonal ferrite is generated excessively, leading to a deterioration of hole expandability. Thus, the Mn content is set to 1.0% or more and preferably set to 2.0% or more. On the other hand, when the Mn content is greater than 4.0%, the strength of the slab and a hot-rolled steel sheet increases too much. Thus, the Mn content is set to 4.0% or less and preferably set to 3.0% or less.


(P: 0.015% or Less)


Phosphorus (P) is not an essential element and is contained as an impurity in steel, for example. P segregates in the center portion of the steel sheet in the thickness direction, to reduce toughness and make a welded portion brittle. Therefore, a lower P content is better. When the P content is greater than 0.015%, in particular, the reduction in toughness and the embrittlement of weldability are prominent. Thus, the P content is set to 0.015% or less and preferably set to 0.010% or less. It is costly to reduce the P content, and if the P content is tried to be reduced to less than 0.0001%, the cost rises significantly. Therefore, the P content may be set to 0.0001% or more.


(S: 0.050% or Less)


Sulfur (S) is not an essential element and is contained as an impurity in steel, for example. S reduces manufacturability of casting and hot rolling, and forms coarse MnS to reduce hole expandability. Therefore, a lower S content is better. When the S content is greater than 0.050%, in particular, the reduction in weldability, the reduction in manufacturability, and the reduction in hole expandability are prominent. Thus, the S content is set to 0.050% or less and preferably set to 0.0050% or less. It is costly to reduce the S content, and if the S content is tried to be reduced to less than 0.0001%, the cost rises significantly. Therefore, the S content may be set to 0.0001% or more.


(N: 0.01% or Less)


Nitrogen (N) is not an essential element and is contained as an impurity in steel, for example. N forms coarse nitrides to degrade bendability and hole expandability and cause blowholes to occur at the time of welding. Therefore, a lower N content is better. When the N content is greater than 0.01%, in particular, the reduction in bendability and the reduction in hole expandability and the occurrence of blowholes are prominent. Thus, the N content is set to 0.01% or less. It is costly to reduce the N content, and if the N content is tried to be reduced to less than 0.0005%, the cost rises significantly. Therefore, the N content may be set to 0.0005% or more.


(Al: 2.0% or Less)


Aluminum (Al) functions as a deoxidizing material and suppresses precipitation of iron-based carbide in austenite, but is not an essential element. When the Al content is greater than 2.0%, the transformation into polygonal ferrite from austenite is promoted to excessively generate polygonal ferrite, leading to a deterioration of hole expandability. Thus, the Al content is set to 2.0% or less and preferably set to 1.0% or less. It is costly to reduce the Al content, and if the Al content is tried to be reduced to less than 0.001%, the cost rises significantly. Therefore, the Al content may be set to 0.001% or more.


(Si+Al: 0.5% to 6.0% in Total)


Si and Al both contribute to the improvement in elongation through the improvement in stability of retained austenite. When the total content of Si and Al is less than 0.5%, it is impossible to sufficiently obtain this effect. Thus, the total content of Si and Al is set to 0.5% or more and preferably set to 1.2% or more. Only either Si or Al may be contained, or both Si and Al may be contained.


Ti, Nb, B, Mo, Cr, V, Mg, REM, and Ca are not an essential element, but are an arbitrary element that may be appropriately contained, up to a predetermined amount as a limit, in the steel sheet and the slab.


(Ti: 0.00% to 0.20%)


Titanium (Ti) contributes to the improvement in strength of steel through dislocation strengthening caused by precipitation strengthening and fine grain strengthening. Thus, Ti may be contained. In order to obtain this effect sufficiently, the Ti content is preferably set to 0.01% or more and more preferably set to 0.025% or more. On the other hand, when the Ti content is greater than 0.20%, carbonitride of Ti precipitates excessively, leading to a decrease in formability of the steel sheet. Thus, the Ti content is set to 0.20% or less and preferably set to 0.08% or less.


(Nb: 0.00% to 0.20%)


Niobium (Nb) contributes to the improvement in strength of steel through dislocation strengthening caused by precipitation strengthening and fine grain strengthening. Thus, Nb may be contained. In order to obtain this effect sufficiently, the Nb content is preferably set to 0.005% or more and more preferably set to 0.010% or more. On the other hand, when the Nb content is greater than 0.20%, carbonitride of Nb precipitates excessively, leading to a decrease in formability of the steel sheet. Thus, the Nb content is set to 0.20% or less and preferably set to 0.08% or less.


(B: 0.0000% to 0.0030%)


Boron (B) strengthens grain boundaries and suppresses a polygonal ferrite transformation that occurs in the middle of cooling of first annealing or second annealing. In the case where a hot-dip galvanizing treatment is performed, the polygonal ferrite transformation that occurs in the middle of cooling of this treatment is also suppressed. Thus, B may be contained. In order to obtain this effect sufficiently, the B content is preferably set to 0.0001% or more and more preferably set to 0.0010% or more. On the other hand, when the B content is greater than 0.0030%, the addition effect is saturated and the manufacturability of hot rolling decreases. Thus, the B content is set to 0.0030% or less and preferably set to 0.0025% or less.


(Mo: 0.00% to 0.50%)


Molybdenum (Mo) contributes to the strengthening of steel and suppresses a polygonal ferrite transformation that occurs in the middle of cooling of first annealing or second annealing. In the case where a hot-dip galvanizing treatment is performed, the polygonal ferrite transformation that occurs in the middle of cooling of this treatment is also suppressed. Thus, Mo may be contained. In order to obtain this effect sufficiently, the Mo content is preferably set to 0.01% or more and more preferably set to 0.02% or more. On the other hand, when the Mo content is greater than 0.50%, the manufacturability of hot rolling decreases. Thus, the Mo content is set to 0.50% or less and preferably set to 0.20% or less.


(Cr: 0.0% to 2.0%)


Chromium (Cr) contributes to the strengthening of steel and suppresses a polygonal ferrite transformation that occurs in the middle of cooling of first annealing or second annealing. In the case where a hot-dip galvanizing treatment is performed, the polygonal ferrite transformation that occurs in the middle of cooling of this treatment is also suppressed. Thus, Cr may be contained. In order to obtain this effect sufficiently, the Cr content is preferably set to 0.01% or more and more preferably set to 0.02% or more. On the other hand, when the Cr content is greater than 2.0%, the manufacturability of hot rolling decreases. Thus, the Cr content is set to 2.0% or less and preferably set to 0.10% or less.


(V: 0.00% to 0.50%)


Vanadium (V) contributes to the improvement in strength of steel through dislocation strengthening caused by precipitation strengthening and fine grain strengthening. Thus, V may be contained. In order to obtain this effect sufficiently, the V content is preferably set to 0.01% or more and more preferably set to 0.02% or more. On the other hand, when the V content is greater than 0.50%, carbonitride of V precipitates excessively, leading to a decrease in formability of the steel sheet. Thus, the Nb content is set to 0.50% or less and preferably set to 0.10% or less.


(Mg: 0.000% to 0.040%, REM: 0.000% to 0.040%, Ca: 0.000% to 0.040%)


Magnesium (Mg), rare earth metal (REM), and calcium (Ca) exist in steel as oxide or sulfide and contribute to the improvement in hole expandability. Thus, Mg, REM, or Ca, or an arbitrary combination of these may be contained. In order to obtain this effect sufficiently, the Mg content, the REM content, and the Ca content are each preferably set to 0.0005% or more, and more preferably set to 0.0010% or more. On the other hand, when the Mg content, the REM content, or the Ca content is greater than 0.040%, coarse oxides are formed, leading to a decrease in hole expandability. Thus, the Mg content, the REM content, and the Ca content are each set to 0.040% or less and preferably set to 0.010% or less.


REM (rare earth metal) refers to 17 elements in total of Sc, Y, and lanthanoids, and the “REM content” means the total content of these 17 elements. REM is contained in misch metal, for example, and misch metal contains lanthanoids in addition to La and Ce in some cases. Metal alone, such as metal La and metal Ce, may be used to add REM.


Examples of the impurities include ones contained in raw materials such as ore and scrap and ones contained in manufacturing steps. Concrete examples of the impurities include P, S, O, Sb, Sn, W, Co, As, Pb, Bi, and H. The O content is preferably set to 0.010% or less, the Sb content, the Sn content, the W content, the Co content, and the As content are preferably set to 0.1% or less, the Pb content and the Bi content are preferably set to 0.005% or less, and the H content is preferably set to 0.0005% or less.


According to this embodiment, it is possible to obtain excellent collision safety and formability. It is possible to obtain mechanical properties in which the hole expandability is 30% or more, the ratio of a minimum bend radius (R (mm)) to a sheet thickness (t (mm)) (R/t) is 0.5 or less, the total elongation is 21% or more, the 0.2% proof stress is 680 MPa or more, the tensile strength is 980 MPa or more, and the ductile-brittle transition temperature is −60° C. or less, for example. In the case where the area fraction of the polygonal ferrite is 5% to 20% and the area fraction of the bainitic ferrite is 75% or more, in particular, the hole expandability of 50% or more can be obtained, and in the case where the area fraction of the polygonal ferrite is greater than 20% and 40% or less, the total elongation of 26% or more can be obtained.


Next, there will be explained a manufacturing method of the steel sheet according to the embodiment of the present invention. In the manufacturing method of the steel sheet according to the embodiment of the present invention, hot rolling, pickling, cold rolling, first annealing, and second annealing of a slab having the above-described chemical composition are performed in this order.


(Hot Rolling)


In the hot rolling, rough rolling, finish rolling, and coiling of the slab are performed. As the slab, for example, a slab obtained by continuous casting or a slab fabricated by a thin slab caster can be used. The slab may be provided into a hot rolling facility while maintaining the slab to a temperature of 1000° C. or more after casting, or may also be provided into a hot rolling facility after the slab is cooled down to a temperature of less than 1000° C. and then is heated.


A rolling temperature in the final pass of the rough rolling is set to 1000° C. to 1150° C., and a reduction ratio in the final pass is set to 40% or more. When the rolling temperature in the final pass is less than 1000° C., an austenite grain diameter after finish rolling becomes small excessively. In this case, the transformation from austenite into polygonal ferrite is promoted excessively and the uniformity of the metal structure decreases, failing to obtain sufficient formability. Thus, the rolling temperature in the final pass is set to 1000° C. or more. On the other hand, when the rolling temperature in the final pass is greater than 1150° C., the austenite grain diameter after finish rolling becomes large excessively. In this case as well, the uniformity of the metal structure decreases, failing to obtain sufficient formability. Thus, the rolling temperature in the final pass is set to 1150° C. or less. When the reduction ratio in the final pass is less than 40%, the austenite grain diameter after finish rolling becomes large excessively and the uniformity of the metal structure decreases, failing to obtain sufficient formability. Thus, the reduction ratio in the final pass is set to 40% or more.


The rolling temperature of the finish rolling is set to the Ar3 point or more. When the rolling temperature is less than the Ar3 point, austenite and ferrite are contained in the metal structure of a hot-rolled steel sheet, failing to obtain sufficient formability because there are differences in the mechanical properties between the austenite and the ferrite. Thus, the rolling temperature is set to the Ar3 point or more. When the rolling temperature is set to the Ar3 point or more, it is possible to relatively reduce a rolling load during the finish rolling. In the finish rolling, the product formed by joining a plurality of rough-rolled sheets obtained by the rough rolling may be rolled continuously. Once the rough-rolled sheet is coiled, the finish rolling may be performed while uncoiling the rough-rolled sheet.


A coiling temperature is set to 750° C. or less. When the coiling temperature is greater than 750° C., coarse ferrite or pearlite is generated in the structure of the hot-rolled steel sheet and the uniformity of the metal structure decreases, failing to obtain sufficient formability. Oxides are formed on the surface thickly, leading to a decrease in picklability in some cases. Thus, the coiling temperature is set to 750° C. or less. The lower limit of the coiling temperature is not limited in particular, but coiling at a temperature lower than room temperature is difficult. By hot rolling of the slab, a hot-rolled steel sheet coil is obtained.


(Pickling)


After the hot rolling, pickling is performed while uncoiling the hot-rolled steel sheet coil. The pickling is performed once or twice or more. By the pickling, the oxide on the surface of the hot-rolled steel sheet is removed and chemical conversion treatability and platability improve.


(Cold Rolling)


After the pickling, cold rolling is performed. A reduction ratio of the cold rolling is set to 40% to 80%. When the reduction ratio of the cold rolling is less than 40%, it is difficult to keep the shape of a cold-rolled steel sheet flat or it is impossible to obtain sufficient ductility in some cases. Thus, the reduction ratio is set to 40% or more and preferably set to 50% or more. On the other hand, when the reduction ratio is greater than 80%, a rolling load becomes large excessively, recrystallization of ferrite is promoted excessively, coarse polygonal ferrite is formed, and the area fraction of the polygonal ferrite exceeds 40%. Thus, the reduction ratio is set to 80% or less and preferably set to 70% or less. The number of times of rolling pass and the reduction ratio for each pass are not limited in particular. The cold-rolled steel sheet is obtained by cold rolling of the hot-rolled steel sheet.


(First Annealing)


After the cold rolling, first annealing is performed. In the first annealing, of the cold-rolled steel sheet, first heating, first cooling, second cooling, and first retention are performed. The first annealing can be performed in a continuous annealing line, for example.


An annealing temperature of the first annealing is set to 750° C. to 900° C. When the annealing temperature is less than 750° C., the area fraction of the polygonal ferrite becomes large excessively and the area fraction of the bainitic ferrite becomes small excessively. Thus, the annealing temperature is set to 750° C. or more and preferably set to 780° C. or more. On the other hand, when the annealing temperature is greater than 900° C., austenite grains become coarse and the transformation from austenite into bainitic ferrite or tempered martensite is delayed. Then, due to the transformation delay, the area fraction of the bainitic ferrite becomes small excessively. Thus, the annealing temperature is set to 900° C. or less and preferably set to 870° C. or less. An annealing time is not limited in particular, and is set to 1 second or more and 1000 seconds or less, for example.


A cooling stop temperature of the first cooling is set to 600° C. to 720° C., and a cooling rate up to the cooling stop temperature is set to 1° C./second or more and less than 10° C./second. When the cooling stop temperature of the first cooling is less than 600° C., the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling stop temperature is set to 600° C. or more and preferably set to 620° C. or more. On the other hand, when the cooling stop temperature is greater than 720° C., the area fraction of the retained austenite becomes short. Thus, the cooling stop temperature is set to 720° C. or less and preferably set to 700° C. or less. When the cooling rate of the first cooling is less than 1.0° C./second, the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling rate is set to 1.0° C./second or more and preferably set to 3° C./second or more. On the other hand, when the cooling rate is 10° C./second or more, the area fraction of the retained austenite becomes short. Thus, the cooling rate is set to less than 10° C./second and preferably set to 8° C./second or less.


A cooling stop temperature of the second cooling is set to 150° C. to 500° C., and a cooling rate up to the cooling stop temperature is set to 10° C./second to 60° C./second. When the cooling stop temperature of the second cooling is less than 150° C., the lath width of the bainitic ferrite or the tempered martensite becomes fine and the retained austenite remaining between laths becomes a fine film. As a result, the area fraction of the retained austenite grains in a predetermined form becomes small excessively. Thus, the cooling stop temperature is set to 150° C. or more and preferably set to 200° C. or more. On the other hand, when the cooling stop temperature is greater than 500° C., the generation of polygonal ferrite is promoted and the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling stop temperature is set to 500° C. or less, preferably set to 450° C. or less, and more preferably set to about room temperature. Further, the cooling stop temperature is preferably set to the Ms point or less according to the composition. When the cooling rate of the second cooling is less than 10° C./s, the generation of polygonal ferrite is promoted and the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling rate is set to 10° C./second or more and preferably set to 20° C./second or more. On the other hand, when the cooling rate is greater than 60° C./second, the area fraction of the retained austenite becomes less than the lower limit. Thus, the cooling rate is set to 60° C./second or less and preferably set to 50° C./second or less.


The method of the first cooling and the second cooling is not limited, and for example, roll cooling, air cooling or water cooling, or an arbitrary combination of these can be used.


After the second cooling, the cold-rolled steel sheet is retained at a temperature of 150° C. to 500° C. only for a time period of t1 seconds to 1000 seconds determined by the following equation (1). This retention (first retention) is performed directly after the second cooling without lowering the temperature to less than 150° C., for example. In the equation (1), T0 denotes the retention temperature and T1 denotes the cooling stop temperature (° C.) of the second cooling.






t1=20×[C]+40×[Mn]−0.1×T0+T1−0.1   (1)


During the first retention, diffusion of C into the retained austenite is promoted. As a result, the stability of the retained austenite improves, thereby making it possible to secure the retained austenite by 5% or more of the area fraction. When the retention time is less than t1 seconds, C does not concentrate sufficiently in the retained austenite and the retained austenite is transformed into martensite during the subsequent temperature lowering, resulting in that the area fraction of the retained austenite becomes small excessively. Thus, the retention time is set to t1 seconds or more. When the retention time is greater than 1000 seconds, decomposition of the retained austenite is promoted and the area fraction of the retained austenite becomes small excessively. Thus, the retention time is set to 1000 seconds or less. An intermediate steel sheet is obtained by first annealing of the cold-rolled steel sheet.


The first retention may be performed by lowering the temperature to less than 150° C. and then reheating the steel sheet up to a temperature of 150° C. to 500° C., for example. When a reheating temperature is less than 150° C., the lath width of the bainitic ferrite or the tempered martensite becomes fine and the retained austenite remaining between laths becomes a fine film. As a result, the area fraction of the retained austenite grains in a predetermined form becomes small excessively. Thus, the reheating temperature is set to 150° C. or more and preferably set to 200° C. or more. On the other hand, when the reheating temperature is greater than 500° C., the generation of polygonal ferrite is promoted and the area fraction of the polygonal ferrite becomes large excessively. Thus, the reheating temperature is set to 500° C. or less and preferably set to 450° C. or less.


The intermediate steel sheet has a metal structure represented by, for example, in area fraction, polygonal ferrite: 40% or less, bainitic ferrite or tempered martensite, or both: 40% to 95% in total, and retained austenite: 5% to 60%. Further, for example, in area fraction, 80% or more of the retained austenite is composed of retained austenite grains with an aspect ratio of 0.03 to 1.00.


(Second Annealing)


After the first annealing, second annealing is performed. In the second annealing, of the intermediate steel sheet, second heating, third cooling, and second retention are performed. The second annealing can be performed in a continuous annealing line, for example. The second annealing is performed under the following conditions, and thereby, it is possible to reduce the dislocation density of the bainitic ferrite and to increase the area fraction of the bainitic ferrite grains in a predetermined form with a dislocation density of 8×102 (cm/cm3) or less.


An annealing temperature of the second annealing is set to 760° C. to 800° C. When the annealing temperature is less than 760° C., the area fraction of the polygonal ferrite becomes large excessively and the area fraction of the bainitic ferrite grains, the area fraction of the retained austenite, or the area fractions of the both become small excessively. Thus, the annealing temperature is set to 760° C. or more and preferably set to 770° C. or more. On the other hand, when the annealing temperature is greater than 800° C., with the austenite transformation, the area fraction of the austenite becomes large and the area fraction of the bainitic ferrite becomes small excessively. Thus, the annealing temperature is set to 800° C. or less and preferably set to 790° C. or less.


A cooling stop temperature of the third cooling is set to 600° C. to 750° C., and a cooling rate up to the cooling stop temperature is set to 1° C./second to 10° C./second. When the cooling stop temperature is less than 600° C., the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling stop temperature is set to 600° C. or more and preferably set to 630° C. or more. On the other hand, when the cooling stop temperature is greater than 750° C., the area fraction of the martensite becomes large excessively. Thus, the cooling stop temperature is set to 750° C. or less and preferably set to 730° C. or less. When the cooling rate of the third cooling is less than 1.0° C./second, the area fraction of the polygonal ferrite becomes large excessively. Thus, the cooling rate is set to 1.0° C./second or more and preferably set to 3° C./second or more. On the other hand, when the cooling rate is greater than 10° C./second, the area fraction of the bainitic ferrite becomes small excessively. Thus, the cooling rate is set to 10° C./second or less and preferably set to 8° C./second or less.


When the hole expandability is more important than the ductility, the cooling stop temperature is preferably set to 710° C. or more and more preferably set to 720° C. or more. This is because it is easy to bring the area fraction of the polygonal ferrite to 20% or less. When the ductility is more important than the hole expandability, the cooling stop temperature is preferably set to less than 710° C. and more preferably set to 690° C. or less. This is because it is easy to bring the area fraction of the polygonal ferrite to greater than 20% and 40% or less.


After the third cooling, the steel sheet is cooled down to a temperature of 150° C. to 550° C. and is retained at the temperature for one second or more. During this retention (the second retention), the diffusion of C into the retained austenite is promoted. When the retention time is less than one second, C does not concentrate in the retained austenite sufficiently, the stability of the retained austenite decreases, and the area fraction of the retained austenite becomes small excessively. Thus, the retention time is set to one second or more and preferably set to two seconds or more. When the retention temperature is less than 150° C., C does not concentrate in the retained austenite sufficiently, the stability of the retained austenite decreases, and the area fraction of the retained austenite becomes small excessively. Thus, the retention temperature is set to 150° C. or more and preferably set to 200° C. or more. On the other hand, when the retention temperature is greater than 550° C., the transformation from austenite into bainitic ferrite is delayed, and thus, the diffusion of C into retained austenite is not promoted, the stability of the retained austenite decreases, and the area fraction of the retained austenite becomes small excessively. Thus, the retention temperature is set to 550° C. or less and preferably set to 500° C. or less.


In this manner, the steel sheet according to the embodiment of the present invention can be manufactured.


In the embodiment of the present invention described above, a part of the austenite is transformed into ferrite by controlling the primary cooling rate of the first annealing to 1° C./s or more and less than 10° C./s. With the generation of ferrite, Mn is diffused into untransformed austenite to concentrate therein. By the concentration of Mn in the austenite, during the second retention of the second annealing, a yield stress of the austenite increases and a crystal orientation advantageous for mitigating a transformation stress to occur with the transformation into bainitic ferrite is preferentially generated. Therefore, the strain introduced into the bainitic ferrite is reduced, thereby making it possible to control the dislocation density to 8×102 (cm/cm3) or less. Controlling the dislocation density of the bainitic ferrite to 8×102 (cm/cm3) or less makes it possible to increase working efficacy at the time of plastic deformation, and thus, it is possible to obtain excellent ductility. The mechanism, in which by reducing the dislocation density of the bainitic ferrite, the ductility improves, is as follows. When martensite is generated from retained austenite by strain-induced transformation, dislocation is introduced into adjacent bainitic ferrite to work-harden a TRIP steel. When the dislocation density of the bainitic ferrite is low, a work hardening rate can be maintained high even in a region with large strain, and thus uniform elongation improves.


On the steel sheet, a plating treatment such as an electroplating treatment or a deposition plating treatment may be performed, and further an alloying treatment may be performed after the plating treatment. On the steel sheet, surface treatments such as organic coating film forming, film laminating, organic salts/inorganic salts treatment, and non-chromium treatment may be performed.


When a hot-dip galvanizing treatment is performed on the steel sheet as the plating treatment, for example, the steel sheet is heated or cooled to a temperature that is equal to or more than a temperature 40° C. lower than the temperature of a galvanizing bath and is equal to or less than a temperature 50° C. higher than the temperature of the galvanizing bath and is passed through the galvanizing bath. By the hot-dip galvanizing treatment, a steel sheet having a hot-dip galvanizing layer provided on the surface, namely a hot-dip galvanized steel sheet is obtained. The hot-dip galvanizing layer has a chemical composition represented by, for example, Fe: 7 mass % or more and 15 mass % or less and the balance: Zn, Al, and impurities.


When an alloying treatment is performed after the hot-dip galvanizing treatment, for example, the hot-dip galvanized steel sheet is heated to a temperature that is 460° C. or more and 600° C. or less. When the temperature is less than 460° C., alloying sometimes becomes short in some cases. When the temperature is greater than 600° C., alloying becomes excessive and corrosion resistance deteriorates in some cases. By the alloying treatment, a steel sheet having an alloyed hot-dip galvanizing layer provided on the surface, namely, an alloyed hot-dip galvanized steel sheet is obtained.


It should be noted that the above-described embodiment merely illustrates a concrete example of implementing the present invention, and the technical scope of the present invention is not to be construed in a restrictive manner by the embodiment. That is, the present invention may be implemented in various forms without departing from the technical spirit or main features thereof.


EXAMPLE

Next, there will be explained examples of the present invention. Conditions of the examples are condition examples employed for confirming the applicability and effects of the present invention, and the present invention is not limited to these condition examples. The present invention can employ various conditions as long as the object of the present invention is achieved without departing from the spirit of the invention.


(First Test)


In a first test, slabs having chemical compositions illustrated in Table 1 to Table 3 were manufactured. Each space in Table 1 to Table 3 indicates that the content of a corresponding element is less than a detection limit, and the balance is Fe and impurities. Each underline in Table 1 to Table 3 indicates that a corresponding numerical value is out of the range of the present invention.











TABLE 1







STEEL
CHEMICAL COMPOSITION (MASS %)


























No.
C
Si
Mn
P
S
N
Al
Si + Al
Ti
Nb
B
Mo
Cr
V
Mg
REM
Ca
Ar3




























1
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


2

0.064

1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


3
0.145
1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


4
0.191
1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


5
0.270
1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


6

0.651

1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


7
0.195

0.4

2.6
0.009
0.003
0.003
0.035

0.4










810


8
0.195
0.9
2.6
0.009
0.003
0.003
0.035
0.9









820


9
0.199
1.8
2.6
0.009
0.003
0.003
0.035
1.8









820


10
0.195
2.3
2.6
0.009
0.003
0.003
0.035
2.3









820


11
0.195

4.9

2.6
0.009
0.003
0.003
0.035
4.9









830


12
0.195
1.8

0.3

0.009
0.003
0.003
0.035
1.8









920


13
0.195
1.8
1.5
0.009
0.003
0.003
0.035
1.8









880


14
0.195
1.7
2.6
0.009
0.003
0.003
0.035
1.8









820


15
0.195
1.8
3.3
0.009
0.003
0.003
0.035
1.8









810


16
0.195
1.8

4.8

0.009
0.003
0.003
0.035
1.8









800


17
0.195
1.9
2.6
0.009
0.003
0.003
0.035
1.8









820


18
0.195
1.8
2.6

0.034

0.003
0.003
0.035
1.8









820


19
0.191
1.7
2.6
0.009
0.003
0.003
0.035
1.8









820


20
0.195
1.8
2.6
0.009
0.010
0.003
0.035
1.8









820


21
0.195
1.8
2.6
0.009

0.120

0.003
0.035
1.8









820


22
0.199
1.9
2.6
0.009
0.003
0.003
0.035
1.8









820


23
0.195
1.8
2.6
0.009
0.003

0.020

0.035
1.8









820


24
0.191
1.9
2.6
0.009
0.003
0.003
0.035
1.8









820


25
0.195
1.8
2.6
0.009
0.003
0.003
1.400
3.2









820


26
0.195
1.8
2.6
0.009
0.003
0.003

2.500

4.3









820


27
0.199
1.7
2.6
0.009
0.003
0.003
0.035
1.8









820


28
0.195
1.8
2.5
0.009
0.003
0.003
0.035
1.8









820


29
0.195
1.8
2.7
0.009
0.003
0.003
0.035
1.8









820


30
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8
0.015








820


















TABLE 2







STEEL
CHEMICAL COMPOSITION (MASS %)


























No.
C
Si
Mn
P
S
N
Al
Si + Al
Ti
Nb
B
Mo
Cr
V
Mg
REM
Ca
Ar3





31
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8
0.025








820


32
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8
0.090








820


33
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8

0.250









820


34
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8

0.008







820


35
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8

0.018







820


36
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8

0.095







820


37
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.230








820


38
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0008






820


39
0.195
1.8
2.6
0.009
0.003
0.003
0 035
1.8


0.0017






820


40
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0028






820


41
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8



0.0100







820


42
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8



0.012





820


43
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8



0.035





820


44
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8



0.100





820


45
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8




0.650






820


46
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8




0.014




820


47
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8




0.025




820


48
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8




0.065




820


49
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8





2.800





820


50
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8





0.015



820


51
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8





0.025



820


52
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8





0.150



820


53
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8






0.770




820


54
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8






0.0008


820


55
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8






0.0015


820


56
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8






0.0210


820


57
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8







0.0500



820


58
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8







0.0007

820


59
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8







0.0017

820


60
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8







0.0210

820


















TABLE 3







STEEL
CHEMICAL COMPOSITION (MASS %)


























No.
C
Si
Mn
P
S
N
Al
Si + Al
Ti
Nb
B
Mo
Cr
V
Mg
REM
Ca
Ar3






















61
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0450


820


62
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0006
820


63
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0018
820


64
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8


0.0220
820


65
0.195
1.8
2.6
0.009
0.003
0.003
0.035
1.8



0.0470

820


66
0.191
1.8
2.7
0.009
0.003
0.003
0.035
1.8



820


67
0.121
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


68
0.153
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


69
0.172
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


70
0.219
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


71
0.254
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


72
0.313
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


73
0.404
1.8
2.6
0.009
0.003
0.003
0.035
1.8



820


74
0.195
0.7
2.6
0.009
0.003
0.003
0.035
0.7



820


75
0.195
1.2
2.6
0.009
0.003
0.003
0.035
1.2



820


76
0.195
1.5
2.6
0.009
0.003
0.003
0.035
1.5



820


77
0.195
2.1
2.6
0.009
0.003
0.003
0.035
2.1



820


78
0.195
2.8
2.6
0.009
0.003
0.003
0.035
2.8



820


79
0.195
3.4
2.6
0.009
0.003
0.003
0.035
3.4



820


80
0.195
1.8
1.2
0.009
0.003
0.003
0.035
1.8



820


81
0.195
1.8
1.5
0.009
0.003
0.003
0.035
1.8



820


82
0.195
1.8
1.8
0.009
0.003
0.003
0.035
1.8



820


83
0.195
1.8
2.9
0.009
0.003
0.003
0.035
1.8



820


84
0.195
1.8
3.2
0.009
0.003
0.003
0.035
1.8



820


85
0.195
1.8
3.7
0.009
0.003
0.003
0.035
1.8



820


86
0.193
1.8
2.7
0.009
0.003
0.003
0.035
1.8



820


87
0.192
1.8
2.7
0.009
0.003
0.003
0.035
1.8



820









Then, once cooled, or without cooling, the slabs were directly heated to 1100° C. to 1300° C. and hot rolled under the conditions illustrated in Table 4 to Table 7 to obtain hot-rolled steel sheets. Thereafter, pickling was performed and cold rolling was performed under the conditions illustrated in Table 4 to Table 7 to obtain cold-rolled steel sheets. Each underline in Table 4 to Table 7 indicates that a corresponding numerical value is out of the range suitable for manufacturing the steel sheet according to the present invention.











TABLE 4









HOT ROLLING











ROUGH ROLLING
FINISH ROLLING


















TEMPERATURE
REDUCTION
FINISHING

COILING


MANUFACTURE
STEEL
NUMBER OF
OF FINAL PASS
RATIO OF
TEMPERATURE
Ar3
TEMPERATURE


No.
No.
TIMES
(° C.)
FINAL PASS (%)
(° C.)
(° C.)
(° C.)





1
1
5
1080
52
920
820
650


2
1

0

NONE
NONE
920
820
650


3
1
5
780
52
920
820
650


4
1
5
1080
52
920
820
650


5
1
5

1260

52
920
820
650


6
1
5
1080

14

920
820
650


7
1
5
1080
52
920
820
650


8
1
5
1080
52

670

820
650


9
1
5
1080
52
920
820
650


10
1
5
1080
52
920
820
550


11
1
5
1080
52
920
820
650


12
1
5
1080
52
920
820

790



13
1
5
1080
52
920
820
650


14
1
5
1080
52
920
820
650


15
1
5
1080
52
920
820
650


16
1
5
1080
52
920
820
650


17
1
5
1080
52
920
820
650


18
1
5
1080
52
920
820
650


19
1
5
1080
52
920
820
650


20
1
5
1080
52
920
820
650


21
1
5
1080
52
920
820
650


22
1
5
1080
52
920
820
650


23
1
5
1080
52
920
820
650


24
1
5
1080
52
920
820
650


25
1
5
1080
52
920
820
650


26
1
5
1080
52
920
820
650


27
1
5
1080
52
920
820
650


28
1
5
1080
52
920
820
650


29
1
5
1080
52
920
820
650


30
1
5
1080
52
920
820
650


31
1
5
1080
52
920
820
650


32
1
5
1080
52
920
820
650


33
1
5
1080
52
920
820
650


34
1
5
1080
52
920
820
650


35
1
5
1080
52
920
820
650


36
1
5
1080
52
920
820
650


37
1
5
1080
52
920
820
650


38
1
5
1080
52
920
820
650


39
1
5
1080
52
920
820
650


40
1
5
1080
52
920
820
650














HOT ROLLING
COLD ROLLING















THICKNESS OF

THICKNESS OF




MANUFACTURE
HOT-ROLLED
REDUCTION
COLD-ROLLED



No.
SHEET (mm)
RATIO (%)
SHEET (mm)
NOTE







1
2.9
59
1.2
FOR INVENTION EXAMPLE



2
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



3
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



4
2.4
59
1.0
FOR INVENTION EXAMPLE



5
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



6
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



7
2.4
59
1.0
FOR INVENTION EXAMPLE



8
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



9
3.4
59
1.4
FOR INVENTION EXAMPLE



10
2.9
59
1.2
FOR INVENTION EXAMPLE



11
2.9
59
1.2
FOR INVENTION EXAMPLE



12
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



13
1.9

25

1.4
FOR COMPARATIVE EXAMPLE



14
2.1
44
1.2
FOR INVENTION EXAMPLE



15
3.4
59
1.4
FOR INVENTION EXAMPLE



16
4.3
72
1.2
FOR INVENTION EXAMPLE



17
16.7

94

1.0
FOR COMPARATIVE EXAMPLE



18
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



19
2.9
59
1.2
FOR INVENTION EXAMPLE



20
2.4
59
1.0
FOR INVENTION EXAMPLE



21
2.4
59
1.0
FOR INVENTION EXAMPLE



22
3.4
59
1.4
FOR INVENTION EXAMPLE



23
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



24
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



25
2.4
59
1.0
FOR INVENTION EXAMPLE



26
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



27
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



28
3.4
59
1.4
FOR INVENTION EXAMPLE



29
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



30
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



31
3.4
59
1.4
FOR INVENTION EXAMPLE



32
2.9
59
1.2
FOR INVENTION EXAMPLE



33
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



34
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



35
3.4
59
1.4
FOR INVENTION EXAMPLE



36
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



37
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



38
2.4
59
1.0
FOR INVENTION EXAMPLE



39
3.4
59
1.4
FOR INVENTION EXAMPLE



40
2.9
59
1.2
FOR COMPARATIVE EXAMPI.F.



















TABLE 5









HOT ROLLING











ROUGH ROLLING
FINISH ROLLING


















TEMPERATURE
REDUCTION
FINISHING

COILING


MANUFACTURE
STEEL
NUMBER OF
OF FINAL PASS
RATIO OF
TEMPERATURE
Ar3
TEMPERATURE


No.
No.
TIMES
(° C.)
FINAL PASS (%)
(° C.)
(° C.)
(° C.)





41
1
5
1080
52
920
820
650


42
1
5
1080
52
920
820
650


43
1
5
1080
52
920
820
650


44
1
5
1080
52
920
820
650


45
1
5
1080
52
920
820
650


46
1
5
1080
52
920
820
650


47
1
5
1080
52
920
820
650


48
1
5
1080
52
920
820
650


49
1
5
1080
52
920
820
650


50
1
5
1080
52
920
820
650


51
1
5
1080
52
920
820
650


52
1
5
1080
52
920
820
650


53
1
5
1080
52
920
820
650


54
1
5
1080
52
920
820
650


55
1
5
1080
52
920
820
650


56
1
5
1080
52
920
820
650


57
1
5
1080
52
920
820
650


58
1
5
1080
52
920
820
650


59
1
5
1080
52
920
820
650


60
1
5
1080
52
920
820
650


61
1
5
1080
52
920
820
650


62
1
5
1080
52
920
820
650


63
1
5
1080
52
920
820
650


64
1
5
1080
52
920
820
650


65
1
5
1080
52
920
820
650


66

2

5
1080
52
920
820
650


67
3
5
1080
52
920
820
650


68
4
5
1080
52
920
820
650


69
5
5
1080
52
920
820
650


70

6

5
1080
52
920
820
650


71

7

5
1080
52
920
810
650


72
8
5
1080
52
920
820
650


73
9
5
1080
52
920
820
650


74
10 
5
1080
52
920
820
650


75

11

5
1080
52
920
830
650


76

12

5
1080
52
920
920
650


77
13 
5
1080
52
920
880
650


78
14 
5
1080
52
920
820
650


79
15 
5
1080
52
920
810
650


80

16

5
1080
52
920
800
650














HOT ROLLING
COLD ROLLING















THICKNESS OF

THICKNESS OF




MANUFACTURE
HOT-ROLLED
REDUCTION
COLD-ROLLED



No.
SHEET (mm)
RATIO (%)
SHEET (mm)
NOTE







41
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



42
2.9
59
1.2
FOR INVENTION EXAMPLE



43
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



44
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



45
2.9
59
1.2
FOR INVENTION EXAMPLE



46
3.4
59
1.4
FOR INVENTION EXAMPLE



47
2.4
59
1.0
FOR INVENTION EXAMPLE



48
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



49
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



50
2.9
59
1.2
FOR INVENTION EXAMPLE



51
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



52
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



53
2.9
59
1.2
FOR INVENTION EXAMPLE



54
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



55
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



56
2.4
59
1.0
FOR INVENTION EXAMPLE



57
3.4
59
1.4
FOR INVENTION EXAMPLE



58
2.9
59
1.2
FOR INVENTION EXAMPLE



59
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



60
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



61
3.4
59
1.4
FOR INVENTION EXAMPLE



62
2.9
59
1.2
FOR INVENTION EXAMPLE



63
2.9
59
1.2
FOR INVENTION EXAMPLE



64
2.4
59
1.0
FOR INVENTION EXAMPLE



65
3.4
59
1.4
FOR INVENTION EXAMPLE



66
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



67
2.9
59
1.2
FOR INVENTION EXAMPLE



68
2.4
59
1.0
FOR INVENTION EXAMPLE



69
3.4
59
1.4
FOR INVENTION EXAMPLE



70
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



71
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



72
2.4
59
1.0
FOR INVENTION EXAMPLE



73
3.4
59
1.4
FOR INVENTION EXAMPLE



74
2.9
59
1.2
FOR INVENTION EXAMPLE



75
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



76
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



77
3.4
59
1.4
FOR INVENTION EXAMPLE



78
2.9
59
1.2
FOR INVENTION EXAMPLE



79
3.4
59
1.4
FOR INVENTION EXAMPLE



80
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



















TABLE 6









HOT ROLLING











ROUGH ROLLING
FINISH ROLLING


















TEMPERATURE
REDUCTION
FINISHING

COILING


MANUFACTURE
STEEL
NUMBER OF
OF FINAL PASS
RATIO OF
TEMPERATURE
Ar3
TEMPERATURE


No.
No.
TIMES
(° C.)
FINAL PASS (%)
(° C.)
(° C.)
(° C.)





81
17
5
1080
52
920
820
650


82

18

5
1080
52
920
820
650


83
19
5
1080
52
920
820
650


84
20
5
1080
52
920
820
650


85

21

5
1080
52
920
820
650


86
22
5
1080
52
920
820
650


87

23

5
1080
52
920
820
650


88
24
5
1080
52
920
810
650


89
25
5
1080
52
920
820
650


90

26

5
1080
52
920
820
650


91
27
5
1080
52
920
810
650


92
28
5
1080
52
920
820
650


93
29
5
1080
52
920
830
650


94
30
5
1080
52
920
820
650


95
31
5
1080
52
920
820
650


96
32
5
1080
52
920
820
650


97

33

5
1080
52
920
820
650


98
34
5
1080
52
920
820
650


99
35
5
1080
52
920
820
650


100
36
5
1080
52
920
820
650


101

37

5
1080
52
920
820
650


102
38
5
1080
52
920
820
650


103
39
5
1080
52
920
820
650


104
40
5
1080
52
920
820
650


105

41

5
1080
52
920
820
650


106
42
5
1080
52
920
820
650


107
43
5
1080
52
920
820
650


108
44
5
1080
52
920
820
650


109

45

5
1080
52
920
820
650


110
46
5
1080
52
920
820
650


111
47
5
1080
52
920
820
650


112
48
5
1080
52
920
820
650


113

49

5
1080
52
920
820
650


114
50
5
1080
52
920
820
650


115
51
5
1080
52
920
820
650


116
52
5
1080
52
920
820
650


117

53

5
1080
52
920
820
650


118
54
5
1080
52
920
820
650


119
55
5
1080
52
920
820
650


120
56
5
1080
52
920
820
650














HOT ROLLING
COLD ROLLING















THICKNESS OF

THICKNESS OF




MANUFACTURE
HOT-ROLLED
REDUCTION
COLD-ROLLED



No.
SHEET (mm)
RATIO (%)
SHEET (mm)
NOTE







81
2.4
59
1.0
FOR INVENTION EXAMPLE



82
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



83
2.9
59
1.2
FOR INVENTION EXAMPLE



84
2.4
59
1.0
FOR INVENTION EXAMPLE



85
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



86
3.4
59
1.4
FOR INVENTION EXAMPLE



87
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



88
2.9
59
1.2
FOR INVENTION EXAMPLE



89
2.4
59
1.0
FOR INVENTION EXAMPLE



90
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



91
2.9
59
1.2
FOR INVENTION EXAMPLE



92
3.4
59
1.4
FOR INVENTION EXAMPLE



93
2.9
59
1.2
FOR INVENTION EXAMPLE



94
2.4
59
1.0
FOR INVENTION EXAMPLE



95
3.4
59
1.4
FOR INVENTION EXAMPLE



96
2.9
59
1.2
FOR INVENTION EXAMPLE



97
2.4
59
1.0
FOR COMPARATIVE EXAMPLE



98
2.4
59
1.0
FOR INVENTION EXAMPLE



99
3.4
59
1.4
FOR INVENTION EXAMPLE



100
2.9
59
1.2
FOR INVENTION EXAMPLE



101
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



102
2.4
59
1.0
FOR INVENTION EXAMPLE



103
3.4
59
1.4
FOR INVENTION EXAMPLE



104
2.9
59
1.2
FOR INVENTION EXAMPLE



105
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



106
2.9
59
1.2
FOR INVENTION EXAMPLE



107
2.4
59
1.0
FOR INVENTION EXAMPLE



108
3.4
59
1.4
FOR INVENTION EXAMPLE



109
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



110
2.4
59
1.0
FOR INVENTION EXAMPLE



111
2.4
59
1.0
FOR INVENTION EXAMPLE



112
3.4
59
1.4
FOR INVENTION EXAMPLE



113
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



114
2.9
59
1.2
FOR INVENTION EXAMPLE



115
2.4
59
1.0
FOR INVENTION EXAMPLE



116
3.4
59
1.4
FOR INVENTION EXAMPLE



117
2.9
59
1.2
FOR COMPARATIVE EXAMPLE



118
3.4
59
1.4
FOR INVENTION EXAMPLE



119
2.9
59
1.2
FOR INVENTION EXAMPLE



120
2.4
59
1.0
FOR INVENTION EXAMPLE



















TABLE 7









HOT ROLLING











ROUGH ROLLING
FINISH ROLLING


















TEMPERATURE
REDUCTION
FINISHING

COILING


MANUFACTURE
STEEL
NUMBER OF
OF FINAL PASS
RATIO OF
TEMPERATURE
Ar3
TEMPERATURE


No.
No.
TIMES
(° C.)
FINAL PASS (%)
(° C.)
(° C.)
(° C.)





121

57

5
1080
52
920
820
650


122
58
5
1080
52
920
820
650


123
59
5
1080
52
920
820
650


124
60
5
1080
52
920
820
650


125

61

5
1080
52
920
820
650


126
62
5
1080
52
920
820
650


127
63
5
1080
52
920
820
650


128
64
5
1080
52
920
820
650


129

65

5
1080
52
920
820
650


130
66
5
1080
52
920
820
650


131
67
5
1080
52
920
820
650


132
68
5
1080
52
920
820
650


133
69
5
1080
52
920
820
650


134
70
5
1080
52
920
820
650


135
71
5
1080
52
920
820
650


136
72
5
1080
52
920
820
650


137
73
5
1080
52
920
820
650


138
74
5
1080
52
920
820
650


139
75
5
1080
52
920
820
650


140
76
5
1080
52
920
820
650


141
77
5
1080
52
920
820
650


142
78
5
1080
52
920
820
650


143
79
5
1080
52
920
820
650


144
80
5
1080
52
920
820
650


145
81
5
1080
52
920
820
650


146
82
5
1080
52
920
820
650


147
83
5
1080
52
920
820
650


148
84
5
1080
52
920
820
650


149
85
5
1080
52
920
820
650


150
86
5
1080
52
920
820
650


151
87
5
1080
52
920
820
650


152
1
5
1080
52
920
638
650














HOT ROLLING
COLD ROLLING















THICKNESS OF

THICKNESS OF




MANUFACTURE
HOT-ROLLED
REDUCTION
COLD-ROLLED



No.
SHEET(mm)
RATIO (%)
SHEET (mm)
NOTE







121
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



122
2.9
59
1.2
FOR INVENTION EXAMPLE



123
2.4
59
1.0
FOR INVENTION EXAMPLE



124
2.4
59
1.0
FOR INVENTION EXAMPLE



125
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



126
2.9
59
1.2
FOR INVENTION EXAMPLE



127
2.9
59
1.2
FOR INVENTION EXAMPLE



128
2.4
59
1.0
FOR INVENTION EXAMPLE



129
3.4
59
1.4
FOR COMPARATIVE EXAMPLE



130
2.9
59
1.2
FOR INVENTION EXAMPLE



131
2.9
59
1.2
FOR INVENTION EXAMPLE



132
2.9
59
1.2
FOR INVENTION EXAMPLE



133
2.9
59
1.2
FOR INVENTION EXAMPLE



134
2.9
59
1.2
FOR INVENTION EXAMPLE



135
2.9
59
1.2
FOR INVENTION EXAMPLE



136
2.9
59
1.2
FOR INVENTION EXAMPLE



137
2.9
59
1.2
FOR INVENTION EXAMPLE



138
2.9
59
1.2
FOR INVENTION EXAMPLE



139
2.9
59
1.2
FOR INVENTION EXAMPLE



140
2.9
59
1.2
FOR INVENTION EXAMPLE



141
2.9
59
1.2
FOR INVENTION EXAMPLE



142
2.9
59
1.2
FOR INVENTION EXAMPLE



143
2.9
59
1.2
FOR INVENTION EXAMPLE



144
2.9
59
1.2
FOR INVENTION EXAMPLE



145
2.9
59
1.2
FOR INVENTION EXAMPLE



146
2.9
59
1.2
FOR INVENTION EXAMPLE



147
2.9
59
1.2
FOR INVENTION EXAMPLE



148
2.9
59
1.2
FOR INVENTION EXAMPLE



149
2.9
59
1.2
FOR INVENTION EXAMPLE



150
2.9
59
1.2
FOR INVENTION EXAMPLE



151
2.9
59
1.2
FOR INVENTION EXAMPLE



152
2.9
59
1.2
FOR COMPARATIVE EXAMPLE










Then, under the conditions illustrated in Table 8 to Table 11, first annealing of the cold-rolled steel sheets was performed to obtain intermediate steel sheets. Each underline in Table 8 to Table 11 indicates that a corresponding numerical value is out of the range suitable for manufacturing the steel sheet according to the present invention.











TABLE 8









FIRST ANNEALING










FIRST COOLING
SECOND COOLING
















COOLING

COOLING




ANNEALING
STOPPING
RATE
STOPPING
RATE


MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
(° C./


No.
(° C.)
(° C.)
SECOND)
T1 (° C.)
SECOND)
REHEATING





1
840
680
3
250
40
NOT PERFORMED


2
840
680
3
250
40
NOT PERFORMED


3
840
680
3
250
40
NOT PERFORMED


4
840
680
3
250
40
NOT PERFORMED


5
840
680
3
250
40
NOT PERFORMED


6
840
680
3
250
40
NOT PERFORMED


7
840
680
3
250
40
NOT PERFORMED


8
840
680
3
250
40
NOT PERFORMED


9
840
680
3
250
40
NOT PERFORMED


10
840
680
3
250
40
NOT PERFORMED


11
840
680
3
250
40
NOT PERFORMED


12
840
680
3
250
40
NOT PERFORMED


13
840
680
3
250
40
NOT PERFORMED


14
840
680
3
250
40
NOT PERFORMED


15
840
680
3
250
40
NOT PERFORMED


16
840
680
3
250
40
NOT PERFORMED


17
840
680
3
250
40
NOT PERFORMED


18

670

680
3
250
40
NOT PERFORMED


19
760
680
3
250
40
NOT PERFORMED


20
800
680
3
250
40
NOT PERFORMED


21
840
680
3
250
40
NOT PERFORMED


22
880
680
3
250
40
NOT PERFORMED


23

920

680
3
250
40
NOT PERFORMED


24
840

550

3
250
40
NOT PERFORMED


25
840
680
3
250
40
NOT PERFORMED


26
840

760

3
250
40
NOT PERFORMED


27
840
680
  0.5
250
40
NOT PERFORMED


28
840
680
3
250
40
NOT PERFORMED


29
840
680

15

250
40
NOT PERFORMED


30
840
680
3

110

40
PERFORMED


31
840
680
3
250
40
NOT PERFORMED


32
840
680
3
400
40
NOT PERFORMED


33
840
680
3

555

40
NOT PERFORMED


34
840
680
3
250
4
NOT PERFORMED


35
840
680
3
250
40
NOT PERFORMED


36
840
680
3
250

77

NOT PERFORMED


37
840
680
3
250
40
NOT PERFORMED


38
840
680
3
250
40
NOT PERFORMED


39
840
680
3
250
40
PERFORMED


40
840
680
3
250
40
PERFORMED













FIRST ANNEALING












REHEATING
FIRST RETENTION














MANUFACTURE
TEMPERATURE
TIME
t1




No.
T2 (° C.)
(SECOND)
(SECOND)
NOTE







1
250
375
206
FOR INVENTION EXAMPLE



2
250
375
206
FOR COMPARATIVE EXAMPLE



3
250
375
206
FOR COMPARATIVE EXAMPLE



4
250
375
206
FOR INVENTION EXAMPLE



5
250
375
206
FOR COMPARATIVE EXAMPLE



6
250
375
206
FOR COMPARATIVE EXAMPLE



7
250
375
206
FOR INVENTION EXAMPLE



8
250
375
206
FOR COMPARATIVE EXAMPLE



9
250
375
206
FOR INVENTION EXAMPLE



10
250
375
206
FOR INVENTION EXAMPLE



11
250
375
206
FOR INVENTION EXAMPLE



12
250
375
206
FOR COMPARATIVE EXAMPLE



13
250
375
206
FOR COMPARATIVE EXAMPLE



14
250
375
206
FOR INVENTION EXAMPLE



15
250
375
206
FOR INVENTION EXAMPLE



16
250
375
206
FOR INVENTION EXAMPLE



17
250
375
206
FOR COMPARATIVE EXAMPLE



18
250
375
223
FOR COMPARATIVE EXAMPLE



19
250
375
214
FOR INVENTION EXAMPLE



20
250
375
210
FOR INVENTION EXAMPLE



21
250
375
206
FOR INVENTION EXAMPLE



22
250
375
202
FOR INVENTION EXAMPLE



23
250
375
198
FOR COMPARATIVE EXAMPLE



24
250
375
219
FOR COMPARATIVE EXAMPLE



25
250
375
206
FOR INVENTION EXAMPLE



26
250
375
198
FOR COMPARATIVE EXAMPLE



27
250
375
206
FOR COMPARATIVE EXAMPLE



28
250
375
206
FOR INVENTION EXAMPLE



29
250
375
206
FOR COMPARATIVE EXAMPLE



30
250
375
66
FOR COMPARATIVE EXAMPLE



31
250
375
206
FOR INVENTION EXAMPLE



32
400
375
356
FOR INVENTION EXAMPLE



33
250
375
511
FOR COMPARATIVE EXAMPLE



34
250
375
206
FOR COMPARATIVE EXAMPLE



35
250
375
206
FOR INVENTION EXAMPLE



36
250
375
206
FOR COMPARATIVE EXAMPLE



37

115

375
206
FOR COMPARATIVE EXAMPLE



38
250
375
206
FOR INVENTION EXAMPLE



39
400
375
206
FOR INVENTION EXAMPLE



40

555

375
206
FOR COMPARATIVE EXAMPLE



















TABLE 9









FIRST ANNEALING










FIRST COOLING
SECOND COOLING
















COOLING

COOLING




ANNEALING
STOPPING
RATE
STOPPING
RATE


MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
(° C./


No.
(° C.)
(° C.)
SECOND)
T1 (° C.)
SECOND)
REHEATING





41
840
680
3
250
40
NOT PERFORMED


42
840
680
3
250
40
NOT PERFORMED


43
840
680
3
250
40
NOT PERFORMED


44
840
680
3
250
40
NOT PERFORMED


45
840
680
3
250
40
NOT PERFORMED


46
840
680
3
250
40
NOT PERFORMED


47
840
680
3
250
40
NOT PERFORMED


48
840
680
3
250
40
NOT PERFORMED


49
840
680
3
250
40
NOT PERFORMED


50
840
680
3
250
40
NOT PERFORMED


51
840
680
3
250
40
NOT PERFORMED


52
840
680
3
250
40
NOT PERFORMED


53
840
680
3
250
40
NOT PERFORMED


54
840
680
3
250
40
NOT PERFORMED


55
840
680
3
250
40
NOT PERFORMED


56
840
680
3
250
40
NOT PERFORMED


57
840
680
3
250
40
NOT PERFORMED


58
840
680
3
250
40
NOT PERFORMED


59
840
680
3
250
40
NOT PERFORMED


60
840
680
3
250
40
NOT PERFORMED


61
840
680
3
250
40
NOT PERFORMED


62
840
680
3
250
40
NOT PERFORMED


63
840
680
3
250
40
PERFORMED


64
840
680
3
250
40
NOT PERFORMED


65
840
680
3
250
40
PERFORMED


66
840
680
3
250
40
NOT PERFORMED


67
840
680
3
250
40
NOT PERFORMED


68
840
680
3
250
40
NOT PERFORMED


69
840
680
3
250
40
NOT PERFORMED


70
840
680
3
250
40
NOT PERFORMED


71
840
680
3
250
40
NOT PERFORMED


72
840
680
3
250
40
NOT PERFORMED


73
840
680
3
250
40
NOT PERFORMED


74
840
680
3
250
40
NOT PERFORMED


75
840
680
3
250
40
NOT PERFORMED


76
840
680
3
250
40
NOT PERFORMED


77
840
680
3
250
40
NOT PERFORMED


78
840
680
3
250
40
NOT PERFORMED


79
840
680
3
250
40
NOT PERFORMED


80
840
680
3
250
40
NOT PERFORMED













FIRST ANNEALING












REHEATING
FIRST RETENTION














MANUFACTURE
TEMPERATURE
TIME
t1




No.
T2 (° C.)
(SECOND)
(SECOND)
NOTE







41
250
21
206
FOR COMPARATIVE EXAMPLE



42
250
375
206
FOR INVENTION EXAMPLE



43
250

1600

206
FOR COMPARATIVE EXAMPLE



44
250
375
206
FOR COMPARATIVE EXAMPLE



45
250
375
206
FOR INVENTION EXAMPLE



46
250
375
206
FOR INVENTION EXAMPLE



47
250
375
206
FOR INVENTION EXAMPLE



48
250
375
206
FOR COMPARATIVE EXAMPLE



49
250
375
206
FOR COMPARATIVE EXAMPLE



50
250
375
206
FOR INVENTION EXAMPLE



51
250
375
206
FOR COMPARATIVE EXAMPLE



52
250
375
206
FOR COMPARATIVE EXAMPLE



53
250
375
206
FOR INVENTION EXAMPLE



54
250
375
206
FOR COMPARATIVE EXAMPLE



55
250
375
206
FOR COMPARATIVE EXAMPLE



56
250
375
206
FOR INVENTION EXAMPLE



57
250
375
206
FOR INVENTION EXAMPLE



58
250
375
206
FOR INVENTION EXAMPLE



59
250
375
206
FOR COMPARATIVE EXAMPLE



60
250
375
206
FOR COMPARATIVE EXAMPLE



61
250
375
206
FOR INVENTION EXAMPLE



62
250
375
206
FOR INVENTION EXAMPLE



63
350
375
206
FOR INVENTION EXAMPLE



64
250
375
206
FOR INVENTION EXAMPLE



65
350
375
206
FOR INVENTION EXAMPLE



66
250
375
203
FOR COMPARATIVE EXAMPLE



67
250
375
205
FOR INVENTION EXAMPLE



68
250
375
206
FOR INVENTION EXAMPLE



69
250
375
207
FOR INVENTION EXAMPLE



70
250
375
215
FOR COMPARATIVE EXAMPLE



71
250
375
206
FOR COMPARATIVE EXAMPLE



72
250
375
206
FOR INVENTION EXAMPLE



73
250
375
206
FOR INVENTION EXAMPLE



74
250
375
206
FOR INVENTION EXAMPLE



75
250
375
206
FOR COMPARATIVE EXAMPLE



76
250
375
114
FOR COMPARATIVE EXAMPLE



77
250
375
162
FOR INVENTION EXAMPLE



78
250
375
206
FOR INVENTION EXAMPLE



79
250
375
234
FOR INVENTION EXAMPLE



80
250
375
294
FOR COMPARATIVE EXAMPLE



















TABLE 10









FIRST ANNEALING










FIRST COOLING
SECOND COOLING
















COOLING

COOLING




ANNEALING
STOPPING
RATE
STOPPING
RATE


MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
(° C./


No.
(° C.)
(° C.)
SECOND)
T1 (° C.)
SECOND)
REHEATING





81
840
680
3
250
40
NOT PERFORMED


82
840
680
3
250
40
NOT PERFORMED


83
840
680
3
250
40
NOT PERFORMED


84
840
680
3
250
40
NOT PERFORMED


85
840
680
3
250
40
NOT PERFORMED


86
840
680
3
250
40
NOT PERFORMED


87
840
680
3
250
40
NOT PERFORMED


88
840
680
3
250
40
NOT PERFORMED


89
840
680
3
250
40
NOT PERFORMED


90
840
680
3
250
40
NOT PERFORMED


91
840
680
3
250
40
NOT PERFORMED


92
840
680
3
250
40
NOT PERFORMED


93
840
680
3
250
40
NOT PERFORMED


94
840
680
3
250
40
NOT PERFORMED


95
840
680
3
250
40
NOT PERFORMED


96
840
680
3
250
40
NOT PERFORMED


97
840
680
3
250
40
NOT PERFORMED


98
840
680
3
250
40
NOT PERFORMED


99
840
680
3
250
40
NOT PERFORMED


100
840
680
3
250
40
NOT PERFORMED


101
840
680
3
250
40
NOT PERFORMED


102
840
680
3
250
40
NOT PERFORMED


103
840
680
3
250
40
NOT PERFORMED


104
840
680
3
250
40
NOT PERFORMED


105
840
680
3
250
40
NOT PERFORMED


106
840
680
3
250
40
NOT PERFORMED


107
840
680
3
250
40
NOT PERFORMED


108
840
680
3
250
40
NOT PERFORMED


109
840
680
3
250
40
NOT PERFORMED


110
840
680
3
250
40
NOT PERFORMED


111
840
680
3
250
40
NOT PERFORMED


112
840
680
3
250
40
NOT PERFORMED


113
840
680
3
250
40
NOT PERFORMED


114
840
680
3
250
40
NOT PERFORMED


115
840
680
3
250
40
NOT PERFORMED


116
840
680
3
250
40
NOT PERFORMED


117
840
680
3
250
40
NOT PERFORMED


118
840
680
3
250
40
NOT PERFORMED


119
840
680
3
250
40
NOT PERFORMED


120
840
680
3
250
40
NOT PERFORMED













FIRST ANNEALING












REHEATING
FIRST RETENTION














MANUFACTURE
TEMPERATURE
TIME
t1




No.
T2 (° C.)
(SECOND)
(SECOND)
NOTE







81
250
375
206
FOR INVENTION EXAMPLE



82
250
375
206
FOR COMPARATIVE EXAMPLE



83
250
375
206
FOR INVENTION EXAMPLE



84
250
375
206
FOR INVENTION EXAMPLE



85
250
375
206
FOR COMPARATIVE EXAMPLE



86
250
375
206
FOR INVENTION EXAMPLE



87
250
375
206
FOR COMPARATIVE EXAMPLE



88
250
375
206
FOR INVENTION EXAMPLE



89
250
375
206
FOR INVENTION EXAMPLE



90
250
375
206
FOR COMPARATIVE EXAMPLE



91
250
375
206
FOR INVENTION EXAMPLE



92
250
375
206
FOR INVENTION EXAMPLE



93
250
375
206
FOR INVENTION EXAMPLE



94
250
375
206
FOR INVENTION EXAMPLE



95
250
375
206
FOR INVENTION EXAMPLE



96
250
375
206
FOR INVENTION EXAMPLE



97
250
375
206
FOR COMPARATIVE EXAMPLE



98
250
375
206
FOR INVENTION EXAMPLE



99
250
375
206
FOR INVENTION EXAMPLE



100
250
375
206
FOR INVENTION EXAMPLE



101
250
375
206
FOR COMPARATIVE EXAMPLE



102
250
375
206
FOR INVENTION EXAMPLE



103
250
375
206
FOR INVENTION EXAMPLE



104
250
375
206
FOR INVENTION EXAMPLE



105
250
375
206
FOR COMPARATIVE EXAMPLE



106
250
375
206
FOR INVENTION EXAMPLE



107
250
375
206
FOR INVENTION EXAMPLE



108
250
375
206
FOR INVENTION EXAMPLE



109
250
375
206
FOR COMPARATIVE EXAMPLE



110
250
375
206
FOR INVENTION EXAMPLE



111
250
375
206
FOR INVENTION EXAMPLE



112
250
375
206
FOR INVENTION EXAMPLE



113
250
375
206
FOR COMPARATIVE EXAMPLE



114
250
375
206
FOR INVENTION EXAMPLE



115
250
375
206
FOR INVENTION EXAMPLE



116
250
375
206
FOR INVENTION EXAMPLE



117
250
375
206
FOR COMPARATIVE EXAMPLE



118
250
375
206
FOR INVENTION EXAMPLE



119
250
375
206
FOR INVENTION EXAMPLE



120
250
375
206
FOR INVENTION EXAMPLE



















TABLE 11









FIRST ANNEALING










FIRST COOLING
SECOND COOLING
















COOLING

COOLING




ANNEALING
STOPPING
RATE
STOPPING
RATE


MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
(° C./


No.
(° C.)
(° C.)
SECOND)
T1 (° C.)
SECOND)
REHEATING





121
840
680
3
250
40
NOT PERFORMED


122
840
680
3
250
40
NOT PERFORMED


123
840
680
3
250
40
NOT PERFORMED


124
840
680
3
250
40
NOT PERFORMED


125
840
680
3
250
40
NOT PERFORMED


126
840
680
3
250
40
NOT PERFORMED


127
840
680
3
250
40
NOT PERFORMED


128
840
680
3
250
40
NOT PERFORMED


129
840
680
3
250
40
NOT PERFORMED


130
840
680
3
250
40
NOT PERFORMED


131
840
680
3
250
40
NOT PERFORMED


132
840
680
3
250
40
NOT PERFORMED


133
840
680
3
250
40
NOT PERFORMED


134
840
680
3
250
40
NOT PERFORMED


135
840
680
3
250
40
NOT PERFORMED


136
840
680
3
250
40
NOT PERFORMED


137
840
680
3
250
40
NOT PERFORMED


138
840
680
3
250
40
NOT PERFORMED


139
840
680
3
250
40
NOT PERFORMED


140
840
680
3
250
40
NOT PERFORMED


141
840
680
3
250
40
NOT PERFORMED


142
840
680
3
250
40
NOT PERFORMED


143
840
680
3
250
40
NOT PERFORMED


144
840
680
3
250
40
NOT PERFORMED


145
840
680
3
250
40
NOT PERFORMED


146
840
680
3
250
40
NOT PERFORMED


147
840
680
3
250
40
NOT PERFORMED


148
840
680
3
250
40
NOT PERFORMED


149
840
680
3
250
40
NOT PERFORMED


150
840
680
3
250
40
NOT PERFORMED


151
840
680
3
250
40
NOT PERFORMED


152
840
680
3
250
40
NOT PERFORMED













FIRST ANNEALING












REHEATING
FIRST RETENTION














MANUFACTURE
TEMPERATURE
TIME
t1




No.
T2 (° C.)
(SECOND)
(SECOND)
NOTE







121
250
375
206
FOR COMPARATIVE EXAMPLE



122
250
375
206
FOR INVENTION EXAMPLE



123
250
375
206
FOR INVENTION EXAMPLE



124
250
375
206
FOR INVENTION EXAMPLE



125
250
375
206
FOR COMPARATIVE EXAMPLE



126
250
375
206
FOR INVENTION EXAMPLE



127
250
375
206
FOR INVENTION EXAMPLE



128
250
375
206
FOR INVENTION EXAMPLE



129
250
375
206
FOR COMPARATIVE EXAMPLE



130
250
375
206
FOR INVENTION EXAMPLE



131
250
375
206
FOR INVENTION EXAMPLE



132
250
375
206
FOR INVENTION EXAMPLE



133
250
375
206
FOR INVENTION EXAMPLE



134
250
375
206
FOR INVENTION EXAMPLE



135
250
375
206
FOR INVENTION EXAMPLE



136
250
375
206
FOR INVENTION EXAMPLE



137
250
375
206
FOR INVENTION EXAMPLE



138
250
375
206
FOR INVENTION EXAMPLE



139
250
375
206
FOR INVENTION EXAMPLE



140
250
375
206
FOR INVENTION EXAMPLE



141
250
375
206
FOR INVENTION EXAMPLE



142
250
375
206
FOR INVENTION EXAMPLE



143
250
375
206
FOR INVENTION EXAMPLE



144
250
375
206
FOR INVENTION EXAMPLE



145
250
375
206
FOR INVENTION EXAMPLE



146
250
375
206
FOR INVENTION EXAMPLE



147
250
375
206
FOR INVENTION EXAMPLE



148
250
375
206
FOR INVENTION EXAMPLE



149
250
375
206
FOR INVENTION EXAMPLE



150
250
375
206
FOR INVENTION EXAMPLE



151
250
375
206
FOR INVENTION EXAMPLE



152
250
375
206
FOR COMPARATIVE EXAMPLE










Then, a metal structure of each of the intermediate steel sheets was observed. In this observation, an area fraction of polygonal ferrite (PF), an area fraction of bainitic ferrite or tempered martensite (BF-tM), and an area fraction of retained austenite (retained γ) were measured, and further, an area fraction of retained austenite grains in a predetermined form was calculated from the shape of retained austenite. These results are illustrated in Table 12 to Table 15. Each underline in Table 12 to Table 15 indicates that a corresponding numerical value is out of the range suitable for manufacturing the steel sheet according to the present invention.












TABLE 12









METAL STRUCTURE OF INTERMEDIATE STEEL SHEET



















RETAINED γ GRAIN



MANUFACTURE
STEEL



IN PREDETERMINED


No.
No.
PF
BF-tM
RETAINED γ
FORM
NOTE
















1
1
 6
79
15
97
FOR INVENTION EXAMPLE


2
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


3
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


4
1
 6
79
15
97
FOR INVENTION EXAMPLE


5
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


6
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


7
1
 6
79
15
97
FOR INVENTION EXAMPLE


8
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


9
1
 6
79
15
97
FOR INVENTION EXAMPLE


10
1
 6
79
15
97
FOR INVENTION EXAMPLE


11
1
10
80
10
91
FOR INVENTION EXAMPLE


12
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


13
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


14
1
10
80
10
91
FOR INVENTION EXAMPLE


15
1
 6
79
15
97
FOR INVENTION EXAMPLE


16
1
10
80
10
91
FOR INVENTION EXAMPLE


17
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


18
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


19
1
10
80
10
91
FOR INVENTION EXAMPLE


20
1
10
80
10
91
FOR INVENTION EXAMPLE


21
1
 6
79
15
97
FOR INVENTION EXAMPLE


22
1
10
80
10
91
FOR INVENTION EXAMPLE


23
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


24
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


25
1
 6
79
15
97
FOR INVENTION EXAMPLE


26
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


27
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


28
1
 6
79
15
97
FOR INVENTION EXAMPLE


29
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


30
1
 6
79
15
7
FOR COMPARATIVE EXAMPLE


31
1
 6
79
15
97
FOR INVENTION EXAMPLE


32
1
10
80
10
91
FOR INVENTION EXAMPLE


33
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


34
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


35
1
 6
79
15
97
FOR INVENTION EXAMPLE


36
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


37
1
 6
79
15
7
FOR COMPARATIVE EXAMPLE


38
1
 6
79
15
97
FOR INVENTION EXAMPLE


39
1
10
80
10
91
FOR INVENTION EXAMPLE


40
1

70


29

1
9
FOR COMPARATIVE EXAMPLE



















TABLE 13









METAL STRUCTURE OF INTERMEDIATE STEEL SHEET



















RETAINED γ GRAIN



MANUFACTURE
STEEL



IN PREDETERMINED


No.
No.
PF
BF-tM
RETAINED γ
FORM
NOTE
















41
1
 6
79
15
7
FOR COMPARATIVE EXAMPLE


42
1
 6
79
15
97
FOR INVENTION EXAMPLE


43
1
 6
79
15
7
FOR COMPARATIVE EXAMPLE


44
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


45
1
10
80
10
91
FOR INVENTION EXAMPLE


46
1
 6
79
15
97
FOR INVENTION EXAMPLE


47
1
 6
84
10
91
FOR INVENTION EXAMPLE


48
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


49
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


50
1
 6
79
15
97
FOR INVENTION EXAMPLE


51
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


52
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


53
1
 6
79
15
97
FOR INVENTION EXAMPLE


54
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


55
1
 6
79
15
7
FOR COMPARATIVE EXAMPLE


56
1
10
80
10
91
FOR INVENTION EXAMPLE


57
1
 6
79
15
97
FOR INVENTION EXAMPLE


58
1
10
80
10
91
FOR INVENTION EXAMPLE


59
1

70


29

1
9
FOR COMPARATIVE EXAMPLE


60
1
10
88
2
91
FOR COMPARATIVE EXAMPLE


61
1
 6
79
15
97
FOR INVENTION EXAMPLE


62
1
10
80
10
91
FOR INVENTION EXAMPLE


63
1
10
77
13
91
FOR INVENTION EXAMPLE


64
1
 6
80
14
97
FOR INVENTION EXAMPLE


65
1
 6
79
15
97
FOR INVENTION EXAMPLE


66
2

70


29

1

11

FOR COMPARATIVE EXAMPLE


67
3
11
79
10
90
FOR INVENTION EXAMPLE


68
4
 6
79
15
97
FOR INVENTION EXAMPLE


69
5
10
80
10
91
FOR INVENTION EXAMPLE


70
6
 3
83
14
9
FOR COMPARATIVE EXAMPLE


71
7

70


29

1

11

FOR COMPARATIVE EXAMPLE


72
8
10
80
10
90
FOR INVENTION EXAMPLE


73
9
 6
79
15
97
FOR INVENTION EXAMPLE


74
10
10
80
10
91
FOR INVENTION EXAMPLE


75
11

70


29

1
9
FOR COMPARATIVE EXAMPLE


76
12

70


29

1

11

FOR COMPARATIVE EXAMPLE


77
13
10
80
10
90
FOR INVENTION EXAMPLE


78
14
 6
79
15
97
FOR INVENTION EXAMPLE


79
15
10
80
10
91
FOR INVENTION EXAMPLE


80
16

70


29

1
9
FOR COMPARATIVE EXAMPLE



















TABLE 14









METAL STRUCTURE OF INTERMEDIATE STEEL SHEET



















RETAINED γ GRAIN



MANUFACTURE
STEEL



IN PREDETERMINED


No.
No.
PF
BF-tM
RETAINED γ
FORM
NOTE
















81
17
 6
79
15
97
FOR INVENTION EXAMPLE


82
18

70


29

1

11

FOR COMPARATIVE EXAMPLE


83
19
 6
79
15
97
FOR INVENTION EXAMPLE


84
20
10
80
10
91
FOR INVENTION EXAMPLE


85
21
 3
83
14
9
FOR COMPARATIVE EXAMPLE


86
22
 6
79
15
97
FOR INVENTION EXAMPLE


87
23
 3
83
14
9
FOR COMPARATIVE EXAMPLE


88
24
10
80
10
90
FOR INVENTION EXAMPLE


89
25
 6
79
15
97
FOR INVENTION EXAMPLE


90
26

70


29

1
9
FOR COMPARATIVE EXAMPLE


91
27
 6
79
15
97
FOR INVENTION EXAMPLE


92
28
 6
79
15
97
FOR INVENTION EXAMPLE


93
29
10
80
10
90
FOR INVENTION EXAMPLE


94
30
10
80
10
91
FOR INVENTION EXAMPLE


95
31
 6
79
15
97
FOR INVENTION EXAMPLE


96
32
10
80
10
91
FOR INVENTION EXAMPLE


97
33

70


29

1
9
FOR COMPARATIVE EXAMPLE


98
34
10
80
10
91
FOR INVENTION EXAMPLE


99
35
 6
79
15
97
FOR INVENTION EXAMPLE


100
36
10
80
10
91
FOR INVENTION EXAMPLE


101
37

70


29

1
9
FOR COMPARATIVE EXAMPLE


102
38
10
80
10
90
FOR INVENTION EXAMPLE


103
39
 6
79
15
97
FOR INVENTION EXAMPLE


104
40
10
80
10
91
FOR INVENTION EXAMPLE


105
41

70


29

1
9
FOR COMPARATIVE EXAMPLE


106
42
10
80
10
90
FOR INVENTION EXAMPLE


107
43
 6
79
15
97
FOR INVENTION EXAMPLE


108
44
10
80
10
91
FOR INVENTION EXAMPLE


109
45

70


29

1
9
FOR COMPARATIVE EXAMPLE


110
46
10
80
10
90
FOR INVENTION EXAMPLE


111
47
 6
79
15
97
FOR INVENTION EXAMPLE


112
48
10
80
10
91
FOR INVENTION EXAMPLE


113
49

70


29

1
9
FOR COMPARATIVE EXAMPLE


114
50
10
80
10
91
FOR INVENTION EXAMPLE


115
51
 6
79
15
97
FOR INVENTION EXAMPLE


116
52
10
80
10
91
FOR INVENTION EXAMPLE


117
53

70


29

1
9
FOR COMPARATIVE EXAMPLE


118
54
10
80
10
91
FOR INVENTION EXAMPLE


119
55
 6
79
15
97
FOR INVENTION EXAMPLE


120
56
10
80
10
91
FOR INVENTION EXAMPLE



















TABLE 15









METAL STRUCTURE OF INTERMEDIATE STEEL SHEET



















RETAINED γ








GRAIN IN


MANUFACTURE
STEEL


RETAINED
PREDETERMINED


No.
No.
PF
BF-tM
γ
FORM
NOTE
















121
57
3
83
14
9
FOR COMPARATIVE EXAMPLE


122
58
10
80
10
91
FOR INVENTION EXAMPLE


123
59
6
79
15
97
FOR INVENTION EXAMPLE


124
60
10
80
10
91
FOR INVENTION EXAMPLE


125
61
3
83
14
9
FOR COMPARATIVE EXAMPLE


126
62
10
80
10
91
FOR INVENTION EXAMPLE


127
63
6
79
15
97
FOR INVENTION EXAMPLE


128
64
10
80
10
91
FOR INVENTION EXAMPLE


129
65
3
83
14
9
FOR COMPARATIVE EXAMPLE


130
66
6
79
15
97
FOR INVENTION EXAMPLE


131
67
6
79
15
95
FOR INVENTION EXAMPLE


132
68
6
79
15
96
FOR INVENTION EXAMPLE


133
69
6
79
15
97
FOR INVENTION EXAMPLE


134
70
6
79
15
97
FOR INVENTION EXAMPLE


135
71
6
79
15
98
FOR INVENTION EXAMPLE


136
72
6
79
15
98
FOR INVENTION EXAMPLE


137
73
6
79
15
98
FOR INVENTION EXAMPLE


138
74
6
79
15
96
FOR INVENTION EXAMPLE


139
75
6
79
15
96
FOR INVENTION EXAMPLE


140
76
6
79
15
97
FOR INVENTION EXAMPLE


141
77
6
79
15
97
FOR INVENTION EXAMPLE


142
78
6
79
15
98
FOR INVENTION EXAMPLE


143
79
6
79
15
98
FOR INVENTION EXAMPLE


144
80
6
79
15
97
FOR INVENTION EXAMPLE


145
81
6
79
15
97
FOR INVENTION EXAMPLE


146
82
6
79
15
97
FOR INVENTION EXAMPLE


147
83
6
79
15
97
FOR INVENTION EXAMPLE


148
84
6
79
15
97
FOR INVENTION EXAMPLE


149
85
6
79
15
97
FOR INVENTION EXAMPLE


150
86
6
79
15
97
FOR INVENTION EXAMPLE


151
87
6
79
15
97
FOR INVENTION EXAMPLE


152
1
6
79
15
97
FOR COMPARATIVE EXAMPLE









Thereafter, under the conditions illustrated in Table 16 to Table 19, second annealing of the intermediate steel sheets was performed to obtain steel sheet samples. In Manufacture No. 150 and No. 151, after the second annealing, a plating treatment was performed, and in Manufacture No. 151, after the plating treatment, an alloying treatment was performed. As the plating treatment, a hot-dip galvanizing treatment was performed, and the temperature of the alloying treatment was set to 500° C. Each underline in Table 16 to Table 19 indicates that a corresponding numerical value is out of the range suitable for manufacturing the steel sheet according to the present invention.











TABLE 16









SECOND ANNEALING










THIRD COOLING











COOLING













ANNEALING
STOPPING
RATE
SECOND RETENTION












MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
TIME


No.
(° C.)
(° C.)
SECOND)
(° C.)
(SECOND)





1
780
680
3
400
375


2
780
680
3
400
375


3
780
680
3
400
375


4
780
680
3
400
375


5
780
680
3
400
375


6
780
680
3
400
375


7
780
680
3
400
375


8
780
680
3
400
375


9
780
680
3
400
375


10
780
680
3
400
375


11
780
680
3
400
375


12
780
680
3
400
375


13
780
680
3
400
375


14
780
680
3
400
375


15
780
680
3
400
375


16
780
680
3
400
375


17
780
680
3
400
375


18
780
680
3
400
375


19
780
680
3
400
375


20
780
680
3
400
375


21
780
680
3
400
375


22
780
680
3
400
375


23
780
680
3
400
375


24
780
630
3
400
375


25
780
680
3
400
375


26
780
680
3
400
375


27
780
680
3
400
375


28
780
680
3
400
375


29
780
680
3
400
375


30
780
680
3
400
375


31
780
680
3
400
375


32
780
680
3
400
375


33
780
680
3
400
375


34
780
680
3
400
375


35
780
680
3
400
375


36
780
680
3
400
375


37
780
680
3
400
375


38
780
680
3
400
375


39
780
630
3
400
375


40
780
680
3
400
375













PLATING














PRESENCE/
PRESENCE/





ABSENCE
ABSENCE



MANUFACTURE
OF
OF



No.
PLATING
ALLOYING
NOTE







1
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



2
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



3
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



4
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



5
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



6
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



7
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



8
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



9
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



10
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



11
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



12
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



13
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



14
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



15
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



16
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



17
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



18
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



19
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



20
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



21
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



22
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



23
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



24
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



25
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



26
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



27
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



28
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



29
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



30
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



31
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



32
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



33
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



34
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



35
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



36
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



37
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



38
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



39
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



40
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



















TABLE 17









SECOND ANNEALING










THIRD COOLING











COOLING













ANNEALING
STOPPING
RATE
SECOND RETENTION












MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
TIME


No.
(° C.)
(° C.)
SECOND)
(° C.)
(SECOND)





41
780
680
3
400
375


42
780
680
3
400
375


43
780
680
3
400
375


44

740

680
3
400
375


45
770
680
3
400
375


46
780
680
3
400
375


47
800
680
3
400
375


48

840

680
3
400
375


49
780

550

3
400
375


50
780
680
3
400
375


51
780

760

3
400
375


52
780
680
  0.5
400
375


53
780
680
3
400
375


54
780
680

45

400
375


55
780
680
3

110

375


56
780
680
3
375
375


57
780
680
3
400
375


58
780
680
3
425
375


5S
780
680
3

570

375


60
780
680
3
400
   0.2


61
780
680
3
400
375


62
780
680
3
400
375


63
780
680
3
400
375


64
780
680
3
400
375


65
780
680
3
400
375


66
780
680
3
400
375


67
780
680
3
400
375


68
780
680
3
400
375


69
780
680
3
400
375


70
780
680
3
400
375


71
780
680
3
400
375


72
780
680
3
400
375


73
780
680
3
400
375


74
780
680
3
400
375


75
780
680
3
400
375


76
780
680
3
400
375


77
780
680
3
400
375


78
780
680
3
400
375


79
780
680
3
400
375


80
780
680
3
400
375













PLATING














PRESENCE/
PRESENCE/





ABSENCE
ABSENCE



MANUFACTURE
OF
OF



No.
PLATING
ALLOYING
NOTE







41
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



42
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



43
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



44
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



45
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



46
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



47
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



48
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



49
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



50
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



51
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



52
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



53
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



54
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



55
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



56
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



57
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



58
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



5S
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



60
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



61
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



62
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



63
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



64
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



65
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



66
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



67
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



68
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



69
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



70
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



71
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



72
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



73
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



74
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



75
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



76
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



77
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



78
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



79
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



80
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



















TABLE 18









SECOND ANNEALING










THIRD COOLING











COOLING













ANNEALING
STOPPING
RATE
SECOND RETENTION












MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
TIME


No.
(° C.)
(° C.)
SECOND)
(° C.)
(SECOND)





81
780
680
3
400
375


82
780
680
3
400
375


83
780
680
3
400
375


84
780
680
3
400
375


85
780
680
3
400
375


86
780
680
3
400
375


87
780
680
3
400
375


88
780
680
3
400
375


89
780
680
3
400
375


90
780
680
3
400
375


91
800
680
3
400
375


92
800
680
3
400
375


93
800
680
3
400
375


94
800
680
3
400
375


95
800
680
3
400
375


96
800
680
3
400
375


97
800
680
3
400
375


98
800
680
3
400
375


99
800
680
3
400
375


100
800
680
3
400
375


101
800
680
3
400
375


102
800
680
3
400
375


103
800
680
3
400
375


104
800
680
3
400
375


105
800
680
3
400
375


106
800
680
3
400
375


107
800
680
3
400
375


108
800
680
3
400
375


109
800
680
3
400
375


110
800
680
3
400
375


111
800
680
3
400
375


112
800
680
3
400
375


113
800
680
3
400
375


114
800
680
3
400
375


115
800
680
3
400
375


116
800
680
3
400
375


117
800
680
3
400
375


118
800
680
3
400
375


119
800
680
3
400
375


120
800
680
3
400
375













PLATING














PRESENCE/
PRESENCE/





ABSENCE
ABSENCE



MANUFACTURE
OF
OF



No.
PLATING
ALLOYING
NOTE







81
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



82
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



83
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



84
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



85
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



86
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



87
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



88
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



89
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



90
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



91
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



92
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



93
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



94
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



95
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



96
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



97
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



98
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



99
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



100
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



101
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



102
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



103
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



104
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



105
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



106
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



107
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



108
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



109
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



110
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



111
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



112
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



113
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



114
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



115
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



116
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



117
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



118
ABSENCE
ABSENCE
FOR INVENTION EIXAMPLE



119
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



120
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



















TABLE 19









SECOND ANNEALING










THIRD COOLING











COOLING













ANNEALING
STOPPING
RATE
SECOND RETENTION












MANUFACTURE
TEMPERATURE
TEMPERATURE
(° C./
TEMPERATURE
TIME


No.
(° C.)
(° C.)
SECOND)
(° C.)
(SECOND)





121
800
680
3
400
375


122
800
680
3
400
375


123
800
680
3
400
375


124
800
680
3
400
375


125
800
680
3
400
375


126
800
680
3
400
375


127
800
680
3
400
375


128
800
680
3
400
375


129
800
680
3
400
375


130
780
680
3
400
375


131
780
680
3
400
375


132
780
680
3
400
375


133
780
680
3
400
375


134
780
680
3
400
375


135
780
680
3
400
375


136
760
680
3
400
375


137
780
680
3
400
375


138
780
680
3
400
375


139
780
680
3
400
375


140
780
680
3
400
375


141
780
680
3
400
375


142
780
680
3
400
375


143
780
680
3
400
375


144
780
680
3
400
375


145
780
680
3
400
375


146
780
680
3
400
375


147
780
680
3
400
375


148
780
680
3
400
375


149
780
680
3
400
375


150
780
680
3
400
375


151
780
680
3
400
375








152
NOT PERFORMED













PLATING














PRESENCE/
PRESENCE/





ABSENCE
ABSENCE



MANUFACTURE
OF
OF



No.
PLATING
ALLOYING
NOTE







121
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



122
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



123
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



124
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



125
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



126
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



127
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



128
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



129
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE



130
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



131
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



132
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



133
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



134
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



135
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



136
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



137
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



138
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



139
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



140
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



141
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



142
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



143
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



144
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



145
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



146
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



147
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



148
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



149
ABSENCE
ABSENCE
FOR INVENTION EXAMPLE



150
PRESENCE
ABSENCE
FOR INVENTION EXAMPLE



151
PRESENCE
PRESENCE
FOR INVENTION EXAMPLE



152
ABSENCE
ABSENCE
FOR COMPARATIVE EXAMPLE










Then, a metal structure of each of the steel sheet samples was observed. In this observation, an area fraction of polygonal ferrite (PF), an area fraction of bainitic ferrite (BF), an area fraction of retained austenite (retained γ), and an area fraction of martensite (M) were measured, and further, an area fraction of retained austenite grains in a predetermined form and an area fraction of bainitic ferrite grains in a predetermined form were calculated from the shapes of retained austenite and bainitic ferrite. These results are illustrated in Table 20 to Table 23. Each underline in Table 20 to Table 23 indicates that a corresponding numerical value is out of the range of the present invention.












TABLE 20









METAL STRUCTURE (%)




















RETAINED γ









GRAIN IN
BF GRAIN IN


MANUFACTURE


RETAINED

PREDETERMINED
PREDETERMINED


No.
PF
BF
γ
M
FORM
FORM
NOTE

















1
25
57
14 
4
88 
90
INVENTION EXAMPLE


2

80


14


1

5

8


69

COMPARATIVE EXAMPLE


3

80


14


1

5

8


69

COMPARATIVE EXAMPLE


4
25
57
14 
4
88 
90
INVENTION EXAMPLE


5
 7

40

13 

40


8


69

COMPARATIVE EXAMPLE


6
 7

40

13 

40


8


69

COMPARATIVE EXAMPLE


7
25
57
14 
4
88 
90
INVENTION EXAMPLE


8

80


14


1

5

8


69

COMPARATIVE EXAMPLE


9
25
57
14 
4
88 
90
INVENTION EXAMPLE


10
25
57
14 
4
88 
90
INVENTION EXAMPLE


11
18
67
9
6
83 
83
INVENTION EXAMPLE


12

80


14


1

5

8


69

COMPARATIVE EXAMPLE


13

80


14


1

5

8


69

COMPARATIVE EXAMPLE


14
18
67
9
6
83 
83
INVENTION EXAMPLE


15
25
57
14 
4
88 
90
INVENTION EXAMPLE


16
18
67
9
6
83 
83
INVENTION EXAMPLE


17

80


14


1

5

8


69

COMPARATIVE EXAMPLE


18

80


14


1

5

8


69

COMPARATIVE EXAMPLE


19
18
67
9
6
83 
83
INVENTION EXAMPLE


20
25
60
9
6
83 
83
INVENTION EXAMPLE


21
25
57
14 
4
88 
90
INVENTION EXAMPLE


22
18
67
9
6
83 
83
INVENTION EXAMPLE


23

80


14


1

5

8


69

COMPARATIVE EXAMPLE


24

80


14


1

5

8


69

COMPARATIVE EXAMPLE


25
25
57
14 
4
88 
90
INVENTION EXAMPLE


26

80


14


1

5

8


69

COMPARATIVE EXAMPLE


27

80


14


1

5

8


69

COMPARATIVE EXAMPLE


28
25
57
14 
4
88 
90
INVENTION EXAMPLE


29

80


14


1

5

8


69

COMPARATIVE EXAMPLE


30
25
57
14 
4

9

90
COMPARATIVE EXAMPLE


31
25
57
14 
4
88 
90
INVENTION EXAMPLE


32
18
67
9
6
83 
83
INVENTION EXAMPLE


33

80


14


1

5

8


69

COMPARATIVE EXAMPLE


34

80


14


1

5

8


69

COMPARATIVE EXAMPLE


35
25
57
14 
4
88 
90
INVENTION EXAMPLE


36

80


14


1

5

8


69

COMPARATIVE EXAMPLE


37
25
57
14 
4

9

90
COMPARATIVE EXAMPLE


38
25
57
14 
4
88 
90
INVENTION EXAMPLE


39
18
67
9
6
83 
83
INVENTION EXAMPLE


40

80


14


1

5

8


69

COMPARATIVE EXAMPLE



















TABLE 21









METAL STRUCTURE (%)




















RETAINED γ









GRAIN IN
BF GRAIN IN


MANUFACTURE


RETAINED

PREDETERMINED
PREDETERMINED


No.
PF
BF
γ
M
FORM
FORM
NOTE





41
25
57
14
4
9
90
COMPARATIVE EXAMPLE


42
25
57
14
4
88
90
INVENTION EXAMPLE


43
25
57
14
4
9
90
COMPARATIVE EXAMPLE


44

80


14

1
5
8

69

COMPARATIVE EXAMPLE


45
18
67
 9
6
83
83
INVENTION EXAMPLE


46
25
57
14
4
88
90
INVENTION EXAMPLE


47
25
60
 9
6
83
83
INVENTION EXAMPLE


48

80


14

1
5
8

69

COMPARATIVE EXAMPLE


49

80


14

1
5
8

69

COMPARATIVE EXAMPLE


50
25
57
14
4
88
90
INVENTION EXAMPLE


51

80


14

1
5
8

69

COMPARATIVE EXAMPLE


52

80


14

1
5
8

69

COMPARATIVE EXAMPLE


53
25
57
14
4
88
90
INVENTION EXAMPLE


54

80


14

1
5
8

69

COMPARATIVE EXAMPLE


55
25
57
14
4
9
90
COMPARATIVE EXAMPLE


56
18
67
 9
6
83
83
INVENTION EXAMPLE


57
25
57
14
4
88
90
INVENTION EXAMPLE


58
18
67
 9
6
83
83
INVENTION EXAMPLE


59

80


14

1
5
8

69

COMPARATIVE EXAMPLE


60
25
57
14
4
9
90
COMPARATIVE EXAMPLE


61
25
57
14
4
88
90
INVENTION EXAMPLE


62
18
67
 9
6
83
83
INVENTION EXAMPLE


63
18
64
12
6
83
83
INVENTION EXAMPLE


64
25
58
13
4
88
90
INVENTION EXAMPLE


65
25
57
14
4
88
90
INVENTION EXAMPLE


66

80


14

1
5

10


50

COMPARATIVE EXAMPLE


67
18
67
 9
6
82
84
INVENTION EXAMPLE


68
25
57
14
4
88
90
INVENTION EXAMPLE


69
18
67
 9
6
83
83
INVENTION EXAMPLE


70
 7

40

13

40

8

69

COMPARATIVE EXAMPLE


71

80


14

1
5
10

50

COMPARATIVE EXAMPLE


72
18
67
 9
6
82
84
INVENTION EXAMPLE


73
25
57
14
4
88
90
INVENTION EXAMPLE


74
18
67
 9
6
83
83
INVENTION EXAMPLE


75

80


14

1
5
8

69

COMPARATIVE EXAMPLE


76

80


14

1
5

10


50

COMPARATIVE EXAMPLE


77
18
67
 9
6
82
84
INVENTION EXAMPLE


78
25
57
14
4
88
90
INVENTION EXAMPLE


79
18
67
 9
6
83
83
INVENTION EXAMPLE


80

80


14

1
5
8

69

COMPARATIVE EXAMPLE



















TABLE 22









METAL STRUCTURE (%)




















RETAINED γ









GRAIN IN
BF GRAIN IN


MANUFACTURE


RETAINED

PREDETERMINED
PREDETERMINED


No.
PF
BF
γ
M
FORM
FORM
NOTE

















81
25
57
14 
4
88
90
INVENTION EXAMPLE


82

80


14


1

5

10


50

COMPARATIVE EXAMPLE


83
25
57
14 
4
88
90
INVENTION EXAMPLE


84
18
67
9
6
83
83
INVENTION EXAMPLE


85
 7

40

13 

40

8

69

COMPARATIVE EXAMPLE


86
25
57
14 
4
88
90
INVENTION EXAMPLE


87
 7

40

13 

40

8

69

COMPARATIVE EXAMPLE


88
25
60
9
6
82
84
INVENTION EXAMPLE


89
18
64
14 
4
88
90
INVENTION EXAMPLE


90

80


14


1

5
8

69

COMPARATIVE EXAMPLE


91
25
57
14 
4
88
90
INVENTION EXAMPLE


92
25
57
14 
4
88
90
INVENTION EXAMPLE


93
25
60
9
6
82
84
INVENTION EXAMPLE


94
18
67
9
6
83
83
INVENTION EXAMPLE


95
25
57
14 
4
88
90
INVENTION EXAMPLE


96
18
67
9
6
83
83
INVENTION EXAMPLE


97

80


14


1

5
8

69

COMPARATIVE EXAMPLE


98
18
67
9
6
83
83
INVENTION EXAMPLE


99
25
57
14 
4
88
90
INVENTION EXAMPLE


100
18
67
9
6
83
83
INVENTION EXAMPLE


101

80


14


1

5
8

69

COMPARATIVE EXAMPLE


102
18
67
9
6
82
84
INVENTION EXAMPLE


103
25
57
14 
4
88
90
INVENTION EXAMPLE


104
18
67
9
6
83
83
INVENTION EXAMPLE


105

80


14


1

5
8

69

COMPARATIVE EXAMPLE


106
18
67
9
6
82
84
INVENTION EXAMPLE


107
25
57
14 
4
88
90
INVENTION EXAMPLE


108
18
67
9
6
83
83
INVENTION EXAMPLE


109

80


14


1

5
8

69

COMPARATIVE EXAMPLE


110
18
67
9
6
82
84
INVENTION EXAMPLE


111
25
57
14 
4
88
90
INVENTION EXAMPLE


112
18
67
9
6
83
83
INVENTION EXAMPLE


113

80


14


1

5
8

69

COMPARATIVE EXAMPLE


114
18
67
9
6
83
83
INVENTION EXAMPLE


115
25
57
14 
4
88
90
INVENTION EXAMPLE


116
18
67
9
6
83
83
INVENTION EXAMPLE


117

80


14


1

5
8

69

COMPARATIVE EXAMPLE


118
18
67
9
6
83
83
INVENTION EXAMPLE


119
25
57
14 
4
88
90
INVENTION EXAMPLE


120
18
67
9
6
83
83
INVENTION EXAMPLE



















TABLE 23









METAL STRUCTURE (%)




















RETAINED γ









GRAIN IN
BF GRAIN IN


MANUFACTURE


RETAINED

PREDETERMINED
PREDETERMINED


No.
PF
BF
γ
M
FORM
FORM
NOTE

















121
7

40

13

40

8

69

COMPARATIVE EXAMPLE


122
18
67
 9
6
83
83
INVENTION EXAMPLE


123
25
57
14
4
88
90
INVENTION EXAMPLE


124
18
67
 9
6
83
83
INVENTION EXAMPLE


125
7

40

13

40

8

69

COMPARATIVE EXAMPLE


126
18
67
 9
6
83
83
INVENTION EXAMPLE


127
25
57
14
4
88
90
INVENTION EXAMPLE


128
18
67
 9
6
83
83
INVENTION EXAMPLE


129
7

40

13

40

8

69

COMPARATIVE EXAMPLE


130
25
57
14
4
88
90
INVENTION EXAMPLE


131
25
57
14
4
86
90
INVENTION EXAMPLE


132
25
57
14
4
87
90
INVENTION EXAMPLE


133
25
57
14
4
88
90
INVENTION EXAMPLE


134
25
57
14
4
90
90
INVENTION EXAMPLE


135
25
57
14
4
90
90
INVENTION EXAMPLE


136
25
57
14
4
91
90
INVENTION EXAMPLE


137
25
57
14
4
91
90
INVENTION EXAMPLE


138
25
57
14
4
86
90
INVENTION EXAMPLE


139
25
57
14
4
86
90
INVENTION EXAMPLE


140
25
57
14
4
88
90
INVENTION EXAMPLE


141
25
57
14
4
88
90
INVENTION EXAMPLE


142
25
57
14
4
89
90
INVENTION EXAMPLE


143
25
57
14
4
89
90
INVENTION EXAMPLE


144
25
57
14
4
88
90
INVENTION EXAMPLE


145
25
57
14
4
88
90
INVENTION EXAMPLE


146
25
57
14
4
88
90
INVENTION EXAMPLE


147
25
57
14
4
88
90
INVENTION EXAMPLE


148
25
57
14
4
88
90
INVENTION EXAMPLE


149
25
57
14
4
88
90
INVENTION EXAMPLE


150
25
57
14
4
88
90
INVENTION EXAMPLE


151
25
57
14
4
88
90
INVENTION EXAMPLE


152
35
2
3
5

55


41

COMPARATIVE EXAMPLE









Then, mechanical properties (total elongation, a 0.2% proof stress, a tensile strength (maximum tensile strength), a hole expansion value, a ratio of a bend radius to a sheet thickness R/t, and a ductile-brittle transition temperature) of the steel sheet samples were measured. When measuring the total elongation, the 0.2% proof stress, and the tensile strength, a JIS No. 5 test piece with the direction vertical to the rolling direction (sheet width direction) set as the longitudinal direction was collected from each of the steel sheet samples to be subjected to a tensile test in conformity with JIS Z 2242. When measuring the hole expansion value, a hole expanding test of JIS Z 2256 was performed. When measuring the ratio R/t, a test of JIS Z 2248 was performed. When measuring the ductile-brittle transition temperature, a test of JIS Z 2242 was performed. These test results are illustrated in Table 24 to Table 27. Each underline in Table 24 to Table 27 indicates that a corresponding numerical value is out of a desirable range.












TABLE 24









MECHANICAL PROPERTIES

















0.2%

HOLE

DUCTILE-BRITTLE





PROOF
TENSILE
EXPANSION

TRANSITION


MANUFACTURE
ELONGATION
STRESS
STRENGTH
VALUE
RATIO
TEMPERATURE


No.
(%)
(MPa)
(MPa)
(%)
(R/t)
(° C.)
NOTE

















1
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


2

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


3

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


4
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


5

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


6

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


7
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


8

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


9
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


10
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


11
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


12

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


13

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


14
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


15
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


16
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


17

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


18

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


19
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


20
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


21
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


22
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


23

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


24

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


25
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


26

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


27

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


28
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


29

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


30

15

714
1020
55
0.3
−70
COMPARATIVE EXAMPLE


31
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


32
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


33
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


34
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


35
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


36
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


37

15

714
1020
55
0.3
−70
COMPARATIVE EXAMPLE


38
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


39
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


40
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE



















TABLE 25









MECHANICAL PROPERTIES

















0.2%

HOLE

DUCTILE-BRITTLE





PROOF
TENSILE
EXPANSION

TRANSITION


MANUFACTURE
ELONGATION
STRESS
STRENGTH
VALUE
RATIO
TEMPERATURE


No.
(%)
(MPa)
(MPa)
(%)
(R/t)
(° C.)
NOTE





41

15

714
1020
55
0.3
−70
COMPARATIVE EXAMPLE


42
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


43

15

714
1020
55
0.3
−70
COMPARATIVE EXAMPLE


44
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


45
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


46
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


47
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


48
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


49
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


50
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


51
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


52
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


53
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


54
 9
938
1340
15
0.9
−65
COMPARATIVE EXAMPLE


55
15
714
1020
55
0.3
−70
COMPARATIVE EXAMPLE


56
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


57
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


58
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


59
9
938
1340

15


0.9

−65
COMPARATIVE EXAMPLE


60

12

756
1680
51
0.5
−65
COMPARATIVE EXAMPLE


61
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


62
22
756
1680
51
0.5
−65
INVENTION EXAMPLE


63
23
756
1680
51
0.5
−65
INVENTION EXAMPLE


64
24
714
1020
55
0.3
−70
INVENTION EXAMPLE


65
25
714
1020
55
0.3
−70
INVENTION EXAMPLE


66

20


552

788
45
0.4
20
COMPARATIVE EXAMPLE


67
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


68
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


69
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


70

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


71

20


552

788
45
0.4
20
COMPARATIVE EXAMPLE


72
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


73
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


74
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


75

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


76

20


552

788
45
0.4
20
COMPARATIVE EXAMPLE


77
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


78
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


79
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


80

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE



















TABLE 26









MECHANICAL PROPERTIES

















0.2%

HOLE

DUCTILE-BRITTLE





PROOF
TENSILE
EXPANSION

TRANSITION


MANUFACTURE
ELONGATION
STRESS
STRENGTH
VALUE
RATIO
TEMPERATURE


No.
(%)
(MPa)
(MPa)
(%)
(R/t)
(° C.)
NOTE

















81
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


82

20


552

788
45
0.4
20
COMPARATIVE EXAMPLE


83
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


84
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


85

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


86
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


87

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


88
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


89
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


90

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


91
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


92
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


93
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


94
27
721
1030
32
0.5
−65
INVENTION EXAMPLE


95
28
732
1045
37
0.3
−70
INVENTION EXAMPLE


96
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


97

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


98
27
721
1030
32
0.5
−65
INVENTION EXAMPLE


99
28
732
1045
37
0.3
−70
INVENTION EXAMPLE


100
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


101

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


102
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


103
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


104
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


105

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


106
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


107
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


108
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


109

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


110
27
693
 990
32
0.5
−65
INVENTION EXAMPLE


111
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


112
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


113

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


114
27
721
1030
32
0.5
−65
INVENTION EXAMPLE


115
28
732
1045
37
0.3
−70
INVENTION EXAMPLE


116
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


117

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


118
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


119
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


120
27
756
1680
32
0.5
−65
INVENTION EXAMPLE



















TABLE 27









MECHANICAL PROPERTIES

















0.2%

HOLE

DUCTILE-BRITTLE





PROOF
TENSILE
EXPANSION

TRANSITION


MANUFACTURE
ELONGATION
STRESS
STRENGTH
VALUE
RATIO
TEMPERATURE


No.
(%)
(MPa)
(MPa)
(%)
(R/t)
(° C.)
NOTE

















121

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


122
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


123
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


124
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


125

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


126
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


127
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


128
27
756
1680
32
0.5
−65
INVENTION EXAMPLE


129

11

938
1340

12


0.9

−65
COMPARATIVE EXAMPLE


130
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


131
28
714
990
37
0.3
−70
INVENTION EXAMPLE


132
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


133
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


134
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


135
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


136
28
714
1191
37
0.3
−70
INVENTION EXAMPLE


137
28
714
1482
37
0.3
−70
INVENTION EXAMPLE


138
28
714
990
37
0.3
−70
INVENTION EXAMPLE


139
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


140
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


141
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


142
28
714
1184
37
0.3
−70
INVENTION EXAMPLE


143
28
714
1199
37
0.3
−70
INVENTION EXAMPLE


144
28
714
984
37
0.3
−70
INVENTION EXAMPLE


145
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


146
28
714
1020
37
0.3
−70
INVENTION EXAMPLE


147
28
714
1187
37
0.3
−70
INVENTION EXAMPLE


148
28
714
1290
37
0.3
−70
INVENTION EXAMPLE


149
28
714
1476
37
0.3
−70
INVENTION EXAMPLE


150
28
714
1476
37
0.3
−70
INVENTION EXAMPLE


151
28
714
1476
37
0.3
−70
INVENTION EXAMPLE


152
9
652
1420

12


0.9

−65
COMPARATIVE EXAMPLE









As illustrated in Table 24 to Table 27, in invention examples such as Test No. 1 and No. 4 falling within the range of the present invention, excellent elongation, 0.2% proof stress, tensile strength, hole expansion value, ratio R/t, and ductile-brittle transition temperature were obtained.


On the other hand, in comparative examples such as Manufacture No. 2 and No. 3, in which the area fraction of the polygonal ferrite became large excessively, the area fraction of the bainitic ferrite became short, the area fraction of the retained austenite became short, the ratio of the retained austenite grains in a predetermined form became short, and the ratio of the bainitic ferrite grains in a predetermined form became short, the elongation, the hole expansion value, and the ratio R/t were low. In comparative examples such as Manufacture No. 5 and No. 6, in which the area fraction of the bainitic ferrite became short, the area fraction of the martensite became large excessively, the ratio of the retained austenite grains in a predetermined form became short, and the ratio of the bainitic ferrite grains in a predetermined form became short, the elongation, the hole expansion value, and the ratio R/t were low. In comparative examples such as Manufacture No. 30 and No. 37, in which the ratio of the retained austenite grains in a predetermined form became short, the elongation was low. In comparative examples such as Manufacture No. 70 and No. 85, in which the area fraction of the bainitic ferrite became short, the area fraction of the martensite became large excessively, the ratio of the retained austenite grains in a predetermined form became short, and the ratio of the bainitic ferrite grains in a predetermined form became short, the elongation, the hole expansion value, and the ratio R/t were low.


INDUSTRIAL APPLICABILITY

The present invention can be utilized in, for example, industries relating to a steel sheet suitable for automotive parts.

Claims
  • 1. A steel sheet, comprising: a chemical composition represented by,in mass %,C: 0.10% to 0.5%,Si: 0.5% to 4.0%,Mn: 1.0% to 4.0%,P: 0.015% or less,S: 0.050% or less,N: 0.01% or less,Al: 2.0% or less,Si and Al: 0.5% to 6.0% in total,Ti: 0.00% to 0.20%,Nb: 0.00% to 0.20%,B: 0.0000% to 0.0030%,Mo: 0.00% to 0.50%,Cr: 0.0% to 2.0%,V: 0.00% to 0.50%,Mg: 0.000% to 0.040%,REM: 0.000% to 0.040%,Ca: 0.000% to 0.040%, andthe balance: Fe and impurities; anda metal structure represented by,in area fraction,polygonal ferrite: 40% or less,martensite: 20% or less,bainitic ferrite: 50% to 95%, andretained austenite: 5% to 50%, whereinin area fraction, 80% or more of the bainitic ferrite is composed of bainitic ferrite grains that have an aspect ratio of 0.1 to 1.0 and have a dislocation density of 8×102 (cm/cm3) or less in a region surrounded by a grain boundary with a misorientation angle of 15° or more, andin area fraction, 80% or more of the retained austenite is composed of retained austenite grains that have an aspect ratio of 0.1 to 1.0, have a major axis length of 1.0 μm to 28.0 μm, and have a minor axis length of 0.1 μm to 2.8 μm.
  • 2. The steel sheet according to claim 1, wherein the metal structure is represented by, in area fraction,polygonal ferrite: 5% to 20%,martensite: 20% or less,bainitic ferrite: 75% to 90%, andretained austenite: 5% to 20%.
  • 3. The steel sheet according to claim 1, wherein the metal structure is represented by, in area fraction,polygonal ferrite: greater than 20% and 40% or less,martensite: 20% or less,bainitic ferrite: 50% to 75%, andretained austenite: 5% to 30%.
  • 4. The steel sheet according to claim 1, wherein in the chemical composition, in mass %,Ti: 0.01% to 0.20%,Nb: 0.005% to 0.20%,B: 0.0001% to 0.0030%,Mo: 0.01% to 0.50%,Cr: 0.01% to 2.0%,V: 0.01% to 0.50%,Mg: 0.0005% to 0.040%,REM: 0.0005% to 0.040%, orCa: 0.0005% to 0.040%,or an arbitrary combination of the above is established.
  • 5. The steel sheet according to claim 1, further comprising: a plating layer formed on a surface thereof.
  • 6. The steel sheet according to claim 2, wherein in the chemical composition, in mass %,Ti: 0.01% to 0.20%,Nb: 0.005% to 0.20%,B: 0.0001% to 0.0030%,Mo: 0.01% to 0.50%,Cr: 0.01% to 2.0%,V: 0.01% to 0.50%,Mg: 0.0005% to 0.040%,REM: 0.0005% to 0.040%, orCa: 0.0005% to 0.040%,or an arbitrary combination of the above is established.
  • 7. The steel sheet according to claim 3, wherein in the chemical composition, in mass %,Ti: 0.01% to 0.20%,Nb: 0.005% to 0.20%,B: 0.0001% to 0.0030%,Mo: 0.01% to 0.50%,Cr: 0.01% to 2.0%,V: 0.01% to 0.50%,Mg: 0.0005% to 0.040%,REM: 0.0005% to 0.040%, orCa: 0.0005% to 0.040%,or an arbitrary combination of the above is established.
  • 8. The steel sheet according to claim 2, further comprising: a plating layer formed on a surface thereof.
  • 9. The steel sheet according to claim 3, further comprising: a plating layer formed on a surface thereof.
  • 10. The steel sheet according to claim 4, further comprising: a plating layer formed on a surface thereof.
  • 11. The steel sheet according to claim 6, further comprising: a plating layer formed on a surface thereof.
  • 12. The steel sheet according to claim 7, further comprising: a plating layer formed on a surface thereof.
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2018/013554 3/30/2018 WO 00