STEEL SHEET

Abstract
A steel sheet includes a predetermined chemical composition and a metal structure represented by, in area fraction, ferrite: 30% to 50%, granular bainite: 5% to 20%, martensite: 30% to 55%, bainite: less than 35%, and retained austenite and pearlite: 10% or less in total. Preferably, of the steel sheet, a tensile strength is 1180 MPa or more, elongation is 10% or more, and a hole expansion value is 20% or more. Further preferably, a VDA bending angle in the case where a thickness is set to t (mm) is “7.69t2−38.4t+109” or more.
Description
TECHNICAL FIELD

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


BACKGROUND ART

In order to suppress the emission of carbon dioxide gas from an automobile, a reduction in weight of an automotive vehicle body using a high-strength steel sheet has been in progress. Further, in order also to secure the safety of a passenger, the high-strength steel sheet has come to be often used for the vehicle body. In order to promote a further reduction in weight of the vehicle body, a further improvement in strength is important. On the other hand, some parts of the vehicle body are required to have excellent formability. For example, a high-strength steel sheet for framework system parts is required to have excellent elongation and hole expandability.


However, it is difficult to achieve both the improvement in strength and the improvement in formability.


For example, Patent Literature 1 describes that the distribution of nanohardness of a steel sheet composed of ferrite and martensite is controlled in order to achieve both strength and workability. Patent Literature 1 also describes that a side bend test simulating stretch flange forming is performed when evaluating the workability. However, there is no description about bendability.


The steel sheet described in Patent Literature 2 has a martensite structure as a main phase and is excellent in strength and bendability, but is poor in ductility, and thus cracking may occur at the time of forming.


As the steel sheet excellent in ductility, for example, there exists a TRIP (Transformation Induced Plasticity) steel containing retained austenite described in Patent Literature 3. In the TRIP steel, retained austenite existing in the steel is transformed into martensite at the time of forming, and thereby excellent ductility can be obtained. However, the martensite obtained by the transformation from the retained austenite at the time of forming is hard and is likely to be a starting point of cracking to thus cause deterioration in hole expandability or bendability.


CITATION LIST
Patent Literature

Patent Literature 1: Japanese Laid-open Patent Publication No. 2011-144409


Patent Literature 2: Japanese Examined Patent Application Publication No. 7-74412


Patent Literature 3: Japanese Laid-open Patent Publication No. 10-130776


SUMMARY OF INVENTION
Technical Problem

An object of the present invention is to provide a steel sheet having a high strength and capable of obtaining excellent elongation and hole expandability.


Solution to Problem

The present inventors conducted earnest examinations in order to solve the above-described problems. As a result, they found out that it is important to set the area fraction of ferrite to 30% to 50, set the area fraction of martensite to 30% to 55%, set the area fraction of granular bainite to 5% to 20%, set the area fraction of bainite to less than 35%, and set the total area fraction of retained austenite and pearlite to 10% or less. The martensite includes tempered martensite. The granular bainite is mainly composed of bainitic ferrite whose dislocation density is low and hardly contains hard cementite, and thus is harder than ferrite and softer than bainite and martensite. Thus, the granular bainite exhibits more excellent elongation than the bainite and the martensite. Further, the granular bainite is harder than ferrite and softer than bainite and martensite, to thus suppress that voids occur from an interface between ferrite and martensite or bainite at the time of hole expanding.


The inventor of the present application further conducted earnest examinations repeatedly based on such findings, and then conceived the following various aspects of the invention consequently.


(1) A steel sheet includes:


a chemical composition represented by, in mass %,


C: 0.09% to 0.15%,


Si: 0.2% to 2.5%,


Al: 0.01% to 1.00%,


Mn: 1.0% to 3.0%,


P: 0.02% or less,


S: 0.01% or less,


N: 0.007% or less,


O: 0.006% or less,


Cr: 0.00% to 1.00%,


Mo: 0.00% to 1.00%,


B: 0.0000% to 0.010%,


Nb: 0.000% to 0.30%,


Ti: 0.000% to 0.30%,


Ni: 0.00% to 1.00%,


Cu: 0.00% to 1.00%,


V: 0.000% to 0.50%,


Mg: 0.0000% to 0.04%,


REM: 0.0000% to 0.04%, and


the balance: Fe and impurities; and


a metal structure represented by, in area fraction,


ferrite: 30% to 50%,


granular bainite: 5% to 20%,


martensite: 30% to 55%,


bainite: less than 35%, and


retained austenite and pearlite: 10% or less in total.


(2) The steel sheet according to (1), in which a tensile strength is 1180 MPa or more, elongation is 10% or more, and a hole expansion value is 20% or more.


(3) The steel sheet according to (1) or (2), in which


a VDA bending angle in the case where a thickness is set to t (mm) is “7.69t2−38.4t+109” or more.


(4) The steel sheet according to any one of (1) to (3), further includes:


a hot-dip galvanizing layer on a surface thereof.


(5) The steel sheet according to any one of (1) to (3), further includes:


an alloyed hot-dip galvanizing layer on a surface thereof.


Advantageous Effects of Invention

According to the present invention, granular bainite, and the like are contained in a metal structure with appropriate area fractions, so that it is possible to obtain a high strength and excellent elongation and hole expandability.







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. Although details will be described later, the steel sheet according to the embodiment of the present invention is manufactured by undergoing hot rolling, cold rolling, annealing, tempering, and so on of a steel. Thus, the metal structure of the steel sheet is one in which not only properties of the steel sheet but also phase transformations by these treatments and so on are considered. The steel sheet according to this embodiment includes a metal structure represented by, in area fraction, ferrite: 30% to 50%, granular bainite: 5% to 20%, martensite: 30% to 55%, bainite: less than 35%, and retained austenite and pearlite: 10% or less in total.


(Ferrite: 30% to 50%)


Ferrite is a soft structure, and thus is deformed easily and contributes to an improvement in elongation. Ferrite contributes also to a phase transformation to granular bainite from austenite. When the area fraction of the ferrite is less than 30%, it is impossible to obtain sufficient elongation. Further, it is impossible to obtain an appropriate area fraction of granular bainite. Thus, the area fraction of the ferrite is set to 30% or more and preferably set to 35% or more. On the other hand, when the area fraction of the ferrite is greater than 50%, it is difficult to obtain a tensile strength of 1180 MPa or more. Thus, the area fraction of the ferrite is set to 50% or less and preferably set to 45% or less.


(Granular bainite: 5% to 20%)


Granular bainite is mainly composed of bainitic ferrite whose dislocation density is as low as the order of about 1013 m/m3 and hardly contains hard cementite, and thus is harder than ferrite and softer than bainite. Thus, the granular bainite exhibits more excellent elongation than bainite. The granular bainite is harder than ferrite and softer than bainite and martensite, and thus suppresses that voids occur from an interface between ferrite and martensite and voids occur from an interface between ferrite and bainite at the time of hole expanding. When the area fraction of the granular bainite is less than 5%, it is impossible to sufficiently obtain these effects. Thus, the area fraction of the granular bainite is set to 5% or more and preferably set to 10% or more. On the other hand, when the area fraction of the granular bainite is greater than 20%, it is impossible to sufficiently obtain martensite, resulting in difficulty in obtaining a tensile strength of 1180 MPa or more. Thus, the area fraction of the granular bainite is set to 20% or less and preferably set to 15% or less.


(Martensite: 30% to 55%)


Martensite has a high dislocation density and is a hard structure, and thus contributes to an improvement in tensile strength. When the area fraction of the martensite is less than 30%, it is impossible to obtain a tensile strength of 1180 MPa or more. Thus, the area fraction of the martensite is set to 30% or more and preferably set to 35% or more. On the other hand, when the area fraction of the martensite is greater than 55%, it is impossible to obtain sufficient elongation. Thus, the area fraction of the martensite is set to 55% or less and preferably set to 50% or less. As-quenched martensite and tempered martensite belong to martensite. That is, the area fraction of the martensite is the total of the area fraction of as-quenched martensite and the area fraction of tempered martensite. The method of obtaining the tempered martensite is not limited, and the tempered martensite can be obtained by self-tempering during cooling, or can also be obtained by a tempering heat treatment after continuous annealing.


(Bainite: less than 35%)


Bainite is composed of bainitic ferrite whose dislocation density is as high as about 1.0×1014 m/m3 and hard cementite mainly and contributes to an improvement in tensile strength. However, when the area fraction of the bainite is 35% or more, the area fraction of martensite, which contributes to an improvement in tensile strength rather than bainite, goes short, resulting in difficulty in obtaining a tensile strength of 1180 MPa or more. Thus, the area fraction of the bainite is set to less than 35%.


(Retained austenite and Pearlite: 10% or less in total)


Retained austenite is transformed into martensite by strain-induced transformation during deformation, bringing about excellent work hardening and high uniform elongation. However, the strain-induced transformed martensite impairs hole expandability significantly. Pearlite contains hard cementite, to thus be a starting point from which voids occur at the time of hole expanding to impair hole expandability. When the total area fraction of the retained austenite and the pearlite is greater than 10% in particular, the impairment of hole expandability is prominent. Thus, the total area fraction of the retained austenite and the pearlite is set to 10% or less.


Identifications of the ferrite, the granular bainite, the martensite, the bainite, the retained austenite, and the pearlite and determinations of the area fractions of them can be performed by, for example, an electron back scattering diffraction (EBSD) method, an X-ray measurement, or a scanning electron microscope (SEM) observation. In the case where the SEM observation is performed, for example, a nital reagent or a LePera reagent is used to corrode a sample and a cross section parallel to a rolling direction and a thickness direction and/or a cross section vertical to the rolling direction are/is observed at 1000-fold to 50000-fold magnification. A metal structure in a region at about a ¼ thickness of the steel sheet as the depth from the surface can represent the metal structure of the steel sheet. In the case of the thickness of the steel sheet being 1.2 mm, for example, a metal structure in a region at a depth of about 0.3 mm from the surface can represent the metal structure of the steel sheet.


The area fraction of the ferrite can be determined by using an electron channeling contrast image to be obtained by the SEM observation, for example. The electron channeling contrast image expresses a crystal misorientation in a crystal grain as a contrast difference, and in the electron channeling contrast image, a portion with a uniform contrast is the ferrite. In this method, for example, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface is set as an object to be observed.


The area fraction of the retained austenite can be determined by the X-ray measurement, for example. In this method, for example, a portion of the steel sheet from the surface to a ¼ thickness of the steel sheet is removed by mechanical polishing and chemical polishing, and as characteristic X-rays, MoKa rays are used. Then, from an integrated intensity ratio 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.





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


(S γ 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 as-quenched martensite can be determined by a field emission-scanning electron microscope (FE-SEM) observation and the X-ray measurement, for example. In this method, for example, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface of the steel sheet is set as an object to be observed and a LePera reagent is used for corrosion. Since the structure that is not corroded by the LePera reagent is as-quenched martensite and retained austenite, it is possible to determine the area fraction of the as-quenched 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 reagent. The area fraction of the as-quenched martensite can also be determined by using the 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 as-quenched martensite. The area fraction of the tempered martensite can be determined by the FE-SEM observation, for example. In this method, for example, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface of the steel sheet is set as an object to be observed and a nital reagent is used for corrosion. Then, as described below, the tempered martensite is identified based on the position of cementite and variants. The tempered martensite contains cementite inside a martensite lath. The cementite contained in the tempered martensite has a plurality of variants because there are two or more types of crystal orientation relationship between the martensite lath and the cementite. The tempered martensite can be identified based on the position of cementite and the variants as above to determine its area fraction.


The bainite can be determined by the FE-SEM observation, for example. In this method, for example, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface of the steel sheet is set as an object to be observed and a nital reagent is used for corrosion. Then, as described below, the bainite is identified based on the position of cementite and variants. The bainite includes upper bainite and lower bainite. The upper bainite contains cementite or retained austenite at an interface of lath-shaped bainitic ferrite. The lower bainite contains cementite inside the lath-shaped bainitic ferrite. The cementite contained in the lower bainite has the same variant because there is one type of crystal orientation relationship between the bainitic ferrite and the cementite. The bainite can be identified based on the position of cementite and the variant as above to determine its area fraction.


The pearlite can be identified by an optical microscope observation, for example, to determine its area fraction. In this method, for example, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface of the steel sheet is set as an object to be observed and a nital reagent is used for corrosion. The region exhibiting a dark contrast by the optical microscope observation is the pearlite.


It is difficult to distinguish the granular bainite from ferrite not only by the conventional corrosion method but also by the secondary electron image observation using a scanning electron microscope. As a result of an earnest examination, the present inventors found out that the granular bainite has a tiny crystal misorientation in a grain. Thus, detecting a tiny crystal misorientation in a grain makes it possible to distinguish the granular bainite from ferrite. Here, there will be explained a concrete method of determining the area fraction of the granular bainite. In this method, a region having a ⅛ to ⅜ thickness of the steel sheet as the depth from the surface of the steel sheet is set as an object to be measured, by the EBSD method, a crystal orientation of a plurality of places (pixels) in this region is measured at 0.2-μm intervals, and a value of a GAM (grain average misorientation) is calculated from this result. In the event of this calculation, it is set that in the case where the crystal misorientation between adjacent pixels is 5° or more, a grain boundary exists between them, and the crystal misorientation between adjacent pixels is calculated in a region surrounded by this grain boundary to find an average value of the crystal misorientations. This average value is the value of GAM. In this manner, it is possible to detect the tiny crystal misorientation of the bainitic ferrite. The region with the value of GAM being 0.5° or more belongs to one of the granular bainite, the bainite, the tempered martensite, the pearlite, and the martensite. Thus, the value obtained by subtracting the total of the area fractions of the bainite, the tempered martensite, the pearlite, and the martensite from the area fraction of the region with the value of GAM being 0.5° or more is the area fraction of the granular bainite.


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, cold rolling, annealing, and so on of the slab. Thus, the chemical composition of the steel sheet and the slab is one in which not only properties of the steel sheet but also these treatments are considered. 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 includes a chemical composition represented by, in mass %, C: 0.09% to 0.15%, Si: 0.2% to 2.5%, Al: 0.01% to 1.00%, Mn: 1.0% to 3.0%, P: 0.02% or less, S: 0.01% or less, N: 0.007% or less, 0: 0.006% or less, Cr: 0.00% to 1.00%, Mo: 0.00% to 1.00%, B: 0.0000% to 0.010%, Nb: 0.000% to 0.30%, Ti: 0.000% to 0.30%, Ni: 0.00% to 1.00%, Cu: 0.00% to 1.00%, V: 0.000% to 0.50%, Mg: 0.0000% to 0.04%, REM: 0.0000% to 0.04%, and the balance: Fe and impurities. Examples of the impurities include ones contained in raw materials such as ore and scrap and ones contained in manufacturing steps.


(C: 0.09% to 0.15%)


C contributes to an improvement in tensile strength. When the C content is less than 0.09%, it is difficult to obtain a tensile strength of 1180 MPa or more. Thus, the C content is set to 0.09% or more and preferably set to 0.10% or more. On the other hand, when the C content is greater than 0.15%, formation of ferrite is suppressed, thus failing to obtain sufficient elongation. Thus, the C content is set to 0.15% or less and preferably set to 0.13% or less.


(Si: 0.2% to 2.5%)


Si suppresses formation of cementite to contribute to formation of granular bainite. The granular bainite is a structure in which a plurality of pieces of bainitic ferrite are turned into a single lump after dislocations existing on their interfaces are recovered. Therefore, when cementite exists on the interface of the bainitic ferrite, no granular bainite is formed there. When the Si content is less than 0.2%, cementite is formed excessively, failing to sufficiently obtain granular bainite. Thus, the Si content is set to 0.2% or more. On the other hand, when the Si content is greater than 2.5%, slab cracking is likely to occur during hot rolling. Thus, the Si content is set to 2.5% or less.


(Al: 0.01% to 1.00%)


Al suppresses formation of cementite to contribute to formation of granular bainite. The granular bainite is a structure in which a plurality of pieces of bainitic ferrite are turned into a single lump after dislocations existing on their interfaces are recovered. Therefore, when cementite exists on the interface of the bainitic ferrite, no granular bainite is formed there. Al is an element that can be utilized also as a deoxidizer. When the Al content is less than 0.01%, cementite is formed excessively, failing to sufficiently obtain granular bainite. Thus, the Al content is set to 0.01% or more. On the other hand, when the Al content is greater than 1.00%, slab cracking is likely to occur during hot rolling. Further, the number density of Al-based coarse inclusions increases, thus causing deterioration in hole expandability. Thus, the Al content is set to 1.00% or less.


(Mn: 1.0% to 3.0%)


Mn suppresses ferrite transformation in continuous annealing after cold rolling or in a heat treatment in a plating line to contribute to an improvement in strength. When the Mn content is less than 1.0% in total, the area fraction of the ferrite becomes excessive, resulting in difficulty in obtaining a tensile strength of 1180 MPa or more. Thus, the Mn content is set to 1.0% or more. On the other hand, when the Mn content is greater than 3.0%, the area fraction of the ferrite becomes too small, failing to obtain sufficient elongation. Thus, the Mn content is set to 3.0% or less in total.


(P: 0.02% or less)


P is not an essential element and is contained in, for example, steel as an impurity. P reduces hole expandability, reduces toughness by being segregated to the middle of the steel sheet in the sheet thickness direction, or makes a welded portion brittle. Thus, a lower P content is better. When the P content is greater than 0.04%, in particular, the reduction in hole expandability is prominent. Thus, the P content is set to 0.04% or less, and preferably set to 0.01% or less. Reducing the P content is expensive, and when the P content is tried to be reduced down to less than 0.0001%, its cost increases significantly.


(S: 0.01% or less)


S is not an essential element, and is contained in steel as an impurity, for example. S reduces weldability, reduces manufacturability at a casting time and a hot rolling time, and reduces hole expandability by forming coarse MnS. Thus, a lower S content is better. When the S content is greater than 0.01%, 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 0.01% or less and preferably set to 0.005% or less. Reducing the S content is expensive, and when the S content is tried to be reduced down to less than 0.0001%, its cost increases significantly.


(N: 0.01% or less)


N is not an essential element, and is contained in steel as an impurity, for example. N forms coarse nitrides. The coarse nitrides cause reductions in bendability and hole expandability and further make blowholes occur at the time of welding. Thus, a lower N content is better. When the N content is greater than 0.01%, in particular, the reduction in hole expandability and the occurrence of blowholes are prominent. Thus, the N content is set to 0.01% or less and preferably set to 0.008% or less. Reducing the N content is expensive, and when the N content is tried to be reduced down to less than 0.0005%, its cost increases significantly.


(0: 0.006% or less) 0 is not an essential element, and is contained in steel as an impurity, for example. 0 forms coarse oxide. The coarse oxide causes reductions in bendability and hole expandability and further makes blowholes occur at the time of welding. Thus, a lower 0 content is better. When the 0 content is greater than 0.006%, in particular, the reduction in hole expandability and the occurrence of blowholes are prominent. Thus, the 0 content is set to 0.006% or less and preferably set to 0.005% or less. Reducing the 0 content is expensive, and when the 0 content is tried to be reduced down to less than 0.0005%, its cost increases significantly.


Cr, Mo, Ni, Cu, Nb, Ti, V, B, Ca, Mg, and REM 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 steel.


(Cr: 0.00% to 1.00%, Mo: 0.00% to 1.00%, Ni: 0.00% to 1.00%, Cu: 0.00% to 1.00%)


Cr, Mo, Ni, and Cu suppress ferrite transformation in the event of annealing after cold rolling or in the event of plating and contribute to an improvement in strength. Thus, Cr, Mo, Ni, or Cu, or an arbitrary combination of these may be contained. In order to obtain this effect sufficiently, preferably, the Cr content is set to 0.10% or more, the Mo content is set to 0.01% or more, the Ni content is set to 0.05% or more, and the Cu content is set to 0.05% or more. However, when the Cr content is greater than 1.00, the Mo content is greater than 1.00%, the Ni content is greater than 1.00%, or the Cu content is greater than 1.00%, the area fraction of the ferrite becomes too small, failing to obtain sufficient elongation. Therefore, the Cr content, the Mo content, the Ni content, and the Cu content are each set to 1.00% or less. That is, preferably, Cr: 0.10% to 1.00%, Mo: 0.01% to 1.00%, Ni: 0.05% to 1.00%, or Cu: 0.05% to 1.00% is satisfied, or an arbitrary combination of these is satisfied.


(Nb: 0.000% to 0.30%, Ti: 0.000% to 0.30%, V: 0.000% to 0.50%)


Nb, Ti, and V increase the area of grain boundaries of austenite by grain refining of austenite during annealing after cold rolling or the like to promote ferrite transformation. Thus, Ni, Ti or V, or an arbitrary combination of these may be contained. In order to obtain this effect sufficiently, preferably, the Nb content is set to 0.005% or more, the Ti content is set to 0.005% or more, and the V content is set to 0.005% or more. However, when the Nb content is greater than 0.30%, the Ti content is greater than 0.30%, or the V content is greater than 0.50%, the area fraction of the ferrite becomes excessive, failing to obtain a sufficient tensile strength. Therefore, the Nb content is set to 0.30% or less, the Ti content is set to 0.30% or less, and the V content is set to 0.50% or less. That is, preferably, Nb: 0.005% to 0.30%, Ti: 0.005% to 0.30%, or V: 0.005% to 0.50% is satisfied, or an arbitrary combination of these is satisfied.


(B: 0.0000% to 0.010%)


B segregates to grain boundaries of austenite during annealing after cold rolling or the like to suppress ferrite transformation. Thus, B may be contained. In order to obtain this effect sufficiently, the B content is preferably set to 0.0001% or more. However, when the B content is greater than 0.010%, the area fraction of the ferrite becomes too small, failing to obtain sufficient elongation. Therefore, the B content is set to 0.010% or less. That is, B: 0.0001% to 0.010% is preferably established.


(Ca: 0.0000% to 0.04%, Mg: 0.0000% to 0.04%, REM: 0.0000% to 0.04%)


Ca, Mg, and REM control forms of oxide and sulfide to contribute to an improvement in hole expandability. Thus, Ca, Mg, or REM or an arbitrary combination of these may be contained. In order to obtain this effect sufficiently, preferably, the Ca content, the Mg content, and the REM content are each set to 0.0005% or more. However, when the Ca content is greater than 0.04%, the Mg content is greater than 0.04%, or the REM content is greater than 0.04%, coarse oxide is formed, failing to obtain sufficient hole expandability. Therefore, the Ca content, the Mg content, and the REM content are each set to 0.04% or less and preferably set to 0.01% or less. That is, preferably, Ca: 0.0005% to 0.04%, Mg: 0.0005% to 0.04%, or REM: 0.0005% to 0.04% is satisfied, or an arbitrary combination of these is satisfied.


REM is a generic term for 17 types of elements in total of Sc, Y, and elements belonging to the lanthanoid series, and the REM content means the total content of these elements. REM is contained in misch metal, for example, and when adding REM, for example, misch metal is added, or metal REM such as metal La or metal Ce is added in some cases.


According to this embodiment, it is possible to obtain a tensile strength of 1180 MPa or more, elongation of 10% or more, hole expandability of 20% or more, and bendability, which is a VDA bending angle in the case where a thickness is set to t (mm) being “7.69t2-38.4t+109” or more. That is, it is possible to obtain a high strength, and excellent elongation, hole expandability, and bendability. This steel sheet is easily formed into framework system parts of automobiles, for example, and can also ensure collision safety.


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


The manufacturing method prior to casting is not limited in particular. That is, following smelting by a shaft furnace, an electric furnace, or the like, various types of secondary refining may be performed. Incidentally, as a raw material, scrap may be used.


A cast slab may be subjected to hot rolling after being cooled down to a low temperature once and then being heated again, or a cast slab may be subjected to hot rolling continuously.


The hot rolling is started at a temperature of 1100° C. or more and is completed at a temperature of the Ar3 point or more. In the cold rolling, a reduction ratio is set to 30% or more and 80% or less. In the annealing, retention is performed for 10 seconds or more to the maximum heating temperature of the Ac1 point or more and the Ac3 point or less, in cooling thereafter, a cooling rate from the Ar3 point to 650° C. is set to 0.5° C./second or more and 50° C./second or less, and a cooling rate from 650° C. to 450° C. is set to 0.5° C./second or more and 5° C./second or less.


When the starting temperature of the hot rolling is less than 1100° C., it is impossible to sufficiently solid-dissolve elements other than Fe in Fe and coarse alloy carbide remains to easily cause embrittlement during hot rolling. Thus, the hot rolling is started at a temperature of 1100° C. or more. The starting temperature of the hot rolling is a slab heating temperature, for example. 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 the temperature of 1100° 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 1100° C. and then is heated.


When the completing temperature of the hot rolling is less than the Ar3 point, austenite and ferrite are contained in a metal structure of a hot-rolled steel sheet, resulting in that the shape of the hot-rolled steel sheet becomes worse to be difficult to perform treatments after the hot rolling such as cold rolling in some cases because the austenite and the ferrite are different in mechanical properties. Thus, the hot rolling is finished at a temperature of the Ar3 point or more. When the hot rolling is finished at a temperature of the Ar3 point or more, it is possible to relatively reduce a rolling load during the hot rolling.


The hot rolling includes rough rolling and finish rolling, and in the finish rolling, one in which a plurality of steel sheets obtained by rough rolling are joined may be rolled continuously. The finish rolling may be performed after a rough-rolled sheet is coiled once. A coiling temperature is set to 500° C. or more and 650° C. or less. When the coiling temperature is greater than 650° C., productivity deteriorates. Thus, the coiling temperature is set to 650° C. or less. On the other hand, when the coiling temperature is less than 500° C., the hardness of the hot-rolled steel sheet rises too high to be difficult to perform cold rolling thereafter. Thus, the coiling temperature is set to 500° C. or more.


The pickling is performed on the hot-rolled steel sheet obtained in this manner in order to remove oxides on the surface. The pickling is performed one time or two or more times. By the pickling, the oxides on the surface of the hot-rolled steel sheet are removed and chemical conversion treatability and platability improve.


When the reduction ratio of the cold rolling is less than 30%, 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 of the cold rolling is set to 30% or more. On the other hand, when the reduction ratio of the cold rolling is greater than 80%, a rolling load becomes large excessively to be difficult to perform the cold rolling. Thus, the reduction ratio of the cold rolling is set to 80% or less.


A heating rate in the case where the cold-rolled steel sheet is passed through in a continuous annealing line or a plating line is not restricted in particular.


In the annealing, the steel sheet is retained to the maximum heating temperature of the Ac1 point or more and the Ac3 point or less for 10 seconds or more, and thereby austenite is formed. The austenite is transformed into ferrite, granular bainite, bainite, or martensite through cooling to be performed later. When the maximum heating temperature is less than the Ac1 point or the retention time is less than 10 seconds, the austenite is not formed sufficiently. On the other hand, when the maximum heating temperature is greater than the Ac3 point, ferrite cannot be obtained and ductility goes short. Thus, the maximum heating temperature is set to the Ac1 point or more and the Ac3 point or less and the retention time is set to 10 seconds or more.


In the cooling from the maximum heating temperature, an average cooling rate from the Ar3 point to 650° C. (first average cooling rate) is set to 0.5° C./second to 50° C./second. When the average cooling rate is less than 0.5° C./second, in the cooling process, ferrite or pearlite is formed excessively from austenite. As a result, it becomes difficult to secure a sufficient area fraction of martensite, resulting in difficulty in obtaining a tensile strength of 1180 MPa or more. No problem is caused in terms of the material even when the average cooling rate is increased, but when the average cooling rate is increased excessively, an increase in manufacturing cost is caused, and thus the average cooling rate is set to 50° C./second or less. A cooling method may be roll cooling, air cooling, or water cooling, or a combination of these.


An average cooling rate from 650° C. to 450° C. (second average cooling rate) is set to 0.5° C./second to 5° C./second, thereby making it possible to form an appropriate area fraction of granular bainite. As described above, the granular bainite is a structure in which a plurality of pieces of bainitic ferrite are turned into a single lump after dislocations existing on their interfaces are recovered. It is possible to generate such a dislocation recovery in a temperature zone of 650° C. or less. However, when the cooling rate in this temperature zone is greater than 5° C./second, it is impossible to sufficiently recover the dislocations, resulting in that the area fraction of the granular bainite sometimes becomes short. Thus, the cooling rate in this temperature zone is set to 5° C./second or less. On the other hand, when the cooling rate in this temperature zone is less than 0.5° C./second, the area fractions of the granular bainite and the bainite increase excessively to be difficult to obtain martensite necessary for a tensile strength of 1180 MPa or more. Thus, the cooling rate in this temperature zone is set to 0.5° C./second or more. A cooling method may be continuous cooling, inclined cooling, or isothermal holding, or a combination of these.


In this manner, it is possible to manufacture the steel sheet according to the embodiment of the present invention.


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 includes 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 this temperature is less than 460° C., alloying sometimes becomes short. When this 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 2 were manufactured, these slabs were hot rolled, and hot-rolled steel sheets were obtained. Each space in Table 1 to Table 2 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 2 indicates that a corresponding numerical value is out of the range of the present invention.










TABLE 1







SYMBOL OF
CHEMICAL COMPOSITION (MASS %)



















STEEL
C
Si
Mn
P
S
Al
N
O
Cr
Mo
Ni
Cu





A
0.13
1.30
2.4
0.018
0.001
0.032
0.0061
0.0022

0.042


B
0.10
2.30
2.9
0.002
0.009
0.025
0.0034
0.0017


C
0.12
0.45
2.3
0.001
0.003
0.230
0.0031
0.0023

0.021


D
0.11
0.23
2.6
0.018
0.001
0.650
0.0046
0.0032

0.041


E
0.13
0.53
1.6
0.012
0.009
0.026
0.0037
0.0013
0.4
0.029


F
0.13
0.67
1.2
0.007
0.006
0.041
0.0029
0.0043
2.9
0.024


G
0.10
0.52
2.5
0.003
0.005
0.051
0.0042
0.0040


H
0.09
0.55
2.8
0.014
0.008
0.030
0.0056
0.0017

0.120


I
0.11
0.39
2.7
0.005
0.003
0.019
0.0052
0.0035

0.065
0.02


J
0.12
0.59
2.2
0.005
0.001
0.026
0.0064
0.0025

0.042
0.09


K
0.11
0.48
2.4
0.002
0.008
0.043
0.0008
0.0046

0.023

0.03


L
0.14
0.78
2.6
0.010
0.004
0.019
0.0001
0.0039

0.068

0.08


M
0.13
0.44
2.1
0.005
0.003
0.033
0.0014
0.0026

0.073


N
0.13
0.45
2.3
0.012
0.005
0.031
0.0030
0.0038

0.046


O
0.12
0.57
2.4
0.013
0.004
0.046
0.0007
0.0048

0.026


P
0.14
0.52
2.6
0.012
0.004
0.042
0.0033
0.0040

0.069


Q
0.12
0.58
2.7
0.011
0.007
0.074
0.0022
0.0012

0.044


R
0.12
0.62
2.3
0.014
0.005
0.070
0.0043
0.0023

0.046


S
0.12
0.55
2.6
0.010
0.008
0.041
0.0031
0.0029

0.058


T
0.12
0.72
2.8
0.018
0.002
0.074
0.0053
0.0047


U
0.11
0.63
2.1
0.008
0.009
0.046
0.0014
0.0038

0.067


V
0.12
0.52
2.6
0.006
0.003
0.049
0.0021
0.0029

0.015


W
0.11
0.50
2.8
0.001
0.004
0.019
0.0049
0.0056


X
0.12
0.52
2.6
0.001
0.001
0.021
0.0041
0.0021

0.050


Y
0.11
0.51
2.8
0.001
0.001
0.071
0.0032
0.0023


Z
0.13
0.61
2.5
0.001
0.001
0.045
0.0026
0.0034


















Ar2





SYMBOL OF
CHEMICAL COMPOSITION (MASS %)
POINT
Ac1
Ac3



















STEEL
Nb
Ti
V
B
Ca
Mg
REM
(° C.)
(° C.)
(° C.)







A
0.007
0.020

0.0028



722
735
871



B

0.008





724
759
905



C
0.014


0.0018



713
711
837



D
0.022
0.023

0.0034



701
702
821



E
0.020
0.015

0.0016



760
721
860



F



0.0011



797
730
878



G
0.012
0.011

0.0043



698
711
837



H
0.010
0.008





668
709
836



I
0.007


0.0029



674
705
825



J

0.025

0.0011



717
717
845



K
0.015
0.025

0.0021



701
711
837



L
0.021
0.009

0.0042



685
718
840



M

0.013

0.0021



718
713
842



N
0.160
0.018

0.0043



702
711
836



O
0.024


0.0013



701
714
839



P
0.016
0.130

0.0020



677
710
828



Q
0.010
0.008
0.1
0.0029



679
711
831



R
0.021
0.025
0.4
0.0033



712
716
845



S
0.013
0.016





685
711
834



T

0.009

0.0065



676
714
833



U
0.020
0.017

0.0036
0.02


731
719
854



V
0.012
0.018

0.0010

0.01

684
710
831



W
0.016
0.011

0.0024


0.01
669
708
826



X
0.030
0.030

0.0030



683
710
832



Y







721
720
865



Z







718
725
864


















TABLE 2







SYMBOL OF
CHEMICAL COMPOSITION (MASS %)



















STEEL
C
Si
Mn
P
S
Al
N
O
Cr
Mo
Ni
Cu





a

0.06

0.50
2.7
0.015
0.002
0.073
0.0024
0.0018

0.041


b

0.18

0.60
2.1
0.014
0.008
0.020
0.0010
0.0050

0.026


c
0.10

0.10

2.3
0.007
0.003
0.086
0.0014
0.0046

0.049


d
0.12

2.90

1.7
0.017
0.001
0.091
0.0065
0.0049

0.048


e
0.11
0.43

0.4

0.002
0.001
0.059
0.0037
0.0038

0.055


f
0.10
0.45

3.4

0.005
0.006
0.059
0.0051
0.0026

0.010


g
0.10
0.54
2.3

0.030

0.004
0.034
0.0034
0.0041

0.012


h
0.13
0.48
2.4
0.009

0.015

0.078
0.0063
0.0049

0.062


i
0.11
0.55
2.1
0.006
0.008

0.000

0.0039
0.0046

0.017


j
0.12
0.65
2.5
0.001
0.001
1.020
0.0020
0.0024

0.029


k
0.14
0.54
2.3
0.008
0.006
0.022

0.0090

0.0037

0.030


l
0.11
0.57
2.3
0.017
0.008
0.083
0.0055

0.0080


0.032


m
0.14
0.52
2.4
0.018
0.008
0.077
0.0054
0.0019

3.2

0.022


n
0.13
0.54
2.5
0.017
0.003
0.025
0.0032
0.0022


1.200



o
0.11
0.48
2.4
0.016
0.009
0.037
0.0003
0.0022

0.020

1.10



p
0.11
0.39
2.3
0.002
0.006
0.072
0.0024
0.0043

0.034


1.2



q
0.12
0.62
2.2
0.009
0.004
0.030
0.0056
0.0015

0.043


r
0.10
0.59
2.5
0.007
0.001
0.077
0.0060
0.0040

0.034


s
0.12
0.72
1.9
0.004
0.006
0.015
0.0018
0.0013

0.031


t
0.11
0.58
2.1
0.002
0.004
0.097
0.0062
0.0019

0.022


u
0.13
0.66
2.3
0.013
0.003
0.044
0.0038
0.0024

0.055


v
0.10
0.49
2.0
0.009
0.008
0.020
0.0002
0.0041

0.057


w
0.10
0.61
2.1
0.002
0.005
0.034
0.0028
0.0033

0.051


















Ar2





SYMBOL OF
CHEMICAL COMPOSITION (MASS %)
POINT
Ac1
Ac3



















STEEL
Nb
Ti
V
B
Ca
Mg
REM
(° C.)
(° C.)
(° C.)







a
0.019
0.008

0.0022



695
709
840



b
0.023
0.026

0.0038



707
718
838



c
0.009
0.008

0.0021



702
701
826



d
0.016
0.009

0.0017



836
789
965



e
0.015
0.021

0.0029



860
731
896



f
0.019
0.023

0.0028



624
700
808



g
0.010
0.020

0.0011



714
714
845



h
0.016
0.024

0.0029



697
711
835



i
0.006
0.020

0.0029



726
717
849



j
0.010
0.026

0.0039



735
715
840



k
0.017
0.018

0.0032



701
714
837



l
0.007
0.022

0.0017



714
715
845



m
0.014
0.009

0.0035



695
712
833



n
0.020
0.023

0.0025



689
712
870



o
0.021
0.008

0.0033



701
711
821



p
0.017
0.021

0.0013



708
710
837



q

0.350

0.017

0.0035



718
718
848



r
0.027

0.320


0.0040



702
713
842



s
0.016
0.026

0.6

0.0032



745
724
861



t
0.026
0.017


0.0120




731
717
851



u
0.024
0.013

0.0011

0.05



709
718
845



v
0.017
0.015

0.0039


0.06


736
716
853



w
0.012
0.018

0.0012



0.05

732
718
855










Next, of the hot-rolled steel sheets, pickling, cold rolling, and annealing were performed, and steel sheets were obtained. Conditions of the hot rolling, the cold rolling, and the annealing are illustrated in Table 3 to Table 7. Each underline in Table 3 to Table 7 indicates that a corresponding numerical value is out of a range suitable for the manufacture of the steel sheet according to the present invention.













TABLE 3









HOT ROLLING

ANNEALING























FINISH

COLD
MAXIMUM








SLAB
ROLLING
COILING
ROLLING
HEATING



SYMBOL
Ar2


HEATING
FINISHING
TEMPER-
REDUCTION
TEMPER-
RETENTION


SAMPLE
OF
POINT
Ac1
Ac3
TEMPERATURE
TEMPERATURE
ATURE
RATIO
ATURE
TIME


NO.
STEEL
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(%)
(° C.)
(SECOND)





1
A
722
735
871
1120
818
618
40
820
134


2
A
722
735
871
1260
834
502
54
824
206


3
A
722
735
871
1169
807
561
60
814
164


4
A
722
735
871
1143
807
643
58
825
206


5
B
724
759
907
1156
744
444
44
856
203


6
B
724
759
907
1199
824
530
56
846
156


7
B
724
759
907
1109
857
564
61
855
18


8
B
724
759
907
1125
869
592
61
856
172


9
C
713
711
837
1170
843
460
52
793
214


10
C
713
711
837
1255
769
630
50
799
80


11
C
713
711
837
1138
823
632
51
787
204


12
C
713
711
837
1109
778
618
54
780
167


13
D
701
702
821
1194
781
592
35
770
187


14
D
701
702
821
1194
781
592
68
772
179


15
D
701
702
821
1194
781
592
57
767
78


16
D
701
702
821
1194
781
592
53
780
118


17
E
760
721
860
1115
886
426
68
794
158


18
E
760
721
860
1115
886
426
49
818
159


19
E
760
721
860
1115
886
426
52
804
97


20
E
760
721
860
1115
886
426
50
817
58


21
F
797
730
878
1123
925
426
68
805
158


22
F
797
730
878
1123
925
426
57
830
201


23
F
797
730
878
1123
925
426
52
830
138


24
F
797
730
878
1123
925
426
62
820
29













ANNEALING

















FIRST
SECOND








AVERAGE
AVERAGE
PRESENCE OR
PRESENCE OR




COOLING
COOLING
ABSENCE OF
ABSENCE OF
PRESENCE OR



SAMPLE
RATE
RATE
PLATING
ALLOYING
ABSENCE OF



NO.
(° C./SECOND)
(° C./SECOND)
TREATMENT
TREATMENT
TEMPERING
NOTE







 1
11
1
ABSENT
ABSENT
ABSENT
EXAMPLE



 2
26
4
ABSENT
ABSENT
ABSENT
EXAMPLE



 3
33
3
ABSENT
ABSENT
ABSENT
EXAMPLE



 4
33
4
ABSENT
ABSENT
ABSENT
EXAMPLE



 5
24
2
ABSENT
ABSENT
ABSENT
EXAMPLE



 6
21
3
ABSENT
ABSENT
ABSENT
EXAMPLE



 7
8
2
ABSENT
ABSENT
ABSENT
EXAMPLE



 8
41
3
ABSENT
ABSENT
ABSENT
EXAMPLE



 9
31
4
ABSENT
ABSENT
ABSENT
EXAMPLE



10
20
3
ABSENT
ABSENT
ABSENT
EXAMPLE



11
19
4
ABSENT
ABSENT
ABSENT
EXAMPLE



12
2
2
ABSENT
ABSENT
ABSENT
EXAMPLE



13
21
2
ABSENT
ABSENT
ABSENT
EXAMPLE



14
32
4
ABSENT
ABSENT
ABSENT
EXAMPLE



15
26
4
ABSENT
ABSENT
ABSENT
EXAMPLE



16
14
4
ABSENT
ABSENT
ABSENT
EXAMPLE



17
31
4
ABSENT
ABSENT
ABSENT
EXAMPLE



18
34
2
ABSENT
ABSENT
ABSENT
EXAMPLE



19
12
3
ABSENT
ABSENT
ABSENT
EXAMPLE



20
44
4
ABSENT
ABSENT
ABSENT
EXAMPLE



21
31
4
ABSENT
ABSENT
ABSENT
EXAMPLE



22
11
4
ABSENT
ABSENT
ABSENT
EXAMPLE



23
28
1
ABSENT
ABSENT
ABSENT
EXAMPLE



24
26
4
ABSENT
ABSENT
ABSENT
EXAMPLE




















TABLE 4









HOT ROLLING























FINISH

COLD
ANNEALING







SLAB
ROLLING

ROLLING
MAXIMUM



SYMBOL
Ar2


HEATING
FINISHING
COILING
REDUCTION
HEATING


SAMPLE
OF
POINT
Ac1
Ac3
TEMPERATURE
TEMPERATURE
TEMPERATURE
RATIO
TEMPERATURE


NO.
STEEL
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(%)
(° C.)





25
G
698
711
837
1251
783
587
58
792


26
G
698
711
837
1251
783
587
46
791


27
G
698
711
837
1251
783
587
54
795


28
G
698
711
837
1251
783
587
55
796


29
G
698
711
837
1251
783
587
61
795


30
H
668
709
836
1215
728
498
60
794


31
H
668
709
836
1215
728
498
66
795


32
H
668
709
836
1215
728
498
43
794


33
H
668
709
836
1215
728
498
61
796


34
H
668
709
836
1215
728
498
53
795


35
H
668
709
836
1215
728
498
50
795


36
I
674
705
825
1184
764
423
67
786


37
I
674
705
825
1184
764
423
65
789


38
I
674
705
825
1184
764
423
53
788


39
I
674
705
825
1184
764
423
45
787


40
I
674
705
825
1184
764
423
65
786


41
I
674
705
825
1184
764
423
53
786


42
J
717
717
845
1167
860
423
67
802


43
J
717
717
845
1167
860
423
65
804


44
J
717
717
845
1167
860
423
53
800


45
J
717
717
845
1167
860
423
45
804


46
J
717
717
845
1167
860
423
57
803


47
J
717
717
845
1167
860
423
52
804













ANNEALING



















FIRST
SECOND









AVERAGE
AVERAGE
PRESENCE OR
PRESENCE OR
PRESENCE




RETENTION
COOLING
COOLING
ABSENCE OF
ABSENCE OF
OR



SAMPLE
TIME
RATE
RATE
PLATING
ALLOYING
ABSENCE OF



NO.
(SECOND)
(° C./SECOND)
(° C./SECOND)
TREATMENT
TREATMENT
TEMPERING
NOTE







25
15
26
4
ABSENT
ABSENT
ABSENT
EXAMPLE



26
300
34
2
ABSENT
ABSENT
ABSENT
EXAMPLE



27
117
23
4
ABSENT
ABSENT
ABSENT
EXAMPLE



28
65
39
3
ABSENT
ABSENT
ABSENT
EXAMPLE



29
61
36
3
ABSENT
ABSENT
ABSENT
EXAMPLE



30
121
1
3
ABSENT
ABSENT
ABSENT
EXAMPLE



31
197
15
2
ABSENT
ABSENT
ABSENT
EXAMPLE



32
136
48
4
ABSENT
ABSENT
ABSENT
EXAMPLE



33
172
24
5
ABSENT
ABSENT
ABSENT
EXAMPLE



34
42
6
4
ABSENT
ABSENT
ABSENT
EXAMPLE



35
162
5
2
ABSENT
ABSENT
ABSENT
EXAMPLE



36
119
33
1
ABSENT
ABSENT
ABSENT
EXAMPLE



37
61
18
2
ABSENT
ABSENT
ABSENT
EXAMPLE



38
151
24
3
ABSENT
ABSENT
ABSENT
EXAMPLE



39
121
11
5
ABSENT
ABSENT
ABSENT
EXAMPLE



40
166
32
1
ABSENT
ABSENT
ABSENT
EXAMPLE



41
63
23
1
ABSENT
ABSENT
ABSENT
EXAMPLE



42
119
33
1
ABSENT
ABSENT
ABSENT
EXAMPLE



43
61
18
2
ABSENT
ABSENT
ABSENT
EXAMPLE



44
151
24
3
ABSENT
ABSENT
ABSENT
EXAMPLE



45
121
11
5
ABSENT
ABSENT
ABSENT
EXAMPLE



46
80
24
1
ABSENT
ABSENT
ABSENT
EXAMPLE



47
30
4
3
ABSENT
ABSENT
ABSENT
EXAMPLE




















TABLE 5









HOT ROLLING























FINISH

COLD
ANNEALING







SLAB
ROLLING

ROLLING
MAXIMUM



SYMBOL
Ar2


HEATING
FINISHING
COILING
REDUCTION
HEATING


SAMPLE
OF
POINT
Ac1
Ac3
TEMPERATURE
TEMPERATURE
TEMPERATURE
RATIO
TEMPERATURE


NO.
STEEL
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(%)
(° C.)





48
K
701
711
837
1146
789
484
45
798


49
K
701
711
837
1150
768
473
50
795


50
K
701
711
837
1106
851
577
50
797


51
K
701
711
837
1249
780
606
65
794


52
K
701
711
837
1122
818
590
64
796


53
L
685
718
840
1188
795
617
64
800


54
M
718
713
842
1151
807
646
51
794


55
N
702
711
836
1166
778
562
65
786


56
O
701
714
839
1140
755
604
62
801


57
P
677
710
828
1153
735
580
63
789


58
Q
679
711
831
1147
799
624
57
784


59
R
712
716
845
1101
796
605
63
801


60
S
685
711
834
1182
789
580
56
794


61
T
676
714
835
1181
751
646
52
794


62
U
731
719
854
1190
810
643
65
809


63
V
684
710
831
1103
744
619
58
791


64
W
669
708
826
1135
778
635
61
786


65
X
683
710
832
1130
760
592
57
786


66
X
683
710
832
1130
760
592
60
790


67
Y
721
720
865
1230
800
560
54
820


68
Z
718
725
864
1200
810
570
58
810













ANNEALING



















FIRST
SECOND









AVERAGE
AVERAGE
PRESENCE OR
PRESENCE OR



SAMPLE
RETENTION
COOLING
COOLING
ABSENCE OF
ABSENCE OF
PRESENCE OR



TIME
RATE
RATE
PLATING
ALLOYING
ABSENCE OF



NO.
(SECOND)
(° C./SECOND)
(° C./SECOND)
TREATMENT
TREATMENT
TEMPERING
NOTE







48
153
26
3
ABSENT
ABSENT
ABSENT
EXAMPLE



49
112
16
4
PRESENT
ABSENT
ABSENT
EXAMPLE



50
221
18
3
PRESENT
PRESENT
ABSENT
EXAMPLE



51
185
30
4
ABSENT
ABSENT
PRESENT
EXAMPLE









(POST-PROCESS)



52
26
22
5
ABSENT
ABSENT
ABSENT
EXAMPLE



53
12
15
2
ABSENT
ABSENT
ABSENT
EXAMPLE



54
165
28
1
ABSENT
ABSENT
ABSENT
EXAMPLE



55
194
14
4
ABSENT
ABSENT
ABSENT
EXAMPLE



56
26
5
3
ABSENT
ABSENT
ABSENT
EXAMPLE



57
40
11
3
ABSENT
ABSENT
ABSENT
EXAMPLE



58
101
25
4
ABSENT
ABSENT
ABSENT
EXAMPLE



59
92
3
5
ABSENT
ABSENT
ABSENT
EXAMPLE



60
86
10
3
ABSENT
ABSENT
ABSENT
EXAMPLE



61
81
11
4
ABSENT
ABSENT
ABSENT
EXAMPLE



62
112
6
1
ABSENT
ABSENT
ABSENT
EXAMPLE



63
49
21
2
ABSENT
ABSENT
ABSENT
EXAMPLE



64
180
43
2
ABSENT
ABSENT
ABSENT
EXAMPLE



65
121
4
3
ABSENT
ABSENT
ABSENT
EXAMPLE



66
75
32
5
ABSENT
ABSENT
ABSENT
EXAMPLE



67
140
21
2
PRESENT
PRESENT
ABSENT
EXAMPLE



68
95
35
3
ABSENT
ABSENT
ABSENT
EXAMPLE




















TABLE 6









HOT ROLLING























FINISH

COLD
ANNEALING







SLAB
ROLLING

ROLLING
MAXIMUM



SYMBOL
Ar3


HEATING
FINISHING
COILING
REDUCTION
HEATING


SAMPLE
OF
POINT
Ac1
Ac3
TEMPERATURE
TEMPERATURE
TEMPERATURE
RATIO
TEMPERATURE


NO.
STEEL
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(%)
(° C.)





71
a
695
709
840
1151
814
565
54
799


72
b
707
718
838
1157
796
562
59
794


73
c
702
701
826
1168
820
650
60
775


74
d
836
789
965
1198
905
641
51
902


75
e
860
731
896
1116
931
644
65
855


76
f
624
700
808
1172
680
587
50
774


77
g
714
714
845
1126
819
587
54
792


78
h
697
711
835
1160
789
606
63
782


79
i
726
717
849
1171
838
616
55
798


80
j
735
715
840
1157
801
560
60
791


81
k
701
714
837
1124
769
588
63
798


82
l
714
715
845
1117
810
573
59
801


83
m
695
712
833
1149
797
570
60
791


84
n
689
712
870
1173
805
628
50
808


85
o
701
711
821
1171
762
621
60
777


86
p
708
710
837
1164
792
582
60
780


87
q
718
718
848
1139
809
595
54
792


88
r
702
713
842
1173
764
632
65
792


89
s
745
724
861
1154
853
625
59
814


90
t
731
717
851
1178
810
565
54
801


91
u
709
718
845
1130
801
635
61
807


92
v
736
716
853
1126
808
630
62
802


93
w
732
718
855
1192
849
623
64
814













ANNEALING

















FIRST
SECOND
PRESENCE
PRESENCE






AVERAGE
AVERAGE
OR
OR



RETENTION
COOLING
COOLING
ABSENCE OF
ABSENCE OF
PRESENCE OR


SAMPLE
TIME
RATE
RATE
PLATING
ALLOYING
ABSENCE OF


NO.
(SECOND)
(° C./SECOND)
(° C./SECOND)
TREATMENT
TREATMENT
TEMPERING
NOTE





71
50
40
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


72
206
13
4
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


73
55
5
1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


74
116
5
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


75
134
34
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


76
99
21
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


77
87
15
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


78
116
2
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


79
114
29
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


80
78
35
4
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


81
56
30
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


82
110
7
5
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


83
107
38
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


84
138
28
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


85
204
24
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


86
51
6
1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


87
183
43
5
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


88
139
17
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


89
31
18
1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


90
81
7
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


91
186
32
1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


92
164
40
1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE


93
94
21
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



















TABLE 7









HOT ROLLING















FINISH






SLAB
ROLLING

COLD
ANNEALING






















HEATING
FINISHING

ROLLING
MAXIMUM




SYMBOL
Ar3


TEM-
TEM-
COILING
REDUCTION
HEATING
RETENTION


SAMPLE
OF
POINT
Ac1
Ac3
PERATURE
PERATURE
TEMPERATURE
RATIO
TEMPERATURE
TIME


NO.
STEEL
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(° C.)
(%)
(° C.)
(SECOND)

















94
X
683
710
832

1000

757
CRACKING OCCURS IN THE MIDDLE OF HOT ROLLING









AND SHEET PASSING THEREAFTER IS IMPOSSIBLE


95
X
683
710
832
1130

653

SHAPE BECOMES WORSE IN THE MIDDLE OF HOT ROLLING









AND SHEET PASSING THEREATER IS IMPOSSIBLE















96
X
683
710
832
1130
813

380

LOAD OF COLD ROLLING BECOMES










LARGE EXCESSIVELY AND COLD ROLLING










IS IMPOSSISLE

















97
X
683
710
832
1130
813

700

61
793
174
















98
X
683
710
832
1130
813
630

13

SHAPE BECOME WORSE IN THE











MIDDLE OF COLD ROLLING











AND SHEET PASSING











THEREAFTER IS IMPOSSIELE


99
X
683
710
832
1130
813
630

90

LOAD OF COLD ROLLING











BECOMES LARGE EXCESSIVELY











AND SHEET PASSING











THREAFTER IS IMPOSSIBLE

















100
X
683
710
832
1130
813
630
47

860

177


101
X
683
710
832
1130
813
630
47

670

 29


102
X
683
710
832
1130
813
630
47
784
0


103
X
683
710
832
1130
813
630
47
788
8


104
X
683
710
832
1130
813
630
47
781
100


105
X
683
710
832
1130
813
630
47
793
100


106
X
683
710
832
1130
813
630
47
798
100


107
X
683
710
832
1130
813
630
47
779
100


108
X
683
710
632
1130
813
630
47
780
100













ANNEALING

















FIRST
SECOND








AVERAGE
AVERAGE
PRESENCE
PRESENCE




COOLING
COOLING
OR
OR
PRESENCE




RATE
RATE
ABSENCE OF
ABSENCE OF
OR



SAMPLE
(° C./
(° C./
PLATING
ALLOYING
ABSENCE OF



NO.
SECOND)
SECOND)
TREATMENT
TREATMENT
TEMPERING
NOTE















94
CRACKING OCCURS IN THE MIDDLE OF HOT ROLLING
COMPARATIVE EXAMPLE




AND SHEET PASSING THEREAFTER IS IMPOSSIBLE



95
SHAPE BECOMES WORSE IN THE MIDDLE OF HOT ROLLING
COMPARATIVE EXAMPLE




AND SHEET PASSING THEREATER IS IMPOSSIBLE



96
LOAD OF COLD ROLLING BECOMES LARGE EXCESSIVELY
COMPARATIVE EXAMPLE




AND COLD ROLLING IS IMPOSSISLE















97
15
4
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE











98
SHAPE BECOME WORSE IN THE MIDDLE OF COLD
COMPARATIVE EXAMPLE




ROLLING AND SHEET PASSING THEREAFTER IS IMPOSSIELE



99
LOAD OF COLD ROLLING BECOMES LARGE
COMPARATIVE EXAMPLE




EXCESSIVELY AND SHEET PASSING THREAFTER IS IMPOSSIBLE















100
24
4
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



101
15
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



102
17
2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



103
32
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



104
  0.1
3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



105

68

2
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



106
24
  0.1
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



107
28
  0.3
ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE



108
24

14

ABSENT
ABSENT
ABSENT
COMPARATIVE EXAMPLE










Thereafter, of each of the steel sheets, an area fraction fF of ferrite, an area fraction fM of martensite, an area fraction fGB of granular bainite, an area fraction fB of bainite, an area fraction fP of pearlite, and an area fraction fR-γ of retained austenite were measured. Results are illustrated in Table 8 to Table 12. Each underline in Table 8 to Table 12 regarding these results indicates that a corresponding numerical value is out of the range of the present invention.


Then, a tensile test, a hole expansion test, and a bending test of each of the steel sheets were performed. In the tensile test, a Japan Industrial Standard JIS No. 5 test piece was taken perpendicularly to the rolling direction from the steel sheet, of which a tensile strength TS and total elongation EL were measured in conformity with JISZ2242. In the hole expansion test, a hole expansion ratio 2. was measured in accordance with the description of JISZ2256. In the bending test, a test in conformity with the stipulation of Standard 238-100 of Verband der Automobilindustrie (VDA) was performed and a VDA bending angle a was measured. These results are also illustrated in Table 8 to Table 12. Each underline in Table 8 to Table 12 regarding these results indicates that a corresponding numerical value is out of a desired range. The desired range to be described here means that TS is 1180 MPa or more, EL is 10% or more, λ is 20% or more, and the VDA bending angle α is equal to or more than a reference value α0 0=7.69t2-38.4t+109 when a thickness is set to t (mm)).















TABLE 8









SYMBOL
METAL STRUCTURE (%)

MECHANICAL PROPERTIES























SAMPLE
OF
fF
fM
fGB
fB
fP
fR−γ
fP + fR−γ
THICKNESS
TS
EL
λ
αO
α



No.
STEEL
(%)
(%)
(%)
(%)
(%)
(%)
(%)
(mm)
(MPa)
(%)
(%)
(°)
(°)
NOTE

























1
A
34
34
18
8
0
6
6
1.80
1236
12
31
65
89
EXAMPLE


2
A
31
38
12
13
0
6
6
1.38
1280
10
44
71
89
EXAMPLE


3
A
42
31
13
14
0
0
0
1.20
1181
13
38
74
81
EXAMPLE


4
A
34
34
14
12
0
6
6
1.26
1234
10
33
73
93
EXAMPLE


5
B
34
32
15
11
0
8
8
1.68
1194
11
53
66
100
EXAMPLE


6
B
39
31
13
12
0
5
5
1.32
1181
12
23
72
77
EXAMPLE


7
B
35
35
15
11
0
4
4
1.17
1182
11
53
75
85
EXAMPLE


8
B
34
35
12
14
0
5
5
1.17
1191
11
27
75
95
EXAMPLE


9
C
35
38
12
13
0
2
2
1.44
1212
11
27
70
79
EXAMPLE


10
C
30
35
13
18
0
4
4
1.50
1216
10
44
69
89
EXAMPLE


11
C
40
40
13
5
0
2
2
1.47
1211
12
44
69
86
EXAMPLE


12
C
43
33
14
9
0
1
1
1.38
1181
13
20
71
86
EXAMPLE


13
D
42
33
13
8
0
4
4
1.95
1182
13
20
63
83
EXAMPLE


14
D
40
32
12
12
0
4
4
0.96
1186
12
31
79
87
EXAMPLE


15
D
44
32
12
8
0
4
4
1.29
1182
13
26
72
75
EXAMPLE


16
D
34
35
12
14
0
5
5
1.41
1208
11
27
70
72
EXAMPLE


17
E
45
32
12
11
0
0
0
0.96
1182
15
21
79
81
EXAMPLE


18
E
30
41
18
11
0
0
0
1.53
1247
10
59
68
91
EXAMPLE


19
E
40
33
14
13
0
0
0
1.44
1195
12
23
70
87
EXAMPLE


20
E
31
46
10
13
0
0
0
1.50
1287
10
33
69
97
EXAMPLE


21
F
46
33
10
11
0
0
0
0.96
1183
14
33
79
94
EXAMPLE


22
F
32
44
10
14
0
0
0
1.29
1268
11
37
72
92
EXAMPLE


23
F
32
37
16
15
0
0
0
1.44
1209
11
27
70
83
EXAMPLE


24
F
39
36
11
14
0
0
0
1.14
1194
12
45
75
100
EXAMPLE






















TABLE 9









SYMBOL
METAL STRUCTURE (%)

MECHANICAL PROPERTIES























SAMPLE
OF
fF
fM
fGB
fB
fP
fR−γ
fP + fR−γ
THICKNESS
TS
EL
λ
αO
α



No.
STEEL
(%)
(%)
(%)
(%)
(%)
(%)
(%)
(mm)
(MPa)
(%)
(%)
(°)
(°)
NOTE

























25
G
36
45
10
9
0
0
0
1.26
1216
12
31
73
78
EXAMPLE


26
G
37
40
15
8
0
0
0
1.62
1185
12
44
67
101
EXAMPLE


27
G
33
46
10
11
0
0
0
1.38
1240
11
27
71
84
EXAMPLE


28
G
32
45
12
11
0
0
0
1.35
1232
11
53
71
102
EXAMPLE


29
G
32
45
14
9
0
0
0
1.17
1214
11
28
75
75
EXAMPLE


30
H
33
44
12
11
0
0
0
1.20
1194
11
37
74
82
EXAMPLE


31
H
32
45
14
9
0
0
0
1.02
1203
11
27
78
78
EXAMPLE


32
H
33
43
10
14
0
0
0
1.71
1196
11
53
66
103
EXAMPLE


33
H
31
47
9
13
0
0
0
1.17
1225
11
51
75
104
EXAMPLE


34
H
32
45
9
14
0
0
0
1.41
1211
12
27
70
82
EXAMPLE


35
H
31
42
14
13
0
0
0
1.50
1185
11
37
69
90
EXAMPLE


36
I
33
40
19
8
0
0
0
0.99
1192
11
53
79
89
EXAMPLE


37
I
30
43
18
9
0
0
0
1.05
1210
10
33
77
92
EXAMPLE


38
I
31
43
12
14
0
0
0
1.41
1218
11
27
70
72
EXAMPLE


39
I
32
42
14
12
0
0
0
1.65
1205
11
27
67
92
EXAMPLE


40
I
33
39
19
9
0
0
0
1.05
1182
10
46
77
90
EXAMPLE


41
I
33
41
19
7
0
0
0
1.41
1188
11
37
70
83
EXAMPLE


42
J
34
39
18
9
0
0
0
0.99
1199
11
27
79
79
EXAMPLE


43
J
32
41
18
9
0
0
0
1.05
1212
11
28
77
80
EXAMPLE


44
J
35
41
15
9
0
0
0
1.41
1217
11
35
70
94
EXAMPLE


45
J
32
39
13
16
0
0
0
1.65
1214
11
34
67
94
EXAMPLE


46
J
33
40
17
10
0
0
0
1.29
1223
11
27
72
82
EXAMPLE


47
J
32
38
13
17
0
0
0
1.44
1210
11
54
70
91
EXAMPLE





















TABLE 10









METAL STRUCTURE (%)

MECHANICAL PROPERTIES























SAMPLE
SYMBOL OF
fF
fM
fGB
fB
fP
fR−γ
fP + fR−γ
THICKNESS
TS
EL
λ
αO
α



No.
STEEL
(%)
(%)
(%)
(%)
(%)
(%)
(%)
(mm)
(MPa)
(%)
(%)
(°)
(°)
NOTE

























48
K
31
39
13
17
0
0
0
1.65
1193
11
38
67
86
EXAMPLE


49
K
34
42
14
10
0
0
0
1.50
1207
12
26
69
82
EXAMPLE


50
K
32
37
13
18
0
0
0
1.50
1182
11
38
69
83
EXAMPLE


51
K
32
36
13
19
0
0
0
1.05
1183
12
63
77
84
EXAMPLE


52
K
33
41
10
16
0
0
0
1.08
1200
11
53
76
104
EXAMPLE


53
L
33
40
18
9
0
0
0
1.08
1244
11
51
76
100
EXAMPLE


54
M
37
36
19
8
0
0
0
1.47
1180
12
32
69
89
EXAMPLE


55
N
40
34
13
13
0
0
0
1.05
1188
13
23
77
84
EXAMPLE


56
O
31
39
12
13
0
0
0
1.14
1216
12
24
75
74
EXAMPLE


57
P
33
39
12
16
0
0
0
1.11
1254
11
50
76
95
EXAMPLE


58
Q
39
38
11
12
0
0
0
1.29
1186
12
32
72
93
EXAMPLE


59
R
34
41
10
15
0
0
0
1.11
1220
11
53
76
92
EXAMPLE


60
S
32
39
13
16
0
0
0
1.32
1209
11
54
72
90
EXAMPLE


61
T
34
40
13
13
0
0
0
1.44
1213
12
45
70
99
EXAMPLE


62
U
34
40
18
8
0
0
0
1.05
1184
12
43
77
104
EXAMPLE


63
V
33
42
15
10
0
0
0
1.26
1223
11
37
73
93
EXAMPLE


64
W
34
41
14
11
0
0
0
1.17
1195
11
50
75
87
EXAMPLE


65
X
38
37
14
11
0
0
0
1.29
1188
13
28
72
83
EXAMPLE


66
X
35
39
12
14
0
0
0
1.20
1207
12
25
74
89
EXAMPLE


67
Y
31
37
14
18
0
0
0
1.38
1181
11
23
71
75
EXAMPLE


68
Z
39
38
12
11
0
0
0
1.26
1205
13
26
73
81
EXAMPLE






















TABLE 11









SYMBOL
METAL STRUCTURE (%)

MECHANICAL PROPERTIES























SAMPLE
OF
fF
fM
fGB
fB
fP
fR−γ
fP + fR−γ
THICKNESS
TS
EL
λ
αO
α



No.
STEEL
(%)
(%)
(%)
(%)
(%)
(%)
(%)
(mm)
(MPa)
(%)
(%)
(°)
(°)
NOTE





71

a

31
40
17
12
0
0
0
1.38

1078

12
31
71
93
COMPARATIVE

















EXAMPLE


72

b

36
32
10
14
8
0
8
1.23
1198
10

18

73

66

COMPARATIVE

















EXAMPLE


73

c

41
33
18
 8
0
0
0
1.20

1086

11
34
74
104 
COMPARATIVE

















EXAMPLE


74

d

36
31
14
19
0
0
0
1.47

1099

10
32
69
100 
COMPARATIVE

















EXAMPLE


75

e


25


25

10

40

0
0
0
1.05

1096

13

18

77
82
COMPARATIVE

















EXAMPLE


76

f

31
45
12
12
0
0
0
1.50
1209
10

19

69

65

COMPARATIVE

















EXAMPLE


77

g

40
36
14
10
0
0
0
1.38

1119

9

17

71

58

COMPARATIVE

















EXAMPLE


78

h

43
33
13
11
0
0
0
1.11

1158

11

16

76

63

COMPARATIVE

















EXAMPLE


79

i

39
35
12
14
0
0
0
1.35

1152

8

17

71

70

COMPARATIVE

















EXAMPLE


80
j
39
35
 9
17
0
0
0
1.20

1173

9

15

74

63

COMPARATIVE

















EXAMPLE


81

k

32
41
17
10
0
0
0
1.11
1259
10

17

76
76
COMPARATIVE

















EXAMPLE


82

l

34
41
 9
16
0
0
0
1.23
1211
11

12

73

60

COMPARATIVE

















EXAMPLE


83

m

35
37
14
14
0
0
0
1.20
1239
10

16

74
75
COMPARATIVE

















EXAMPLE


84

n

39
48
 6
 7
0
0
0
1.50
1277
10

18

69
80
COMPARATIVE

















EXAMPLE


85

o

40
42
10
 8
0
0
0
1.20
1185
11

17

74

72

COMPARATIVE

















EXAMPLE


86

p

45
30
16
 9
0
0
0
1.20

1092

12

19

74
94
COMPARATIVE

















EXAMPLE


87

g

43
30
16
11
0
0
0
1.38

1119

11

14

71
75
COMPARATIVE

















EXAMPLE


88

r

39
38
11
12
0
0
0
1.05

1141

9

13

77

66

COMPARATIVE

















EXAMPLE


89

s

34
40
19
 7
0
0
0
1.23
1204
10

13

73

57

COMPARATIVE

















EXAMPLE


90

t

37
38
12
13
0
0
0
1.38

1170

9

11

71

60

COMPARATIVE

















EXAMPLE


91

u

30
42
18
10
0
0
0
1.17
1245
9

14

75

67

COMPARATIVE

















EXAMPLE


92

v

37
34
16
13
0
0
0
1.14

1119

10

11

75

63

COMPARATIVE

















EXAMPLE


93

w

30
45
13
12
0
0
0
1.08
1218
8

15

76

62

COMPARATIVE

















EXAMPLE






















TABLE 12









SYMBOL
METAL STRUCTURE (%)

MECHANICAL PROPERTIES























SAMPLE
OF
fF
fM
fGB
fB
fP
fR−γ
fP + fR−γ
THICKNESS
TS
EL
λ
αO
α



No.
STEEL
(%)
(%)
(%)
(%)
(%)
(%)
(%)
(mm)
(MPa)
(%)
(%)
(°)
(°)
NOTE













94
X
HOT-ROLLED SHEET SHAPE IS DEFECTIVE
COMPARATIVE





EXAMPLE


95
X
HOT-ROLLED SHEET SHAPE IS DEFECTIVE
COMPARATIVE





EXAMPLE


96
X
COLD ROLLING IS IMPOSSIBLE
COMPARATIVE





EXAMPLE






















97
X
32
31
10
27
0
0
0
1.17
1181
10
20
75
75
EXAMPLE










98
X
COLD ROLLING IS IMPOSSIBLE
COMPARATIVE





EXAMPLE


99
X
COLD ROLLING IS IMPOSSIBLE
COMPARATIVE





EXAMPLE






















100
X
0
49
11 

40

0
0
0
1.59
1341
8
45
67
74
COMPARATIVE

















EXAMPLE


101
X

82

0

0

0
18
0

18

1.59
551
22

13

67
71
COMPARATIVE

















EXAMPLE


102
X

52


26


2

4
16
0

16

1.59
937
15

14

67

66

COMPARATIVE

















EXAMPLE


103
X
42
34

1

3
20
0

20

1.59

1025

13
27
67
87
COMPARATIVE

















EXAMPLE


104
X

56


27

8
9
0
0
0
1.59

1069

16
25
67
71
COMPARATIVE

















EXAMPLE


105
X

28

32

21

7
12
0

12

1.59

1051

11
35
67

65

COMPARATIVE

















EXAMPLE


106
X
44

25

17 
8
6
0
6
1.59

1017

13

18

67

62

COMPARATIVE

















EXAMPLE


107
X
43

16


1


40

0
0
0
1.59

1027

13
26
67

65

COMPARATIVE

















EXAMPLE


108
X
48

12


0


40

0
0
0
1.59

1002

15

17

67

62

COMPARATIVE

















EXAMPLE









As illustrated in Table 8 to Table 10, it was possible to obtain a high strength and excellent elongation and hole expandability in each of samples falling within the present invention range.


In Sample No. 71, the C content was too low, and thus the tensile strength was low. In Sample No. 72, the C content was too high, and thus the hole expansion ratio was low. In Sample No. 73, the Si content was too low, and thus the tensile strength was low. In Sample No. 74, the Si content was too high, and thus the tensile strength was low. In Sample No. 75, the Mn content was too low, and thus the tensile strength and the hole expansion ratio were low. In Sample No. 76, the Mn content was too high, and thus the hole expansion ratio and the VDA bending angle were low. In Sample No. 77, the P content was too high, and thus the tensile strength, the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 78, the S content was too high, and thus the tensile strength and the hole expansion ratio were low. In Sample No. 79, the Al content was too low, and thus the tensile strength, the elongation, and the hole expansion ratio were low. In Sample No. 80, the Al content was too high, and thus the tensile strength, the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 81, the N content was too high, and thus the hole expansion ratio was low. In Sample No. 82, the O content was too high, and thus the hole expansion ratio and the VDA bending angle were low.


In Sample No. 83, the Cr content was too high, and thus the hole expansion ratio was low. In Sample No. 84, the Mo content was too high, and thus the hole expansion ratio was low. In Sample No. 85, the Ni content was too high, and thus the hole expansion ratio was low. In Sample No. 86, the Cu content was too high, and thus the tensile strength and the hole expansion ratio were low. In Sample No. 87, the Nb content was too high, and thus the tensile strength and the hole expansion ratio were low. In Sample No. 88, the Ti content was too high, and thus the tensile strength, the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 89, the V content was too high, and thus the hole expansion ratio and the VDA bending angle were low. In Sample No. 90, the B content was too high, and thus the tensile strength, the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 91, the Ca content was too high, and thus the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 92, the Mg content was too high, and thus the tensile strength, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 93, the REM content was too high, and thus the elongation, the hole expansion ratio, and the VDA bending angle were low.


In Sample No. 94, the slab heating temperature was too low and cracking occurred during hot rolling, failing to perform sheet passing to be performed thereafter. In Sample No. 95, the finishing temperature of the finish rolling was too low, and thus the shape became worse in the middle of hot rolling, failing to perform sheet passing to be performed thereafter. In Sample No. 96, the coiling temperature was too low, and thus the hot-rolled steel sheet became hard excessively, failing to perform cold rolling thereafter. In Sample No. 97, the coiling temperature was too high and the area fraction of the martensite became short, and thus the elongation, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 98, the reduction ratio of the cold rolling was too low, and thus the shape became worse in the middle of cold rolling, failing to perform sheet passing to be performed thereafter. In Sample No. 99, the reduction ratio of the cold rolling was too high, and thus the rolling load became large excessively, failing to perform sheet passing to be performed thereafter. In Sample No. 100, the maximum heating temperature of the annealing was too high, the area fraction of the ferrite became short, and the area fraction of the bainite was excessive, and thus the elongation was low. In Sample No. 101, the maximum heating temperature of the annealing was too low, the area fractions of the ferrite and the pearlite were excessive, and the area fractions of the martensite and the granular bainite became short, and thus the tensile strength and the hole expansion ratio were low. In Sample No. 102, the retention time at the maximum heating temperature was too short, the area fractions of the ferrite and the pearlite were excessive, and the area fractions of the martensite and the granular bainite became short, and thus the tensile strength, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 103, the retention time at the maximum heating temperature was too short, the area fraction of the pearlite was excessive, and the area fraction of the granular bainite became short, and thus the tensile strength was low. In Sample No. 104, the first average cooling rate was too low, the area fraction of the ferrite was excessive, and the area fraction of the martensite became short, and thus the tensile strength was low. In Sample No. 105, the first average cooling rate was too high, the area fraction of the ferrite became short, and the area fractions of the granular bainite and the pearlite were excessive, and thus the tensile strength and the VDA bending angle were low. In Sample No. 106, the second average cooling rate was too low and the area fraction of the martensite became short, and thus the tensile strength, the hole expansion ratio, and the VDA bending angle were low. In Sample No. 107, the second average cooling rate was too low, the area fractions of the martensite and the granular bainite became short, and the area fraction of the bainite was excessive, and thus the tensile strength and the VDA bending angle were low. In Sample No. 108, the second average cooling rate was too high, the area fractions of the martensite and the granular bainite became short, and the area fraction of the bainite was excessive, and thus the tensile strength, the hole expansion ratio, and the VDA bending angle 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: 0.09% to 0.15%,Si: 0.2% to 2.5%,Al: 0.01% to 1.00%,Mn: 1.0% to 3.0%,P: 0.02% or less,S: 0.01% or less,N: 0.007% or less,O: 0.006% or less,Cr: 0.00% to 1.00%,Mo: 0.00% to 1.00%,B: 0.0000% to 0.010%,Nb: 0.000% to 0.30%,Ti: 0.000% to 0.30%,Ni: 0.00% to 1.00%,Cu: 0.00% to 1.00%,V: 0.000% to 0.50%,Mg: 0.0000% to 0.04%,REM: 0.0000% to 0.04%, and the balance: Fe and impurities; anda metal structure represented by, in area fraction,ferrite: 30% to 50%,granular bainite: 5% to 20%,martensite: 30% to 55%,bainite: less than 35%, andretained austenite and pearlite: 10% or less in total.
  • 2. The steel sheet according to claim 1, wherein a tensile strength is 1180 MPa or more,elongation is 10% or more, anda hole expansion value is 20% or more.
  • 3. The steel sheet according to claim 1, wherein a VDA bending angle in the case where a thickness is set to t (mm) is “7.69t2-38.4t+109” or more.
  • 4-5. (canceled)
  • 6. The steel sheet according to claim 2, wherein a VDA bending angle in the case where a thickness is set to t (mm) is “7.69t2-38.4t+109” or more.
  • 7. The steel sheet according to claim 1, further comprising: a hot-dip galvanizing layer on a surface thereof.
  • 8. The steel sheet according to claim 2, further comprising: a hot-dip galvanizing layer on a surface thereof.
  • 9. The steel sheet according to claim 3, further comprising: a hot-dip galvanizing layer on a surface thereof.
  • 10. The steel sheet according to claim 6, further comprising: a hot-dip galvanizing layer on a surface thereof.
  • 11. The steel sheet according to claim 1, further comprising: an alloyed hot-dip galvanizing layer on a surface thereof.
  • 12. The steel sheet according to claim 2, further comprising: an alloyed hot-dip galvanizing layer on a surface thereof.
  • 13. The steel sheet according to claim 3, further comprising: an alloyed hot-dip galvanizing layer on a surface thereof.
  • 14. The steel sheet according to claim 6, further comprising: an alloyed hot-dip galvanizing layer on a surface thereof.
PCT Information
Filing Document Filing Date Country Kind
PCT/JP2017/003109 1/30/2017 WO 00