STEEL SHEET, COATED STEEL SHEET, AND METHODS FOR MANUFACTURING SAME

- JFE STEEL CORPORATION

A steel sheet having TS of 590 MPa or more and YR of 68% or more is obtained by providing a predetermined chemical composition and a predetermined steel microstructure, where an average aspect ratio of crystal grains of each phase (polygonal ferrite, martensite, and retained austenite) is 2.0 or more and 15.0 or less, wherein the polygonal ferrite has an average grain size of 6 μm or less, the martensite has an average grain size of 3 μm or less, the retained austenite has an average grain size of 3 μm or less, and a value obtained by dividing a Mn content in the retained austenite in mass % by a Mn content in the polygonal ferrite in mass % equals 2.0 or more.

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Description
TECHNICAL FIELD

This disclosure relates to a steel sheet, a hot-dip galvanized steel sheet, a hot-dip aluminum-coated steel sheet, and an electrogalvanized steel sheet, and methods for manufacturing the same, and in particular to a steel sheet with excellent formability and hole expansion formability and high yield ratio that is preferably used in parts in the industrial fields of automobiles, electronics, and the like.

BACKGROUND

In recent years, enhancement of fuel efficiency of automobiles has become an important issue from the viewpoint of global environment protection. Consequently, there is an active movement to reduce the thickness of automotive body components through increases in strength of steel sheets as automotive body materials, and thereby reduce the weight of automotive body itself.

In general, however, strengthening of steel sheets leads to deterioration in formability, causing the problem of cracking during forming. It is thus not simple to reduce the thickness of steel sheets. Therefore, it is desirable to develop materials with increased strength and good formability. In addition to good formability, steel sheets with a tensile strength (TS) of 590 MPa or more are required to have, in particular, enhanced impact energy absorption properties. To enhance impact energy absorption properties, it is effective to increase yield ratio (YR). The reason is that a higher yield ratio enables the steel sheet to absorb impact energy more effectively with less deformation.

Moreover, in the case of using a steel sheet in an automotive body, stretch flanging according to the shape of the automotive body is performed, so that excellent hole expansion formability is required, too.

For example, JPS61157625A (PTL 1) proposes a high-strength steel sheet with extremely high ductility having a tensile strength of 1000 MPa or higher and a total elongation (EL) of 30% or more, utilizing deformation induced transformation of retained austenite.

In addition, JPH1259120A (PTL 2) proposes a high-strength steel sheet with well-balanced strength and ductility that is obtained from high-Mn steel through heat treatment in a ferrite-austenite dual phase region.

Moreover, JP2003138345A (PTL 3) proposes a high-strength steel sheet with improved local ductility that is obtained from high-Mn steel through hot rolling to have a microstructure containing bainite and martensite after subjection to the hot rolling, followed by annealing and tempering to cause fine retained austenite, and subsequently tempered bainite or tempered martensite in the microstructure.

CITATION LIST Patent Literature

PTL 1:JPS61157625A

PTL 2: JPH1259120A

PTL 3: JP2003138345A

SUMMARY Technical Problem

The steel sheet described in PTL 1 is manufactured by austenitizing a steel sheet containing C, Si, and Mn as basic components, and subjecting the steel sheet to a so-called austempering process whereby the steel sheet is quenched to and held isothermally in a bainite transformation temperature range. During the austempering process, C concentrates in austenite to form retained austenite.

However, while a high concentration of C beyond 0.3% is required for the formation of a large amount of retained austenite, such a high C concentration above 0.3% leads to a significant decrease in spot weldability, which may not be suitable for practical use in steel sheets for automobiles. Additionally, the main objective of PTL 1 is improving the ductility of steel sheets, without any consideration for the hole expansion formability, bendability, or yield ratio.

PTLs 2 and 3 describe techniques for improving the ductility of steel sheets from the perspective of formability, but do not consider the bendability, yield ratio, or hole expansion formability of the steel sheet.

To address these issues, it could thus be helpful to provide a steel sheet, a hot-dip galvanized steel sheet, a hot-dip aluminum-coated steel sheet, and an electrogalvanized steel sheet that are excellent in formability and hole expansion formability with TS of 590 MPa or more and YR of 68% or more, and methods for manufacturing the same.

Solution to Problem

To manufacture a high-strength steel sheet that can solve the above issues, with excellent formability and hole expansion formability as well as high yield ratio and high tensile strength, we made intensive studies from the perspectives of the chemical compositions and manufacturing methods of steel sheets. As a result, we discovered that a high-strength steel sheet with high yield ratio that is excellent in formability such as ductility and hole expansion formability can be manufactured by appropriately controlling the chemical composition and microstructure of steel.

Specifically, a steel sheet that has a steel composition containing Mn: 2.60 mass % or more and 4.20 mass % or less, with the addition amounts of other alloying elements such as Ti being adjusted appropriately, is hot rolled to obtain a hot-rolled sheet. The hot-rolled sheet is then subjected to pickling to remove scales, retained in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s, and optionally cold rolled at a rolling reduction of less than 30% to obtain a cold-rolled sheet. Further, the hot-rolled sheet as annealed after the hot rolling or the cold-rolled sheet is retained in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s, and subsequently cooled.

Through this process, the hot-rolled sheet or the cold-rolled sheet has a microstructure that contains, in area ratio, 20% or more and 65% or less of polygonal ferrite, 8% or more of non-recrystallized ferrite, and 5% or more and 25% or less of martensite, and, in volume fraction, 8% or more of retained austenite, where the average aspect ratio of crystal grains of each phase (polygonal ferrite, martensite, and retained austenite) is 2.0 or more and 15.0 or less, the polygonal ferrite has an average grain size of 6 μm or less, the martensite has an average grain size of 3 μm or less, and the retained austenite has an average grain size of 3 μm or less. Moreover, the microstructure of the hot-rolled sheet or the cold-rolled sheet can be controlled so that a value obtained by dividing a Mn content in the retained austenite (in mass %) by a Mn content in the polygonal ferrite (in mass %) equals 2.0 or more, making it possible to obtain 8% or more of retained austenite stabilized with Mn.

This disclosure has been made based on these discoveries.

Specifically, the primary features of this disclosure are as described below.

1. A steel sheet comprising: a chemical composition containing (consisting of), in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisiting of Fe and inevitable impurities; and a steel microstructure that contains, in area ratio, 20% or more and 65% or less of polygonal ferrite, 8% or more of non-recrystallized ferrite, and 5% or more and 25% or less of martensite, and that contains, in volume fraction, 8% or more of retained austenite, where an average aspect ratio of crystal grains of each of the polygonal ferrite, the martensite, and the retained austenite is 2.0 or more and 15.0 or less, wherein the polygonal ferrite has an average grain size of 6 μm or less, the martensite has an average grain size of 3 μm or less, the retained austenite has an average grain size of 3 μm or less, and a value obtained by dividing a Mn content in the retained austenite in mass % by a Mn content in the polygonal ferrite in mass % equals 2.0 or more.

2. The steel sheet according to 1., wherein the retained austenite has a C content that satisfies the following formula in relation to the Mn content in the retained austenite:


0.09*[Mn]−0.026−0.150≤[C]≤0.09*[Mn]−0.026+0.150

where

[C] is the C content in the retained austenite in mass %, and

[Mn] is the Mn content in the retained austenite in mass %.

3. A coated steel sheet comprising: the steel sheet according to 1. or 2.; and one selected from a hot-dip galvanized layer, a galvannealed layer, a hot-dip aluminum-coated layer, and an electrogalvanized layer.

4. A method for manufacturing a steel sheet, the method comprising: heating a steel slab having the chemical composition according to 1.; hot rolling the steel slab with a finisher delivery temperature of 750° C. or higher and 1000° C. or lower to obtain a steel sheet; coiling the steel sheet at 300° C. or higher and 750° C. or lower; then subjecting the steel sheet to pickling to remove scales; retaining the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s; optionally cold rolling the steel sheet at a rolling reduction of less than 30%; and then retaining the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s and subsequently cooling the steel sheet, to manufacture the steel sheet according to 1. or 2.

5. The method according to 4., wherein a value obtained by dividing a volume fraction of the retained austenite after performing tensile working with an elongation value of 10% by a volume fraction of the retained austenite before the tensile working equals 0.3 or more.

6. The method according to 4., comprising after the cooling, either subjecting the steel sheet to one selected from hot-dip galvanizing treatment, hot-dip aluminum coating treatment, and electrogalvanizing treatment, or subjecting the steel sheet to hot-dip galvanizing treatment and then to alloying treatment at 450° C. or higher and 600° C. or lower, to manufacture the coated steel sheet according to 3.

Advantageous Effect

According to the disclosure, it becomes possible to provide a high-strength steel sheet with excellent formability and hole expansion formability and high yield ratio that exhibits TS of 590 MPa or more and YR of 68% or more. Steel sheets according to the disclosure are highly beneficial in industrial terms, because they can improve fuel efficiency when applied to, for example, automobile structural parts, by a reduction in the weight of automotive bodies.

BRIEF DESCRIPTION OF THE DRAWING

In the accompanying drawings:

FIG. 1 illustrates the relationship between the working ratio of tensile working and the volume fraction of retained austenite; and

FIG. 2 illustrates the relationship between the elongation of each steel sheet and the value obtained by dividing the volume fraction of retained austenite remaining in the steel sheet after subjection to tensile working with an elongation value of 10% by the volume fraction of retained austenite before the tensile working.

 DETAILED DESCRIPTION

The following describes the present disclosure in detail.

First, the reasons for limiting the chemical composition of the steel to the aforementioned ranges in the present disclosure are explained. The % representations below indicating the chemical composition of the steel or steel slab are in mass % unless stated otherwise. The balance of the chemical composition of the steel or steel slab is Fe and inevitable impurities.

C: 0.030% or More and 0.250% or Less

C is an element necessary for causing a low-temperature transformation phase such as martensite to increase strength. C is also a useful element for increasing the stability of retained austenite and the ductility of steel. If the C content is less than 0.030%, it is difficult to ensure a desired area ratio of martensite, and desired strength is not obtained. It is also difficult to guarantee a sufficient volume fraction of retained austenite, and good ductility is not obtained. On the other hand, if C is excessively added to the steel beyond 0.250%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test, leading to a reduction in bendability and stretch flangeability. If excessive C is added to steel, hardening of welds and the heat-affected zone (HAZ) becomes significant and the mechanical properties of the welds deteriorate, leading to a reduction in spot weldability, arc weldability, and the like. From these perspectives, the C content is 0.030% or more and 0.250% or less. The C content is preferably 0.080% or more. The C content is preferably 0.200% or less.

Si: 0.01% or More and 3.00% or Less

Si is an element that improves the strain hardenability of ferrite, and is thus a useful element for ensuring good ductility. If the Si content is below 0.01%, the addition effect is limited. Thus the lower limit is 0.01%. On the other hand, excessively adding Si beyond 3.00% not only embrittles the steel, but also causes red scales or the like to deteriorate surface characteristics. Therefore, the Si content is 0.01% or more and 3.00% or less. The Si content is preferably 0.20% or more. The Si content is preferably 2.00% or less.

Mn: 2.60% or More and 4.20% or Less

Mn is one of the very important elements for the disclosure. Mn is an element that stabilizes retained austenite, and is thus a useful element for ensuring good ductility. Mn can also increase the TS of the steel through solid solution strengthening. These effects can be obtained when the Mn content in the steel is 2.60% or more. On the other hand, excessively adding Mn beyond 4.20% results in a rise in cost. From these perspectives, the Mn content is 2.60% or more and 4.20% or less. The Mn content is preferably 3.00% or more. The Mn content is preferably 4.20% or less.

P: 0.001% or More and 0.100% or Less

P is an element that has a solid solution strengthening effect and can be added depending on the desired TS. P also facilitates ferrite transformation, and thus is also a useful element for forming a multi-phase structure in the steel sheet. To obtain this effect, the P content in the steel sheet needs to be 0.001 or more. However, if the P content exceeds 0.100%, weldability degrades and, when a galvanized layer is subjected to alloying treatment, the alloying rate decreases, impairing galvanizing quality. Therefore, the P content is 0.001% or more and 0.100% or less. The P content is preferably 0.005% or more. The P content is preferably 0.050% or less.

S: 0.0200% or Less

S segregates to grain boundaries, embrittles the steel during hot working, and forms sulfides to reduce the local deformability of the steel sheet. Therefore, the S content is 0.0200% or less, preferably 0.0100% or less, and more preferably 0.0050% or less. Under production constraints, however, the S content is preferably 0.0001% or more. Therefore, the S content is preferably 0.0001% or more and 0.0200% or less. The S content is more preferably 0.0001% or more. The S content is more preferably 0.0100% or less. The S content is further preferably 0.0001% or more. The S content is further preferably 0.0050% or less.

N: 0.0100% or Less

N is an element that deteriorates the anti-aging property of the steel. The deterioration in anti-aging property becomes more pronounced, particularly when the N content exceeds 0.0100%. Accordingly, smaller N contents are more preferable. However, under production constraints, the N content is preferably 0.0005% or more. Therefore, the N content is preferably 0.0005% or more and 0.0100% or less. The N content is more preferably 0.0010% or more. The N content is more preferably 0.0070% or less.

Ti: 0.005% or More and 0.200% or Less

Ti is one of the very important elements for the disclosure. Ti is useful for achieving strengthening by precipitation of the steel. Ti can also ensure a desired area ratio of non-recrystallized ferrite, and contributes to increasing the yield ratio of the steel sheet. Additionally, making use of relatively hard non-recrystallized ferrite, Ti can reduce the difference in hardness from a hard secondary phase (martensite or retained austenite), and also contributes to improving stretch flangeability. These effects can be obtained when the Ti content is 0.005% or more. On the other hand, if the Ti content in the steel exceeds 0.200%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test, leading to a reduction in the bendability and stretch flangeability of the steel sheet. Therefore, the Ti content is 0.005% or more and 0.200% or less. The Ti content is preferably 0.010% or more. The Ti content is preferably 0.100% or less.

The basic components according to this disclosure have been described above. The balance other than the components described above is Fe and inevitable impurities. Additionally, the following elements may b e optionally contained as appropriate.

The chemical composition of the steel may further contain at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less.

Al is a useful element for increasing the area of a ferrite-austenite dual phase region and reducing annealing temperature dependency, i.e., increasing the stability of the steel sheet as a material. In addition, Al acts as a deoxidizer, and is also a useful element for maintaining the cleanliness of the steel. If the Al content is below 0.01%, however, the addition effect is limited. Thus the lower limit is 0.01%. On the other hand, excessively adding Al beyond 2.00% increases the risk of cracking occurring in a semi-finished product during continuous casting, and inhibits manufacturability. From these perspectives, the Al content is 0.01% or more and 2.00% or less. The Al content is preferably 0.20% or more. The Al content is preferably 1.20% or less.

Nb is useful for achieving strengthening by precipitation of the steel. The addition effect can be obtained when the content is 0.005% or more. Nb can also ensure a desired area ratio of non-recrystallized ferrite, as in the case of adding Ti, and contributes to increasing the yield ratio of the steel sheet. Additionally, making use of relatively hard non-recrystallized ferrite, Nb can reduce the difference in hardness from a hard secondary phase (martensite or retained austenite), and also contributes to improving stretch flangeability. On the other hand, if the Nb content in the steel exceeds 0.200%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test. This leads to a reduction in the bendability and stretch flangeability of the steel sheet. This also increases cost. Therefore, when added to steel, the Nb content is 0.005% or more and 0.200% or less. The Nb content is preferably 0.010% or more. The Nb content is preferably 0.100% or less.

B may be added as necessary, since it has the effect of suppressing the generation and growth of ferrite from austenite grain boundaries and enables microstructure control according to the circumstances. The addition effect can be obtained when the B content is 0.0003% or more. If the B content exceeds 0.0050%, however, the formability of the steel sheet degrades. Therefore, when added to steel, the B content is 0.0003% or more and 0.0050% or less. The B content is preferably 0.0005% or more. The B content is preferably 0.0030% or less.

Ni is an element that stabilizes retained austenite, and is thus a useful element for ensuring good ductility, and that increases the TS of the steel through solid solution strengthening. The addition effect can be obtained when the Ni content is 0.005% or more. On the other hand, if the Ni content in the steel exceeds 1.000%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test. This leads to a reduction in the bendability and stretch flangeability of the steel sheet. This also increases cost. Therefore, when added to steel, the Ni content is 0.005% or more and 1.000% or less.

Cr, V, and Mo are elements that may be added as necessary, since they have the effect of improving the balance between TS and ductility. The addition effect can be obtained when the Cr content is 0.005% or more, the V content is 0.005% or more, and/or the Mo content is 0.005% or more. However, if the Cr content exceeds 1.000%, the V content exceeds 0.500%, and/or the Mo content exceeds 1.000%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test. This leads to a reduction in the bendability and stretch flangeability of the steel sheet, and also causes a rise in cost. Therefore, when added to steel, the Cr content is 0.005% or more and 1.000% or less, the V content is 0.005% or more and 0.500% or less, and/or the Mo content is 0.005% or more and 1.000% or less.

Cu is a useful element for strengthening of steel and may be added for strengthening of steel, as long as the content is within the range disclosed herein. The addition effect can be obtained when the Cu content is 0.005% or more. On the other hand, if the Cu content in the steel exceeds 1.000%, hard martensite excessively increases in area ratio, which causes more microvoids at grain boundaries of martensite and facilitates propagation of cracks during bend test and hole expansion test. This leads to a reduction in the bendability and stretch flangeability of the steel sheet. Therefore, when added to steel, the Cu content is 0.005% or more and 1.000% or less.

Sn and Sb are elements that may be added as necessary from the perspective of suppressing decarbonization of a region extending from the surface layer of the steel sheet to a depth of about several tens of micrometers, which results from nitriding and/or oxidation of the steel sheet surface. Suppressing nitriding and/or oxidation in this way is useful for preventing a reduction in the area ratio of martensite in the steel sheet surface, and for ensuring the TS and stability of the steel sheet as a material. However, excessively adding Sn or Sb beyond 0.200% reduces toughness. Therefore, when Sn and/or Sb is added to steel, the content of each added element is 0.002% or more and 0.200% or less.

Ta forms alloy carbides or alloy carbonitrides, and contributes to increasing the strength of the steel, as is the case with Ti and Nb. It is also believed that Ta has the effect of effectively suppressing coarsening of precipitates when partially dissolved in Nb carbides or Nb carbonitrides to form complex precipitates, such as (Nb, Ta) (C, N), and providing a stable contribution to increasing the strength of the steel sheet through strengthening by precipitation. Therefore, Ta is preferably added to the steel according to the disclosure. The addition effect of Ta can be obtained when the Ta content is 0.001% or more. Excessively adding Ta, however, fails to increase the addition effect, but instead results in a rise in alloying cost. Therefore, when added to steel, the Ta content is 0.001% or more and 0.010% or less.

Ca, Mg, and REM are useful elements for causing spheroidization of sulfides and mitigating the adverse effect of sulfides on hole expansion formability (stretch flangeability). To obtain this effect, it is necessary to add any of these elements to steel in an amount of 0.0005% or more. However, if the content of each added element exceeds 0.0050%, more inclusions occur, for example, and some defects such as surface defects and internal defects are caused in the steel sheet. Therefore, when Ca, Mg, and/or REM is added to steel, the content of each added element is 0.0005% or more and 0.0050% or less.

The following provides a description of the microstructure. Sufficient ductility of the steel sheet can be ensured by facilitating the formation of polygonal ferrite in the microstructure. This, however, causes decreases in tensile strength and yield strength. Besides, therse mechanical properties also vary depending on the area ratio of martensite, and the ductility is greatly affected by the amount of retained austenite. Hence, the mechanical properties of the high-strength steel sheet can be effectively obtained by controlling the amounts (area ratio, volume fraction) of these phases (microstructures). As a result of conducting studies from this perspective, we newly discovered that the area ratios of polygonal ferrite and non-recrystallized ferrite are controllable by the rolling reduction in cold rolling. We also found out that the area ratio of martensite and the volume fraction of retained austenite are mainly determined by the addition amount of Mn. We further found out that, by omitting cold rolling or by limiting the rolling reduction in cold rolling to 30% or less, not only the area ratio of polygonal ferrite is reduced (i.e. can be controlled to an appropriate range) (relative to the whole microstructure), but also the microstructure shape of the final product changes greatly, yielding a steel sheet having crystal grains with a high aspect ratio. The value of hole expansion formability X is thus improved. In detail, the microstructure of a steel sheet with high ductility and favorable hole expansion formability is as follows.

Area Ratio of Polygonal Ferrite: 20% or More and 65% or Less

According to the disclosure, the area ratio of polygonal ferrite needs to be 20% or more to ensure sufficient ductility. On the other hand, to guarantee a TS of 590 MPa or more, the area ratio of soft polygonal ferrite needs to be 65% or less. The area ratio of polygonal ferrite is preferably 30% or more. The area ratio of polygonal ferrite is preferably 55% or less. As used herein, “polygonal ferrite” refers to ferrite that is relatively soft and that has high ductility.

Area Ratio of Non-Recrystallized Ferrite: 8% or More

In this disclosure, it is very important to set the area ratio of non-recrystallized ferrite to be 8% or more. In this regard, non-recrystallized ferrite is useful for increasing the strength of the steel sheet. However, non-recrystallized ferrite may cause a significant decrease in the ductility of the steel sheet, and thus is normally reduced in a general process. In contrast, according to the present disclosure, by using polygonal ferrite and retained austenite to provide good ductility and intentionally utilizing relatively hard non-recrystallized ferrite, it is possible to provide the steel sheet with the intended TS, without having to form a large amount of martensite, such as exceeding 25% in area ratio.

Moreover, according to the present disclosure, interfaces between different phases, namely, between polygonal ferrite and martensite, are reduced, making it possible to increase the yield point (YP) and YR of the steel sheet.

To obtain these effects, the area ratio of non-recrystallized ferrite needs to be 8% or more, preferably 10% or more. As used herein, “non-recrystallized ferrite” refers to ferrite that contains strain in the grains with a crystal orientation difference of less than 15°, and that is harder than the above-described polygonal ferrite with high ductility.

In the disclosure, no upper limit is placed on the area ratio of non-recrystallized ferrite, yet a preferred upper limit is around 45%, considering the possibility of increased material anisotropy in the steel sheet surface.

Area Ratio of Martensite: 5% or More and 25% or Less

To achieve TS of 590 MPa or more, the area ratio of martensite needs to be 5% or more. On the other hand, to ensure good ductility, the area ratio of martensite needs to be limited to 25% or less.

According to the disclosure, the area ratios of ferrite (including polygonal ferrite and non-recrystallized ferrite) and martensite can be determined in the following way.

Specifically, a cross section of a steel sheet that is taken in the sheet thickness direction to be parallel to the rolling direction (which is an L-cross section) is polished, then etched with 3 vol.% nital, and ten locations are observed at 2000 times magnification under an SEM (scanning electron microscope), at a position of sheet thickness x 1/4 (which is the position at a depth of one-fourth of the sheet thickness from the steel sheet surface), to capture microstructure micrographs. The captured microstructure micrographs are used to calculate the area ratios of respective phases (ferrite and martensite) for the ten locations using Image-Pro manufactured by Media Cybernetics, the results are averaged, and each average is used as the area ratio of the corresponding phase. In the microstructure micrographs, polygonal ferrite and non-recrystallized ferrite appear as a gray structure (base steel structure), while martensite as a white structure.

According to the disclosure, the area ratios of polygonal ferrite and non-recrystallized ferrite can be determined in the following way. Specifically, low-angle grain boundaries in which the crystal orientation difference is from 2° to less than 15° and large-angle grain boundaries in which the crystal orientation difference is 15° or more are identified using EBSD (Electron Backscatter Diffraction). An IQ Map is then created, considering ferrite that contains low-angle grain boundaries in the grains as non-recrystallized ferrite. Then, low-angle grain boundaries and large-angle grain boundaries are extracted from the created IQ Map at ten locations, respectively, to determine the areas of low-angle grain boundaries and large-angle grain boundaries at the ten locations. Based on the results, the areas of polygonal ferrite and non-recrystallized ferrite are calculated to determine the area ratios of polygonal ferrite and non-recrystallized ferrite for the ten locations. By averaging the results, the above-described area ratios of polygonal ferrite and non-recrystallized ferrite are determined.

Volume Fraction of Retained Austenite: 8% or More

According to the disclosure, the volume fraction of retained austenite needs to be 8% or more, and is preferably 10% or more, to ensure sufficient ductility. According to the disclosure, no upper limit is placed on the area ratio of retained austenite, yet a preferred upper limit is around 40%, considering the risk of formation of increased amounts of unstable retained austenite resulting from insufficient concentration of C, Mn, and the like, which is less effective in improving ductility.

The volume fraction of retained austenite is calculated by determining the x-ray diffraction intensity of a plane of sheet thickness×¼ (which is the plane at a depth of one-fourth of the sheet thickness from the steel sheet surface), which is exposed by polishing the steel sheet surface to a depth of one-fourth of the sheet thickness. Using an incident x-ray beam of MoKa, the intensity ratio of the peak integrated intensity of the {111}, {200}, {220}, and {311} planes of retained austenite to the peak integrated intensity of the {110}, {200}, and {211} planes of ferrite is calculated for all of the twelve combinations, the results are averaged, and the average is used as the volume fraction of retained austenite.

Average Grain Size of Polygonal Ferrite: 6 μm or Less

Refinement of polygonal ferrite grains contributes to improving YP and TS. Thus, to ensure a high YP and a high YR as well as a desired TS, polygonal ferrite needs to have an average grain size of 6 μm or less, and preferably 5 μm or less.

According to the disclosure, no lower limit is placed on the average grain size of polygonal ferrite, yet, from an industrial perspective, a preferred lower limit is around 0.3 μm.

Average Grain Size of Martensite: 3 μm or Less

Refinement of martensite grains contributes to improving bendability and stretch flangeability (hole expansion formability). Thus, to ensure high bendability and high stretch flangeability (high hole expansion formability), the average grain size of martensite needs to be limited to 3 μm or less, and preferably to 2.5 μm or less.

According to the disclosure, no lower limit is placed on the average grain size of martensite, yet, from an industrial perspective, a preferred lower limit is around 0.1 μm.

Average Grain Size of Retained Austenite: 3 μm or Less

Refinement of retained austenite grains contributes to improving ductility, as well as bendability and stretch flangeability (hole expansion formability). Accordingly, to ensure good ductility, bendability, and stretch flangeability (hole expansion formability) of the steel sheet, the average grain size of retained austenite needs to be 3 μm or less, and preferably 2.5 μm or less. According to the disclosure, no lower limit is placed on the average grain size of retained austenite, yet, from an industrial perspective, a preferred lower limit is around 0.1 μm.

The average grain sizes of polygonal ferrite, martensite, and retained austenite are respectively determined by averaging the results from calculating equivalent circular diameters from the areas of polygonal ferrite grains, martensite grains, and retained austenite grains measured with Image-Pro as mentioned above. Polygonal ferrite, non-recrystallized ferrite, martensite, and retained austenite are separated using EBSD, and martensite and retained austenite are identified using an EBSD phase map. In this case, each of the above-described average grain sizes is determined from the measurements for grains with a grain size of 0.01 μm or more. The reason is that grains with a grain size of less than 0.01 μm have no effect on the disclosure.

Average Aspect Ratio of Crystal Grains of each of Polygonal ferrite, Martensite, and Retained Austenite: 2.0 or More and 15.0 or Less

In this disclosure, it is very important to set the average aspect ratio of crystal grains of each of polygonal ferrite, martensite, and retained austenite to 2.0 or more.

A lower aspect ratio of crystal grains indicates that, during retention in heat treatment after cold rolling (cold-rolled sheet annealing), ferrite and austenite recover and recrystallize and then undergo grain growth, resulting in the formation of crystal grains close to equiaxed grains. The ferrite formed here is soft. In the case where cold rolling is omitted or the rolling reduction in cold rolling is less than 30%, on the other hand, the amount of strain applied decreases, so that the formation of polygonal ferrite is suppressed and a microstructure mainly composed of crystal grains with a high aspect ratio results. Such a microstructure composed of crystal grains with a high aspect ratio is hard because it contains a large amount of strain or has parts where the distance between grain boundaries is short, as compared with the above-mentioned microstructure. Therefore, not only the TS is improved, but also the difference in hardness from hard phases such as retained austenite and martensite decreases, and the hole expansion formability is improved without loss of ductility. If the aspect ratio is more than 15.0, the TS increases extremely, and favorable ductility cannot be achieved.

Thus, the average aspect ratio of crystal grains of each of polygonal ferrite, martensite, and retained austenite is limited to 2.0 or more and 15.0 or less. In terms of ductility, the average aspect ratio is more preferably 2.2 or more, and more preferably 2.4 or more.

The aspect ratio of a crystal grain mentioned here is a value obtained by dividing the major axis length of the crystal grain by the minor axis length of the crystal grain. The average aspect ratio of each type of crystal grains can be calculated as follows.

For each of polygonal ferrite grains, martensite grains, and retained austenite grains, the major axis length and minor axis length of each of 30 crystal grains are calculated using the above-mentioned Image-Pro, the major axis length is divided by the minor axis length, and the division results are averaged.

A Value Obtained by Dividing the Mn Content in the Retained Austenite (in mass %) by the Mn Content in the Polygonal Ferrite (in mass %): 2.0 or More

In this disclosure, it is very important that the value obtained by dividing the Mn content in the retained austenite (in mass %) by the Mn content in the polygonal ferrite (in mass %) equals 2.0 or more. The reason is that better ductility requires a larger amount of stable retained austenite with concentrated Mn.

According to the disclosure, no upper limit is placed on the value obtained by dividing the Mn content in the retained austenite (in mass %) by the Mn content in the polygonal ferrite (in mass %), yet a preferred upper limit is around 16.0 from the perspective of ensuring stretch flangeability.

The Mn content in the retained austenite (in mass %) and the Mn content in the polygonal ferrite (in mass %) can be determined in the following way.

Specifically, an EPMA (Electron Probe Micro Analyzer) is used to quantify the distribution of Mn in each phase in a cross section along the rolling direction at a position of sheet thickness×¼. Then, 30 retained austenite grains and 30 ferrite grains are analyzed to determine Mn contents, the results are averaged, and each average is used as the Mn content in the corresponding phase.

In addition to the above-described polygonal ferrite, martensite, and so on, the microstructure according to the disclosure may further include carbides ordinarily found in steel sheets, such as granular ferrite, acicular ferrite, bainitic ferrite, tempered martensite, pearlite, and cementite (excluding cementite in pearlite). Any of these structures may be included as long as the area ratio is 10% or less, without impairing the effect of the disclosure.

We made further investigations on the microstructures of steel sheets upon performing press forming and working.

As a result, it was discovered that there are two types of retained austenite: one transforms to martensite immediately upon the subjection of the steel sheet to press forming or working, while the other persists until the working ratio becomes high enough to cause the retained austenite to eventually transform to martensite, bringing about a TRIP phenomenon (transformation induced plasticity phenomenon). It was also revealed that good elongation can be obtained in a particularly effective way when a large amount of retained austenite transforms to martensite after the working ratio becomes high enough.

Specifically, as a result of collecting samples with good and poor elongation and measuring the quantity of retained austenite by varying the degree of tensile working from 0% to 20%, the working ratio and the quantity of retained austenite showed a tendency as illustrated in FIG. 1. As used herein, “the working ratio” refers to the elongation ratio that is determined from a tensile test performed on a JIS No. 5 test piece sampled from a steel sheet with the tensile direction being perpendicular to the rolling direction of the steel sheet.

It can be seen from FIG. 1 that the samples with good elongation each showed a gentle decrease in the quantity of retained austenite as the working ratio increased.

Accordingly, we further measured the quantity of retained austenite in each sample with TS of 780 MPa after subjection to tensile working with an elongation value of 10%, and examined the effect of the ratio of the quantity of retained austenite after the tensile working to the quantity before the tensile working on the total elongation of the steel sheet. The results are shown in FIG. 2.

It can be seen from FIG. 2 that elongation is good if the value obtained by dividing the volume fraction of retained austenite remaining in a steel after subjection to tensile working with an elongation value of 10% by the volume fraction of retained austenite before the tensile working equals 0.3 or more, but otherwise elongation is poor.

Therefore, it is preferable in the disclosure that the value obtained by dividing the volume fraction of retained austenite remaining in a steel after subjection to tensile working with an elongation value of 10% by the volume fraction of retained austenite before the tensile working equals 0.3 or more. The reason is that this set up may ensure the transformation of sufficient retained austenite to martensite after the working ratio becomes high enough.

The above-described TRIP phenomenon requires retained austenite to be present before performing press forming or working. To cause retained austenite to be present before performing press forming or working, the Ms point (martensite transformation start temperature) which depends on the elements contained in the steel microstructure needs to be as low as approximately 15° C. or lower.

Specifically, in the tensile working with an elongation value of 10% according to the disclosure, a tensile test is performed on a JIS No. 5 test piece sampled from a steel sheet with the tensile direction being perpendicular to the rolling direction of the steel sheet, and the test is interrupted when the elongation ratio reaches 10%, thus applying tensile working with an elongation value of 10% to the test piece.

The volume fraction of retained austenite can be determined in the above-described way.

Upon a detailed study of samples satisfying the above conditions, we discovered that a TRIP phenomenon providing high strain hardenability occurs upon working and even better elongation can be achieved if the C content and the Mn content in the retained austenite satisfy the following relation:


0.09*[Mn]−0.026−0.150≤[C]≤0.09*[Mn]−0.026+0.150

where

[C content] is the C content in the retained austenite in mass %, and

[Mn content] is the Mn content in the retained austenite in mass %.

When the above requirements are met, it is possible to cause a TRIP phenomenon, which is a key factor of improving ductility, to occur intermittently up until the final stage of working performed on the steel sheet, guaranteeing the generation of so-called stable retained austenite.

The C content in the retained austenite (in mass %) can be determined in the following way.

Specifically, an EPMA is used to quantify the distribution of C in each phase in a cross section along the rolling direction at a position of sheet thickness×¼. Then, 30 retained austenite grains are analyzed to determine C contents, the results are averaged, and the average is used as the C content.

Note that the Mn content in the retained austenite (in mass %) can be determined in the same way as the C content in the retained austenite.

The following describes the production conditions.

Steel Slab Heating Temperature: 1100° C. or Higher and 1300° C. or Lower

Precipitates that are present at the time of heating of a steel slab (hereinafter, also referred to simply as a “slab”) will remain as coarse precipitates in the resulting steel sheet, making no contribution to strength. Thus, remelting of any Ti- and Nb-based precipitates formed during casting is required.

In this respect, if a steel slab is heated at a temperature below 1100° C., it is difficult to cause sufficient dissolution of carbides, leading to problems such as an increased risk of trouble during the hot rolling resulting from increased rolling load. Therefore, the steel slab heating temperature is preferably 1100° C. or higher.

In addition, from the perspective of obtaining a smooth steel sheet surface by scaling-off defects in the surface layer of the slab, such as blow hole generation, segregation, and the like, and reducing cracks and irregularities over the steel sheet surface, the steel slab heating temperature is preferably 1100° C. or higher.

If the steel slab heating temperature exceeds 1300° C., however, scale loss increases as oxidation progresses. Therefore, the steel slab heating temperature is preferably 1300° C. or lower. For this reason, the steel slab heating temperature is preferably 1100° C. or higher and 1300° C. or lower. The steel slab heating temperature is further preferably 1150° C. or higher. The steel slab heating temperature is further preferably 1250° C. or lower.

A steel slab is preferably made with continuous casting to prevent macro segregation, yet may be produced with other methods such as ingot casting or thin slab casting. The steel slab thus produced may be cooled to room temperature and then heated again according to a conventional process. Moreover, energy-saving processes are applicable without any problem, such as hot direct rolling or direct rolling in which either a warm steel slab without being fully cooled to room temperature is charged into a heating furnace, or a steel slab is hot rolled immediately after being subjected to heat retaining for a short period. A steel slab is subjected to rough rolling under normal conditions and formed into a sheet bar. When the heating temperature is low, it is preferable to additionally heat the sheet bar using a bar heater or the like prior to finish rolling, from the viewpoint of preventing troubles during the hot rolling.

Finisher delivery temperature in hot rolling: 750° C. or higher and 1000° C. or lower

The heated steel slab is hot rolled through rough rolling and finish rolling to form a hot-rolled sheet. At this point, when the finisher delivery temperature exceeds 1000° C., the amount of oxides (scales) generated suddenly increases and the interface between the steel substrate and oxides becomes rough, which tends to lower the surface quality of the steel sheet after subjection to pickling and cold rolling. In addition, any hot rolling scales persisting after pickling adversely affect the ductility and stretch flangeability of the steel sheet. Moreover, grain size is excessively coarsened, causing surface deterioration in a pressed part during working. On the other hand, if the finisher delivery temperature is below 750° C., rolling load increases and rolling is performed more often with austenite being in a non-recrystallized state. As a result, an abnormal texture develops in the steel sheet, and the final product has a significant planar anisotropy such that the material properties not only become less uniform (the stability as a material decreases), but the ductility itself also deteriorates. Besides, if the finisher delivery temperature in the hot rolling is lower than 750° C. or higher than 1000° C., a microstructure having 8% or more of retained austenite in volume fraction cannot be obtained.

Therefore, the finisher delivery temperature in the hot rolling needs to be 750° C. or higher and 1000° C. or lower. The finisher delivery temperature is preferably 800° C. or higher. The finisher delivery temperature is preferably 950° C. or lower.

Average Coiling Temperature after Hot Rolling: 300° C. or Higher and 750° C. or Lower

When the average coiling temperature after the hot rolling is above 750° C., the grain size of ferrite in the microstructure of the hot-rolled sheet increases, making it difficult to ensure a desired strength of the final-annealed sheet. Besides, when the average coiling temperature after the hot rolling is above 750° C., a microstructure with an average grain size of polygonal ferrite of 6 μm or less, an average grain size of martensite of 3 μm or less, and an average grain size of retained austenite of 3 μm or less cannot be obtained. On the other hand, when the average coiling temperature after the hot rolling is below 300° C., there is an increase in the strength of the hot-rolled sheet and in the rolling load for cold rolling, and the steel sheet suffers malformation. As a result, productivity decreases. Therefore, the average coiling temperature after the hot rolling needs to be 300° C. or higher and 750° C. or lower. The average coiling temperature is preferably 400° C. or higher. The average coiling temperature is preferably 650° C. or lower.

According to the disclosure, finish rolling may be performed continuously by joining rough-rolled sheets during the hot rolling. Rough-rolled sheets may be coiled on a temporary basis. At least part of finish rolling may be conducted as lubrication rolling to reduce the rolling load during the hot rolling. Conducting lubrication rolling in such a manner is effective from the perspective of making the shape and material properties of the steel sheet uniform. In lubrication rolling, the coefficient of friction is preferably 0.10 or more. The coefficient of friction is preferably 0.25 or less.

The hot-rolled sheet thus produced is subjected to pickling. Pickling enables removal of oxides from the steel sheet surface, and is thus important to ensure that the high-strength steel sheet as the final product has good chemical convertibility and sufficient coating quality. The pickling may be performed in one or more batches.

Hot Band Annealing (First Heat Treatment): to Retain in a Temperature Range of [Ac1 Transformation Temperature+20° C.] to [Ac1 Transformation Temperature+120° C.] for 600 s to 21,600 s

In this disclosure, it is very important to retain the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s.

If the hot band annealing is performed at an annealing temperature below [Ac1 transformation temperature+20° C.] or above [Ac1 transformation temperature+120° C], or if the holding time is shorter than 600 s, concentration of Mn in austenite does not proceed in either case, making it difficult to ensure a sufficient volume fraction of retained austenite after the final annealing. As a result, ductility decreases. Besides, a microstructure in which the value obtained by dividing the Mn content in retained austenite (in mass %) by the Mn content in polygonal ferrite (in mass %) equals 2.0 or more cannot be obtained. On the other hand, if the steel sheet is retained for more than 21,600 s, concentration of Mn in austenite reaches a plateau, and becomes less effective in improving ductility after the final annealing, resulting in a rise in costs.

Therefore, in the hot band annealing (first heat treatment) according to the disclosure, the steel sheet is retained in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s.

The above-described heat treatment process may be continuous annealing or batch annealing. After the above-described heat treatment, the steel sheet is cooled to room temperature. The cooling process and cooling rate are not particularly limited, however, and any type of cooling may be performed, including furnace cooling and air cooling in batch annealing and gas jet cooling, mist cooling, and water cooling in continuous annealing. The pickling may be performed according to a conventional process.

Annealing (Second Heat Treatment): to Retain in a Temperature Range of [Ac1 Transformation Temperature+10° C.] to [Ac1 Transformation Temperature+100° C.] for 20 s to 900 s

In this disclosure, it is very important to retain the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s. When the annealing temperature is below [Ac1 transformation temperature+10° C.] or above [Ac1 transformation temperature+100° C], or if the holding time is shorter than 20 s, concentration of Mn in austenite does not proceed in either case, making it difficult to ensure a sufficient volume fraction of retained austenite. As a result, ductility decreases. Besides, a microstructure in which the value obtained by dividing the Mn content in retained austenite (in mass %) by the Mn content in polygonal ferrite (in mass %) equals 2.0 or more cannot be obtained. On the other hand, if the steel sheet is retained for more than 900 s, the area ratio of non-crystallized ferrite decreases and the interfaces between different phases, namely, between ferrite and hard secondary phases (martensite and retained austenite), are reduced, leading to a reduction in both YP and YR. Besides, a microstructure with an average grain size of martensite of 3μm or less and an average grain size of retained austenite of 3 μm or less cannot be obtained.

Rolling Reduction in Cold Rolling: Less than 30%

Cold rolling may be performed after the hot band annealing and before the annealing (second heat treatment). In this case, the rolling reduction needs to be less than 30%. By omitting the cold rolling or performing the cold rolling with a rolling reduction of less than 30%, polygonal ferrite which forms by recrystallization after the heat treatment does not form and a microstructure elongated in the rolling direction remains, and eventually polygonal ferrite, retained austenite, and martensite with a high aspect ratio are obtained. Thus, not only the strength-ductility balance is improved, but also the stretch flangeability (hole expansion formability) is improved. If the rolling reduction is 30% or more, a microstructure having 20% or more and 65% or less of polygonal ferrite in area ratio and a microstructure having an average aspect ratio of crystal grains of each of polygonal ferrite, martensite, and retained austenite of 2.0 or more and 15.0 or less cannot be obtained.

Hot-Dip Galvanizing Treatment

In hot-dip galvanizing treatment according to the disclosure, the steel sheet subjected to the above-described annealing (second heat treatment) is dipped in a galvanizing bath at 440° C. or higher and 500° C. or lower for hot-dip galvanizing. Subsequently, the coating weight on the steel sheet surface is adjusted using gas wiping or the like. Preferably, the hot-dip galvanizing is performed using a galvanizing bath containing 0.10 mass % or more and 0.22 mass % or less of Al.

Moreover, when a hot-dip galvanized layer is subjected to alloying treatment, the alloying treatment may be performed in a temperature range of 450° C. to 600° C. after the above-described hot-dip galvanizing treatment. If the alloying treatment is performed at a temperature above 600° C., untransformed austenite transforms to pearlite, where a desired volume fraction of retained austenite cannot be ensured and ductility degrades. On the other hand, if the alloying treatment is performed at a temperature below 450° C., the alloying process does not proceed, making it difficult to form an alloy layer.

Therefore, when the galvanized layer is subjected to alloying treatment, the alloying treatment is performed in a temperature range of 450° C. to 600° C.

Although other manufacturing conditions are not particularly limited, the series of processes including the annealing, hot-dip galvanizing, and alloying treatment described above may preferably be performed in a continuous galvanizing line (CGL), which is a hot-dip galvanizing line, from the perspective of productivity.

When hot-dip aluminum coating treatment is performed, the steel sheet subjected to the above-described annealing treatment is dipped in an aluminum molten bath at 660° C. to 730° C. for hot-dip aluminum coating treatment. Subsequently, the coating weight is adjusted using gas wiping or the like. If the steel sheet has a composition such that the temperature of the aluminum molten bath falls within the temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C], the steel sheet is preferably subjected to hot-dip aluminum coating treatment because finer and more stable retained austenite can be formed, and therefore further improvement in ductility can be achieved.

Electrogalvanizing treatment

According to the disclosure, electrogalvanizing treatment may also be performed on the steel sheet after the heat treatment. No particular limitations are placed on the electrogalvanizing treatment conditions, yet the electrogalvanizing treatment conditions are preferably set so that the plated layer has a thickness of 5 μm to 15 μm.

According to the disclosure, the above-described steel sheet, hot-dip galvanized steel sheet, hot-dip aluminum-coated steel sheet, and electrogalvanized steel sheet may be subjected to skin pass rolling for the purposes of straightening, adjustment of roughness on the sheet surface, and the like. The skin pass rolling is preferably performed at a rolling reduction of 0.1% or more. The skin pass rolling is preferably performed at a rolling reduction of 2.0% or less.

When the rolling reduction is less than 0.1%, the skin pass rolling becomes less effective and more difficult to control. Thus, a preferable range for the rolling reduction has a lower limit of 0.1%. On the other hand, when the skin pass rolling is performed at a rolling reduction above 2.0%, the productivity of the steel sheet decreases significantly. Thus, the preferable range for the rolling reduction has an upper limit of 2.0%.

The skin pass rolling may be performed on-line or off-line. Skin pass may be performed in one or more batches to achieve a target rolling reduction.

Moreover, the steel sheet, the hot-dip galvanized steel sheet, the hot-dip aluminum-coated steel sheet, and the electrogalvanized steel sheet according to the disclosure may be subjected to a variety of coating treatment options, such as those using coating of resin, fats and oils, and the like.

EXAMPLES

Steels having the chemical compositions as presented in Table 1, with the balance consisting of Fe and inevitable impurities, were prepared by steelmaking in a converter, and formed into slabs through continuous casting. The slabs thus obtained were formed into a variety of steel sheets, as described below, by varying the conditions as listed in Table 2.

After being hot rolled, each steel sheet was annealed in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C]. After being cold rolled (or without cold rolling), each steel sheet was annealed in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C]. Consequently, a cold-rolled steel sheet (CR) was obtained, and subjected to coating treatment to form a hot-dip galvanized steel sheet (GI), a galvannealed steel sheet (GA), a hot-dip aluminum-coated steel sheet (Al), an electrogalvanized steel sheet (EG), or the like.

Used as hot-dip galvanizing baths were a zinc bath containing 0.19 mass % of Al for hot-dip galvanized steel sheets (GI) and a zinc bath containing 0.14 mass % of Al for galvannealed steel sheets (GA). In either case, the bath temperature was 465° C. and the coating weight per side was 45 g/m2 (in the case of both-sided coating). For GA, the Fe concentration in the coating layer was adjusted to be 9 mass % or more and 12 mass % or less. The bath temperature of the hot-dip aluminum molten bath for hot-dip aluminum-coated steel sheets was set at 700° C.

For each of the steel sheets thus obtained, the cross-sectional microstructure, tensile property, hole expansion formability, bendability, and the like were investigated. The results are listed in Tables 3 to 5.

The Ac1 transformation temperature was calculated by:


[Ac1 transformation temperature (° C.)]=751−16*(% C)+11*(% Si)−28*(% Mn)−5.5*(% Cu)−16*(% Ni)+13*(% Cr)+3.4*(% Mo)

where (% C), (% Si), (% Mn), (% Ni), (% Cu), (% Cr), and (% Mo) each represent the content in steel (in mass %) of the element in the parentheses.

Tensile test was performed in accordance with JIS Z 2241 (2011) to measure YP, YR, TS, and EL using JIS No. 5 test pieces, each of which was sampled in a manner that the tensile direction was perpendicular to the rolling direction of the steel sheet. Note that YR is YP divided by TS, expressed as a percentage. In this case, the results were determined to be good when YR 68% and when TS * EL≥24,000 MPa·%. Also, EL was determined to be good when EL≥34% for TS 590 MPa grade, EL≥30% for TS 780 MPa grade, and EL≥24% for TS 980 MPa grade. In this case, a steel sheet of TS 590 MPa grade refers to a steel sheet with TS of 590 MPa or more and less than 780 MPa, a steel sheet of TS 780 MPa grade refers to a steel sheet with TS of 780 MPa or more and less than 980 MPa, and a steel sheet of TS 980 MPa grade refers to a steel sheet with TS of 980 MPa or more and less than 1180 MPa.

Bend test was performed according to the V-block method specified in JIS Z 2248 (1996). Each steel sheet was visually observed under a stereoscopic microscope for cracks on the outside of the bent portion, and the minimum bending radius without cracks was used as the limit bending radius R. In this case, the bendability of the steel sheet was determined to be good if the following condition was satisfied: limit bending radius R at 90° V-bending/t≤1.5 (where t is the thickness of the steel sheet).

Hole expansion test was performed in accordance with JIS Z 2256 (2010). Each of the steel sheets obtained was cut to a size of 100 mm * 100 mm, and a hole of 10 mm in diameter was drilled through each sample with clearance 12%±1%. Then, each steel sheet was clamped into a die having an inner diameter of 75 mm with a blank holding force of 9 tons (88.26 kN). In this state, a conical punch of 60° was pushed into the hole, and the hole diameter at the crack initiation limit was measured. Then, to evaluate hole expansion formability, the maximum hole expansion ratio (%) was calculated by:


Maximum hole expansion ratio λ(%)={(Df-D0)/D0}*100

where Df is a hole diameter at the time of occurrence of cracking (mm) and D0 is an initial hole diameter (mm).

In this case, the maximum hole expansion ratio was determined to be good when λ≥34% for TS 590 MPa grade, λ≥30% for TS 780 MPa grade, and λ≥25% for TS 980 MPa grade.

The sheet passage ability during hot rolling was determined to be low when it was considered that the risk of troubles, such as malformation during hot rolling due to increased rolling load, would increase because, for example, the hot-rolling finisher delivery temperature was low and rolling would be performed more often with austenite being in a non-crystallized state, or rolling would be performed in an austenite-ferrite dual phase region. The sheet passage ability during cold rolling was determined to be low when it was considered that the risk of troubles, such as malformation during cold rolling due to increased rolling load, would increase because, for example, the coiling temperature during hot rolling was low and the hot-rolled sheet had a steel microstructure in which low-temperature transformation phases, such as bainite and martensite, were dominantly present.

The surface characteristics of each final-annealed sheet were determined to be poor when defects such as blow hole generation and segregation on the surface layer of the slab could not be scaled-off, cracks and irregularities on the steel sheet surface increased, and a smooth steel sheet surface could not be obtained. The surface characteristics of each final-annealed sheet were also determined to be poor when the amount of oxides (scales) generated suddenly increased, interfaces between the steel substrate and oxides were roughened, and the surface quality after pickling and cold rolling degraded, or when hot-rolling scales persisted at least in part after pickling.

In this case, productivity was evaluated according to the lead time costs, including: (1) malformation of a hot-rolled sheet occurred; (2) a hot-rolled sheet requires straightening before proceeding to the subsequent steps; and (3) a prolonged holding time during the annealing treatment. The productivity was determined to be “high” when none of (1) to (3) applied and “low” when any of (1) to (3) applied.

Tensile working was performed in accordance with JIS Z 2241 (2011) using JIS No. 5 test pieces, each of which was sampled in a manner that the tensile direction was perpendicular to the rolling direction of the steel sheet. A value was obtained by dividing the volume fraction of retained austenite remaining in each steel sheet after subjection to tensile working with an elongation value of 10% by the volume fraction of retained austenite before the working (10% application). The volume fraction of retained austenite was measured in accordance with the above procedure.

The measurement results are also listed in Table 4.

The C content in the retained austenite (in mass %) and the Mn content in the retained austenite (in mass %) were measured in accordance with the above procedure.

The measurement results are also listed in Table 4.

TABLE 1 Chemical composition (mass %) Steel sample ID C Si Mn P S N Ti Al Nb B Ni Cr V Mo A 0.111 0.34 3.55 0.023 0.0022 0.0037 0.035 — — — — — — — B 0.156 0.65 3.91 0.028 0.0019 0.0035 0.038 — — — — — — — C 0.170 1.24 4.11 0.024 0.0023 0.0033 0.035 — — — — — — — D 0.070 1.25 3.51 0.027 0.0020 0.0031 0.033 — — — — — — — E 0.155 0.80 3.78 0.031 0.0019 0.0035 0.033 — — — — — — — F 0.141 0.05 3.80 0.021 0.0025 0.0032 0.015 — — — — — — — G 0.198 0.87 3.78 0.025 0.0020 0.0041 0.022 — — — — — — — H 0.166 0.74 2.87 0.025 0.0020 0.0034 0.035 — — — — — — — I 0.160 0.52 3.91 0.028 0.0025 0.0031 0.041 — — — — — — — IA 0.030 0.42 3.55 0.027 0.0021 0.0031 0.041 — — — — — — — IB 0.152 3.00 3.87 0.028 0.0020 0.0032 0.042 — — — — — — — IC 0.115 0.52 2.60 0.021 0.0021 0.0035 0.035 — — — — — — — ID 0.156 0.51 2.99 0.001 0.0019 0.0034 0.035 — — — — — — — IE 0.151 0.34 3.01 0.100 0.0021 0.0029 0.036 — — — — — — — IF 0.152 0.36 3.15 0.031 0.0001 0.0035 0.038 — — — — — — — IG 0.118 0.51 3.00 0.034 0.0200 0.0031 0.039 — — — — — — — IH 0.124 0.45 3.25 0.025 0.0022 0.0005 0.041 — — — — — — — II 0.147 0.48 3.45 0.031 0.0023 0.0100 0.041 — — — — — — — IJ 0.142 0.35 3.69 0.028 0.0018 0.0031 0.005 — — — — — — — IK 0.145 0.41 3.57 0.029 0.0025 0.0032 0.200 — — — — — — — IL 0.148 4.22 3.87 0.031 0.0025 0.0035 0.042 — — — — — — — IM 0.115 0.55 3.45 0.031 0.0019 0.0034 0.210 — — — — — — — J 0.010 0.52 3.21 0.031 0.0021 0.0031 0.039 — — — — — — — K 0.199 4.51 2.51 0.028 0.0025 0.0038 0.024 — — — — — — — L 0.186 1.01 2.25 0.025 0.0025 0.0034 0.025 — — — — — — — M 0.181 0.78 3.80 0.022 0.0021 0.0038 0.001 — — — — — — — N 0.205 0.89 3.51 0.024 0.0029 0.0038 0.033 0.45 — — — — — — O 0.200 1.02 3.78 0.028 0.0025 0.0034 0.033 — 0.042 — — — — — P 0.191 0.83 3.54 0.027 0.0024 0.0041 0.035 — — 0.0015 — — — — Q 0.210 1.01 3.57 0.029 0.0023 0.0032 0.021 — — — 0.312 — — — R 0.212 0.55 4.11 0.029 0.0022 0.0031 0.025 — — — — 0.355 — — S 0.225 0.78 3.76 0.031 0.0023 0.0032 0.023 — — — — — 0.035 — T 0.201 0.98 3.29 0.031 0.0022 0.0041 0.035 — — — — — — 0.329 U 0.202 1.32 3.12 0.025 0.0025 0.0033 0.041 — — — — — — — V 0.189 1.02 3.55 0.026 0.0029 0.0034 0.045 — — — — — — — W 0.190 0.88 3.45 0.025 0.0025 0.0035 0.033 — — — — — — — X 0.199 0.78 3.52 0.026 0.0025 0.0033 0.035 — 0.047 — — — — — Y 0.208 0.51 3.23 0.029 0.0027 0.0041 0.036 — 0.032 — — — — — Z 0.204 0.29 3.65 0.027 0.0019 0.0031 0.034 — 0.038 — — — — — AA 0.199 1.01 3.87 0.025 0.0025 0.0037 0.037 — — — — — — — AB 0.210 1.28 4.02 0.029 0.0029 0.0041 0.033 — — — — — — — AC 0.199 1.11 4.09 0.031 0.0021 0.0035 0.033 — — — — — — — AD 0.188 0.81 3.54 0.028 0.0020 0.0039 0.026 — — — — — — — Ac1 transformation Chemical composition (mass %) temperature Steel sample ID Cu Sn Sb Ta Ca Mg REM (° C.) Remarks A — — — — — — — 654 Conforming steel B — — — — — — — 646 Conforming steel C — — — — — — — 647 Conforming steel D — — — — — — — 665 Conforming steel E — — — — — — — 651 Conforming steel F — — — — — — — 643 Conforming steel G — — — — — — — 652 Conforming steel H — — — — — — — 676 Conforming steel I — — — — — — — 645 Conforming steel IA — — — — — — — 656 Conforming steel IB — — — — — — — 673 Conforming steel IC — — — — — — — 670 Conforming steel ID — — — — — — — 670 Conforming steel IE — — — — — — — 668 Conforming steel IF — — — — — — — 664 Conforming steel IG — — — — — — — 671 Conforming steel IH — — — — — — — 663 Conforming steel II — — — — — — — 657 Conforming steel IJ — — — — — — — 649 Conforming steel IK — — — — — — — 653 Conforming steel IL — — — — — — — 687 Comparative steel IM — — — — — — — 659 Comparative steel J — — — — — — — 667 Comparative steel K — — — — — — — 727 Comparative steel L — — — — — — — 696 Comparative steel M — — — — — — — 650 Comparative steel N — — — — — — — 659 Conforming steel O — — — — — — — 653 Conforming steel P — — — — — — — 658 Conforming steel Q — — — — — — — 654 Conforming steel R — — — — — — — 643 Conforming steel S — — — — — — — 651 Conforming steel T — — — — — — — 668 Conforming steel U 0.259 — — — — — — 674 Conforming steel V — 0.006 — — — — — 660 Conforming steel W — — — 0.005 — — — 661 Conforming steel X — — — — — — — 658 Conforming steel Y — — 0.007 — — — — 663 Conforming steel Z — — — 0.008 — — — 649 Conforming steel AA — — — — 0.0021 — — 651 Conforming steel AB — — — — — 0.0021 — 649 Conforming steel AC — — — — — — 0.0028 646 Conforming steel AD — — — — — — — 658 Conforming steel Underline: outside range according to present disclosure

TABLE 2 Finisher Average hot-rolled sheet heat treatment Steel Slab heating delivery coiling Heat treatment Heat treatment sample temperature temperature temperature temperature time No. ID (° C.) (° C.) (° C.) (° C.) (s) 1 A 1230 900 540 703 18000 2 B 1240 890 500 688 20000 3 C 1200 890 600 690 15000 4 C 1100 890 600 690 20000 5 C 1300 880 580 700 21000 6 C 1200 750 600 690 20000 7 C 1200 1000  680 710 18000 8 C 1150 880 300 690 19000 9 C 1180 870 750 690 20000 10 C 1180 870 600 670 19000 11 C 1190 860 550 760 18000 12 C 1200 850 600 690  600 13 C 1210 850 540 680 17000 14 C 1200 890 540 680 17000 15 C 1250 870 660 690 19000 16 C 1220 700 540 690 20000 17 C 1230 1100  490 690 10000 18 C 1240 860 850 690  7000 19 C 1250 870 510 500 16000 20 C 1240 880 490 850 17000 21 C 1250 890 570 690  300 22 C 1250 890 600 690 19000 23 C 1240 890 600 690 20000 24 C 1230 860 610 690 19000 25 C 1230 860 610 690  6000 26 C 1240 880 590 690  6000 27 C 1210 880 560 690 10000 28 C 1230 860 560 690 16000 29 C 1200 890 570 690 20000 30 D 1240 860 530 696 18000 31 E 1240 890 520 689  6000 32 F 1250 900 550 690 18000 33 G 1240 890 590 687  7000 34 H 1260 860 560 715  9000 35 I 1240 920 600 691 15000 36 IA 1250 890 600 700 15000 37 IB 1250 890 600 710 18000 38 IC 1240 890 560 750 18000 39 ID 1230 880 570 700 18000 40 IE 1250 890 580 710 19000 41 IF 1240 860 560 710 18000 42 IG 1230 860 560 710 18000 43 IH 1250 860 570 715 18000 44 II 1250 870 600 712 18000 45 IJ 1250 890 580 720 18000 46 IK 1230 880 580 690 18000 47 IL 1240 870 590 710 18000 48 IM 1250 870 570 710 18000 49 J 1220 860 630 717 17000 50 K 1210 870 620 764 20000 51 L 1240 840 570 729 19000 52 M 1250 830 540 688 5000 53 N 1260 850 580 684 6000 54 O 1270 870 540 695 15000 55 P 1220 900 520 695 18000 56 Q 1260 840 600 696 19000 57 R 1270 830 560 683 14000 58 S 1240 880 620 690 8000 59 T 1250 820 600 700 8000 60 U 1250 850 530 715 15000 61 V 1240 920 570 692 13000 62 W 1230 910 500 705 10000 63 X 1250 890 590 695 16000 64 Y 1260 900 520 702 9000 65 Z 1250 880 540 686 18000 66 AA 1260 900 520 686 9000 67 AB 1250 880 540 694 15000 68 AC 1260 860 530 686 6000 69 AD 1250 870 540 696 8000 70 B 1230 890 550 695 10000 71 B 1250 870 530 698 8000 Annealing treatment Rolling reduction Heat treatment Heat treatment in cold rolling temperature time No. (%) (° C.) (s) Type* Remarks 1 27.6 688 500 CR Example 2 27.6 673 300 CR Example 3 28.6 675 350 GA Example 4 28.6 680 500 CR Example 5 28.6 680 350 CR Example 6 22.2 675 350 CR Example 7 29.6 690 400 GA Example 8 28.6 675 400 GA Example 9 25.9 690 400 CR Example 10 25.9 700 350 CR Example 11 28.6 690 500 CR Example 12 25.0 680 500 GA Example 13 25.0 740 500 GA Example 14 22.2 680  20 GA Example 15 28.6 670 900 CR Example 16 28.6 675 250 CR Comparative Example 17 27.6 675 350 CR Comparative Example 18 29.6 675 800 CR Comparative Example 19 25.9 675 700 EG Comparative Example 20 25.0 675 500 CR Comparative Example 21 27.6 675 600 CR Comparative Example 22 10.3 675 550 CR Example 23  0.0 675 550 CR Example 24 57.5 675 650 CR Comparative Example 25 36.4 675 650 CR Comparative Example 26 28.6 520 750 CR Comparative Example 27 29.6 850 400 Al Comparative Example 28 28.6 675  2 CR Comparative Example 29 28.6 675 1500  CR Comparative Example 30 27.6 688 600 CR Example 31 27.6 674 700 GI Example 32 24.1 675 500 CR Example 33 25.0 672 550 Al Example 34 28.6 700 540 CR Example 35 28.6 676 290 GA Example 36 28.6 680 650 GA Example 37 28.6 690 650 CR Example 38 28.6 710 550 CR Example 39 28.6 700 600 CR Example 40 28.6 700 600 GA Example 41 28.6 690 600 GA Example 42 28.6 690 650 CR Example 43 28.6 690 650 CR Example 44 28.6 680 600 CR Example 45 28.6 690 550 CR Example 46 28.6 710 580 GA Example 47 28.6 710 600 GA Comparative Example 48 28.6 680 600 GA Comparative Example 49 25.9 702 300 GI Comparative Example 50 29.6 749 200 EG Comparative Example 51 29.6 714 280 CR Comparative Example 52 28.6 673 360 EG Comparative Example 53 21.4 669 370 GI Example 54 28.6 680 400 CR Example 55 28.6 680 300 GA Example 56 27.6 681 320 CR Example 57 28.6 668 300 EG Example 58 27.6 675 300 Al Example 59 29.6 685 200 GI Example 60 29.6 700 250 GI Example 61 28.6 677 280 GI Example 62 27.6 690 250 EG Example 63 22.2 680 300 Al Example 64 25.0 687 340 GA Example 65 28.6 671 600 G1 Example 66 29.6 671 500 Al Example 67 29.6 679 500 CR Example 68 29.6 671 350 CR Example 69 28.6 692 400 CR Example 70 25.9 657 200 CR Example 71 28.6 658 180 CR Example Underline: outside range according to present disclosure *CR: cold-rolled steel sheet (no coating), GI: hot-dip galvanized steel sheet (no galvannealing), GA: galvannealed steel sheet Al: hot-dip aluminum-coated steel sheet, EG: electrogalvanized steel sheet

TABLE 3 Rolling Volume Average Steel reduction in Area ratio Area ratio Area ratio fraction of grain size Aspect ratio of sample cold rolling of F of F′ of M RA (μm) crystal grains No. ID (%) (%) (%) (%) (%) F M RA F M RA Balance Remarks 1 A 27.6 64.9 8.0  6.3 13.1 4.9 2.6 2.4 4.3 3.5 4.2 BF, P, θ Example 2 B 27.6 55.2 9.2 10.6 19.2 4.3 1.7 1.8 4.5 4.0 4.3 BF, P, θ Example 3 C 28.6 42.5 16.9  13.5 24.6 3.2 1.0 1.1 4.4 4.1 4.3 BF, P, θ Example 4 C 28.6 45.1 8.5 13.5 22.5 4.2 2.1 1.2 4.5 4.1 4.2 BF, P, θ Example 5 C 28.6 42.1 9.2 12.6 23.4 4.1 2.0 1.1 4.8 4.0 4.3 BF, P, θ Example 6 C 22.2 42.5 10.2  15.4 22.1 3.2 1.9 1.3 4.5 4.1 4.3 BF, P, θ Example 7 C 29.6 43.1 9.8 12.5 20.6 3.0 1.8 2.1 4.4 4.2 4.2 BF, P, θ Example 8 C 28.6 42.5 9.1 14.1 25.1 3.5 1.3 2.2 5.1 4.5 4.3 BF, P, θ Example 9 C 25.9 41.6 9.1 13.8 22.6 3.6 1.5 2.5 4.8 4.2 4.1 BF, P, θ Example 10 C 25.9 38.1 10.1  12.8 22.4 3.8 2.0 1.2 4.5 4.1 4.1 BF, P, θ Example 11 C 28.6 50.6 11.2  14.1 23.5 5.0 2.1 1.3 4.5 4.2 4.2 BF, P, θ Example 12 C 25.0 32.1 17.2  17.8 24.8 4.5 2.3 1.5 4.7 4.0 4.2 BF, P, θ Example 13 C 25.0 46.9 12.1  12.9 25.1 3.9 1.5 1.5 4.8 4.0 4.3 BF, P, θ Example 14 C 22.2 41.0 11.2  14.1 22.6 5.0 1.9 1.6 4.7 4.1 4.4 BF, P, θ Example 15 C 28.6 42.6 12.5  16.5 23.9 4.1 2.1 1.4 4.8 4.1 4.1 BF, P, θ Example 16 C 28.6 55.2 10.2  12.8  7.1 3.9 1.5 1.6 4.4 4.2 4.5 BF, P, θ Comparative Example 17 C 27.6 60.8 10.8  13.4  7.4 4.1 1.8 1.4 3.5 4.0 4.2 BF, P, θ Comparative Example 18 C 29.6 55.9 10.3  12.5 18.6 7.8 4.2 4.1 5.5 4.1 4.5 BF, P, θ Comparative Example 19 C 25.9 59.1 10.4  15.4  6.4 5.4 1.8 1.7 4.4 4.3 4.4 BF, P, θ Comparative Example 20 C 25.0 59.3 12.1  16.8  6.9 5.2 1.5 1.4 4.6 4.4 4.1 BF, P, θ Comparative Example 21 C 27.6 50.2 11.4  14.9  6.2 5.1 1.6 1.5 4.7  4.4. 4.3 BF, P, θ Comparative Example 22 C 10.3 40.1 9.3 10.4 18.5 4.2 2.1 2.0 5.8 4.8 4.1 BF, P, θ Example 23 C  0.0 45.3 9.3 10.4 18.5 4.2 2.1 2.0 8.1 4.2 4.1 BF, P, θ Example 24 C 57.5 70.0 10.8   8.0  8.0 6.5 2.7 2.9 1.4 1.4 1.5 BF, P, θ Comparative Example 25 C 36.4 65.5 10.8   8.5  8.1 5.1 2.7 2.9 1.9 1.8 1.9 BF, P, θ Comparative Example 26 C 28.6 55.8 10.4  18.1  6.2 4.5 2.3 2.1 3.8 4.2 4.3 BF, P, θ Comparative Example 27 C 29.6 53.8 10.9  17.1  6.5 4.6 2.1 2.4 4.2 4.5 4.6 BF, P, θ Comparative Example 28 C 28.6 54.2 11.2  18.5  6.3 4.2 2.3 2.2 3.9 4.0 4.7 BF, P, θ Comparative Example 29 C 28.6 58.2 1.2  8.4 23.4 5.6 4.1 3.9 4.1 3.8 4.1 BF, P, θ Comparative Example 30 D 27.6 50.1 9.8 10.4 18.4 4.2 1.8 1.8 4.2 4.2 5.0 BF, P, θ Example 31 E 27.6 52.1 10.1  10.6 16.8 4.1 1.5 1.9 4.5 4.4 4.2 BF, P, θ Example 32 F 24.1 50.1 9.8 10.9 19.2 3.9 1.9 1.8 4.5 4.7 4.4 BF, P, θ Example 33 G 25.0 64.5 8.1  8.5 12.8 5.1 2.7 2.3 4.4 4.8 4.3 BF, P, θ Example 34 H 28.6 63.1 8.5  8.8 13.8 4.8 2.5 2.2 4.6 4.6 4.3 BF, P, θ Example 35 I 28.6 64.7 8.0  8.8 13.5 4.6 2.4 2.4 4.7 4.5 4.2 BF, P, θ Example 36 IA 28.6 64.8 8.5  8.5 12.6 5.1 2.5 1.8 4.5 4.5 4.2 BF, P, θ Example 37 IB 28.6 65.0 9.1  8.5 13.5 5.5 2.6 1.5 4.5 4.5 4.3 BF, P, θ Example 38 IC 28.6 64.8 8.1  8.9 14.0 5.1 2.4 2.2 4.4 4.6 4.1 BF, P, θ Example 39 ID 28.6 55.1 9.1 10.1 18.1 4.9 2.1 1.9 4.2 4.2 4.2 BF, P, θ Example 40 IE 28.6 52.0 9.2 10.2 15.6 4.6 2.2 2.0 4.4 4.1 4.3 BF, P, θ Example 41 IF 28.6 54.0 9.8 10.1 15.7 4.2 2.3 2.1 4.2 4.6 4.2 BF, P, θ Example 42 IG 28.6 53.1 8.7 10.2 16.8 4.5 2.1 2.2 4.5 4.3 4.1 BF, P, θ Example 43 IH 28.6 59.1 10.1  10.5 17.2 5.1 2.5 1.9 4.1 4.2 4.4 BF, P, θ Example 44 II 28.6 60.1 8.9 10.5 18.1 4.9 2.4 1.5 4.5 4.1 4.1 BF, P, θ Example 45 IJ 28.6 58.1 9.5 10.9 15.4 4.6 2.5 1.8 4.7 4.2 4.5 BF, P, θ Example 46 IK 28.6 61.2 8.5 11.1 16.9 4.5 2.4 1.5 4.6 4.1 4.3 BF, P, θ Example 47 IL 28.6 66.1 8.0 10.5 10.2 5.6 2.0 1.9 4.1 4.1 4.1 BF, P, θ Comparative Example 48 IM 28.6 63.5 12.5  14.5  9.0 4.0 2.1 2.1 4.5 4.5 4.2 BF, P, θ Comparative Example 49 J 25.9 65.0 8.9  3.8  3.6 7.4 0.6 0.5 4.3 4.4 4.2 BF, P, θ Comparative Example 50 K 29.6 50.4 18.4  15.4  6.8 5.4 3.9 3.8 4.4 4.1 4.1 BF, P, θ Comparative Example 51 L 29.6 60.3 13.2  15.9  6.2 5.8 4.5 3.9 4.4 4.1 4.1 BF, P, θ Comparative Example 52 M 28.6 50.3 2.2 11.4 13.2 7.1 4.1 4.0 4.2 4.1 3.9 BF, P, θ Comparative Example 53 N 21.4 55.1 10.4  11.4 18.4 4.2 1.6 1.9 4.3 4.2 4.1 BF, P, θ Example 54 O 28.6 54.2 10.5   9.8 17.4 4.3 1.7 1.4 4.2 4.3 4.2 BF, P, θ Example 55 P 28.6 55.7 10.1  10.5 19.5 4.1 1.4 1.5 3.9 4.3 4.6 BF, P, θ Example 56 Q 27.6 56.1 10.3  10.8 19.6 4.3 1.7 1.6 4.0 4.2 4.3 BF, P, θ Example 57 R 28.6 65.0 8.2  7.5 12.8 5.1 2.5 2.3 3.9 4.1 4.5 BF, P, θ Example 58 S 27.6 64.8 8.1  8.2 12.4 4.8 2.4 2.1 4.3 4.2 4.3 BF, P, θ Example 59 T 29.6 60.9 8.0  7.2 14.2 4.6 2.3 2.1 4.2 4.5 4.4 BF, P, θ Example 60 U 29.6 63.9 8.1  7.6 13.5 4.5 2.4 2.5 4.4 4.2 4.5 BF, P, θ Example 61 V 28.6 65.0 8.7  7.5 12.9 4.8 2.1 2.4 4.0 4.1 4.7 BF, P, θ Example 62 W 27.6 64.9 8.0  6.8 13.2 4.7 2.3 2.1 3.9 3.9 4.1 BF, P, θ Example 63 X 22.2 50.7 10.4  10.2 18.4 4.1 1.6 1.7 3.7 3.1 4.2 BF, P, θ Example 64 Y 25.0 62.8 10.5  10.6 15.0 4.5 1.7 1.8 3.9 4.2 4.4 BF, P, θ Example 65 Z 28.6 55.5 9.8  9.8 20.1 4.2 1.8 1.6 4.2 4.2 4.3 BF, P, θ Example 66 AA 29.6 50.8 10.6  10.6 19.4 3.9 1.9 1.5 4.1 4.1 4.2 BF, P, θ Example 67 AB 29.6 52.1 10.1   9.6 18.4 4.1 1.7 1.5 4.2 4.5 4.6 BF, P, θ Example 68 AC 29.6 52.9 9.9 10.3 18.2 4.2 1.6 1.8 4.4 4.5 4.7 BF, P, θ Example 69 AD 28.6 51.2 11.1  12.1 19.6 3.9 1.4 1.6 4.3 4.3 4.1 BF, P, θ Example 70 B 25.9 48.0 10.1  11.2 18.4 4.5 1.9 1.7 4.1 4.2 4.2 BF, P, θ Example 71 B 28.6 50.5 10.5  10.8 19.1 4.6 1.8 1.8 3.9 4.4 4.4 BF, P, θ Example Underline: outside range according to present disclosure F: polygonal ferrite, F′: non-recrystallized ferrite, BF: bainitic ferrite, RA: retained austenite, M: martensite, P: pearlite, θ: carbide (such as cementite)

TABLE 4 Value obtained by dividing RA remaining volume Average fraction after Mn content 0.09 × (Mn 0.09 × (Mn 10% tensile Average Average in RA/ content in content in working by Steel Mn content Mn content Average RA) − 0.026 − RA) − 0.026 + C content RA volume sample in RA in F Mn content 0.150 0.150 in RA fraction before No. ID (mass %) (mass %) in F (mass %) (mass %) (mass %) working Remarks 1 A 6.89 2.84 2.43 0.444 0.744 0.63 0.77 Example 2 B 7.68 3.02 2.54 0.515 0.815 0.71 0.81 Example 3 C 8.22 3.08 2.67 0.564 0.864 0.75 0.68 Example 4 C 7.88 2.87 2.75 0.533 0.833 0.75 0.65 Example 5 C 8.02 2.88 2.78 0.546 0.846 0.75 0.68 Example 6 C 7.55 3.01 2.51 0.504 0.804 0.78 0.74 Example 7 C 8.01 3.01 2.66 0.545 0.845 0.68 0.74 Example 8 C 7.89 3.05 2.59 0.534 0.834 0.74 0.65 Example 9 C 7.99 2.98 2.68 0.543 0.843 0.78 0.68 Example 10 C 7.75 2.99 2.59 0.522 0.822 0.75 0.71 Example 11 C 7.98 3.01 2.65 0.542 0.842 0.75 0.64 Example 12 C 5.87 2.89 2.03 0.352 0.652 0.62 0.51 Example 13 C 7.89 2.89 2.73 0.534 0.834 0.76 0.71 Example 14 C 7.99 3.05 2.62 0.543 0.843 0.74 0.72 Example 15 C 7.84 3.01 2.60 0.530 0.830 0.76 0.74 Example 16 C 7.45 2.79 2.67 0.495 0.795 0.43 0.25 Comparative Example 17 C 7.35 2.89 2.54 0.486 0.786 0.65 0.42 Comparative Example 18 C 6.89 2.97 2.32 0.444 0.744 0.63 0.51 Comparative Example 19 C 5.41 3.57 1.52 0.311 0.611 0.50 0.39 Comparative Example 20 C 5.32 3.67 1.45 0.303 0.603 0.49 0.52 Comparative Example 21 C 5.26 3.68 1.43 0.297 0.597 0.49 0.44 Comparative Example 22 C 7.48 2.99 2.50 0.497 0.797 0.69 0.69 Example 23 C 7.48 2.99 2.50 0.497 0.797 0.69 0.69 Example 24 C 7.55 2.75 2.75 0.504 0.804 0.79 0.19 Comparative Example 25 C 7.32 2.75 2.66 0.483 0.783 0.79 0.19 Comparative Example 26 C 5.67 3.64 1.56 0.334 0.634 0.29 0.22 Comparative Example 27 C 5.54 3.75 1.48 0.323 0.623 0.46 0.46 Comparative Example 28 C 5.28 3.87 1.36 0.299 0.599 0.49 0.53 Comparative Example 29 C 8.26 2.67 3.09 0.567 0.867 0.76 0.39 Comparative Example 30 D 7.54 2.89 2.61 0.503 0.803 0.69 0.71 Example 31 E 7.32 2.78 2.63 0.483 0.783 0.62 0.75 Example 32 F 7.84 2.97 2.64 0.530 0.830 0.72 0.64 Example 33 G 6.95 2.85 2.44 0.450 0.750 0.62 0.69 Example 34 H 7.08 2.76 2.57 0.461 0.761 0.63 0.70 Example 35 I 6.85 2.66 2.58 0.441 0.741 0.61 0.74 Example 36 IA 7.55 3.15 2.40 0.504 0.804 0.55 0.48 Example 37 IB 7.15 2.58 2.77 0.468 0.768 0.52 0.55 Example 38 IC 4.51 1.55 2.91 0.230 0.530 0.51 0.38 Example 39 ID 6.95 3.15 2.21 0.450 0.750 0.61 0.68 Example 40 IE 7.10 3.21 2.21 0.463 0.763 0.58 0.70 Example 41 IF 6.88 3.01 2.29 0.443 0.743 0.58 0.74 Example 42 IG 7.15 3.21 2.23 0.468 0.768 0.61 0.74 Example 43 IH 6.99 2.89 2.42 0.453 0.753 0.62 0.75 Example 44 II 7.15 2.97 2.41 0.468 0.768 0.65 0.76 Example 45 IJ 7.10 2.88 2.47 0.463 0.763 0.58 0.81 Example 46 IK 7.02 2.78 2.53 0.456 0.756 0.58 0.56 Example 47 IL 6.87 3.10 2.22 0.442 0.742 0.55 0.25 Comparative Example 48 IM 6.55 3.15 2.08 0.414 0.714 0.35 0.21 Comparative Example 49 J 6.45 2.79 2.31 0.405 0.705 0.38 0.24 Comparative Example 50 K 7.29 2.87 2.54 0.480 0.780 0.67 0.52 Comparative Example 51 L 3.40 2.08 1.63 0.130 0.430 0.30 0.43 Comparative Example 52 M 7.28 2.89 2.52 0.479 0.779 0.65 0.46 Comparative Example 53 N 7.59 2.98 2.55 0.507 0.807 0.70 0.62 Example 54 O 7.64 2.85 2.68 0.512 0.812 0.65 0.68 Example 55 P 7.49 2.89 2.59 0.498 0.798 0.69 0.74 Example 56 Q 7.39 2.98 2.48 0.489 0.789 0.63 0.84 Example 57 R 6.58 2.75 2.39 0.416 0.716 0.59 0.86 Example 58 S 6.87 2.81 2.44 0.442 0.742 0.58 0.81 Example 59 T 6.89 2.74 2.51 0.444 0.744 0.63 0.75 Example 60 U 6.99 2.65 2.64 0.453 0.753 0.61 0.78 Example 61 V 6.48 2.71 2.39 0.407 0.707 0.55 0.74 Example 62 W 6.78 2.68 2.53 0.434 0.734 0.59 0.76 Example 63 X 7.85 2.89 2.72 0.531 0.831 0.69 0.79 Example 64 Y 7.46 2.79 2.67 0.495 0.795 0.66 0.83 Example 65 Z 7.59 2.68 2.83 0.507 0.807 0.68 0.74 Example 66 AA 7.36 2.89 2.55 0.486 0.786 0.63 0.78 Example 67 AB 7.56 2.78 2.72 0.504 0.804 0.67 0.77 Example 68 AC 7.54 2.79 2.70 0.503 0.803 0.64 0.68 Example 69 AD 7.94 2.91 2.73 0.539 0.839 0.70 0.72 Example 70 B 7.24 3.24 2.23 0.476 0.776 0.45 0.29 Example 71 B 7.18 3.28 2.19 0.470 0.770 0.46 0.28 Example Underline: outside range according to present disclosure F: polygonal ferrite, F′: non-recrystallized ferrite, BF: bainitic ferrite, RA: retained austenite, M: martensite, P: pearlite, θ: carbide (such as cementite)

TABLE 5 Steel Sheet Sheet passage Sheet passage Surface sample thickness ability during ability during characteristics of No. ID (mm) hot rolling cold rolling final-annealed sheet Productivity 1 A 2.1 Good Good Good Good 2 B 2.1 Good Good Good Good 3 C 2.0 Good Good Good Good 4 C 2.0 Good Good Good Good 5 C 2.0 Good Good Good Good 6 C 2.1 Good Good Good Good 7 C 1.9 Good Good Good Good 8 C 2.0 Good Good Good Good 9 C 2.0 Good Good Good Good 10 C 2.0 Good Good Good Good 11 C 2.0 Good Good Good Good 12 C 2.1 Good Good Good Good 13 C 2.1 Good Good Good Good 14 C 2.1 Good Good Good Good 15 C 2.0 Good Good Good Good 16 C 2.0 Poor Poor Poor Poor 17 C 2.1 Good Poor Poor Poor 18 C 1.9 Good Good Good Good 19 C 2.0 Good Poor Good Good 20 C 2.1 Good Good Good Good 21 C 2.1 Good Poor Good Good 22 C 2.6 Good Good Good Good 23 C 2.8 Good Good Good Good 24 C 1.7 Good Good Good Good 25 C 2.1 Good Good Good Good 26 C 2.0 Good Good Good Good 27 C 1.9 Good Good Good Poor 28 C 2.0 Good Good Good Good 29 C 2.0 Good Good Good Good 30 D 2.1 Good Good Good Good 31 E 2.1 Good Good Good Good 32 F 2.2 Good Good Good Good 33 G 2.1 Good Good Good Good 34 H 2.0 Good Good Good Good 35 I 2.0 Good Good Good Good 36 IA 2.0 Good Good Good Good 37 IB 2.0 Good Good Good Good 38 IC 2.0 Good Good Good Good 39 ID 2.0 Good Good Good Good 40 IE 2.0 Good Good Good Good 41 IF 2.0 Good Good Good Good 42 IG 2.0 Good Good Good Good 43 IH 2.0 Good Good Good Good 44 II 2.0 Good Good Good Good 45 IJ 2.0 Good Good Good Good 46 IK 2.0 Good Good Good Good 47 IL 2.0 Good Good Good Good 48 IM 2.0 Good Good Good Good 49 J 2.0 Good Good Good Good 50 K 1.9 Good Good Poor Good 51 L 1.9 Good Good Good Good 52 M 2.0 Good Good Good Good 53 N 2.2 Good Good Good Good 54 O 2.0 Good Good Good Good 55 P 2.0 Good Good Good Good 56 Q 2.1 Good Good Good Good 57 R 2.0 Good Good Good Good 58 S 2.1 Good Good Good Good 59 T 1.9 Good Good Good Good 60 U 1.9 Good Good Good Good 61 V 2.0 Good Good Good Good 62 W 2.1 Good Good Good Good 63 X 2.1 Good Good Good Good 64 Y 2.1 Good Good Good Good 65 Z 2.0 Good Good Good Good 66 AA 1.9 Good Good Good Good 67 AB 1.9 Good Good Good Good 68 AC 1.9 Good Good Good Good 69 AD 2.0 Good Good Good Good 70 B 2.0 Good Good Good Good 71 B 2.0 Good Good Good Good YP YR TS EL TS × EL λ No. (MPa) (%) (MPa) (%) (MPa · %) R/t (%) Remarks 1 515 79.2 650 38.2 24830 0.1 61 Example 2 691 85.1 812 35.1 28501 0.2 52 Example 3 996 97.8 1018 31.4 31965 0.5 40 Example 4 990 97.9 1011 32.0 32352 0.5 49 Example 5 950 96.4 985 31.5 31028 0.5 52 Example 6 950 96.5 984 31.4 30898 0.5 51 Example 7 960 95.8 1002 35.1 35170 0.5 52 Example 8 950 96.3 987 32.6 32176 0.5 51 Example 9 940 94.9 990 35.1 34749 0.5 49 Example 10 950 94.1 1010 33.1 33431 0.5 52 Example 11 950 94.8 1002 31.2 31262 0.5 55 Example 12 980 97.5 1005 31.8 31959 0.5 56 Example 13 900 91.5 984 31.5 30996 0.5 52 Example 14 910 91.9 990 31.4 31086 0.5 51 Example 15 950 95.0 1000 32.1 32100 0.5 51 Example 16 695 82.7 840 21.9 18396 1.5 25 Comparative Example 17 689 83.5 825 22.4 18480 1.4 30 Comparative Example 18 501 91.3 549 28.4 15592 1.1 28 Comparative Example 19 699 82.8 844 22.5 18990 0.5 44 Comparative Example 20 691 80.3 861 23.5 20234 0.5 43 Comparative Example 21 663 80.9 820 23.7 19434 0.5 42 Comparative Example 22 653 76.8 850 35.9 30515 0.6 56 Example 23 649 76.7 846 35.9 30371 0.5 56 Example 24 659 79.4 830 21.6 17928 1.9 22 Comparative Example 25 654 79.7 821 21.6 17734 1.5 22 Comparative Example 26 697 80.1 870 21.5 18705 0.5 31 Comparative Example 27 705 82.0 860 20.6 17716 0.5 41 Comparative Example 28 694 79.0 878 20.9 18350 0.5 40 Comparative Example 29 488 58.8 830 36.2 30046 1.3 25 Comparative Example 30 693 84.0 825 34.9 28793 0.2 41 Example 31 661 77.6 852 32.8 27946 0.4 45 Example 32 702 82.8 848 35.1 29765 0.2 46 Example 33 518 79.7 650 37.8 24570 0.1 59 Example 34 512 81.4 629 38.6 24279 0.1 65 Example 35 519 82.6 628 38.9 24429 0.1 65 Example 36 510 85.7 595 41.0 24395 0.5 60 Example 37 610 93.8 650 38.0 24700 0.5 62 Example 38 550 92.0 598 42.0 25116 0.5 58 Example 39 600 91.9 653 38.0 24814 0.5 55 Example 40 580 93.1 623 40.2 25045 0.5 56 Example 41 560 88.9 630 39.1 24633 0.5 60 Example 42 550 88.3 623 38.6 24048 0.5 55 Example 43 510 85.4 597 42.5 25373 0.5 52 Example 44 560 82.4 680 35.8 24344 0.5 55 Example 45 560 86.2 650 39.7 25805 0.5 50 Example 46 650 82.5 788 32.1 25295 0.5 56 Example 47 660 84.0 786 30.1 23659 0.5 55 Comparative Example 48 660 83.7 789 21.4 16885 0.5 53 Comparative Example 49 330 60.6 545 31.9 17386 0.1 63 Comparative Example 50 905 75.7 1195 15.8 18881 1.3 12 Comparative Example 51 631 76.0 830 20.8 17264 0.8 37 Comparative Example 52 499 59.1 845 28.9 24421 1.0 15 Comparative Example 53 674 81.2 830 36.4 30212 0.2 40 Example 54 661 77.7 851 35.8 30466 0.3 45 Example 55 709 87.5 810 35.9 29079 0.4 51 Example 56 710 89.0 798 36.4 29047 0.2 48 Example 57 505 80.8 625 39.4 24625 0.1 53 Example 58 531 83.0 640 39.5 25280 0.1 58 Example 59 501 83.4 601 41.2 24761 0.1 55 Example 60 534 78.1 684 37.5 25650 0.1 65 Example 61 550 83.5 659 36.9 24317 0.1 55 Example 62 545 82.1 664 36.7 24369 0.1 59 Example 63 726 83.5 869 34.8 30241 0.2 48 Example 64 709 82.5 859 35.1 30151 0.4 45 Example 65 710 85.5 830 36.4 30212 0.3 50 Example 66 678 82.6 821 36.9 30295 0.4 47 Example 67 661 81.1 815 34.8 28362 0.3 53 Example 68 702 84.9 827 35.2 29110 0.3 44 Example 69 785 79.2 991 32.6 32307 0.3 42 Example 70 591 74.6 792 31.5 24948 0.5 40 Example 71 598 75.3 794 30.8 24455 0.5 41 Example

From above, it can be seen that the steel sheets according to the disclosure each exhibited TS of 590 MPa or more and YR of 68% or more, and are thus considered as high-strength steel sheets having excellent formability and high yield ratio and hole expansion formability. In contrast, the comparative examples are inferior in terms of at least one of YR, TS, EL, λ, or R/t.

INDUSTRIAL APPLICABILITY

According to the disclosure, it becomes possible to manufacture high-strength steel sheets with excellent formability and high yield ratio and hole expansion formability that exhibit TS of 590 MPa or more and YR of 68% or more and that satisfy the condition of TS * EL≥24,000 MPa·%. Steel sheets according to the disclosure are highly beneficial in industrial terms, because they can improve fuel efficiency when applied to, for example, automobile structural parts, by a reduction in the weight of automotive bodies.

Claims

1-6. (canceled)

7. A steel sheet comprising:

a chemical composition containing, in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisting of Fe and inevitable impurities; and
a steel microstructure that contains, in area ratio, 20% or more and 65% or less of polygonal ferrite, 8% or more of non-recrystallized ferrite, and 5% or more and 25% or less of martensite, and that contains, in volume fraction, 8% or more of retained austenite, where an average aspect ratio of crystal grains of each of the polygonal ferrite, the martensite, and the retained austenite is 2.0 or more and 15.0 or less,
wherein the polygonal ferrite has an average grain size of 6 μm or less, the martensite has an average grain size of 3 μm or less, the retained austenite has an average grain size of 3 μm or less, and a value obtained by dividing a Mn content in the retained austenite in mass % by a Mn content in the polygonal ferrite in mass % equals 2.0 or more.

8. The steel sheet according to claim 7, wherein the retained austenite has a C content that satisfies the following formula in relation to the Mn content in the retained austenite:

0.09*[Mn]−0.026−0.150≤[C]≤0.09*[Mn]−0.026+0.150
where [C] is the C content in the retained austenite in mass %, and [Mn] is the Mn content in the retained austenite in mass %.

9. A coated steel sheet comprising:

the steel sheet according to claim 7; and
one selected from a hot-dip galvanized layer, a galvannealed layer, a hot-dip aluminum-coated layer, and an electrogalvanized layer provided on the steel sheet.

10. A coated steel sheet comprising:

the steel sheet according to claim 8; and
one selected from a hot-dip galvanized layer, a galvannealed layer, a hot-dip aluminum-coated layer, and an electrogalvanized layer provided on the steel sheet.

11. A method for manufacturing the steel sheet according to claim 7, the method comprising:

(i) heating a steel slab having a chemical composition containing, in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisting of Fe and inevitable impurities;
(ii) hot rolling the steel slab with a finisher delivery temperature of 750° C. or higher and 1000° C. or lower to obtain a steel sheet;
(iii) coiling the steel sheet at 300° C. or higher and 750° C. or lower;
(iv) then subjecting the steel sheet to pickling to remove scales;
(v) retaining the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 S;
(vi) optionally cold rolling the steel sheet at a rolling reduction of less than 30%; and
(vii) then retaining the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s and subsequently cooling the steel sheet.

12. A method for manufacturing the steel sheet according to claim 8, the method comprising:

(i) heating a steel slab having a chemical composition containing, in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisting of Fe and inevitable impurities;
(ii) hot rolling the steel slab with a finisher delivery temperature of 750° C. or higher and 1000° C. or lower to obtain a steel sheet;
(iii) coiling the steel sheet at 300° C. or higher and 750° C. or lower;
(iv) then subjecting the steel sheet to pickling to remove scales;
(v) retaining the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s;
(vi) optionally cold rolling the steel sheet at a rolling reduction of less than 30%; and
(vii) then retaining the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s and subsequently cooling the steel sheet.

13. The method according to claim 11,

wherein a value obtained by dividing a volume fraction of the retained austenite after performing tensile working with an elongation value of 10% by a volume fraction of the retained austenite before the tensile working equals 0.3 or more.

14. The method according to claim 12,

wherein a value obtained by dividing a volume fraction of the retained austenite after performing tensile working with an elongation value of 10% by a volume fraction of the retained austenite before the tensile working equals 0.3 or more.

15. A method for manufacturing the coated steel sheet according to claim 9, comprising:

(i) heating a steel slab having a chemical composition containing, in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisting of Fe and inevitable impurities;
(ii) hot rolling the steel slab with a finisher delivery temperature of 750° C. or higher and 1000° C. or lower to obtain a steel sheet;
(iii) coiling the steel sheet at 300° C. or higher and 750° C. or lower;
(iv) then subjecting the steel sheet to pickling to remove scales;
(v) retaining the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s;
(vi) optionally cold rolling the steel sheet at a rolling reduction of less than 30%;
(vii) then retaining the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s and subsequently cooling the steel sheet; and
(viii) thereafter, either subjecting the steel sheet after cooling to one selected from hot-dip galvanizing treatment, hot-dip aluminum coating treatment, and electrogalvanizing treatment, or subjecting the steel sheet after cooling to hot-dip galvanizing treatment and then to alloying treatment at 450° C. or higher and 600° C. or lower.

16. A method for manufacturing the coated steel sheet according to claim 10, comprising:

(i) heating a steel slab having a chemical composition containing, in mass %, C: 0.030% or more and 0.250% or less, Si: 0.01% or more and 3.00% or less, Mn: 2.60% or more and 4.20% or less, P: 0.001% or more and 0.100% or less, S: 0.0200% or less, N: 0.0100% or less, and Ti: 0.005% or more and 0.200% or less, and optionally further containing, in mass %, at least one selected from the group consisting of Al: 0.01% or more and 2.00% or less, Nb: 0.005% or more and 0.200% or less, B: 0.0003% or more and 0.0050% or less, Ni: 0.005% or more and 1.000% or less, Cr: 0.005% or more and 1.000% or less, V: 0.005% or more and 0.500% or less, Mo: 0.005% or more and 1.000% or less, Cu: 0.005% or more and 1.000% or less, Sn: 0.002% or more and 0.200% or less, Sb: 0.002% or more and 0.200% or less, Ta: 0.001% or more and 0.010% or less, Ca: 0.0005% or more and 0.0050% or less, Mg: 0.0005% or more and 0.0050% or less, and REM: 0.0005% or more and 0.0050% or less, with the balance consisting of Fe and inevitable impurities;
(ii) hot rolling the steel slab with a finisher delivery temperature of 750° C. or higher and 1000° C. or lower to obtain a steel sheet;
(iii) coiling the steel sheet at 300° C. or higher and 750° C. or lower;
(iv) then subjecting the steel sheet to pickling to remove scales;
(v) retaining the steel sheet in a temperature range of [Ac1 transformation temperature+20° C.] to [Ac1 transformation temperature+120° C.] for 600 s to 21,600 s;
(vi) optionally cold rolling the steel sheet at a rolling reduction of less than 30%;
(vii) then retaining the steel sheet in a temperature range of [Ac1 transformation temperature+10° C.] to [Ac1 transformation temperature+100° C.] for 20 s to 900 s and subsequently cooling the steel sheet; and
(viii) thereafter, either subjecting the steel sheet after cooling to one selected from hot-dip galvanizing treatment, hot-dip aluminum coating treatment, and electrogalvanizing treatment, or subjecting the steel sheet after cooling to hot-dip galvanizing treatment and then to alloying treatment at 450° C. or higher and 600° C. or lower.
Patent History
Publication number: 20190276907
Type: Application
Filed: Mar 8, 2017
Publication Date: Sep 12, 2019
Applicant: JFE STEEL CORPORATION (Chiyoda-ku Tokyo)
Inventors: Takako YAMASHITA (Chiyoda-ku, Tokyo), Yoshiyasu KAWASAKI (Chiyoda-ku, Tokyo), Takashi KOBAYASHI (Chiyoda-ku, Tokyo), Masayasu UENO (Chiyoda-ku, Tokyo), Yasunobu NAGATAKI (Chiyoda-ku Tokyo)
Application Number: 16/090,883
Classifications
International Classification: C21D 8/02 (20060101); C22C 38/00 (20060101); C22C 38/06 (20060101); C22C 38/04 (20060101); C22C 38/02 (20060101); C22C 38/14 (20060101); C22C 38/12 (20060101); C22C 38/60 (20060101); C22C 38/08 (20060101); C22C 38/28 (20060101); C22C 38/38 (20060101); C22C 38/16 (20060101); C21D 9/46 (20060101); C23C 2/02 (20060101); C23C 2/06 (20060101); C23C 2/12 (20060101); C23C 2/28 (20060101); C23C 2/40 (20060101);