STEEL SHEET AND MANUFACTURING METHOD THEREFOR

21-01-2021 дата публикации
Номер:
US20210017620A1
Принадлежит: NIPPON STEEL CORPORATION
Контакты:
Номер заявки: 03-20-1698
Дата заявки: 30-03-2018

TECHNICAL FIELD OF THE INVENTION

[0001]

The present invention relates to a steel sheet and a method for manufacturing the same.

RELATED ART

[0002]

In recent years, awareness of environmental problems has increased. Therefore, in the automotive industry, it is important to reduce the weight of the vehicle body for the purpose of improving fuel efficiency. On the other hand, there is also a need to increase the vehicle body strength of a vehicle to secure collision safety. In order to achieve both a reduction in the weight of the vehicle body and collision safety, a high strength steel sheet may be used as the material of the vehicle body. However, the higher the strength of the steel sheet, the more difficult the press formability. This is because, in general, the higher the strength of the steel sheet, the lower the formability such as ductility, bendability, and hole expansibility.

[0003]

In the case of an ultrahigh-strength steel sheet having a tensile strength of more than 980 MPa, it is necessary to solve problems of not only the formability but also the hydrogen embrittlement cracking of the steel sheet. Hydrogen embrittlement cracking is a phenomenon in which a steel member, to which a high stress is applied in use, suddenly fractures due to hydrogen infiltrating into the steel from the environment. This phenomenon is also called delayed fracture because of the form of occurrence of fracture. It is generally known that hydrogen embrittlement cracking of a steel sheet is more likely to occur as the tensile strength of the steel sheet increases. It is considered that this is because the higher the tensile strength of the steel sheet, the greater the residual stress in the steel sheet after forming a component. The susceptibility to hydrogen embrittlement cracking (delayed fracture) is called hydrogen embrittlement resistance. In the case of steel sheets for vehicles, hydrogen embrittlement cracking is particularly likely to occur in a bent portion to which a large plastic strain is applied. Therefore, in a case where a high strength steel sheet is used for a vehicle member, there is a demand for the improvement in not only the formability such as ductility, bendability, and hole expansibility but also the hydrogen embrittlement resistance of the bent portion.

[0004]

In the related art, dual phase steel (DP steel) containing ferrite and martensite is known as a high strength steel sheet having high press formability (for example, refer to Patent Document 1). DP steel has excellent ductility. However, DP steel has a hard phase serving as the origin of void formation and is thus inferior in hole expansibility and bendability.

[0005]

In addition, as a high strength steel sheet having excellent ductility, there is TRIP steel that contains austenite remaining in the steel structure and utilizes a transformation-induced plasticity (TRIP) effect (for example, refer to Patent Documents 2 and 3). TRIP steel has a higher ductility than DP steel. However, TRIP steel is inferior in hole expansibility. In addition, TRIP steel needs to contain a large amount of alloys of Si and the like in order to retain austenite. Therefore, TRIP steel is inferior in plating adhesion and chemical convertibility.

[0006]

In addition, Patent Document 4 describes a high strength steel sheet having a microstructure containing bainite or bainitic ferrite in an area ratio of 70% or more and having a tensile strength of 800 MPa or more and excellent hole expansibility. Patent Document 5 describes a high strength steel sheet having a microstructure containing bainite or bainitic ferrite as the primary phase, austenite as the secondary phase, and ferrite or martensite as the remainder, and having a tensile strength of 800 MPa or more and excellent hole expansibility and ductility.

[0007]

Furthermore, Non-Patent Document 1 discloses that the elongation and hole expansibility of a steel sheet are improved by using a double annealing method in which a steel sheet is subjected to double annealing.

[0008]

However, it has been difficult to simultaneously improve the ductility and hole expansibility of a high strength steel sheet in the related art, and the hydrogen embrittlement resistance of a bent portion.

PRIOR ART DOCUMENT

Patent Document

[0000]

  • [Patent Document 1] Japanese Unexamined Patent Application, First Publication No. H6-128688
  • [Patent Document 2] Japanese Unexamined Patent Application, First Publication No. 2006-274418
  • [Patent Document 3] Japanese Unexamined Patent Application, First Publication No. 2008-56993
  • [Patent Document 4] Japanese Unexamined Patent Application, First Publication No. 2003-193194
  • [Patent Document 5] Japanese Unexamined Patent Application, First Publication No. 2003-193193

Non-Patent Document

[0000]

  • [Non-Patent Document 1] K. Sugimoto et al., ISIJ International, Vol. 33 (1993), No. 7, pp. 775-782

DISCLOSURE OF THE INVENTION

Problems to be Solved by the Invention

[0015]

The present invention has been made in view of the above circumstances. An object of the present invention is to provide a high strength steel sheet excellent in formability, fatigue properties, and hydrogen embrittlement resistance of a bent portion, and a method for manufacturing the same.

Means for Solving the Problem

[0016]

The present inventors conducted extensive studies in order to solve the above problems. As a result, it was found that by subjecting a hot-rolled steel sheet or a cold-rolled steel sheet having a predetermined chemical composition to two heat treatments (annealing) under different conditions, it is effective to cause the inside of the steel sheet to have a predetermined steel structure, and to form a surface layer having a predetermined thickness and a steel structure.

[0017]

It was also found that by forming an internal oxide layer containing Si oxides at a predetermined depth, it is possible to secure the plating adhesion and chemical convertibility required for a steel sheet for a vehicle.

[0018]

Specifically, by the first heat treatment, the metallographic structure of the steel sheet inside and the steel sheet surface layer becomes a structure primarily containing a lath-like structure such as martensite. In addition, in the second heat treatment, a highest heating temperature is set to a dual phase region of α (ferrite) and γ (austenite), and a decarburization treatment is performed at the same time. As a result, in the steel sheet obtained after the two heat treatments, the steel sheet inside has a steel structure in which acicular retained austenite is dispersed, and the surface layer has a steel structure primarily containing lath-like ferrite having a large aspect ratio and having a predetermined thickness. It was found that such a steel sheet is excellent in all of formability, fatigue properties, and hydrogen embrittlement resistance of a bent portion.

[0019]

Furthermore, in the first and second heat treatments described above, oxidation of alloying elements such as Si contained in the steel outside the steel sheet is suppressed, and an internal oxide layer containing Si oxides at a predetermined depth is formed, whereby excellent chemical convertibility is obtained. Moreover, in a case where a plated layer is formed on the surface of the steel sheet, excellent plating adhesion is obtained.

[0020]

The present invention has been made based on the above findings. The gist of the present invention is as follows.

[0021]

(1) A steel sheet according to an aspect of the present invention includes, as a chemical composition, by mass %: C: 0.050% to 0.500%; Si: 0.01% to 3.00%; Mn: 0.50% to 5.00%; P: 0.0001% to 0.1000%; S: 0.0001% to 0.0100%; Al: 0.001% to 2.500%; N: 0.0001% to 0.0100%; O: 0.0001% to 0.0100%; Ti: 0% to 0.300%; V: 0% to 1.00%; Nb: 0% to 0.100%; Cr: 0% to 2.00%; Ni: 0% to 2.00%; Cu: 0% to 2.00%; Co: 0% to 2.00%; Mo: 0% to 1.00%; W: 0% to 1.00%; B: 0% to 0.0100%; Sn: 0% to 1.00%; Sb: 0% to 1.00%; Ca: 0% to 0.0100%; Mg: 0% to 0.0100%; Ce: 0% to 0.0100%; Zr: 0% to 0.0100%; La: 0% to 0.0100%; Hf: 0% to 0.0100%; Bi: 0% to 0.0100%; REM: 0% to 0.0100%; and a remainder including Fe and impurities, in which a steel structure in a ⅛ to ⅜ thickness range centered on a ¼ thickness position from a surface contains, by volume fraction, a soft ferrite: 0% to 30%, a retained austenite: 3% to 40%, a fresh martensite: 0% to 30%, a sum of pearlite and cementite: 0% to 10%, and a remainder includes hard ferrite, in the ⅛ to ⅜ thickness range, a number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is 50% or more, when a region having a hardness of 80% or less of a hardness of the ⅛ to ⅜ thickness range is defined as a soft layer, the soft layer having a thickness of 1 to 100 μm from the surface in a sheet thickness direction is present, in ferrite contained in the soft layer, a volume fraction of grains having an aspect ratio of 3.0 or more is 50% or more, a volume fraction of retained austenite in the soft layer is 80% or less of the volume fraction of the retained austenite in the ⅛ to ⅜ thickness range, and when an emission intensity at a wavelength indicating Si is analyzed in the sheet thickness direction from the surface by a radio-frequency glow discharge analysis method, a peak of the emission intensity at the wavelength indicating Si appears in a range of more than 0.2 μm and 10.0 μm or less from the surface.

[0022]

(2) The steel sheet according to (1), in which the chemical composition includes one or two or more selected from the group consisting of Ti: 0.001% to 0.300%, V: 0.001% to 1.00%, and Nb: 0.001% to 0.100%.

[0023]

(3) The steel sheet according to (1) or (2), in which the chemical composition includes one or two or more selected from the group consisting of Cr: 0.001% to 2.00%, Ni: 0.001% to 2.00%, Cu: 0.001% to 2.00%, Co: 0.001% to 2.00%, Mo: 0.001% to 1.00%, W: 0.001% to 1.00%, and B: 0.0001% to 0.0100%.

[0024]

(4) The steel sheet according to any one of (1) to (3), in which the chemical composition includes one or two selected from the group consisting of Sn: 0.001% to 1.00%, and Sb: 0.001% to 1.00%.

[0025]

(5) The steel sheet according to any one of (1) to (4), in which the chemical composition includes one or two or more selected from the group consisting of Ca: 0.0001% to 0.0100%, Mg: 0.0001% to 0.0100%, Ce: 0.0001% to 0.0100%, Zr: 0.0001% to 0.0100%, La: 0.0001% to 0.0100%, Hf: 0.0001% to 0.0100%, Bi: 0.0001% to 0.0100%, and REM: 0.0001% to 0.0100%.

[0026]

(6) The steel sheet according to any one of (1) to (5), in which the chemical composition satisfies Expression (i).

[0000]


Si+0.1×Mn+0.6×Al≥0.35  (i)

[0027]

(Si, Mn, and Al in the Expression (i) are respectively amounts of corresponding elements by mass %)

[0028]

(7) The steel sheet according to any one of (1) to (6), in which the steel sheet has a hot-dip galvanized layer or an electrogalvanized layer on the surface.

[0029]

(8) A method for manufacturing a steel sheet according to another aspect of the present invention is a method for manufacturing the steel sheet according to any one of (1) to (6), the method including: performing a first heat treatment satisfying (a) to (e) on a hot-rolled steel sheet which has been obtained by hot-rolling a slab having the chemical composition according to any one of claims 1 to 6 and pickling, or on a cold-rolled steel sheet which has been obtained by cold-rolling the hot-rolled steel sheet; and thereafter performing a second heat treatment satisfying (A) to (E).

[0030]

(a) An atmosphere containing 0.1 vol % or more of H2and satisfying Expression (ii) is adopted from 650° C. to a highest heating temperature is reached.

[0031]

(b) Holding is performed at the highest heating temperature of Ac3−30° C. to 1000° C. for 1 second to 1000 seconds.

[0032]

(c) Heating is performed such that an average heating rate in a temperature range from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s.

[0033]

(d) After holding at the highest heating temperature, cooling is performed such that an average cooling rate in a temperature range from 700° C. to Ms is 5° C./s or more.

[0034]

(e) Cooling at the average cooling rate of 5° C./s or more to a cooling stop temperature of Ms or lower.

[0035]

(A) An atmosphere containing 0.1 vol % or more of H2 and 0.020 vol % or less of O2and having a log(PH2O/PH2) satisfying Expression (iii) is adopted from 650° C. to a highest heating temperature is reached.

[0036]

(B) Holding is performed at the highest heating temperature of Ac1+25° C. to Ac3−10° C. for 1 second to 1000 seconds.

[0037]

(C) Heating is performed such that an average heating rate from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s.

[0038]

(D) Cooling is performed such that an average cooling rate in a temperature range of 700° C. to 600° C. is 3° C./s or more.

[0039]

(E) After cooling at the average cooling rate of 3° C./s or more, holding is performed at 300° C. to 480° C. for 10 seconds or more.

[0000]


log(PH2O/PH2)<−1.1  (ii)

[0000]


−1.1≤log(PH2O/PH2)≤−0.07  (iii)

[0040]

(In Expression (ii) and Expression (iii), PH2O represents a partial pressure of water vapor, and PH2represents a partial pressure of hydrogen.)

[0041]

(9) The method for manufacturing the steel sheet according to (8), in which hot-dip galvanizing is performed after the cooling in (D).

Effects of the Invention

[0042]

According to the above aspects of the present invention, it is possible to provide a high strength steel sheet having excellent ductility and hole expansibility, excellent chemical convertibility and plating adhesion, and good fatigue properties and hydrogen embrittlement resistance of a bent portion, and a method for manufacturing the same.

BRIEF DESCRIPTION OF THE DRAWINGS

[0043]

FIG. 1 is a cross-sectional view of a steel sheet according to the present embodiment, which is parallel to a rolling direction and a sheet thickness direction.

[0044]

FIG. 2 is a graph showing a relationship between a depth from a surface and an emission intensity at a wavelength indicating Si when the steel sheet according to the present embodiment is analyzed by a radio-frequency glow discharge analysis method in a depth direction (sheet thickness direction) from the surface.

[0045]

FIG. 3 is a graph showing a relationship between a depth from a surface and an emission intensity at a wavelength indicating Si when a steel sheet (comparative steel sheet) different from the present embodiment is analyzed by the radio-frequency glow discharge analysis method in a depth direction (sheet thickness direction) from the surface.

[0046]

FIG. 4 is a diagram showing a first example of a temperature-time pattern of a second heat treatment to a hot-dip galvanizing and alloying treatment in a method for manufacturing the steel sheet according to the present embodiment.

[0047]

FIG. 5 is a diagram showing a second example of the temperature-time pattern of the second heat treatment to the hot-dip galvanizing and alloying treatment in the method for manufacturing the steel sheet according to the present embodiment.

[0048]

FIG. 6 is a diagram showing a third example of the temperature-time pattern of the second heat treatment to the hot-dip galvanizing and alloying treatment in the method for manufacturing the steel sheet according to the present embodiment.

[0049]

FIG. 7 is a schematic view showing an example of hardness measurement of the steel sheet according to the present embodiment.

EMBODIMENTS OF THE INVENTION

[0050]

“Steel Sheet”

[0051]

Hereinafter, a steel sheet according to an embodiment of the present invention (a steel sheet according to the present embodiment) will be described in detail.

[0052]

First, the chemical composition of the steel sheet according to the present embodiment will be described. In the following description, [%] indicating the amount of an element means [mass %].

[0053]

“C: 0.050% to 0.500%”

[0054]

C is an element that greatly increases the strength of the steel sheet. In addition, C stabilizes austenite and is thus an element necessary for obtaining retained austenite that contributes to the improvement in ductility. Therefore, C is effective in achieving both strength and formability. When the C content is less than 0.050%, sufficient retained austenite cannot be obtained, and it becomes difficult to secure sufficient strength and formability. Therefore, the C content is set to 0.050% or more. In order to further enhance strength and formability, the C content is preferably 0.075% or more, and is more preferably 0.100% or more.

[0055]

On the other hand, when the C content exceeds 0.500%, weldability significantly deteriorates. Therefore, the C content is set to 0.500% or less. From the viewpoint of spot weldability, the C content is preferably 0.350% or less, and is more preferably 0.250% or less.

[0056]

“Si: 0.01% to 3.00%”

[0057]

Si is an element that stabilizes retained austenite by suppressing the generation of iron-based carbides in the steel sheet, and thus enhances strength and formability. When the Si content is less than 0.01%, a large amount of coarse iron-based carbide is generated, and the strength and formability deteriorate. Therefore, the Si content is set to 0.01% or more. From this viewpoint, the lower limit of Si is preferably 0.10% or more, and is more preferably 0.25% or more.

[0058]

On the other hand, Si is an element that makes the steel material brittle. When the Si content exceeds 3.00%, the hole expansibility of the steel sheet becomes insufficient. In addition, when the Si content exceeds 3.00%, problems such as cracking in a cast slab are likely to occur. Therefore, the Si content is set to 3.00% or less. Furthermore, Si impairs the impact resistance of the steel sheet. Therefore, the Si content is preferably 2.50% or less, and is more preferably 2.00% or less.

[0059]

“Mn: 0.50% to 5.00%”

[0060]

Mn is contained in order to enhance the strength by enhancing the hardenability of the steel sheet. When the Mn content is less than 0.50%, a large amount of soft structure is formed during cooling after annealing, so that it becomes difficult to secure a sufficiently high tensile strength. Therefore, the Mn content needs to be 0.50% or more. In order to further increase the strength, the Mn content is preferably 0.80% or more, and is more preferably 1.00% or more.

[0061]

On the other hand, when the Mn content exceeds 5.00%, the elongation and hole expansibility of the steel sheet become insufficient. On the other hand, when the Mn content exceeds 5.00%, a coarse Mn-concentrated portion occurs at the sheet thickness center portion of the steel sheet, embrittlement easily occurs, and problems such as cracking in a cast slab are likely to occur. Therefore, the Mn content is set to 5.00% or less. In addition, since the spot weldability deteriorates as the Mn content increases, the Mn content is preferably 3.50% or less, and is more preferably 3.00% or less.

[0062]

“P: 0.0001% to 0.1000%”

[0063]

P is an element that makes the steel material brittle. When the P content exceeds 0.1000%, the elongation and hole expansibility of the steel sheet become insufficient. When the P content exceeds 0.1000%, problems such as cracking in a cast slab are likely to occur. Therefore, the P content is set to 0.1000% or less. Furthermore, P is an element that embrittles a melted portion produced by spot welding. In order to obtain a sufficient welded joint strength, the P content is preferably set to 0.0400% or less, and is more preferably set to 0.0200% or less.

[0064]

On the other hand, setting the P content to less than 0.0001% causes a significant increase in manufacturing cost. From this, the P content is set to 0.0001% or more. The P content is preferably set to 0.0010% or more.

[0065]

“S: 0.0001% to 0.0100%”

[0066]

S is an element which is bonded to Mn to form coarse MnS and reduces formability such as ductility, hole expansibility (stretch flangeability), and bendability. Therefore, the S content is set to 0.0100% or less. In addition, S deteriorates spot weldability. Therefore, the S content is preferably set to 0.0070% or less, and is more preferably set to 0.0050% or less.

[0067]

On the other hand, setting the S content to less than 0.0001% causes a significant increase in manufacturing cost. Therefore, the S content is set to 0.0001% or more. The S content is preferably set to 0.0003% or more, and is more preferably set to 0.0006% or more.

[0068]

“Al: 0.001% to 2.500%”

[0069]

Al is an element that makes the steel material brittle. When the Al content exceeds 2.500%, problems such as cracking in a cast slab are likely to occur. Therefore, the Al content is set to 2.500% or less. As the Al content increases, spot weldability deteriorates. Therefore, the Al content is set to more preferably 2.000% or less, and even more preferably 1.500% or less.

[0070]

On the other hand, although the effect can be obtained even if the lower limit of the Al content is not particularly specified, Al is an impurity that is present in a trace amount in the raw material, and setting the Al content to less than 0.001% causes a significant increase in manufacturing cost. Therefore, the Al content is set to 0.001% or more. Al is an element effective as a deoxidizing agent, and in order to obtain a sufficient deoxidizing effect, the Al content is preferably set to 0.010% or more. Furthermore, Al is an element that suppresses the generation of coarse carbides, and may be contained for the purpose of stabilizing retained austenite. In order to stabilize the retained austenite, the Al content is preferably set to 0.100% or more, and is more preferably set to 0.250% or more.

[0071]

“N: 0.0001% to 0.0100%”

[0072]

N forms coarse nitrides and deteriorates formability such as ductility, hole expansibility (stretch flangeability), and bendability. Therefore, it is necessary to suppress the N content. When the N content exceeds 0.0100%, the deterioration of the formability is significant. Therefore, the N content is set to 0.0100% or less. In addition, since N causes the generation of blowholes during welding, the N content may be small. The N content is preferably 0.0075% or less, and is more preferably 0.0060% or less.

[0073]

The effect is obtained even if the lower limit of the N content is not particularly specified. However, setting the N content to less than 0.0001% causes a significant increase in manufacturing cost. From this, the N content is set to 0.0001% or more. The N content is preferably 0.0003% or more, and is more preferably 0.0005% or more.

[0074]

“O: 0.0001% to 0.0100%”

[0075]

O forms oxides and deteriorates formability such as ductility, hole expansibility (stretch flangeability), and bendability. Therefore, it is necessary to suppress the O content. When the O content exceeds 0.0100%, the deterioration of the formability is significant. Therefore, the upper limit of the O content is set to 0.0100%. The O content is preferably 0.0050% or less, and is more preferably 0.0030% or less.

[0076]

The effect is obtained even if the lower limit of the O content is not particularly specified. However, setting the O content to less than 0.0001% causes a significant increase in manufacturing cost. Therefore, the lower limit thereof is set to 0.0001%.

[0000]


Si+0.1×Mn+0.6×Al≥0.35

[0077]

There is concern that retained austenite may be decomposed into bainite, pearlite, or coarse cementite during a heat treatment. Si, Mn, and Al are elements that are particularly important for suppressing the decomposition of retained austenite and enhancing formability. In order to suppress the decomposition of retained austenite, it is preferable to satisfy Expression (1). The value on the left side of Expression (1) is more preferably 0.60 or more, and even more preferably 0.80 or more.

[0000]


Si+0.1×Mn+0.6×Al≥0.35  (1)

[0078]

(Si, Mn, and Al in Expression (1) are respectively the amounts of the corresponding elements by mass %)

[0079]

The steel sheet according to the present embodiment basically contains the above-mentioned elements, but may also contain one or two or more elements selected from Ti, V, Nb, Cr, Ni, Cu, Co, Mo, W, B, Sn, Sb, Ca, Mg, Ce, Zr, La, Hf, Bi, and REM. These elements are optional elements and are not necessarily contained. Therefore, the lower limit thereof is 0%.

[0080]

“Ti: 0% to 0.300%”

[0081]

Ti is an element that contributes to an increase in the strength of the steel sheet by precipitation strengthening, grain refinement strengthening by suppressing the growth of ferrite grains, and dislocation strengthening by suppressing recrystallization. However, when the Ti content exceeds 0.300%, the precipitation of carbonitrides increases and the formability deteriorates. Therefore, even in a case where Ti is contained, the Ti content is preferably 0.300% or less. In addition, from the viewpoint of formability, the Ti content is more preferably 0.150% or less.

[0082]

The effect is obtained even if the lower limit of the Ti content is not particularly specified. However, in order to sufficiently obtain the strength increasing effect by including Ti, the Ti content is preferably 0.001% or more. For further high-strengthening of the steel sheet, the Ti content is more preferably 0.010% or more.

[0083]

“V: 0% to 1.00%”

[0084]

V is an element that contributes to an increase in the strength of the steel sheet by precipitation strengthening, grain refinement strengthening by suppressing the growth of ferrite grains, and dislocation strengthening by suppressing recrystallization. However, when the V content exceeds 1.00%, carbonitrides are excessively precipitated and the formability deteriorates. Therefore, even in a case where V is contained, the V content is preferably 1.00% or less, and is more preferably 0.50% or less. The effect is obtained even if the lower limit of the V content is not particularly specified. However, in order to sufficiently obtain the strength increasing effect by including V, the V content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0085]

“Nb: 0% to 0.100%”

[0086]

Nb is an element that contributes to an increase in the strength of the steel sheet by precipitation strengthening, grain refinement strengthening by suppressing the growth of ferrite grains, and dislocation strengthening by suppressing recrystallization. However, when the Nb content exceeds 0.100%, the precipitation of carbonitrides increases and the formability deteriorates. Therefore, even in a case where Nb is contained, the Nb content is preferably 0.100% or less. From the viewpoint of formability, the Nb content is more preferably 0.060% or less. The effect is obtained even if the lower limit of the Nb content is not particularly specified. However, in order to sufficiently obtain the strength increasing effect by including Nb, the Nb content is preferably 0.001% or more. For further high-strengthening of the steel sheet, the Nb content is more preferably 0.005% or more.

[0087]

“Cr: 0% to 2.00%”

[0088]

Cr is an element that enhances the hardenability of the steel sheet and is effective in high-strengthening. However, when the Cr content exceeds 2.00%, hot workability is impaired and productivity decreases. From this, even in a case where Cr is contained, the Cr content is preferably set to 2.00% or less, and is more preferably set to 1.20% or less.

[0089]

The effect is obtained even if the lower limit of the Cr content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Cr, the Cr content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0090]

“Ni: 0% to 2.00%”

[0091]

Ni is an element that suppresses phase transformation at a high temperature and is effective in high-strengthening of the steel sheet. However, when the Ni content exceeds 2.00%, the weldability is impaired. From this, even in a case where Ni is contained, the Ni content is preferably set to 2.00% or less, and is more preferably set to 1.20% or less.

[0092]

The effect is obtained even if the lower limit of the Ni content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Ni, the Ni content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0093]

“Cu: 0% to 2.00%”

[0094]

Cu is an element that enhances the strength of the steel sheet by being present in the steel as fine particles. However, when the Cu content exceeds 2.00%, the weldability is impaired. Therefore, even in a case where Cu is contained, the Cu content is preferably set to 2.00% or less, and is more preferably set to 1.20% or less. The effect is obtained even if the lower limit of the Cu content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Cu, the Cu content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0095]

“Co: 0% to 2.00%”

[0096]

Co is an element that enhances the hardenability and is effective in high-strengthening of the steel sheet. However, when the Co content exceeds 2.00%, the hot workability is impaired and the productivity decreases. From this, even in a case where Co is contained, the Co content is preferably 2.00% or less, and is more preferably 1.20% or less.

[0097]

The effect is obtained even if the lower limit of the Co content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Co, the Co content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0098]

“Mo: 0% to 1.00%”

[0099]

Mo is an element that suppresses phase transformation at a high temperature and is effective in high-strengthening of the steel sheet. However, when the Mo content exceeds 1.00%, the hot workability is impaired and the productivity decreases. From this, even in a case where Mo is contained, the Mo content is preferably set to 1.00% or less, and is more preferably set to 0.50% or less.

[0100]

The effect is obtained even if the lower limit of the Mo content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Mo, the Mo content is preferably 0.001% or more, and is more preferably 0.005% or more.

[0101]

“W: 0% to 1.00%”

[0102]

W is an element that suppresses phase transformation at a high temperature and is effective in high-strengthening of the steel sheet. However, when the W content exceeds 1.00%, the hot workability is impaired and the productivity decreases. From this, even in a case where W is contained, the W content is preferably 1.00% or less, and is more preferably 0.50% or less.

[0103]

The effect is obtained even if the lower limit of the W content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including W, the W content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0104]

“B: 0% to 0.0100%”

[0105]

B is an element that suppresses phase transformation at a high temperature and is effective in high-strengthening of the steel sheet. However, when the B content exceeds 0.0100%, the hot workability is impaired and the productivity decreases. From this, even in a case where B is contained, the B content is preferably set to 0.0100% or less. From the viewpoint of productivity, the B content is more preferably 0.0050% or less.

[0106]

The effect is obtained even if the lower limit of the B content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including B, the B content is preferably set to 0.0001% or more. For further high-strengthening, the B content is more preferably 0.0005% or more.

[0107]

“Sn: 0% to 1.00%”

[0108]

Sn is an element that suppresses the coarsening of the structure and is effective in high-strengthening of the steel sheet. However, when the Sn content exceeds 1.00%, the steel sheet may be excessively embrittled and the steel sheet may fracture during rolling. Therefore, even in a case where Sn is contained, the Sn content is preferably 1.00% or less.

[0109]

The effect is obtained even if the lower limit of the Sn content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Sn, the Sn content is preferably 0.001% or more, and is more preferably 0.010% or more.

[0110]

“Sb: 0% to 1.00%”

[0111]

Sb is an element that suppresses the coarsening of the structure and is effective in high-strengthening of the steel sheet. However, when the Sb content exceeds 1.00%, the steel sheet may be excessively embrittled and the steel sheet may fracture during rolling. Therefore, even in a case where Sb is contained, the Sb content is preferably 1.00% or less.

[0112]

The effect is obtained even if the lower limit of the Sb content is not particularly specified. However, in order to sufficiently obtain the high-strengthening effect by including Sb, the Sb content is preferably 0.001% or more, and is more preferably 0.005% or more.

[0113]

“One or Two or More Selected from the Group Consisting of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM Each in 0% to 0.0100%”

[0114]

REM is an abbreviation for rare earth metals, and in the present embodiment, refers to elements belonging to the lanthanoid series excluding Ce and La. In the present embodiment, REM, Ce, and La are often added as mischmetal, and there are cases where elements in the lanthanoid series in a composite form. Even if the elements in the lanthanoid series other than La and/or Ce are included as impurities, the effect is obtained. Furthermore, even if the metal La and/or Ce is added, the effect is obtained. In the present embodiment, the REM content is the total value of the amounts of elements belonging to the lanthanoid series excluding Ce and La.

[0115]

The reason for including these elements is as follows.

[0116]

Ca, Mg, Ce, Zr, La, Hf, Bi, and REM are elements effective in improving formability, and one or two or more thereof may be contained each in 0.0001% to 0.0100%. When the amounts of one or two or more selected from the group consisting of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM each exceed 0.0100%, there is concern that the ductility may decrease. Therefore, even in a case where these elements, the amount of each of the elements is preferably 0.0100% or less, and is more preferably 0.0070% or less. In a case where two or more of the above elements, the total amount of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM is preferably set to 0.0100% or less.

[0117]

The effect is obtained even if the lower limit of the amount of each of the elements is not particularly specified. However, in order to sufficiently obtain the effect of improving the formability of the steel sheet, the amount of each of the elements is 0.0001% or more. From the viewpoint of formability, the total amount of one or two or more selected from the group consisting of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM is more preferably 0.0010% or more.

[0118]

The steel sheet according to the present embodiment contains the above elements, and the remainder consisting of Fe and impurities. A case where Ti, V, Nb, Cr, Ni, Cu, Co, Mo, W, B, Sn, and Sb described above are all contained as impurities in small amounts lower than the lower limits is allowed.

[0119]

In addition, including Ca, Mg, Ce, Zr, La, Hf, Bi, and REM as impurities in trace amounts lower than the lower limits is also allowed.

[0120]

Furthermore, including H, Na, Cl, Sc, Zn, Ga, Ge, As, Se, Y, Tc, Ru, Rh, Pd, Ag, Cd, in, Te, Cs, Ta, Re, Os, Ir, Pt, Au, and Pb as impurities in a total amount of 0.0100% or less is allowed.

[0121]

Next, the steel structure (microstructure) of the steel sheet according to the present embodiment will be described. [%] in the description of the amount of each structure is [vol %].

[0122]

(Steel Structure of Steel Sheet Inside)

[0123]

As illustrated in FIG. 1, in a steel sheet 1 according to the present embodiment, the steel structure (hereinafter, sometimes referred to as “steel structure of the steel sheet inside”) in a ⅛ to ⅜ thickness range 11 centered on a ¼ thickness position (¼ position of the sheet thickness from the surface in a sheet thickness direction) of the sheet thickness from the surface of the steel sheet 1 contains 0% to 30% of soft ferrite, 3% to 40% of retained austenite, 0% to 30% of fresh martensite, and 0% to 10% of the sum of pearlite and cementite, and the number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is 50% or more.

[0124]

“Soft Ferrite: 0% to 30%”

[0125]

Ferrite is a structure having excellent ductility. However, ferrite has low strength and is thus a structure that is difficult to be utilized in a high strength steel sheet. In the steel sheet according to the present embodiment, the steel structure of the steel sheet inside (microstructure of the steel sheet inside) contains 0% to 30% of soft ferrite.

[0126]

The “soft ferrite” in the present embodiment means a ferrite that does not contain retained austenite in the grains. The soft ferrite has low strength, and strain is more likely to be concentrated and fracture is more likely to occur than in the peripheral portions. When the volume fraction of the soft ferrite exceeds 30%, the balance between strength and formability deteriorates significantly. Therefore, the soft ferrite is limited to 30% or less. The soft ferrite is more preferably limited to 15% or less, and may be 0%.

[0127]

“Retained Austenite: 3% to 40%”

[0128]

Retained austenite is a structure that enhances the balance between strength and ductility. In the steel sheet according to the present embodiment, the steel structure of the steel sheet inside contains 3% to 40% of retained austenite. From the viewpoint of formability, the volume fraction of the retained austenite of the steel sheet inside is preferably set to 3% or more, more preferably 5% or more, and even more preferably 7% or more.

[0129]

On the other hand, in order to cause the volume fraction of the retained austenite to exceed 40%, it is necessary to contain a large amount of C, Mn, and/or Ni. In this case, the weldability is significantly impaired. Therefore, the volume fraction of the retained austenite is set to 40% or less. In order to improve the weldability and the convenience of the steel sheet, the volume fraction of the retained austenite is preferably set to 30% or less, and is more preferably set to 20% or less.

[0130]

“Fresh Martensite: 0% to 30%”

[0131]

Fresh martensite greatly improves tensile strength. On the other hand, fresh martensite becomes the origin of fracture and significantly deteriorates impact resistance. Therefore, the volume fraction of the fresh martensite is set to 30% or less. In particular, in order to improve impact resistance, the volume fraction of the fresh martensite is preferably set to 15% or less, and is more preferably set to 7% or less. The fresh martensite may be 0%, but is preferably 2% or more in order to secure the strength of the steel sheet.

[0132]

“Sum of Pearlite and Cementite: 0% to 10%”

[0133]

The steel structure of the steel sheet inside may contain pearlite and/or cementite. However, when the volume fraction of the pearlite and/or cementite is high, the ductility deteriorates. Therefore, the total volume fraction of the pearlite and/or cementite is limited to 10% or less. The volume fraction of the pearlite and/or cementite is preferably 5% or less in total, and may be 0%.

[0134]

“Number Proportion of Retained Austenite Having Aspect Ratio of 2.0 or More is 50% or More of Total Retained Austenite”

[0135]

In the present embodiment, the aspect ratio of retained austenite grains in the steel structure of the steel sheet inside is important. Retained austenite having a large aspect ratio, that is, stretched retained austenite is stable in the early stage of deformation of the steel sheet due to working. However, in the retained austenite having a large aspect ratio, strain is concentrated at the tip end portion as the working progresses, and the retained austenite is appropriately transformed to cause the transformation-induced plasticity (TRIP) effect. Therefore, the steel structure of the steel sheet inside contains the retained austenite having a large aspect ratio, whereby the ductility can be improved without impairing the toughness, hydrogen embrittlement resistance, hole expansibility, and the like. From the above viewpoint, in the steel sheet according to the present embodiment, the number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is set to 50% or more. The number proportion of the retained austenite having an aspect ratio of 2.0 or more is preferably 70% or more, and is more preferably 80% or more.

[0136]

“Tempered Martensite”

[0137]

Tempered martensite is a structure that greatly improves the tensile strength of the steel sheet without impairing the impact resistance, and may be contained in the steel structure of the steel sheet inside. However, when a large amount of tempered martensite is generated in the steel sheet inside, there may be cases where retained austenite is not sufficiently obtained. Therefore, the volume fraction of the tempered martensite is preferably limited to 50% or less, and is more preferably 30% or less.

[0138]

In the steel sheet according to the present embodiment, the residual structure in the steel structure of the steel sheet inside primarily contains “hard ferrite” containing retained austenite in the grains. “Primarily contains” means that hard ferrite has the largest volume fraction in the residual structure.

[0139]

The hard ferrite is formed by subjecting a steel sheet for a heat treatment having a steel structure including a lath-like structure including one or two or more selected from the group consisting of bainite, tempered martensite, and fresh martensite to a second heat treatment, which will be described later. Hard ferrite contains retained austenite in the grains and thus has high strength. In addition, hard ferrite is less likely to cause interfacial delamination between ferrite and the retained austenite compared to a case where retained austenite is present in ferrite grain boundaries, and thus has good formability.

[0140]

Furthermore, the residual structure in the steel structure of the steel sheet inside may contain bainite in addition to the above-mentioned hard ferrite. The bainite in the present embodiment includes granular bainite composed of fine BCC crystals and coarse iron-based carbides, upper bainite composed of lath-like BCC crystals and coarse iron-based carbides, lower bainite composed of plate-like BCC crystals and fine iron-based carbides arranged in parallel therein, and bainitic ferrite containing no iron-based carbides.

[0141]

(Microstructure of Surface Layer)

[0142]

Next, the steel structure (microstructure) of the surface layer of the steel sheet will be described.

[0143]

“When Region Having Hardness of 80% or Less of Hardness in ⅛ to ⅜ Thickness Range (Steel Sheet Inside) is Defined as Soft Layer, Soft Layer Having Thickness of 1 to 100 μm is Present on Surface Layer”

[0144]

In order to improve bendability after working, softening the surface layer of the steel sheet is one of the requirements. In the steel sheet according to the present embodiment, when a region having a hardness of 80% or less of the hardness (average hardness) of the steel sheet inside is defined as a soft layer, a soft layer having a thickness of 1 to 100 μm from the surface of the steel sheet in the sheet thickness direction is present. In other words, a soft layer having a hardness of 80% or less of the average hardness of the steel sheet inside is present in the surface layer portion of the steel sheet, and the thickness of the soft layer is 1 to 100 μm.

[0145]

When the thickness of the soft layer is less than 1 μm in a depth direction (sheet thickness direction) from the surface, sufficient bendability after working cannot be obtained. The thickness (depth range from the surface) of the soft layer is preferably 5 μm or more, and is more preferably 10 μm or more.

[0146]

On the other hand, when the thickness of the soft layer exceeds 100 μm, the strength of the steel sheet is significantly reduced. Therefore, the thickness of the soft layer is set to 100 μm or less. The thickness of the soft layer is preferably 70 μm or less.

[0147]

[Volume Fraction of Grains Having Aspect Ratio of 3.0 or More in Ferrite Contained in Soft Layer is 50% or More]

[0148]

When the volume fraction of grains having an aspect ratio of 3.0 or more in the ferrite contained in the soft layer (the ratio of ferrite grains having an aspect ratio of less than 3.0 to the volume fraction of all ferrite grains in the soft layer) is less than 50%, the hydrogen embrittlement resistance of the bent portion deteriorates. Therefore, the volume fraction of grains having an aspect ratio of 3.0 or more in the ferrite contained in the soft layer is set to 50% or more. The volume fraction thereof is preferably 60% or more, and is more preferably 70% or more. Here, the target ferrite includes soft ferrite and hard ferrite.

[0149]

The reason why the aspect ratio of the ferrite in the soft layer affects the hydrogen embrittlement resistance of the bent portion is not necessarily clear, but it is presumed as follows. That is, in the steel sheet according to the present embodiment, the steel structure of the soft layer and the steel structure of the steel sheet inside (internal structure) are significantly different from each other. However, in the steel sheet according to the present embodiment, since the number proportion of grains having an aspect ratio of 3.0 or more contained in the surface layer is 50% or more, the shape similarity between the surface layer and the internal structure is high. As a result, it is presumed that the local concentration of stress and strain due to bending at the boundary between the surface layer and the inside is suppressed, and the hydrogen embrittlement resistance is improved.

[0150]

[Volume Fraction of Retained Austenite in Soft Layer is 80% or Less of Volume Fraction of Retained Austenite of Steel Sheet Inside]

[0151]

When the volume fraction of retained austenite contained in the soft layer is limited to 80% or less of the volume fraction of retained austenite contained in the ⅛ to ⅜ thickness range centered on the ¼ thickness position of the sheet thickness of the steel sheet from the surface, the hydrogen embrittlement resistance of the bent portion is improved. The volume fraction of the retained austenite contained in the soft layer with respect to the volume fraction of the retained austenite contained in the ⅛ to ⅜ thickness range is preferably 50% or less, and is more preferably 30% or less.

[0152]

The mechanism by which the hydrogen embrittlement resistance of the bent portion is improved by the volume fraction of the retained austenite in the soft layer is not clear, but it is estimated as follows. That is, in the bent portion, a large plastic strain occurs from the center of the sheet thickness toward the outer surface of the bend. Therefore, most of the retained austenite present in the vicinity of the surface on the outside of the bend is transformed into martensite by strain-induced transformation. It is considered that such martensite into which the retained austenite is transformed by strain-induced transformation is extremely hard and brittle, and thus adversely affects hydrogen embrittlement cracking resistance. Therefore, it is considered that as the volume fraction of the retained austenite contained in the soft layer decreases with respect to the volume fraction of the retained austenite contained in the ⅛ to ⅜ thickness range of the steel sheet, the hydrogen embrittlement resistance of the bent portion is improved.

[0153]

“Internal Oxide Layer Containing Si Oxides”

[0154]

In the steel sheet according to the present embodiment, when the emission intensity at a wavelength indicating Si is analyzed by a radio-frequency glow discharge (radio-frequency GDS) analysis method in the depth direction (sheet thickness direction) from the surface, a peak of the emission intensity at the wavelength indicating Si appears in a range of more than 0.2 μm to 10.0 μm or less from the surface. The peak of the emission intensity at the wavelength indicating Si appearing in the range of more than 0.2 μm to 10.0 μm or less from the surface indicates that the steel sheet is internally oxidized and an internal oxide layer containing Si oxides is provided in a range of more than 0.2 μm to 10.0 μm or less from the surface of the steel sheet. The steel sheet having the internal oxide layer in the above depth range has excellent chemical convertibility and plating adhesion because the generation of oxide films such as Si oxides on the surface of the steel sheet due to heat treatments during manufacturing is suppressed.

[0155]

The steel sheet according to the present embodiment may have a peak of the emission intensity at the wavelength indicating Si in both the range of more than 0.2 μm to 10.0 μm or less from the surface and a range of 0 μm to 0.2 μm (a region shallower than a depth of 0.2 μm) from the surface when analyzed by the radio-frequency glow discharge analysis method in the depth direction from the surface. Having a peak in both ranges indicates that the steel sheet has the internal oxide layer and an external oxide layer containing Si oxides on the surface.

[0156]

FIG. 2 is a graph showing the relationship between the depth from the surface and the emission intensity at the wavelength indicating Si when the emission intensity at the wavelength indicating Si is analyzed by the radio-frequency glow discharge analysis method in the depth direction from the surface in the steel sheet according to the present embodiment. In the steel sheet according to the present embodiment shown in FIG. 2, a peak of the emission intensity at the wavelength indicating Si (derived from the internal oxide layer) appears in the range of more than 0.2 μm to 10.0 μm or less from the surface. In addition, a peak of the emission intensity at the wavelength indicating Si (derived from the external oxide layer (IMAX)) appears also in the range of 0 (outermost surface) to 0.2 μm from the surface. Therefore, it can be seen that the steel sheet shown in FIG. 2 has the internal oxide layer and the external oxide layer.

[0157]

FIG. 3 is a graph showing the relationship between the depth from the surface and the emission intensity at the wavelength indicating Si when a steel sheet different from the present embodiment is analyzed by the radio-frequency glow discharge analysis method in the depth direction from the surface. In the steel sheet shown in FIG. 3, a peak of the emission intensity at the wavelength indicating Si appears in the range of 0 (outermost surface) to 0.2 μm from the surface, but does not appear in the range of more than 0.2 μm to 10.0 μm or less. This means that the steel sheet does not have an internal oxide layer but has only an external oxide layer.

[0158]

“Galvanized Layer”

[0159]

A galvanized layer (hot-dip galvanized layer or electrogalvanized layer) may be formed on the surface (both sides or one side) of the steel sheet according to the present embodiment. The hot-dip galvanized layer may be a hot-dip galvannealed layer obtained by alloying the hot-dip galvanized layer.

[0160]

In a case where the hot-dip galvanized layer is not alloyed, the Fe content in the hot-dip galvanized layer is preferably less than 7.0 mass %.

[0161]

In a case where the hot-dip galvanized layer is a hot-dip galvannealed layer which is alloyed, the Fe content is preferably 6.0 mass % or more. The hot-dip galvannealed steel sheet has better weldability than the hot-dip galvanized steel sheet.

[0162]

The plating adhesion amount of the galvanized layer is not particularly limited, but from the viewpoint of corrosion resistance, is preferably 5 g/m2or more per side, more preferably in a range of 20 to 120 g/m2, and even more preferably in a range of 25 to 75 g/m2.

[0163]

The steel sheet according to the present embodiment may be provided with the galvanized layer, and furthermore, on the galvanized layer, an upper layer plated layer for the purpose of improving coatability, weldability, and the like. Furthermore, the galvanized steel sheet may be subjected to various treatments such as a chromate treatment, a phosphate treatment, a lubricity improvement treatment, and a weldability improvement treatment.

[0164]

The steel sheet according to the present embodiment is formed by performing a second heat treatment, which will be described later, on the following steel sheet (a material before the second heat treatment; hereinafter referred to as “steel sheet for a heat treatment”) obtained by steps including a first heat treatment.

[0165]

“Steel Sheet for Heat Treatment”

[0166]

The steel sheet for a heat treatment according to the present embodiment is used as a material of the steel sheet according to the present embodiment.

[0167]

Specifically, it is preferable that the steel sheet for a heat treatment which is to be the material of the steel sheet according to the present embodiment has the same chemical composition as the steel sheet according to the above-mentioned embodiment, and has a steel structure (microstructure) described below. In the description of the amount of each structure, [%] indicates [vol %] unless otherwise specified.

[0168]

That is, it is preferable that the steel structure (the steel structure of the steel sheet inside) in the ⅛ to ⅜ thickness range centered on the ¼ thickness position of the sheet thickness from the surface contains a lath-like structure including one or two or more selected from the group consisting of bainite, tempered martensite, and fresh martensite in a volume fraction of 70% or more in total, contains retained austenite, and has a number density of retained austenite grains having an aspect ratio of less than 1.3 and a major axis of more than 2.5 μm of 1.0×10−2/m2or less, and the steel structure of the surface layer portion in the range of 0 to 20 μm in the depth direction from the surface has a volume fraction of ferrite of less than 50%. In addition, the bainite includes granular bainite composed of fine BCC crystals and coarse iron-based carbides, upper bainite composed of lath-like BCC crystals and coarse iron-based carbides, lower bainite composed of plate-like BCC crystals and fine iron-based carbides arranged in parallel therein, and bainitic ferrite containing no iron-based carbides.

[0169]

A preferable steel structure (microstructure) of the steel sheet for a heat treatment which is to be the material of the steel sheet according to the present embodiment will be described below. [%] in the description of the amount of each structure is [vol %].

[0170]

(Steel Structure of Inside of Steel Sheet for Heat Treatment)

[0171]

“Lath-Like Structure in Volume Fraction of 70% or More in Total”

[0172]

It is preferable that in the steel sheet for a heat treatment of the present embodiment, the steel structure (the steel structure of the steel sheet inside) in the ⅛ to ⅜ thickness range centered on the ¼ thickness position of the sheet thickness of the steel sheet from the surface contains the lath-like structure including one or two or more selected from the group consisting of bainite, tempered martensite, and fresh martensite in a volume fraction of 70% or more in total.

[0173]

By including the lath-like structure in a volume fraction of 70% or more in total, in the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment described later, the steel structure of the steel sheet inside primarily contains hard ferrite. When the total volume fraction of the lath-like structure is less than 70%, in the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment, the steel structure of the steel sheet inside contains a large amount of soft ferrite, so that the steel sheet according to the present embodiment cannot be obtained. The steel structure of the steel sheet inside in the steel sheet for a heat treatment contains the lath-like structure preferably in a volume fraction of 80% or more in total, and more preferably 90% or more in total, and may be 100%.

[0174]

“Number Density of Retained Austenite Grains Having Aspect Ratio of Less than 1.3 and Major Axis of More than 2.5 mm”

[0175]

The steel structure of the steel sheet inside in the steel sheet for a heat treatment may contain retained austenite in addition to the above-mentioned lath-like structure. However, in a case where retained austenite is contained, it is preferable to limit the number density of retained austenite grains having an aspect ratio of less than 1.3 and a major axis of more than 2.5 μm to 1.0×10−2/μm2or less.

[0176]

When the retained austenite present in the steel structure of the steel sheet inside is in the form of coarse lumps, coarse lump-like retained austenite grains are present inside the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment, and a sufficient number proportion of retained austenite having an aspect ratio of 2.0 or more cannot be secured in some cases. Therefore, the number density of coarse lump-like retained austenite grains having an aspect ratio of less than 1.3 and a major axis of more than 2.5 μm is set to 1.0×10−2/μm2or less. The number density of coarse lump-like retained austenite grains is preferably as low as possible, and is preferably 0.5×10−2/μm2or less.

[0177]

When the retained austenite is excessively present in the steel sheet inside of the steel sheet for a heat treatment, the retained austenite partially becomes isotropic by subjecting the steel sheet for a heat treatment to the second heat treatment described later. As a result, there are cases where retained austenite having an aspect ratio of 2.0 or more cannot be sufficiently secured inside the steel sheet obtained after the second heat treatment. Therefore, it is preferable that the volume fraction of the retained austenite contained in the steel structure of the steel sheet inside of the steel sheet for a heat treatment is preferably 10% or less.

[0178]

(Microstructure of Surface Layer of Steel Sheet for Heat Treatment)

[0179]

“Volume Fraction of Ferrite in Surface Layer Portion within Range from Surface of Steel Sheet to 20 μm in Depth Direction is Less than 20%”

[0180]

In the steel sheet for a heat treatment which is to be the material of the steel sheet according to the present embodiment, it is preferable that the volume fraction of ferrite is less than 20% in a range from the surface of the steel sheet to 20 μm in the depth direction. When the volume fraction of ferrite is 20% or more, in the soft layer formed on the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment, the volume fraction of ferrite grains having an aspect ratio of more than 3.0 does not satisfy a predetermined range. The volume fraction of ferrite is preferably as small as possible, and is more preferably 10% or less, and may be 0%.

[0181]

“Method for Manufacturing Steel Sheet According to Present Embodiment”

[0182]

Next, a method for manufacturing the steel sheet according to the present embodiment will be described.

[0183]

In the method for manufacturing the steel sheet according to the present embodiment, a hot-rolled steel sheet which has been obtained by hot-rolling a slab having the above chemical composition and pickling, or a cold-rolled steel sheet which has been obtained by cold-rolling a hot-rolled steel sheet is subjected to the first heat treatment described below, whereby the steel sheet for a heat treatment is manufactured. Then, the steel sheet for a heat treatment is subjected to the second heat treatment described below. The first heat treatment and/or the second heat treatment may be performed using a dedicated heat treatment line or may be performed using an existing annealing line.

[0184]

(Casting Step)

[0185]

In order to manufacture the steel sheet according to the present embodiment, first, a slab having the above chemical composition (composition) is cast. As the slab to be subjected to hot rolling, a continuous cast slab or one manufactured by or a thin slab caster can be used. The slab after casting may be once cooled to room temperature and then hot-rolled, or may be directly hot-rolled while being at a high temperature. It is preferable to directly subject the slab after casting to hot rolling while being at a high temperature because the energy required for heating in hot rolling can be reduced.

[0186]

(Slab Heating)

[0187]

The slab is heated prior to hot rolling. In a case of manufacturing the steel sheet according to the present embodiment, it is preferable to select slab heating conditions that satisfy Expression (4).

[0000]

(Expression1)104·ΣAC1AC3fγ·WMnγ·D·ts(T)ΣAC1AC3D·ts(T)1.0(4)

[0188]

(in Expression (4), fγ is a value represented by Expression (5), WMnγ is a value represented by Expression (6), D is a value represented by Expression (7), and Ac1is a value represented by Expression (8), Ac3is a value represented by Expression (9), and ts(T) is a slab retention time (sec) at a slab heating temperature T)

[0000]

(Expression2)fγ=WC0.8+(1-WC0.8)·T-AC1AC3-AC1(5)

[0189]

(in Expression (5), T is a slab heating temperature (° C.), WC is a C content (mass %) in steel, Ac1is a value represented by Expression (8), and Ac3is a value represented by Expression (9))

[0190]

(Expression 3)

[0191]

(in Expression (6), T is a slab heating temperature (° C.), WMn is a Mn content (mass %) in steel, Ac1is a value represented by Expression (8), and Ac3is a value represented by Expression (9))

[0000]

(Expression4)D=10-4.8·exp(-262000R·T)(7)

[0192]

(in Expression (7), T is a slab heating temperature (° C.), and R is a gas constant; 8.314 J/mol)

[0000]


Ac1=723−10.7×Mn−16.9×Ni+29.1×Si+16.9×Cr  (8)

[0000]

(element symbols in Expression (8) indicate the mass % of the corresponding elements in steel)

[0000]


Ac3=879−346×C+65×Si−18×Mn+54×Al  (9)

[0193]

(element symbols in Expression (9) indicate the mass % of the corresponding elements in steel)

[0194]

The numerator of Expression (4) represents the degree of Mn content to which Mn is distributed from α to γ during retention in a dual phase region of α (ferrite) and γ (austenite). The larger the numerator of Expression (4), the more inhomogeneous the Mn concentration distribution in the steel.

[0195]

The denominator of Expression (4) is a term corresponding to the distance of Mn atoms diffusing into γ during the retention in a γ single phase region. The larger the denominator of Expression (4), the more homogeneous the Mn concentration distribution. In order to sufficiently homogenize the Mn concentration distribution in the steel, it is preferable to select the slab heating conditions so that the value of Expression (4) is 1.0 or less. The smaller the value of Expression (4), the more the number density of coarse lump-like austenite grains in the steel sheet inside of the steel sheet obtained by performing the second heat treatment on the steel sheet for a heat treatment can be reduced.

[0196]

(Hot Rolling)

[0197]

After heating the slab, hot rolling is performed. When the hot rolling completion temperature (finishing temperature) is lower than 850° C., the rolling reaction force increases and it becomes difficult to stably obtain a specified sheet thickness. Therefore, the hot rolling completion temperature is preferably set to 850° C. or higher. From the viewpoint of rolling reaction force, the hot rolling completion temperature is preferably set to 870° C. or higher. On the other hand, in order to cause the hot rolling completion temperature to be higher than 1050° C., it is necessary to heat the steel sheet using a heating apparatus or the like in the steps from the end of the heating of the slab to the end of the hot rolling, which requires a high cost. For this reason, it is preferable to set the hot rolling completion temperature to 1050° C. or lower. In order to easily secure the steel sheet temperature during hot rolling, the hot rolling completion temperature is preferably set to 1000° C. or lower, and is more preferably set to 980° C. or lower.

[0198]

(Pickling Step)

[0199]

Next, the hot-rolled steel sheet thus manufactured is pickled. The pickling is a step of removing oxides on the surface of the hot-rolled steel sheet, and is important for improving the chemical convertibility and plating adhesion of the steel sheet. The pickling of the hot-rolled steel sheet may be performed once or may be performed a plurality of times.

[0200]

(Cold Rolling)

[0201]

The pickled hot-rolled steel sheet may be cold-rolled into a cold-rolled steel sheet. By performing cold rolling on the hot-rolled steel sheet, it is possible to manufacture a steel sheet having a predetermined sheet thickness with high accuracy. In the cold rolling, when the total rolling reduction (cumulative rolling reduction in the cold rolling) exceeds 85%, the ductility of the steel sheet is lost, and the risk of the steel sheet fracturing during the cold rolling increases. Therefore, the total rolling reduction is preferably set to 85% or less, and is more preferably set to 75% or less. The lower limit of the total rolling reduction in the cold rolling step is not particularly specified, and cold rolling may be omitted. In order to improve the shape homogeneity of the steel sheet to obtain a good external appearance and to cause the steel sheet temperature during the first heat treatment and the second heat treatment to be uniform to obtain good ductility, the total rolling reduction in the cold rolling is preferably set to 0.5% or more, and is more preferably set to 1.0% or more.

[0202]

(First Heat Treatment)

[0203]

Next, the pickled hot-rolled steel sheet or the cold-rolled steel sheet obtained by cold-rolling the hot-rolled steel sheet is subjected to the first heat treatment, whereby the steel sheet for a heat treatment is manufactured. The first heat treatment is performed under the conditions that satisfy the following (a) to (e).

[0204]

(a) An atmosphere containing 0.1 vol % or more of H2and satisfying Expression (3) is adopted from 650° C. to a highest heating temperature reached.

[0000]


log(PH2O/PH2)<−1.1  (3)

[0205]

(in Expression (3), log represents the common logarithm, PH2O represents the partial pressure of water vapor, and PH2represents the partial pressure of hydrogen)

[0206]

In the first heat treatment, by satisfying the above (a), a decarburization reaction in the steel sheet surface layer portion is suppressed, and thus the formation of ferrite is suppressed.

[0207]

When H2in the atmosphere is less than 0.1 vol %, an oxide film present on the surface of the steel sheet cannot be sufficiently reduced and the oxide film is formed on the steel sheet. For this reason, the chemical convertibility and plating adhesion of the steel sheet obtained after the second heat treatment are reduced.

[0208]

On the other hand, when the H2content in the atmosphere exceeds 20 vol %, the effect is saturated. When the H2content in the atmosphere exceeds 20 vol %, the risk of hydrogen explosion during an operation increases. Therefore, it is preferable to set the H2content in the atmosphere to 20 vol % or less.

[0209]

In a case where the log(PH2O/PH2) is −1.1 or more, the decarburization reaction proceeds on the surface layer portion of the steel sheet and ferrite is formed in the surface layer portion. As a result, in the steel sheet after the second heat treatment, the proportion of ferrite grains having an aspect ratio of less than 3.0 increases.

[0210]

(b) Holding is performed at a highest heating temperature of Ac3−30° C. to 1000° C. for 1 second to 1000 seconds.

[0211]

In the first heat treatment, the highest heating temperature is set to Ac3−30° C. or higher. When the highest heating temperature is lower than Ac3−30° C., lump-like coarse ferrite remains in the steel structure of the steel sheet inside of the steel sheet for a heat treatment. As a result, the volume fraction of the soft ferrite of the steel sheet obtained after the second heat treatment of the steel sheet for a heat treatment becomes excessive, and the number proportion of retained austenite having an aspect ratio of 2.0 or more becomes insufficient, resulting in the deterioration of properties. The highest heating temperature is preferably set to Ac3−15° C. or higher, and is more preferably set to Ac3+5° C. or higher. On the other hand, heating to an excessively high temperature increases the fuel cost required for heating and also causes damage to the furnace body. Therefore, the highest heating temperature is set to 1000° C. or lower.

[0212]

In the first heat treatment, the retention time at the highest heating temperature is set to 1 second to 1000 seconds. When the retention time is shorter than 1 second, lump-like coarse ferrite remains in the steel structure of the steel sheet inside in the steel sheet for a heat treatment. As a result, the volume fraction of soft ferrite in the steel sheet obtained after the second heat treatment becomes excessive, resulting in the deterioration of properties. The retention time is preferably 10 seconds or more, and is more preferably 50 seconds or more. On the other hand, when the retention time is too long, not only is the effect of heating to the highest heating temperature saturated, but also productivity is impaired. Therefore, the retention time is set to 1000 seconds or shorter.

[0213]

(c) Heating is performed such that the average heating rate in a temperature range from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s.

[0214]

In the first heat treatment, during heating, when the average heating rate is less than 0.5° C./s in a temperature range from 650° C. to the highest heating temperature, Mn segregation proceeds during the heating treatment, and a coarse lump-like Mn-concentrated region is formed. In this case, the properties of the steel sheet obtained after the second heat treatment deteriorate. In order to suppress the generation of lump-like austenite, the average heating rate from 650° C. to the highest heating temperature is set to 0.5° C./s or more. The average heating rate is preferably 1.5° C./s or more.

[0215]

On the other hand, regarding the upper limit of the average heating rate, the upper limit of the average heating rate is set to 500° C./s because the average heating rate of more than 500° C./s causes a difficulty in actual operations and it is also difficult to perform temperature control. The average heating rate from 650° C. to the highest heating temperature is obtained by dividing the difference between 650° C. and the highest heating temperature by the elapsed time from when the surface temperature of the steel sheet reaches 650° C. until the highest heating temperature is reached.

[0216]

(d) After holding at the highest heating temperature, cooling is performed such that the average cooling rate in a temperature range from 700° C. to Ms is 5° C./s or more.

[0217]

In the first heat treatment, in order to cause the steel structure of the steel sheet inside of the steel sheet for a heat treatment to primarily have a lath-like structure, cooling is performed so that a cooling rate in a temperature range from 700° C. to Ms represented by Expression (10) after holding at the highest heating temperature is 5° C./s or more in terms of average cooling rate. When the average cooling rate is less than 5° C./s, there are cases where lump-like ferrite is formed in the steel sheet for a heat treatment. In this case, the volume fraction of soft ferrite in the steel sheet obtained after the second heat treatment becomes excessive, and the properties such as tensile strength deteriorate. The average cooling rate is preferably set to 10° C./s or more, and is more preferably set to 30° C./s or more.

[0218]

The upper limit of the average cooling rate need not be particularly specified, but special equipment is required to perform cooling at an average cooling rate of more than 500° C./s. Therefore, the average cooling rate is preferably 500° C./s or less. The average cooling rate in the temperature range from 700° C. to Ms or lower is obtained by dividing the difference between 700° C. and Ms by the elapsed time until the steel sheet surface temperature reaches from 700° C. to Ms.

[0000]


Ms=561−407×C−7.3×Si−37.8×Mn−20.5×Cu−19.5×Ni−19.8×Cr−4.5×Mo  (10)

[0219]

(element symbols in Expression (10) indicate the mass % of the corresponding elements in steel)

[0220]

(e) Cooling at the average cooling rate of 5° C./s or more is performed to a cooling stop temperature of Ms or lower.

[0221]

In the first heat treatment, cooling in which the average cooling rate in the temperature range of 700° C. to Ms is 5° C./s or more is performed to a cooling stop temperature of Ms or lower represented by Expression (10). The cooling stop temperature may be room temperature (25° C.). By setting the cooling stop temperature to Ms or lower, the steel structure of the steel sheet inside of the steel sheet for a heat treatment obtained after the first heat treatment primarily has the lath-like structure.

[0222]

In the manufacturing method of the present embodiment, the steel sheet cooled to the cooling stop temperature of Ms or lower and room temperature or higher in the first heat treatment may be continuously subjected to the second heat treatment described below. In the first heat treatment, the second heat treatment described below may be performed after cooling to room temperature and winding.

[0223]

The steel sheet cooled to room temperature in the first heat treatment is the steel sheet for a heat treatment of the present embodiment described above. The steel sheet for a heat treatment becomes the steel sheet according to the present embodiment by performing the second heat treatment described below.

[0224]

In the present embodiment, various treatments may be performed on the steel sheet for a heat treatment before performing the second heat treatment. For example, the steel sheet for a heat treatment may be subjected to a temper rolling treatment in order to correct the shape of the steel sheet for a heat treatment. Otherwise, in order to remove oxides present on the surface of the steel sheet for a heat treatment, the steel sheet for a heat treatment may be subjected to a pickling treatment.

[0225]

(Second Heat Treatment)

[0226]

The second heat treatment is applied to the steel sheet (steel sheet for a heat treatment) subjected to the first heat treatment. The second heat treatment is performed under the conditions that satisfy the following (A) to (E).

[0227]

(A) An atmosphere containing 0.1 vol % or more of H2and 0.020 vol % or less of O2and having a log(PH2O/PH2) satisfying Expression (4) is adopted from 650° C. to a highest heating temperature reached.

[0000]


−1.1≤log(PH2O/PH2)≤−0.07  (4)

[0228]

(in Expression (3), log represents the common logarithm, PH2O represents the partial pressure of water vapor, and PH2represents the partial pressure of hydrogen)

[0229]

In the second heat treatment, by satisfying the above (A), an oxidation reaction outside the steel sheet is suppressed, and the decarburization reaction in the surface layer portion is promoted.

[0230]

When H2in the atmosphere is less than 0.1 vol % or O2is more than 0.020 vol %, the oxide film present on the surface of the steel sheet cannot be sufficiently reduced and the oxide film is formed on the steel sheet. As a result, the chemical convertibility and plating adhesion of the steel sheet obtained after the second heat treatment are reduced. A preferable range of H2is 1.0 vol % or more, and is more preferably 2.0 vol % or more. A preferable range of O2is 0.010 vol % or less, and is more preferably 0.005 vol % or less.

[0231]

When the H2content in the atmosphere exceeds 20 vol %, the effect is saturated. When the H2content in the atmosphere exceeds 20 vol %, the risk of hydrogen explosion during an operation increases. Therefore, it is preferable to set the H2content in the atmosphere to 20 vol % or less.

[0232]

In a case where the log(PH2O/PH2) is less than −1.1, external oxidation of Si and Mn in the surface layer of the steel sheet occurs, and the decarburization reaction becomes insufficient, so that the surface layer structure of the steel sheet obtained after the second heat treatment does not satisfy a desired range. Therefore, log(PH2O/PH2) is set to −1.1 or more. log(PH2O/PH2) is preferably −0.8 or more.

[0233]

On the other hand, when the log(PH2O/PH2) exceeds −0.07, the decarburization reaction proceeds excessively, and the strength of the steel sheet obtained after the second heat treatment becomes insufficient. Therefore, log(PH2O/PH2) is set to −0.07 or less.

[0234]

(B) Holding is performed at a highest heating temperature of (Ac1+25)° C. to (Ac3−10)° C. for 1 second to 1000 seconds.

[0235]

In the second heat treatment, the highest heating temperature is set to (Ac1+25)° C. to (Ac3−10)° C. When the highest heating temperature is lower than (Ac1+25)° C., cementite in the steel is left dissolved, and the retained austenite fraction in the internal structure of the steel sheet obtained after the second heat treatment becomes insufficient, resulting in the deterioration of properties. The highest heating temperature is preferably set to (Ac1+40)° C. or higher in order to increase the hard structure fraction of the steel sheet obtained after the second heat treatment and obtain a steel sheet having higher strength.

[0236]

On the other hand, when the highest heating temperature exceeds (Ac3−10)° C., most or all of the steel structure of the inside becomes austenite, so that the lath-like structure in the steel sheet (steel sheet for a heat treatment) before the second heat treatment disappears, and the lath-like structure of the steel sheet before the second heat treatment is not remained to the steel sheet after the second heat treatment. As a result, the retained austenite fraction in the internal structure of the steel sheet obtained after the second heat treatment becomes insufficient, and the number proportion of retained austenite having an aspect ratio of 2.0 or more becomes insufficient, resulting in a significant deterioration in properties. Therefore, the highest heating temperature is set to (Ac3−10)° C. or lower. The highest heating temperature is preferably set to (Ac3−20)° C. or lower, and is more preferably set to (Ac3−30)° C. or lower in order to cause the lath-like structure in the steel sheet before the second heat treatment to be sufficiently remained and further improve the properties of the steel sheet.

[0237]

In the second heat treatment, the retention time at the highest heating temperature is set to 1 second to 1000 seconds. When the retention time is shorter than 1 second, there is concern that cementite in the steel may remain dissolved and the properties of the steel sheet may deteriorate. The retention time is preferably 30 seconds or more. On the other hand, when the retention time is too long, not only is the effect of heating to the highest heating temperature saturated, but also productivity is reduced. Therefore, the retention time is set to 1000 seconds or shorter.

[0238]

(C) Heating is performed such that the average heating rate from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s.

[0239]

When the average heating rate from 650° C. to the highest heating temperature in the second heat treatment is less than 0.5° C./s, recovery of the lath-like structure generated in the first heat treatment progresses and the volume fraction of soft ferrite having no austenite grains in the grains increases. On the other hand, when the average heating rate exceeds 500° C./s, the decarburization reaction does not proceed sufficiently.

[0240]

(D) Cooling from the highest heating temperature to 480° C. or lower is performed such that the average cooling rate from 700° C. to 600° C. is 3° C./s or more.

[0241]

In the second heat treatment, cooling from the highest heating temperature to 480° C. or lower is performed. Here, the average cooling rate between 700° C. and 600° C. is set to 3° C./s or more. When cooling of the above range is performed at an average cooling rate of less than 3° C./s, coarse carbides are generated and the properties of the steel sheet are impaired. The average cooling rate is preferably set to 10° C./s or more. The upper limit of the average cooling rate need not be particularly provided, but a special cooling device is required to perform cooling at more than 200° C./s. Therefore, the upper limit is preferably set to 200° C./s or less.

[0242]

(E) Holding is performed at 300° C. to 480° C. for 10 seconds or more.

[0243]

Subsequently, the steel sheet is held for 10 seconds or more in a temperature range between 300° C. and 480° C. When the retention time is shorter than 10 seconds, carbon is not sufficiently concentrated in untransformed austenite. In this case, lath-like ferrite does not grow sufficiently and concentration of C in austenite does not proceed. As a result, fresh martensite is generated during the final cooling after the holding, and the properties of the steel sheet greatly deteriorate. The retention time is preferably set to 100 seconds or more in order to cause the concentration of carbon into austenite to sufficiently proceed, reduce the amount of martensite produced, and improve the properties of the steel sheet. Although it is not necessary to limit the upper limit of the retention time, the retention time may be set to 1000 seconds or shorter because an excessively long retention time causes a reduction in productivity.

[0244]

In a case where the cooling stop temperature is lower than 300° C., the steel sheet may be reheated to 300° C. to 480° C. and then held.

[0245]

<Galvanizing Step>

[0246]

The steel sheet after the second heat treatment may be subjected to hot-dip galvanizing to form a hot-dip galvanized layer on the surface. Furthermore, subsequent to the formation of the hot-dip galvanized layer, an alloying treatment may be performed on the plated layer.

[0247]

Moreover, electrogalvanizing may be performed on the steel sheet after the second heat treatment to form an electrogalvanized layer on the surface.

[0248]

The hot-dip galvanizing, alloying treatment, and electrogalvanizing may be performed at any timing after the completion of the cooling step (D) in the second heat treatment as long as the conditions specified by the present invention are satisfied. For example, as shown as a pattern [1] in FIG. 4, a plating treatment (and an alloying treatment as necessary) may be performed after the cooling step (D) and the isothermal holding step (E). Otherwise, as shown as a pattern [2] in FIG. 5, a plating treatment (and an alloying treatment as necessary) may be performed after the cooling step (D), and thereafter the isothermal holding step (E) may be performed. Alternatively, as shown as a pattern [3] in FIG. 6, cooling to room temperature is performed once after the cooling step (D) and the isothermal holding step (E), and thereafter a plating treatment (and an alloying treatment as necessary) may be performed.

[0249]

As plating conditions such as a molten zinc bath temperature and a molten zinc bath composition in the hot-dip galvanizing step, general conditions can be used, and there is no particular limitation. For example, the plating bath temperature may be 420° C. to 500° C., the sheet temperature of the steel sheet input to the plating bath may be 420° C. to 500° C., and the immersion time may be 5 seconds or shorter. The plating bath is preferably a plating bath containing 0.08% to 0.2% of Al, but may further contain Fe, Si, Mg, Mn, Cr, Ti, and Pb as unavoidable impurities. Furthermore, it is preferable to control the hot-dip galvanizing adhesion amount by a known method such as gas wiping. The adhesion amount may be usually 5 g/m2or more per side, but is preferably 20 to 120 g/m2, and is more preferably 25 to 75 g/m2.

[0250]

The high strength hot-dip galvanized steel sheet on which the hot-dip galvanized layer is formed may be subjected to an alloying treatment, as necessary, as described above.

[0251]

In the alloying treatment, the alloying treatment temperature is preferably set to 460° C. to 600° C. When the alloying treatment is performed at lower than 460° C., the alloying rate becomes slow, the productivity is lowered, and an irregular alloying treatment occurs.

[0252]

On the other hand, when the alloying treatment temperature exceeds 600° C., alloying proceeds excessively and the plating adhesion of the steel sheet deteriorates. The alloying treatment temperature is more preferably 480° C. to 580° C. The heating time of the alloying treatment is preferably set to 5 to 60 seconds.

[0253]

Furthermore, the alloying treatment is preferably performed under the condition that the iron concentration in the hot-dip galvanized layer is 6.0 mass % or more.

[0254]

In a case of performing electrogalvanizing, the conditions thereof are not particularly limited.

[0255]

By performing the second heat treatment described above, the steel sheet according to the present embodiment described above is obtained.

[0256]

In the present embodiment, the steel sheet may be subjected to cold rolling for the purpose of shape correction. The cold rolling may be performed after performing the first heat treatment or after performing the second heat treatment. Otherwise, the cold rolling may be performed both after performing the first heat treatment and after performing the second heat treatment. Regarding the rolling reduction of the cold rolling, the rolling reduction is preferably set to 3.0% or less, and is more preferably set to 1.2% or less. When the rolling reduction of the cold rolling exceeds 3.0%, a part of the retained austenite is transformed into martensite by strain-induced transformation, and there is concern that the volume fraction of the retained austenite may decrease and the properties may be impaired. On the other hand, the lower limit of the rolling reduction of the cold rolling is not particularly specified, and the properties of the steel sheet according to the present embodiment can also be obtained without cold rolling.

[0257]

Next, a method for measuring each configuration of the steel sheet according to the present embodiment and the steel sheet for a heat treatment according to the present embodiment will be described.

[0258]

“Measurement of Steel Structure”

[0259]

The volume fractions of ferrite (soft ferrite, hard ferrite), bainite, tempered martensite, fresh martensite, pearlite, cementite, and retained austenite contained in the steel structures of the steel sheet inside and the soft layer can be measured using the method described below.

[0260]

A sample is taken with a sheet thickness cross section parallel to the rolling direction of the steel sheet as an observed section, and the observed section is polished and subjected to nital etching. Next, in the case of observing the steel structure of the inside of the steel sheet, in one or a plurality of observed visual fields of the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface of the observed section, and in the case of observing the steel structure of the soft layer, in one or a plurality of observed visual fields of the region including the depth range of the soft layer from the outermost layer of the steel sheet, a total area of 2.0×10−9m2or more is observed with a field emission scanning electron microscope (FE-SEM). In addition, the area fractions of ferrite, bainite, tempered martensite, fresh martensite, pearlite, cementite, and retained austenite are measured, and are regarded as the volume fractions.

[0261]

Here, a region having a substructure in the grains and containing carbides precipitated with a plurality of variants is determined as tempered martensite. A region where cementite is precipitated in a lamellar form is determined as pearlite or cementite. A region where the brightness is low and the substructure is not recognized is determined as ferrite (soft ferrite or hard ferrite). A region where the brightness is high and the substructure is not revealed by etching is determined as fresh martensite or retained austenite. The remainder is determined as bainite. The volume fraction of each thereof is calculated by a point counting method and determined as the volume fraction of each structure.

[0262]

Regarding the volume fractions of hard ferrite and soft ferrite, the volume fraction of each thereof is obtained by the method described below based on the measured volume fraction of ferrite.

[0263]

The volume fraction of fresh martensite can be obtained by subtracting the volume fraction of retained austenite obtained by an X-ray diffraction method described below from the volume fraction of fresh martensite or retained austenite.

[0264]

In the steel sheet according to the present embodiment and the steel sheet for a heat treatment which is to be the material thereof, the volume fraction of retained austenite contained in the steel sheet inside is evaluated by the X-ray diffraction method. Specifically, in the ⅛ to ⅜ thickness range centered on the ¼ thickness position of the sheet thickness from the surface, a surface parallel to the sheet surface is mirror-finished, and the area fraction of FCC iron is measured by the X-ray diffraction method and is determined as the volume fraction of retained austenite.

[0265]

“Ratio Between Volume Fraction of Retained Austenite Contained in Soft Layer and Volume Fraction of Retained Austenite Contained in Steel Sheet Inside”

[0266]

In the steel sheet according to the present embodiment, the ratio between the volume fraction of retained austenite contained in the soft layer and the volume fraction of retained austenite of the steel sheet inside is evaluated by performing a high-resolution crystal structure analysis by an electron back scattering diffraction (EBSD) method. Specifically, a sample is taken with a sheet thickness cross section parallel to the rolling direction of the steel sheet as an observed section, and the observed section is polished and mirror-finished. Furthermore, in order remove the processed layer of the surface layer, electrolytic polishing or mechanical polishing using colloidal silica is performed. Next, for the surface layer portion of the steel sheet including the soft layer and the steel sheet inside (in the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface), a crystal structure analysis according to the EBSD method is performed so that the total area of the observed visual fields is 2.0×10−9m2or more in total (allowed in a plurality of visual fields or the same visual field). For the analysis of the data obtained by the EBSD method in the measurement, “OIM Analysis 6.0” manufactured by TSL is used. A step size is set to 0.01 to 0.20 μm. From the observation result, the region determined as FCC iron is determined as retained austenite, and the volume fraction of retained austenite of each of the soft layer and the steel sheet inside is calculated.

[0267]

“Measurement of Aspect Ratio and Major Axis of Retained Austenite Grains”

[0268]

The aspect ratio and major axis of the retained austenite grains contained in the steel structure of the steel sheet inside are evaluated by performing a high-resolution crystal orientation analysis by the EBSD method. Specifically, a sample is taken with a sheet thickness cross section parallel to the rolling direction of the steel sheet as an observed section, and the observed section is polished and mirror-finished. Furthermore, in order remove the processed layer of the surface layer, electrolytic polishing or mechanical polishing using colloidal silica is performed. Next, for the steel sheet inside (in the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface), a crystal structure analysis according to the EBSD method is performed on an area of 2.0×10−9m2or more in total (allowed in a plurality of visual fields or the same visual field). From the observation result, the region determined as FCC iron is determined as retained austenite.

[0269]

Next, from the crystal orientations of the retained austenite grains measured by the above method, in order to avoid a measurement error, only austenite grains having a major axis length of 0.1 μm or more are extracted and a crystal orientation map is drawn. A boundary that causes a crystal orientation difference of 10° or more is regarded as a grain boundary between retained austenite grains. The aspect ratio is a value obtained by dividing the major axis length of the retained austenite grains by the minor axis length. The major axis is the major axis length of the retained austenite grains. From this result, the number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is obtained.

[0270]

For the analysis of the data obtained by the EBSD method, “OIM Analysis 6.0” manufactured by TSL is used. The distance between marks (step) is set to 0.01 to 0.20

[0271]

“Ferrite Grains Containing Austenite Grains (Hard Ferrite)/Ferrite Grains not Containing Austenite Grains (Soft Ferrite)”

[0272]

A method for separating ferrite grains into grains containing (encapsulating) austenite grains and grains not containing austenite grains will be described. First, grains are observed using FE-SEM, and a high-resolution crystal orientation analysis is performed by the EBSD method. Specifically, a sample is taken with a sheet thickness cross section parallel to the rolling direction of the steel sheet as an observed section, and the observed section is polished and mirror-finished. Furthermore, in order remove the processed layer of the surface layer, electrolytic polishing or mechanical polishing using colloidal silica is performed. Next, for the steel sheet inside (in the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface), a crystal structure analysis according to the EBSD method is performed on an area of 2.0×10−9m2or more in total (allowed in a plurality of visual fields or the same visual field). Next, for the data obtained from BCC iron, a boundary that causes a crystal orientation difference of 15° or more is regarded as a grain boundary, and a grain boundary map of ferrite grains is drawn. Next, from the data obtained from FCC iron, in order to avoid a measurement error, a grain distribution map is drawn only with austenite grains with a major axis length of 0.1 μm or more, and is superimposed on the grain boundary map of ferrite grains.

[0273]

When one ferrite grain has one or more austenite grains completely incorporated therein, the ferrite grain is referred to as “ferrite grain containing austenite grain”. Furthermore, a case where the austenite grains are not adjacent to each other or only the austenite grains are adjacent to each other only at the boundary between the other grains is determined as “ferrite grains containing no austenite grain”.

[0274]

“Hardness from Surface Layer to Steel Sheet Inside”

[0275]

The hardness distribution from the surface layer to the steel sheet inside for determining the thickness of the soft layer can be obtained, for example, by the following method.

[0276]

A sample is taken with a sheet thickness cross section parallel to the rolling direction of the steel sheet as an observed section, the observed section is polished and mirror-finished, and chemical polishing is performed using colloidal silica to remove the processed layer of the surface layer. For the observed section of the obtained sample, using a micro hardness measuring device, a Vickers indenter having a square-based pyramid shape with an apex angle of 136° is pressed against a range from a position at a depth of 5 μm from the outermost layer as the starting point to a ⅛ thickness position of the sheet thickness from the surface, at a pitch of 10 μm in the thickness direction of the steel sheet. At this time, the pressing load is set so that the Vickers indentations do not interfere with each other. For example, the pressing load is 2 gf. Thereafter, the diagonal length of the indentation is measured using an optical microscope, a scanning electron microscope, or the like, and converted into a Vickers hardness (Hv).

[0277]

Next, the measurement position is moved by 10 μm or more in the rolling direction, and the same measurement is performed on a range from a position at a depth of 10 μm from the outermost layer as the starting point to a ⅛ thickness position of the sheet thickness. Next, the measurement position is moved again by 10 μm or more in the rolling direction, and the same measurement is performed on a range from a position at a depth of 5 μm from the outermost layer as the starting point to a ⅛ thickness position of the sheet thickness. Next, the measurement position is moved by 10 μm or more in the rolling direction, and the same measurement is performed on a range from a position at a depth of 10 μm from the outermost layer as the starting point to a ⅛ thickness position of the sheet thickness. As illustrated in FIG. 7, by repeating this, five Vickers hardnesses were measured at each thickness position. In this manner, in effect, hardness measurement data can be obtained at a pitch of 5 μm in the depth direction. The measurement interval is not simply set to a pitch of 5 μm in order to avoid interference between the indentations. The average value of the 5 points is taken as the hardness at that thickness position. By interpolating the data with a straight line, a hardness profile in the depth direction is obtained. The thickness of the soft layer is obtained by reading the depth position where the hardness is 80% or less of the hardness of the base metal from the hardness profile.

[0278]

On the other hand, the hardness of the steel sheet inside is obtained by measuring at least five hardnesses in the ⅛ to ⅜ thickness range centered on the ¼ thickness position using the micro hardness measuring device in the same manner as above and averaging the values.

[0279]

As the micro hardness measuring device, for example, FISCHERSCOPE (registered trademark) HM2000 XYp can be used.

[0280]

“Aspect Ratio of Ferrite Contained in Soft Layer and Proportion of Grains Having Aspect Ratio of 3.0 or More”

[0281]

The aspect ratio of ferrite in the soft layer is evaluated by observing grains using FE-SEM and performing a high-resolution crystal orientation analysis by the electron back scattering diffraction (EBSD) method. For the analysis of the data obtained by the EBSD method, “OIM Analysis 6.0” manufactured by TSL is used. A step size is set to 0.01 to 0.20 μm.

[0282]

From the observation result, a region determined as BCC iron is regarded as ferrite, and a crystal orientation map is drawn. In addition, a boundary that causes a crystal orientation difference of 15° or more is regarded as a grain boundary. The aspect ratio is a value obtained by dividing the major axis length of each ferrite grain by the minor axis length.

[0283]

“Radio-Frequency Glow Discharge (Radio-Frequency GDS) Analysis”

[0284]

When the steel sheet and the steel sheet for a heat treatment according to the present embodiment are analyzed by a radio-frequency glow discharge analysis method, a known radio-frequency GDS analysis method can be used.

[0285]

Specifically, a method in which the surface of the steel sheet is analyzed in the depth direction while the surface of the steel sheet is sputtered in a state where a glow plasma is generated by applying a voltage in an Ar atmosphere. In addition, an element contained in the material (steel sheet) is identified from the emission spectrum wavelength peculiar to the element that is emitted when atoms are excited in the glow plasma, and the amount of the element contained in the material is estimated from the emission intensity of the identified element. Data in the depth direction can be estimated from a sputtering time. Specifically, the sputtering time can be converted into a sputtering depth by obtaining the relationship between the sputtering time and the sputtering depth using a standard sample in advance. Therefore, the sputtering depth converted from the sputtering time can be defined as the depth from the surface of the material.

[0286]

In the radio-frequency GDS analysis, a commercially available analyzer can be used. In the present embodiment, a radio-frequency glow discharge optical emission spectrometer GD-Profiler 2 manufactured by Horiba Ltd. is used.

Example

[0287]

Next, examples of the present invention will be described. The conditions in the examples are one example of conditions adopted to confirm the feasibility and effects of the present invention. The present invention is not limited to this one example of conditions. The present invention can adopt various conditions as long as the object of the present invention is achieved without departing from the gist of the present invention.

[0288]

Steel having the chemical composition shown in Table 1 was melted to produce a slab. This slab was heated at the slab heating temperature shown in Tables 2 to 5 under the slab heating conditions having the numerical values of Expression (4) shown in Tables 2 to 5, and subjected to hot rolling at the temperature shown in Tables 2 to 5 as the rolling completion temperature, whereby a hot-rolled steel sheet was manufactured. Thereafter, the hot-rolled steel sheet was pickled to remove the scale on the surface. Thereafter, some of the hot-rolled steel sheets were subjected to cold rolling to obtain cold-rolled steel sheets.

[0000]

Kind
ofCSiMnPSAlNONbTiV
steelmass % remainder consisting of Fe and impurities
A0.1951.122.450.0050.00160.0590.00350.0008
B0.2201.712.480.0120.00150.0350.00140.0011
C0.3501.802.800.0050.00110.0300.00080.0032
D0.0791.092.600.0090.00050.0200.00150.00170.030
E0.1551.151.280.0050.00300.0420.00200.00120.036
F0.1350.861.920.0050.00160.0590.00350.0008
G0.3090.712.950.0150.00340.0350.00730.0010
H0.3600.382.350.0080.00480.7500.00140.00100.013
I0.1941.193.090.0120.00380.0860.00080.0020
J0.1940.222.940.0080.00401.2460.00220.00190.109
K0.1930.940.940.0170.00030.0380.00170.0025
L0.1051.762.870.0160.00400.0810.00500.0018
M0.1110.942.410.0110.00150.0040.00300.0027
N0.0861.521.560.0140.00080.0460.00960.0008
O0.1700.332.490.0120.00290.6440.00080.0012
P0.1711.902.000.0100.00690.0270.00410.0015
Q0.2201.203.200.0070.00300.0320.00300.0010
R0.2101.152.200.0110.00340.0400.00350.00100.020
S0.1802.202.700.0110.00480.0350.00320.00200.050
T0.1630.250.800.0090.00260.0200.00420.0013
U0.2201.502.400.0130.00150.0400.00430.00200.050
V0.1801.602.600.0080.00110.0320.00430.00080.0200.020
W0.0411.151.860.0060.00280.0540.00270.0009
X0.1630.381.920.0090.00260.0630.00420.00130.350
Y0.1561.170.470.0100.00240.0590.00350.0011
Z0.2003.201.200.0080.00330.0350.00420.0012
AA0.2101.105.200.1500.00300.0350.00350.0013
Kind
ofNiCuCrMoBOthersFormulaAc1Ac3Ms
steelmass % remainder consisting of Fe and impurities(1)° C.° C.° C.
A1.40729825381
BCo: 0.131.98746846365
CCa: 0.00182.10745812300
D0.2001.36727856422
E1.30743861441
F1.09727841427
G1.03712775319
H1.07709868323
I1.55725822357
J1.26698953369
K1.051.05758847419
LSb: 0.0862.10744878397
M0.00141.18725837418
N0.3500.0900.00201.70751892456
OLa: 0.00160.97706887395
P0.1602.12757880401
QZr: 0.003,1.54724802342
REM: 0.003
R0.0500.00201.39733832384
SW: 0.03,2.49758871370
Sn: 0.03
T0.40Mg: 0.0040.34728826455
UHf: 0.0051.76741840370
VBi: 0.002,1.88742844378
Ce: 0.002
W1.37737889466
X0.61714816419
Y1.25752888471
Z3.34803945411
AA1.64699853271
* Underlined values are outside the range of the present invention

[0000]

Hot rolling stepCold rolling
Rollingstep
Experi-Slab heatingcompletionCold rolling
mentalKind oftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
1A12600.690053
2A12500.693053
3A12200.695053
4A12901.494053
5A12800.697053
6A12900.697053
7A12300.495053
8A12000.899053
9A12200.594053
10A12000.689053
11A12900.595053
12A12500.599053
13B12900.696053
14B12700.489053
15B13000.595053
16B12600.592053
17B12500.590053
18C12800.695053
19C12401.389053
20C12600.598053
21C12000.795053
22D12300.695053
23D12400.595053
24D12800.899053
25D12100.595053
26D12200.693053
27D12300.795053
28D12800.692053
29D12800.796053
30E12500.596053
31E12800.497053
32F12500.495053
33F12500.599053
34G13000.590053
35G13000.795053
36G12500.894053
37G12900.690053
38G12300.693053
39H12400.591053
* Underlined values are outside the range of the present invention

[0000]

Hot rolling stepCold rolling
Rollingstep
Experi-Slab heatingcompletionCold rolling
mentalKind oftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
40I12100.598053
41I12900.694053
42I12100.695053
43I12600.896053
44I12600.698053
45I12700.5920Absent
46I12200.6950Absent
47I12900.699053
48I12600.597053
49I12701.698053
50J12100.797053
51J12500.599053
52K12100.794053
53L12200.694053
54L12000.593053
55M12600.797053
56N12300.794053
57O12600.594053
58P12000.894053
59Q12900.694053
60R12500.599053
61S12000.694053
62T12800.689053
63U12900.590053
64U12600.890053
65U12200.489053
66U12400.695053
67U12300.792053
68U12900.692053
69U12500.494053
70V13000.695053
71W12900.596053
72X12600.899053
73Y12500.594053
74Z12400.691053
75AA12400.596053
76A12200.698053
77A12800.799053
78A12000.790053
* Underlined values are outside the range of the present invention

[0000]

Hot rolling stepCold rolling
Rollingstep
Experi-Slab heatingcompletionCold rolling
mentalKind oftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
 1′A12700.795053
 2′A12000.595053
 3′A12600.791053
 4′A12301.594053
 5′A12700.693053
 6′A12900.697053
 7′A12100.593053
 8′A12300.691053
 9′A12600.493053
10′A12600.894053
11′A12600.590053
12′A12300.599053
13′A12700.890053
14′A12900.897053
15′A12400.791053
16′A12300.792053
17′A12900.592053
18′B12200.693053
19′B12300.689053
20′B12200.693053
21′B12300.694053
22′B12700.499053
23′C12000.698053
24′C12201.293053
25′C12500.594053
26′C12800.595053
27′D12200.695053
28′D12500.691053
29′D13000.796053
30′D12300.595053
31′D12100.592053
32′D12100.699053
33′D12600.695053
34′D12500.789053
35′E12300.592053
36′E12900.692053
37′F12100.593053
38′F12700.690053
39′G12200.499053
40′G13000.790053
41′G12400.899053
42′G12600.591053
43′G12900.796053
* Underlined values are outside the range of the present invention

[0000]

Hot rolling stepCold rolling
Rollingstep
Experi-Slab heatingcompletionCold rolling
mentalKind oftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
44′H12500.696053
45′I12000.591053
46′I12900.595053
47′I12200.693053
48′I12000.691053
49′I12800.791053
50′I12900.5940Absent
51′I12300.8950Absent
52′I12700.598053
53′I12500.698053
54′I12801.799053
55′J12900.798053
56′J12300.692053
57′K13000.798053
58′L12000.897053
59′L12200.593053
60′M12300.793053
61′N12500.699053
62′O12200.694053
63′P12500.696053
64′Q12900.699053
65′R12900.590053
66′S12700.696053
67′T13000.894053
68′U12400.491053
69′U12300.893053
70′U13000.494053
71′U12800.598053
72′U12500.797053
73′U13000.692053
74′U12700.497053
75′V12900.792053
76′W12000.499053
77′X13000.799053
78′Y12600.595053
79′Z12100.689053
80′AA13000.594053
81′A13000.693053
82′A12000.899053
83′A12700.692053
84′A12300.596053
85′A12800.691053
86′A12900.589053
87′B13000.489053
88′C12600.696053
89′A12100.794053
* Underlined values are outside the range of the present invention

[0289]

The hot-rolled steel sheet having a sheet thickness of 1.2 mm or the cold-rolled steel sheet having a sheet thickness of 1.2 mm thus obtained was subjected to the following first heat treatment and/or second heat treatment. In some of the examples, the cold-rolled steel sheet cooled to the cooling stop temperature shown in Tables 6 to 9 in the first heat treatment was continuously subjected to the second heat treatment without being cooled to room temperature. In the other examples, after cooling to the cooling stop temperature in the first heat treatment and then cooling to room temperature, the second heat treatment was performed. In addition, in some of the examples, the second heat treatment was performed without performing the first heat treatment.

[0290]

(First Heat Treatment)

[0291]

Under the conditions shown in Tables 6 to 9, heating to the highest heating temperature was performed and holding at the highest heating temperature was performed. Then, cooling to the cooling stop temperature was performed. In the first heat treatment, heating was performed in the atmosphere containing H2at the concentration shown in Tables 6 to 9 and having a log(PH2O/PH2) of the numerical value shown in Tables 6 to 9 until the temperature reached from 650° C. to the highest heating temperature.

[0292]

Ac3was obtained by Expression (9), and Ms was obtained by Expression (10).

[0000]


Ac3=879−346C+65Si−18Mn+54Al  (9)

[0293]

(element symbols in Expression (9) indicate the mass % of the corresponding elements in steel)

[0000]


Ms=561−407×C−7.3×Si−37.8×Mn−20.5×Cu−19.5×Ni−19.8×Cr−4.5×Mo  (10)

[0294]

(element symbols in Expression (10) indicate the mass % of the corresponding elements in steel)

[0000]

First heat treatment
Average heatingHighestAverage cooling
Experi-rate at 650° C.heatingRetentionAtmosphererate betweenCooling stop
mentalAc3Msor highertemperaturetimelog(PH20/H2700° C. and Mstemperature
Example° C.° C.° C./s° C.sPH2)vol %° C./s° C.
18253812.085060−1.92.040.0Room temperature
28253812.078060−1.92.040.0Room temperature
38253812.099060−2.02.040.0Room temperature
48253812.082060−1.72.040.0Room temperature
58253810.0486060−1.92.040.0Room temperature
68253812.0840600.72.040.0Room temperature
78253812.084560−1.82.012.0Room temperature
88253812.085560−1.92.02.0Room temperature
98253812.086060−1.92.040.0Room temperature
108253812.085060−1.92.040.0Room temperature
11825381Absent
128253812.086060−1.92.040.0220
138463652.088060−1.82.040.0Room temperature
148463652.086060−1.82.040.0280
158463652.085060−0.72.040.0Room temperature
168463652.088060−0.82.040.0Room temperature
17846365Absent
188123002.082060−2.02.040.0Room temperature
198123002.082060−2.02.040.0Room temperature
208123002.082060−1.92.040.0Room temperature
218123002.083060−1.92.040.0230
228564222.085060−1.92.040.0Room temperature
238564222.090560−1.82.040.0Room temperature
248564222.090560−0.72.040.0Room temperature
258564222.086560−1.92.040.0Room temperature
268564222.087560−1.92.040.0Room temperature
278564222.08955−2.02.040.0Room temperature
288564222.087560−1.92.040.0310
29856422Absent
308614412.088060−1.82.040.0Room temperature
318614412.089060−1.92.040.0320
328414272.085060−1.92.040.0Room temperature
338414272.089060−1.92.040.0240
347753192.079060−2.02.040.0Room temperature
357753192.081060−1.92.040.0Room temperature
367753192.081060−1.92.040.0Room temperature
377753192.080060−2.02.040.0270
387753192.080060−1.92.040.0400
398683232.086060−1.92.040.0Room temperature
* Underlined values are outside the range of the present invention

[0000]

First heat treatment
Average heatingHighestAverage cooling
Experi-rate at 650° C.heatingRetentionAtmosphererate betweenCooling stop
mentalAc3Msor highertemperaturetimelog(PH20/H2700° C. and Mstemperature
Example° C.° C.° C./s° C.sPH2)vol %° C./s° C.
408223572.083060−2.02.040.0Room temperature
418223570.781560−2.02.040.0Room temperature
428223572.082560−2.02.040.0Room temperature
438223572.087060−2.02.040.0Room temperature
448223572.084060−2.02.040.0260
458223572.086560−2.02.040.0Room temperature
468223572.080560−2.02.040.0Room temperature
47822357Absent
48822357Absent
498223572.087060−1.92.040.0Room temperature
509533692.096060−2.02.040.0Room temperature
519533692.098060−1.92.040.0Room temperature
528474192.084060−1.92.040.0Room temperature
538783972.089060−1.92.040.0Room temperature
548783972.090060−1.92.040.0Room temperature
558374182.086060−1.92.040.0Room temperature
568924562.093060−1.92.040.0Room temperature
578873952.094060−2.02.040.0Room temperature
588804012.090560−1.92.040.0Room temperature
598023422.088060−1.92.040.0Room temperature
608323842.085060−1.92.040.0Room temperature
618713702.087060−1.92.040.0Room temperature
628264552.086560−1.92.040.0Room temperature
638403702.088060−2.02.040.0Room temperature
648403702.086060−1.92.040.0Room temperature
658403702.084060−1.92.040.0Room temperature
668403702.084560−1.22.040.0Room temperature
678403702.088060−2.02.040.0300
688403702.088060−2.02.040.0190
698403702.083560−1.92.040.0Room temperature
708443782.089560−1.92.040.0Room temperature
718894662.090060−1.92.040.0Room temperature
728164192.087060−1.92.040.0Room temperature
738884712.091560−1.92.040.0Room temperature
749454112.094560−1.92.040.0Room temperature
758532712.088560−1.92.040.0Room temperature
768253812.083060−1.94.040.0Room temperature
778253812.085060−1.92.040.0Room temperature
788253812.085060−1.92.040.0Room temperature
* Underlined values are outside the range of the present invention

[0000]

First heat treatment
Average heatingHighestAverage cooling
Experi-rate at 650° C.heatingRetentionAtmosphererate betweenCooling stop
mentalAc3Msor highertemperaturetimelog(PH20/H2700° C. and Mstemperature
Example° C.° C.° C./s° C.sPH2)vol %° C./s° C.
 1′8253812.083060−1.92.040.0Room temperature
 2′8253812.079060−2.02.040.0Room temperature
 3′8253812.098060−1.92.040.0Room temperature
 4′8253812.082060−1.92.040.0Room temperature
 5′8253810.0584060−1.92.040.0Room temperature
 6′8253812.087060−0.72.040.0Room temperature
 7′8253812.084560−1.82.012.0Room temperature
 8′8253812.085560−1.92.02.0Room temperature
 9′8253812.083060−1.92.040.0Room temperature
10′8253812.084060−1.92.040.0Room temperature
11′8253812.084060−2.26.040.0Room temperature
12′8253812.087060−1.92.040.0Room temperature
13′8253812.082060−1.92.040.0Room temperature
14′8253812.086060−1.92.040.0Room temperature
15′825381Absent
16′8253812.087060−1.82.040.0250
17′8253812.086060−2.02.040.0Room temperature
18′8463652.087060−1.82.040.0Room temperature
19′8463652.086060−1.82.040.0260
20′8463652.086060−0.72.040.0Room temperature
21′8463652.088060−0.62.040.0Room temperature
22′846365Absent
23′8123002.084060−1.92.040.0Room temperature
24′8123002.083060−2.02.040.0Room temperature
25′8123002.084060−2.02.040.0Room temperature
26′8123002.084060−1.92.040.0170
27′8564222.084060−1.92.040.0Room temperature
28′8564222.086560−2.02.040.0Room temperature
29′8564222.086560−0.62.040.0Room temperature
30′8564222.088560−2.02.040.0Room temperature
31′8564222.090560−2.02.040.0Room temperature
32′8564222.08855−1.92.040.0Room temperature
33′8564222.085560−2.02.040.0310
34′856422Absent
35′8614412.090060−2.22.040.0Room temperature
36′8614412.088060−2.22.040.0290
37′8414272.087060−2.02.040.0Room temperature
38′8414272.088060−2.02.040.0240
39′7753192.079060−1.92.040.0Room temperature
40′7753192.079060−2.12.040.0Room temperature
41′7753192.078060−2.02.040.0Room temperature
42′7753192.082060−2.02.040.0280
43′7753192.080060−2.02.040.0400
* Underlined values are outside the range of the present invention

[0000]

First heat treatment
Average heatingHighestAverage cooling
Experi-rate at 650° C.heatingRetentionAtmosphererate betweenCooling stop
mentalAc3Msor highertemperaturetimelog(PH20/H2700° C. and Mstemperature
Example° C.° C.° C./s° C.sPH2)vol %° C./s° C.
44′8683232.086060−1.92.040.0Room temperature
45′8223572.082060−2.22.040.0Room temperature
46′8223570.782560−2.12.040.0Room temperature
47′8223572.082560−2.02.040.0Room temperature
48′8223572.087060−2.22.040.0Room temperature
49′8223572.085060−2.02.040.0230
50′8223572.085560−2.12.040.0Room temperature
51′8223572.079560−1.92.040.0Room temperature
52′822357Absent
53′822357Absent
54′8223572.085060−2.22.040.0Room temperature
55′9533692.099060−2.12.040.0Room temperature
56′9533692.095060−2.22.040.0Room temperature
57′8474192.086060−1.92.040.0Room temperature
58′8783972.090060−1.92.040.0Room temperature
59′8783972.091060−2.02.040.0Room temperature
60′8374182.084060−2.22.040.0Room temperature
61′8924562.093060−1.92.040.0Room temperature
62′8873952.095060−1.92.040.0Room temperature
63′8804012.089560−2.12.040.0Room temperature
64′8023422.090060−2.22.040.0Room temperature
65′8323842.083060−2.02.040.0Room temperature
66′8713702.089060−1.92.040.0Room temperature
67′8264552.085560−2.12.040.0Room temperature
68′8403702.084060−2.12.040.0Room temperature
69′8403702.085060−2.02.040.0Room temperature
70′8403702.087060−2.22.040.0Room temperature
71′8403702.084560−1.22.040.0Room temperature
72′8403702.084060−1.92.040.0310
73′8403702.086060−1.92.040.0190
74′8403702.087560−1.92.040.0Room temperature
75′8443782.091560−2.22.040.0Room temperature
76′8894662.092060−2.22.040.0Room temperature
77′8164192.087060−2.02.040.0Room temperature
78′8884712.089560−2.22.040.0Room temperature
79′9454112.095560−1.92.040.0Room temperature
80′8532712.091560−1.92.040.0Room temperature
81′8253812.085560−1.92.040.0Room temperature
82′8253812.085560−1.92.040.0Room temperature
83′8253812.086560−2.22.040.0200
84′8253812.086560−2.22.040.0Room temperature
85′8253812.083560−2.12.040.0Room temperature
86′8253812.083560−2.02.040.0Room temperature
87′8463652.088060−2.02.040.0Room temperature
88′8123002.086060−1.92.040.0Room temperature
89′8253812.086560−1.92.040.0Room temperature
* Underlined values are outside the range of the present invention

[0295]

(Second Heat Treatment)

[0296]

Heating to the highest heating temperature was performed and holding at the highest heating temperature was performed so that the average heating rate from 650° C. to the highest heating temperature became the condition shown in Tables 10 to 13. Thereafter, cooling to the cooling stop temperature was performed so that the average cooling rate between 700° C. and 600° C. became the average cooling rate shown in Tables 10 to 13. In the second heat treatment, heating was performed in the atmosphere shown in Tables 10 to 13 from 650° C. to the highest heating temperature is reached.

[0297]

Next, electrogalvanizing is performed on some of the high strength steel sheets (Experimental Examples Nos. 54 and 69) after the second heat treatment to form electrogalvanized layers on both surfaces of the high strength steel sheet, whereby electrogalvanized steel sheets (EG) were obtained.

[0298]

Furthermore, among the experimental examples, in Experimental Examples Nos. 1′ to 80′, hot-dip galvannealing was performed at the timing after cooling and isothermal holding (that is, at the timing shown in the pattern [1] in FIG. 4) under the conditions shown in the tables. In addition, in Experimental Examples 1′ to 16′, 18′ to 58′, 60′ to 73′, and 75′ to 80′ among Experimental Examples 1′ to 80′, an alloying treatment was performed subsequent to hot-dip galvanizing, whereas in Experimental Examples 17′, 59′, and 74′, an alloying treatment was not performed after hot-dip galvanizing

[0299]

In Experimental Examples Nos. 81′ to 88′, according to the pattern [2] shown in FIG. 5, as shown in the tables, heating to the highest heating temperature was performed, cooling to the average cooling rate was thereafter performed, hot-dip galvannealing and an alloying treatment excluding Experimental Example No. 86 were subsequently performed, and cooling and isothermal holding were performed under the conditions shown in Tables 10 to 13.

[0300]

In addition, in Experimental Example No. 89′, according to the pattern [3] shown in FIG. 6, under the conditions shown in the tables, heating to the highest heating temperature was performed under the conditions shown in the tables according to the, cooling to room temperature was then performed once, and hot-dip galvannealing and an alloying treatment were thereafter performed again.

[0301]

The hot-dip galvanizing was performed in each of the examples by immersing the steel sheet into a molten zinc bath at 460° C. to cause the adhesion amount to both surfaces of the steel sheet to be 50 g/m2per side.

[0302]

Ac1was obtained by Expression (8), and Ac3was obtained by Expression (9).

[0000]


Ac1=723−10.7×Mn−16.9×Ni+29.1×Si+16.9×Cr  (8)

[0000]

(element symbols in Expression (8) indicate the mass % of the corresponding elements in steel)

[0000]

Second heat treatment
AverageAverage
heating rateHighestcooling rateCooling
Experi-at 650° C.heatingRetentionAtmospherebetween 700° C.stop
mentalor highertemperaturetimelog(PH20/H2O2and 600° C.temperature
Example° C.° C.sPH2)vol %vol %° C./s° C.
11.877590−0.72.00.00340370
21.879590−0.72.00.00340370
31.8780110−0.72.00.00340390
41.877590−0.72.00.00340400
51.879590−0.72.00.00340400
61.879590−0.72.00.00340410
71.878590−0.72.00.00340390
81.878090−0.72.00.00340360
91.877590−1.62.00.00340360
101.879020−1.02.00.00340360
111.878090−0.72.00.00340360
121.879590−0.72.00.00340370
131.882590−0.72.00.00340190
141.881590−0.72.00.00340190
151.882090−1.62.00.00340230
161.880590−0.72.00.00340200
171.883090−0.72.00.00340270
181.878590−0.72.00.00340140
191.880090−0.72.00.00340200
201.878090−1.52.00.00340140
211.879090−0.72.00.00340120
221.882590−0.72.00.00340380
231.881090−0.72.00.00340340
241.882590−1.62.00.00340390
251.882090−1.62.00.00340350
261.889590−0.72.00.00340380
271.880590−0.72.00.00340360
281.881090−0.72.00.00340360
291.882590−0.72.00.00340280
301.881090−0.72.00.00340360
311.882090−0.72.00.00340380
321.880090−0.72.00.00340320
331.880590−0.72.00.00340320
341.874090−0.72.00.00340360
351.874590−0.72.00.00340400
361.875590−0.72.00.00340390
371.875590−0.72.00.00340390
381.874590−0.72.00.00340360
391.879590−0.72.00.00340410
Second heat treatment
Retention time
Experi-Holdingbetween 300° C.AlloyingPlating
mentaltemperatureand 480° C.temperaturetreatmentAc1Ac3
Example° C.s° C.timing° C.° C.
1410205729825
2390205729825
3400250729825
4400205729825
5400205729825
6390205729825
7390205729825
8380205729825
9400205729825
10410205729825
11380205729825
12400205729825
13390205746846
14400205746846
15390205746846
16410205746846
17400205746846
18410205745812
19390205745812
20400205745812
21400205745812
22400205727856
23380205727856
24390205727856
25370205727856
26390205727856
27380205727856
28370205727856
29400205727856
30390205743861
31400205743861
32360205727841
33340205727841
34400205712775
354007712775
36390 50712775
37390205712775
38400205712775
39400205709868
* Underlined values are outside the range of the present invention

[0000]

Second heat treatment
AverageAverage
heating rateHighestcooling rateCooling
Experi-at 650° C.heatingRetentionAtmospherebetween 700° C.stop
mentalor highertemperaturetimelog(PH20/H2O2and 600° C.temperature
Example° C.° C.sPH2)vol %vol %° C./s° C.
401.8780110−0.72.00.00340410
411.8780110−0.72.00.00340380
421.87855−0.72.00.00340380
431.8785110−0.72.00.0032375
441.8785110−0.72.00.00340380
451.8770110−0.72.00.00340365
461.8780110−0.72.00.00340365
471.8790110−0.72.00.00340400
481.8790110−1.52.00.00340400
491.8790110−0.72.00.00340400
501.8880110−0.72.00.00340360
511.8880110−1.52.00.00340360
521.8800110−0.72.00.00340320
531.8820110−0.72.00.00340330
541.8815110−0.72.00.00340330
551.8790110−0.72.00.00340260
561.8830110−0.72.00.00340350
571.8805110−0.72.00.00340350
581.8825110−0.72.00.00340350
591.8765110−0.72.00.00340300
601.8780110−0.72.00.00340340
611.8830110−0.72.00.00340380
621.8785110−0.72.00.00340395
631.8790110−0.72.00.00340375
641.8730110−0.72.00.00340380
651.8800110−0.032.00.00340380
661.8790110−0.72.00.00340400
671.8775110−0.72.00.00340380
681.8825110−0.72.00.00340370
691.8795110−0.72.00.00340380
701.8800110−0.72.00.00340400
711.8810110−0.72.00.00340400
721.8775110−0.72.00.00340370
731.8820110−0.72.00.00340390
741.8875110−0.72.00.00340390
751.8765110−0.72.00.00340390
761.8780110−0.75.00.00340390
7715.0790110−0.72.00.00340390
780.6770110−0.72.00.00340390
Second heat treatment
Retention time
Experi-Holdingbetween 300° C.AlloyingPlating
mentaltemperatureand 480° C.temperaturetreatmentAc1Ac3
Example° C.s° C.timing° C.° C.
40410250725822
41390250725822
42400250725822
43375250725822
44400250725822
45375250725822
46385250725822
47420250725822
48420250725822
49400250725822
50380250698953
51370250698953
52380250758847
5333080744878
54340250744878
55400250725837
56350250751892
57370250706887
58350250757880
59310250724802
60350250733832
61380250758871
62395250728826
63395250741840
64380250741840
65390250741840
66420250741840
67380250741840
68370250741840
69390250741840
70410250742844
71420250737889
72370250714816
73400250752888
74410250803945
75410250699853
76390250729825
77400250729825
78390250729825
* Underlined values are outside the range of the present invention

[0000]

Second heat treatment
AverageAverage
heating rateHighestcooling rateCooling
Experi-at 650° C.heatingRetentionAtmospherebetween 700° C.stop
mentalor highertemperaturetimelog(PH20/H2O2and 600° C.temperature
Example° C.° C.sPH2)vol %vol %° C./s° C.
 1′1.3790108−0.74.00.00330410
 2′1.3790108−0.74.00.00330400
 3′1.3780108−0.74.00.00330420
 4′1.3790108−0.74.00.00330420
 5′1.3790108−0.74.00.00330400
 6′1.3790108−0.74.00.00330400
 7′1.3790108−0.74.00.00330390
 8′1.3790108−0.74.00.00330400
 9′1.3790108−1.64.00.00330420
10′1.3790108−1.04.00.00330400
11′1.3780108−0.72.00.00330400
12′1.3780108−0.74.00.00830410
13′16.0790108−0.74.00.00330390
14′0.5790108−0.74.00.00330410
15′1.3800108−0.74.00.00330410
16′1.3790108−0.74.00.00330400
17′1.3790108−0.74.00.00330400
18′1.3810108−0.74.00.00330220
19′1.3800108−0.74.00.00330220
20′1.3810108−1.74.00.00330220
21′1.3810108−0.74.00.00330220
22′1.3815108−1.74.00.00330260
23′1.3790108−0.74.00.00330170
24′1.3790108−0.74.00.00330210
25′1.3780108−1.54.00.00330170
26′1.3790108−0.74.00.00330180
27′1.3820108−0.74.00.00330370
28′1.3810108−0.74.00.00330370
29′1.3820108−1.54.00.00330370
30′1.3820108−1.64.00.00330370
31′1.3880108−0.74.00.00330370
32′1.3810108−0.74.00.00330370
33′1.3810108−0.74.00.00330370
34′1.3810108−0.74.00.00330370
35′1.3810108−0.74.00.00330380
36′1.3810108−0.74.00.00330380
37′1.3800108−0.74.00.00330350
38′1.3800108−0.74.00.00330350
39′1.3740108−0.74.00.00330390
40′1.3740108−0.74.00.00330390
41′1.3740108−0.74.00.00330390
42′1.3740108−0.74.00.00330390
43′1.3740108−0.74.00.00330390
Second heat treatment
Retention time
Experi-Holdingbetween 300° C.AlloyingPlating
mentaltemperatureand 480° C.temperaturetreatmentAc1Ac3
Example° C.s° C.timing° C.° C.
 1′410120490[1]729825
 2′410120500[1]729825
 3′410120500[1]729825
 4′410120500[1]729825
 5′400120490[1]729825
 6′410120500[1]729825
 7′390120500[1]729825
 8′410120500[1]729825
 9′410120490[1]729825
10′410120490[1]729825
11′400120490[1]729825
12′400120500[1]729825
13′400120490[1]729825
14′410120480[1]729825
15′400120480[1]729825
16′390120490[1]729825
17′400120[1]729825
18′380120490[1]746846
19′380120490[1]746846
20′380120480[1]746846
21′390120480[1]746846
22′390120490[1]746846
23′380120490[1]745812
24′380120490[1]745812
25′380120490[1]745812
26′390120500[1]745812
27′380120490[1]727856
28′380120490[1]727856
29′380120490[1]727856
30′380120480[1]727856
31′380120480[1]727856
32′380120490[1]727856
33′380120490[1]727856
34′380120490[1]727856
35′380120490[1]743861
36′380120490[1]743861
37′350120490[1]727841
38′350120490[1]727841
39′400120480[1]712775
40′4007480[1]712775
41′400 40480[1]712775
42′410120490[1]712775
43′400120490[1]712775
* Underlined values are outside the range of the present invention

[0000]

Second heat treatment
AverageAverage
heating rateHighestcooling rateCooling
Experi-at 650° C.heatingRetentionAtmospherebetween 700° C.stop
mentalor highertemperaturetimelog(PH20/and 600° C.temperature
Example° C.° C.sPH2)H2O2° C./s° C.
44′1.3800108−0.74.00.00330400
45′1.3780108−0.74.00.00330400
46′1.3780108−0.74.00.00330400
47′1.37905−0.74.00.00330390
48′1.3790108−0.74.00.0032390
49′1.3790108−0.74.00.00330390
50′1.3780108−0.74.00.00330380
51′1.3780108−0.74.00.00330380
52′1.3780108−0.74.00.00330390
53′1.3800108−1.54.00.00330380
54′1.3790108−0.74.00.00330390
55′1.3870108−0.74.00.00330380
56′1.3870108−1.64.00.00330370
57′1.3800108−0.74.00.00330350
58′1.3810108−0.74.00.00330350
59′1.3820108−0.74.00.00330350
60′1.3790108−0.74.00.00330230
61′1.3820108−0.74.00.00330370
62′1.3810108−0.74.00.00330370
63′1.3830108−0.74.00.00330370
64′1.3770108−0.74.00.00330300
65′1.3780108−0.74.00.00330350
66′1.3830108−0.74.00.00330400
67′1.3780108−0.74.00.00330400
68′1.3790108−0.74.00.00330430
69′1.3735108−0.74.00.00330430
70′1.38001080.04.00.00330430
71′1.3790108−0.74.00.00330430
72′1.3775108−0.74.00.00330430
73′1.3820108−0.74.00.00330420
74′1.3795108−0.74.00.00330430
75′1.3800108−0.74.00.00330410
76′1.3810108−0.74.00.00330410
77′1.3775108−0.74.00.00330400
78′1.3820108−0.74.00.00330400
79′1.3875108−0.74.00.00330400
80′1.3765108−0.74.00.00330400
81′1.3785108−0.74.00.00330400
82′1.3790108−0.74.00.00330200
83′1.3785108−0.74.00.00330310
84′1.3795108−0.74.00.0033060
85′1.3785108−0.74.00.00330180
86′1.3790108−0.74.00.00330200
87′1.3810108−0.74.00.00330180
88′1.3790108−0.74.00.00330170
89′1.3790108−0.74.00.00330410
Second heat treatment
Retention time
Experi-Holdingbetween 300° C.AlloyingPlating
mentaltemperatureand 480° C.temperaturetreatmentAc1Ac3
Example° C.s° C.timing° C.° C.
44′390120480[1]709868
45′410120490[1]725822
46′380120490[1]725822
47′380120480[1]725822
48′380120480[1]725822
49′380120480[1]725822
50′370120480[1]725822
51′370120480[1]725822
52′400120480[1]725822
53′380120480[1]725822
54′400120480[1]725822
55′390120490[1]698953
56′390120490[1]698953
57′380120490[1]758847
58′38080490[1]744878
59′400120[1]744878
60′380120490[1]725837
61′380120490[1]751892
62′400120490[1]706887
63′400120480[1]757880
64′380120490[1]724802
65′380120490[1]733832
66′410120480[1]758871
67′410120490[1]728826
68′420120480[1]741840
69′430120490[1]741840
70′420120490[1]741840
71′420120490[1]741840
72′420120490[1]741840
73′420120490[1]741840
74′420120[1]741840
75′400120490[1]742844
76′410120480[1]737889
77′390120500[1]714816
78′390120490[1]752888
79′400120490[1]803945
80′400120490[1]699853
81′390120500[2]729825
82′400120490[2]729825
83′400120490[2]729825
84′400120500[2]729825
85′390300500[2]729825
86′400120[2]729825
87′380120490[2]746846
88′380120490[2]745812
89′400120490[3]729825
* Underlined values are outside the range of the present invention

[0303]

Next, for the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to No. 89′ thus obtained, the steel structure (the steel structure of the steel sheet inside) in the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface was measured by the above-described method, and the volume fractions of soft ferrite, retained austenite, tempered martensite, fresh martensite, sum of pearlite and cementite, hard ferrite, and bainite were examined.

[0304]

In addition, for the steel sheet inside of the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the number proportion of retained austenite having an aspect ratio of 2.0 or more in the total retained austenite was examined by the above-described method.

[0305]

The results are shown in Tables 14 to 17.

[0000]

Internal structure
Retained austenite
Proportion
Experi-Softwith aspectTemperedFreshPearlite +HardPrimary
mentalferriteFractionratio ≥2.0martensitemartensitecementiteBainiteferriteresidual
Examplevol %vol %%%vol %vol %vol %vol %structureNote
1614830401561Hard αPresent Invention
23114410701434Hard αComparative Example
3514840301167Hard αPresent Invention
4814660501558Hard αPresent Invention
5614440403046Hard αComparative Example
6613890401166Hard αComparative Example
723 12710302438Hard αPresent Invention
83913700303114BainiteComparative Example
9914840301559Hard αComparative Example
10712820401661Hard αPresent Invention
11381346060430BainiteComparative Example
12513830501463Hard αPresent Invention
13516842040055Hard αPresent Invention
146157621301045Hard αPresent Invention
15517811940946Hard αComparative Example
16515871540952Hard αComparative Example
1728 15452350280BainiteComparative Example
18026812590040Hard αPresent Invention
19021641618 0739Hard αPresent Invention
20027742570041Hard αComparative Example
21025832670637Hard αPresent Invention
2221  7870401256Hard αPresent Invention
237 5900501568Hard αPresent Invention
248 6810501665Hard αComparative Example
254 5830401572Hard αComparative Example
2610 2504350400BainiteComparative Example
2719  7760301457Hard αPresent Invention
288 6860201569Hard αPresent Invention
29401572820290BainiteComparative Example
30610760401565Hard αPresent Invention
31612820401563Hard αPresent Invention
32810800401563Hard αPresent Invention
335 8810401370Hard αPresent Invention
34420830601357Hard αPresent Invention
359188303201031Hard αComparative Example
3671985014 01149Hard αPresent Invention
3781878040862Hard αPresent Invention
3819 17381410 0329BainiteComparative Example
39423780901351Hard αPresent Invention
* Underlined values are outside the range of the present invention

[0000]

Internal structure
Retained austenite
Proportion
Experi-Softwith aspectTemperedFreshPearlite +HardPrimary
mentalferriteFractionratio ≥2.0martensitemartensitecementiteBainiteferriteresidual
Examplevol %vol %%%vol %vol %vol %vol %structureNote
40613790501759Hard αPresent Invention
41714560501460Hard αPresent Invention
427 5870461266Hard αPresent Invention
43727502121265Hard αComparative Example
44612790401365Hard αPresent Invention
4511 15840501455Hard αPresent Invention
4625 14750501145Hard αPresent Invention
4711 1242090680BainiteComparative Example
4813 1447090640BainiteComparative Example
49713600401363Hard αPresent Invention
5010 13780301460Hard αPresent Invention
51913880301263Hard αComparative Example
5224 1285037846Hard αPresent Invention
539 68401101064Hard αPresent Invention
54510860301567Hard αPresent Invention
557 48431002038Hard αPresent Invention
568 5890501864Hard αPresent Invention
57610840201567Hard αPresent Invention
58113880501269Hard αPresent Invention
59016860701265Hard αPresent Invention
60014900301667Hard αPresent Invention
61014880501764Hard αPresent Invention
6225  58418061135Hard αPresent Invention
63218900401660Hard αPresent Invention
6460026860BainiteComparative Example
65411850301270Hard αComparative Example
66317850401462Hard αPresent Invention
67316630401760Hard αPresent Invention
6812 136510701246Hard αPresent Invention
69419860401162Hard αPresent Invention
70615890401857Hard αPresent Invention
7125 2840501157Hard αComparative Example
7213  5790201664Hard αComparative Example
7368 537018216Hard αComparative Example
743188301301452Hard αComparative Example
750 8420250958Hard αComparative Example
76614780501659Hard αPresent Invention
77812810401561Hard αPresent Invention
7821 14700601247Hard αPresent Invention
* Underlined values are outside the range of the present invention

[0000]

Internal structure
Retained austenite
Proportion
Experi-Softwith aspectTemperedFreshPearlite +HardPrimary
mentalferriteFractionratio ≥2.0martensitemartensitecementiteBainiteferriteresidual
Examplevol %vol %%%vol %vol %vol %vol %structureNote
 1′616780301758Hard αPresent Invention
 2′3614410401432Hard αComparative Example
 3′514840201168Hard αComparative Example
 4′914640401459Hard αPresent Invention
 5′713380403145Hard αComparative Example
 6′915900401062Hard αComparative Example
 7′22 13720402833Hard αPresent Invention
 8′3713650503213BainiteComparative Example
 9′714820201463Hard αComparative Example
10′914800401063Hard αPresent Invention
11′714870401659Hard αPresent Invention
12′614790301661Hard αPresent Invention
13′515860501659Hard αPresent Invention
14′13 15750401256Hard αPresent Invention
15′41 938070430BainiteComparative Example
16′615790301363Hard αPresent Invention
17′715910401361Hard αPresent Invention
18′318871830256Hard αPresent Invention
19′3159520301346Hard αPresent Invention
20′717751840747Hard αComparative Example
21′5169314301151Hard αComparative Example
22′26 14432550300BainiteComparative Example
23′028752470041Hard αPresent Invention
24′021591619 0737Hard αPresent Invention
25′028712470437Hard αComparative Example
26′025772470539Hard αPresent Invention
27′20  6930201062Hard αPresent Invention
28′6 4850401571Hard αPresent Invention
29′8 5790501270Hard αComparative Example
30′3 6820401770Hard αComparative Example
31′9 5474350380BainiteComparative Example
32′19  6780401556Hard αPresent Invention
33′7 5930401272Hard αPresent Invention
34′392522820290BainiteComparative Example
35′511840301467Hard αPresent Invention
36′713870301463Hard αPresent Invention
37′710880301862Hard αPresent Invention
38′7 8890201667Hard αPresent Invention
39′618790701455Hard αPresent Invention
40′8177403301032Hard αComparative Example
41′41889015 0855Hard αPresent Invention
42′818840401555Hard αPresent Invention
43′18 17401410 02912BainiteComparative Example
* Underlined values are outside the range of the present invention

[0000]

Internal structure
Retained austenite
Proportion
Experi-Softwith aspectTemperedFreshPearlite +HardPrimary
mentalferriteFractionratio ≥2.0martensitemartensitecementiteBainiteferriteresidual
Examplevol %vol %%%vol %vol %vol %vol %structureNote
44′322790801651Hard αPresent Invention
45′615910301264Hard αPresent Invention
46′415680401562Hard αPresent Invention
47′6 6780561760Hard αPresent Invention
48′7 38201131363Hard αComparative Example
49′612800501265Hard αPresent Invention
50′813780301165Hard αPresent Invention
51′27 1385040848Hard αPresent Invention
52′12 1245090670BainiteComparative Example
53′12 1447090650BainiteComparative Example
54′610630401268Hard αPresent Invention
55′11 13800101164Hard αPresent Invention
56′913830301758Hard αComparative Example
57′24 1279027847Hard αPresent Invention
58′9 89401201061Hard αPresent Invention
59′611800301466Hard αPresent Invention
60′7 58333101836Hard αPresent Invention
61′7 4840601370Hard αPresent Invention
62′510830201271Hard αPresent Invention
63′214820401268Hard αPresent Invention
64′016860701661Hard αPresent Invention
65′016840201369Hard αPresent Invention
66′016870401169Hard αPresent Invention
67′23  5841616842Hard αPresent Invention
68′117850501859Hard αPresent Invention
69′4180026870BainiteComparative Example
70′414890501265Hard αComparative Example
71′318810201562Hard αPresent Invention
72′318630401560Hard αPresent Invention
73′12 116410601249Hard αPresent Invention
74′317820401363Hard αPresent Invention
75′716850501656Hard αPresent Invention
76′26 2880401454Hard αComparative Example
77′11  4870301270Hard αComparative Example
78′68136018319Hard αComparative Example
79′4208601301251Hard αComparative Example
80′0 64502601157Hard αComparative Example
81′717830501358Hard αPresent Invention
82′620872040941Hard αPresent Invention
83′61982540858Hard αPresent Invention
84′615884310431Hard αPresent Invention
85′417852420845Hard αPresent Invention
86′5198218201046Hard αPresent Invention
87′319882410746Hard αPresent Invention
88′029744150520Hard αPresent Invention
89′611826101561Hard αPresent Invention
* Underlined values are outside the range of the present invention

[0306]

Next, for the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the steel structure and hardness were measured by the above-described method, and the thickness of the soft layer, the volume fraction of ferrite having an aspect ratio of 3.0 or more in the ferrite in the soft layer, and the ratio between the volume fractions of the retained austenite in the soft layer and the retained austenite in the steel sheet inside were examined. The results are shown in Tables 18 to 21.

[0307]

Furthermore, for the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the peak of the emission intensity at a wavelength indicating Si was analyzed in the depth direction from the surface by the radio-frequency glow discharge analysis method, and whether or not a peak (a peak indicating that an internal oxide layer containing Si oxides was present) of the emission intensity at a wavelength indicating Si had appeared in a depth range of more than 0.2 μm to 10.0 μm or less was examined.

[0308]

In addition, for the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the peak of the emission intensity at a wavelength indicating Si appearing between the depths of more than 0.2 μm and 10.0 μm or less in the depth direction from the surface was evaluated as an internal oxide peak “present”, and no peak appeared was evaluated as an internal oxide peak “absent”. The results are shown in Tables 18 to 21.

[0000]

Surface layer structure
Proportion of ferriteResidual γ in soft
Soft layerhaving aspect ratiolayer/residual γ ofInternal
Experimentalthicknessof 3.0 or moresteel sheet insideoxide
Exampleμm%%peakNote
1287125PresentPresent Invention
2344822PresentComparative Example
3358527PresentPresent Invention
4326323PresentPresent Invention
5317826PresentComparative Example
6382517PresentComparative Example
7355325PresentPresent Invention
8474420PresentComparative Example
90AbsentComparative Example
10217572PresentPresent Invention
11291826PresentComparative Example
12308329PresentPresent Invention
13387630PresentPresent Invention
14357728PresentPresent Invention
15292782PresentComparative Example
16432116PresentComparative Example
17401418PresentComparative Example
18477920PresentPresent Invention
19557122PresentPresent Invention
200AbsentComparative Example
21508225PresentPresent Invention
22156019PresentPresent Invention
23176518PresentPresent Invention
24162084PresentComparative Example
250AbsentComparative Example
26203533PresentComparative Example
27235221PresentPresent Invention
28167310PresentPresent Invention
29202912PresentComparative Example
30267321PresentPresent Invention
31297724PresentPresent Invention
32228415PresentPresent Invention
33228012PresentPresent Invention
34357120PresentPresent Invention
35357623PresentComparative Example
36397514PresentPresent Invention
373285 9PresentPresent Invention
38353728PresentComparative Example
39417825PresentPresent Invention
* Underlined values are outside the range of the present invention

[0000]

Surface layer structure
Proportion of ferriteResidual γ in soft
Soft layerhaving aspect ratiolayer/residual γ ofInternal
Experimentalthicknessof 3.0 or moresteel sheet insideoxide
Exampleμm%%peakNote
40337923PresentPresent Invention
41338528PresentPresent Invention
42168045PresentPresent Invention
434160 0PresentComparative Example
44358430PresentPresent Invention
45308125PresentPresent Invention
46317825PresentPresent Invention
47332618PresentComparative Example
480AbsentComparative Example
49348227PresentPresent Invention
502690 7PresentPresent Invention
510AbsentComparative Example
521986 4PresentPresent Invention
53218015PresentPresent Invention
54208523PresentPresent Invention
553070 0PresentPresent Invention
561881 0PresentPresent Invention
57308018PresentPresent Invention
58257414PresentPresent Invention
59287018PresentPresent Invention
60268518PresentPresent Invention
61297016PresentPresent Invention
62347815PresentPresent Invention
63268826PresentPresent Invention
642581 0PresentComparative Example
6511276 5PresentComparative Example
66405911PresentPresent Invention
67318523PresentPresent Invention
68328218PresentPresent Invention
69297521PresentPresent Invention
70226831PresentPresent Invention
711056 0PresentComparative Example
72256425PresentComparative Example
731730 0PresentComparative Example
74457530PresentComparative Example
75215618PresentComparative Example
76308521PresentPresent Invention
77138020PresentPresent Invention
78446611PresentPresent Invention
* Underlined values are outside the range of the present invention

[0000]

Surface layer structure
Proportion of ferriteResidual γ in soft
Soft layerhaving aspect ratiolayer/residual γ ofInternal
Experimentalthicknessof 3.0 or moresteel sheet insideoxide
Exampleμm%%peakNote
 1′318228PresentPresent Invention
 2′364519PresentComparative Example
 3′338924PresentPresent Invention
 4′306627PresentPresent Invention
 5′356025PresentComparative Example
 6′392415PresentComparative Example
 7′325530PresentPresent Invention
 8′333920PresentComparative Example
 9′0AbsentComparative Example
10′147774PresentPresent Invention
11′268133PresentPresent Invention
12′407728PresentPresent Invention
13′209044PresentPresent Invention
14′436513PresentPresent Invention
15′323625PresentComparative Example
16′388623PresentPresent Invention
17′397530PresentPresent Invention
18′538522PresentPresent Invention
19′508024PresentPresent Invention
20′343183PresentComparative Example
21′582714PresentComparative Example
22′0AbsentComparative Example
23′518529PresentPresent Invention
24′538228PresentPresent Invention
25′0AbsentComparative Example
26′558333PresentPresent Invention
27′185417PresentPresent Invention
28′166115PresentPresent Invention
29′123082PresentComparative Example
30′0AbsentComparative Example
31′223419PresentComparative Example
32′185620PresentPresent Invention
33′175920PresentPresent Invention
34′203522PresentComparative Example
35′267122PresentPresent Invention
36′317525PresentPresent Invention
37′258512PresentPresent Invention
38′2578 9PresentPresent Invention
39′366918PresentPresent Invention
40′397323PresentComparative Example
41′437712PresentPresent Invention
42′378710PresentPresent Invention
43′403524PresentComparative Example
* Underlined values are outside the range of the present invention

[0000]

Surface layer structure
Proportion of ferriteResidual γ in soft
Soft layerhaving aspect ratiolayer/residual γ ofInternal
Experimentalthicknessof 3.0 or moresteel sheet insideoxide
Exampleμm%%peakNote
44′448022PresentPresent Invention
45′337925PresentPresent Invention
46′378528PresentPresent Invention
47′218344PresentPresent Invention
48′4163 0PresentComparative Example
49′358932PresentPresent Invention
50′358224PresentPresent Invention
51′327824PresentPresent Invention
52′343116PresentComparative Example
53′0AbsentComparative Example
54′348125PresentPresent Invention
55′2988 8PresentPresent Invention
56′0AbsentComparative Example
57′2182 6PresentPresent Invention
58′268314PresentPresent Invention
59′208124PresentPresent Invention
60′3269 0PresentPresent Invention
61′2180 0PresentPresent Invention
62′308320PresentPresent Invention
63′307013PresentPresent Invention
64′337319PresentPresent Invention
65′278718PresentPresent Invention
66′316615PresentPresent Invention
67′357517PresentPresent Invention
68′288427PresentPresent Invention
69′3182 0PresentComparative Example
70′11572 4PresentComparative Example
71′406012PresentPresent Invention
72′338624PresentPresent Invention
73′358420PresentPresent Invention
74′337521PresentPresent Invention
75′226432PresentPresent Invention
76′ 955 0PresentComparative Example
77′246623PresentComparative Example
78′1831 0PresentComparative Example
79′457532PresentComparative Example
80′225815PresentComparative Example
81′378920PresentPresent Invention
82′368431PresentPresent Invention
83′428428PresentPresent Invention
84′408424PresentPresent Invention
85′368623PresentPresent Invention
86′378327PresentPresent Invention
87′449121PresentPresent Invention
88′498524PresentPresent Invention
89′357729PresentPresent Invention
* Underlined values are outside the range of the present invention

[0309]

For the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the maximum tensile stress (TS), elongation (El), hole expansibility (hole expansion ratio), hydrogen embrittlement resistance of a bent portion, chemical convertibility, and plating adhesion were examined. The results are shown in Tables 22 to 25.

[0310]

A JIS No. 5 tensile test piece was taken so that the direction perpendicular to the rolling direction was the tensile direction, the maximum tensile stress and elongation were measured according to JIS Z 2241, and the hole expansibility was measured according to JIS Z 2256. Those having a maximum tensile stress of 700 MPa or more were evaluated as good.

[0311]

In addition, in order to evaluate the balance between strength, elongation, and hole expansibility, a value represented by Expression (11) was calculated using the results of the maximum tensile stress (TS), elongation (El), and hole expansibility (hole expansion ratio) measured by the above-described methods. The larger the value represented by Expression (11), the better the balance between strength, elongation, and hole expansibility. Those having a value of Expression (11) of 80×10−7or more were evaluated as good.

[0000]


TS2×El×λ  (11)

[0312]

(in Expression (11), TS represents the maximum tensile stress (MPa), El represents the elongation (%), and λ represents the hole expansibility (%))

[0313]

The results are shown in Tables 22 to 25.

[0314]

The hydrogen embrittlement resistance of the bent portion was evaluated by the following method.

[0315]

First, a strip-shaped test piece of 30 mm×120 mm was taken from a steel sheet so that the longitudinal direction of the test piece and the rolling direction of the steel sheet were perpendicular to each other, and both ends of the test piece were drilled for bolt fastening. Next, the test piece was bent by 180° with a punch having a radius of 5 mm. Thereafter, the U-bending test piece after springback was fastened with a bolt and a nut to apply stress. At this time, a GL-5 mm strain gauge was attached to the top portion of the U-bending test piece, and a stress of 0.8 times the tensile strength was applied by controlling the amount of strain. At that time, the stress was set by converting the strain into a stress from a stress-strain curve obtained in advance by a tensile test. The end surface of the U-bending test piece was subjected to shear-cut.

[0316]

The U-bending test piece after the stress was applied was continuously subjected to cathodic hydrogen charging using an electrochemical cell until the test piece fractured. An electrolyte used was a 3% NaCl aqueous solution to which 3 g/L of ammonium thiocyanate was added, and a charge current density was −0.05 mA/cm2. The test piece after fracture was immediately stored in liquid nitrogen, and the amount of hydrogen in the steel was measured by a temperature-programmed hydrogen analysis method (temperature rising rate: 100° C./hour, measured up to 300° C.) using a gas chromatograph. The amount of hydrogen released from the steel material from room temperature to 200° C. was determined as the amount of diffusible hydrogen.

[0317]

The same test was performed 3 times, and the average value was defined as the limit diffusion hydrogen amount. For materials having a tensile strength of 1100 MPa or less, those with a limit diffusion hydrogen amount of 1.0 ppm or more were determined as “Ex”, those with 0.6 to 1.0 ppm as “G”, and those with less than 0.6 ppm as “B”. For materials with a tensile strength of more than 1100 MPa and less than 1350 MPa, those with a limit diffusion hydrogen amount of 0.8 ppm or more were determined as “Ex”, those with 0.5 to 0.8 ppm as “G”, and those with less than 0.5 ppm as “B”. For materials with a tensile strength of more than 1350 MPa, those with a limit diffusion hydrogen amount of 0.6 ppm or more were determined as “Ex”, those with 0.3 to 0.6 ppm as “G”, and those with less than 0.3 ppm as “B”.

[0318]

In addition, for the steel sheets of Experimental Examples Nos. 1 to 78 excluding Nos. 54 and 69, chemical convertibility was measured by the following method.

[0319]

The steel sheet was cut into 70 mm×150 mm, and an 18 g/l aqueous solution of a degreasing agent (trade name: FINECLEANER E2083) manufactured by Nihon Parkerizing Co., Ltd. was sprayed and applied thereto at 40° C. for 120 seconds. Next, the steel sheet to which the degreasing agent was applied was washed with water to be degreased, and immersed in a 0.5 g/l aqueous solution of a surface conditioner (trade name: PREPALENE XG) manufactured by Nippon Parkerizing Co., Ltd. at room temperature for 60 seconds. Thereafter, the steel sheet to which the surface conditioner was applied was immersed in a zinc phosphate treatment agent (trade name: PALBOND L3065) manufactured by Nippon Parkerizing Co., Ltd. for 120 seconds, washed with water, and dried. As a result, a chemical conversion film formed of the zinc phosphate coating was formed on the surface of the steel sheet.

[0320]

A test piece having a width of 70 μmm and a length of 150 mm was taken from the steel sheet on which the chemical conversion film was formed. Thereafter, three locations (center portion and both end portions) along the length direction of the test piece were observed with a scanning electron microscope (SEM) at a magnification of 1,000 folds. For each test piece, the degree of adhesion of grains of the chemical conversion film was evaluated according to the following criteria.

[0321]

“Ex” Zinc phosphate crystals of the chemical conversion film are densely attached to the surface.

[0322]

“G” Zinc phosphate crystals are sparse, and there is a slight gap between adjacent crystals (a portion commonly referred to as “lack of hiding” where the zinc phosphate coating is not attached).

[0323]

“B” Points that are not coated with the chemical conversion coating are clearly seen on the surface.

[0324]

“EG”, “GI”, and “GA” described regarding the surface in Tables 21 to 25 respectively indicate an electrogalvanized steel sheet, a hot-dip galvanized steel sheet, and a hot-dip galvannealed steel sheet.

[0325]

In addition, for the steel sheets of Experimental Examples Nos. 54, 69, and 1′ to 89′, the plating adhesion was measured by the method described below.

[0326]

A 30 mm×100 mm test piece was taken from these steel sheets and subjected to a 90° V bending test. Thereafter, a commercially available sellotape (registered trademark) was attached along the bend ridge, and the width of the plating attached to the tape was measured as the peeling width. The evaluation was performed as follows.

[0327]

Ex: Small plating peeling (peeling width less than 5 mm)

[0328]

G: Peeling to the extent that there is no practical problem (peeling width of 5 mm or more and less than 10 mm)

[0329]

B: Peeling is severe (peeling width 10 mm or more)

[0330]

The plating adhesion grades Ex and G were determined to be acceptable.

[0331]

The evaluation results for each experimental example will be described below.

[0000]

1101229.830.153161ExExPresent Invention
298531.731.21546BExComparative Example
3101628.529.048141ExGPresent Invention
4106228.830.635113ExExPresent Invention
5103828.229.32576ExExComparative Example
6105628.129.650156BExComparative Example
796829.728.839108GExPresent Invention
890833.630.52877BExComparative Example
9104527.929.148145BBComparative Example
10100528.228.448136GGPresent Invention
1194332.230.41646BExComparative Example
12102228.328.950148ExExPresent Invention
13119622.326.746149ExExPresent Invention
14119422.026.350155ExExPresent Invention
15124321.726.943145BExComparative Example
16122022.727.746156BExComparative Example
17123120.725.52270BExComparative Example
18151321.532.528139ExExPresent Invention
19160719.631.51681ExExPresent Invention
20155021.733.730156BBComparative Example
21149021.932.731152ExExPresent Invention
2272337.026.752100ExExPresent Invention
2381732.526.554117ExExPresent Invention
2483231.826.454118BExComparative Example
2584731.626.353119BBComparative Example
2611339.811.13949BExComparative Example
2773632.123.65495ExExPresent Invention
2877530.123.360109ExExPresent Invention
2987920.117.65078BExComparative Example
3096328.026.950130ExExPresent Invention
3193428.226.349122ExExPresent Invention
3291127.625.249113ExExPresent Invention
3391527.825.454126ExExPresent Invention
34118727.232.242159ExExPresent Invention
35156023.035.9845BExComparative Example
36135725.134.124113ExExPresent Invention
37116927.231.838142ExExPresent Invention
38136821.829.8937BExComparative Example
39131226.434.62298ExExPresent Invention

[0000]

40102027.628.245130ExExPresent Invention
41101027.227.438106ExExPresent Invention
42102923.524.23895ExExPresent Invention
4391822.921.03261ExExComparative Example
4499126.125.850128ExExPresent Invention
45100426.326.444117ExExPresent Invention
4693929.127.342109ExExPresent Invention
47109725.628.12371BExComparative Example
48113026.329.82273BBComparative Example
49102728.128.940120ExExPresent Invention
5096927.927.052137ExExPresent Invention
51101827.928.448137BBComparative Example
5291930.127.73898ExExPresent Invention
53104123.224.23999ExExPresent Invention
54EG89428.325.356128ExExPresent Invention
55106515.216.163108ExExPresent Invention
5682628.423.554105ExExPresent Invention
5794527.525.954133ExExPresent Invention
58101027.928.240114ExExPresent Invention
59121824.630.041148ExExPresent Invention
60104526.627.853153ExExPresent Invention
61105527.328.849147ExExPresent Invention
6297422.021.549102ExExPresent Invention
63108227.329.551162ExExPresent Invention
6487519.216.84668BExComparative Example
6569131.721.95481ExExComparative Example
66109227.229.745145ExGPresent Invention
67109527.530.137121ExExPresent Invention
68116722.125.83399ExExPresent Invention
69EG107728.530.649160ExExPresent Invention
70101428.028.447136ExExPresent Invention
7161138.423.55072ExExComparative Example
7291226.123.81737ExExComparative Example
7364833.221.585118ExExComparative Example
74119821.525.7618BExComparative Example
7514619.513.848BExComparative Example
76104626.527.753154ExExPresent Invention
77101027.527.852146ExExPresent Invention
7898127.727.238101ExExPresent Invention

[0000]

 1′GA101827.327.850141ExExPresent Invention
 2′GA103329.430.31341BExComparative Example
 3′GA99834.334.261208ExGPresent Invention
 4′GA103228.329.23297ExExPresent Invention
 5′GA104027.428.52472ExExComparative Example
 6′GA101928.328.845132BExComparative Example
 7′GA94929.628.138103ExExPresent Invention
 8′GA87732.928.82769BExComparative Example
 9′GA103225.826.648131BBComparative Example
10′GA104926.427.748141GGPresent Invention
11′GA104025.226.253143ExExPresent Invention
12′GA104028.329.448145ExGPresent Invention
13′GA108328.931.349166ExExPresent Invention
14′GA95232.230.737108ExExPresent Invention
15′GA96532.331.21443BExComparative Example
16′GA103627.328.344129ExExPresent Invention
17′GI101829.129.753159ExExPresent Invention
18′GA121021.125.542130ExExPresent Invention
19′GA123820.925.952167ExExPresent Invention
20′GA125222.327.942148BExComparative Example
21′GA122123.929.248172BExComparative Example
22′GA118420.524.22058BBComparative Example
23′GA156920.732.526133ExExPresent Invention
24′GA153320.231.01886ExExPresent Invention
25′GA149520.230.227122BBComparative Example
26′GA145322.232.326122ExExPresent Invention
27′GA71639.027.94794ExExPresent Invention
28′GA82431.726.157124ExExPresent Invention
29′GA83330.925.754115BExComparative Example
30′GA83829.825.052109BBComparative Example
31′GA111312.814.24064BExComparative Example
32′GA77133.325.756111ExExPresent Invention
33′GA74929.422.066109ExExPresent Invention
34′GA86820.217.64975BExComparative Example
35′GA93529.127.250126ExExPresent Invention
36′GA94827.426.047117ExExPresent Invention
37′GA86129.125.052112ExExPresent Invention
38′GA87028.224.553114ExExPresent Invention
39′GA121126.131.639151ExExPresent Invention
40′GA156823.036.11374ExExComparative Example
41′GA130525.132.726111ExExPresent Invention
42′GA110028.030.837127ExExPresent Invention
43′GA131622.129.01869ExExComparative Example

[0000]

44′GA134025.734.423106ExExPresent Invention
45′GA106928.930.947154ExExPresent Invention
46′GA102227.428.041116ExExPresent Invention
47′GA100323.423.53786ExExPresent Invention
48′GA92322.120.43565ExExComparative Example
49′GA105124.625.850136ExExPresent Invention
50′GA96827.226.442107ExExPresent Invention
51′GA88029.125.64294ExExPresent Invention
52′GA114825.729.51758BExComparative Example
53′GA108525.727.81957BBComparative Example
54′GA109428.831.532110ExExPresent Invention
55′GA91827.024.845103ExExPresent Invention
56′GA104925.827.154153BBComparative Example
57′GA94330.028.239103ExExPresent Invention
58′GA107522.924.741108ExExPresent Invention
59′GI88527.124.059124ExExPresent Invention
60′GA105116.016.857100ExExPresent Invention
61′GA82429.924.64897ExExPresent Invention
62′GA97727.827.156150ExExPresent Invention
63′GA102028.729.237111ExExPresent Invention
64′GA125825.732.343173ExExPresent Invention
65′GA101628.729.257169ExExPresent Invention
66′GA102827.728.551149ExExPresent Invention
67′GA98022.421.94086ExExPresent Invention
68′GA111627.330.444148ExExPresent Invention
69′GA91418.817.24469ExExComparative Example
70′GA68434.123.35587ExExComparative Example
71′GA105628.630.244140ExGPresent Invention
72′GA107527.529.542132ExExPresent Invention
73′GA113022.525.43396ExExPresent Invention
74′GI107427.829.946148ExExPresent Invention
75′GA101729.329.846139ExExPresent Invention
76′GA62837.023.25175ExExComparative Example
77′GA86824.821.61631ExExComparative Example
78′GA65632.821.582116ExExComparative Example
79′GA122920.825.539BExComparative Example
80′GA15349.113.9816BExComparative Example
81′GA103829.730.848154ExExPresent Invention
82′GA105526.928.457171ExExPresent Invention
83′GA105429.130.751165ExExPresent Invention
84′GA112422.325.144124ExExPresent Invention
85′GA102627.728.458169ExExPresent Invention
86′GI101829.630.151156ExExPresent Invention
87′GA126321.827.545156ExExPresent Invention
88′GA160919.731.731158ExExPresent Invention
89′GA93625.624.056126ExExPresent Invention

[0332]

Experimental Examples Nos. 1, 3, 4, 7, 10, 12 to 14, 18, 19, 21 to 23, 27, 28, 30 to 34, 36, 37, 39 to 42, 44 to 46, 49, 50, 52 to 63, 66 to 70, 76 to 78, 1′, 3′, 4′, 7′, 10′ to 14′, 16′ to 19′, 23′, 24′, 26′ to 28′, 32′, 33′, 35′ to 39′, 41′, 42′, 44′ to 47′, 49′ to 51′, 54′, 55′, 57′ to 68′, 71′ to 75′, and 81′ to 89′, which are examples of the present invention, had high strength, excellent ductility and hole expansibility, and good bendability after working, chemical convertibility, and plating adhesion.

[0333]

Regarding the steel sheets of Experimental Examples Nos. 11, 17, 29, 47, and 48, since the first heat treatment was not performed and the metallographic structure did not contain hard ferrite, the balance between strength, elongation, and hole expansion ratio was poor.

[0334]

In the steel sheet of Experimental Example No. 2, since the highest heating temperature in the first heat treatment was low, the amount of soft ferrite is large, and the number proportion of retained austenite having an aspect ratio of 2.0 or more is insufficient, so that the balance between strength, elongation, and hole expansion ratio was poor.

[0335]

In the steel sheet of Experimental Example No. 5, since the average heating rate from 650° C. to the highest heating temperature in the first heat treatment was slow, the number proportion of retained austenite having an aspect ratio of 2.0 or more was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0336]

In the steel sheets of Experimental Examples Nos. 6, 15, 16, and 24, since the log(PH2O/PH2) in the first heat treatment was high and a desired surface layer structure could not be obtained, the hydrogen embrittlement of the bent portion was poor.

[0337]

In the steel sheet of Experimental Example No. 8, since the cooling rate in the first heat treatment was slow, the fraction of soft ferrite in the internal structure of the steel sheet was large. For this reason, the steel sheet of Experimental Example No. 8 had a poor balance between strength, elongation, and hole expansion ratio.

[0338]

In the steel sheets of Experimental Examples Nos. 9, 15, 20, 25, 48, and 51, since the log(PH2O/PH2) in the second heat treatment was low and a desired surface layer structure could not be obtained, the hydrogen embrittlement resistance of the bent portion was poor.

[0339]

Regarding the steel sheets of Experimental Examples Nos. 9, 20, 25, 48, and 51, since there was no internal oxidation peak, the chemical convertibility was evaluated as “B”.

[0340]

In the steel sheet of Experimental Example No. 26, since the highest heating temperature in the second heat treatment was high, the metallographic structure did not contain hard ferrite, and furthermore, a desired surface layer structure could not be obtained. Therefore, the balance between strength, elongation, and hole expansion ratio was poor, and the hydrogen embrittlement resistance of the bent portion was poor.

[0341]

In the steel sheet of Experimental Example No. 35, since the retention time at 300° C. to 480° C. in the second heat treatment was insufficient, the fraction of fresh martensite in the internal structure was large, and the balance between strength, elongation and hole expansion ratio was poor.

[0342]

In the steel sheet of Experimental Example No. 38, since the cooling stop temperature in the first heat treatment was high, the number proportion of retained austenite having an aspect ratio of 2.0 or more was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0343]

In the steel sheet of Experimental Example No. 43, since the cooling rate in the second heat treatment was slow, the fraction of the sum of pearlite and cementite in the internal structure of the steel sheet was large, and the balance between strength, elongation, and hole expansion ratio was poor.

[0344]

In the steel sheet of Experimental Example No. 64, since the highest heating temperature in the second heat treatment was low, the fraction of retained austenite in the internal structure of the steel sheet was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0345]

In the steel sheet of Experimental Example No. 65, since the log(PH2O/PH2) in the second heat treatment was large, the thickness of the soft layer in the surface layer structure of the steel sheet was large, and the maximum tensile stress (TS) was insufficient.

[0346]

In the steel sheets of Experimental Examples Nos. 71 to 75, the chemical composition was outside the range of the present invention. In the steel sheet of Experimental Example No. 71, since the C content was insufficient, the maximum tensile stress (TS) was insufficient. In the steel sheet of Experimental Example No. 72, since the Nb content was large, the bendability after working was poor. In the steel sheet of Experimental Example No. 73, since the Mn content was insufficient, the maximum tensile stress (TS) was insufficient. In the steel sheet of Experimental Example No. 74, since the Si content was large, the hole expansibility was poor. In the steel sheet of Experimental Example No. 75, since the Mn content and the P content were large, the elongation and the hole expansibility were poor.

[0347]

In the steel sheets of Experimental Examples No. 15′, 22′, 34′, 52′, and 53′, since the first heat treatment was not performed, the metallographic structure did not contain hard ferrite, so that the balance between strength, elongation, and hole expansion ratio was poor.

[0348]

In the steel sheet of Experimental Example No. 2′, since the highest heating temperature in the first heat treatment was low, the number proportion of retained austenite having an aspect ratio of 2.0 or more was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0349]

In the steel sheet of Experimental Example No. 5′, since the average heating rate from 650° C. to the highest heating temperature in the first heat treatment was slow, the number proportion of retained austenite having an aspect ratio of 2.0 or more was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0350]

In the steel sheets of Experimental Examples Nos. 6′, 20′, 21′, and 29′, since the log(PH2O/PH2) in the first heat treatment was high and a desired surface layer structure could not be obtained, the hydrogen embrittlement of the bent portion was poor.

[0351]

In the steel sheet of Experimental Example No. 8′, since the cooling rate in the first heat treatment was slow, the fraction of soft ferrite was large. Therefore, the balance between strength, elongation, and hole expansion ratio was poor.

[0352]

In the steel sheets of Experimental Examples Nos. 9′, 20′, 22′, 25′, 29′, 30′, 53′, and 56′, since the log(PH2O/PH2) in the second heat treatment was low and a desired surface layer structure could not be obtained, the hydrogen embrittlement resistance of the bent portion was poor.

[0353]

Regarding the steel sheets of Experimental Examples No. 9′, 22′, 25′, 30′, 53′ and 56′, since no soft layer was formed in the surface layer structure of the steel sheet and there was no internal oxidation peak, the plating adhesion was evaluated as “B”.

[0354]

In the steel sheet of Experimental Example No. 31′, since the maximum attainment temperature in the second heat treatment was high, the metallographic structure did not contain hard ferrite, and furthermore, a desired surface layer structure could not be obtained. Therefore, the balance between strength, elongation, and hole expansion ratio was poor, and the hydrogen embrittlement resistance of the bent portion was poor.

[0355]

In the steel sheet of Experimental Example No. 40′, since the retention time at 300° C. to 480° C. in the second heat treatment was insufficient, the fraction of fresh martensite in the internal structure was large, and the balance between strength, elongation and hole expansion ratio was poor.

[0356]

In the steel sheet of Experimental Example No. 43′, since the cooling stop temperature in the first heat treatment was high, the number proportion of retained austenite having an aspect ratio of 2.0 or more was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0357]

In the steel sheet of Experimental Example No. 48′, since the cooling rate in the second heat treatment was slow, the fraction of the sum of pearlite and cementite in the internal structure of the steel sheet was large, and the balance between strength, elongation, and hole expansion ratio was poor.

[0358]

In the steel sheet of Experimental Example No. 69′, since the maximum attainment temperature in the second heat treatment was low, the fraction of retained austenite in the internal structure of the steel sheet was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

[0359]

In the steel sheet of Experimental Example No. 70′, since the log(PH2O/PH2) in the second heat treatment was large, the thickness of the soft layer in the surface layer structure of the steel sheet was large, and the maximum tensile stress (TS) was insufficient.

[0360]

In the steel sheets of Experimental Examples Nos. 76′ to 80′, the chemical composition was outside the range of the present invention. In particular, in the steel sheet of Experimental Example No. 76′, since the C content was insufficient, the maximum tensile stress (TS) was insufficient. In the steel sheet of Experimental Example No. 77′, since the Nb content was large, the bendability after working was poor. In the steel sheet of Experimental Example No. 78′, since the Mn content was insufficient, the maximum tensile stress (TS) was insufficient. In the steel sheet of Experimental Example No. 79′, since the Si content was large, the hole expansibility was poor. In the steel sheet of Experimental Example No. 80′, since the Mn content and the P content were large, the elongation and the hole expansibility were poor.

[0361]

While the preferred embodiments and examples of the present invention have been described above, these embodiments and examples are merely examples within the scope of the gist of the present invention, and additions, omissions, substitutions, and other changes of the configuration can be made without departing from the gist of the present invention. That is, the present invention is not limited by the above description, but is limited only by the appended claims, and can be appropriately changed within the scope.

INDUSTRIAL APPLICABILITY

[0362]

According to the present invention, it is possible to provide a high strength steel sheet having excellent ductility and hole expansibility, and excellent chemical convertibility and plating adhesion, and further having good bendability after working, and a method for manufacturing the same.

[0363]

Since the steel sheet of the present invention has excellent ductility and hole expansibility and has good bendability after working, the steel sheet is suitable as a steel sheet for a vehicle which is formed into various shapes by press working or the like. Moreover, since the steel sheet of the present invention is excellent in chemical convertibility and plating adhesion, the steel sheet is suitable as a steel sheet in which a chemical conversion film or a plated layer is formed on the surface.

BRIEF DESCRIPTION OF THE REFERENCE SYMBOLS

[0000]

    • 1 Steel sheet
    • 11 ⅛ to ⅜ thickness range centered on ¼ thickness position from surface of steel sheet (steel sheet inside)
    • 12 Soft layer



This steel sheet has a predetermined chemical composition, in which a steel structure of an inside of the steel sheet contains, by volume fraction, soft ferrite: 0% to 30%, retained austenite: 3% to 40%, fresh martensite: 0% to 30%, a sum of pearlite and cementite: 0% to 10%, and a remainder includes hard ferrite, a number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is 50% or more, a soft layer having a thickness of 1 to 100 μm from a surface in a sheet thickness direction is present, in ferrite contained in the soft layer, a volume fraction of grains having an aspect ratio of 3.0 or more is 50% or more, a volume fraction of retained austenite in the soft layer is 80% or less of the volume fraction of the retained austenite in the inside of the steel sheet, and a peak of an emission intensity at a wavelength indicating Si appears in a range of more than 0.2 μm and 10.0 μm or less from the surface.



1-9. (canceled)

10. A steel sheet comprising, as a chemical composition, by mass %:

C: 0.050% to 0.500%;

Si: 0.01% to 3.00%;

Mn: 0.50% to 5.00%;

P: 0.0001% to 0.1000%;

S: 0.0001% to 0.0100%;

Al: 0.001% to 2.500%;

N: 0.0001% to 0.0100%;

O: 0.0001% to 0.0100%;

Ti: 0% to 0.300%;

V: 0% to 1.00%;

Nb: 0% to 0.100%;

Cr: 0% to 2.00%;

Ni: 0% to 2.00%;

Cu: 0% to 2.00%;

Co: 0% to 2.00%;

Mo: 0% to 1.00%;

W: 0% to 1.00%;

B: 0% to 0.0100%;

Sn: 0% to 1.00%;

Sb: 0% to 1.00%;

Ca: 0% to 0.0100%;

Mg: 0% to 0.0100%;

Ce: 0% to 0.0100%;

Zr: 0% to 0.0100%;

La: 0% to 0.0100%;

Hf: 0% to 0.0100%;

Bi: 0% to 0.0100%;

REM: 0% to 0.0100%; and

a remainder including Fe and impurities,

wherein a steel structure in a ⅛ to ⅜ thickness range centered on a ¼ thickness position from a surface contains, by volume fraction,

a soft ferrite: 0% to 30%,

a retained austenite: 3% to 40%,

a fresh martensite: 0% to 30%,

a sum of pearlite and cementite: 0% to 10%, and

a remainder includes hard ferrite,

in the ⅛ to ⅜ thickness range, a number proportion of the retained austenite having an aspect ratio of 2.0 or more in the total retained austenite is 50% or more,

when a region having a hardness of 80% or less of a hardness of the ⅛ to ⅜ thickness range is defined as a soft layer, the soft layer having a thickness of 1 to 100 μm from the surface in a sheet thickness direction is present,

in ferrite contained in the soft layer, a volume fraction of grains having an aspect ratio of 3.0 or more is 50% or more,

a volume fraction of retained austenite in the soft layer is 80% or less of the volume fraction of the retained austenite in the ⅛ to ⅜ thickness range, and

when an emission intensity at a wavelength indicating Si is analyzed in the sheet thickness direction from the surface by a radio-frequency glow discharge analysis method, a peak of the emission intensity at the wavelength indicating Si appears in a range of more than 0.2 μm and 10.0 μm or less from the surface.

11. The steel sheet according to claim 10,

wherein the chemical composition includes one or two or more of

Ti: 0.001% to 0.300%,

V: 0.001% to 1.00%,

Nb: 0.001% to 0.100%,

Cr: 0.001% to 2.00%,

Ni: 0.001% to 2.00%,

Cu: 0.001% to 2.00%,

Co: 0.001% to 2.00%,

Mo: 0.001% to 1.00%,

W: 0.001% to 1.00%,

B: 0.0001% to 0.0100%,

Sn: 0.001% to 1.00%,

Sb: 0.001% to 1.00%,

Ca: 0.0001% to 0.0100%,

Mg: 0.0001% to 0.0100%,

Ce: 0.0001% to 0.0100%,

Zr: 0.0001% to 0.0100%,

La: 0.0001% to 0.0100%,

Hf: 0.0001% to 0.0100%,

Bi: 0.0001% to 0.0100%, and

REM: 0.0001% to 0.0100%.

12. The steel sheet according to claim 10,

wherein the chemical composition satisfies Expression (i),


Si+0.1×Mn+0.6×Al≥0.35  (i)

(Si, Mn, and Al in the Expression (i) are respectively amounts of corresponding elements by mass %).

13. The steel sheet according to claim 11,

wherein the chemical composition satisfies Expression (i),


Si+0.1×Mn+0.6×Al≥0.35  (i)

(Si, Mn, and Al in the Expression (i) are respectively amounts of corresponding elements by mass %).

14. The steel sheet according to claim 10,

wherein the steel sheet has a hot-dip galvanized layer or an electrogalvanized layer on the surface.

15. The steel sheet according to claim 11,

wherein the steel sheet has a hot-dip galvanized layer or an electrogalvanized layer on the surface.

16. The steel sheet according to claim 12,

wherein the steel sheet has a hot-dip galvanized layer or an electrogalvanized layer on the surface.

17. The steel sheet according to claim 13,

wherein the steel sheet has a hot-dip galvanized layer or an electrogalvanized layer on the surface.

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

performing a first heat treatment satisfying (a) to (e) on a hot-rolled steel sheet which has been obtained by hot-rolling a slab having said chemical composition and pickling, or on a cold-rolled steel sheet which has been obtained by cold-rolling the hot-rolled steel sheet,

where (a) an atmosphere containing 0.1 vol % or more of H2and satisfying Expression (ii) is adopted from 650° C. to a highest heating temperature reached,

(b) holding is performed at the highest heating temperature of Ac3−30° C. to 1000° C. for 1 second to 1000 seconds,

(c) Heating is performed such that an average heating rate in a temperature range from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s, and

(d) After holding at the highest heating temperature, cooling is performed such that an average cooling rate in a temperature range from 700° C. to Ms is 5° C./s or more.

(e) Cooling at the average cooling rate of 5° C./s or more to a cooling stop temperature of Ms or lower; and

thereafter performing a second heat treatment satisfying (A) to (E),

where (A) an atmosphere containing 0.1 vol % or more of H2and 0.020 vol % or less of O2and having a log(PH2O/PH2) satisfying Expression (iii) is adopted from 650° C. to a highest heating temperature reached,

(B) holding is performed at the highest heating temperature of Ac1+25° C. to Ac3−10° C. for 1 second to 1000 seconds,

(C) heating is performed such that an average heating rate from 650° C. to the highest heating temperature is 0.5° C./s to 500° C./s,

(D) cooling is performed such that an average cooling rate in a temperature range of 700° C. to 600° C. is 3° C./s or more, and

(E) After cooling at the average cooling rate of 3° C./s or more, holding is performed at 300° C. to 480° C. for 10 seconds or more,


log(PH2O/PH2)≤−1.1  (ii)


−1.1≤log(PH2O/PH2)≤−0.07  (iii)

(In Expression (ii) and Expression (iii), PH2O represents a partial pressure of water vapor, and PH2represents a partial pressure of hydrogen).

19. The method for manufacturing the steel sheet according to claim 18,

wherein hot-dip galvanizing is performed after the cooling in (D).