USPatent applicationPatented

Steel sheet and manufacturing method of therefor

Granted 20 Sep 2022 · 1 office action

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Abstract

A steel sheet wherein 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 including hard ferrite. In the steel sheet, in a ⅛ to ⅜ thickness range, a proportion of retained austenite having an aspect ratio of 2.0 or more is 50% or more, and a soft layer having a thickness of 1 to 100 μm from a surface in a sheet thickness direction is present. 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 appears in a range of more than 0.2 μm and 5.0 μm or less from the surface.

Description

26 parts
›TECHNICAL FIELD OF THE INVENTION

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

›RELATED ART

In recent years, from the viewpoint of regulating greenhouse gas emissions associated with countermeasures against global warming, a further improvement in fuel efficiency of vehicles is required. In addition, in order to reduce the weight of a vehicle body and secure collision safety, the application of a high strength steel sheet to a component for a vehicle gradually expands.

Needless to say, a steel sheet used for a component for a vehicle is required to have not only strength but also various workability such as press formability and weldability required for forming components. Specifically, from the viewpoint of press formability, a steel sheet is often required to have excellent elongation (total elongation in a tension test; El) and stretch flangeability (hole expansion ratio: λ).

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.

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 Document 2). 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 chemical convertibility and plating adhesion.

Patent Document 3 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 4 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.

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

However, the ductility and hole expansibility of a high strength steel sheet in the related art have not been sufficient to meet the demands of automobile companies in recent years.

In addition, from the viewpoint of securing the safety of occupants, a high strength steel sheet for a vehicle is required to be free from cracking during collision deformation after being processed into a component. Since the deformation applied to the component at the time of collision is mainly bending deformation in many cases, the steel sheet as the material is required to have bendability. The bendability in this case is bendability after the steel sheet receives strain by press working or the like. Therefore, the steel sheet which is to become the material of the component is required to have good bendability even after working.

However, there have been no studies for improving bendability after working.

›PRIOR ART DOCUMENT

Patent Document

[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. 2003-193194

[Patent Document 4] Japanese Unexamined Patent Application, First Publication No. 2003-193193

Non-Patent Document

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

›DISCLOSURE OF THE INVENTION · 1 of 2

Problems to be Solved by the Invention

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 having excellent ductility and hole expansibility and good bendability after working, and a method for manufacturing the same.

Means for Solving the Problem

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. 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.

Specifically, by the first heat treatment, the steel sheet inside has a steel structure primarily containing a lath-like structure such as martensite, and the surface layer has a steel structure primarily containing ferrite. 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 ferrite and having a predetermined thickness. Such a steel sheet has high strength, excellent ductility and hole expansibility, and good bendability after working. In addition, a galvanized steel sheet obtained by performing hot-dip galvanizing on such a steel sheet as a base metal also has excellent ductility and hole expansibility, and good bendability after working.

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.

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

(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 less than 3.0 is 50% or more, a volume fraction of retained austenite in the soft layer is less than 50% 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 5.0 μm or less from the surface.

(2) In the steel sheet according to (1), wherein the chemical composition may include 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%.

(3) In the steel sheet according to (1) or (2), wherein the chemical composition may include 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%.

(4) In the steel sheet according to any one of (1) to (3), wherein the chemical composition may include one or two selected from the group consisting of Sn: 0.001% to 1.00%, and Sb: 0.001% to 1.00% may be contained.

(5) In the steel sheet according to any one of (1) to (4), wherein the chemical composition may include 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%.

(6) In the steel sheet according to any one of (1) to (5), the chemical composition may satisfy Expression (1).

Si+0.1×Mn+0.6×Al≥0.35  (1)

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

(7) In the steel sheet according to any one of (1) to (6), the steel sheet may have a hot-dip galvanized layer or an electrogalvanized layer on the surface.

›DISCLOSURE OF THE INVENTION · 2 of 2

(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 (1) to (6) and pickling, or on a cold-rolled steel sheet which has been obtained by cold-rolling the steel sheet; and thereafter performing a second heat treatment satisfying (A) to (E).

(a) An atmosphere containing 0.1 vol % or more of H 2 and satisfying Expression (3) is adopted from 650° C. to a highest heating temperature reached.

(b) Holding is performed at the highest heating temperature of A c3 −30° C. to 1000° C. for 1 second to 1000 seconds.

(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.

(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.

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

(A) An atmosphere containing 0.1 vol % or more of H 2 and 0.020 vol % or less of O 2 and having a log(PH 2 O/PH 2 ) satisfying Expression (3) is adopted until a temperature reaches from 650° C. to a highest heating temperature.

(B) Holding is performed at a highest heating temperature of A c1 +25° C. to A c3 −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.

(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.

−1.1≤log(PH 2 O/PH 2 )≤−0.07  (3)

(in Expression (3), PH 2 O represents a partial pressure of water vapor, and PH 2 represents a partial pressure of hydrogen).

(9) In the method for manufacturing the steel sheet according to (8), hot-dip galvanizing may be performed at a later stage than (D).

Effects of the Invention

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, and excellent chemical convertibility and plating adhesion, and further having good bendability after working, and a method for manufacturing the same.

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 DRAWINGS

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.

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.

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.

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.

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.

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.

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 · 1 of 14

“Steel Sheet”

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.

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 %].

“C: 0.050% to 0.500%”

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.

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.

“Si: 0.01% to 3.00%”

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.

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.

“Mn: 0.50% to 5.00%”

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.

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.

“P: 0.0001% to 0.1000%”

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 0.0200% or less.

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.

“S: 0.0001% to 0.0100%”

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.

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.

“Al: 0.001% to 2.500%”

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 preferably set to 2.000% or less, and is even more preferably set to 1.500% or less.

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.

›EMBODIMENTS OF THE INVENTION · 2 of 14

“N: 0.0001% to 0.0100%”

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.

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.

“O: 0.0001% to 0.0100%”

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.

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%.

“Si+0.1×Mn+0.6×Al≥0.35”

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.

Si+0.1×Mn+0.6×Al≥0.35  (1)

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

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 the group consisting of 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%.

“Ti: 0% to 0.300%”

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.

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.

“V: 0% to 1.00%”

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.

“Nb: 0% to 0.100%”

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.

“Cr: 0% to 2.00%”

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.

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.

“Ni: 0% to 2.00%”

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 1.20% or less.

›EMBODIMENTS OF THE INVENTION · 3 of 14

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.

“Cu: 0% to 2.00%”

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.

“Co: 0% to 2.00%”

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.

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.

“Mo: 0% to 1.00%”

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.

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.

“W: 0% to 1.00%”

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.

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.

“B: 0% to 0.0100%”

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.

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.

“Sn: 0% to 1.00%”

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.

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.

“Sb: 0% to 1.00%”

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.

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.

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

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 are contained 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.

The reason for including these elements is as follows.

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 of 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 are contained, 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 are contained, the total amount of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM is preferably set to 0.0100% or less.

›EMBODIMENTS OF THE INVENTION · 4 of 14

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 of the group consisting of Ca, Mg, Ce, Zr, La, Hf, Bi, and REM is more preferably 0.0010% or more.

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.

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.

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.

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 %].

(Steel Structure of Steel Sheet Inside)

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.

“Soft Ferrite: 0% to 30%”

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.

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%.

“Retained Austenite: 3% to 40%”

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 is even more preferably set to 7% or more.

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.

“Fresh Martensite: 0% to 30%”

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.

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

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%.

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

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.

›EMBODIMENTS OF THE INVENTION · 5 of 14

“Tempered Martensite”

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 to 30% or less.

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.

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 of 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.

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.

(Microstructure of Surface Layer)

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

“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”

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.

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.

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.

“Volume Fraction of Grains Having Aspect Ratio of Less than 3.0 in Ferrite Contained in Soft Layer is 50% or More”

When the volume fraction of grains (grains of ferrite) having an aspect ratio of less than 3.0 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 bendability after working deteriorates. Therefore, the volume fraction of grains having an aspect ratio of less than 3.0 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.

“Volume Fraction of Retained Austenite in Soft Layer is Less than 50% of Volume Fraction of Retained Austenite of Steel Sheet Inside”

The retained austenite contained in the soft layer may be transformed into hard martensite by working and may become the origin of cracking during bending after working in some cases. Therefore, the smaller the volume fraction of the retained austenite contained in the soft layer, the more desirable. The volume fraction of the retained austenite in the soft layer is set to less than 50% of the volume fraction of the retained austenite in the steel sheet inside. The volume fraction thereof is more preferably less than 30%.

The volume fraction of the retained austenite in the steel sheet inside means the volume fraction of the 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.

“Internal Oxide Layer Containing Si Oxides”

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 5.0 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 5.0 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 5.0 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.

›EMBODIMENTS OF THE INVENTION · 6 of 14

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 5.0 μm or less from the surface and a range of 0 μm to 0.2 μm (a region shallower than 0.2 μm depth) 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.

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 5.0 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 (I MAX )) 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.

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 depth range of more than 0.2 μm to 5.0 μm or less. This means that the steel sheet does not have an internal oxide layer but has only an external oxide layer.

“Rate of Change in Hardness from Surface to ⅛ Thickness of Sheet Thickness”

In addition, in the steel sheet according to the present embodiment, it is preferable that the maximum value of the rate of change in hardness per 10 μm in thickness calculated from the result of measuring the hardness from the surface to a ⅛ thickness of the sheet thickness (⅛ thickness) at a pitch of 10 μm is 100 Hv or less (the rate of change in hardness is 100 Hv/10 μm or less, in other words, 100 Hv/0.01 mm or less). Accordingly, it becomes possible to further improve the bendability after working. Although the reason for this is not clear, it is presumed that by not allowing a region where the hardness changes sharply to be present, the affinity between the steel structure of the steel sheet inside (base metal structure) and the steel structure of the surface layer increases, and the generation of voids at the boundary between the structure of the surface layer and the base metal structure during bending is suppressed.

“Galvanized Layer”

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.

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 %.

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.

The plating adhesion amount of the galvanized layer is not particularly limited, but from the viewpoint of corrosion resistance, is preferably 5 g/m 2 or more per side, more preferably in a range of 20 to 120 g/m 2 , and even more preferably in a range of 25 to 75 g/m 2 .

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.

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.

“Steel Sheet for Heat Treatment”

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.

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.

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 of 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 /μm 2 or less, a surface layer including a soft layer containing ferrite in a volume fraction of 80% or more is formed in the depth direction from the surface, the thickness of the soft layer is 1 μm to 50 μm, and when analysis is performed by the radio-frequency glow discharge analysis method in the depth direction from the surface, a peak of the emission intensity at a wavelength indicating Si appears at a depth of more than 0.2 μm and 5.0 μm or less. 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.

›EMBODIMENTS OF THE INVENTION · 7 of 14

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 detail.

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

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

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 of the group consisting of bainite, tempered martensite, and fresh martensite in a volume fraction of 70% or more in total.

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%.

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

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 /m 2 or less.

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 /m 2 or less. The number density of coarse lump-like retained austenite grains is preferably as low as possible, and is preferably 0.5×10 −2 /m 2 or less.

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.

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

“Soft Layer Containing Ferrite in Volume Fraction of 80% or More”

In the steel sheet for a heat treatment, which is to be the material of the steel sheet according to the present embodiment, a surface layer including a soft layer containing ferrite in a volume fraction of 80% or more is preferably formed in the depth direction (sheet thickness direction) from the surface. The thickness of the soft layer is preferably 1 μm to 50 μm. When the thickness of the soft layer is less than 1 μm in the depth direction from the surface, the thickness of the soft layer formed in the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment is insufficient.

On the other hand, when the thickness of the soft layer exceeds 50 μm in the depth direction from the surface, the thickness (depth range from the surface) of the soft layer formed in the steel sheet obtained by subjecting the steel sheet for a heat treatment to the second heat treatment becomes excessive and the strength of the steel sheet is reduced. Therefore, the thickness of the soft layer is preferably 50 μm or less, more preferably 10 μm or less.

“Internal Oxide Layer Containing Si Oxides”

It is preferable that when the steel sheet for a heat treatment according to the present embodiment is analyzed by the radio-frequency glow discharge (radio-frequency GDS) analysis method in the depth 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 5.0 μm or less from the surface. The peak appearing at this position indicates that the steel sheet for a heat treatment is internally oxidized and an internal oxide layer containing Si oxides is provided in a range of more than 0.2 μm to 5.0 μm or less from the surface. In the steel sheet for a heat treatment having the internal oxide layer at the above depth from the surface, the generation of an oxide film such as Si oxides on the surface of the steel sheet due to the heat treatment during manufacturing is suppressed.

The steel sheet for a heat treatment may have a peak of the emission intensity at the wavelength indicating Si in both the range of more than 0.2 μm to 5.0 μm or less 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 of the emission intensity at the wavelength indicating Si in both ranges indicates that the steel sheet for a heat treatment has the internal oxide layer and an external oxide layer containing Si oxides on the surface.

›EMBODIMENTS OF THE INVENTION · 8 of 14

Method for Manufacturing Steel Sheet According to Present Embodiment

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

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.

(Casting Step)

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.

(Slab Heating)

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).

(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 A c1 is a value represented by Expression (8), A c3 is a value represented by Expression (9), and ts(T) is a slab retention time (sec) at a slab heating temperature T)

(in Expression (5), T is a slab heating temperature (° C.), WC is a C content (mass %) in steel, A c1 is a value represented by Expression (8), and A c3 is a value represented by Expression (9))

(in Expression (6), T is a slab heating temperature (° C.), WMn is a Mn content (mass %) in steel, A c1 is a value represented by Expression (8), and A c3 is a value represented by Expression (9))

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

A c1 =723−10.7×Mn−16.9×Ni+29.1×Si+16.9×Cr  (8)

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

A c3 =879−346×C+65×Si−18×Mn+54×Al  (9)

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

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.

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.

(Hot Rolling)

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.

(Pickling Step)

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.

(Cold Rolling)

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.

›EMBODIMENTS OF THE INVENTION · 9 of 14

(First Heat Treatment)

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).

(a) An atmosphere containing 0.1 vol % or more of H 2 and satisfying Expression (3) is adopted from 650° C. to a highest heating temperature reached.

−1.1≤log(PH 2 O/PH 2 )≤−0.07  (3)

(in Expression (3), log represents the common logarithm, PH 2 O represents the partial pressure of water vapor, and PH 2 represents the partial pressure of hydrogen)

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

When H 2 in 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.

On the other hand, when the H 2 content in the atmosphere exceeds 20 vol %, the effect is saturated. When the H 2 content in the atmosphere exceeds 20 vol %, the risk of hydrogen explosion during an operation increases. Therefore, it is preferable to set the H 2 content in the atmosphere to 20 vol % or less.

In a case where the log(PH 2 O/PH 2 ) 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 thickness of the soft layer formed in the surface layer portion of the steel sheet for a heat treatment decreases. As a result, the thickness of the soft layer is insufficient even in the steel sheet after the second heat treatment.

On the other hand, when the log(PH 2 O/PH 2 ) exceeds −0.07, the decarburization reaction proceeds excessively, and the strength of the steel sheet after the second heat treatment becomes insufficient. As a result, the strength is insufficient even in the steel sheet after the second heat treatment.

(b) Holding is performed at a highest heating temperature of A c3 −30° C. to 1000° C. for 1 second to 1000 seconds.

In the first heat treatment, the highest heating temperature is set to A c3 −30° C. or higher. When the highest heating temperature is lower than A c3 −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 A c3 −15° C. or higher, and is more preferably set to A c3 +5° C. or higher.

On the other hand, when heating to an excessively high temperature is performed, there is concern that decarburization of the surface layer may proceed excessively, and the cost required for heating also increases. Therefore, the highest heating temperature is set to 1000° C. or lower.

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.

(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.

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.

On the other hand, when the average heating rate exceeds 500° C./s, the decarburization reaction does not proceed sufficiently. Therefore, the average heating rate is set to 500° C./s or less.

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.

(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.

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.

›EMBODIMENTS OF THE INVENTION · 10 of 14

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. Ms.

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

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

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

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.

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.

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.

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.

(Second Heat Treatment)

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).

(A) An atmosphere containing 0.1 vol % or more of H 2 and 0.020 vol % or less of O 2 and having a log(PH 2 O/PH 2 ) satisfying Expression (3) is adopted from 650° C. to a highest heating temperature reached.

−1.1≤log(PH 2 O/PH 2 )≤−0.07  (3)

(in Expression (3), log represents the common logarithm, PH 2 O represents the partial pressure of water vapor, and PH 2 represents the partial pressure of hydrogen)

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

When H 2 in the atmosphere is less than 0.1 vol % or O 2 is 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 H 2 is 1.0 vol % or more, and is more preferably 2.0 vol % or more. A preferable range of O 2 is 0.010 vol % or less, and is more preferably 0.005 vol % or less.

When the H 2 content in the atmosphere exceeds 20 vol %, the effect is saturated. When the H 2 content in the atmosphere exceeds 20 vol %, the risk of hydrogen explosion during an operation increases. Therefore, it is preferable to set the H 2 content in the atmosphere to 20 vol % or less.

In a case where the log(PH 2 O/PH 2 ) 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 thickness of the soft layer formed in the surface layer of the steel sheet obtained after the second heat treatment decreases. Therefore, the log(PH 2 O/PH 2 ) is set to −1.1 or more. When the log(PH 2 O/PH 2 ) is −0.8 or more, the steel sheet obtained after the second heat treatment has a rate of change in hardness from the surface to the ⅛ thickness in a preferable range, which is preferable. It is considered that this is because by setting the log(PH 2 O/PH 2 ) to −0.8 or more, the decarburization reaction proceeds even in a deep portion of the steel sheet, and the decarburization reaction proceeds even in a region where the decarburization reaction had not occurred in the first heat treatment.

On the other hand, when the log(PH 2 O/PH 2 ) exceeds −0.07, the decarburization reaction proceeds excessively, and the strength of the steel sheet obtained after the second heat treatment becomes insufficient. Therefore, the log(PH 2 O/PH 2 ) is set to −0.07 or less.

(B) Holding is performed at a highest heating temperature of (A c1 +25°) C to (A c3 −10°) C for 1 second to 1000 seconds.

In the second heat treatment, the highest heating temperature is set to (A c1 +25°) C to (A c3 −10°) C. When the highest heating temperature is lower than (A c1 +25°) C, cementite in the steel is left dissolve, 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 (A c1 +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.

›EMBODIMENTS OF THE INVENTION · 11 of 14

On the other hand, when the highest heating temperature exceeds (A c3 −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 (A c3 −10°) C or lower. The highest heating temperature is preferably set to (A c3 −20°) C or lower, and is more preferably set to (A c3 −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.

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, the effect of heating to the highest heating temperature is saturated, and productivity is reduced. Therefore, the retention time is set to 1000 seconds or shorter.

(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.

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.

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

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 reduced. 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.

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

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 into 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 in 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.

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.

<Galvanizing Step>

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.

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

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.

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/m 2 or more per side, but is preferably 20 to 120 g/m 2 , and is more preferably 25 to 75 g/m 2 .

›EMBODIMENTS OF THE INVENTION · 12 of 14

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.

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.

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.

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.

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

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

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.

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.

“Measurement of Steel Structure”

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.

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 −9 m 2 or 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.

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.

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. 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.

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.

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

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 −9 m 2 or 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.

›EMBODIMENTS OF THE INVENTION · 13 of 14

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

The aspect ratio and major axis of the retained austenite grains contained in the steel structure of the steel sheet inside are evaluated by observing the grains using FE-SEM and performing a high-resolution crystal orientation analysis by the 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. Next, an area of 2.0×10 −9 m 2 or more in total is observed with FE-SEM in one or a plurality of visual fields in the ⅛ to ⅜ thickness range centered on the ¼ thickness position from the surface of the observed section. From the observation result, the region determined as FCC iron is determined as retained austenite.

Next, from the crystal orientation of the retained austenite 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. In addition, 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. 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 0.03 to 0.20 μm.

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

A method for separating ferrite 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 data obtained from BCC iron, a boundary that causes a crystal orientation difference of 150 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.

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”.

“Hardness from Surface Layer to Steel Sheet Inside”

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.

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).

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.

›EMBODIMENTS OF THE INVENTION · 14 of 14

Similarly, the maximum value of the rate of change in hardness can be calculated from the hardness profile in the depth direction.

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.

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

“Aspect Ratio of Ferrite Grains Contained in Soft Layer and Proportion of Grains Having Aspect Ratio of Less than 3.0”

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.

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 150 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.

The proportion (volume fraction) of grains having an aspect ratio of less than 3.0 in the ferrite contained in the soft layer is obtained.

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

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.

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.

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 · 1 of 4

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.

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, 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.

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.

(First Heat Treatment)

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 between 700° C. to Ms to the cooling stop temperature was performed at the average cooling rate shown in Tables 6 to 9. In the first heat treatment, heating was performed in the atmosphere containing H 2 at the concentration shown in Tables 6 to 9 and having a log(PH 2 O/PH 2 ) of the numerical value shown in Tables 6 to 9 until the temperature reached from 650° C. to the highest heating temperature.

A c3 was obtained by Expression (9), and Ms was obtained by Expression (10).

A c3 =879−346×C+65×Si−18×Mn+54×Al  (9)

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

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

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

(Second Heat Treatment)

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 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.

Next, an electrogalvanizing step is performed on some of the high strength steel sheets 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.

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 Tables 8 and 9. 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.

In Experimental Examples Nos. 81′ to 88′, according to the pattern [ 2 ] shown in FIG. 5 , under the conditions shown in Table 13, heating, cooling, plating, and an alloying treatment excluding Experimental Example No. 86 were performed, and cooling and isothermal holding were further performed.

In addition, in Experimental Example No. 89′, according to the pattern [ 3 ] shown in FIG. 6 , under the conditions shown in Table 13, heating, cooling, and isothermal holding were performed, cooling to room temperature was then performed once, and hot-dip galvannealing and an alloying treatment were thereafter performed again.

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/m 2 per side.

A c1 was obtained by Expression (8), and A c3 was obtained by Expression (9).

A c1 =723−10.7×Mn−16.9×Ni+29.1×Si+16.9×Cr  (8)

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

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.

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.

›Example · 2 of 4

The results are shown in Tables 14 to 17.

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 (depth range from the surface) of the soft layer was examined. At the same time, the maximum value of the rate of change in hardness from the surface to the ⅛ thickness was examined by the method described above.

In addition, for the steel sheets of Experimental Examples Nos. 1 to 78 and Experimental Examples Nos. 1′ to 89′, the number proportion of grains having an aspect ratio of less than 3.0 in ferrite grains contained in the soft layer, and the ratio between retained austenite contained in the soft layer and retained austenite contained in the internal structure were examined by the method described above.

The results are shown in Tables 18 to 21.

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 5.0 μm or less was examined.

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 in the depth range of more than 0.2 μm to 5.0 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.

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), bendability after working (minimum bend radius after pre-strain), chemical convertibility, and plating adhesion were examined. The results are shown in Tables 22 to 25.

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.

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 −7 or more were evaluated as good.

TS 2 ×El×λ  (11)

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

The results are shown in Tables 22 to 25.

The bendability after working was evaluated by the following method. A JIS No. 5 tensile test piece was taken so that the direction perpendicular to the rolling direction was the tensile direction, and a pre-strain of 4% was applied at a crosshead speed of 2 mm/min. Then, a 25 mm×60 mm test piece was taken from a parallel portion of the tensile test piece, and a 90 degree V-bending test was performed using a 90° die and a punch with a tip R of 1 to 6 mm. The surface of the test piece after the bending test was observed with a magnifying glass, and the minimum bend radius without cracking was defined as the minimum bend radius after pre-strain. Those having a minimum bend radius of 3.0 mm or less were evaluated as good.

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.

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.

A test piece having a width of 70 mm 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.

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

“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).

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

“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.

›Example · 3 of 4

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.

A 30 mm×100 mm test piece was taken from these steel sheets and subjected to a 900 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.

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

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

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

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

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

The steel sheets of Experimental Examples Nos. 1, 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′, 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.

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

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.

In the steel sheet of Experimental Example No. 3, since the highest heating temperature in the first heat treatment was high, the thickness of the soft layer in the steel sheet was large, and the strength of the steel sheet was low.

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.

In the steel sheets of Experimental Examples Nos. 6 and 16, since the log(PH 2 O/PH 2 ) in the first heat treatment was low, the proportion of ferrite having an aspect ratio of less than 3.0 in the soft layer was small, and the bendability after working was poor.

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.

In the steel sheets of Experimental Examples Nos. 9, 15, 20, 25, and 51, since the log(PH 2 O/PH 2 ) in the second heat treatment was low, the residual γ fraction in the soft layer/the residual γ fraction in the steel sheet inside was large, so that the bendability after working was poor.

In the steel sheet of Experimental Example No. 24, since the log(PH 2 O/PH 2 ) in the first heat treatment and the second heat treatment was low, the thickness of the soft layer in the steel sheet was insufficient, and the bendability after working was poor.

Regarding the steel sheets of Experimental Examples No. 17, 24, and 48, since no soft layer was formed in the surface layer structure of the steel sheet and there was no internal oxidation peak, the chemical convertibility was evaluated as “B”.

In the steel sheet of Experimental Example No. 26, since the highest heating temperature in the second heat treatment was high, the retained austenite was insufficient, and the balance between strength, elongation, and hole expansion ratio was poor.

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.

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.

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.

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.

In the steel sheet of Experimental Example No. 65, since the log(PH 2 O/PH 2 ) 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.

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.

›Example · 4 of 4

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, and as a result, the balance between strength, elongation, and hole expansion ratio was poor.

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.

In the steel sheet of Experimental Example No. 3′, since the highest heating temperature in the first heat treatment was high, the thickness of the soft layer was large and the strength was low.

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.

In the steel sheets of Experimental Examples Nos. 6′ and 21, since the log(PH 2 O/PH 2 ) in the first heat treatment was low, the proportion of ferrite having an aspect ratio of less than 3.0 in the soft layer was small, and the bendability after working was poor.

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.

In the steel sheets of Experimental Examples Nos. 9′, 20′, 22′, 25′, 29′, 30′, and 56′, since the log(PH 2 O/PH 2 ) in the second heat treatment was low, the residual γ fraction in the soft layer/the residual γ fraction in the steel sheet inside was large, and the bendability after working was poor.

Regarding the steel sheets of Experimental Examples No. 22′, 29′, and 53′, 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”.

In the steel sheet of Experimental Example No. 31′, since the maximum attainment temperature in the second 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.

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.

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.

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.

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.

In the steel sheet of Experimental Example No. 70′, since the log(PH 2 O/PH 2 ) 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.

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.

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

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.

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

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

›Tables in the description — 24
(
Expression⁢
⁢1
)
1⁢
04
·
∑
A
c⁢
⁢1
A
c⁢
⁢3
⁢
·WMn
⁢
⁢
γ·
D·ts⁡(T)
∑
A
c⁢
⁢1
A
c⁢
⁢3
⁢
D·
ts⁡
(T)
≦1.0
(4)
(
Expression⁢
⁢3
)
WMn⁢
⁢γ
=
{
3.4·MWn
-
2.4·WMn·
T-
A
c⁢
⁢1
A
c⁢
⁢3
-
A
c⁢
⁢1
}
/100
(6)
TABLE 1 — Kind
ofCSiMnPSAlNONbTiVNiCu
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—————
D0.0791.092.600.0090.00050.0200.00150.0017—0.030———
E0.1551.151.280.0050.00300.0420.00200.0012—0.036———
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————
10.1941.193.090.0120.00380.0860.00080.0020—————
J0.1940.222.940.0080.00401.2460.00220.0019——0.109——
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———0.3500.090
00.1700.332.490.0120.00290.6440.00080.0012—————
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—————
U0.2201.502.400.0130.00150.0400.00430.0020—0.050———
V0.1801.602.600.0080.00110.0320.00430.00080.0200.020———
W
0.041
1.151.860.0060.00280.0540.00270.0009—————
X0.1630.381.920.0090.00260.0630.00420.0013
0.350
————
Y0.1561.17
0.47
0.0100.00240.0590.00350.0011—————
Z0.200
3.20
1.200.0080.00330.0350.00420.0012—————
ΛΛ0.2101.10
5.20
0.150
0.00300.0350.00350.0013—————
Kind
ofCrMoBOthersFormulaAc1Ac3Ms
steelmass % remainder consisting of Fe and impurities(1)° C.° C.° C.Note
A———1.40729825381Example
B———Co: 0.131.98746846365Example
C———Ca: 0.00182.10745812300Example
D—0.200—1.36727856422Example
E———1.30743861441Example
F———1.09727841427Example
G———1.03712775319Example
H———1.07709868323Example
1———1.55725822357Example
J———1.26698953369Example
K1.05——1.05758847419Example
L———Sb: 0.0862.10744878397Example
M——0.00141.18725837418Example
N——0.00201.70751892456Example
0———La: 0.00160.97706887395Example
P—0.160—2.12757880401Example
Q———Zr: 0.003,1.54724802342Example
REM: 0.003
R—0.0500.00201.39733832384Example
S———W: 0.03,2.49758871370Example
Sn: 0.03
T0.40——Mg: 0.0040.34728826455Example
U———Hf: 0.0051.76741840370Example
V———Bi: 0.002,1.88742844378Example
W———Ce:0.0021.37737889466Comparative
Example
X———0.61714816419Comparative
Example
Y———1.25752888471Comparative
Example
Z———3.34803945411Comparative
Example
ΛΛ———1.64699853271Comparative
Example
* Underlined values are outside the range of the present invention
TABLE 2 — Cold rolling
Hot rolling stepstep
RollingCold
KindSlab heatingcompletionrolling
ExperimentaloftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
1A12300.795053
2A12500.691053
3A12200.695053
4A12301.391053
5A12400.694053
6A12300.694053
7A12300.591053
8A12400.792053
9A12400.591053
10A12200.795053
11A12500.694053
12A12600.692053
13B12400.592053
14B12200.592053
15B12600.691053
16B12200.691053
17B12200.595053
18C12300.694053
19C12501.592053
20C12500.591053
21C12400.691053
22D12500.692053
23D12500.595053
24D12300.795053
25D12200.592053
26D12600.695053
27D12300.792053
28D12300.794053
29D12600.793053
30E12300.695053
31E12600.593053
32F12300.595053
33F12400.592053
34G12500.593053
35G12400.791053
36G12200.792053
37G12500.595053
38G12600.793053
39H12600.594053
* Underlined values are outside the range of the present invention
TABLE 3 — Cold rolling
Hot rolling stepstep
RollingCold
KindSlab heatingcompletionrolling
ExperimentaloftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
40I12400.592053
41I12400.692053
42I12200.792053
43I12400.793053
44I12600.794053
45I12500.5930Absent
46I12300.7910Absent
47I12400.591053
48I12200.591053
49I12301.591053
50J12200.791053
51J12200.692053
52K12300.693053
53L12600.795053
54L12600.695053
55M12300.695053
56N12200.695053
57O12500.694053
58P12500.794053
59Q12400.692053
60R12200.694053
61S12500.693053
62T12300.692053
63U12400.593053
64U12600.793053
65U12400.591053
66U12500.593053
67U12500.795053
68U12200.594053
69U12600.592053
70V12300.694053
71
W
12500.591053
72X12400.695053
73
Y
12400.591053
74
Z
12500.693053
75
AA
12500.592053
76A12400.693053
77A12500.695053
78A12400.893053
* Underlined values are outside the range of the present invention
TABLE 4 — Cold rolling
Hot rolling stepstep
RollingCold
KindSlab heatingcompletionrolling
ExperimentaloftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
1′A12300.795053
2′A12500.691053
3′A12200.695053
4′A12301.391053
5′A12400.694053
6′A12300.694053
7′A12300.591053
8′A12400.792053
9′A12400.591053
10′A12200.795053
11′A12400.693053
12′A12500.695053
13′A12400.893053
14′A12400.893053
15′A12500.694053
16′A12600.692053
17′A12500.694053
18′B12400.592053
19′B12200.592053
20′B12600.691053
21′B12200.691053
22′B12200.595053
23′C12300.694053
24′C12501.592053
25′C12500.591053
26′C12400.691053
27′D12500.692053
28′D12500.595053
29′D12300.795053
30′D12200.592053
31′D12600.695053
32′D12300.792053
33′D12300.794053
34′D12600.793053
35′E12300.695053
36′E12600.593053
37′F12300.595053
38′F12400.592053
39′G12500.593053
40′G12400.791053
41′G12200.792053
42′G12500.595053
43′G12600.793053
* Underlined values are outside the range of the present invention
TABLE 5 — Cold rolling
Hot rolling stepstep
RollingCold
KindSlab heatingcompletionrolling
ExperimentaloftemperatureFormulatemperaturereduction
Examplesteel° C.(4)° C.%
44′II12600.594053
45′I12400.592053
46′I12400.692053
47′I12200.792053
48′I12400.793053
49′I12600.794053
50′I12500.5930Absent
51′I12300.7910Absent
52′I12400.591053
53′I12200.591053
54′I12301.591053
55′J12200.791053
56′J12200.692053
57′K12300.693053
58′L12600.795053
59′L12600.695053
60′M12300.695053
61′N12200.695053
62′O12500.694053
63′P12500.794053
64′Q12400.692053
65′R12200.694053
66′S12500.693053
67′T12300.692053
68′U12400.593053
69′U12600.793053
70′U12400.591053
71′U12500.593053
72′U12500.795053
73′U12200.594053
74′U12600.592053
75′V12300.694053
76′
W
12500.591053
77′X12400.695053
78′
Y
12400.591053
79′
Z
12500.693053
80′
AA
12500.592053
81′A12400.794053
82′A12400.794053
83′A12400.794053
84′A12400.794053
85′A12400.794053
86′A12400.794053
87′B12400.592053
88′C12300.694053
89′A12400.695053
* Underlined values are outside the range of the present invention
TABLE 6 — First heat treatment Average
Averagecooling rate
heating rateHighestbetweenCooling
at 650° C. orheatingRetentionAtmosphere700° C.stop
ExperimentalAc3MshighertemperaturetimelogH 2and Mstemperature
Example° C.° C.° C./s° C.s(P H2O /P H2 )vol %° C./s° C.
18253812.084060−0.62.040.0Room
temperature
28253812.0
780
60−0.62.040.0Room
temperature
38253812.0113060−0.62.040.0Room
temperature
48253812.084060−0.62.040.0Room
temperature
5825381
0.05
85060−0.62.040.0Room
temperature
68253812.085060− 1.72.040.0Room
temperature
78253812.083560−0.62.012.0Room
temperature
88253812.084560−0.62.02.0Room
temperature
98253812.085060−0.62.040.0Room
temperature
108253812.085060−0.62.040.0Room
temperature
11825381Absent
128253812.085060−0.62.040.0250
138463652.087060−0.62.040.0Room
temperature
148463652.087060−0.62.040.0270
158463652.087060−0.62.040.0Room
temperature
168463652.087060− 1.22.040.0Room
temperature
17846365Absent
188123002.084060−0.62.040.0Room
temperature
198123002.083060−0.62.040.0Room
temperature
208123002.083060−0.62.040.0Room
temperature
218123002.083060−0.62.040.0230
228564222.084060−0.62.040.0Room
temperature
238564222.088560−0.62.040.0Room
temperature
248564222.088560
−1.3
2.040.0Room
temperature
258564222.088560−0.62.040.0Room
temperature
268564222.088560−0.62.040.0Room
temperature
278564222.08755−0.62.040.0Room
temperature
288564222.087560−0.62.040.0340
29856422Absent
308614412.090060−0.62.040.0Room
temperature
318614412.090060−0.62.040.0330
328414272.087060−0.62.040.0Room
temperature
338414272.087060−0.62.040.0250
347753192.080060−0.62.040.0Room
temperature
357753192.080060−0.62.040.0Room
temperature
367753192.080060−0.62.040.0Room
temperature
377753192.080060−0.62.040.0280
387753192.080060−0.62.040.0
400
398683232.088060−0.62.040.0Room
temperature
* Underlined values are outside the range of the present invention
TABLE 7 — First heat treatment Average
Averagecooling rate
heating rateHighestbetweenCooling
at 650° C. orheatingRetentionAtmosphere700° C.stop
ExperimentalAc3MshighertemperaturetimelogH 2and Mstemperature
Example° C.° C.° C./s° C.s(P H2O /P H2 )vol %° C./s° C.
408223572.084060−0.62.040.0Room
temperature
418223570.783560−0.62.040.0Room
temperature
428223572.083560−0.62.040.0Room
temperature
438223572.085060−0.62.040.0Room
temperature
448223572.084060−0.62.040.0280
458223572.084560−0.62.040.0Room
temperature
468223572.080560−0.62.040.0Room
temperature
47822357Absent
48822357Absent
498223572.085060−0.62.040.0Room
temperature
509533692.097060−0.62.040.0Room
temperature
519533692.097060−0.62.040.0Room
temperature
528474192.086060−0.62.040.0Room
temperature
538783972.091060−0.62.040.0Room
temperature
548783972.091060−0.62.040.0Room
temperature
558374182.085060−0.62.040.0Room
temperature
568924562.092060−0.62.040.0Room
temperature
578873952.093060−0.62.040.0Room
temperature
588804012.089560−0.62.040.0Room
temperature
598023422.088060−0.62.040.0Room
temperature
608323842.085060−0.62.040.0Room
temperature
618713702.089060−0.62.040.0Room
temperature
628264552.087560−0.62.040.0Room
temperature
638403702.086060−0.62.040.0Room
temperature
648403702.086060−0.62.040.0Room
temperature
658403702.086060−0.62.040.0Room
temperature
668403702.085560−1.02.040.0Room
temperature
678403702.086060−0.62.040.0320
688403702.086060−0.62.040.0170
698403702.085560−0.62.040.0Room
temperature
708443782.090560−0.62.040.0Room
temperature
718894662.092060−0.62.040.0Room
temperature
728164192.087060−0.62.040.0Room
temperature
738884712.090560−0.62.040.0Room
temperature
749454112.096560−0.62.040.0Room
temperature
758532712.089560−0.62.040.0Room
temperature
768253812.084060−0.64.040.0Room
temperature
778253812.085060−0.62.040.0Room
temperature
788253812.084060−0.62.040.0Room
temperature
* Underlined values are outside the range of the present invention
TABLE 8 — First heat treatment Average
Averagecooling rate
heating rateHighestbetweenCooling
Experi-at 650° C.heatingRetentionAtmosphere700° C.stop
mentalAc3Msor highertemperaturetimelogH 2and Mstemperature
Example° C.° C.° C./s° C.s(P H20 /P H2 )vol %° C./s° C.
1′8253812.084060−0.62.040.0Room
temperature
2′8253812.0
780
60−0.62.040.0Room
temperature
3′8253812.0113060−0.62.040.0Room
temperature
4′8253812.084060−0.62.040.0Room
temperature
5′825381
0.05
85060−0.62.040.0Room
temperature
6′8253812.085060
−1.6
2.040.0Room
temperature
7′8253812.083560−0.62.012.0Room
temperature
8′8253812.084560−0.62.02.0Room
temperature
9′8253812.085060−0.62.040.0Room
temperature
10′8253812.085060−0.62.040.0Room
temperature
11′8253812.084060−0.64.040.0Room
temperature
12′8253812.085060−0.62.040.0Room
temperature
13′8253812.084060−0.62.040.0Room
temperature
14′8253812.084060−0.62.040.0Room
temperature
15′825381Absent
16′8253812.085060−0.62.040.0250
17′8253812.085060−0.62.040.0Room
temperature
18′8463652.087060−0.62.040.0Room
temperature
19′8463652.087060−0.62.040.0270
20′8463652.087060−0.62.040.0Room
temperature
21′8463652.087060
−1.2
2.040.0Room
temperature
22′846365Absent
23′8123002.084060−0.62.040.0Room
temperature
24′8123002.083060−0.62.040.0Room
temperature
25′8123002.083060−0.62.040.0Room
temperature
26′8123002.083060−0.62.040.0230
27′8564222.084060−0.62.040.0Room
temperature
28′8564222.088560−0.62.040.0Room
temperature
29′8564222.088560
−1.3
2.040.0Room
temperature
30′8564222.088560−0.62.040.0Room
temperature
31′8564222.088560−0.62.040.0Room
temperature
32′8564222.08755−0.62.040.0Room
temperature
33′8564222.087560−0.62.040.0340
34′856422Absent
35′8614412.090060−0.62.040.0Room
temperature
36′8614412.090060−0.62.040.0330
37′8414272.087060−0.62.040.0Room
temperature
38′8414272.087060−0.62.040.0250
39′7753192.080060−0.62.040.0Room
temperature
40′7753192.080060−0.62.040.0Room
temperature
41′7753192.080060−0.62.040.0Room
temperature
42′7753192.080060−0.62.040.0280
43′7753192.080060−0.62.040.0
400
* Underlined values are outside the range of the present invention
TABLE 9 — First heat treatment
AverageAverage
heatingcooling rate
rate atHighestbetweenCooling
Experi-650° C. orheatingRetentionAtmosphere700° C.stop
mentalAc3MshighertemperaturetimeH 2and Mstemperature
Example° C.° C.° C./s° C.slog (P H20 /P H2 )vol %° C./s° C.
44′8683232.088060−0.62.040.0Room
temperature
45′8223572.084060−0.62.040.0Room
temperature
46′8223570.783560−0.62.040.0Room
temperature
47′8223572.083560−0.62.040.0Room
temperature
48′8223572.085060−0.62.040.0Room
temperature
49′8223572.084060−0.62.040.0280
50′8223572.084560−0.62.040.0Room
temperature
51′8223572.080560−0.62.040.0Room
temperature
52′822357Absent
53′822357Absent
54′8223572.085060−0.62.040.0Room
temperature
55′9533692.097060−0.62.040.0Room
temperature
56′9533692.097060−0.62.040.0Room
temperature
57′8474192.086060−0.62.040.0Room
temperature
58′8783972.091060−0.62.040.0Room
temperature
59′8783972.091060−0.62.040.0Room
temperature
60′8374182.085060−0.62.040.0Room
temperature
61′8924562.092060−0.62.040.0Room
temperature
62′8873952.093060−0.62.040.0Room
temperature
63′8804012.089560−0.62.040.0Room
temperature
64′8023422.088060−0.62.040.0Room
temperature
65′8323842.085060−0.62.040.0Room
temperature
66′8713702.089060−0.62.040.0Room
temperature
67′8264552.087560−0.62.040.0Room
temperature
68′8403702.086060−0.62.040.0Room
temperature
69′8403702.086060−0.62.040.0Room
temperature
70′8403702.086060−0.62.040.0Room
temperature
71′8403702.085560−1.02.040.0Room
temperature
72′8403702.086060−0.62.040.0320
73′8403702.086060−0.62.040.0170
74′8403702.085560−0.62.040.0Room
temperature
75′8443782.090560−0.62.040.0Room
temperature
76′8894662.092060−0.62.040.0Room
temperature
77′8164192.087060−0.62.040.0Room
temperature
78′8884712.090560−0.62.040.0Room
temperature
79′9454112.096560−0.62.040.0Room
temperature
80′8532712.089560−0.62.040.0Room
temperature
81′8253812.084560−0.62.040.0Room
temperature
82′8253812.084560−0.62.040.0Room
temperature
83′8253812.084560−0.62.040.0180
84′8253812.084560−0.62.040.0Room
temperature
85′8253812.084560−0.62.040.0Room
temperature
86′8253812.084560−0.62.040.0Room
temperature
87′8463652.087060−0.62.040.0Room
temperature
88′8123002.084060−0.62.040.0Room
temperature
89′8253812.084560−0.62.040.0Room
temperature
* Underlined values are outside the range of the present invention
TABLE 10 — Second heat treatment
AverageAverage
heatingcooling rateCooling
rate atHighestbetweenstop
650° C.heatingRetentionAtmosphere700° C.temper-
Experimentalor highertemperaturetimelogH 2O 2and 600° C.ature
Example° C.° C.s(P H20 /P H2 )vol %vol %° C./s° C.
11.8780110−0.72.00.00340390
21.8780110−0.72.00.00340390
31.8780110−0.72.00.00340390
41.8780110−0.72.00.00340390
51.8780110−0.72.00.00340390
61.8780110−0.72.00.00340390
71.8780110−0.72.00.00340390
81.8780110−0.72.00.00340390
91.8780110−1.62.00.00340390
101.8780110−1.02.00.00340390
111.8780110−0.72.00.00340390
121.8780110−0.72.00.00340390
131.8810110−0.72.00.00340140
141.8800110−0.72.00.00340220
151.8810110−1.62.00.00340220
161.8810110−0.72.00.00340230
171.8815110−1.72.00.00340260
181.8780110−0.72.00.00340100
191.8790110−0.72.00.00340200
201.8780110−1.52.00.00340150
211.8780110−0.72.00.00340150
221.8810110−0.72.00.00340370
231.8805110−0.72.00.00340370
241.8810110−1.62.00.00340370
151.8815110−1.62.00.00340370
261.8
880
110−0.72.00.00340370
271.8800110−0.72.00.00340370
281.8800110−0.72.00.00340370
291.8810110−0.72.00.00340280
301.8810110−0.72.00.00340380
311.8810110−0.72.00.00340380
321.8800110−0.72.00.00340350
331.8800110−0.72.00.00340350
341.8740110−0.72.00.00340390
351.8740110−0.72.00.00340390
361.8740110−0.72.00.00340390
371.8740110−0.72.00.00340390
381.8740110−0.72.00.00340390
391.8790110−0.72.00.00340390
Second heat treatment
HoldingRetention time
temper-between 300° C.AlloyingPlating
Experimentalatureand 480° C.temperaturetreatmentAc1Ac3
Example° C.sec° C.timing° C.° C.
1410250——729825
2390250——729825
3400250——729825
4410250——729825
5400250——729825
6390250——729825
7400250——729825
8390250——729825
9410250——729825
10400250——729825
11390250——729825
12390250——729825
13400250——746846
14400250——746846
15400250——746846
16400250——746846
17400250——746846
18400250——745812
19400250——745812
20400250——745812
21400250——745812
22390250——727856
23390250——727856
24390250——727856
15380250——727856
26390250——727856
27370250——727856
28370250——727856
29400250——727856
30380250——743861
31400250——743861
32360250——727841
33350250——727841
34400250——712775
354008——712775
3640050——712775
37400250——712775
38390250——712775
39410250——709868
* Underlined values are outside the range of the present invention
TABLE 11 — Second heat treatment Average
AveragecoolingRetention
heatingHighestrateCoolingtime
rate atheatingbetweenstopHoldingbetweenAlloyingPlating
Experi-650° C. ortemper-RetentionAtmosphere700° C. andtemper-temper-300° C. andtemper-treat-
mentalhigheraturetimelogH 2O 2600° C.atureature480° C.aturementA c1A c3
Example° C.° C.s(P H2O / PH2 )vol %vol %° C./s° C.° C.s° C.timing° C.° C.
401.8780110−0.72.00.00340410410250——725822
411.8780110−0.72.00.00340380390250——725822
421.87855−0.72.00.00340380400250——725822
431.8785110−0.72.00.0032375375250——725822
441.8785110−0.72.00.00340380400250——725822
451.8770110−0.72.00.00340365375250——725822
461.8780110−0.72.00.00340365385250——725822
471.8790110−0.72.00.00340400420250——725822
481.8790110
−1.5
2.00.00340400420250——725822
491.8790110−0.72.00.00340400400250——725822
501.8880110−0.72.00.00340360380250——698953
511.8880110
−1.5
2.00.00340360370250——698953
521.8800110−0.72.00.00340320380250——758847
531.8820110−0.72.00.0034033033080——744878
541.8815110−0.72.00.00340330340250——744878
551.8790110−0.72.00.00340260400250——725837
561.8830110−0.72.00.00340350350250——751892
571.8805110−0.72.00.00340350370250——706887
581.8825110−0.72.00.00340350350250——757880
591.8765110−0.72.00.00340300310250——724802
601.8780110−0.72.00.00340340350250——733832
611.8830110−0.72.00.00340380380250——758871
621.8785110−0.72.00.00340395395250——728826
631.8790110−0.72.00.00340375395250——741840
641.8
750
110−0.72.00.00340380380250——741840
651.8800110−0.032.00.00340380390250——741840
661.8790110−0.72.00.00340400420250——741840
671.8775110−0.72.00.00340380380250——741840
681.8825110−0.72.00.00340370370250——741840
691.8795110−0.72.00.00340380390250——741840
701.8800110−0.72.00.00340400410250——742844
711.8810110−0.72.00.00340400420250——737889
721.8775110−0.72.00.00340370370250——714816
731.8820110−0.72.00.00340390400250——752888
741.8875110−0.72.00.00340390410250——803945
751.8765110−0.72.00.00340390410250——699853
761.8780110−0.74.00.00340390390250——729825
7715.0790110−0.72.00.00340390400250——729825
780.6770110−0.72.00.00340390390250——729825
* Underlined values are outside the range of the present invention
TABLE 12 — Second heat treatment
AverageAverageRetention
heatingHighestcoolingCoolingtime
rate atheatingratestopHoldingbetweenAlloyingPlating
Experi-650° C. ortemper-RetentionAtmosphere700° C. andtemper-temper-300° C. andtemper-treat-
mentalhigheraturetimelogH 2O 2600.°atureature480° C.aturementA c1A c3
Example° C.° C.s(P H2O / PH2 )vol %vol %° C./s° C.° C.s° C.timing° C.° C.
1′1.3790108−0.74.00.00330410410120490[1]729825
2′1.3790108−0.74.00.00330400410120500[1]729825
3′1.3780108−0.74.00.00330420410120500[1]729825
4′1.3790108−0.74.00.00330420410120500[1]729825
5′1.3790108−0.74.00.00330400400120490[1]729825
6′1.3790108−0.74.00.00330400410120500[1]729825
7′1.3790108−0.74.00.00330390390120500[1]729825
8′1.3790108−0.74.00.00330400410120500[1]729825
9′1.3790108
−1.6
4.00.00330420410120490[1]729825
10′1.3790108−0.94.00.00330400410120490[1]729825
11′1.3780108−0.72.00.00330400400120490[1]729825
12′1.3780108−0.74.00.00630410400120500[1]729825
13′16.0790108−0.74.00.00330390400120490[1]729825
14′0.5790108−0.74.00.00330410410120480[1]729825
15′1.3800108−0.74.00.00330410400120480[1]729825
16′1.3790108−0.74.00.00330400390120490[1]729825
17′1.3790108−0.74.00.00330400400120—[1]729825
18′1.3810108−0.74.00.00330160380120490[1]746846
19′1.3800108−0.74.00.00330220380120490[1]746846
20′1.3810108
−1.7
4.00.00330220380120480[1]746846
21′1.3810108−0.74.00.00330220390120480[1]746846
22′1.3815108
−1.7
4.00.00330260390120490[1]746846
23′1.3790108−0.74.00.00330150380120490[1]745812
24′1.3790108−0.74.00.00330210380120490[1]745812
25′1.3780108
−1.5
4.00.00330170380120490[1]745812
26′1.3790108−0.74.00.00330180390120500[1]745812
27′1.3820108−0.74.00.00330370380120490[1]727856
28′1.3810108−0.74.00.00330370380120490[1]727856
29′1.3820108
−1.5
4.00.00330370380120490[1]727856
30′1.3820108
−1.6
4.00.00330370380120480[1]727856
31′1.3
880
108−0.74.00.00330370380120480[1]727856
32′1.3810108−0.74.00.00330370380120490[1]727856
33′1.3810108−0.74.00.00330370380120490[1]727856
34′1.3810108−0.74.00.00330370380120490[1]727856
35′1.3810108−0.74.00.00330380380120490[1]743861
36′1.3810108−0.74.00.00330380380120490[1]743861
37′1.3800108−0.74.00.00330350350120490[1]727841
38′1.3800108−0.74.00.00330350350120490[1]727841
39′1.3740108−0.74.00.00330390400120480[1]712775
40′1.3740108−0.74.00.003303904007480[1]712775
41′1.3740108−0.74.00.0033039040040480[1]712775
42′1.3740108−0.74.00.00330390410120490[1]712775
43′1.3740108−0.74.00.00330390400120490[1]712775
* Underlined values are outside the range of the present invention
TABLE 13 — Second heat treatment
AverageRetention
Averagecoolingtime
heatingHighestrateCoolingbetween
rate atheatingbetweenstopHolding300° C.AlloyingPlating
Experi-650° C. ortemper-RetentionAtmosphere700° C. andtemper-temper-andtemper-treat-
mentalhigheraturetimelog600° C.atureature480° C.aturementA c1A c3
Example° C.° C.s(P H2O /P H2 )H 2O 2° C./s° C.° C.s° C.timing° C.° C.
44′1.3800108−0.74.00.00330400390120480[1]709868
45′1.3780108−0.74.00.00330400410120490[1]725822
46′1.3780108−0.74.00.00330400380120490[1]725822
47′1.37905−0.74.00.00330390380120480[1]725822
48′1.3790108−0.74.00.0032390380120480[1]725822
49′1.3790108−0.74.00.00330390380120480[1]725822
50′1.3780108−0.74.00.00330380370120480[1]725822
51′1.3780108−0.74.00.00330380370120480[1]725822
52′1.3780108−0.74.00.00330390400120480[1]725822
53′1.3800108
−1.5
4.00.00330380380120480[1]725822
54′1.3790108−0.74.00.00330390400120480[1]725822
55′1.3870108−0.74.00.00330380390120490[1]698953
56′1.3870108
−1.6
4.00.00330370390120490[1]698953
57′1.3800108−0.74.00.00330350380120490[1]758847
58′1.3810108−0.74.00.0033035038080490[1]744878
59′1.3820108−0.74.00.00330350400120—[1]744878
60′1.3790108−0.74.00.00330230380120490[1]725837
61′1.3820108−0.74.00.00330370380120490[1]751892
62′1.3810108−0.74.00.00330370400120490[1]706887
63′1.3830108−0.7400.00330370400120480[1]757880
64′1.3770108−0.74.00.00330300380120490[1]724802
65′1.3780108−0.74.00.00330350380120490[1]733832
66′1.3830108−0.74.00.00330400410120480[1]758871
67′1.3780108−0.74.00.00330400410120490[1]728826
68′1.3790108−0.74.00.00330430420120480[1]741840
69′1.3
745
108−0.74.00.00330430430120490[1]741840
70′1.3800108
−0.03
4.00.00330430420120490[1]741840
71′1.3790108−0.74.00.00330430420120490[1]741840
72′1.3775108−0.74.00.00330430420120490[1]741840
73′1.3820108−0.74.00.00330420420120490[1]741840
74′1.3795108−0.74.00.00330430420120—[1]741840
75′1.3800108−0.74.00.00330410400120490[1]742844
76′1.3810108−0.74.00.00330410410120480[1]737889
77′1.3775108−0.74.00.00330400390120500[1]714816
78′1.3820108−0.74.00.00330400390120490[1]752888
79′1.3875108−0.74.00.00330400400120490[1]803945
80′1.3765108−0.74.00.00330400400120490[1]699853
81′1.3785108−0.74.00.00330400390120500[2]729825
82′1.3790108−0.74.00.00330200400120490[2]729825
83′1.3785108−0.74.00.00330310400120490[2]729825
84′1.3795108−0.74.00.0033060400120500[2]729825
85′1.3785108−0.74.00.00330180390300500[2]729825
86′1.3790108−0.74.00.00330200400120—[2]729825
87′1.3810108−0.74.00.00330180380120490[2]746846
88′1.3790108−0.74.00.00330170380120490[2]745812
89′1.3790108−0.74.00.00330410400120490[3]729825
* Underlined values are outside the range of the present invention
TABLE 17 — Internal structure Retained austenite Proportion with
Experi-SoftaspectTemperedFreshPearlite +HardPrimary
mentalferriteFractionratio ≥ 2.0martensitemartensitecementiteBainiteferriteresidual
Examplevol %vol %%%vol %vol %vol %vol %structureNote
44′421750801354Hard αPresent Invention
45′614900301463Hard αPresent Invention
46′514680301662Hard αPresent Invention
47′57780461662Hard αPresent Invention
48′848001
13
1460Hard α
Comparative Example
49′712800401463Hard αPresent Invention
50′814800201165Hard αPresent Invention
51′2614840401046Hard αPresent Invention
52′1313
45
080660Bainite
Comparative Example
53′1313
46
080660Bainite
Comparative Example
54′711630401266Hard αPresent Invention
55′1013840101363Hard αPresent Invention
56′814860201463Hard α
Comparative Example
57′2513820271043Hard αPresent Invention
58′979101101262Hard αPresent Invention
59′610850301665Hard αPresent Invention
60′658432101838Hard αPresent Invention
61′85870501369Hard αPresent Invention
62′511830201270Hard αPresent Invention
63′213850401269Hard αPresent Invention
64′015900601663Hard αPresent Invention
65′016850201270Hard αPresent Invention
66′015830401269Hard αPresent Invention
67′2348316161040Hard αPresent Invention
68′117860401564Hard αPresent Invention
69′4284026860Bainite
Comparative Example
70′413920401365Hard α
Comparative Example
71′318810201265Hard αPresent Invention
72′317630401462Hard αPresent Invention
73′12126110601050Hard αPresent Invention
74′417860301561Hard αPresent Invention
75′615880501559Hard αPresent Invention
76′272860401354Hard α
Comparative Example
77′124830301467Hard α
Comparative Example
78′
69
2
36
008417Hard α
Comparative Example
79′520900120954Hard α
Comparative Example
80′07
43
02501058Hard α
Comparative Example
81′618810501358Hard αPresent Invention
82′519842030845Hard αPresent Invention
83′518825401058Hard αPresent Invention
84′515884400630Hard αPresent Invention
85′5188523101043Hard αPresent Invention
86′619851920945Hard αPresent Invention
87′319842510844Hard αPresent Invention
88′029774050521Hard αPresent Invention
89′612856001462Hard αPresent Invention
* Underlined values are outside the range of the present invention
TABLE 18 — Soft layer
ProportionResidualMaximum
of ferriteγ in softvalue of rate
having aspectlayer/residualof change in
Exper-ratio ofγ of steelhardness fromInternal
mentalThicknessless than 3.0sheet insidesurface layeroxide
Exampleμm%%HV/10 μmpeakNote
133741537PresentPresent Invention
234871639PresentComparative Example
3
197
82732PresentComparative Example
432701342PresentPresent Invention
535771540PresentComparative Example
630
28
2562PresentComparative Example
740791335PresentPresent Invention
848861230PresentComparative Example
92080
69
119PresentComparative Example
10247541105PresentPresent Invention
1133822067PresentComparative Example
1236781838PresentPresent Invention
1346791245PresentPresent Invention
1444781553PresentPresent Invention
153771
74
137PresentComparative Example
1638
30
2360PresentComparative Example
170
-
-
—
Absent
Comparative Example
1853831439PresentPresent Invention
1955781844PresentPresent Invention
204180
70
51PresentComparative Example
2150851241PresentPresent Invention
2217881543PresentPresent Invention
2320901338PresentPresent Invention
240
-
-
—
Absent
Comparative Example
251385
57
61PresentComparative Example
2619841152PresentComparative Example
2716881443PresentPresent Invention
2816831045PresentPresent Invention
2920901275PresentComparative Example
3031761941PresentPresent Invention
3133781646PresentPresent Invention
3225871029PresentPresent Invention
3326831235PresentPresent Invention
3438791647PresentPresent Invention
3542821558PresentComparative Example
3641801473PresentPresent Invention
3740841344PresentPresent Invention
3840761348PresentComparative Example
3944791445PresentPresent Invention
* Underlined values are outside the range of the present invention
TABLE 19 — Soft layer
ProportionResidualMaximum
of ferriteγ in softvalue of rate
having aspectlayer/residualof change in
Experi-ratio ofγ of steelhardness fromInternal
mentalThicknessless than 3.0sheet insidesurface layeroxide
Exampleμm%%HV/10 μmpeakNote
4038741341PresentPresent Invention
4136771439PresentPresent Invention
4228801048PresentPresent Invention
434082033PresentComparative Example
4435761243PresentPresent Invention
4540771836PresentPresent Invention
4642791930PresentPresent Invention
4735811062PresentComparative Example
480
-
-
—
Absent
Comparative Example
4936801544PresentPresent Invention
5032831245PresentPresent Invention
512482
73
68PresentComparative Example
522588949PresentPresent Invention
5327801545PresentPresent Invention
5424821546PresentPresent Invention
553979036PresentPresent Invention
562484039PresentPresent Invention
5735811034PresentPresent Invention
5831841141PresentPresent Invention
5937801642PresentPresent Invention
6031851243PresentPresent Invention
6136801337PresentPresent Invention
6239791432PresentPresent Invention
6332791543PresentPresent Invention
643683032PresentComparative Example
65
135
90820PresentComparative Example
6633621362PresentPresent Invention
6736871040PresentPresent Invention
6837821641PresentPresent Invention
6936791440PresentPresent Invention
7030671148PresentPresent Invention
711492023PresentComparative Example
7228821857PresentComparative Example
731593045PresentComparative Example
7451712040PresentComparative Example
7525552488PresentComparative Example
7634821139PresentPresent Invention
7716801148PresentPresent Invention
7845831430PresentPresent Invention
* Underlined values are outside the range of the present invention
TABLE 20 — Soft layer
ProportionResidualMaximum
of ferriteγ in softvalue of rate
having aspectlayer/residualof change in
Experi-ratio ofγ of steelhardness fromInternal
mentalThicknessless than 3.0sheet insidesurface layeroxide
Exampleμm%%HV/10 μmpeakNote
1′45761234PresentPresent Invention
2′37771642PresentComparative Example
3′
201
90621PresentComparative Example
4′34721346PresentPresent Invention
5′34741546PresentComparative Example
6′30
26
2052PresentComparative Example
7′46811131PresentPresent Invention
8′40801134PresentComparative Example
9′2875
66
55PresentComparative Example
10′368129110PresentPresent Invention
11′51791332PresentPresent Invention
12′47741834PresentPresent Invention
13′17751788PresentPresent Invention
14′63751423PresentPresent Invention
15′38821579PresentComparative Example
16′53781230PresentPresent Invention
17′45731334PresentPresent Invention
18′48801237PresentPresent Invention
19′46791340PresentPresent Invention
20′3572
68
119PresentComparative Example
21′37
30
2265PresentComparative Example
22′0
-
——
Absent
Comparative Example
23′60791536PresentPresent Invention
24′64812041PresentPresent Invention
25′4177
70
91PresentComparative Example
26′58761638PresentPresent Invention
27′21922144PresentPresent Invention
28′21902047PresentPresent Invention
29′0
-
-
—
Absent
Comparative Example
30′1687
60
61PresentComparative Example
31′21791667PresentComparative Example
32′17881846PresentPresent Invention
33′17832146PresentPresent Invention
34′20921579PresentComparative Example
35′35761739PresentPresent Invention
36′37791742PresentPresent Invention
37′29862239PresentPresent Invention
38′32812139PresentPresent Invention
39′35731550PresentPresent Invention
40′45801453PresentComparative Example
41′44781478PresentPresent Invention
42′40911446PresentPresent Invention
43′43811446PresentComparative Example
* Underlined values are outside the range of the present invention
TABLE 21 — Soft layer
ProportionResidualMaximum
of ferriteγ in softvalue of rate
having aspectlayer/residualof change in
Experi-ratio ofγ of steelhardness fromInternal
mentalThicknessless than 3.0sheet insidesurface layeroxide
Exampleμm%%HV/10 μmpeakNote
44′42781443PresentPresent Invention
45′36761443PresentPresent Invention
46′39751536PresentPresent Invention
47′27881050PresentPresent Invention
48′4175034PresentComparative Example
49′38831347PresentPresent Invention
50′43811935PresentPresent Invention
51′42872031PresentPresent Invention
52′35811166PresentComparative Example
53′0
-
-
—
Absent
Comparative Example
54′37851543PresentPresent Invention
55′30801249PresentPresent Invention
56′2484
72
63PresentComparative Example
57′25901045PresentPresent Invention
58′28871641PresentPresent Invention
59′23761651PresentPresent Invention
60′3985038PresentPresent Invention
61′2579039PresentPresent Invention
62′32891135PresentPresent Invention
63′32771142PresentPresent Invention
64′40851543PresentPresent Invention
65′32791344PresentPresent Invention
66′34861435PresentPresent Invention
67′39771432PresentPresent Invention
68′29741547PresentPresent Invention
69′3381034PresentComparative Example
70′
126
83821PresentComparative Example
71′31581460PresentPresent Invention
72′3992940PresentPresent Invention
73′36791642PresentPresent Invention
74′37821440PresentPresent Invention
75′29661046PresentPresent Invention
76′1398025PresentComparative Example
77′28751963PresentComparative Example
78′1694047PresentComparative Example
79′49652136PresentComparative Example
80′27572391PresentComparative Example
81′41791539PresentPresent Invention
82′42781633PresentPresent Invention
83′47802038PresentPresent Invention
84′45801935PresentPresent Invention
85′42831740PresentPresent Invention
86′44811637PresentPresent Invention
87′48831540PresentPresent Invention
88′57841442PresentPresent Invention
89′43751532PresentPresent Invention
* Underlined values are outside the range of the present invention
TABLE 22 — Minimum
TS · EL/Holebend
Experi-1000expanisonradius afterChemical
mentalTSElMPa · %/ratiopre-strainconverti-Plating
ExamplePlatingMPa%1000%TS 2 *El*λ*10 −7mmbilityadhesionNote
199328.628.4481362.0Ex—Present Invention
297030.329.414405.0Ex—Comparative Example
369637.626.252952.0Ex—Comparative Example
4104127.728.833993.0Ex—Present Invention
5103027.828.626763.0Ex—Comparative Example
6104627.428.6461394.0G—Comparative Example
795429.628.735953.0Ex—Present Invention
889532.429.027704.0Ex—Comparative Example
9102227.628.2461334.0G—Comparative Example
1099928.128.1471313.0G—Present Invention
1193531.529.415405.0Ex—Comparative Example
12102027.628.1471352.0Ex—Present Invention
13118822.426.7441412.0Ex—Present Invention
14118922.026.1491512.0Ex—Present Invention
15122621.726.6451474.0G—Comparative Example
16119422.827.3471534.0G—Comparative Example
17121921.626.419615.0B—Comparative Example
18149222.133.0291443.0Ex—Present Invention
19161120.432.915803.0Ex—Present Invention
20152821.733.7291475.0G—Comparative Example
21147322.137.6321543.0Ex—Present Invention
2270438.026.751953.0Ex—Present Invention
2378833.526.4541132.0Ex—Present Invention
2481232.626.5511094.0B—Comparative Example
2582132.126.4531144.0Ex—Comparative Example
26112210.712.038513.0Ex—Comparative Example
2771833.023.753913.0Ex—Present Invention
2875331.123.4611082.0Ex—Present Invention
2986220.617.750775.0Ex—Comparative Example
3094128.026.3491222.0Ex—Present Invention
3192728.526.4501242.0Ex—Present Invention
3288528.625.3511152.0Ex—Present Invention
3389827.925.0511152.0Ex—Present Invention
34117727.732.5411562.0Ex—Present Invention
35155323.135.99503.0Ex—Comparative Example
36133425.233.6261193.0Ex—Present Invention
37114628.232.3401493.0Ex—Present Invention
38133822.730.39374.0Ex—Comparative Example
39128827.435.3231032.0Ex—Present Invention
TABLE 23 — Minimum
TS · EL/Holebend
Experi-1000expansionradius afterChemical
mentalTSElMPa · %/ratiopre-strainconverti-Plating
ExamplePlatingMPa%1000%TS 2 *El*λ*10 −7mmbilityadhesionNote
40101728.028.5471372.0Ex—Present Invention
41101028.228.4391133.0Ex—Present Invention
42101024.124.339972.0Ex—Present Invention
4390123.220.933623.0Ex—Comparative Example
4498426.526.0471203.0Ex—Present Invention
4598026.826.3451163.0Ex—Present Invention
4691929.427.039983.0Ex—Present Invention
47109726.529.120644.0Ex—Comparative Example
48110926.429.321675.0B—Comparative Example
49100628.228.4371072.0Ex—Present Invention
5096728.427.5491312.0Es—Present Invention
51100328.228.3501404.0G—Comparative Example
5289830.527.436902.0Ex—Present Invention
53104023.924.936942.0Ex—Present Invention
54EG87628.625.1561243.0—ExPresent Invention
55104016.116.7601042.0Ex—Present Invention
5679729.423.4531002.0Ex—Present Invention
5792028.225.9541292.0Ex—Present Invention
5899428.228.0381062.0Ex—Present Invention
59119725.330.3431552.0Ex—Present Invention
60104127.628.7521552.0Es—Present Invention
61104027.728.8471392.0Ex—Present Invention
6295222.321.346932.0Ex—Present Invention
63106728.129.9481532.0Es—Present Invention
6486919.917.345682.0Ex—Comparative Example
6567732.422.056832.0Ex—Comparative Example
66107028.230.2471503.0G—Present Invention
67106727.929.8391232.0Ex—Present Invention
68114422.926.231962.0Ex—Present Invention
69EG106029.030.7471512.0—ExPresent Invention
7099328.428.2491372.0Ex—Present Invention
7158238.422.348632.0Ex—Comparative Example
7290426.323.714306.0Ex—Comparative Example
7363933.321.3841142.0Ex—Comparative Example
74119022.426.65165.0Ex—Comparative Example
75145810.214.86135.0Ex—Comparative Example
76101727.227.7521462.0Ex—Present Invention
77100327.527.6501382.0Ex—Present Invention
7896227.926.838982.0Ex—Present Invention
TABLE 24 — Minimum
TS · EL/Holebend
Experi-1000expansionradius afterChemical
mentalTSElMPa · %/ratiopre-strainconverti-Plating
ExamplePlatingMPa%1000%TS 2 *El*λ*10 −7mmbilityadhesionNote
1′GA99828.228.1511432.0—ExPresent Invention
2′GA100929.429.614425.0—ExComparative Example
3′GA66135.023.259902.0—ExComparative Example
4′GA102028.829.4341023.0—ExPresent Invention
5′GA101928.328.925753.0—ExComparative Example
6′GA101528.528.9451324.0—GComparative Example
7′GA93530.228.236963.0—ExPresent Invention
8′GA86833.128.727684.0—ExComparative Example
9′GA100226.826.8481294.0—BComparative Example
10′GA104927.028.3481443.0—GPresent Invention
11′GA103726.127.1531482.0—GPresent Invention
12′GA103328.929.8501532.0—GPresent Invention
13′GA106529.731.7511723.0—ExPresent Invention
14′GA94432.230.4351002.0—ExPresent Invention
15′GA95433.031.514435.0—ExComparative Example
16′GA102027.628.1451302.0—ExPresent Invention
17′GI99829.329.3531532.0—ExPresent Invention
18′GA118821.825.9421302.0—ExPresent Invention
19′GA121220.925.3491512.0—ExPresent Invention
20′GA125122.327.9441554.0—GComparative Example
21′GA120624.028.9461614.0—GComparative Example
22′GA115821.024.319545.0—BComparative Example
23′GA155220.932.4281413.0—ExPresent Invention
24′GA151621.031.917823.0—ExPresent Invention
25′GA148321.131.3291355.0—GComparative Example
26′GA142923.233.2271283.0—ExPresent Invention
27′GA70239.527.749963.0—ExPresent Invention
28′GA81131.825.8561182.0—ExPresent Invention
29′GA81231.325.4511044.0—BComparative Example
30′GA81330.524.8501014.0—ExComparative Example
31′GA108813.314.537583.0—ExComparative Example
32′GA74733.625.1561053.0—ExPresent Invention
31′GA73829.922.0631032.0—ExPresent Invention
34′GA85120.317.349725.0—ExComparative Example
35′GA92229.126.8471162.0—ExPresent Invention
36′GA93627.926.1481192.0—ExPresent Invention
37′GA84129.524.8501042.0—ExPresent Invention
38′GA85328.724.5521092.0—ExPresent Invention
39′GA120026.832.2401562.0—ExPresent Invention
40′GA155324.037.410583.0—ExComparative Example
41′GA128126.033.2271153.0—ExPresent Invention
42′GA110029.031.9391393.0—ExPresent Invention
43′GA129822.729.415574.0—ExComparative Example
TABLE 25 — Minimum
TS · EL/Holebend
Experi-1000expansionradius after
mentalTSElMPa · %/ratiopre-strainChemicalPlating
ExamplePlatingMPa%1000%TS 2 *El*λ*10 −7mmconvertibilityadhesionNote
44′GA132726.635.3231082.0—ExPresent Invention
45′GA106728.930.8491602.0—ExPresent Invention
46′GA102028.228.7381102.0—ExPresent Invention
47′GA98024.123.639892.0—ExPresent Invention
48′GA91022.720.732593.0—ExComparative Example
49′GA103325.426.2491333.0—ExPresent Invention
50′GA94128.126.5431073.0—ExPresent Invention
51′GA87329.125.441903.0—ExPresent Invention
52′GA114126.029.719644.0—ExComparative Example
53′GA107626.228.221635.0—BComparative Example
54′GA106828.830.7341113.0—ExPresent Invention
55′GA91827.325.1441022.0—ExPresent Invention
56′GA104326.827.9521514.0—GComparative Example
57′GA92530.928.5401052.0—ExPresent Invention
58′GA106023.424.8401052.0—ExPresent Invention
59′GI88527.524.3591263.0—ExPresent Invention
60′GA104016.116.7591022.0—ExPresent Invention
61′GA82130.925.4481002.0—ExPresent Invention
62′GA94728.226.7571452.0—ExPresent Invention
63′GA100429.129.2341002.0—ExPresent Invention
64′GA125726.633.4431792.0—ExPresent Invention
65′GA101028.729.0571672.0—ExPresent Invention
66′GA99828.027.9481342.0—ExPresent Invention
67′GA96223.022.142902.0—ExPresent Invention
68′GA111027.530.5441482.0—ExPresent Invention
69′GA90419.217.446722.0—ExComparative Example
70′GA67734.123.155852.0—ExComparative Example
71′GA104928.730.2421333.0—GPresent Invention
72′GA104628.529.8411262.0—ExPresent Invention
73′GA110923.426.031902.0—ExPresent Invention
74′GI107027.829.8461472.0—ExPresent Invention
75′QA100329.329.4481412.0—ExPresent Invention
76′GA60538.023.052732.0—ExComparative Example
77′GA85925.722.114276.0—ExComparative Example
78′GA62633.621.0841112.0—ExComparative Example
79′GA121321.526.05165.0—ExComparative Example
80′GA15169.914.96135.0—ExComparative Example
81′GA102129.830.4491522.0—ExPresent Invention
82′GA104927.128.4551642.0—ExPresent Invention
83′GA102629.530.3481492.0—ExPresent Invention
84′GA110823.225.7461312.0—ExPresent Invention
85′GA100628.028.2591672.0—ExPresent Invention
86′GI100030.430.4481462.0—ExPresent Invention
87′GA124722.628.2431512.0—ExPresent Invention
88′GA158320.131.8291463.0—ExPresent Invention
89′GA93526.424.7551272.0—ExPresent Invention

Claims as granted

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Classifications

16 codes
IPC · International Patent Classification
Section C — Chemistry; metallurgy
  • C21D9/00
  • C22C38/52
  • C22C38/46
  • C22C38/50
  • C22C38/58
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  • C22C38/02
  • C23C2/40
  • C22C38/54
  • C21D9/46
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  • C21D8/02
  • C23C2/06
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  • C22C38/00

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⤢ drag to zoomJan 2018Jul 2018Jan 2019Jul 2019Jan 2020Jul 2020Jan 2021Jul 2021Jan 2022Jul 2022USPTOApplicantNon-final rejection
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Pendency
4.5 y
1,635 days filing → grant
Office actions
1
non-final + final
Responses
1
no RCE
Examiner
Anthony M Liang
art unit 1738 · TC 1700
Citations: 26 back · 1 forward

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