USPatent applicationPatented

High-strength steel sheet excellent in impact resistance and manufacturing method thereof, and high-strength galvanized steel sheet and manufacturing method thereof

Granted 16 Jul 2019 · 5 office actions

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Abstract

The present invention provides a high-strength steel sheet excellent in impact resistance. The high-strength steel sheet contains predetermined contents of C, Si, Mn, P, S, Al, Ti, N, and O, with the balance being iron and inevitable impurities, and has a steel sheet structure in which, in a ⅛ thickness to ⅜ thickness region across ¼ of a sheet thickness, 1 to 8% retained austenite is contained in volume fraction, an average aspect ratio of the retained austenite is 2.0 or less, an amount of solid-solution Mn in the retained austenite is 1.1 times an average amount of Mn or more, and TiN grains having a 0.5 μm average grain diameter or less are contained, and a density of AlN grains with a 1 μm grain diameter or more is 1.0 pieces/mm 2 or less, wherein a maximum tensile strength is 900 MPa or more.

Description

16 parts
›TECHNICAL FIELD

The present invention relates to a high-strength steel sheet and a manufacturing method thereof, and a high-strength galvanized steel sheet and a manufacturing method thereof, and more particularly to a high-strength steel sheet having excellent impact resistance and a manufacturing method thereof. This application is based upon and claims the benefit of priority of the prior Japanese Patent Application No. 2011-167661, filed on Jul. 29, 2011, the entire contents of which are incorporated herein by reference.

›BACKGROUND ART

In recent years, there has been a demand not only for improvement in strength of steel sheets used in automobiles but also for improvement in impact resistance thereof, in order to enhance collision safety while realizing a weight reduction of automobiles.

As a high-strength steel sheet having large collision absorbing energy, Patent Document 1 describes a high-strength steel sheet containing, in weight %, C: 0.05 to 0.3%, Si: 2.0% or less, Al: 0.01 to 2.0%, Mn: 0.5 to 4.0%, Ni: 0 to 5.0%, P: 0.1% or less, S: 0.1% or less, and N: 0.01% or less, with the balance being Fe and inevitable impurities, and having a chemical composition satisfying 1.5−3.0×C≤Si+Al≤3.5−5.0×C and Mn+(Ni/3)≥1.0(%), wherein a bake hardening amount of the steel sheet is 50 MPa or more.

Further, as a high-tension steel sheet excellent in collision absorbency, Patent Document 2 describes a high-ductility, high-tension steel sheet which has a steel structure including: bainite having a volume fraction VB given by an expression VB≤(TSs/60)−1 (TSs: tensile strength (MPa) in a static tensile test); and retained austenite whose C content is 1.2 mass % or less and whose volume fraction is 5% or more, with the balance being ferrite, wherein a yield ratio in the static tensile test is 0.6 or more, and a static-dynamic ratio of the steel sheet is high, with a ratio TSd/TSs between tensile strength in a dynamic tensile test and tensile strength in the static tensile test satisfying a relation given by an expression TSd/TSs≥0.8+(300/TSs) (Tsd: the tensile strength (MPa) in the dynamic tensile test at a 1000/s strain rate).

Further, as a method of manufacturing a high-strength cold-rolled steel sheet excellent in impact property, Patent Document 3 describes a manufacturing method including: hot-rolling a slab which has a composition containing C: 0.08 to 0.18 mass %, Si: 1.00 to 2.0 mass %, Mn: 1.5 to 3.0 mass %, P: 0.03 mass % or less, S: 0.005% mass % or less, and T.Al: 0.01 to 0.1 mass % and in which a Mn segregation degree defined by an expression (Mn segregation degree=(a Mn concentration at a center portion of the slab−a Mn concentration at a base)/the Mn concentration at the base) is 1.05 to 1.10; after cold-rolling, performing heating in a two-phase region or a single-phase region of 750 to 870° C. for a 60 second retention time or longer on a continuous annealing line; thereafter, after cooling in a 720 to 600° C. temperature region at a 10° C./s average cooling rate or less, performing cooling to 350 to 460° C. at a 10° C./s average cooling rate or more to keep this temperature for 30 seconds to 20 minutes, and thereafter performing cooling to room temperature to produce a five-phase structure of polygonal ferrite+acicular ferrite+bainite+retained austenite+martensite.

As a steel sheet used as a steel sheet for automobiles, Patent Document 4 describes an alloyed hot-dip galvanized steel sheet containing, in mass %, C: 0.05 to 0.25%, Si: 0.5% or less, Mn: 1 to 3%, P: 0.1% or less, S: 0.01% or less, Al: 0.1 to 2%, and N: less than 0.005%, with the balance being Fe and inevitable impurities, wherein Si+Al≥0.6%, (0.0006Al) %≤N≤0.0058%−(0.0026×Al) %, and Al≤(1.25×C 0.5 −0.57 Si+0.625 Mn) % are satisfied.

As a high-strength alloyed hot-dip galvanized steel sheet excellent in energy absorbency, Patent Document 5 describes one whose base material is a steel sheet having: a component composition containing C: 0.05 to 0.20 mass %, Si: 0.3 to 1.5 mass %, Mn: 1.0 to 2.5 mass %, and P: 0.1 mass % or less, with the balance being Fe and inevitable impurities; and a microstructure containing one or two out of martensite and retained austenite totally in 25 to 50 vol %, with the balance being ferrite and bainite, wherein alloying hot-dip galvanization is applied to both surfaces of the steel sheet.

As a high-ductility, high-tension cold-rolled steel sheet excellent in surface property and impact absorbency, Patent Document 6 describes one containing, in weight ratio, C: 0.06 to 0.25%, Si: 2.5% or less, Mn: 0.5 to 3.0%, P: 0.1% or less, S: 0.03% or less, Al: 0.1 to 2.5%, Ti: 0.003 to 0.08%, and N: 0.01% or less, with the balance being Fe and inevitable impurities, wherein a Ti content satisfies a relation of (48/14)N≤Ti≤(48/14)N+(48/32)S+0.01, and a structure after cold rolling-recrystallization annealing is a structure containing 5% retained austenite or more in volume fraction.

As a high-ductility, high-strength steel sheet excellent in low-temperature toughness, Patent Document 7 describes one having a structure which contains, in area %, 60% bainite or more and 1 to 20% retained γ, with the balance being substantially ferrite, wherein the retained γ exists in a grain of the bainite.

›PRIOR ART DOCUMENT

Patent Document

Patent Document 1: Japanese Laid-open Patent Publication No. 2001-11565

Patent Document 2: Japanese Laid-open Patent Publication No. 2002-294400

Patent Document 3: Japanese Laid-open Patent Publication No. 2004-300452

Patent Document 4: Japanese Laid-open Patent Publication No. 2006-307327

Patent Document 5: Japanese Laid-open Patent Publication No. 2009-68039

Patent Document 6: Japanese Laid-open Patent Publication No. H10-130776

Patent Document 7: Japanese Laid-open Patent Publication No. H11-21653

›DISCLOSURE OF THE INVENTION · 1 of 2

Problems to be Solved by the Invention

However, in the conventional arts, it is not possible to obtain sufficient impact resistance in a high-strength steel sheet having 900 MPa maximum tensile strength or more, and there has been a demand for a further improvement in impact resistance.

In view of the above-described circumstances, the present invention provides a high-strength steel sheet having excellent impact resistance and a manufacturing method thereof, and a high-strength galvanized steel sheet in which a galvanized layer is formed on a surface of a high-strength steel sheet excellent in impact resistance and a manufacturing method thereof.

Means for Solving the Problems

The present inventors repeated studious studies for obtaining a high-strength steel sheet whose maximum tensile strength is 900 MPa or more with which excellent impact resistance is obtained. As a result, the present inventors have found out that it is necessary that a steel sheet has a predetermined chemical composition containing Al: 0.001 to 0.050%, Ti: 0.0010 to 0.0150%, and N: 0.0001 to 0.0050%, and in a ⅛ thickness to ⅜ thickness region across ¼ of a sheet thickness, a steel sheet structure contains 1 to 8% retained austenite in volume fraction, an average aspect ratio of the retained austenite is 2.0 or less, an amount of solid-solution Mn in the retained austenite is 1.1 times an average amount of Mn or more, TiN grains with a 0.5 μm average grain diameter or less are contained, and a density of AlN grains with a 1 μm grain diameter or more is 1.0 pieces/mm 2 or less.

That is, the above-described high-strength steel sheet is one which contains Al, Ti, and N in the aforesaid ranges and in which the generation of the AlN grains with an 1 μm average grain diameter or more which become starting points of destruction at low temperatures is suppressed by the generation of the fine TiN grains with a 0.5 μm grains diameter or less, and therefore, the density of the AlN grains with a 1 μM grain diameter or more is low, that is, 1.0 pieces/mm 2 or less. Therefore, in the above-described high-strength steel sheet, destruction starting from the AlN grains is prevented.

Further, in the above-described high-strength steel sheet, the volume fraction of the retained austenite which become the starting points of the destruction is 1 to 8% and thus is small, the retained austenite has a stable shape excellent in isotropy, with the average aspect ratio being 2.0 or less, and the retained austenite is chemically stable, with an amount of the solid-solution Mn in the retained austenite being 1.1 times the average amount of Mn or more. Therefore, in the above-described high-strength steel sheet, destruction starting from the retained austenite is prevented.

As described above, in the above-described high-strength steel sheet, since the destruction starting from the AlN grains and the destruction starting from the retained austenite are prevented, it is possible to obtain excellent impact resistance.

The present invention was completed based on such findings, and its gist is as follows.

(1)

A high-strength steel sheet excellent in impact resistance containing, in mass %, C: 0.075 to 0.300%, Si: 0.30 to 2.50%, Mn: 1.30 to 3.50%, P: 0.001 to 0.050%, S: 0.0001 to 0.0050%, Al: 0.001 to 0.050%, Ti: 0.0010 to 0.0150%, N: 0.0001 to 0.0050%, and O: 0.0001 to 0.0030%, with the balance being iron and inevitable impurities, and having a steel sheet structure in which, in a ⅛ thickness to ⅜ thickness region across ¼ of a sheet thickness, 1 to 8% retained austenite is contained in volume fraction, an average aspect ratio of the retained austenite is 2.0 or less, an amount of solid-solution Mn in the retained austenite is 1.1 times an average amount of Mn or more, TiN grains having a 0.5 μm average grain diameter or less are contained, and a density of AlN grains with a 1 μm grain diameter or more is 1.0 pieces/mm 2 or less, wherein maximum tensile strength is 900 MPa or more.

(2)

The high-strength steel sheet excellent in impact resistance according to (1), wherein the steel sheet structure contains, in volume fraction, 10 to 75% ferrite, one of or both of bainitic ferrite and bainite totally in 10 to 50%, and 10 to 50% tempered martensite, and

wherein pearlite is limited to 5% or less in volume fraction, and fresh martensite is limited to 15% or less in volume fraction.

(3)

The high-strength steel sheet excellent in impact resistance according to (1), further containing, in mass %, one or two or more of Nb: 0.0010 to 0.0150%, V: 0.010 to 0.150%, and B: 0.0001 to 0.0100%.

(4)

The high-strength steel sheet excellent in impact resistance according to (1), further containing, in mass %, one or two or more of Cr: 0.01 to 2.00%, Ni: 0.01 to 2.00%, Cu: 0.01 to 2.00%, Mo: 0.01 to 1.00%, and W: 0.01 to 1.00%.

(5)

The high-strength steel sheet excellent in impact resistance according to (1), further containing one or two or more of Ca, Ce, Mg, Zr, Hf, and REM totally in 0.0001 to 0.5000 mass %.

(6)

The high-strength galvanized steel sheet excellent in impact resistance according to (1), wherein a galvanized layer is formed on a surface.

(7)

The high-strength galvanized steel sheet excellent in impact resistance according to (6), wherein a coating film made of a phosphorus oxide and/or a composite oxide containing phosphorus is formed on the surface of the galvanized layer.

(8)

A manufacturing method of a high-strength steel sheet excellent in impact resistance, the method including: a hot-rolling step in which a slab containing, in mass %, C: 0.075 to 0.300%, Si: 0.30 to 2.50%, Mn: 1.30 to 3.50%, P: 0.001 to 0.050%, S: 0.0001 to 0.0050%, Al: 0.001 to 0.050%, Ti: 0.0010 to 0.0150%, N: 0.0001 to 0.0050%, and O: 0.0001 to 0.0030%, with the balance being iron and inevitable impurities is heated to 1210° C. or higher, reduction is performed under a condition satisfying the following (Expression 1) at least in a temperature range of 1100 to 1000° C., the reduction is finished at a finish hot-rolling temperature that is not lower than a higher temperature of 800° C. and an Ar 3 transformation point nor higher than 970° C., coiling is performed in a temperature region of 750° C. or lower, and cooling is performed at an average cooling rate of 15° C./hour or less; a cold-rolling step in which cold-rolling is performed at a reduction ratio of 30 to 75% after the hot-rolling step; and a continuous annealing step of performing, after the cold-rolling step, annealing where heating is performed in a temperature range of 550 to 700° C. at an average heating rate of 10° C./second or less, a maximum heating temperature is set to a temperature between (an Ac 1 transformation point+40) and 1000° C., cooling is performed in a temperature range of the maximum heating temperature to 700° C. at an average cooling rate of 1.0 to 10.0° C./second, cooling is performed in a temperature range of 700 to 500° C. at an average cooling rate of 5.0 to 200.0° C./second, and a retention process is performed in a temperature range of 350 to 450° C. for 30 to 1000 seconds.

›DISCLOSURE OF THE INVENTION · 2 of 2

In (Expression 1), i represents the number of passes, Ti represents a working temperature of the i th pass, ti represents an elapsed time from the i th pass to the i+1 th pass, and εi represents a reduction ratio of the i th pass.

(9)

A method of manufacturing a high-strength galvanized steel sheet excellent in impact resistance, wherein, in the continuous annealing step of the manufacturing method according to (8), a galvanized layer is formed on a surface of the steel sheet by applying electrogalvanization after the retention process.

(10)

A manufacturing method of a high-strength galvanized steel sheet excellent in impact resistance, wherein, in the continuous annealing step of the manufacturing method according to (8), after the cooling in the temperature range of 700 to 500° C., the steel sheet is immersed in a galvanizing bath to form a galvanized layer on a surface of the steel sheet before the retention process in the temperature range of 350 to 450° C. or after the retention process.

(11)

The manufacturing method of the high-strength galvanized steel sheet excellent in impact resistance according to (10), wherein, after immersed in the galvanizing bath, the steel sheet is re-heated to 460 to 600° C. and is retained for two seconds or longer to alloy the galvanized layer.

(12)

The manufacturing method of the high-strength galvanized steel sheet excellent in impact resistance according to (10), wherein, after the galvanized layer is formed, a coating film made of a phosphorus oxide and/or a composite oxide containing phosphorus is applied on a surface of the galvanized layer.

(13)

The manufacturing method of the high-strength galvanized steel sheet excellent in impact resistance according to (11), wherein, after the galvanized layer is alloyed, a coating film made of a phosphorus oxide and/or a composite oxide containing phosphorus is applied on a surface of the alloyed galvanized layer.

Effect of the Invention

In the high-strength steel sheet of the present invention, since the AlN grains and the retained austenite are prevented from working as starting points of destruction, it is possible to obtain a high-strength steel sheet having excellent impact resistance and having a maximum tensile strength of 900 MPa or more. Further, according to the manufacturing method of the high-strength steel sheet of the present invention, it is possible to provide a high-strength steel sheet having excellent impact resistance and having maximum tensile strength of 900 MPa or more. Further, according to the present invention, it is possible to provide a high-strength galvanized steel sheet in which a galvanized layer is formed on a surface of a high-strength steel sheet excellent in impact resistance and a manufacturing method thereof.

›BEST MODE FOR CARRYING OUT THE INVENTION · 1 of 9

(Chemical Components)

First, chemical components (composition) of the high-strength steel sheet of the present invention will be described. Note that [%] in the following description represents [mass %].

The high-strength steel sheet of the present invention contains C: 0.075 to 0.300%, Si: 0.30 to 2.50%, Mn: 1.30 to 3.50%, P: 0.001 to 0.050%, S: 0.0001 to 0.0050%, Al: 0.001 to 0.050%, Ti: 0.0010 to 0.0150%, N: 0.0001 to 0.0050%, and O: 0.0001 to 0.0030%, with the balance being iron and inevitable impurities.

“C: 0.075 to 0.300%”

C is contained in order to increase strength of the high-strength steel sheet. However, when the content of C is over 0.300%, weldability becomes insufficient. In view of weldability, the content of C is preferably 0.250% or less, and more preferably 0.220% or less. On the other hand, when the content of C is less than 0.075%, strength lowers and it is not possible to ensure maximum tensile strength of 900 MPa or more. In order to increase strength, the content of C is preferably 0.090% or more, and more preferably 0.100% or more.

“Si: 0.30 to 2.50%”

Si is an element necessary for suppressing the generation of an iron-based carbide in the steel sheet and for increasing strength and formability. However, when the content of Si is over 2.50%, the steel sheet becomes brittle, so that its ductility deteriorates. In view of ductility, the content of Si is preferably 2.20% or less, and more preferably 2.00% or less. On the other hand, when the content of Si is less than 0.30%, a large amount of a coarse iron-based carbide is generated in an annealing step, resulting in deterioration in strength and formability. From this point of view, a lower limit value of Si is preferably 0.50% or more, and more preferably 0.70% or more.

“Mn: 1.30 to 3.50%”

Mn is added to the steel sheet of the present invention in order to increase strength of the steel sheet. However, when the content of Mn is over 3.50%, a coarse Mn concentrated portion is generated in a thickness center portion of the steel sheet, which is likely to cause embrittlement and to cause a trouble such as cracking of a cast slab. Further, when the content of Mn is over 3.50%, weldability also deteriorates. Therefore, the content of Mn needs to be 3.50% or less. In view of weldability, the content of Mn is preferably 3.20% or less, and more preferably 3.00% or less. On the other hand, when the content of Mn is less than 1.30%, a large amount of a soft structure is formed during cooling after the annealing, which makes it difficult to ensure the maximum tensile strength of 900 MPa or more. Therefore, the content of Mn needs to be 1.30% or more. In order to increase strength, the content of Mn is preferably 1.50% or more, and more preferably 1.70% or more.

“P: 0.001 to 0.050%”

P tends to segregate in the thickness center portion of the steel sheet and makes a welded portion brittle. When the content of P is over 0.050%, the welded portion is greatly made brittle, and therefore, the content of P is limited to 0.050% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of P, but setting the content of P to less than 0.001% is accompanied by a great increase in manufacturing cost, and therefore, 0.001% is set as the lower limit value.

“S: 0.0001 to 0.0050%”

S has an adverse effect on weldability and manufacturability at the time of casting and at the time of hot-rolling. Further, S coupled with Ti generates a sulfide to prevent Ti from becoming a nitride and to indirectly induce the generation of an Al nitride, and therefore, an upper limit value of the content of S is set to 0.0050%. From this point of view, the content of S is preferably 0.035% or less, and more preferably 0.0025% or less. The effects of the present invention are exhibited without particularly limiting the lower limit of the content of S, but setting the content of S to less than 0.0001% is accompanied by a great increase in manufacturing cost, and therefore, 0.0001% is set as the lower limit value.

“Al: 0.001% to 0.050%”

Al, when added in large amount, forms a coarse nitride to lower a drawing value at low temperatures and to deteriorate impact resistance, and therefore, an upper limit of the content of Al is set to 0.050%. In order to avoid the generation of the coarse nitride, the content of Al is preferably 0.035% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of Al, but setting the content of Al to less than 0.001% is accompanied by a great increase in manufacturing cost, and therefore, 0.001% is set as the lower limit value. Further, Al is an effective element as a deoxidizing material, and from this point of view, the content of Al is preferably 0.005% or more, and more preferably 0.010% or more.

“N: 0.0001 to 0.0050%”

Since N forms a coarse nitride working as a starting point of destruction at low temperatures and deteriorates impact resistance, its addition amount needs to be reduced. When the content of N is over 0.0050%, this influence becomes prominent, and therefore, a range of the content of N is set to 0.0050% or less. From this point of view, the content of N is preferably 0.0040% or less, and more preferably 0.0030% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of N, but setting the content of N to less than 0.0001% causes a great increase in manufacturing cost, and therefore, 0.0001% is set as the lower limit value.

“O: 0.0001 to 0.0030%”

Since O forms a coarse oxide and generates a starting point of destruction at low temperatures, its content needs to be reduced. When the content of O is over 0.0030%, this influence becomes prominent, and therefore, an upper limit of the content of O is set to 0.0030% or less. From this point of view, the content of O is preferably 0.0020% or less, and more preferably 0.0010% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of 0, but setting the content of O to less than 0.0001% is accompanied by a great increase in manufacturing cost, and therefore, 0.0001% is set as the lower limit.

›BEST MODE FOR CARRYING OUT THE INVENTION · 2 of 9

“Ti: 0.0010 to 0.0150%”

Ti is an element that forms a fine nitride as a result of hot-rolling under an appropriate condition and suppresses the generation of the coarse Al nitride, and it reduces the starting points of destruction at low temperatures and improves impact resistance. In order to obtain this effect, the content of Ti needs to be 0.0010% or more, and the content of Ti is preferably 0.0030% or more, and more preferably 0.0050% or more. On the other hand, when the content of Ti is over 0.0150%, formability of a soft portion in the steel sheet deteriorates due to the segregation of a fine carbonitride, which lowers a drawing value at low temperatures, instead. Therefore, the content of Ti is set to 0.0150% or less. In view of formability, the content of Ti is preferably 0.0120% or less, and more preferably 0.0100% or less.

The high-strength steel sheet of the present invention may further contain the following elements when necessary.

“Nb: 0.0010 to 0.0150%”

Nb is an element that forms a fine nitride as a result of applying the hot-rolling under an appropriate condition and suppresses the generation of the coarse Al nitride, and it reduces the starting points of destruction at low temperatures. In order to obtain this effect, the content of Nb is preferably 0.0010% or more, and the content of Nb is more preferably 0.0030% or more, and still more preferably 0.0050% or more. On the other hand, when the content of Nb is over 0.0150%, formability of the soft portion in the steel sheet deteriorates due to the segregation of a fine carbonitride, which lowers the drawing value at low temperatures, instead, and therefore, the content of Nb is preferably 0.0150% or less. In view of formability, the content of Nb is more preferably 0.0120% or less, and still more preferably 0.0100% or less.

“V: 0.010 to 0.150%”

V is an element that forms a fine nitride as a result of applying the hot rolling under an appropriate condition and suppresses the generation of the coarse Al nitride, and reduces the starting points of destruction at low temperatures. In order to obtain this effect, the content of V needs to be 0.010% or more, and its content is preferably 0.030% or more, and more preferably 0.050% or more. On the other hand, when the content of V is over 0.150%, formability of the soft portion in the steel sheet deteriorates due to the segregation of a fine carbonitride, which lowers the drawing value at low temperatures, instead, and therefore, the content of V is preferably 0.150% or less. In view of formability, the content of V is more preferably 0.120% or less, and still more preferably 0.100% or less.

“B: 0.0001 to 0.0100%”

B is an element that forms a fine nitride as a result of applying the hot rolling under an appropriate condition and suppresses the generation of the coarse Al nitride, and reduces the starting points of destruction at low temperatures. In order to obtain this effect, the content of B is preferably 0.0001% or more, and the content of B is preferably 0.0003% or more, and more preferably 0.0005% or more. Further, B is an element that suppresses phase transformation at high temperatures and that is effective for increasing strength, and may be added more, but when the content of B is over 0.0100%, workability in the hot working is impaired, leading to deterioration in productivity, and therefore, the content of B is preferably 0.0100% or less. In view of productivity, the content of B is more preferably 0.0050% or less, and still more preferably 0.0030% or less.

“Cr: 0.01 to 2.00%”

Cr is an element that suppresses the phase transformation at high temperatures and is effective for increasing strength, and may be added instead of part of C and/or Mn. When the content of Cr is over 2.00%, workability in the hot working is impaired, leading to deterioration in productivity, and therefore, the content of Cr is preferably 2.00% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of Cr, but in order to sufficiently obtain the effect of increasing strength by Cr, the content of Cr is preferably 0.01% or more.

“Ni: 0.01 to 2.00%”

Ni is an element that suppresses the phase transformation at high temperatures and is effective for increasing strength, and may be added instead of part of C and/or Mn. When the content of Ni is over 2.00%, weldability is impaired, and therefore, the content of Ni is preferably 2.00% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of Ni, but in order to sufficiently obtain the effect of increasing strength by Ni, the content of Ni is preferably 0.01% or more.

“Cu: 0.01 to 2.00%”

Cu is an element that increases strength when existing in steel as fine grains, and may be added instead of part of C and/or Mn. When the content of Cu is over 2.00%, weldability is impaired, and therefore, the content of Cu is preferably 2.00% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of Cu, but in order to sufficiently obtain the effect of increasing strength by Cu, the content of Cu is preferably 0.01% or more.

“Mo: 0.01 to 1.00%”

Mo is an element that suppresses the phase transformation at high temperatures and is effective for increasing strength, and may be added instead of part of C and/or Mn. When the content of Mo is over 1.00%, workability in the hot working is impaired, leading to deterioration in productivity. Therefore, the content of Mo is preferably 1.00% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of Mo, but in order to sufficiently obtain the effect of increasing strength by Mo, the content of Mo is preferably 0.01% or more.

“W: 0.01 to 1.00%”

W is an element that suppresses the phase transformation at high temperatures and is effective for increasing strength, and may be added instead of part of C and/or Mn. When the content of W is over 1.00%, workability in the hot working is impaired, leading to deterioration in productivity, and therefore, the content of W is preferably 1.00% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of W, but in order to sufficiently obtain the effect of increasing strength by W, the content of W is preferably 0.01% or more.

›BEST MODE FOR CARRYING OUT THE INVENTION · 3 of 9

“One or two or more of Ca, Ce, Mg, Zr, Hf, and REM totally in 0.0001 to 0.5000%”

Ca, Ce, Mg, Zr, Hf, and REM are elements effective for improving formability, and one or two or more thereof can be added. However, when the total content of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM is over 0.5000%, ductility is liable to be lost, instead. Therefore, the total content of the elements is preferably 0.5000% or less. The effects of the present invention are exhibited without particularly setting a lower limit of the content of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM, but in order to sufficiently obtain the effect of improving formability of the steel sheet, the total content of the elements is preferably 0.0001% or more. In view of formability, the total content of one or two or more of Ca, Ce, Mg, Zr, Hf, and REM is more preferably 0.0005% or more, and still more preferably 0.0010% or more.

Note that REM stands for Rare Earth Metal and refers to an element belonging to a lanthanoid series. In the present invention, REM and Ce are often added as misch metal, and elements of the lanthanoid series are sometimes contained in a complex form in addition to La and Ce. Even when an element of the lanthanoid series other than these La and Ce is contained as inevitable impurities, the effects of the present invention are exhibited. Even when the metals La and Ce are added, the effects of the present invention are exhibited.

(Steel Sheet Structure)

A reason why the structure of the high-strength steel sheet of the present invention is stipulated is as follows.

“TiN Grains”

A steel sheet structure of the high-strength steel sheet of the present invention contains TiN grains having a 0.5 μm average grain diameter or less. Coarse TiN grains work as the starting points of destruction, but the fine TiN grains whose average grain diameter is 0.5 μm or less do not work as the starting points of the destruction. The average grain diameter of the TiN grains is preferably 0.3 μm or less, and more preferably 0.1 μm or less in order to effectively prevent the TiN grains from working as the starting points of destruction and to further improve impact resistance of the high-strength steel sheet.

The average grain diameter of the TiN grains is found by the following method, for instance.

Specifically, a sample for transmission electron microscope (TEM) containing TiN grains is prepared from a thicknesswise cross section parallel to a rolling direction by an extraction replica method, and 10 pieces or more of the TiN grains are observed by using a transmission electron microscope. A grain diameter of each of the TiN grains is defined as a diameter of a circle having an area equal to a projected area of the TiN grain obtained by image analysis. Then, the grain diameters of the 10 pieces or more of the TiN grains are measured, and from an average value thereof, the average grain diameter of the TiN grains is found.

“AlN Grains”

Further, in the steel sheet structure of the high-strength steel sheet of the present invention, a density of AlN grains having a 1 μm grain diameter or more is 1.0 pieces/mm 2 or less. The coarse AlN grains having a 1 μm grain diameter or more work as the starting points of destruction. In the steel sheet structure of the high-strength steel sheet of the present invention, since the density of the AlN grains having a 1 μm grain diameter or more is 1.0 pieces/mm 2 or less, the destruction starting from the AlN grains is prevented. In order to more effectively prevent the destruction starting from the AlN grains, the density of the AlN grains having a 1 μM grain diameter or more is preferably 0.5 pieces/mm 2 or less, and more preferably 0.1 pieces/mm 2 or less.

Incidentally, the average grain diameter of the TiN grains and the density of the AlN grains having a 1 μm grain diameter or more may be measured at any thickness position in the steel sheet except the uppermost surface of the steel sheet where an amount of the grains is small. For example, similarly to later-described retained austenite, ferrite, and so on, they are preferably measured at a ⅛ to ⅜ thickness position as an area representing the steel sheet, for instance.

In the present invention, the AlN grain having a 1 μM grain diameter or more means an AlN grain whose circle-equivalent diameter d is 1 μm or more. The circle-equivalent diameter d is a diameter of a circle having an area equal to a projected area S of the grain obtained by image analysis, and is found by the following expression. d=√{square root over ( )}(4S/π)

The density of the AlN grains in the present invention is found by the following method, for instance.

Specifically, a 10.0 mm 2 area or larger of the thicknesswise cross section parallel to the rolling direction is observed by using a field emission scanning electron microscope (FE-SEM), the number of 1 μm AlN grains or larger are counted, and the density thereof is calculated. Note that components of the AlN grains can be confirmed by using an energy dispersive X-ray spectroscope attached to the FE-SEM.

The steel sheet structure of the high-strength steel sheet of the present invention contains 1 to 8% retained austenite in volume fraction in a ⅛ thickness to ⅜ thickness region across ¼ of a sheet thickness, and an average aspect ratio of the retained austenite is 2.0 or less, and an amount of solid-solution Mn in the retained austenite is 1.1 times an average amount of Mn or more.

The volume fraction of the retained austenite is desirably 1 to 8% in the whole steel sheet structure. However, a metal structure in the ⅛ thickness to ⅜ thickness region across ¼ of the thickness of the steel sheet represents the structure of the whole steel sheet. Therefore, if the volume fraction of the retained austenite contained in the ⅛ thickness to ⅜ thickness region of the steel sheet is 1 to 8%, it can be considered that the volume fraction of the retained austenite contained in the whole structure of the steel sheet is 1 to 8%. Therefore, in the present invention, a range of the volume fraction of the retained austenite in the ⅛ thickness to ⅜ thickness region of the base steel sheet is stipulated.

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Further, it is preferable that, in the ⅛ thickness to ⅜ thickness region, the steel sheet structure of the high-strength steel sheet of the present invention contains, in volume fraction, 10 to 75% ferrite, one of or both of bainitic ferrite and bainite totally in 10 to 50%, and 5 to 50% tempered martensite besides the retained austenite, pearlite is limited to 5% or less in volume fraction, and fresh martensite is limited to 15% or less in volume fraction. The high-strength steel sheet of the present invention, when having such a steel sheet structure, has more excellent formability.

Similarly, these metal structures such as the ferrite are desirably in the predetermined ranges in the whole steel sheet structure. However, the metal structure in the ⅛ thickness to ⅜ thickness region across ¼ of the thickness of the steel sheet represents the structure of the whole steel sheet. Therefore, if, in the ⅛ thickness to ⅜ thickness region of the steel sheet, 10 to 75% ferrite, one of or both of bainitic ferrite and bainite totally in 10 to 50%, and 5 to 50% tempered martensite are contained in volume fraction, pearlite is limited to 5% or less in volume fraction, and fresh martensite is limited to 15% or less in volume fraction, it can be considered that these metal structures such as the ferrite are substantially in the predetermined ranges in the whole structure of the steel sheet. Therefore, in the present invention, in the ⅛ thickness to ⅜ thickness region of the steel sheet, the ranges of the volume fractions of these metal structures such as the ferrite are stipulated.

“Retained Austenite”

The retained austenite needs to be contained within a range not impairing the drawing value at low temperatures in order to greatly improve strength and ductility. When the volume fraction of the retained austenite is less than 1%, the improvement in strength and ductility is insufficient, and this is set as a low limit. In view of strength and formability, an amount of the retained austenite is preferably 1.5% or more, and preferably 2.0% or more. On the other hand, since the retained austenite works as the starting point of destruction to greatly deteriorate bendability; its volume fraction in the steel sheet structure needs to be limited to 8% or less. In order to increase bendability, the volume fraction of the retained austenite is more preferably 6% or less.

Further, in order to prevent the destruction starting from the retained austenite, it is preferable that the retained austenite has a stable shape and is chemically stable.

In the present invention, the retained austenite has a 2.0 average aspect ratio or less and has a stable shape excellent in isotropy. In order to make the shape of the retained austenite more stable, the average aspect ratio of the retained austenite is preferably 1.8 or less, and more preferably 1.6 or less. A lower limit of the average aspect ratio of the retained austenite is 1.0. When the average aspect ratio is over 2.0, part of the retained austenite easily transforms into martensite when stretched at low temperatures, so that the starting point of destruction is generated, leading to deterioration in the drawing value.

In the present invention, the amount of the solid-solution Mn in the retained austenite is 1.1 times the average amount of Mn or more “(the amount of the solid-solution Mn in the retained austenite/the average amount of Mn)≥1.1”, whereby the retained austenite is made chemically stable. In order to make the retained austenite more chemically stable, the amount of the solid-solution Mn in the retained austenite is preferably 1.2 times the average amount of Mn or more, and more preferably 1.3 times or more. Its upper limit is not particularly set, but to set it 2.0 times or more requires special facility, and 2.0 times is set as a practical upper limit.

“Ferrite”

The ferrite is a structure effective for improving the drawing value at low temperatures and is preferably contained in the steel sheet structure in 10 to 75% in volume fraction. When the volume fraction of the ferrite is less than 10%, a sufficient drawing value may not be obtained. In view of the drawing value, the volume fraction of the ferrite contained in the steel sheet structure is preferably 15% or more, and more preferably 20% or more. On the other hand, since the ferrite is a soft structure, when its volume fraction is over 75%, sufficient strength is not sometimes obtained. In order to sufficiently increase tensile strength of the steel sheet, the volume fraction of the ferrite contained in the steel sheet structure is preferably 65% or less, and more preferably 50% or less.

“Pearlite”

When an amount of the pearlite is large, ductility deteriorates. From this, the volume fraction of the pearlite contained in the structure of the steel sheet is preferably limited to 5% or less, and more preferably 2% or less.

“Bainitic Ferrite, Bainite”

The bainitic ferrite and the bainite are structures excellent in balance of strength and ductility, and the steel sheet structure preferably contains one of or both of the bainitic ferrite and the bainite totally in a 10 to 50% volume fraction. Further, the bainitic ferrite and the bainite are microstructures having intermediate strength between those of soft ferrite and hard martensite and between those of tempered martensite and retained austenite, and in view of stretch flangeability, their total content is preferably 15% or more, and still more preferably 20% or more. On the other hand, when the total volume fraction of the bainitic ferrite and the bainite is over 50%, a yield stress excessively increases to deteriorate shape fixability, which is not preferable. Incidentally, only one of the bainitic ferrite and the bainite may be contained, or both of them may be contained.

“Fresh Martensite”

The fresh martensite greatly improves tensile strength, but on the other hand, works as the starting point of destruction to greatly deteriorate the drawing value at low temperatures, and therefore its volume fraction in the steel sheet structure is preferably limited to 15% or less. In order to increase the drawing value at low temperatures, the volume fraction of the fresh martensite is more preferably 10% or less, and still more preferably 5% or less.

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“Tempered Martensite”

The tempered martensite is a structure that greatly improves tensile strength and may be contained in the steel sheet structure in 50% volume fraction or less. In view of tensile strength, the volume fraction of the tempered martensite is preferably 10% or more. On the other hand, when the volume fraction of the tempered martensite contained in the steel sheet structure is over 50%, a yield stress excessively increases and shape fixability deteriorates, which is not preferable.

“Others”

The steel sheet structure of the high-strength steel sheet may contain structures such as coarse cementite other than the above. However, when an amount of the coarse cementite becomes large in the steel sheet structure, bendability deteriorates. From this, the volume fraction of the coarse cementite contained in the steel sheet structure is preferably 10% or less, and more preferably 5% or less.

The volume fractions of the respective structures contained in the steel sheet structure of the high-strength steel sheet of the present invention can be measured by the following methods, for instance.

As for the volume fraction of the retained austenite, an X-ray diffraction test is conducted on a given surface that is parallel to a sheet surface of the steel sheet and is in the ⅛ thickness to ⅜ thickness region, an area fraction of the retained austenite is calculated, and this area fraction can be regarded as the volume fraction in the ⅛ thickness to ⅜ thickness region.

The microstructure in the ⅛ thickness to ⅜ thickness region has high homogeneity, and by the measurement in a sufficiently wide range, it is possible to obtain a microstructure fraction representing the fraction in the ⅛ thickness to ⅜ thickness region, at whichever place of the ⅛ thickness to ⅜ thickness the measurement is conducted. Concretely, the X-ray diffraction test is preferably conducted in a 250000 square En range or larger in a ¼ thickness surface parallel to the sheet surface of the steel sheet.

Further, the fractions of the microstructures (ferrite, bainitic ferrite, bainite, tempered martensite, pearlite, fresh martensite) except the retained austenite can be measured by the observation in the ⅛ thickness to ⅜ thickness region by an electron microscope. Concretely, a surface perpendicular to the sheet surface of the base steel sheet and parallel to the rolling direction (reduction direction) is set as an observation surface, and a sample is picked up therefrom, and the observation surface is polished and nital-etched. Then, the ⅛ thickness to ⅜ thickness region across ¼ of the sheet thickness is observed by a field emission scanning electron microscope (FE-SEM) to measure the area fraction. In this case, for example, the observation by the electron microscope is conducted in three or more fields of view which are set at intervals of 1 mm or more in the ⅛ thickness to ⅜ thickness region. Then, the area fractions of the respective structures such as the ferrite in a totally 5000 square μM region or larger of the observation area are calculated, and these area fractions can be regarded as the volume fractions of the respective structures in the ⅛ thickness to ⅜ thickness region.

The ferrite is a nugget-shaped crystal grain and is an area in which an iron-based carbide with a 100 nm major axis or more does not exist. Note that the volume fraction of the ferrite is the sum of a volume fraction of ferrite remaining at a maximum heating temperature and a volume fraction of ferrite newly generated at a ferrite transformation temperature region.

The bainitic ferrite is an aggregation of lath-shaped crystal grains and does not contain, inside the lath, an iron-based carbide having a 20 nm major axis or more.

The bainite is an aggregation of lath-shaped crystal grains and has, inside the lath, a plurality of iron-based carbides having a 20 nm major axis or more, and these carbides belong to a single variant, that is, to an iron-based carbide group extending in the same direction. Here, the iron-based carbide group extending in the same direction means that a difference in the extension direction in the iron-carbide group is within 5°.

The tempered martensite is an aggregation of lath-shaped crystal grains and has, inside the lath, a plurality of iron-based carbides having a 20 nm major axis or more, and these carbides belong to a plurality of variants, that is, a plurality of iron-based carbide groups extending in different directions.

By observing the iron-based carbides inside the lath-shaped crystal grains by using FE-SEM and examining the extension directions thereof, it is possible to easily discriminate between the bainite and the tempered martensite.

Further, the fresh martensite and the retained austenite are not corroded sufficiently by the nital etching. Therefore, in the observation by FE-SEM, they can be clearly discriminated from the aforesaid structures (ferrite, bainitic ferrite, bainite, and tempered martensite).

Therefore, the volume fraction of the fresh martensite is found as a difference between an area fraction of an uncorroded area observed by FE-SEM and an area fraction of the retained austenite measured by an X-ray.

(Galvanized Layer)

Further, the present invention can be a high-strength galvanized steel sheet excellent in impact resistance in which a galvanized layer is formed on a surface of the high-strength steel sheet. The galvanized layer may be alloyed. When the galvanized layer is formed on the surface of the high-strength steel sheet, the steel sheet has excellent corrosion resistance. Further, when the alloyed galvanized layer is formed on the surface of the high-strength steel sheet, the steel sheet has excellent corrosion resistance and is excellent in adhesiveness of a coating material. Further, the galvanized layer or the alloyed galvanized layer may contain Al as impurities.

The alloyed galvanized layer may contain one or two or more of Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi, Sr, I, Cs, and REM, or they may be mixed therein. Even when the alloyed galvanized layer contains one or two or more of the aforesaid elements, or they are mixed therein, the effects of the present invention are not impaired, and depending on the content thereof, this is sometimes preferable since corrosion resistance and workability are improved.

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Regarding an coating weight of the galvanized layer or the alloyed galvanized layer, any special restriction is not provided, but the coating weight is desirably 20 g/m 2 or more in view of corrosion resistance and 150 g/m 2 or less from an economic point of view. Further, an average thickness of the galvanized layer or the alloyed galvanized layer is set to not less than 1.0 μm nor more than 50 μm. When the average thickness is less than 1.0 μm, sufficient corrosion resistance is not obtained. Preferably, the average thickness is 2.0 μm or more. On the other hand, the average thickness of over 50.0 μm is not preferable because this is not economical and impairs strength of the steel sheet. In view of material cost, the thickness of the galvanized layer or the alloyed galvanized layer is preferably as small as possible, and is preferably 30.0 μm or less.

As for the average thickness of the plated layer, a thicknesswise cross section parallel to the rolling direction of the steel sheet is mirror-finished, the cross section is observed by using FE-SEM, and the thickness of the plated layer is measured at five points on each of a front surface and a rear surface of the steel sheet, totally at ten points, and an average value of the measured values is set as the thickness of the plated layer.

Incidentally, when the alloying process is applied, the content of iron of the alloyed galvanized layer is set to 8.0% or more and is preferably 9.0% or more in order to ensure good flaking resistance. Further, in order to ensure good powdering resistance, the content of the iron in the alloyed galvanized layer is set to 12.0% or less, and preferably 11.0% or less.

Further, in the present invention, a coating film made of a phosphorus oxide and/or a composite oxide containing phosphorus may be formed on the surface of the aforesaid galvanized layer or alloyed galvanized layer. The coating film made of the composite oxide containing the phosphorus oxide and/or phosphorus can function as a lubricant when the steel sheet is worked, and can protect the galvanized layer formed on the surface of the steel sheet.

(Manufacturing Method)

Next, a manufacturing method of the high-strength steel sheet of the present invention will be described in detail.

In order to manufacture the high-strength steel sheet of the present invention, a slab having the aforesaid chemical components (composition) is first formed by casting.

As the slab to be hot-rolled, a continuously cast slab or one manufactured by a thin slab caster or the like is usable. The manufacturing method of the high-strength steel sheet of the present invention is compatible with a process such as continuous casting-direct rolling (CC-DR) in which the hot rolling is performed immediately after the casting.

(Hot-Rolling Step)

In a hot-rolling step, a slab heating temperature needs to be 1210° C. or higher in order to sufficiently melt a Ti-based inclusion generated at the time of the casting and uniformly solid-dissolve Ti in the steel, and is preferably 1225° C. or higher. Further, when the slab heating temperature is excessively low, a finish rolling temperature becomes lower than an Ar 3 transformation point. As a result, the rolling is performed in a two-phase region of ferrite and austenite, a hot-rolled sheet structure becomes a heterogeneous duplex grain structure, and even after a cold-rolling step and a continuous annealing step, the heterogeneous structure does not disappear, resulting in a steel sheet poor in ductility and bendability. Further, the decrease in the slab heating temperature leads to an excessive increase in a rolling load, which involves a concern that the rolling becomes difficult and a shape of the steel sheet having undergone the rolling becomes poor. The effects of the present invention are exhibited without particularly setting an upper limit of the slab heating temperature, but excessively increasing the heating temperature is not preferable from an economic point of view, and therefore, the upper limit of the slab heating temperature is desirably 1350° C. or lower.

The Ar 3 transformation point is calculated by the following expression.

Ar 3 =901−325×C+33×Si−92×(Mn+Ni/2+Cr/2+Cu/2+Mo/2)+52×Al

In the above expression, C, Si, Mn, Ni, Cr, Cu, Mo, and Al are contents [mass %] of the respective elements. Elements not contained are calculated as 0.

In the present invention, after the heating to the aforesaid slab heating temperature, reduction is applied under a condition satisfying the following (Expression 1) in a temperature range of at least 1100 to 1000° C. In (Expression 1), i represents the number of passes, Ti represents a working temperature of the i th pass, ti is an elapsed time from the i th pass to the i+1 th pass, and εi represents a reduction ratio of the i th pass.

In order to manufacture a steel sheet containing fine TiN grains while suppressing the generation of coarse Ti nitride and Al nitride, a large amount of dislocation being a generation site of the Ti nitride needs to be introduced into the steel by hot rolling in a temperature range of 1100 to 1000° C. However, in the temperature range of 1100 to 1000° C., the dislocation introduced by the working easily extinguish due to the diffusion of Fe atoms. Therefore, the working (reduction) by which a strain amount large enough to sufficiently introduce the dislocation is obtained needs to be continuously performed in a relatively short time. That is, the number of passes needs to be plural, the elapsed time between the adjacent passes needs to be short, and a working temperature and a reduction ratio in each of the passes need to be appropriately controlled.

In the hot-rolling step, after the slab is taken out from a heating furnace, it is possible to perform the reduction of an arbitrary number of the passes in a temperature region up to a rolling completion temperature whose lower limit is the higher one of 850° C. and the Ar3 temperature. In the hot-rolling, the reduction performed in the range of 1100 to 1000° C. has a great influence on a dispersion state of the problematic TiN and AlN grains, and therefore, the hot rolling condition in the same temperature range is stipulated by using (Expression 1).

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Reduction performed in a temperature range of over 1100° C. does not influence the dispersion state of the problematic TiN and AlN grains since the dislocation introduced at the time of the transformation instantaneously extinguishes and does not work as a segregation site of TiN. On the other hand, by the time rolling is applied in a range of lower than 1000° C., the generation of nuclei of grains that can be coarse TiN and AlN is completed, and the rolling thereafter (the temperature range of lower than 1000° C.) does not influence the dispersion state of the problematic TiN and AlN grains.

Generally, during a period from an instant when the slab is taken out from the heating furnace to an instant when the rolling is completed, the rolling of 8 to 25 passes is performed. The reduction in the range of 1100° C. to 1000° C. is performed for 2 to 10 passes. Generally, the reduction in this temperature range starts from a 200 to 500 mm sheet thickness, and the rolling is performed up to a 10 to 50 mm sheet thickness. A sheet width is generally 500 to 2000 mm. Note that the temperature of the steel sheet is a temperature on the surface, and though its measuring method may be any, the temperature may be directly measured by using a thermocouple, for instance.

In (Expression 1), concretely, the number i of the passes can be in a range of 2 to 10, preferably in a range of 5 to 8, for instance. The elapsed time from the pass to i+1 th pass can be in a range of 2 to 300 seconds, preferably in a range of 5 to 180 seconds, and more preferably in a range of 10 to 120 seconds.

Further, the working temperature of the 1st pass being the initial pass in the hot-rolling in the temperature range of 1100 to 1000° C. can be in a range of 1100 to 1050° C., and preferably in a range of 1090 to 1065° C. The reduction ratio of the i th pass can be in a range of 5 to 50%, and preferably in a range of 15 to 35%.

In (Expression 1), which is an empirical formula expressing a generation behavior of the TiN grains, a diffusion distance of atoms is expressed by a product of a term of a polynomial expressing a driving force of the grain generation, an exp term expressing a diffusion coefficient of the atoms, and time t, and an amount of the dislocation introduced in accordance with the working is representatively expressed by the strain amount ε, and they are multiplied. When a value expressed by (Expression 1) is blow 1.0, the generation of TiN is insufficient, solid-solution N remains until an instant of the hot-rolling to 1000° C., and coarse AlN is generated. On the other hand, when the value expressed by (Expression 1) is over 5.0, the generation of TiN becomes excessively active, TiN is promoted to be coarse, and the property is impaired, instead.

In the present invention, by performing the reduction in the temperature range of at least 1100 to 1000° C. under the condition satisfying the above (Expression 1), the elapsed time between the adjacent plural passes is controlled to be relatively short and the working temperature and the reduction ratio in each of the passes are appropriately controlled, and therefore, a large amount of the dislocation being the generation site of the Ti nitride can be introduced into the steel, and the fine Ti nitride can be generated in the steel. Note that the reduction performed in the temperature range of over 1100° C. and the reduction performed in the temperature range of lower than 1000° C. are not particularly limited. For example, the reduction may be performed in the temperature range of over 1100° C. under the condition satisfying the above (Expression 1) or may be performed under a condition not satisfying the above (Expression 1). Alternatively, the reduction in the temperature range of over 1100° C. need not be performed. Similarly, the reduction in the temperature range of lower than 1000° C. may be performed under the condition satisfying the above (Expression 1) or may be performed under a condition not satisfying the above (Expression 1).

In the present invention, after the hot rolling is performed in the temperature range of at least 1100 to 1000° C. under the condition satisfying the above (Expression 1), the hot rolling is completed at the finish hot-rolling temperature that is not lower than the higher temperature of 800° C. and the Ar 3 transformation point nor higher than 970° C., and coiling is performed in a temperature region of 750° C. or lower. Note that a sheet thickness after the finish rolling is, for example, 2 mm to 10 mm. When the finish rolling temperature is lower than 800° C., the rolling load at the time of the finish rolling becomes high, which is liable to make the hot rolling difficult and to cause a poor shape of the hot-rolled steel sheet obtained after the hot rolling. Further, when the finish rolling temperature is lower than the Ar 3 transformation point, the hot rolling becomes the rolling in the two phase region of ferrite and austenite, which sometimes makes the structure of the hot-rolled steel sheet a heterogeneous duplex grain structure. On the other hand, when an upper limit of the finish rolling temperature is 970° C. or higher, the generation of TiN becomes insufficient, and there is a possibility that extra N generates a nitride with Al.

In the present invention, in the hot-rolling step, the hot rolling is performed in the temperature range of 1100 to 1000° C. under the condition satisfying the above (Expression 1), and the hot rolling is completed at the finish hot rolling temperature that is not lower than the higher temperature of 800° C. and the Ar 3 transformation point nor higher than 970° C., which makes it possible to suppress the generation of the coarse Ti nitride in the temperature range of 1100 to 1000° C. and to generate the fine TiN grains during a period until the temperature reaches the finish hot-rolling temperature from 1000° C. As a result, the finally obtained high-strength steel sheet has excellent impact resistance.

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In order to prevent deterioration in picklability due to an excessive increase in a thickness of an oxide formed on a surface of the hot-rolled steel sheet, the coiling temperature is set to 750° C. or lower. In order to further enhance picklability, the coiling temperature is preferably 720° C. or lower, and more preferably 700° C. or lower.

On the other hand, when the coiling temperature is lower than 500° C., strength of the hot-rolled steel sheet excessively increases and cold rolling becomes difficult, and therefore, the coiling temperature is preferably 500° C. or higher. In order to reduce a load of the cold rolling, the coiling temperature is preferably 550° C. or higher, and more preferably 600° C. or higher.

Next, the hot-rolled steel sheet coiled in the above temperature region is cooled at an average cooling rate of 15° C./hour or less. Consequently, the distribution of Mn solid-dissolved in the steel sheet is promoted, which makes it possible to selectively leave the retained austenite in an area where Mn is concentrated and increase an amount of the solid-solution Mn in the retained austenite. As a result, the finally obtained high-strength steel sheet becomes one in which an amount of the solid-solution Mn in the retained austenite is 1.1 times an average amount of Mn or more. The distribution of Mn after the coiling progresses more as the temperature is higher. Therefore, it is necessary to set the cooling rate of the steel sheet to 15° C./hour or less, especially in a range from the coiling temperature (coiling temperature−50° C.).

Next, the hot-rolled steel sheet thus manufactured is preferably pickled. The pickling is important for improving platability of the steel sheet because it removes the oxide on the surface of the hot-rolled steel sheet. Further, the pickling may be performed once or may be performed in a plurality of separate stages.

(Cold-Rolling Step)

Next, in order for the retained austenite to have a stable shape excellent in isotropy, the hot-rolled steel sheet having undergone the pickling is subjected to a cold-rolling step where it is cold-rolled at a reduction ratio of 30 to 75%. When the reduction ratio is less than 30%, the retained austenite cannot have a stable shape, and in the finally obtained high-strength steel sheet, the average aspect ratio of the retained austenite does not become 2.0 or less. In order for the retained austenite to have a stable shape, the reduction ratio in the cold-rolling step is preferably 40% or more, and more preferably 45% or more. On the other hand, when the reduction ratio in the cold rolling is over 75%, the cold-rolling load becomes excessively large and the cold rolling becomes difficult. Therefore, the reduction ratio is preferably 75% or less. In view of the cold-rolling load, the reduction ratio is more preferably 70% or less.

Note that the effects of the present invention are exhibited without particularly stipulating the number of the rolling passes and the reduction ratio of each of the rolling passes in the cold-rolling step.

(Continuous Annealing Step)

Next, the cold-rolled steel sheet obtained after the cold-rolling step is subjected to a continuous annealing step where it passes through a continuous annealing line. In the continuous annealing step in the present invention, annealing is performed where heating is performed in a temperature range of 550 to 700° C. at an average heating rate of 10° C./second or less, a maximum heating temperature is set to (an Ac 1 transformation point+40) to 1000° C., and cooling is performed in a temperature range of the maximum heating temperature to 700° C. at an average cooling rate of 1.0 to 10.0° C./second, cooling is performed in a temperature range of 700 to 500° C. at an average cooling rate of 5.0 to 200.0° C./second, and a retention process is performed for 30 to 1000 seconds in a temperature range of 350 to 450° C. Consequently, the high-strength steel sheet of the present invention is obtained.

In the continuous annealing step, as a result of the heating in the temperature range of 550 to 700° C. at the average heating rate of 10° C./second or less, recrystallization of the cold-rolled steel sheet sufficiently progresses, the retained austenite has a stable shape more excellent in isotropy, and the finally remaining austenite has a shape close to a sphere shape. When the average heating rate in the temperature range of 550 to 700° C. is over 10° C./second, the retained austenite cannot have a stable shape.

Further, when the maximum heating temperature in the continuous annealing step is lower than (the Ac 1 transformation point+40)° C., many coarse iron-based carbides are left unmelted in the steel sheet and formability greatly deteriorates, and therefore the maximum heating temperature is set to (the Ac 1 transformation point+40)° C. or higher. In view of formability, the maximum heating temperature is preferably (the Ac 1 transformation point+50)° C. or higher, and more preferably (the Ac 1 transformation point+60)° C. or higher. On the other hand, when the maximum heating temperature is higher than 1000° C., the diffusion of atoms is promoted and the distribution of Si, Mn, and Al weakens, and therefore, the maximum heating temperature is set to 1000° C. or lower. In order to control amounts of Si, Mn, and Al in the retained austenite, the maximum heating temperature is preferably the Ac 3 transformation point temperature or lower.

In the temperature range of the maximum heating temperature to 700° C., when the average cooling rate is over 10.0° C./second, a ferrite fraction in the steel sheet is likely to be uneven, resulting in deterioration in formability, and therefore, an upper limit of the average cooling rate is set to 10.0° C./second. On the other hand, when the average cooling rate is less than 1.0° C./second, ferrite and pearlite are generated in large amount and the retained austenite is not obtained, and therefore, a lower limit of the average cooling rate is set to 1.0° C./second. In order to obtain the retained austenite, the average cooling rate is preferably 2.0° C./second or more, and more preferably 3.0° C./second or more.

›BEST MODE FOR CARRYING OUT THE INVENTION · 9 of 9

In the temperature range of 700 to 500° C., when the average cooling rate is less than 5.0° C./second or less, pearlite and/or an iron-based carbide are generated in large amount and the retained austenite does not remain, and therefore, a lower limit of the average cooling rate is set to 5.0° C./second or more. From this point of view, the average cooling rate is preferably 7.0° C./second or more, and more preferably 8.0° C./second or more. On the other hand, the effects of the present invention are exhibited without particularly setting an upper limit of the average cooling rate, but in order for the average cooling rate to be over 200° C./second, a special facility is required, and the upper limit of the average cooling rate is set to 200° C./second in view of cost.

Further, in order to promote bainite transformation to obtain the retained austenite, the retention process for the retention in the temperature range of 350 to 450° C. for 30 to 1000 seconds is performed. When the retention time is short, the bainite transformation does not progress and the concentration of C into the retained austenite becomes insufficient, so that the retained austenite cannot be sufficiently left. From this point of view, a lower limit of the retention time is set to 30 seconds. The retention time is preferably 40 seconds or longer, and more preferably 60 seconds or longer. On the other hand, when the retention time is excessively long, the iron-based carbide is generated, C is consumed by this iron-based carbide, and the retained austenite cannot be sufficiently obtained, and therefore, the retention time is set to 1000 seconds or shorter. From this point of view, the retention time is preferably 800 seconds or shorter, and more preferably 600 seconds or shorter.

Further, in the present invention, in the continuous annealing step of the above-described manufacturing method, electrogalvanization may be applied after the aforesaid retention process to form a galvanized layer on the surface of the steel sheet, thereby producing a high-strength galvanized steel sheet.

Further, in the present invention, in the continuous annealing step of the above-described manufacturing method, after the cooling in the temperature range of 700 to 500° C., the steel sheet may be immersed in a galvanizing bath before the retention process in the temperature range of 350 to 450° C. or after the retention process, to form a galvanized layer on the surface of the steel sheet, thereby producing a high-strength galvanized steel sheet.

Consequently, a high-strength galvanized steel sheet excellent in impact resistance on whose surface the galvanized layer is formed is obtained.

The galvanizing bath is not particularly limited, and even when the galvanizing bath contains one or two or more of Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi, Sr, I, Cs, and REM, the effects of the present invention are not impaired, and depending on an amount thereof, this has an advantage such as an improvement in corrosion resistance and workability. Further, Al may be contained in the galvanizing bath. In this case, an Al concentration in the bath is preferably not lower than 0.05% nor higher than 0.15%.

Further, a temperature after the alloying process is preferably 480 to 560° C., and the retention time in the alloying process is preferably 15 to 60 seconds.

Further, after the steel sheet is immersed in the galvanizing bath, the alloying process may be applied in which the steel sheet is re-heated to 460° C. to 600° C. and is kept for 2 seconds or more, whereby the galvanized layer is alloyed.

As a result of performing such an alloying process, a Zn—Fe alloy which is an alloyed galvanized layer is formed on the surface, so that a high-strength galvanized steel sheet having the alloyed galvanized layer on the surface is obtained.

Further, on the surface of the galvanized layer or the alloyed galvanized layer of the high-strength galvanized steel sheet, a coating film made of a phosphorus oxide and/or a composite oxide containing phosphorus may be applied.

In this embodiment, the alloying process is preferably followed by the retention at a temperature of 200 to 350° C. for 30 to 1000 seconds. Consequently, the steel sheet structure contains tempered martensite.

Further, instead of the retention at the temperature of 200 to 350° C. for 30 to 1000 seconds after the alloying process, the tempered martensite may be generated by cooling the steel sheet having undergone the alloying process to 350° C. or lower to generate martensite, thereafter re-heating the steel sheet to a temperature range of not lower than 350° C. nor higher than 550° C., followed by 2 second retention or longer. Alternatively, the tempered martensite is generated in the base steel sheet structure also by further cooling the steel sheet, which has been cooled to a temperature region of 500° C. or lower in the continuous annealing step, to 350° C. or lower to generate martensite, and thereafter reheating the steel sheet, followed by the retention at 400 to 500° C.

Note that the present invention is not limited to the above-described example.

For example, in order to improve plating adhesiveness, the steel sheet before being annealed may be plated with one kind or a plurality of kinds selected from Ni, Cu, Co, and Fe.

Further, in this embodiment, the steel sheet having undergone the annealing may be subjected to temper rolling for the purpose of shape correction. However, when a reduction ratio after the annealing is over 10%, a soft ferrite portion is work-hardened, resulting in great deterioration in the ductility, and therefore, the reduction ratio is preferably less than 10%.

›EXAMPLES · 1 of 2

The present invention will be described in more detail by using examples.

Slabs having chemical components (compositions) A to AF shown in Table 1 and Table 2 and chemical components (compositions) BA to BC shown in Table 3 were formed by casting, and immediately after the casting, they were hot-rolled under conditions (slab heating temperature, rolling start temperature, value of (Expression 1) in hot-rolling in a temperature range of 1100 to 1000° C., finish hot-rolling temperature) shown in Table 4 to Table 7, were cooled, were coiled at coiling temperatures shown in Table 4 to Table 7, were cooled at average cooling rates shown in Table 4 to Table 7, and were subjected to pickling. Thereafter, they were cold-rolled at reduction ratios shown in Table 4 to Table 7.

Subsequently, annealing was applied under conditions shown in Table 8 to Table 11 to produce steel sheets of experimental examples 1 to 108, 201 to 208. In the annealing step, heating was performed in a temperature range of 550 to 700° C. at average heating rates shown in Table 6 to Table 8, and after heating to maximum heating temperatures shown in Table 8 to Table 11, cooling was performed in a temperature range of the maximum heating temperatures to 700° C. at average cooling rates (cooling rates 1) shown in Table 8 to Table 11, cooling was performed in a temperature range of 700 to 500° C. at average cooling rates (cooling rates 2) shown in Table 8 to Table 11, and a retention process for the retention times shown in Table 8 to Table 11 was performed in a temperature range of 350 to 450° C., followed by cooling to room temperature.

After the cooling to room temperature, 0.15% cold rolling was applied in the experimental examples 6 to 20 and the experimental examples 70 to 108, 1.50% cold rolling was applied in the experimental example 23, 1.00% cold rolling was applied in the experimental example 28, and 0.25% cold rolling was applied in the experimental examples 31 to 55.

Further, in the experimental examples 34, 44, 78, 81, after the annealing step, electroplating was applied on an electroplating line to produce electrogalvanized steel sheets.

In the experimental examples 19, 24, 84, after the cooling to 500° C. at the cooling rates 2, immersion in a galvanizing bath was performed during a period up to the cooling to the temperature range of 350 to 450° C., thereby producing a hot-dip galvanized steel sheet.

Further, in the experimental examples 29, 87, after the retention process in the temperature range of 350 to 450° C., immersion in a galvanizing bath was performed and then cooling to room temperature was performed, thereby producing a hot-dip galvanized steel sheet.

In the experimental examples 4, 14, 75, after the cooling to 500° C. at the cooling rates 2, immersion in a galvanizing bath was performed during a period up to the cooling to the temperature range of 350 to 450° C., and an alloying process was applied by 30 second retention at alloying temperatures shown in Table 8 to Table 11, thereby producing alloyed hot-dip galvanized steel sheets.

Further, in the experimental examples 9, 58, 72, immersion in a galvanizing bath was performed after the retention process in the temperature range of 350 to 450° C., and further an alloying process was applied by 30 second retention at alloying temperatures shown in Table 8 to Table 11, thereby producing alloyed hot-dip galvanized steel sheets.

Further, in the experimental examples 14 and 72, a coating film made of a composite oxide containing phosphorus was applied on a surface of a galvanized layer.

In Table 8 to Table 11, “CR” means a cold-rolled steel sheet, “GA” means an alloyed hot-dip galvanized steel sheet, “GI” means a hot-dip galvanized steel sheet, and “EG” means an electrogalvanized steel sheet.

Microstructures in a ⅛ thickness to ⅜ thickness region in each of the steel sheets of the experimental examples 1 to 108, 201 to 208 were observed and their volume fractions were measured. The results thereof are shown in Table 12 to Table 15. In Table 12 to Table 15, “F” means ferrite, “B” means bainite, “BF” means bainitic ferrite, “TM” means tempered martensite, “M” means fresh martensite, and “retained γ” means retained austenite.

A thicknesswise cross section was cut out, and an amount of the retained austenite out of the microstructure fractions was measured by an electron back scattaring diffraction (EBSD) analyzer attached to a field emission scanning electron microscope (FE-SEM) in the mirror-polished cross section, and the others were found by nital-etching the mirror-polished cross section and observing the cross section by using FE-SEM.

Further, as an average aspect ratio of the retained austenite (γ) (γ aspect ratio), measurement results of aspect ratios of 20 largest retained austenites in a retained austenite map obtained by the aforesaid EBSD analyzer and measurement results of aspect ratios of 20 largest retained austenites obtained by the similar EBSD analysis of a test piece fabricated for the observation of a ¼ thickness surface parallel to a sheet surface were added, and an average value of the aspect ratios of the 40 retained austenites was found.

Further, as an average grain diameter of TiN grains (TiN average size), a sample for transmission electron microscope (TEM) was fabricated by an extraction replica method from the surface where the volume fractions of the microstructures were observed, grain diameters (circle-equivalent diameters) of 10 TiN were measured by TEM, and an average value thereof was found.

As the density of AlN grains having a 1 μm grain diameter or more, inclusions in a 10.0 mm 2 range were observed by FE-SEM in the surface where the volume fractions of the microstructures were observed, the composition of inclusions whose circle-equivalent diameter was over 1.0 μm was measured, the number of inclusions confirmed as MN was counted, and the density was found.

A ratio (WMnγ/WMn) of an amount of solid-solution Mn (WMnγ) in the retained austenite to an average amount of Mn (WMn) was found by measuring WMn and WMnγ by the following method.

›EXAMPLES · 2 of 2

Specifically, in the observation surface where the microstructure fractions were found, EPMA analysis was conducted in the same range as that of the EBSD analysis, WMn was found from an obtained Mn concentration map, and the Mn concentration map and the retained austenite map were further laid one on the other, whereby only measurement values of the Mn concentration in the retained austenite was extracted, and WMNγ was obtained as an average value thereof.

Table 16 to Table 19 show results obtained when properties of the steel sheets of the experimental examples 1 to 108, 201 to 208 were evaluated by the following method.

From the steel sheets of the experimental examples 1 to 108, 201 to 208, tensile test pieces conforming to JIS Z 2201 were picked up, a tensile test was conducted in conformity with JIS Z 2241, and yield stress “YS”, tensile strength “TS”, and total elongation “EL” were measured.

Further, a hole expansion test (JFST1001) for evaluating flangeability was conducted, and a hole expansion limit value “λ” which is an index of stretch flangeability was calculated.

Further, the same tensile test piece was immersed in alcohol in which liquid nitrogen was added, was cooled to −60° C., taken out, and immediately subjected to the tensile test, and a drawing ratio (drawing value) of its fractured portion was found.

As shown in Table 16 to Table 19, in all the experimental examples being examples of the present invention out of the experimental examples 1 to 108, 201 to 208, tensile strength was 900 MPa or more and the result of the drawing value was 20% or more and thus was high, and they were excellent in impact resistance.

On the other hand, in the experimental examples being comparative examples out of the experimental examples 1 to 108, tensile strength was less than 900 MPa, and/or the result of the drawing value was low, and they did not have high strength and was not excellent in impact resistance.

Further, the experimental examples 14 and 72 are examples where the coating film made of the composite oxide containing phosphorus is applied on the surface of the galvanized layer, and they have good properties.

The experimental example 5 is an example where the slab heating temperature before the hot rolling is low, and coarse TiN remains and the drawing value at low temperatures is inferior.

The experimental example 10 is an example where the value of (Expression 1) is large, and coarse TiN exists, and the experimental example 59 is an example where the value of (Expression 1) is small, and coarse AlN exists. In the experimental example 10 and the experimental example 59, the drawing value at low temperatures is inferior.

The experimental example 15 is an example where the finish hot-rolling temperature of the hot-rolling is low, and since the microstructures extend in one direction and are uneven, ductility, stretch flangeability, and the drawing value at low temperatures are inferior.

The experimental example 20 is an example where the coiling after the hot rolling is high, and since the microstructures become very coarse, ductility, stretch flangeability, and the drawing value at low temperatures are inferior.

In the experimental example 25, the average cooling rate after the coiling is high, WMnγ/WMn is low, the Mn concentrated to the retained austenite is insufficient, and the drawing value at low temperatures is inferior.

In the experimental example 30, since the reduction ratio of the cold rolling is small and the aspect ratio of the retained austenite (γ aspect ratio) is large, the drawing value at low temperatures is inferior.

In the experimental example 35, since the average heating rate of the annealing is high and the aspect ratio of the retained austenite (γ aspect ratio) is large, the drawing value at low temperatures is inferior.

The experimental example 40 is an example where the maximum heating temperature in the annealing is low, and since it contains many coarse iron-based carbides working as the starting point of destruction, ductility, stretch flangeability, and the drawing value at low temperatures are inferior.

In the experimental example 45, since the cooling rate to 700° C. is excessively high and a sufficient soft structure is not obtained, ductility and the drawing value at low temperatures are inferior.

In the experimental example 50, the cooling rate 1 is excessively low, a coarse carbide is generated, a soft structure is not sufficiently obtained, strength is inferior, and ductility, stretch flangeability, and the drawing value at low temperatures are inferior.

In the experimental example 54, the retention time at 350 to 450° C. is short, an amount of the retained austenite is small, and ductility and the drawing value at low temperatures are inferior.

In the experimental example 55, the retention time at 350 to 450° C. is long, an amount of the retained austenite is small, a coarse carbide is generated, and ductility and the drawing value at low temperature are inferior.

In the experimental example 60, the cooling rate 2 is low, a coarse carbide is generated, and ductility, stretch flangeability, and the drawing value at low temperatures are inferior.

The experimental examples 103 to 108 are examples where the chemical components fall out of the predetermined ranges, and in any of them, a sufficient drawing value at low temperatures is not obtained.

›Tables in the description — 18
TABLE 1
CHEMICALCSiMnPSAlNOTi
COMPONENTMASS %MASS %MASS %MASS %MASS %MASS %MASS %MASS %MASS %
A0.2011.111.670.0190.00250.0140.00210.00200.008
B0.1621.182.370.0220.00190.0300.00240.00070.005
C0.1341.662.270.0100.00320.0280.00150.00160.007
D0.2300.592.100.0220.00310.0360.00360.00140.010
E0.1080.591.500.0140.00300.0260.00120.00110.004
F0.2131.502.340.0220.00160.0440.00160.00050.002
G0.0911.762.020.0170.00210.0170.00120.00080.009
H0.1621.062.870.0100.00350.0300.00250.00200.007
I0.1820.392.590.0230.00160.0370.00410.00170.004
J0.1471.302.070.0150.00350.0160.00270.00060.001
K0.2020.861.850.0100.00160.0290.00370.00100.008
L0.1181.151.810.0220.00230.0360.00280.00040.013
M0.1110.772.570.0160.00280.0180.00180.00110.004
N0.1691.991.970.0120.00310.0320.00330.00080.011
O0.1350.502.270.0130.00250.0150.00260.00240.008
P0.2091.391.400.0190.00260.0220.00110.00120.012
Q0.1212.072.380.0070.00330.0110.00130.00070.007
R0.2630.852.400.0160.00270.0310.00120.00280.003
S0.1171.411.770.0130.00340.0300.00290.00160.011
T0.1491.271.650.0180.00180.0090.00210.00130.006
U0.1001.562.670.0160.00250.0190.00260.00230.005
V0.1771.212.500.0090.00410.0290.00090.00180.002
W0.1180.981.690.0220.00190.0180.00340.00130.005
X0.0820.742.040.0100.00220.0330.00140.00170.011
Y0.1770.642.310.0210.00220.0290.00080.00110.004
Z0.1030.543.130.0240.00320.0220.00240.00050.005
AA0.1040.952.030.0150.00280.0410.00340.00220.000
AB0.0951.022.020.0130.00250.0350.00330.0022
0.094
AC0.1011.052.050.0190.00300.0370.0033
0.0096
0.004
AD0.0981.012.040.016
0.0095
0.0340.00270.00160.005
AE0.1021.052.030.0160.0033
0.499
0.00310.00240.004
AF0.0960.991.970.0200.00340.034
0.0096
0.00170.004
TABLE 2
NbBCrNiCuMoVCaCeMgZrHfREM
MASSMASSMASSMASSMASSMASSMASSMASSMASSMASSMASSMASSMASS
%%%%%%%%%%%%%
AEXAMPLE
BEXAMPLE
CEXAMPLE
DEXAMPLE
E0.013EXAMPLE
F0.0016EXAMPLE
G0.20EXAMPLE
H0.35EXAMPLE
I0.0070.0020EXAMPLE
J0.20EXAMPLE
K0.130.0005EXAMPLE
L0.55EXAMPLE
M0.0015EXAMPLE
N0.28EXAMPLE
O0.035EXAMPLE
P0.0140.0031EXAMPLE
Q0.0030EXAMPLE
R0.0015EXAMPLE
S0.640.56EXAMPLE
T0.00090.069EXAMPLE
U0.0018EXAMPLE
V0.0029EXAMPLE
W0.0040.00150.0013EXAMPLE
X0.320.100.0028EXAMPLE
Y0.120.09EXAMPLE
Z0.0026EXAMPLE
AA
COMPARATIVE
EXAMPLE
AB
COMPARATIVE
EXAMPLE
ACCOMPARATIVE
EXAMPLE
ADCOMPARATIVE
EXAMPLE
AECOMPARATIVE
EXAMPLE
AFCOMPARATIVE
EXAMPLE
TABLE 4 — HOT ROLLING
FINISHCOLD-
SLABAr 3HOT-AVERAGEROLLING
EXPERI-HEATINGTRANSFOR-STARTROLLINGCOILINGCOOLINGREDUC-
MENTALCHEMICALTEMPER-MATIONTEMPER-TEMPER-TEMPER-RATETION
EXAM-COMPO-ATUREPOINTATUREATUREEXPRES-ATURE° C./RATIO
PLENENT° C.° C.° C.° C.SION 1° C.HOUR%
1A123571911548933.56521240EXAMPLE
2A122071910919322.06671140EXAMPLE
3A125071911669082.46541167EXAMPLE
4A122571910848972.06431467EXAMPLE
5A
1100
71911409002.36801367COMPARATIVE
EXAMPLE
6B122567110849453.76511454EXAMPLE
7B123067111439441.86531154EXAMPLE
8B122567111299181.96791354EXAMPLE
9B124567111539322.66121454EXAMPLE
10B12306711092910
6.1
5981354COMPARATIVE
EXAMPLE
11C128570510879002.06061154EXAMPLE
12C125570510659552.65991154EXAMPLE
13C123070511489241.86091154EXAMPLE
14C126070511619272.56281154EXAMPLE
15C12657051144
701
2.56121254COMPARATIVE
EXAMPLE
16D125565411429272.76591171EXAMPLE
17D127565411188851.86531360EXAMPLE
18D126565410779663.36471160EXAMPLE
19D125065411139532.86021450EXAMPLE
20D125565411019392.5
800
1160COMPARATIVE
EXAMPLE
21E128574910818862.15841150EXAMPLE
22E125074911809703.16411350EXAMPLE
23E123074911199691.76351147EXAMPLE
24E124574910869091.96521147EXAMPLE
25E124574910979002.1580
35
50COMPARATIVE
EXAMPLE
26F125566811648853.56151271EXAMPLE
27F123566811459421.67141360EXAMPLE
28F124066811518892.46201460EXAMPLE
29F126066810648992.86361133EXAMPLE
30F126066810729552.662311
10
COMPARATIVE
EXAMPLE
TABLE 5 — HOT ROLLING
FINISHCOLD-
SLABAr 3HOT-AVERAGEROLLING
EXPERI-HEATINGTRANSFOR-STARTROLLINGCOILINGCOOLINGREDUC-
MENTALCHEMICALTEMPER-MATIONTEMPER-TEMPER-TEMPER-RATETION
EXAM-COMPO-ATUREPOINTATUREATUREEXPRES-ATURE° C./RATIO
PLENENT° C.° C.° C.° C.SION 1° C.HOUR%
31G127573511119433.46421340EXAMPLE
32G126073511629102.26551240EXAMPLE
33G125073511189512.36761274EXAMPLE
34G127573510889573.47061454EXAMPLE
35G122573511548922.85871154COMPARATIVE
EXAMPLE
36H124560511238952.55971454EXAMPLE
37H126560511269642.65841454EXAMPLE
38H126060511098943.36111236EXAMPLE
39H123060511619513.66251254COMPARATIVE
EXAMPLE
40H125060511569601.76711260EXAMPLE
41I123561810939081.86211160EXAMPLE
42I122561811388872.66371160EXAMPLE
43I123061811699021.96211360EXAMPLE
44I122061810989212.96451360EXAMPLE
45I124061811589172.16541460COMPARATIVE
EXAMPLE
46J124569711139151.86601367EXAMPLE
47J122069711589611.85391367EXAMPLE
48J125069710919533.06561367EXAMPLE
49J126569711239133.06761136EXAMPLE
50J125069710899322.95901167COMPARATIVE
EXAMPLE
51K125568911119413.46821450EXAMPLE
52K127568910649313.75871350EXAMPLE
53K124068910609322.15881167EXAMPLE
54K123068911269623.06421167COMPARATIVE
EXAMPLE
55K126068911589452.66651167COMPARATIVE
EXAMPLE
56L128571111029161.66791247EXAMPLE
57L124071111659182.86751147EXAMPLE
58L123571111668842.95901547EXAMPLE
59L12257111067909
0.9
6211138COMPARATIVE
EXAMPLE
60L125571110668913.56651247COMPARATIVE
EXAMPLE
TABLE 6 — HOT ROLLING
FINISHCOLD-
SLABAr 3HOT-AVERAGEROLLING
EXPERI-HEATINGTRANSFOR-STARTROLLINGCOILINGCOOLINGREDUC-
MENTALCHEMICALTEMPER-MATIONTEMPER-TEMPER-TEMPER-RATETION
EXAM-COMPO-ATUREPOINTATUREATUREEXPRES-ATURE° C./RATIO
PLENENT° C.° C.° C.° C.SION 1° C.HOUR%
61M124065511659623.76061350EXAMPLE
62M122065511229353.36051250EXAMPLE
63M122065510819662.56521450EXAMPLE
64N128571911769382.05911150EXAMPLE
65N122071910899673.36431450EXAMPLE
66N125071911629473.26511450EXAMPLE
67O128566611189243.16101367EXAMPLE
68O125066611638902.85881467EXAMPLE
69O127566611309501.96321367EXAMPLE
70P124575111719672.06091450EXAMPLE
71P127575110659612.36101250EXAMPLE
72P127575110749332.85391150EXAMPLE
73Q124071211769293.66011250EXAMPLE
74Q122571210609642.66561350EXAMPLE
75Q122071210819273.66091450EXAMPLE
76R127062410609352.06511454EXAMPLE
77R124062411299592.96501254EXAMPLE
78R124562411259623.56401454EXAMPLE
79S125069311229153.76081154EXAMPLE
80S127069310989522.96741254EXAMPLE
81S122069310789303.46571254EXAMPLE
82T128574310939562.86351440EXAMPLE
83T124574311468872.96121340EXAMPLE
84T123574311409073.66181140EXAMPLE
85U124067510629563.66421247EXAMPLE
86U123067511609461.86431350EXAMPLE
87U123567510728932.35891267EXAMPLE
88V127065510769542.66011160EXAMPLE
89V126065511099522.56131360EXAMPLE
90V123565510938981.96191371EXAMPLE
91W124574011259301.76301460EXAMPLE
92W122574011788841.96411460EXAMPLE
93W126074011109423.35891360EXAMPLE
94X127569310639521.86401240EXAMPLE
95X123069311489312.46061260EXAMPLE
96X122569311519503.36611450EXAMPLE
97Y126064411359122.15971150EXAMPLE
98Y127564411459312.86301150EXAMPLE
99Y125564410929692.65961150EXAMPLE
100Z128059910639521.75811160EXAMPLE
101Z127059910839072.66111360EXAMPLE
102Z124559911409602.75841160EXAMPLE
103AA123071411609682.45861150COMPARATIVE
EXAMPLE
104AB128072011448941.96461450COMPARATIVE
EXAMPLE
105AC126071610808873.36741350COMPARATIVE
EXAMPLE
106AD126571710858973.36601250COMPARATIVE
EXAMPLE
107AE127074210758973.56021350COMPARATIVE
EXAMPLE
108AF128572311058952.26231250COMPARATIVE
EXAMPLE
TABLE 7 — HOT ROLLING
FINISHCOLD-
SLABAr 3HOT-AVERAGEROLLING
EXPERI-HEATINGTRANSFOR-STARTROLLINGCOILINGCOOLINGREDUC-
MENTALCHEMICALTEMPER-MATIONTEMPER-TEMPER-TEMPER-RATETION
EXAM-COMPO-ATUREPOINTATUREATUREEXPRES-ATURE° C./RATIO
PLENENT° C.° C.° C.° C.SION 1° C.HOUR%
201BA124564310878742.95921367EXAMPLE
202BA124064310908953.26041467EXAMPLE
203BB124071011229042.86211267EXAMPLE
204BB125571010958813.16101167EXAMPLE
205BC125572211018813.25891467EXAMPLE
206BC126072210999082.85911167EXAMPLE
TABLE 8
AVERAGEMAXIMUMALLOY-
EXPERI-HEATINGHEATINGCOOLINGCOOLINGRETEN-ING
MENTALCHEMICALRATETEMPER-RATE 1RATE 2TIONTEMPER-
EXAM-COMPO-STEELAc 1Ac 3° C./ATURE° C./° C./TIMEATURE
PLENENTTYPE° C.° C.SECOND° C.SECONDSECONDSECOND° C.
1ACR72582857864.512.6190EXAMPLE
2ACR72582857922.313.3164EXAMPLE
3ACR72582838911.765.7204EXAMPLE
4AGA72582837865.37.498501EXAMPLE
5ACR72582838075.511.2218COMPARATIVE
EXAMPLE
6BCR71483428001.712.6333EXAMPLE
7BCR71483428051.36.8345EXAMPLE
8BCR71483428094.99.170EXAMPLE
9BGA71483457953.69.6324532EXAMPLE
10BCR71483427863.110.3282COMPARATIVE
EXAMPLE
11CCR73484258053.87.3112EXAMPLE
12CCR73484248111.711.1133EXAMPLE
13CCR73484278205.847.0142EXAMPLE
14CGA73484258051.674.2122544EXAMPLE
15CCR73484248182.413.3136COMPARATIVE
EXAMPLE
16DCR71777747641.79.8184EXAMPLE
17DCR71777757634.913.2158EXAMPLE
18DCR71777738154.611.6176EXAMPLE
19DGI71777798091.85.4207EXAMPLE
20DCR71777757645.68.0144COMPARATIVE
EXAMPLE
21ECR71583057962.3111.0315EXAMPLE
22ECR71583027841.912.6403EXAMPLE
23ECR71583077964.57.261EXAMPLE
24EGI71583047909.16.9322EXAMPLE
25ECR71583048016.012.0280COMPARATIVE
EXAMPLE
26FCR72583427995.07.2648EXAMPLE
27FCR72583477954.38.3312EXAMPLE
28FCR72583428244.79.3314EXAMPLE
29FGI72583478173.88.1462EXAMPLE
30FCR72583467933.49.3102COMPARATIVE
EXAMPLE
TABLE 9
AVERAGEMAXIMUMALLOY-
EXPERI-HEATINGHEATINGCOOLINGCOOLINGRETEN-ING
MENTALCHEMICALRATETEMPER-RATE 1RATE 2TIONTEMPER-
EXAM-COMPO-STEELAc 1Ac 3° C./ATURE° C./° C./TIMEATURE
PLENENTTYPE° C.° C.SECOND° C.SECONDSECONDSECOND° C.
31GCR72986038342.533.6133EXAMPLE
32GCR72986068522.420.9103EXAMPLE
33GCR72986068185.335.3108EXAMPLE
34GEG72986068272.728.776EXAMPLE
35GCR729860308225.827.8138COMPARATIVE
EXAMPLE
36HCR71978557655.337.1602EXAMPLE
37HCR71978547634.925.7512EXAMPLE
38HCR71978567714.833.2526EXAMPLE
39HCR71978527695.928.3536EXAMPLE
40HCR7197853
725
1.725.0522COMPARATIVE
EXAMPLE
41ICR70378837814.77.6468EXAMPLE
42ICR70378847705.610.6226EXAMPLE
43ICR70378838251.713.3194EXAMPLE
44IEG70378837705.77.6464EXAMPLE
45ICR703788478733.111.7131COMPARATIVE
EXAMPLE
46JCR73083457955.19.059EXAMPLE
47JCR73083437963.09.462EXAMPLE
48JCR73083438084.835.957EXAMPLE
49JCR73083458121.829.260EXAMPLE
50JCR7308343809
0.2
12.479COMPARATIVE
EXAMPLE
51KCR72182127954.59.9124EXAMPLE
52KCR72182138013.57.898EXAMPLE
53KCR72182147953.512.5113EXAMPLE
54KCR72182167875.711.715COMPARATIVE
EXAMPLE
55KCR72182137873.66.83600COMPARATIVE
EXAMPLE
56LCR73884428185.69.8234EXAMPLE
57LCR73884428034.25.8204EXAMPLE
58LGA73884458015.512.5196481EXAMPLE
59LCR73884458102.812.3176COMPARATIVE
EXAMPLE
60LCR73884488012.51.3210COMPARATIVE
EXAMPLE
TABLE 10
AVERAGEMAXIMUMALLOY-
EXPERI-HEATINGHEATINGCOOLINGCOOLINGRETEN-ING
MENTALCHEMICALRATETEMPER-RATE 1RATE 2TIONTEMPER-
EXAM-COMPO-STEELAc 1Ac 3° C./ATURE° C./° C./TIMEATURE
PLENENTTYPE° C.° C.SECOND° C.SECONDSECONDSECOND° C.
61MCR71080767824.831.7525EXAMPLE
62MCR71080737743.812.6470EXAMPLE
63MCR71080777683.712.0445EXAMPLE
64NCR74586568331.620.7142EXAMPLE
65NCR74586538392.811.3139EXAMPLE
66NCR74586528205.313.3112EXAMPLE
67OCR70779327664.031.9237EXAMPLE
68OCR70779357674.224.6209EXAMPLE
69OCR70779347704.233.474EXAMPLE
70PCR73683748175.87.874EXAMPLE
71PCR73683738281.810.183EXAMPLE
72PGA73683748124.611.462519EXAMPLE
73QCR73887539226.67.7498EXAMPLE
74QCR73887558464.611.4444EXAMPLE
75QGA73887578424.97.8125499EXAMPLE
76RCR71579347652.287.2204EXAMPLE
77RCR71579347713.3130.2198EXAMPLE
78REG71579367642.5112.0184EXAMPLE
79SCR71883938294.67.6125EXAMPLE
80SCR71883928172.88.3124EXAMPLE
81SEG71883958295.113.3131EXAMPLE
TCR72485038428.025.957EXAMPLE
83TCR72485068343.335.2101EXAMPLE
84TGI72485068392.738.8126EXAMPLE
85UCR72783538123.679.4118EXAMPLE
86UCR72783558015.787.6138EXAMPLE
87UGI72783537953.961.9121EXAMPLE
88VCR71783268061.642.3340EXAMPLE
89VCR71783238033.384.0364EXAMPLE
90VCR71783237863.867.5400EXAMPLE
91WCR72884078035.978.498EXAMPLE
92WCR72884027995.954.6121EXAMPLE
93WCR72884048131.849.8143EXAMPLE
94XCR71284438242.77.2240EXAMPLE
95XCR71284458155.69.0282EXAMPLE
96XCR71284439041.312.8252EXAMPLE
97YCR71880267855.011.3115EXAMPLE
98YCR71880247762.110.9114EXAMPLE
99YCR71880267852.810.4142EXAMPLE
100ZCR69676857394.511.9255EXAMPLE
101ZCR69676837392.012.0288EXAMPLE
102ZCR69676877472.813.0270EXAMPLE
103AACR72582958014.733.0249COMPARATIVE
EXAMPLE
104ABCR72485458042.228.2342COMPARATIVE
EXAMPLE
105ACCR72283557974.239.4309COMPARATIVE
EXAMPLE
106ADCR72185158044.728.0267COMPARATIVE
EXAMPLE
107AECR73592158004.535.9297COMPARATIVE
EXAMPLE
108AFCR71883558004.134.0300COMPARATIVE
EXAMPLE
TABLE 11
AVERAGEMAXIMUMALLOY-
EXPERI-HEATINGHEATINGCOOLINGCOOLINGRETEN-ING
MENTALCHEMICALRATETEMPER-RATE 1RATE 2TIONTEMPER-
EXAM-COMPO-STEELAc1Ac3° C./ATURE° C./° C./TIMEATURE
PLENENTTYPE° C.° C.SECOND° C.SECONDSECONDSECOND° C.
201BACR69584938232.223.386EXAMPLE
202BAGA69584928272.023.181564EXAMPLE
203BBCR71082328121.823.775EXAMPLE
204BBGI71082338102.124.777EXAMPLE
205BCCR70884228282.225.580EXAMPLE
206BCEG70884228302.422.687EXAMPLE
TABLE 12 — COMPO-
MICROSTRUCTURE OBSERVATION RESULTNENT
VOLUME FRACTIONPRECIPITATESANAL-
EXPERI-COLD-RE-SHAPETiNAlNYSIS
MENTALROLLEDTAINEDγAVERAGEDENSITYRESULT
EXAM-STEELSTEELFBBFTMMγOTHERSASPECTSIZEPIECES/W Mnγ /
PLESHEETTYPE%%%%%%%RATIOμmmm 2W Mn
1ACR541019111501.10.30.81.33EXAMPLE
2ACR49725103511.60.20.61.35EXAMPLE
3ACR29837211401.40.20.51.17EXAMPLE
4AGA54718150421.40.30.81.31EXAMPLE
5ACR291326290301.5
4.2
0.41.29COMPARA-
TIVE
EXAMPLE
6BCR382210220711.20.10.51.23EXAMPLE
7BCR371028181511.80.20.21.27EXAMPLE
8BCR281523262601.50.40.21.23EXAMPLE
9BGA46241591501.50.20.81.27EXAMPLE
10BCR54189141401.7
0.8
0.41.29COMPARA-
TIVE
EXAMPLE
11CCR451525100321.30.20.51.25EXAMPLE
12CCR44209200521.40.50.71.25EXAMPLE
13CCR262421242301.40.20.21.27EXAMPLE
14CGA451211272301.20.50.31.31EXAMPLE
15CCR332122221101.50.50.31.37COMPARA-
TIVE
EXAMPLE
16DCR321728180321.80.30.21.57EXAMPLE
17DCR362223160211.10.10.31.52EXAMPLE
18DCR203017301201.70.10.61.37EXAMPLE
19DGI212931150311.20.20.81.23EXAMPLE
20DCR33927251411.10.20.21.71COMPARA-
TIVE
EXAMPLE
21ECR421910233301.30.30.31.35EXAMPLE
22ECR482212131311.70.10.41.23EXAMPLE
23ECR361721250101.70.20.51.33EXAMPLE
24EGI382022160221.10.10.41.39EXAMPLE
25ECR342817161311.30.30.5
1.05
COMPARA-
TIVE
EXAMPLE
26FCR44921190701.30.20.31.25EXAMPLE
27FCR471715150601.70.30.81.29EXAMPLE
28FCR151733290601.20.20.51.21EXAMPLE
29FGI242527190411.20.40.21.37EXAMPLE
TABLE 13
MICROSTRUCTURE OBSERVATION RESULTCOMPO-
NENT
VOLUME FRACTIONPRECIPITATESANAL-
EXPERI-COLD-RE-SHAPETiNAlNYSIS
MENTALROLLEDTAINEDγAVERAGEDENSITYRESULT
EXAM-STEELSTEELFBBFTMMγOTHERSASPECTSIZEPIECES/W Mnγ /
PLESHEETTYPE%%%%%%%RATIOμmmm 2W Mn
30FCR50171115151
2.5
0.10.81.35COMPARA-
TIVE
EXAMPLE
31GCR291619302401.20.40.31.15EXAMPLE
32GCR153122270411.70.10.21.17EXAMPLE
33GCR412318140311.10.40.41.19EXAMPLE
34GEG362522120501.50.20.71.17EXAMPLE
35GCR37271415160
2.3
0.30.31.21COMPARA-
TIVE
EXAMPLE
36HCR422013210401.30.40.81.37EXAMPLE
37HCR422016171311.80.20.51.27EXAMPLE
38HCR28289281511.20.10.71.48EXAMPLE
39HCR331426220501.50.30.81.52EXAMPLE
40HCR8300002151.40.20.41.76COMPARA-
TIVE
EXAMPLE
41ICR143014373201.20.30.51.30EXAMPLE
42ICR302019262301.50.10.61.50EXAMPLE
43ICR143415332201.20.20.51.27EXAMPLE
44IEG322225180121.40.40.41.48EXAMPLE
45ICR42746180411.50.10.71.25COMPARA-
TIVE
EXAMPLE
46JCR371416262501.10.30.71.27EXAMPLE
47JCR392113190621.30.30.41.21EXAMPLE
48JCR261825241511.30.40.31.23EXAMPLE
49JCR281025310511.40.20.51.37EXAMPLE
50JCR302219190371.40.30.81.29COMPARA-
TIVE
EXAMPLE
51KCR291824232401.20.40.41.27EXAMPLE
52KCR223116270311.30.40.81.27EXAMPLE
53KCR243015290201.70.40.51.35EXAMPLE
54KCR3026121813
0
1—0.40.8—COMPARA-
TIVE
EXAMPLE
55KCR372419130
0
7—0.20.7—COMPARA-
TIVE
EXAMPLE
56LCR31252991501.70.20.61.29EXAMPLE
57LCR46138272401.70.10.21.35EXAMPLE
58LGA491915131301.60.30.21.21EXAMPLE
59LCR42922211501.60.1
2.5
1.27COMPARA-
TIVE
EXAMPLE
TABLE 14
MICROSTRUCTURE OBSERVATION RESULTCOMPO-
NENT
VOLUME FRACTIONPRECIPITATESANAL-
EXPERI-COLD-RE-SHAPETiNAlNYSIS
MENTALROLLEDTAINEDγAVERAGEDENSITYRESULT
EXAM-STEELSTEELFBBFTMMγOTHERSASPECTSIZEPIECES/W Mnγ /
PLESHEETTYPE%%%%%%%RATIOμmmm 2W Mn
60LCR5516863391.50.20.51.29COMPARA-
TIVE
EXAMPLE
61MCR312219220511.40.40.41.37EXAMPLE
62MCR411921111611.40.40.81.37EXAMPLE
63MCR441320152601.30.30.21.29EXAMPLE
64NCR351126220601.30.10.41.15EXAMPLE
65NCR293211220511.20.40.81.11EXAMPLE
66NCR501118122701.40.30.71.19EXAMPLE
67OCR422416131311.40.50.81.44EXAMPLE
68OCR40258231211.30.30.61.31EXAMPLE
69OCR411817211201.70.10.51.35EXAMPLE
70PCR32922283511.50.20.41.19EXAMPLE
71PCR15331462301.20.40.41.27EXAMPLE
72PGA34615373501.50.30.21.25EXAMPLE
73QCR162628240511.30.30.71.15EXAMPLE
74QCR341618250611.20.10.51.15EXAMPLE
75QGA331828171301.50.40.61.11EXAMPLE
76RCR49191951611.20.20.51.44EXAMPLE
77RCR362122134401.50.50.81.41EXAMPLE
78REG49820160521.50.50.41.35EXAMPLE
79SCR133521230621.50.40.51.29EXAMPLE
80SCR281530240301.50.10.71.25EXAMPLE
81SEG122527280621.10.40.41.29EXAMPLE
82TCR113126260511.80.40.21.13EXAMPLE
83TCR223317221411.30.40.21.25EXAMPLE
84TGI163618260311.70.40.31.27EXAMPLE
85UCR321832110521.40.40.21.25EXAMPLE
86UCR391724150501.70.30.51.19EXAMPLE
87UGI471616151501.10.10.31.29EXAMPLE
88VCR323610161501.70.20.71.31EXAMPLE
89VCR331030180721.60.30.21.19EXAMPLE
90VCR51186182501.60.10.71.31EXAMPLE
91WCR46925160311.50.10.71.19EXAMPLE
92WCR492110151401.20.30.51.25EXAMPLE
93WCR332724111311.70.40.61.25EXAMPLE
94XCR243027132401.30.10.21.27EXAMPLE
95XCR281428250321.30.30.21.29EXAMPLE
96XCR153026221601.30.40.31.11EXAMPLE
97YCR223129110611.50.20.61.48EXAMPLE
98YCR351727142501.70.40.61.50EXAMPLE
99YCR232628181311.70.10.71.35EXAMPLE
100ZCR521212162601.10.10.31.57EXAMPLE
101ZCR501020131511.10.30.61.55EXAMPLE
102ZCR421523121611.20.10.81.64EXAMPLE
103AACR372013241501.30.0
4.6
1.27COMPARA-
TIVE
EXAMPLE
104ABCR531112190321.7
0.7
0.3
1.25COMPARA-
TIVE
EXAMPLE
105ACCR45279120611.30.4
5.2
1.25COMPARA-
TIVE
EXAMPLE
106ADCR431419201301.40.3
5.7
1.21COMPARA-
TIVE
EXAMPLE
107AECR748651601.70.3
1.8
1.11COMPARA-
TIVE
EXAMPLE
108AFCR382512180611.3
1.3
3.0
1.27COMPARA-
TIVE
EXAMPLE
TABLE 15
MICROSTRUCTURE OBSERVATION RESULTCOMPO-
NENT
VOLUME FRACTIONPRECIPITATESANALY-
EXPERI-COLD-RE-SHAPETiNAlNSIS
MENTALROLLEDTAINEDγAVERAGEDENSITYRESULT
EXAM-STEELSTEELFBBFTMMγOTHERSASPECTSIZEPIECES/WMnγ/
PLESHEETTYPE%%%%%%%RATIOμmmm 2WMn
201BACR63420126601.70.30.61.38EXAMPLE
202BAGA64131782411.80.20.71.35EXAMPLE
203BBCR62313116301.90.30.71.49EXAMPLE
204BBGI61174113311.60.40.71.46EXAMPLE
205BCCR67182164301.60.30.61.40EXAMPLE
206BCEG67184180201.60.20.61.39EXAMPLE
TABLE 16
COLD-MATERIAL QUALITY MEASUREMENT RESULT
ROLLEDDRAWING
EXPERIMENTALSTEELSTEELYSTSELλVALUE
EXAMPLESHEETTYPEMPaMPa%%%
1ACR6141114214934EXAMPLE
2ACR570995214829EXAMPLE
3ACR7831040185442EXAMPLE
4AGA6271082224929EXAMPLE
5ACR864106222466COMPARATIVE
EXAMPLE
6BCR8011087214846EXAMPLE
7BCR8001196214236EXAMPLE
8BCR8111050225032EXAMPLE
9BGA672998245147EXAMPLE
10BCR5911032233811COMPARATIVE
EXAMPLE
11CCR6801116185143EXAMPLE
12CCR6621099233635EXAMPLE
13CCR9211116195228EXAMPLE
14CGA7421093195428EXAMPLE
15CCR7861118887COMPARATIVE
EXAMPLE
16DCR7611069224446EXAMPLE
17DCR7601082204031EXAMPLE
18DCR9081060244435EXAMPLE
19DGI800940244229EXAMPLE
20DCR750995111311COMPARATIVE
EXAMPLE
21ECR684997254432EXAMPLE
22ECR6481034212926EXAMPLE
23ECR712984243432EXAMPLE
24EGI7471008224246EXAMPLE
25ECR7701023252813COMPARATIVE
EXAMPLE
26FCR9181345184544EXAMPLE
27FCR7941357164430EXAMPLE
28FCR11471338184532EXAMPLE
29FGI10081294174841EXAMPLE
30FCR7761223205015COMPARATIVE
EXAMPLE
TABLE 17
COLD-MATERIAL QUALITY MEASUREMENT RESULT
ROLLEDDRAWING
EXPERIMENTALSTEELSTEELYSTSELλVALUE
EXAMPLESHEETTYPEMPaMPa%%%
31GCR731961246148EXAMPLE
32GCR9221065225137EXAMPLE
33GCR6961029244130EXAMPLE
34GEG7081032234839EXAMPLE
35GCR7371074204013COMPARATIVE
EXAMPLE
36HCR7291051204430EXAMPLE
37HCR7121048234245EXAMPLE
38HCR8071025185948EXAMPLE
39HCR719980224442EXAMPLE
40HCR610765277COMPARATIVE
EXAMPLE
41ICR830904264348EXAMPLE
42ICR7781014204728EXAMPLE
43ICR795911265726EXAMPLE
44IEG780994224843EXAMPLE
45ICR9821033145114COMPARATIVE
EXAMPLE
46JCR7761067234036EXAMPLE
47JCR6951036235741EXAMPLE
48JCR8891063214041EXAMPLE
49JCR7991079214134EXAMPLE
50JCR616831151612COMPARATIVE
EXAMPLE
51KCR8841150204736EXAMPLE
52KCR9881194184729EXAMPLE
53KCR9031126215144EXAMPLE
54KCR854113713336COMPARATIVE
EXAMPLE
55KCR7711114123213COMPARATIVE
EXAMPLE
56LCR7691073203936EXAMPLE
57LCR611979235629EXAMPLE
58LGA5961056204840EXAMPLE
59LCR68199016197COMPARATIVE
EXAMPLE
60LCR54097415158COMPARATIVE
EXAMPLE
TABLE 18
COLD-MATERIAL QUALITY MEASUREMENT RESULT
ROLLEDDRAWING
EXPERIMENTALSTEELSTEELYSTSELλVALUE
EXAMPLESHEETTYPEMPaMPa%%%
61MCR695920213836EXAMPLE
62MCR636918263839EXAMPLE
63MCR592969224528EXAMPLE
64NCR9451346163743EXAMPLE
65NCR10921406145126EXAMPLE
66NCR7671338173440EXAMPLE
67OCR6381018204746EXAMPLE
68OCR632979243534EXAMPLE
69OCR646970225135EXAMPLE
70PCR10061323154744EXAMPLE
71PCR12471472133548EXAMPLE
72PGA10101355165045EXAMPLE
73QCR9621094174848EXAMPLE
74QCR7601067186031EXAMPLE
75QGA7901048224544EXAMPLE
76RCR7641274163245EXAMPLE
77RCR8621265163635EXAMPLE
78REG7981225164231EXAMPLE
79SCR10041082194536EXAMPLE
80SCR8521096205448EXAMPLE
81SEG9381001224640EXAMPLE
82TCR9491022224937EXAMPLE
83TCR9801134195038EXAMPLE
84TGI9291061175332EXAMPLE
85UCR8571091183843EXAMPLE
86UCR6791052184441EXAMPLE
87UGI6981057195231EXAMPLE
88VCR8991173184246EXAMPLE
89VCR8521140164744EXAMPLE
90VCR6521122193929EXAMPLE
91WCR6771066195229EXAMPLE
92WCR6191048205231EXAMPLE
93WCR7351046185627EXAMPLE
94XCR710886235527EXAMPLE
95XCR746913253638EXAMPLE
96XCR878989224646EXAMPLE
97YCR8371020204542EXAMPLE
98YCR681969204740EXAMPLE
99YCR8491017213941EXAMPLE
100ZCR5381015213537EXAMPLE
101ZCR562932224827EXAMPLE
102ZCR676980223234EXAMPLE
103AACR746102921424COMPARATIVE
EXAMPLE
104ABCR55793320529COMPARATIVE
EXAMPLE
105ACCR687103220511COMPARATIVE
EXAMPLE
106ADCR65694225455COMPARATIVE
EXAMPLE
107AECR29995022372COMPARATIVE
EXAMPLE
108AFCR69693425463COMPARATIVE
EXAMPLE
TABLE 19
COLD-MATERIAL QUALITY MEASUREMENT RESULT
ROLLEDDRAWING
EXPERIMENTALSTEELSTEELYSTSELλVALUE
EXAMPLESHEETTYPEMPaMPa%%%
201BACR633918235228EXAMPLE
202BAGA695985234836EXAMPLE
203BBCR7531280183522EXAMPLE
204BBGI6491064234035EXAMPLE
205BCCR737908224233EXAMPLE
206BCEG680923244136EXAMPLE

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Classifications

22 codes
IPC · International Patent Classification
Section B — Performing operations; transporting
  • B32B15/01
Section C — Chemistry; metallurgy
  • C22C38/02
  • C22C38/00
  • C22C38/06
  • C22C38/12
  • C22C38/04
  • C22C38/16
  • C25D5/48
  • C22C18/04
  • C25D5/36
  • C23C2/02
  • C22C38/08
  • C23C2/28
  • C22C38/34
  • C21D8/02
  • C22C38/22
  • C22C38/28
  • C25D7/06
  • C22C38/38
  • C22C38/14
  • C22C18/00
  • C23C2/06

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