This application is a Divisional of co-pending application Ser. No. 14/112,187, filed Oct. 16, 2013, which is the National Stage Entry of PCT International Application No. PCT/JP2012/060634, filed on Apr. 19, 2012, which claims priority under 35 USC 119(a) to Japanese Patent Application No. 2011-095254, filed in Japan on Apr. 21, 2011 all of which are hereby expressly incorporated by reference into the present application.

TECHNICAL FIELD

The present invention relates to a high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability that is mainly used for automobile parts and the like, and a manufacturing method thereof.

This application is based upon and claims the benefit of priority of the prior Japanese Patent Application No. 2011-095254, filed on Apr. 21, 2011, the entire contents of which are incorporated herein by reference.

BACKGROUND ART

In order to abate emission of carbon dioxide gas from automobiles, a reduction in weight of automobile vehicle bodies has been promoted by using high-strength steel sheets. Further, in order also to secure the safety of a passenger, a high-strength steel sheet has been increasingly used for an automobile vehicle body in addition to a soft steel sheet. In order to further promote the reduction in weight of automobile vehicle bodies from now on, the strength of the high-strength steel sheet has to be increased more than conventionally.

In order to use the high-strength steel sheet for an underbody part, for example, burring workability has to be improved in particular. However, when a steel sheet is increased in strength in general, formability decreases, and uniform elongation important for drawing and bulging decreases.

In Non-Patent Document 1, there is disclosed a method in which austenite is made to remain in a steel sheet structure to secure uniform elongation. Further, in Non-Patent Document 2, there is disclosed a method of securing uniform elongation with the same strength by making a metal structure of a steel sheet complex.

Meanwhile, there is also disclosed control of a metal structure that improves local ductility necessary for bending, hole expanding, and burring. Non-Patent Document 3 discloses that controlling inclusions, making a structure uniform, and further decreasing hardness difference between structures are effective for improvement of bendability and hole expandability.

This is a method to improve the hole expandability by making a structure uniform by structure control, but in order to make a structure uniform, a heat treatment from an austenite single phase becomes a basis as disclosed in Non-Patent Document 4.

In order to attain achievement of strength and ductility, Non-Patent Document 4 discloses that a transformation structure is controlled by cooling control, thereby obtaining appropriate fractions of ferrite and bainite. However, all the cases are to improve local deformability relying on the structure control, and desired properties are greatly affected by how the structure is formed.

Meanwhile, as a method of improving a material of a hot-rolled steel sheet, there is disclosed a technique of increasing a reduction amount in continuous hot rolling. This is what is called a technique of making crystal grains fine, in which heavy reduction is performed at as low temperature as possible in an austenite region and non-recrystallized austenite is transformed to ferrite, to achieve making crystal grains of ferrite, which is the main phase of a product, fine.

Non-Patent Document 5 discloses that by this grain refining, increasing strength and increasing toughness are aimed. However, Non-Patent Document 5 pays no attention to the improvement of hole expandability, which is desired to be solved by the present invention, and does not disclose also a means applied to a cold-rolled steel sheet.

PRIOR ART DOCUMENTNon-Patent Document

Non-Patent Document 1: Takahashi, Nippon Steel Technical Report (2003) No. 378, p. 7

Non-Patent Document 2: O. Matsumura et al., Trans. ISIJ (1987) vol. 27, p. 570

Non-Patent Document 3: Kato et al., Steelmaking Research (1984) vol. 312, p. 41

Non-Patent Document 4: K. Sugimoto et al., (2000) Vol. 40, p. 920

Non-Patent Document 5: Nakayama Steel Works, Ltd. NFG Catalog

DISCLOSURE OF THE INVENTIONProblems to Be Solved by the Invention

As described above, performing structure control including inclusions is the main method for improving local ductility performance of a high-strength steel sheet. However, since the structure control is performed, form of precipitates and fractions of ferrite and bainite need to be controlled, and it is essential to limit a metal structure to be a base.

Thus, the present invention has a task to improve uniform elongation and burring workability of a high-strength steel sheet and improve also anisotropy in the steel sheet by controlling the fractions and form of a metal structure to be a base and controlling a texture. The present invention has an object to provide a high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability that solves this task, and a manufacturing method thereof.

Means for Solving the Problems

The present inventors earnestly examined a method of solving the above-described task. As a result, it was found that when rolling conditions and cooling conditions are controlled to required ranges to form a predetermined texture and steel sheet structure, a high-strength cold-rolled steel sheet having excellent isotropic workability can be thereby manufactured.

The present invention is made based on the above-described knowledge and the gist thereof is as follows.

A high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability contains:

in mass %,
C: 0.01 to 0.4%;
Si: 0.001 to 2.5%;
Mn: 0.001 to 4.0%;
P: 0.001 to 0.15%;
S: 0.0005 to 0.03%;
Al: 0.001 to 2.0%;
N: 0.0005 to 0.01%; and
O: 0.0005 to 0.01%; in which Si+Al is limited to less than 1.0%, and a balance being composed of iron and inevitable impurities, in which at a sheet thickness center portion being a range of â… to â…œ in sheet thickness from the surface of the steel sheet, an average value of pole densities of the {100}<011> to {223}<110> orientation group represented by respective crystal orientations of {100}<011>, {116}<110>, {114}<110>, {113}<110>, {112}<110>, {335}<110>, and {223}<110> is 5.0 or less, and a pole density of the {332}<113> crystal orientation is 4.0 or less,
a metal structure contains 5 to 80% of ferrite, 5 to 80% of bainite, and 1% or less of martensite in terms of an area ratio and the total of martensite, pearlite, and retained austenite is 5% or less, and
an r value (rC) in a direction perpendicular to a rolling direction is 0.70 or more and an r value (r30) in a direction 30Â° from the rolling direction is 1.10 or less.
[2]

The high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [1], in which an r value (rL) in the rolling direction is 0.70 or more and an r value (r60) in a direction 60Â° from the rolling direction is 1.10 or less.

The high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [1], in which in the metal structure, a mean volume diameter of crystal grains is 7 Î¼m or less, and an average value of a ratio of, of the crystal grains, a length dL in the rolling direction to a length dt in a sheet thickness direction: dL/dt is 3.0 or less.

The high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [1], further contains:

one type or two or more types of
in mass %,
Ti: 0.001 to 0.2%,
Nb: 0.001 to 0.2%,
B: 0.0001 to 0.005%,
Mg: 0.0001 to 0.01%,
Rem: 0.0001 to 0.1%,
Ca: 0.0001 to 0.01%,
Mo: 0.001 to 1.0%,
Cr: 0.001 to 2.0%,
V: 0.001 to 1.0%,
Ni: 0.001 to 2.0%,
Cu: 0.001 to 2.0%,
Zr: 0.0001 to 0.2%,
W: 0.001 to 1.0%,
As: 0.0001 to 0.5%,
Co: 0.0001 to 1.0%,
Sn: 0.0001 to 0.2%,
Pb: 0.001 to 0.1%,
Y: 0.001 to 0.10%, and
Hf: 0.001 to 0.10%.
[5]

The high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [1], in which on the surface, hot-dip galvanizing is performed.

The high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [1], in which after the hot-dip galvanizing, an alloying treatment is performed at 450 to 600Â° C.

A manufacturing method of a high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability, includes:

on a steel billet containing:
in mass %,
C: 0.01 to 0.4%;
Si: 0.001 to 2.5%;
Mn: 0.001 to 4.0%;
P: 0.001 to 0.15%;
S: 0.0005 to 0.03%;
Al: 0.001 to 2.0%;
N: 0.0005 to 0.01%; and
O: 0.0005 to 0.01%; in which Si+Al is limited to less than 1.0%, and a balance being composed of iron and inevitable impurities, performing first hot rolling in which rolling at a reduction ratio of 40% or more is performed one time or more in a temperature range of not lower than 1000Â° C. nor higher than 1200Â° C.;
setting an austenite grain diameter to 200 Î¼m or less by the first hot rolling; performing second hot rolling in which rolling at a reduction ratio of 30% or more is performed in one pass at least one time in a temperature region of not lower than a temperature T1+30Â° C. nor higher than T1+200Â° C. determined by Expression (1) below;
setting the total reduction ratio in the second hot rolling to 50% or more;
performing final reduction at a reduction ratio of 30% or more in the second hot rolling and then starting pre-cold rolling primary cooling in such a manner that a waiting time t second satisfies Expression (2) below;
setting an average cooling rate in the primary cooling to 50Â° C./second or more and performing the primary cooling in a manner that a temperature change is in a range of not less than 40Â° C. nor more than 140Â° C.;
performing cold rolling at a reduction ratio of not less than 30% nor more than 70%;
performing heating up to a temperature region of 700 to 900Â° C. and
performing holding for not shorter than 1 second nor longer than 1000 seconds;
performing post-cold rolling primary cooling down to a temperature region of 580 to 750Â° C. at an average cooling rate of 12Â° C./second or less;
performing post-cold rolling secondary cooling down to a temperature region of 350 to 500Â° C. at an average cooling rate of 4 to 300Â° C./second; and
performing an overaging heat treatment in which holding is performed for not shorter than t2 seconds satisfying Expression (4) below nor longer than 400 seconds in a temperature region of not lower than 350Â° C. nor higher than 500Â° C.

T1 (Â° C.)=850+10Ã—(C+N)Ã—Mn+350Ã—Nb+250Ã—Ti+40Ã—B+10Ã—Cr+100Ã—Mo+100Ã—V â€ƒâ€ƒ(1)

Here, C, N, Mn, Nb, Ti, B, Cr, Mo, and V each represent the content of the element (mass %).

tâ‰¦2.5Ã—t1 â€ƒâ€ƒ(2)

Here, t1 is obtained by Expression (3) below.

t1=0.001Ã—((Tfâˆ’T1)Ã—P1/100)²âˆ’0.109Ã—((Tfâˆ’T1)Ã—P1/100)+3.1 â€ƒâ€ƒ(3)

Here, in Expression (3) above, Tf represents the temperature of the steel billet obtained after the final reduction at a reduction ratio of 30% or more, and P1 represents the reduction ratio of the final reduction at 30% or more.

log(t2)=0.0002(T2âˆ’425)²+1.18 â€ƒâ€ƒ(4)

Here, T2 represents an overaging treatment temperature, and the maximum value of t2 is set to 400.
[8]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], further includes:

after performing the pre-cold rolling primary cooling, performing pre-cold rolling secondary cooling down to a cooling stop temperature of 600Â° C. or lower at an average cooling rate of 10 to 300Â° C./second before performing the cold rolling, and performing coiling at 600Â° C. or lower to obtain a hot-rolled steel sheet.

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], in which the total reduction ratio in a temperature range of lower than T1+30Â° C. is 30% or less.

[10]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], in which the waiting time t second further satisfies Expression (2a) below.

t<t1 â€ƒâ€ƒ(2a)

[11]

t1â‰¦tâ‰¦t1Ã—2.5 â€ƒâ€ƒ(2b)

[12]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], in which post-hot rolling primary cooling is started between rolling stands.

[13]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], in which when the heating is performed up to the temperature region of 700 to 900Â° C. after the cold rolling, an average heating rate of not lower than room temperature nor higher than 650Â° C. is set to HR1 (Â° C./second) expressed by Expression (5) below, and

an average heating rate of higher than 650Â° C. to 700 to 900Â° C. is set to HR2 (Â° C./second) expressed by Expression (6) below.

HR1â‰§0.3 â€ƒâ€ƒ(5)

HR2â‰¦0.5Ã—HR1 â€ƒâ€ƒ(6)

[14]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [7], further includes:

performing hot-dip galvanizing on the surface.
[15]

The manufacturing method of the high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability according to [14], further includes:

performing an alloying treatment at 450 to 600Â° C. after performing the hot-dip galvanizing.

Effect of the Invention

According to the present invention, it is possible to provide a high-strength cold-rolled steel sheet that is not large in anisotropy even when Nb, Ti, and/or the like are/is added and has excellent uniform elongation and hole expandability.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is an explanatory view of a continuous hot rolling line.

MODE FOR CARRYING OUT THE INVENTION

Hereinafter, the present invention will be explained in detail.

First, there will be explained a high-strength cold-rolled steel sheet having excellent uniform elongation and hole expandability of the present invention, (which will be sometimes called a â€œpresent invention steel sheetâ€ hereinafter).

(Crystal Orientation)

In the present invention steel sheet, an average value of pole densities of the {100}<011> to {223}<110> orientation group at a sheet thickness center portion being a range of â… to â…œ in sheet thickness from the surface of the steel sheet is a particularly important characteristic value. As long as the average value of the pole densities of the {100}<011> to {223}<110> orientation group is 5.0 or less when X-ray diffraction is performed at the sheet thickness center portion being the range of â… to â…œ in sheet thickness from the surface of the steel sheet to obtain pole densities of respective orientations, it is possible to satisfy a sheet thickness/a bend radius â‰§1.5 that is required to work a framework part to be required in recent years.

When the above-described average value exceeds 5.0, anisotropy of mechanical properties of the steel sheet becomes strong extremely, and further local deformability only in a certain direction is improved, but a material in a direction different from it deteriorates significantly, resulting in that it becomes impossible to satisfy the sheet thickness/the bend radius â‰§1.5.

The average value of the pole densities of the {100}<011> to {223}<110> orientation group is desirably 4.0 or less. When more excellent hole expandability and small limited bendability are required, the above-described average value is desirably 3.0 or less.

On the other hand, when the above-described average value becomes less than 0.5, which is difficult to be achieved in a current general continuous hot rolling process, deterioration of the local deformability is concerned, so that the above-described average value is preferably 0.5 or more.

The {100}<011>, {116}<110>, {114}<110>, {113}<110>, {112}<110>, {335}<110>, and {223}<110> orientations are included in the {100}<011> to {223}<110> orientation group.

The pole density is synonymous with an X-ray random intensity ratio. The pole density (X-ray random intensity ratio) is a numerical value obtained by measuring X-ray intensities of a standard sample not having accumulation in a specific orientation and a test sample under the same conditions by X-ray diffractometry or the like and dividing the obtained X-ray intensity of the test sample by the X-ray intensity of the standard sample. This pole density is measured by using a device of X-ray diffraction, EBSD (Electron Back Scattering Diffraction), or the like. Further, it can be measured by an EBSP (Electron Back Scattering Pattern) method or an ECP (Electron Channeling Pattern) method. It may be obtained from a three-dimensional texture calculated by a vector method based on a pole figure of {110}, or may also be obtained from a three-dimensional texture calculated by a series expansion method using a plurality (preferably three or more) of pole figures out of pole figures of {110}, {100}, {211}, and {310}.

For example, for the pole density of each of the above-described crystal orientations, each of intensities of (001)[1-10], (116)[1-10], (114)[1-10], (113)[1-10], (112)[1-10], (335)[1-10], and (223)[1-10] at a Ï†2=45Â° cross-section in the three-dimensional texture (ODF) may be used as it is.

The average value of the pole densities of the {100}<011> to {223}<110> orientation group is an arithmetic average of the pole densities of these orientations. When it is impossible to obtain all the intensities of these orientations, the arithmetic average of the pole densities of the respective orientations of {100}<011>, {116}<110>, {114}<110>, {112}<110>, and {223}<110> may also be used as a substitute.

Further, due to the similar reason, a pole density of the {332}<113> crystal orientation of a sheet plane at the sheet thickness center portion being the range of â… to â…œ in sheet thickness from the surface of the steel sheet has to be 4.0 or less. As long as it is 4.0 or less, it is possible to satisfy the sheet thickness/the bend radius â‰§1.5 that is required to work a framework part to be required in recent years. It is desirably 3.0 or less.

When the pole density of the {332}<113> crystal orientation is greater than 4.0, the anisotropy of the mechanical properties of the steel sheet becomes strong extremely, and further the local deformability only in a certain direction is improved, but the material in a direction different from it deteriorates significantly, resulting in that it becomes impossible to securely satisfy the sheet thickness/the bend radius â‰§1.5. On the other hand, when the pole density becomes less than 0.5, which is difficult to be achieved in a current general continuous hot rolling process, the deterioration of the local deformability is concerned, so that the pole density of the {332}<113> crystal orientation is preferably 0.5 or more.

The reason why the pole densities of the above-described crystal orientations are important for shape freezing property at the time of bending working is not necessarily obvious, but is inferentially related to slip behavior of crystal at the time of bending deformation.

The sample to be subjected to the X-ray diffraction is fabricated in such a manner that the steel sheet is reduced in thickness to a predetermined sheet thickness by mechanical polishing or the like, and next strain is removed by chemical polishing, electrolytic polishing, or the like, and in the range of â… to â…œ in sheet thickness from the surface of the steel sheet, an appropriate plane becomes a measuring plane. As a matter of course, the pole density satisfies the above-described pole density limited range not only at the sheet thickness center portion being the range of â… to â…œ in sheet thickness from the surface of the steel sheet, but also at as many thickness positions as possible, and thereby the uniform elongation and the hole expandability are further improved. However, the range of â… to â…œ from the surface of the steel sheet is measured, to thereby make it possible to represent the material property of the entire steel sheet generally. Thus, â… to â…œ of the sheet thickness is prescribed as the measuring range.

Incidentally, the crystal orientation represented by {hkl}<uvw> means that the normal direction of the steel sheet plane is parallel to <hkl> and the rolling direction is parallel to <uvw>. With regard to the crystal orientation, normally, the orientation vertical to the sheet plane is represented by [hkl] or {hkl} and the orientation parallel to the rolling direction is represented by (uvw) or <uvw>. {hkl} and <uvw> are generic terms for equivalent planes, and [hkl] and (uvw) each indicate an individual crystal plane. That is, in the present invention, a body-centered cubic structure is targeted, and thus, for example, the (111), (âˆ’111), (1-11), (11-1), (âˆ’1-11), (âˆ’11-1), (1-1-1), and (âˆ’1-1-1) planes are equivalent to make it impossible to make them different. In such a case, these orientations are generically referred to as {111}. In an ODF representation, [hkl](uvw) is also used for representing orientations of other low symmetric crystal structures, and thus it is general to represent each orientation as [hkl](uvw), but in the present invention, [hkl](uvw) and {hkl}<uvw> are synonymous with each other. The measurement of crystal orientation by an X ray is performed according to the method described in, for example, Cullity, Elements of X-ray Diffraction, new edition (published in 1986, translated by MATSUMURA, Gentaro, published by AGNE Inc.) on pages 274 to 296.

(r Value)

An r value (rC) in a direction perpendicular to the rolling direction is important in the present invention steel sheet. As a result of earnest examination, the present inventors found that good hole expandability and bendability cannot always be obtained even when the pole densities of the various crystal orientations are in the appropriate ranges. In order to obtain good hole expandability and bendability, the ranges of the above-described pole densities need to be satisfied, and at the same time, rC needs to be 0.70 or more. The upper limit of rC is not determined in particular, but if it is 1.10 or less, more excellent hole expandability can be obtained.

An r value (r30) in a direction 30Â° from the rolling direction is important in the present invention steel sheet. As a result of earnest examination, the present inventors found that good hole expandability and bendability cannot always be obtained even when the pole densities of the various crystal orientations are in the appropriate ranges. In order to obtain good hole expandability and bendability, the ranges of the above-described pole densities need to be satisfied, and at the same time, r30 needs to be 1.10 or less. The lower limit of r30 is not determined in particular, but if it is 0.70 or more, more excellent hole expandability can be obtained.

As a result of earnest examination, the present inventors found that if in addition to the pole densities of the various crystal orientations, rC, and r30, an r value (rL) in the rolling direction and an r value (r60) in a direction 60Â° from the rolling direction are rLâ‰§0.70 and r60â‰¦1.10 respectively, better hole expandability can be obtained.

The upper limits of rL and r60 are not determined in particular, but if rL is 1.00 or less and r60 is 0.90 or more, more excellent hole expandability can be obtained.

The above-described r values can be obtained by a tensile test using a JIS No. 5 tensile test piece. Tensile strain to be applied is normally 5 to 15% in the case of a high-strength steel sheet, and the r values may be evaluated in a range of the uniform elongation. Incidentally, the direction in which bending working is performed varies depending on parts to be worked, and thus it is not particularly limited, and in the case of the present invention steel sheet, the similar bendability can be obtained even when the present invention steel sheet is bent in any one of the directions.

Generally, a texture and the r values are correlated with each other, but in the present invention steel sheet, limitation on the pole densities of the crystal orientations and limitation on the r values are not synonymous with each other, and unless both the limitations are satisfied at the same time, good hole expandability cannot be obtained.

(Metal Structure)

Next, there will be explained limiting reasons related to a metal structure of the present invention steel sheet.

The structure of the present invention steel sheet contains 5 to 80% of ferrite in terms of an area ratio. Due to the existence of ferrite having excellent deformability, the uniform elongation improves, but when the area ratio is less than 5%, good uniform elongation cannot be obtained, so that the lower limit is set to 5%. On the other hand, when ferrite being greater than 80% in terms of an area ratio exists, the hole expandability deteriorates drastically, so that the upper limit is set to 80%.

Further, the present invention steel sheet contains 5 to 80% of bainite in terms of an area ratio. When the area ratio is less than 5%, strength decreases significantly, so that the lower limit is set to 5%. On the other hand, when bainite being greater than 80% exists, the hole expandability deteriorates significantly, so that the upper limit is set to 80%.

In the present invention steel sheet, as the balance, the total area ratio of 5% or less of martensite, pearlite, and retained austenite is allowed.

An interface between martensite and ferrite or bainite becomes a starting point of cracking to thus deteriorate the hole expandability, so that martensite is set to 1% or less.

Retained austenite is strain-induced transformed to be martensite. An interface between martensite and ferrite or bainite becomes a starting point of cracking, to thus deteriorate the hole expandability. Further, when a lot of pearlite exists, the strength and workability are sometimes impaired. Therefore, the total area ratio of martensite, pearlite, and retained austenite is set to 5% or less.

(Mean Volume Diameter of Crystal Grains)

In the present invention steel sheet, it is necessary to set a mean volume diameter of crystal grains in a grain unit to 7 Î¼m or less. When crystal grains having a mean volume diameter of greater than 7 Î¼m exist, the uniform elongation is low and further the hole expandability is also low, so that the mean volume diameter of the crystal grains is set to 7 Î¼m or less.

Here, conventionally, the definition of crystal grains is extremely vague and quantification of them is difficult. In contrast to this, the present inventors found it possible to solve the problem of the quantification of crystal grains if a â€œgrain unitâ€ of crystal grains is determined in the following manner.

The â€œgrain unitâ€ of crystal grains determined in the present invention is determined in the following manner in an analysis of the orientations of the steel sheet by an EBSP (Electron Back Scattering Pattern). That is, in an analysis of the orientations of the steel sheet by an EBSP, for example, the orientations are measured at 1500 magnifications with a measured step of 0.5 Î¼m or less, and a position at which a misorientation between adjacent measured points exceeds 15Â° is set to a boundary between crystal grains. Then, a region surrounded with this boundary is determined to be the â€œgrain unitâ€ of crystal grains.

With respect to the crystal grains of the grain unit determined in this manner, a circle-equivalent diameter d is obtained and the volume of the crystal grains of each grain unit is obtained by 4/3Ï€d³. Then, a weighted mean of the volume is calculated and the mean volume diameter (Mean Volume Diameter) is obtained.

As there are more large crystal grains even though the number of them is small, deterioration of local ductility becomes larger. Therefore, the size of the crystal grains is not an ordinary size mean, and the mean volume diameter defined as a weighted mean of volume is strongly correlated with the local ductility. In order to obtain this effect, the mean volume diameter of the crystal grains needs to be 7 Î¼m or less. It is desirably 5 Î¼m or less in order to secure the hole expandability at a higher level. Incidentally, the method of measuring crystal grains is set as described previously.

(Equiaxial Property of Crystal Grains)

Further, as a result of earnest examination, the present inventors found that when a ratio of, of the crystal grains in the grain unit, a length dL in the rolling direction to a length dt in a sheet thickness direction: dL/dt is 3.0 or less, the hole expandability improves greatly. This physical meaning is not obvious, but it is conceivable that the shape of the crystal grains in the grain unit is similar to a sphere rather than an ellipsoid, and thus stress concentration in grain boundaries is alleviated and thus the hole expandability improves.

Further, as a result of earnest examination, the present inventors found that when an average value of the ratio of the length dL in the rolling direction to the length dt in the sheet thickness direction: dL/dt is 3.0 or less, good hole expandability can be obtained. When the average value of the ratio of the length dL in the rolling direction to the length dt in the sheet thickness direction: dL/dt is greater than 3.0, the hole expandability deteriorates.

(Chemical Composition)

Next, there will be explained reasons for limiting a chemical composition of the present invention steel sheet. Incidentally, % according to the chemical composition means mass %.

C: 0.01 to 0.4%

C is an element effective for improving mechanical strength, so that 0.01% or more is added. It is preferably 0.03% or more, and is more preferably 0.05% or more. On the other hand, when it exceeds 0.4%, the workability and weldability deteriorate, so that the upper limit is set to 0.4%. It is preferably 0.3% or less, and is more preferably 0.25% or less.

Si: 0.001 to 2.5%

Si is an element effective for improving the mechanical strength. However, when Si becomes greater than 2.5%, the workability deteriorates and further a surface flaw occurs, so that 2.5% is set to the upper limit. On the other hand, it is difficult to decrease Si to less than 0.001% in a practical steel, so that 0.001% is set to the lower limit.

Mn: 0.001 to 4.0%

Mn is also an element effective for improving the mechanical strength, but when Mn becomes greater than 4.0%, the workability deteriorates, so that 4.0% is set to the upper limit. It is preferably 3.0% or less. On the other hand, it is difficult to decrease Mn to less than 0.001% in a practical steel, so that 0.001% is set to the lower limit. When elements such as Ti that suppress occurrence of hot cracking caused by S are not sufficiently added except Mn, Mn satisfying Mn/Sâ‰§20 in mass % is desirably added.

P: 0.001 to 0.15%

The upper limit of P is set to 0.15% in order to prevent the deterioration of the workability and cracking at the time of hot rolling or cold rolling. It is preferably 0.04% or less. The lower limit is set to 0.001% applicable in current general refining (including secondary refining).

S: 0.0005 to 0.03%

The upper limit of S is set to 0.03% in order to prevent deterioration of the workability and cracking at the time of hot rolling or cold rolling. It is preferably 0.01% or less. The lower limit is set to 0.0005% applicable in current general refining (including secondary refining).

Al: 0.001 to 2.0%

For deoxidation, 0.001% or more of Al is added. Further, Al significantly increases a Î³ to Î± transformation point, to thus be an effective element when hot rolling at an Ar₃point or lower is directed in particular, but when it is too much, the weldability deteriorates, so that the upper limit is set to 2.0%.

N and O: 0.0005 to 0.01%

N and O are impurities, and both elements are set to 0.01% or less in order to prevent the workability from deteriorating. The lower limits are each set to 0.0005% applicable in current general refining (including secondary refining).

Si+Al: less than 1.0%

When Si and Al are contained excessively in the present invention steel sheet, precipitation of cementite during an overaging treatment is suppressed and the fraction of retained austenite becomes too large, so that the total added amount of Si and Al is set to less than 1%.

In the present invention steel sheet, one type or two or more types of Ti, Nb, B, Mg, Rem, Ca, Mo, Cr, V, W, Zr, Cu, Ni, As, Co, Sn, Pb, Y, and Hf, being elements that have been used up to now may be contained in order to improve the hole expandability by controlling inclusions to make precipitates fine.

Ti, Nb, and B are elements to improve the material through mechanisms of fixation of carbon and nitrogen, precipitation strengthening, structure control, fine grain strengthening, and the like, so that according to needs, 0.001% or of Ti is added, 0.001% or more of Nb is added, and 0.0001% or more of B is added. Ti is preferably 0.01% or more, and Nb is preferably 0.005% or more.

However, even when they are added excessively, no significant effect is obtained, and the workability and manufacturability deteriorate instead, so that the upper limit of Ti is set to 0.2%, the upper limit of Nb is set to 0.2%, and the upper limit of B is set to 0.005%. B is preferably 0.003% or less.

Mg, Rem, and Ca are elements to make inclusions harmless, so that the lower limit of each of them is set to 0.0001%. Mg is preferably 0.0005% or more, Rem is preferably 0.001% or more, and Ca is preferably 0.0005% or more. On the other hand, when they are added excessively, cleanliness of the steel deteriorates, so that the upper limit of Mg is set to 0.01%, the upper limit of Rem is set to 0.1%, and the upper limit of Ca is set to 0.01%. Ca is preferably 0.01% or less.

Mo, Cr, Ni, W, Zr, and As are elements effective for increasing the mechanical strength and improving the material, so that according to need, 0.001% or more of Mo is added, 0.001% or more of Cr is added, 0.001% or more of Ni is added, 0.001% or more W is added, 0.0001% or more of Zr is added, and 0.0001% or more of As is added. Mo is preferably 0.01% or more, Cr is preferably 0.01% or more, Ni is preferably 0.05% or more, and W is preferably 0.01% or more.

However, when they are added excessively, the workability is deteriorated by contraries, so that the upper limit of Mo is set to 1.0%, the upper limit of Cr is set to 2.0%, the upper limit of Ni is set to 2.0%, the upper limit of W is set to 1.0%, the upper limit of Zr is set to 0.2%, and the upper limit of As is set to 0.5%. Zr is preferably 0.05% or less.

V and Cu, similarly to Nb and Ti, are elements effective for precipitation strengthening, and are elements causing less deterioration of the local deformability ascribable to strengthening by addition than Nb and Ti, so that V and Cu are elements more effective than Nb and Ti when high strength and better hole expandability are required. Therefore, the lower limits of V and Cu are both set to 0.001%. They are each preferably 0.01% or more.

However, when they are added excessively, the workability deteriorates, so that the upper limit of V is set to 1.0% and the upper limit of Cu is set to 2.0%. V is preferably 0.5% or less.

Co significantly increases the Î³ to Î± transformation point, to thus be an effective element when hot rolling at the Ar₃point or lower is directed in particular. In order to obtain an addition effect, 0.0001% or more is added. It is preferably 0.001% or more. However, when it is added excessively, the weldability deteriorates, so that the upper limit is set to 1.0%. It is preferably 0.1% or less.

Sn and Pb are elements effective for improving wettability and adhesiveness of galvanizing, so that 0.0001% or more of Sn is added and 0.001% or more of Pb is added. Sn is preferably 0.001% or more. However, when they are added excessively, a flaw is likely to occur at the time of manufacture, and further toughness decreases, so that the upper limit of Sn is set to 0.2% and the upper limit of Pb is set to 0.1%. Sn is preferably 0.1% or less.

Y and Hf are elements effective for improving corrosion resistance. When the elements are each less than 0.001%, an addition effect is not obtained, so that the lower limits of them are set to 0.001%. On the other hand, when they each exceed 0.10%, the hole expandability deteriorates, so that the upper limit of each of the elements is set to 0.10%.

(Manufacturing Method)

Next, there will be explained a manufacturing method of the present invention steel sheet, (which will be sometimes called a â€œpresent invention manufacturing methodâ€ hereinafter). In order to achieve excellent uniform elongation and hole expandability, it is important to form a texture that is random in terms of pole densities and to control conditions of structural fractions of ferrite and bainite and form dispersion. Hereinafter, details will be explained.

A manufacturing method prior to hot rolling is not limited in particular. That is, subsequently to melting by a shaft furnace, an electric furnace, or the like, secondary refining may be variously performed, and then casting may be performed by normal continuous casting, or by an ingot method, or further by thin slab casting, or the like. In the case of a continuous cast slab, it is possible that a continuous cast slab is once cooled down to low temperature and thereafter is reheated to then be subjected to hot rolling, or it is also possible that a continuous cast slab is subjected to hot rolling continuously after casting. Incidentally, a scrap may also be used for a raw material of the steel.

(First Hot Rolling)

A slab extracted from a heating furnace is subjected to a rough rolling process being first hot rolling to be rough rolled, and thereby a rough bar is obtained. The present invention steel sheet needs to satisfy the following requirements. First, an austenite grain diameter after the rough rolling, namely an austenite grain diameter before finish rolling is important. The austenite grain diameter before the finish rolling is desirably small, and the austenite grain diameter of 200 Î¼m or less greatly contributes to making crystal grains fine and homogenization of crystal grains, thereby making it possible to finely and uniformly disperse martensite to be formed in a process later.

In order to obtain the austenite grain diameter of 200 Î¼m or less before the finish rolling, it is necessary to perform rolling at a reduction ratio of 40% or more one time or more in the rough rolling in a temperature region of 1000 to 1200Â° C.

The austenite grain diameter before the finish rolling is desirably 100 Î¼m or less, and in order to obtain this grain diameter, rolling at 40% or more is performed two times or more. However, when in the rough rolling, the reduction is greater than 70% or rolling is performed greater than 10 times, there is a concern that the rolling temperature decreases or a scale is generated excessively.

In this manner, when the austenite grain diameter before the finish rolling is set to 200 Î¼m or less, recrystallization of austenite is promoted in the finish rolling, and through the formation of the texture and uniformalization of the grain unit, uniform elongation and hole expandability of a final product are improved.

It is supposed that this is because an austenite grain boundary after the rough rolling (namely before the finish rolling) functions as one of recrystallization nuclei during the finish rolling. The austenite grain diameter after the rough rolling is confirmed in a manner that a steel sheet piece before being subjected to the finish rolling is quenched as much as possible, (which is cooled at 10Â° C./second or more, for example), and a cross section of the steel sheet piece is etched to make austenite grain boundaries appear, and the austenite grain boundaries are observed by an optical microscope. On this occasion, at 50 or more magnifications, the austenite grain diameter of 20 visual fields or more is measured by image analysis or a point counting method.

(Second Hot Rolling)

After the rough rolling process (first hot rolling) is completed, a finish rolling process being second hot rolling is started. The time between the completion of the rough rolling process and the start of the finish rolling process is desirably set to 150 seconds or shorter.

In the finish rolling process (second hot rolling), a finish rolling start temperature is desirably set to 1000Â° C. or higher. When the finish rolling start temperature is lower than 1000Â° C., at each finish rolling pass, the temperature of the rolling to be applied to the rough bar to be rolled is decreased, the reduction is performed in a non-recrystallization temperature region, the texture develops, and thus the isotropy deteriorates.

Incidentally, the upper limit of the finish rolling start temperature is not limited in particular. However, when it is 1150Â° C. or higher, a blister to be the starting point of a scaly spindle-shaped scale defect is likely to occur between a steel sheet base iron and a surface scale before the finish rolling and between passes, and thus the finish rolling start temperature is desirably lower than 1150Â° C.

In the finish rolling, a temperature determined by the chemical composition of the steel sheet is set to T1, and in a temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C., the rolling at 30% or more is performed in one pass at least one time. Further, in the finish rolling, the total reduction ratio is set to 50% or more. By satisfying this condition, at the sheet thickness center portion being the range of â… to â…œ in sheet thickness from the surface of the steel sheet, the average value of the pole densities of the {100}<011> to {223}<110> orientation group becomes 5.0 or less and the pole density of the {332}<113> crystal orientation becomes 4.0 or less. This makes it possible to secure the uniform elongation and the hole expandability of the final product.

Here, T1 is the temperature calculated by Expression (1) below.

T1 (Â° C.)=850+10Ã—(C+N)Ã—Mn+350Ã—Nb+250Ã—Ti+40Ã—B+10Ã—Cr+100Ã—Mo+100Ã—V â€ƒâ€ƒ(1)

C, N, Mn, Nb, Ti, B, Cr, Mo, and V each represent the content of the element (mass %).

Heavy reduction in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. and light reduction at lower than T1+30Â° C. thereafter control the average value of the pole densities of the {100}<011> to {223}<110> orientation group and the pole density of the {332}<113> crystal orientation at the sheet thickness center portion being the range of â… to â…œ in sheet thickness from the surface of the steel sheet, and thereby the uniform elongation and the hole expandability of the final product are improved drastically, as shown in Examples to be described later.

This T1 temperature itself is obtained empirically. The present inventors learned empirically by experiments that the recrystallization in an austenite region of each steel is promoted on the basis of the T1 temperature. In order to obtain better uniform elongation and hole expandability, it is important to accumulate strain by the heavy reduction, and the total reduction ratio of 50% or more is essential in the finish rolling. Further, it is desired to take reduction at 70% or more, and on the other hand, if the reduction ratio greater than 90% is taken, securing temperature and excessive rolling load are as a result added.

When the total reduction ratio in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. is less than 50%, rolling strain to be accumulated during the hot rolling is not sufficient and the recrystallization of austenite does not advance sufficiently. Therefore, the texture develops and the isotropy deteriorates. When the total reduction ratio is 70% or more, the sufficient isotropy can be obtained even though variations ascribable to temperature fluctuation or the like are considered. On the other hand, when the total reduction ratio exceeds 90%, it becomes difficult to obtain the temperature region of T1+200Â° C. or lower due to heat generation by working, and further a rolling load increases to cause a risk that the rolling becomes difficult to be performed.

In the finish rolling, in order to promote the uniform recrystallization caused by releasing the accumulated strain, the rolling at 30% or more is performed in one pass at least one time at not lower than T1+30Â° C. nor higher than T1+200Â° C.

Incidentally, in order to promote the uniform recrystallization, it is necessary to suppress a working amount in a temperature region of lower than T1+30Â° C. as small as possible. In order to achieve it, the reduction ratio at lower than T1+30Â° C. is desirably 30% or less. In terms of sheet thickness accuracy and sheet shape, the reduction ratio of 10% or less is desirable. When the isotropy is further obtained, the reduction ratio in the temperature region of lower than T1+30Â° C. is desirably 0%.

The finish rolling is desirably finished at T1+30Â° C. or higher. In the hot rolling at lower than T1+30Â° C., the granulated austenite grains that are recrystallized once are elongated, thereby causing a risk that the isotropy deteriorates.

That is, in the manufacturing method of the present invention, in the finish rolling, by recrystallizing austenite uniformly and finely, the texture of the product is controlled and the uniform elongation and the hole expandability are improved.

A rolling ratio can be obtained by actual performances or calculation from the rolling load, sheet thickness measurement, or/and the like. The temperature can be actually measured by a thermometer between stands, or can be obtained by calculation simulation considering the heat generation by working from a line speed, the reduction ratio, or/and like. Thereby, it is possible to easily confirm whether or not the rolling prescribed in the present invention is performed.

When the hot rolling is finished at Ar₃or lower, the hot rolling becomes two-phase region rolling of austenite and ferrite, and accumulation to the {100}<011> to {223}<110> orientation group becomes strong. As a result, the uniform elongation and the hole expandability deteriorate significantly.

In order to make the crystal grains fine and suppress elongated grains, a maximum working heat generation amount at the time of the reduction at not lower than T1+30Â° C. nor higher than T1+200Â° C., namely a temperature increased margin by the reduction is desirably suppressed to 18Â° C. or less. For achieving this, inter-stand cooling or the like is desirably applied.

(Pre-Cold Rolling Primary Cooling)

After final reduction at a reduction ratio of 30% or more is performed in the finish rolling, pre-cold rolling primary cooling is started in such a manner that a waiting time t second satisfies Expression (2) below.

tâ‰¦2.5Ã—t1 â€ƒâ€ƒ(2)

Here, t1 is obtained by Expression (3) below.

t1=0.001Ã—((Tfâˆ’T1)Ã—P1/100)²âˆ’0.109Ã—((Tfâˆ’T1)Ã—P1/100)+3.1 â€ƒâ€ƒ(3)

Here, in Expression (3) above, Tf represents the temperature of a steel billet obtained after the final reduction at a reduction ratio of 30% or more, and P1 represents the reduction ratio of the final reduction at 30% or more.

Incidentally, the â€œfinal reduction at a reduction ratio of 30% or moreâ€ indicates the rolling performed finally among the rollings whose reduction ratio becomes 30% or more out of the rollings in a plurality of passes performed in the finish rolling. For example, when among the rollings in a plurality of passes performed in the finish rolling, the reduction ratio of the rolling performed at the final stage is 30% or more, the rolling performed at the final stage is the â€œfinal reduction at a reduction ratio of 30% or more.â€ Further, when among the rollings in a plurality of passes performed in the finish rolling, the reduction ratio of the rolling performed prior to the final stage is 30% or more and after the rolling performed prior to the final stage (rolling at a reduction ratio of 30% or more) is performed, the rolling whose reduction ratio becomes 30% or more is not performed, the rolling performed prior to the final stage (rolling at a reduction ratio of 30% or more) is the â€œfinal reduction at a reduction ratio of 30% or more.â€

In the finish rolling, the waiting time t second until the pre-cold rolling primary cooling is started after the final reduction at a reduction ratio of 30% or more is performed greatly affects the austenite grain diameter. That is, it greatly affects an equiaxed grain fraction and a coarse grain area ratio of the steel sheet.

When the waiting time t exceeds t1Ã—2.5, the recrystallization is already almost completed, but the crystal grains grow significantly and grain coarsening advances, and thereby the r values and the elongation are decreased.

The waiting time t second further satisfies Expression (2a) below, thereby making it possible to preferentially suppress the growth of the crystal grains. Consequently, even though the recrystallization does not advance sufficiently, it is possible to sufficiently improve the elongation of the steel sheet and to improve fatigue property simultaneously.

t<t1 â€ƒâ€ƒ(2a)

At the same time, the waiting time t second further satisfies Expression (2b) below, and thereby the recrystallization advances sufficiently and the crystal orientations are randomized. Therefore, it is possible to sufficiently improve the elongation of the steel sheet and to greatly improve the isotropy simultaneously.

t1â‰¦tâ‰¦t1Ã—2.5 â€ƒâ€ƒ(2b)

Here, as shown in FIG. 1, on a continuous hot rolling line 1, the steel billet (slab) heated to a predetermined temperature in the heating furnace is rolled in a roughing mill 2 and in a finishing mill 3 sequentially to be a hot-rolled steel sheet 4 having a predetermined thickness, and the hot-rolled steel sheet 4 is carried out onto a run-out-table 5. In the manufacturing method of the present invention, in the rough rolling process (first hot rolling) performed in the roughing mill 2, the rolling at a reduction ratio of 20% or more is performed on the steel billet (slab) one time or more in the temperature range of not lower than 1000Â° C. nor higher than 1200Â° C.

The rough bar rolled to a predetermined thickness in the roughing mill 2 in this manner is next finish rolled (is subjected to the second hot rolling) through a plurality of rolling stands 6 of the finishing mill 3 to be the hot-rolled steel sheet 4. Then, in the finishing mill 3, the rolling at 30% or more is performed in one pass at least one time in the temperature region of not lower than the temperature T1+30Â° C. nor higher than T1+200Â° C. Further, in the finishing mill 3, the total reduction ratio becomes 50% or more.

Further, in the finish rolling process, after the final reduction at a reduction ratio of 30% or more is performed, the pre-cold rolling primary cooling is started in such a manner that the waiting time t second satisfies Expression (2) above or either Expression (2a) or (2b) above. The start of this pre-cold rolling primary cooling is performed by inter-stand cooling nozzles 10 disposed between the respective two of the rolling stands 6 of the finishing mill 3, or cooling nozzles 11 disposed in the run-out-table 5.

For example, when the final reduction at a reduction ratio of 30% or more is performed only at the rolling stand 6 disposed at the front stage of the finishing mill 3 (on the left side in FIG. 1, on the upstream side of the rolling) and the rolling whose reduction ratio becomes 30% or more is not performed at the rolling stand 6 disposed at the rear stage of the finishing mill 3 (on the right side in FIG. 1, on the downstream side of the rolling), if the start of the pre-cold rolling primary cooling is performed by the cooling nozzles 11 disposed in the run-out-table 5, a case that the waiting time t second does not satisfy Expression (2) above or Expressions (2a) and (2b) above is sometimes caused. In such a case, the pre-cold rolling primary cooling is started by the inter-stand cooling nozzles 10 disposed between the respective two of the rolling stands 6 of the finishing mill 3.

Further, for example, when the final reduction at a reduction ratio of 30% or more is performed at the rolling stand 6 disposed at the rear stage of the finishing mill 3 (on the right side in FIG. 1, on the downstream side of the rolling), even though the start of the pre-cold rolling primary cooling is performed by the cooling nozzles 11 disposed in the run-out-table 5, there is sometimes a case that the waiting time t second can satisfy Expression (2) above or Expressions (2a) and (2b) above. In such a case, the pre-cold rolling primary cooling may also be started by the cooling nozzles 11 disposed in the run-out-table 5. Needless to say, as long as the performance of the final reduction at a reduction ratio of 30% or more is completed, the pre-cold rolling primary cooling may also be started by the inter-stand cooling nozzles 10 disposed between the respective two of the rolling stands 6 of the finishing mill 3.

Then, in this pre-cold rolling primary cooling, the cooling that at an average cooling rate of 50Â° C./second or more, a temperature change (temperature drop) becomes not less than 40Â° C. nor more than 140Â° C. is performed.

When the temperature change is less than 40Â° C., the recrystallized austenite grains grow and low-temperature toughness deteriorates. The temperature change is set to 40Â° C. or more, thereby making it possible to suppress coarsening of the austenite grains. When the temperature change is less than 40Â° C., the effect cannot be obtained. On the other hand, when the temperature change exceeds 140Â° C., the recrystallization becomes insufficient to make it difficult to obtain a targeted random texture. Further, a ferrite phase effective for the elongation is also not obtained easily and the hardness of a ferrite phase becomes high, and thereby the uniform elongation and the hole expandability also deteriorate. Further, when the temperature change is greater than 140Â° C., an overshoot to/beyond an Ar3 transformation point temperature is likely to be caused. In the case, even by the transformation from recrystallized austenite, as a result of sharpening of variant selection, the texture is formed and the isotropy decreases consequently.

When the average cooling rate in the pre-cold rolling primary cooling is less than 50Â° C./second, as expected, the recrystallized austenite grains grow and the low-temperature toughness deteriorates. The upper limit of the average cooling rate is not determined in particular, but in terms of the steel sheet shape, 200Â° C./second or less is considered to be proper.

Further, in order to suppress the grain growth and obtain more excellent low-temperature toughness, a cooling device between passes or the like is desirably used to bring the heat generation by working between the respective stands of the finish rolling to 18Â° C. or lower.

The rolling ratio (reduction ratio) can be obtained by actual performances or calculation from the rolling load, sheet thickness measurement, or/and the like. The temperature of the steel billet during the rolling can be actually measured by a thermometer being disposed between the stands, or can be obtained by simulation by considering the heat generation by working from a line speed, the reduction ratio, or/and like, or can be obtained by the both methods.

Further, as has been explained previously, in order to promote the uniform recrystallization, the working amount in the temperature region of lower than T1+30Â° C. is desirably as small as possible and the reduction ratio in the temperature region of lower than T1+30Â° C. is desirably 30% or less. For example, in the event that in the finishing mill 3 on the continuous hot rolling line 1 shown in FIG. 1, in passing through one or two or more of the rolling stands 6 disposed on the front stage side (on the left side in FIG. 6, on the upstream side of the rolling), the steel sheet is in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C., and in passing through one or two or more of the rolling stands 6 disposed on the subsequent rear stage side (on the right side in FIG. 6, on the downstream side of the rolling), the steel sheet is in the temperature region of lower than T1+30Â° C., when the steel sheet passes through one or two or more of the rolling stands 6 disposed on the subsequent rear stage side (on the right side in FIG. 1, on the downstream side of the rolling), even though the reduction is not performed or is performed, the reduction ratio at lower than T1+30Â° C. is desirably 30% or less in total. In terms of the sheet thickness accuracy and the sheet shape, the reduction ratio at lower than T1+30Â° C. is desirably a reduction ratio of 10% or less in total. When the isotropy is further obtained, the reduction ratio in the temperature region of lower than T1+30Â° C. is desirably 0%.

In the present invention manufacturing method, a rolling speed is not limited in particular. However, when the rolling speed on the final stand side of the finish rolling is less than 400 mpm, Î³ grains grow to be coarse, regions in which ferrite can precipitate for obtaining the ductility are decreased, and thus the ductility is likely to deteriorate. Even though the upper limit of the rolling speed is not limited in particular, the effect of the present invention can be obtained, but it is actual that the rolling speed is 1800 mpm or less due to facility restriction. Therefore, in the finish rolling process, the rolling speed is desirably not less than 400 mpm nor more than 1800 mpm.

(Pre-Cold Rolling Secondary Cooling)

In the present invention manufacturing method, it is preferred that after the pre-cold rolling primary cooling, pre-cold rolling secondary cooling should be performed to control the structure. The pattern of the pre-cold rolling secondary cooling is also important.

The pre-cold rolling secondary cooling is desirably performed within three seconds after the pre-cold rolling primary cooling. When the time to the start of the pre-cold rolling secondary cooling after the pre-cold rolling primary cooling exceeds three seconds, the austenite grains become coarse and the strength and the elongation decrease.

In the pre-cold rolling secondary cooling, the cooling is performed down to a cooling stop temperature of 600Â° C. or lower at an average cooling rate of 10 to 300Â° C./second. When the stop temperature of this pre-cold rolling secondary cooling is higher than 600Â° C. and the average cooling rate of the pre-cold rolling secondary cooling is less than 10Â° C./second, there is a possibility that surface oxidation advances and the surface of the steel sheet deteriorates. When the average cooling rate exceeds 300Â° C./second, martensite transformation is promoted to drastically increase the strength, resulting in that subsequent cold rolling becomes difficult to be performed.

(Coiling)

After being obtained in this manner, the hot-rolled steel sheet can be coiled at 600Â° C. or lower. When a coiling temperature exceeds 600Â° C., the area ratio of ferrite structure increases and the area ratio of bainite does not become 5% or more. In order to bring the area ratio of bainite to 5% or more, the coiling temperature is preferably set to 600Â° C. or lower.

(Cold Rolling)

A hot-rolled original sheet manufactured as described above is pickled according to need to be subjected to cold rolling at a reduction ratio of not less than 30% nor more than 70%. When the reduction ratio is 30% or less, it becomes difficult to cause recrystallization in heating and holding later, resulting in that the equiaxed grain fraction decreases and further the crystal grains after heating become coarse. When rolling at over 70% is performed, a texture at the time of heating is developed, and thus the anisotropy becomes strong. Therefore, the reduction ratio is set to 70% or less.

(Heating and Holding)

The steel sheet that has been subjected to the cold rolling (a cold-rolled steel sheet) is thereafter heated up to a temperature region of 700 to 900Â° C. and is held for not shorter than 1 second nor longer than 1000 seconds in the temperature region of 700 to 900Â° C. By this heating and holding, work hardening is removed. When the steel sheet after the cold rolling is heated up to the temperature region of 700 to 900Â° C. in this manner, an average heating rate of not lower than room temperature nor higher than 650Â° C. is set to HR1 (Â° C./second) expressed by Expression (5) below, and an average heating rate of higher than 650Â° C. to the temperature region of 700 to 900Â° C. is set to HR2 (Â° C./second) expressed by Expression (6) below.

HR1â‰§0.3 â€ƒâ€ƒ(5)

HR2â‰¦0.5Ã—HR1 â€ƒâ€ƒ(6)

The hot rolling is performed under the above-described condition, and further post-hot rolling primary cooling is performed, and thereby making the crystal grains fine and randomization of the crystal orientations are achieved. However, by the cold rolling performed thereafter, the strong texture develops and the texture becomes likely to remain in the steel sheet. As a result, the r values and the elongation of the steel sheet decrease and the isotropy decreases. Thus, it is desired to make the texture that has developed by the cold rolling disappear as much as possible by appropriately performing the heating to be performed after the cold rolling. In order to achieve it, it is necessary to divide the average heating rate of the heating into two stages expressed by Expressions (5) and (6) above.

The detailed reason why the texture and properties of the steel sheet are improved by this two-stage heating is unclear, but this effect is thought to be related to recovery of dislocation introduced at the time of the cold rolling and the recrystallization. That is, driving force of the recrystallization to occur in the steel sheet by the heating is strain accumulated in the steel sheet by the cold rolling. When the average heating rate HR1 in the temperature range of not lower than room temperature nor higher than 650Â° C. is small, the dislocation introduced by the cold rolling recovers and the recrystallization does not occur. As a result, the texture that has developed at the time of the cold rolling remains as it is and the properties such as the isotropy deteriorate. When the average heating rate HR1 in the temperature range of not lower than room temperature nor higher than 650Â° C. is less than 0.3Â° C./second, the dislocation introduced by the cold rolling recovers, resulting in that the strong texture formed at the time of the cold rolling remains. Therefore, it is necessary to set the average heating rate HR1 in the temperature range of not lower than room temperature nor higher than 650Â° C. to 0.3 (Â° C./second) or more.

On the other hand, when the average heating rate HR2 of higher than 650Â° C. to the temperature region of 700 to 900Â° C. is large, ferrite existing in the steel sheet after the cold rolling does not recrystallize and non-recrystallized ferrite in a state of being worked remains. When the steel containing C of 0.01% or more in particular is heated to a two-phase region of ferrite and austenite, formed austenite blocks growth of recrystallized ferrite, and thus non-recrystallized ferrite becomes more likely to remain. This non-recrystallized ferrite has a strong texture, to thus adversely affect the properties such as the r values and the isotropy, and this non-recrystallized ferrite contains a lot of dislocations, to thus deteriorate the ductility drastically. Therefore, in the temperature range of higher than 650Â° C. to the temperature region of 700 to 900Â° C., the average heating rate HR2 needs to be 0.5Ã—HR1 (Â° C./second) or less.

Further, when a heating temperature is lower than 700Â° C. or a holding time in the temperature region of 700 to 900Â° C. is shorter than one second, reverse transformation from ferrite does not advance sufficiently and in subsequent cooling, a bainite phase cannot be obtained, resulting in that sufficient strength cannot be obtained. On the other hand, when the heating temperature is higher than 900Â° C. or the holding time in the temperature region of 700 to 900Â° C. is longer than 1000 seconds, the crystal grains become coarse and the area ratio of the crystal grains each having a grain diameter of 200 Î¼m or more increases.

(Post-Cold-Rolling Primary Cooling)

After the heating and holding, post-cold rolling primary cooling is performed down to a temperature region of 580 to 750Â° C. at an average cooling rate of 12Â° C./second or less. When a finishing temperature of the post-cold rolling primary cooling exceeds 750Â° C., ferrite transformation is promoted to make it impossible to obtain 5% or more of bainite in terms of an area ratio. When the average cooling rate of this post-cold rolling primary cooling exceeds 12Â° C./second and the finishing temperature of the post-cold rolling primary cooling is lower than 580Â° C., the grain growth of ferrite does not advance sufficiently to make it impossible to obtain 5% or more of ferrite in terms of an area ratio.

(Post-Cold Rolling Secondary Cooling)

After the post-cold rolling primary cooling, post-cold rolling secondary cooling is performed down to a temperature region of 350 to 500Â° C. at an average cooling rate of 4 to 300Â° C./second. When the average cooling rate of the post-cold rolling secondary cooling is less than 4Â° C./second or the post-cold rolling secondary cooling is finished at a temperature of higher than 500Â° C., pearlite transformation advances excessively to create a possibility that 5% or more of bainite cannot be obtained finally in terms of an area ratio. Further, when the average cooling rate of the post-cold rolling secondary cooling is greater than 300Â° C./second or the post-cold rolling secondary cooling is finished at a temperature of lower than 350Â° C., martensite transformation advances and there is a risk that the area ratio of martensite becomes greater than 1%.

(Overaging Heat Treatment)

Subsequently to the post-cold rolling secondary cooling, an overaging heat treatment is performed in a temperature range of not lower than 350Â° C. nor higher than 500Â° C. A holding time in this temperature range is set to t2 seconds satisfying Expression (4) below according to an overaging treatment temperature T2 or longer. However, in consideration of an applicable temperature range of Expression (4), the maximum value of t2 is set to 400 seconds.

log(t2)=0.0002(T2âˆ’425)²+1.18 â€ƒâ€ƒ(4)

Incidentally, in this overaging heat treatment, the holding does not mean only isothermal holding, and it is sufficient if the steel sheet is retained in the temperature range of not lower than 350Â° C. nor higher than 500Â° C. For example, the steel sheet may be once cooled to 350Â° C. to then be heated up to 500Â° C., or the steel sheet may also be cooled to 500Â° C. to then be cooled down to 350Â° C.

Incidentally, even when a surface treatment is performed on the high-strength cold-rolled steel sheet of the present invention, the effect of improving the hole expandability does not disappear, and for example, a hot-dip galvanized layer, or an alloyed hot-dip galvanized layer may be formed on the surface of the steel sheet. In this case, the effect of the present invention can be obtained even when any one of electroplating, hot dipping, deposition plating, organic coating film forming, film laminating, organic salts/inorganic salts treatment, non-chromium treatment, and so on is performed. Further, the steel sheet according to the present invention can be applied not only to bulging forming but also to combined forming mainly composed of bending working such as bending, bulging, and drawing.

When hot-dip galvanizing is performed on the present invention steel sheet, an alloying treatment may be performed after the galvanizing. The alloying treatment is performed in a temperature region of 450 to 600Â° C. When an alloying treatment temperature is lower than 450Â° C., the alloying does not advance sufficiently, and when it exceeds 600Â° C., on the other hand, the alloying advances too much and corrosion resistance deteriorates. Therefore, the alloying treatment is performed in the temperature region of 450 to 600Â° C.

EXAMPLE

Next, examples of the present invention will be explained. Incidentally, conditions of the examples are condition examples employed for confirming the applicability and effects of the present invention, and the present invention is not limited to these condition examples. The present invention can employ various conditions as long as the object of the present invention is achieved without departing from the spirit of the invention. Chemical compositions of respective steels used in examples are shown in Table 1. Respective manufacturing conditions are shown in Tables 2 and 3. Further, structural constitutions and mechanical properties of respective steel types under the manufacturing conditions in Tables 2 and 3 are shown in Tables 4 and 5. Incidentally, each underline in Tables indicates that a numeral value is outside the range of the present invention or is outside the range of a preferred range of the present invention. Further, in Table 2 to Table 5, English letters A to T and English letters a to i that are added to the steel types indicate to be components of Steels A to T and a to i in Table 1 respectively.

There will be explained results of examinations using invention steels â€œA to Tâ€ and using comparative steels â€œa to h,â€ which have the chemical compositions shown in Table 1. Incidentally, in Table 1, each numerical value of the chemical compositions means mass %.

These steels were cast and then as they were, or were heated to a temperature region of 1000 to 1300Â° C. after once being cooled down to room temperature, and thereafter were subjected to hot rolling, cold rolling, and cooling under the conditions shown in Table 2 and Table 3.

In the hot rolling, first, in rough rolling being first hot rolling, rolling was performed one time or more at a reduction ratio of 40% or more in a temperature region of not lower than 1000Â° C. nor higher than 1200Â° C. However, with respect to Steel types A3, E3, and M2, in the rough rolling, the rolling at a reduction ratio of 40% or more in one pass was not performed. The number of times of reduction at a reduction ratio of 40% or more and each reduction ratio (%) in the rough rolling, and an austenite grain diameter (Î¼m) after the rough rolling (before finish rolling) are shown in Table 2. Incidentally, a temperature T1 (Â° C.) and a temperature Ac1 (Â° C.) of the respective steel types are shown in Table 2.

After the rough rolling was finished, the finish rolling being second hot rolling was performed. In the finish rolling, rolling at a reduction ratio of 30% or more was performed in one pass at least one time in a temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C., and in a temperature range of lower than T1+30Â° C., the total reduction ratio was set to 30% or less. Incidentally, in the finish rolling, rolling at a reduction ratio of 30% or more in one pass was performed in a final pass in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C.

However, with respect to Steel types A4, A5, A6, and B3, the rolling at a reduction ratio of 30% or more was not performed in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. Further, with regard to Steel types P2 and P3, the total reduction ratio in the temperature range of lower than T1+30Â° C. was greater than 30%.

Further, in the finish rolling, the total reduction ratio was set to 50% or more. However, with regard to Steel types A4, A5, A6, B3, and C3, the total reduction ratio in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. was less than 50%.

Table 2 shows, in the finish rolling, the reduction ratio (%) in the final pass in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. and the reduction ratio in a pass at one stage earlier than the final pass (reduction ratio in a pass before the final) (%). Further, Table 2 shows, in the finish rolling, the total reduction ratio (%) in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C., a temperature (Â° C.) after the reduction in the final pass in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C., and a maximum working heat generation amount (Â° C.) at the time of the reduction in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C.

After the final reduction in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. was performed in the finish rolling, pre-cold rolling primary cooling was started before a waiting time t second exceeding 2.5Ã—t1. In the pre-cold rolling primary cooling, an average cooling rate was set to 50Â° C./second or more. Further, a temperature change (a cooled temperature amount) in the pre-cold rolling primary cooling was set to fall within a range of not less than 40Â° C. nor more than 140Â° C.

However, with respect to Steel type J2, the pre-cold rolling primary cooling was started after the waiting time t second exceeded 2.5Ã—t1 since the final reduction in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. in the finish rolling. With regard to Steel type T2, the temperature change (cooled temperature amount) in the pre-cold rolling primary cooling was less than 40Â° C., and with regard to Steel type J3, the temperature change (cooled temperature amount) in the pre-cold rolling primary cooling was greater than 140Â° C. With regard to Steel type T3, the average cooling rate in the pre-cold rolling primary cooling was less than 50Â° C./second.

Table 2 shows t1 (second) of the respective steel types, the waiting time t (second) from the final reduction in the temperature region of not lower than T1+30Â° C. nor higher than T1+200Â° C. to the start of the pre-cold rolling primary cooling in the finish rolling, t/t1, the temperature change (cooled amount) (Â° C.) in the pre-cold rolling primary cooling, and the average cooling rate (Â° C./second) in the pre-cold rolling primary cooling.

After the pre-cold rolling primary cooling, pre-cold rolling secondary cooling was performed. After the pre-cold rolling primary cooling, the pre-cold rolling secondary cooling was started within three seconds. Further, in the pre-cold rolling secondary cooling, the cooling was performed down to a cooling stop temperature of 600Â° C. or lower at an average cooling rate of 10 to 300Â° C./second, coiling was performed at 600Â° C. or lower, and hot-rolled original sheets each having a thickness of 2 to 5 mm were obtained.

However, with regard to Steel type D3, three seconds passed until the pre-cold rolling secondary cooling was started after the pre-cold rolling primary cooling. Further, with regard to Steel type D3, the average cooling rate of the pre-cold rolling secondary cooling was greater than 300Â° C./second. Further, with regard to Steel type E3, the cooling stop temperature of the pre-cold rolling secondary cooling (coiling temperature) was higher than 600Â° C. Table 2 shows, of the respective steel types, the time(second) to the start of the pre-cold rolling secondary cooling after the pre-cold rolling primary cooling, the average cooling rate (Â° C./second) of the pre-cold rolling secondary cooling, and the cooling stop temperature (Â° C.) of the pre-cold rolling secondary cooling (coiling temperature).

Next, the hot-rolled original sheets were each pickled to then be subjected to cold rolling at a reduction ratio of not less than 30% nor more than 70%. However, with regard to Steel type T4, the reduction ratio of the cold rolling was less than 30%. Further, with regard to Steel type T5, the reduction ratio of the cold rolling was greater than 70%. Table 3 shows the reduction ratio (%) of the cold rolling of the respective steel types.

After the cold rolling, heating was performed up to a temperature region of 700 to 900Â° C. and holding was performed for not shorter than 1 second nor longer than 1000 seconds. Further, when the heating was performed up to the temperature region of 700 to 900Â° C., an average heating rate HR1 (Â° C./second) of not lower than room temperature nor higher than 650Â° C. was set to 0.3 or more (HR1â‰§0.3), and an average heating rate HR2 (Â° C./second) of higher than 650Â° C. to 700 to 900Â° C. was set to 0.5Ã—HR1 or less (HR2â‰¦0.5Ã—HR1).

However, with regard to Steel type A1, a heating temperature was higher than 900Â° C. With regard to Steel type Q2, the heating temperature was lower than 700Â° C. With regard to Steel type Q3, a heating and holding time was shorter than one second. With regard to Steel type Q4, the heating and holding time was longer than 1000 seconds. Further, with regard to Steel type T6, the average heating rate HR1 was less than 0.3 (Â° C./second). With regard to Steel type T7, the average heating rate HR2 (Â° C./second) was greater than 0.5Ã—HR1. Table 3 shows the heating temperature (Â° C.) and the average heating rates HR1 and HR2 (Â° C./second) of the respective steel types.

After the heating and holding, post-cold rolling primary cooling was performed down to a temperature region of 580 to 750Â° C. at an average cooling rate of 12Â° C./second or less. However, with regard to Steel type A2, the average cooling rate in the post-cold rolling primary cooling was greater than 12Â° C./second. Further, with regard to Steel type A2, a stop temperature of the post-cold rolling primary cooling was lower than 580Â° C., and with regard to Steel type K1, the stop temperature of the post-cold rolling primary cooling was higher than 740Â° C. Table 3 shows, of the respective steel types, the average cooling rate (Â° C./second) and the cooling stop temperature (Â° C.) in the post-cold rolling primary cooling.

Subsequently to the post-cold rolling primary cooling, post-cold rolling secondary cooling was performed down to a temperature region of 350 to 500Â° C. at an average cooling rate of 4 to 300Â° C./second. However, with regard to Steel type A5, the average cooling rate of the post-cold rolling secondary cooling was less than 4Â° C./second. With regard to Steel type P4, the average cooling rate of the post-cold rolling secondary cooling was greater than 300Â° C./second. Further, with regard to Steel type A2, a stop temperature of the post-cold rolling secondary cooling was higher than 500Â° C., and with regard to Steel type G1, the stop temperature of the post-cold rolling secondary cooling was lower than 350Â° C. Table 3 shows the average cooling rate (Â° C./second) in the post-cold rolling secondary cooling of the respective steel types.

Subsequently to the post-cold rolling secondary cooling, an overaging heat treatment (OA) was performed at the stop temperature of the post-cold rolling secondary cooling. The range of the temperature of this overaging heat treatment (OA) (stop temperature of the post-cold rolling secondary cooling) was set to not lower than 350Â° C. nor higher than 500Â° C. Further, the time of the overaging heat treatment (OA) was set to not shorter than t2 seconds nor longer than 400 seconds. However, with regard to Steel type A2, a heat treatment temperature of the overaging was higher than 500Â° C., and with regard to Steel type G1, the heat treatment temperature of the overaging was lower than 350Â° C. Further, with regard to Steel type D1, a treatment time of the overaging was shorter than t2 seconds, and with regard to Steel types C2 and G1, the treatment time of the overaging was longer than 400 seconds. Table 3 shows the heat treatment temperature of the overaging (Â° C.), t2 (second), and the treatment time (second) of the respective steel types.

After the overaging heat treatment, skin pass rolling at 0.5% was performed and material evaluation was performed. Incidentally, on Steel type S1, a hot-dip galvanizing treatment was performed. On Steel type T1, an alloying treatment was performed in a temperature region of 450 to 600Â° C. after galvanizing.

Table 4 shows area ratios (structural fractions) (%) of ferrite, bainite, pearlite, martensite, and retained austenite in a metal structure of the respective steel types, and, of the respective steel types, a mean volume diameter dia (average value) of crystal grains (Î¼m), and a ratio of, of the crystal grains, a length dL in the rolling direction to a length dt in the sheet thickness direction: dL/dt. Table 5 shows, of the respective steel types, an average value of pole densities of the {100}<011> to {223}<110> orientation group and a pole density of the {332}<113> crystal orientation at a sheet thickness center portion being a range of â… to â…œ in sheet thickness from the surface of the steel sheet. Incidentally, the structural fraction was evaluated by the structural fraction before the skin pass rolling. Further, Table 5 shows, as mechanical properties of the respective steel types, tensile strength TS (MPa), uniform elongation u-El (%), an elongation percentage El (%), and a hole expansion ratio Î» (%) as an index of the local deformability. Table 5 shows rC, rL, r30, and r60 each being the r value.

Incidentally, a tensile test was based on JIS Z 2241. A hole expansion test was based on the Japan Iron and Steel Federation standard JFS T1001. The pole density of each of the crystal orientations was measured using the previously described EBSP at a 0.5 Î¼m pitch on a â…œ to â… region at sheet thickness of a cross section parallel to the rolling direction. Further, as indexes of the uniform elongation and the hole expandability, TSÃ—EL was set to 8000 (MPaÂ·%) or more, and desirably set to 9000 (MPaÂ·%) or more, and TSÃ—Î» was set to 30000 (MPaÂ·%) or more, preferably set to 40000 (MPaÂ·%) or more, and still more preferably set to 50000 (MPaÂ·%) or more.

TABLE 1T1/Â° C.CSiMnPSAlNOSi + AlTiNbBMgRemCaA8510.0700.081.300.0150.0040.0400.00260.00320.12â€”0.00â€”â€”â€”â€”B8510.0700.081.300.0150.0040.0400.00260.00320.12â€”0.000.005â€”â€”â€”C8650.0800.311.350.0120.0050.0160.00320.00230.33â€”0.04â€”â€”â€”â€”D8650.0800.311.350.0120.0050.0160.00320.00230.33â€”0.04â€”â€”â€”0.002â€‚E8580.0600.871.200.0090.0040.0380.00330.00260.91â€”0.02â€”â€”0.002â€”F8580.0600.301.200.0090.0040.5000.00330.00260.80â€”0.02â€”â€”0.002â€”G8650.2100.151.620.0120.0030.0260.00330.00210.180.0210.000.002â€”â€”â€”H8650.2100.901.620.0120.0030.0260.00330.00210.930.0210.000.002â€”â€”â€”I8610.0350.671.880.0150.0030.0450.00280.00290.72â€”0.02â€”0â€”0.0015J8860.0350.671.880.0150.0030.0450.00280.00290.720.10.02â€”0â€”0.0015K8750.1800.482.720.0090.0030.0500.00360.00220.53â€”â€”â€”0â€”â€”L8920.1800.482.720.0090.0030.0500.00360.00220.53â€”0.05â€”0â€”0.002â€‚M8920.0600.112.120.01â€‚0.0050.0330.00280.00350.140.036â€‚0.0890.001â€”â€”â€”N8860.0600.112.120.01â€‚0.0050.0330.00280.00350.140.089â€‚0.0360.001â€”â€”â€”O9030.0400.131.330.01â€‚0.0050.0380.00320.00260.170.042â€‚0.1219Eâˆ’04â€”â€”â€”P9030.0400.131.330.01â€‚0.0050.0380.00360.00290.170.042â€‚0.1219Eâˆ’04â€”0.004â€”Q8520.1800.500.900.0080.0030.0450.00280.00290.55â€”â€”â€”â€”â€”â€”R8520.1800.301.300.08â€‚0.0020.0300.00320.00220.33â€”â€”â€”â€”â€”â€”S8520.1800.211.300.01â€‚0.0020.6500.00320.00350.86â€”â€”â€”â€”â€”â€”T8800.0350.021.300.01â€‚0.0020.0350.00230.00330.060.12â€”â€”â€”â€”â€”a8560.4500.521.330.26â€‚0.0030.0450.00260.00190.57â€”â€”â€”â€”â€”â€”b13760.0720.151.420.0140.0040.0360.00220.00250.19â€”1.5â€‚â€”â€”â€”â€”c8510.1100.231.120.0210.0030.0260.00250.00230.26â€”â€”â€”â€ƒâ€‰0.15â€”â€”d11540.2500.231.560.0240.12â€‚0.0340.00220.00230.26â€”â€”â€”â€”â€”â€”e8540.2500.231.540.02â€‚0.0020.0380.00260.00320.27â€”â€”â€”â€”â€”â€”f8540.2500.211.540.02â€‚0.0020.0340.00260.00230.24â€”â€”â€”â€”â€”â€”g8530.2200.21.530.0150.0040.0310.00280.00260.23â€”â€”â€”â€”â€”â€”h8520.1802.300.900.0080.0030.0450.00280.00222.35â€”â€”â€”â€”â€”â€”MoCrNiWZrAsVCuCoSnPbYHfNOTEAâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELBâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELCâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELDâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELEâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELFâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELG0.030.35â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELH0.030.35â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELIâ€”â€”â€”â€”â€”â€”â€‚0.03â€”â€”â€”â€”â€”â€”INVENTION STEELJâ€”â€”â€”â€”â€”â€”â€‚0.03â€”â€”â€”â€”â€”â€”INVENTION STEELK0.1â€‚â€”â€”â€”â€”â€”0.1â€”â€”â€”â€”â€”â€”INVENTION STEELL0.1â€‚â€”â€”â€”â€”â€”0.1â€”â€”â€”â€”â€”â€”INVENTION STEELMâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”0â€‚â€‰â€”INVENTION STEELNâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”0INVENTION STEELOâ€”â€”â€”â€”0â€”â€”â€”â€”0â€”â€”â€”INVENTION STEELPâ€”â€”â€”â€”â€”â€”â€”â€”0â€‰â€‚â€”â€”â€”â€”INVENTION STEELQâ€”â€”â€”0.1â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELRâ€”â€”0.1â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”INVENTION STEELSâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”0â€‰â€‚â€”â€”INVENTION STEELTâ€”â€”â€”â€”â€”0..002â€”0.2â€”â€”â€”â€”â€”INVENTION STEELaâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”COMPARATIVE STEELbâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”COMPARATIVE STEELcâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”COMPARATIVE STEELdâ€”5.0â€‚â€”â€”â€”â€”2.5â€”â€”â€”â€”â€”â€”COMPARATIVE STEELeâ€”â€”â€”â€”â€”â€”â€”â€”1.2â€”â€”â€”â€”COMPARATIVE STEELfâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”0.3â€”â€”COMPARATIVE STEELgâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”0.3â€”COMPARATIVE STEELhâ€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”â€”COMPARATIVE STEEL

TABLE 2NUMBER OF TIMESOF REDUCTIONREDUCTION RATIOMAXIMUMTf:AT 40% OR MOREAT 40% OR MOREWORKING HEATTEMPERATUREREDUCTIONREDUCTIONAT NOT LOWER THANAT NOT LOWER THANAUSTENITEREDUCTIONGENERATIONAFTER FINALRATIO OF PASSRATIO OF1000Â° C.1000Â° C.GRAINRATIOAT REDUCTIONREDUCTIONBEFORE FINALFINAL PASSSTEELAc1/T1/NOR HIGHER THANNOR HIGHER THANDIAMETERAT T1 + 30AT T1 + 30AT 30% OR MORE/AT T1 + 30AT T1 + 30TYPEÂ° C.Â° C.1200Â° C.1200Â° C.Î¼mTO T1 + 200Â° C./%TO T1 + 200Â° C./%Â° C.TO T1 + 200Â° C./%TO T1 + 200Â° C./%A1711851150140â€‚85159354040A2711851245/408580â€‚58914035A37118510â€”290â€‚65189303030A4711851245/459045189252020A5711851245/408545189302020A6711851245/409043189352020B1711851150145â€‚85159354040B2711851245/408575â€‚58923535B3711851245/408544189302020C1718865245/408079159453737C2718865245/458076189204031C3718865245/458044151080â€‚1030D1718865245/458082159504037D2718865245/458067189223131D3718865340/40/406076189224031E1735858245/459067139553131E2735858245/459085149334040E37358580â€”320â€‚65139303030F1719858245/409067139553131F2719858245/409085149334040F3719858245/409567139553131G1716865245/459585149354040G2716865240/459565128753030H1738865340/40/405565169703030I1722861245/409575179614030I2722861150130â€‚65189223030I3722861170140â€‚85408604040J1722886245/408565179603030J2722886150125â€‚65189203030J3722886150125â€‚65189203030K1708875340/40/406575189904030L1708892340/40/407065189903030M1704892340/40/406575109433535M27048920â€”390â€‚65309422040N1704886340/40/406575109403535O1713903245/457585159854040O2713903245/45120â€‚65128803030P1713903245/457085131012â€‚4040P2713903245/408078149443838P3713903245/458068189243030P4713903245/459084159304040Q1728852245/458085109584040Q2728852245/409576189624030Q3728852150145â€‚84149384240Q4728852150130â€‚66179253132R1733852245/458085129964040R2733852245/457585129904040R3733852245/458065139963535R4733852245/457085129994040S1715852245/458075129583040S2715852245/456575129583040S3715852245/458070169603535S4715852245/458575129593040T1710880245/457570129853035T2710880245/457570129843035T3710880245/45110â€‚75129843535T4710880245/458075149843040T5710880245/457565129833535T6710880245/458575159843040T7710880245/457580129823035a1724855CRACKING OCCURRED DURING HOT ROLLINGb17121376c1718851d17981154e1713850f1713850g1712850h1780852t:REDUCTIONWAITING TIMERATIOTO START OFPRE-COLDPRE-COLDTIMEPRE-COLDAT REDUCTIONPRE-COLD ROLLINGROLLINGROLLINGTO STARTROLLINGIN TEMPERATUREPRIMARY COOLINGPRIMARYPRIMARYOF PRE-COLDSECONDARYREGIONAFTER COMPLETIONCOOLINGCOOLINGROLLINGCOOLINGCOILINGSTEELOF LOWER THANOF FINAL ROLLINGAMOUNT/RATE/SECONDARYRATE/TEMPERATURE/TYPET1 + 30Â° C./%t1AT 30% OR MORE/st/t1Â° C.Â° C./sCOOLING/sÂ° C./sÂ° C.A100.570.681.2085713.0185.0426A201.772.121.2095603.0190.0427A301.081.291.20100â€‚604.0140.0413A410â€‚1.702.051.20125â€‚603.0220.0377A510â€‚1.631.951.20130â€‚603.0â€‚10.0328A610â€‚1.551.861.20115â€‚583.0â€‚83.0596B100.570.681.20110â€‚603.0225.0312B201.752.091.2090693.0189.0434B310â€‚1.631.961.20130â€‚603.0â€‚75.0335C100.760.911.2090602.0130.0423C201.541.851.20100â€‚603.0200.0426C300.230.271.20110â€‚552.0210.0329D100.670.801.20110â€‚603.0200.0496D201.501.801.2090753.0110.0452D301.501.801.20957038.0â€‚320.0514E100.730.871.2080733.0215.0477E200.730.881.2075703.0205.0518E301.212.311.90100â€‚713.0135.0660F100.731.381.9080703.0210.0477F200.731.391.90110â€‚703.0200.0518F300.731.381.90100â€‚100â€‚3.0158.0484G100.841.591.9090703.0165.0448G210â€‚2.795.301.90125â€‚703.0160.0494H100.661.261.90110â€‚703.0â€‚77.0416I100.731.391.90110â€‚793.0188.0546I201.442.731.90110â€‚703.0â€‚75.0443I320â€‚3.146.912.2090703.0175.0521J101.172.582.2095702.0160.0465J202.0910.30â€‚4.93100â€‚633.0â€‚70.0532J302.094.602.20235â€‚703.0â€‚78.0380K100.531.172.2090703.0165.0437L100.771.692.2090703.0â€‚75.0375M101.463.212.20125â€‚743.0145.0378M201.322.902.2080703.0166.0394N101.403.092.20100â€‚653.0186.0431O100.611.342.20110â€‚652.0100.0335O220â€‚3.928.622.2090503.0â€‚95.0384P100.250.562.2095653.0104.0435P240â€‚0.760.931.2395552.0135.0425P335â€‚1.501.821.2295753.0105.0455P400.730.891.2275773.0210.0510Q100.280.622.20110â€‚653.0â€‚75.0482Q200.731.401.92115â€‚803.0192.0549Q300.570.691.21105â€‚653.0221.0316Q401.442.751.91105â€‚753.0â€‚78.0448R100.140.312.2090653.0180.0410R200.130.100.8090753.0180.0410R300.150.100.7090652.5145.0420R400.150.110.7590653.0180.0425S100.280.622.2090533.0140.0401S200.280.180.6590653.0140.0401S300.410.370.9090652.0160.0430S400.270.210.8090693.0140.0435T100.440.982.2095752.0180.0359T200.461.022.2025752.0180.0356T300.461.022.2095302.0167.0478T400.300.662.2095752.0166.0359T500.481.052.2095682.5180.0440T600.300.662.2095752.0187.0362T700.491.082.2095753.0180.0355a1CRACKING OCCURRED DURING HOT ROLLINGb1c1d1e1f1g1h1

TABLE 3POST-COLDPOST-COLDPOST-COLDROLLINGROLLINGROLLINGPRIMARYPRIMARYSECONDARYTEMPER-COLDHEATINGHOLDING TIMECOOLINGCOOLING STOPCOOLINGATUREHOLDINGALLOYINGSTEELROLLINGHR1/HR2/TEMPERATURE/AT HEATINGRATE/TEMPERATURE/RATE/AT OA/TIMEPRESENCE/ABSENCETEMPERATURE/TYPERATIO/%Â° C./sÂ° C./sÂ° C.TEMPERATURE/sÂ° C./sÂ° C.Â° C./sÂ° C.AT OA/st2/sOF GALVANIZINGÂ° C.A1347.02.5956168116505048022661ABSENCEâ€”A2382.60.9750131445105048022661ABSENCEâ€”A3420.90.3800142107405037022661ABSENCEâ€”A4395.31.8834104126555037022661ABSENCEâ€”A5417.92.877812111639â€‚3570230400ABSENCEâ€”A6521.80.6770128117005037222055ABSENCEâ€”B1608.83.1776149116895045018520ABSENCEâ€”B2608.83.1820113106884945018520ABSENCEâ€”B3418.83.1792â€‚91126325044018217ABSENCEâ€”C1474.41.5840157117274945018520ABSENCEâ€”C2328.83.18301461168248317550400ABSENCEâ€”C3608.83.1808174126814948022661ABSENCEâ€”D1327.02.5780â€‚461067349480â€‚3661ABSENCEâ€”D2311.80.68861761165949326276400ABSENCEâ€”D3383.51.2843145â€‚95885040518318ABSENCEâ€”E1480.90.3867111106944940618318ABSENCEâ€”E2507.01.7774114â€‚97374938020338ABSENCEâ€”E3337.91.9756150127004941518116ABSENCEâ€”F1481.80.4867163106944840618318ABSENCEâ€”F2500.90.2780â€‚66â€‚97374844418318ABSENCEâ€”F3538.82.1760118106664841018217ABSENCEâ€”G1438.82.18081231259849265575400ABSENCEâ€”G2606.21.5768â€‚99116795045819025ABSENCEâ€”H1443.50.8794117107024836325489ABSENCEâ€”I1347.01.7895158106365045618924ABSENCEâ€”I2404.41.1856â€‚681270748356301136ABSENCEâ€”I3381.80.4880168125914936524479ABSENCEâ€”J1355.31.3775127â€‚97334837321853ABSENCEâ€”J2576.21.5783111107255045919126ABSENCEâ€”J3666.21.5846180â€‚97374937022661ABSENCEâ€”K1446.21.5770103â€‚97604943418116ABSENCEâ€”L1528.82.1775136â€‚96575041618116ABSENCEâ€”M1407.02.5780152117304844118217ABSENCEâ€”M2350.90.3870110116124938519732ABSENCEâ€”N1317.92.9850142125884947621550ABSENCEâ€”O1541.80.6756131116605047721853ABSENCEâ€”O2477.92.9790166126474940618318ABSENCEâ€”P1338.83.2850124125934945919126ABSENCEâ€”P2464.31.5842158117264945218520ABSENCEâ€”P3301.70.68881751166049325276400ABSENCEâ€”P4517.11.7775113â€‚9740358â€‚37920338ABSENCEâ€”Q1557.02.7899157107464945018520ABSENCEâ€”Q2357.01.7588159106355045518924ABSENCEâ€”Q3628.93.1778â€‚â€‰â€ƒ0.4116905044918520ABSENCEâ€”Q4414.41.18571360â€‚1270548357301136ABSENCEâ€”R1375.32.0883158117195046619833ABSENCEâ€”R2446.22.3873â€‚67117254947721853ABSENCEâ€”R3370.90.3870â€‚99107185047621550ABSENCEâ€”R4360.90.3854111117194842018015ABSENCEâ€”S1501.80.7766101116525045018520PRESENCENO ALLOYINGS2488.83.3770119126624744918520ABSENCEâ€”S3497.02.7780â€‚87116705045819025ABSENCEâ€”S4500.90.3765â€‚95â€‚96684845218621ABSENCEâ€”T1471.80.7760121126424942218015PRESENCE585T2476.22.3880â€‚54126704937820742ABSENCEâ€”T3440.90.3776â€‚74116555037621146ABSENCEâ€”T4141.80.7890â€‚91126575044618419ABSENCEâ€”T5898.83.3774130â€‚96604938919227ABSENCEâ€”T6470.20.1768138107354846719934ABSENCEâ€”T7431.81.6761â€‚85127324938919227ABSENCEâ€”a1CRACKING OCCURRED DURING HOT ROLLINGb1c1d1e1f1g1h1

TABLE 4RE-TAINEDFERRITEBAINITEPEARLITEMARTENSITEÎ³EXPRES-STEELFRAC-FRAC-FRAC-FRACTIONFRAC-diaSION 3TYPETION/%TION/%TION/%fM/%TION/%(Î¼m)dL (Î¼m)dT (Î¼m)dL/dtNOTEA157.239.53.10.10.1230.0â€ƒ235.9213.81.1COMPARATIVE STEELA2â€‚2.097.40.20.30.15.85.43.21.7COMPARATIVE STEELA359.240.00.10.40.310.0â€‚9.69.61.0COMPARATIVE STEELA462.936.00.20.60.38.07.62.33.3COMPARATIVE STEELA556.233.40.110.1â€‚0.28.07.61.94.0COMPARATIVE STEELA661.638.00.10.10.27.97.50.89.0COMPARATIVE STEELB160.639.00.10.10.25.34.92.71.8PRESENT INVENTION STEELB255.044.00.10.70.25.85.42.52.1PRESENT INVENTION STEELB360.737.00.10.91.38.07.61.84.1COMPARATIVE STEELC164.035.00.10.60.35.55.12.61.9PRESENT INVENTION STEELC260.0â€‚4.30.10.834.8â€‚6.15.72.42.3COMPARATIVE STEELC365.433.00.40.90.35.75.32.52.1COMPARATIVE STEELD153.8â€‚6.00.139.8â€‚0.35.45.02.02.6COMPARATIVE STEELD258.038.03.10.80.16.16.94.61.5PRESENT INVENTION STEELD342.357.00.10.50.111.0â€‚11.87.81.5COMPARATIVE STEELE155.541.92.10.40.16.06.83.32.1PRESENT INVENTION STEELE253.142.74.00.00.25.36.13.31.8PRESENT INVENTION STEELE367.228.03.70.90.210.9â€‚11.77.81.5COMPARATIVE STEELF155.541.91.50.90.26.06.85.61.2PRESENT INVENTION STEELF253.143.03.10.50.35.36.13.21.9PRESENT INVENTION STEELF353.344.71.50.30.26.06.83.91.7PRESENT INVENTION STEELG157.4â€‚2.00.240.2â€‚0.25.36.13.21.9COMPARATIVE STEELG259.836.03.70.30.26.47.27.01.0COMPARATIVE STEELH156.240.03.20.50.16.06.83.02.2PRESENT INVENTION STEELI150.946.02.70.20.26.16.93.32.1PRESENT INVENTION STEELI267.930.01.30.50.36.27.02.52.8PRESENT INVENTION STEELI356.740.02.40.60.38.39.14.52.0COMPARATIVE STEELJ152.845.01.50.50.26.16.02.72.2PRESENT INVENTION STEELJ258.040.01.70.10.29.08.94.12.2COMPARATIVE STEELJ353.143.03.50.20.26.26.15.01.2COMPARATIVE STEELK190.7â€‚2.07.10.10.16.05.93.41.7COMPARATIVE STEELL147.352.10.20.30.16.06.33.61.7PRESENT INVENTION STEELM164.235.00.30.40.15.65.92.02.9PRESENT INVENTION STEELM253.943.02.80.20.28.38.65.71.5COMPARATIVE STEELN156.439.04.10.30.25.65.92.92.0PRESENT INVENTION STEELO158.138.03.30.40.25.15.43.21.7PRESENT INVENTION STEELO262.133.04.30.40.28.38.62.43.6COMPARATIVE STEELP156.940.02.70.30.15.15.42.12.5PRESENT INVENTION STEELP264.035.00.10.60.32.52.80.64.7COMPARATIVE STEELP358.038.03.10.80.12.82.90.74.1COMPARATIVE STEELP443.2â€‚1.00.155.4â€‚0.35.36.13.31.8COMPARATIVE STEELQ159.738.02.10.10.15.25.52.42.3PRESENT INVENTION STEELQ286.0â€‚2.211.4â€‚0.20.26.16.93.32.1COMPARATIVE STEELQ378.9â€‚1.50.119.3â€‚0.25.34.92.71.8COMPARATIVE STEELQ467.930.01.30.50.3220.5â€ƒ221.0220.02.8COMPARATIVE STEELR163.334.52.00.10.15.15.42.12.6PRESENT INVENTION STEELR263.135.21.30.20.24.14.41.82.5PRESENT INVENTION STEELR361.835.72.10.20.24.24.51.92.4PRESENT INVENTION STEELR458.938.91.90.10.24.04.31.92.3PRESENT INVENTION STEELS157.440.02.40.10.15.25.53.31.7PRESENT INVENTION STEELS259.439.21.10.20.14.04.31.72.5PRESENT INVENTION STEELS358.839.01.90.10.24.04.32.02.2PRESENT INVENTION STEELS452.945.21.60.10.24.14.41.62.8PRESENT INVENTION STEELT161.636.02.20.10.15.55.83.51.7PRESENT INVENTION STEELT261.536.51.80.10.18.68.92.43.7COMPARATIVE STEELT361.038.00.80.10.18.58.82.53.5COMPARATIVE STEELT456.940.32.10.40.39.09.30.910.0â€‚COMPARATIVE STEELT561.437.90.40.20.14.04.31.92.3COMPARATIVE STEELT660.638.60.50.20.13.84.11.82.3COMPARATIVE STEELT759.039.80.50.40.34.44.72.81.7COMPARATIVE STEELa1CRACKING OCCURRED DURING HOT ROLLINGCOMPARATIVE STEELb1COMPARATIVE STEELc1COMPARATIVE STEELd1COMPARATIVE STEELe1COMPARATIVE STEELf1COMPARATIVE STEELg1COMPARATIVE STEELh1COMPARATIVE STEEL

TABLE 5AVERAGEVALUEOF POLE DENSITIESOF {100}<011>POLE DENSITYTO {223}<110>OF {332}<113>STEELORIENTATIONCRYSTALTYPETS (Mpn)u-EL (%)EL (%)Î» (%)GROUPORIENTATIONrCrLr30r60NOTEA1645101244.02.92.60.790.841.101.10COMPARATIVE STEELA25606936.01.72.00.740.791.061.04COMPARATIVE STEELA3830111586.62.92.40.740.790.970.98COMPARATIVE STEELA4751121844.01.82.40.580.631.211.31COMPARATIVE STEELA5886142043.02.92.40.740.790.970.98COMPARATIVE STEELA6779131839.02.92.40.740.790.970.98COMPARATIVE STEELB1804131891.71.51.70.710.761.031.02PRESENT INVENTION STEELB2914141982.82.12.60.710.761.071.05PRESENT INVENTION STEELB3797131845.03.71.60.540.591.271.22COMPARATIVE STEELC1737121895.41.72.50.710.761.031.02PRESENT INVENTION STEELC2814132265.22.42.80.710.761.051.04COMPARATIVE STEELC3708121796.61.92.70.540.591.221.01COMPARATIVE STEELD11083111548.02.73.00.710.761.031.02COMPARATIVE STEELD2855131985.41.71.60.710.761.051.04PRESENT INVENTION STEELD31168152255.01.91.90.710.761.051.04COMPARATIVE STEELE1904141982.62.12.50.720.771.071.06PRESENT INVENTION STEELE2956142078.51.82.20.720.771.091.07PRESENT INVENTION STEELE3668121790.03.33.40.720.771.061.04COMPARATIVE STEELF1900141983.41.41.30.720.771.071.05PRESENT INVENTION STEELF2954142078.42.12.10.720.771.081.07PRESENT INVENTION STEELF3947142080.44.32.00.850.901.441.35PRESENT INVENTION STEELG1107391362.61.62.60.710.761.031.02COMPARATIVE STEELG2817131939.05.24.50.690.741.231.18COMPARATIVE STEELH1891141982.42.22.70.700.751.021.02PRESENT INVENTION STEELI1997142075.92.52.20.720.771.071.05PRESENT INVENTION STEELI2657121799.53.13.10.740.791.111.09PRESENT INVENTION STEELI3881141946.02.31.60.740.791.091.09COMPARATIVE STEELJ1959142078.92.02.70.720.771.071.06PRESENT INVENTION STEELJ2854131944.02.52.40.740.791.091.09COMPARATIVE STEELJ3953142039.04.84.30.550.601.091.09COMPARATIVE STEELK1365162232.01.52.20.700.751.051.04COMPARATIVE STEELL1853121785.91.52.20.710.761.061.04PRESENT INVENTION STEELM1727121795.52.93.60.700.751.041.03PRESENT INVENTION STEELM2936142038.04.10.90.880.931.041.03COMPARATIVE STEELN1883141982.91.92.60.700.751.051.04PRESENT INVENTION STEELO1852131985.81.82.00.700.751.031.02PRESENT INVENTION STEELO2764131841.05.64.40.550.601.461.37COMPARATIVE STEELP1873131984.12.23.30.710.761.041.03PRESENT INVENTION STEELP2105191026.16.15.80.490.541.511.21COMPARATIVE STEELP3104291025.86.05.80.480.551.491.25COMPARATIVE STEELP411136723.11.82.20.720.771.091.07COMPARATIVE STEELQ1818131988.92.32.70.710.761.041.03PRESENT INVENTION STEELQ2485121355.02.52.20.720.771.071.05COMPARATIVE STEELQ3568101151.21.51.70.710.761.031.02COMPARATIVE STEELQ4657111234.03.13.10.740.791.111.09COMPARATIVE STEELR1752131893.32.63.10.710.761.041.03PRESENT INVENTION STEELR21080172474.02.63.00.690.741.031.04PRESENT INVENTION STEELR31073172473.72.52.90.770.821.021.02PRESENT INVENTION STEELR41060162374.32.32.60.720.771.041.03PRESENT INVENTION STEELS1868131985.81.62.10.710.761.051.04PRESENT INVENTION STEELS21020162277.02.02.40.720.771.051.03PRESENT INVENTION STEELS31050162374.91.92.30.710.761.021.03PRESENT INVENTION STEELS41020152175.21.51.80.780.831.081.04PRESENT INVENTION STEELT1780131892.11.81.90.710.761.071.05PRESENT INVENTION STEELT27201217395.74.60.520.571.471.39COMPARATIVE STEELT37351217415.54.30.530.581.451.37COMPARATIVE STEELT49861521365.54.40.550.601.441.40COMPARATIVE STEELT59981622356.25.10.580.631.571.42COMPARATIVE STEELT68981420326.14.60.550.601.621.41COMPARATIVE STEELT788069336.24.70.570.621.591.44COMPARATIVE STEELa1CRACKING OCCURRED DURING HOT ROLLINGCOMPARATIVE STEELb1COMPARATIVE STEELc1COMPARATIVE STEELd1COMPARATIVE STEELe1COMPARATIVE STEELf1COMPARATIVE STEELg1COMPARATIVE STEELh1COMPARATIVE STEEL

INDUSTRIAL APPLICABILITY

As described previously, according to the present invention, it is possible to provide a high-strength cold-rolled steel sheet that is not large in anisotropy even when Nb, Ti, and/or the like are/is added and has excellent uniform elongation and hole expandability. Thus, the present invention is the invention having high industrial applicability.

EXPLANATION OF CODES

1 continuous hot rolling line
2 roughing mill
3 finishing mill
4 hot-rolled steel sheet
5 run-out-table
6 rolling stand
10 inter-stand cooling nozzle
11 cooling nozzle 11