Hot-rolled steel sheet and method for producing same

Information

  • Patent Grant
  • 10167539
  • Patent Number
    10,167,539
  • Date Filed
    Wednesday, March 15, 2017
    7 years ago
  • Date Issued
    Tuesday, January 1, 2019
    5 years ago
Abstract
A hot-rolled steel sheet wherein an average pole density of orientation group of {100}<011> to {223}<110> is 1.0 to 5.0 and pole density of crystal orientation {332}<113> is 1.0 to 4.0. The hot-rolled steel sheet includes, as a metallographic structure, by area %, 30% to 99% ferrite and bainite in total, and 1% to 70% martensite. The hot-rolled steel sheet satisfies Expression 1: dia≤13 μm, and also satisfies Expression 2: TS/fM×dis/dia≥500, wherein an area fraction of the martensite is defined as fM in unit of area %, an average size of the martensite is defined as dia in unit of μm, an average distance between the martensite is defined as dis in unit of μm, and tensile strength of the steel sheet is defined as TS in unit of MPa.
Description
TECHNICAL FIELD

The present invention relates to a high-strength hot-rolled steel sheet which is excellent in uniform deformability contributing to stretchability, drawability, or the like and is excellent in local deformability contributing to bendability, stretch flangeability, burring formability, or the like, and relates to a method for producing the same. Particularly, the present invention relates to a steel sheet including a Dual Phase (DP) structure.


BACKGROUND OF INVENTION

In order to suppress emission of carbon dioxide gas from a vehicle, a weight reduction of an automobile body has been attempted by utilization of a high-strength steel sheet. Moreover, from a viewpoint of ensuring safety of a passenger, the utilization of the high-strength steel sheet for the automobile body has been attempted in addition to a mild steel sheet. However, in order to further improve the weight reduction of the automobile body in future, a usable strength level of the high-strength steel sheet should be increased as compared with that of conventional one. Moreover, in order to utilize the high-strength steel sheet for suspension parts or the like of the automobile body, the local deformability contributing to the burring formability or the like should also be improved in addition to the uniform deformability.


However, in general, when the strength of steel sheet is increased, the formability (deformability) is decreased. For example, Non-Patent Document 1 discloses that uniform elongation which is important for drawing or stretching is decreased by strengthening the steel sheet.


Contrary, Non-Patent Document 2 discloses a method which secures the uniform elongation by compositing metallographic structure of the steel sheet even when the strength is the same.


In addition, Non-Patent Document 3 discloses a metallographic structure control method which improves local ductility representing the bendability, hole expansibility, or the burring formability by controlling inclusions, controlling the microstructure to single phase, and decreasing hardness difference between microstructures. In the Non-Patent Document 3, the microstructure of the steel sheet is controlled to the single phase by microstructure control, and thus, the local deformability contributing to the hole expansibility or the like is improved. However, in order to control the microstructure to the single phase, a heat treatment from an austenite single phase is a basis producing method as described in Non-Patent Document 4.


In addition, the Non-Patent Document 4 discloses a technique which satisfies both the strength and the ductility of the steel sheet by controlling a cooling after a hot-rolling in order to control the metallographic structure, specifically, in order to obtain intended morphologies of precipitates and transformation structures and to obtain an appropriate fraction of ferrite and bainite. However, all techniques as described above are the improvement methods for the local deformability which rely on the microstructure control, and are largely influenced by a microstructure formation of a base.


Also, a method, which improves material properties of the steel sheet by increasing reduction at a continuous hot-rolling in order to refine grains, is known as a related art. For example, Non-Patent Document 5 discloses a technique which improves the strength and toughness of the steel sheet by conducting a large reduction rolling in a comparatively lower temperature range within an austenite range in order to refine the grains of ferrite which is a primary phase of a product by transforming non-recrystallized austenite into the ferrite. However, in Non-Patent Document 5, a method for improving the local deformability to be solved by the present invention is not considered at all.


RELATED ART DOCUMENTS
Non-Patent Documents



  • [Non-Patent Document 1] Kishida: Nippon Steel Technical Report No. 371 (1999), p. 13.

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

  • [Non-Patent Document 3] Katoh et al: Steel-manufacturing studies vol. 312 (1984), p. 41.

  • [Non-Patent Document 4] K. Sugimoto et al: ISIJ International vol. 40 (2000), p. 920.

  • [Non-Patent Document 5] NFG product introduction of NAKAYAMA STEEL WORKS, LTD.



SUMMARY OF INVENTION
Technical Problem

As described above, it is the fact that the technique, which simultaneously satisfies the high-strength and both properties of the uniform deformability and the local deformability, is not found. For example, in order to improve the local deformability of the high-strength steel sheet, it is necessary to conduct the microstructure control including the inclusions. However, since the improvement relies on the microstructure control, it is necessary to control the fraction or the morphology of the microstructure such as the precipitates, the ferrite, or the bainite, and therefore the metallographic structure of the base is limited. Since the metallographic structure of the base is restricted, it is difficult not only to improve the local deformability but also to simultaneously improve the strength and the local deformability.


An object of the present invention is to provide a hot-rolled steel sheet which has the high-strength, the excellent uniform deformability, the excellent local deformability, and small orientation dependence (anisotropy) of formability by controlling texture and by controlling the size or the morphology of the grains in addition to the metallographic structure of the base, and is to provide a method for producing the same. Herein, in the present invention, the strength mainly represents tensile strength, and the high-strength indicates the strength of 440 MPa or more in the tensile strength. In addition, in the present invention, satisfaction of the high-strength, the excellent uniform deformability, and the excellent local deformability indicates a case of simultaneously satisfying all conditions of TS≥440 (unit: MPa), TS×u-EL≥7000 (unit: MPa·%), TS×λ≥30000 (unit: MPa·%), and d/RmC≥1 (no unit) by using characteristic values of the tensile strength (TS), the uniform elongation (u-EL), hole expansion ratio (λ), and d/RmC which is a ratio of thickness d to minimum radius RmC of bending to a C-direction.


Solution to Problem

In the related arts, as described above, the improvement in the local deformability contributing to the hole expansibility, the bendability, or the like has been attempted by controlling the inclusions, by refining the precipitates, by homogenizing the microstructure, by controlling the microstructure to the single phase, by decreasing the hardness difference between the microstructures, or the like. However, only by the above-described techniques, main constituent of the microstructure must be restricted. In addition, when an element largely contributing to an increase in the strength, such as representatively Nb or Ti, is added for high-strengthening, the anisotropy may be significantly increased. Accordingly, other factors for the formability must be abandoned or directions to take a blank before forming must be limited, and as a result, the application is restricted. On the other hand, the uniform deformability can be improved by dispersing hard phases such as martensite in the metallographic structure.


In order to obtain the high-strength and to improve both the uniform deformability contributing to the stretchability or the like and the local deformability contributing to the hole expansibility, the bendability, or the like, the inventors have newly focused influences of the texture of the steel sheet in addition to the control of the fraction or the morphology of the metallographic structures of the steel sheet, and have investigated and researched the operation and the effect thereof in detail. As a result, the inventors have found that, by controlling a chemical composition, the metallographic structure, and the texture represented by pole densities of each orientation of a specific crystal orientation group of the steel sheet, the high-strength is obtained, the local deformability is remarkably improved due to a balance of Lankford-values (r values) in a rolling direction, in a direction (C-direction) making an angle of 90° with the rolling direction, in a direction making an angle of 30° with the rolling direction, or in a direction making an angle of 60° with the rolling direction, and the uniform deformability is also secured due to the dispersion of the hard phases such as the martensite.


An aspect of the present invention employs the following.


(1) A hot-rolled steel sheet according to an aspect of the present invention includes, as a chemical composition, by mass %, C: 0.01% to 0.4%, Si: 0.001% to 2.5%, Mn: 0.001% to 4.0%, Al: 0.001% to 2.0%, P: limited to 0.15% or less, S: limited to 0.03% or less, N: limited to 0.01% or less, O: limited to 0.01% or less, and a balance consisting of Fe and unavoidable impurities, wherein: an average pole density of an orientation group of {100}<011> to {223}<110>, which is a pole density represented by an arithmetic average of pole densities of each crystal orientation {100}<011>, {116}<110>, {114}<110>, {112}<110>, and {223}<110>, is 1.0 to 5.0 and a pole density of a crystal orientation {332}<113> is 1.0 to 4.0 in a thickness central portion which is a thickness range of ⅝ to ⅜ based on a surface of the steel sheet; the steel sheet includes, as a metallographic structure, plural grains, and includes, by area %, a ferrite and a bainite of 30% to 99% in total and a martensite of 1% to 70%; and when an area fraction of the martensite is defined as fM in unit of area %, an average size of the martensite is defined as dia in unit of μm, an average distance between the martensite is defined as dis in unit of μm, and a tensile strength of the steel sheet is defined as TS in unit of MPa, a following Expression 1 and a following Expression 2 are satisfied.

dia≤13μm  (Expression 1)
TS/fM×dis/dia≤500  (Expression 2)


(2) The hot-rolled steel sheet according to (1) may further includes, as the chemical composition, by mass %, at least one selected from the group consisting of Mo: 0.001% to 1.0%, Cr: 0.001% to 2.0%, Ni: 0.001% to 2.0%, Cu: 0.001% to 2.0%, B: 0.0001% to 0.005%, Nb: 0.001% to 0.2%, Ti: 0.001% to 0.2%, V: 0.001% to 1.0%, W: 0.001% to 1.0%, Ca: 0.0001% to 0.01%, Mg: 0.0001% to 0.01%, Zr: 0.0001% to 0.2%, Rare Earth Metal: 0.0001% to 0.1%, As: 0.0001% to 0.5%, Co: 0.0001% to 1.0%, Sn: 0.0001% to 0.2%, Pb: 0.0001% to 0.2%, Y: 0.0001% to 0.2%, and Hf: 0.0001% to 0.2%.


(3) In the hot-rolled steel sheet according to (1) or (2), a volume average diameter of the grains may be 5 μm to 30 μm.


(4) In the hot-rolled steel sheet according to (1) or (2), the average pole density of the orientation group of {100}<011> to {223}<110> may be 1.0 to 4.0, and the pole density of the crystal orientation {332}<113> may be 1.0 to 3.0.


(5) In the hot-rolled steel sheet according to any one of (1) to (4), when a major axis of the martensite is defined as La, and a minor axis of the martensite is defined as Lb, an area fraction of the martensite satisfying a following Expression 3 may be 50% to 100% as compared with the area fraction fM of the martensite.

La/Lb≤5.0  (Expression 3)


(6) In the hot-rolled steel sheet according to any one of (1) to (5), the steel sheet may include, as the metallographic structure, by area %, the ferrite of 30% to 99%.


(7) In the hot-rolled steel sheet according to any one of (1) to (6), the steel sheet may include, as the metallographic structure, by area %, the bainite of 5% to 80%.


(8) In the hot-rolled steel sheet according to any one of (1) to (7), the steel sheet may include a tempered martensite in the martensite.


(9) In the hot-rolled steel sheet according to any one of (1) to (8), an area fraction of coarse grain having grain size of more than 35 μm may be 0% to 10% among the grains in the metallographic structure of the steel sheet.


(10) In the hot-rolled steel sheet according to any one of (1) to (9), a hardness H of the ferrite may satisfy a following Expression 4.

H<200+30×[Si]+21×[Mn]+270×[P]+78×[Nb]1/2+108×[Ti]1/2  (Expression 4)


(11) In the hot-rolled steel sheet according to any one of (1) to (10), when a hardness of the ferrite or the bainite which is a primary phase is measured at 100 points or more, a value dividing a standard deviation of the hardness by an average of the hardness may be 0.2 or less.


(12) A method for producing a hot-rolled steel sheet according to an aspect of the present invention includes: first-hot-rolling a steel in a temperature range of 1000° C. to 1200° C. under conditions such that at least one pass whose reduction is 40% or more is included so as to control an average grain size of an austenite in the steel to 200 μm or less, wherein the steel includes, as a chemical composition, by mass %, C: 0.01% to 0.4%, Si: 0.001% to 2.5%, Mn: 0.001% to 4.0%, Al: 0.001% to 2.0%, P: limited to 0.15% or less, S: limited to 0.03% or less, N: limited to 0.01% or less, O: limited to 0.01% or less, and a balance consisting of Fe and unavoidable impurities; second-hot-rolling the steel under conditions such that, when a temperature calculated by a following Expression 5 is defined as T1 in unit of ° C. and a ferritic transformation temperature calculated by a following Expression 6 is defined as Ar3 in unit of ° C., a large reduction pass whose reduction is 30% or more in a temperature range of T1+30° C. to T1+200° C. is included, a cumulative reduction in the temperature range of T1+30° C. to T1+200° C. is 50% or more, a cumulative reduction in a temperature range of Ar3 to lower than T1+30° C. is limited to 30% or less, and a rolling finish temperature is Ar3 or higher; first-cooling the steel under conditions such that, when a waiting time from a finish of a final pass in the large reduction pass to a cooling start is defined as tin unit of second, the waiting time t satisfies a following Expression 7, an average cooling rate is 50° C./second or faster, a cooling temperature change which is a difference between a steel temperature at the cooling start and a steel temperature at a cooling finish is 40° C. to 140° C., and the steel temperature at the cooling finish is T1+100° C. or lower; second-cooling the steel to a temperature range of 600° C. to 800° C. under an average cooling rate of 15° C./second to 300° C./second after finishing the second-hot-rolling; holding the steel in the temperature range of 600° C. to 800° C. for 1 second to 15 seconds; third-cooling the steel to a temperature range of a room temperature to 350° C. under an average cooling rate of 50° C./second to 300° C./second after finishing the holding; coiling the steel in the temperature range of the room temperature to 350° C.

T1=850+10×([C]+[N])×[Mn]  (Expression 5)


here, [C], [N], and [Mn] represent mass percentages of C, N, and Mn respectively.

Ar3=879.4−516.1×[C]−65.7×[Mn]+38.0×[Si]+274.7×[P]   (Expression 6)


here, in Expression 6, [C], [Mn], [Si] and [P] represent mass percentages of C, Mn, Si, and P respectively.

t≤2.5×t1  (Expression 7)

here, t1 is represented by a following Expression 8.

t1=0.001×((Tf−T1)×P1/100)2−0.109×((Tf−T1)×P1/100)+3.1   (Expression 8)

here, Tf represents a celsius temperature of the steel at the finish of the final pass, and P1 represents a percentage of a reduction at the final pass.


(13) In the method for producing the hot-rolled steel sheet according to (12), the steel may further includes, as the chemical composition, by mass %, at least one selected from the group consisting of Mo: 0.001% to 1.0%, Cr: 0.001% to 2.0%, Ni: 0.001% to 2.0%, Cu: 0.001% to 2.0%, B: 0.0001% to 0.005%, Nb: 0.001% to 0.2%, Ti: 0.001% to 0.2%, V: 0.001% to 1.0%, W: 0.001% to 1.0%, Ca: 0.0001% to 0.01%, Mg: 0.0001% to 0.01%, Zr: 0.0001% to 0.2%, Rare Earth Metal: 0.0001% to 0.1%, As: 0.0001% to 0.5%, Co: 0.0001% to 1.0%, Sn: 0.0001% to 0.2%, Pb: 0.0001% to 0.2%, Y: 0.0001% to 0.2%, and Hf: 0.0001% to 0.2%, wherein a temperature calculated by a following Expression 9 may be substituted for the temperature calculated by the Expression 5 as T1.

T1=850+10×([C]+[N])×[Mn]+350×[Nb]+250×[Ti]+40×[B]+10×[Cr]+100×[Mo]+100×[V]  (Expression 9)


here, [C], [N], [Mn], [Nb], [Ti], [B], [Cr], [Mo], and [V] represent mass percentages of C, N, Mn, Nb, Ti, B, Cr, Mo, and V respectively.


(14) In the method for producing the hot-rolled steel sheet according to (12) or (13), the waiting time t may further satisfy a following Expression 10.

0≤t<t1  (Expression 10)


(15) In the method for producing the hot-rolled steel sheet according to (12) or (13), the waiting time t may further satisfy a following Expression 11.

t1≤t t1×2.5  (Expression 11)


(16) In the method for producing the hot-rolled steel sheet according to any one of (12) to (15), in the first-hot-rolling, at least two times of rollings whose reduction is 40% or more may be conducted, and the average grain size of the austenite may be controlled to 100 μm or less.


(17) In the method for producing the hot-rolled steel sheet according to any one of (12) to (16), the second-cooling may start within 3 seconds after finishing the second-hot-rolling.


(18) In the method for producing the hot-rolled steel sheet according to any one of (12) to (17), in the second-hot-rolling, a temperature rise of the steel between passes may be 18° C. or lower.


(19) In the method for producing the hot-rolled steel sheet according to any one of (12) to (18), a final pass of rollings in the temperature range of T1+30° C. to T1+200° C. may be the large reduction pass.


(20) In the method for producing the hot-rolled steel sheet according to any one of (12) to (19), in the holding, the steel may be held in a temperature range of 600° C. to 680° C. for 3 seconds to 15 seconds.


(21) In the method for producing the hot-rolled steel sheet according to any one of (12) to (20), the first-cooling may be conducted at an interval between rolling stands.


Advantageous Effects of Invention

According to the above aspects of the present invention, it is possible to obtain a hot-rolled steel sheet which has the high-strength, the excellent uniform deformability, the excellent local deformability, and the small anisotropy even when the element such as Nb or Ti is added.





BRIEF DESCRIPTION OF DRAWINGS


FIG. 1 shows a relationship between an average pole density D1 of an orientation group of {100}<011> to {223}<110> and d/RmC (thickness d/minimum bend radius RmC).



FIG. 2 shows a relationship between a pole density D2 of a crystal orientation {332}<113> and d/RmC.





DETAILED DESCRIPTION OF PREFERRED EMBODIMENTS

Hereinafter, a hot-rolled steel sheet according to an embodiment of the present invention will be described in detail. First, a pole density of a crystal orientation of the hot-rolled steel sheet will be described.


Average Pole Density D1 of Crystal Orientation: 1.0 to 5.0


Pole Density D2 of Crystal Orientation: 1.0 to 4.0


In the hot-rolled steel sheet according to the embodiment, as the pole densities of two kinds of the crystal orientations, the average pole density D1 of an orientation group of {100}<011> to {223}<110> (hereinafter, referred to as “average pole density”) and the pole density D2 of a crystal orientation {332}<113> in a thickness central portion, which is a thickness range of ⅝ to ⅜ (a range which is ⅝ to ⅜ of the thickness distant from a surface of the steel sheet along a normal direction (a depth direction) of the steel sheet), are controlled in reference to a thickness-cross-section (a normal vector thereof corresponds to the normal direction) which is parallel to a rolling direction.


In the embodiment, the average pole density D1 is an especially-important characteristic (orientation integration and development degree of texture) of the texture (crystal orientation of grains in metallographic structure). Herein, the average pole density D1 is the pole density which is represented by an arithmetic average of pole densities of each crystal orientation {100}<011>, {116}<110>, {114}<110>, {112}<110>, and {223}<110>.


A intensity ratio of electron diffraction intensity or X-ray diffraction intensity of each orientation to that of a random sample is obtained by conducting Electron Back Scattering Diffraction (EBSD) or X-ray diffraction on the above cross-section in the thickness central portion which is the thickness range of ⅝ to ⅜, and the average pole density D1 of the orientation group of {100}<011> to {223}<110> can be obtained from each intensity ratio.


When the average pole density D1 of the orientation group of {100}<011> to {223}<110> is 5.0 or less, it is satisfied that d/RmC (a parameter in which the thickness d is divided by a minimum bend radius RmC (C-direction bending)) is 1.0 or more, which is minimally-required for working suspension parts or frame parts. Particularly, the condition is a requirement in order that tensile strength TS, hole expansion ratio λ, and total elongation EL preferably satisfy TS×λ≥30000 and TS×EL≥14000 which are two conditions required for the suspension parts of the automobile body.


In addition, when the average pole density D1 is 4.0 or less, a ratio (Rm45/RmC) of a minimum bend radius Rm45 of 45°-direction bending to the minimum bend radius RmC of the C-direction bending is decreased, in which the ratio is a parameter of orientation dependence (isotropy) of formability, and the excellent local deformability which is independent of the bending direction can be secured. As described above, the average pole density D1 may be 5.0 or less, and may be preferably 4.0 or less. In a case where the further excellent hole expansibility or small critical bending properties are needed, the average pole density D1 may be more preferably less than 3.5, and may be furthermore preferably less than 3.0.


When the average pole density D1 of the orientation group of {100}<011> to {223}<110> is more than 5.0, the anisotropy of mechanical properties of the steel sheet is significantly increased. As a result, although the local deformability in only a specific direction is improved, the local deformability in a direction different from the specific direction is significantly decreased. Therefore, in the case, the steel sheet cannot satisfy d/RmC≥1.0.


On the other hand, when the average pole density D1 is less than 1.0, the local deformability may be decreased. Accordingly, preferably, the average pole density D1 may be 1.0 or more.


In addition, from the similar reasons, the pole density D2 of the crystal orientation {332}<113> in the thickness central portion which is the thickness range of ⅝ to ⅜ may be 4.0 or less. The condition is a requirement in order that the steel sheet satisfies d/RmC≥1.0, and particularly, that the tensile strength TS, the hole expansion ratio λ, and the total elongation EL preferably satisfy TS×λ≥30000 and TS×EL≥14000 which are two conditions required for the suspension parts.


Moreover, when the pole density D2 is 3.0 or less, TS×λ or d/RmC can be further improved. The pole density D2 may be preferably 2.5 or less, and may be more preferably 2.0 or less. When the pole density D2 is more than 4.0, the anisotropy of the mechanical properties of the steel sheet is significantly increased. As a result, although the local deformability in only a specific direction is improved, the local deformability in a direction different from the specific direction is significantly decreased. Therefore, in the case, the steel sheet cannot sufficiently satisfy d/RmC≥1.0.


On the other hand, when the average pole density D2 is less than 1.0, the local deformability may be decreased. Accordingly, preferably, the pole density D2 of the crystal orientation {332}<113> may be 1.0 or more.


The pole density is synonymous with an X-ray random intensity ratio. The X-ray random intensity ratio can be obtained as follows. Diffraction intensity (X-ray or electron) of a standard sample which does not have a texture to a specific orientation and diffraction intensity of a test material are measured by the X-ray diffraction method in the same conditions. The X-ray random intensity ratio is obtained by dividing the diffraction intensity of the test material by the diffraction intensity of the standard sample. The pole density can be measured by using the X-ray diffraction, the Electron Back Scattering Diffraction (EBSD), or Electron Channeling Pattern (ECP). For example, the average pole density D1 of the orientation group of {100}<011> to {223}<110> can be obtained as follows. The pole densities of each orientation {100}<110>, {116}<110>, {114}<110>, {112}<110>, and {223}<110> are obtained from a three-dimensional texture (ODF: Orientation Distribution Functions) which is calculated by a series expanding method using plural pole figures in pole figures of {110}, {100}, {211}, and {310} measured by the above methods. The average pole density D1 is obtained by calculating an arithmetic average of the pole densities.


With respect to samples which are supplied for the X-ray diffraction, the EBSD, and the ECP, the thickness of the steel sheet may be reduced to a predetermined thickness by mechanical polishing or the like, strain may be removed by chemical polishing, electrolytic polishing, or the like, the samples may be adjusted so that an appropriate surface including the thickness range of ⅝ to ⅜ is a measurement surface, and then the pole densities may be measured by the above methods. With respect to a transverse direction, it is preferable that the samples are collected in the vicinity of ¼ or ¾ position of the thickness (a position which is at ¼ of a steel sheet width distant from a side edge the steel sheet).


When the above pole densities are satisfied in many other thickness portions of the steel sheet in addition to the thickness central portion, the local deformability is further improved. However, since the texture in the thickness central portion significantly influences the anisotropy of the steel sheet, the material properties of the thickness central portion approximately represent the material properties of the entirety of the steel sheet. Accordingly, the average pole density D1 of the orientation group of {100}<011> to {223}<110> and the pole density D2 of the crystal orientation {332}<113> in the thickness central portion of ⅝ to ⅜ are prescribed.


Herein, {hkl}<uvw> indicates that the normal direction of the sheet surface is parallel to <hkl> and the rolling direction is parallel to <uvw> when the sample is collected by the above-described method. In addition, generally, in the orientation of the crystal, an orientation perpendicular to the sheet surface is represented by (hkl) or {hkl} and an orientation parallel to the rolling direction is represented by [uvw] or <uvw>. {hkl}<uvw> indicates collectively equivalent planes, and (hkl)[uvw] indicates each crystal plane. Specifically, since the embodiment targets a body centered cubic (bcc) structure, for example, (111), (−111), (1−11), (11−1), (−1−11), (−11−1), (1−1−1), and (−1−1−1) planes are equivalent and cannot be classified. In the case, the orientation is collectively called as {111}. Since the ODF expression is also used for orientation expressions of other crystal structures having low symmetry, generally, each orientation is represented by (hkl)[uvw] in the ODF expression. However, in the embodiment, {hkl}<uvw> and (hkl)[uvw] are synonymous.


Next, a metallographic structure of the hot-rolled steel sheet according to the embodiment will be described.


A metallographic structure of the hot-rolled steel sheet according to the embodiment is fundamentally to be a Dual Phase (DP) structure which includes plural grains, includes ferrite and/or bainite as a primary phase, and includes martensite as a secondary phase. The strength and the uniform deformability can be increased by dispersing the martensite which is the secondary phase and the hard phase to the ferrite or the bainite which is the primary phase and has the excellent deformability. The improvement in the uniform deformability is derived from an increase in work hardening rate by finely dispersing the martensite which is the hard phase in the metallographic structure. Moreover, herein, the ferrite or the bainite includes polygonal ferrite and bainitic ferrite.


The hot-rolled steel sheet according to the embodiment includes residual austenite, pearlite, cementite, plural inclusions, or the like as the microstructure in addition to the ferrite, the bainite, and the martensite. It is preferable that the microstructures other than the ferrite, the bainite, and the martensite are limited to, by area %, 0% to 10%. Moreover, when the austenite is retained in the microstructure, secondary work embrittlement or delayed fracture properties deteriorates. Accordingly, except for the residual austenite of approximately 5% in area fraction which unavoidably exists, it is preferable that the residual austenite is not substantially included.


Area Fraction of Ferrite and Bainite which are Primary Phase: 30% to Less than 99%


The ferrite and the bainite which are the primary phase are comparatively soft, and have the excellent deformability. When the area fraction of the ferrite and the bainite is 30% or more in total, both properties of the uniform deformability and the local deformability of the hot-rolled steel sheet according to the embodiment are satisfied. More preferably, the ferrite and the bainite may be, by area %, 50% or more in total. On the other hand, when the area fraction of the ferrite and the bainite is 99% or more in total, the strength and the uniform deformability of the steel sheet are decreased.


Preferably, the area fraction of the ferrite which is the primary phase may be 30% to 99%. By controlling the area fraction of the ferrite which is comparatively excellent in the deformability to 30% to 99%, it is possible to preferably increase the ductility (deformability) in a balance between the strength and the ductility (deformability) of the steel sheet. Particularly, the ferrite contributes to the improvement in the uniform deformability.


Alternatively, the area fraction of the bainite which is the primary phase may be 5% to 80%. By controlling the area fraction of the bainite which is comparatively excellent in the strength to 5% to 80%, it is possible to preferably increase the strength in a balance between the strength and the ductility (deformability) of the steel sheet. By increasing the area fraction of the bainite which is harder phase than the ferrite, the strength of the steel sheet is improved. In addition, the bainite, which has small hardness difference from the martensite as compared with the ferrite, suppresses initiation of voids at an interface between the soft phase and the hard phase, and improves the hole expansibility.


Area Fraction fM of Martensite: 1% to 70%


By dispersing the martensite, which is the secondary phase and is the hard phase, in the metallographic structure, it is possible to improve the strength and the uniform deformability. When the area fraction of the martensite is less than 1%, the dispersion of the hard phase is insufficient, the work hardening rate is decreased, and the uniform deformability is decreased. Preferably, the area fraction of the martensite may be 3% or more. On the other hand, when the area fraction of the martensite is more than 70%, the area fraction of the hard phase is excessive, and the deformability of the steel sheet is significantly decreased. In accordance with the balance between the strength and the deformability, the area fraction of the martensite may be 50% or less. Preferably, the area fraction of the martensite may be 30% or less. More preferably, the area fraction of the martensite may be 20% or less.


Average Grain Size dia of Martensite: 13 μm or Less


When the average size of the martensite is more than 13 μm, the uniform deformability of the steel sheet may be decreased, and the local deformability may be decreased. It is considered that the uniform elongation is decreased due to the fact that contribution to the work hardening is decreased when the average size of the martensite is coarse, and that the local deformability is decreased due to the fact that the voids easily initiates in the vicinity of the coarse martensite. Preferably, the average size of the martensite may be less than 10 μm. More preferably, the average size of the martensite may be 7 μm or less.


Relationship of TS/fM×dis/dia: 500 or More


Moreover, as a result of the investigation in detail by the inventors, it is found that, when the tensile strength is defined as TS (tensile strength) in unit of MPa, the area fraction of the martensite is defined as fM (fraction of Martensite) in unit of %, an average distance between the martensite grains is defined as dis (distance) in unit of μm, and the average grain size of the martensite is defined as dia (diameter) in unit of μm, the uniform deformability of the steel sheet is improved in a case that a relationship among the TS, the fM, the dis, and the dia satisfies a following Expression 1.

TS/fM×dis/dia≥500  (Expression 1)


When the relationship of TS/fM×dis/dia is less than 500, the uniform deformability of the steel sheet may be significantly decreased. A physical meaning of the Expression 1 has not been clear. However, it is considered that the work hardening more effectively occurs as the average distance dis between the martensite grains is decreased and as the average grain size dia of the martensite is increased. Moreover, the relationship of TS/fM×dis/dia does not have particularly an upper limit. However, from an industrial standpoint, since the relationship of TS/fM×dis/dia barely exceeds 10000, the upper limit may be 10000 or less.


Fraction of Martensite Having 5.0 or Less in Ratio of Major Axis to Minor Axis: 50% or More


In addition, when a major axis of a martensite grain is defined as La in unit of μm and a minor axis of a martensite grain is defined as Lb in unit of μm, the local deformability may be preferably improved in a case that an area fraction of the martensite grain satisfying a following Expression 2 is 50% to 100% as compared with the area fraction fM of the martensite.

La/Lb≤5.0  (Expression 2)


The detail reasons why the effect is obtained has not been clear. However, it is considered that the local deformability is improved due to the fact that the shape of the martensite varies from an acicular shape to a spherical shape and that excessive stress concentration to the ferrite or the bainite near the martensite is relieved. Preferably, the area fraction of the martensite grain having La/Lb of 3.0 or less may be 50% or more as compared with the fM. More preferably, the area fraction of the martensite grain having La/Lb of 2.0 or less may be 50% or more as compared with the fM. Moreover, when the fraction of equiaxial martensite is less than 50% as compared with the fM, the local deformability may deteriorate. Moreover, a lower limit of the Expression 2 may be 1.0.


Moreover, all or part of the martensite may be a tempered martensite. When the martensite is the tempered martensite, although the strength of the steel sheet is decreased, the hole expansibility of the steel sheet is improved by a decrease in the hardness difference between the primary phase and the secondary phase. In accordance with the balance between the required strength and the required deformability, the area fraction of the tempered martensite may be controlled as compared with the area fraction fM of the martensite.


The metallographic structure such as the ferrite, the bainite, or the martensite as described above can be observed by a Field Emission Scanning Electron Microscope (FE-SEM) in a thickness range of ⅛ to ⅜ (a thickness range in which ¼ position of the thickness is the center). The above characteristic values can be determined from micrographs which are obtained by the observation. In addition, the characteristic values can be also determined by the EBSD as described below. For the observation of the FE-SEM, samples are collected so that an observed section is the thickness-cross-section (the normal vector thereof corresponds to the normal direction) which is parallel to the rolling direction of the steel sheet, and the observed section is polished and nital-etched. Moreover, in the thickness direction, the metallographic structure (constituent) of the steel sheet may be significantly different between the vicinity of the surface of the steel sheet and the vicinity of the center of the steel sheet because of decarburization and Mn segregation. Accordingly, in the embodiment, the metallographic structure based on ¼ position of the thickness is observed.


Volume Average Diameter of Grains: 5 μm to 30 μm


Moreover, in order to further improve the deformability, size of the grains in the metallographic structure, particularly, the volume average diameter may be refined. Moreover, fatigue properties (fatigue limit ratio) required for an automobile steel sheet or the like are also improved by refining the volume average diameter. Since the number of coarse grains significantly influences the deformability as compared with the number of fine grains, the deformability significantly correlates with the volume average diameter calculated by the weighted average of the volume as compared with a number average diameter. Accordingly, in order to obtain the above effects, the volume average diameter may be 5 μm to 30 μm, may be more preferably 5 μm to 20 μm, and may be furthermore preferably 5 μm to 10 μm.


Moreover, it is considered that, when the volume average diameter is decreased, local strain concentration occurred in micro-order is suppressed, the strain can be dispersed during local deformation, and the elongation, particularly, the uniform elongation is improved. In addition, when the volume average diameter is decreased, a grain boundary which acts as a barrier of dislocation motion may be appropriately controlled, the grain boundary may affect repetitive plastic deformation (fatigue phenomenon) derived from the dislocation motion, and thus, the fatigue properties may be improved.


Moreover, as described below, the diameter of each grain (grain unit) can be determined. The pearlite is identified through a metallographic observation by an optical microscope. In addition, the grain units of the ferrite, the austenite, the bainite, and the martensite are identified by the EBSD. If crystal structure of an area measured by the EBSD is a face centered cubic structure (fcc structure), the area is regarded as the austenite. Moreover, if crystal structure of an area measured by the EBSD is the body centered cubic structure (bcc structure), the area is regarded as the any one of the ferrite, the bainite, and the martensite. The ferrite, the bainite, and the martensite can be identified by using a Kernel Average Misorientation (KAM) method which is added in an Electron Back Scatter Diffraction Pattern-Orientation Image Microscopy (EBSP-OIM, Registered Trademark). In the KAM method, with respect to a first approximation (total 7 pixels) using a regular hexagonal pixel (central pixel) in measurement data and 6 pixels adjacent to the central pixel, a second approximation (total 19 pixels) using 12 pixels further outside the above 6 pixels, or a third approximation (total 37 pixels) using 18 pixels further outside the above 12 pixels, an misorientation between each pixel is averaged, the obtained average is regarded as the value of the central pixel, and the above operation is performed on all pixels. The calculation by the KAM method is performed so as not to exceed the grain boundary, and a map representing intragranular crystal rotation can be obtained. The map shows strain distribution based on the intragranular local crystal rotation.


In the embodiment, the misorientation between adjacent pixels is calculated by using the third approximation in the EBSP-OIM (registered trademark). For example, the above-described orientation measurement is conducted by a measurement step of 0.5 μm or less at a magnification of 1500-fold, a position in which the misorientation between the adjacent measurement points is more than 15° is regarded as a grain border (the grain border is not always a general grain boundary), the circle equivalent diameter is calculated, and thus, the grain sizes of the ferrite, the bainite, the martensite, and the austenite are obtained. When the pearlite is included in the metallographic structure, the grain size of the pearlite can be calculated by applying an image processing method such as binarization processing or an intercept method to the micrograph obtained by the optical microscope.


In the grain (grain unit) defined as described above, when a circle equivalent radius (a half value of the circle equivalent diameter) is defined as r, the volume of each grain is obtained by 4×π×r3 3, and the volume average diameter can be obtained by the weighted average of the volume. In addition, an area fraction of coarse grains described below can be obtained by dividing area of the coarse grains obtained using the method by measured area. Moreover, except for the volume average diameter, the circle equivalent diameter or the grain size obtained by the binarization processing, the intercept method, or the like is used, for example, as the average grain size dia of the martensite.


The average distance dis between the martensite grains may be determined by using the border between the martensite grain and the grain other than the martensite obtained by the EBSD method (however, FE-SEM in which the EBSD can be conducted) in addition to the FE-SEM observation method.


Area Fraction of Coarse Grains Having Grain Size of More than 35 μm: 0% to 10%


In addition, in order to further improve the local deformability, with respect to all constituents of the metallographic structure, the area fraction (the area fraction of the coarse grains) which is occupied by grains (coarse grains) having the grain size of more than 35 μm occupy per unit area may be limited to be 0% to 10%. When the grains having a large size are increased, the tensile strength may be decreased, and the local deformability may be also decreased. Accordingly, it is preferable to refine the grains. Moreover, since the local deformability is improved by straining all grains uniformly and equivalently, the local strain of the grains may be suppressed by limiting the fraction of the coarse grains.


Standard Deviation of Average Distance dis Between Martensite Grains: 5 μm or Less


Moreover, in order to further improve the local deformability such as the bendability, the stretch flangeability, the burring formability, or the hole expansibility, it is preferable that the martensite which is the hard phase is dispersed in the metallographic structure. Therefore, it is preferable that the standard deviation of the average distance dis between the martensite grains is 0 μm to 5 μm. In the case, the average distance dis and the standard deviation thereof may be obtained by measuring the distance between the martensite grains at 100 points or more.


Hardness H of Ferrite: It is Preferable to Satisfy a Following Expression 3


The ferrite which is the primary phase and the soft phase contributes to the improvement in the deformability of the steel sheet. Accordingly, it is preferable that the average hardness H of the ferrite satisfies the following Expression 3. When a ferrite which is harder than the following Expression 3 is contained, the improvement effects of the deformability of the steel sheet may not be obtained. Moreover, the average hardness H of the ferrite is obtained by measuring the hardness of the ferrite at 100 points or more under a load of 1 mN in a nano-indenter.

H<200+30×[Si]+21×[Mn]+270×[P]+78×[Nb]1/2+108×[Ti]1/2  (Expression 3)


Here, [Si], [Mn], [P], [Nb], and [Ti] represent mass percentages of Si, Mn, P, Nb, and Ti respectively.


Standard Deviation/Average of Hardness of Ferrite or Bainite: 0.2 or Less


As a result of investigation which is focused on the homogeneity of the ferrite or bainite which is the primary phase by the inventors, it is found that, when the homogeneity of the primary phase is high in the microstructure, the balance between the uniform deformability and the local deformability may be preferably improved. Specifically, when a value, in which the standard deviation of the hardness of the ferrite is divided by the average of the hardness of the ferrite, is 0.2 or less, the effects may be preferably obtained. Moreover, when a value, in which the standard deviation of the hardness of the bainite is divided by the average of the hardness of the bainite, is 0.2 or less, the effects may be preferably obtained. The homogeneity can be obtained by measuring the hardness of the ferrite or the bainite which is the primary phase at 100 points or more under the load of 1 mN in the nano-indenter and by using the obtained average and the obtained standard deviation. Specifically, the homogeneity increases with a decrease in the value of the standard deviation of the hardness/the average of the hardness, and the effects may be obtained when the value is 0.2 or less. In the nano-indenter (for example, UMIS-2000 manufactured by CSIRO corporation), by using a smaller indenter than the grain size, the hardness of a single grain which does not include the grain boundary can be measured.


Next, a chemical composition of the hot-rolled steel sheet according to the embodiment will be described.


Hereinafter, description will be given of the base elements of the hot rolled steel sheet according to the embodiment and of the limitation range and reasons for the limitation. Moreover, the % in the description represents mass %.


C: 0.01% to 0.4%


C (carbon) is an element which increases the strength of the steel sheet, and is an essential element to obtain the area fraction of the martensite. A lower limit of C content is to be 0.01% in order to obtain the martensite of 1% or more, by area %. On the other hand, when the C content is more than 0.40%, the deformability of the steel sheet is decreased, and weldability of the steel sheet also deteriorates. Preferably, the C content may be 0.30% or less.


Si: 0.001% to 2.5%


Si (silicon) is a deoxidizing element of the steel and is an element which is effective in an increase in the mechanical strength of the steel sheet. Moreover, Si is an element which stabilizes the ferrite during the temperature control after the hot-rolling and suppresses cementite precipitation during the bainitic transformation. However, when Si content is more than 2.5%, the deformability of the steel sheet is decreased, and surface dents tend to be made on the steel sheet. On the other hand, when the Si content is less than 0.001%, it is difficult to obtain the effects.


Mn: 0.001% to 4.0%


Mn (manganese) is an element which is effective in an increase in the mechanical strength of the steel sheet. However, when Mn content is more than 4.0%, the deformability of the steel sheet is decreased. Preferably, the Mn content may be 3.5% or less. More preferably, the Mn content may be 3.0% or less. On the other hand, when the Mn content is less than 0.001%, it is difficult to obtain the effects. In addition, Mn is also an element which suppresses cracks during the hot-rolling by fixing S (sulfur) in the steel. When elements such as Ti which suppresses occurrence of cracks due to S during the hot-rolling are not sufficiently added except for Mn, it is preferable that the Mn content and the S content satisfy Mn/S≥20 by mass %.


Al: 0.001% to 2.0%


Al (aluminum) is a deoxidizing element of the steel. Moreover, Al is an element which stabilizes the ferrite during the temperature control after the hot-rolling and suppresses the cementite precipitation during the bainitic transformation. In order to obtain the effects, Al content is to be 0.001% or more. However, when the Al content is more than 2.0%, the weldability deteriorates. In addition, although it is difficult to quantitatively show the effects, Al is an element which significantly increases a temperature Ar3 at which transformation starts from γ(austenite) to α(ferrite) at the cooling of the steel. Accordingly, Ar3 of the steel may be controlled by the Al content.


The hot-rolled steel sheet according to the embodiment includes unavoidable impurities in addition to the above described base elements. Here, the unavoidable impurities indicate elements such as P, S, N, O, Cd, Zn, or Sb which are unavoidably mixed from auxiliary raw materials such as scrap or from production processes. In the elements, P, S, N, and O are limited to the following in order to preferably obtain the effects. It is preferable that the unavoidable impurities other than P, S, N, and O are individually limited to 0.02% or less. Moreover, even when the impurities of 0.02% or less are included, the effects are not affected. The limitation range of the impurities includes 0%, however, it is industrially difficult to be stably 0%. Here, the described % is mass %.


P: 0.15% or Less


P (phosphorus) is an impurity, and an element which contributes to crack during the hot-rolling or the cold-rolling when the content in the steel is excessive. In addition, P is an element which deteriorates the ductility or the weldability of the steel sheet. Accordingly, the P content is limited to 0.15% or less. Preferably, the P content may be limited to 0.05% or less. Moreover, since P acts as a solid solution strengthening element and is unavoidably included in the steel, it is not particularly necessary to prescribe a lower limit of the P content. The lower limit of the P content may be 0%. Moreover, considering current general refining (includes secondary refining), the lower limit of the P content may be 0.0005%.


S: 0.03% or Less


S (sulfur) is an impurity, and an element which deteriorates the deformability of the steel sheet by forming MnS stretched by the hot-rolling when the content in the steel is excessive. Accordingly, the S content is limited to 0.03% or less. Moreover, since S is unavoidably included in the steel, it is not particularly necessary to prescribe a lower limit of the S content. The lower limit of the S content may be 0%. Moreover, considering the current general refining (includes the secondary refining), the lower limit of the S content may be 0.0005%.


N: 0.01% or Less


N (nitrogen) is an impurity, and an element which deteriorates the deformability of the steel sheet. Accordingly, the N content is limited to 0.01% or less. Moreover, since N is unavoidably included in the steel, it is not particularly necessary to prescribe a lower limit of the N content. The lower limit of the N content may be 0%. Moreover, considering the current general refining (includes the secondary refining), the lower limit of the N content may be 0.0005%.


O: 0.01% or Less


O (oxygen) is an impurity, and an element which deteriorates the deformability of the steel sheet. Accordingly, the O content is limited to 0.01% or less. Moreover, since 0 is unavoidably included in the steel, it is not particularly necessary to prescribe a lower limit of the O content. The lower limit of the O content may be 0%. Moreover, considering the current general refining (includes the secondary refining), the lower limit of the O content may be 0.0005%.


The above chemical elements are base components (base elements) of the steel in the embodiment, and the chemical composition, in which the base elements are controlled (included or limited) and the balance consists of Fe and unavoidable impurities, is a base composition of the embodiment. However, in addition to the base elements (instead of a part of Fe which is the balance), in the embodiment, the following chemical elements (optional elements) may be additionally included in the steel as necessary. Moreover, even when the optional elements are unavoidably included in the steel (for example, amount less than a lower limit of each optional element), the effects in the embodiment are not decreased.


Specifically, the hot-rolled steel sheet according to the embodiment may further include, as a optional element, at least one selected from a group consisting of Mo, Cr, Ni, Cu, B, Nb, Ti, V, W, Ca, Mg, Zr, REM, As, Co, Sn, Pb, Y, and Hf in addition to the base elements and the impurity elements. Hereinafter, numerical limitation ranges and the limitation reasons of the optional elements will be described. Here, the described % is mass %.


Ti: 0.001% to 0.2%


Nb: 0.001% to 0.2%


B: 0.001% to 0.005%


Ti (titanium), Nb (niobium), and B (boron) are the optional elements which form fine carbon-nitrides by fixing the carbon and the nitrogen in the steel, and which have the effects such as precipitation strengthening, microstructure control, or grain refinement strengthening for the steel. Accordingly, as necessary, at least one of Ti, Nb, and B may be added to the steel. In order to obtain the effects, preferably, Ti content may be 0.001% or more, Nb content may be 0.001% or more, and B content may be 0.0001% or more. However, when the optional elements are excessively added to the steel, the effects may be saturated, the control of the crystal orientation may be difficult because of suppression of recrystallization after the hot-rolling, and the workability (deformability) of the steel sheet may deteriorate. Accordingly, preferably, the Ti content may be 0.2% or less, the Nb content may be 0.2% or less, and the B content may be 0.005% or less. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. Moreover, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


Mg: 0.0001% to 0.01%


REM: 0.0001% to 0.1%


Ca: 0.0001% to 0.01%


Ma (magnesium), REM (Rare Earth Metal), and Ca (calcium) are the optional elements which are important to control inclusions to be harmless shapes and to improve the local deformability of the steel sheet. Accordingly, as necessary, at least one of Mg, REM, and Ca may be added to the steel. In order to obtain the effects, preferably, Mg content may be 0.0001% or more, REM content may be 0.0001% or more, and Ca content may be 0.0001% or more. On the other hand, when the optional elements are excessively added to the steel, inclusions having stretched shapes may be formed, and the deformability of the steel sheet may be decreased. Accordingly, preferably, the Mg content may be 0.01% or less, the REM content may be 0.1% or less, and the Ca content may be 0.01% or less. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. Moreover, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


In addition, here, the REM represents collectively a total of 16 elements which are 15 elements from lanthanum with atomic number 57 to lutetium with atomic number 71 in addition to scandium with atomic number 21. In general, REM is supplied in the state of misch metal which is a mixture of the elements, and is added to the steel.


Mo: 0.001% to 1.0%


Cr: 0.001% to 2.0%


Ni: 0.001% to 2.0%


W: 0.001% to 1.0%


Zr: 0.0001% to 0.2%


As: 0.0001% to 0.5%


Mo (molybdenum), Cr (chromium), Ni (nickel), W (tungsten), Zr (zirconium), and As (arsenic) are the optional elements which increase the mechanical strength of the steel sheet. Accordingly, as necessary, at least one of Mo, Cr, Ni, W, Zr, and As may be added to the steel. In order to obtain the effects, preferably, Mo content may be 0.001% or more, Cr content may be 0.001% or more, Ni content may be 0.001% or more, W content may be 0.001% or more, Zr content may be 0.0001% or more, and As content may be 0.0001% or more. However, when the optional elements are excessively added to the steel, the deformability of the steel sheet may be decreased. Accordingly, preferably, the Mo content may be 1.0% or less, the Cr content may be 2.0% or less, the Ni content may be 2.0% or less, the W content may be 1.0% or less, the Zr content may be 0.2% or less, and the As content may be 0.5% or less. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. Moreover, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


V: 0.001% 1.0%


Cu: 0.001% to 2.0%


V (vanadium) and Cu (copper) are the optional elements which is similar to Nb,


Ti, or the like and which have the effect of the precipitation strengthening. In addition, a decrease in the local deformability due to addition of V and Cu is small as compared with that of addition of Nb, Ti, or the like. Accordingly, in order to obtain the high-strength and to further increase the local deformability such as the hole expansibility or the bendability, V and Cu are more effective optional elements than Nb, Ti, or the like. Therefore, as necessary, at least one of V and Cu may be added to the steel. In order to obtain the effects, preferably, V content may be 0.001% or more and Cu content may be 0.001% or more. However, the optional elements are excessively added to the steel, the deformability of the steel sheet may be decreased. Accordingly, preferably, the V content may be 1.0% or less and the Cu content may be 2.0% or less. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. In addition, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


Co: 0.0001% to 1.0%


Although it is difficult to quantitatively show the effects, Co (cobalt) is the optional element which significantly increases the temperature Ar3 at which the transformation starts from y (austenite) to a (ferrite) at the cooling of the steel. Accordingly, Ar3 of the steel may be controlled by the Co content. In addition, Co is the optional element which improves the strength of the steel sheet. In order to obtain the effect, preferably, the Co content may be 0.0001% or more. However, when Co is excessively added to the steel, the weldability of the steel sheet may deteriorate, and the deformability of the steel sheet may be decreased. Accordingly, preferably, the Co content may be 1.0% or less. Moreover, even when the optional element having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. In addition, since it is not necessary to add the optional element to the steel intentionally in order to reduce costs of alloy, a lower limit of an amount of the optional element may be 0%.


Sn: 0.0001% to 0.2%


Pb: 0.0001% to 0.2%


Sn (tin) and Pb (lead) are the optional elements which are effective in an improvement of coating wettability and coating adhesion. Accordingly, as necessary, at least one of Sn and Pb may be added to the steel. In order to obtain the effects, preferably, Sn content may be 0.0001% or more and Pb content may be 0.0001% or more. However, when the optional elements are excessively added to the steel, the cracks may occur during the hot working due to high-temperature embrittlement, and surface dents tend to be made on the steel sheet. Accordingly, preferably, the Sn content may be 0.2% or less and the Pb content may be 0.2% or less. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. In addition, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


Y: 0.0001% to 0.2%


Hf: 0.0001% to 0.2%


Y (yttrium) and Hf (hafnium) are the optional elements which are effective in an improvement of corrosion resistance of the steel sheet. Accordingly, as necessary, at least one of Y and Hf may be added to the steel. In order to obtain the effect, preferably, Y content may be 0.0001% or more and Hf content may be 0.0001% or more. However, when the optional elements are excessively added to the steel, the local deformability such as the hole expansibility may be decreased. Accordingly, preferably, the Y content may be 0.20% or less and the Hf content may be 0.20% or less. Moreover, Y has the effect which forms oxides in the steel and which adsorbs hydrogen in the steel. Accordingly, diffusible hydrogen in the steel is decreased, and an improvement in hydrogen embrittlement resistance properties in the steel sheet can be expected. The effect can be also obtained within the above-described range of the Y content. Moreover, even when the optional elements having the amount less than the lower limit are included in the steel, the effects in the embodiment are not decreased. In addition, since it is not necessary to add the optional elements to the steel intentionally in order to reduce costs of alloy, lower limits of amounts of the optional elements may be 0%.


As described above, the hot-rolled steel sheet according to the embodiment has the chemical composition which includes the above-described base elements and the balance consisting of Fe and unavoidable impurities, or has the chemical composition which includes the above-described base elements, at least one selected from the group consisting of the above-described optional elements, and the balance consisting of Fe and unavoidable impurities.


Moreover, surface treatment may be conducted on the hot-rolled steel sheet according to the embodiment. For example, the surface treatment such as electro coating, hot dip coating, evaporation coating, alloying treatment after coating, organic film formation, film laminating, organic salt and inorganic salt treatment, or non-chrome treatment (non-chromate treatment) may be applied, and thus, the hot-rolled steel sheet may include various kinds of the film (film or coating). For example, a galvanized layer or a galvannealed layer may be arranged on the surface of the hot-rolled steel sheet. Even if the hot-rolled steel sheet includes the above-described coating, the steel sheet can obtain the high-strength and can sufficiently secure the uniform deformability and the local deformability.


Moreover, in the embodiment, a thickness of the hot-rolled steel sheet is not particularly limited. However, for example, the thickness may be 1.5 mm to 10 mm, and may be 2.0 mm to 10 mm. Moreover, the strength of the hot-rolled steel sheet is not particularly limited, and for example, the tensile strength may be 440 MPa to 1500 MPa.


The hot-rolled steel sheet according to the embodiment can be applied to general use for the high-strength steel sheet, and has the excellent uniform deformability and the remarkably improved local deformability such as the bending workability or the hole expansibility of the high-strength steel sheet.


In addition, since the directions in which the bending for the hot-rolled steel sheet is conducted differ in the parts which are bent, the direction is not particularly limited. In the hot-rolled steel sheet according to the embodiment, the similar properties can be obtained in any bending direction, and the hot-rolled steel sheet can be subjected to the composite forming including working modes such as bending, stretching, or drawing.


Next, a method for producing the hot-rolled steel sheet according to an embodiment of the present invention will be described. In order to produce the hot-rolled steel sheet which has the high-strength, the excellent uniform deformability, and the excellent local deformability, it is important to control the chemical composition of the steel, the metallographic structure, and the texture which is represented by the pole densities of each orientation of a specific crystal orientation group. The details will be described below.


The production process prior to the hot-rolling is not particularly limited. For example, the steel (molten steel) may be obtained by conducting a smelting and a refining using a blast furnace, an electric furnace, a converter, or the like, and subsequently, by conducting various kinds of secondary refining, in order to melt the steel satisfying the chemical composition. Thereafter, in order to obtain a steel piece or a slab from the steel, for example, the steel can be cast by a casting process such as a continuous casting process, an ingot making process, or a thin slab casting process in general. In the case of the continuous casting, the steel may be subjected to the hot-rolling after the steel is cooled once to a lower temperature (for example, room temperature) and is reheated, or the steel (cast slab) may be continuously subjected to the hot-rolling just after the steel is cast. In addition, scrap may be used for a raw material of the steel (molten steel).


In order to obtain the high-strength steel sheet which has the high-strength, the excellent uniform deformability, and the excellent local deformability, the following conditions may be satisfied. Moreover, hereinafter, the “steel” and the “steel sheet” are synonymous.


First-Hot-Rolling Process


In the first-hot-rolling process, using the molten and cast steel piece, a rolling pass whose reduction is 40% or more is conducted at least once in a temperature range of 1000° C. to 1200° C. (preferably, 1150° C. or lower). By conducting the first-hot-rolling under the conditions, the average grain size of the austenite of the steel sheet after the first-hot-rolling process is controlled to 200 μm or less, which contributes to the improvement in the uniform deformability and the local deformability of the finally obtained hot-rolled steel sheet.


The austenite grains are refined with an increase in the reduction and an increase in the frequency of the rolling. For example, in the first-hot-rolling process, by conducting at least two times (two passes) of the rolling whose reduction is 40% or more per one pass, the average grain size of the austenite may be preferably controlled to 100 or less. In addition, in the first-hot-rolling, by limiting the reduction to 70% or less per one pass, or by limiting the frequency of the rolling (the number of times of passes) to 10 times or less, a temperature fall of the steel sheet or excessive formation of scales may can be decreased. Accordingly, in the rough rolling, the reduction per one pass may be 70% or less, and the frequency of the rolling (the number of times of passes) may be 10 times or less.


As described above, by refining the austenite grains after the first-hot-rolling process, it is preferable that the austenite grains can be further refined by the post processes, and the ferrite, the bainite, and the martensite transformed from the austenite at the post processes may be finely and uniformly dispersed. As a result, the anisotropy and the local deformability of the steel sheet are improved due to the fact that the texture is controlled, and the uniform deformability and the local deformability (particularly, uniform deformability) of the steel sheet are improved due to the fact that the metallographic structure is refined. Moreover, it seems that the grain boundary of the austenite refined by the first-hot-rolling process acts as one of recrystallization nuclei during a second-hot-rolling process which is the post process.


In order to inspect the average grain size of the austenite after the first-hot-rolling process, it is preferable that the steel sheet after the first-hot-rolling process is rapidly cooled at a cooling rate as fast as possible. For example, the steel sheet is cooled under the average cooling rate of 10° C./second or faster. Subsequently, the cross-section of the sheet piece which is taken from the steel sheet obtained by the cooling is etched in order to make the austenite grain boundary visible, and the austenite grain boundary in the microstructure is observed by an optical microscope. At the time, visual fields of 20 or more are observed at a magnification of 50-fold or more, the grain size of the austenite is measured by the image analysis or the intercept method, and the average grain size of the austenite is obtained by averaging the austenite grain sizes measured at each of the visual fields.


After the first-hot-rolling process, sheet bars may be joined, and the second-hot-rolling process which is the post process may be continuously conducted.


At the time, the sheet bars may be joined after a rough bar is temporarily coiled in a coil shape, stored in a cover having a heater as necessary, and recoiled again.


Second-Hot-Rolling Process


In the second-hot-rolling process, when a temperature calculated by a following Expression 4 is defined as T1 in unit of ° C., the steel sheet after the first-hot-rolling process is subjected to a rolling under conditions such that, a large reduction pass whose reduction is 30% or more in a temperature range of T1+30° C. to T1+200° C. is included, a cumulative reduction in the temperature range of T1+30° C. to T1+200° C. is 50% or more, a cumulative reduction in a temperature range of Ar3° C. to lower than T1+30° C. is limited to 30% or less, and a rolling finish temperature is Ar3° C. or higher.


As one of the conditions in order to control the average pole density D1 of the orientation group of {100}<011> to {223}<110> and the pole density D2 of the crystal orientation {332}<113> in the thickness central portion which is the thickness range of ⅝ to ⅜ to the above-described ranges, in the second-hot-rolling process, the rolling is controlled based on the temperature T1 (unit: ° C.) which is determined by the following Expression 4 using the chemical composition (unit: mass %) of the steel.

T1=850+10×([C]+[N])×[Mn]+350×[Nb]+250×[Ti]+40×[B]+10×[Cr]+100×[Mo]+100×[V]  (Expression 4)


In Expression 4, [C], [N], [Mn], [Nb], [Ti], [B], [Cr], [Mo], and [V] represent mass percentages of C, N, Mn, Nb, Ti, B, Cr, Mo, and V respectively.


The amount of the chemical element, which is included in Expression 4 but is not included in the steel, is regarded as 0% for the calculation. Accordingly, in the case of the chemical composition in which the steel includes only the base elements, a following Expression 5 may be used instead of the Expression 4.

T1=850+10×([C]+[N])×[Mn]  (Expression 5)


In addition, in the chemical composition in which the steel includes the optional elements, the temperature calculated by Expression 4 may be used for T1 (unit: ° C.), instead of the temperature calculated by Expression 5.


In the second-hot-rolling process, on the basis of the temperature T1 (unit: ° C.) obtained by the Expression 4 or 5, the large reduction is included in the temperature range of T1+30° C. to T1+200° C. (preferably, in a temperature range of T1+50° C. to T1+100° C.), and the reduction is limited to a small range (includes 0%) in the temperature range of Ar3° C. to lower than T1+30° C. By conducting the second-hot-rolling process in addition to the first-hot-rolling process, the uniform deformability and the local deformability of the steel sheet is preferably improved. Particularly, by including the large reduction in the temperature range of T1+30° C. to T1+200° C. and by limiting the reduction in the temperature range of Ar3° C. to lower than T1+30° C., the average pole density D1 of the orientation group of {100}<011> to {223}<110> and the pole density D2 of the crystal orientation {332}<113> in the thickness central portion which is the thickness range of ⅝ to ⅜ are sufficiently controlled, and as a result, the anisotropy and the local deformability of the steel sheet are remarkably improved.


The temperature T1 itself is empirically obtained. It is empirically found by the inventors through experiments that the temperature range in which the recrystallization in the austenite range of each steels is promoted can be determined based on the temperature T1. In order to obtain the excellent uniform deformability and the excellent local deformability, it is important to accumulate a large amount of the strain by the rolling and to obtain the fine recrystallized grains. Accordingly, the rolling having plural passes is conducted in the temperature range of T1+30° C. to T1+200° C., and the cumulative reduction is to be 50% or more. Moreover, in order to further promote the recrystallization by the strain accumulation, it is preferable that the cumulative reduction is 70% or more. Moreover, by limiting an upper limit of the cumulative reduction, a rolling temperature can be sufficiently held, and a rolling load can be further suppressed. Accordingly, the cumulative reduction may be 90% or less.


When the rolling having the plural passes is conducted in the temperature range of T1+30° C. to T1+200° C., the strain is accumulated by the rolling, and the recrystallization of the austenite is occurred at an interval between the rolling passes by a driving force derived from the accumulated strain. Specifically, by conducting the rolling having the plural passes in the temperature range of T1+30° C. to T1+200° C., the recrystallization is repeatedly occurred every pass. Accordingly, it is possible to obtain the recrystallized austenite structure which is uniform, fine, and equiaxial. In the temperature range, dynamic recrystallization is not occurred during the rolling, the strain is accumulated in the crystal, and static recrystallization is occurred at the interval between the rolling passes by the driving force derived from the accumulated strain. In general, in dynamic-recrystallized structure, the strain which introduced during the working is accumulated in the crystal thereof, and a recrystallized area and a non-crystallized area are locally mixed. Accordingly, the texture is comparatively developed, and thus, the anisotropy appears. Moreover, the metallographic structures may be a duplex grain structure. In the method for producing the hot-rolled steel sheet according to the embodiment, the austenite is recrystallized by the static recrystallization. Accordingly, it is possible to obtain the recrystallized austenite structure which is uniform, fine, and equiaxial, and in which the development of the texture is suppressed.


In order to increase the homogeneity, and to preferably increase the uniform deformability and the local deformability of the steel sheet, the second-hot-rolling is controlled so as to include at least one large reduction pass whose reduction per one pass is 30% or more in the temperature range of T1+30° C. to T1+200° C. In the second-hot-rolling, in the temperature range of T1+30° C. to T1+200° C., the rolling whose reduction per one pass is 30% or more is conducted at least once. Particularly, considering a cooling process as described below, the reduction of a final pass in the temperature range may be preferably 25% or more, and may be more preferably 30% or more. Specifically, it is preferable that the final pass in the temperature range is the large reduction pass (the rolling pass with the reduction of 30% or more). In a case that the further excellent deformability is required in the steel sheet, it is further preferable that all reduction of first half passes are less than 30% and the reductions of the final two passes are individually 30% or more. In order to more preferably increase the homogeneity of the steel sheet, a large reduction pass whose reduction per one pass is 40% or more may be conducted. Moreover, in order to obtain a more excellent shape of the steel sheet, a large reduction pass whose reduction per one pass is 70% or less may be conducted.


Moreover, in the rolling in the temperature range of T1+30° C. to T1+200° C., by suppressing a temperature rise of the steel sheet between passes of the rolling to 18° C. or lower, it is possible to preferably obtain the recrystallized austenite which is more uniform.


In order to suppress the development of the texture and to keep the equiaxial recrystallized structure, after the rolling in the temperature range of T1+30° C. to T1+200° C., an amount of working in the temperature range of Ar3° C. to lower than T1+30° C. (preferably, T1 to lower than T1+30° C.) is suppressed as small as possible. Accordingly, the cumulative reduction in the temperature range of Ar3° C. to lower than T1+30° C. is limited to 30% or less. In the temperature range, it is preferable that the cumulative reduction is 10% or more in order to obtain the excellent shape of the steel sheet, and it is preferable that the cumulative reduction is 10% or less in order to further improve the anisotropy and the local deformability. In the case, the cumulative reduction may be more preferably 0%. Specifically, in the temperature range of Ar3° C. to lower than T1+30° C., the rolling may not be conducted, and the cumulative reduction is to be 30% or less even when the rolling is conducted.


When the cumulative reduction in the temperature range of Ar3° C. to lower than T1+30° C. is large, the shape of the austenite grain recrystallized in the temperature range of T1+30° C. to T1+200° C. is not to be equiaxial due to the fact that the grain is stretched by the rolling, and the texture is developed again due to the fact that the strain is accumulated by the rolling. Specifically, as the production conditions according to the embodiment, the rolling is controlled at both of the temperature range of T1+30° C. to T1+200° C. and the temperature range of Ar3° C. to lower than T1+30° C. in the second-hot-rolling process. As a result, the austenite is recrystallized so as to be uniform, fine, and equiaxial, the texture, the metallographic structure, and the anisotropy of the steel sheet are controlled, and therefore, the uniform deformability and the local deformability can be improved. In addition, the austenite is recrystallized so as to be uniform, fine, and equiaxial, and therefore, the ratio of major axis to minor axis of the martensite, the average size of the martensite, the average distance between the martensite, and the like of the finally obtained hot-rolled steel sheet can be controlled.


In the second-hot-rolling process, when the rolling is conducted in the temperature range lower than Ar3° C. or the cumulative reduction in the temperature range of Ar3° C. to lower than T1+30° C. is excessive large, the texture of the austenite is developed. As a result, the finally obtained hot-rolled steel sheet does not satisfy at least one of the condition in which the average pole density D1 of the orientation group of {100}<011> to {223}<110> is 1.0 to 5.0 and the condition in which the pole density D2 of the crystal orientation {332}<113> is 1.0 to 4.0 in the thickness central portion. On the other hand, in the second-hot-rolling process, when the rolling is conducted in the temperature range higher than T1+200° C. or the cumulative reduction in the temperature range of T1+30° C. to T1+200° C. is excessive small, the recrystallization is not uniformly and finely occurred, coarse grains or mixed grains may be included in the metallographic structure, and the metallographic structure may be the duplex grain structure. Accordingly, the area fraction or the volume average diameter of the grains which is more than 35 μm is increased.


Moreover, when the second-hot-rolling is finished at a temperature lower than Ar3 (unit: ° C.), the steel is rolled in a temperature range of the rolling finish temperature to lower than Ar3 (unit: ° C.) which is a range where two phases of the austenite and the ferrite exist (two-phase temperature range). Accordingly, the texture of the steel sheet is developed, and the anisotropy and the local deformability of the steel sheet significantly deteriorate. Here, when the rolling finish temperature of the second-hot-rolling is Tl or more, the anisotropy may be further decreased by decreasing an amount of the strain in the temperature range lower than T1, and as a result, the local deformability may be further increased. Therefore, the rolling finish temperature of the second-hot-rolling may be T1 or more.


Here, the reduction can be obtained by measurements or calculations from a rolling force, a thickness, or the like. Moreover, the rolling temperature (for example, the above each temperature range) can be obtained by measurements using a thermometer between stands, by calculations using a simulation in consideration of deformation heating, line speed, the reduction, or the like, or by both (measurements and calculations). Moreover, the above reduction per one pass is a percentage of a reduced thickness per one pass (a difference between an inlet thickness before passing a rolling stand and an outlet thickness after passing the rolling stand) to the inlet thickness before passing the rolling stand. The cumulative reduction is a percentage of a cumulatively reduced thickness (a difference between an inlet thickness before a first pass in the rolling in each temperature range and an outlet thickness after a final pass in the rolling in each temperature range) to the reference which is the inlet thickness before the first pass in the rolling in each temperature range. Ar3, which is a ferritic transformation temperature from the austenite during the cooling, is obtained by a following Expression 6 in unit of ° C. Moreover, although it is difficult to quantitatively show the effects as described above, Al and Co also influence Ar3.

Ar3=879.4−516.1×[C]−65.7×[Mn]+38.0×[Si]+274.7×[P]   (Expression 6)


In the Expression 6, [C], [Mn], [Si] and [P] represent mass percentages of C, Mn, Si and P respectively.


First-Cooling Process


In the first-cooling process, after a final pass among the large reduction passes whose reduction per one pass is 30% or more in the temperature range of T1+30° C. to T1+200° C. is finished, when a waiting time from the finish of the final pass to a start of the cooling is defined as t in unit of second, the steel sheet is subjected to the cooling so that the waiting time t satisfies a following Expression 7. Here, t1 in the Expression 7 can be obtained from a following Expression 8. In the Expression 8, Tf represents a temperature (unit: ° C.) of the steel sheet at the finish of the final pass among the large reduction passes, and P1 represents a reduction (unit: %) at the final pass among the large reduction passes.

T≤2.5×t1  (Expression 7)
t1=0.001×((Tf−T1)×P1/100)2−0.109×((Tf−T1)×P1/100)+3.1   (Expression 8)


The first-cooling after the final large reduction pass significantly influences the grain size of the finally obtained hot-rolled steel sheet. Moreover, by the first-cooling, the austenite can be controlled to be a metallographic structure in which the grains are equiaxial and the coarse grains rarely are included (namely, uniform sizes). Accordingly, the finally obtained hot-rolled steel sheet has the metallographic structure in which the grains are equiaxial and the coarse grains rarely are included (namely, uniform sizes), and the ratio of the major axis to the minor axis of the martensite, the average size of the martensite, the average distance between the martensite, and the like may be preferably controlled.


The right side value (2.5×t1) of the Expression 7 represents a time at which the recrystallization of the austenite is substantially finished. When the waiting time t is more than the right side value (2.5×t1) of the Expression 7, the recrystallized grains are significantly grown, and the grain size is increased. Accordingly, the strength, the uniform deformability, the local deformability, the fatigue properties, or the like of the steel sheet are decreased. Therefore, the waiting time t is to be 2.5×t1 seconds or less. In a case where runnability (for example, shape straightening or controllability of a second-cooling) is considered, the first-cooling may be conducted between rolling stands. Moreover, a lower limit of the waiting time t is to be 0 seconds or more.


Moreover, when the waiting time t is limited to 0 second to shorter than t1 seconds so that 0≤t<t1 is satisfied, it may be possible to significantly suppress the grain growth. In the case, the volume average diameter of the finally obtained hot-rolled steel sheet may be controlled to 30 μm or less. As a result, even if the recrystallization of the austenite does not sufficiently progress, the properties of the steel sheet, particularly, the uniform deformability, the fatigue properties, or the like may be preferably improved.


Moreover, when the waiting time t is limited to t1 seconds to 2.5×t1 seconds so that t1≤t≤2.5×t1 is satisfied, it may be possible to suppress the development of the texture. In the case, although the volume average diameter may be increased because the waiting time t is prolonged as compared with the case where the waiting time t is shorter than t1 seconds, the crystal orientation may be randomized because the recrystallization of the austenite sufficiently progresses. As a result, the anisotropy, the local deformability, and the like of the steel sheet may be preferably improved.


Moreover, the above-described first-cooling may be conducted at an interval between the rolling stands in the temperature range of T1+30° C. to T1+200° C., or may be conducted after a final rolling stand in the temperature range. Specifically, as long as the waiting time t satisfies the condition, a rolling whose reduction per one pass is 30% or less may be further conducted in the temperature range of T1+30° C. to T1+200° C. and between the finish of the final pass among the large reduction passes and the start of the first-cooling. Moreover, after the first-cooling is conducted, as long as the reduction per one pass is 30% or less, the rolling may be further conducted in the temperature range of T1+30° C. to T1+200° C. Similarly, after the first-cooling is conducted, as long as the cumulative reduction is 30% or less, the rolling may be further conducted in the temperature range of Ar3° C. to T1+30° C. (or Ar3° C. to Tf ° C.). As described above, as long as the waiting time t after the large reduction pass satisfies the condition, in order to control the metallographic structure of the finally obtained hot-rolled steel sheet, the above-described first-cooling may be conducted either at the interval between the rolling stands or after the rolling stand.


In the first-cooling, it is preferable that a cooling temperature change which is a difference between a steel sheet temperature (steel temperature) at the cooling start and a steel sheet temperature (steel temperature) at the cooling finish is 40° C. to 140° C. When the cooling temperature change is 40° C. or higher, the growth of the recrystallized austenite grains may be further suppressed. When the cooling temperature change is 140° C. or lower, the recrystallization may more sufficiently progress, and the pole density may be preferably improved. Moreover, by limiting the cooling temperature change to 140° C. or lower, in addition to the comparatively easy control of the temperature of the steel sheet, variant selection (variant limitation) may be more effectively controlled, and the development of the recrystallized texture may be preferably controlled. Accordingly, in the case, the isotropy may be further increased, and the orientation dependence of the formability may be further decreased. When the cooling temperature change is higher than 140° C., the progress of the recrystallization may be insufficient, the intended texture may not be obtained, the ferrite may not be easily obtained, and the hardness of the obtained ferrite is increased. Accordingly, the uniform deformability and the local deformability of the steel sheet may be decreased.


Moreover, it is preferable that the steel sheet temperature T2 at the first-cooling finish is T1+100° C. or lower. When the steel sheet temperature T2 at the first-cooling finish is T1+100° C. or lower, more sufficient cooling effects are obtained. By the cooling effects, the grain growth may be suppressed, and the growth of the austenite grains may be further suppressed.


Moreover, it is preferable that an average cooling rate in the first-cooling is 50° C./second or faster. When the average cooling rate in the first-cooling is 50° C./second or faster, the growth of the recrystallized austenite grains may be further suppressed. On the other hand, it is not particularly necessary to prescribe an upper limit of the average cooling rate. However, from a viewpoint of the sheet shape, the average cooling rate may be 200° C./second or slower.


Second-Cooling Process


In the second-cooling process, the steel sheet after the second-hot-rolling and after the first-cooling process may be preferably cooled to a temperature range of 600° C. to 800° C. under an average cooling rate of 15° C./second to 300° C./second. When a temperature (unit: ° C.) of the steel sheet becomes Ar3 or lower by cooling the steel sheet during the second-cooling process, the martensite starts to be transformed to the ferrite. When the average cooling rate is 15° C./second or faster, grain coarsening of the austenite may be preferably suppressed. It is not particularly necessary to prescribe an upper limit of the average cooling rate. However, from a viewpoint of the sheet shape, the average cooling rate may be 300° C./second or slower. In addition, it is preferable to start the second-cooling within 3 seconds after finishing the second-hot-rolling or after the first-cooling process. When the second-cooling start exceeds 3 seconds, coarsening of the austenite may occur.


Holding Process


In the holding process, the steel sheet after the second-cooling process is held in the temperature range of 600° C. to 800° C. for 1 second to 15 seconds. By holding in the temperature range, the transformation from the austenite to the ferrite progresses, and therefore, the area fraction of the ferrite can be increased. It is preferable that the steel is held in a temperature range of 600° C. to 680° C. By conducting the ferritic transformation in the above comparatively lower temperature range, the ferrite structure may be controlled to be fine and uniform. Accordingly, the bainite and the martensite which are formed in the post process may be controlled to be fine and uniform in the metallographic structure. In addition, in order to accelerate the ferritic transformation, a holding time is to be 1 second or longer. However, when the holding time is longer than 15 seconds, the ferrite grains may be coarsened, and the cementite may precipitate. In a case where the steel is held in the comparatively lower temperature range of 600° C. to 680° C., it is preferable that the holding time is 3 seconds to 15 seconds.


Third-Cooling Process


In the third-cooling process, the steel sheet after the holding process is cooled to a temperature range of a room temperature to 350° C. under an average cooling rate of 50° C./second to 300° C./second. During the third-cooling process, the austenite which is not transformed to the ferrite even after the holding process is transformed to the bainite and the martensite. When the third-cooling process is stopped at a temperature higher than 350° C., the bainitic transformation excessively progresses due to the excessive high temperature, and the martensite of 1% or more in unit of area % cannot be finally obtained. Moreover, it is not particularly necessary to prescribe a lower limit of the cooling stop temperature of the third-cooling process. However, in a case where water cooling is conducted, the lower limit may be the room temperature. In addition, when the average cooling rate is slower than 50° C./second, the pearlitic transformation may occur during the cooling. Moreover, it is not particularly necessary to prescribe an upper limit of the average cooling rate in the third-cooling process. However, from an industrial standpoint, the upper limit may be 300° C./second. By decreasing the average cooling rate within the above-described range of the average cooling rate, the area fraction of the bainite may be increased. On the other hand, by increasing the average cooling rate within the above-described range of the average cooling rate, the area fraction of the martensite may be increased. In addition, the grain sizes of the bainite and the martensite are also refined.


In accordance with properties required for the hot-rolled steel sheet, the area fractions of the ferrite and the bainite which are the primary phase may be controlled, and the area fraction of the martensite which is the second phase may be controlled. As described above, the ferrite can be mainly controlled in the holding process, and the bainite and the martensite can be mainly controlled in the third-cooling process. In addition, the grain sizes or the morphologies of the ferrite and the bainite which are the primary phase and of the martensite which is the secondary phase significantly depend on the grain size or the morphology of the austenite which is the microstructure before the transformation. Moreover, the grain sizes or the morphologies also depend on the holding process and the third-cooling process. Accordingly, for example, the value of TS/fM×dis/dia, which is the relationship of the area fraction fM of the martensite, the average size dia of the martensite, the average distance dis between the martensite, and the tensile strength TS of the steel sheet, may be satisfied by multiply controlling the above-described production processes.


Coiling Process


In the coiling process, the steel sheet after the third-cooling starts to be coiled at a temperature of the room temperature to 350° C. which is the cooling stop temperature of the third-cooling, and the steel sheet is air-cooled. As described above, the hot-rolled steel sheet according to the embodiment can be produced.


Moreover, as necessary, the obtained hot-rolled steel sheet may be subjected to a skin pass rolling. By the skin pass rolling, it may be possible to suppress a stretcher strain which is formed during working of the steel sheet, or to straighten the shape of the steel sheet.


Moreover, the obtained hot-rolled steel sheet may be subjected to a surface treatment. For example, the surface treatment such as the electro coating, the hot dip coating, the evaporation coating, the alloying treatment after the coating, the organic film formation, the film laminating, the organic salt and inorganic salt treatment, or the non-chromate treatment may be applied to the obtained hot-rolled steel sheet. For example, a galvanized layer or a galvannealed layer may be arranged on the surface of the hot-rolled steel sheet. Even if the surface treatment is conducted, the uniform deformability and the local deformability are sufficiently maintained.


Moreover, as necessary, a tempering treatment or an ageing treatment may be conducted as a reheating treatment. By the treatment, Nb, Ti, Zr, V, W, Mo, or the like which is solid-soluted in the steel may be precipitated as carbides, and the martensite may be softened as the tempered martensite. As a result, the hardness difference between the ferrite and the bainite which are the primary phase and the martensite which is the secondary phase is decreased, and the local deformability such as the hole expansibility or the bendability is improved. The effects of the reheating treatment may be also obtained by heating for the hot dip coating, the alloying treatment, or the like.


EXAMPLE

Hereinafter, the technical features of the aspect of the present invention will be described in detail with reference to the following examples. However, the condition in the examples is an example condition employed to confirm the operability and the effects of the present invention, and therefore, the present invention is not limited to the example condition. The present invention can employ various conditions as long as the conditions do not depart from the scope of the present invention and can achieve the object of the present invention.


Steels S1 to S98 including chemical compositions (the balance consists of Fe and unavoidable impurities) shown in Tables 1 to 6 were examined, and the results are described. After the steels were melt and cast, or after the steels were cooled once to the room temperature, the steels were reheated to the temperature range of 900° C. to 1300° C. Thereafter, the hot-rolling and the temperature control (cooling, holding, or the like) were conducted under production conditions shown in Tables 7 to 14, and hot-rolled steel sheets having the thicknesses of 2 to 5 mm were obtained.


In Tables 15 to 22, the characteristics such as the metallographic structure, the texture, or the mechanical properties are shown. Moreover, in Tables, the average pole density of the orientation group of {100}<011> to {223}<110> is shown as D1 and the pole density of the crystal orientation {332}<113> is shown as D2. In addition, the area fractions of the ferrite, the bainite, the martensite, the pearlite, and the residual austenite are shown as F, B, fM, P, and y respectively. Moreover, the average size of the martensite is shown as dia, and the average distance between the martensite is shown as dis. Moreover, in Tables, the standard deviation ratio of hardness represents a value dividing the standard deviation of the hardness by the average of the hardness with respect to the phase having higher area fraction among the ferrite and the bainite.


As a parameter of the local deformability, the hole expansion ratio λ and the critical bend radius (d/RmC) by 90° V-shape bending of the final product were used. The bending test was conducted to C-direction bending. Moreover, the tensile test (measurement of TS, u-EL and EL), the bending test, and the hole expansion test were respectively conducted based on JIS Z 2241, JIS Z 2248 (V block 90° bending test) and Japan Iron and Steel Federation Standard JFS T1001. Moreover, by using the above-described EBSD, the pole densities were measured by a measurement step of 0.5 μm in the thickness central portion which was the range of ⅝ to ⅜ of the thickness-cross-section (the normal vector thereof corresponded to the normal direction) which was parallel to the rolling direction at ¼ position of the transverse direction. Moreover, the r values (Lankford-values) of each direction were measured based on JIS Z 2254 (2008) (ISO 10113 (2006)). Moreover, the underlined value in the Tables indicates out of the range of the present invention, and the blank column indicates that no alloying element was intentionally added.


Production Nos. P1, P2, P7, P10, P11, P13, P14, P16 to P19, P21, P23 to P27, P29 to P31, P33, P34, P36 to P41, P48 to P77, and P141 to P180 are the examples which satisfy the conditions of the present invention. In the examples, since all conditions of TS≥440 (unit: MPa), TS×u-EL 7000 (unit: MPa·%), TS×λ≥30000 (unit: MPa·%), and d/RmC≥1 (no unit) were simultaneously satisfied, it can be said that the hot-rolled steel sheets have the high-strength, the excellent uniform deformability, and the excellent local deformability.


On the other hand, P3 to P6, P8, P9, P12, P15, P20, P22, P28, P32, P35, P42 to P47, and P78 to P140 are the comparative examples which do not satisfy the conditions of the present invention. In the comparative examples, at least one condition of TS≥440 (unit: MPa), TS×u-EL 7000 (unit: MPa·%), TS×λ≥30000 (unit: MPa·%), and d/RmC≥1 (no unit) was not satisfied.


In regard to the examples and the comparative examples, the relationship between D1 and d/RmC is shown in FIG. 1, and the relationship between D2 and d RmC is shown in FIG. 2. As shown in FIG. 1 and FIG. 2, when D1 is 5.0 or less and when D2 is 4.0 or less, d/RmC≥1 is satisfied.


[Table 1]


[Table 2]


[Table 3]


[Table 4]


[Table 5]


[Table 6]


[Table 7]


[Table 8]


[Table 9]


[Table 10]


[Table 11]


[Table 12]


[Table 13]


[Table 14]


[Table 16]


[Table 17]


[Table 18]


[Table 19]


[Table 20]


[Table 21]


[Table 22]


INDUSTRIAL APPLICABILITY

According to the above aspects of the present invention, it is possible to obtain the hot-rolled steel sheet which simultaneously has the high-strength, the excellent uniform deformability, and the excellent local deformability. Accordingly, the present invention has significant industrial applicability.










TABLE 1







STEEL
CHEMICAL COMPOSITION/mass %






















No.
C
Si
Mn
Al
P
S
N
O
Mo
Cr
Ni
Cu
B
Nb
Ti





S1
0.070
0.080
1.300
0.040
0.015
0.004
0.0026
0.0032









S2
0.078
0.070
1.230
0.026
0.011
0.003
0.0046
0.0038




0.0050


S3
0.080
0.310
1.350
0.016
0.012
0.005
0.0032
0.0023





0.040


S4
0.084
0.360
1.310
0.021
0.013
0.004
0.0038
0.0022





0.041


S5
0.061
0.870
1.200
0.038
0.009
0.004
0.0030
0.0029





0.025


S6
0.060
0.300
1.220
0.500
0.009
0.003
0.0033
0.0026





0.021


S7
0.210
0.150
1.620
0.026
0.012
0.003
0.0033
0.0021
0.029
0.344


0.0025

0.021


S8
0.208
1.200
1.640
0.025
0.010
0.003
0.0036
0.0028
0.030
0.350


0.0022

0.021


S9
0.035
0.670
1.880
0.045
0.015
0.003
0.0028
0.0029





0.021


S10
0.034
0.720
1.810
0.035
0.011
0.002
0.0027
0.0033





0.020
0.100


S11
0.180
0.480
2.720
0.050
0.009
0.003
0.0036
0.0022
0.107


S12
0.187
0.550
2.810
0.044
0.011
0.003
0.0034
0.0032
0.100




0.050


S13
0.060
0.110
2.120
0.033
0.010
0.005
0.0028
0.0035




0.0011
0.089
0.036


S14
0.064
0.200
2.180
0.023
0.010
0.004
0.0048
0.0039




0.0012
0.036
0.089


S15
0.040
0.130
1.330
0.038
0.010
0.005
0.0032
0.0026




0.0010
0.120
0.042


S16
0.044
0.133
1.410
0.028
0.010
0.005
0.0038
0.0029




0.0009
0.121
0.040


S17
0.280
1.200
0.900
0.045
0.008
0.003
0.0028
0.0029


S18
0.260
2.300
0.900
0.045
0.008
0.003
0.0028
0.0022


S19
0.060
0.300
1.300
0.030
0.080
0.002
0.0032
0.0022


S20
0.200
0.210
1.300
1.400
0.010
0.002
0.0032
0.0035


S21
0.035
0.021
1.300
0.035
0.010
0.002
0.0023
0.0033






0.120


S22
0.350
0.520
1.330
0.045

0.260

0.003
0.0026
0.0019


S23
0.072
0.150
1.420
0.036
0.014
0.004
0.0022
0.0025






1.500



S24
0.110
0.230
1.120
0.026
0.021
0.003
0.0025
0.0023


S25
0.250
0.230
1.560
0.034
0.024

0.120

0.0022
0.0023


5.000



S26
0.090

3.000

1.000
0.036
0.008

0.040

0.0035
0.0022


S27
0.070
0.210

5.000

0.033
0.008
0.002
0.0023
0.0036


S28

0.008

0.080
1.331
0.045
0.016
0.007
0.0023
0.0029


S29

0.401

0.079
1.294
0.044
0.011
0.006
0.0024
0.0031


S30
0.070
0.0009
1.279
0.042
0.016
0.006
0.0021
0.0030


S31
0.073

2.510

1.264
0.037
0.013
0.008
0.0027
0.0037


S32
0.070
0.076
0.0009
0.042
0.011
0.008
0.0027
0.0029


S33
0.067
0.081
4.010
0.040
0.017
0.005
0.0028
0.0037


























TABLE 2







STEEL












No.
V
W
Ca
Mg
Zr
REM
As
Co
Sn
Pb





S1


S2


S3


S4


0.0020


S5





0.0013


S6





0.0015


S7


S8


S9
0.028

0.0015
0.0021


S10
0.029

0.0014
0.0022


S11
0.100


0.0020


S12
0.090

0.0020
0.0023


S13


S14


S15




0.0010



0.0020


S16





0.0040

0.0030


S17

0.100


S18


S19


S20





0.0030



0.0030


S21






0.0020


S22


S23


S24




0.1500



S25

2.500



S26


S27


S28


S29


S30


S31


S32


S33





















CALCULATED








VALUE OF





T1/

HARDNESS


STEEL No.
Y
Hf
° C.
Ar3/° C.
OF FERRITE/—
REMARKS





S1


851
765
234
EXAMPLE


S2


851
764
231
EXAMPLE


S3


865
764
256
EXAMPLE


S4


866
767
258
EXAMPLE


S5


860
805
266
EXAMPLE


S6


858
782
248
EXAMPLE


S7


865
674
257
EXAMPLE


S8


865
713
289
EXAMPLE


S9


861
767
275
EXAMPLE


S10


886
773
308
EXAMPLE


S11


876
629
274
EXAMPLE


S12


892
622
296
EXAMPLE


S13
0.0040

892
716
294
EXAMPLE


S14

0.0030
886
713
301
EXAMPLE


S15


903
779
284
EXAMPLE


S16


903
772
285
EXAMPLE


S17


853
724
257
EXAMPLE


S18


852
776
290
EXAMPLE


S19


851
796
258
EXAMPLE


S20


853
751
236
EXAMPLE


S21


880
779
268
EXAMPLE


S22


855
703
314
COMPARATIVE EXAMPLE


S23


1376
758
334
COMPARATIVE EXAMPLE


S24


851
764
236
COMPARATIVE EXAMPLE


S25


1154
663
246
COMPARATIVE EXAMPLE


S26


851
883
313
COMPARATIVE EXAMPLE


S27


854
525
313
COMPARATIVE EXAMPLE


S28


850
795
235
COMPARATIVE EXAMPLE


S29


855
594
233
COMPARATIVE EXAMPLE


S30


851
764
231
COMPARATIVE EXAMPLE


S31


851
858
305
COMPARATIVE EXAMPLE


S32


850
849
205
COMPARATIVE EXAMPLE


S33


853
589
291
COMPARATIVE EXAMPLE

















TABLE 3







STEEL
CHEMICAL COMPOSITION/mass %






















No.
C
Si
Mn
Al
P
S
N
O
Mo
Cr
Ni
Cu
B
Nb
Ti





S34
0.070
0.078
1.308
0.0009
0.014
0.008
0.0029
0.0110









S35
0.073
0.077
1.340

2.010

0.012
0.006
0.0021
0.0030


S36
0.068
0.079
1.250
0.042

0.151

0.006
0.0030
0.0034


S37
0.067
0.078
1.255
0.036
0.011

0.031

0.0023
0.0036


S38
0.070
0.082
1.326
0.044
0.017
0.007

0.0110

0.0031


S39
0.069
0.080
1.349
0.042
0.011
0.008
0.0029

0.0110



S40
0.069
0.076
1.334
0.038
0.012
0.005
0.0031
0.0037

1.010



S41
0.072
0.079
1.272
0.036
0.013
0.008
0.0027
0.0035


2.010



S42
0.065
0.084
1.312
0.043
0.014
0.007
0.0028
0.0027



2.010



S43
0.065
0.076
1.286
0.036
0.010
0.008
0.0028
0.0037




2.010



S44
0.068
0.077
1.337
0.037
0.011
0.004
0.0030
0.0032





0.0051



S45
0.067
0.076
1.331
0.039
0.015
0.004
0.0024
0.0037






0.201



S46
0.074
0.077
1.344
0.037
0.010
0.008
0.0023
0.0027







0.201



S47
0.071
0.084
1.350
0.040
0.015
0.008
0.0022
0.0035


S48
0.074
0.077
1.296
0.036
0.015
0.007
0.0025
0.0031


S49
0.071
0.079
1.302
0.044
0.016
0.006
0.0030
0.0030


S50
0.069
0.083
1.337
0.037
0.018
0.006
0.0025
0.0035


S51
0.069
0.084
1.284
0.041
0.019
0.007
0.0030
0.0032


S52
0.070
0.084
1.350
0.040
0.015
0.005
0.0026
0.0035


S53
0.072
0.084
1.342
0.043
0.010
0.006
0.0022
0.0029


S54
0.073
0.081
1.293
0.041
0.016
0.006
0.0026
0.0028


S55
0.070
0.081
1.287
0.044
0.011
0.006
0.0025
0.0031


S56
0.073
0.084
1.275
0.035
0.012
0.007
0.0029
0.0036


S57
0.067
0.084
1.312
0.042
0.014
0.006
0.0023
0.0032


S58
0.072
0.082
1.337
0.040
0.015
0.004
0.0026
0.0028


S59
0.073
0.083
1.320
0.042
0.015
0.004
0.0026
0.0036


1.000


S60
0.070
0.080
1.300
0.040
0.015
0.004
0.0026
0.0035



1.000


S61
0.065
0.080
1.272
0.036
0.012
0.006
0.0028
0.0027
0.0009


S62
0.068
0.076
1.312
0.037
0.013
0.006
0.0030
0.0035
0.030


S63
0.067
0.079
1.286
0.039
0.014
0.008
0.0024
0.0031

0.0009


S64
0.074
0.084
1.337
0.037
0.010
0.008
0.0023
0.0030

0.005


S65
0.071
0.076
1.331
0.040
0.011
0.005
0.0022
0.0035


0.0009


S66
0.074
0.077
1.344
0.036
0.015
0.008
0.0025
0.0032


0.005


























TABLE 4







STEEL












No.
V
W
Ca
Mg
Zr
REM
As
Co
Sn
Pb





S34


S35


S36


S37


S38


S39


S40


S41


S42


S43


S44


S45


S46


S47

1.010



S48


1.010



S49



0.0110



S50




0.0110



S51





0.2010



S52






0.1010



S53







0.5010



S54








1.0100



S55









0.2010



S56










0.2010



S57


S58


S59


S60


S61


S62


S63


S64


S65


S66























CALCULATED









VALUE OF



STEEL


T1/
Ar3/
HARDNESS



No.
Y
Hf
° C.
° C.
OF FERRITE/—
REMARKS







S34


851
764
234
COMPARATIVE EXAMPLE



S35


851
836
234
COMPARATIVE EXAMPLE



S36


851
807
269
COMPARATIVE EXAMPLE



S37


851
768
232
COMPARATIVE EXAMPLE



S38


851
764
235
COMPARATIVE EXAMPLE



S39


851
761
234
COMPARATIVE EXAMPLE



S40


952
762
234
COMPARATIVE EXAMPLE



S41


871
765
232
COMPARATIVE EXAMPLE



S42


851
766
234
COMPARATIVE EXAMPLE



S43


851
767
232
COMPARATIVE EXAMPLE



S44


851
762
233
COMPARATIVE EXAMPLE



S45


921
764
269
COMPARATIVE EXAMPLE



S46


901
758
282
COMPARATIVE EXAMPLE



S47


952
762
235
COMPARATIVE EXAMPLE



S48


851
763
234
COMPARATIVE EXAMPLE



S49


851
765
234
COMPARATIVE EXAMPLE



S50


851
764
235
COMPARATIVE EXAMPLE



S51


851
768
235
COMPARATIVE EXAMPLE



S52


851
762
235
COMPARATIVE EXAMPLE



S53


851
760
233
COMPARATIVE EXAMPLE



S54


851
842
234
COMPARATIVE EXAMPLE



S55


851
765
232
COMPARATIVE EXAMPLE



S56


851
764
232
COMPARATIVE EXAMPLE



S57

0.2010


851
766
234
COMPARATIVE EXAMPLE



S58


0.2010

851
762
235
COMPARATIVE EXAMPLE



S59


851
762
234
EXAMPLE



S60


851
765
234
EXAMPLE



S61


851
769
232
EXAMPLE



S62


854
764
233
EXAMPLE



S63


851
767
233
EXAMPLE



S64


851
759
233
EXAMPLE



S65


851
761
233
EXAMPLE



S66


851
760
234
EXAMPLE


















TABLE 5







STEEL
CHEMICAL COMPOSITION/mass %






















No.
C
Si
Mn
Al
P
S
N
O
Mo
Cr
Ni
Cu
B
Nb
Ti





S67
0.071
0.076
1.350
0.044
0.010
0.006
0.0030
0.0035




0.0009






S68
0.069
0.077
1.296
0.037
0.015
0.008
0.0025
0.0029



0.005


S69
0.069
0.084
1.302
0.040
0.015
0.007
0.0030
0.0028





0.00009



S70
0.070
0.077
1.337
0.036
0.015
0.008
0.0026
0.0035




0.0008


S71
0.071
0.076
1.284
0.044
0.010
0.004
0.0022
0.0027






0.0009



S72
0.069
0.077
1.350
0.037
0.015
0.004
0.0024
0.0037





0.003


S73
0.069
0.084
1.342
0.041
0.015
0.008
0.0021
0.0032







0.0009



S74
0.070
0.077
1.255
0.040
0.016
0.008
0.0027
0.0037






0.003


S75
0.072
0.079
1.326
0.043
0.018
0.007
0.0027
0.0027


S76
0.073
0.083
1.349
0.041
0.019
0.006
0.0028
0.0035


S77
0.070
0.084
1.334
0.044
0.015
0.006
0.0029
0.0031


S78
0.070
0.084
1.272
0.035
0.010
0.007
0.0021
0.0030


S79
0.069
0.084
1.312
0.042
0.016
0.007
0.0022
0.0029


S80
0.069
0.081
1.286
0.036
0.017
0.006
0.0025
0.0031


S81
0.072
0.079
1.337
0.044
0.011
0.006
0.0030
0.0030


S82
0.065
0.078
1.331
0.042
0.012
0.006
0.0025
0.0037


S83
0.065
0.082
1.344
0.038
0.013
0.006
0.0030
0.0029


S84
0.068
0.080
1.350
0.036
0.014
0.007
0.0026
0.0037


S85
0.067
0.076
1.296
0.043
0.010
0.005
0.0022
0.0031


S86
0.074
0.079
1.344
0.036
0.011
0.006
0.0026
0.0030


S87
0.071
0.084
1.350
0.044
0.015
0.006
0.0025
0.0035


S88
0.070
0.076
1.296
0.037
0.010
0.006
0.0029
0.0032


S89
0.073
0.077
1.302
0.041
0.015
0.007
0.0023
0.0035


S90
0.068
0.076
1.337
0.040
0.015
0.008
0.0026
0.0029


S91
0.067
0.077
1.284
0.043
0.010
0.005
0.0023
0.0028


S92
0.070
0.084
1.350
0.041
0.015
0.008
0.0024
0.0031


S93
0.069
0.077
1.342
0.036
0.015
0.007
0.0021
0.0036


S94
0.069
0.079
1.293
0.037
0.016
0.008
0.0027
0.0032


S95
0.072
0.084
1.287
0.039
0.018
0.004
0.0027
0.0037


S96
0.071
0.084
1.275
0.037
0.019
0.004
0.0028
0.0027


S97
0.069
0.081
1.255
0.040
0.015
0.008
0.0029
0.0035


S98
0.069
0.081
1.326
0.036
0.010
0.008
0.0021
0.0031

























TABLE 6







STEEL











No.
V
W
Ca
Mg
Zr
REM
As
Co
Sn





S67


S68


S69


S70


S71


S72


S73


S74


S75

0.0009



S76
0.005


S77


0.0009



S78

0.005


S79



0.00009



S80


0.0004


S81




0.00009



S82



0.0003


S83





0.00009



S84




0.0100


S85






0.00009



S86





0.0005


S87







0.00009



S88






0.0010


S89








0.00009



S90







0.0005


S91









0.00009



S92








0.0100


S93


S94


S95


S96


S97


S98

























CALCULATED










VALUE OF



STEEL



T1/
Ar3/
HARDNESS



No.
Pb
Y
Hf
° C.
° C.
OF FERRITE/—
REMARKS







S67



851
760
233
EXAMPLE



S68



851
766
234
EXAMPLE



S69



851
766
234
EXAMPLE



S70



851
762
234
EXAMPLE



S71



851
764
234
EXAMPLE



S72



852
762
239
EXAMPLE



S73



851
763
238
EXAMPLE



S74



852
768
239
EXAMPLE



S75



851
763
235
EXAMPLE



S76



852
762
236
EXAMPLE



S77



851
763
235
EXAMPLE



S78



851
766
232
EXAMPLE



S79



851
765
234
EXAMPLE



S80



851
767
234
EXAMPLE



S81



851
760
233
EXAMPLE



S82



851
764
234
EXAMPLE



S83



851
764
234
EXAMPLE



S84



851
762
234
EXAMPLE



S85



851
766
232
EXAMPLE



S86



851
759
234
EXAMPLE



S87



851
762
235
EXAMPLE



S88



851
764
232
EXAMPLE



S89



851
763
234
EXAMPLE



S90



851
763
234
EXAMPLE



S91



851
766
232
EXAMPLE



S92



851
762
235
EXAMPLE



S93

0.00009



851
763
235
EXAMPLE



S94
0.0050


851
766
234
EXAMPLE



S95


0.00009


851
766
234
EXAMPLE



S96

0.0500

851
768
234
EXAMPLE



S97



0.00009

851
769
233
EXAMPLE



S98


0.0500
851
763
233
EXAMPLE




















TABLE 7









ROLLING IN RANGE OF
ROLLING IN RANGE OF



1000° C. TO 1200° C.
T1 + 30° C. to T1 + 200° C.
















FREQUENCY




FREQUENCY




OF
EACH
GRAIN


OF




REDUCTION
REDUCTION
SIZE OF

FREQUENCY
REDUCTION


STEEL
PRODUCTION
OF 40%
OF 40%
AUSTENITE/
CUMULATIVE
OF
OF 30%


No.
No.
OR MORE/—
OR MORE/%
μm
REDUCTION/%
REDUCTION/—
OR MORE/—





S1
P1
1
50
150 
85
6
2


S1
P2
2
45/45
90
95
6
6


S1
P3
2
45/45
90

45

4
1


S1
P4
2
45/45
90
55
4
1


S1
P5
2
45/45
90
55
4
1


S1
P6
2
45/45
90
55
4
1


S2
P7
1
50
140 
85
6
2


S2
P8
2
45/45
80
75
6

0



S2
P9
0


250

65
6
2


S3
P10
2
45/45
80
75
6
2


S3
P11
2
45/45
80
85
6
2


S3
P12
2
45/45
80

45

4
1


S4
P13
2
45/45
80
75
6
2


S4
P14
2
45/45
80
85
6
2


S4
P15
2
45/45
80
85
6
2


S5
P16
2
45/45
95
85
6
2


S5
P17
2
45/45
95
95
6
6


S6
P18
2
45/45
90
85
6
2


S6
P19
2
45/45
90
95
6
6


S6
P20
0


300

85
6
2


S7
P21
3
40/40/40
75
80
6
2


S7
P22
3
40/40/40
75
80
6
2


S8
P23
3
40/40/40
70
80
6
2


S9
P24
2
45/40
95
80
6
2


S9
P25
1
50
120 
80
6
2


S10
P26
2
45/40
100 
80
6
2


S10
P27
1
50
120 
80
6
2


S10
P28
1
50
120 
80
6
2


S11
P29
3
40/40/40
70
95
6
6


S12
P30
3
40/40/40
75
95
6
6


S13
P31
3
40/40/40
65
95
6
6


S13
P32
0


350


45

4
1


S14
P33
3
40/40/40
70
95
6
6


S15
P34
2
45/45
70
85
6
2


S15
P35
2
45/45
120 

35

4
1


S16
P36
2
45/45
75
85
6
2


S17
P37
2
45/45
80
80
6
2


S18
P38
2
45/45
75
85
6
2


S19
P39
2
45/45
80
85
6
2


S20
P40
2
45/45
80
95
6
6


S21
P41
2
45/45
75
85
6
2









S22
P42
Cracks occur during Hot rolling


S23
P43
Cracks occur during Hot rolling


S24
P44
Cracks occur during Hot rolling


S25
P45
Cracks occur during Hot rolling














ROLLING IN RANGE OF Ar3



ROLLING IN RANGE OF T1 + 30° C. to T1 + 200° C.
TO LOWER THAN T1 + 30° C.



















MAXIMUM OF

ROLLING







TEMPERATURE

FINISH


STEEL
PRODUCTION
EACH


RISE BETWEEN PASSES/
CUMULATIVE
TEMPERATURE/


No.
No.
REDUCTION/%
P1/%
Tf/° C.
° C.
REDUCTION/%
° C.





S1
P1
20/20/25/25/30/40
40
935
15
0
935


S1
P2
40/40/40/40/30/35
35
892
5
0
892


S1
P3
 7/7/8/30
30
930
20
0
930


S1
P4
13/13/15/30
30
930
20
0
930


S1
P5
13/13/15/30
30
930
20
0
930


S1
P6
13/13/15/30
30
930
20
7
920


S2
P7
15/15/25/25/40/40
40
935
15
0
935


S2
P8
20/20/20/20/20/25


5
0
891


S2
P9
 5/8/10/10/30/30
30
850
18
0
850


S3
P10
10/15/15/15/30/37
37
945
15
0
945


S3
P11
25/25/25/25/30/31
31
920
18
0
920


S3
P12
 7/7/8/30
30
1075
15
0
1075


S4
P13
10/15/15/15/30/37
37
950
15
7
940


S4
P14
25/25/25/25/30/31
31
922
18
0
922


S4
P15
25/25/25/25/30/31
31
922
18
0
922


S5
P16
25/25/25/25/30/31
31
955
13
0
955


S5
P17
40/40/40/40/30/40
40
935
14
0
935


S6
P18
25/25/25/25/30/30
30
955
13
0
955


S6
P19
40/40/40/40/30/40
40
933
14
0
933


S6
P20
25/25/25/25/30/30
30
890
13
0
890


S7
P21
20/20/20/20/30/30
30
970
16
0
970


S7
P22
20/20/20/20/30/30
30
970
16
0
970


S8
P23
20/20/20/20/30/30
30
970
16
0
970


S9
P24
20/20/20/20/30/30
30
961
17
0
961


S9
P25
20/20/20/20/30/30
30
922
18
0
922


S10
P26
15/15/18/20/30/40
40
960
17
0
960


S10
P27
20/20/20/20/30/30
30
920
18
0
920


S10
P28
20/20/20/20/30/30
30
920
18
0
920


S11
P29
42/42/42/42/30/30
30
990
18
0
990


S12
P30
42/42/42/42/30/30
30
990
18
0
990


S13
P31
40/40/40/40/30/35
35
943
10
0
943


S13
P32
 5/5/6/35
35
910
30
0
910


S14
P33
40/40/40/40/30/35
35
940
10
0
940


S15
P34
20/20/25/25/30/40
40
1012
13
0
1012


S15
P35
 2/2/3/30
30
880
12
0
880


S16
P36
20/20/25/25/30/40
40
985
15
0
985


S17
P37
15/15/18/20/30/40
40
958
10
0
958


S18
P38
20/25/25/25/30/35
35
967
10
0
967


S19
P39
20/20/25/25/30/40
40
996
12
0
996


S20
P40
40/40/40/40/30/40
40
958
12
0
958


S21
P41
20/25/25/25/30/35
35
985
12
0
985









S22
P42
Cracks occur during Hot rolling


S23
P43
Cracks occur during Hot rolling


S24
P44
Cracks occur during Hot rolling


S25
P45
Cracks occur during Hot rolling












FIRST-COOLING























AVERAGE
COOLING
TEMPERATURE









COOLING
TEMPERATURE
AT COOLING



STEEL
PRODUCTION




RATE/
CHANGE/
FINISH/



No.
No.
t1/s
2.5 × t1/s
t/s
t/t1/—
° C./second
° C.
° C.







S1
P1
0.57
1.41
0.45
0.80
133
110
825



S1
P2
1.74
4.35
1.39
0.80
108
 90
802



S1
P3
1.08
2.69
0.86
0.80
157
130
800



S1
P4
1.08
2.69
0.86
0.80
108
 90
840



S1
P5
1.08
2.69
0.86
0.80
157
130
800



S1
P6
1.08
2.69
0.86
0.80
157
130
790



S2
P7
0.57
1.43
0.10
0.18
 96
 80
855



S2
P8


1.06

120
100
791



S2
P9
3.14
7.85
2.51
0.80
120
100
750



S3
P10
0.75
1.88
0.46
0.61
108
 90
855



S3
P11
1.54
3.84
0.93
0.60
133
110
810



S3
P12
0.20
0.50
0.16
0.79
133
110
965



S4
P13
0.67
1.67
0.40
0.60
145
120
820



S4
P14
1.50
3.74
0.90
0.60
108
 90
832



S4
P15
1.50
3.74
0.90
0.60
114
 95
827



S5
P16
0.75
1.87
0.44
0.58
120
100
855



S5
P17
0.72
1.80
0.42
0.58
108
 90
845



S6
P18
0.78
1.94
0.44
0.56
 96
 80
875



S6
P19
0.73
1.83
0.44
0.60
120
100
833



S6
P20
2.15
5.37
1.29
0.60
120
100
790



S7
P21
0.66
1.65
0.40
0.60
108
 90
880



S7
P22
0.66
1.65

2.00

3.03
24
20
950



S8
P23
0.66
1.66
0.40
0.60
133
110
860



S9
P24
0.73
1.82
0.44
0.60
133
110
851



S9
P25
1.44
3.59
0.86
0.60
145
120
802



S10
P26
0.74
1.85
0.70
0.95
114
 95
865



S10
P27
2.08
5.20
1.25
0.60
120
100
820



S10
P28
2.08
5.20
1.25
0.60
193

160

760



S11
P29
0.54
1.35
0.32
0.59
108
 90
900



S12
P30
0.76
1.89
0.46
0.61
108
 90
900



S13
P31
1.46
3.65
0.88
0.60
157
130
813



S13
P32
2.44
6.09
1.46
0.60
 96
 80
830



S14
P33
1.41
3.52
0.84
0.60
120
100
840



S15
P34
0.25
0.62
0.15
0.61
120
100
912



S15
P35
3.90
9.76
2.35
0.60
108
 90
790



S16
P36
0.60
1.50
0.37
0.61
133
110
875



S17
P37
0.29
0.72
0.17
0.60
133
110
848



S18
P38
0.33
0.83
0.20
0.60
145
120
847



S19
P39
0.14
0.36
0.09
0.60
108
 90
906



S20
P40
0.29
0.72
0.17
0.60
114
 95
863



S21
P41
0.44
1.11
0.27
0.60
120
100
885











S22
P42
Cracks occur during Hot rolling



S23
P43
Cracks occur during Hot rolling



S24
P44
Cracks occur during Hot rolling



S25
P45
Cracks occur during Hot rolling




















TABLE 8









ROLLING IN RANGE OF
ROLLING IN RANGE OF



1000° C. TO 1200° C.
T1 + 30° C. to T1 + 200° C.
















FREQUENCY




FREQUENCY




OF
EACH
GRAIN


OF




REDUCTION
REDUCTION
SIZE OF

FREQUENCY
REDUCTION


STEEL
PRODUCTION
OF 40%
OF 40%
AUSTENITE/
CUMULATIVE
OF
OF 30%


No.
No.
OR MORE/—
OR MORE/%
μm
REDUCTION/%
REDUCTION/—
OR MORE/—





S26
P46
2
45/45
80
65
6
2


S27
P47
2
45/45
80
70
6
2


S1
P48
1
45
180 
55
4
1


S1
P49
1
45
180 
55
4
1


S1
P50
1
45
180 
55
4
1


S1
P51
1
45
180 
55
4
1


S1
P52
2
45/45
90
55
4
1


S1
P53
2
45/45
90
75
5
1


S1
P54
2
45/45
90
80
6
2


S1
P55
2
45/45
90
80
6
2


S1
P56
2
45/45
90
80
6
2


S1
P57
2
45/45
90
80
6
2


S1
P58
2
45/45
90
80
6
2


S1
P59
2
45/45
90
80
6
2


S1
P60
2
45/45
90
80
6
2


S1
P61
2
45/45
90
80
6
2


S1
P62
2
45/45
90
80
6
2


S1
P63
2
45/45
90
80
6
2


S1
P64
1
45
180 
55
4
1


S1
P65
1
45
180 
55
4
1


S1
P66
2
45/45
90
55
4
1


S1
P67
2
45/45
90
75
5
1


S1
P68
2
45/45
90
80
6
2


S1
P69
2
45/45
90
80
6
2


S1
P70
2
45/45
90
80
6
2


S1
P71
2
45/45
90
80
6
2


S1
P72
2
45/45
90
80
6
2


S1
P73
2
45/45
90
80
6
2


S1
P74
2
45/45
90
80
6
2


S1
P75
2
45/45
90
80
6
2


S1
P76
2
45/45
90
80
6
2


S1
P77
2
45/45
90
80
6
2


S1
P78

0



250

55
4
1


S1
P79
1
45
180 

45

4
1


S1
P80
1
45
180 
55
4

0



S1
P81
1
45
180 
55
4
1


S1
P82
1
45
180 
55
4
1


S1
P83
1
45
180 
55
4
1


S1
P84
1
45
180 
55
4
1


S1
P85
1
45
180 
55
4
1


S1
P86
1
45
180 
55
4
1


S1
P87
1
45
180 
55
4
1


S1
P88
1
45
180 
55
4
1


S1
P89
1
45
180 
55
4
1


S1
P90
1
45
180 
55
4
1













ROLLING IN RANGE OF T1 + 30° C. to T1 + 200° C.











MAXIMUM OF
ROLLING IN RANGE OF Ar3



TEMPERATURE
TO LOWER THAN T1 + 30° C.



















RISE

ROLLING







BETWEEN

FINISH


STEEL
PRODUCTION
EACH

Tf/
PASSES/
CUMULATIVE
TEMPERATURE/


No.
No.
REDUCTION/%
P1/%
° C.
° C.
REDUCTION/%
° C.





S26
P46
 3/5/5/5/30/40
40
956
10
0
956


S27
P47
10/10/10/10/30/35
35
919
10
0
919


S1
P48
13/13/15/30
30
935
20
0
935


S1
P49
13/13/15/30
30
935
17
0
935


S1
P50
13/13/15/30
30
935
17
0
935


S1
P51
13/13/15/30
30
935
20
0
935


S1
P52
13/13/15/30
30
935
17
0
935


S1
P53
20/20/25/25/30
30
935
17
0
935


S1
P54
20/20/20/20/30/30
30
935
17
0
935


S1
P55
30/30/20/20/20/20
30
935
17
0
880


S1
P56
15/15/18/20/30/40
40
915
17
0
915


S1
P57
20/20/20/20/30/30
30
935
17
20 
890


S1
P58
20/20/20/20/30/30
30
935
17
8
890


S1
P59
30/30/20/20/20/20
30
935
17
0
830


S1
P60
15/15/18/20/30/40
40
915
17
0
915


S1
P61
15/15/18/20/30/40
40
915
17
0
915


S1
P62
15/15/18/20/30/40
40
915
17
0
915


S1
P63
15/15/18/20/30/40
40
915
17
0
915


S1
P64
13/13/15/30
30
935
20
0
935


S1
P65
13/13/15/30
30
935
20
0
935


S1
P66
13/13/15/30
30
935
17
0
935


S1
P67
20/20/25/25/30
30
935
17
0
935


S1
P68
20/20/20/20/30/30
30
935
17
0
935


S1
P69
30/30/20/20/20/20
30
935
17
0
880


S1
P70
15/15/18/20/30/40
40
915
17
0
915


S1
P71
20/20/20/20/30/30
30
935
17
20 
890


S1
P72
20/20/20/20/30/30
30
935
17
8
890


S1
P73
30/30/20/20/20/20
30
935
17
0
830


S1
P74
15/15/18/20/30/40
40
915
17
0
915


S1
P75
15/15/18/20/30/40
40
915
17
0
915


S1
P76
15/15/18/20/30/40
40
915
17
0
915


S1
P77
15/15/18/20/30/40
40
915
17
0
915


S1
P78
13/13/15/30
30
935
20
0
935


S1
P79
 7/7/8/30
30
935
20
0
935


S1
P80
12/20/20/20


20
0
935


S1
P81
13/13/15/30
30
935
20

35

890


S1
P82
13/13/15/30
30
760
20
0

760



S1
P83
13/13/15/30
30
935
20
0
935


S1
P84
13/13/15/30
30
935
20
0
935


S1
P85
13/13/15/30
30
935
20
0
935


S1
P86
13/13/15/30
30
995
20
0
995


S1
P87
13/13/15/30
30
935
20
0
935


S1
P88
13/13/15/30
30
935
20
0
935


S1
P89
13/13/15/30
30
935
20
0
935


S1
P90
13/13/15/30
30
935
20
0
935












FIRST-COOLING























AVERAGE
COOLING
TEMPERATURE









COOLING
TEMPERATURE
AT COOLING



STEEL
PRODUCTION




RATE/
CHANGE/
FINISH/



No.
No.
t1/s
2.5 × t1/s
t/s
t/t1/—
° C./second
° C.
° C.







S26
P46
0.29
0.72
0.27
0.93
120
100
856



S27
P47
1.14
2.84
0.68
0.60
120
100
819



S1
P48
0.99
2.47
0.90
0.91
113
90
842



S1
P49
0.99
2.47
0.90
0.91
113
90
842



S1
P50
0.99
2.47
0.90
0.91
113
90
842



S1
P51
0.99
2.47
0.10
0.10
113
90
845



S1
P52
0.99
2.47
0.90
0.91
113
90
842



S1
P53
0.99
2.47
0.90
0.91
113
90
842



S1
P54
0.99
2.47
0.90
0.91
113
90
842



S1
P55
0.99
2.47
0.90
0.91
113
90
787



S1
P56
0.96
2.41
0.90
0.93
113
90
822



S1
P57
0.99
2.47
0.90
0.91
113
90
797



S1
P58
0.99
2.47
0.90
0.91
113
90
797



S1
P59
0.99
2.47
0.90
0.91
113
45
782



S1
P60
0.96
2.41
0.90
0.93
113
90
822



S1
P61
0.96
2.41
0.90
0.93
113
90
822



S1
P62
0.96
2.41
0.90
0.93
113
90
822



S1
P63
0.96
2.41
0.50
0.52
113
90
824



S1
P64
0.99
2.47
1.10
1.11
113
90
842



S1
P65
0.99
2.47
2.40
2.43
113
90
838



S1
P66
0.99
2.47
1.10
1.11
113
90
842



S1
P67
0.99
2.47
1.10
1.11
113
90
842



S1
P68
0.99
2.47
1.10
1.11
113
90
842



S1
P69
0.99
2.47
1.10
1.11
113
90
787



S1
P70
0.96
2.41
1.10
1.14
113
90
822



S1
P71
0.99
2.47
1.10
1.11
113
90
797



S1
P72
0.99
2.47
1.10
1.11
113
90
797



S1
P73
0.99
2.47
1.10
1.11
113
45
782



S1
P74
0.96
2.41
1.10
1.14
113
90
822



S1
P75
0.96
2.41
1.10
1.14
113
90
822



S1
P76
0.96
2.41
1.10
1.14
113
90
822



S1
P77
0.96
2.41
1.50
1.56
113
90
821



S1
P78
0.99
2.47
0.90
0.91
113
90
842



S1
P79
0.99
2.47
0.90
0.91
113
90
842



S1
P80


0.90

113
90
842



S1
P81
0.99
2.47
0.90
0.91
113
90
797



S1
P82
6.82
17.05 
6.20
0.91
113
45
696



S1
P83
0.99
2.47
0.90
0.91
45
90
842



S1
P84
0.99
2.47
0.90
0.91
113

35

897



S1
P85
0.99
2.47
0.90
0.91
113

145

787



S1
P86
0.26
0.64
0.24
0.91
 50
40

954




S1
P87
0.99
2.47
0.90
0.91
113
90
842



S1
P88
0.99
2.47
0.90
0.91
113
90
842



S1
P89
0.99
2.47
0.90
0.91
113
90
842



S1
P90
0.99
2.47
0.90
0.91
113
90
842




















TABLE 9









ROLLING IN RANGE OF




1000° C. TO 1200° C.
ROLLING IN RANGE OF T1 + 30° C. to T1 + 200° C.




















FREQUENCY OF
EACH
GRAIN


FREQUENCY OF



MAXIMUM OF




REDUCTION
REDUCTION
SIZE OF

FREQUENCY
REDUCTION



TEMPERATURE



PRODUCTION
OF 40%
OF 40%
AUSTENITE/
CUMULATIVE
OF
OF 30%
EACH


RISE BETWEEN


STEEL No.
No.
OR MORE/—
OR MORE/%
μm
REDUCTION/%
REDUCTION/—
OR MORE/—
REDUCTION/%
P1/%
Tf/° C.
PASSES/° C.





S1
P91
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P92
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P93
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P94

0



250

55
4
1
13/13/15/30
30
935
20


S1
P95
1
45
180
45
4
1
7/7/8/30
30
935
20


S1
P96
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P97
1
45
180
55
4
1
13/13/15/30
30
760
20


S1
P98
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P99
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P100
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P101
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P102
1
45
180
55
4
1
13/13/15/30
30
995
20


S1
P103
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P104
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P105
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P106
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P107
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P108
1
45
180
55
4
1
13/13/15/30
30
935
20


S1
P109
1
45
180
55
4
1
13/13/15/30
30
935
20


S28
P110
1
45
180
55
4
1
13/13/15/30
30
935
20


S29
P111
1
45
180
55
4
1
13/13/15/30
30
935
20


S30
P112
1
45
180
55
4
1
13/13/15/30
30
935
20


S31
P113
1
45
180
55
4
1
13/13/15/30
30
935
20


S32
P114
1
45
180
55
4
1
13/13/15/30
30
935
20


S33
P115
1
45
180
55
4
1
13/13/15/30
30
935
20


S34
P116
1
45
180
55
4
1
13/13/15/30
30
935
20


S35
P117
1
45
180
55
4
1
13/13/15/30
30
935
20









S36
P118
Cracks occur during Hot rolling


















S37
P119
1
45
180
55
4
1
13/13/15/30
30
935
20


S38
P120
1
45
180
55
4
1
13/13/15/30
30
935
20


S39
P121
1
45
180
55
4
1
13/13/15/30
30
935
20


S40
P122
1
45
180
55
4
1
13/13/15/30
30
935
20


S41
P123
1
45
180
55
4
1
13/13/15/30
30
935
20


S42
P124
1
45
180
55
4
1
13/13/15/30
30
935
20


S43
P125
1
45
180
55
4
1
13/13/15/30
30
935
20


S44
P126
1
45
180
55
4
1
13/13/15/30
30
935
20


S45
P127
1
45
180
55
4
1
13/13/15/30
30
935
20


S46
P128
1
45
180
55
4
1
13/13/15/30
30
935
20


S47
P129
1
45
180
55
4
1
13/13/15/30
30
935
20


S48
P130
1
45
180
55
4
1
13/13/15/30
30
935
20


S49
P131
1
45
180
55
4
1
13/13/15/30
30
935
20


S50
P132
1
45
180
55
4
1
13/13/15/30
30
935
20


S51
P133
1
45
180
55
4
1
13/13/15/30
30
935
20


S52
P134
1
45
180
55
4
1
13/13/15/30
30
935
20


S53
P135
1
45
180
55
4
1
13/13/15/30
30
935
20













ROLLING IN RANGE OF Ar3




TO LOWER THAN T1 + 30° C.
FIRST-COOLING






















ROLLING




AVERAGE
COOLING
TEMPERATURE






FINISH




COOLING
TEMPERATURE
AT COOLING



STEEL
PRODUCTION
CUMULATIVE
TEMPERATURE/




RATE/
CHANGE/
FINISH/



No.
No.
REDUCTION/%
° C.
t1/s
2.5 × t1/s
t/s
t/t1/—
° C./second
° C.
° C.







S1
P91
0
935
0.99
2.47
0.90
0.91
113
90
842



S1
P92
0
935
0.99
2.47
0.90
0.91
113
90
842



S1
P93
0
935
0.99
2.47
0.90
0.91
113
90
842



S1
P94
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P95
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P96

35

890
0.99
2.47
1.10
1.11
113
90
797



S1
P97
0

760

6.82
17.05 
7.60
1.11
113
45
692



S1
P98
0
935
0.99
2.47

2.50

2.53
113
90
838



S1
P99
0
935
0.99
2.47
1.10
1.11
45
90
842



S1
P100
0
935
0.99
2.47
1.10
1.11
113

35

897



S1
P101
0
935
0.99
2.47
1.10
1.11
113

145

787



S1
P102
0
995
0.26
0.64
0.29
1.11
50
40

954




S1
P103
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P104
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P105
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P106
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P107
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P108
0
935
0.99
2.47
1.10
1.11
113
90
842



S1
P109
0
935
0.99
2.47
1.10
1.11
113
90
842



S28
P110
0
935
0.97
2.43
0.90
0.92
113
90
842



S29
P111
0
935
1.06
2.66
0.90
0.85
113
90
842



S30
P112
0
935
0.99
2.47
0.90
0.91
113
90
842



S31
P113
0
935
0.99
2.47
0.90
0.91
113
90
842



S32
P114
0
935
0.97
2.43
0.90
0.93
113
90
842



S33
P115
0
935
1.02
2.55
0.90
0.88
113
90
842



S34
P116
0
935
0.99
2.47
0.90
0.91
113
90
842



S35
P117
0
935
0.99
2.47
0.90
0.91
113
90
842











S36
P118
Cracks occur during Hot rolling



















S37
P119
0
935
0.99
2.47
0.90
0.91
113
90
842



S38
P120
0
935
0.99
2.47
0.90
0.91
113
90
842



S39
P121
0
935
0.99
2.47
0.90
0.91
113
90
842



S40
P122
0
935
3.68
9.20
0.90
0.24
113
90
842



S41
P123
0
935
1.38
3.44
0.90
0.65
113
90
842



S42
P124
0
935
0.99
2.47
0.90
0.91
113
90
842



S43
P125
0
935
0.99
2.47
0.90
0.91
113
90
842



S44
P126
0
935
0.99
2.48
0.90
0.91
113
90
842



S45
P127
0
935
2.67
6.67
0.90
0.34
113
90
842



S46
P128
0
935
2.10
5.25
0.90
0.43
113
90
842



S47
P129
0
935
3.68
9.20
0.90
0.24
113
90
842



S48
P130
0
935
0.99
2.47
0.90
0.91
113
90
842



S49
P131
0
935
0.99
2.47
0.90
0.91
113
90
842



S50
P132
0
935
0.99
2.47
0.90
0.91
113
90
842



S51
P133
0
935
0.99
2.47
0.90
0.91
113
90
842



S52
P134
0
935
0.99
2.47
0.90
0.91
113
90
842



S53
P135
0
935
0.99
2.47
0.90
0.91
113
90
842



















TABLE 10








ROLLING IN RANGE OF
ROLLING IN RANGE OF T1 + 30° C. to T1 + 200° C.











1000° C. TO 1200° C.

MAXIMUM OF




















FREQUENCY








TEMPERATURE




OF
EACH
GRAIN


FREQUENCY



RISE




REDUCTION
REDUCTION
SIZE OF

FREQUENCY
OF REDUCTION



BETWEEN


STEEL
PRODUCTION
OF 40%
OF 40%
AUSTENITE/
CUMULATIVE
OF
OF 30%
EACH


PASSES/


No.
No.
OR MORE/—
OR MORE/%
μm
REDUCTION/%
REDUCTION/—
OR MORE/—
REDUCTION/%
P1/%
Tf/° C.
° C.





S54
P136
1
45
180
55
4
1
13/13/15/30
30
935
20









S55
P137
Cracks occur during Hot rolling


S56
P138
Cracks occur during Hot rolling


















S57
P139
1
45
180
55
4
1
13/13/15/30
30
935
20


S58
P140
1
45
180
55
4
1
13/13/15/30
30
935
20


S59
P141
1
45
180
55
4
1
13/13/15/30
30
935
20


S60
P142
1
45
180
55
4
1
13/13/15/30
30
935
20


S61
P143
1
45
180
55
4
1
13/13/15/30
30
935
20


S62
P144
1
45
180
55
4
1
13/13/15/30
30
935
20


S63
P145
1
45
180
55
4
1
13/13/15/30
30
935
20


S64
P146
1
45
180
55
4
1
13/13/15/30
30
935
20


S65
P147
1
45
180
55
4
1
13/13/15/30
30
935
20


S66
P148
1
45
180
55
4
1
13/13/15/30
30
935
20


S67
P149
1
45
180
55
4
1
13/13/15/30
30
935
20


S68
P150
1
45
180
55
4
1
13/13/15/30
30
935
20


S69
P151
1
45
180
55
4
1
13/13/15/30
30
935
20


S70
P152
1
45
180
55
4
1
13/13/15/30
30
935
20


S71
P153
1
45
180
55
4
1
13/13/15/30
30
935
20


S72
P154
1
45
180
55
4
1
13/13/15/30
30
935
20


S73
P155
1
45
180
55
4
1
13/13/15/30
30
935
20


S74
P156
1
45
180
55
4
1
13/13/15/30
30
935
20


S75
P157
1
45
180
55
4
1
13/13/15/30
30
935
20


S76
P158
1
45
180
55
4
1
13/13/15/30
30
935
20


S77
P159
1
45
180
55
4
1
13/13/15/30
30
935
20


S78
P160
1
45
180
55
4
1
13/13/15/30
30
935
20


S79
P161
1
45
180
55
4
1
13/13/15/30
30
935
20


S80
P162
1
45
180
55
4
1
13/13/15/30
30
935
20


S81
P163
1
45
180
55
4
1
13/13/15/30
30
935
20


S82
P164
1
45
180
55
4
1
13/13/15/30
30
935
20


S83
P165
1
45
180
55
4
1
13/13/15/30
30
935
20


S84
P166
1
45
180
55
4
1
13/13/15/30
30
935
20


S85
P167
1
45
180
55
4
1
13/13/15/30
30
935
20


S86
P168
1
45
180
55
4
1
13/13/15/30
30
935
20


S87
P169
1
45
180
55
4
1
13/13/15/30
30
935
20


S88
P170
1
45
180
55
4
1
13/13/15/30
30
935
20


S89
P171
1
45
180
55
4
1
13/13/15/30
30
935
20


S90
P172
1
45
180
55
4
1
13/13/15/30
30
935
20


S91
P173
1
45
180
55
4
1
13/13/15/30
30
935
20


S92
P174
1
45
180
55
4
1
13/13/15/30
30
935
20


S93
P175
1
45
180
55
4
1
13/13/15/30
30
935
20


S94
P176
1
45
180
55
4
1
13/13/15/30
30
935
20


S95
P177
1
45
180
55
4
1
13/13/15/30
30
935
20


S96
P178
1
45
180
55
4
1
13/13/15/30
30
935
20


S97
P179
1
45
180
55
4
1
13/13/15/30
30
935
20


S98
P180
1
45
180
55
4
1
13/13/15/30
30
935
20













ROLLING IN RANGE OF Ar3




TO LOWER THAN T1 + 30° C.
FIRST-COOLING






















ROLLING




AVERAGE
COOLING
TEMPERATURE






FINISH




COOLING
TEMPERATURE
AT COOLING



STEEL
PRODUCTION
CUMULATIVE
TEMPERATURE/




RATE/
CHANGE/
FINISH/



No.
No.
REDUCTION/%
° C.
t1/s
2.5 × t1/s
t/s
t/t1/—
° C./second
° C.
° C.






S54
P136
0
935
0.99
2.47
0.90
0.91
113
90
842











S55
P137
Cracks occur during Hot rolling



S56
P138
Cracks occur during Hot rolling



















S57
P139
0
935
0.99
2.47
0.90
0.91
113
90
842



S58
P140
0
935
0.99
2.47
0.90
0.91
113
90
842



S59
P141
0
935
0.99
2.47
0.90
0.91
113
90
842



S60
P142
0
935
0.99
2.47
0.90
0.91
113
90
842



S61
P143
0
935
0.99
2.47
0.90
0.91
113
90
842



S62
P144
0
935
1.04
2.60
0.90
0.86
113
90
842



S63
P145
0
935
0.99
2.47
0.90
0.91
113
90
842



S64
P146
0
935
0.99
2.47
0.90
0.91
113
90
842



S65
P147
0
935
0.99
2.47
0.90
0.91
113
90
842



S66
P148
0
935
0.99
2.47
0.90
0.91
113
90
842



S67
P149
0
935
0.99
2.47
0.90
0.91
113
90
842



S68
P150
0
935
0.99
2.47
0.90
0.91
113
90
842



S69
P151
0
935
0.99
2.47
0.90
0.91
113
90
842



S70
P152
0
935
0.99
2.47
0.90
0.91
113
90
842



S71
P153
0
935
0.99
2.48
0.90
0.91
113
90
842



S72
P154
0
935
1.01
2.52
0.90
0.89
113
90
842



S73
P155
0
935
0.99
2.48
0.90
0.91
113
90
842



S74
P156
0
935
1.00
2.50
0.90
0.90
113
90
842



S75
P157
0
935
0.99
2.47
0.90
0.91
113
90
842



S76
P158
0
935
1.00
2.49
0.90
0.90
113
90
842



S77
P159
0
935
0.99
2.47
0.90
0.91
113
90
842



S78
P160
0
935
0.99
2.47
0.90
0.91
113
90
842



S79
P161
0
935
0.99
2.47
0.90
0.91
113
90
842



S80
P162
0
935
0.99
2.47
0.90
0.91
113
90
842



S81
P163
0
935
0.99
2.47
0.90
0.91
113
90
842



S82
P164
0
935
0.99
2.47
0.90
0.91
113
90
842



S83
P165
0
935
0.99
2.47
0.90
0.91
113
90
842



S84
P166
0
935
0.99
2.47
0.90
0.91
113
90
842



S85
P167
0
935
0.99
2.47
0.90
0.91
113
90
842



S86
P168
0
935
0.99
2.47
0.90
0.91
113
90
842



S87
P169
0
935
0.99
2.47
0.90
0.91
113
90
842



S88
P170
0
935
0.99
2.47
0.90
0.91
113
90
842



S89
P171
0
935
0.99
2.47
0.90
0.91
113
90
842



S90
P172
0
935
0.99
2.47
0.90
0.91
113
90
842



S91
P173
0
935
0.99
2.47
0.90
0.91
113
90
842



S92
P174
0
935
0.99
2.47
0.90
0.91
113
90
842



S93
P175
0
935
0.99
2.47
0.90
0.91
113
90
842



S94
P176
0
935
0.99
2.47
0.90
0.91
113
90
842



S95
P177
0
935
0.99
2.47
0.90
0.91
113
90
842



S96
P178
0
935
0.99
2.47
0.90
0.91
113
90
842



S97
P179
0
935
0.99
2.47
0.90
0.91
113
90
842



S98
P180
0
935
0.99
2.47
0.90
0.91
113
90
842




















TABLE 11








SECOND-COOLING
HOLDING
THIRD-COOLING

















TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE
COILING



SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
TEMPER-


PRODUCTION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
ATURE/


No.
START/s
° C./second
° C.
° C.
TIME/s
° C./second
° C.
° C.





P1
1.6
46
684
676
3.0
205
323
323


P2
1.6
50
647
639
3.0
222
292
292


P3
1.6
37
684
674
4.0
234
278
278


P4
1.6
2

830


820

4.0
232
327
327


P5
1.6
40
675
665
4.0
10
277
277


P6
1.6
43
656
646
4.0
105

600


600



P7
1.6
62
664
654
4.0
201
205
205


P8
1.6
47
647
639
3.0
183
285
285


P9
1.6
31
651
641
4.0
 82
232
232


P10
1.6
57
680
675
2.0
170
228
228


P11
1.6
53
647
639
3.0
146
210
210


P12
1.6
98
665
660
2.0
45
307
307


P13
1.6
43
688
680
3.0
224
247
247


P14
1.6
51
675
665
4.0
223
326
326


P15
1.6
18
769
644

50.0

 63
314
314


P16
1.6
58
677
669
3.0
 96
221
221


P17
1.6
62
656
648
3.0
 87
315
315


P18
1.6
72
654
644
4.0
159
231
231


P19
1.6
62
643
633
4.0
 79
319
319


P20
1.6
45
650
640
4.0
231
214
214


P21
1.6
68
670
665
2.0
100
327
327


P22
1.6
95
659
654
2.0
117
237
237


P23
1.6
70
646
638
3.0
184
278
278


P24
1.6
56
677
667
4.0
239
277
277


P25
1.6
52
643
635
3.0
166
284
284


P26
1.6
69
652
647
2.0
107
251
251


P27
1.6
59
640
632
3.0
161
234
234


P28
1.6
27
674
666
3.0
167
318
318


P29
1.6
74
674
666
3.0
 97
333
333


P30
1.6
78
663
655
3.0
122
341
341


P31
1.6
53
651
643
3.0
234
267
267


P32
1.6
55
659
649
4.0
 74
308
308


P33
1.6
57
664
656
3.0
 82
328
328


P34
1.6
82
661
651
4.0
164
337
337


P35
1.6
38
672
662
4.0
105
331
331


P36
1.6
65
674
669
2.0
180
232
232


P37
1.6
52
687
679
3.0
143
222
222


P38
1.6
62
656
648
3.0
 95
256
256


P39
1.6
80
663
655
3.0
221
347
347


P40
1.6
70
649
639
4.0
230
239
239


P41
1.6
77
651
646
2.0
 86
311
311








P42
Cracks occur during Hot rolling


P43
Cracks occur during Hot rolling


P44
Cracks occur during Hot rolling


P45
Cracks occur during Hot rolling




















TABLE 12








SECOND-COOLING
HOLDING
THIRD-COOLING

















TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE
COILING



SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
TEMPER-


PRODUCTION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
ATURE/


No.
START/s
° C./second
° C.
° C.
TIME/s
° C./second
° C.
° C.





P46
1.6
45

500






500



P47
1.6
45

500






500



P48
3.5
36
724
700
8.0
70
330
330


P49
3.5
36
724
700
8.0
70
330
330


P50
2.8
37
724
700
8.0
70
330
330


P51
3.5
37
724
700
8.0
70
330
330


P52
2.8
37
724
700
8.0
70
330
330


P53
2.8
37
724
700
8.0
70
330
330


P54
2.8
37
724
700
8.0
70
330
330


P55
2.8
18
724
700
8.0
70
330
330


P56
2.8
30
724
700
8.0
70
330
330


P57
2.8
22
724
700
8.0
70
330
330


P58
2.8
22
724
700
8.0
70
330
330


P59
2.8
17
724
700
8.0
70
330
330


P60
2.8
48
669
630
13.0 
70
 80
 80


P61
2.8
35
709
700
3.0
60
330
330


P62
2.8
37
703
700
1.0
250 
 50
 50


P63
2.8
30
724
700
8.0
70
330
330


P64
3.5
36
724
700
8.0
70
330
330


P65
3.5
34
724
700
8.0
70
330
330


P66
2.8
36
724
700
8.0
70
330
330


P67
2.8
36
724
700
8.0
70
330
330


P68
2.8
36
724
700
8.0
70
330
330


P69
2.8
18
724
700
8.0
70
330
330


P70
2.8
30
724
700
8.0
70
330
330


P71
2.8
21
724
700
8.0
70
330
330


P72
2.8
21
724
700
8.0
70
330
330


P73
2.8
16
724
700
8.0
70
330
330


P74
2.8
48
669
630
13.0 
70
 80
 80


P75
2.8
35
709
700
3.0
60
330
330


P76
2.8
37
703
700
1.0
250 
 50
 50


P77
2.8
29
724
700
8.0
70
330
330


P78
3.5
36
724
700
8.0
70
330
330


P79
3.5
36
724
700
8.0
70
330
330


P80
3.5
36
724
700
8.0
70
330
330


P81
3.5
21
724
700
8.0
70
330
330


P82
3.5
17
634
610
8.0
70
330
330


P83
3.5
36
724
700
8.0
70
330
330


P84
3.5
54
724
700
8.0
70
330
330


P85
3.5
18
724
700
8.0
70
330
330


P86
3.5
73
724
700
8.0
70
330
330


P87
3.5

10

724
700
8.0
70
330
330


P88
3.5
36

829


805

8.0
250 
 50
 50


P89
3.5
43
702
700

0.5

250 
 50
 50


P90
3.5
28
748
700

16.0

70
330
330




















TABLE 13








SECOND-COOLING
HOLDING
THIRD-COOLING

















TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE
COILING



SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
TEMPER-


PRODUCTION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
ATURE/


No.
START/s
° C./second
° C.
° C.
TIME/s
° C./second
° C.
° C.





P91
3.5
36
724
700
8.0

20

330
330


P92
3.5
36
724
700
8.0
70

355

330


P93
3.5
36
724
700
8.0
70
330

355



P94
3.5
36
724
700
8.0
70
330
330


P95
3.5
36
724
700
8.0
70
330
330


P96
3.5
21
724
700
8.0
70
330
330


P97
3.5
16
634
610
8.0
70
330
330


P98
3.5
34
724
700
8.0
70
330
330


P99
3.5
36
724
700
8.0
70
330
330


P100
3.5
54
724
700
8.0
70
330
330


P101
3.5
17
724
700
8.0
70
330
330


P102
3.5
73
724
700
8.0
70
330
330


P103
3.5

10

724
700
8.0
70
330
330


P104
3.5
36

829


805

8.0
250 
50
50


P105
3.5
43
702
700

0.5

250 
50
50


P106
3.5
28
748
700

16.0

70
330
330


P107
3.5
36
724
700
8.0

20

330
330


P108
3.5
36
724
700
8.0
70

355

330


P109
3.5
36
724
700
8.0
70
330

355



P110
3.5
36
724
700
8.0
70
330
330


P111
3.5
36
724
700
8.0
70
330
330


P112
3.5
36
724
700
8.0
70
330
330


P113
3.5
36
724
700
8.0
70
330
330


P114
3.5
36
724
700
8.0
70
330
330


P115
3.5
36
724
700
8.0
70
330
330


P116
3.5
36
724
700
8.0
70
330
330


P117
3.5
36
724
700
8.0
70
330
330








P118
Cracks occur during Hot rolling















P119
3.5
36
724
700
8.0
70
330
330


P120
3.5
36
724
700
8.0
70
330
330


P121
3.5
36
724
700
8.0
70
330
330


P122
3.5
36
724
700
8.0
70
330
330


P123
3.5
36
724
700
8.0
70
330
330


P124
3.5
36
724
700
8.0
70
330
330


P125
3.5
36
724
700
8.0
70
330
330


P126
3.5
36
724
700
8.0
70
330
330


P127
3.5
36
724
700
8.0
70
330
330


P128
3.5
36
724
700
8.0
70
330
330


P129
3.5
36
724
700
8.0
70
330
330


P130
3.5
36
724
700
8.0
70
330
330


P131
3.5
36
724
700
8.0
70
330
330


P132
3.5
36
724
700
8.0
70
330
330


P133
3.5
36
724
700
8.0
70
330
330


P134
3.5
36
724
700
8.0
70
330
330


P135
3.5
36
724
700
8.0
70
330
330




















TABLE 14








SECOND-COOLING
HOLDING
THIRD-COOLING

















TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE
COILING



SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
TEMPER-


PRODUCTION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
ATURE/


No.
START/s
° C./second
° C.
° C.
TIME/s
° C./second
° C.
° C.


















P136
3.5
36
724
700
8.0
70
330
330








P137
Cracks occur during Hot rolling


P138
Cracks occur during Hot rolling















P139
3.5
36
724
700
8.0
70
330
330


P140
3.5
36
724
700
8.0
70
330
330


P141
3.5
36
724
700
8.0
70
330
330


P142
3.5
36
724
700
8.0
70
330
330


P143
3.5
36
724
700
8.0
70
330
330


P144
3.5
36
724
700
8.0
70
330
330


P145
3.5
36
724
700
8.0
70
330
330


P146
3.5
36
724
700
8.0
70
330
330


P147
3.5
36
724
700
8.0
70
330
330


P148
3.5
36
724
700
8.0
70
330
330


P149
3.5
36
724
700
8.0
70
330
330


P150
3.5
36
724
700
8.0
70
330
330


P151
3.5
36
724
700
8.0
70
330
330


P152
3.5
36
724
700
8.0
70
330
330


P153
3.5
36
724
700
8.0
70
330
330


P154
3.5
36
724
700
8.0
70
330
330


P155
3.5
36
724
700
8.0
70
330
330


P156
3.5
36
724
700
8.0
70
330
330


P157
3.5
36
724
700
8.0
70
330
330


P158
3.5
36
724
700
8.0
70
330
330


P159
3.5
36
724
700
8.0
70
330
330


P160
3.5
36
724
700
8.0
70
330
330


P161
3.5
36
724
700
8.0
70
330
330


P162
3.5
36
724
700
8.0
70
330
330


P163
3.5
36
724
700
8.0
70
330
330


P164
3.5
36
724
700
8.0
70
330
330


P165
3.5
36
724
700
8.0
70
330
330


P166
3.5
36
724
700
8.0
70
330
330


P167
3.5
36
724
700
8.0
70
330
330


P168
3.5
36
724
700
8.0
70
330
330


P169
3.5
36
724
700
8.0
70
330
330


P170
3.5
36
724
700
8.0
70
330
330


P171
3.5
36
724
700
8.0
70
330
330


P172
3.5
36
724
700
8.0
70
330
330


P173
3.5
36
724
700
8.0
70
330
330


P174
3.5
36
724
700
8.0
70
330
330


P175
3.5
36
724
700
8.0
70
330
330


P176
3.5
36
724
700
8.0
70
330
330


P177
3.5
36
724
700
8.0
70
330
330


P178
3.5
36
724
700
8.0
70
330
330


P179
3.5
36
724
700
8.0
70
330
330


P180
3.5
36
724
700
8.0
70
330
330

















TABLE 15








AREA FRACTION OF METALLOGRAPHIC STRUCTURE














PHASE WITH
AREA





EXCEPTION
FRACTION


PRODUCTION
TEXTURE

OF F, B,
OF COARSE

















No.
D1/—
D2/—
F/%
B/%
F + B/%
fM/%
P/%
γ/%
AND M/%
GRAINS/%





P1
4.8
3.8
93.6
0.0
93.6
6.4
0.0
0.0
0.0
6.2


P2
4.9
3.5
91.1
0.0
91.1
8.9
0.0
0.0
0.0
6.0


P3

5.3


4.3

93.0
0.0
93.0
7.0
0.0
0.0
0.0
13.5


P4
4.3
3.3
29.0
0.0

29.0


71.0

0.0
0.0
0.0
13.8


P5

5.9


4.9

75.0
0.0
75.0

0.0

25.0
0.0
25.0
10.0


P6
4.4
3.2
100.0
0.0

100.0


0.0

0.0
0.0
0.0
10.0


P7
4.7
3.6
95.0
0.0
95.0
5.0
0.0
0.0
0.0
6.0


P8

6.9


5.1

91.1
0.0
91.1
8.9
0.0
0.0
0.0
12.0


P9

5.6


4.6

93.0
0.0
93.0
7.0
0.0
0.0
0.0
16.0


P10
4.6
3.7
92.0
0.0
92.0
8.0
0.0
0.0
0.0
6.0


P11
4.6
3.8
94.3
0.0
94.3
5.7
0.0
0.0
0.0
6.1


P12

5.3


4.3

58.1
30.0
88.1
1.4
10.5
0.0
10.5
13.8


P13
4.7
3.5
92.0
0.0
92.0
8.0
0.0
0.0
0.0
6.3


P14
4.7
3.6
88.1
0.0
88.1
11.9 
0.0
0.0
0.0
6.2


P15
4.6
3.4
92.0
0.0
92.0
8.0
0.0
0.0
0.0
25.0


P16
4.4
3.3
94.5
0.0
94.5
5.5
0.0
0.0
0.0
6.8


P17
4.5
3.6
95.4
0.0
95.4
4.6
0.0
0.0
0.0
6.4


P18
4.5
3.7
91.2
0.0
91.2
8.8
0.0
0.0
0.0
6.6


P19
4.6
3.5
93.0
0.0
93.0
7.0
0.0
0.0
0.0
6.7


P20

5.8


4.8

93.6
0.0
93.6
6.4
0.0
0.0
0.0
18.0


P21
4.3
3.7
83.0
0.0
83.0
17.0 
0.0
0.0
0.0
6.4


P22

5.8


4.8

84.7
0.0
84.7
15.3 
0.0
0.0
0.0
19.0


P23
4.3
3.8
80.0
0.0
80.0
16.0 
0.0
2.0
4.0
6.5


P24
4.4
3.5
97.6
0.0
97.6
2.4
0.0
0.0
0.0
6.6


P25
4.3
3.3
96.6
0.0
96.6
3.4
0.0
0.0
0.0
6.7


P26
4.3
3.4
97.6
0.0
97.6
2.4
0.0
0.0
0.0
6.3


P27
4.4
3.5
95.0
0.0
95.0
5.0
0.0
0.0
0.0
6.5


P28

5.2


4.8

44.0
51.0
95.0
4.3
0.0
0.0
0.7
10.0


P29
4.3
3.3
90.0
0.0
90.0
10.0 
0.0
0.0
0.0
6.2


P30
4.4
3.4
81.0
0.0
81.0
19.0 
0.0
0.0
0.0
6.3


P31
4.5
3.6
93.6
0.0
93.6
6.4
0.0
0.0
0.0
6.9


P32

6.8


5.1

94.9
0.0
94.9
5.1
0.0
0.0
0.0
15.0


P33
4.6
3.7
93.6
0.0
93.6
6.4
0.0
0.0
0.0
6.6


P34
4.7
3.9
94.2
0.0
94.2
5.8
0.0
0.0
0.0
6.5


P35

7.1


5.8

97.2
0.0
97.2
2.8
0.0
0.0
0.0
14.0


P36
4.8
3.8
94.2
0.0
94.2
5.8
0.0
0.0
0.0
6.3


P37
4.7
3.8
78.0
0.0
78.0
22.0 
0.0
0.0
0.0
6.5


P38
4.4
3.7
71.0
0.0
71.0
21.0 
0.0
0.0
8.0
6.6


P39
4.6
3.6
94.5
0.0
94.5
5.5
0.0
0.0
0.0
6.7


P40
4.3
3.3
75.0
0.0
75.0
25.0 
0.0
0.0
0.0
6.4


P41
4.4
3.4
97.6
0.0
97.6
2.4
0.0
0.0
0.0
6.8








P42
Cracks occur during Hot rolling


P43
Cracks occur during Hot rolling


P44
Cracks occur during Hot rolling


P45
Cracks occur during Hot rolling













SIZE OF METALLOGRAPHIC




STRUCTURE















VOLUME


AREA FRACTION




AVERAGE


WHERE La/Lb



PRODUCTION
DIAMETER/
dia/
dis/
≤5.0 IS



No.
μm
μm
μm
SATISFIED/%






P1
14.3
1.3
11.0
56.0



P2
13.8
1.2
10.0
56.0



P3
31.1

15.0

33.0
53.0



P4
31.7

20.0

35.0
53.0



P5
23.0






P6
23.0






P7
13.8
0.8
13.0
55.0



P8
41.0

15.0

35.0
43.0



P9
36.8

15.0

35.0
53.0



P10
13.8
1.0
14.0
54.0



P11
14.0
1.1
11.0
54.0



P12
31.7

14.0

34.0
56.0



P13
14.5
1.0
14.0
54.0



P14
14.3
1.2
12.0
53.0



P15
57.5
10.6 
28.0
78.0



P16
15.6
1.2
10.0
54.0



P17
14.7
1.2
9.0
58.0



P18
15.2
1.6
12.0
51.0



P19
15.4
1.3
10.0
51.0



P20
41.4

16.0

36.0
51.0



P21
14.7
1.1
18.0
50.0



P22
43.7

15.5

35.5
75.0



P23
15.0
1.2
19.0
51.0



P24
15.2
1.4
6.0
51.0



P25
15.4
1.0
9.0
51.0



P26
14.5
1.1
8.0
55.0



P27
15.0
1.2
7.0
51.0



P28
23.0
10.0 
30.0
51.0



P29
14.3
1.9
13.0
51.0



P30
14.5
1.4
18.0
51.0



P31
15.9
1.0
13.0
51.0



P32
34.5

13.5

32.0
51.0



P33
15.2
1.1
11.0
51.0



P34
15.0
1.4
8.0
56.0



P35
32.2

13.3

30.0
51.0



P36
14.5
0.9
13.0
55.0



P37
15.0
1.1
25.0
55.0



P38
15.2
1.1
23.0
55.0



P39
15.4
1.3
9.0
55.0



P40
14.7
1.4
20.0
56.0



P41
15.6
1.0
8.0
55.0











P42
Cracks occur during Hot rolling




P43
Cracks occur during Hot rolling




P44
Cracks occur during Hot rolling




P45
Cracks occur during Hot rolling


















TABLE 16









AREA FRACTION OF METALLOGRAPHIC STRUCTURE
















PHASE WITH
AREA






EXCEPTION
FRACTION


PRODUCTION
TEXTURE


OF F, B,
OF COARSE

















No.
D1/—
D2/—
F/%
B/%
F + B/%
fM/%
P/%
γ/%
AND M/%
GRAINS/%





P46
4.6
3.2
14.4
85.6

100.0


0.0

0.0
0.0
0.0
10.0


P47
4.5
3.3
7.6
92.4

100.0


0.0

0.0
0.0
0.0
10.0


P48
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P49
4.5
3.5
75.0
12.0
87.0
1.7
0.0
0.0
11.3
9.5


P50
4.4
3.4
81.0
12.0
93.0
1.9
0.0
0.0
5.1
9.0


P51
4.9
3.8
81.0
10.0
91.0
1.5
0.0
0.0
7.5
7.5


P52
4.2
3.2
78.0
17.0
95.0
2.0
0.0
0.0
3.0
8.0


P53
4.0
3.0
79.0
13.0
92.0
1.7
0.0
0.0
6.3
7.5


P54
3.8
2.8
83.0
10.0
93.0
1.8
0.0
0.0
5.2
7.3


P55
4.4
3.4
82.0
13.0
95.0
2.3
0.0
0.0
2.7
9.0


P56
3.7
2.7
79.0
18.0
97.0
1.5
0.0
0.0
1.5
7.2


P57
4.2
3.2
81.0
12.0
93.0
1.8
0.0
0.0
5.2
8.0


P58
3.9
2.9
75.0
17.0
92.0
2.0
0.0
0.0
6.0
7.4


P59
4.6
3.6
75.0
14.0
89.0
2.1
0.0
0.0
8.9
9.0


P60
3.7
2.7
95.0
3.0
98.0
2.0
0.0
0.0
0.0
12.0


P61
3.7
2.7
22.0
75.0
97.0
2.0
1.0
0.0
1.0
7.2


P62
3.7
2.7
35.0
2.0
37.0
60.0 
0.0
3.0
3.0
7.2


P63
3.8
2.8
75.0
22.0
97.0
3.0
0.0
0.0
0.0
5.0


P64
4.0
3.0
75.0
15.0
90.0
2.3
0.0
0.0
7.7
14.0


P65
3.8
2.8
76.0
17.0
93.0
1.7
0.0
0.0
5.3
15.0


P66
3.5
2.5
82.0
12.0
94.0
1.5
0.0
0.0
4.5
10.0


P67
3.3
2.3
76.0
11.0
87.0
1.6
0.0
0.0
11.4
9.5


P68
3.1
2.1
82.0
10.0
92.0
1.5
0.0
0.0
6.5
9.3


P69
3.7
2.7
78.0
18.0
96.0
2.0
0.0
0.0
2.0
11.0


P70
3.0
2.0
77.0
17.0
94.0
1.9
0.0
0.0
4.1
9.2


P71
3.5
2.5
82.0
14.0
96.0
2.2
0.0
0.0
1.8
10.0


P72
3.2
2.2
75.0
12.0
87.0
1.9
0.0
0.0
11.1
9.4


P73
3.9
2.9
78.0
17.0
95.0
1.5
0.0
0.0
3.5
11.0


P74
3.0
2.0
95.0
3.0
98.0
2.0
0.0
0.0
0.0
9.2


P75
3.0
2.0
22.0
75.0
97.0
2.0
1.0
0.0
1.0
9.2


P76
3.0
2.0
35.0
2.0
37.0
60.0 
0.0
3.0
3.0
9.2


P77
2.9
1.9
75.0
22.0
97.0
3.0
0.0
0.0
0.0
9.7


P78

5.8


4.8

81.0
14.0
95.0
1.9
0.0
0.0
3.1
20.0


P79

5.8


4.8

75.0
10.0
85.0
2.2
0.0
0.0
12.8
20.0


P80

5.8


4.8

79.0
18.0
97.0
2.0
0.0
0.0
1.0
14.0


P81

5.8


4.8

83.0
14.0
97.0
1.7
0.0
0.0
1.3
20.0


P82

5.8


4.8

79.0
12.0
91.0
1.8
0.0
0.0
7.2
14.0


P83
4.7
3.7
79.0
12.0
91.0
1.6
0.0
0.0
7.4
20.0


P84
4.7
3.7
81.0
11.0
92.0
1.6
0.0
0.0
6.4
20.0


P85

5.8


4.8

77.0
18.0
95.0
1.6
0.0
0.0
3.4
14.0


P86
4.0
3.1
76.0
16.0
92.0
1.5
0.0
0.0
6.5
20.0


P87
4.5
2.9
78.0
14.0
92.0
2.0
0.0
0.0
6.0
20.0


P88
4.8
3.5
21.5
2.0

23.5


71.0

0.0
5.5
5.5
12.0


P89
4.0
3.0
21.5
2.0

23.5


71.0

0.0
5.5
5.5
12.0


P90
4.3
2.6
95.0
2.0
97.0
1.0
0.0
0.0
2.0
20.0













SIZE OF METALLOGRAPHIC




STRUCTURE















VOLUME


AREA FRACTION




AVERAGE


WHERE La/Lb



PRODUCTION
DIAMETER/
dia/
dis/
≤5.0 IS



No.
μm
μm
μm
SATISFIED/%






P46
23.0






P47
23.0






P48
29.5
7.5
27.0
51.0



P49
28.5
7.0
26.5
53.0



P50
27.5
6.5
26.0
54.0



P51
22.0
5.5
25.5
55.0



P52
25.0
6.0
25.8
55.0



P53
22.0
5.5
25.5
56.0



P54
20.0
5.3
25.0
57.0



P55
27.5
6.5
26.0
54.0



P56
19.0
5.2
25.0
57.5



P57
25.0
6.0
25.8
55.0



P58
21.0
5.4
25.3
56.0



P59
27.5
6.5
26.0
54.0



P60
29.5
5.0
24.5
58.0



P61
19.0
5.2
25.0
57.5



P62
19.0
1.0
25.0
57.5



P63
15.0
4.2
24.3
59.5



P64
31.0
8.0
27.5
51.0



P65
35.0
8.5
28.0
50.6



P66
26.5
6.5
26.3
55.0



P67
23.5
6.0
26.0
56.0



P68
21.5
5.8
25.5
57.0



P69
29.0
7.0
26.5
54.0



P70
20.5
5.7
25.5
57.5



P71
26.5
6.5
26.3
55.0



P72
22.5
5.9
25.8
56.0



P73
29.0
7.0
26.5
54.0



P74
20.5
5.5
25.0
58.0



P75
20.5
5.7
25.5
57.5



P76
20.5
1.0
25.0
57.5



P77
22.5
6.0
26.2
57.3



P78
40.0

15.0

35.0
50.0



P79
40.0

15.0

35.0
50.0



P80
40.0

15.0

35.0
50.0



P81
42.0

15.0

35.0
45.0



P82
29.5
10.0 
30.0
45.0



P83
40.0

15.0

35.0
50.0



P84
40.0

15.0

35.0
50.0



P85
29.5
10.0 
30.0
50.0



P86
40.0

15.0

35.0
50.0



P87
40.0

15.0

35.0
50.0



P88
29.5

15.0

27.0
51.0



P89
29.5

15.0

27.0
51.0



P90
40.0
7.5
27.0
51.0

















TABLE 17








AREA FRACTION OF METALLOGRAPHIC STRUCTURE














PHASE WITH
AREA





EXCEPTION
FRACTION


PRODUCTION
TEXTURE

OF F, B,
OF COARSE

















No.
D1/—
D2/—
F/%
B/%
F + B/%
fM/%
P/%
γ/%
AND M/%
GRAINS/%





P91

5.8


4.8

75.0
2.0
77.0
3.0
20.0
0.0
20.0
12.0


P92
4.4
3.2
77.0
23.0

100.0


0.0

0.0
0.0
0.0
12.0


P93
4.5
3.3
77.0
23.0

100.0


0.0

0.0
0.0
0.0
12.0


P94

5.1


4.1

75.0
10.0
85.0
2.4
0.0
0.0
12.6
22.0


P95

5.1


4.1

75.0
19.0
94.0
1.6
0.0
0.0
4.4
22.0


P96

5.1


4.1

79.0
17.0
96.0
1.9
0.0
0.0
2.1
22.0


P97

5.1


4.1

75.0
10.0
85.0
2.3
0.0
0.0
12.7
16.0


P98

5.1


4.1

76.0
10.0
86.0
2.1
0.0
0.0
11.9
18.0


P99
4.2
2.8
84.0
13.0
97.0
2.2
0.0
0.0
0.8
22.0


P100
4.0
3.1
75.0
18.0
93.0
2.0
0.0
0.0
5.0
22.0


P101

5.1


4.1

75.0
14.0
89.0
1.8
0.0
0.0
9.2
16.0


P102
4.2
2.8
76.0
18.0
94.0
2.1
0.0
0.0
3.9
22.0


P103
4.0
2.9
75.0
12.0
87.0
1.8
0.0
0.0
11.2
22.0


P104
4.9
3.7
21.5
2.0

23.5


71.0

0.0
5.5
5.5
14.0


P105
4.4
3.3
21.5
2.0

23.5


71.0

0.0
5.5
5.5
14.0


P106
4.5
3.1
95.0
2.0
97.0
1.0
0.0
0.0
2.0
22.0


P107

5.1


4.1

75.0
2.0
77.0
3.0
20.0
0.0
20.0
14.0


P108
4.0
3.0
77.0
23.0

100.0


0.0

0.0
0.0
0.0
14.0


P109
4.0
3.0
77.0
23.0

100.0


0.0

0.0
0.0
0.0
14.0


P110
4.1
3.2
76.5
23.3

99.8


0.2

0.0
0.0
0.0
21.0


P111
4.1
2.8
80.0
17.0
97.0
3.0
0.0
0.0
0.0
21.0


P112
4.3
3.3
75.0
19.0
94.0
2.4
0.0
0.0
3.6
26.0


P113
4.1
3.1
82.0
10.0
92.0
1.6
0.0
0.0
6.4
29.0


P114
4.6
3.6
83.0
10.0
93.0
1.5
0.0
0.0
5.5
28.0


P115
4.6
3.7
76.0
12.0
88.0
2.4
0.0
0.0
9.6
28.0


P116
4.7
3.0
79.0
17.0
96.0
1.9
0.0
0.0
2.1
22.0


P117
4.4
3.6
83.0
14.0
97.0
2.1
0.0
0.0
0.9
22.0








P118
Cracks occur during Hot rolling

















P119
4.2
2.8
82.0
15.0
97.0
1.8
0.0
0.0
1.2
20.0


P120
4.5
3.0
84.0
13.0
97.0
2.1
0.0
0.0
0.9
23.0


P121
4.1
2.4
83.0
14.0
97.0
2.4
0.0
0.0
0.6
22.0


P122
4.4
3.0
75.0
17.0
92.0
2.1
0.0
0.0
5.9
29.0


P123
4.0
3.1
79.0
12.0
91.0
2.2
0.0
0.0
6.8
22.0


P124
4.9
4.0
81.0
16.0
97.0
2.2
0.0
0.0
0.8
21.0


P125
4.0
2.5
79.0
13.0
92.0
1.7
0.0
0.0
6.3
29.0


P126

5.8


4.8

77.0
15.0
92.0
2.4
0.0
0.0
5.6
24.0


P127

5.8


4.8

78.0
13.0
91.0
1.5
0.0
0.0
7.5
24.0


P128

5.8


4.8

79.0
10.0
89.0
2.0
0.0
0.0
9.0
26.0


P129
4.1
2.4
77.0
15.0
92.0
2.1
0.0
0.0
5.9
28.0


P130
4.2
3.4
77.0
16.0
93.0
2.3
0.0
0.0
4.7
22.0


P131
4.1
2.6
84.0
12.0
96.0
1.7
0.0
0.0
2.3
29.0


P132
4.7
3.4
75.0
18.0
93.0
1.9
0.0
0.0
5.1
20.0


P133
4.6
2.9
84.0
12.0
96.0
1.7
0.0
0.0
2.3
27.0


P134
4.3
2.7
83.0
14.0
97.0
2.4
0.0
0.0
0.6
25.0


P135
4.2
3.3
80.0
14.0
94.0
2.2
0.0
0.0
3.8
29.0













SIZE OF METALLOGRAPHIC




STRUCTURE















VOLUME


AREA FRACTION




AVERAGE


WHERE La/Lb



PRODUCTION
DIAMETER/
dia/
dis/
≤5.0 IS



No.
μm
μm
μm
SATISFIED/%






P91
29.5
7.5
27.0
51.0



P92
29.5






P93
29.5






P94
41.5

15.5

35.5
50.0



P95
41.5

15.5

35.5
50.0



P96
43.5

15.5

35.5
45.0



P97
31.0
10.5 
30.5
45.0



P98
34.0
10.5 
30.5
51.0



P99
41.5

15.5

35.5
50.0



P100
41.5

15.5

35.5
50.0



P101
31.0
10.5 
30.5
50.0



P102
41.5

15.5

35.5
50.0



P103
41.5

15.5

35.5
50.0



P104
31.0

15.5

27.5
51.0



P105
31.0

15.5

27.5
51.0



P106
41.5
8.0
27.5
51.0



P107
31.0
8.0
27.5
51.0



P108
31.0






P109
31.0






P110
37.0
7.3
28.0
52.0



P111
42.0
7.7
25.0
54.0



P112
36.0
7.8
26.0
56.0



P113
40.0
7.9
25.0
55.0



P114
37.0
7.0
26.0
59.0



P115
35.0
7.2
23.0
56.0



P116
39.0
7.8
27.0
53.0



P117
41.0
7.0
24.0
55.0











P118
Cracks occur during Hot rolling














P119
42.0
7.0
22.0
52.0



P120
42.0
7.7
20.0
56.0



P121
43.0
7.0
28.0
51.0



P122
40.0
7.5
21.0
51.0



P123
39.0
7.3
22.0
53.0



P124
44.0
7.7
28.0
53.0



P125
39.0
7.1
20.0
53.0



P126
44.0
7.3
25.0
58.0



P127
35.0
7.8
26.0
56.0



P128
37.0
7.7
27.0
52.0



P129
35.0
7.0
21.0
53.0



P130
43.0
7.6
21.0
57.0



P131
36.0
7.9
23.0
58.0



P132
40.0
7.4
22.0
53.0



P133
43.0
7.4
27.0
50.0



P134
38.0
7.8
21.0
56.0



P135
36.0
7.0
25.0
54.0

















TABLE 18








AREA FRACTION OF METALLOGRAPHIC STRUCTURE














PHASE WITH
AREA





EXCEPTION
FRACTION


PRODUCTION
TEXTURE

OF F, B,
OF COARSE

















No.
D1/—
D2/—
F/%
B/%
F + B/%
fM/%
P/%
γ/%
AND M/%
GRAINS/%





P136
4.5
3.5
82.0
15.0
97.0
2.2
0.0
0.0
0.8
26.0








P137
Cracks occur during Hot rolling


P138
Cracks occur during Hot rolling

















P139
4.0
2.8
76.0
13.0
89.0
2.1
0.0
0.0
8.9
26.0


P140
4.1
3.4
75.0
11.0
86.0
2.0
0.0
0.0
12.0
21.0


P141
4.5
4.0
83.0
14.0
97.0
1.8
0.0
0.0
1.2
24.0


P142
4.5
3.3
84.0
13.0
97.0
1.5
0.0
0.0
1.5
25.0


P143
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P144
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P145
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P146
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P147
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P148
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P149
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P150
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P151
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P152
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P153
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P154
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P155
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P156
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P157
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P158
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P159
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P160
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P161
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P162
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P163
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P164
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P165
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P166
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P167
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P168
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P169
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P170
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P171
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P172
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P173
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P174
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P175
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P176
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P177
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P178
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P179
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0


P180
4.7
3.7
75.0
11.0
86.0
2.2
0.0
0.0
11.8
12.0













SIZE OF METALLOGRAPHIC




STRUCTURE













VOLUME


AREA FRACTION



AVERAGE


WHERE La/Lb


PRODUCTION
DIAMETER/
dia/
dis/
≤5.0 IS


No.
μm
μm
μm
SATISFIED/%





P136
39.0
7.1
26.0
56.0









P137
Cracks occur during Hot rolling



P138
Cracks occur during Hot rolling












P139
35.0
7.3
28.0
58.0


P140
43.0
7.3
21.0
52.0


P141
35.0
7.6
29.0
50.0


P142
44.0
7.1
24.0
54.0


P143
29.5
7.5
27.0
51.0


P144
29.5
7.5
27.0
51.0


P145
29.5
7.5
27.0
51.0


P146
29.5
7.5
27.0
51.0


P147
29.5
7.5
27.0
51.0


P148
29.5
7.5
27.0
51.0


P149
29.5
7.5
27.0
51.0


P150
29.5
7.5
27.0
51.0


P151
29.5
7.5
27.0
51.0


P152
29.5
7.5
27.0
51.0


P153
29.5
7.5
27.0
51.0


P154
29.5
7.5
27.0
51.0


P155
29.5
7.5
27.0
51.0


P156
29.5
7.5
27.0
51.0


P157
29.5
7.5
27.0
51.0


P158
29.5
7.5
27.0
51.0


P159
29.5
7.5
27.0
51.0


P160
29.5
7.5
27.0
51.0


P161
29.5
7.5
27.0
51.0


P162
29.5
7.5
27.0
51.0


P163
29.5
7.5
27.0
51.0


P164
29.5
7.5
27.0
51.0


P165
29.5
7.5
27.0
51.0


P166
29.5
7.5
27.0
51.0


P167
29.5
7.5
27.0
51.0


P168
29.5
7.5
27.0
51.0


P169
29.5
7.5
27.0
51.0


P170
29.5
7.5
27.0
51.0


P171
29.5
7.5
27.0
51.0


P172
29.5
7.5
27.0
51.0


P173
29.5
7.5
27.0
51.0


P174
29.5
7.5
27.0
51.0


P175
29.5
7.5
27.0
51.0


P176
29.5
7.5
27.0
51.0


P177
29.5
7.5
27.0
51.0


P178
29.5
7.5
27.0
51.0


P179
29.5
7.5
27.0
51.0


P180
29.5
7.5
27.0
51.0



















TABLE 19








PRODUCTION
LANKFORD-VLAUE















No.
rL/—
rC/—
r30/—
r60/—
REMARKS






P1
0.78
0.80
1.10
1.10
EXAMPLE



P2
0.68
0.70
1.10
1.00
EXAMPLE



P3
0.54
0.56
1.65
1.70
COMPARATIVE EXAMPLE



P4
0.78
0.80
1.40
1.42
COMPARATIVE EXAMPLE



P5
0.52
0.54
1.67
1.69
COMPARATIVE EXAMPLE



P6
0.78
0.80
1.40
1.42
COMPARATIVE EXAMPLE



P7
0.68
0.70
1.20
1.20
EXAMPLE



P8
0.48
0.50
1.60
1.58
COMPARATIVE EXAMPLE



P9
0.52
0.54
1.67
1.69
COMPARATIVE EXAMPLE



P10
0.68
0.70
1.00
1.00
EXAMPLE



P11
0.68
0.70
1.20
1.10
EXAMPLE



P12
0.52
0.54
1.67
1.69
COMPARATIVE EXAMPLE



P13
0.68
0.70
1.00
1.00
EXAMPLE



P14
0.68
0.70
1.00
1.00
EXAMPLE



P15
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P16
0.68
0.70
1.10
1.10
EXAMPLE



P17
0.68
0.70
1.10
1.10
EXAMPLE



P18
0.68
0.70
1.10
1.10
EXAMPLE



P19
0.98
1.00
1.00
1.00
EXAMPLE



P20
0.52
0.54
1.67
1.69
COMPARATIVE EXAMPLE



P21
0.68
0.70
1.00
1.00
EXAMPLE



P22
0.52
0.54
1.67
1.69
COMPARATIVE EXAMPLE



P23
0.69
0.71
1.00
1.00
EXAMPLE



P24
0.68
0.70
1.10
1.10
EXAMPLE



P25
0.69
0.71
1.10
1.10
EXAMPLE



P26
0.68
0.70
1.10
1.10
EXAMPLE



P27
0.68
0.70
1.10
1.10
EXAMPLE



P28
0.48
0.50
1.58
1.57
COMPARATIVE EXAMPLE



P29
0.68
0.70
1.00
1.00
EXAMPLE



P30
0.68
0.70
1.10
1.00
EXAMPLE



P31
0.69
0.71
1.00
1.00
EXAMPLE



P32
0.46
0.48
1.66
1.67
COMPARATIVE EXAMPLE



P33
0.68
0.70
1.00
1.00
EXAMPLE



P34
0.68
0.70
1.00
1.00
EXAMPLE



P35
0.57
0.59
1.55
1.60
COMPARATIVE EXAMPLE



P36
0.68
0.70
1.00
1.00
EXAMPLE



P37
0.68
0.70
1.00
1.00
EXAMPLE



P38
0.68
0.70
1.00
1.00
EXAMPLE



P39
0.68
0.70
1.00
1.00
EXAMPLE



P40
0.68
0.70
1.10
1.10
EXAMPLE



P41
0.68
0.70
1.00
1.00
EXAMPLE












P42
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE



P43
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE



P44
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE



P45
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE













MECHANICAL PROPERTIES




















STANDARD











HARDNESS
DEVIATION










PRODUCTION
H OF
RATIO OF
TS/



TS × u-EL/
TS × EL/
TS × λ/



No.
FERRITE/—
HARDNESS/—
MPa
u-EL/%
EL/%
λ/%
MPa %
MPa %
MPa %
REMARKS





P1
232
0.23
540
15
35.2
102.7
8100
19008
55458
EXAMPLE


P2
228
0.23
582
14
32.7
115.3
8148
19031
67105
EXAMPLE


P3
233
0.23
525
9
26.2
58.1
4725
13755
30503
COMPARATIVE EXAMPLE


P4
228
0.23
1207
2
10.7
3.3
2414
12915
3983
COMPARATIVE EXAMPLE


P5
220
0.22
450
7
21.0
53.0
3150
9450
23850
COMPARATIVE EXAMPLE


P6
233
0.23
489
7
21.0
66.0
3423
10269
32274
COMPARATIVE EXAMPLE


P7
224
0.22
524
19
36.3
112.4
9956
19021
58898
EXAMPLE


P8
228
0.23
577
8
23.0
43.0
4616
13271
24811
COMPARATIVE EXAMPLE


P9
228
0.23
525
9
24.0
55.4
4725
12600
29085
COMPARATIVE EXAMPLE


P10
249
0.25
567
18
33.5
115.8
10206
18995
65659
EXAMPLE


P11
253
0.25
531
18
35.8
107.8
9558
19010
57242
EXAMPLE


P12
253
0.25
550
5
20.6
54.5
2750
11330
29975
COMPARATIVE EXAMPLE


P13
256
0.26
560
18
33.9
100.2
10080
18984
56112
EXAMPLE


P14
250
0.25
659
13
30.2
109.4
8567
19902
72095
EXAMPLE


P15
251
0.25
405
15
33.3
70.0
6075
13487
28350
COMPARATIVE EXAMPLE


P16
259
0.26
529
17
35.9
112.5
8993
18991
59513
EXAMPLE


P17
257
0.26
518
22
36.7
119.6
11396
19011
61953
EXAMPLE


P18
240
0.24
600
17
31.7
122.6
10200
19020
73560
EXAMPLE


P19
244
0.24
552
17
34.4
110.8
9384
18989
61162
EXAMPLE


P20
244
0.24
519
8
23.0
55.1
4152
11937
28597
COMPARATIVE EXAMPLE


P21
250
0.25
698
17
27.2
100.6
11866
18986
70219
EXAMPLE


P22
236
0.24
430
7
21.0
64.0
3010
9030
27520
COMPARATIVE EXAMPLE


P23
282
0.28
734
13
25.9
83.4
9542
19011
61216
EXAMPLE


P24
269
0.27
485
19
39.2
115.0
9215
19012
55775
EXAMPLE


P25
271
0.27
496
20
38.3
105.0
9920
18997
52080
EXAMPLE


P26
296
0.30
522
23
39.2
119.4
12006
20462
62327
EXAMPLE


P27
297
0.30
485
23
36.4
109.6
11155
17654
53156
EXAMPLE


P28
312
0.31
495
8
23.0
36.4
3960
11385
18018
COMPARATIVE EXAMPLE


P29
265
0.26
760
10
25.0
96.1
7600
19000
73036
EXAMPLE


P30
284
0.28
780
15
24.4
92.0
11700
19032
71760
EXAMPLE


P31
291
0.29
536
20
35.4
100.0
10720
18974
53600
EXAMPLE


P32
281
0.28
499
7
22.0
55.5
3493
10978
27695
COMPARATIVE EXAMPLE


P33
291
0.29
543
15
35.0
113.8
8145
19005
61793
EXAMPLE


P34
275
0.28
536
16
35.4
119.6
8576
18974
64106
EXAMPLE


P35
273
0.27
479
7
22.0
57.0
3353
10538
27303
COMPARATIVE EXAMPLE


P36
279
0.28
530
20
35.9
108.5
10600
19027
57505
EXAMPLE


P37
253
0.25
846
9
22.5
66.9
7614
19035
56597
EXAMPLE


P38
285
0.29
794
11
23.9
69.6
8734
18977
55262
EXAMPLE


P39
250
0.25
532
19
35.7
124.4
10108
18992
66181
EXAMPLE


P40
232
0.23
888
14
21.4
72.0
12432
19003
63936
EXAMPLE


P41
261
0.26
485
26
39.2
121.0
12610
19012
58685
EXAMPLE









P42
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE


P43
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE


P44
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE


P45
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE













OTHERS














PRODUCTION

Rm45/
TS/fM ×




No.
d/RmC/—
RmC/—
dis/dia/—
REMARKS






P1
1.3
1.7
714
EXAMPLE



P2
1.2
1.8
545
EXAMPLE



P3
0.8
2.3

165

COMPARATIVE EXAMPLE



P4
1.6
1.3
30
COMPARATIVE EXAMPLE



P5
0.8
2.3

COMPARATIVE EXAMPLE



P6
1.8
1.0

COMPARATIVE EXAMPLE



P7
1.4
1.5
1703 
EXAMPLE



P8
0.5
2.7

151

COMPARATIVE EXAMPLE



P9
0.5
2.7

175

COMPARATIVE EXAMPLE



P10
1.5
1.4
992
EXAMPLE



P11
1.3
1.7
932
EXAMPLE



P12
0.7
2.5
954
COMPARATIVE EXAMPLE



P13
1.5
1.4
980
EXAMPLE



P14
1.6
1.3
554
EXAMPLE



P15
1.5
1.4

134

COMPARATIVE EXAMPLE



P16
1.9
0.9
802
EXAMPLE



P17
1.6
1.3
845
EXAMPLE



P18
1.5
1.4
511
EXAMPLE



P19
1.9
0.9
607
EXAMPLE



P20
0.4
2.9

182

COMPARATIVE EXAMPLE



P21
1.2
1.8
672
EXAMPLE



P22
0.6
2.6
64
COMPARATIVE EXAMPLE



P23
1.6
1.3
726
EXAMPLE



P24
1.4
1.5
866
EXAMPLE



P25
1.3
1.7
1313 
EXAMPLE



P26
1.6
1.3
1582 
EXAMPLE



P27
1.7
1.2
566
EXAMPLE



P28
0.9
2.2

345

COMPARATIVE EXAMPLE



P29
1.6
1.3
520
EXAMPLE



P30
1.7
1.2
528
EXAMPLE



P31
1.6
1.3
1089 
EXAMPLE



P32
0.4
2.9

232

COMPARATIVE EXAMPLE



P33
1.5
1.4
848
EXAMPLE



P34
1.5
1.4
528
EXAMPLE



P35
0.3
3.0

386

COMPARATIVE EXAMPLE



P36
1.1
1.9
1320 
EXAMPLE



P37
1.2
1.8
874
EXAMPLE



P38
1.6
1.3
791
EXAMPLE



P39
1.5
1.4
670
EXAMPLE



P40
1.1
1.9
507
EXAMPLE



P41
1.6
1.3
1617 
EXAMPLE











P42
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE



P43
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE



P44
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE



P45
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE



















TABLE 20








PRODUCTION
LANKFORD-VLAUE















No.
rL/—
rC/—
r30/—
r60/—
REMARKS






P46
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P47
0.76
0.78
1.42
1.43
COMPARATIVE EXAMPLE



P48
0.74
0.76
1.44
1.45
EXAMPLE



P49
0.76
0.78
1.42
1.43
EXAMPLE



P50
0.78
0.80
1.40
1.42
EXAMPLE



P51
0.72
0.74
1.46
1.48
EXAMPLE



P52
0.84
0.85
1.35
1.36
EXAMPLE



P53
0.86
0.87
1.33
1.34
EXAMPLE



P54
0.89
0.91
1.29
1.31
EXAMPLE



P55
0.78
0.80
1.40
1.42
EXAMPLE



P56
0.92
0.92
1.28
1.28
EXAMPLE



P57
0.84
0.85
1.35
1.36
EXAMPLE



P58
0.86
0.87
1.33
1.34
EXAMPLE



P59
0.76
0.77
1.43
1.44
EXAMPLE



P60
0.92
0.92
1.28
1.28
EXAMPLE



P61
0.92
0.92
1.28
1.28
EXAMPLE



P62
0.92
0.92
1.28
1.28
EXAMPLE



P63
0.90
0.92
1.28
1.29
EXAMPLE



P64
0.89
0.91
1.29
1.31
EXAMPLE



P65
0.95
0.96
1.24
1.25
EXAMPLE



P66
0.98
1.00
1.20
1.22
EXAMPLE



P67
1.00
1.01
1.19
1.20
EXAMPLE



P68
1.04
1.04
1.16
1.16
EXAMPLE



P69
0.92
0.94
1.26
1.28
EXAMPLE



P70
1.06
1.07
1.13
1.14
EXAMPLE



P71
0.98
1.00
1.20
1.22
EXAMPLE



P72
1.00
1.01
1.19
1.20
EXAMPLE



P73
0.90
0.92
1.28
1.29
EXAMPLE



P74
1.06
1.07
1.13
1.14
EXAMPLE



P75
1.06
1.07
1.13
1.14
EXAMPLE



P76
1.06
1.07
1.13
1.14
EXAMPLE



P77
1.08
1.09
1.11
1.12
EXAMPLE



P78
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P79
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P80
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P81
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P82
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P83
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P84
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P85
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P86
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P87
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P88
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P89
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P90
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE













MECHANICAL PROPERTIES




















STANDARD











HARDNESS
DEVIATION










PRODUCTION
H OF
RATIO OF
TS/



TS × u-EL/
TS × EL/
TS × λ/



No.
FERRITE/—
HARDNESS/—
MPa
u-EL/%
EL/%
λ/%
MPa %
MPa %
MPa %
REMARKS





P46
302
0.30
654
7
21.0
41.8
4578
13734
27337
COMPARATIVE EXAMPLE


P47
302
0.30
555
8
23.0
23.2
4440
12765
12876
COMPARATIVE EXAMPLE


P48
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P49
220
0.23
610
16
31.0
73.0
9760
18910
44530
EXAMPLE


P50
220
0.23
620
17
33.0
74.0
10540
20460
45880
EXAMPLE


P51
220
0.23
630
18
34.0
67.0
11340
21420
42210
EXAMPLE


P52
220
0.23
625
18
34.0
79.0
11250
21250
49375
EXAMPLE


P53
220
0.22
630
19
36.0
80.0
11970
22680
50400
EXAMPLE


P54
220
0.21
640
20
37.0
82.0
12800
23680
52480
EXAMPLE


P55
220
0.21
620
17
33.0
74.0
10540
20460
45880
EXAMPLE


P56
220
0.18
645
21
39.0
83.0
13545
25155
53535
EXAMPLE


P57
220
0.21
620
18
34.0
79.0
11160
21080
48980
EXAMPLE


P58
220
0.21
640
20
37.0
81.0
12800
23680
51840
EXAMPLE


P59
190
0.21
620
17
33.0
72.0
10540
20460
44640
EXAMPLE


P60
220
0.18
580
25
45.0
85.0
14500
26100
49300
EXAMPLE


P61
220
0.18
900
18
34.0
95.0
16200
30600
85500
EXAMPLE


P62
220
0.18
1220
8
12.0
65.0
9760
14640
79300
EXAMPLE


P63
220
0.18
655
23
42.0
81.0
15065
27510
53055
EXAMPLE


P64
220
0.23
590
12
26.0
80.0
7080
15340
47200
EXAMPLE


P65
220
0.23
560
13
25.0
81.0
7280
14000
45360
EXAMPLE


P66
220
0.23
600
14
28.0
88.0
8400
16800
52800
EXAMPLE


P67
220
0.22
610
15
29.0
89.0
9150
17690
54290
EXAMPLE


P68
220
0.21
620
16
31.0
91.0
9920
19220
56420
EXAMPLE


P69
220
0.21
600
13
27.0
85.0
7800
16200
51000
EXAMPLE


P70
220
0.18
625
17
33.0
94.0
10625
20625
58750
EXAMPLE


P71
220
0.21
600
14
28.0
88.0
8400
16800
52800
EXAMPLE


P72
220
0.21
620
16
31.0
90.0
9920
19220
55800
EXAMPLE


P73
190
0.21
600
13
27.0
81.0
7800
16200
48600
EXAMPLE


P74
220
0.18
560
21
39.0
94.0
11760
21840
52640
EXAMPLE


P75
220
0.18
880
14
16.0
104.0
12320
14080
91520
EXAMPLE


P76
220
0.18
1200
8
12.0
74.0
9600
14400
88800
EXAMPLE


P77
220
0.18
615
16
31.0
94.5
9840
19065
58118
EXAMPLE


P78
220
0.23
460
9
24.3
51.0
4140
11178
23460
COMPARATIVE EXAMPLE


P79
220
0.24
460
9
23.8
51.0
4140
10948
23460
COMPARATIVE EXAMPLE


P80
220
0.24
460
9
23.9
55.0
4140
10994
25300
COMPARATIVE EXAMPLE


P81
220
0.22
470
9
23.8
55.0
4230
11186
25850
COMPARATIVE EXAMPLE


P82
230
0.23
470
9
23.9
57.0
4230
11233
26790
COMPARATIVE EXAMPLE


P83
220
0.23
460
9
24.0
65.0
4140
11040
29900
COMPARATIVE EXAMPLE


P84
220
0.23
460
9
23.9
65.0
4140
10994
29900
COMPARATIVE EXAMPLE


P85
240
0.22
490
9
24.3
50.0
4410
11907
24500
COMPARATIVE EXAMPLE


P86
220
0.23
460
9
23.6
65.0
4140
10856
29900
COMPARATIVE EXAMPLE


P87
220
0.24
460
9
24.4
65.0
4140
11224
29900
COMPARATIVE EXAMPLE


P88
220
0.23
1290
1
11.0
65.0
1290
14190
83850
COMPARATIVE EXAMPLE


P89
220
0.24
1290
1
10.0
65.0
1290
12900
83850
COMPARATIVE EXAMPLE


P90
220
0.24
425
15
29.0
66.0
6375
12325
28050
COMPARATIVE EXAMPLE













OTHERS














PRODUCTION

Rm45/
TS/fM ×




No.
d/RmC/—
RmC/—
dis/dia/—
REMARKS






P46
1.6
1.3

COMPARATIVE EXAMPLE



P47
1.6
1.3

COMPARATIVE EXAMPLE



P48
1.4
1.5
 982
EXAMPLE



P49
1.6
1.3
1358
EXAMPLE



P50
1.7
1.2
1305
EXAMPLE



P51
1.3
1.7
1947
EXAMPLE



P52
1.8
1.0
1344
EXAMPLE



P53
1.9
0.9
1718
EXAMPLE



P54
2.0
0.8
1677
EXAMPLE



P55
1.7
1.2
1078
EXAMPLE



P56
2.0
0.7
2067
EXAMPLE



P57
1.8
1.0
1481
EXAMPLE



P58
1.9
0.9
1499
EXAMPLE



P59
1.5
1.4
1181
EXAMPLE



P60
2.2
0.5
1421
EXAMPLE



P61
2.5
0.5
2163
EXAMPLE



P62
1.4
0.9
 508
EXAMPLE



P63
2.0
0.8
1263
EXAMPLE



P64
1.9
0.9
 882
EXAMPLE



P65
2.0
0.8
1085
EXAMPLE



P66
2.3
0.4
1618
EXAMPLE



P67
2.3
0.3
1652
EXAMPLE



P68
2.4
0.3
1817
EXAMPLE



P69
2.1
0.6
1136
EXAMPLE



P70
2.5
0.4
1472
EXAMPLE



P71
2.3
0.4
1103
EXAMPLE



P72
2.3
0.3
1427
EXAMPLE



P73
2.0
0.8
1514
EXAMPLE



P74
2.6
0.4
1273
EXAMPLE



P75
2.8
0.5
1968
EXAMPLE



P76
1.8
0.5
 500
EXAMPLE



P77
2.6
0.2
 895
EXAMPLE



P78
0.6
2.6
 565
COMPARATIVE EXAMPLE



P79
0.6
2.6
488
COMPARATIVE EXAMPLE



P80
0.6
2.6
 537
COMPARATIVE EXAMPLE



P81
0.6
2.6
 645
COMPARATIVE EXAMPLE



P82
0.6
2.6
 783
COMPARATIVE EXAMPLE



P83
1.4
1.5
 671
COMPARATIVE EXAMPLE



P84
1.4
1.5
 671
COMPARATIVE EXAMPLE



P85
0.6
2.6
 919
COMPARATIVE EXAMPLE



P86
1.9
0.9
 716
COMPARATIVE EXAMPLE



P87
1.6
1.3
 537
COMPARATIVE EXAMPLE



P88
1.3
1.7
33
COMPARATIVE EXAMPLE



P89
1.9
0.9
33
COMPARATIVE EXAMPLE



P90
1.1
1.9
1530
COMPARATIVE EXAMPLE




















TABLE 21








PRODUCTION
LANKFORD-VLAUE
















No.
rL/—
rC/—
r30/—
r60/—
REMARKS






P91
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P92
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P93
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P94
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P95
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P96
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P97
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P98
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P99
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P100
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P101
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P102
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P103
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P104
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P105
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P106
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P107
0.68
0.66
1.52
1.54
COMPARATIVE EXAMPLE



P108
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P109
0.89
0.91
1.29
1.31
COMPARATIVE EXAMPLE



P110
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P111
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P112
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P113
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P114
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P115
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P116
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P117
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE












P118
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE














P119
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P120
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P121
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P122
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P123
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P124
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P125
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P126
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P127
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P128
0.52
0.56
1.66
1.69
COMPARATIVE EXAMPLE



P129
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P130
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P131
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P132
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P133
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P134
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE



P135
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE













MECHANICAL PROPERTIES




















STANDARD











HARDNESS
DEVIATION










PRODUCTION
H OF
RATIO OF
TS/



TS × u-EL/
TS × EL/
TS × λ/



No.
FERRITE/—
HARDNESS/—
MPa
u-EL/%
EL/%
λ/%
MPa %
MPa %
MPa %
REMARKS





P91
220
0.23
500
8
22.0
55.0
4000
11000
27500
COMPARATIVE EXAMPLE


P92
220
0.22
430
7
21.0
66.0
3010
9030
28380
COMPARATIVE EXAMPLE


P93
220
0.23
430
7
21.0
66.0
3010
9030
28380
COMPARATIVE EXAMPLE


P94
220
0.23
440
5
19.0
62.0
2200
8360
27280
COMPARATIVE EXAMPLE


P95
220
0.24
440
5
19.0
62.0
2200
8360
27280
COMPARATIVE EXAMPLE


P96
220
0.23
450
7
21.0
58.0
3150
9450
26100
COMPARATIVE EXAMPLE


P97
230
0.23
450
7
21.0
55.0
3150
9450
24750
COMPARATIVE EXAMPLE


P98
220
0.23
430
8
22.0
63.0
3440
9460
27090
COMPARATIVE EXAMPLE


P99
220
0.23
440
7
21.0
75.0
3080
9240
33000
COMPARATIVE EXAMPLE


P100
220
0.23
440
7
21.0
75.0
3080
9240
33000
COMPARATIVE EXAMPLE


P101
240
0.23
470
5
19.0
64.0
2350
8930
30080
COMPARATIVE EXAMPLE


P102
220
0.22
440
7
21.0
75.0
3080
9240
33000
COMPARATIVE EXAMPLE


P103
220
0.23
440
7
21.0
75.0
3080
9240
33000
COMPARATIVE EXAMPLE


P104
220
0.23
1270
1
10.0
65.0
1270
12700
82550
COMPARATIVE EXAMPLE


P105
220
0.22
1270
1
10.0
65.0
1270
12700
82550
COMPARATIVE EXAMPLE


P106
220
0.23
405
11
23.0
75.0
4455
9315
30375
COMPARATIVE EXAMPLE


P107
220
0.22
480
4
18.0
64.0
1920
8640
30720
COMPARATIVE EXAMPLE


P108
220
0.23
410
3
17.0
75.0
1230
6970
30750
COMPARATIVE EXAMPLE


P109
220
0.23
410
3
17.0
75.0
1230
6970
30750
COMPARATIVE EXAMPLE


P110
220
0.23
410
7
21.0
66.0
2870
8610
27060
COMPARATIVE EXAMPLE


P111
220
0.22
850
8
22.0
62.0
6800
18700
52700
COMPARATIVE EXAMPLE


P112
220
0.23
430
15
29.0
71.0
6450
12470
30530
COMPARATIVE EXAMPLE


P113
220
0.23
850
8
22.0
62.0
6800
18700
52700
COMPARATIVE EXAMPLE


P114
204
0.24
430
15
29.0
71.0
6450
12470
30530
COMPARATIVE EXAMPLE


P115
220
0.24
850
8
22.0
62.0
6800
18700
52700
COMPARATIVE EXAMPLE


P116
220
0.22
590
8
22.0
62.0
4720
12980
36580
COMPARATIVE EXAMPLE


P117
220
0.23
590
11
29.0
62.0
6490
17110
36580
COMPARATIVE EXAMPLE









P118
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE

















P119
220
0.23
765
8
22.3
56.0
6041
17054
42825
COMPARATIVE EXAMPLE


P120
220
0.22
600
9
21.7
56.0
5460
13020
33600
COMPARATIVE EXAMPLE


P121
220
0.22
771
7
21.5
64.0
5626
16570
49326
COMPARATIVE EXAMPLE


P122
220
0.23
771
9
22.1
59.0
6782
17033
45472
COMPARATIVE EXAMPLE


P123
220
0.24
767
8
22.3
57.0
6138
17110
43733
COMPARATIVE EXAMPLE


P124
220
0.23
772
8
22.1
57.0
6172
17050
43976
COMPARATIVE EXAMPLE


P125
220
0.24
766
8
21.6
55.0
6050
16541
42119
COMPARATIVE EXAMPLE


P126
220
0.23
770
9
21.6
55.0
7007
16632
42350
COMPARATIVE EXAMPLE


P127
220
0.23
888
8
22.2
55.0
7283
19717
48849
COMPARATIVE EXAMPLE


P128
220
0.23
930
9
21.5
55.0
8459
19986
51127
COMPARATIVE EXAMPLE


P129
220
0.22
776
8
22.3
64.0
6204
17294
49633
COMPARATIVE EXAMPLE


P130
220
0.23
771
8
22.0
62.0
6169
16964
47809
COMPARATIVE EXAMPLE


P131
220
0.23
773
9
21.5
64.0
6568
16613
49452
COMPARATIVE EXAMPLE


P132
220
0.23
777
7
22.0
64.0
5669
17084
49700
COMPARATIVE EXAMPLE


P133
220
0.22
774
8
22.2
63.0
6192
17184
48764
COMPARATIVE EXAMPLE


P134
220
0.24
776
8
21.9
62.0
6204
16984
48083
COMPARATIVE EXAMPLE


P135
220
0.24
770
8
22.4
62.0
5855
17256
47761
COMPARATIVE EXAMPLE













OTHERS














PRODUCTION

Rm45/
TS/fM ×




No.
d/RmC/—
RmC/—
dis/dia/—
REMARKS






P91
0.6
2.6
 600
COMPARATIVE EXAMPLE



P92
1.9
0.9

COMPARATIVE EXAMPLE



P93
2.0
0.8

COMPARATIVE EXAMPLE



P94
0.9
2.2
420
COMPARATIVE EXAMPLE



P95
0.9
2.2
 630
COMPARATIVE EXAMPLE



P96
0.9
2.2
 542
COMPARATIVE EXAMPLE



P97
0.9
2.2
 568
COMPARATIVE EXAMPLE



P98
0.9
2.2
 595
COMPARATIVE EXAMPLE



P99
1.6
1.3
458
COMPARATIVE EXAMPLE



P100
1.6
1.3
 504
COMPARATIVE EXAMPLE



P101
0.9
2.2
 758
COMPARATIVE EXAMPLE



P102
1.6
1.3
480
COMPARATIVE EXAMPLE



P103
1.6
1.3
 560
COMPARATIVE EXAMPLE



P104
1.1
2.0
32
COMPARATIVE EXAMPLE



P105
1.1
2.0
32
COMPARATIVE EXAMPLE



P106
1.6
1.3
1392
COMPARATIVE EXAMPLE



P107
0.9
2.2
 550
COMPARATIVE EXAMPLE



P108
2.2
0.5

COMPARATIVE EXAMPLE



P109
2.3
0.4

COMPARATIVE EXAMPLE



P110
1.8
1.0
7863
COMPARATIVE EXAMPLE



P111
1.9
0.9
 920
COMPARATIVE EXAMPLE



P112
1.6
1.3
 597
COMPARATIVE EXAMPLE



P113
1.8
1.0
1681
COMPARATIVE EXAMPLE



P114
1.5
1.4
1065
COMPARATIVE EXAMPLE



P115
1.5
1.4
1131
COMPARATIVE EXAMPLE



P116
1.4
1.5
1075
COMPARATIVE EXAMPLE



P117
1.7
1.2
 963
COMPARATIVE EXAMPLE











P118
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE













P119
1.8
1.0
1335
COMPARATIVE EXAMPLE



P120
1.6
1.3
 742
COMPARATIVE EXAMPLE



P121
1.9
0.9
1285
COMPARATIVE EXAMPLE



P122
1.7
1.2
1028
COMPARATIVE EXAMPLE



P123
1.9
0.9
1051
COMPARATIVE EXAMPLE



P124
1.1
1.9
1275
COMPARATIVE EXAMPLE



P125
1.9
0.9
1269
COMPARATIVE EXAMPLE



P126
0.6
2.6
1099
COMPARATIVE EXAMPLE



P127
0.6
2.6
1974
COMPARATIVE EXAMPLE



P128
0.6
2.6
1630
COMPARATIVE EXAMPLE



P129
1.9
0.9
1108
COMPARATIVE EXAMPLE



P130
1.8
1.0
 926
COMPARATIVE EXAMPLE



P131
1.9
0.9
1323
COMPARATIVE EXAMPLE



P132
1.4
1.5
1215
COMPARATIVE EXAMPLE



P133
1.5
1.4
1661
COMPARATIVE EXAMPLE



P134
1.6
1.3
 870
COMPARATIVE EXAMPLE



P135
1.8
1.0
1251
COMPARATIVE EXAMPLE


















TABLE 22







PRODUCTION
LANKFORD-VLAUE













No.
rL/—
rC/—
r30/—
r60/—
REMARKS





P136
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE










P137
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE


P138
Cracks occur during Hot rolling

COMPARATIVE EXAMPLE












P139
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE


P140
0.74
0.76
1.44
1.45
COMPARATIVE EXAMPLE


P141
0.74
0.76
1.44
1.45
EXAMPLE


P142
0.74
0.76
1.44
1.45
EXAMPLE


P143
0.74
0.76
1.44
1.45
EXAMPLE


P144
0.74
0.76
1.44
1.45
EXAMPLE


P145
0.74
0.76
1.44
1.45
EXAMPLE


P146
0.74
0.76
1.44
1.45
EXAMPLE


P147
0.74
0.76
1.44
1.45
EXAMPLE


P148
0.74
0.76
1.44
1.45
EXAMPLE


P149
0.74
0.76
1.44
1.45
EXAMPLE


P150
0.74
0.76
1.44
1.45
EXAMPLE


P151
0.74
0.76
1.44
1.45
EXAMPLE


P152
0.74
0.76
1.44
1.45
EXAMPLE


P153
0.74
0.76
1.44
1.45
EXAMPLE


P154
0.74
0.76
1.44
1.45
EXAMPLE


P155
0.74
0.76
1.44
1.45
EXAMPLE


P156
0.74
0.76
1.44
1.45
EXAMPLE


P157
0.74
0.76
1.44
1.45
EXAMPLE


P158
0.74
0.76
1.44
1.45
EXAMPLE


P159
0.74
0.76
1.44
1.45
EXAMPLE


P160
0.74
0.76
1.44
1.45
EXAMPLE


P161
0.74
0.76
1.44
1.45
EXAMPLE


P162
0.74
0.76
1.44
1.45
EXAMPLE


P163
0.74
0.76
1.44
1.45
EXAMPLE


P164
0.74
0.76
1.44
1.45
EXAMPLE


P165
0.74
0.76
1.44
1.45
EXAMPLE


P166
0.74
0.76
1.44
1.45
EXAMPLE


P167
0.74
0.76
1.44
1.45
EXAMPLE


P168
0.74
0.76
1.44
1.45
EXAMPLE


P169
0.74
0.76
1.44
1.45
EXAMPLE


P170
0.74
0.76
1.44
1.45
EXAMPLE


P171
0.74
0.76
1.44
1.45
EXAMPLE


P172
0.74
0.76
1.44
1.45
EXAMPLE


P173
0.74
0.76
1.44
1.45
EXAMPLE


P174
0.74
0.76
1.44
1.45
EXAMPLE


P175
0.74
0.76
1.44
1.45
EXAMPLE


P176
0.74
0.76
1.44
1.45
EXAMPLE


P177
0.74
0.76
1.44
1.45
EXAMPLE


P178
0.74
0.76
1.44
1.45
EXAMPLE


P179
0.74
0.76
1.44
1.45
EXAMPLE


P180
0.74
0.76
1.44
1.45
EXAMPLE













MECHANICAL PROPERTIES




















STANDARD











HARDNESS
DEVIATION










PRODUCTION
H OF
RATIO OF
TS/



TS × u-EL/
TS × EL/
TS × λ/



No.
FERRITE/—
HARDNESS/—
MPa
u-EL/%
EL/%
λ/%
MPa %
MPa %
MPa %
REMARKS





P136
220
0.22
772
8
22.3
64.0
6097
17210
49391
COMPARATIVE EXAMPLE









P137
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE


P138
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE

















P139
220
0.23
600
11
23.0
62.0
6600
13800
37200
COMPARATIVE EXAMPLE


P140
220
0.23
600
11
23.0
62.0
6600
13800
37200
COMPARATIVE EXAMPLE


P141
220
0.24
750
14
28.0
68.0
10500
21000
51000
EXAMPLE


P142
220
0.23
750
15
29.0
69.0
11250
21750
51750
EXAMPLE


P143
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P144
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P145
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P146
220
0.23
655
15
29.0
71.0
9825
18995
46505
EXAMPLE


P147
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P148
220
0.23
660
15
29.0
71.0
9900
19140
46860
EXAMPLE


P149
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P150
220
0.23
690
15
29.0
71.0
10350
20010
48990
EXAMPLE


P151
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P152
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P153
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P154
220
0.23
690
15
29.0
66.0
10350
20010
45540
EXAMPLE


P155
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P156
220
0.23
660
15
29.0
66.0
9900
19140
43560
EXAMPLE


P157
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P158
220
0.23
680
15
29.0
71.0
10200
19720
48280
EXAMPLE


P159
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P160
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P161
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P162
220
0.23
580
16
30.0
76.0
9280
17400
44080
EXAMPLE


P163
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P164
220
0.23
580
16
31.0
76.0
9280
17980
44080
EXAMPLE


P165
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P166
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P167
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P168
220
0.23
580
16
30.0
76.0
9280
17400
44080
EXAMPLE


P169
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P170
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P171
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P172
220
0.23
650
15
29.0
71.0
9750
18850
46150
EXAMPLE


P173
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P174
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P175
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P176
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P177
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P178
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P179
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE


P180
220
0.23
600
15
29.0
71.0
9000
17400
42600
EXAMPLE













OTHERS














PRODUCTION

Rm45/
TS/fM ×




No.
d/RmC/—
RmC/—
dis/dia/—
REMARKS






P136
1.6
1.3
1285
COMPARATIVE EXAMPLE











P137
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE



P138
Cracks occur during Hot rolling
COMPARATIVE EXAMPLE













P139
1.9
0.9
1096
COMPARATIVE EXAMPLE



P140
1.9
0.9
863
COMPARATIVE EXAMPLE



P141
1.6
1.3
1590
EXAMPLE



P142
1.6
1.3
1690
EXAMPLE



P143
1.4
1.5
982
EXAMPLE



P144
1.3
1.5
1064
EXAMPLE



P145
1.4
1.5
982
EXAMPLE



P146
1.3
1.5
1072
EXAMPLE



P147
1.4
1.5
982
EXAMPLE



P148
1.3
1.5
1080
EXAMPLE



P149
1.4
1.5
982
EXAMPLE



P150
1.4
1.5
1129
EXAMPLE



P151
1.4
1.5
982
EXAMPLE



P152
1.3
1.5
1064
EXAMPLE



P153
1.4
1.5
982
EXAMPLE



P154
1.3
1.5
1129
EXAMPLE



P155
1.4
1.5
982
EXAMPLE



P156
1.3
1.5
1080
EXAMPLE



P157
1.4
1.5
982
EXAMPLE



P158
1.4
1.5
1113
EXAMPLE



P159
1.4
1.5
982
EXAMPLE



P160
1.3
1.5
1064
EXAMPLE



P161
1.4
1.5
982
EXAMPLE



P162
1.5
1.5
949
EXAMPLE



P163
1.4
1.5
982
EXAMPLE



P164
1.5
1.5
949
EXAMPLE



P165
1.4
1.5
982
EXAMPLE



P166
1.3
1.5
1064
EXAMPLE



P167
1.4
1.5
982
EXAMPLE



P168
1.5
1.5
949
EXAMPLE



P169
1.4
1.5
982
EXAMPLE



P170
1.3
1.5
1064
EXAMPLE



P171
1.4
1.5
982
EXAMPLE



P172
1.4
1.5
1064
EXAMPLE



P173
1.4
1.5
982
EXAMPLE



P174
1.4
1.5
982
EXAMPLE



P175
1.4
1.5
982
EXAMPLE



P176
1.4
1.5
982
EXAMPLE



P177
1.4
1.5
982
EXAMPLE



P178
1.4
1.5
982
EXAMPLE



P179
1.4
1.5
982
EXAMPLE



P180
1.4
1.5
982
EXAMPLE








Claims
  • 1. A hot-rolled steel sheet comprising, as a chemical composition, by mass %, C: 0.01% to 0.4%,Si: 0.001% to 2.5%,Mn: 0.001% to 4.0%,Al: 0.001% to 2.0%,P: limited to 0.15% or less,S: limited to 0.03% or less,N: limited to 0.01% or less,O: limited to 0.01% or less, anda balance comprising Fe and unavoidable impurities, wherein:an average pole density of an orientation group of {100}<011>to {223}<110>, which is a pole density represented by an arithmetic average of pole densities of each crystal orientation {100}<011>, {116}<110>, {114}<110>, {112}<110>, and {223}<110>, is 1.0 to 5.0, and a pole density of a crystal orientation {332}<113>is 1.0 to 4.0 in a thickness central portion, which is a thickness range of ⅝ to ⅜ based on a surface of the steel sheet;the steel sheet includes, as a metallographic structure, plural grains, and includes, by area %, 30% to 99% in total of a ferrite and a bainite, and 1% to 70% of a martensite; andan area fraction of the martensite is defined as fM in unit of area %, an average size of the martensite is defined as dia in unit of μm, an average distance between the martensite is defined as dis in unit of μm, and a tensile strength of the steel sheet is defined as TS in unit of MPa, and a following Expression 1 and a following Expression 2 are satisfied: dia≤13 μm  (Expression 1)TS/fM×dis/dia≥500  (Expression 2).
  • 2. The hot-rolled steel sheet according to claim 1, further comprising, as the chemical composition, by mass %, at least one selected from the group consisting of: Mo: 0.001% to 1.0%,Cr: 0.001% to 2.0%,Ni: 0.001% to 2.0%,Cu: 0.001% to 2.0%,B: 0.0001% to 0.005%,Nb: 0.001% to 0.2%,Ti: 0.001% to 0.2%,V: 0.001% to 1.0%,W: 0.001% to 1.0%,Ca: 0.0001% to 0.01%,Mg: 0.0001% to 0.01%,Zr: 0.0001% to 0.2%,Rare Earth Metal: 0.0001% to 0.1%,As: 0.0001% to 0.5%,Co: 0.0001% to 1.0%,Sn: 0.0001% to 0.2%,Pb: 0.0001% to 0.2%,Y: 0.0001% to 0.2%, andHf: 0.0001% to 0.2%.
  • 3. The hot-rolled steel sheet according to claim 1, wherein a volume average diameter of the grains is 5 μm to 30 μm.
  • 4. The hot-rolled steel sheet according to claim 1, wherein the average pole density of the orientation group of {100}<011>to {223}<110>is 1.0 to 4.0, and the pole density of the crystal orientation {332}<113>is 1.0 to 3.0.
  • 5. The hot-rolled steel sheet according to claim 1, wherein a major axis of the martensite is defined as La, a minor axis of the martensite is defined as Lb, and an area fraction of the martensite satisfying a following Expression 3 is 50% to 100% as compared with the area fraction fM of the martensite: La/Lb≤5.0  (Expression 3).
  • 6. The hot-rolled steel sheet according to claim 1, wherein the steel sheet includes, as the metallographic structure, by area %, 30% to 99% of the ferrite.
  • 7. The hot-rolled steel sheet according to claim 1, wherein the steel sheet includes, as the metallographic structure, by area %, 5% to 80% of the bainite.
  • 8. The hot-rolled steel sheet according to claim 1, wherein the steel sheet includes a tempered martensite in the martensite.
  • 9. The hot-rolled steel sheet according to claim 1, wherein an area fraction of coarse grains having a grain size of more than 35 μm is 0% to 10% among the grains in the metallographic structure of the steel sheet.
  • 10. The hot-rolled steel sheet according to claim 1, wherein a hardness H of the ferrite under a load of 1 mN in a nano-indenter satisfies a following Expression 4: H<200+30×[Si]+21×[Mn]+270×[P]+78×[Nb]1/2+108×[Ti]1/2  (Expression 4).
  • 11. The hot-rolled steel sheet according to claim 1, wherein a hardness of the ferrite or the bainite which is a primary phase is measured at 100 points or more under a load of 1 mN in a nano-indenter, and a value dividing a standard deviation of the hardness by an average of the hardness is 0.2 or less.
  • 12. The hot-rolled steel sheet according to claim 2, wherein a volume average diameter of the grains is 5 μm to 30 μm.
  • 13. The hot-rolled steel sheet according to claim 2, wherein the average pole density of the orientation group of {100}<011>to {223 } <110>is 1.0 to 4.0, and the pole density of the crystal orientation {332}<113>is 1.0 to 3.0.
  • 14. The hot-rolled steel sheet according to claim 2, wherein a major axis of the martensite is defined as La, a minor axis of the martensite is defined as Lb, and an area fraction of the martensite satisfying a following Expression 3 is 50% to 100% as compared with the area fraction fM of the martensite: La/Lb≤5.0  (Expression 3).
  • 15. The hot-rolled steel sheet according to claim 2, wherein the steel sheet includes, as the metallographic structure, by area %, 30% to 99% of the ferrite.
  • 16. The hot-rolled steel sheet according to claim 2, wherein the steel sheet includes, as the metallographic structure, by area %, 5% to 80% of the bainite.
  • 17. The hot-rolled steel sheet according to claim 2, wherein the steel sheet includes a tempered martensite in the martensite.
  • 18. The hot-rolled steel sheet according to claim 2, wherein an area fraction of coarse grains having a grain size of more than 35 μm is 0% to 10% among the grains in the metallographic structure of the steel sheet.
  • 19. The hot-rolled steel sheet according to claim 2, wherein a hardness H of the ferrite under a load of 1 mN in a nano-indenter satisfies a following Expression 4: H<200+30×[Si]+21×[Mn]+270×[P]+78×[Nb]1/2+108×[Ti]1/2  (Expression 4).
  • 20. The hot-rolled steel sheet according to claim 2, wherein a hardness of the ferrite or the bainite which is a primary phase is measured at 100 points or more under a load of 1 mN in a nano-indenter, and a value dividing a standard deviation of the hardness by an average of the hardness is 0.2 or less.
Priority Claims (1)
Number Date Country Kind
2011-117432 May 2011 JP national
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Divisional of U.S. patent application Ser. No. 14/119,124, filed on Jan. 8, 2014, which is the National Phase of PCT International Application No. PCT/JP2012/063273, filed on May 24, 2012, and which claims priority under 35 U.S.C. 119(a) to Japanese Application No. 2011-117432, filed on May 25, 2011, all of which are hereby expressly incorporated by reference into the present application.

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Related Publications (1)
Number Date Country
20170191140 A1 Jul 2017 US
Divisions (1)
Number Date Country
Parent 14119124 US
Child 15460024 US