Hot-rolled steel sheet and method for producing same

Information

  • Patent Grant
  • 9631265
  • Patent Number
    9,631,265
  • Date Filed
    Thursday, May 24, 2012
    12 years ago
  • Date Issued
    Tuesday, April 25, 2017
    7 years ago
Abstract
A hot-rolled steel sheet satisfies that 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. Moreover, the hot-rolled steel sheet includes, as a metallographic structure, by area %, ferrite and bainite of 30% to 99% in total and martensite of 1% to 70%. Moreover, the hot-rolled steel sheet satisfies following Expressions 1 and 2 when area fraction of the martensite is defined as fM in unit of area %, average size of the martensite is defined as dia in unit of μm, 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. dia≦13 μm  (Expression 1)TS/fM×dis/dia≧500  (Expression 2)
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.


Priority is claimed on Japanese Patent Application No. 2011-117432, filed on May 25, 2011, and the content of which is incorporated herein by reference.


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, 0: 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≦13 μm  (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, 0: 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 t in 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×   (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 initial-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 CHEW 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 O 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 γ (austenite) to α (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 galvanized 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 μm 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 T1 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 galvanized 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 γ 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 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 15]


[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




STEEL


T1/°
Ar3
HARDNESS




No.
Y
Hf
C.
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
Pb





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










0.00009



S94









0.0050 


S95












S96












S97












S98























CALCULATED









VALUE OF




STEEL


T1/°
Ar3
HARDNESS




No.
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


851
763
235
EXAMPLE



S94


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 7-1









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




1000° C. TO 1200° C.
to T1 + 200° C.















FREQUENCY OF
EACH
GRAIN
CUMU-
FREQUENCY



PRODUC-
REDUCTION
REDUCTION
SIZE OF
LATIVE
OF


STEEL
TION
OF 40% OR
OF 40%
AUSTEN-
REDUC-
REDUC-


No.
No.
MORE/—
OR MORE/%
ITE/μm
TION/%
TION/—





S1
P1
1
50
150 
85
6


S1
P2
2
45/45
90
95
6


S1
P3
2
45/45
90

45

4


S1
P4
2
45/45
90
55
4


S1
P5
2
45/45
90
55
4


S1
P6
2
45/45
90
55
4


S2
P7
1
50
140 
85
6


S2
P8
2
45/45
80
75
6


S2
P9

0



250

65
6


S3
P10
2
45/45
80
75
6


S3
P11
2
45/45
80
85
6


S3
P12
2
45/45
80

45

4


S4
P13
2
45/45
80
75
6


S4
P14
2
45/45
80
85
6


S4
P15
2
45/45
80
85
6


S5
P16
2
45/45
95
85
6


S5
P17
2
45/45
95
95
6


S6
P18
2
45/45
90
85
6


S6
P19
2
45/45
90
95
6


S6
P20

0



300

85
6


S7
P21
3
40/40/40
75
80
6


S7
P22
3
40/40/40
75
80
6


S8
P23
3
40/40/40
70
80
6


S9
P24
2
45/40
95
80
6


S9
P25
1
50
120 
80
6


S10
P26
2
45/40
100 
80
6


S10
P27
1
50
120 
80
6


S10
P28
1
50
120 
80
6


S11
P29
3
40/40/40
70
95
6


S12
P30
3
40/40/40
75
95
6


S13
P31
3
40/40/40
65
95
6


S13
P32

0



350


45

4


S14
P33
3
40/40/40
70
95
6


S15
P34
2
45/45
70
85
6


S15
P35
2
45/45
120 

35

4


S16
P36
2
45/45
75
85
6


S17
P37
2
45/45
80
80
6


S18
P38
2
45/45
75
85
6


S19
P39
2
45/45
80
85
6


S20
P40
2
45/45
80
95
6


S21
P41
2
45/45
75
85
6









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 T1 + 30° C.




to T1 + 200° C.















FREQUENCY OF



MAXIMUM OF




REDUCTION
EACH


TEMPERATURE



STEEL
OF 30% OR
REDUC-


RISE BETWEEN



No.
MORE/—
TION/%
P1/%
Tf/° C.
PASSES/° C.






S1
2
20/20/25/25/30/40
40
935
15



S1
6
40/40/40/40/30/35
35
892
5



S1
1
7/7/8/30
30
930
20



S1
1
13/13/15/30
30
930
20



S1
1
13/13/15/30
30
930
20



S1
1
13/13/15/30
30
930
20



S2
2
15/15/25/25/40/40
40
935
15



S2

0

20/20/20/20/20/25


5



S2
2
5/8/10/10/30/30
30
850
18



S3
2
10/15/15/15/30/37
37
945
15



S3
2
25/25/25/25/30/31
31
920
18



S3
1
7/7/8/30
30
1075
15



S4
2
10/15/15/15/30/37
37
950
15



S4
2
25/25/25/25/30/31
31
922
18



S4
2
25/25/25/25/30/31
31
922
18



S5
2
25/25/25/25/30/31
31
955
13



S5
6
40/40/40/40/30/40
40
935
14



S6
2
25/25/25/25/30/30
30
955
13



S6
6
40/40/40/40/30/40
40
933
14



S6
2
25/25/25/25/30/30
30
890
13



S7
2
20/20/20/20/30/30
30
970
16



S7
2
20/20/20/20/30/30
30
970
16



S8
2
20/20/20/20/30/30
30
970
16



S9
2
20/20/20/20/30/30
30
961
17



S9
2
20/20/20/20/30/30
30
922
18



S10
2
15/15/18/20/30/40
40
960
17



S10
2
20/20/20/20/30/30
30
920
18



S10
2
20/20/20/20/30/30
30
920
18



S11
6
42/42/42/42/30/30
30
990
18



S12
6
42/42/42/42/30/30
30
990
18



S13
6
40/40/40/40/30/35
35
943
10



S13
1
5/5/6/35
35
910
30



S14
6
40/40/40/40/30/35
35
940
10



S15
2
20/20/25/25/30/40
40
1012
13



S15
1
2/2/3/30
30
880
12



S16
2
20/20/25/25/30/40
40
985
15



S17
2
15/15/18/20/30/40
40
958
10



S18
2
20/25/25/25/30/35
35
967
10



S19
2
20/20/25/25/30/40
40
996
12



S20
6
40/40/40/40/30/40
40
958
12



S21
2
20/25/25/25/30/35
35
985
12










S22
Cracks occur during Hot rolling



S23
Cracks occur during Hot rolling



S24
Cracks occur during Hot rolling



S25
Cracks occur during Hot rolling


















TABLE 7-2








ROLLING IN RANGE OF Ar3
FIRST-COOLING












To LOWER THAN T1 + 30° C.

AVERAGE



















PRODUC-

ROLLING




COOLING
COOLING
TEMPERATURE


STEEL
TION
CUMULATIVE
FINISH

2.5 ×


RATE/°
TEMPERATURE
AT COOLING


No.
No.
REDUCTION/%
TEMPERATURE/° C.
t1/s
t1/s
t/s
t/t1/—
C./second
CHANGE/° C.
FINISH/° C.




















S1
P1
0
935
0.57
1.41
0.45
0.80
133
110
825


S1
P2
0
892
1.74
4.35
1.39
0.80
108
 90
802


S1
P3
0
930
1.08
2.69
0.86
0.80
157
130
800


S1
P4
0
930
1.08
2.69
0.86
0.80
108
 90
840


S1
P5
0
930
1.08
2.69
0.86
0.80
157
130
800


S1
P6
7
920
1.08
2.69
0.86
0.80
157
130
790


S2
P7
0
935
0.57
1.43
0.10
0.18
 96
 80
855


S2
P8
0
891


1.06

120
100
791


S2
P9
0
850
3.14
7.85
2.51
0.80
120
100
750


S3
P10
0
945
0.75
1.88
0.46
0.61
108
 90
855


S3
P11
0
920
1.54
3.84
0.93
0.60
133
110
810


S3
P12
0
1075
0.20
0.50
0.16
0.79
133
110
965


S4
P13
7
940
0.67
1.67
0.40
0.60
145
120
820


S4
P14
0
922
1.50
3.74
0.90
0.60
108
 90
832


S4
P15
0
922
1.50
3.74
0.90
0.60
114
 95
827


S5
P16
0
955
0.75
1.87
0.44
0.58
120
100
855


S5
P17
0
935
0.72
1.80
0.42
0.58
108
 90
845


S6
P18
0
955
0.78
1.94
0.44
0.56
 96
 80
875


S6
P19
0
933
0.73
1.83
0.44
0.60
120
100
833


S6
P20
0
890
2.15
5.37
1.29
0.60
120
100
790


S7
P21
0
970
0.66
1.65
0.40
0.60
108
 90
880


S7
P22
0
970
0.66
1.65

2.00

3.03
24
20
950


S8
P23
0
970
0.66
1.66
0.40
0.60
133
110
860


S9
P24
0
961
0.73
1.82
0.44
0.60
133
110
851


S9
P25
0
922
1.44
3.59
0.86
0.60
145
120
802


S10
P26
0
960
0.74
1.85
0.70
0.95
114
 95
865


S10
P27
0
920
2.08
5.20
1.25
0.60
120
100
820


S10
P28
0
920
2.08
5.20
1.25
0.60
193

160

760


S11
P29
0
990
0.54
1.35
0.32
0.59
108
 90
900


S12
P30
0
990
0.76
1.89
0.46
0.61
108
 90
900


S13
P31
0
943
1.46
3.65
0.88
0.60
157
130
813


S13
P32
0
910
2.44
6.09
1.46
0.60
 96
 80
830


S14
P33
0
940
1.41
3.52
0.84
0.60
120
100
840


S15
P34
0
1012
0.25
0.62
0.15
0.61
120
100
912


S15
P35
0
880
3.90
9.76
2.35
0.60
108
 90
790


S16
P36
0
985
0.60
1.50
0.37
0.61
133
110
875


S17
P37
0
958
0.29
0.72
0.17
0.60
133
110
848


S18
P38
0
967
0.33
0.83
0.20
0.60
145
120
847


S19
P39
0
996
0.14
0.36
0.09
0.60
108
 90
906


S20
P40
0
958
0.29
0.72
0.17
0.60
114
 95
863


S21
P41
0
985
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 8-1









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




1000° C. TO 1200° C.
to T1 + 200° C.















FREQUENCY OF
EACH
GRAIN
CUMU-
FREQUENCY



PRODUC-
REDUCTION
REDUCTION
SIZE OF
LATIVE
OF


STEEL
TION
OF 40% OR
OF 40%
AUSTEN-
REDUC-
REDUC-


No.
No.
MORE/—
OR MORE/%
ITE/μm
TION/%
TION/—





S26
P46
2
45/45
80
65
6


S27
P47
2
45/45
80
70
6


S1
P48
1
45
180 
55
4


S1
P49
1
45
180 
55
4


S1
P50
1
45
180 
55
4


S1
P51
1
45
180 
55
4


S1
P52
2
45/45
90
55
4


S1
P53
2
45/45
90
75
5


S1
P54
2
45/45
90
80
6


S1
P55
2
45/45
90
80
6


S1
P56
2
45/45
90
80
6


S1
P57
2
45/45
90
80
6


S1
P58
2
45/45
90
80
6


S1
P59
2
45/45
90
80
6


S1
P60
2
45/45
90
80
6


S1
P61
2
45/45
90
80
6


S1
P62
2
45/45
90
80
6


S1
P63
2
45/45
90
80
6


S1
P64
1
45
180 
55
4


S1
P65
1
45
180 
55
4


S1
P66
2
45/45
90
55
4


S1
P67
2
45/45
90
75
5


S1
P68
2
45/45
90
80
6


S1
P69
2
45/45
90
80
6


S1
P70
2
45/45
90
80
6


S1
P71
2
45/45
90
80
6


S1
P72
2
45/45
90
80
6


S1
P73
2
45/45
90
80
6


S1
P74
2
45/45
90
80
6


S1
P75
2
45/45
90
80
6


S1
P76
2
45/45
90
80
6


S1
P77
2
45/45
90
80
6


S1
P78

0



250

55
4


S1
P79
1
45
180 

45

4


S1
P80
1
45
180 
55
4


S1
P81
1
45
180 
55
4


S1
P82
1
45
180 
55
4


S1
P83
1
45
180 
55
4


S1
P84
1
45
180 
55
4


S1
P85
1
45
180 
55
4


S1
P86
1
45
180 
55
4


S1
P87
1
45
180 
55
4


S1
P88
1
45
180 
55
4


S1
P89
1
45
180 
55
4


S1
P90
1
45
180 
55
4














ROLLING IN RANGE OF T1 + 30° C.




to T1 + 200° C.















FREQUENCY OF



MAXIMUM OF




REDUCTION



TEMPERATURE



STEEL
OF 30% OR
EACH


RISE BETWEEN



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






S26
2
3/5/5/5/30/40
40
956
10



S27
2
10/10/10/10/30/35
35
919
10



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
17



S1
1
13/13/15/30
30
935
17



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
17



S1
1
20/20/25/25/30
30
935
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
30/30/20/20/20/20
30
935
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
30/30/20/20/20/20
30
935
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/15/18/20/30/40
40
915
17



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
17



S1
1
20/20/25/25/30
30
935
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
30/30/20/20/20/20
30
935
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
20/20/20/20/30/30
30
935
17



S1
2
30/30/20/20/20/20
30
935
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/15/18/20/30/40
40
915
17



S1
2
15/16/18/20/30/40
40
915
17



S1
1
13/13/15/30
30
935
20



S1
1
7/7/8/30
30
935
20



S1

0

12/20/20/20


20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
760
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
995
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20


















TABLE 8-2








ROLLING IN RANGE OF Ar3
FIRST-COOLING












TO LOWER THAN T1 + 30° C.

AVERAGE



















PRODUC-

ROLLING




COOLING
COOLING
TEMPERATURE


STEEL
TION
CUMULATIVE
FINISH

2.5 ×


RATE/°
TEMPERATURE
AT COOLING


No.
No.
REDUCTION/%
TEMPERATURE/° C.
t1/s
t1/s
t/s
t/t1
C./second
CHANGE/° C.
FINISH/° C.





S26
P46
0
956
0.29
0.72
0.27
0.93
120
100 
856


S27
P47
0
919
1.14
2.84
0.68
0.60
120
100 
819


S1
P48
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P49
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P50
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P51
0
935
0.99
2.47
0.10
0.10
113
90
845


S1
P52
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P53
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P54
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P55
0
880
0.99
2.47
0.90
0.91
113
90
787


S1
P56
0
915
0.96
2.41
0.90
0.93
113
90
822


S1
P57
20 
890
0.99
2.47
0.90
0.91
113
90
797


S1
P58
8
890
0.99
2.47
0.90
0.91
113
90
797


S1
P59
0
830
0.99
2.47
0.90
0.91
113
45
782


S1
P60
0
915
0.96
2.41
0.90
0.93
113
90
822


S1
P61
0
915
0.96
2.41
0.90
0.93
113
90
822


S1
P62
0
915
0.96
2.41
0.90
0.93
113
90
822


S1
P63
0
915
0.96
2.41
0.50
0.52
113
90
824


S1
P64
0
935
0.99
2.47
1.10
1.11
113
90
842


S1
P65
0
935
0.99
2.47
2.40
2.43
113
90
838


S1
P66
0
935
0.99
2.47
1.10
1.11
113
90
842


S1
P67
0
935
0.99
2.47
1.10
1.11
113
90
842


S1
P68
0
935
0.99
2.47
1.10
1.11
113
90
842


S1
P69
0
880
0.99
2.47
1.10
1.11
113
90
787


S1
P70
0
915
0.96
2.41
1.10
1.14
113
90
822


S1
P71
20 
890
0.99
2.47
1.10
1.11
113
90
797


S1
P72
8
890
0.99
2.47
1.10
1.11
113
90
797


S1
P73
0
830
0.99
2.47
1.10
1.11
113
45
782


S1
P74
0
915
0.96
2.41
1.10
1.14
113
90
822


S1
P75
0
915
0.96
2.41
1.10
1.14
113
90
822


S1
P76
0
915
0.96
2.41
1.10
1.14
113
90
822


S1
P77
0
915
0.96
2.41
1.50
1.56
113
90
821


S1
P78
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P79
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P80
0
935


0.90

113
90
842


S1
P81

35

890
0.99
2.47
0.90
0.91
113
90
797


S1
P82
0

760

6.82
17.05 
6.20
0.91
113
45
696


S1
P83
0
935
0.99
2.47
0.90
0.91
45
90
842


S1
P84
0
935
0.99
2.47
0.90
0.91
113

35

897


S1
P85
0
935
0.99
2.47
0.90
0.91
113

145

787


S1
P86
0
995
0.26
0.64
0.24
0.91
 50
40

954



S1
P87
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P88
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P89
0
935
0.99
2.47
0.90
0.91
113
90
842


S1
P90
0
935
0.99
2.47
0.90
0.91
113
90
842



















TABLE 9-1









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




1000° C. TO 1200° C.
to T1 + 200° C.















FREQUENCY OF
EACH
GRAIN
CUMU-
FREQUENCY



PRODUC-
REDUCTION
REDUCTION
SIZE OF
LATIVE
OF


STEEL
TION
OF 40% OR
OF 40%
AUSTEN-
REDUC-
REDUC-


No.
No.
MORE/—
OR MORE/%
ITE/μm
TION/%
TION/—





S1
P91
1
45
180
55
4


S1
P92
1
45
180
55
4


S1
P93
1
45
180
55
4


S1
P94

0



250

55
4


S1
P95
1
45
180

45

4


S1
P96
1
45
180
55
4


S1
P97
1
45
180
55
4


S1
P98
1
45
180
55
4


S1
P99
1
45
180
55
4


S1
P100
1
45
180
55
4


S1
P101
1
45
180
55
4


S1
P102
1
45
180
55
4


S1
P103
1
45
180
55
4


S1
P104
1
45
180
55
4


S1
P105
1
45
180
55
4


S1
P106
1
45
180
55
4


S1
P107
1
45
180
55
4


S1
P108
1
45
180
55
4


S1
P109
1
45
180
55
4


S28
P110
1
45
180
55
4


S29
P111
1
45
180
55
4


S30
P112
1
45
180
55
4


S31
P113
1
45
180
55
4


S32
P114
1
45
180
55
4


S33
P115
1
45
180
55
4


S34
P116
1
45
180
55
4


S35
P117
1
45
180
55
4









S36
P118
Cracks occur during Hot rolling













S37
P119
1
45
180
55
4


S38
P120
1
45
180
55
4


S39
P121
1
45
180
55
4


S40
P122
1
45
180
55
4


S41
P123
1
45
180
55
4


S42
P124
1
45
180
55
4


S43
P125
1
45
180
55
4


S44
P126
1
45
180
55
4


S45
P127
1
45
180
55
4


S46
P128
1
45
180
55
4


S47
P129
1
45
180
55
4


S48
P130
1
45
180
55
4


S49
P131
1
45
180
55
4


S50
P132
1
45
180
55
4


S51
P133
1
45
180
55
4


S52
P134
1
45
180
55
4


S53
P135
1
45
180
55
4














ROLLING IN RANGE OF T1 + 30° C.




to T1 + 200° C.















FREQUENCY OF



MAXIMUM OF




REDUCTION
EACH


TEMPERATURE



STEEL
OF 30% OR
REDUC-


RISE BETWEEN



No.
MORE/—
TION/%
P1/%
Tf/° C.
PASSES/° C.






S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
7/7/8/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
760
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
995
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S1
1
13/13/15/30
30
935
20



S28
1
13/13/15/30
30
935
20



S29
1
13/13/15/30
30
935
20



S30
1
13/13/15/30
30
935
20



S31
1
13/13/15/30
30
935
20



S32
1
13/13/15/30
30
935
20



S33
1
13/13/15/30
30
935
20



S34
1
13/13/15/30
30
935
20



S35
1
13/13/15/30
30
935
20










S36
Cracks occur during Hot rolling














S37
1
13/13/15/30
30
935
20



S38
1
13/13/15/30
30
935
20



S39
1
13/13/15/30
30
935
20



S40
1
13/13/15/30
30
935
20



S41
1
13/13/15/30
30
935
20



S42
1
13/13/15/30
30
935
20



S43
1
13/13/15/30
30
935
20



S44
1
13/13/15/30
30
935
20



S45
1
13/13/15/30
30
935
20



S46
1
13/13/15/30
30
935
20



S47
1
13/13/15/30
30
935
20



S48
1
13/13/15/30
30
935
20



S49
1
13/13/15/30
30
935
20



S50
1
13/13/15/30
30
935
20



S51
1
13/13/15/30
30
935
20



S52
1
13/13/15/30
30
935
20



S53
1
13/13/15/30
30
935
20


















TABLE 9-2








ROLLING IN RANGE OF Ar3




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




















ROLLING




AVERAGE
COOLING
TEMPERATURE



PRO-

FINISH




COOLING
TEMPERATURE
AT COOLING


STEEL
DUCTION
CUMULATIVE
TEMPERATURE/

2.5 ×


RATE/
CHANGE/
FINISH/


No.
No.
REDUCTION/%
° C.
t1/s
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 10-1








ROLLING IN RANGE OF




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





















EACH







MAXIMUM OF




FREQUENCY
REDUC-


FRE-
FREQUENCY



TEMPERATURE



PRO-
OF
TION
GRAIN
CUMU-
QUENCY
OF



RISE



DUC-
REDUCTION
OF 40%
SIZE OF
LATIVE
OF
REDUCTION
EACH


BETWEEN


STEEL
TION
OF 40%
OR
AUSTENITE/
REDUC-
REDUC-
OF 30%
REDUC-
P1/
Tf/
PASSES/


No.
No.
OR MORE/—
MORE/%
μm
TION/%
TION/—
OR MORE/—
TION/%
%
° 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


















TABLE 10-2








ROLLING IN RANGE OF Ar3




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




















ROLLING




AVERAGE
COOLING
TEMPERATURE



PRODUC-

FINISH




COOLING
TEMPERATURE
AT COOLING


STEEL
TION
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
247
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


S98
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
















PRO-
TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE



DUC-
SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
COILING


TION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
TEMPERATURE/


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
















PRO-
TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE



DUC-
SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
COILING


TION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
TEMPERATURE/


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


P85
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
















PRO-
TIME UNTIL
AVERAGE
TEMPERATURE
AVERAGE

AVERAGE
TEMPERATURE



DUC-
SECOND
COOLING
AT COOLING
HOLDING

COOLING
AT COOLING
COILING


TION
COOLING
RATE/
FINISH/
TEMPERATURE/
HOLDING
RATE/
FINISH/
TEMPERATURE/


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 15-1








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 curing Hot rolling


P43
Cracks occur during Hot rolling


P44
Cracks occur during Hot rolling


P45
Cracks occur during Hot rolling

















TABLE 15-2








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 16-1








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

















TABLE 16-2








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 17-1








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 curing 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

















TABLE 17-2








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 18-1








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

















TABLE 18-2








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 19-1







PRO-




DUC-




TION
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
1.56
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


















TABLE 19-2








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
11
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
498
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
3980
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
19021
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


















TABLE 19-3







PRODUC-
OTHERS












TION
d/
Rm45/
TS/fM ×



No.
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
COMPARATIVE EXAMPLE



Hot rolling



P43
Cracks occur during
COMPARATIVE EXAMPLE



Hot rolling



P44
Cracks occur during
COMPARATIVE EXAMPLE



Hot rolling



P45
Cracks occur during
COMPARATIVE EXAMPLE



Hot rolling


















TABLE 20-1







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


















TABLE 20-2








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


















TABLE 20-3








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 21-1







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









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


















TABLE 21-2








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
8840
30720
COMPARATIVE EXAMPLE


P108
220
0.23
410
3
11.0
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
21060
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
16832
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


















TABLE 21-3








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 22-1







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


















TABLE 22-2








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


















TABLE 22-3








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 method for producing a hot-rolled steel sheet, comprising: 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, anda 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 t in 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]+2743×[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.
  • 2. The method for producing the hot-rolled steel sheet according to claim 1, wherein the waiting time t further satisfies a following Expression 10, 0≦t<t1  (Expression 10).
  • 3. The method for producing the hot-rolled steel sheet according to claim 1, wherein the waiting time t further satisfies a following Expression 11, t1≦t≦t1×2.5  (Expression 11).
  • 4. The method for producing the hot-rolled steel sheet according to claim 1, wherein, in the first-hot-rolling, at least two times of rollings whose reduction is 40% or more are conducted, and the average grain size of the austenite is controlled to 100 μm or less.
  • 5. The method for producing the hot-rolled steel sheet according to claim 1, wherein the second-cooling starts within 3 seconds after finishing the second-hot-rolling.
  • 6. The method for producing the hot-rolled steel sheet according to claim 1, wherein, in the second-hot-rolling, a temperature rise of the steel between passes is 18° C. or lower.
  • 7. The method for producing the hot-rolled steel sheet according to claim 1, wherein a final pass of rollings in the temperature range of T1+30° C. to T1+200° C. is the large reduction pass.
  • 8. The method for producing the hot-rolled steel sheet according to claim 1, wherein, in the holding, the steel is held in a temperature range of 600° C. to 680° C. for 3 seconds to 15 seconds.
  • 9. The method for producing the hot-rolled steel sheet according to claim 1, wherein the first-cooling is conducted at an interval between rolling stands.
  • 10. A method for producing a hot-rolled steel sheet, comprising: 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, andat 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%, anda balance consisting of Fe and unavoidable impurities;second-hot-rolling the steel under conditions such that, when a temperature calculated by a following Expression 9 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 t in 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]+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; 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.
Priority Claims (1)
Number Date Country Kind
2011-117432 May 2011 JP national
PCT Information
Filing Document Filing Date Country Kind 371c Date
PCT/JP2012/063273 5/24/2012 WO 00 1/8/2014
Publishing Document Publishing Date Country Kind
WO2012/161248 11/29/2012 WO A
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Related Publications (1)
Number Date Country
20140110022 A1 Apr 2014 US