Patent Publication Number: US-9896737-B2

Title: Hot-rolled steel sheet

Description:
TECHNICAL FIELD 
     The present invention relates to a hot-rolled steel sheet. 
     BACKGROUND ART 
     Conventionally, for the purpose of reducing the weight of automobile bodies, high-strength steel sheets have been often used for suspension parts or structural parts of automobile bodies. Suspension parts of automobiles are required to have fatigue characteristics of a notch-free material and notch fatigue characteristics, but there has been a problem in that conventional high-strength steel sheets are insufficient in such performance and do not allow parts to be reduced in sheet thickness. 
     To improve fatigue characteristics of a notch-free material, it is effective to make the structure finer. For example, Patent Literatures 1 and 2 describe hot-rolled steel sheets that contain ultrafine ferrite grains with an average grain size of less than 2 μm as hot-rolled. It is described that these steel sheets are excellent in ductility, toughness, fatigue strength, and the like, and have low anisotropy in these characteristics. In addition, since a fatigue crack occurs from near the surface, it is also effective to make the structure near the surface finer. Patent Literature 3 describes a hot-rolled steel sheet having a crystal grain size gradient structure in which the average crystal grain size of polygonal ferrite gradually decreases from the center of the sheet thickness toward the surface layer. Furthermore, grain refining of a martensite structure is also effective in improving fatigue characteristics. Patent Literature 4 describes a machine structural steel pipe in which 80% or more in area fraction of the microstructure is martensite, the average block diameter of the martensitic structure is 3 μm or less, and the maximum block diameter is 1 to 3 times the average block diameter. However, although grain refining improves fatigue characteristics of a notch-free material, it has no effect of delaying a crack propagation rate, thus not contributing to an improvement in notch fatigue characteristics. 
     Regarding an improvement in notch fatigue characteristics, it has been reported that it is effective to reduce a crack propagation rate by forming a composite structure. In Patent Literature 5, hard bainite or martensite is dispersed in a structure whose main phase is fine ferrite; thus, fatigue characteristics of a notch-free material and notch fatigue characteristics are both achieved. It is reported in Patent Literatures 6 and 7 that increasing an aspect ratio of martensite in a composite structure reduces a crack propagation rate. 
     CITATION LIST 
     Patent Literature 
     Patent Literature 1: JP H11-92859A 
     Patent Literature 2: JP H11-152544A 
     Patent Literature 3: JP 2004-211199A 
     Patent Literature 4: JP 2010-70789A 
     Patent Literature 5: JP H04-337026A 
     Patent Literature 6: JP 2005-320619A 
     Patent Literature 7: JP H07-90478A 
     SUMMARY OF INVENTION 
     Technical Problem 
     Patent Literature 5 does not describe a technique for improving press formability, and does not pay particular attention to the hardness and shape of bainite and martensite; hence, it seems that favorable press formability is not achieved. 
     Patent Literatures 6 and 7 lack consideration of ductility and workability (e.g., hole expandability), which are needed in press forming. 
     The present invention has been made in order to solve such problems, and aims to provide a hot-rolled steel sheet having excellent fatigue characteristics in the rolling direction and workability. 
     Solution to Problem 
     The present inventors have carried out extensive research in order to achieve the above object, and have succeeded in producing a steel sheet with excellent fatigue characteristics in the rolling direction and workability, by optimizing the chemical composition and production conditions of a high-strength hot-rolled steel sheet to control the microstructure of the steel sheet. The gist of the present invention is as follows. 
     (1) 
     A hot-rolled steel sheet having a chemical composition consisting of, in mass %, 
     C: 0.03 to 0.2%, 
     Mn: 0.1 to 3.0%, 
     P: 0.10% or less, 
     S: 0.03% or less, 
     Al+Si: 0.2 to 3.0%, 
     N: more than 0% and equal to or less than 0.01%, 
     O: more than 0% and equal to or less than 0.01%, 
     Ti: 0 to 0.3%, 
     Nb: 0 to 0.3%, 
     Mg: 0 to 0.01%, 
     Ca: 0 to 0.01%, 
     REM: 0 to 0.1%, 
     B: 0 to 0.01%, 
     Cu: 0 to 2.0%, 
     Ni: 0 to 2.0%, 
     Mo: 0 to 1.0%, 
     V: 0 to 0.3%, 
     Cr: 0 to 2.0%, and 
     the balance: iron and impurities, 
     wherein a microstructure of the hot-rolled steel sheet contains ferrite as the main constituent, and contains hard phases constituted by martensite and/or austenite in an amount of, in area fraction, equal to or more than 3% and less than 20%, 
     hard phases with an aspect ratio of 3 or more accounts for 60% or more of the hard phases present in a sheet-thickness central portion, 
     a length in a rolling direction of the hard phases present in the sheet-thickness central portion is less than 20 μm, 
     an average aspect ratio of ferrite grains is less than 5, and 
     the sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction is 3.5 or more, and an X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction is 1.0 or less. 
     (2) 
     The hot-rolled steel sheet according to (1), containing, in mass %, 
     one or more selected from 
     Ti: equal to or more than (0.005+48/14[N]+48/32[S])% to equal to or less than 0.3%, and 
     Nb: 0.01 to 0.3%, 
     where [N] indicates an N content (mass %) and [S] indicates an S content (mass %). 
     (3) 
     The hot-rolled steel sheet according to (1), containing, in mass %, 
     one or more selected from 
     Mg: 0.0005 to 0.01%, 
     Ca: 0.0005 to 0.01%, and 
     REM: 0.0005 to 0.1%. 
     (4) 
     The hot-rolled steel sheet according to (1), containing, in mass %, 
     B: 0.0002 to 0.01%. 
     (5) 
     The hot-rolled steel sheet according to (1), containing, in mass %, 
     one or more selected from 
     Cu: 0.01 to 2.0%, 
     Ni: 0.01 to 2.0%, 
     Mo: 0.01 to 1.0%, 
     V: 0.01 to 0.3%, and 
     Cr: 0.01 to 2.0%. 
     (6) 
     The hot-rolled steel sheet according to (1), comprising a hot-dip galvanized layer or a galvannealed layer on its surface. 
     Advantageous Effects of Invention 
     According to the present invention, a hot-rolled steel sheet having excellent fatigue characteristics in the rolling direction and workability can be provided. The present invention can be suitably applied to steel sheets with a sheet thickness of 8 mm or less. A hot-rolled steel sheet according to the present invention can prolong fatigue life of suspension parts and the like of automobile materials, thus significantly contributing to the industry. 
    
    
     
       BRIEF DESCRIPTION OF DRAWINGS 
         FIG. 1  is a schematic diagram illustrating the shape and dimensions of test pieces used for a fatigue test.  FIG. 1( a )  is a plan view and a front view of a test piece for measuring fatigue strength without a notch.  FIG. 1( b )  is a plan view and a front view of a test piece for measuring fatigue strength with a notch. 
     
    
    
     DESCRIPTION OF EMBODIMENTS 
     1. Microstructure of Hot-Rolled Steel Sheet 
     1-1. Area Fraction of Each Phase Constituting Hot-Rolled Steel Sheet 
     A hot-rolled steel sheet of the present invention is required to contain ferrite as the main constituent, and contain hard phases constituted by martensite and/or austenite in an amount of, in area fraction, equal to or more than 3% and less than 20%. When the microstructure is a composite structure having hard phases as a secondary phase in ferrite serving as the main phase, ferrite improves ductility and the hard phases improve strength, so that the steel sheet has a favorable balance between strength and ductility. Furthermore, hard phases have an effect of obstructing fatigue crack propagation in ferrite, to reduce a fatigue crack propagation rate; therefore, a steel sheet having the above-described composite structure has excellent punching fatigue characteristics. Hence, a hot-rolled steel sheet of the present invention is made to have a microstructure whose main constituent is ferrite and in which hard phases constituted by martensite and/or austenite are distributed as a secondary phase. Containing ferrite as the main constituent means that ferrite serving as the main phase in the hot-rolled steel sheet has the highest area fraction. The area fraction of ferrite is preferably 70 to 97%. 
     The hard phases exert the effect of inhibiting fatigue crack propagation when its area fraction is 3% or more. On the other hand, when the hard phases have an area fraction of 20% or more, the hard phases serve as a starting point of a defect called a void to reduce a hole expansion ratio, so that “(tensile strength (MPa))×(hole expansion ratio (%))≧35000”, which is required of suspension parts of automobiles, is not satisfied. For this reason, hard phases constituted by martensite or austenite are made to be present in an amount of equal to or more than 3% and less than 20% in area fraction in a microstructure whose main constituent is ferrite. The hard phases are preferably present in an amount of, in area fraction, 5% or more, further preferably 7% or more. 
     1-2. Aspect Ratio of Hard Phase Present in Sheet-Thickness Central Portion 
     Next, description is given on an aspect ratio of hard phases present in a sheet-thickness central portion. When a punching fatigue test is performed in an axial fatigue test, a fatigue crack occurs from the sheet-thickness central portion, and the crack propagates in the sheet thickness direction, resulting in rupture. Here, to inhibit the occurrence of a crack and initial propagation, the forms of the hard phases in the sheet-thickness central portion are particularly important. 
     An aspect ratio of a hard phase is defined by (the length of the major axis of the hard phase/the length of the minor axis of the hard phase). In a hot-rolled steel sheet of the present invention, “the length of the major axis of the hard phase” is “the length of the hard phase in the rolling direction of the steel sheet”, and “the length of the minor axis of the hard phase” is “the length of the hard phase in the thickness direction of the steel sheet”. With an increase in the aspect ratio of the hard phase, the frequency at which a crack hits the hard phase, which obstructs fatigue crack propagation, increases, and also the detouring/branching distance of the crack increases, which is effective in reducing a fatigue crack propagation rate. Here, a hard phase whose aspect ratio is less than 3 has a small effect of inhibiting crack propagation because the detouring/branching distance when a crack hits the hard phase is small. Therefore, it is effective to increase hard phases whose aspect ratio is 3 or more. For this reason, in the hot-rolled steel sheet of the present invention, hard phases with an aspect ratio of 3 or more are made to account for 60% or more of the hard phases present in the sheet-thickness central portion. The hard phases with an aspect ratio of 3 or more preferably account for 80% or more of the hard phase present in the sheet-thickness central portion. 
     1-3. Length in Rolling Direction of Hard Phases Present in Sheet-Thickness Central Portion 
     Description will be given on the length in the rolling direction of the hard phases present in the sheet-thickness central portion. When steel with a composite structure containing ferrite and hard phase are deformed, the ferrite side, which is soft, preferentially undergoes plastic deformation, and accordingly stress on the hard phases increases with the deformation, so that great strain occurs at the interface between ferrite and the hard phases. 
     When the stress on the hard phases or the strain at the interfaces between ferrite and the hard phases exceeds a certain degree, defects called voids occur in the steel, and these voids connect to each other, resulting in rupture. A material in which voids easily occur is vulnerable to local deformation and has low hole expandability. 
     When the hard phases extend in the rolling direction, stress and strain in deformation are concentrated on the hard phases, causing voids to occur early; thus, hole expandability is likely to deteriorate. In addition, in the sheet-thickness central portion, plastic constraint is stronger than in the surface layer portion, and thus voids easily occur. Therefore, the length of the hard phases in the sheet-thickness central portion is particularly important. 
     According to the study by the present inventors, when the length in the rolling direction of the hard phases present in the sheet-thickness central portion is controlled to less than 20 μm, the occurrence of voids can be inhibited, and “(tensile strength (MPa))×(hole expansion ratio (%))≧35000”, which is required of suspension parts of automobiles, can be achieved. Hence, in a hot-rolled steel sheet of the present invention, the length in the rolling direction of the hard phases present in the sheet-thickness central portion is specified as less than 20 μm. The length in the rolling direction of the hard phases in the sheet-thickness central portion is preferably less than 18 μm. 
     The hard phases are constituted by martensite and/or austenite. That is, there are the following three forms: a hard phase containing only martensite, a hard phase containing only austenite, and a hard phase containing both martensite and austenite. The hard phase may be constituted by a single grain (martensite grain or austenite grain), or a plurality of grains may aggregate to integrally constitute the hard phase. Examples of a hard phase in which a plurality of grains aggregate include an aggregate of a plurality of martensite grains, an aggregate of a plurality of austenite grains, and an aggregate of one or a plurality of martensite grains and one or a plurality of austenite grains. 
     1-4. Aspect Ratio of Ferrite Grain 
     Description will be given on the average aspect ratio of ferrite grains. The aspect ratio of a ferrite grain is defined by (the length of the major axis of the ferrite grain/the length of the minor axis of the ferrite grain). In a hot-rolled steel sheet of the present invention, “the length of the major axis of the ferrite grain” is “the length of the ferrite grain in the rolling direction of the steel sheet”, and “the length of the minor axis of the ferrite grain” is “the length of the ferrite grain in the thickness direction of the steel sheet”. In the case where finish rolling is completed in an austenite region, the average aspect ratio of ferrite grains is less than 5. In contrast, in the case where a final rolling temperature is low and rolling is performed in a dual-phase region of austenite and ferrite, ferrite grains stretch in the rolling direction, so that the average aspect ratio of the ferrite grains is 5 or more. When the average aspect ratio of ferrite grains is 5 or more, the ferrite grains undergo work hardening, which reduces the ductility of the steel sheet and does not allow (tensile strength (MPa))×(total elongation (%))≧18000 to be satisfied. Hence, in a hot-rolled steel sheet of the present invention, the average aspect ratio of ferrite grains is made less than 5. 
     1-5. X-Ray Random Intensity Ratio 
     Description will be given on an X-ray random intensity ratio. Fatigue life of a notch-free material is greatly influenced by life until occurrence of a fatigue crack. The occurrence of a fatigue crack is known to proceed in a process of three steps: (1) saturation of a dislocation structure, (2) formation of intrusion and extrusion, and (3) formation of a fatigue crack. 
     As a result of extensive studies, the present inventors have found that by appropriately controlling crystal orientation in the stress loading direction in a fatigue test to make the X-ray random intensity ratio satisfy a predetermined condition, it is possible to delay (1) saturation of a dislocation structure of the process of three steps, and improve fatigue life of a notch-free material in the rolling direction. A mechanism for this is described below. 
     A crystal structure of iron is a body-centered cubic (b.c.c.) structure, and it is said that 42 slip systems of {110}&lt;111&gt; system, {112}&lt;111&gt; system, and {123}&lt;111&gt; system work. Notation of crystal orientation will be described later. In polycrystals, deformability varies depending on crystal orientation, and the degree of difficulty of deformation is decided by a Taylor factor. The Taylor factor is a value defined by formula (F).
 
 dΣΓ   i   =Mdε   (F),
 
     where Γ i  denotes the amount of slip of a slip system i, ΣΓ i  denotes the total sum of slip amounts of the whole slip that has worked, M denotes the Taylor factor, and c denotes the whole plastic strain amount. 
     With a decrease in the Taylor factor, the whole plastic strain amount increases even when the total sum of slip amounts of the slip systems is small, which allows plastic deformation with small energy. The Taylor factor changes depending on crystal orientation with respect to the stress loading direction; thus, a crystal grain in an orientation with a small Taylor factor is easily deformed, and a crystal grain in an orientation with a large Taylor factor is difficult to deform. 
     Researchers have carried out calculation to reveal that, if the above-described 42 slip systems are assumed in b.c.c. metal, values of Taylor factors when &lt;001&gt; orientation, &lt;011&gt; orientation, and &lt;111&gt; orientation are subjected to tensile deformation are 2.1, 3.2, and 3.2, respectively, and &lt;001&gt; orientation is deformed most easily, which leads to early formation of a dislocation structure. In contrast, &lt;011&gt; orientation and &lt;111&gt; orientation are difficult to deform, which leads to late formation of a dislocation structure. That is, a crystal grain facing &lt;001&gt; orientation with respect to the stress loading direction has a short fatigue crack initiation life, and crystal grains facing &lt;011&gt; orientation and &lt;111&gt; orientation have a long fatigue crack initiation life. 
     The present inventors have found as a result of study that, when the sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction is controlled to 3.5 or more and an X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction is controlled to 1.0 or less, fatigue characteristics in the rolling direction exhibit a favorable value of (fatigue limit)/(tensile strength) of 0.55 or more. “Fatigue limit” here refers to fatigue strength at 10 million cycles obtained with a notch-free fatigue test piece, which is described later. 
     On the basis of this finding, in a hot-rolled steel sheet of the present invention, the sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction is set to 3.5 or more, and an X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction is set to 1.0 or less. The sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction is preferably 4.0 or more. An X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction is preferably 0.8 or less. 
     1-6. Method for Measuring Microstructure of Hot-Rolled Steel Sheet and X-Ray Random Intensity 
     (1) Method for Measuring Area Fractions of Ferrite and Hard Phases 
     The area fractions of ferrite and hard phases constituted by martensite and/or austenite, which constitute the structure of a hot-rolled steel sheet of the present invention as described above, are measured by using a sample obtained by taking, as an observation surface, a cross-section perpendicular to the width direction of the steel sheet. The observation surface of the sample is polished and subjected to nital etching. Ranges of ¼ thickness (This means a position at ¼ of the thickness of the steel sheet in the thickness direction of the steel sheet from the surface of the steel sheet. The same applies to the following.), ⅜ thickness, and ½ thickness of the sheet thickness of the observation surface subjected to nital etching are observed with a FE-SEM. 
     For an observation target range of each sample, ten fields of view are observed at a 1000-fold magnification, and in each field of view, the proportions of areas occupied by ferrite and the hard phases are measured. The area of the hard phases is the total area of martensite and austenite. Then, the average values of the proportions of areas occupied by ferrite and the hard phases of all fields of view are obtained as the area fraction of ferrite and the hard phases. 
     (2) Aspect Ratio and Length in Rolling Direction of Hard Phases Present in Sheet-Thickness Central Portion, and Aspect Ratio of Ferrite Phase 
     The aspect ratio and the length in the rolling direction of the hard phases present in the sheet-thickness central portion are determined regarding hard phases located at ½ thickness of the sheet thickness in the above-described sample. 50 or more hard phases located at ½ thickness of the sheet thickness in the above-described sample are observed using a FE-SEM, and the length in the steel sheet rolling direction and the length in the steel sheet thickness direction of each hard phase are measured. From the measurement results of these lengths, an aspect ratio of each hard phase is calculated. The proportion of hard phases with an aspect ratio of 3 or more among the observed hard phases is calculated. In addition, the average value of the lengths in the rolling direction of the observed hard phases is obtained as the length in the rolling direction of the hard phases present in the sheet-thickness central portion. 
     The sheet-thickness central portion refers to a position at ½ of the thickness of the steel sheet in the thickness direction of the steel sheet from the surface of the steel sheet. For example, in the sheet-thickness central portion, any 50 hard phases in a field-of-view range of 50 μm×200 μm are selected, and the length in the rolling direction and the length in the steel sheet thickness direction of each hard phase are measured. To increase measurement precision, instead of selecting any 50 hard phases, the length in the rolling direction and the length in the thickness direction may be measured for all of the hard phases in the field-of-view range. 
     The average aspect ratio of ferrite grains is determined regarding ferrite grains located at ¼ thickness to ½ thickness of the sheet thickness in the above-described sample. 50 or more ferrite grains located at ¼ thickness to ½ thickness of the sheet thickness in the above-described sample are observed using a FE-SEM, and the length in the steel sheet rolling direction and the length in the steel sheet thickness direction of each ferrite grain are measured. From the measurement results of these lengths, an aspect ratio of each ferrite grain is calculated, and the average value of the aspect ratios of the observed ferrite grains is obtained as the average aspect ratio of the ferrite grains. 
     (3) X-Ray Random Intensity Ratio 
     X-ray random intensity ratios of &lt;001&gt; orientation, &lt;011&gt; orientation, and &lt;111&gt; orientation as viewed from the rolling direction may be determined from an inverse pole figure measured by X-ray diffraction. An X-ray random intensity ratio is a value obtained in the following manner: X-ray intensities of a standard sample without integration in a particular orientation and a sample are measured under the same conditions by X-ray diffraction or the like, and the X-ray intensity of the sample is divided by the X-ray intensity of the standard sample. 
     Here, for a hot-rolled steel sheet, crystal orientation perpendicular to the sheet surface is normally denoted by [hkl] or {hkl}, and crystal orientation parallel to the rolling direction is normally denoted by (uvw) or &lt;uvw&gt;. {hkl} and &lt;uvw&gt; collectively refer to equivalent planes, and [hkl] and (uvw) refer to individual crystal planes. In the present invention, which is targeted at a hot-rolled steel sheet whose main constituent is ferrite with a b.c.c. structure, for example, (111), (−111), (1−11), (11−1), (−1−11), (−11−1), (1−1−1), and (−1−1−1) planes are equivalent and undistinguishable. In such a case, these orientations are collectively referred to as &lt;111&gt;. In crystallography, as for “−1”, “−” is put above “1” in the formal notation of orientation, but here, “−1” is used for notation because of constraints in description. 
     A sample for X-ray diffraction is fabricated in the following manner. A rolling-direction cross-section (a cross-section perpendicular to the rolling direction) of the steel sheet is polished by mechanical polishing, chemical polishing, or the like and mirror-finished by buffing, and then strain is removed by electrolytic polishing, chemical polishing, or the like. The range of X-ray diffraction is the whole sheet thickness. If the whole sample cannot be measured at once, measurement may be performed with the sheet thickness direction divided into several fields of view, and the results may be averaged. If measurement by X-ray diffraction is difficult, a statistically sufficient number of samples may be measured by an electron back scattering pattern (EBSP) method or an electron channeling pattern (ECP) method, and an X-ray diffraction random intensity ratio of each orientation may be determined. 
     2. Chemical Composition of Steel Sheet 
     A hot-rolled steel sheet of the present invention has a chemical composition containing the following elements. Hereinafter, the elements will be described along with the reasons for confining the contents of the elements. In the description, “%” of the content of each element means “mass %”. 
     C: 0.03 to 0.2% 
     Carbon (C) is an important element in the present invention. C generates martensite and stabilizes austenite, thus contributing to strength improvement of the hot-rolled steel sheet by structure strengthening, and also has an effect of inhibiting crack propagation. Note that a C content less than 0.03% does not allow a predetermined area fraction of the hard phases to be achieved; thus, an effect of improving punching fatigue characteristics is not exhibited. On the other hand, a C content exceeding 0.2% leads to an excessive area fraction of a low-temperature transformation product constituting the hard phases serving as a secondary phase, which reduces hole expandability. Accordingly, the C content is set to 0.03% to 0.2%. The lower limit of the C content is preferably 0.06%, and the upper limit is preferably 0.18%. 
     Mn: 0.1 to 3.0% 
     Manganese (Mn) is contained for solid solution strengthening and also in order to increase hardenability to generate martensite or austenite in the steel sheet structure. A Mn content exceeding 3% saturates this effect. On the other hand, a Mn content less than 0.1% makes it difficult to exert an effect of inhibiting generation of pearlite and bainite during cooling. Accordingly, the Mn content is set to 0.1 to 3.0%. The lower limit of the Mn content is preferably 0.3%, and the upper limit is preferably 2.5%. 
     P: 0.10% or Less 
     Phosphorus (P), which is an impurity contained in hot metal, is segregated at a grain boundary and reduces low-temperature toughness along with an increase in its content. Therefore, the P content is preferably as low as possible. A P content exceeding 0.10% adversely affects workability and weldability. Accordingly, the P content is set to 0.10% or less. Particularly in terms of weldability, the upper limit of the P content is preferably 0.03%. 
     S: 0.03% or Less 
     Sulfur (S), which is an impurity contained in hot metal, when contained too much, causes a crack in hot rolling and also generates an inclusion, such as MnS, which causes hole expandability to deteriorate. Therefore, the S content should be reduced as far as possible, whereas 0.03% or less is an allowable range. Accordingly, the S content is set to 0.03% or less. Note that when a certain degree of hole expandability is needed, the upper limit of the S content is preferably 0.01%, further preferably 0.005%. 
     Si+Al: 0.2 to 3.0% 
     Silicon (Si) and aluminum (Al) are both important elements in the present invention. Si and Al has an effect of inhibiting {112}&lt;111&gt; slip in the iron, thus delaying formation of a dislocation structure to improve fatigue crack initiation life. This effect is obtained at a total content of Si and Al (Si+Al) of 0.2% or more, and is significant at 0.5% or more. Si+Al exceeding 3.0% saturates the effect and leads to poor economic efficiency. Accordingly, Si+Al is set to 0.2 to 3.0%. The lower limit of Si+Al is preferably 0.5%. The Al content in the present invention refers to acid-soluble Al (so-called “sol.Al”). Only one of Si and Al may be contained in an amount of 0.2 to 3.0%, or both Si and Al may be contained in a total amount of 0.2 to 3.0%. 
     N: More than 0% and Equal to or Less than 0.01% 
     Nitrogen (N), when present in steel as TiN, contributes to an improvement in low-temperature toughness by making a crystal grain size finer in slab heating. Therefore, N may be contained. Note that an N content more than 0.01% may cause a blowhole to be formed in welding of a steel sheet to reduce joint strength of a weld. Accordingly, the N content is set to 0.01% or less. On the other hand, an N content less than 0.0001% is not preferable in terms of economic efficiency. Therefore, the lower limit of the N content is preferably 0.0001% or more, further preferably 0.0005%. 
     O: More than 0% and Equal to or Less than 0.01% 
     Oxygen (O) forms oxide, which causes formability to deteriorate; hence, its content needs to be suppressed. In particular, an O content exceeding 0.01% leads to significant deterioration of formability. Accordingly, the O content is set to 0.01% or less. On the other hand, an O content less than 0.001% is not preferable in terms of economic efficiency. Therefore, the lower limit of the O content is preferably 0.001% or more. 
     Ti: 0 to 0.3% 
     Nb: 0 to 0.3% 
     Titanium (Ti) achieves both excellent low-temperature toughness and high strength due to precipitation strengthening. Therefore, Ti may be contained as necessary. Carbonitride of Ti or solid solution Ti delays grain growth in hot rolling, which makes a grain size of the hot-rolled steel sheet finer and contributes to an improvement in low-temperature toughness. However, a Ti content exceeding 0.3% saturates this effect and leads to poor economic efficiency. Accordingly, the Ti content is set to 0 to 0.3%. In addition, a Ti content less than (0.005+48/14[N]+48/32[S])% may be unable to provide this effect sufficiently. Hence, the Ti content is preferably equal to or more than 0.005+48/14[N]+48/32[S] (%) and equal to or less than 0.3%. Here, [N] and [S] denote the N content (%) and the S content (%), respectively. Furthermore, a Ti content exceeding 0.15% may cause a tundish nozzle to be clogged up easily in casting. Hence, the upper limit of the Ti content is preferably 0.15%. 
     Niobium (Nb) improves low-temperature toughness of a hot-rolled steel sheet. Therefore, Nb may be contained as necessary. Carbonitride of Nb or solid solution Nb delays grain growth in hot rolling, which makes a grain size of the hot-rolled steel sheet finer and contributes to an improvement in low-temperature toughness. However, a Nb content exceeding 0.3% saturates this effect and leads to poor economic efficiency. Accordingly, the Nb content is set to 0 to 0.3%. In addition, a Nb content less than 0.01% may be unable to provide this effect sufficiently. Therefore, the lower limit of the Nb content is preferably 0.01%, and the upper limit is preferably 0.1%. 
     Mg: 0 to 0.01% 
     Ca: 0 to 0.01% 
     REM: 0 to 0.1% 
     Magnesium (Mg), calcium (Ca), and rare earth metal (REM) control the form of a non-metallic inclusion, which serves as a starting point of breaking to cause deterioration of workability, and thus improve workability. Therefore, one or more of these elements may be contained as necessary. However, an Mg content exceeding 0.01%, a Ca content exceeding 0.01%, or a REM content exceeding 0.1% saturates this effect and leads to poor economic efficiency. Accordingly, the Mg content is set to 0 to 0.01%, the Ca content is set to 0 to 0.01%, and the REM content is set to 0 to 0.1%. When Mg, Ca, and REM are each contained in an amount of 0.0005% or more, the above effect is significantly exhibited. Therefore, the lower limit of the Mg content is preferably 0.0005%, the lower limit of the Ca content is preferably 0.0005%, and the lower limit of the REM content is preferably 0.0005%. Note that REM collectively refers to 17 elements in total, including Sc, Y, and lanthanoid, and the REM content means the total amount of these elements. 
     B: 0 to 0.01% 
     B is segregated at a grain boundary and increases grain boundary strength to improve low-temperature toughness. Therefore, B may be contained in the steel sheet as necessary. However, a B content exceeding 0.01% not only saturates this effect but also leads to inferior economic efficiency. Accordingly, the B content is set to 0 to 0.01%. The above effect is significant when the steel sheet has a B content of 0.0002% or more. Therefore, the lower limit of the B content is preferably 0.0002%, further preferably 0.0005%. The upper limit of the B content is preferably 0.005%, further preferably 0.002%. 
     Cu: 0 to 2.0% 
     Ni: 0 to 2.0% 
     Mo: 0 to 1.0% 
     V: 0 to 0.3% 
     Cr: 0 to 2.0% 
     Copper (Cu), nickel (Ni), molybdenum (Mo), vanadium (V), and chromium (Cr) have an effect of improving the strength of a hot-rolled steel sheet by precipitation strengthening or solid solution strengthening. Therefore, one or more of these elements may be contained as necessary. However, a Cu content exceeding 2.0%, a Ni content exceeding 2.0%, a Mo content exceeding 1.0%, a V content exceeding 0.3%, or a Cr content exceeding 2.0% saturates this effect and leads to poor economic efficiency. Accordingly, the Cu content is set to 0 to 2.0%, the Ni content is set to 0 to 2.0%, the Mo content is set to 0 to 1.0%, the V content is set to 0 to 0.3%, and the Cr content is set to 0 to 2.0%. When Cu, Ni, Mo, V, and Cu are each contained in an amount of less than 0.01%, this effect is not provided sufficiently. Therefore, the lower limit of the Cu content is preferably 0.01%, further preferably 0.02%. The lower limit of the Ni content is preferably 0.01%, the lower limit of the Mo content is preferably 0.01%, the lower limit of the V content is preferably 0.01%, and the lower limit of the Cr content is preferably 0.01%. In addition, the upper limit of the Cu content is preferably 1.2%, the upper limit of the Ni content is preferably 0.6%, the upper limit of the Mo content is preferably 0.7%, the upper limit of the V content is preferably 0.2%, and the upper limit of the Cr content is preferably 1.2%. 
     Described above is a basic chemical composition of a hot-rolled steel sheet of the present invention. The balance of the chemical composition of the hot-rolled steel sheet of the present invention consists of iron and impurities. Impurities mean components that are mixed in due to raw materials, such as ores or scrap, or other factors when a steel material is produced industrially. 
     It has been confirmed that, as an element other than the above elements, one or more of Zr, Sn, Co, Zn, and W may be contained in a total amount of 1% or less, instead of part of iron, without impairment of the excellent fatigue characteristics in the rolling direction and workability of the hot-rolled steel sheet of the present invention. Among these elements, Sn may cause a flaw in hot rolling; hence, the upper limit of the Sn content is preferably 0.05%. 
     A hot-rolled steel sheet of the present invention having the above-described structure and composition can have improved corrosion resistance by comprising, on the surface, a hot-dip galvanized layer formed by hot dip galvanizing and a galvannealed layer formed by alloying after plating. The plating layer is not limited to pure zinc, and may contain elements such as Si, Mg, Al, Fe, Mn, Ca, and Zr for further improved corrosion resistance. Comprising this plating layer does not impair the excellent punching fatigue characteristics and workability of the hot-rolled steel sheet of the present invention. 
     Moreover, a hot-rolled steel sheet of the present invention may comprise a surface-treating layer formed by any of formation of an organic film, film laminating, organic salts/inorganic salts treatment, non-chromium treatment, and the like, and still achieve an effect of the present invention. 
     3. Method for Producing Hot-Rolled Steel Sheet of the Present Invention 
     A method for producing a hot-rolled steel sheet is not particularly limited, as long as a hot-rolled steel sheet having the aforementioned microstructure is obtained. For example, a production method comprising the following steps [a] to [h] allows a hot-rolled steel sheet of the present invention to be stably obtained. Hereinafter, details of each step will be described as an example. 
     [a] Slab Casting Step 
     There is no particular limitation on a method for producing a slab prior to hot rolling. That is, subsequent to production of ingot steel using a blast furnace, an electric furnace, or the like, various kinds of secondary smelting may be performed for adjustment to the above-described chemical composition, and then, a slab may be casted by a normal method, such as continuous casting or thin slab casting. On this occasion, scrap may be used as a raw material as long as a component range of the present invention can be obtained by control. 
     [b] Slab Heating Step 
     The casted slab is heated to a predetermined temperature for hot rolling. In the case of continuous casting, the slab may be once cooled to a low temperature and then heated again and subjected to hot rolling, or may be directly heated and subjected to hot rolling subsequent to continuous casting without being cooled. Heating time for the slab is equal to or more than time t 1 (s) specified in formula (A).
 
 t   1 ( s )=1.4×10 −6 ×Exp{3.2×10 4 /( T   1 +273)}  (A),
 
     where T 1  (° C.) is the average temperature of the slab in a soaking area. 
     The heating time is thus specified for the following reason. In the structure of the casted slab, segregation of Mn is present in the center of the slab. Therefore, when the slab is not sufficiently heated, segregation of Mn remains in a sheet-thickness central portion of a hot-rolled steel sheet obtained by rolling. Since Mn stabilizes austenite, a region in which austenite is likely to remain along the Mn segregation occurs during cooling after the rolling. Consequently, martensite into which austenite has been transformed at low temperature or remaining austenite is likely to be present along the Mn segregation, which increases the length in the rolling direction of the hard phases in the sheet-thickness central portion of the hot-rolled steel sheet. 
     As a result of extensive studies, the present inventors have found that in order to make the length in the rolling direction of the hard phases 20 μm or less, it is necessary to set the heating time for the slab to time t 1 (s), specified in formula (A), or more. Presumably, sufficiently long heating time for the slab promotes diffusion of Mn, reducing the length in the rolling direction of the hard phases. An effect of the present invention is exerted even when the upper limit of the slab heating temperature is not set, but excessively high heating temperature is not preferable in terms of economic efficiency. Hence, the slab heating temperature is preferably lower than 1300° C. The lower limit of the slab heating temperature is preferably 1150° C. The heating time for the slab is not the elapsed time from heating start, but time during which the slab is held at a predetermined heating temperature (e.g., a temperature equal to or higher than 1150° C. and lower than 1300° C.). 
     [c] Rough Rolling Step 
     After the slab heating step, a rough rolling step of hot rolling starts to be performed without a wait on the slab extracted from a heating furnace; thus, a rough bar is obtained. In the rough rolling step, the total reduction ratio during rough rolling is set to 50% or more, and a slab surface layer is cooled to Ar 3  transformation point, expressed by formula (B) below, or lower twice or more, preferably three times or more, during rough rolling. Specifically, the rough rolling step is performed as multi-pass hot rolling, and a surface layer of the slab that has gone through the previous pass is once cooled to Ar 3  transformation point or lower and then recuperated to a temperature higher than Ar 3  transformation point. The slab whose surface layer has been recuperated is rolled in a subsequent pass, and a surface layer of the slab is cooled again to Ar 3  transformation point or lower. This process is repeated. The temperature of the slab surface layer in the present invention refers to the temperature of the slab in a portion at 1 mm in the depth direction from the slab surface, and can be estimated by thermal transfer calculation, for example. Cooling the inside of the slab as well as the slab outermost surface to Ar 3  transformation point or lower increases the effect of recuperation.
 
Ar 3 (° C.)=901−325×C+33×Si+287×P+40×Al−92×(Mn+Mo+Cu)−46×Ni  (B),
 
     where each chemical symbol denotes the content (mass %) of the element. 
     The rough rolling conditions are thus specified for the following reason. To obtain an effect of the present invention of obtaining a hot-rolled steel sheet with favorable fatigue characteristics in the rolling direction, it is essential that, in the hot-rolled steel sheet, the sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction be 3.5 or more, and an X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction be 1.0 or less than 1.0. To thus control crystal orientation, it is important to make shear force act on the steel sheet to develop &lt;011&gt; orientation and &lt;111&gt; orientation as strongly as possible so that they reach a portion close to the center of the sheet thickness. The influence of a structure formed by the action of shear force during rough rolling is normally eliminated by recrystallization after rough rolling. The study by the present inventors, however, has revealed that when the slab surface layer is once cooled to Ar 3  transformation point or lower during rough rolling, the structure during rough rolling exerts a preferable influence on a final structure. A presumable mechanism is described below. 
     When sufficient shear force is applied during rough rolling and the slab surface layer is once cooled to Ar 3  transformation point or lower, the structure around the surface layer is partly transformed from austenite to ferrite. At this time, ferrite is influenced by the shear force during rough rolling; thus, as viewed from the rolling direction, &lt;111&gt; orientation and &lt;011&gt; orientation increase and &lt;001&gt; orientation decreases. 
     Ferrite in the surface layer is recuperated and reversely transformed to austenite by the next pass. On this occasion, austenite that has undergone reverse transformation has an orientation having a certain orientation relationship with the crystal orientation of ferrite before transformation. When the surface layer austenite after reverse transformation is further subjected to rough rolling and cooled again to Ar 3  transformation point or lower, the surface layer structure is partly transformed from austenite to ferrite again. The crystal orientation of austenite before transformation is influenced by the crystal orientation of former ferrite; thus, &lt;111&gt; orientation and &lt;011&gt; orientation of ferrite after transformation further increase as compared with after the previous pass. 
     In this manner, during rough rolling, applying sufficient shear force in each pass and transforming a surface layer by cooling to Ar 3  transformation point or lower are repeated; thus, near the surface layer, &lt;111&gt; orientation and &lt;011&gt; orientation increase and &lt;001&gt; orientation decreases. To sufficiently exert this effect, it is necessary to set the reduction ratio during rough rolling to 50% or more to apply sufficient shear force; hence, in this step, the slab surface layer is cooled to Ar 3  transformation point or lower twice or more, preferably three times or more. 
     [d] Finish Rolling Step 
     In a finish rolling step following the rough rolling step, two passes or more of rolling in which a shape ratio X, determined from formula (C) below, is 2.3 or more are performed at a slab surface layer temperature of 1100° C. or lower to make the total reduction ratio 40% or more. 
     
       
         
           
             
               
                 
                   [ 
                   
                     Math 
                     . 
                     
                         
                     
                     ⁢ 
                     1 
                   
                   ] 
                 
               
               
                 
                     
                 
               
             
             
               
                 
                   X 
                   = 
                   
                     
                       
                         
                           L 
                           × 
                           
                             ( 
                             
                               
                                 h 
                                 
                                   i 
                                   ⁢ 
                                   
                                       
                                   
                                   ⁢ 
                                   n 
                                 
                               
                               - 
                               
                                 h 
                                 out 
                               
                             
                             ) 
                           
                         
                         2 
                       
                     
                     
                       
                         ( 
                         
                           
                             h 
                             
                               i 
                               ⁢ 
                               
                                   
                               
                               ⁢ 
                               n 
                             
                           
                           + 
                           
                             h 
                             out 
                           
                         
                         ) 
                       
                       2 
                     
                   
                 
               
               
                 
                   ( 
                   C 
                   ) 
                 
               
             
           
         
       
     
     where L denotes the diameter of a rolling mill roll, h in  denotes the sheet thickness on the rolling mill roll entry side, and h out  denotes the sheet thickness on the rolling mill roll exit side. 
     The present inventors have found that, to make shear force of hot rolling act on the steel sheet deeply by rolling at 1100° C. or lower, it is necessary to satisfy a shape ratio X, specified in formula (C), of 2.3 or more in at least two passes of the total number of passes of hot rolling. As expressed by formulae (C1) to (C3) below, the shape ratio X is a ratio between contact arc length l d  and average sheet thickness h m  of the rolling mill roll and the steel sheet.
 
 X=l   d   /h   m   (C1)
 
 l   d =( L ×( h   in   −h   out )/2) 1/2   (C2)
 
 h   m =( h   in   +h   out )/2  (C3)
 
     Even if the shape ratio X determined from formula (C) is 2.3 or more, one pass of rolling is not enough for sufficient introduction depth of shear strain. When the introduction depth of shear strain is insufficient, alignment of ferrite in &lt;111&gt; orientation and &lt;011&gt; orientation as viewed from the rolling direction is weak, which results in a reduction in fatigue characteristics in the rolling direction. Accordingly, the number of passes in which the shape ratio X is 2.3 or more is set to two or more. 
     The number of passes of rolling in the finish rolling step is preferably as large as possible. When the number of passes is three or more, the shape ratio X may be set to 2.3 or more in all passes. To increase the thickness of a shear layer, the value of the shape ratio X is preferably as large as possible. The value of the shape ratio X is preferably 2.5 or more, further preferably 3.0 or more. 
     When rolling in which the shape ratio X is 2.3 or more is performed at high temperature, subsequent recrystallization may break textures increasing Young&#39;s modulus. Hence, rolling in which the number of passes in which the shape ratio X is set to 2.3 or more is confined is performed in a state where the slab surface layer temperature is 1100° C. or lower. In addition, a larger amount of introduction of shear strain leads to further development of crystal grains in &lt;111&gt; orientation and &lt;011&gt; orientation as viewed from the rolling direction, which improve fatigue characteristics in the rolling direction of the steel sheet. This effect is significant when the total reduction ratio at 1100° C. or lower is 40% or more; hence, the total reduction ratio at 1100° C. or lower is set to 40% or more. 
     Reduction in the final pass of finish rolling is performed at equal to or higher than (T 2 −100) ° C. and lower than (T 2 +20) ° C., preferably equal to or higher than (T 2 −100) ° C. and lower than T 2  (° C.), and the reduction ratio is set to equal to or more than 3% and less than 40%. The reduction ratio is preferably equal to or more than 10% and less than 40%. T 2  is a temperature specified in formula (D) below.
 
 T   2 (° C.)=870+10×(C+N)×Mn+350×Nb+250×Ti+40×B+10×Cr+100×Mo+100×V  (D),
 
     where each chemical symbol denotes the content (mass %) of the element. 
     Reduction conditions in this final pass are very important in controlling an aspect ratio of the hard phases in the sheet-thickness central portion. Performing rolling in a temperature range of equal to or higher than (T 2 −100) ° C. and lower than (T 2 +20) ° C. increases the aspect ratio of the hard phases in the sheet-thickness central portion, presumably because rolling in a state where recrystallization is inhibited increases the aspect ratio of austenite, and the shapes are inherited by the hard phases. To exert this effect of increasing the aspect ratio of the hard phases, it is necessary to set the reduction ratio in the final reduction to 3% or more. Rolling with a reduction ratio of 40% or more places a great burden on a rolling mill; hence, a reduction ratio equal to or more than 3% and less than 40% is preferable. 
     If reduction in the final pass is performed in a temperature range of lower than (T 2 −100) ° C., rolling proceeds in a dual-phase region of ferrite and austenite, and ferrite undergoes work hardening, which results in a reduction in the ductility of the steel sheet. If reduction in the final pass is performed in a temperature range of (T 2 +20) ° C. or higher, the aspect ratio of the hard phases in the sheet-thickness central portion is small. This is presumably because promotion of recrystallization of austenite, resulting in reduced aspect ratio of austenite, influences the forms of the hard phases. Hence, reduction in the final pass is performed in a temperature range of equal to or higher than (T 2 −100) ° C. and lower than (T 2 +20) ° C. Reduction under these conditions makes the aspect ratio of the hard phases 3 or more. 
     [e] First Cooling Step 
     In a first cooling step following the finish rolling step, the average cooling rate from the final reduction temperature of finish rolling to 750° C. is set to 60° C./s or more, because a cooling rate less than 60° C./s may cause the length in the sheet thickness direction of the hard phases in the sheet-thickness central portion to be 20 μm or more. Although the cause of the correlation between cooling rate and the length in the sheet thickness direction of the hard phases is uncertain, there is a possibility that a cooling rate of 60° C./s or more makes it difficult for dislocation introduced in the final reduction of finish rolling to recover, and the dislocation works as the core of ferrite transformation; thus, untransformed austenite in the sheet-thickness central portion is divided by ferrite, which results in a reduction in the length in the sheet thickness direction of the hard phases. 
     In the field of steel plates, there has been an example aiming at inhibition of fatigue crack propagation by control of an aspect ratio of hard phases, but no document has reported achievement of both the inhibition of fatigue crack propagation and workability such as hole expandability, probably for the following reasons. In the field of steel plates, rolling strain does not easily reach a plate-thickness central portion. In addition, because of thick plate thickness, cooling rate in the plate-thickness central portion is not enough, so that recovery of dislocation proceeds; consequently, the core of ferrite transformation cannot be introduced sufficiently, which prevents a reduction in the length of the hard phases. 
     [f] Soaking Step 
     In a soaking step following the first cooling step, the steel sheet is held for 5 s or more in a temperature range of equal to or higher than 600° C. and lower than 750° C. The soaking step is essential to obtaining a microstructure whose main constituent is ferrite. The holding time is set to 5 s or more, because holding time of 5 s or less does not allow ferrite to serve as the main constituent of the microstructure or makes an area fraction of the hard phases 20% or more, which reduces ductility and a hole expansion ratio. 
     [g] Second Cooling Step 
     In a second cooling step following the soaking step, with regard to a temperature T 3 (° C.) specified in formula (E) below, the average cooling rate in a temperature range of equal to or higher than T 3 (° C.) and lower than 600° C. is set to 50° C./s or more. The average cooling rate is set to 50° C./s or more because an average cooling rate of less than 50° C./s leads to generation of bainite and pearlite in the structure, making it difficult to obtain enough fraction of the hard phases, which causes notch fatigue characteristics to deteriorate.
 
 T   3 (° C.)=561−474×C−33×Mn−17×Ni−17×Cr−21×Mo  (E),
 
     where each chemical symbol denotes the content (mass %) of the element. 
     [h] Winding Step 
     The steel sheet is wound after the second cooling step. The temperature of the steel sheet in winding (winding temperature) is set to T 3 (° C.), specified in formula (E), or lower. Winding at a high temperature exceeding T 3 (° C.) leads to generation of bainite and pearlite in the structure, making it difficult to obtain enough fraction of the hard phases, which causes punching fatigue characteristics to deteriorate. 
     Through the production steps described above, a hot-rolled steel sheet of the present invention is produced. 
     After the completion of all of the steps [a] to [h], for the purpose of correcting the shape of the steel sheet or of improving ductility by introducing mobile dislocation, or the like, skin pass rolling in which a reduction ratio is equal to or more than 0.1% and equal to or less than 2% is preferably performed. In addition, after the completion of all of the steps, for the purpose of removing scales attached on the surface of the obtained hot-rolled steel sheet, pickling may be performed on the obtained hot-rolled steel sheet as necessary. Furthermore, after pickling, skin pass rolling or cold rolling in which a reduction ratio is 10% or less may be performed on the obtained hot-rolled steel sheet in-line or off-line. 
     A hot-rolled steel sheet of the present invention is produced through, in addition to the rolling steps specified in the present invention, continuous casting, pickling, and the like, which are normal hot-rolling steps. Even if produced with the steps other than those specified in the present invention partly skipped, the hot-rolled steel sheet can have excellent fatigue characteristics in the rolling direction and workability, which are effects of the present invention. 
     Moreover, even if, after the hot-rolled steel sheet is once produced, heat treatment is performed on-line or off-line in a temperature range of 100 to 600° C. for the purpose of improving ductility, the hot-rolled steel sheet can have excellent fatigue characteristics in the rolling direction and workability, which are effects of the present invention. 
     The hot-rolled steel sheet produced through the above steps may be subjected to an additional step, such as performing hot dip galvanizing or alloyed hot dip galvanizing, or performing surface treatment by formation of an organic film, film laminating, organic salts/inorganic salts treatment, non-chromium treatment, and the like. 
     4. Method for Evaluating Characteristics of Hot-Rolled Steel Sheet 
     (1) Tensile Strength Characteristics 
     Of mechanical properties of a hot-rolled steel sheet, tensile strength characteristics (tensile strength and total elongation) are evaluated in conformance with JIS Z 2241 2011. A test piece is No. 5 test piece of JIS Z 2241 2011, taken from a ¼W (This means a position at ¼ of the width of the steel sheet in the width direction of the steel sheet from the end portion in the width direction of the steel sheet. The same applies to the following.) or ¾W position of the sheet width of the steel sheet with the rolling direction serving as the longitudinal direction. 
     (2) Hole Expansion Ratio 
     A hole expansion ratio of a hot-rolled steel sheet is evaluated by a hole expansion test in conformance with a test method described in the Japan Iron and Steel Federation Standard JFS T 1001-1996. A test piece is taken from a position similar to that of the tensile test piece, and is provided with a punching hole by a cylindrical punch. A steel sheet with excellent workability in the present invention refers to a steel sheet that satisfies (tensile strength (MPa))×(total elongation (%)) 18000 and (tensile strength (MPa))×(hole expansion ratio (%))≧35000. 
     (3) Fatigue Characteristics 
       FIG. 1  is a schematic diagram illustrating the shape and dimensions of test pieces used for a fatigue test.  FIG. 1( a )  is a plan view and a front view of a test piece for measuring fatigue strength without a notch.  FIG. 1( b )  is a plan view and a front view of a test piece for measuring fatigue strength with a notch. 
     To evaluate fatigue characteristics in the rolling direction of a hot-rolled steel sheet, test pieces with the shape and dimensions illustrated in  FIG. 1  are used. Each test piece is taken from a position similar to that of the tensile test piece with the rolling direction serving as the longitudinal direction. The test piece illustrated in  FIG. 1( a )  is a test piece for obtaining fatigue strength without a notch. The test piece illustrated in  FIG. 1( b )  is a punched test piece for obtaining fatigue strength of a notched material, and is provided with a punching hole  1  by a cylindrical punch like the hole expansion test piece in order to allow evaluation close to fatigue characteristics evaluation in actual use of automobile parts. A punching clearance is set to 10%. Both fatigue test pieces are subjected to grinding for three triangle finish (expressed by surface roughness finish symbols) from the outermost layer to a depth of approximately 0.05 mm. 
     Using these test pieces, a stress controlled tensile-tensile fatigue test is performed under conditions of a stress ratio R of 0.1 and a frequency of 15 to 25 Hz. A steel sheet with excellent fatigue characteristics in the rolling direction in the present invention refers to a steel sheet whose value (fatigue limit ratio) obtained by dividing fatigue strength at 10 million cycles obtained with the notch-free fatigue test piece by tensile strength obtained in the tensile test is 0.55 or more, and whose value (punching fatigue limit ratio) obtained by dividing fatigue strength at 10 million cycles obtained in the punching fatigue test by tensile strength obtained in the tensile test is 0.30 or more. 
     Hereinafter, the present invention will be described more specifically in Examples. Note that the present invention is not limited by the following Examples. 
     EXAMPLES 
     Molten steel having chemical compositions shown in Table 1 was produced. 
     
       
         
           
               
             
               
                 TABLE 1 
               
             
            
               
                   
               
               
                 Chemical components (mass %) 
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Steel 
                 C 
                 Si 
                 Mn 
                 P 
                 S 
                 Al 
                 N 
                 O 
                 Ti 
                 Nb 
                 Others 
                 Si + Al 
                 Remarks 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 A 
                 0.035 
                 0.13 
                 0.96 
                 0.016 
                 0.0028 
                 0.15 
                 0.0036 
                 0.0016 
                 0.043 
                 0.012 
                 — 
                 0.280 
                 Invention steel 
               
               
                 B 
                 0.119 
                 0.82 
                 0.93 
                 0.015 
                 0.0027 
                 0.03 
                 0.0028 
                 0.0023 
                 0.011 
                 0.000 
                 — 
                 0.850 
                 Invention steel 
               
               
                 C 
                 0.062 
                 0.00 
                 1.13 
                 0.009 
                 0.0032 
                 0.53 
                 0.0030 
                 0.0022 
                 0.034 
                 0.010 
                 — 
                 0.530 
                 Invention steel 
               
               
                 D 
                 0.073 
                 1.30 
                 0.42 
                 0.018 
                 0.0019 
                 0.03 
                 0.0037 
                 0.0021 
                 0.000 
                 0.013 
                 B = 0.0007 
                 1.330 
                 Invention steel 
               
               
                 E 
                 0.064 
                 1.27 
                 1.01 
                 0.011 
                 0.0024 
                 0.03 
                 0.0024 
                 0.0028 
                 0.010 
                 0.012 
                 Cu = 0.11 
                 1.300 
                 Invention steel 
               
               
                 F 
                 0.067 
                 1.16 
                 2.10 
                 0.016 
                 0.0020 
                 0.32 
                 0.0019 
                 0.0012 
                 0.011 
                 0.010 
                 Ni = 0.32 
                 1.480 
                 Invention steel 
               
               
                 G 
                 0.065 
                 1.16 
                 0.90 
                 0.072 
                 0.0038 
                 0.03 
                 0.0017 
                 0.0013 
                 0.000 
                 0.013 
                 Ca = 0.001 
                 1.194 
                 Invention steel 
               
               
                 H 
                 0.060 
                 1.27 
                 1.06 
                 0.013 
                 0.0089 
                 0.00 
                 0.0023 
                 0.0038 
                 0.011 
                 0.000 
                 Mo = 0.42 
                 1.270 
                 Invention steel 
               
               
                 I 
                 0.066 
                 0.59 
                 1.00 
                 0.018 
                 0.0031 
                 1.86 
                 0.0031 
                 0.0012 
                 0.013 
                 0.010 
                 V = 0.13 
                 2.450 
                 Invention steel 
               
               
                 a 
                 0.018 
                 1.10 
                 0.98 
                 0.012 
                 0.0022 
                 0.03 
                 0.0038 
                 0.0025 
                 0.010 
                 0.011 
                 — 
                 1.130 
                 Comparative steel 
               
               
                 b 
                 0.254 
                 1.09 
                 0.85 
                 0.013 
                 0.0021 
                 0.04 
                 0.0027 
                 0.0022 
                 0.000 
                 0.011 
                 — 
                 1.130 
                 Comparative steel 
               
               
                 c 
                 0.060 
                 1.23 
                 0.86 
                 0.155 
                 0.0012 
                 0.04 
                 0.0029 
                 0.0032 
                 0.000 
                 0.000 
                 — 
                 1.273 
                 Comparative steel 
               
               
                 d 
                 0.068 
                 0.89 
                 1.20 
                 0.020 
                 0.0361 
                 0.02 
                 0.0022 
                 0.0032 
                 0.020 
                 0.000 
                 — 
                 0.911 
                 Comparative steel 
               
               
                   
               
            
           
         
       
     
     According to Table 1, chemical compositions of steels A to I were within a chemical composition range specified in the present invention. Meanwhile, steel “a” had too low a C content, steel “b” had too high a C content, steel “c” had too high a P content, and steel “d” had too high a S content. The underlines indicate component amounts falling outside the invention range. 
     Using the molten steel with the chemical compositions of steels A to I and steels “a” to “d”, hot-rolled steel sheets were produced by the above-described steps [a] to [h]. Each step was performed under conditions shown in Tables 2 and 3. In step [d], rolling at 1100° C. or lower was performed in six passes of P 1  to P 6 . Steels A to I and steels “a” to “d” shown in Tables 2 and 3 correspond to the molten steel with the chemical compositions shown in Table 1, and indicate the used molten steel. As T 1  (° C.), the average temperature of a soaking area of a heating furnace was measured as the average temperature of the slab in a soaking area. P 1  to P 6  indicate first to sixth passes in the finish rolling step. 
     
       
         
           
               
             
               
                 TABLE 2 
               
               
                   
               
               
                 Production conditions 
               
               
                   
               
             
            
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
            
               
                   
                 Average 
                   
                   
                 Reduction 
                   
                 Number of times 
                   
               
               
                   
                 temperature of 
                   
                   
                 ratio 
                   
                 of cooling slab 
                 Shape ratio X in 
               
               
                   
                 soaking area of 
                   
                 Slab 
                 during 
                   
                 surface layer 
                 each rolling at 
               
               
                   
                 heating furnace, 
                 t1 
                 heating 
                 rough 
                 Ar3 
                 to Ar3 point 
                 1100° C. or lower 
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Steel 
                 T1 (° C.) 
                 (s) 
                 time (s) 
                 rolling (%) 
                 (° C.) 
                 or lower 
                 P1 
                 P2 
                 P3 
                 P4 
                 P5 
                 P6 
               
               
                   
               
               
                 A-1 
                 1205 
                 3540 
                 5374 
                 77 
                 816 
                 4 
                 1.7 
                 1.7 
                 2.6 
                 4.1 
                 5.0 
                 2.9 
               
               
                 B-1 
                 1216 
                 3540 
                 7355 
                 84 
                 809 
                 4 
                 1.7 
                 2.1 
                 2.6 
                 4.8 
                 4.0 
                 4.9 
               
               
                 C-1 
                 1216 
                 3540 
                 6323 
                 82 
                 801 
                 3 
                 1.7 
                 2.1 
                 3.9 
                 4.0 
                 5.5 
                 3.3 
               
               
                 C-2 
                 1251 
                 3540 
                 5763 
                 81 
                 801 
                 3 
                 2.0 
                 2.2 
                 4.9 
                 5.5 
                 4.3 
                 4.4 
               
               
                 C-3 
                 1183 
                 3540 
                 7700 
                 85 
                 801 
                 3 
                 1.5 
                 1.9 
                 5.0 
                 5.6 
                 2.7 
                 4.7 
               
               
                 C-4 
                 1239 
                 3540 
                 4551 
                 83 
                 801 
                 3 
                 1.7 
                 2.2 
                 4.8 
                 5.4 
                 4.8 
                 4.4 
               
               
                 C-5 
                 1196 
                 3540 
                 8549 
                 83 
                 801 
                 4 
                 1.9 
                 1.9 
                 3.5 
                 4.6 
                 3.4 
                 3.9 
               
               
                 C-6 
                 1239 
                 3540 
                 5600 
                 90 
                 801 
                 4 
                 1.7 
                 1.6 
                 5.0 
                 4.4 
                 2.6 
                 5.0 
               
               
                 C-7 
                 1205 
                 3540 
                 8427 
                 87 
                 801 
                 4 
                 1.9 
                 1.7 
                 4.8 
                 4.4 
                 5.0 
                 4.5 
               
               
                 C-8 
                 1243 
                 3540 
                 5428 
                 85 
                 801 
                 3 
                 1.5 
                 2.0 
                 4.2 
                 3.0 
                 2.9 
                 5.5 
               
               
                 D-1 
                 1260 
                 3540 
                 6411 
                 81 
                 888 
                 3 
                 2.1 
                 3.4 
                 3.0 
                 4.2 
                 2.8 
                 5.5 
               
               
                 E-1 
                 1180 
                 3540 
                 8445 
                 90 
                 823 
                 3 
                 2.1 
                 2.0 
                 4.1 
                 2.7 
                 3.2 
                 5.0 
               
               
                 E-2 
                 1280 
                 3540 
                 1168 
                 83 
                 823 
                 4 
                 2.0 
                 1.7 
                 3.1 
                 3.1 
                 5.2 
                 2.6 
               
               
                 E-3 
                 1184 
                 3540 
                 5024 
                 79 
                 823 
                 4 
                 1.7 
                 1.6 
                 2.6 
                 3.2 
                 5.3 
                 3.7 
               
               
                 E-4 
                 1218 
                 3540 
                 7026 
                 46 
                 823 
                 4 
                 1.5 
                 2.0 
                 4.0 
                 5.7 
                 4.9 
                 4.5 
               
               
                 E-5 
                 1226 
                 3540 
                 7209 
                 60 
                 823 
                 3 
                 2.2 
                 2.2 
                 3.2 
                 5.3 
                 5.5 
                 3.6 
               
               
                 E-6 
                 1243 
                 3540 
                 5124 
                 91 
                 823 
                 1 
                 1.9 
                 1.6 
                 5.3 
                 3.9 
                 5.3 
                 4.9 
               
               
                 E-7 
                 1185 
                 3540 
                 9927 
                 86 
                 823 
                 2 
                 1.8 
                 1.8 
                 4.1 
                 3.6 
                 3.8 
                 4.6 
               
               
                 E-8 
                 1273 
                 3540 
                 6624 
                 85 
                 823 
                 4 
                 1.9 
                 1.5 
                 2.0 
                 1.9 
                 1.5 
                 3.8 
               
               
                 E-9 
                 1213 
                 3540 
                 6677 
                 81 
                 823 
                 4 
                 1.5 
                 1.7 
                 2.0 
                 2.2 
                 2.3 
                 2.4 
               
               
                 E-10 
                 1229 
                 3540 
                 6864 
                 75 
                 823 
                 4 
                 3.7 
                 4.3 
                 3.0 
                 3.6 
                 3.6 
                 2.7 
               
               
                 E-11 
                 1270 
                 3540 
                 4782 
                 90 
                 823 
                 4 
                 2.0 
                 1.6 
                 2.5 
                 2.7 
                 1.7 
                 1.9 
               
               
                 E-12 
                 1199 
                 3540 
                 7356 
                 75 
                 823 
                 3 
                 2.0 
                 1.6 
                 5.0 
                 3.9 
                 2.8 
                 4.8 
               
               
                 E-13 
                 1193 
                 3540 
                 8699 
                 85 
                 823 
                 4 
                 2.1 
                 1.9 
                 4.3 
                 5.7 
                 4.4 
                 4.8 
               
               
                 E-14 
                 1227 
                 3540 
                 5354 
                 83 
                 823 
                 4 
                 2.0 
                 1.8 
                 3.4 
                 4.7 
                 4.8 
                 4.0 
               
               
                 E-15 
                 1180 
                 3540 
                 9445 
                 78 
                 823 
                 4 
                 1.9 
                 2.1 
                 3.2 
                 4.3 
                 5.4 
                 3.8 
               
               
                 E-16 
                 1225 
                 3540 
                 4494 
                 89 
                 823 
                 3 
                 1.7 
                 1.7 
                 3.0 
                 4.6 
                 4.6 
                 2.0 
               
               
                 E-17 
                 1234 
                 3540 
                 5702 
                 77 
                 823 
                 4 
                 1.8 
                 1.8 
                 4.1 
                 2.7 
                 3.1 
                 2.5 
               
               
                 E-18 
                 1266 
                 3540 
                 4734 
                 87 
                 823 
                 4 
                 1.5 
                 1.6 
                 5.4 
                 4.6 
                 3.1 
                 5.0 
               
               
                 F-1 
                 1185 
                 3540 
                 9750 
                 78 
                 727 
                 3 
                 1.5 
                 1.7 
                 4.1 
                 4.5 
                 5.0 
                 5.7 
               
               
                 G-1 
                 1247 
                 3540 
                 4460 
                 81 
                 857 
                 3 
                 1.7 
                 2.2 
                 2.9 
                 2.6 
                 5.6 
                 2.8 
               
               
                 H-1 
                 1228 
                 3540 
                 5035 
                 87 
                 791 
                 3 
                 2.2 
                 1.7 
                 4.0 
                 5.1 
                 5.3 
                 3.8 
               
               
                 I-1 
                 1244 
                 3540 
                 6445 
                 79 
                 887 
                 3 
                 2.0 
                 1.5 
                 2.0 
                 3.7 
                 2.7 
                 3.2 
               
               
                 a-1 
                 1203 
                 3540 
                 7598 
                 75 
                 846 
                 4 
                 1.9 
                 1.7 
                 3.0 
                 3.1 
                 3.0 
                 3.9 
               
               
                 b-1 
                 1232 
                 3540 
                 6433 
                 86 
                 782 
                 4 
                 1.6 
                 2.0 
                 5.3 
                 4.1 
                 4.7 
                 4.0 
               
               
                 c-1 
                 1280 
                 3540 
                 6363 
                 87 
                 889 
                 3 
                 1.6 
                 1.7 
                 4.0 
                 2.9 
                 3.0 
                 2.7 
               
               
                 d-1 
                 1191 
                 3540 
                 7037 
                 79 
                 804 
                 3 
                 2.0 
                 2.2 
                 4.2 
                 4.2 
                 3.1 
                 3.7 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
            
               
                   
                   
                 Number of times 
                 Reduction ratio 
                   
                 Final reduction 
                 Final reduction 
                   
               
               
                   
                   
                 of rolling 
                 of rolling at 
                   
                 temperature of 
                 ratio of 
                   
               
               
                   
                   
                 in which 
                 1100° C. or 
                 T2 
                 finish rolling 
                 finish rolling 
                   
               
               
                   
                 Steel 
                 X ≧ 2.3 
                 lower (%) 
                 (° C.) 
                 (° C.) 
                 (%) 
                 Remarks 
               
               
                   
               
               
                   
                 A-1 
                 4 
                 84 
                 885 
                 871 
                 29 
                 Developed steel 
               
               
                   
                 B-1 
                 4 
                 70 
                 874 
                 861 
                 25 
                 Developed steel 
               
               
                   
                 C-1 
                 4 
                 77 
                 883 
                 854 
                 17 
                 Developed steel 
               
               
                   
                 C-2 
                 4 
                 70 
                 883 
                 850 
                 21 
                 Comparative steel 
               
               
                   
                 C-3 
                 4 
                 71 
                 883 
                 857 
                 23 
                 Developed steel 
               
               
                   
                 C-4 
                 4 
                 87 
                 883 
                 868 
                 23 
                 Comparative steel 
               
               
                   
                 C-5 
                 4 
                 87 
                 883 
                 858 
                 29 
                 Developed steel 
               
               
                   
                 C-6 
                 4 
                 83 
                 883 
                 873 
                 30 
                 Comparative steel 
               
               
                   
                 C-7 
                 4 
                 71 
                 883 
                 840 
                 28 
                 Developed steel 
               
               
                   
                 C-8 
                 4 
                 84 
                 883 
                 823 
                 27 
                 Comparative steel 
               
               
                   
                 D-1 
                 5 
                 90 
                 875 
                 868 
                 17 
                 Developed steel 
               
               
                   
                 E-1 
                 4 
                 76 
                 877 
                 868 
                 25 
                 Developed steel 
               
               
                   
                 E-2 
                 4 
                 71 
                 877 
                 837 
                 15 
                 Comparative steel 
               
               
                   
                 E-3 
                 4 
                 89 
                 877 
                 858 
                 29 
                 Developed steel 
               
               
                   
                 E-4 
                 4 
                 95 
                 877 
                 805 
                 29 
                 Comparative steel 
               
               
                   
                 E-5 
                 4 
                 88 
                 877 
                 807 
                 25 
                 Developed steel 
               
               
                   
                 E-6 
                 4 
                 75 
                 877 
                 802 
                 23 
                 Comparative steel 
               
               
                   
                 E-7 
                 4 
                 76 
                 877 
                 834 
                 27 
                 Developed steel 
               
               
                   
                 E-8 
                 1 
                 66 
                 877 
                 855 
                 18 
                 Comparative steel 
               
               
                   
                 E-9 
                 2 
                 69 
                 877 
                 816 
                 19 
                 Developed steel 
               
               
                   
                 E-10 
                 6 
                 67 
                 877 
                 846 
                 19 
                 Developed steel 
               
               
                   
                 E-11 
                 2 
                 35 
                 877 
                 876 
                 10 
                 Comparative steel 
               
               
                   
                 E-12 
                 4 
                 70 
                 877 
                 762 
                 20 
                 Comparative steel 
               
               
                   
                 E-13 
                 4 
                 86 
                 877 
                 783 
                 20 
                 Developed steel 
               
               
                   
                 E-14 
                 4 
                 67 
                 877 
                 895 
                 21 
                 Developed steel 
               
               
                   
                 E-15 
                 4 
                 79 
                 877 
                 913 
                 27 
                 Comparative steel 
               
               
                   
                 E-16 
                 3 
                 82 
                 877 
                 819 
                 2 
                 Comparative steel 
               
               
                   
                 E-17 
                 4 
                 80 
                 877 
                 872 
                 9 
                 Developed steel 
               
               
                   
                 E-18 
                 4 
                 88 
                 877 
                 797 
                 38 
                 Developed steel 
               
               
                   
                 F-1 
                 4 
                 79 
                 878 
                 842 
                 16 
                 Developed steel 
               
               
                   
                 G-1 
                 4 
                 84 
                 875 
                 857 
                 16 
                 Developed steel 
               
               
                   
                 H-1 
                 4 
                 88 
                 915 
                 914 
                 30 
                 Developed steel 
               
               
                   
                 I-1 
                 3 
                 73 
                 890 
                 882 
                 29 
                 Developed steel 
               
               
                   
                 a-1 
                 4 
                 79 
                 877 
                 877 
                 22 
                 Comparative steel 
               
               
                   
                 b-1 
                 4 
                 88 
                 876 
                 800 
                 27 
                 Comparative steel 
               
               
                   
                 c-1 
                 4 
                 72 
                 871 
                 812 
                 28 
                 Comparative steel 
               
               
                   
                 d-1 
                 4 
                 72 
                 876 
                 868 
                 30 
                 Comparative steel 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 3 
               
             
            
               
                   
               
               
                 Production conditions 
               
            
           
           
               
               
               
               
               
               
               
            
               
                   
                 Cooling 
                   
                   
                   
                   
                   
               
               
                   
                 rate 
                   
                   
                 Cooling 
                   
                   
               
               
                   
                 from 
                 Holding 
                   
                 rate 
                   
                   
               
               
                   
                 final 
                 time at 
                   
                 from 
                   
                   
               
               
                   
                 reduc- 
                 750° C. 
                   
                 600° C. 
                   
                   
               
               
                   
                 tion to 
                 to 
                   
                 to 
                 Winding 
                   
               
               
                   
                 750° C. 
                 600° C. 
                 T3 
                 T3° C. 
                 temper- 
                   
               
               
                 Steel 
                 (° C./s) 
                 (s) 
                 (° C.) 
                 (° C./s) 
                 ature 
                 Remarks 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
            
               
                 A-1 
                 118 
                 7.9 
                 513 
                 80 
                 162 
                 Developed steel 
               
               
                 B-1 
                 73 
                 8.3 
                 474 
                 102 
                 294 
                 Developed steel 
               
               
                 C-1 
                 114 
                 8.1 
                 494 
                 97 
                 196 
                 Developed steel 
               
               
                 C-2 
                 43 
                 6.6 
                 494 
                 59 
                 104 
                 Comparative steel 
               
               
                 C-3 
                 61 
                 8.1 
                 494 
                 75 
                 147 
                 Developed steel 
               
               
                 C-4 
                 119 
                 3.1 
                 494 
                 83 
                 301 
                 Comparative steel 
               
               
                 C-5 
                 98 
                 18 
                 494 
                 68 
                 90 
                 Developed steel 
               
               
                 C-6 
                 77 
                 12.1 
                 494 
                 43 
                 70 
                 Comparative steel 
               
               
                 C-7 
                 86 
                 10.1 
                 494 
                 56 
                 107 
                 Developed steel 
               
               
                 C-8 
                 114 
                 12.2 
                 494 
                 62 
                 513 
                 Comparative steel 
               
               
                 D-1 
                 98 
                 11.8 
                 513 
                 73 
                 174 
                 Developed steel 
               
               
                 E-1 
                 76 
                 11.9 
                 497 
                 67 
                 147 
                 Developed steel 
               
               
                 E-2 
                 114 
                 10.3 
                 497 
                 67 
                 107 
                 Comparative steel 
               
               
                 E-3 
                 91 
                 8.6 
                 497 
                 79 
                 265 
                 Developed steel 
               
               
                 E-4 
                 94 
                 12.2 
                 497 
                 96 
                 301 
                 Comparative steel 
               
               
                 E-5 
                 78 
                 8.2 
                 497 
                 60 
                 184 
                 Developed steel 
               
               
                 E-6 
                 71 
                 10.9 
                 497 
                 73 
                 84 
                 Comparative steel 
               
               
                 E-7 
                 80 
                 8.5 
                 497 
                 87 
                 455 
                 Developed steel 
               
               
                 E-8 
                 111 
                 8 
                 497 
                 89 
                 133 
                 Comparative steel 
               
               
                 E-9 
                 83 
                 12 
                 497 
                 64 
                 58 
                 Developed steel 
               
               
                 E-10 
                 101 
                 6.6 
                 497 
                 95 
                 303 
                 Developed steel 
               
               
                 E-11 
                 114 
                 8.9 
                 497 
                 100 
                 85 
                 Comparative steel 
               
               
                 E-12 
                 113 
                 9.7 
                 497 
                 92 
                 112 
                 Comparative steel 
               
               
                 E-13 
                 70 
                 7.4 
                 497 
                 91 
                 108 
                 Developed steel 
               
               
                 E-14 
                 88 
                 9.5 
                 497 
                 76 
                 134 
                 Developed steel 
               
               
                 E-15 
                 75 
                 8.2 
                 497 
                 68 
                 282 
                 Comparative steel 
               
               
                 E-16 
                 118 
                 9.1 
                 497 
                 71 
                 213 
                 Comparative steel 
               
               
                 E-17 
                 106 
                 6.7 
                 497 
                 97 
                 153 
                 Developed steel 
               
               
                 E-18 
                 95 
                 9.1 
                 497 
                 81 
                 104 
                 Developed steel 
               
               
                 F-1 
                 83 
                 9.3 
                 455 
                 87 
                 413 
                 Developed steel 
               
               
                 G-1 
                 69 
                 11.3 
                 500 
                 66 
                 175 
                 Developed steel 
               
               
                 H-1 
                 93 
                 8.9 
                 489 
                 62 
                 120 
                 Developed steel 
               
               
                 I-1 
                 86 
                 8.3 
                 497 
                 101 
                 79 
                 Developed steel 
               
               
                 a-1 
                 83 
                 12.3 
                 520 
                 83 
                 139 
                 Comparative steel 
               
               
                 b-1 
                 85 
                 8.8 
                 413 
                 91 
                 75 
                 Comparative steel 
               
               
                 c-1 
                 88 
                 6.9 
                 504 
                 63 
                 62 
                 Comparative steel 
               
               
                 d-1 
                 121 
                 7.1 
                 489 
                 84 
                 62 
                 Comparative steel 
               
               
                   
               
            
           
         
       
     
     Regarding the produced hot-rolled steel sheets, area fractions of ferrite, hard phases (martensite and austenite), and the other structure were determined, and the shapes of ferrite grains and the hard phases and an X-ray random intensity ratio were measured. In addition, tensile strength characteristics, a hole expansion ratio, and fatigue characteristics were measured. As conditions for measuring these characteristics, the above-described measurement conditions were used. Fatigue test pieces with the shape and dimensions illustrated in  FIG. 1  were used, and the thickness of each test piece was set to 3 mm. Tables 4 and 5 show the measurement results of the characteristics. Steel grades of the hot-rolled steel sheets were a hot-rolled steel sheet without plating (HR), a hot-dip galvanized steel sheet without alloying after plating (GI), and an alloyed hot-dip galvanized steel sheet (GA). 
     
       
         
           
               
             
               
                 TABLE 4 
               
               
                   
               
               
                 Properties 
               
               
                   
               
             
            
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
            
               
                   
                   
                   
                   
                   
                   
                 Proportion of hard 
                 Length in rolling 
               
               
                   
                   
                   
                   
                   
                 Volume 
                 phase with aspect 
                 direction of hard 
               
               
                   
                   
                 Ferrite 
                 Sum of volume 
                   
                 fraction 
                 ratio of 3 or more 
                 phase in sheet- 
               
               
                   
                   
                 volume 
                 fractions of 
                 Name of 
                 of other 
                 in hard phase in 
                 thickness 
               
               
                   
                 Steel 
                 fraction 
                 martensite and 
                 other 
                 structure 
                 sheet-thickness 
                 central portion 
               
               
                 Steel 
                 grade* 
                 (%) 
                 austenite (%) 
                 structure 
                 (%) 
                 central portion (%) 
                 (μm) 
               
               
                   
               
               
                 A-1 
                 HR 
                 95.5 
                 4.5 
                   
                   
                 84.712 
                 8.5 
               
               
                 B-1 
                 HR 
                 81.1 
                 18.9 
                   
                   
                 83.3 
                 14.9 
               
               
                 C-1 
                 HR 
                 90.5 
                 9.5 
                   
                   
                 90.9 
                 10.2 
               
               
                 C-2 
                 HR 
                 89.4 
                 10.6 
                   
                   
                 86.3 
                 22.9 
               
               
                 C-3 
                 HR 
                 90.3 
                 8.7 
                   
                   
                 91.6 
                 19.2 
               
               
                 C-4 
                 GI 
                 17.0 
                 83.0 
                   
                   
                 81.5 
                 6.1 
               
               
                 C-5 
                 HR 
                 93.3 
                 6.7 
                   
                   
                 84.5 
                 11.2 
               
               
                 C-6 
                 HR 
                 90.9 
                 2.8 
                 bainite 
                 6.3 
                 89 
                 13.7 
               
               
                 C-7 
                 HR 
                 90.4 
                 3.9 
                 bainite 
                 5.7 
                 89.3 
                 13.5 
               
               
                 C-8 
                 GA 
                 93.6 
                 1.4 
                 bainite 
                 5 
                 88 
                 9.3 
               
               
                 D-1 
                 HR 
                 88.0 
                 12.0 
                   
                   
                 83.7 
                 10.7 
               
               
                 E-1 
                 HR 
                 89.5 
                 10.5 
                   
                   
                 83.9 
                 12.5 
               
               
                 E-2 
                 HR 
                 88.1 
                 11.9 
                   
                   
                 89 
                 25.5 
               
               
                 E-3 
                 HR 
                 86.5 
                 13.5 
                   
                   
                 91.9 
                 17.8 
               
               
                 E-4 
                 GA 
                 92.0 
                 8.0 
                   
                   
                 91.2 
                 12.7 
               
               
                 E-5 
                 HR 
                 86.4 
                 13.8 
                   
                   
                 95 
                 12.9 
               
               
                 E-6 
                 HR 
                 89.2 
                 10.8 
                   
                   
                 93.5 
                 16.1 
               
               
                 E-7 
                 GI 
                 88.0 
                 14.0 
                   
                   
                 89.3 
                 14.3 
               
               
                 E-8 
                 HR 
                 85.7 
                 14.3 
                   
                   
                 82.2 
                 9.6 
               
               
                 E-9 
                 HR 
                 91.0 
                 8.0 
                   
                   
                 87.1 
                 12.1 
               
               
                 E-10 
                 HR 
                 83.7 
                 16.3 
                   
                   
                 85.1 
                 11.8 
               
               
                 E-11 
                 HR 
                 85.0 
                 15.0 
                   
                   
                 85.1 
                 9.9 
               
               
                 E-12 
                 GA 
                 87.6 
                 12.4 
                   
                   
                 100 
                 10.1 
               
               
                 E-13 
                 HR 
                 84.5 
                 15.5 
                   
                   
                 98.8 
                 14.6 
               
               
                 E-14 
                 HR 
                 86.4 
                 13.8 
                   
                   
                 62.1 
                 11.9 
               
               
                 E-15 
                 HR 
                 85.2 
                 14.8 
                   
                   
                 55.4 
                 13.3 
               
               
                 E-16 
                 HR 
                 86.0 
                 14.0 
                   
                   
                 51.9 
                 8.5 
               
               
                 E-17 
                 HR 
                 88.8 
                 13.2 
                   
                   
                 65 
                 9.3 
               
               
                 E-18 
                 HR 
                 85.7 
                 14.3 
                   
                   
                 97.9 
                 12.8 
               
               
                 F-1 
                 HR 
                 88.4 
                 11.6 
                   
                   
                 86.6 
                 13.9 
               
               
                 G-1 
                 HR 
                 90.2 
                 9.6 
                   
                   
                 83.8 
                 16.0 
               
               
                 H-1 
                 HR 
                 89.3 
                 10.7 
                   
                   
                 84.1 
                 12.7 
               
               
                 I-1 
                 HR 
                 89.2 
                 10.8 
                   
                   
                 84.8 
                 13.8 
               
               
                 a-1 
                 HR 
                 97.5 
                 2.5 
                   
                   
                 85 
                 11.5 
               
               
                 b-1 
                 HR 
                 58.5 
                 43.5 
                   
                   
                 94.6 
                 12.8 
               
               
                 c-1 
                 HR 
                 90.3 
                 9.7 
                   
                   
                 85.9 
                 13.5 
               
               
                 d-1 
                 HR 
                 87.0 
                 13.0 
                   
                   
                 82.8 
                 7.2 
               
               
                   
               
            
           
           
               
               
               
               
               
               
            
               
                   
                   
                   
                 Sum of X-ray random 
                   
                   
               
               
                   
                   
                 Average 
                 intensity ratios 
                 Sum of X-ray random 
                   
               
               
                   
                   
                 aspect 
                 of &lt;011&gt; orientation 
                 intensity ratios 
                   
               
               
                   
                   
                 ratio of 
                 and &lt;111&gt; orientation 
                 of &lt;001&gt; orientation 
                   
               
               
                   
                   
                 ferrite 
                 as viewed from 
                 as viewed from 
                   
               
               
                   
                 Steel 
                 grains 
                 rolling direction 
                 rolling direction 
                 Remarks 
               
               
                   
               
               
                   
                 A-1 
                 2.4 
                 4.39 
                 0.67 
                 Developed steel 
               
               
                   
                 B-1 
                 2.1 
                 5.25 
                 0.61 
                 Developed steel 
               
               
                   
                 C-1 
                 2.7 
                 5.31 
                 0.65 
                 Developed steel 
               
               
                   
                 C-2 
                 2.6 
                 5.57 
                 0.57 
                 Comparative steel 
               
               
                   
                 C-3 
                 2.3 
                 4.90 
                 0.64 
                 Developed steel 
               
               
                   
                 C-4 
                 1.9 
                 5.71 
                 0.57 
                 Comparative steel 
               
               
                   
                 C-5 
                 2.8 
                 4.81 
                 0.67 
                 Developed steel 
               
               
                   
                 C-6 
                 1.9 
                 5.35 
                 0.65 
                 Comparative steel 
               
               
                   
                 C-7 
                 3.0 
                 5.51 
                 0.64 
                 Developed steel 
               
               
                   
                 C-8 
                 3.7 
                 5.04 
                 0.68 
                 Comparative steel 
               
               
                   
                 D-1 
                 1.8 
                 5.70 
                 0.58 
                 Developed steel 
               
               
                   
                 E-1 
                 1.9 
                 4.65 
                 0.69 
                 Developed steel 
               
               
                   
                 E-2 
                 2.7 
                 4.80 
                 0.6 
                 Comparative steel 
               
               
                   
                 E-3 
                 2.6 
                 4.52 
                 0.70 
                 Developed steel 
               
               
                   
                 E-4 
                 4.0 
                 3.26 
                 1.03 
                 Comparative steel 
               
               
                   
                 E-5 
                 3.6 
                 5.99 
                 0.55 
                 Developed steel 
               
               
                   
                 E-6 
                 3.8 
                 3.04 
                 1.16 
                 Comparative steel 
               
               
                   
                 E-7 
                 3.2 
                 3.70 
                 0.92 
                 Developed steel 
               
               
                   
                 E-8 
                 2.3 
                 2.91 
                 1.38 
                 Comparative steel 
               
               
                   
                 E-9 
                 3.5 
                 4.10 
                 0.78 
                 Developed steel 
               
               
                   
                 E-10 
                 2.6 
                 6.08 
                 0.57 
                 Developed steel 
               
               
                   
                 E-11 
                 1.7 
                 2.82 
                 1.43 
                 Comparative steel 
               
               
                   
                 E-12 
                 6.3 
                 5.28 
                 0.60 
                 Comparative steel 
               
               
                   
                 E-13 
                 4.8 
                 5.08 
                 0.67 
                 Developed steel 
               
               
                   
                 E-14 
                 1.5 
                 5.24 
                 0.63 
                 Developed steel 
               
               
                   
                 E-15 
                 1.3 
                 5.21 
                 0.63 
                 Comparative steel 
               
               
                   
                 E-16 
                 3.7 
                 4.20 
                 0.74 
                 Comparative steel 
               
               
                   
                 E-17 
                 2.0 
                 4.26 
                 0.70 
                 Developed steel 
               
               
                   
                 E-18 
                 4.3 
                 5.52 
                 0.59 
                 Developed steel 
               
               
                   
                 F-1 
                 2.6 
                 5.70 
                 0.64 
                 Developed steel 
               
               
                   
                 G-1 
                 2.0 
                 4.59 
                 0.71 
                 Developed steel 
               
               
                   
                 H-1 
                 1.8 
                 4.93 
                 0.71 
                 Developed steel 
               
               
                   
                 I-1 
                 2.3 
                 4.14 
                 0.73 
                 Developed steel 
               
               
                   
                 a-1 
                 1.5 
                 4.65 
                 0.68 
                 Comparative steel 
               
               
                   
                 b-1 
                 3.7 
                 5.52 
                 0.63 
                 Comparative steel 
               
               
                   
                 c-1 
                 3.8 
                 4.39 
                 0.74 
                 Comparative steel 
               
               
                   
                 d-1 
                 2.1 
                 4.48 
                 0.70 
                 Comparative steel 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 5 
               
             
            
               
                   
               
               
                 Properties 
               
            
           
           
               
               
               
               
               
               
               
               
               
            
               
                   
                   
                   
                   
                   
                   
                   
                 Punching 
                   
               
               
                   
                   
                   
                 Hole 
                   
                   
                 Fatigue 
                 fatigue limit 
                   
               
               
                   
                 Tensile 
                 Total 
                 expansion 
                   
                   
                 limit ratio 
                 ratio in 
                   
               
               
                   
                 strength, 
                 elongation, 
                 ratio, 
                   
                   
                 in rolling 
                 rolling 
                   
               
               
                 Steel 
                 TS (MPa) 
                 El (%) 
                 λ (%) 
                 TS × El 
                 TS × λ 
                 direction 
                 direction 
                 Remarks 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
            
               
                 A-1 
                 663 
                 30.0 
                 93 
                 19890 
                 61659 
                 0.57 
                 0.31 
                 Developed steel 
               
               
                 B-1 
                 668 
                 28.0 
                 56 
                 18704 
                 37408 
                 0.66 
                 0.42 
                 Developed steel 
               
               
                 C-1 
                 595 
                 34.0 
                 95 
                 20230 
                 56525 
                 0.59 
                 0.38 
                 Developed steel 
               
               
                 C-2 
                 622 
                 33.0 
                 54 
                 20526 
                 33588 
                 0.58 
                 0.37 
                 Comparative steel 
               
               
                 C-3 
                 624 
                 32.0 
                 63 
                 19968 
                 39312 
                 0.58 
                 0.38 
                 Developed steel 
               
               
                 C-4 
                 993 
                 12.0 
                 41 
                 11916 
                 40713 
                 0.59 
                 0.36 
                 Comparative steel 
               
               
                 C-5 
                 595 
                 35.0 
                 101 
                 20825 
                 60095 
                 0.57 
                 0.34 
                 Developed steel 
               
               
                 C-6 
                 591 
                 34.0 
                 108 
                 20094 
                 63828 
                 0.59 
                 0.25 
                 Comparative steel 
               
               
                 C-7 
                 625 
                 33.0 
                 106 
                 20625 
                 66250 
                 0.55 
                 0.30 
                 Developed steel 
               
               
                 C-8 
                 571 
                 36.0 
                 117 
                 20556 
                 66807 
                 0.58 
                 0.19 
                 Comparative steel 
               
               
                 D-1 
                 586 
                 34.0 
                 86 
                 19924 
                 50396 
                 0.70 
                 0.35 
                 Developed steel 
               
               
                 E-1 
                 579 
                 34.0 
                 88 
                 19686 
                 50952 
                 0.68 
                 0.35 
                 Developed steel 
               
               
                 E-2 
                 619 
                 32.0 
                 56 
                 19808 
                 34664 
                 0.70 
                 0.36 
                 Comparative steel 
               
               
                 E-3 
                 625 
                 32.0 
                 62 
                 20000 
                 38750 
                 0.66 
                 0.40 
                 Developed steel 
               
               
                 E-4 
                 580 
                 35.0 
                 93 
                 20300 
                 53940 
                 0.51 
                 0.35 
                 Comparative steel 
               
               
                 E-5 
                 625 
                 32.0 
                 81 
                 20000 
                 50625 
                 0.61 
                 0.37 
                 Developed steel 
               
               
                 E-6 
                 596 
                 33.0 
                 86 
                 19635 
                 51170 
                 0.52 
                 0.38 
                 Comparative steel 
               
               
                 E-7 
                 640 
                 30.0 
                 79 
                 19200 
                 50560 
                 0.57 
                 0.35 
                 Developed steel 
               
               
                 E-8 
                 664 
                 30.0 
                 77 
                 19920 
                 51128 
                 0.50 
                 0.35 
                 Comparative steel 
               
               
                 E-9 
                 571 
                 35.0 
                 92 
                 19985 
                 52532 
                 0.61 
                 0.35 
                 Developed steel 
               
               
                 E-10 
                 669 
                 29.0 
                 70 
                 19401 
                 46830 
                 0.72 
                 0.40 
                 Developed steel 
               
               
                 E-11 
                 648 
                 30.0 
                 74 
                 19440 
                 47952 
                 0.54 
                 0.38 
                 Comparative steel 
               
               
                 E-12 
                 604 
                 28.0 
                 87 
                 16912 
                 52548 
                 0.66 
                 0.39 
                 Comparative steel 
               
               
                 E-13 
                 660 
                 28.0 
                 68 
                 18480 
                 44880 
                 0.69 
                 0.37 
                 Developed steel 
               
               
                 E-14 
                 655 
                 30.0 
                 70 
                 19650 
                 45850 
                 0.66 
                 0.34 
                 Developed steel 
               
               
                 E-15 
                 650 
                 30.0 
                 69 
                 19500 
                 44850 
                 0.70 
                 0.20 
                 Comparative steel 
               
               
                 E-16 
                 650 
                 31.0 
                 69 
                 20180 
                 44850 
                 0.61 
                 0.25 
                 Comparative steel 
               
               
                 E-17 
                 620 
                 32.0 
                 84 
                 19840 
                 52080 
                 0.62 
                 0.33 
                 Developed steel 
               
               
                 E 18 
                 609 
                 29.0 
                 75 
                 19401 
                 50175 
                 0.72 
                 0.43 
                 Developed steel 
               
               
                 F-1 
                 608 
                 33.0 
                 90 
                 20064 
                 54720 
                 0.72 
                 0.35 
                 Developed steel 
               
               
                 G-1 
                 581 
                 31.0 
                 82 
                 18011 
                 47642 
                 0.69 
                 0.38 
                 Developed steel 
               
               
                 H-1 
                 596 
                 34.0 
                 65 
                 20264 
                 38740 
                 0.64 
                 0.38 
                 Developed steel 
               
               
                 I-1 
                 600 
                 33.0 
                 84 
                 19800 
                 50400 
                 0.62 
                 0.36 
                 Developed steel 
               
               
                 a-1 
                 448 
                 47.0 
                 146 
                 21056 
                 65408 
                 0.69 
                 0.20 
                 Comparative steel 
               
               
                 b-1 
                 1002 
                 17.0 
                 31 
                 17034 
                 31062 
                 0.69 
                 0.36 
                 Comparative steel 
               
               
                 c-1 
                 583 
                 28.0 
                 54 
                 16324 
                 31482 
                 0.67 
                 0.38 
                 Comparative steel 
               
               
                 d-1 
                 643 
                 31.0 
                 52 
                 19933 
                 33436 
                 0.64 
                 0.39 
                 Comparative steel 
               
               
                   
               
            
           
         
       
     
     As shown in Tables 2 to 5, steels A-1, B-1, C-1, C-3, C-5, C-7, D-1, E-1, E-3, E-5, E-7, E-9, E-10, E-13, E-14, E-17, E-18, F-1, G-1, H-1, I-1, and J-1 are examples each having a chemical composition and microstructure of steel satisfying those specified in the present invention. Meanwhile, steels C-2, C-4, C-6, C-8, E-2, E-4, E-6, E-8, E-11, E-12, E-15, E-16, a-1, b-1, c-1, and d-1 are examples each having a chemical composition and microstructure of steel not satisfying those specified in the present invention. The “other structure” of each of C-6 to C-8 was bainite. 
     For all of the hot-rolled steel sheets of the present invention examples, such as steel A-1, the area fraction of the hard phases, the proportion of the hard phases with an aspect ratio of 3 or more in the hard phases present in the sheet-thickness central portion, the length in the rolling direction of the hard phases present in the sheet-thickness central portion, the average aspect ratio of ferrite grains, and the X-ray random intensity ratios all satisfied those specified in the present invention. Furthermore, all of the hot-rolled steel sheets of the present invention examples satisfied (tensile strength (MPa))×(total elongation (%))≧18000 and (tensile strength (MPa))×(hole expansion ratio (%))≧35000, and exhibited a fatigue limit of 0.55 or more and a punching fatigue limit of 0.30 or more. 
     For steel C-2 as a comparative example, the average cooling rate from the final reduction temperature to 750° C. in step [e] was 43° C./s, which is too low. Therefore, the length in the rolling direction of the hard phases in the sheet-thickness central portion was as long as 22.9 μm, and (tensile strength (MPa))×(hole expansion ratio (%))≧35000 was not satisfied. 
     For steel C-4, the holding time in a temperature range of equal to or higher than 600° C. and lower than 750° C. in step [f] was 3.1 s, which is too short; thus, the area fraction of the hard phases was as high as 83.0%, ferrite not serving as the main constituent of the microstructure. Therefore, low ductility was exhibited, and (tensile strength (MPa))×(total elongation (%))≧18000 was not satisfied. 
     For steel C-6, the average cooling rate in a temperature range of equal to or higher than T 3 (° C.) and lower than 600° C. in step [g] was too low. For steel C-8, the winding temperature in step [h] was 513° C., which is higher than T 3  (494° C.). Therefore, bainite was generated in the structure of the hot-rolled steel sheet, and the area fraction of the hard phases was as low as less than 3%. Consequently, the punching fatigue limit ratio in the rolling direction was as low as less than 0.3. 
     For steel E-2, the slab heating time in step [b] was 1168 s, which is shorter than time t 1  (1244 s) specified in formula (A). Therefore, the length in the rolling direction of the hard phases in the sheet-thickness central portion was as long as 25.5 μm, and (tensile strength (MPa))×(hole expansion ratio (%))≧35000 was not satisfied. 
     For steel E-4, the total reduction ratio during rough rolling in step [c] was as low as 46%. For steel E-6, the number of times of cooling the slab surface layer to Ar 3  transformation point or lower during rough rolling in step [c] was only once. For steel E-8, of the six rolling passes in step [d], only one pass satisfied a shape ratio X of 2.3 or more. For steel E-11, the reduction ratio of rolling at 1100° C. or lower in step [d] was as low as 35%. Therefore, in these steels, the sum of X-ray random intensity ratios of &lt;011&gt; orientation and &lt;111&gt; orientation as viewed from the rolling direction was as low as less than 3.5, and an X-ray random intensity ratio of &lt;001&gt; orientation as viewed from the rolling direction was more than 1.0. Consequently, these steels all exhibited a fatigue limit ratio in the rolling direction as low as less than 0.55. 
     For steel E-12, the reduction temperature in the final pass of finish rolling in step [d] was 762° C., which is lower than T 2  (877° C.), specified in formula (D), by more than 100° C. Therefore, the average aspect ratio of ferrite grains was as large as 6.3, and in the tensile test, ferrite grains underwent work hardening to reduce the ductility of the steel sheet. Consequently, (tensile strength (MPa))×(total elongation (%))≧18000 was not satisfied. 
     For steel E-15, the reduction temperature in the final pass of finish rolling in step [d] was 913° C., which is higher than T 2  (877° C.), specified in formula (D), by more than 20° C. For steel E-16, the reduction ratio in the final pass of finish rolling in step [d] was as low as 2%. Therefore, for both examples, the proportion of the hard phases with an aspect ratio of 3 or more in the hard phases present in the sheet-thickness central portion was as low as less than 60%, and the punching fatigue limit ratio in the rolling direction was as low as less than 0.3. 
     For steel a-1, the C content was 0.018%, which is too low. Therefore, the punching fatigue limit ratio in the rolling direction was as low as less than 0.3. 
     For steel b-1, the C content was 0.254%, which is too high. For steel d-1, the S content was 0.0361%, which is too high. Therefore, both examples exhibited low hole expandability and did not satisfy (tensile strength (MPa))×(hole expansion ratio (%))≧35000. 
     For steel c-1, the P content was 0.155%, which is too high. Therefore, low workability was exhibited, and neither (tensile strength (MPa))×(total elongation (%))≧18000 nor (tensile strength (MPa))×(hole expansion ratio (%))≧35000 was satisfied. 
     INDUSTRIAL APPLICABILITY 
     According to the present invention, a hot-rolled steel sheet having excellent fatigue characteristics in the rolling direction and workability can be provided. The present invention can be suitably applied to steel sheets with a sheet thickness of 8 mm or less. A hot-rolled steel sheet according to the present invention can prolong fatigue life of suspension parts and the like of automobile materials, thus significantly contributing to the industry. 
     REFERENCE SIGNS LIST 
     
         
           1  punching hole of fatigue test piece