Patent Publication Number: US-2022235443-A1

Title: Non-heat treated wire rod with excellent wire drawability and impact toughness and manufacturing method therefor

Description:
TECHNICAL FIELD 
     The present disclosure relates to a non-quenched and tempered wire rod and a method of manufacturing the same, and more particularly, to a non-quenched and tempered wire rod having excellent drawability and impact toughness suitable for materials for automobiles or mechanical parts and a method of manufacturing the same. 
     BACKGROUND ART 
     Most structural steels that have been used for mechanical structures or automobile parts are quenched and tempered steels having improved strength and toughness via reheating, quenching, and tempering processes after a hot process. 
     On the contrary, non-heat-treated steels are steels having similar strength to those of quenched and tempered steels, which are heat-treated, without undergoing heat treatment after hot working. Non-quenched and tempered wire rods have excellent economic feasibility by lowering manufacturing costs by omitting a heat treatment process involved in manufacturing processes of conventional quenched and tempered wire rods. Also, linearity of the non-quenched and tempered wire rods is maintained since heat treatment deflection, i.e., defect caused during heat treatment, is not generated by omitting final quenching and tempering steps. Thus, application of such non-quenched and tempered wire rods to various products has been attempted. 
     Particularly, ferritic-pearlitic non-quenched and tempered wire rods are advantageous in that components may be designed with low costs and a uniform structure may be stably obtained in a Stelmor cooling conveyer. However, as drawability increases, strength of products increases but problems of rapid decreases in ductility and toughness occur. 
     As a method to solve the above problems, a technique of obtaining a bainite-based microstructure using an expensive quenching element such as molybdenum (Mo) and boron (B) has been reported, but this technique is difficult to apply for commercial production due to deviation of physical properties caused by non-uniformity of the bainite structure by cooling deviation on the Stelmor cooling conveyer during manufacturing wire rods. 
     DISCLOSURE 
     Technical Problem 
     The present disclosure has been proposed to solve the above problems and an object of the present disclosure is to provide a non-quenched and tempered wire rod having excellent drawability and impact toughness without additional heat treatment and a method of manufacturing the same. 
     Technical Solution 
     One aspect of the present disclosure provides a non-quenched and tempered wire rod having excellent drawability and impact toughness including, in percent by weight (wt %), 0.05 to 0.35% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.5 to 2.0% of manganese (Mn), 1.0% or less of chromium (Cr), 0.03% or less of phosphorus (P), 0.03% or less of sulfur (S), 0.01 to 0.07% of soluble aluminum (sol.Al), 0.01% or less of nitrogen (N), at least one of 0.1% or less of niobium (Nb), 0.5% or less of vanadium (V), and 0.1% or less of titanium (Ti), and the remainder of iron (Fe) and inevitable impurities; and a ferrite-pearlite layered structure, as a microstructure, in a rolling direction. 
     In addition, an average thickness of a ferrite band in an L cross-section, as a cross-section parallel to the rolling direction, may be from 5 μm to 30 μm. 
     In addition, an average particle diameter of the ferrite in a C cross-section, as a cross-section perpendicular to the rolling direction, may be from 3 μm to 20 μm. 
     In addition, a fraction of the ferrite may be from 30% to 90%. 
     In addition, an average lamellar space of the perlite may be from 0.03 μm to 0.3 μm. 
     In addition, a carbon equivalent Ceq represented by the following formula may be from 0.4 to 0.6: 
     
       
         
           
             
               
                 
                   Ceq 
                   ⁢ 
                   
                     = 
                     
                       
                         [ 
                         C 
                         ] 
                       
                       + 
                       
                         
                           [ 
                           
                             S 
                             ⁢ 
                             i 
                           
                           ] 
                         
                         / 
                         9 
                       
                       + 
                       
                         
                           [ 
                           
                             M 
                             ⁢ 
                             n 
                           
                           ] 
                         
                         / 
                         5 
                       
                       + 
                       
                         
                           
                             [ 
                             
                               C 
                               ⁢ 
                               r 
                             
                             ] 
                           
                           / 
                           1 
                         
                         ⁢ 
                         2 
                       
                     
                   
                 
               
               
                 
                     
                 
               
             
           
         
       
     
     (wherein [C], [Si], [Mn], and [Cr] are contents (%) of corresponding elements, respectively). 
     In addition, a difference between a maximum hardness and a minimum hardness in the C cross-section, as the cross-section perpendicular to the rolling direction, may be 30 Hv or less. 
     In addition, an average room temperature impact toughness may be 100 J or more in 30% to 60% drawing. 
     In addition, the wire rod may satisfy Equation (1) below in 30% to 60% drawing: 
     
       
         
           
             
               
                 
                   
                     
                       I 
                       ⁢ 
                       
                           
                       
                       ⁢ 
                       max 
                     
                     - 
                     
                       I 
                       ⁢ 
                       
                           
                       
                       ⁢ 
                       min 
                     
                   
                   ≤ 
                   
                     40 
                     ⁢ 
                     J 
                   
                 
               
               
                 
                   ( 
                   1 
                   ) 
                 
               
             
           
         
       
     
     (wherein Imax is a maximum value of average room temperature impact toughness after drawing and Imin is a minimum value of average room temperature impact toughness after drawing). 
     Another aspect of the present disclosure provides a method of manufacturing a non-quenched and tempered wire rod having excellent drawability and impact toughness including: preparing a billet including, in percent by weight (wt %), 0.05 to 0.35% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.5 to 2.0% of manganese (Mn), 1.0% or less of chromium (Cr), 0.03% or less of phosphorus (P), 0.03% or less of sulfur (S), 0.01 to 0.07% of soluble aluminum (sol.Al), 0.01% or less of nitrogen (N), at least one of 0.1% or less of niobium (Nb), 0.5% or less of vanadium (V), and 0.1% or less of titanium (Ti), and the remainder of iron (Fe) and inevitable impurities; reheating the billet at a reheating temperature Tr satisfying Equation (2) below; rolling the reheated billet into a wire rod; and coiling the rolled wire rod followed by cooling: 
     
       
         
           
             
               
                 
                   T 
                   ⁢ 
                   
                       
                   
                   ⁢ 
                   1 
                   ⁢ 
                   
                     
                       ≤ 
                       
                         T 
                         ⁢ 
                         r 
                       
                       ≤ 
                       
                         1 
                         ⁢ 
                         2 
                         ⁢ 
                         0 
                         ⁢ 
                         
                           0 
                           
                             o 
                             ⁢ 
                             
                                 
                             
                           
                         
                         ⁢ 
                         C 
                       
                     
                     . 
                   
                 
               
               
                 
                   ( 
                   2 
                   ) 
                 
               
             
           
         
       
     
     (wherein T1=757+606[C]+80[Nb]/[C]+1023√[Nb]+330[V], and [C], [Nb], and [V] are contents (%) of corresponding elements, respectively). 
     In addition, the rolling of the reheated billet into the wire rod includes rolling the reheated billet at a final rolling temperature Tf satisfying Equation (3) below: 
     
       
         
           
             
               
                 
                   
                     T 
                     ⁢ 
                     2 
                   
                   ≤ 
                   
                     T 
                     ⁢ 
                     f 
                   
                   ≤ 
                   
                     T 
                     ⁢ 
                     3 
                   
                 
               
               
                 
                   ( 
                   3 
                   ) 
                 
               
             
           
         
       
     
     (wherein T2=955−396[C]+24.6[Si]−68.1[Mn]−24.8[Cr]−36.1[Nb]−20.7[V], 
     T3=734+465[C]−355[Si]+360[Al]+891[Ti]+6800[Nb]−650√[Nb]+730[V]−232√[V], and 
     [C], [Si], [Mn], [Cr], [Al], [Ti], [Nb], and [V] are contents (%) of corresponding elements, respectively). 
     In addition, the cooling includes cooling the wire rod at an average rate of 0.1° C./s to 2° C./s. 
     Advantageous Effects 
     According to an embodiment of the present disclosure, a non-quenched and tempered wire rod having excellent drawability and impact toughness prepared by controlling alloy compositions and manufacturing conditions without additional heat treatment and a method of manufacturing the same may be provided. 
     BEST MODE 
     A non-quenched and tempered wire rod having excellent drawability and impact toughness according to an embodiment of the present disclosure includes: in percent by weight (wt %), 0.05 to 0.35% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.5 to 2.0% of manganese (Mn), 1.0% or less of chromium (Cr), 0.03% or less of phosphorus (P), 0.03% or less of sulfur (S), 0.01 to 0.07% of soluble aluminum (sol.Al), 0.01% or less of nitrogen (N), at least one of 0.1% or less of niobium (Nb), 0.5% or less of vanadium (V), and 0.1% or less of titanium (Ti), and the remainder of iron (Fe) and inevitable impurities, and has a ferrite-pearlite layered structure, as a microstructure, in a rolling direction. 
    
    
     
       DESCRIPTION OF DRAWINGS 
         FIG. 1  is a photograph of a ferrite-pearlite layered structure of a non-quenched and tempered wire rod according to an embodiment of the present disclosure. 
     
    
    
     MODES OF THE INVENTION 
     Hereinafter, embodiments of the present disclosure will be described in detail with reference to the accompanying drawings. The invention may, however, be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of the invention to those skilled in the art. 
     The terms used in the present specification are merely used to describe particular embodiments, and are not intended to limit the present disclosure. An expression used in the singular encompasses the expression of the plural, unless it has a clearly different meaning in the context. In the present specification, it is to be understood that the terms such as “comprise” or “include” are intended to indicate the existence of the features, operations, functions, components, or combinations thereof disclosed in the specification, and are not intended to preclude the possibility that one or more other features, operations, functions, components, or combinations thereof may exist or may be added. 
     The terms used in the present specification have the meaning commonly understood by one of ordinary skill in the art to which the present specification belongs. Terms commonly used should be interpreted in a consistent sense in the context of the present specification. Further, terms used in the present specification should not be interpreted in an idealistic or formal sense unless the meaning is clearly defined. An expression used in the singular encompasses the expression of the plural unless it has a clearly different meaning in the context. 
     Words of degree, such as “about,” “substantially,” and the like are used herein in the sense of “at, or nearly at, when given the manufacturing, design, and material tolerances inherent in the stated circumstances” and are used to prevent the unscrupulous infringer from unfairly taking advantage of the invention disclosure where exact or absolute figures and operational or structural relationships are stated as an aid to understanding the invention. 
     A non-quenched and tempered steel (non-heat-treated steel) refers to a steel having strength similar to that of a quenched and tempered steel that has been heat-treated, without heat treatment after hot working. Non-quenched and tempered wire rods have excellent economic feasibility by lowering manufacturing costs by omitting a heat treatment process involved in manufacturing processes of conventional quenched and tempered wire rods. Also, linearity of the non-quenched and tempered wire rods is maintained since heat treatment deflection, i.e., defect caused during heat treatment, is not generated by omitting final quenching and tempering steps. Thus, application of such non-quenched and tempered wire rods to various products has been attempted. 
     Particularly, ferritic-pearlitic non-quenched and tempered wire rods are advantageous in that components may be designed with low costs and a uniform structure may be stably obtained in a Stelmor cooling conveyer manufacturing process. However, as drawability increases, strength of products increases but problems of rapid decreases in ductility and toughness occur. 
     The present inventors have made intensive efforts, in many different ways, to provide a non-quenched and tempered wire rod having excellent drawability and impact toughness after drawing. As a result, the present inventors have found that increased strength may be obtained together with excellent impact toughness without additional heat treatment by appropriately adjusting the alloy compositions and the microstructure of the non-quenched and tempered wire rod, thereby completing the present disclosure. 
     A non-quenched and tempered wire rod having excellent drawability and impact toughness according to an aspect of the present disclosure includes in percent by weight (wt %), 0.05 to 0.35% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.5 to 2.0% of manganese (Mn), 1.0% or less of chromium (Cr), 0.03% or less of phosphorus (P), 0.03% or less of sulfur (S), 0.01 to 0.07% of soluble aluminum (sol.Al), 0.01% or less of nitrogen (N), at least one of 0.1% or less of niobium (Nb), 0.5% or less of vanadium (V), and 0.1% or less of titanium (Ti), and the remainder of iron (Fe) and inevitable impurities. 
     Hereinafter, the reasons for limitation of the alloy composition of the non-quenched and tempered wire rod will be described in detail. 
     Carbon (C): 0.05 to 0.35 wt % 
     Carbon (C) plays a role in improving strength of a wire rod. The C content is preferably controlled to be 0.05 wt % or more to obtain such effects in the present disclosure. However, when the C content is excessive, deformation resistance of the steel rapidly increases, and thus cold processibility deteriorates thereby. Therefore, it is preferable to control an upper limit of the C content to be 0.35 wt %. 
     Silicon (Si): 0.05 to 0.5 wt % 
     Silicon is an effective element as a deoxidizer. The Si content is preferably controlled to 0.05 wt % or more to obtain such effects in the present disclosure. However, when the Si content is excessive, deformation resistance of a steel rapidly increases due to solid solution strengthening, and thus cold processibility deteriorates thereby. Therefore, an upper limit of the Si content is preferably 0.5 wt % and more preferably 0.25 wt %. 
     Manganese (Mn): 0.5 to 2.0 wt % 
     Manganese is an effective element as a deoxidizer and desulfurizer. The Mn content is preferably controlled to 0.5 wt % or more and more preferably 0.8 wt % or more to obtain such effects in the present disclosure. However, when the Mn content is excessive, strength of a steel increases too high and deformation resistance of the steel increases, thereby deteriorating cold processibility thereof. Therefore, an upper limit of the Mn content is preferably controlled to 2.0 wt % and more preferably 1.8 wt %. 
     Chromium (Cr): 1.0 wt % or less 
     Chromium plays a role in promoting transformation of ferrite and pearlite during hot rolling. Also, Cr contributes to reduction of a period of dynamic harmful effects caused by solid-solution carbon by decreasing the content of the solid-solution carbon by precipitating carbides in a steel without increasing strength of a steel more than necessary. However, when the Cr content is excessive, the strength of the steel increases too high and deformation resistance of the steel rapidly increases, thereby deteriorating cold processibilty thereof. Therefore, the Cr content is preferably 1.0 wt % and more preferably controlled to 0.5 wt %. 
     Phosphorus (P): 0.03 wt % or less 
     Phosphorus, as an impurity inevitably contained in steels, is an element segregated in grain boundaries to decrease toughness of the steels and acts as a main cause of reducing delayed fraction resistance, and it is preferable to control the P content to be as low as possible. Although it is advantageous to control the P content to 0 wt % in theory, P is inevitably contained during a manufacturing process. Therefore, it is important to control an upper limit of the P content, and thus the upper limit of the P content is controlled to 0.03 wt % in the present disclosure. 
     Sulfur (S): 0.03 wt % or less 
     Sulfur, as an impurity inevitably contained in steels, is an element segregated in grain boundaries to significantly decrease ductility of the steels and acting as a main cause of deteriorating delayed fraction resistance and stress relaxation properties by forming sulfides in the steels. Thus, it is preferable to control the S content to be as low as possible. Although it is preferable to control the S content to 0 wt % in theory, S is inevitably contained during a manufacturing process. Therefore, it is important to control an upper limit of the S content, and thus the upper limit of the S content is controlled to 0.03 wt % in the present disclosure. 
     Soluble aluminum (sol.Al): 0.01 to 0.07 wt % 
     Soluble aluminum is an element effectively acting as a deoxidizer. It is preferable that the sol.Al content is 0.01 wt % or more to obtain such effects in the present disclosure. The sol.Al content is more preferably 0.015 wt % or more and even more preferably 0.02 wt % or more. However, when the sol.Al content is excessive, particle diameter refinement effects of austenite increase due to formation of AIN, and thus cold forgeability thereof may deteriorate. Therefore, an upper limit of the sol.Al content is preferably 0.07 wt %. 
     Nitrogen (N): 0.01 wt % or less 
     Nitrogen is an impurity inevitably contained in steels. When the N content is excessive, deformation resistance of a steel rapidly increases due to an increased content of solid-solution nitrogen and thus cold processibilty deteriorates thereby. Although it is preferable to control the N content to 0 wt % in theory, N is inevitably contained during a manufacturing process. Therefore, it is important to control an upper limit of the N content, and thus the upper limit of the N content is controlled preferably to 0.01 wt %, more preferably to 0.008 wt %, and even more preferably to 0.007 wt % in the present disclosure. 
     In addition, the wire rod according to the present disclosure may include the above-described components and at least one of niobium (Nb), vanadium (V) and titanium (Ti). 
     Niobium (Nb): 0.1 wt % or less 
     Niobium is an element playing a role in limiting migration of grain boundaries of austenite and ferrite by forming a carbide and a carbonitride. However, when the Nb content is excessive, the carbonitride acts as a starting point of destruction, thereby deteriorating impact toughness and a problem of forming coarse precipitates may occur. Therefore, it is preferable to add niobium below a solubility limit. Therefore, an upper limit of the Nb content is preferably controlled to 0.1 wt %. 
     Vanadium (V): 0.5 wt % or less 
     Vanadium, like niobium, plays a role in limiting migration of grain boundaries of austenite and ferrite by forming a carbide and a carbonitride. However, when the V content is excessive, the carbonitride acts as a starting point of destruction, thereby deteriorating impact toughness and a problem of forming coarse precipitates may occur. Therefore, it is preferable to add vanadium below a solubility limit. Therefore, an upper limit of the V content is preferably controlled to 0.5 wt %. 
     Titanium (Ti): 0.1 wt % or less 
     Titanium also binds to carbon and nitrogen to form a carbonitride, thereby having an effect on limiting grain boundary size of austenite. However, when the Ti content is excessive, coarse precipitates are formed and the possibility of acting as a major crack generation site for destruction of inclusions increases. Therefore, an upper limit of titanium is preferably controlled to 0.1 wt %. 
     The remainder other than the above-described alloy elements is iron (Fe). In addition, the wire rod for drawing of the present disclosure may include other impurities that may be inevitably contained therein in general industrial manufacturing processes of steels. Since these impurities can be known to anyone skilled in the ordinary manufacturing process, types and contents thereof are not particularly limited in the present specification. 
     In the non-quenched and tempered wire rod according to an embodiment of the present disclosure, a carbon equivalent Ceq represented by the following formula may be from 0.4 to 0.6. When the carbon equivalent Ceq is less than 0.4, a target strength may be difficult to obtain. When the carbon equivalent is greater than 0.6, deformation resistance of a steel rapidly increases, thereby deteriorating cold processibility. 
     
       
         
           
             
               
                 
                   Ceq 
                   ⁢ 
                   
                     = 
                     
                       
                         [ 
                         C 
                         ] 
                       
                       + 
                       
                         
                           [ 
                           
                             S 
                             ⁢ 
                             i 
                           
                           ] 
                         
                         / 
                         9 
                       
                       + 
                       
                         
                           [ 
                           
                             M 
                             ⁢ 
                             n 
                           
                           ] 
                         
                         / 
                         5 
                       
                       + 
                       
                         
                           
                             [ 
                             
                               C 
                               ⁢ 
                               r 
                             
                             ] 
                           
                           / 
                           1 
                         
                         ⁢ 
                         2 
                       
                     
                   
                 
               
               
                 
                     
                 
               
             
           
         
       
     
     In this regard, [C], [Si], [Mn], and [Cr] are contents (%) of corresponding elements, respectively. 
     Hereinafter, a microstructure of the non-quenched and tempered wire rod according to the present disclosure will be described. 
     The non-quenched and tempered wire rod according to an embodiment of the present disclosure includes ferrite and pearlite as a microstructure. Referring to  FIG. 1 , the ferrite and pearlite may form a ferrite-pearlite layered structure (band structure). Also, the layered structure may be a ferrite-pearlite layered structure in a rolling direction according to an embodiment. 
     In this regard, the ferrite-pearlite layered structure in the rolling direction indicates that lengths and widths of a ferrite layer and a pearlite layer are formed in a direction parallel to the rolling direction and in a direction perpendicular to the rolling direction, respectively. 
     The ferrite-pearlite layered structure in the rolling direction has excellent drawability since an initial structure before drawing is aligned in a direction effective for drawing, and the ferrite-pearlite layered structure stretched in the rolling direction by drawing has improved impact toughness since an impact is difficult to propagate in the thickness direction and propagates along a ferrite-pearlite interface that is the weakest portion. 
     In addition, according to an embodiment, the non-quenched and tempered wire rod may include ferrite in an area fraction of 30 to 90%. When the wire rod has the structure as described above, excellent drawability and impact toughness may be obtained together with strength. 
     In the ferrite structure of the present disclosure, an average thickness of a ferrite layer (band) may be from 5 to 30 μm in an L cross-section that is a cross-section parallel to the rolling direction. In addition, an average particle diameter of the ferrite in a C cross-section that is a cross-section perpendicular to the rolling direction may be from 3 μm to 20 μm. 
     The thickness of the ferrite layer refers to a thickness of a ferrite band in the L cross-section that is a cross-section parallel to the rolling direction. When the average thickness of the ferrite band is less than 5 μm, strength increases, thereby deteriorating cold processibility. On the contrary, when the average thickness is greater than 30 μm, a target strength may be difficult to obtain. 
     A particle diameter of the ferrite refers to a particle diameter of ferrite in the C cross-section that is a cross-section perpendicular to the rolling direction. When the average particle diameter of the ferrite is less than 3 μm, strength increases due to grain boundary refinement and thus cold forgeability may decrease. On the contrary, when the average particle diameter is greater than 20 μm, a target strength may be difficult to obtain. In this regard, the average particle diameter refers to an average equivalent circular diameter detected by observing one cross-section of a steel sheet. Since an average particle diameter of pearlite formed therewith is affected by the average particle diameter of the ferrite, it is not particularly limited. 
     An average lamellar space of the pearlite structure of the present disclosure may be from 0.03 to 0.3 μm. As the lamellar space of the pearlite structure decrease, the strength of the wire rod increases. However, when the lamellar space is less than 0.03 μm, cold processibility may deteriorate. When the lamellar space is greater than 0.3 μm, a target strength may be difficult to obtain. 
     Hereinafter, the non-quenched and tempered wire rod having excellent drawability and impact toughness and including the above-described composition range and microstructure will be described. 
     According to an embodiment, a difference between a maximum hardness and a minimum hardness in the C cross-section, which is the cross-section perpendicular to the rolling direction, is 30 Hv or less. 
     According to another embodiment, an average room temperature impact toughness of the non-quenched and tempered wire rod is 100 J or more in 30% to 60% drawing. 
     According to another embodiment, the non-quenched and tempered wire rod satisfies Equation (1) below in 30 to 60% drawing. 
     
       
         
           
             
               
                 
                   
                     I 
                     ⁢ 
                     
                         
                     
                     ⁢ 
                     max 
                   
                   - 
                   
                     I 
                     ⁢ 
                     
                         
                     
                     ⁢ 
                     min 
                     ⁢ 
                     
                       ≤ 
                       
                         4 
                         ⁢ 
                         0 
                         ⁢ 
                         J 
                       
                     
                   
                 
               
               
                 
                   ( 
                   1 
                   ) 
                 
               
             
           
         
       
     
     Here, Imax is a maximum value of average room temperature impact toughness after drawing and Imin is a minimum value of average room temperature impact toughness after drawing. 
     In this regard, the room temperature impact toughness is evaluated by Charpy impact energy value obtained by performing a Charpy impact test on a specimen having a U-notch (U-notch standard sample, 10×10×55 mm) at 25° C. 
     Hereinafter, a method of manufacturing a wire rod according to an embodiment of the present disclosure will be described in detail. 
     The present inventors have found that both excellent drawability and impact toughness are obtained by forming a ferrite-pearlite layered structure (F-P band structure) well developed in the rolling direction through various experiments and proposed the present disclosure. 
     The method of manufacturing the non-quenched and tempered wire rod according to the present disclosure includes preparing a billet, reheating the billet at a reheating temperature, rolling the reheated billet into a wire rod, and coiling the rolled wire rod followed by cooling. 
     The billet prepared according to an embodiment of the present disclosure includes, in percent by weight (wt %), 0.05 to 0.35% of carbon (C), 0.05 to 0.5% of silicon (Si), 0.5 to 2.0% of manganese (Mn), 1.0% or less of chromium (Cr), 0.03% or less of phosphorus (P), 0.03% or less of sulfur (S), 0.01 to 0.07% of soluble aluminum (sol.Al), 0.01% or less of nitrogen (N), at least one of 0.1% or less of niobium (Nb), 0.5% or less of vanadium (V), and 0.1% or less of titanium (Ti), and the remainder of iron (Fe) and inevitable impurities. 
     Hereinafter, each step will be described in more detail. 
     Reheating Billet 
     In the step of reheating the billet, the billet having the above-described composition range may be reheated at a reheating temperature satisfying Equation (2) below. 
     
       
         
           
             
               
                 
                   
                     
                       T 
                       ⁢ 
                       
                           
                       
                       ⁢ 
                       1 
                     
                     ≤ 
                     
                       T 
                       ⁢ 
                       r 
                     
                     ≤ 
                     
                       1 
                       ⁢ 
                       2 
                       ⁢ 
                       0 
                       ⁢ 
                       
                         0 
                         
                           o 
                           ⁢ 
                           
                               
                           
                         
                       
                       ⁢ 
                       
                         C 
                         . 
                         
                           
 
                         
                         ⁢ 
                         Here 
                       
                     
                   
                   , 
                   
                     
                       T 
                       ⁢ 
                       
                           
                       
                       ⁢ 
                       1 
                     
                     = 
                     
                       757 
                       + 
                       
                         6 
                         ⁢ 
                         0 
                         ⁢ 
                         
                           6 
                           ⁡ 
                           
                             [ 
                             C 
                             ] 
                           
                         
                       
                       + 
                       
                         
                           80 
                           ⁡ 
                           
                             [ 
                             Nb 
                             ] 
                           
                         
                         / 
                         
                           [ 
                           C 
                           ] 
                         
                       
                       + 
                       
                         1023 
                         ⁢ 
                         
                           √ 
                           
                             [ 
                             Nb 
                             ] 
                           
                         
                       
                       + 
                       
                         3 
                         ⁢ 
                         3 
                         ⁢ 
                         
                           
                             0 
                             ⁡ 
                             
                               [ 
                               V 
                               ] 
                             
                           
                           . 
                         
                       
                     
                   
                 
               
               
                 
                   ( 
                   2 
                   ) 
                 
               
             
           
         
       
     
     The step of reheating the billet at the reheating temperature Tr satisfying Equation (2) is a step for re-solid-solubilizing a carbonitride formed of Nb, V, or any combination thereof among the components in a base material. When the carbonitride formed of Nb, V, or any combination thereof remains in a heating furnace without being dissolved, continuous coarsening makes refinement of ferrite crystal grains difficult in a subsequent process of rolling the wire rod and a mixed grain structure may be formed during cooling. 
     In Equation (2) above, when the billet-reheating temperature is below T1, coarse carbonitrides formed of Nb, V, or any combination thereof cannot be completely re-solid-solubilized. When the reheating temperature for the billet exceeds 1200° C., an austenite structure excessively grows, thereby deteriorating ductility. 
     Rolling Reheated Billet into Wire Rod 
     The step of rolling the reheated billet into a wire rod may include hot rolling at a finish rolling temperature Tf satisfying Equation (3) below. 
     
       
         
           
             
               
                 
                   
                     
                       T 
                       ⁢ 
                       2 
                     
                     ≤ 
                     
                       T 
                       ⁢ 
                       f 
                     
                     ≤ 
                     T3 
                   
                   ⁢ 
                   
                     
 
                   
                   ⁢ 
                   
                     Here 
                     , 
                     
                       T2 
                       = 
                       
                         955 
                         - 
                         
                           39 
                           ⁢ 
                           
                             6 
                             ⁡ 
                             
                               [ 
                               C 
                               ] 
                             
                           
                         
                         + 
                         
                           2 
                           ⁢ 
                           
                             4 
                             . 
                             
                               6 
                               ⁡ 
                               
                                 [ 
                                 
                                   S 
                                   ⁢ 
                                   i 
                                 
                                 ] 
                               
                             
                           
                         
                         - 
                         
                           6 
                           ⁢ 
                           
                             8 
                             . 
                             
                               1 
                               ⁡ 
                               
                                 [ 
                                 
                                   M 
                                   ⁢ 
                                   n 
                                 
                                 ] 
                               
                             
                           
                         
                         - 
                         
                           2 
                           ⁢ 
                           
                             4 
                             . 
                             
                               8 
                               ⁡ 
                               
                                 [ 
                                 
                                   C 
                                   ⁢ 
                                   r 
                                 
                                 ] 
                               
                             
                           
                         
                         - 
                         
                           36.1 
                           ⁡ 
                           
                             [ 
                             Nb 
                             ] 
                           
                         
                         - 
                         
                           2 
                           ⁢ 
                           
                             0 
                             . 
                             
                               7 
                               ⁡ 
                               
                                 [ 
                                 V 
                                 ] 
                               
                             
                           
                         
                       
                     
                     , 
                     and 
                   
                   ⁢ 
                   
                       
                   
                   ⁢ 
                   
                     
 
                   
                   ⁢ 
                   
                     
                       T 
                       ⁢ 
                       
                           
                       
                       ⁢ 
                       3 
                     
                     = 
                     
                       734 
                       + 
                       
                         4 
                         ⁢ 
                         6 
                         ⁢ 
                         
                           5 
                           ⁡ 
                           
                             [ 
                             C 
                             ] 
                           
                         
                       
                       - 
                       
                         3 
                         ⁢ 
                         5 
                         ⁢ 
                         
                           5 
                           ⁡ 
                           
                             [ 
                             
                               S 
                               ⁢ 
                               i 
                             
                             ] 
                           
                         
                       
                       + 
                       
                         3 
                         ⁢ 
                         6 
                         ⁢ 
                         
                           0 
                           ⁡ 
                           
                             [ 
                             Al 
                             ] 
                           
                         
                       
                       + 
                       
                         89 
                         ⁢ 
                         
                           1 
                           ⁡ 
                           
                             [ 
                             
                               T 
                               ⁢ 
                               i 
                             
                             ] 
                           
                         
                       
                       + 
                       
                         6800 
                         ⁡ 
                         
                           [ 
                           Nb 
                           ] 
                         
                       
                       - 
                       
                         650 
                         ⁢ 
                         
                           √ 
                           
                             [ 
                             Nb 
                             ] 
                           
                         
                       
                       + 
                       
                         7 
                         ⁢ 
                         3 
                         ⁢ 
                         
                           0 
                           ⁡ 
                           
                             [ 
                             V 
                             ] 
                           
                         
                       
                       - 
                       
                         232 
                         ⁢ 
                         
                           
                             √ 
                             
                               [ 
                               V 
                               ] 
                             
                           
                           . 
                         
                       
                     
                   
                 
               
               
                 
                   ( 
                   3 
                   ) 
                 
               
             
           
         
       
     
     Because the finish rolling temperature Tf affects a microstructure of an alloy, this is a very important process for forming a ferrite-pearlite layered structure. When a final rolling process is performed under the conditions satisfying Equation (3), the ferrite-pearlite layered structure is well formed. 
     When the finish rolling temperature Tf is below T2 in Equation (3), there is a possibility of deterioration in cold forgeability as deformation resistance caused by ferrite grain boundary refinement increases. When the finish rolling temperature Tf exceeds T3, the ferrite-pearlite layered structure may not be well formed. 
     Also, the rolling step at the finish rolling temperature may form fine ferrite and improve uniformity of ferrite distribution in the ferrite-pearlite layered structure by performing the rolling step at the finish rolling temperature Tf satisfying Equation (2) after the reheating step satisfying Equation (1) that is a pre-heating step. 
     Coiling Rolled Wire Rod Followed by Cooling 
     The step of coiling the rolled wire rod and cooling the resultant according to the present disclosure corresponds to a step of controlling lamellar spaces of pearlite in the ferrite-pearlite layered structure formed under the final rolling conditions in the previous process. 
     Basically, although pearlite is advantageous in terms of strength in a structure formed of ferrite and pearlite, it acts as a main factor for reducing toughness. In this case, a smaller lamellar space of pearlite is relatively advantageous to toughness. 
     Therefore, in the cooling step of the present disclosure, there is a need to appropriately control a cooling rate to decrease lamellar spaces of pearlite. When the cooling rate is too low, lamellar spaces may be widened raising a concern of decreasing ductility. When the cooling rate is too high, a low temperature structure is generated raising a concern of a rapid decrease in toughness. 
     In the present disclosure, an average cooling rate during cooling is preferably from 0.1 to 2° C./sec. When the average cooling rate is less than 0.1° C./sec, lamellar spaces of the pearlite structure may be widened raising a concern of decreasing ductility. When the average cooling rate exceeds 2° C./sec, a low temperature structure is generated raising concerns of an excessive increase in strength of the steel and a rapid decrease in toughness. 
     During cooling, the average cooling rate is more preferably from 0.3 to 1° C./sec. Within the ranges described above, a non-quenched and tempered wire rod having excellent ductility and toughness with sufficient strength may be obtained. 
     In the present disclosure as described above, the reheating temperature of the billet, the rolling temperature, and the subsequent cooling process are controlled to form the ferrite-pearlite layered structure. That is, the present disclosure is characterized in that the reheating, rolling, and cooling conditions are optimized in a series of processes consisting of reheating-rolling-cooling of the billet satisfying the above-described components. 
     Hereinafter, the present disclosure will be described in more detail through examples. However, it is necessary to note that the following examples are only intended to illustrate the present disclosure in more detail and are not intended to limit the scope of the present disclosure. This is because the scope of the present disclosure is determined by matters described in the claims and able to be reasonably inferred therefrom. 
     EXAMPLES 
     Billets having alloy compositions as shown in Table 1 below were heated for 3 hours at heating temperatures suitable for conditions of components, and then rolled to a wire diameter of 20 mm to prepare a wire rod. In this case, finish rolling temperatures were set in accordance with conditions for the components and the resultants were coiled and cooled at respective cooling rates. 
     Then, types and fractions of microstructures, thicknesses of ferrite bands, and lamellar spaces of pearlite were analyzed and measured by using an electron microscope, and the results are shown in Table 2 below. 
     Then, after 30 to 60% drawing, presence or absence of wire breakage, room temperature tensile strength, and room temperature impact toughness were measured, and the results are shown in Table 3 below. Drawability was indicated by ∘ when wire breakage did not occur during drawing and indicated by X when wire breakage occurred once or more. 
     In this regard, the room temperature tensile strength was measured at the center of the non-heat-treated steel samples at 25° C., and the room temperature impact toughness was evaluated by Charpy impact energy value obtained by performing a Charpy impact test on a specimen having a U-notch (U-notch standard sample, 10×10×55 mm) at 25° C. 
     
       
         
           
               
               
               
             
               
                 TABLE 1 
               
             
            
               
                   
               
               
                   
                 Alloy composition (wt %) 
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Steel type 
                 C 
                 Si 
                 Mn 
                 Cr 
                 P 
                 S 
                 sol. Al 
                 N 
                 Nb 
                 V 
                 Ti 
                 Ceq 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Example 1 
                 0.06 
                 0.25 
                 1.65 
                 0.3 
                 0.012 
                 0.0052 
                 0.034 
                 0.0055 
                 0.050 
                 0.110 
                 0 
                 0.443 
               
               
                 Example 2 
                 0.11 
                 0.21 
                 1.48 
                 0 
                 0.011 
                 0.0043 
                 0.041 
                 0.0046 
                 0.038 
                 0.054 
                 0 
                 0.430 
               
               
                 Example 3 
                 0.18 
                 0.22 
                 1.37 
                 0 
                 0.010 
                 0.0038 
                 0.030 
                 0.0040 
                 0.030 
                 0.050 
                 0 
                 0.478 
               
               
                 Example 4 
                 0.25 
                 0.24 
                 1.28 
                 0.15 
                 0.009 
                 0.0046 
                 0.026 
                 0.0045 
                 0.019 
                 0 
                 0 
                 0.546 
               
               
                 Example 5 
                 0.33 
                 0.23 
                 1.15 
                 0 
                 0.011 
                 0.0050 
                 0.032 
                 0.0052 
                 0.010 
                 0 
                 0.010 
                 0.586 
               
               
                 Comparative 
                 0.07 
                 0.12 
                 1.22 
                 0.24 
                 0.010 
                 0.0062 
                 0.031 
                 0.0048 
                 0.043 
                 0.152 
                 0 
                 0.347 
               
               
                 Example 1 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 0.15 
                 0.16 
                 1.41 
                 0.15 
                 0.012 
                 0.0055 
                 0.035 
                 0.0042 
                 0.032 
                 0.104 
                 0 
                 0.462 
               
               
                 Example 2 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 0.26 
                 0.14 
                 1.52 
                 0.11 
                 0.011 
                 0.0043 
                 0.042 
                 0.0058 
                 0.029 
                 0.046 
                 0 
                 0.589 
               
               
                 Example 3 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 0.32 
                 0.21 
                 1.67 
                 0 
                 0.010 
                 0.0051 
                 0.033 
                 0.0060 
                 0.021 
                 0.038 
                 0 
                 0.677 
               
               
                 Example 4 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 0.38 
                 0.25 
                 1.02 
                 0 
                 0.009 
                 0.0047 
                 0.024 
                 0.0053 
                 0.017 
                 0 
                 0.015 
                 0.612 
               
               
                 Example 5 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 0.43 
                 0.27 
                 0.15 
                 0 
                 0.010 
                 0.0056 
                 0.027 
                 0.0047 
                 0.013 
                 0 
                 0 
                 0.690 
               
               
                 Example 6 
               
               
                   
               
               
                 Here, Ceq = [C] + [Si]/9 + [Mn]/5 + [Cr]/12, and [C], [Si], [Mn], and [Cr] are contents (%) of corresponding elements, respectively. 
               
            
           
         
       
     
     
       
         
           
               
               
               
               
               
               
               
               
               
               
               
               
               
             
               
                 TABLE 2 
               
               
                   
               
               
                   
                   
                   
                   
                   
                   
                   
                   
                   
                 Average 
                 Average 
                   
                   
               
               
                   
                   
                   
                   
                   
                   
                   
                   
                   
                 thickness 
                 particle 
                   
                 Hardness 
               
               
                   
                   
                   
                   
                   
                 Final 
                   
                   
                   
                 of ferrite 
                 diameter of 
                 Average 
                 difference 
               
               
                   
                   
                 Reheating 
                   
                   
                 rolling 
                 Average 
                   
                   
                 band in L 
                 ferrite in C 
                 lamellar 
                 in C 
               
               
                   
                   
                 temperature 
                   
                   
                 temperature 
                 cooling 
                   
                 Ferrite 
                 cross- 
                 cross- 
                 space of 
                 cross- 
               
               
                   
                 T1 
                 Tr 
                 T2 
                 T3 
                 Tf 
                 rate 
                   
                 fraction 
                 section 
                 section 
                 pearlite 
                 section 
               
               
                 Steel type 
                 (° C.) 
                 (° C.) 
                 (° C.) 
                 (° C.) 
                 (° C.) 
                 (° C./s) 
                 Structure 
                 (%) 
                 (μm) 
                 (μm) 
                 (μm) 
                 (Hv) 
               
               
                   
               
             
            
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Example 1 
                 1122 
                 1156 
                 814 
                 880 
                 834 
                 1.6 
                 F + P 
                 84 
                 23 
                 15 
                 0.26 
                 9 
               
               
                 Example 2 
                 1069 
                 1085 
                 813 
                 841 
                 828 
                 1.1 
                 F + P 
                 77 
                 22 
                 12 
                 0.24 
                 15 
               
               
                 Example 3 
                 1073 
                 1097 
                 794 
                 826 
                 815 
                 0.8 
                 F + P 
                 69 
                 17 
                 7 
                 0.25 
                 20 
               
               
                 Example 4 
                 1056 
                 1073 
                 770 
                 813 
                 806 
                 0.4 
                 F + P 
                 56 
                 15 
                 8 
                 0.20 
                 18 
               
               
                 Example 5 
                 1062 
                 1082 
                 751 
                 829 
                 789 
                 1.0 
                 F + P 
                 42 
                 10 
                 11 
                 0.16 
                 26 
               
               
                 Comparative 
                 1111 
                 1135 
                 836 
                 914 
                 812 
                 1.3 
                 F + P 
                 82 
                 32 
                 12 
                 0.30 
                 32 
               
               
                 Example 1 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 1082 
                 1104 
                 796 
                 862 
                 887 
                 0.9 
                 F + P 
                 71 
                 36 
                 25 
                 0.28 
                 26 
               
               
                 Example 2 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 1113 
                 1065 
                 747 
                 891 
                 834 
                 0.08 
                 F + P 
                 53 
                 19 
                 14 
                 0.34 
                 19 
               
               
                 Example 3 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 1117 
                 1087 
                 718 
                 851 
                 856 
                 2.4 
                 F + P 
                 35 
                 31 
                 18 
                 0.21 
                 28 
               
               
                 Example 4 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 1124 
                 1132 
                 741 
                 875 
                 862 
                 0.05 
                 F + P 
                 28 
                 26 
                 22 
                 0.32 
                 36 
               
               
                 Example 5 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 1137 
                 1154 
                 713 
                 862 
                 841 
                 1.2 
                 F + P 
                 21 
                 24 
                 16 
                 0.27 
                 41 
               
               
                 Example 6 
               
               
                   
               
               
                 Here, T1 = 757 + 606[C] + 80[Nb]/[C] + 1023√[Nb] + 330[V], T2 = 955 − 396[C] + 24.6[Si] − 68.1[Mn] − 24.8[Cr] − 36.1[Nb] − 20.7[V], T3 = 734 + 465[C] − 355[Si] + 360[Al] + 891[Ti] + 6800[Nb] − 650√[Nb] + 730[V] − 232√[V] 
               
            
           
         
       
     
     
       
         
           
               
               
               
               
               
               
             
               
                 TABLE 3 
               
             
            
               
                   
               
               
                   
                 0% drawing 
                 35% drawing 
                 45% drawing 
                 55% drawing 
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                   
                 Tensile 
                 Impact 
                 Tensile 
                 Impact 
                   
                 Tensile 
                 Impact 
                   
                 Tensile 
                 Impact 
                   
                   
               
               
                 Sample 
                 strength 
                 toughness 
                 strength 
                 toughness 
                 Draw- 
                 strength 
                 toughness 
                 Draw- 
                 strength 
                 toughness 
                 Draw- 
                 I max -I min   
               
               
                 No. 
                 (Mpa) 
                 (J) 
                 (Mpa) 
                 (J) 
                 ability 
                 (Mpa) 
                 (J) 
                 ability 
                 (Mpa) 
                 (J) 
                 ability 
                 (J) 
               
               
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
               
               
               
               
            
               
                 Example 1 
                 546 
                 345 
                 738 
                 253 
                 ◯ 
                 781 
                 221 
                 ◯ 
                 824 
                 224 
                 ◯ 
                 32 
               
               
                 Example 2 
                 574 
                 316 
                 771 
                 219 
                 ◯ 
                 813 
                 210 
                 ◯ 
                 857 
                 216 
                 ◯ 
                 9 
               
               
                 Example 3 
                 621 
                 256 
                 822 
                 209 
                 ◯ 
                 870 
                 206 
                 ◯ 
                 909 
                 190 
                 ◯ 
                 19 
               
               
                 Example 4 
                 613 
                 211 
                 840 
                 188 
                 ◯ 
                 887 
                 179 
                 ◯ 
                 933 
                 168 
                 ◯ 
                 20 
               
               
                 Example 5 
                 642 
                 185 
                 867 
                 164 
                 ◯ 
                 908 
                 153 
                 ◯ 
                 958 
                 162 
                 ◯ 
                 11 
               
               
                 Comparative 
                 617 
                 225 
                 807 
                 168 
                 ◯ 
                 845 
                 135 
                 ◯ 
                 889 
                 103 
                 ◯ 
                 65 
               
               
                 Example 1 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 625 
                 212 
                 826 
                 151 
                 ◯ 
                 873 
                 116 
                 ◯ 
                 924 
                 97 
                 ◯ 
                 54 
               
               
                 Example 2 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 689 
                 156 
                 908 
                 102 
                 ◯ 
                 953 
                 88 
                 ◯ 
                 997 
                 61 
                 X 
                 41 
               
               
                 Example 3 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 696 
                 143 
                 927 
                 94 
                 ◯ 
                 979 
                 74 
                 X 
                 1029 
                 52 
                 X 
                 42 
               
               
                 Example 4 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 742 
                 133 
                 970 
                 81 
                 ◯ 
                 1022 
                 62 
                 X 
                 1063 
                 38 
                 X 
                 43 
               
               
                 Example 5 
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
                   
               
               
                 Comparative 
                 770 
                 115 
                 996 
                 61 
                 X 
                 1041 
                 43 
                 X 
                 1088 
                 25 
                 X 
                 36 
               
               
                 Example 6 
               
               
                   
               
               
                 Here, I max  is a maximum value of average room temperature impact toughness after drawing and I min  is a minimum value of average room temperature impact toughness 
               
            
           
         
       
     
     Hereinafter, based on Tables 1 to 3, samples of the examples and comparative examples were evaluated by comparison therebetween. 
     Referring to Tables 1 to 3, in the cases of Examples 1 to 5 satisfying the alloy compositions and manufacturing conditions of the present disclosure, excellent drawability and impact toughness with strength were obtained due to the ferrite-pearlite layered structure developed in the rolling direction. 
     On the contrary, in the cases of Comparative Examples 1 to 6 which do not satisfy the manufacturing conditions suggested by the present disclosure, the ferrite-pearlite layered structure could not be sufficiently formed in the rolling direction suggested by the present disclosure, occurrence rates of wire breakage were higher during drawing and impact toughness was lower compared to Examples 1 to 5. 
     In the case of Comparative Example 1, the carbon equivalent Ceq (0.347) was lower than 0.4 and the finish rolling temperature Tf was lower than T2. Thus, the average thickness (32 μm) of the ferrite band of the non-quenched and tempered wire rod of Comparative Example 1 in the L cross-section was greater than 30 μm, the hardness difference (32 Hv) in the C cross-section was greater than 30 Hv, and the difference (65 J) of the average room temperature impact toughness after 30 to 60% drawing was greater than 40 J, and thus the sample of Comparative Example 1 did not satisfy Equation (1) of the present disclosure. 
     In the case of Comparative Example 2, the final rolling temperature Tf exceeded T3. In addition, the average thickness (36 □m) of the ferrite band of the non-quenched and tempered wire rod of Comparative Example 2 in the L cross-section was greater than 30 □m, the average particle diameter (25 μm) of ferrite in the C cross-section was greater than 20 μm, the impact toughness (97 J) after 55% drawing was lower than 100 J, and the difference (54 J) between average room temperature impact toughness after 30 to 60% drawing was 40 J, and thus the sample of Comparative Example 2 did not satisfy Equation (1) of the present disclosure. 
     In the case of Comparative Example 3, the reheating temperature Tr exceeded T1 and the average cooling rate (0.08° C./s) was lower than 0.1° C./s. In addition, the average lamellar space (0.34 μm) of pearlite of the non-quenched and tempered wire rod of Comparative Example 3 was greater than 0.3 μm, impact toughness after 45% and 55% drawing were 88 J and 61 J, respectively, which were lower than 100 J, wire breakage occurred after 55% drawing, and the difference (41 J) between average room temperature impact toughness after 30 to 60% drawing was greater than 40 J, and thus the sample of Comparative Example 3 did not satisfy Equation (1) of the present disclosure. 
     In the case of Comparative Example 4, the carbon equivalent Ceq (0.677) was greater than 0.6, the reheating temperature Tr exceeded T1, the final rolling temperature Tf exceeded T3, and the average cooling rate (2.4° C./s) exceeded 2° C./s. In addition, the average thickness (31 μm) of the ferrite band in the L cross-section of Comparative Example 4 was greater than 30 μm, impact toughness after 35%, 45%, and 55% drawing was 94 J, 74 J, and 52 J which were lower than 100 J, wire breakage occurred after 45% and 55% drawing, and the difference (42 J) between average room temperature impact toughness after 30 to 60% drawing was greater than 40 J, and thus the non-quenched and tempered wire rod of Comparative Example 4 did not satisfy Equation (1) of the present disclosure 
     In the case of Comparative Example 5, the C content (0.38 wt %) exceeded 0.35 wt %, the carbon equivalent Ceq (0.612) exceeded 0.6, and the average cooling rate (0.05° C./s) was lower than 0.1° C./s. In addition, the ferrite fraction (28%) was lower than 30%, the average particle diameter (22 μm) of ferrite in the C cross-section exceeded 20 μm, the average lamellar space (0.32 μm) of pearlite exceeded 0.3 μm, the hardness difference (36 Hv) in the C cross-section exceeded 30 Hv, impact toughness after 35%, 45, and 55% drawing was 81 J, 62 J, and 38 J, which were lower than 100 J, wire breakage occurred after 45% and 55% drawing, and the difference (43 J) of average room temperature impact toughness after 30 to 60% drawing was 40 J, and thus the non-quenched and tempered wire rod of Comparative Example 5 did not satisfy Equation (1) of the present disclosure. 
     In the case of Comparative Example 6, the C content (0.43 wt %) exceeded 0.35 wt % and the carbon equivalent Ceq (0.690) exceeded 0.6. In addition, the ferrite fraction (21%) was lower than 30%, the hardness difference (41 Hv) of the C cross-section exceeded 30 Hv, impact toughness after 35%, 45%, and 55% drawing was 61 J, 43 J, and 25 J, which were lower than 100 J, wire breakage occurred after 35%, 45%, and 55% drawing. 
     According to the non-quenched and tempered wire rod and the method of manufacturing the same according to the embodiments of the present disclosure, a non-quenched and tempered wire rod having excellent drawability and impact toughness may be provided without additional heat treatment by controlling alloy compositions and manufacturing conditions and a method of manufacturing the same may be provided. 
     While the present disclosure has been particularly described with reference to exemplary embodiments, it should be understood by those of skilled in the art that various changes in form and details may be made without departing from the spirit and scope of the present disclosure.