Classifications

• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D6/00—Heat treatment of ferrous alloys
  • C21D6/008—Heat treatment of ferrous alloys containing Si
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0226—Hot rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
  • C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
  • C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/001—Ferrous alloys, e.g. steel alloys containing N
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese

Definitions

• the present disclosure relates to a steel plate and a production method therefor.
• JP S58-167045 A discloses "A steel material hot forging method of performing extend forging on an axisymmetric steel material between an upper anvil and a lower anvil, comprising a step of forming a shape of a cross section perpendicular to an extend forging direction of the steel material into a rectangle or substantially rectangle whose ratio of a length of a long side and a length of a short side is at least 1.4, between start of the extend forging and end of the extend forging.”
• JP 6137080 B2 discloses "A slab forging method comprising continuously subjecting a slab to reduction in a width direction and thereafter in a thickness direction using asymmetric anvils that are upper and lower anvils with different widths, wherein the reduction in the width direction is performed from one end in a longitudinal direction of the slab, at which time a ratio ⁇ L/B is limited to 0.20 or less where ⁇ L is an amount of deviation between end positions of the upper and lower anvils at the other end in the longitudinal direction of the slab and B is a shorter contact length out of respective contact lengths of the upper and lower anvils with the slab.”
• JP 6156321 B2 discloses "A slab hot forging method comprising continuously subjecting a slab produced by continuous casting to reduction in a width direction and thereafter in a thickness direction using asymmetric upper and lower anvils, wherein the reduction of the slab in the width direction is performed in two stages of a first and second stages between which the slab is reversed and in each of which reduction is performed at least twice, the reduction of the slab in the width direction in each stage is performed using an anvil of 400 mm to 1200 mm in width as a short side anvil and an anvil of 800 mm to 1500 mm in width as a long side anvil while shifting a reduction phase at a reduction position by the short side anvil so that ⁇ L ⁇ 0.20B where ⁇ L is a deviation between a slab feed margin boundary during first reduction of the slab and a center of an anvil contact length (B) during next reduction, and each reduction ratio in the reduction of the slab in the width direction is 4 % or more and a total reduction ratio in the reduction of the slab
• JP H6-69569 B2 discloses "A production method for an ultra-thick steel plate having excellent internal properties, comprising subjecting cast steel produced by continuous casting to broad side pass rolling in a rough rolling step and further performing rolling to a product thickness in a finish rolling step, wherein in the finish rolling step, rolling is performed in a plurality of passes at a rolling rate of 200 mm/sec to 350 mm/sec".
• JP S59-74220 A discloses "A production method for a high-toughness steel plate with excellent internal quality through continuous casting, comprising a sequential combination of: immediately after cutting a continuous cast strand of aluminum killed steel containing Al: 0.07 wt% or less into a hot slab with a certain length, hot charging the hot slab into a blooming soaking furnace, soaking the hot slab to a temperature of 1050 °C to 1150 °C, and performing slab rolling so that a value of a shape ratio R according to the following formula will be 0.5 or more; thereafter subjecting the slab to dehydrogenation treatment to reduce diffusible hydrogen contained in a thickness center part of the slab to 1.2 ppm or less; thereafter reheating the slab to 950 °C to 1050 °C and subjecting the slab to plate rolling to obtain a plate with a finished thickness planned to be a required thickness of 50 mm or more; and, after the plate rolling ends, performing accelerated cooling from Ar 3 or a temperature not lower than Ar 3 by
• PTL 1 to PTL 3 involve hot forging a slab.
• the production efficiency of hot forging is much lower than the production efficiency of hot rolling.
• the production capacity is low and the production costs are high.
• the techniques in PTL 4 and PTL 5 involve hot rolling a slab instead of hot forging, but require reduction by rolling (hereinafter referred to as rolling reduction) with a high rolling shape ratio.
• rolling reduction reduction by rolling
• the rolling reduction amount per pass needs to be increased. This requires introducing an expensive rolling line with a high upper limit of load capacity and a high upper limit of torque.
• a steel plate according to the present disclosure is not limited to any particular use, and can be used in a wide range of fields in which steel plates are typically used, such as ships, line pipes, buildings, bridges, marine structures, wind power generators, construction machinery, and pressure vessels.
• a steel plate according to the present disclosure will be described below by way of embodiments.
• C is an element that can improve the strength of the steel at the lowest cost. C also contributes to strengthening austenite grain boundaries. If the C content is less than 0.03 %, the grain boundary strength of austenite decreases and the slab undergoes hot cracking. This significantly decreases productivity. Moreover, sufficient strength cannot be obtained. If the C content is more than 0.18 %, weldability decreases, and also toughness decreases. The C content is therefore 0.03 % to 0.18 %. The C content is preferably 0.05 % or more. The C content is preferably 0.17 % or less.
• Si is an element effective for deoxidation. If the Si content is less than 0.03 %, the effect is insufficient. If the Si content is more than 0.70 %, weldability decreases. The Si content is therefore 0.03 % to 0.70 %.
• the Si content is preferably 0.04 % or more.
• the Si content is preferably 0.60 % or less.
• Mn is an element that improves the quench hardenability of the steel and improves the strength of the steel at low cost.
• the Mn content is 0.30 % or more. If the Mn content is more than 2.50 %, weldability decreases. The Mn content is therefore 0.30 % to 2.50 %.
• the Mn content is preferably 0.50 % or more.
• the Mn content is preferably 2.20 % or less.
• P is an element that has a strong effect of embrittling grain boundaries. If the P content is high, the toughness of the steel decreases. The P content is therefore 0.030 % or less. The P content is preferably 0.025 % or less. Since a lower P content is more desirable, no lower limit is placed on the P content, and the P content may be 0 %. However, P is an element that is inevitably contained in steel as impurities, and an excessively low P content leads to longer refining time and higher cost. Accordingly, the P content is preferably 0.001 % or more.
• the S content decreases the toughness of the steel.
• the S content is therefore 0.0200 % or less.
• the S content is preferably 0.0100 % or less. Since a lower S content is more desirable, no lower limit is placed on the S content, and the S content may be 0 %.
• S is an element that is inevitably contained in steel as impurities, and an excessively low S content leads to longer refining time and higher cost. Accordingly, the S content is preferably 0.0001 % or more.
• Al is an element effective for deoxidation. Al also has the effect of reducing the austenite grain size by forming nitrides. In order to achieve these effects, the Al content is 0.001 % or more. If the Al content is more than 0.100 %, the cleanliness of the steel decreases. This results in decreases in ductility and toughness. The Al content is therefore 0.001 % to 0.100 %. The Al content is preferably 0.005 % or more. The Al content is preferably 0.080 % or less.
• O is an element that decreases ductility and toughness.
• the O content is therefore 0.0100 % or less. Since a lower O content is more desirable, no lower limit is placed on the O content, and the O content may be 0 %.
• O is an element that is inevitably contained in steel as impurities, and an excessively low O content leads to longer refining time and higher cost. Accordingly, the O content is preferably 0.0005 % or more.
• N is an element that decreases ductility and toughness.
• the N content is therefore 0.0100 % or less. Since a lower N content is more desirable, no lower limit is placed on the N content, and the N content may be 0 %.
• N is an element that is inevitably contained in steel as impurities, and the N content may be more than 0 % industrially. An excessively low N content leads to longer refining time and higher cost. Accordingly, the N content is preferably 0.0005 % or more.
• the chemical composition may optionally further contain one or more of the following elements as optional components from the viewpoint of further improving strength and weldability (such as weld toughness and welding activity):
• Cu is an element that improves the strength of the steel without greatly degrading toughness. If the Cu content is more than 2.00 %, hot cracking is caused by a Cu-enriched layer formed directly below scale. Accordingly, in the case where Cu is contained, the Cu content is preferably 2.00 % or less. The Cu content is more preferably 0.01 % or more. The Cu content is more preferably 1.50 % or less.
• Ni is an element that enhances the quench hardenability of the steel. Ni also has the effect of improving toughness. If the Ni content is more than 2.50 %, the production costs increase. Accordingly, in the case where Ni is contained, the Ni content is preferably 2.50 % or less. The Ni content is more preferably 0.01 % or more. The Ni content is more preferably 2.00 % or less.
• Cr is an element that improves the strength of the steel by improving the quench hardenability of the steel. If the Cr content is more than 1.50 %, weldability decreases. Accordingly, in the case where Cr is contained, the Cr content is preferably 1.50 % or less. The Cr content is more preferably 0.01 % or more. The Cr content is more preferably 1.20 % or less.
• Mo is an element that improves the strength of the steel by improving the quench hardenability of the steel. If the Mo content is more than 1.00 %, weldability decreases. Accordingly, in the case where Mo is contained, the Mo content is preferably 1.00 % or less. The Mo content is more preferably 0.01 % or more. The Mo content is more preferably 0.80 % or less.
• Nb is an element that suppresses recrystallization when strain is applied to austenite microstructure, by solute Nb or finely precipitated NbC. Nb also has the effect of raising the non-recrystallization temperature range. If the Nb content is more than 0.100 %, weldability decreases. Accordingly, in the case where Nb is contained, the Nb content is preferably 0.100 % or less. The Nb content is more preferably 0.001 % or more, and further preferably 0.005 % or more. The Nb content is more preferably 0.075 % or less, and further preferably 0.050 % or less.
• Ti is an element that has the effect of, by precipitating as TiN, pinning crystal grain boundaries and inhibiting grain growth. If the Ti content is more than 0.100 %, the cleanliness of the steel decreases. This results in decreases in ductility and toughness. Accordingly, in the case where Ti is contained, the Ti content is preferably 0.100 % or less. The Ti content is more preferably 0.001 % or more. The Ti content is more preferably 0.080 % or less.
• V 0.30 % or less
• V is an element that improves the strength of the steel by improving the quench hardenability of the steel and forming carbonitrides. If the V content is more than 0.30 %, weldability decreases. Accordingly, in the case where V is contained, the V content is preferably 0.30 % or less. The V content is more preferably 0.01 % or more. The V content is more preferably 0.25 % or less.
• B is an element that improves the strength of the steel by improving the quench hardenability of the steel. If the B content is more than 0.0100 %, weldability decreases. Accordingly, in the case where B is contained, the B content is preferably 0.0100 % or less. The B content is more preferably 0.0001 % or more. The B content is more preferably 0.0070 % or less.
• W is an element that improves the strength of the steel by improving the quench hardenability of the steel. If the W content is more than 0.50 %, weldability decreases. Accordingly, in the case where W is contained, the W content is preferably 0.50 % or less. The W content is more preferably 0.01 % or more. The W content is more preferably 0.40 % or less.
• Ca is an element that improves weldability by forming oxysulfides having high stability at high temperature. If the Ca content is more than 0.0200 %, the cleanliness of the steel decreases and the toughness of the steel decreases. Accordingly, in the case where Ca is contained, the Ca content is preferably 0.0200 % or less. The Ca content is more preferably 0.0001 % or more. The Ca content is more preferably 0.0180 % or less.
• Mg is an element that improves weldability by forming oxysulfides having high stability at high temperature. If the Mg content is more than 0.0200 %, the Mg addition effect is saturated and the effect appropriate to the content cannot be expected, which is economically disadvantageous. Accordingly, in the case where Mg is contained, the Mg content is preferably 0.0200 % or less. The Mg content is more preferably 0.0001 % or more. The Mg content is more preferably 0.0180 % or less.
• the REM (rare earth metal) is an element that improves weldability by forming oxysulfides having high stability at high temperature. If the REM content is more than 0.0500 %, the REM addition effect is saturated and the effect appropriate to the content cannot be expected, which is economically disadvantageous. Accordingly, in the case where REM is contained, the REM content is preferably 0.0500 % or less. The REM content is more preferably 0.0001 % or more. The REM content is more preferably 0.0450 % or less.
• the balance other than the foregoing elements in the chemical composition of the steel plate according to one embodiment of the present disclosure consists of Fe and inevitable impurities. If the content of any of the foregoing elements as optional components is less than the preferable lower limit, the element is treated as inevitable impurities.
• the area ratio of void defects at the thickness center position is 0.5 % or less.
• Void defects inside a steel plate serve as initiation points for fractures such as ductile fractures, brittle fractures, and fatigue fractures.
• the area ratio of void defects at the thickness center position is therefore 0.5 % or less.
• the area ratio of void defects at the thickness center position is preferably 0.3 % or less. No lower limit is placed on the area ratio of void defects at the thickness center position, and the area ratio of void defects at the thickness center position may be 0 %.
• the area ratio of void defects at the thickness center position is measured in the manner described in the EXAMPLES section below.
• excellent internal properties means that the area reduction ratio in the thickness direction of the steel plate measured in a tensile test in accordance with ASTM A370 (2010) is 35 % or more. Detailed test conditions are as described in [Tensile test in thickness direction] in the EXAMPLES section below.
• the thickness of the steel plate according to one embodiment of the present disclosure is preferably 30 mm to 240 mm.
• the thickness of the steel plate according to one embodiment of the present disclosure is more preferably 50 mm or more, and further preferably 101 mm or more.
• the thickness of the steel plate according to one embodiment of the present disclosure is more preferably 230 mm or less.
• the production method for the steel plate according to one embodiment of the present disclosure comprises: preparing a slab (steel material) having the foregoing chemical composition (preparation step); and hot rolling the slab (hot rolling step), wherein a total rolling reduction ratio in rolling passes that satisfy the following (a) and (b) in the hot rolling is more than 30 %:
• the steel plate according to one embodiment of the present disclosure can be produced favorably.
• Each step will be described below.
• the surface temperature of the slab can be measured using a radiation thermometer, for example.
• the temperature at the thickness center position of the slab can be measured, for example, by attaching a thermocouple at the thickness center position of the slab, or by calculating the temperature distribution in the cross section of the slab by thermal analysis and correcting the result using the surface temperature of the slab.
• the temperature of the slab and steel plate denotes the surface temperature unless otherwise specified.
• the material to be rolled during the hot rolling step is hereafter referred to as "slab” and not “steel plate” (hot-rolled steel plate), for the sake of convenience.
• a slab having the foregoing chemical composition is prepared.
• the preparation method is not limited.
• molten steel is obtained by a known steelmaking method such as a converter, an electric furnace, or a vacuum melting furnace. Secondary refining such as ladle refining may be optionally performed.
• the obtained molten steel is then made into a slab by continuous casting, ingot casting, or the like, and thus a slab having the foregoing chemical composition is prepared. Conditions may be according to conventional methods.
• the slab prepared in the preparation step is optionally heated, and subjected to hot rolling to obtain a steel plate (hot-rolled steel plate). It is very important to satisfy the following conditions in the hot rolling.
• An effective way of closing void defects present near the thickness center position of the slab and annihilating them through metal bonding is to apply strain in a state in which the temperature at the thickness center position of the slab is 700 °C or more.
• the total rolling reduction ratio in the rolling passes under the predetermined conditions is more than 30 %.
• the total rolling reduction ratio in the rolling passes under the predetermined conditions is preferably 40 % or more.
• the total rolling reduction ratio in the rolling passes under the predetermined conditions is preferably 65 % or less.
• r t is the total rolling reduction ratio (%) in the rolling passes under the predetermined conditions
• t iN is the thickness (mm) of the slab at the start of rolling in the Nth rolling pass among the rolling passes under the predetermined conditions
• t fN is the thickness (mm) of the slab at the end of rolling in the Nth rolling pass among the rolling passes under the predetermined conditions
• N is the number of rolling passes under the predetermined conditions.
• Whether the temperature conditions (a) and (b) are satisfied is determined based on the surface temperature of the slab and the temperature at the thickness center position of the slab at the start of rolling in each rolling pass.
• the method of adjusting the temperature difference between the surface and the thickness center position of the slab is not limited.
• the temperature difference between the surface and the thickness center position of the slab can be adjusted to the foregoing range by forced-cooling the surface of the slab through air cooling, water cooling, or the like.
• the slab heating temperature is preferably 950 °C to 1300 °C.
• the total number of rolling passes in the hot rolling is preferably 5 passes to 60 passes.
• N the number of rolling passes under the predetermined conditions is preferably 5 passes to 50 passes.
• the rolling finish temperature i.e. the delivery temperature in the final pass
• cooling treatment may be further performed.
• optional heat treatment such as quenching, annealing, and tempering may be performed. Cooling treatment conditions and heat treatment conditions are not limited and may be according to conventional methods.
• Molten steels having the chemical compositions shown in Table 1 were obtained by steelmaking, and slabs of 260 mm to 600 mm in thickness were prepared by continuous casting, ingot casting, or the like.
• Each blank space in the element columns in Table 1 indicates that the element is not intentionally added, including not only the case where the element is not contained (0 %) but also the case where the element is inevitably contained.
• Each prepared slab was then subjected to hot rolling under the conditions shown in Table 2 to obtain a steel plate having the thickness (mm) shown in Table 2.
• the rolling reduction ratio in the hot rolling was in the range of 2.5 to 3.5, and N (the number of rolling passes under the predetermined conditions) was 5 passes to 37 passes.
• the surface temperature of the slab was measured using a radiation thermometer, and the temperature of the thickness center of the slab was measured using a thermocouple.
• the temperature difference between the surface and the thickness center position of the slab was adjusted by forced-cooling the surface of the slab through air cooling, water cooling, or the like. Conditions other than the above were according to conventional methods.
• a sample for the entire width of the steel plate was collected at the center position in the longitudinal direction (i.e. the rolling direction) of the steel plate so that the cross section in the width direction (i.e. the direction orthogonal to the rolling direction) of the steel plate at the thickness center position of the steel plate would be the evaluation plane.
• the obtained sample was then mirror polished through alumina buffing for finish. Setting the evaluation region in the sample to the thickness center position ⁇ 3 mm in the thickness direction and the entire plate width in the width direction, the area ratio of void defects in the evaluation region was measured through image analysis. The measured value was taken to be the area ratio of void defects at the thickness center position.
• a tensile test piece was collected at the center position in the longitudinal direction (i.e. the rolling direction) of the steel plate so that the longitudinal direction of the tensile test piece would be parallel to the thickness direction of the steel plate.
• the tensile test piece was collected so that the longitudinal center position of the tensile test piece would be the thickness center position (i.e. the position of 1/2 of the thickness) of the steel plate.
• Such tensile test pieces were collected over the entire width of the steel plate with a collection pitch of 100 mm in the width direction of the steel plate.
• the shape of the tensile test piece was Type 3 shape in ASTM A770 (2007).
• the steel plate of each Example had excellent internal properties. Moreover, the steel plate of each Example was capable of being produced using a usual hot rolling line at low cost (i.e. with high productivity) with no need for special equipment.

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