THICK-WALLED HIGH-TOUGHNESS HIGH-STRENGTH STEEL PLATE AND METHOD FOR MANUFACTURING THE SAME

Abstract
A thick-walled, high-toughness, high-strength steel plate manufactured from steel having a particular composition and casted under conditions where the cooling rate of a surface during solidification is 1° C./s or less. The surface of the steel plate has a toughness (vE-40) of 70 J or more, and the steel plate has a thickness of 100 mm or more.
Description
TECHNICAL FIELD OF THE INVENTION

The present invention relates to a thick-walled high-toughness high-strength steel plate for use in steel structures in construction, bridges, shipbuilding, offshore structures, construction and industrial machinery, tanks, penstocks, and the like and to a method for manufacturing the thick-walled high-toughness high-strength steel plate. In particular, the surface of the steel plate has high toughness, and the inner part of the steel plate has high strength and toughness. The steel plate has a thickness of 100 mm or more and a yield strength of 620 MPa or more.


BACKGROUND OF THE INVENTION

In general, steel for use in construction, bridges, shipbuilding, offshore structures, construction and industrial machinery, tanks, penstocks, and other fields is welded to have a desired shape. In recent years, with significantly increasing in size of steel structures, the strength and thickness of steel to be used have also been greatly increased.


Despite trying to manufacture a thick-walled high-strength steel plate having a thickness of 100 mm or more and having high strength and toughness in a half-thickness portion (the central portion in the thickness direction), a structure having relatively low strength, such as ferrite, tends to be formed in the half-thickness portion due to a decreased cooling rate. Thus, the addition of large amounts of alloying elements is required to reduce the formation of such a structure.


In particular, in order to achieve high strength and toughness of a half-thickness portion of a thick-walled material (a thick-walled steel plate having a thickness of 100 mm or more), it is important to form bainite or a mixed structure of bainite and martensite in the half-thickness portion during quenching. This requires the addition of large amounts of alloying elements, such as Mn, Ni, Cr, and/or Mo.


The cooling rate is higher on the surface of a steel plate than in the half-thickness portion. Thus, a martensite structure having low toughness is formed on the surface of the steel plate. Thus, a high-strength steel plate having a thickness of 100 mm or more rarely has both high surface toughness and high strength and toughness of the inner part thereof.


A steel plate is described in the following two pieces of non-patent literature. Non Patent Literature 1 describes a material having a thickness of 210 mm, and Non Patent Literature 2 describes a material having a thickness of 180 mm.


Non-Patent Literature



  • NPL 1: Nippon Steel Technical Report, 348 (1993), 10-16

  • NPL 2: Nippon Kokan Technical Report, 107 (1985), 21-30



SUMMARY OF THE INVENTION

These pieces of non-patent literature describe high strength and toughness of the half-thickness portion. However, these pieces of non-patent literature do not describe the toughness (Charpy impact characteristics) of the surface of a steel plate. In general, thick-walled materials are manufactured by a quenching and tempering process. The formation of a martensite structure on the surface of a steel plate, on which the cooling rate is higher than in the half-thickness portion, deteriorates the toughness (Charpy impact characteristics) of the surface of the steel plate. However, these pieces of non-patent literature do not describe the manufacture of a steel plate consistently having a tough surface.


The present invention has been made to solve such problems and aims to provide a thick-walled high-toughness high-strength steel plate that has high surface toughness and high strength and toughness of the inner part thereof and a method for manufacturing the thick-walled high-toughness high-strength steel plate.


In order to solve the problems, the present inventors have extensively studied the microstructure control factors that satisfy high toughness of the surface of a thick-walled steel plate having a yield strength of 620 MPa or more and a thickness of 100 mm or more and also satisfy high strength and toughness of the half-thickness portion of the thick-walled steel plate, and have found the following.


1. When the cooling rate during the solidification of a raw material steel exceeds 1° C./s, microsegregation competes with the solidification reaction. This reduces microsegregation. In the manufacture of a large piece of steel, the cooling rate during the solidification of the steel decreases to 1° C./s or less, and consequently microsegregation becomes noticeable. Even in such a case, in order to achieve high toughness of the surface of a steel plate, on which a martensite structure is formed during quenching, it is important to reduce the P content and microsegregation during solidification. When primary crystals during solidification form a δ phase, and the percentage of the δ phase at the beginning of the formation of a γ phase is 30% or more, this results in reduced microsegregation and improved toughness. The percentage % described above refers to % by volume.


2. In order to achieve high strength and toughness of the half-thickness portion, in which the cooling rate is much lower than on the surface of a steel plate during cooling after hot working, it is important to appropriately select the steel composition (components) so as to form a martensite and/or bainite microstructure even at a low cooling rate. To this end, the alloy components should be appropriately selected, and in particular the carbon equivalent (Ceq) should be 0.65% or more. In addition to the appropriate component design, it is also important to form the desired structure by hot working and heat treatment.


3. Refinement of prior γ grain size is effective in improving toughness. Refinement of prior γ grain size before heat treatment, that is, refinement of prior γ grain size just after hot working is important for refinement of prior γ grain size after heat treatment. Thus, it is important to select appropriate hot working conditions and rolling conditions.


As a result of further investigation of these findings, the present invention provides for the following embodiments.


[1] A thick-walled high-toughness high-strength steel plate having a thickness of 100 mm or more, containing, on a mass percent basis, C: 0.08% to 0.20%, Si: 0.40% or less, Mn: 0.5% to 5.0%, P: 0.010% or less, S: 0.0050% or less, Cr: 3.0% or less, Ni: 0.1% to 5.0%, Al: 0.010% to 0.080%, N: 0.0070% or less, and O: 0.0025% or less, formulae (1) and (2) being satisfied, the remainder being Fe and incidental impurities, a surface of the steel plate having a toughness (vE-40) of 70 J or more,





CeqIIW=C+Mn/6+(Cu+Ni)/15+(Cr+Mo+V)/5≧0.65   (1)





(CL−C)/CL×100≧30  (2)


wherein CL is defined by the following formula:





CL=0.2−(−0.1×(0.2−Si)−0.03×(1.1−Mn)−0.12×(0.2−Cu)−0.11×(3−Ni)+0.025×(1.2−Cr)+0.1×(0.5−Mo)+0.2×(0.04−V)−0.05×(0.06−Al))  (3)


wherein element symbols in the formulae denote the respective alloy component contents (% by mass), and, in the absence of an element, the element symbol is denoted by 0.


The surface of the steel plate has high toughness, and the inner part of the steel plate has high strength and toughness.


[2] The thick-walled high-toughness high-strength steel plate according to [1], further containing, on a mass percent basis, one or two or more of Cu: 0.50% or less, Mo: 1.50% or less, V: 0.400% or less, Nb: 0.100% or less, and Ti: 0.005% to 0.020%.


[3] The thick-walled high-toughness high-strength steel plate according to [1] or [2], further containing, on a mass percent basis, at least one of Mg: 0.0001% to 0.0050%, Ta: 0.01% to 0.20%, Zr: 0.005% to 0.1%, Y: 0.001% to 0.01%, B: 0.0030% or less, Ca: 0.0005% to 0.0050%, and REM: 0.0005% to 0.0100%.


[4] The thick-walled high-toughness high-strength steel plate according to any one of [1] to [3], wherein the thick-walled high-toughness high-strength steel plate has a yield strength of 620 MPa or more.


[5] The thick-walled high-toughness high-strength steel plate according to any one of [1] to [4], wherein the reduction of area in the thickness direction at half the thickness of the plate is 40% or more.


[6] The method for manufacturing the thick-walled high-toughness high-strength steel plate according to any one of [1] to [5],


heating steel to 1200° C. to 1350° C., hot-forging the steel at a cumulative rolling reduction of 25% or more, heating the steel to an Ac3 temperature or more and 1200° C. or less, hot-rolling the steel at a cumulative rolling reduction of 40% or more, leaving the steel to cool, reheating the steel to the Ac3 temperature or more and 1050° C. or less, rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, and tempering the steel at a temperature in the range of 450° C. to 700° C.


[7] The method for manufacturing the thick-walled high-toughness high-strength steel plate according to any one of [1] to [5],


heating steel to 1200° C. to 1350° C., hot-forging the steel at a cumulative rolling reduction of 25% or more, heating the steel to an Ac3 temperature or more and 1200° C. or less, hot-rolling the steel at a cumulative rolling reduction of 40% or more, rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, and tempering the steel at a temperature in the range of 450° C. to 700° C.


[8] The method for manufacturing the thick-walled high-toughness high-strength steel plate according to any one of [1] to [5],


heating steel to 1200° C. to 1350° C., slabbing the steel at a cumulative rolling reduction of 40% or more, heating the steel to an Ac3 temperature or more and 1200° C. or less, hot-rolling the steel at a cumulative rolling reduction of 40% or more, leaving the steel to cool, reheating the steel to the Ac3 temperature or more and 1050° C. or less, rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, and tempering the steel at a temperature in the range of 450° C. to 700° C.


[9] The method for manufacturing the thick-walled high-toughness high-strength steel plate according to any one of [1] to [5],


heating steel to 1200° C. to 1350° C., slabbing the steel at a cumulative rolling reduction of 40% or more, heating the steel to an Ac3 temperature or more and 1200° C. or less, hot-rolling the steel at a cumulative rolling reduction of 40% or more, rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, and tempering the steel at a temperature in the range of 450° C. to 700° C.


In certain embodiments, the present invention provides for a thick-walled high-toughness high-strength steel plate having a thickness of 100 mm or more and having a yield strength of 620 MPa or more and high toughness. The thick-walled high-toughness high-strength steel plate can be used to manufacture steel structures having high safety.







DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

Embodiments of the present invention will be described below. The present invention is not limited to these embodiments.


<Thick-Walled High-Toughness High-Strength Steel Plate>

A thick-walled high-toughness high-strength steel plate according to the present invention has a composition containing, on a mass percent basis, C: 0.08% to 0.20%, Si: 0.40% or less (including 0%), Mn: 0.5% to 5.0%, P: 0.010% or less (including 0%), S: 0.0050% or less (including 0%), Cr: 3.0% or less (including 0%), Ni: 0.1% to 5.0%, Al: 0.010% to 0.080%, N: 0.0070% or less (including 0%), and O: 0.0025% or less (including 0%). Each of the components will be described below. The symbol “%” in the component content refers to “% by mass”.


C: 0.08% to 0.20%

C is an element useful for achieving the strength necessary for structural steel at low cost. This effect requires a C content of 0.08% or more. In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, however, a C content of more than 0.20% significantly deteriorates toughness of the base metal and weld. Thus, the C content has an upper limit of 0.20%. The C content preferably ranges from 0.08% to 0.14%.


Si: 0.40% or Less

Si is added for deoxidation. When another element is added for deoxidation, however, a steel plate according to the present invention does not necessarily contain Si. In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, a Si content of more than 0.40% significantly deteriorates toughness of the base metal and heat-affected zone. Thus, the Si content is 0.40% or less, preferably 0.05% to 0.3%, more preferably 0.1% to 0.3%.


Mn: 0.5% to 5.0%

Mn is added to ensure high strength of the base metal. This effect is insufficient at a Mn content of less than 0.5%. A Mn content of more than 5.0% promotes center segregation, results in a larger casting defect of the slab, and deteriorates mechanical properties of the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. Thus, the Mn content has an upper limit of 5.0%. The Mn content preferably ranges from 0.6% to 2%, more preferably 0.6% to 1.6%.


P: 0.010% or Less

In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, a P content of more than 0.010% significantly deteriorates toughness of the base metal and heat-affected zone. Thus, the P content is preferably minimized (may be zero) and is limited to 0.010% or less.


S: 0.0050% or Less

In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, a S content of more than 0.0050% significantly deteriorates toughness of the base metal and heat-affected zone. Thus, the S content is preferably minimized (may be zero) and is 0.0050% or less.


Cr: 3.0% or Less

Cr is an element effective in strengthening the base metal. However, an excessively high Cr content deteriorates weldability. Thus, the Cr content is 3.0% or less, preferably 0.1% to 2%, more preferably 0.7% to 1.7%. The Cr content may be 0%.


Ni: 0.1% to 5.0%

Ni is an element useful for improving the strength of steel and the toughness of the heat-affected zone. This effect requires a Ni content of 0.1% or more. However, a Ni content of more than 5.0% significantly deteriorates economic efficiency. Thus, the Ni content has an upper limit of 5.0%. The Ni content preferably ranges from 0.4% to 4%, more preferably 0.8% to 3.8%.


Al: 0.010% to 0.080%

Al is added for sufficient deoxidation of molten steel. An Al content of less than 0.010% is insufficient for the effect. On the other hand, an Al content of more than 0.080% deteriorates toughness of the base metal due to an increased dissolved Al content in the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. Thus, the Al content is 0.080% or less, preferably 0.030% to 0.080%, more preferably 0.030% to 0.070%.


N: 0.0070% or Less

N, together with Ti, forms a nitride and thereby performs refinement of the structure and improves the toughness of the base metal and heat-affected zone in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. The toughness can be improved by a constituent other than N. Thus, a steel plate according to the present invention does not necessarily contain N. When trying to produce this effect with N, the N content is preferably 0.0015% or more. In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, however, a N content of more than 0.0070% deteriorates toughness of the base metal due to an increased dissolved N content in the base metal and deteriorates toughness of the heat-affected zone due to the formation of coarse carbonitride. Thus, the N content is 0.0070% or less, preferably 0.006% or less, more preferably 0.005% or less.


O: 0.0025% or Less

An O content of more than 0.0025% significantly deteriorates toughness due to the formation of a hard oxide in steel. Thus, the O content is preferably minimized (may be zero) and is 0.0025% or less.


In addition to these elements, a thick-walled high-toughness high-strength steel plate according to the present invention can contain at least one of Cu, Mo, V, Nb, and Ti in order to further improve strength and/or toughness.


Cu: 0.50% or Less

Cu can improve the strength of steel without reducing toughness. A Cu content of more than 0.50% may cause a crack on the surface of a steel plate during hot working. Thus, the Cu content, if any, is 0.50% or less.


Mo: 1.50% or Less

Mo contributes to high strength of the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. However, a Mo content of more than 1.50% results in increased hardness and deteriorates toughness due to the precipitation of alloy carbide. Thus, the Mo content, if any, has an upper limit of 1.50%. The Mo content preferably ranges from 0.2% to 0.8%.


V: 0.400% or Less

V contributes to improved strength and toughness of the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. V precipitates as VN and is effective in decreasing the amount of dissolved N. However, a V content of more than 0.400% deteriorates toughness due to the precipitation of hard VC. Thus, the V content, if any, is preferably 0.400% or less, more preferably 0.01% to 0.1%.


Nb: 0.100% or Less

Nb is effective in improving the strength of the base metal. A Nb content of more than 0.100% deteriorates toughness of the base metal. Thus, the Nb content has an upper limit of 0.100%. The Nb content is preferably 0.025% or less.


Ti: 0.005% to 0.020%

Ti forms TiN during heating and effectively suppresses the coarsening of austenite. In a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding, Ti improves the toughness of the base metal and heat-affected zone. However, a Ti content of more than 0.020% results in coarsening of Ti nitride and deteriorates toughness of the base metal. Thus, the Ti content, if any, ranges from 0.005% to 0.020%, preferably 0.008% to 0.015%.


In addition to these components, a thick-walled high-toughness high-strength steel plate according to the present invention can further contain at least one of Mg, Ta, Zr, Y, B, Ca, and REM to improve the material quality.


Mg: 0.0001% to 0.0050%

Mg forms a stable oxide at high temperatures, effectively suppresses the coarsening of prior γ grains in the heat-affected zone, and is effective in improving the toughness of the weld. These effects require a Mg content of 0.0001% or more. However, a Mg content of more than 0.0050% results in an increased number of inclusions and deteriorates toughness. Thus, the Mg content, if any, is preferably 0.0050% or less, more preferably 0.0001% to 0.015%.


Ta: 0.01% to 0.20%

The addition of an adequate amount of Ta is effective in improving strength. More specifically, a Ta content of 0.01% or more is effective. However, a Ta content of more than 0.20% deteriorates toughness due to formation of precipitates. Thus, the Ta content, if any, ranges from 0.01% to 0.20%.


Zr: 0.005% to 0.1%

Zr is an element effective in improving strength. A Zr content of 0.005% or more is effective in producing this effect. However, a Zr content of more than 0.1% deteriorates toughness due to the formation of a coarse precipitate. Thus, the Zr content, if any, ranges from 0.005% to 0.1%.


Y: 0.001% to 0.01%

Y forms a stable oxide at high temperatures, effectively suppresses the coarsening of prior γ grains in the heat-affected zone, and is effective in improving the toughness of the weld. An Y content of 0.001% or more is effective in producing these effects. However, an Y content of more than 0.01% results in an increased number of inclusions and deteriorates toughness. Thus, the Y content, if any, ranges from 0.001% to 0.01%.


B: 0.0030% or Less

B segregates at austenite grain boundaries, suppresses ferrite transformation from the grain boundaries, and improves hardenability. However, a B content of more than 0.0030% deteriorates hardenability and toughness due to the precipitation of B as a carbonitride. Thus, the B content is 0.0030% or less. The B content, if any, preferably ranges from 0.0003% to 0.0030%, more preferably 0.0005% to 0.002%.


Ca: 0.0005% to 0.0050%

Ca is an element useful for the morphology control of a sulfide inclusion. This effect requires a Ca content of 0.0005% or more. However, a Ca content of more than 0.0050% deteriorates cleanliness and toughness. Thus, the Ca content, if any, is preferably 0.0050% or less, more preferably 0.0005% to 0.0025%.


REM: 0.0005% to 0.0100%

Like Ca, REM forms an oxide and a sulfide in steel and is effective in improving the material quality. This effect requires a REM content of 0.0005% or more. However, the effect levels off at a REM content of 0.0100% or more. Thus, the REM content, if any, is 0.0100% or less, preferably 0.0005% to 0.005%.


These optional elements in amounts below the lower limits do not reduce the advantages of the present invention. Thus, the optional elements in amounts below the lower limits are considered to be contained as incidental impurities.


CeqIIW≧0.65%

In embodiments of the present invention, an appropriate alloy component needs to be added to ensure that a half-thickness portion of a thick-walled high-toughness high-strength steel plate having a thickness of 100 mm or more has a yield strength of 620 MPa or more and high toughness. More specifically, as represented by the following formula (1), alloying element contents need to be adjusted such that the carbon equivalent (CeqIIW) is 0.65% or more.





CeqIIW=C+Mn/6+(Cu+Ni)/15+(Cr+Mo+V)/5≧0.65   (1)


The element symbols in the formula denote the corresponding element contents (% by mass). In the absence of an element, the element symbol is denoted by 0.





(CL−C)/CL×100≧30  (2)


As described later, embodiments of the present invention provides a steel plate having desirable characteristics even when the steel plate is manufactured from steel casted under conditions where the cooling rate of a slab surface during solidification is 1° C./s or less. In embodiments of the present invention, microsegregation needs to be reduced to achieve high toughness (vE-40≧70 J) of the surface of a thick-walled high-toughness high-strength steel plate having a thickness of 100 mm or more, particularly manufactured from steel casted under conditions where the cooling rate of a slab surface during solidification is 1° C./s or less. To this end, primary crystals during solidification need to form a δ phase, and the percentage ((CL−C)/CL×100) of the δ phase at the beginning of the formation of a γ phase needs to be 30% or more.





CL=0.2−(−0.1×(0.2−Si)−0.03×(1.1−Mn)−0.12×(0.2−Cu)−0.11×(3−Ni)+0.025×(1.2−Cr)+0.1×(0.5−Mo)+0.2×(0.04−V)−0.05×(0.06−Al))  (3)


In the formula (3), the element symbols denote the respective alloy component contents (% by mass), and in the absence of an element, the element symbol is denoted by 0.


In order to form a δ phase, the C content needs to be specified depending on each component other than C, such as Si or Mn. The effects of an alloying element on the C solid solubility limit (CL) of the δ phase were calculated using thermodynamic calculation software “Thermo-Calc”. The result was used to determine the factor. For example, the factor “−0.1” for “Si” means that 1% Si decreases the C solid solubility limit of the δ phase by 0.1%, and the C content of the base metal needs to be decreased to achieve the required percentage of the δ phase. In embodiments of the present invention, the calculation of CL was based on the component of C: 0.12%, Si: 0.2%, Mn: 1.1%, Cu: 0.2%, Cr: 1.2%, Ni: 3%, Mo: 0.5%, V: 0.04% and Al: 0.06%, and the factors for the calculation of CL were determined by calculating a variation from the dissolved C content caused by a variation in each alloying element content. When the percentage (CL−C)/CL×100 of C to be added relative to the C solid solubility limit in the δ phase thus calculated is 30% or more, the percentage of the δ phase at the beginning of the formation of the γ phase can be 30% or more.


In embodiments of the present invention, in order to ensure the safety of steel during use, the reduction of area in the thickness direction at half the thickness of the plate is preferably 40% or more when measured by a method described in the example.


<Method for Manufacturing Thick-Walled High-Toughness High-Strength Steel Plate>

The manufacturing conditions in embodiments of the present invention will be described below. In the description, the temperature “° C.” refers to the temperature in the half-thickness portion except for the quenching temperature in the case of quenching without leaving to cool after rolling. The quenching temperature in the case of quenching without leaving to cool after rolling is the surface temperature of the steel plate. This is because the temperature distribution of the steel plate in the thickness direction increases during rolling, and a decrease in the surface temperature of the steel plate needs to be considered. The temperature of the half-thickness portion is determined, for example, by simulation calculation from the thickness, surface temperature, and cooling conditions. For example, the temperature of the half-thickness portion is determined by calculating the temperature distribution in the thickness direction using finite difference methods.


Steel

A molten steel having the composition described above is produced by a conventional method, such as with a converter, an electric furnace, or a vacuum melting furnace, and is formed into a piece of steel, such as a slab or billet, by a conventional casting method, such as a continuous casting process or an ingot casting process. The cooling rate during solidification is determined by direct measurement with a thermocouple or by simulation calculation, such as heat-transfer calculation. As described above, in embodiments of the present invention, steel manufactured under conditions where the cooling rate of a surface during solidification is 1° C./s or less can preferably be used.


When the loads of a forging machine and a rolling mill and so on are restricted, the thickness of the material may be reduced by slabbing.


Hot-Forging Conditions for Steel

A cast bloom or steel bloom having the composition described above is heated to a temperature in the range of 1200° C. to 1350° C. A reheating temperature of less than 1200° C. results in not only an insufficient rolling reduction due to an increased load to achieve a predetermined cumulative rolling reduction in hot working but also low production efficiency due to additional heating as required during working. Thus, the reheating temperature is 1200° C. or more. A large amount of additive alloying element as steel having a carbon equivalent of 0.65% or more according to embodiments of the present invention results in a casting defect such as a center porosity or porous shrinkage cavity, having a much increased size in steel. In order to make them harmless by pressure bonding, the cumulative rolling reduction needs to be 25% or more. On the other hand, a reheating temperature of more than 1350° C. results in excessive energy consumption, increased likelihood of occurrence of surface flaws due to scales during heating, and increased repair load after hot forging. Thus, the upper limit is 1350° C.


Slabbing Conditions for Steel

A cast bloom or steel bloom having the composition described above is heated to a temperature in the range of 1200° C. to 1350° C. A reheating temperature of less than 1200° C. results in not only an insufficient rolling reduction due to an increased load to achieve a predetermined cumulative rolling reduction in hot working but also low production efficiency due to additional heating as required during working. Thus, the reheating temperature is 1200° C. or more. In order to make casting defects harmless by pressure bonding and to provide the advantages of embodiments of the present invention, the cumulative rolling reduction is 30% or more, preferably 40% or more in terms of good reduction of area (RA). On the other hand, a reheating temperature of more than 1350° C. results in excessive energy consumption, increased likelihood of surface flaws due to scales during heating, and increased repair load after hot forging. Thus, the upper limit is 1350° C.


Reheating of Steel after Forging or after Slabbing


Steel after forging is heated to an Ac3 transformation temperature or more and 1200° C. or less in order that the steel may have a uniform austenite structure alone. The heating temperature preferably ranges from 1000° C. to 1200° C.


The Ac3 transformation temperature is calculated using the following formula (4).





Ac3=937.2−476.5C+56Si−19.7Mn−16.3Cu−26.6Ni−4.9Cr+38.1Mo+124.8V+136.3Ti+198.4Al+3315B  (4)


The element symbols in the formula (4) denote the respective alloy component contents (% by mass).


Hot Rolling Conditions

Steel is hot-rolled to form a plate having a desired thickness. In order to ensure desirable mechanical properties of a half-thickness portion of a thick-walled steel plate having a thickness of 100 mm or more, it is necessary to adjust the steel in the rolling step in order to sufficiently elicit an effect of adjusting and refining of the prior γ grain size. More specifically, rolling at a cumulative rolling reduction of 40% or more can adjust the grain size in the rolling step even in the half-thickness portion in which recrystallization rarely occurs in processing.


Heat-Treatment Conditions

In order to achieve high strength and toughness of a half-thickness portion, in embodiments of the present invention, a steel plate is left to cool (for example, air cooling) after hot rolling or is rapidly cooled from the Ar3 temperature or more to 350° C. or less without leaving to cool after hot rolling. When the steel plate is left to cool, the steel plate is reheated to the Ac3 temperature to 1050° C. and is rapidly cooled from the Ac3 temperature or more to 350° C. or less. The reason for the reheating temperature of 1050° C. or less is that reheating at a high temperature of more than 1050° C. results in coarsening of austenite grains and significantly deteriorates toughness of the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding. The reheating temperature is the Ac3 temperature or more in order that the steel plate may entirely have an austenite structure. The quenching temperature is the Ac3 temperature or more because the desirable characteristics are not obtained at a temperature below the Ac3 temperature due to the formation of a nonuniform structure composed of ferrite and austenite. In the case of rapid cooling without leaving to cool, the quenching temperature is the Ar3 temperature or more for quenching from the austenite single phase region. The rapid cooling stop temperature is a lower temperature selected from 350° C. or less and the Ar3 temperature or less in order to ensure that the steel plate entirely has a transformed structure. The stop temperature should be the Ar3 temperature or less and 350° C. or less.


The Ar3 transformation temperature is calculated using the following formula (5).





Ar3=910−310C−80Mn−20Cu−15Cr−55Ni−80Mo  (5)


The element symbols in the formula (5) denote the respective alloy component contents (% by mass).


In general, the rapid cooling method is industrially water cooling. It is desirable that the cooling rate be as high as possible. Thus, the cooling method is not necessarily water cooling and may be gas cooling, for example.


Tempering Conditions

The reason for tempering at a temperature in the range of 450° C. to 700° C. after rapid cooling is described below. Residual stress is not effectively relieved at less than 450° C. On the other hand, a temperature of more than 700° C. results in precipitation of various carbides and coarsens the structure of the base metal and deteriorates strength and toughness of the base metal in a steel structure manufactured from a thick-walled high-toughness high-strength steel plate by welding.


Industrially, quenching is sometimes repeated to strengthen steel. Although quenching may be repeated also in embodiments of the present invention, final quenching requires rapid cooling to 350° C. or less after heating to the Ac3 temperature to 1050° C. and requires subsequent tempering at 450° C. to 700° C.


Examples

Steel plate samples No. 1 to No. 38 were manufactured by melting and casting steel No. 1 to No. 30 listed in Table 1 under the conditions listed in Table 2, performing hot forging (except for the samples No. 5, No. 6, and No. 41) or slabbing (the samples No. 5, No. 6, and No. 41), hot-rolling the steel to form a steel plate having a thickness listed in Table 2, and subjecting the steel plate to water quenching and tempering. The steel plate samples No. 1 to No. 38 were subjected to the following tests. In reheating and quenching in this example, the reheating temperature corresponds to the quenching temperature.


The percentage of the δ phase is calculated using the formula (2) from CL calculated using the formula (3) with each base metal component and the C content of the base metal.


The cooling rate during solidification in the manufacture of steel is determined by heat-transfer calculation from the mold surface temperature data measured with a radiation thermometer.


Tensile Test

A round bar tensile test piece (φ2.5 mm, GL 50 mm) was taken from the half-thickness portion of each steel plate in the direction perpendicular to the rolling direction and was measured in terms of yield strength (YS) and tensile strength (TS).


Charpy Impact Test

Three 2-mm V-notched Charpy impact test specimens were taken from each surface and half-thickness portion of the steel plates. The rolling direction was the longitudinal direction. The absorbed energies of the test specimens were measured at a test temperature of −40° C. in a Charpy impact test and were averaged (the average value for the test specimens taken from the half-thickness portion and the average value for the test specimens taken from the surface).


Tensile Test in Thickness Direction

A round bar tensile test piece (φ10 mm) was taken from a region including the half-thickness portion of each steel plate in the thickness direction and was measured in terms of reduction of area (RA). The reduction of area is the percentage of the difference between the minimum cross-sectional area after the test specimen was broken and the original cross-sectional area relative to the original cross-sectional area.


Table 2 shows the test results. The results showed that the steel plates of the examples having a steel composition according to the present invention (samples No. 1 to No. 21 and No. 41) had YS of 620 MPa or more, TS of 720 MPa or more, and toughness (vE-40) of 70 J or more at −40° C. in the surface and half-thickness portion of the base metal, showing high strength and toughness of the base metal. A comparison between Nos. 5 and 6 and No. 41 showed that reduction of area (RA) was also satisfactory under particular slabbing conditions.


In contrast, in the steel plates according to comparative examples having a composition outside the scope of the present invention (samples No. 22 to No. 32), the base metal had at least one of YS of less than 620 MPa, TS of less than 720 MPa, and toughness (vE-40) of less than 70 J, thus deteriorating characteristics.


As in samples No. 33 to No. 40, even if steel plates had a steel composition according to the present invention, steel plates manufactured under the conditions outside the scope of the present invention had at least one deterioration in YS, TS, and toughness (vE-40) (No. 41, which had a cumulative rolling reduction of 30% and satisfied the minimum conditions required to provide the advantages of the present invention, is not outside the scope of the present invention).











TABLE 1








Steel




ingot
Chemical composition (mass %)





















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





Example
1
0.085
0.18
1.61
0.006
0.0012
0.66
0.88

0.063
0.0041
0.0013
0.25
0.45



2
0.095
0.22
1.15
0.005
0.0006
1.80
1.95

0.045
0.0022






3
0.128
0.21
0.98
0.005
0.0011
0.81
1.01
0.010
0.045
0.0040
0.0011
0.28
0.54



4
0.120
0.22
1.14
0.006
0.0006
0.94
1.94

0.062
0.0049
0.0011
0.18
0.49



5
0.126
0.20
1.15
0.003
0.0008
0.95
2.05
0.010
0.043
0.0028
0.0009
0.22
0.51



6
0.123
0.20
1.18
0.004
0.0007
0.87
2.44

0.066
0.0050
0.0012
0.19
0.52



7
0.109
0.17
0.85
0.003
0.0004
1.13
3.56

0.071
0.0049
0.0010
0.08
0.53



8
0.121
0.22
0.88
0.006
0.0011
1.49
2.93

0.068
0.0046
0.0008
0.21
0.55



9
0.142
0.21
0.69
0.006
0.0009
1.51
2.87

0.071
0.0038
0.0013
0.20
0.50



10
0.113
0.11
0.81
0.006
0.0005
1.53
3.61

0.069
0.0052
0.0010
0.02
0.56



11
0.178
0.09
0.60
0.006
0.0006
1.14
2.84

0.078
0.0054
0.0009
0.11
0.55



12
0.196
0.06
0.53
0.009
0.0007
1.35
3.65

0.062
0.0046


1.43



13
0.095
0.23
2.21
0.006
0.0004

0.74

0.035
0.0039
0.0011
0.20
0.65



14
0.118
0.21
1.13
0.006
0.0008
1.44
3.49

0.065
0.0045

0.12
0.57



15
0.142
0.05
0.57
0.009
0.0012
2.41
0.15
0.009
0.026
0.0050
0.0009
0.14
1.07



16
0.161
0.22
1.03
0.005
0.0013
1.55
0.98
0.011
0.045
0.0033
0.0011
0.32




17
0.103
0.20
0.98
0.006
0.0018
0.56
2.21

0.049
0.0063
0.0013
0.18
0.55



18
0.132
0.13
1.01
0.005
0.0006
0.86
1.44
0.012
0.065
0.0041
0.0009
0.22
0.44



19
0.162
0.16
0.59
0.006
0.0019
1.41
3.98

0.063
0.0038
0.0018
0.16
1.47


Comparative
20
0.113
0.22
1.14
0.006
0.0006
0.81
3.57

0.070
0.0050
0.0012
0.20
0.51


example
21
0.083
0.16
1.45
0.007
0.0011
0.67
0.45

0.006
0.0043
0.0014
0.21
0.45



22
0.221
0.55
1.02
0.006
0.0006
0.91
0.89
0.010
0.044
0.0028
0.0011
0.12
0.46



23
0.058
0.39
1.41
0.010
0.0018
1.23
1.96

0.045
0.0056
0.0012
0.23
0.41



24
0.129
0.63
1.33
0.009
0.0009
0.98
0.65

0.058
0.0049
0.0009
0.21
0.55



25
0.153
0.18
6.11
0.009
0.0009
1.04
1.21

0.066
0.0051
0.0009
0.21
0.44



26
0.124
0.22
1.41
0.018
0.0007
0.91
2.11

0.056
0.0048
0.0007
0.19
0.38



27
0.135
0.21
1.14
0.005
0.0069
1.21
1.48

0.065
0.0044
0.0009

0.48



28
0.124
0.26
0.65
0.005
0.0006
4.10
1.38

0.056
0.0038
0.0007

0.25



29
0.131
0.24
1.15
0.009
0.0008
1.05
1.95
0.006
0.098
0.0069
0.0009
0.29
0.48



30
0.133
0.26
1.13
0.009
0.0018
0.96
1.99

0.063
0.0123
0.0008
0.22
0.43



























Steel












δ















ingot
Chemical composition (mass %)
Ac3
Ar3
fraction























Category
No.
V
O
Nb
Mg
Ta
Zr
Y
Ca
REM
CeqIIW
° C.
° C.
%






Example
1
0.035
0.0021





0.0017

0.658
883
656
78




2

0.0015







0.777
830
654
68




3
0.045
0.0018





0.0019
0.0021
0.656
873
675
69




4
0.039
0.0016





0.0017

0.745
850
618
61




5
0.042
0.0018





0.0015

0.769
840
607
58




6
0.041
0.0019





0.0020

0.781
836
585
52




7
0.040
0.0022





0.0012

0.833
819
551
34




8
0.038
0.0021





0.0019

0.893
828
570
46




9
0.037
0.0019





0.0018

0.871
823
586
39




10
0.040
0.0023





0.0016

0.916
813
543
39




11
0.041
0.0024







0.821
807
587
31




12
0.059
0.0021







1.095
807
471
31




13

0.0022





0.0022

0.656
874
607
76




14
0.045
0.0021





0.0013

0.958
809
521
30




15
0.328
0.0022
0.031






1.018
934
688
80




16
0.043
0.0009

0.0013



0.0019

0.738
833
694
56




17
0.036
0.0022


0.048


0.0022

0.655
855
622
63




18
0.028
0.0019



0.015

0.0018

0.677
853
657
64




19
0.115
0.0018




0.005
0.0016

1.135
831
452
31



Comparative
20
0.040
0.0020





0.0016

0.826
813
530
9



example
21
0.038
0.0022





0.0018

0.600
887
693
82




22

0.0013







0.732
844
658
43




23
0.041
0.0018





0.0023

0.775
875
616
79




24
0.039
0.0021






0.0016
0.722
900
665
68




25
0.041
0.0016





0.0014

1.570
751
252
36




26

0.0026





0.0016

0.770
827
595
52




27
0.026
0.0019







0.767
854
639
65




28

0.0016





0.0026

1.194
846
662
72




29

0.0016







0.778
845
610
54




30

0.0022





0.0018

0.747
836
616
53





CeqIIW, Ac3, Ar3, and δ fraction were calculated using the formulae (1), (2), (4), and (5), respectively.





















TABLE 2











Cooling
Hot forging









rate
or slabbing

Thick-




















Thick-
during

Cumulative
Hot rolling
ness




















Steel
ness of
solidi-

rolling

Cumulative
of




Sample
ingot
material
fication
Heating
reduction
Heating
rolling
product
Type of


Category
No.
No.
(mm)
° C./s
(° C.)
(%)
(° C.)
reduction (%)
(mm)
heat treatment





Example
1
1
1000
0.32
1270
80
1130
43
100
Direct quenching



2
2
 500
0.64
1230
65
1130
43
100
Reheating quenching



3
3
 300
0.90
1200
30
1130
50
100
Reheating quenching



4
4
1000
0.33
1270
70
1160
43
150
Reheating quenching



5
4
1000
0.33
1320
55
1200
53
210
Reheating quenching



6
4
1000
0.33
1300
55
1180
67
150
Direct quenching



7
5
 500
0.61
1270
45
1160
43
150
Reheating quenching



8
6
1000
0.32
1270
55
1130
60
180
Reheating quenching



9
7
1000
0.31
1270
55
1130
53
210
Reheating quenching



10
8
1000
0.31
1300
55
1130
53
210
Reheating quenching



11
9
1000
0.30
1270
55
1130
53
210
Reheating quenching



12
10
1200
0.25
1270
55
1160
50
250
Reheating quenching



13
11
1000
0.29
1270
70
1160
43
150
Reheating quenching



14
12
1300
0.19
1270
60
1160
50
250
Reheating quenching



15
13
1200
0.32
1270
85
1130
43
100
Reheating quenching



16
14
1000
0.31
1270
55
1160
53
210
Reheating quenching



17
15
1000
0.32
1270
55
1160
53
210
Reheating quenching



18
16
 500
0.64
1230
65
1130
43
100
Reheating quenching



19
17
 500
0.65
1230
65
1160
43
100
Reheating quenching



20
18
 300
0.91
1200
40
1160
43
100
Direct quenching



21
19
1000
0.29
1350
50
1160
50
250
Reheating quenching


Compar-
22
20
1000
0.29
1270
55
1160
53
210
Reheating quenching


ative
23
21
 300
0.92
1200
40
1160
43
100
Reheating quenching


example
24
22
1000
0.31
1270
70
1160
43
150
Reheating quenching



25
23
1000
0.29
1270
70
1160
53
210
Reheating quenching



26
24
1000
0.29
1270
55
1130
50
250
Reheating quenching



27
25
1200
0.24
1270
55
1160
43
150
Reheating quenching



28
26
1000
0.28
1270
70
1160
53
210
Reheating quenching



29
27
1000
0.31
1270
55
1130
53
210
Reheating quenching



30
28
1000
0.29
1270
55
1130
53
210
Reheating quenching



31
29
1000
0.32
1270
55
1130
43
150
Reheating quenching



32
30
1000
0.31
1270
70
1160
60
100
Reheating quenching



33
3
 300
0.91
1200
15
1130
20
100
Reheating quenching



34
3
 300
0.89
1200
55
1130
50
100
Reheating quenching



35
3
 300
0.90
1200
30
1130
50
100
Reheating quenching



36
3
 300
0.92
1200
30
1130
50
100
Reheating quenching



37
3
 300
0.90
1200
30
1130
50
100
Direct quenching



38
3
 300
0.91
1200
30
1130
50
100
Reheating quenching



39
3
 300
0.90
1200
30
1130
50
100
Reheating quenching



40
3
 300
0.91
1200
30
1130
50
100
Reheating quenching


Example
41
5
 500
0.61
1300
30
1180
40
210
Reheating quenching



















Mechanical properties







of base metal (1/2t)
Tough-






















Tensile
ness





Final heat



RA in
of base





treatment conditions



thickness
metal




















Quenching
Cooling




direction
(surface)




Sample
temperature
stop
Tempering
YS
TS
vE-40
RA
vE-40



Category
No.
(° C.)
(° C.)
(° C.)
(MPa)
(MPa)
(J)
(%)
(J)






Example
1
850
150
630
695
786
108
73
 98




2
930
100
650
698
795
167
63
105




3
930
100
630
725
793
102
70
116




4
900
100
630
785
856
205
65
221




5
900
100
630
743
829
145
71
124




6
860
100
630
751
832
126
58
159




7
900
100
630
725
821
153
63
205




8
880
100
630
705
816
238
61
211




9
880
100
650
756
864
216
63
163




10
880
100
650
741
836
193
60
121




11
880
100
650
759
857
186
62
101




12
900
100
630
748
852
221
59
146




13
880
100
630
728
839
169
71
101




14
880
100
660
793
912
221
68
145




15
930
100
650
665
756
103
73
126




16
880
100
650
723
814
203
69
163




17
1050
150
670
641
738
145
70
101




18
930
100
650
732
841
167
77
 83




19
900
100
650
703
789
196
73
113




20
880
150
650
752
846
138
65
106




21
900
100
650
746
863
231
62
 93



Compar-
22
880
100
640
716
815
196
61
 43



ative
23
930
100
650
589
695
 22
69
121



example
24
900
100
630
845
956
 19
62
 96




25
930
100
630
547
663
 21
68
124




26
930
100
650
728
823
 41
64
 39




27
880
100
630
802
915
 23
51
 96




28
880
100
630
731
829
 32
57
 23




29
900
100
650
741
854
 35
63
 31




30
900
100
650
796
921
 43
61
 89




31
900
100
650
732
816
 48
72
 56




32
900
100
630
698
784
 61
70
 52




33
930
100
630
716
804
 43
23
115




34
930
100
630
722
816
 45
35
 96




35
1100
100
630
735
824
 36
53
 49




36
840
100
630
536
646
 46
49
 52




37
623
100
630
596
683
 52
51
 61




38
930
400
630
503
641
 32
64
103




39
930
100
720
569
657
153
68
146




40
930
100
400
793
902
 41
63
 53



Example
41
900
100
600
683
766
105
29
192








Claims
  • 1. A thick-walled, high-toughness, high-strength steel plate having a thickness of 100 mm or more, comprising, on a mass percent basis, C: 0.08% to 0.20%,Si: 0.40% or less,Mn: 0.5% to 5.0%,P: 0.010% or less,S: 0.0050% or less,Cr: 3.0% or less,Ni: 0.1% to 5.0%,Al: 0.010% to 0.080%,N: 0.0070% or less, andO: 0.0025% or less,wherein the following formulae (1) and (2) being satisfied, a remainder being Fe and incidental impurities: CeqIIW=C+Mn/6+(Cu+Ni)/15+(Cr+Mo+V)/5≧0.65  (1);(CL−C)/CL×100≧30  (2);wherein CL is defined by the following formula: CL=0.2−(−0.1×(0.2−Si)−0.03×(1.1−Mn)−0.12×(0.2−Cu)−0.11×(3−Ni)+0.025×(1.2−Cr)+0.1×(0.5−Mo)+0.2×(0.04−V)−0.05×(0.06−Al))  (3);wherein element symbols in the formulae denote the respective alloy component contents (% by mass), and in the absence of an element the element symbol is denoted by 0;and a surface of the steel plate having a toughness (vE-40) of 70 J or more.
  • 2. The thick-walled, high-toughness, high-strength steel plate according to claim 1, further comprising, on a mass percent basis, at least one of: Cu: 0.50% or less,Mo: 1.50% or less,V: 0.400% or less,Nb: 0.100% or less, andTi: 0.005% to 0.020%.
  • 3. The thick-walled, high-toughness, high-strength steel plate according to claim 1, further comprising, on a mass percent basis, at least one of: Mg: 0.0001% to 0.0050%,Ta: 0.01% to 0.20%,Zr: 0.005% to 0.1%,Y: 0.001% to 0.01%,B: 0.0030% or less,Ca: 0.0005% to 0.0050%, andREM: 0.0005% to 0.0100%.
  • 4. The thick-walled, high-toughness, high-strength steel plate according to claim 1, wherein the steel plate has a yield strength of 620 MPa or more.
  • 5. The thick-walled, high-toughness, high-strength steel plate according to claim 1, wherein a reduction of area in a thickness direction at half the thickness of the plate is 40% or more.
  • 6. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 1, comprising: heating steel to 1200° C. to 1350° C.,hot-forging the steel at a cumulative rolling reduction of 25% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,leaving the steel to cool,reheating the steel to a temperature in the range of from the Ac3 temperature to 1050° C.,rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 7. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 1, comprising: heating steel to 1200° C. to 1350° C.,hot-forging the steel at a cumulative rolling reduction of 25% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 8. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 1, comprising: heating steel to 1200° C. to 1350° C.,slabbing the steel at a cumulative rolling reduction of 40% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more, leaving the steel to cool,reheating the steel to a temperature in the range of from the Ac3 temperature to 1050° C.,rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 9. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 1, comprising: heating steel to 1200° C. to 1350° C.,slabbing the steel at a cumulative rolling reduction of 40% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 10. The thick-walled, high-toughness, high-strength steel plate according to claim 2, further comprising, on a mass percent basis, at least one of: Mg: 0.0001% to 0.0050%,Ta: 0.01% to 0.20%,Zr: 0.005% to 0.1%,Y: 0.001% to 0.01%,B: 0.0030% or less,Ca: 0.0005% to 0.0050%, andREM: 0.0005% to 0.0100%.
  • 11. The thick-walled, high-toughness, high-strength steel plate according to claim 2, wherein the steel plate has a yield strength of 620 MPa or more.
  • 12. The thick-walled, high-toughness, high-strength steel plate according to claim 3, wherein the steel plate has a yield strength of 620 MPa or more.
  • 13. The thick-walled, high-toughness, high-strength steel plate according to claim 2, wherein a reduction of area in a thickness direction at half the thickness of the plate is 40% or more.
  • 14. The thick-walled, high-toughness, high-strength steel plate according to claim 3, wherein a reduction of area in a thickness direction at half the thickness of the plate is 40% or more.
  • 15. The thick-walled, high-toughness, high-strength steel plate according to claim 4, wherein a reduction of area in a thickness direction at half the thickness of the plate is 40% or more.
  • 16. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 2, comprising: heating steel to 1200° C. to 1350° C.,hot-forging the steel at a cumulative rolling reduction of 25% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,leaving the steel to cool,reheating the steel to a temperature in the range of from the Ac3 temperature to 1050° C.,rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 17. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 2, comprising: heating steel to 1200° C. to 1350° C.,hot-forging the steel at a cumulative rolling reduction of 25% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 18. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 2, comprising: heating steel to 1200° C. to 1350° C.,slabbing the steel at a cumulative rolling reduction of 40% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more, leaving the steel to cool,reheating the steel to a temperature in the range of from the Ac3 temperature to 1050° C.,rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 19. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 2, comprising: heating steel to 1200° C. to 1350° C.,slabbing the steel at a cumulative rolling reduction of 40% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,rapidly cooling the steel from the Ar3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
  • 20. A method for manufacturing the thick-walled, high-toughness, high-strength steel plate according to claim 3, comprising: heating steel to 1200° C. to 1350° C.,hot-forging the steel at a cumulative rolling reduction of 25% or more,heating the steel to a temperature in the range of from an Ac3 temperature to 1200° C.,hot-rolling the steel at a cumulative rolling reduction of 40% or more,leaving the steel to cool,reheating the steel to a temperature in the range of from the Ac3 temperature to 1050° C.,rapidly cooling the steel from the Ac3 temperature or more to a lower temperature selected from 350° C. or less and an Ar3 temperature or less, andtempering the steel at a temperature in the range of from 450° C. to 700° C.
Priority Claims (1)
Number Date Country Kind
2015-006670 Jan 2015 JP national
CROSS REFERENCE TO RELATED APPLICATIONS

This is the U.S. National Phase application of PCT/JP2016/000197, filed Jan. 15, 2016, which claims priority to Japanese Patent Application No. 2015-006670, filed Jan. 16, 2015, the disclosures of these applications being incorporated herein by reference in their entireties for all purposes.

PCT Information
Filing Document Filing Date Country Kind
PCT/JP2016/000197 1/15/2016 WO 00