WO2020111860A2 - 취성균열전파 저항성이 우수한 극후물 강재 및 그 제조방법 - Google Patents
취성균열전파 저항성이 우수한 극후물 강재 및 그 제조방법 Download PDFInfo
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- 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
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- 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
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- 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/02—Hardening articles or materials formed by forging or rolling, with no further heating beyond that required for the formation
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- 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
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- 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
- C21D6/001—Heat treatment of ferrous alloys containing Ni
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- 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
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/021—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving particular fabrication steps or treatments of ingots or slabs
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- C—CHEMISTRY; METALLURGY
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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0231—Warm rolling
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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties of ferrous metals or ferrous alloys 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
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- 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
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- 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
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- 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
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- 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
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- 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
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- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
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- 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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
Definitions
- the present invention relates to an extremely thick steel having excellent brittle crack propagation resistance and a method for manufacturing the same.
- the NDTT (Nil-Ductility Transition Temperature) value based on 1/4t is -45°C or less, effectively securing brittle crack propagation resistance.
- An object of the present invention is to provide an extremely thick steel having excellent brittle crack propagation resistance and a method for manufacturing the same.
- NRL-DWT Neuro Research Laboratory- NRL-DWT
- the surface portion of the steel material is a region where a rapid cooling rate is applied during water cooling compared to the center of the steel material or the t/4 part (where t denotes the thickness of the steel material, hereinafter the same), and the yield strength is high, such as a 500MPa grade steel material.
- a steel material having hardenability a large amount of low-temperature transformation phases may be formed. Therefore, despite the fact that the measured brittle crack propagation related index in the actual large-scale tensile test is excellent, the NRL-DWT test result shows a tendency to be poorly evaluated.
- Patent Document 1 Republic of Korea Patent Publication No. 10-2016-0079163 (2016.07.06. public)
- an extremely thick steel having excellent brittle crack propagation resistance and a method of manufacturing the same can be provided.
- the extreme thick steel having excellent brittle crack propagation resistance is, by weight, C: 0.02 to 0.07%, Mn: 1.8 to 2.2%, Ni: 0.7 to 1.2%, Nb: 0.005 to 0.02%, Ti: 0.005 to 0.02%, Cu: 0.1 to 0.4%, P: 0.01% or less, S: 0.004% or less, including the remaining Fe and unavoidable impurities, and t/4 to (3*t)/8 regions (where: t denotes the thickness of the steel, and the average particle size of the crystal grains having a high boundary angle of 15 degrees or more as measured by EBSD in the following) may be 15 ⁇ m or less.
- the NDT (Nil-Ductility Transition) temperature may be -45°C or less.
- the impact transition temperature of the test sample collected in the t/4 region of the steel may be -60°C or less.
- the microstructure of the test sample collected in the t/4 region of the steel material may include a composite structure of cyclic circular ferrite and granular bainite, and may further include a phase martensite in the second phase.
- the cyclic circular ferrite may be included at a ratio of 60 to 80 area%, the granular bainite at a rate of 20 to 40 area%, and the island martensite at a rate of 10 area% or less.
- the thickness of the steel material may be 50 ⁇ 120mm.
- the yield strength of the steel material may be 500 MPa or more.
- the extreme thick steel having excellent brittle crack propagation resistance is, by weight, C: 0.02 to 0.07%, Mn: 1.8 to 2.2%, Ni: 0.7 to 1.2%, Nb: 0.005 to 0.02%, Ti: 0.005 to 0.02%, Cu: 0.1 to 0.4%, P: 0.01% or less, S: 0.004% or less, reheat the slab containing the remaining Fe and unavoidable impurities, roughly roll the reheated slab, and 50%
- the rough rolled slab may be finished rolling at the above cumulative rolling reduction ratio, and may be manufactured by cooling the finished rolled steel.
- the slab can be reheated in a temperature range of 1000 to 1120°C.
- the reheated slab can be rough rolled at a cumulative coalescence rate of 40% or more in a temperature range of 850 to 1050°C.
- the finishing rolling may be initiated in a temperature range of 700 to 850°C.
- the finished rolled steel can be cooled to a temperature range of 500°C or less at a cooling rate of 3°C/s or more.
- the present invention relates to an extremely thick steel material having excellent brittle crack propagation resistance and a method for manufacturing the same, and the following will describe preferred embodiments of the present invention.
- the embodiments of the present invention may be modified in various forms, and the scope of the present invention should not be construed as being limited to the embodiments described below.
- the present embodiments are provided to those skilled in the art to further detail the present invention.
- an extremely thick steel having excellent brittle crack propagation resistance is, by weight, carbon (C): 0.02 to 0.07%, manganese (Mn): 1.8 to 2.2%, nickel (Ni): 0.7 to 1.2. %, Niobium (Nb): 0.005 to 0.02%, Titanium (Ti): 0.005 to 0.02%, Copper (Cu): 0.1 to 0.4%, Phosphorus (P): 0.01% or less, Sulfur (S): 0.004% or less, The remaining Fe and unavoidable impurities may be included.
- Carbon (C) is the most effective element for securing the strength of the steel, and therefore needs to be contained in the steel within an appropriate range.
- the present invention can limit the lower limit of the carbon (C) content to 0.02% to secure the strength.
- the lower limit of the preferred carbon (C) content may be 0.03%.
- the upper limit of the preferred carbon (C) content may be 0.06%.
- Manganese (Mn) is an element that effectively improves the strength of steel through solid solution strengthening and hardenability improvement.
- the present invention can limit the lower limit of the manganese (Mn) content to 1.8% in order to secure a strength of at least 500 MPa yield strength.
- the present invention may limit the upper limit of the manganese (Mn) content to 2.2%.
- the upper limit of the preferred manganese (Mn) content may be 2.1%.
- Nickel (Ni) is an element that contributes to improving impact toughness by facilitating cross slip of dislocation at low temperatures, and is also an element contributing to the improvement of strength of steel by improving hardenability.
- the present invention can limit the lower limit of the nickel (Ni) content to 0.7% in order to achieve this effect.
- the lower limit of the preferred nickel (Ni) content may be 0.75%.
- the upper limit of the nickel (Ni) content may be limited to 1.2%.
- the upper limit of the preferred nickel (Ni) content may be 1.15%.
- Niobium (Nb) is an element that contributes to the enhancement of the strength of the base material by precipitation with carbide or nitride.
- niobium (Nb) employed during reheating at a high temperature is very finely precipitated in the form of carbide (NbC) during rolling and suppresses recrystallization of austenite, thus effectively contributing to the refinement of the structure.
- the present invention can limit the lower limit of the niobium (Nb) content to 0.005% to achieve this effect.
- the present invention is niobium.
- the upper limit of the (Nb) content can be limited to 0.02%.
- the upper limit of the preferred niobium (Nb) content may be 0.017%.
- Titanium (Ti) is an element that effectively contributes to the improvement of low-temperature toughness by inhibiting grain growth of the base material and the welding heat-affected zone by forming a TiN precipitate.
- the present invention can limit the addition amount of titanium (Ti) to 0.005% or more for forming a TiN precipitate.
- titanium (Ti) is excessively added, a problem occurs in that low-temperature toughness is inferior due to coarse TiN crystallization, and thus the present invention may limit the upper limit of the titanium (Ti) content to 0.02%.
- the upper limit of the preferred titanium (Ti) content may be 0.015%.
- Copper (Cu) is an element that contributes to improving the strength of steel by improving hardenability and solid solution strengthening.
- copper (Cu) is also an element that contributes to the improvement of yield strength by generating epsilon copper (Cu) precipitates during heat treatment.
- copper (Cu) of 0.1% or more may be added to achieve such an effect of improving strength.
- the lower limit of the preferred copper (Cu) content may be 0.15%.
- the present invention may limit the upper limit of the copper (Cu) content to 0.4%.
- the upper limit of the preferred copper (Cu) content may be 0.35%.
- Phosphorus (P) and sulfur (S) is an element that causes brittleness at a grain boundary or forms coarse inclusions, thereby inducing brittleness, so the present invention uses phosphorus (P) and sulfur (S) contents to secure brittle crack propagation resistance. It can be limited to 0.01% or less and 0.004% or less, respectively.
- the present invention in addition to the above-described steel composition may be Fe and unavoidable impurities.
- the unavoidable impurities may be unintentionally incorporated in the ordinary steel manufacturing process, and cannot be completely excluded, and the meaning can be easily understood by those skilled in the ordinary steel manufacturing field.
- this invention does not exclude the addition of the composition other than the steel composition mentioned above entirely.
- Crystal grains having a high boundary angle of 15 degrees or more measured by EBSD in t/4 to (3*t)/8 regions of steel according to an aspect of the present invention (where t denotes the thickness of the steel, hereinafter the same)
- the average particle size may be 15 ⁇ m or less.
- the NDT (Nil-Ductility Transition) temperature It may be below -45°C, and the NDT temperature of the more preferable t/4 region may be below -50°C.
- the impact transition temperature of the test sample collected in the t/4 region of the steel according to an aspect of the present invention may be -60°C or less, and the impact transition temperature of the more preferable t/4 region may be -70°C or less.
- the microstructure of the test sample collected in the t/4 region of the steel includes a composite structure of cyclic circular ferrite and granular bainite, and may further include a phase martensite in the second phase.
- the fraction of the cyclic circular ferrite in the t/4 region may be 60 to 80 area%, and the fraction of the granular bainite in the t/4 region may be 20 to 40 area%.
- the fraction of the island martesite of the present invention may be 10 area% or less based on the t/4 area.
- granular bainite is generated from the residual austenite after the simultaneous generation of the ecological ferrite generated at high temperature in the grain boundary and in the mouth.
- coarse bainite packets By suppressing the generation of coarse bainite packets, it is possible to refine the t/4 part structure.
- island martensite it is preferable in terms of securing impact toughness and NRL-DWT properties to suppress the fraction as much as possible because it acts as a crack initiation point during deformation.
- the thickness of the steel according to an aspect of the present invention may be 50 ⁇ 120mm.
- the preferred thickness of the steel material may be 50 to 100 mm, and the more preferred thickness of the steel material may be 70 to 100 mm.
- the yield strength of the steel according to an aspect of the present invention may be 500 MPa or more, and a more preferable yield strength may be 520 MPa or more.
- the extreme thick steel having excellent brittle crack propagation resistance is, by weight, C: 0.02 to 0.07%, Mn: 1.8 to 2.2%, Ni: 0.7 to 1.2%, Nb: 0.005 to 0.02%, Ti: 0.005 to 0.02%, Cu: 0.1 to 0.4%, P: 0.01% or less, S: 0.004% or less, reheat the slab containing the remaining Fe and inevitable impurities, and roughly roll the reheated slab,
- the rolled slab can be manufactured by finishing rolling at a cumulative rolling reduction of 50% or more at a finishing temperature of 700 to 850°C, and cooling the finished rolled steel.
- the slab of the present invention is provided with the alloy composition corresponding to the alloy composition of the aforementioned steel material, the description of the slab alloy composition of the present invention is replaced by the description of the alloy composition of the above-mentioned steel material.
- the slab provided with the composition may be reheated in a temperature range of 1000 to 1120°C.
- the austenite may be misaligned, so it is preferable to perform the slab reheating in a temperature range of 1120°C or lower.
- Rough rolling can be performed to adjust the shape of the reheated slab.
- the coarse austenite can be miniaturized through recrystallization along with the destruction of the casting structure such as dendrites formed during casting by rough rolling.
- the rough rolling temperature may be limited to a range of 850 to 1050°C.
- rough rolling may be performed under a total cumulative reduction rate of 40% or more.
- Finish rolling is an important process for securing the t/4 part structure and physical properties of the steel material desired by the present invention, so it is necessary to control strict process conditions. Finish rolling is performed to introduce a non-uniform microstructure into austenite of a rough-rolled steel material, and may be performed in a temperature range of 700 to 850°C so that deformation applied to the t/4 part of the steel material can be maintained. In addition, in order to achieve a particle size refinement effect, the total cumulative rolling reduction may be performed by finishing rolling under conditions of 50% or more.
- the finishing rolling of the present invention is preferably initiated in a temperature range of 700 to 850°C, and a more preferred starting temperature of finishing rolling may be in the range of 730 to 850°C.
- the cooling method of the present invention is not particularly limited, but water cooling may be preferable in terms of cooling efficiency.
- the finished rolled steel can be cooled to a temperature range of 500°C or less at a cooling rate of 3°C/s or higher. If the cooling rate is less than 3°C/s, the microstructure of the central portion of the steel material is not properly formed and yield strength may be lowered. In addition, when the cooling end temperature exceeds 500°C, the microstructure of the steel material is not properly formed and yield strength may be lowered.
- the steel material produced by the manufacturing method according to an aspect of the present invention is measured by EBSD in t/4 to (3*t)/8 regions of steel (where t denotes the thickness of the steel material, hereinafter the same).
- the average particle size of the crystal grains having a high boundary angle of more than 15 degrees may be less than 15 ⁇ m.
- the steel material produced by the manufacturing method according to an aspect of the present invention is a test piece collected in the t/4 region of the steel material, when performing NRL-DWT (Naval Research Laboratory-Drop Weight Test) specified in ASTM E208-06
- NRL-DWT Vehicle Research Laboratory-Drop Weight Test
- the NDT (Nil-Ductility Transition) temperature may be -45°C or less, and the NDT temperature in the more preferable t/4 region may be -50°C or less.
- the impact transition temperature of the test sample collected in the t/4 region of the steel material may be -60°C or less, and the more preferable impact temperature in the t/4 region is- It may be 70 °C or less.
- the test piece collected from the t/4 region of the steel produced by the manufacturing method according to one aspect of the present invention includes a composite structure of cyclic circular ferrite and granular bainite as a microstructure, and a phase-like martensite in a second phase. It may further include.
- the fraction of the cyclic circular ferrite in the t/4 region may be 60 to 80 area%, and the fraction of the granular bainite in the t/4 region may be 20 to 40 area%.
- the fraction of the island martesite of the present invention may be 10 area% or less based on t/4.
- the thickness of the steel material produced by the manufacturing method according to an aspect of the present invention may be 50 ⁇ 120mm.
- the preferred thickness of the steel material may be 50 to 100 mm, and the more preferred thickness of the steel material may be 70 to 100 mm.
- the yield strength of the steel material produced by the manufacturing method according to an aspect of the present invention may be 500 MPa or more, and the more preferable yield strength may be 520 MPa or more.
- a steel slab having a thickness of 400 mm was prepared by the alloy composition of Table 1 below. After reheating each steel slab in a temperature range of 1030 to 1090°C, rough rolling was performed in a temperature range of 910 to 1040°C to produce a rough rolling bar, and a total rolling reduction of 40% or more was applied during rough rolling. After rough rolling, finishing rolling was performed as shown in Table 2 below, and water was cooled to a range of 350 to 480°C at a cooling rate of 3.5 to 5°C/s to prepare a specimen.
- the microstructure, yield strength, impact transition temperature and NDT temperature were evaluated for the specimens in Table 2, and the results are shown in Table 3 below.
- the microstructure was collected from specimens of t/4 to (3*t)/8 areas of each specimen and observed and evaluated using an optical microscope and EBSD, and the yield strength was evaluated by conducting a tensile test on each specimen.
- the impact transition temperature of each specimen was lowered from 0°C to 20°C, and the point at which 50% of the upper absorbed energy was evaluated as the impact transition temperature from the impact test results, and the NDT temperature was t of each specimen.
- Test pieces were taken and evaluated by the DRL-DWT test specified in ASTM E208-06.
- FIG. 1 is a photograph obtained by observing the t/4 portion of the specimen 1 with an optical microscope, and it can be confirmed that the microscopic cyclic ferrite and granular bainite composite structures are provided.
- the specimen 11 since it contains a nickel (Ni) having a content lower than the nickel (Ni) content suggested by the present invention, even when sufficiently fine bainite is formed on the surface, toughness is caused by the low nickel (Ni) content. You can see that it has been done. That is, in the case of the specimen 11, it can be confirmed that the NDT temperature of the t/4 part exceeds -45°C, and the impact transition temperature of the t/4 part exceeds -60°C, so that the desired physical properties are not provided.
- the present invention contains titanium (Ti) and niobium (Nb) having higher contents than the titanium (Ti) and niobium (Nb) contents, toughness deterioration was caused by excessive hardenability and precipitate formation. You can confirm that. That is, it can be confirmed that the specimen 12 also has an NDT temperature of t/4 part exceeding -45°C and an impact transition temperature of t/4 part exceeding -60°C, and thus does not have desired physical properties.
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Abstract
Description
Claims (11)
- 중량%로, C: 0.02~0.07%, Mn: 1.8~2.2%, Ni: 0.7~1.2%, Nb: 0.005~0.02%, Ti: 0.005~0.02%, Cu: 0.1~0.4%, P: 0.01% 이하, S: 0.004% 이하, 나머지 Fe 및 불가피한 불순물을 포함하고, t/4~(3*t)/8 영역(여기서, t는 강재 두께를 의미함, 이하 동일)에서 EBSD로 측정한 15도 이상의 고경계각을 가지는 결정립의 평균 입도가 15㎛ 이하인, 취성균열전파 저항성이 우수한 극후물 강재.
- 제1항에 있어서,t/4 영역에서 채취되는 시험편으로 ASTM E208-06에 규정된 NRL-DWT(Naval Research Laboratory-Drop Weight Test)를 실시하는 경우 NDT(Nil-Ductility Transition) 온도가 -45℃ 이하인, 취성균열전파 저항성이 우수한 극후물 강재.
- 제1항에 있어서,t/4 영역에서 채취되는 시험편의 충격천이 온도가 -60℃ 이하인, 취성균열전파 저항성이 우수한 극후물 강재.
- 제1항에 있어서,t/4 영역에서 채취되는 시험편의 미세조직은 에시큘러 페라이트와 그래뉼러 베이나이트의 복합조직을 포함하고, 제2상으로 도상 마르텐사이트를 더 포함하는, 취성균열전파 저항성이 우수한 극후물 강재.
- 제4항에 있어서서,상기 에시큘러 페라이트는 60~80면적%의 비율로, 상기 그래뉼러 베이나이트는 20~40면적%의 비율로, 상기 도상 마르텐사이트는 10면적% 이하의 비율로 포함되는, 취성균열전파 저항성이 우수한 극후물 강재.
- 제1항에 있어서,상기 강재의 두께는 50~120mm인, 취성균열전파 저항성이 우수한 극후물 강재.
- 제1항에 있어서,상기 강재의 항복강도는 500MPa 이상인, 취성균열전파 저항성이 우수한 극후물 강재.
- 중량%로, C: 0.02~0.07%, Mn: 1.8~2.2%, Ni: 0.7~1.2%, Nb: 0.005~0.02%, Ti: 0.005~0.02%, Cu: 0.1~0.4%, P: 0.01% 이하, S: 0.004% 이하, 나머지 Fe 및 불가피한 불순물을 포함하는 슬라브를 재가열하고,상기 재가열된 슬라브를 조압연하고,50% 이상의 누적압하율로 상기 조압연된 슬라브를 사상압연하고,상기 사상압연된 강재를 냉각하되,상기 사상압연은 700~850℃의 온도범위에서 개시되는, 취성균열전파 저항성이 우수한 극후물 강재의 제조방법.
- 제8항에 있어서,1000~1120℃의 온도범위에서 상기 슬라브를 재가열하는, 취성균열저파 저항성이 우수한 극후물 강재의 제조방법.
- 제8항에 있어서,850~1050℃의 온도범위에서 40% 이상의 누적합하율로 상기 재가열된 슬라브를 조압연하는, 취성균열전파 저항성이 우수한 극후물 강재의 제조방법.
- 제8항에 있어서,3℃/s 이상의 냉각속도로 500℃ 이하의 온도범위까지 상기 사상압연된 강재를 냉각하는, 취성균열전파 저항성이 우수한 극후물 강재의 제조방법.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP19891138.0A EP3889295A4 (en) | 2018-11-30 | 2019-11-29 | ULTRA THICK STEEL WITH EXCELLENT BRITTLE STRENGTH AND PRODUCTION PROCESSES FOR THEREOF |
| JP2021530867A JP7265009B2 (ja) | 2018-11-30 | 2019-11-29 | 脆性割れ伝播抵抗性に優れた極厚物鋼材及びその製造方法 |
| US17/297,940 US12338515B2 (en) | 2018-11-30 | 2019-11-29 | Ultra-thick steel excellent in brittle crack arrestability and manufacturing method therefor |
| CN201980078893.2A CN113166888A (zh) | 2018-11-30 | 2019-11-29 | 脆性裂纹止裂特性优异的超厚钢及其制造方法 |
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| KR1020180151871A KR102209561B1 (ko) | 2018-11-30 | 2018-11-30 | 취성균열전파 저항성이 우수한 극후물 강재 및 그 제조방법 |
| KR10-2018-0151871 | 2018-11-30 |
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| EP (1) | EP3889295A4 (ko) |
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| CN116113721A (zh) * | 2020-08-25 | 2023-05-12 | 浦项股份有限公司 | 表面部nrl-dwt性能优异的结构用超厚钢材及其制造方法 |
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| KR20160079163A (ko) | 2014-12-25 | 2016-07-06 | 주식회사 포스코 | 취성균열전파 저항성이 우수한 고강도 강재 및 그 제조방법 |
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| JP5348386B2 (ja) * | 2008-10-24 | 2013-11-20 | Jfeスチール株式会社 | 低降伏比かつ耐脆性亀裂発生特性に優れた厚肉高張力鋼板およびその製造方法 |
| KR101360737B1 (ko) * | 2009-12-28 | 2014-02-07 | 주식회사 포스코 | 취성 균열 발생 저항성이 우수한 고강도 강판 및 그 제조방법 |
| JP2013221190A (ja) | 2012-04-17 | 2013-10-28 | Nippon Steel & Sumitomo Metal Corp | 脆性亀裂伝播停止性能に優れた高強度厚鋼板 |
| JP5811032B2 (ja) * | 2012-05-23 | 2015-11-11 | 新日鐵住金株式会社 | Lpgタンク用鋼板 |
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| CN107109597B (zh) | 2014-12-24 | 2020-01-31 | Posco公司 | 耐脆性裂纹扩展性优异的高强度钢材及其制造方法 |
| KR101657827B1 (ko) | 2014-12-24 | 2016-09-20 | 주식회사 포스코 | 취성균열전파 저항성이 우수한 구조용 극후물 강재 및 그 제조방법 |
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| KR101726082B1 (ko) | 2015-12-04 | 2017-04-12 | 주식회사 포스코 | 취성균열전파 저항성 및 용접부 취성균열개시 저항성이 우수한 고강도 강재 및 그 제조방법 |
| KR101819356B1 (ko) | 2016-08-08 | 2018-01-17 | 주식회사 포스코 | 취성균열전파 저항성이 우수한 극후물 강재 및 그 제조방법 |
| KR101917456B1 (ko) | 2016-12-22 | 2018-11-09 | 주식회사 포스코 | 표면부 nrl-dwt 물성이 우수한 극후물 강재 및 그 제조방법 |
| KR101908819B1 (ko) | 2016-12-23 | 2018-10-16 | 주식회사 포스코 | 저온에서의 파괴 개시 및 전파 저항성이 우수한 고강도 강재 및 그 제조방법 |
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| KR102209547B1 (ko) * | 2018-12-19 | 2021-01-28 | 주식회사 포스코 | 취성균열개시 저항성이 우수한 구조용 극후물 강재 및 그 제조방법 |
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| CN116113721A (zh) * | 2020-08-25 | 2023-05-12 | 浦项股份有限公司 | 表面部nrl-dwt性能优异的结构用超厚钢材及其制造方法 |
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| WO2020111860A3 (ko) | 2020-08-06 |
| KR102209561B1 (ko) | 2021-01-28 |
| JP2022510936A (ja) | 2022-01-28 |
| US20220025491A1 (en) | 2022-01-27 |
| EP3889295A2 (en) | 2021-10-06 |
| EP3889295A4 (en) | 2022-03-09 |
| JP7265009B2 (ja) | 2023-04-25 |
| US12338515B2 (en) | 2025-06-24 |
| CN113166888A (zh) | 2021-07-23 |
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