EP4455349A1 - Austenitic steel having excellent ultra-low temperature toughness in weld heat-affected zone, and manufacturing method therefor - Google Patents

Austenitic steel having excellent ultra-low temperature toughness in weld heat-affected zone, and manufacturing method therefor Download PDF

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EP4455349A1
EP4455349A1 EP22911856.7A EP22911856A EP4455349A1 EP 4455349 A1 EP4455349 A1 EP 4455349A1 EP 22911856 A EP22911856 A EP 22911856A EP 4455349 A1 EP4455349 A1 EP 4455349A1
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steel
affected zone
weld heat
present disclosure
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German (de)
French (fr)
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EP4455349A4 (en
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Soon-Gi Lee
Sang-Deok Kang
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Posco Holdings Inc
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Posco Co Ltd
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/26Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/002Heat treatment of ferrous alloys containing Cr
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    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
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    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying 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
    • C21D8/0226Hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying 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
    • C21D8/0263Modifying 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
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/24Ferrous alloys, e.g. steel alloys containing chromium with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/28Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/38Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING 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
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/004Dispersions; Precipitations

Definitions

  • the present disclosure relates to an austenitic steel and a manufacturing method therefor, and more particularly, to an austenitic high-manganese steel having excellent ultra-low temperature toughness in a weld heat-affected zone and a manufacturing method therefor.
  • Liquefied gases such as liquefied hydrogen (boiling point: -253°C), liquefied natural gas (LNG, boiling point: -164°C), liquefied oxygen (boiling point: -183°C), and liquefied nitrogen (boiling point: -196°C) need to be stored at ultra-low temperatures. Therefore, in order to store these gases, structures such as pressure vessels made of materials with sufficient toughness and strength at ultra-low temperatures are required.
  • Cr-Ni-based stainless steel alloys such as AISI 304, 9% of Ni steel, or 5000 series aluminum alloys have been used.
  • the alloy cost is high and a design thickness of the structure increases due to low strength, and its use is limited due to poor weldability.
  • the Cr-Ni-based stainless and 9% of nickel (Ni) steel have greatly improved physical properties of aluminum, the Cr-Ni-based stainless and 9% of nickel (Ni) steel contain a large amount of expensive nickel (Ni), which is not preferable from an economic perspective.
  • the present disclosure provides an austenitic steel that has excellent ultra-low temperature toughness in a weld heat-affected zone to be able to be used as a structural material in ultra-low temperature environments such as a liquefied gas storage tank and a liquefied gas transportation facility, and a manufacturing method therefor.
  • an austenitic steel including: by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn] ⁇ 25 and 33.5*[C]-[Mn] ⁇ 18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities, wherein, when a Charpy impact test at -253°C is performed on a weld heat-affected zone, a lateral expansion in the weld heat-affected zone may be 0.32 mm or more.
  • the [C] and [Mn] in the above equation may mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the steel.
  • a room temperature yield strength of the steel may be 270 MPa or more and less than 400 MPa.
  • the weld heat-affected zone may include, as a microstructure, 95 area% or more of austenite and 5 area% or less (excluding 0 area%) of grain boundary carbides.
  • An average grain size of the weld heat-affected zone may be 5 to 200 ⁇ m.
  • An average grain aspect ratio of the weld heat-affected zone may be 1.0 to 5.0.
  • a dislocation density of the steel may be 2.3*10 15 to 3.3*10 15 /mm 2 .
  • a manufacturing method for an austenitic steel including: preparing, a slab including, by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn] ⁇ 25 and 33.5*[C]-[Mn] ⁇ 18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities; providing a hot-rolled steel sheet by heating the slab and then hot-rolling the heated slab; and performing heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in a temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more.
  • the [C] and [Mn] in the above equation may mean a content (w
  • an austenitic steel that has excellent ultra-low temperature toughness in a weld heat-affected zone to be able to be used as a structural material in ultra-low temperature environments, such as a liquefied gas storage tank and a liquefied gas transportation facility, and a manufacturing method therefor.
  • the present disclosure relates to austenitic steel and a manufacturing method therefor, and preferred embodiments of the present disclosure will be described below.
  • Implementation embodiments of the present disclosure may be modified into several forms, and it is not to be interpreted that the scope of the present disclosure is limited to exemplary embodiments described in detail below.
  • the present implementation embodiments are provided to explain the present disclosure in more detail to those skilled in the art to which the present disclosure pertains.
  • An austenitic steel includes: by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn] ⁇ 25 and 33.5*[C] - [Mn] ⁇ 18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities, wherein, when a Charpy impact test at -253°C is performed on a weld heat-affected zone, a lateral expansion in the weld heat-affected zone may be 0.32 mm or more.
  • Manganese is an element that plays an important role in stabilizing austenite. In order to stabilize austenite at ultra-low temperature, it is preferable that 10% or more of manganese (Mn) is contained. When the manganese (Mn) content is less than 10%, metastable phase, epsilon martensite, is formed and is easily transformed into alpha martensite by strain-induced transformation at ultra-low temperature, making it impossible to secure toughness. In order to suppress the formation of the epsilon martensite, there is a method for stabilizing austenite by increasing the carbon (C) content, but in this case, a large amount of carbides may be precipitated and physical properties may rapidly deteriorate. Therefore, the manganese (Mn) content is preferably 10% or more.
  • a preferable manganese (Mn) content may be 15% or more, and a more preferable manganese (Mn) content may be 18% or more.
  • the manganese (Mn) content is preferably 45% or less.
  • a preferable manganese (Mn) content may be 40% or less, and a more preferable manganese (Mn) content may be 35% or less.
  • Carbon (C) Range satisfying 24*[C]+[Mn] ⁇ 25 and 33.5*[C]-[Mn] ⁇ 18
  • Carbon (C) is an element that stabilizes austenite and increases strength.
  • the carbon (C) plays a role in lowering a transformation point Ms or Md from austenite to epsilon or alpha martensite during a cooling process, a processing process, etc. Therefore, carbon (C) is a component that effectively contributes to the stabilization of austenite.
  • the carbon (C) content is insufficient, the stability of austenite is insufficient, so it is impossible to obtain stable austenite at ultra-low temperature, and external stress may easily cause strain-induced transformation into the epsilon or alpha martensite, so it is possible to reduce the toughness of the steel or lower the strength of the steel.
  • the carbon (C) content is excessive, the toughness of the steel may rapidly deteriorate due to carbide precipitation, and the strength of the steel may increase excessively, resulting in reduced processability.
  • the inventors of the present disclosure have conducted in-depth research on the relative behavior between the carbon (C) and manganese (Mn) contents in relation to carbide formation, and as a result, as illustrated in FIG. 1 , and came to the conclusion that determining the relative content relationship between the carbon (C) and manganese (Mn) may effectively stabilize the austenite and effectively control the amount of carbide precipitates.
  • the carbide is formed by the carbon (C), but the carbon (C) does not independently affect the formation of the carbide, but compositely acts with the manganese (Mn) to affect the formation of the carbide.
  • the value of 33.5*[C]-[Mn] (here, [C] and [Mn] mean the content of each component expressed in units of wt%) to 18 or less under the premise that other components meet the range specified in the present disclosure.
  • the carbon (C) is preferably added to satisfy 24*[C]+[Mn] ⁇ 25 and 33.5*[C]-[Mn] ⁇ 18.
  • the lowest limit of the carbon (C) content within the range that satisfies the above-mentioned equation is 0%.
  • Chromium (Cr) is also an austenite stabilizing element. Up to the appropriate amount of chromium added, the austenite is stabilized to improve the low-temperature impact toughness of steel, and the chromium is dissolved in the austenite to play a role in increasing the strength of steel.
  • the chromium (Cr) is also a component that effectively contributes to improving the corrosion resistance of steel. Therefore, the present disclosure adds the chromium (Cr) as an essential component.
  • the preferable lower limit of the chromium (Cr) content may be 1%, and the more preferable lower limit of the chromium (Cr) content may be 2%.
  • the chromium (Cr) is a carbide forming element, and in particular, it may reduce the low-temperature impact toughness of steel by forming carbides at austenite grain boundaries.
  • the amount of chromium (Cr) added exceeds a certain level, the excessive carbides may precipitate in the weld heat-affected zone (HAZ), resulting in poor ultra-low temperature toughness. Therefore, the present disclosure may limit the upper limit of the chromium (Cr) content to 10%.
  • the preferable upper limit of the chromium (Cr) content may be 8%, and the more preferable upper limit of the chromium (Cr) content may be 7%.
  • Ti titanium
  • Nb niobium
  • V vanadium
  • Titanium (Ti) is an element that increases strength through solid solution and precipitation hardening effects, and in particular, an advantageous element that may prevent a deterioration in strength by suppressing grain growth in the weld heat-affected zone by titanium carbon/nitride.
  • the titanium (Ti) is an element that may improve strength due to the precipitation of carbonitride during heat treatment. According to the present disclosure, the titanium (Ti) may be added for this effect. However, when the titanium (Ti) is added excessively, the coarse precipitates or crystals are generated to cause surface cracks during the rolling and deteriorating physical properties of steel, so it is preferable to limit the content to a certain range.
  • the niobium (Nb) is an element that increases strength through solid solution and precipitation hardening effects, and in particular, is an element that may increase recrystallization stop temperature (Tnr) of steel, improve yield strength through grain refinement during the low-temperature rolling, and improve strength through carbonitride precipitation during the heat treatment.
  • the present disclosure may add the niobium (Nb) for this effect.
  • the present disclosure may add the vanadium (V) for this effect.
  • the present disclosure may limit the respective contents of titanium (Ti), niobium (Nb), and vanadium (V) to 0.5% or less.
  • the total content of titanium (Ti), niobium (Nb), and vanadium (V) may be limited to 0.5% or less.
  • the austenitic steel according to an aspect of the present disclosure may contain the balance of iron (Fe) and other inevitable impurities in addition to the above-described components.
  • Fe iron
  • the unintended impurities from raw materials or the surrounding environment may inevitably be mixed in a normal manufacturing process, the unintended impurities may not be completely excluded. Since these impurities are known to those skilled in the art, all of them are not specifically mentioned in this specification. In addition, the additional addition of the effective components in addition to the above-described components is not completely excluded.
  • the austenitic steel according to an aspect of the present disclosure may include austenite of 95 area% or more as a microstructure in terms of securing the desired physical properties.
  • a preferable fraction of the austenite may be 97 area% or more, and may include a case where the fraction of the austenite is close to 100 area%.
  • the fraction of the carbides may be actively suppressed to 5 area% or less to prevent the deterioration in the ultra-low temperature impact toughness.
  • a preferred fraction of carbides may be 3 area% or less.
  • the austenitic steel according to an aspect of the present disclosure contains one or more types selected from the titanium (Ti), niobium (Nb), and vanadium (V), which are carbide generating elements, 0% may be excluded from the lower limit of the fraction of carbides.
  • the method for measuring a fraction of austenite and a fraction of carbides is not particularly limited, and it may be easily confirmed through measurement methods commonly used by those skilled in the art to measure the microstructure and carbide.
  • a dislocation density of the austenitic steel according to an aspect of the present disclosure may satisfy the range of 2.3*10 15 to 3.3*10 15 /mm 2 .
  • the dislocation density of steel may be measured by measuring the strength of a specific surface of steel using X-ray diffraction and then using the Williamson-Hall method, etc.
  • a person skilled in the art to which the present disclosure pertains may measure the dislocation density of steel without any particular technical difficulties. When the dislocation density of steel does not reach a certain level, the suitable strength as a structural material may not be secured. Therefore, the present disclosure may limit the lower limit of the dislocation density of steel to 2.3*10 15 /mm 2 .
  • the present disclosure may limit the upper limit of the dislocation density of the steel to 3.3*10 15 /mm 2 .
  • the room temperature yield strength of the austenitic steel according to an aspect of the present disclosure may satisfy 270 MPa or more and less than 400 MPa.
  • the low-temperature impact toughness decreases, and in particular, when the yield strength of steel used at ultra-low temperature of -253°C as in the present disclosure is excessively high, the possibility of not securing the desired impact toughness increases.
  • it is difficult for commonly used austenitic welding materials to exceed the strength of the base material when the strength of the base material is maintained high, a difference in strength may occur between the weld zone and the base material, which may reduce structural stability.
  • the room temperature yield strength of the austenitic steel according to an aspect of the present disclosure is less than 400 MPa. Meanwhile, when the room temperature yield strength of steel is excessively low, the thickness of the base material may excessively increase to ensure the stability of the structure, and the weight of the structure may excessively increase accordingly, so the austenitic steel according to an aspect of the present disclosure may limit the lower limit of the room temperature yield strength to 270 MPa.
  • the austenitic steel according to an aspect of the present disclosure seeks to secure not only the ultra-low temperature impact toughness of the base material itself, but also the ultra-low temperature impact toughness of the weld heat-affected zone (HAZ). Therefore, the present disclosure controls not only the microstructure of the base material but also the fraction and shape of the microstructure of the weld heat-affected zone to a specific range.
  • the weld heat-affected zone may include 95 area% or more of austenite and 5 area% or less of carbide.
  • the fraction of the austenite included in the weld heat-affected zone may be 97 area% or more, and may include the case where the fraction of the austenite is close to 100 area%.
  • the fraction of carbides contained in the weld heat-affected zone may be limited to 3 area% or less.
  • the austenitic steel according to an aspect of the present disclosure contains one or more types selected from the titanium (Ti), niobium (Nb), and vanadium (V), which are carbide generating elements, 0% may be excluded from the fraction of carbides in the weld heat-affected zone (HAZ).
  • the average grain size of the austenite in the weld heat-affected zone (HAZ) may satisfy the range of 5 to 200 ⁇ m.
  • the austenitic steel according to an aspect of the present disclosure may limit the average austenite grain size in the weld heat-affected zone (HAZ) to 5 ⁇ m or more.
  • the present disclosure may limit the average austenite grain size in the weld heat-affected zone (HAZ) to 200 ⁇ m or less.
  • the present disclosure may limit the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) to a level of 1.0 or more.
  • the present disclosure may limit the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) to a level of 5.0 or less.
  • the lateral expansion value in the weld heat-affected zone (HAZ) of the specimen subjected to the Charpy impact test at -253 ⁇ C may be 0.32mm or more.
  • the inventors of the present disclosure found that plastic deformation characteristics are major factors in securing the safety in the case of the steel applied in the ultra-low temperature environments. That is, after in-depth research, the inventors of the present disclosure found that in the case of the steel that satisfies the composition system proposed by the present disclosure, the lateral expansion value (mm) is a more important factor in securing the safety of the weld zone than the Charpy impact energy value (J) of the weld heat-affected zone (HAZ).
  • the lateral expansion value in the weld heat-affected zone means the average value of the lateral plastic deformation of the specimen subjected to the Charpy impact test at -253°C.
  • FIG. 2 illustrates a photograph of the specimen subjected to the Charpy impact test based on - 253°C. As illustrated in FIG. 2 , an increase amount ( ⁇ X1+ ⁇ X2) of lateral length near the fracture surface may be calculated to calculate the lateral expansion value.
  • the lateral expansion value in the weld heat-affected zone (HAZ) is 0.32 mm or more, it may be determined to have the minimum low-temperature safety required for the ultra-low temperature structure.
  • the Charpy impact energy (J) based on -253°C and the lateral expansion value (mm) of the corresponding specimen generally showed a similar tendency to equation 1 below, and the lateral expansion value was 0.32mm or more. It can be seen that as the larger the lateral expansion value (mm), the better the low-temperature impact toughness it has, and it is more effective that the lateral expansion value is 0.72 to 1.4 mm.
  • a manufacturing method for an austenitic steel may include: preparing, a slab containing, by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn] ⁇ 25 and 33.5*[C] - [Mn] ⁇ 18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V) : 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities; providing a hot-rolled steel sheet by heating the slab and then hot-rolling the heated slab; and performing heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in the corresponding temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more.
  • the [C] and [Mn] in the above equation may mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the slab.
  • a steel slab having a predetermined alloy composition is prepared. Since the steel slab of the present disclosure has the steel composition corresponding to the austenitic steel described above, the description of the alloy composition of the steel slab is replaced with the description of the steel composition of the austenitic steel described above.
  • the thickness of the steel slab is also not particularly limited, and a steel slab having a thickness suitable for manufacturing materials for low or ultra-low temperature structures may be used.
  • the prepared slab may be heated and hot rolled into steel having the desired thickness.
  • the heating temperature and hot rolling conditions of the slab are not particularly limited, but as a non-limiting example, the heating of the slab may be performed in a temperature range of 1000 to 1300°C and the finish rolling may be performed in a temperature range of 800 to 1100°C.
  • the reduction rate during the hot rolling may be applied in an appropriate range depending on the desired plate thickness, and as a non-limiting example, the final thickness of the hot-rolled steel sheet may satisfy a range of 6 mm or more.
  • Heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in the corresponding temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more may be performed.
  • the heat treatment after the heat rolling is performed not only to appropriately control the grain size and shape of the final austenite, but also to remove the internal strain energy present in the steel.
  • the present disclosure may limit the lower limit of the heat treatment temperature to 500°C.
  • the heat treatment temperature is low, the reduction in the dislocation density by heat treatment is not sufficient, and it is difficult to secure the desired strength characteristics due to the insufficient formation of precipitates, so the heat treatment temperature may be limited to 500°C.
  • the preferred lower limit of the heat treatment temperature may be 600°C.
  • the present disclosure may limit the upper limit of the heat treatment temperature to 1000°C.
  • the preferred upper limit of the heat treatment temperature may be 950°C.
  • the heat treatment time is insufficient compared to the thickness of the steel, since it may be insufficient to remove the internal strain energy in the center of the steel, the heat treatment is performed for a time of 1.3t (thickness of hot rolled steel sheet, mm) + 5 minutes or more to sufficiently heat the center of the steel.
  • each specimen was manufactured by applying process conditions shown in Table 2 below.
  • Each steel slab contains iron (Fe) and other inevitable impurities in addition to the alloy components listed in Table 1.
  • Comparative Examples 2 and 4 are cases where heat treatment was not performed.
  • [Table 1] Steel Type Alloy Component (wt%) Mn 24* [C] + [Mn] 33.

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Abstract

According to one aspect of the present invention, an austenitic high-manganese steel having excellent ultra-low temperature toughness in a weld heat-affected zone, and a manufacturing method therefor can be provided.

Description

    [Technical Field]
  • The present disclosure relates to an austenitic steel and a manufacturing method therefor, and more particularly, to an austenitic high-manganese steel having excellent ultra-low temperature toughness in a weld heat-affected zone and a manufacturing method therefor.
  • [Background Art]
  • Liquefied gases such as liquefied hydrogen (boiling point: -253°C), liquefied natural gas (LNG, boiling point: -164°C), liquefied oxygen (boiling point: -183°C), and liquefied nitrogen (boiling point: -196°C) need to be stored at ultra-low temperatures. Therefore, in order to store these gases, structures such as pressure vessels made of materials with sufficient toughness and strength at ultra-low temperatures are required.
  • As materials that can be used at low temperatures in a liquefied gas atmosphere, Cr-Ni-based stainless steel alloys such as AISI 304, 9% of Ni steel, or 5000 series aluminum alloys have been used. However, in the case of the aluminum alloy, the alloy cost is high and a design thickness of the structure increases due to low strength, and its use is limited due to poor weldability. Although the Cr-Ni-based stainless and 9% of nickel (Ni) steel have greatly improved physical properties of aluminum, the Cr-Ni-based stainless and 9% of nickel (Ni) steel contain a large amount of expensive nickel (Ni), which is not preferable from an economic perspective.
  • [Disclosure] [Technical Problem]
  • The present disclosure provides an austenitic steel that has excellent ultra-low temperature toughness in a weld heat-affected zone to be able to be used as a structural material in ultra-low temperature environments such as a liquefied gas storage tank and a liquefied gas transportation facility, and a manufacturing method therefor.
  • The subject of the present disclosure is not limited to the above. A person skilled in the art will have no difficulty understanding the further subject matter of the present disclosure from the general content of this specification.
  • [Technical Solution]
  • In an aspect in the present disclosure, there is provided, an austenitic steel, including: by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C]-[Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities, wherein, when a Charpy impact test at -253°C is performed on a weld heat-affected zone, a lateral expansion in the weld heat-affected zone may be 0.32 mm or more. The [C] and [Mn] in the above equation may mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the steel.
  • A room temperature yield strength of the steel may be 270 MPa or more and less than 400 MPa.
  • The weld heat-affected zone may include, as a microstructure, 95 area% or more of austenite and 5 area% or less (excluding 0 area%) of grain boundary carbides.
  • An average grain size of the weld heat-affected zone may be 5 to 200µm.
  • An average grain aspect ratio of the weld heat-affected zone may be 1.0 to 5.0.
  • A dislocation density of the steel may be 2.3*1015 to 3.3*1015/mm2.
  • In another aspect in the present disclosure, there is provided a manufacturing method for an austenitic steel, including: preparing, a slab including, by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C]-[Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities; providing a hot-rolled steel sheet by heating the slab and then hot-rolling the heated slab; and performing heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in a temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more. The [C] and [Mn] in the above equation may mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the slab.
  • Solutions to the above problems do not enumerate all the features of the present disclosure, and the various features of the present disclosure and the advantages and effects thereof will be understood in more detail with reference to the specific implementation embodiments and embodiments below.
  • [Advantageous Effects]
  • According to an aspect of the present disclosure, it is possible to provide an austenitic steel that has excellent ultra-low temperature toughness in a weld heat-affected zone to be able to be used as a structural material in ultra-low temperature environments, such as a liquefied gas storage tank and a liquefied gas transportation facility, and a manufacturing method therefor.
  • Effects of the present disclosure are not limited to the above matters, and may be interpreted as including technical effects that can be inferred from the details described in this specification.
  • [Brief Description of Drawings]
    • FIG. 1 is a diagram illustrating a correlation between a carbon content of and manganese content of an austenitic steel according to an aspect of the present disclosure.
    • FIG. 2 is a diagram schematically illustrating a method for measuring a lateral expansion value in the weld heat-affected zone of the austenitic steel according to an aspect of the present disclosure.
    [Best Mode]
  • The present disclosure relates to austenitic steel and a manufacturing method therefor, and preferred embodiments of the present disclosure will be described below. Implementation embodiments of the present disclosure may be modified into several forms, and it is not to be interpreted that the scope of the present disclosure is limited to exemplary embodiments described in detail below. The present implementation embodiments are provided to explain the present disclosure in more detail to those skilled in the art to which the present disclosure pertains.
  • Hereinafter, an austenitic steel according to an aspect of the present disclosure will be described in more detail.
  • An austenitic steel according to an aspect of the present disclosure includes: by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C] - [Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities, wherein, when a Charpy impact test at -253°C is performed on a weld heat-affected zone, a lateral expansion in the weld heat-affected zone may be 0.32 mm or more.
  • Hereinafter, a steel composition included in the austenitic steel according to an aspect of the present disclosure will be described in more detail. Hereinafter, unless otherwise specified, % indicating the content of each element is based on weight.
  • Manganese (Mn): 10 to 45%
  • Manganese is an element that plays an important role in stabilizing austenite. In order to stabilize austenite at ultra-low temperature, it is preferable that 10% or more of manganese (Mn) is contained. When the manganese (Mn) content is less than 10%, metastable phase, epsilon martensite, is formed and is easily transformed into alpha martensite by strain-induced transformation at ultra-low temperature, making it impossible to secure toughness. In order to suppress the formation of the epsilon martensite, there is a method for stabilizing austenite by increasing the carbon (C) content, but in this case, a large amount of carbides may be precipitated and physical properties may rapidly deteriorate. Therefore, the manganese (Mn) content is preferably 10% or more. A preferable manganese (Mn) content may be 15% or more, and a more preferable manganese (Mn) content may be 18% or more. When the manganese (Mn) content is excessive, not only can a corrosion rate of steel be reduced, but it is also not preferable from an economic perspective. Therefore, the manganese (Mn) content is preferably 45% or less. A preferable manganese (Mn) content may be 40% or less, and a more preferable manganese (Mn) content may be 35% or less.
  • Carbon (C): Range satisfying 24*[C]+[Mn]≥25 and 33.5*[C]-[Mn]≤18
  • Carbon (C) is an element that stabilizes austenite and increases strength. In particular, the carbon (C) plays a role in lowering a transformation point Ms or Md from austenite to epsilon or alpha martensite during a cooling process, a processing process, etc. Therefore, carbon (C) is a component that effectively contributes to the stabilization of austenite. When the carbon (C) content is insufficient, the stability of austenite is insufficient, so it is impossible to obtain stable austenite at ultra-low temperature, and external stress may easily cause strain-induced transformation into the epsilon or alpha martensite, so it is possible to reduce the toughness of the steel or lower the strength of the steel. On the other hand, when the carbon (C) content is excessive, the toughness of the steel may rapidly deteriorate due to carbide precipitation, and the strength of the steel may increase excessively, resulting in reduced processability.
  • The inventors of the present disclosure have conducted in-depth research on the relative behavior between the carbon (C) and manganese (Mn) contents in relation to carbide formation, and as a result, as illustrated in FIG. 1, and came to the conclusion that determining the relative content relationship between the carbon (C) and manganese (Mn) may effectively stabilize the austenite and effectively control the amount of carbide precipitates. The carbide is formed by the carbon (C), but the carbon (C) does not independently affect the formation of the carbide, but compositely acts with the manganese (Mn) to affect the formation of the carbide.
  • In order to stabilize the austenite, it is preferable to control the value of 24*[C]+[Mn] (here, [C] and [Mn] mean the content of each component expressed in units of wt%) to 25 or more under the premise that other components meet the range specified in the present disclosure. The boundary refers to an inclined left boundary of a parallelogram area illustrated in FIG. 1. When 24*[C]+[Mn] is less than 25, the stability of the austenite decreases and the strain-induced transformation is caused due to impact at ultra-low temperature, so the impact toughness of the steel may decrease. On the other hand, in order to stabilize the austenite, it is preferable to control the value of 33.5*[C]-[Mn] (here, [C] and [Mn] mean the content of each component expressed in units of wt%) to 18 or less under the premise that other components meet the range specified in the present disclosure. When 33.5*[C]-[Mn] exceeds 18, carbides may precipitate due to the excessive addition of carbon (C), which may reduce the low-temperature impact toughness of the steel. Therefore, in the present disclosure, the carbon (C) is preferably added to satisfy 24*[C]+[Mn]≥25 and 33.5*[C]-[Mn]≤18. As can be seen in FIG. 1, the lowest limit of the carbon (C) content within the range that satisfies the above-mentioned equation is 0%.
  • Chrome (Cr): 10% or less (excluding 0%)
  • Chromium (Cr) is also an austenite stabilizing element. Up to the appropriate amount of chromium added, the austenite is stabilized to improve the low-temperature impact toughness of steel, and the chromium is dissolved in the austenite to play a role in increasing the strength of steel. In addition, the chromium (Cr) is also a component that effectively contributes to improving the corrosion resistance of steel. Therefore, the present disclosure adds the chromium (Cr) as an essential component. The preferable lower limit of the chromium (Cr) content may be 1%, and the more preferable lower limit of the chromium (Cr) content may be 2%. However, the chromium (Cr) is a carbide forming element, and in particular, it may reduce the low-temperature impact toughness of steel by forming carbides at austenite grain boundaries. In addition, when the amount of chromium (Cr) added exceeds a certain level, the excessive carbides may precipitate in the weld heat-affected zone (HAZ), resulting in poor ultra-low temperature toughness. Therefore, the present disclosure may limit the upper limit of the chromium (Cr) content to 10%. The preferable upper limit of the chromium (Cr) content may be 8%, and the more preferable upper limit of the chromium (Cr) content may be 7%.
  • One or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%)
  • Titanium (Ti) is an element that increases strength through solid solution and precipitation hardening effects, and in particular, an advantageous element that may prevent a deterioration in strength by suppressing grain growth in the weld heat-affected zone by titanium carbon/nitride. In addition, the titanium (Ti) is an element that may improve strength due to the precipitation of carbonitride during heat treatment. According to the present disclosure, the titanium (Ti) may be added for this effect. However, when the titanium (Ti) is added excessively, the coarse precipitates or crystals are generated to cause surface cracks during the rolling and deteriorating physical properties of steel, so it is preferable to limit the content to a certain range.
  • The niobium (Nb) is an element that increases strength through solid solution and precipitation hardening effects, and in particular, is an element that may increase recrystallization stop temperature (Tnr) of steel, improve yield strength through grain refinement during the low-temperature rolling, and improve strength through carbonitride precipitation during the heat treatment. The present disclosure may add the niobium (Nb) for this effect.
  • Since the vanadium (V) is an element that increases strength through the solid solution and precipitation hardening effects, the present disclosure may add the vanadium (V) for this effect.
  • However, when the titanium (Ti), niobium (Nb), and vanadium (V) are added excessively, the coarse precipitates may be generated to cause a deterioration in the physical properties of steel, and the coarse precipitates or crystals may be generated to cause the surface cracks during the hot rolling, so the present disclosure may limit the respective contents of titanium (Ti), niobium (Nb), and vanadium (V) to 0.5% or less. Preferably, the total content of titanium (Ti), niobium (Nb), and vanadium (V) may be limited to 0.5% or less.
  • The austenitic steel according to an aspect of the present disclosure may contain the balance of iron (Fe) and other inevitable impurities in addition to the above-described components. However, since the unintended impurities from raw materials or the surrounding environment may inevitably be mixed in a normal manufacturing process, the unintended impurities may not be completely excluded. Since these impurities are known to those skilled in the art, all of them are not specifically mentioned in this specification. In addition, the additional addition of the effective components in addition to the above-described components is not completely excluded.
  • The austenitic steel according to an aspect of the present disclosure may include austenite of 95 area% or more as a microstructure in terms of securing the desired physical properties. A preferable fraction of the austenite may be 97 area% or more, and may include a case where the fraction of the austenite is close to 100 area%. Meanwhile, in the austenitic steel according to an aspect of the present disclosure, the fraction of the carbides may be actively suppressed to 5 area% or less to prevent the deterioration in the ultra-low temperature impact toughness. A preferred fraction of carbides may be 3 area% or less. However, since the austenitic steel according to an aspect of the present disclosure contains one or more types selected from the titanium (Ti), niobium (Nb), and vanadium (V), which are carbide generating elements, 0% may be excluded from the lower limit of the fraction of carbides. In the present disclosure, the method for measuring a fraction of austenite and a fraction of carbides is not particularly limited, and it may be easily confirmed through measurement methods commonly used by those skilled in the art to measure the microstructure and carbide.
  • A dislocation density of the austenitic steel according to an aspect of the present disclosure may satisfy the range of 2.3*1015 to 3.3*1015/mm2. The dislocation density of steel may be measured by measuring the strength of a specific surface of steel using X-ray diffraction and then using the Williamson-Hall method, etc. A person skilled in the art to which the present disclosure pertains may measure the dislocation density of steel without any particular technical difficulties. When the dislocation density of steel does not reach a certain level, the suitable strength as a structural material may not be secured. Therefore, the present disclosure may limit the lower limit of the dislocation density of steel to 2.3*1015/mm2. On the other hand, when the dislocation density is excessively high, it is advantageous in terms of securing the strength of steel, but is not preferable in terms of securing the ultra-low temperature toughness, so the present disclosure may limit the upper limit of the dislocation density of the steel to 3.3*1015/mm2.
  • The room temperature yield strength of the austenitic steel according to an aspect of the present disclosure may satisfy 270 MPa or more and less than 400 MPa. As the strength of steel increases, the low-temperature impact toughness decreases, and in particular, when the yield strength of steel used at ultra-low temperature of -253°C as in the present disclosure is excessively high, the possibility of not securing the desired impact toughness increases. In addition, since it is difficult for commonly used austenitic welding materials to exceed the strength of the base material, when the strength of the base material is maintained high, a difference in strength may occur between the weld zone and the base material, which may reduce structural stability. Therefore, it is preferable that the room temperature yield strength of the austenitic steel according to an aspect of the present disclosure is less than 400 MPa. Meanwhile, when the room temperature yield strength of steel is excessively low, the thickness of the base material may excessively increase to ensure the stability of the structure, and the weight of the structure may excessively increase accordingly, so the austenitic steel according to an aspect of the present disclosure may limit the lower limit of the room temperature yield strength to 270 MPa.
  • Since the structure is generally provided by processing and welding the steel material, even if the ultra-low temperature impact toughness of the base material itself is secured, when the ultra-low impact toughness is not secured at the weld zone, the safety of the structure itself may be greatly reduced. Therefore, the austenitic steel according to an aspect of the present disclosure seeks to secure not only the ultra-low temperature impact toughness of the base material itself, but also the ultra-low temperature impact toughness of the weld heat-affected zone (HAZ). Therefore, the present disclosure controls not only the microstructure of the base material but also the fraction and shape of the microstructure of the weld heat-affected zone to a specific range.
  • By using the austenitic steel according to an aspect of the present disclosure as the base material, when welding is performed under normal welding conditions for welding the ultra-low temperature structures using solid arc welding rods, flux cored arc welding wires, TIG welding rods and wires, submerged arc welding wires, flux, etc., the weld heat-affected zone (HAZ) may include 95 area% or more of austenite and 5 area% or less of carbide. As described in relation to the microstructure of the base material described above, the fraction of the austenite included in the weld heat-affected zone (HAZ) may be 97 area% or more, and may include the case where the fraction of the austenite is close to 100 area%. In addition, in order to prevent the ultra-low impact toughness from being lowered in the weld zone, the fraction of carbides contained in the weld heat-affected zone (HAZ) may be limited to 3 area% or less. However, since the austenitic steel according to an aspect of the present disclosure contains one or more types selected from the titanium (Ti), niobium (Nb), and vanadium (V), which are carbide generating elements, 0% may be excluded from the fraction of carbides in the weld heat-affected zone (HAZ).
  • The average grain size of the austenite in the weld heat-affected zone (HAZ) may satisfy the range of 5 to 200µm. When the average grain size of the austenite in the weld heat-affected zone (HAZ) is excessively small, the strength of the weld zone is improved, but the deterioration in the localized ultra-low temperature impact toughness may occur in the weld heat-affected zone (HAZ). Therefore, the austenitic steel according to an aspect of the present disclosure may limit the average austenite grain size in the weld heat-affected zone (HAZ) to 5µm or more. Meanwhile, as the average austenite grain size in the weld heat-affected zone (HAZ) increases, it is advantageous to secure the ultra-low temperature impact toughness of the weld zone, but the deterioration in the localized strength in the weld heat-affected zone (HAZ) may occur. Therefore, the present disclosure may limit the average austenite grain size in the weld heat-affected zone (HAZ) to 200µm or less.
  • In terms of securing the physical properties in the weld heat-affected zone (HAZ), not only the fraction and average grain size of the austenite, but also the average aspect ratio of the austenite grain are influential factors. When the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) is excessively small, it is advantageous in terms of securing the ultra-low impact toughness of the weld heat-affected zone (HAZ), but it is disadvantageous in terms of securing the strength of the weld heat-affected zone (HAZ). Therefore, the present disclosure may limit the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) to a level of 1.0 or more. On the other hand, when the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) is excessively large, it is advantageous in terms of securing the strength of the weld heat-affected zone (HAZ), but it is disadvantageous in terms of securing the ultra-low temperature impact toughness of the weld heat-affected zone (HAZ). Therefore, the present disclosure may limit the average grain size aspect ratio of the austenite present in the weld heat-affected zone (HAZ) to a level of 5.0 or less.
  • When welding was performed under normal welding conditions for welding the ultra-low temperature structure using the austenitic steel as the base material according to an aspect of the present disclosure, the lateral expansion value in the weld heat-affected zone (HAZ) of the specimen subjected to the Charpy impact test at -253µC may be 0.32mm or more.
  • The inventors of the present disclosure found that plastic deformation characteristics are major factors in securing the safety in the case of the steel applied in the ultra-low temperature environments. That is, after in-depth research, the inventors of the present disclosure found that in the case of the steel that satisfies the composition system proposed by the present disclosure, the lateral expansion value (mm) is a more important factor in securing the safety of the weld zone than the Charpy impact energy value (J) of the weld heat-affected zone (HAZ).
  • The lateral expansion value in the weld heat-affected zone (HAZ) means the average value of the lateral plastic deformation of the specimen subjected to the Charpy impact test at -253°C. FIG. 2 illustrates a photograph of the specimen subjected to the Charpy impact test based on - 253°C. As illustrated in FIG. 2, an increase amount (ΔX1+ΔX2) of lateral length near the fracture surface may be calculated to calculate the lateral expansion value. When the lateral expansion value in the weld heat-affected zone (HAZ) is 0.32 mm or more, it may be determined to have the minimum low-temperature safety required for the ultra-low temperature structure.
  • According to the present inventor's research results, it was confirmed that the Charpy impact energy (J) based on -253°C and the lateral expansion value (mm) of the corresponding specimen generally showed a similar tendency to equation 1 below, and the lateral expansion value was 0.32mm or more. It can be seen that as the larger the lateral expansion value (mm), the better the low-temperature impact toughness it has, and it is more effective that the lateral expansion value is 0.72 to 1.4 mm.
  • Lateral expansion value (mm) = 0.0088 * Charpy impact energy value (J) + 0.0893
  • When welding was performed under normal welding conditions for welding the ultra-low temperature structure using the austenitic steel as the base material according to an aspect of the present disclosure, since the lateral expansion value in the weld heat-affected zone (HAZ) of the specimen subjected to the Charpy impact test at -253°C is 0.32mm or more, it is possible to secure the excellent structural safety when the ultra-low temperature structure is manufactured using the corresponding steel.
  • Hereinafter, a manufacturing method for an austenitic steel according to an aspect of the present disclosure will be described in more detail.
  • According to an aspect of the present disclosure, a manufacturing method for an austenitic steel may include: preparing, a slab containing, by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C] - [Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V) : 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities; providing a hot-rolled steel sheet by heating the slab and then hot-rolling the heated slab; and performing heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in the corresponding temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more.
  • The [C] and [Mn] in the above equation may mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the slab.
  • Slab Preparation and Hot Rolling
  • A steel slab having a predetermined alloy composition is prepared. Since the steel slab of the present disclosure has the steel composition corresponding to the austenitic steel described above, the description of the alloy composition of the steel slab is replaced with the description of the steel composition of the austenitic steel described above. The thickness of the steel slab is also not particularly limited, and a steel slab having a thickness suitable for manufacturing materials for low or ultra-low temperature structures may be used.
  • The prepared slab may be heated and hot rolled into steel having the desired thickness. The heating temperature and hot rolling conditions of the slab are not particularly limited, but as a non-limiting example, the heating of the slab may be performed in a temperature range of 1000 to 1300°C and the finish rolling may be performed in a temperature range of 800 to 1100°C. The reduction rate during the hot rolling may be applied in an appropriate range depending on the desired plate thickness, and as a non-limiting example, the final thickness of the hot-rolled steel sheet may satisfy a range of 6 mm or more.
  • Heat Treatment
  • Heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in the corresponding temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more may be performed.
  • The heat treatment after the heat rolling is performed not only to appropriately control the grain size and shape of the final austenite, but also to remove the internal strain energy present in the steel. When the heat treatment temperature does not fall within a certain range, since the internal strain energy may not be sufficiently removed, the present disclosure may limit the lower limit of the heat treatment temperature to 500°C. When the heat treatment temperature is low, the reduction in the dislocation density by heat treatment is not sufficient, and it is difficult to secure the desired strength characteristics due to the insufficient formation of precipitates, so the heat treatment temperature may be limited to 500°C. The preferred lower limit of the heat treatment temperature may be 600°C. Meanwhile, when the heat treatment temperature exceeds a certain range, since the excessive growth of the final tissue may be a problem, the present disclosure may limit the upper limit of the heat treatment temperature to 1000°C. The preferred upper limit of the heat treatment temperature may be 950°C.
  • Meanwhile, when the heat treatment time is insufficient compared to the thickness of the steel, since it may be insufficient to remove the internal strain energy in the center of the steel, the heat treatment is performed for a time of 1.3t (thickness of hot rolled steel sheet, mm) + 5 minutes or more to sufficiently heat the center of the steel.
  • [Mode for Invention]
  • Hereinafter, an austenitic steel and a manufacturing method therefor according to an aspect of the present disclosure will be described in more detail with respect to specific embodiments. It is to be noted that the examples below are only for understanding of the present disclosure and are not intended to specify the scope of the present disclosure. The scope of rights of the present disclosure may be determined by matters stated in claims and matters reasonably inferred therefrom.
  • (Example)
  • After preparing a 250 mm thick steel slab with alloy compositions shown in Table 1 below, each specimen was manufactured by applying process conditions shown in Table 2 below. Each steel slab contains iron (Fe) and other inevitable impurities in addition to the alloy components listed in Table 1. Comparative Examples 2 and 4 are cases where heat treatment was not performed. [Table 1]
    Steel Type Alloy Component (wt%)
    Mn 24* [C] + [Mn] 33. 5* [C] - [Mn] Cr Ti Nb V
    A 24.50 32.90 -12.78 3.25 - 0.02 -
    B 23.20 32.32 -10.47 2.74 - 0.11 -
    C 32.20 37.96 -24.16 1.64 0.03 - -
    D 35.10 41.82 -25.72 2.31 - - 0.42
    E 22.60 29.08 -13.56 3.70 - 0.02 0.31
    F 24.20 32.36 -12.81 3.23 - - -
    G 24.20 32.84 -12.14 2.51 0.85 - -
    H 33.60 39.60 -25.23 11.70 - - -
    I 17.20 23.44 -8.49 0.80 - - -
    J 15.30 44.34 25.24 1.12 - - -
    [Table 2]
    Division Stee l Type Slab Heating Temperatur e (°C) FDT (°C ) Steel Thicknes s (mm) Heat Treatment Temperatur e (°C) Heat Treatmen t Time (Minute)
    Example 1 A 1180 915 12 900 45
    Example 2 B 1180 870 25 860 40
    Example 3 C 1200 921 32 790 52
    Example 4 D 1195 885 32 670 50
    Example 5 E 1200 908 18 902 45
    Comparativ e Example 1 F 1185 923 12 900 45
    Comparativ e Example 2 G 1203 872 25 - -
    Comparativ e Example 3 H 1193 925 35 865 55
    Comparativ e Example 4 I 1200 915 18 - -
    Comparativ e Example 5 J 1205 916 25 800 42
  • The microstructures of each Example and Comparative Example listed in Table 2 were observed using an optical microscope, and the results are shown in Table 3 below. In addition, the dislocation densities of each Example and Comparative Example were measured using X-ray diffraction analysis and the room temperature yield strengths were measured using a tensile tester, and the results were listed in Table 3. Thereafter, the welding was performed for each Example and Comparative Example using normal welding conditions used for welding ultra-low temperature structures, and the results are listed in Table 3. In this case, the optical microscope was used to observe the microstructure of the weld heat-affected zone, and the impact energy for the weld heat-affected zone was measured using a Charpy impact tester at -235°C. In addition, the lateral expansion value was measured at an impact test fracture surface of each specimen, and the results are listed in Table 3. [Table 3]
    Divisi on St ee l Ty pe Base Material Weld Heat-affected Zone
    Microst ructure (area%) Room Temper ature Yield Streng th (MPa) Disloc ation Densit y (*1015 / mm2) γ Fractio n (area%) γ Ave rag e Gra in Siz e (µm ) γ Ave rag e Asp ect Rat io Cha rpy Imp act Ene rgy (J) Later al Expan sion (mm)
    Exampl e 1 A Austeni te about 100% (some Nb carboni trides) 330 2.47 Austeni te about 100% (some Nb carboni trides) 32 1.0 4 134 0.97
    Exampl e 2 B Austeni te about 100% (some Nb carboni trides) 352 2.60 Austeni te about 100% (some Nb carboni trides) 29 1.3 6 118 0.85
    Exampl e 3 C Austeni te 97%, carbide s 3% (some Ti carboni trides) 361 2.68 Austeni te 97%, carbide s 3% (some Ti carboni trides) 23 1.0 5 58 0.48
    Example 4 D Austenite 100%, carbide s 3% (some V carboni trides) 378 3.15 Austenite 96%, carbide s 4% (some V carboni trides) 25 1.11 62 0.50
    Exampl e 5 E Austeni te about 100% (some Nb, V carboni trides) 388 2.31 Austeni te about 100% (some Nb, V carboni trides) 31 1.0 2 141 1.01
    Compar ative Exampl e 1 F Austeni te 100% 265 2.44 Austeni te 100% 43 1.0 4 171 1.28
    Compar ative Exampl e 2 G Rolled materia l crack - - - - - - -
    Compar ative Example 3 H Austeni te 91%, Carbides 9% 384 2.53 Austeni te 89%, Carbides 11% 32 1.1 1 1 0.00
    Compar ative Exampl e 4 I Austeni te 75%, Epsilon martens ite 25% 365 3.10 Austeni te 73%, Epsilon martens ite 27% 52 1.1 3 2 0.01
    Compar ative Exampl e 5 J Austeni te 83%, Carbide s 17% 445 2.90 Austeni te 81%, Carbide s 19% 38 1.0 9 1 0.00
  • As shown in Tables 1 to 3, it can be seen that examples that satisfy the alloy components and process conditions limited by the present disclosure have the desired room temperature yield strength and lateral expansion value in the weld heat-affected zone (HAZ), but Comparative Examples that do not satisfy any one or more of the alloy components or process conditions limited by the present disclosure may not satisfy any one of the desired room temperature yield strength or lateral expansion value in the weld heat-affected zone (HAZ). Meanwhile, in Comparative Example 2, cracks occurred in the rolled material, so the microstructure observation and physical property evaluation were omitted.
  • Although the present disclosure has been described in detail through embodiments above, other types of embodiments are also possible. Therefore, the spirit and scope of the claims set forth below are not limited to the embodiments.

Claims (7)

  1. An austenitic steel, comprising:
    by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C]-[Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V): 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities,
    wherein, when a Charpy impact test at -253°C is performed on a weld heat-affected zone, a lateral expansion in the weld heat-affected zone is 0.32 mm or more, and
    wherein the [C] and [Mn] in the above equation mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the steel.
  2. The austenitic steel of claim 1, wherein a room temperature yield strength of the steel is 270 MPa or more and less than 400 MPa.
  3. The austenitic steel of claim 1, wherein the weld heat-affected zone includes, as a microstructure, 95 area% or more of austenite and 5 area% or less (excluding 0 area%) of grain boundary carbides.
  4. The austenitic steel of claim 1, wherein an average grain size of the weld heat-affected zone is 5 to 200µm.
  5. The austenitic steel of claim 1, wherein an average grain aspect ratio of the weld heat-affected zone is 1.0 to 5.0.
  6. The austenitic steel of claim 1, wherein a dislocation density of the steel is 2.3*1015 to 3.3*1015/mm2.
  7. A manufacturing method for an austenitic steel, comprising:
    preparing, a slab including, by wt%, manganese (Mn): 10 to 45%, carbon (C): range satisfying 24*[C]+[Mn]≥25 and 33.5*[C] - [Mn]≤18, chromium (Cr): 10% or less (excluding 0%), one or more of titanium (Ti), niobium (Nb), and vanadium (V) : 0.5% or less (excluding 0%), and the balance of iron (Fe) and inevitable impurities;
    providing a hot-rolled steel sheet by heating the slab and then hot-rolling the heated slab; and
    performing heat treatment that heats the hot-rolled steel sheet to a temperature range of 500 to 1000°C and maintains the heated hot-rolled steel sheet in a temperature range for 1.3t (hot-rolled steel sheet thickness, mm) + 5 minutes or more,
    wherein the [C] and [Mn] in the above equation mean a content (wt%) of the carbon (C) and manganese (Mn) contained in the slab.
EP22911856.7A 2021-12-21 2022-12-20 AUSTENITIC STEEL WITH EXCELLENT RESISTANCE TO EXTREMELY LOW TEMPERATURES IN HEAT-EXPOSED WELDING ZONE AND MANUFACTURING METHOD FOR IT Pending EP4455349A4 (en)

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JP6693217B2 (en) * 2015-04-02 2020-05-13 日本製鉄株式会社 High Mn steel for cryogenic temperatures
US11078555B2 (en) * 2016-03-01 2021-08-03 Tata Steel Nederland Technology B.V. Austenitic, low-density, high-strength steel strip or sheet having a high ductility, method for producing said steel and use thereof
WO2017203313A1 (en) * 2016-05-24 2017-11-30 Arcelormittal Method for the manufacture of a recovered steel sheet having an austenitic matrix
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