Classifications

• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
  • C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
• • C—CHEMISTRY; METALLURGY
  • 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
• • 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
  • C21D6/005—Heat treatment of ferrous alloys containing Mn
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
• • C—CHEMISTRY; METALLURGY
  • C21—METALLURGY OF IRON
  • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
  • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
  • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
  • C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
  • C21D8/0226—Hot rolling
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
  • C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C13/00—Details of vessels or of the filling or discharging of vessels
  • F17C13/08—Mounting arrangements for vessels
• • 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
  • C21D2201/00—Treatment for obtaining particular effects
  • C21D2201/05—Grain orientation
• • 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
  • C21D2211/001—Austenite
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2203/00—Vessel construction, in particular walls or details thereof
  • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
  • F17C2203/0634—Materials for walls or layers thereof
  • F17C2203/0636—Metals
  • F17C2203/0639—Steels
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2203/00—Vessel construction, in particular walls or details thereof
  • F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
  • F17C2203/0634—Materials for walls or layers thereof
  • F17C2203/0636—Metals
  • F17C2203/0648—Alloys or compositions of metals
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2221/00—Handled fluid, in particular type of fluid
  • F17C2221/03—Mixtures
  • F17C2221/032—Hydrocarbons
  • F17C2221/033—Methane, e.g. natural gas, CNG, LNG, GNL, GNC, PLNG
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
  • F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
  • F17C2223/0146—Two-phase
  • F17C2223/0153—Liquefied gas, e.g. LPG, GPL
  • F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
• • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  • F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
  • F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
  • F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
  • F17C2223/03—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the pressure level
  • F17C2223/033—Small pressure, e.g. for liquefied gas

Definitions

• the present invention relates to a steel material suitable for serving as a structural steel, such as a liquefied gas storage tank, used in an ultra-low temperature environment, and a production method therefor.
• the present invention also relates to a tank that uses this steel material.
• the steel plate In order to use a hot rolled steel plate as a material for a liquefied gas storage structure, the steel plate is required to have high strength and excellent low-temperature toughness since the service environment involves a very low temperature. For example, when a hot rolled steel plate is to be used in a storage of a liquefied natural gas, excellent toughness must be secured at a boiling point of the liquefied natural gas, -164°C, or lower. If the low-temperature toughness of the steel material is poor, the soundness as an ultra-low temperature storage structure may not be able to be maintained, and thus the steel material applied thereto is strongly required to have improved low-temperature toughness. In the description below, temperatures including an ultra-low temperature range of - 164°C or lower are generally referred to as "low temperature".
• austenite stainless steel in which austenite, which is not brittle at low temperature, constitutes the steel plate microstructure, 9% Ni steel, and 5000-series aluminum alloys have been used.
• austenite which is not brittle at low temperature, constitutes the steel plate microstructure
• Ni steel 9% Ni steel
• 5000-series aluminum alloys have been used.
• Patent Literature 1 has proposed, as a novel steel material that replaces existing low-temperature steel, a high-Mn steel that contains a large amount of a relatively inexpensive austenite-stabilizing element, Mn, to be used as a structural steel for a low-temperature environment.
• Patent Literature 1 proposes a technology of obtaining low-temperature toughness in a weld heat affected zone by controlling the carbide area fraction to 5% or less, etc.
• the cooling rate of the welded heat affected zone is limited to 10°C/s or more from the viewpoint of suppressing carbides.
• the steel plate When a steel plate having a thickness of less than 10 mm is cooled at 10°C/s or more, the steel plate is likely to undergo warping and strain, and this requires additional steps such as shape correction, and degrades the productivity.
• the low-temperature toughness in the rolling width direction (C direction) tends to be inferior to the low-temperature toughness in the rolling direction (L direction); however, Patent Literature 1 does not examine the low-temperature toughness in the C direction.
• a liquefied gas storage structure for example, a liquefied natural gas storage tank
• a tank Since inner pressure by the liquefied natural gas is applied to the inner wall of the liquefied gas storage tank (hereinafter may be referred to as a tank), tensile stress occurs in the tank-constituting steel materials not only in the rolling direction (L direction) and the plate width direction (C direction) but also in all directions inside the steel plate plane (hereinafter, these directions may be referred to as "all directions"). Furthermore, tensile stress in the L direction and the C direction occurs also in the weld zones of the tank.
• the base material (base material portion) and the weld zones must have properties that can withstand the load caused by the tensile stress in all directions, in particular, in the L direction and the C direction.
• all directions refer to all directions including directions perpendicular to the rolling direction and parallel to the rolling direction.
• a steel material to be used in the aforementioned usage is also known to exhibit toughness degradation known as strain aging embrittlement after plastic deformation that occurs not only at the material preparation stage but also during working and unintended accidents.
• the present invention has been made in view of the issues described above, and an object thereof is to provide a steel material having excellent low-temperature toughness and a production method therefor, and a tank.
• welded heat affected zone refers to a coarse grain heat affected zone (CGHAZ) where degradation of toughness occurs in general steel material.
• CGHAZ coarse grain heat affected zone
• excellent low-temperature toughness means that, in a steel material, the Charpy impact absorbed energy (vE -196 ) at -196°C at a 1/2 plate thickness position is 41 J or more in all directions. Usually, the Charpy impact absorbed energy in the C direction is the lowest compared to those in the L direction and the Z direction (plate thickness direction). Thus, in the present invention, the case in which the absorbed energy (vE -196 ) in the C direction is at least 41 J is considered as having "excellent low-temperature toughness".
• this "41 J” is a proposed spec for the absorbed energy at -196°C in the L direction of a high-Mn steel drafted as of 2019 by International Association of Classification Societies (IACS), and 27 J is being proposed as the absorbed energy in the C direction.
• the spec in the L direction can also be satisfied in the C-direction Charpy impact test.
• austenite steel materials for example, high-Mn steel materials
• the inventors of the present invention have focused on austenite steel materials (for example, high-Mn steel materials) and conducted extensive studies on the chemical composition, the microstructure, and the production method of the steel materials (steel plates), and various factors that determine the properties of a weld zone obtained by welding the steel material.
• austenite steel materials for example, high-Mn steel materials
• the production method of the steel materials steel plates
• the present invention can provide a steel material having excellent low-temperature toughness, and a production method therefor.
• the steel material of the present invention is suitable for use as a material of a steel structure (such as a liquefied gas storage tank) used in a low-temperature environment, and thus a tank having excellent low-temperature toughness in a base material and a welded heat affected zone after welding can be provided.
• a steel structure such as a liquefied gas storage tank
• the present invention can significantly contribute to improving the soundness and lifetime of the steel structure, and offers a prominent industrial advantage.
• the production method of the present invention does not cause productivity degradation or increase the production cost, a production method with significant economic advantages can be provided.
• an austenite steel material for example, a high-Mn steel material
• a high-Mn steel material is available as an inexpensive steel material having excellent low-temperature toughness.
• the tank inner wall and weld zones are required to have properties that can withstand the inner pressure of the gas to be stored, in particular, properties that can withstand the load caused by tensile stress acting not only in the L direction and the C direction but also in all directions.
• a high-Mn steel material (this means a steel plate having a Mn content of 20.0 to 40.0 mass% here) is an austenite steel material, basically, brittle fractures do not occur, and most fractures are ductile fractures.
• an ordinary steel (this means a low-carbon steel plate having a BCC crystal structure at room temperature)
• ductile fracture is irrelevant to the texture, and the shelf energy (maximum absorbed energy) of the ordinary steel is 200 J or more and may even exceed 300 J depending on the conditions.
• the shelf energy (maximum absorbed energy) of the ordinary steel is 200 J or more and may even exceed 300 J depending on the conditions.
• the inner pressure of the liquefied natural gas are applied to the inner wall and the weld zones of the tank in the L direction, the C direction, and all directions inside the inner surfaces (inner wall) of all steel materials constituting the tank; thus, it is necessary that a sufficient toughness value be obtained with respect to all directions.
• a rolled steel material is known to exhibit the lowest toughness when a Charpy impact test specimen is taken in the C direction with respect to the rolling direction. Thus, it is critical that the toughness value of the C-direction Charpy impact test be improved.
• C direction refers to a direction perpendicular to the rolling direction (L direction).
• C-direction Charpy impact test refers to the case in which the longitudinal direction of the Charpy impact test specimen is parallel to the C direction and the notch faces in the rolling direction.
• rolling direction refers to the rolling direction with the largest total rolling reduction amount among various rolling directions.
• the inventors of the present invention have then further investigated the cause thereof, and have newly found that such a difference in absorbed energy is attributable to the rolling texture (a texture formed by rolling), in other words, the relationship between ductile fractures and the texture.
• the relationship between ductile fractures and the texture will now be described.
• the direction in which the Charpy test specimen is impacted in the Charpy impact test has been focused.
• the direction of impact is studied for an L-direction Charpy test specimen (here, the notch faces in the C direction) taken from a steel plate in such a way that the longitudinal direction of the Charpy test specimen is the rolling direction, and a C-direction Charpy test specimen (here, the notch faces in the L direction) taken from a steel plate in such a way that the longitudinal direction of the Charpy test specimen is perpendicular to the rolling direction.
• the higher the (110) texture the lower the toughness.
• the absorbed energy cannot be predicted from the texture; thus, although the reason is not exactly clear, the (110) [001] texture is considered to have some influence as described below.
• the (110) [001] texture is considered to have some influence as described below.
• the (100) faces align in the C direction and the (110) faces align in the L direction.
• JIS Japanese Industrial Standards
• the C-direction Charpy impact absorbed energy is specified as 27 J or more, and even such a low value is acceptable.
• an absorbed energy comparable to that in the L direction is preferably obtained in the C direction also.
• the base material does not undergo transformation when heated; thus, the texture of a weld zone obtained by welding the austenite steel material is almost the same as the base material, in other words, remains unchanged. Thus, it is critical that the texture be elaborately controlled during the production of an austenite steel material that serves as the base material.
• a (110) [001] texture which is easily formed during typical rolling, and a different texture in which another orientation is developed by cross rolling that involves rotating the workpiece by 90 degrees are mixed as equally as possible so as to decrease the strength of the (110)[001] texture (in other words, preclude development of the (110) [001] texture).
• the (110) face has the smallest surface atomic density, and the surface with the smallest surface atomic density is the weakest bonding surface. In a ductile fracture, such a weakest bonding surface is prone to breaking, and thus the absorbed energy is considered to be low.
• the Charpy absorbed energy in the L direction and the C direction can be equalized.
• the FCC structure accounts for 95% or more of the microstructure in terms of area fraction at normal pressure, the (110)[001] texture strength at the 1/2 plate thickness position is less than 10.0, the hardness at the 1/2 plate thickness position is less than 300 HV, and the Charpy impact absorbed energy in the C direction at -196°C at the 1/2 plate thickness position is 41 J or more.
• the Charpy impact absorbed energy in the C direction at - 196°C can be 41 J or more after strain aging and in a coarse grain heat affected zone caused by welding.
• the microstructure can have a cleanliness for sulfide inclusions of less than 1.0%.
• FCC structure accounts for 95% or more in terms of area fraction
• the "microstructure at normal pressure” means a microstructure in the temperature range of 1300°C to -273°C at a pressure of 1 atm.
• the FCC accounts for 95% or more of the microstructure in terms of area fraction in the temperature range of 1300°C or lower (for example, 1250°C).
• the base phase of the steel material is required to have a face-centered cubic (FCC) crystal structure.
• the "base phase is austenite” means that the austenite phase accounts for 95% or more of the entire microstructure in terms of area fraction.
• the austenite phase preferably accounts for 97% or more.
• the balance other than the austenite phase is a ferrite phase and/or a martensite phase.
• the total area fraction of the phases constituting the balance other than the austenite phase is preferably 5% or less.
• the area fraction of the austenite etc. can be measured by the method described in Examples below.
• the present invention it is critical that hot rolling be performed under appropriate conditions in order to improve the low temperature toughness of the steel material (base material) and the welded heat affected zones.
• the (110)[001] texture strength in the microstructure can be decreased, and Charpy absorbed energy in the C direction and the L direction can be equalized.
• the (110) [001] texture strength in the microstructure at the 1/2 plate thickness position is 10.0 or more, cracks readily propagate. As a result, the absorbed energy decreases.
• the (110) [001] texture strength is to be less than 10.0.
• the (110) [001] texture strength is 9.0 or less. More preferably, the (110) [001] texture strength is 6.0 or less.
• the (110)[001] texture strength in the microstructure at the 1/2 plate thickness position is preferably 1.0 or more otherwise the absorbed energy decreases in the L direction. More preferably, the (110)[001] texture strength is 4.0 or more.
• the hardness at the 1/2 plate thickness position is 300 HV or more, the ductility and the absorbed energy decrease.
• the hardness is to be less than 300 HV.
• the hardness is 280 HV or less. More preferably, the hardness is 260 HV or less.
• the hardness at the 1/2 plate thickness position is preferably 200 HV or more otherwise the strength of the steel material decreases. More preferably, the hardness is 220 HV or more.
• the cleanliness for sulfide inclusions in the microstructure at the 1/2 plate thickness position is 1.0% or more, fracture initiates from sulfide inclusions As a result, the absorbed energy may decrease.
• the cleanliness for sulfide inclusions is preferably less than 1.0%. More preferably, the cleanliness for sulfide inclusions is 0.8% or less. Yet more preferably, the cleanliness for sulfide inclusions is 0.6% or less. Although the lower limit of the cleanliness is not particularly limited, 0.1% or more is preferable from the production cost viewpoint.
• the cleanliness is calculated from formula (2) below.
• d n / p ⁇ f ⁇ 100
• p the total number of grating points in a visual field
• f the number of visual fields
• n the number of grating point centers occupied by inclusions in f visual fields.
• the cleanliness is a value obtained by calculating the area percentage occupied by the sulfide inclusions at the 1/2 plate thickness position of the steel material, and indicates the sulfide inclusions in the C direction. Examples of the sulfide inclusions include MnS.
• the aforementioned (110)[001] texture strength: less than 10.0, hardness: less than 300 HV, and cleanliness for sulfide inclusions: less than 1.0% can be realized by performing hot rolling under the conditions described below.
• the aforementioned texture strength, hardness, and cleanliness for sulfide inclusions can be measured by the methods described in Examples below.
• the steel material of the present invention having the aforementioned microstructure has excellent low temperature toughness.
• the Charpy impact absorbed energy at -196°C is measured not only on the steel material (base material) having the aforementioned microstructure but also after strain aging and in a welded heat affected zone.
• an absorbed energy (vE -196 ) of 41 J or more can be realized at the 1/2 plate thickness position of the steel material in all directions including the C direction and the L direction. In this manner, even in a weld zone where the steel material of the present invention is welded, an absorbed energy (vE -196 ) of 41 J or more can be realized in the C direction of the coarse grain heat affected zone.
• an absorbed energy (vE -196 ) of 41 J or more can be realized in the C direction after strain aging that involves applying a pre-strain and an aging process to the steel material of the present invention under designated conditions (for example, the conditions described in Examples).
• the welding conditions such as a preferable heat input etc., are the same as the preferable welding conditions for a tank described below, and the description therefor is omitted here.
• an absorbed energy (vE -196 ) of 41 J or more can be further effectively obtained also in the C direction in which a lower value is generally exhibited.
• the base material and the weld zone have the same chemical composition and microstructure (however, the austenite grain size in the weld zone is larger).
• an austenite steel material and a steel slab used in producing the austenite steel material have the aforementioned chemical composition.
• the chemical composition of the austenite steel material of the present invention and the reasons for limitations will now be described. Unless otherwise noted, the notation “%” regarding the chemical composition means “mass%”.
• Carbon (C) is an inexpensive austenite-stabilizing element and is a critical element for obtaining austenite.
• the C content is preferably 0.100% or more.
• Cr carbides are excessively formed, and the low-temperature toughness may be degraded.
• the C content is preferably 0.100% or more and 0.700% or less.
• the C content is more preferably 0.200% or more and more preferably 0.600% or less.
• the C content is yet more preferably 0.250% or more and yet more preferably 0.550% or less.
• Si 0.05% or more and 1.00% or less
• the Si acts as a deoxidizing agent, is necessary for steel making, and has an effect of strengthening the steel material through solid-solution strengthening as a solute in the steel.
• the Si content is preferably 0.05% or more. Meanwhile, at a Si content exceeding 1.00%, a thermal stress increases excessively, and the low-temperature toughness may be degraded.
• the Si content is preferably 0.05% or more and 1.00% or less.
• the Si content is more preferably 0.07% or more and more preferably 0.80% or less.
• the Si content is yet more preferably 0.10% or more and yet more preferably 0.60% or less.
• Mn 20.0% or more and 40.0% or less
• Mn is a relatively inexpensive austenite-stabilizing element.
• Mn is a critical element for achieving both strength and low-temperature toughness.
• the Mn content is preferably 20.0% or more.
• the low-temperature toughness may be degraded.
• weldability and cutting performance may be degraded.
• segregation and occurrence of stress corrosion cracking are accelerated.
• the Mn content is preferably 20.0% or more and 40.0% or less.
• the Mn content is more preferably 23.0% or more and yet more preferably 24.0% or more.
• the Mn content is more preferably 35.0% or less and yet more preferably 30.0% or less.
• the upper limit is 0.030%, and the P content is preferably decreased as much as feasibly possible.
• the P content is 0.030% or less.
• the P content is preferably 0.002% or more.
• the P content is more preferably 0.005% or more and yet more preferably 0.010% or more.
• the P content is more preferably 0.028% or less and yet more preferably 0.024% or less.
• the S content is 0.0050% or less.
• the S content is more preferably 0.0045% or less and yet more preferably 0.0040% or less. Excessively decreasing the S content increases the refining cost and brings about economic disadvantages; thus, the S content is preferably 0.0010% or more. More preferably, the S content is 0.0012% or more.
• the Al acts as a deoxidizing agent, and is the most versatile element used in deoxidizing process of the steel making for plate material. Moreover, the yield strength and local elongation during the tensile test are improved.
• the Al content is preferably 0.01% or more. Meanwhile, at an Al content exceeding 5.00%, a large amount of inclusions are formed and degrade the low-temperature toughness; thus, the Al content is 5.00% or less.
• the Al content is more preferably 0.01% or more and yet more preferably 0.02% or more.
• the Al content is more preferably 4.00% or less and yet more preferably 3.50% or less.
• the Cr content is preferably 0.5% or more.
• the Cr content is preferably 0.5% or more, more preferably 1.0% or more, and yet more preferably 1.2% or more.
• the Cr content is more preferably 6.7% or less and yet more preferably 6.5% or less.
• the Cr content is further more preferably 2.0% or more and 6.0% or less.
• N is an austenite-stabilizing element and is an element effective for improving the low-temperature toughness.
• the N content is preferably 0.0050% or more.
• the N content is preferably 0.0500% or less.
• the N content is preferably 0.0050% or more, more preferably 0.0060% or more, and yet more preferably 0.0070% or more.
• the N content is more preferably 0.0400% or less and yet more preferably 0.0300% or less.
• the O content is in the range of 0.0050% or less.
• the O content is preferably 0.0045% or less, more preferably 0.0040% or less, and yet more preferably 0.0035% or less.
• the O content is preferably 0.0010% or more. More preferably, the O content is 0.0012% or more.
• Ti and Nb form high melting-point carbonitrides in the steel, and thus degrade the low-temperature toughness.
• Ti and Nb are incidental impurities mixed in the raw materials etc., and are usually mixed in amounts of Ti: 0.005% or more and 0.010% or less and Nb: 0.005% or more and 0.010% or less.
• incidental mixing of Ti and Nb must be avoided through the steel making technique described below, and the Ti and Nb contents must be suppressed to less than 0.005% respectively.
• the Ti and Nb contents are 0.003% or less respectively.
• the Ti and Nb contents may be 0%. More preferably, the Ti and Nb contents are 0.001% or more respectively.
• Ca, Mg, and rare earth metals are elements useful in controlling the morphology of inclusions.
• Controlling the morphology of inclusions refers to changing elongated sulfide inclusions into spheroidized inclusions.
• the ductility, toughness, and sulfide stress corrosion cracking resistance are improved by controlling the morphology of the inclusions.
• the Ca and Mg contents are preferably 0.0005% or more respectively, and the REM content is preferably 0.0010% or more. Meanwhile, when any of these elements is contained in a large amount, the amount of non-metallic inclusions increases, and the ductility, toughness, and sulfide stress corrosion cracking resistance are degraded. This is also economically disadvantageous.
• the amount thereof is preferably 0.0100% or less respectively, and when REM is to be contained, the amount thereof is preferably 0.0200% or less.
• the Ca content is 0.0005% or more, the Mg content is 0.0005% or more, and the REM content is 0.0010% or more. More preferably, the Ca content is 0.0010% or more and 0.0080% or less, the Mg content is 0.0010% or more and 0.0080% or less, and the REM content is 0.0020% or more and 0.0150% or less. Still more preferably, the Ca content is 0.0050% or less and the Mg content is 0.0050% or less.
• the balance other than the aforementioned composition is iron (Fe) and incidental impurities.
• the incidental impurities include H and B, and such incidental impurities are acceptable as long as the total content thereof is 0.01% or less.
• the basic chemical composition is preferably composed of the aforementioned elements.
• the properties targeted by the present invention can be obtained by this basic chemical composition.
• following elements can be contained as necessary in addition to the aforementioned elements.
• Cu and Ni are elements that not only strengthen the steel material by solid-solution strengthening, but also improve dislocation mobility and low-temperature toughness.
• the Cu and Ni contents are preferably 0.01% or more respectively. Meanwhile, at a Cu content and a Ni content exceeding 1.0%, the surface quality is degraded upon rolling, and the production cost is boosted up.
• the contents thereof are preferably 1.0% or less respectively.
• the contents are more preferably 0.03% or more and more preferably 0.7% or less.
• the contents are further preferably 0.5% or less.
• Mo 2.0% or less
• V 2.0% or less
• W 2.0% or less
• Mo, V, and W contribute to stabilizing austenite and improving the base material strength.
• the Mo, V, and W contents are preferably 0.001% or more respectively.
• the contents thereof are preferably 2.0% or less respectively.
• the contents are more preferably 0.003% or more and more preferably 1.7% or less.
• the contents are further preferably 1.5% or less.
• the "steel material (austenite steel material)" refers to a steel plate having a plate thickness of 6 mm or more. From the view point of using the steel material for a structural steel plate to be used in an ultra-low temperature environment, the plate thickness is preferably more than 9 mm and more preferably 12 mm or more. The upper limit of the plate thickness is not particularly limited, and the thickness may be arbitrary but is preferably 40 mm or less.
• the steel material (austenite steel material) of the present invention can be made by a known steel making method that processes a molten metal having the aforementioned chemical composition in a converter, an electric furnace, or the like. Secondary refining may be performed in a vacuum degassing furnace.
• a known casting method such as a continuous casting method or an ingot making and slabbing method may be performed to produce a steel material such as a slab of a particular size.
• a steel slab be heated to a temperature range of 1100°C or higher and 1300°C or lower, subjected to particular cross rolling, and hot-rolled under conditions that the rolling reduction of the finish rolling final pass is 30% or less and the finish rolling delivery temperature is 750°C or higher.
• the temperature control here is on the basis of the surface temperature of the steel in process.
• the notation "°C” indicates the surface temperature of the steel slab or the steel plate unless otherwise noted.
• the surface temperature can be measured by, for example, a radiation thermometer.
• the temperature of the plate thickness center position of a slab or a steel plate can be determined by measurement by attaching a thermocouple to the plate thickness center of the steel plate, or by calculating the temperature distribution in the steel plate cross section by heat-transfer analysis and determining the result according to the surface temperature of the steel plate.
• Steel slab heating temperature 1100°C or higher and 1300°C or lower
• the heating temperature of the steel slab for hot rolling is set to 1100°C or higher.
• the heating temperature is 1130°C or higher and 1270°C or lower.
• Cross rolling ratio calculated from formula (1): 20 or less
• Cross rolling ratio reduction ratio in rolling direction / reduction ratio in direction perpendicular to rolling direction
• the reduction ratio in rolling direction refers to the reduction ratio in the rolling direction relative to the total rolling reduction.
• the “ reduction ratio in direction perpendicular to rolling direction” refers to the reduction ratio in a direction perpendicular to the rolling direction relative to the total rolling reduction.
• reduction ratio in rolling direction/ reduction ratio in direction perpendicular to rolling direction refers to the reduction ratio in the rolling direction relative to the reduction ratio in a direction perpendicular to the rolling direction.
• the (110) [001] texture is likely to develop.
• the extent of the (110)[001] texture is decreased, and the strength of the (110) [001] texture can be decreased.
• the cross rolling ratio calculated from formula (1) is to be 20 or less.
• cross rolling ratio is 20 or less so as to decrease the area fraction of the sulfide inclusions in the C direction.
• the cross rolling ratio is preferably 18 or less and more preferably 15 or less.
• the (110)[001] texture develops by repeating rolling in the same direction, it is preferable for homogenization of the texture to alternate rolling in the rolling direction and rolling in a direction perpendicular to the rolling direction.
• the rolling direction alternation is repeated twice or more.
• the rolling direction alternation is performed three times or less.
• the rolling reduction of the finish rolling final pass is 30% or less.
• the rolling reduction is preferably less than 25% and more preferably 20% or less.
• the finish rolling delivery temperature is 750°C or higher.
• the finish rolling delivery temperature is preferably 780°C or higher and more preferably 800°C or higher.
• the upper limit of the finish rolling delivery temperature is not particularly limited; however, from the viewpoint of securing the strength, the finish rolling delivery temperature is preferably 950°C or lower and more preferably 920°C or lower.
• the lower limit of the rolling reduction of the finish rolling final pass is not particularly limited, from the viewpoint of securing the strength, the rolling reduction of the finish rolling final pass is preferably 5% or more and more preferably 10% or more.
• the conditions for cross rolling are preferably controlled as below.
• the rolling start temperature is preferably 1100 to 1250°C. At a temperature lower than 1100°C, the rolling temperature decreases to lower than 780°C, and the texture may develop excessively. At a temperature higher than 1250°C, the texture may remain unchanged.
• the rolling temperature (temperature during rolling) is preferably 780 to 1250°C. At a temperature lower than 780°C, the texture may develop excessively. At a temperature higher than 1250°C, the texture may remain unchanged.
• the rolling reduction amount in the temperature range of 780 to 1250°C is preferably 60 to 98%. At a rolling reduction amount less than 60%, the texture may remain unchanged. At a rolling reduction amount exceeding 98%, the texture may develop excessively.
• the rolling reduction amount indicates the total rolling reduction in the temperature range of 780 to 1250°C.
• cooling is performed.
• the cooling conditions are not particularly specified. Cooling is preferably performed from a temperature equal to or higher than (hot rolling delivery temperature - 100°C) to a temperature equal to or lower than 600°C at an average cooling rate of 1.0°C/s or more. In this manner, carbide formation and grain boundary segregation of P are suppressed, and the properties of the steel material are further improved.
• the "hot rolling delivery temperature” refers to the finish rolling delivery temperature.
• a tank of the present invention is constructed by welding the aforementioned steel material. As described in the finding d above, in the steel material of the present invention, the microstructure before welding is maintained even after welding. Thus, the chemical composition and microstructure of the base material of the tank of the present invention are the same as the aforementioned steel material (austenite steel material).
• a tank having a Charpy impact absorbed energy of 41 J or more at -196°C at the 1/2 plate thickness position of the base material can be obtained by specifying the chemical composition and microstructure of the base material (steel material) as described above.
• the Charpy impact absorbed energy at -196°C can be controlled to 41 J or more.
• the Charpy impact absorbed energy at -196°C after strain aging can be controlled to 41 J or more.
• the tank of the present invention has the aforementioned properties, the tank can be used as, for example, a liquefied gas storage tank to be used in an ultra-low temperature environment.
• the tank of the present invention is constructed by welding the aforementioned steel material.
• the method for producing a steel material (austenite steel material) used is already described above, and thus the description therefor is skipped.
• preferable welding conditions are described.
• the type of welding is preferably gas metal arc welding.
• the heat input range is preferably 3.0 kJ/mm or less. More preferably, the heat input range is 0.5 kJ/mm or more. When such a heat input range is satisfied, the aforementioned properties can be satisfied.
• the average cooling rate in the temperature range of 500 to 800°C is preferably 10°C/s or more. When the average cooling rate in this temperature range is less than 10°C/s, carbides are formed, and the absorbed energy is decreased.
• the Charpy impact absorbed energy can be equalized in all directions of the steel material, in particular, the L direction and the C direction, and thus the orientation dependence of the impact toughness of the steel material (base material) and weld zones can be decreased. As a result, the reliability of the material is improved.
• Steel slabs having chemical compositions shown Table 1 were prepared by a converter-ladle refining-continuous casting method.
• "-" means that the corresponding composition was not intentionally added, and includes the case where the content was zero (0%) and the case where the corresponding composition was incidentally contained.
• each of the obtained steel slabs was hot-rolled under the conditions shown Table 2 and cooled to prepare a steel material (steel plate) having a plate thickness of 6 to 40 mm.
• the cross rolling was appropriately controlled so that the temperature during rolling was 780 to 1250°C, the rolling reduction amount at 780 to 1250°C was 60 to 98%, and the cooling condition after the rolling was 1.0°C/s or more.
• the "cooling condition after the rolling” refers to the average cooling rate from a temperature equal to or higher than (hot rolling delivery temperature - 100°C) to a temperature equal to or lower than 600°C.
• Test specimens for joints were taken from the obtained steel plate, and welded joints were prepared by welding the L direction to the L direction and the C direction to the C direction.
• the welding conditions were as follows: shape of the groove: single bevel groove, backing material: ceramic, shield gas: Ar-30% CO 2 , and torch drag angle: 5 to 10°.
• the tensile test properties, low-temperature toughness, and microstructure of the steel plates were evaluated, and low-temperature toughness of coarse grain heat affected zones of the welded joints was evaluated by the procedures described below.
• a tensile test specimen described below was taken from the 1/2 plate thickness position at the center position in the longitudinal direction and the width direction of the steel plate. From a steel plate having a plate thickness exceeding 15 mm, a JIS No. 4 tensile test specimen was taken, and from a steel plate having a plate thickness of 15 mm or less, a round bar tensile test specimen was taken. A tensile test in compliance with the provisions of JIS Z 2241 (2011) was performed on the tensile test specimens to evaluate the tensile strength (TS) and yield stress (YS). In Examples, samples which had a yield stress of 400 MPa or more were evaluated as having "excellent base material strength".
• the low-temperature toughness of the steel plate was evaluated as follows.
• C-direction Charpy V-notch test specimens were taken in a direction perpendicular to the rolling direction from each of the obtained steel plates at the 1/2 plate thickness position from the surface of the steel plate.
• L-direction Charpy V-notch test specimens were taken in a direction parallel to the rolling direction from each of the obtained steel plates at the 1/2 plate thickness position from the surface of the steel plate.
• Tensile test specimens having a gauge length of 200 mm were taken in the L direction and the C direction at the 1/2 plate thickness position from the steel plate surface of the obtained steel plate, and were subjected to 5% tensile pre-strain and then to an aging treatment at 250°C for 1 hour. Then Charpy V-notch test specimens were taken in the L direction and the C direction from the resulted tensile test specimens.
• the Charpy impact test was performed on three specimens of each steel plate to determine the absorbed energy at -196°C and evaluate the steel material (base material) toughness. As described above, a low toughness value is exhibited in the steel plate C direction. Thus, in these examples, the sample in which the average of the absorbed energy (vE -196 ) values of the three test specimens was 41 J or more in the C direction was evaluated as having "excellent base material toughness".
• a subsize (5 mm) Charpy V-notch test specimen was prepared in the C direction, and the Charpy impact test was performed on three specimens from each sample at -196°C.
• Table 3 the samples with which subsize Charpy V-notch test specimens were used are indicated by "*1" under the absorbed energy column.
• the sample in which the average of the absorbed energy (vE -196 ) values of the three test specimens was 27 J or more in the C direction was evaluated as having "excellent base material toughness".
• the low-temperature toughness of the welded joints was evaluated as follows.
• the area fraction of each phase of the microstructure was determined from the phase map of the EBSD analysis.
• An EBSD analysis test specimen was taken from a cross section parallel to the rolling direction at the 1/2 plate thickness position of the obtained steel plate, EBSD analysis was performed in a 500 ⁇ m ⁇ 200 ⁇ m visual field at a measurement step of 0.3 ⁇ m, and the values indicated in the phase map were respectively assumed to be the area fraction of the austenite phase, the ferrite phase, and the martensite phase.
• “Other phases” means the balance other than the austenite phase, namely, the total area fraction of the ferrite phase and/or martensite phase.
• a measurement test specimen was taken from the 1/2 plate thickness position at the center position in the longitudinal direction and the width direction of the steel plate.
• the texture strength of the ND plane was measured by X-ray diffraction from each of the measurement test specimens.
• the maximum value of the texture strength was determined from the obtained orientation distribution function (ODF). Note that the ODF can be obtained from a pole figure ((110) [001], (100) [011], (100) [010], (110) [112], and (112)[111]) measured by X-ray diffraction (internally standardized) after removing residual stress on the specimen surface by chemical polishing.
• the hardness HV10kg was measured at the 1/2 plate thickness position at 100 points at the center position of the steel plate in the longitudinal direction and the width direction of the steel plate. The maximum value was used as the maximum hardness value.
• d n / p ⁇ f ⁇ 100
• p the total number of grating points in a visual field
• f the number of visual fields
• n the number of grating point centers occupied by inclusions in f visual fields. Note that the cleanliness for MnS as the sulfide inclusion was calculated.
• the austenite steel materials of the present invention satisfied the aforementioned target performance ((110)[001]texture strength of less than 10.0, a hardness of less than 300 HV, and a Charpy impact absorbed energy (vE -196 ) of 41 J or more at the 1/2 plate thickness position of the steel material). Moreover, it was confirmed that welded joints obtained by welding the austenite steel materials of the present invention satisfied the aforementioned target performance (a Charpy impact absorbed energy (vE -196 ) of 41 J or more in the coarse grain heat affected zone). Furthermore, the aforementioned performance (a Charpy impact absorbed energy (vE -196 ) of 41 J or more after strain aging) was satisfied even after the strain aging treatment.
• the austenite steel materials of Comparative Examples outside the ranges of the present invention could not satisfy the target performance.
• the absorbed energy of the welded joints obtained therefrom could not satisfy the aforementioned target performance. It was confirmed that the aforementioned target performance was satisfied after the strain aging treatment.

Landscapes

• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Materials Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Physics & Mathematics (AREA)
• Thermal Sciences (AREA)
• Crystallography & Structural Chemistry (AREA)
• General Engineering & Computer Science (AREA)
• Heat Treatment Of Steel (AREA)
• Filling Or Discharging Of Gas Storage Vessels (AREA)

Applications Claiming Priority (2)

Publications (1)

Family

ID=77670492

Family Applications (1)

Country Status (5)

Families Citing this family (2)

Family Cites Families (10)

• 2020
  • 2020-03-11 JP JP2020537251A patent/JP7024877B2/ja active Active
  • 2020-03-11 WO PCT/JP2020/010410 patent/WO2021181543A1/fr active Application Filing
• 2021
  • 2021-02-25 JP JP2021532003A patent/JP7272438B2/ja active Active
  • 2021-02-25 KR KR1020227029930A patent/KR20220131996A/ko not_active Application Discontinuation
  • 2021-02-25 CN CN202180018720.9A patent/CN115210400B/zh active Active
  • 2021-02-25 WO PCT/JP2021/006963 patent/WO2021182110A1/fr unknown
  • 2021-02-25 EP EP21768230.1A patent/EP4089196A1/fr active Pending

Also Published As

Similar Documents

Legal Events