EP4682285A1 - Steel - Google Patents

Steel

Info

Publication number
EP4682285A1
EP4682285A1 EP24771022.1A EP24771022A EP4682285A1 EP 4682285 A1 EP4682285 A1 EP 4682285A1 EP 24771022 A EP24771022 A EP 24771022A EP 4682285 A1 EP4682285 A1 EP 4682285A1
Authority
EP
European Patent Office
Prior art keywords
less
steel product
steel
toughness
present disclosure
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
EP24771022.1A
Other languages
German (de)
French (fr)
Inventor
Tetsuya Uchiyama
Daiki NAKANISHI
Hirokazu USUKI
Hiroyuki Shirahata
Nobuyuki Yoshimura
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nippon Steel Corp
Original Assignee
Nippon Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nippon Steel Corp filed Critical Nippon Steel Corp
Publication of EP4682285A1 publication Critical patent/EP4682285A1/en
Pending legal-status Critical Current

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Classifications

    • 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
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • 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
    • C21D6/001Heat treatment of ferrous alloys containing Ni
    • 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
    • C21D6/005Heat treatment of ferrous alloys containing Mn
    • 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
    • C21D6/008Heat treatment of ferrous alloys containing Si
    • 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
    • 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
    • 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
    • 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
    • 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
    • C21D9/50Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for welded joints
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • 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
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/14Ferrous alloys, e.g. steel alloys containing 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
    • C22C38/16Ferrous alloys, e.g. steel alloys containing copper
    • 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
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • 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
    • C22C38/44Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • 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
    • 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
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • 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
    • C21D2211/002Bainite
    • 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
    • C21D2211/008Martensite

Definitions

  • the present disclosure relates to a steel product.
  • Steel products can be used in welded structures such as buildings, bridges, ships, pipelines, offshore structures, pressure vessels and tanks. Steel products having excellent strength and adaptability to low-temperature toughness are effective in low-temperature applications.
  • Cryogenic steel is used in cryogenic pressure vessels such as storage tanks for liquefied gases.
  • Al-killed steel, nickel steel, high-Mn steel, austenitic stainless steel and the like exist in a cryogenic steel, in accordance with the usage temperature.
  • nickel steel such as 3.5% Ni steel is used as a material for tanks that store liquefied ethane or liquefied ethylene whose usage temperatures are around -100°C.
  • Patent Document 1 proposes a nickel-containing steel product for low temperatures that has excellent toughness and has a specific chemical composition containing 2.7% or more and 5.0% or less Ni, wherein the prior austenite grain diameter at the time of quenching heating is 20 ⁇ m or less, and the effective crystal grain diameter after a heat treatment is 12 ⁇ m or less, and the tensile strength is 450 MPa or more and 690 MPa or less.
  • a cryogenic pressure vessel is manufactured by welding a steel product, and, in order to eliminate residual stress that arises due to the welding, there are cases in which a post weld heat treatment (called PWHT upon occasion) is carried out. Recently, the demand for low-temperature toughness of steel products after PWHT has increased even more.
  • a topic of the present disclosure is the provision of a steel product that is suited to low-temperature applications and that has good low-temperature toughness regardless of whether before or after a post weld heat treatment.
  • the gist of the present disclosure is as follows.
  • a steel product that is suited to low-temperature applications and that has good low-temperature toughness regardless of whether before or after a post weld heat treatment can be provided.
  • Fig. 1 is a diagram illustrating an example of results of discriminating the microstructure.
  • post weld heat treatment in the present disclosure means a post weld heat treatment based on the contents prescribed in JIS Z 3700:2009 “Method of post weld heat treatment Method", unless otherwise specified.
  • the "steel product” and the “base metal” in the present disclosure mean the steel product portion that does not include a surface treated layer such as a plating layer or a coated film. However, a surface treated layer such as a plating layer or a coated film may be formed on the surface of the steel product relating to the present disclosure.
  • the "base metal" in a welded joint means the steel product portion that is not affected by welding, in contrast to the welded portion (the welded metal or the heat affected zone).
  • step is not only an independent step and includes steps that, even in a case in which that step cannot be clearly distinguished from another step, achieve the intended object of that step.
  • the inventors of the present disclosure carried out studies in order to improve the strength of steel products.
  • the tensile strength of a steel product is ensured by the configuration of the microstructure.
  • the inventors of the present disclosure took samples from a 1/4t portion (t: thickness of the steel product) of a steel product after hot rolling and accelerated cooling, and carried out tensile test thereon, and observed the microstructures.
  • the area ratio of ferrite is less than 10.0%
  • the total of the area ratios of upper bainite, lower bainite and martensite is 90.0% or more.
  • the total of the area ratios of upper bainite, lower bainite and martensite was measured by using electron back scatter diffraction (hereinafter called "EBSD").
  • the inventors of the present disclosure carried out studies in order to improve the toughness of steel products.
  • the toughness of a steel product is ensured by the configuration of the microstructure.
  • the inventors of the present disclosure took samples from the 1/4t portion of a steel product after hot rolling and accelerated cooling, and carried out Charpy impact test, and observed the microstructures.
  • the total of the area ratios of lower bainite and martensite is 15.0% or more and the area ratio of the residual austenite is less than 1.7%.
  • the total of the area ratios of lower bainite and martensite was measured by using EBSD.
  • the area ratio of the residual austenite was measured by X-ray diffraction.
  • the volume ratio of the residual austenite measured by the X-ray diffraction may be considered to be the area ratio.
  • the inventors of the present disclosure carried out studies in order to ensure the toughness of steel products.
  • the toughness of a steel product is ensured by making the region, at which the difference in crystal orientation is 15° or more and which is surrounded by a high angle grain boundary, small.
  • the inventors of the present disclosure took samples from the 1/4t portion of a steel product manufactured by controlling the cooling rate and the cooling stoppage temperature after hot rolling, and measured the circle equivalent diameter of the region surrounded by a high angle grain boundary by EBSD.
  • the circle equivalent diameter of the region surrounded by a high angle grain boundary is called the crystal grain diameter hereinafter.
  • the sample was subjected to mechanical polishing and electrolytic polishing, and analysis was carried out on a 4 mm 2 region by an EBSD device equipped with an FE-SEM (field emission scanning electron microscope).
  • C is an element that improves the strength of the steel product. From the standpoint of ensuring the strength of the steel product that is used in a structure, in the present disclosure, the C content is 0.03% or more. The C content is preferably 0.05% or more, or 0.07% or more. On the other hand, C is an element that reduces toughness, and, from the standpoint of ensuring the toughness of the heat affected zone (hereinafter called "HAZ" upon occasion), in the present disclosure, the C content is 0.20% or less. The C content is preferably 0.16% or less, 0.14% or less, or 0.12% or less.
  • the Si is an element that is used as a deoxidizing agent, and further, that dissolves into the steel and increases the strength. From the standpoint of controlling the O concentration contained in molten steel, in the present disclosure, the Si content is 0.01% or more. The Si content is preferably 0.03% or more, 0.05% or more, 0.10% or more, or 0.12% or more. On the other hand, if the Si content is excessive, there are cases in which a hard phase forms in the HAZ, and the toughness decreases. Accordingly, from the standpoint of ensuring the toughness of the HAZ, in the present disclosure, the Si content is 0.50% or less. The Si content is preferably 0.30% or less, or 0.20% or less.
  • Mn is an element that is used as a deoxidizing agent, and further, that improves the hardenability of the steel and contributes to increasing the strength. From the standpoint of controlling the O concentration contained in molten steel, in the present disclosure, the Mn content is 0.10% or more. Moreover, due to Mn in an amount of 0.10% or more, by forming MnS, the solid-solution S is reduced, and hot cracking is prevented. From the standpoint of ensuring the strength of the steel product and the toughness of the HAZ, the Mn content is preferably 0.30% or more, or 0.50% or more.
  • the Mn content is 2.00% or less.
  • the Mn content is preferably 1.80% or less, or 1.50% or less.
  • the P is an impurity element.
  • the P content may be 0.001% or more.
  • the P content is 0.025% or less.
  • the P content is preferably 0.016% or less, 0.012% or less, or 0.008% or less.
  • the S content is an impurity element.
  • the S content may be 0.0001% or more.
  • the S content is 0.0250% or less.
  • the S content is preferably 0.0100% or less or 0.0050% or less.
  • Ni is an element that is effective in improving the hardenability and toughness of the steel. Therefore, in the present embodiment, the Ni content is 4.51% or more.
  • the Ni content is preferably 5.00% or more, or 5.25% or more.
  • Ni is an expensive element, and, from the standpoint of cost reduction, in the present disclosure, the Ni content is 6.10% or less.
  • the Ni content is preferably 6.00% or less, or 5.75% or less.
  • Al is an element that is effective in deoxidation, and is an element that, by forming a nitride, refines the crystal grain diameter at the time of quenching. Therefore, in the present disclosure, the Al content is 0.001% or more. However, if Al is excessively contained, there is the concern that the Al will generate a coarse nitride, and the toughness of the steel product and the HAZ will decrease. Accordingly, the Al content is 0.100% or less.
  • the Al content is preferably 0.080%, or 0.050% or less.
  • the O content is an impurity element.
  • the lower limit of the O content is not limited, from the standpoint of the manufacturing cost, in the present disclosure, the O content may be 0.0001% or more.
  • the O content is excessive, there are cases in which a coarse oxide is generated, and the toughness and ductility of the steel product and the HAZ deteriorate.
  • the O content is 0.0100% or less.
  • the O content is preferably 0.0060% or less, or 0.0040% or less.
  • N is an impurity element.
  • the N content may be 0.0001% or more. From the standpoint of ensuring the properties of the steel product and the toughness of the HAZ, in the present disclosure, the N content is 0.0100% or less.
  • the N content is preferably 0.0050% or less, or 0.0040% or less.
  • the steel product relating to the present disclosure may contain other elements (optional elements) instead of some of the Fe.
  • the following optional elements are given as examples, but the contents of these elements may be 0%.
  • the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Cu, Cr, Mo, and B that are described hereinafter and have the effect of improving the hardenability.
  • Cu is an element that is sometimes mixed into the steel product in the manufacturing process.
  • the lower limit value of the Cu content is not limited and may be 0%.
  • Cu has little adverse effect on the weldability and on the toughness of the HAZ, and has the effect of improving the hardenability of steel, and therefore, is an element that improves the strength of the steel product.
  • the Cu content may be 0.01% or more.
  • the Cu content is preferably 0.10% or more.
  • the Cu content is 1.50% or less.
  • the Cu content is preferably 1.00% or less, 0.80% or less, 0.60% or less, or 0.50% or less.
  • the Cr content is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Cr content is not limited, and may be 0%.
  • Cr is also an element that improves the strength of a steel product because it has the effect of increasing the hardenability of the steel. Therefore, in the present disclosure, the Cr content may be 0.01% or more.
  • the Cr content is preferably 0.10% or more.
  • the Cr content is 3.00% or less.
  • the Cr content is preferably 2.20% or less, 1.40% or less, or 0.80% or less.
  • Mo is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Mo content is not limited, and may be 0%.
  • Mo is also an element that improves the strength of a steel product because it has the effect of increasing the hardenability of the steel. Therefore, in the present disclosure, the Mo content may be 0.01% or more.
  • the Mo content is preferably 0.05% or more, 0.10% or more, 0.20% or more or 0.30% or more.
  • the Mo content is 2.00% or less.
  • the Mo content is preferably 1.20% or less, or 0.80% or less.
  • B is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the B content is not limited, and may be 0%.
  • B is also an element that exhibits a marked effect of increasing the hardenability of steel and improves the strength of a steel product. Therefore, in the present disclosure, the B content may be 0.0003% or more.
  • the B content is 0.0050% or less.
  • the B content is preferably 0.0030% or less, or 0.0020% or less.
  • the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Nb, Ti, and V that are described hereinafter and have the effect of increasing the strength of the steel product by precipitates such as carbides or nitrides.
  • Nb is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Nb content is not limited, and may be 0%.
  • Nb is also an element that forms a carbide or a nitride, and has the effect of refining the microstructure, and improves the strength of the steel product. Therefore, in the present disclosure, the Nb content may be 0.001% or more.
  • the Nb content is 0.050% or less.
  • the Nb content is preferably 0.040% or less, or 0.030% or less. In particular, from the standpoint of ensuring the toughness of the steel product after PWHT, the Nb content may be 0.004% or less.
  • Ti is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Ti content is not limited, and may be 0%.
  • Ti is also an element that forms a carbide or a nitride, and has the effect of refining the microstructure, and improves the strength of the steel product. Therefore, in the present disclosure, the Ti content may be 0.001% or more.
  • the Ti content is 0.050% or less.
  • the Ti content is preferably 0.040% or less, or 0.030% or less. In particular, from the standpoint of ensuring the toughness of the steel product after PWHT, the Ti content may be 0.004% or less, or 0.002% or less.
  • V is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the V content is not limited, and may be 0%.
  • V is also an element that forms a carbide or a nitride, and improves the strength of the steel product. Therefore, in the present disclosure, the V content may be 0.01% or more.
  • the V content is 0.10% or less.
  • the V content is preferably 0.08% or less, or 0.05% or less.
  • the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Mg, Ca, and REM that are described hereinafter.
  • Mg is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Mg content is not limited, and may be 0%.
  • Mg is also an element that forms an oxide and improves the toughness of the heat affected zone. Therefore, in the present disclosure, the Mg content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more.
  • the Mg content is 0.0200% or less.
  • the Mg content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • Ca is an element that is sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the Ca content is not limited, and may be 0%.
  • Ca is also an element that, by spheroidizing the sulfide within the steel product, mitigates the effect of the MnS that decreases the toughness of the steel product and the heat affected zone. Therefore, in the present disclosure, the Ca content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more.
  • the Ca content is if the Ca content is excessive, there are cases in which the Ca forms a coarse oxide and decreases the toughness of the steel. Accordingly, from the standpoint of ensuring the toughness, in the present disclosure, the Ca content is 0.0200% or less.
  • the Ca content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • Rare earth metal is a collective term for a total of 17 elements that are the two elements of Sc and Y and fifteen lanthanoid elements such as La, Ce, Nd.
  • the REM content means the total content of the aforementioned 17 elements.
  • REMs are elements that are sometimes mixed into a steel product in the manufacturing process.
  • the lower limit value of the REM content is not limited, and may be 0%.
  • REMs are also elements that form oxides and improve the toughness of the heat affected zone. Therefore, in the present disclosure, the REM content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more.
  • the REM content is 0.0200% or less.
  • the REM content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • the balance of the chemical composition of the steel product relating to the present disclosure is iron (Fe) and impurities.
  • Impurities mean components that are mixed due to raw materials such as ore and scrap, and other factors, at the time of industrially manufacturing the steel product.
  • 0.50 ⁇ ⁇ [C] ⁇ (1+0.64[Si]) ⁇ (1+4.10[Mn]) ⁇ (1+0.27[Cu]) ⁇ (1+0.52[Ni]) ⁇ (1+2.33[Cr]) ⁇ (1+3.14[Mo])
  • [C], [Si], [Mn], [Cu], [Ni], [Cr] and [Mo] are the contents (mass%) of C, Si, Mn, Cu, Ni, Cr and Mo in the steel. In a case in which a given element is not contained, zero is substituted in. Note that ⁇ [C] has the same meaning as [C] 1/2 .
  • the range of value ⁇ is 5.0 - 16.0. This is an index expressing the hardenability of the steel product.
  • the greater the value ⁇ the more that lower bainite and martensite microstructures having a superior balance of strength and toughness can be formed.
  • is in the appropriate range, in the microstructure of the HAZ as well, the ratio of the lower bainite and martensite microstructures having a superior balance of strength and toughness becomes high, and the HAZ toughness also can be ensured.
  • is 5.0 or more, the hardenability of the base metal is ensured, and the ratio of the lower bainite and martensite having a favorable balance of strength and toughness increases, and a deterioration in toughness is suppressed.
  • value ⁇ is preferably 5.5 or more, 6.0 or more, or 7.0 or more. Further, value ⁇ is preferably 15.5 or less or 15.0 or less.
  • the microstructure of the steel product relating to the present disclosure is described next.
  • the microstructure of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product relating to the present disclosure contains lower bainite and martensite. Further, in addition to lower bainite, upper bainite also may be contained as bainite.
  • “Bainite” is a collective term for upper bainite and lower bainite.
  • “Upper bainite” is one of or both of upper bainite that contains residual austenite or an MA phase (martensite-austenite mixed phase) between the laths, and upper bainite that contains a carbide between the laths.
  • “Lower bainite” is lath-shaped lower bainite containing a carbide within the laths.
  • Lath martensite is a microstructure that is composed of packets and blocks formed from groups of laths having a specific arrangement, and in which a single austenite grain is divided into plural packets.
  • Lower bainite and martensite are hard phases and increase the toughness of the steel product. From the standpoint of ensuring the toughness of the steel product, the area ratio of lower bainite and martensite at the 1/4t portion is 15.0% or more. The area ratio of lower bainite and martensite at the 1/4t portion is preferably 20.0% or more, or 30.0% or more. The total of the area ratio of the lower bainite and the area ratio of the martensite at the 1/4t portion may be 100%.
  • the total of the area ratios of upper bainite and lower bainite and martensite at the 1/4t portion is 90.0% or more.
  • the total of the area ratios of upper bainite, lower bainite and martensite at the 1/4t portion may be 100%.
  • the upper bainite of the 1/4t portion may be 1.0% or more.
  • the area ratio of the residual austenite of the 1/4t portion is less than 1.7%.
  • the area ratio of the residual austenite of the 1/4t portion is preferably 1.0% or less, and may be 0%. This is thought to be because, in the Ni-containing, steel plate of the present disclosure, the Ni content is lower than conventional 9% Ni steel, and therefore, even if residual austenite were to exist at -110°C, it would be unstable, and, if the steel structure were to incur plastic deformation at the crack tip, the residual austenite would change into martensite due to plasticity-induced martensitic transformation. Thus, the residual austenite at room temperature is made to be less than 1.7% as a volume ratio.
  • the higher the Ni content the easier it is for the volume ratio of the residual austenite to increase as well.
  • an increase in the Ni content is also not preferable in that it leads to an increase in cost.
  • Observation of the microstructure of the steel product is carried out by using a sample in which a 1/4t portion of the steel product serves as the observed surface.
  • Two types of samples on which (a) electrolytic polishing or (b) nital etching is carried out are prepared.
  • Each sample of (a) and (b) is measured at three places by the following method, and the average value of the three places is used as the area ratio of the microstructure of that steel product. Note that three of each sample of (a) and (b) may be prepared, and the averages of the respective samples may be computed. Or, three places of one sample of each may be measured in a visual field, and the average of each computed.
  • CI value The confidence index
  • the determination of ferrite, and upper bainite, lower bainite and martensite, is carried out by setting the threshold value of the Grain Average Misorientation (hereinafter called "GAM") to 0.5.
  • GAM Grain Average Misorientation
  • the GAM value is an index defined in OIM Analysis (EBSD crystal orientation analyzing software manufactured by TSL, United States).
  • OIM Analysis EBSD crystal orientation analyzing software manufactured by TSL, United States.
  • the region in which the GAM is 0.5 or less is ferrite.
  • the region in which the GAM exceeds 0.5 is upper bainite, lower bainite, martensite or residual austenite.
  • the upper bainite, lower bainite, martensite and residual austenite in the present disclosure are determined by using the GAM of EBSD as the threshold value, not only upper bainite, lower bainite, martensite and residual austenite, but also tempered upper bainite, tempered lower bainite and tempered martensite are included. Comparing the microstructures of direct quenching (DQ) and (DQT) that is carried out thereafter up to tempering (T), although dissolution of the MA and coarsening of carbide occur after tempering, the way of looking at the microstructure does not vary greatly.
  • DQ direct quenching
  • DQT direct quenching
  • T tempering
  • Measurement of the area ratio of the upper bainite by SEM observation is carried out by using a nital etched sample.
  • the measurement magnification is 500 ⁇ , and measurement of a range of 360 ⁇ m ⁇ 480 ⁇ m is carried out.
  • the portion, which has a clear lath structure and at which carbide and MA have formed along the lath boundary, is upper bainite.
  • An example of the results of discriminating the microstructures is shown in Fig. 1.
  • (A) and (B) are SEM images of the same region of a steel product that is manufactured by DQT and whose value ⁇ is 9.9.
  • the regions surrounded by the white lines are upper bainite (Bu), and the other regions are lower bainite + martensite (B L +M).
  • upper bainite (Bu) carbides appearing white are sparsely distributed, and regions with varying density are present.
  • lower bainite + martensite (B L +M) the carbides are densely and uniformly distributed.
  • the total of the area ratios of the lower bainite, martensite and residual austenite is determined by subtracting the area ratio of the upper bainite from the total of the area ratios of the upper bainite, lower bainite, martensite and residual austenite, which were measured as described above.
  • the area ratio of the residual austenite is determined by the measuring method described hereinafter, and the total of the area ratios of the lower bainite and martensite is determined by subtracting the area ratio of the residual austenite from the total of the area ratios of the lower bainite, martensite and residual austenite.
  • the area ratio of the residual austenite is measured by X-ray diffraction. Measurement of the area ratio of the residual austenite is carried out by using a sample at which the region, which is 1/4 of the thickness in the thickness direction from the surface of the steel product (also called “1/4t portion" in the present specification), is the measured area.
  • the sample is a 2-mm thick test piece, and is taken from a position that is 1/4 of the width from a width direction end portion of the steel product, and chemical polishing is carried out thereon, and the sample is used in measuring the volume ratio of the residual austenite by X-ray diffraction using an Mo tube.
  • Quantification is carried out on the basis of the ratios of the integrated intensities of the (200), (211) diffraction peaks of the ferrite phase and the integrated intensities of the (200), (220), (311) diffraction peaks of the austenite phase, and the average values of the six combinations are employed.
  • the integrated intensities of the diffraction peaks are determined by fitting the backgrounds on the basis of the signals before and after the peaks, and subtracting the signal differences.
  • the volume ratio measured by the X-ray diffraction is considered to be the area ratio.
  • the average crystal grain diameter (effective crystal grain diameter) of the 1/4t portion of the steel product is preferably 20.0 ⁇ m or less. This is because it was learned that, if the average crystal grain diameter of the 1/4t portion of the steel product is 20.0 ⁇ m or less, the toughness of the steel product tends to improve even more regardless of whether before or after PWHT. However, the average crystal grain diameter of the 1/4t portion of the steel product may exceed 20.0 ⁇ m. The smaller the average crystal grain diameter of the steel product, the more preferable, and therefore, the lower limit value thereof is not limited. Usually, the average crystal grain diameter is 10 ⁇ m or more. The effective crystal grain diameter is determined by a weighted average.
  • Effective crystal grain diameter D area that is determined by a weighted average is calculated by the following formula by using, of the crystal grain diameters that are measured in a 4 mm 2 region, area Si and grain diameter d i of the ith crystal grain detected at the time of measurement.
  • D area ⁇ S i ⁇ d i / ⁇ S i
  • the form of the prior austenite crystal grains (called prior austenite grains or prior ⁇ grains upon occasion) of the steel product of the present disclosure may be a form that is flat in the rolling direction. If the prior austenite grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product are made to be flat grains of an aspect ratio of 1.5 or more, an even greater improvement in the toughness of the steel product is possible. This is because, by increasing the grain boundary area by making the prior austenite grains flat, there is a substantial refining of the austenite grains, and this is effective in refining the effective crystal grain diameter.
  • the aspect ratio of prior austenite grains is usually 4.0 or less, and may be 3.5 or less.
  • the aspect ratio of the prior austenite crystal grains of the 1/4t portion may be less than 1.5.
  • the aspect ratio of the prior austenite crystal grains of the 1/4t portion may be 1.4 or less, or 1.3 or less.
  • the aspect ratio of the prior austenite crystal grains (hereinafter called prior austenite grains upon occasion) of the steel product is determined as follows.
  • An L cross-section (a cross-section parallel to the rolling direction and the thickness direction of the steel product) of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is mirror polished, and corrosion is carried out by a corrosive liquid of a saturated solution base of 2 - 4% picric acid, and the prior austenite grain boundaries of an arbitrary region of 1.0 mm in the rolling direction ⁇ 0.5 mm in the thickness direction are made to appear.
  • the long diameters and short diameters of the individual prior austenite grains are measured, and the aspect ratio of each prior austenite grain is calculated by long diameter ⁇ short diameter.
  • the arithmetic mean of the calculated aspect ratios of all of the prior austenite grains is determined as the "aspect ratio of the prior austenite grains". Note that the maximum length of the prior austenite grain is used as the long diameter, and the maximum interval between two lines, which contact the grain and are parallel to the long diameter direction, is used as the short diameter.
  • the steel product relating to the present disclosure has mechanical properties that are such that the steel product has both strength and low-temperature toughness. In addition to having excellent toughness at -110°C in particular, the steel product can exhibit excellent low-temperature toughness after PWHT as well.
  • the tensile strength of the steel product is 615 - 930 MPa.
  • a steel product that can ensure strength of a structure even if the thickness is thin is necessary. Because steel products that are selected as steel products to be used in such applications usually are steel products having the aforementioned tensile strength, the steel product relating to the present disclosure also is manufactured to have the aforementioned tensile strength.
  • the Charpy impact absorption energy at -110°C of the steel product of the present disclosure is preferably 150 J or more. Due to the steel product of the present disclosure having low-temperature toughness of a Charpy impact absorption energy at -110°C of 150 J or more, a transport tank formed from the steel product of the present disclosure can be suitably used for transporting liquid carbon dioxide for example.
  • the steel product of the present disclosure may have low-temperature toughness of a Charpy impact absorption energy at -110°C of 100 J or more. Note that the Charpy impact absorption energy at -110°C is a numerical value measured by using a sample taken from a position of 1/4 of the thickness.
  • the Charpy impact absorption energy at -110°C is preferably 150 J or more.
  • the Charpy impact absorption energy at -110°C after PWHT may be 100 J or more.
  • the Charpy impact absorption energy at -110°C after PWHT also is a numerical value measured by using a sample taken from a position of 1/4 of the thickness.
  • the Charpy impact absorption energy at -110°C after thermal cycling is preferably 50 J or more. Due to the steel product of the present disclosure having low-temperature toughness that is such that the Charpy impact absorption energy at -110°C after thermal cycling is 50 J or more, a transport tank formed from the steel product of the present disclosure can be suitably used for transporting liquid carbon dioxide for example.
  • the Charpy impact absorption energy at -110°C after thermal cycling may be 40 J or more.
  • the Charpy impact absorption energy at -110°C after thermal cycling is a numerical value measured by using a sample taken from a position of 1/4 of the thickness of the steel product as a thermal cycling test piece, and providing it with a thermal history of raising the temperature at 60°C/s to 1350°C, and, after maintenance at 1350°C for 1 s, cooling at 20°C/s to room temperature, and thereafter, taking a Charpy test piece therefrom.
  • PWHT is carried out on the welded portions of cryogenic tanks after being assembled into transport tanks, in order to prevent breakage in advance.
  • PWHT in which the rate of temperature increase and the rate of temperature decrease are 55°C/h in the temperature region of 425°C or more, and the steel product is held for 2 hours at 600°C, is carried out on the steel product of the present disclosure, and thereafter, a Charpy test piece is taken, and measurement is carried out.
  • the Charpy impact absorption energy at -110°C is preferably 50 J or more.
  • the Charpy impact absorption energy at -110°C of the portion at which PWHT is carried out after the above-described thermal cycling test may be 40 J or more.
  • the tensile strength (TS) and the yield strength (YS) are measured in accordance with a tensile test that is based on JIS Z2241:2011.
  • the tensile test uses a JIS14A test piece that has been taken from a position of 1/4 of the thickness and whose length direction is the direction (the C direction) parallel to the width direction of the steel product.
  • TS and YS are computed by using three test pieces and taking the averages thereof.
  • the yield ratio (YR, %) is computed by (YS/TS) ⁇ 100, on the basis of the respective average values of TS and YS.
  • the Charpy impact absorption energy is measured by a Charpy impact test at -110°C on the basis of the prescriptions of JIS Z2242:2018 and by using an impact blade of a radius of 2 mm.
  • the Charpy impact absorption energy is calculated by measuring by using three test pieces, and taking the average thereof.
  • the Charpy impact absorption energy test uses a V-notched test piece that has been taken from a position of 1/4 of the thickness of the steel product and whose length direction is the direction (the C direction) parallel to the width direction of the steel product.
  • the form of the steel product relating to the present disclosure is not particularly limited, and examples are steel plates, steel strips, structural steel and steel pipes.
  • steel pipes and structural steel include steel products in which steel plates are joined, e.g., in addition to welded steel pipes and welded structural steel, structural steel joined by rivets, and the like.
  • the thickness of the steel product such as steel plates, steel strips, structural steel and steel pipes (the thickness of the flanges in the case of structural steel) is not particularly limited, and usually is 3 mm or more and 150 mm or less.
  • the thickness of the steel product may be 6 mm or more, 10 mm or more, 15 mm or more, or 30 mm or more. Further, the thickness of the steel product may be 100 mm or less, 80 mm or less, or 60 mm or less.
  • the steel product relating to the present disclosure has mechanical properties such that the steel product has both strength and low-temperature toughness, and, in particular, can exhibit excellent low-temperature toughness even after PWHT. Therefore, the steel product relating to the present disclosure can be suitably used as a tank that stores and transports liquefied gasses, and liquid carbon dioxide in particular.
  • the method of manufacturing the steel product relating to the present disclosure is not particularly limited, but, for example, after melting a steel that satisfies the above-described chemical composition, a steel slab is manufactured by continuous casting.
  • the steel slab is subjected to either direct quenching (DQ), in which it is heated, hot rolled, and then directly water-cooled, or reheat quenching (RQ), in which it is hot rolled, air-cooled, reheated, and then water-cooled, to made into a steel product.
  • DQ direct quenching
  • RQ reheat quenching
  • T tempering
  • DQT is preferable in the manufacturing of the steel product relating to the present disclosure.
  • An example of a preferable manufacturing process is given hereinafter.
  • the heating temperature of the steel slab on which the hot rolling is carried out is Ac 3 or more.
  • the heating temperature of the steel slab is preferably 1000°C or more.
  • the heating temperature of the hot rolling is 1250°C or less.
  • the heating temperature of the hot rolling is preferably 1200°C or less.
  • the element symbols in the formula mean the content (mass%) of each element contained in the steel slab.
  • the hot rolling is structured by rolling in a temperature range in which recrystallization occurs (rolling in the recrystallization temperature range) and rolling in a temperature range in which recrystallization is suppressed (rolling in the non-recrystallization temperature range).
  • Rolling in the recrystallization temperature range is hot rolling carried out with the temperature of the rolled steel during rolling being 900°C or more.
  • the cumulative rolling reduction ratio of the rolling in the recrystallization temperature range is preferably 20% or more, and more preferably 30% or more.
  • Rolling in the non-recrystallization temperature range is hot rolling carried out with the temperature of the rolled steel during rolling being less than 900°C.
  • the cumulative rolling reduction ratio of the rolling in the non-recrystallization temperature range is preferably 20% or more, and more preferably 30% or more.
  • the cumulative rolling reduction ratio of the rolling in the non-recrystallization temperature range is determined from the difference between the thickness of the rolled steel at 900°C and the thickness of the steel product after rolling ends.
  • Cumulative rolling reduction ratio (%) of rolling in non-recrystallization temperature range 100 ⁇ ([thickness of rolled steel at 900°C] - [thickness of steel product after rolling ends]) / [thickness of rolled steel at 900°C]
  • the end temperature of the hot rolling is Ar 3 or more.
  • accelerated cooling such as water cooling is carried out on the steel product.
  • the start temperature of the accelerated cooling is Ar 3 or more.
  • the element symbols in the formula mean the content (mass%) of each element contained in the steel product, and t means the thickness (mm) of the steel product.
  • the cooling rate is 1.0°C/s or more.
  • the cooling rate of the accelerated cooling is preferably 5.0°C/s or more, or 10.0°C/s or more.
  • the cooling rate is a value obtained by calculating the cooling rate at a position of 1/4 of the thickness by simulation in accordance with thermal transfer calculation.
  • the stoppage temperature of the accelerated cooling is 400°C or less.
  • the stoppage temperature of the accelerated cooling is preferably 350°C or less. Accelerated cooling may be carried out to room temperature. From the standpoint of dehydrogenation of the steel product, the stoppage temperature is preferably 100°C or more.
  • a tempering treatment may be carried out on the steel product.
  • the heating temperature of the tempering treatment is preferably 650°C or less, 620°C or less, or 590°C or less.
  • the heating temperature of the tempering treatment is preferably 350°C or more, or 400°C or more.
  • the steel product relating to the present disclosure is manufactured by RQ
  • the effects of the heating temperature and the rolling reduction ratio of the steel slab at the time of the hot rolling on the mechanical properties of the steel product are small.
  • the heating temperature of the steel slab is preferably 1000°C or more.
  • the rolling reduction ratio is insufficient, there are cases in which initial stage defects from the time of manufacturing the steel slab remain at the thickness central portion, and the quality of the steel product decreases. Therefore, the total of the rolling reduction ratios of hot rolling (also called cumulative rolling reduction ratio) is preferably 35% or more.
  • the steel slab may, as is, be water-cooled or air-cooled.
  • the reheating temperature of the steel product is Ac 3 or more, because quenching is carried out from an austenite single-phase microstructure. From the standpoint of ensuring the homogeneity of the microstructure, the reheating temperature of the steel product is preferably 750°C or more, 850°C or more, 880°C or more, or 900°C or more.
  • the upper limit temperature of the reheating temperature is not particularly stipulated, there are cases in which excessive heating to a high temperature leads to coarsening of the austenite grains and a decrease in toughness, and therefore, the upper limit temperature of the reheating temperature is preferably 1000°C or less, 950°C or less, or 930°C or less.
  • a tempering treatment may be carried out on the steel product.
  • the heating temperature of the tempering treatment is preferably 660°C or less, or 640°C or less.
  • the heating temperature of the tempering treatment is preferably 400°C or more, 450°C or more, or 500°C or more.
  • Tempor heat treatment is the heating temperature in the tempering treatment after the quenching.
  • Table 2 No. plate thickness (mm) Ac 3 [°C] hot rolling conditions
  • Temper heat treatment [°C] heating temperature [°C] cumulative rolling reduction [%] ratio at 900°C or more cumulative rolling reduction ratio [%] at less than 900°C end temperature [°C] cooling after rolling start temperature [°C] stoppage temperature [°C] cooling rate [°C/s] 2A 35 697 1230 23 60 820 water cooling 404 800 180 9.5 510 3A 25 725 1150 30 50 810 water cooling 453 800 160 5.3 540 4A 15 725 1150 31 59 790 water cooling 446 770 150 5.7 640 6A 35 751 1130 31 45 770 water cooling 495 750 270 12.2 610 7A 60 763 1170 32 30 780 water cooling 497 760 290 2.9
  • microstructures and mechanical properties of the obtained steel products were measured by the above-described methods. The results are shown in Table 3. The meanings of the symbols of the microstructures are as follows. Note that the remainders of the microstructures were pearlite, MA phase, and ferrite.
  • Nos. 2A - 26A, 101A - 113A are Examples of the present invention, and Nos. 28A - 32A, 114A - 118A are Comparative Examples.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive. Because there was also too much residual ⁇ , sufficient low-temperature toughness was not obtained.
  • value ⁇ was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • the chemical compositions and microstructures of the steel products were controlled appropriately, and the tensile strengths were in the appropriate range of 615 MPa or more and 930 MPa or less.
  • low-temperature toughness at -110°C of 100 J or more was obtained regardless of whether before or after PWHT.
  • microstructures and mechanical properties of the obtained steel products were measured by the above-described methods. The results are shown in Table 6. The meanings of the symbols of the microstructures are as follows. Note that the remainders of the microstructures were MA phase and ferrite.
  • Nos. 2B - 24B and 101B - 113B are Examples of the present invention, and Nos. 25B - 29B and 114B - 119B are Comparative Examples.
  • value ⁇ was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • value ⁇ was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • value ⁇ exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive. Further, because there was also too much residual ⁇ , sufficient low-temperature toughness was not obtained.
  • the chemical compositions and microstructures of the steel products were controlled appropriately, and the tensile strengths were in the appropriate range of 615 MPa or more and 930 MPa or less.
  • low-temperature toughness at -110°C of 100 J or more was obtained regardless of whether before or after PWHT.
  • low-temperature toughness at -110°C of 150 J or more was obtained regardless of whether before or after PWHT.
  • the steel products relating to the present disclosure can be used mainly for transport tanks of liquefied carbon dioxide. Further, the steel products relating to the present disclosure can also be used in other welded structures such as buildings, bridges, ships, pipelines, offshore structures, pressure vessels and tanks.

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Abstract

A steel product having a specific chemical composition, in which α expressed by a following formula is 5.0 or more and 16.0 or less; having a tensile strength of 615 MPa or more and 930 MPa or less; and having a microstructure in a region that is 1/4 of a thickness from a surface that contains lower bainite and martensite, with a total of area ratios of the lower bainite and the martensite being 15.0% or more, a total of area ratios of upper bainite, the lower bainite, and the martensite being 90.0% or more, and an area ratio of residual austenite being less than 1.7%. α = 0.50 × √[C] × (1+0.64[Si]) × (1+4.10[Mn]) × (1+0.27[Cu]) × (1+0.52[Ni]) × (1+2.33[Cr]) × (1+3.14[Mo])

Description

    Technical Field
  • The present disclosure relates to a steel product.
  • Background Art
  • Steel products can be used in welded structures such as buildings, bridges, ships, pipelines, offshore structures, pressure vessels and tanks. Steel products having excellent strength and adaptability to low-temperature toughness are effective in low-temperature applications.
  • Cryogenic steel is used in cryogenic pressure vessels such as storage tanks for liquefied gases. Al-killed steel, nickel steel, high-Mn steel, austenitic stainless steel and the like exist in a cryogenic steel, in accordance with the usage temperature. For example, nickel steel such as 3.5% Ni steel is used as a material for tanks that store liquefied ethane or liquefied ethylene whose usage temperatures are around -100°C.
  • As with this 3.5% Ni steel, steel products that require ensured low-temperature toughness-exemplified by those used in cryogenic pressure vessels-are often made to contain Ni.
  • For example, Patent Document 1 proposes a nickel-containing steel product for low temperatures that has excellent toughness and has a specific chemical composition containing 2.7% or more and 5.0% or less Ni, wherein the prior austenite grain diameter at the time of quenching heating is 20 µm or less, and the effective crystal grain diameter after a heat treatment is 12 µm or less, and the tensile strength is 450 MPa or more and 690 MPa or less.
  • Further, various steel products of prescribed chemical compositions and microstructures (metal structures) have been proposed for the purposes of low-temperature toughness and high strength (see, for example, Patent Documents 2 through 6).
    • Patent Document 1: Japanese Patent Application Laid-Open ( JP-A) No. 2019-81930
    • Patent Document 2: JP-A No. H06-192729
    • Patent Document 3: JP-A No. H07-331328
    • Patent Document 4: International Publication No. 2007/034576
    • Patent Document 5: International Publication No. 2020/184162
    • Patent Document 6: International Publication No. 2014/017057
    SUMMARY OF INVENTION Technical Problem
  • Having both high strength and the ensuring of low-temperature toughness is desirable for cryogenic steels that are used in cryogenic pressure vessels. Further, a cryogenic pressure vessel is manufactured by welding a steel product, and, in order to eliminate residual stress that arises due to the welding, there are cases in which a post weld heat treatment (called PWHT upon occasion) is carried out. Recently, the demand for low-temperature toughness of steel products after PWHT has increased even more.
  • A topic of the present disclosure is the provision of a steel product that is suited to low-temperature applications and that has good low-temperature toughness regardless of whether before or after a post weld heat treatment.
  • Solution to Problem
  • The gist of the present disclosure is as follows.
    • <1> A steel product having a chemical composition including, in mass%,
      • C: 0.03% or more and 0.20% or less,
      • Si: 0.01% or more and 0.50% or less,
      • Mn: 0.10% or more and 2.00% or less,
      • P: 0.025% or less,
      • S: 0.0250% or less,
      • Ni: 4.51% or more and 6.10% or less,
      • Al: 0.001% or more and 0.100% or less,
      • O: 0.0100% or less,
      • N: 0.0100% or less,
      • Cu: 0 - 1.50%,
      • Cr: 0 - 3.00%,
      • Mo: 0 - 2.00%,
      • B: 0 - 0.0050%,
      • Nb: 0 - 0.050%,
      • Ti: 0 - 0.050%,
      • V: 0 - 0.10%,
      • Mg: 0 - 0.0200%,
      • Ca: 0 - 0.0200%,
      • REM: 0 - 0.0200%,
      • balance: Fe and impurities,
      • and in which α expressed by following formula (1) is 5.0 or more and 16.0 or less,
      • wherein:
        • a tensile strength is 615 MPa or more and 930 MPa or less, and
        • a microstructure of a region that is 1/4 of a thickness in a thickness direction from a surface of the steel product contains lower bainite and martensite, and a total of area ratios of the lower bainite and the martensite is 15.0% or more, and a total of area ratios of upper bainite and the lower bainite and the martensite is 90.0% or more, and an area ratio of residual austenite is less than 1.7%. α = 0.50 × √[C] × (1+0.64[Si]) × (1+4.10[Mn]) × (1+0.27[Cu]) × (1+0.52[Ni]) × (1+2.33[Cr]) × (1+3.14[Mo])
        • wherein [element symbol] in formula (1) represents content (mass%) of a respectively corresponding element contained in the steel product, and, in a case in which an element is not contained, zero is substituted in therefor.
    • <2> The steel product of <1>, wherein, in the microstructure of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product, an average crystal grain diameter is 20.0 µm or less.
    • <3> The steel product of <1> or <2>, wherein a Charpy impact absorption energy at -110°C is 150 J or more.
    • <4> The steel product of any one of <1> through <3>, wherein, in a case in which a heat treatment, in which a rate of temperature increase and a rate of temperature decrease in a temperature region of 425°C or more are 55°C/h and temperature is held for 2 hours at 600°C, is carried out on the steel product, a Charpy impact absorption energy at -110°C of portions where the heat treatment has been carried out is 150 J or more.
    • <5> The steel product of any one of <1> through <4>, wherein an aspect ratio of prior austenite crystal grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is 1.5 or more.
    • <6> The steel product of any one of <1> through <4>, wherein an aspect ratio of prior austenite crystal grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is less than 1.5.
    Advantageous Effects of Invention
  • In accordance with the present disclosure, a steel product that is suited to low-temperature applications and that has good low-temperature toughness regardless of whether before or after a post weld heat treatment can be provided.
  • BRIEF DESCRIPTION OF DRAWINGS
  • Fig. 1 is a diagram illustrating an example of results of discriminating the microstructure.
  • DESCRIPTION OF EMBODIMENTS
  • The present disclosure is described in detail hereinafter.
  • The "post weld heat treatment" in the present disclosure means a post weld heat treatment based on the contents prescribed in JIS Z 3700:2009 "Method of post weld heat treatment Method", unless otherwise specified.
  • The "steel product" and the "base metal" in the present disclosure mean the steel product portion that does not include a surface treated layer such as a plating layer or a coated film. However, a surface treated layer such as a plating layer or a coated film may be formed on the surface of the steel product relating to the present disclosure. Further, the "base metal" in a welded joint means the steel product portion that is not affected by welding, in contrast to the welded portion (the welded metal or the heat affected zone).
  • In the present disclosure, numerical ranges expressed by using "-" mean ranges in which the numerical values listed before and after the "-" are included as the lower limit value and upper limit value, respectively. However, numerical value ranges in which "exceeds" or "less than" is appended to the numerical value listed before or after the "-" mean a range in which these numerical values are not included as the lower limit value or the upper limit value.
  • With respect to the contents of the elements in a chemical composition, "%" means "mass%".
  • The term "step" is not only an independent step and includes steps that, even in a case in which that step cannot be clearly distinguished from another step, achieve the intended object of that step.
  • A steel product relating to an embodiment of the present disclosure is described hereinafter. The new knowledge, which was obtained as the result of studies by the inventors of the present disclosure and which was arrived at in completing the steel product relating to the present disclosure, is described in detail first.
  • The inventors of the present disclosure carried out studies in order to improve the strength of steel products. The tensile strength of a steel product is ensured by the configuration of the microstructure. The inventors of the present disclosure took samples from a 1/4t portion (t: thickness of the steel product) of a steel product after hot rolling and accelerated cooling, and carried out tensile test thereon, and observed the microstructures. As a result, it was learned that, at the microstructure of the 1/4t portion of a steel product having a tensile strength of 615 MPa or more and 930 MPa or less, the area ratio of ferrite is less than 10.0%, and the total of the area ratios of upper bainite, lower bainite and martensite is 90.0% or more. Note that the total of the area ratios of upper bainite, lower bainite and martensite was measured by using electron back scatter diffraction (hereinafter called "EBSD").
  • Further, the inventors of the present disclosure carried out studies in order to improve the toughness of steel products. The toughness of a steel product is ensured by the configuration of the microstructure. The inventors of the present disclosure took samples from the 1/4t portion of a steel product after hot rolling and accelerated cooling, and carried out Charpy impact test, and observed the microstructures. As a result, it was found that, in a steel product exhibiting a Charpy impact absorption energy of 150 J or more at -110°C, the total of the area ratios of lower bainite and martensite is 15.0% or more and the area ratio of the residual austenite is less than 1.7%. Note that the total of the area ratios of lower bainite and martensite was measured by using EBSD. Note that the area ratio of the residual austenite was measured by X-ray diffraction. The volume ratio of the residual austenite measured by the X-ray diffraction may be considered to be the area ratio.
  • Moreover, the inventors of the present disclosure carried out studies in order to ensure the toughness of steel products. The toughness of a steel product is ensured by making the region, at which the difference in crystal orientation is 15° or more and which is surrounded by a high angle grain boundary, small. The inventors of the present disclosure took samples from the 1/4t portion of a steel product manufactured by controlling the cooling rate and the cooling stoppage temperature after hot rolling, and measured the circle equivalent diameter of the region surrounded by a high angle grain boundary by EBSD. The circle equivalent diameter of the region surrounded by a high angle grain boundary is called the crystal grain diameter hereinafter. The sample was subjected to mechanical polishing and electrolytic polishing, and analysis was carried out on a 4 mm2 region by an EBSD device equipped with an FE-SEM (field emission scanning electron microscope). The value calculated by an area weighted average that was weighted by the area per crystal grain among the crystal grain diameters measured in the 4 mm2 region, was used as the average crystal grain diameter (also called "effective crystal grain diameter" upon occasion). It was learned that, if the average crystal grain diameter of a 1/4t portion of a steel product is 20.0 µm or less, there is the tendency for the toughness of the steel product to improve more regardless of whether before or after a post weld heat treatment.
  • Further, the inventors of the present disclosure have found that similar results can be obtained not only with steel products after hot rolling and accelerated cooling, but also with steel products after reheat quenching.
  • <Chemical Composition>
  • Alloy elements that constitute the chemical composition of the steel product relating to the present disclosure are described next. Note that, in the following description of the alloy elements, the "%" of the content means "mass%".
  • (C: 0.03% or more and 0.20% or less)
  • C is an element that improves the strength of the steel product. From the standpoint of ensuring the strength of the steel product that is used in a structure, in the present disclosure, the C content is 0.03% or more. The C content is preferably 0.05% or more, or 0.07% or more. On the other hand, C is an element that reduces toughness, and, from the standpoint of ensuring the toughness of the heat affected zone (hereinafter called "HAZ" upon occasion), in the present disclosure, the C content is 0.20% or less. The C content is preferably 0.16% or less, 0.14% or less, or 0.12% or less.
  • (Si: 0.01% or more and 0.50% or less)
  • Si is an element that is used as a deoxidizing agent, and further, that dissolves into the steel and increases the strength. From the standpoint of controlling the O concentration contained in molten steel, in the present disclosure, the Si content is 0.01% or more. The Si content is preferably 0.03% or more, 0.05% or more, 0.10% or more, or 0.12% or more. On the other hand, if the Si content is excessive, there are cases in which a hard phase forms in the HAZ, and the toughness decreases. Accordingly, from the standpoint of ensuring the toughness of the HAZ, in the present disclosure, the Si content is 0.50% or less. The Si content is preferably 0.30% or less, or 0.20% or less.
  • (Mn: 0.10% or more and 2.00% or less)
  • Mn is an element that is used as a deoxidizing agent, and further, that improves the hardenability of the steel and contributes to increasing the strength. From the standpoint of controlling the O concentration contained in molten steel, in the present disclosure, the Mn content is 0.10% or more. Moreover, due to Mn in an amount of 0.10% or more, by forming MnS, the solid-solution S is reduced, and hot cracking is prevented. From the standpoint of ensuring the strength of the steel product and the toughness of the HAZ, the Mn content is preferably 0.30% or more, or 0.50% or more. On the other hand, if the Mn content is excessive, there are cases in which the toughness after PWHT decreases due to the Mn segregating at the grain boundary at the time of PWHT. Accordingly, from the standpoint of ensuring the toughness of the steel product after PWHT, in the present disclosure, the Mn content is 2.00% or less. The Mn content is preferably 1.80% or less, or 1.50% or less.
  • (P: 0.025% or less)
  • P is an impurity element. Although the lower limit of the P content is not limited, from the standpoint of the manufacturing cost, in the present disclosure, the P content may be 0.001% or more. On the other hand, if the P content is excessive, there are cases in which the toughness after PWHT decreases due to the P segregating at the grain boundary at the time of PWHT. Accordingly, in the present disclosure, the P content is 0.025% or less. The P content is preferably 0.016% or less, 0.012% or less, or 0.008% or less.
  • (S: 0.0250% or less)
  • S is an impurity element. Although the lower limit of the S content is not limited, from the standpoint of the manufacturing cost, in the present disclosure, the S content may be 0.0001% or more. On the other hand, if the S content is excessive, there are cases in which elongated MnS is generated at the centerline segregation area, and the toughness and ductility of the steel product and the HAZ deteriorate. From the standpoint of ensuring the toughness and ductility of the steel product and the HAZ, the S content is 0.0250% or less. The S content is preferably 0.0100% or less or 0.0050% or less.
  • (Ni: 4.51% or more and 6.10% or less)
  • Ni is an element that is effective in improving the hardenability and toughness of the steel. Therefore, in the present embodiment, the Ni content is 4.51% or more. The Ni content is preferably 5.00% or more, or 5.25% or more. However, Ni is an expensive element, and, from the standpoint of cost reduction, in the present disclosure, the Ni content is 6.10% or less. The Ni content is preferably 6.00% or less, or 5.75% or less.
  • (Al: 0.001% or more and 0.100% or less)
  • Al is an element that is effective in deoxidation, and is an element that, by forming a nitride, refines the crystal grain diameter at the time of quenching. Therefore, in the present disclosure, the Al content is 0.001% or more. However, if Al is excessively contained, there is the concern that the Al will generate a coarse nitride, and the toughness of the steel product and the HAZ will decrease. Accordingly, the Al content is 0.100% or less. The Al content is preferably 0.080%, or 0.050% or less.
  • (O: 0.0100% or less)
  • O is an impurity element. Although the lower limit of the O content is not limited, from the standpoint of the manufacturing cost, in the present disclosure, the O content may be 0.0001% or more. On the other hand, if the O content is excessive, there are cases in which a coarse oxide is generated, and the toughness and ductility of the steel product and the HAZ deteriorate. From the standpoint of ensuring the toughness and ductility of the steel product and the HAZ, the O content is 0.0100% or less. The O content is preferably 0.0060% or less, or 0.0040% or less.
  • (N: 0.0100% or less)
  • N is an impurity element. Although the lower limit of the N content is not limited, from the standpoint of the manufacturing cost, in the present disclosure, the N content may be 0.0001% or more. From the standpoint of ensuring the properties of the steel product and the toughness of the HAZ, in the present disclosure, the N content is 0.0100% or less. The N content is preferably 0.0050% or less, or 0.0040% or less.
  • The steel product relating to the present disclosure may contain other elements (optional elements) instead of some of the Fe. The following optional elements are given as examples, but the contents of these elements may be 0%.
  • In order to improve the strength and toughness, as needed, the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Cu, Cr, Mo, and B that are described hereinafter and have the effect of improving the hardenability.
  • (Cu: 1.50% or less)
  • Cu is an element that is sometimes mixed into the steel product in the manufacturing process. However, the lower limit value of the Cu content is not limited and may be 0%. Further, Cu has little adverse effect on the weldability and on the toughness of the HAZ, and has the effect of improving the hardenability of steel, and therefore, is an element that improves the strength of the steel product. Thus, in the present disclosure, the Cu content may be 0.01% or more. The Cu content is preferably 0.10% or more. However, from the standpoint of suppressing the occurrence of Cu cracking at the time of hot rolling of the steel product, in the present disclosure, the Cu content is 1.50% or less. The Cu content is preferably 1.00% or less, 0.80% or less, 0.60% or less, or 0.50% or less.
  • (Cr: 3.00% or less)
  • Cr is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Cr content is not limited, and may be 0%. Further, Cr is also an element that improves the strength of a steel product because it has the effect of increasing the hardenability of the steel. Therefore, in the present disclosure, the Cr content may be 0.01% or more. The Cr content is preferably 0.10% or more. However, from the standpoint of suppressing deterioration in the toughness and weldability of the HAZ, in the present disclosure, the Cr content is 3.00% or less. The Cr content is preferably 2.20% or less, 1.40% or less, or 0.80% or less.
  • (Mo: 2.00% or less)
  • Mo is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Mo content is not limited, and may be 0%. Further, Mo is also an element that improves the strength of a steel product because it has the effect of increasing the hardenability of the steel. Therefore, in the present disclosure, the Mo content may be 0.01% or more. The Mo content is preferably 0.05% or more, 0.10% or more, 0.20% or more or 0.30% or more. However, from the standpoints of suppressing deterioration in the toughness and weldability of the HAZ, and suppressing an increase in the alloy cost, in the present disclosure, the Mo content is 2.00% or less. The Mo content is preferably 1.20% or less, or 0.80% or less.
  • (B: 0.0050% or less)
  • B is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the B content is not limited, and may be 0%. Further, B is also an element that exhibits a marked effect of increasing the hardenability of steel and improves the strength of a steel product. Therefore, in the present disclosure, the B content may be 0.0003% or more. However, from the standpoint of suppressing deterioration in the surface quality of a steel slab manufactured in continuous casting, in the present disclosure, the B content is 0.0050% or less. The B content is preferably 0.0030% or less, or 0.0020% or less.
  • In order to improve the strength, as needed, the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Nb, Ti, and V that are described hereinafter and have the effect of increasing the strength of the steel product by precipitates such as carbides or nitrides.
  • (Nb: 0.050% or less)
  • Nb is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Nb content is not limited, and may be 0%. Further, Nb is also an element that forms a carbide or a nitride, and has the effect of refining the microstructure, and improves the strength of the steel product. Therefore, in the present disclosure, the Nb content may be 0.001% or more. However, from the standpoint of suppressing deterioration in the toughness and weldability of the HAZ, the Nb content is 0.050% or less. The Nb content is preferably 0.040% or less, or 0.030% or less. In particular, from the standpoint of ensuring the toughness of the steel product after PWHT, the Nb content may be 0.004% or less.
  • (Ti: 0.050% or less)
  • Ti is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Ti content is not limited, and may be 0%. Further, Ti is also an element that forms a carbide or a nitride, and has the effect of refining the microstructure, and improves the strength of the steel product. Therefore, in the present disclosure, the Ti content may be 0.001% or more. However, from the standpoint of suppressing deterioration in the toughness and weldability of the HAZ, the Ti content is 0.050% or less. The Ti content is preferably 0.040% or less, or 0.030% or less. In particular, from the standpoint of ensuring the toughness of the steel product after PWHT, the Ti content may be 0.004% or less, or 0.002% or less.
  • (V: 0.10% or less)
  • V is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the V content is not limited, and may be 0%. Further, V is also an element that forms a carbide or a nitride, and improves the strength of the steel product. Therefore, in the present disclosure, the V content may be 0.01% or more. However, from the standpoints of suppressing deterioration in the toughness and weldability of the HAZ, and suppressing an increase in the alloy cost, the V content is 0.10% or less. The V content is preferably 0.08% or less, or 0.05% or less.
  • In order to improve the toughness of the HAZ, as needed, the steel product relating to the present disclosure may be made to contain one or two or more of the optional elements Mg, Ca, and REM that are described hereinafter.
  • (Mg: 0.0200% or less)
  • Mg is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Mg content is not limited, and may be 0%. Further, Mg is also an element that forms an oxide and improves the toughness of the heat affected zone. Therefore, in the present disclosure, the Mg content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more. On the other hand, if the Mg content is excessive, there are cases in which the Mg forms a coarse oxide and decreases the toughness of the steel. Accordingly, from the standpoint of ensuring the toughness, in the present disclosure, the Mg content is 0.0200% or less. The Mg content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • (Ca: 0.0200% or less)
  • Ca is an element that is sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the Ca content is not limited, and may be 0%. Further, Ca is also an element that, by spheroidizing the sulfide within the steel product, mitigates the effect of the MnS that decreases the toughness of the steel product and the heat affected zone. Therefore, in the present disclosure, the Ca content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more. On the other hand, if the Ca content is excessive, there are cases in which the Ca forms a coarse oxide and decreases the toughness of the steel. Accordingly, from the standpoint of ensuring the toughness, in the present disclosure, the Ca content is 0.0200% or less. The Ca content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • (REM: 0.0200% or less)
  • Rare earth metal (REM) is a collective term for a total of 17 elements that are the two elements of Sc and Y and fifteen lanthanoid elements such as La, Ce, Nd. The REM content means the total content of the aforementioned 17 elements. REMs are elements that are sometimes mixed into a steel product in the manufacturing process. However, the lower limit value of the REM content is not limited, and may be 0%. Further, REMs are also elements that form oxides and improve the toughness of the heat affected zone. Therefore, in the present disclosure, the REM content may be 0.0003% or more, 0.0006% or more, or 0.0010% or more. On the other hand, if the REM content is excessive, there are cases in which the REMs form coarse oxides and decrease the toughness of the steel. Accordingly, from the standpoint of ensuring the toughness, in the present disclosure, the REM content is 0.0200% or less. The REM content is preferably 0.0100% or less, 0.0060% or less, or 0.0040% or less.
  • (Balance: Fe and Impurities)
  • The balance of the chemical composition of the steel product relating to the present disclosure is iron (Fe) and impurities. Impurities mean components that are mixed due to raw materials such as ore and scrap, and other factors, at the time of industrially manufacturing the steel product.
  • In addition to the limits on the contents of the respective elements, in the present disclosure, the range of value α is limited as follows.
  • (Value α: 5.0 or more and 16.0 or less)
  • Value α is computed by following formula (1). α = 0.50 × √[C] × (1+0.64[Si]) × (1+4.10[Mn]) × (1+0.27[Cu]) × (1+0.52[Ni]) × (1+2.33[Cr]) × (1+3.14[Mo])
  • Wherein [C], [Si], [Mn], [Cu], [Ni], [Cr] and [Mo] are the contents (mass%) of C, Si, Mn, Cu, Ni, Cr and Mo in the steel. In a case in which a given element is not contained, zero is substituted in. Note that √[C] has the same meaning as [C]1/2.
  • In the present disclosure, the range of value α is 5.0 - 16.0. This is an index expressing the hardenability of the steel product. The greater the value α, the more that lower bainite and martensite microstructures having a superior balance of strength and toughness can be formed. When α is in the appropriate range, in the microstructure of the HAZ as well, the ratio of the lower bainite and martensite microstructures having a superior balance of strength and toughness becomes high, and the HAZ toughness also can be ensured. When α is 5.0 or more, the hardenability of the base metal is ensured, and the ratio of the lower bainite and martensite having a favorable balance of strength and toughness increases, and a deterioration in toughness is suppressed. Further, in the microstructure of the HAZ as well, it is easy for the ratio of the lower bainite and martensite to increase, and the HAZ toughness also improves. On the other hand, if value α is 16.0 or less, toughness can be ensured without the strength of the steel product becoming too high. Further, when value α is 16.0 or less, the toughness after PWHT also can be ensured. Moreover, the HAZ toughness also is ensured without the HAZ becoming too hard.
  • Due to the aforementioned numerical value range relating to value α being satisfied, there can be provided a nickel-containing steel product for low temperatures that has excellent strength and toughness. Value α is preferably 5.5 or more, 6.0 or more, or 7.0 or more. Further, value α is preferably 15.5 or less or 15.0 or less.
  • <Microstructure>
  • The microstructure of the steel product relating to the present disclosure is described next. The microstructure of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product relating to the present disclosure contains lower bainite and martensite. Further, in addition to lower bainite, upper bainite also may be contained as bainite.
  • "Bainite" is a collective term for upper bainite and lower bainite. "Upper bainite" is one of or both of upper bainite that contains residual austenite or an MA phase (martensite-austenite mixed phase) between the laths, and upper bainite that contains a carbide between the laths. "Lower bainite" is lath-shaped lower bainite containing a carbide within the laths.
  • There are four forms of "martensite" that are lath, butterfly, lenticular and plate-shaped, but mainly lath martensite is generated in the components of the present disclosure. Lath martensite is a microstructure that is composed of packets and blocks formed from groups of laths having a specific arrangement, and in which a single austenite grain is divided into plural packets.
  • (Total of Area Ratios of Lower Bainite and Martensite: 15.0% or more)
  • Lower bainite and martensite are hard phases and increase the toughness of the steel product. From the standpoint of ensuring the toughness of the steel product, the area ratio of lower bainite and martensite at the 1/4t portion is 15.0% or more. The area ratio of lower bainite and martensite at the 1/4t portion is preferably 20.0% or more, or 30.0% or more. The total of the area ratio of the lower bainite and the area ratio of the martensite at the 1/4t portion may be 100%.
  • (Total of Area Ratios of Upper Bainite, Lower Bainite, and Martensite: 90.0% or more)
  • From the standpoint of ensuring the strength of the steel product, the total of the area ratios of upper bainite and lower bainite and martensite at the 1/4t portion is 90.0% or more. The total of the area ratios of upper bainite, lower bainite and martensite at the 1/4t portion may be 100%. Further, the upper bainite of the 1/4t portion may be 1.0% or more.
  • (Area Ratio of Residual Austinite: less than 1.7%)
  • From the standpoint of ensuring the toughness of the steel product, the area ratio of the residual austenite of the 1/4t portion is less than 1.7%. The area ratio of the residual austenite of the 1/4t portion is preferably 1.0% or less, and may be 0%. This is thought to be because, in the Ni-containing, steel plate of the present disclosure, the Ni content is lower than conventional 9% Ni steel, and therefore, even if residual austenite were to exist at -110°C, it would be unstable, and, if the steel structure were to incur plastic deformation at the crack tip, the residual austenite would change into martensite due to plasticity-induced martensitic transformation. Thus, the residual austenite at room temperature is made to be less than 1.7% as a volume ratio.
  • Further, the higher the Ni content, the easier it is for the volume ratio of the residual austenite to increase as well. However, an increase in the Ni content is also not preferable in that it leads to an increase in cost.
  • Observation of the microstructure of the steel product is carried out by using a sample in which a 1/4t portion of the steel product serves as the observed surface. Two types of samples on which (a) electrolytic polishing or (b) nital etching is carried out are prepared. Each sample of (a) and (b) is measured at three places by the following method, and the average value of the three places is used as the area ratio of the microstructure of that steel product. Note that three of each sample of (a) and (b) may be prepared, and the averages of the respective samples may be computed. Or, three places of one sample of each may be measured in a visual field, and the average of each computed.
  • By using an electrolytically polished sample that, after mirror finishing by mechanical polishing, is subjected to electrolytic polishing that removes the strained layers arising due to the mechanical polishing, measurement of the total of the area ratios of the upper bainite, lower bainite, martensite and residual austenite is carried out by EBSD. The measurement magnification is 200×, and measurement of a range of 400 µm × 400 µm is carried out at a pitch of 0.4 µm. The measuring is carried out in a state in which the beam diameter of the electron beam is 0.4 µm or less. The confidence index (hereinafter called "CI value") is set to 0.1 or more. The determination of ferrite, and upper bainite, lower bainite and martensite, is carried out by setting the threshold value of the Grain Average Misorientation (hereinafter called "GAM") to 0.5. Note that the GAM value is an index defined in OIM Analysis (EBSD crystal orientation analyzing software manufactured by TSL, United States). The region in which the GAM is 0.5 or less is ferrite. The region in which the GAM exceeds 0.5 is upper bainite, lower bainite, martensite or residual austenite. Because the upper bainite, lower bainite, martensite and residual austenite in the present disclosure are determined by using the GAM of EBSD as the threshold value, not only upper bainite, lower bainite, martensite and residual austenite, but also tempered upper bainite, tempered lower bainite and tempered martensite are included. Comparing the microstructures of direct quenching (DQ) and (DQT) that is carried out thereafter up to tempering (T), although dissolution of the MA and coarsening of carbide occur after tempering, the way of looking at the microstructure does not vary greatly.
  • Measurement of the area ratio of the upper bainite by SEM observation is carried out by using a nital etched sample. The measurement magnification is 500×, and measurement of a range of 360 µm × 480 µm is carried out. The portion, which has a clear lath structure and at which carbide and MA have formed along the lath boundary, is upper bainite. The microstructure of the region, at which the internal structure of the microstructure is relatively coarse, and the density of carbide is low and both sparse and dense, is upper bainite. An example of the results of discriminating the microstructures is shown in Fig. 1. (A) and (B) are SEM images of the same region of a steel product that is manufactured by DQT and whose value α is 9.9. In (B), the regions surrounded by the white lines are upper bainite (Bu), and the other regions are lower bainite + martensite (BL+M). In the portions identified as upper bainite (Bu), carbides appearing white are sparsely distributed, and regions with varying density are present. On the other hand, at the portions identified as lower bainite + martensite (BL+M), the carbides are densely and uniformly distributed. The total of the area ratios of the lower bainite, martensite and residual austenite is determined by subtracting the area ratio of the upper bainite from the total of the area ratios of the upper bainite, lower bainite, martensite and residual austenite, which were measured as described above. Moreover, the area ratio of the residual austenite is determined by the measuring method described hereinafter, and the total of the area ratios of the lower bainite and martensite is determined by subtracting the area ratio of the residual austenite from the total of the area ratios of the lower bainite, martensite and residual austenite.
  • (Area Ratio of Residual Austenite)
  • The area ratio of the residual austenite is measured by X-ray diffraction. Measurement of the area ratio of the residual austenite is carried out by using a sample at which the region, which is 1/4 of the thickness in the thickness direction from the surface of the steel product (also called "1/4t portion" in the present specification), is the measured area. The sample is a 2-mm thick test piece, and is taken from a position that is 1/4 of the width from a width direction end portion of the steel product, and chemical polishing is carried out thereon, and the sample is used in measuring the volume ratio of the residual austenite by X-ray diffraction using an Mo tube. Quantification is carried out on the basis of the ratios of the integrated intensities of the (200), (211) diffraction peaks of the ferrite phase and the integrated intensities of the (200), (220), (311) diffraction peaks of the austenite phase, and the average values of the six combinations are employed. The integrated intensities of the diffraction peaks are determined by fitting the backgrounds on the basis of the signals before and after the peaks, and subtracting the signal differences. The volume ratio measured by the X-ray diffraction is considered to be the area ratio.
  • (Average Crystal Grain Diameter of 1/4t Portion of Steel Product)
  • In the present disclosure, the average crystal grain diameter (effective crystal grain diameter) of the 1/4t portion of the steel product is preferably 20.0 µm or less. This is because it was learned that, if the average crystal grain diameter of the 1/4t portion of the steel product is 20.0 µm or less, the toughness of the steel product tends to improve even more regardless of whether before or after PWHT. However, the average crystal grain diameter of the 1/4t portion of the steel product may exceed 20.0 µm. The smaller the average crystal grain diameter of the steel product, the more preferable, and therefore, the lower limit value thereof is not limited. Usually, the average crystal grain diameter is 10 µm or more. The effective crystal grain diameter is determined by a weighted average. Effective crystal grain diameter Darea that is determined by a weighted average is calculated by the following formula by using, of the crystal grain diameters that are measured in a 4 mm2 region, area Si and grain diameter di of the ith crystal grain detected at the time of measurement. D area = ΣS i · d i / ΣS i
  • (Aspect Ratio of Prior Austenite Crystal Grains of 1/4t Portion of Steel Product)
  • The form of the prior austenite crystal grains (called prior austenite grains or prior γ grains upon occasion) of the steel product of the present disclosure may be a form that is flat in the rolling direction. If the prior austenite grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product are made to be flat grains of an aspect ratio of 1.5 or more, an even greater improvement in the toughness of the steel product is possible. This is because, by increasing the grain boundary area by making the prior austenite grains flat, there is a substantial refining of the austenite grains, and this is effective in refining the effective crystal grain diameter. The aspect ratio of prior austenite grains is usually 4.0 or less, and may be 3.5 or less.
  • On the other hand, from the standpoint of ensuring the homogeneity of the microstructure, the aspect ratio of the prior austenite crystal grains of the 1/4t portion may be less than 1.5. The aspect ratio of the prior austenite crystal grains of the 1/4t portion may be 1.4 or less, or 1.3 or less.
  • The aspect ratio of the prior austenite crystal grains (hereinafter called prior austenite grains upon occasion) of the steel product is determined as follows. An L cross-section (a cross-section parallel to the rolling direction and the thickness direction of the steel product) of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is mirror polished, and corrosion is carried out by a corrosive liquid of a saturated solution base of 2 - 4% picric acid, and the prior austenite grain boundaries of an arbitrary region of 1.0 mm in the rolling direction × 0.5 mm in the thickness direction are made to appear.
  • Next, the long diameters and short diameters of the individual prior austenite grains are measured, and the aspect ratio of each prior austenite grain is calculated by long diameter ÷ short diameter. The arithmetic mean of the calculated aspect ratios of all of the prior austenite grains is determined as the "aspect ratio of the prior austenite grains". Note that the maximum length of the prior austenite grain is used as the long diameter, and the maximum interval between two lines, which contact the grain and are parallel to the long diameter direction, is used as the short diameter.
  • <Mechanical Properties>
  • The steel product relating to the present disclosure has mechanical properties that are such that the steel product has both strength and low-temperature toughness. In addition to having excellent toughness at -110°C in particular, the steel product can exhibit excellent low-temperature toughness after PWHT as well.
  • (Tensile Strength: 615 MPa or more and 930 MPa or less)
  • In the present disclosure, the tensile strength of the steel product is 615 - 930 MPa. In order to reduce the weight of large welded structures such as transport tanks, a steel product that can ensure strength of a structure even if the thickness is thin is necessary. Because steel products that are selected as steel products to be used in such applications usually are steel products having the aforementioned tensile strength, the steel product relating to the present disclosure also is manufactured to have the aforementioned tensile strength.
  • (Yield Ratio)
  • The yield ratio (YR = [yield strength] / [tensile strength] × 100) of the steel product relating to the present disclosure is not particularly limited and is preferably 90% or less. In a case in which there is no yield point, the yield strength is determined by using 0.2% proof stress.
  • (Charpy Impact Absorption Energy at -110°C)
  • In order to ensure high toughness at low temperatures, the Charpy impact absorption energy at -110°C of the steel product of the present disclosure is preferably 150 J or more. Due to the steel product of the present disclosure having low-temperature toughness of a Charpy impact absorption energy at -110°C of 150 J or more, a transport tank formed from the steel product of the present disclosure can be suitably used for transporting liquid carbon dioxide for example. The steel product of the present disclosure may have low-temperature toughness of a Charpy impact absorption energy at -110°C of 100 J or more. Note that the Charpy impact absorption energy at -110°C is a numerical value measured by using a sample taken from a position of 1/4 of the thickness.
  • (Charpy Absorption Energy at -110°C after PWHT)
  • There are cases in which PWHT is carried out on the welded portions of cryogenic tanks after being assembled into transport tanks, in order to prevent breakage in advance. At this time, not only the welded portions, but also the base metal portion (also simply called base metal) of the steel product that is not affected by welding are heated. If the time over which the base metal is heated in the temperature range of 425°C or more is long, the toughness of the base metal tends to decrease. In the steel product of the present disclosure, in a case in which PWHT, in which the holding temperature is 600°C, and the holding time is 2 hours, and the rate of temperature increase and the rate of temperature decrease are 55°C/h in the temperature region of 425°C or more, is carried out on the steel product, with regard to the toughness of the portion where the PWHT has been carried out, the Charpy impact absorption energy at -110°C is preferably 150 J or more. The Charpy impact absorption energy at -110°C after PWHT may be 100 J or more. The Charpy impact absorption energy at -110°C after PWHT also is a numerical value measured by using a sample taken from a position of 1/4 of the thickness.
  • Note that there are cases in which the toughness of the steel product decreases due to PWHT. Although the reason for this is not clear, it is assumed that P (phosphorus) and Mn diffuse at the grain boundaries, and growth or aggregation of inclusions arises within the microstructure, and due thereto, the brittleness decreases and the toughness decreases. A decrease in the toughness due to PWHT is suppressed by limiting the contents of P and Mn and making the average crystal grain diameter of the steel product small.
  • (Charpy Impact Absorption Energy at -110°C after Thermal Cycling)
  • In the steel product of the present disclosure, in order to ensure high toughness after a thermal cycling test that simulates the welded portions at a low temperature, the Charpy impact absorption energy at -110°C after thermal cycling is preferably 50 J or more. Due to the steel product of the present disclosure having low-temperature toughness that is such that the Charpy impact absorption energy at -110°C after thermal cycling is 50 J or more, a transport tank formed from the steel product of the present disclosure can be suitably used for transporting liquid carbon dioxide for example. The Charpy impact absorption energy at -110°C after thermal cycling may be 40 J or more. Note that the Charpy impact absorption energy at -110°C after thermal cycling is a numerical value measured by using a sample taken from a position of 1/4 of the thickness of the steel product as a thermal cycling test piece, and providing it with a thermal history of raising the temperature at 60°C/s to 1350°C, and, after maintenance at 1350°C for 1 s, cooling at 20°C/s to room temperature, and thereafter, taking a Charpy test piece therefrom.
  • (Charpy Impact Absorption Energy at -110°C after Thermal Cycling and PWHT)
  • There are cases in which PWHT is carried out on the welded portions of cryogenic tanks after being assembled into transport tanks, in order to prevent breakage in advance. After the above-described thermal cycling test, PWHT, in which the rate of temperature increase and the rate of temperature decrease are 55°C/h in the temperature region of 425°C or more, and the steel product is held for 2 hours at 600°C, is carried out on the steel product of the present disclosure, and thereafter, a Charpy test piece is taken, and measurement is carried out. In this case, with regard to the toughness of the portion where the PWHT has been carried out, the Charpy impact absorption energy at -110°C is preferably 50 J or more. The Charpy impact absorption energy at -110°C of the portion at which PWHT is carried out after the above-described thermal cycling test may be 40 J or more.
  • Note that there are cases in which the toughness of the steel product decreases due to PWHT. Although the reason for this is not clear, it is assumed that P (phosphorus) and Mn diffuse at the grain boundaries, and growth or aggregation of inclusions arises within the microstructure, and due thereto, the brittleness decreases and the toughness decreases. A decrease in the toughness due to PWHT is suppressed by limiting the contents of P and Mn and making the average crystal grain diameter of the steel product small.
  • The tensile strength (TS) and the yield strength (YS) are measured in accordance with a tensile test that is based on JIS Z2241:2011. The tensile test uses a JIS14A test piece that has been taken from a position of 1/4 of the thickness and whose length direction is the direction (the C direction) parallel to the width direction of the steel product. TS and YS are computed by using three test pieces and taking the averages thereof. The yield ratio (YR, %) is computed by (YS/TS) × 100, on the basis of the respective average values of TS and YS.
  • The Charpy impact absorption energy is measured by a Charpy impact test at -110°C on the basis of the prescriptions of JIS Z2242:2018 and by using an impact blade of a radius of 2 mm. The Charpy impact absorption energy is calculated by measuring by using three test pieces, and taking the average thereof. The Charpy impact absorption energy test uses a V-notched test piece that has been taken from a position of 1/4 of the thickness of the steel product and whose length direction is the direction (the C direction) parallel to the width direction of the steel product.
  • The form of the steel product relating to the present disclosure is not particularly limited, and examples are steel plates, steel strips, structural steel and steel pipes. However, steel pipes and structural steel include steel products in which steel plates are joined, e.g., in addition to welded steel pipes and welded structural steel, structural steel joined by rivets, and the like. The thickness of the steel product such as steel plates, steel strips, structural steel and steel pipes (the thickness of the flanges in the case of structural steel) is not particularly limited, and usually is 3 mm or more and 150 mm or less. The thickness of the steel product may be 6 mm or more, 10 mm or more, 15 mm or more, or 30 mm or more. Further, the thickness of the steel product may be 100 mm or less, 80 mm or less, or 60 mm or less.
  • Further, although the application of the steel product relating to the present disclosure also is not particularly limited, the steel product relating to the present disclosure has mechanical properties such that the steel product has both strength and low-temperature toughness, and, in particular, can exhibit excellent low-temperature toughness even after PWHT. Therefore, the steel product relating to the present disclosure can be suitably used as a tank that stores and transports liquefied gasses, and liquid carbon dioxide in particular.
  • (Method of Manufacturing Steel Product)
  • The method of manufacturing the steel product relating to the present disclosure is not particularly limited, but, for example, after melting a steel that satisfies the above-described chemical composition, a steel slab is manufactured by continuous casting. The steel slab is subjected to either direct quenching (DQ), in which it is heated, hot rolled, and then directly water-cooled, or reheat quenching (RQ), in which it is hot rolled, air-cooled, reheated, and then water-cooled, to made into a steel product. Note that, in the case of RQ, the hot rolled steel does not necessarily have to be air-cooled before reheating, but water cooling may be used.
    Moreover, tempering (T) may also be carried out.
    1. (1) DQT: direct quenching (DQ) and tempering (T)
    2. (2) RQT: air cooling or water cooling, reheat quenching (RQ), and tempering (T)
    (1) DQT
  • From the standpoint of the manufacturing cost, DQT is preferable in the manufacturing of the steel product relating to the present disclosure. An example of a preferable manufacturing process is given hereinafter.
  • In the case of manufacturing the steel product relating to the present disclosure by DQ, from the standpoint of carrying out hot rolling in a temperature range in which the microstructure of the rolled steel is austenite, the heating temperature of the steel slab on which the hot rolling is carried out is Ac3 or more. From the standpoint of decreasing the deformation resistance, the heating temperature of the steel slab is preferably 1000°C or more. On the other hand, from the standpoint of suppressing coarsening of the heated γ grains, the heating temperature of the hot rolling is 1250°C or less. The heating temperature of the hot rolling is preferably 1200°C or less. Note that Ac3 is a value computed by the following formula. Ac3 = 937.2 - 436.5C + 56Si - 19.7Mn - 16.3Cu - 26.6Ni - 4.9Cr + 38.1Mo + 124.8V + 136.3Ti - 19.1Nb + 198.4Al + 3315B
  • The element symbols in the formula mean the content (mass%) of each element contained in the steel slab.
  • There are cases in which the hot rolling is structured by rolling in a temperature range in which recrystallization occurs (rolling in the recrystallization temperature range) and rolling in a temperature range in which recrystallization is suppressed (rolling in the non-recrystallization temperature range).
  • Rolling in the recrystallization temperature range is hot rolling carried out with the temperature of the rolled steel during rolling being 900°C or more. From the standpoint of refining the austenite grain diameter of the steel product, the cumulative rolling reduction ratio of the rolling in the recrystallization temperature range is preferably 20% or more, and more preferably 30% or more. The cumulative rolling reduction ratio of the rolling in the recrystallization temperature range is determined from the difference between the thickness of the steel slab before hot rolling and the thickness of the rolled steel at 900°C. Cumulative rolling reduction ratio (%) of rolling in recrystallization temperature range = 100 × ([thickness of steel slab] - [thickness of rolled steel at 900°C]) / [thickness of steel slab]
  • Rolling in the non-recrystallization temperature range is hot rolling carried out with the temperature of the rolled steel during rolling being less than 900°C. From the standpoint of refining the average crystal grain diameter of the steel product, the cumulative rolling reduction ratio of the rolling in the non-recrystallization temperature range is preferably 20% or more, and more preferably 30% or more. The cumulative rolling reduction ratio of the rolling in the non-recrystallization temperature range is determined from the difference between the thickness of the rolled steel at 900°C and the thickness of the steel product after rolling ends. Cumulative rolling reduction ratio (%) of rolling in non-recrystallization temperature range = 100 × ([thickness of rolled steel at 900°C] - [thickness of steel product after rolling ends]) / [thickness of rolled steel at 900°C]
  • From the standpoint of suppressing the generation of ferrite that decreases strength, the end temperature of the hot rolling is Ar3 or more. After hot rolling ends, accelerated cooling such as water cooling is carried out on the steel product. From the standpoint of suppressing the generation of ferrite that decreases strength, the start temperature of the accelerated cooling is Ar3 or more. Note that Ar3 is a value computed by the following formula. Ar 3 = 910 310 C 80 Mn 20 Cu 15 Cr 55 Ni 80 Mo + 0.35 t 8
  • The element symbols in the formula mean the content (mass%) of each element contained in the steel product, and t means the thickness (mm) of the steel product.
  • From the standpoint of promoting bainitic transformation and martensitic transformation, the cooling rate is 1.0°C/s or more. The cooling rate of the accelerated cooling is preferably 5.0°C/s or more, or 10.0°C/s or more. The faster the cooling rate of the accelerated cooling, the more preferable, but from standpoints such as cost and homogeneity of the accelerated cooling, the cooling rate is preferably 50.0°C/s or less, or 30.0°C/s or less. The cooling rate is a value obtained by calculating the cooling rate at a position of 1/4 of the thickness by simulation in accordance with thermal transfer calculation.
  • From the standpoint of improving the strength of the steel product by ensuring the upper bainite, lower bainite and martensite, the stoppage temperature of the accelerated cooling is 400°C or less. The stoppage temperature of the accelerated cooling is preferably 350°C or less. Accelerated cooling may be carried out to room temperature. From the standpoint of dehydrogenation of the steel product, the stoppage temperature is preferably 100°C or more.
  • After accelerated cooling, a tempering treatment may be carried out on the steel product. From the standpoint of suppressing a decrease in strength, the heating temperature of the tempering treatment is preferably 650°C or less, 620°C or less, or 590°C or less. On the other hand, from the standpoint of improving the toughness, the heating temperature of the tempering treatment is preferably 350°C or more, or 400°C or more.
  • (2) RQT
  • In a case in which the steel product relating to the present disclosure is manufactured by RQ, the effects of the heating temperature and the rolling reduction ratio of the steel slab at the time of the hot rolling on the mechanical properties of the steel product are small. However, if the heating temperature of the steel slab is too low, the deformation resistance increases, and therefore, the heating temperature of the steel slab is preferably 1000°C or more. Further, if the rolling reduction ratio is insufficient, there are cases in which initial stage defects from the time of manufacturing the steel slab remain at the thickness central portion, and the quality of the steel product decreases. Therefore, the total of the rolling reduction ratios of hot rolling (also called cumulative rolling reduction ratio) is preferably 35% or more. After the hot rolling, the steel slab may, as is, be water-cooled or air-cooled.
  • After the hot rolling, reheat quenching is carried out on the steel product. The reheating temperature of the steel product is Ac3 or more, because quenching is carried out from an austenite single-phase microstructure. From the standpoint of ensuring the homogeneity of the microstructure, the reheating temperature of the steel product is preferably 750°C or more, 850°C or more, 880°C or more, or 900°C or more. On the other hand, although the upper limit temperature of the reheating temperature is not particularly stipulated, there are cases in which excessive heating to a high temperature leads to coarsening of the austenite grains and a decrease in toughness, and therefore, the upper limit temperature of the reheating temperature is preferably 1000°C or less, 950°C or less, or 930°C or less.
  • After the reheat quenching, a tempering treatment may be carried out on the steel product. From the standpoint of suppressing a decrease in strength, the heating temperature of the tempering treatment is preferably 660°C or less, or 640°C or less. On the other hand, from the standpoint of improving the toughness, the heating temperature of the tempering treatment is preferably 400°C or more, 450°C or more, or 500°C or more.
  • EXAMPLES
  • The steel product relating to the present disclosure is described concretely hereinafter by way of Examples. However, the conditions in the following Examples are examples of conditions that are employed in order to confirm the feasibility and the effects of the present disclosure, and the present disclosure is not limited to the following Examples.
  • <Manufacturing by Direct Quenching and Tempering> [Manufacturing of Steel Product]
  • First, slabs having the chemical compositions shown in Table 1 were cast by continuous casting. The balance, which is other than the components listed in Table 1, is Fe and impurities. Further, blank cells mean that the alloy elements were not intentionally added in the steelmaking process. The underlines mean that the value is outside of the scope of the present disclosure. [Table 1]
    No. chemical composition (mass%)
    C Si Mn P S Ni Al N O Ti Nb Mg Ca REM Cu Cr Mo V B α
    2A 0.14 0.14 1.81 0.011 0.0060 5.95 0.033 0.0019 0.0022 7.0
    3A 0.14 0.18 1.45 0.012 0.0071 5.52 0.030 0.0021 0.0024 0.004 0.004 0.06 5.6
    4A 0.11 0.19 1.47 0.004 0.0041 5.73 0.005 0.0018 0.0025 0.002 0.0013 0.04 5.2
    6A 0.06 0.13 0.66 0.006 0.0029 5.88 0.036 0.0073 0.0018 0.001 0.003 0.56 0.42 0.15 6.7
    7A 0.06 0.18 1.07 0.006 0.0024 5.62 0.029 0.0021 0.0015 0.22 0.18 0.0003 6.8
    8A 0.15 0.26 1.20 0.008 0.0021 5.88 0.026 0.0027 0.0019 0.0023 0.20 0.11 7.7
    9A 0.17 0.22 1.40 0.007 0.0027 5.90 0.020 0.0030 0.0022 0.15 0.05 7.8
    10A 0.08 0.13 0.62 0.005 0.0015 5.52 0.029 0.0019 0.0036 0.47 0.20 0.51 0.0005 9.0
    11A 0.12 0.15 0.80 0.005 0.0026 5.27 0.034 0.0071 0.0041 0.0014 0.0011 0.60 0.76 9.8
    12A 0.10 0.12 0.75 0.006 0.0019 5.71 0.055 0.0039 0.0022 0.002 0.0014 0.32 0.43 0.02 11.3
    13A 0.07 0.17 0.73 0.006 0.0032 5.44 0.046 0.0043 0.0028 0.002 0.54 0.46 12.4
    14A 0.08 0.13 0.98 0.011 0.0116 5.21 0.056 0.0021 0.0015 0.65 0.43 0.25 12.0
    15A 0.06 0.17 0.73 0.009 0.0032 5.44 0.046 0.0043 0.0028 0.002 0.33 0.43 0.52 0.02 11.9
    16A 0.05 0.13 1.15 0.008 0.0075 5.35 0.034 0.0025 0.0019 0.002 0.0010 0.44 0.39 0.33 11.4
    17A 0.11 0.12 1.28 0.007 0.0053 5.83 0.006 0.0063 0.0019 0.40 0.43 0.10 13.1
    19A 0.07 0.06 1.31 0.009 0.0044 5.11 0.038 0.0038 0.0027 0.003 0.0012 1.03 13.6
    20A 0.09 0.11 0.85 0.010 0.0065 5.33 0.029 0.0031 0.0015 0.43 0.71 0.22 13.6
    21A 0.11 0.07 1.26 0.007 0.0038 5.30 0.035 0.0035 0.0022 0.003 0.44 0.22 13.7
    22A 0.08 0.13 0.80 0.006 0.0056 5.12 0.025 0.0028 0.0017 0.002 0.0013 0.43 0.71 0.35 14.9
    24A 0.14 0.14 1.69 0.013 0.0064 5.85 0.029 0.0020 0.0019 0.003 6.5
    25A 0.05 0.05 0.33 0.008 0.0018 5.80 0.006 0.0028 0.0021 1.63 0.0011 5.2
    26A 0.10 0.19 1.12 0.014 0.0008 5.44 0.029 0.0048 0.0029 0.002 0.003 0.0020 0.0014 0.74 12.6
    28A 0.15 0.07 1.80 0.012 0.0019 5.25 0.074 0.0034 0.0023 0.15 0.23 0.25 18.0
    30A 0.06 0.13 1.45 0.007 0.0051 6.34 0.025 0.0028 0.0017 0.002 0.0010 0.43 0.71 0.35 24.6
    31A 0.05 0.12 2.43 0.013 0.0009 5.30 0.028 0.0023 0.0019 0.10 0.15 0.27 12.7
    32A 0.10 0.13 0.87 0.008 0.0022 4.98 0.022 0.0031 0.0033 0.0012 0.22 0.42 0.29 0.02 11.2
    101A 0.08 0.05 1.32 0.014 0.0036 4.78 0.004 0.0021 0.0033 0.011 0.20 0.28 0.03 6.5
    102A 0.14 0.08 1.41 0.008 0.0041 5.45 0.032 0.0018 0.0024 5.1
    103A 0.11 0.15 1.50 0.009 0.0053 5.11 0.034 0.0032 0.0019 0.008 0.023 0.0061 0.23 8.2
    104A 0.08 0.09 1.34 0.007 0.0022 4.91 0.027 0.0024 0.0018 0.0046 0.40 0.36 0.25 12.6
    105A 0.09 0.07 1.22 0.005 0.0037 5.47 0.032 0.0031 0.0036 0.014 0.23 0.23 0.31 11.6
    106A 0.11 0.05 0.95 0.006 0.0018 5.87 0.025 0.0039 0.0027 0.0044 0.45 0.17 0.42 0.0010 12.3
    107A 0.10 0.15 0.89 0.007 0.0023 5.05 0.031 0.0041 0.0025 0.28 0.33 0.46 13.6
    108A 0.08 0.11 1.17 0.008 0.0016 5.35 0.028 0.0024 0.0034 0.009 0.35 0.46 0.34 15.6
    109A 0.09 0.07 1.34 0.004 0.0034 5.81 0.025 0.0019 0.0018 0.030 0.44 0.21 0.37 14.7
    110A 0.11 0.17 1.32 0.011 0.0034 5.74 0.026 0.0027 0.0027 0.003 0.32 8.2
    111A 0.08 0.17 1.50 0.006 0.0044 5.30 0.031 0.0032 0.0022 0.0005 0.37 9.1
    112A 0.07 0.08 1.22 0.007 0.0026 4.99 0.028 0.0024 0.0017 0.0005 0.35 0.30 0.24 9.8
    113A 0.12 0.05 0.98 0.005 0.0015 5.77 0.033 0.0039 0.0025 0.0005 0.40 0.10 0.36 10.4
    114A 0.08 0.13 1.05 0.012 0.0036 5.21 0.033 0.0026 0.0018 0.03 3.3
    115A 0.07 0.15 1.24 0.009 0.0028 5.46 0.029 0.0021 0.0022 0.04 3.7
    116A 0.12 0.09 1.73 0.011 0.0025 5.67 0.032 0.0028 0.0028 0.13 0.25 0.26 17.4
    117A 0.17 0.12 1.89 0.014 0.0028 5.43 0.034 0.0031 0.0022 0.17 0.23 0.17 18.3
    118A 0.08 0.11 1.32 0.006 0.0051 5.12 0.033 0.0025 0.0026 0.004 0.19 5.1
  • Next, steel products were manufactured from these slabs under the manufacturing conditions listed in Table 2. "Temper heat treatment" is the heating temperature in the tempering treatment after the quenching. [Table 2]
    No. plate thickness (mm) Ac3 [°C] hot rolling conditions Ar3 [°C] direct quenching (accelerated cooling) conditions Temper heat treatment [°C]
    heating temperature [°C] cumulative rolling reduction [%] ratio at 900°C or more cumulative rolling reduction ratio [%] at less than 900°C end temperature [°C] cooling after rolling start temperature [°C] stoppage temperature [°C] cooling rate [°C/s]
    2A 35 697 1230 23 60 820 water cooling 404 800 180 9.5 510
    3A 25 725 1150 30 50 810 water cooling 453 800 160 5.3 540
    4A 15 725 1150 31 59 790 water cooling 446 770 150 5.7 640
    6A 35 751 1130 31 45 770 water cooling 495 750 270 12.2 610
    7A 60 763 1170 32 30 780 water cooling 497 760 290 2.9 600
    8A 40 712 1200 19 65 810 water cooling 443 790 250 3.1 610
    9A 20 694 1100 22 43 775 water cooling 418 750 220 4.1 590
    10A 35 769 1240 34 44 750 water cooling 488 720 115 3.3 580
    11A 20 731 1150 38 45 730 water cooling 500 715 320 4.2 510
    12A 50 762 1020 39 33 820 water cooling 480 800 360 2.7 570
    13A 55 781 1080 42 31 770 water cooling 502 745 220 10.7 610
    14A 60 760 1070 37 38 740 water cooling 499 710 240 3.7 620
    15A 40 786 1200 25 45 740 water cooling 490 722 320 4.5 605
    16A 55 768 1100 44 37 760 water cooling 484 748 180 6.3 560
    17A 50 712 1160 32 29 820 water cooling 445 800 210 4.2 530
    19A 55 795 1080 33 38 760 water cooling 437 725 290 5.4 560
    20A 50 749 1100 36 31 840 water cooling 499 815 105 2.2 480
    21A 35 741 1200 38 50 800 water cooling 469 784 243 2.9 490
    22A 40 765 1100 30 40 790 water cooling 504 779 219 3.6 590
    24A 57 701 1200 35 13 780 water cooling 427 756 320 5.4 490
    25A 55 754 1130 12 35 790 water cooling 541 778 290 7.8 460
    26A 60 772 1200 32 11 740 water cooling 449 730 240 4.6 560
    28A 55 721 1120 33 36 720 water cooling 421 700 270 4.3 550
    30A 40 729 1150 35 38 750 water cooling 391 730 220 7.4 560
    31A 61 747 1200 32 41 780 water cooling 401 753 227 4.1 550
    32A 50 763 1100 28 29 840 water cooling 516 820 105 0.5 490
    101A 50 765 1150 58 60 810 water cooling 505 790 310 12.5 510
    102A 40 714 1200 60 60 820 water cooling 465 800 283 13.1 460
    103A 70 748 1100 50 53 790 water cooling 478 778 216 7.9 610
    104A 53 757 1170 60 56 780 water cooling 490 764 189 15.2 550
    105A 45 747 1150 55 58 790 water cooling 464 768 223 10.5 420
    106A 40 733 1200 58 67 810 water cooling 443 792 196 6.9 580
    107A 50 768 1100 49 59 770 water cooling 497 746 143 7.9 480
    108A 55 755 1070 60 54 790 water cooling 473 774 178 15.7 500
    109A 48 731 1200 56 63 800 water cooling 428 769 221 18.3 530
    110A 57 724 1200 12 56 810 water cooling 467 788 343 14.2 470
    111A 55 762 1200 55 58 810 water cooling 461 793 230 10.2 530
    112A 45 762 1100 55 61 820 water cooling 499 806 312 12.5 420
    113A 65 728 1150 52 55 790 water cooling 459 776 187 6.8 620
    114A 40 758 1200 43 40 780 water cooling 523 765 253 12.1 580
    115A 50 751 1100 37 45 790 water cooling 503 778 344 10.9 470
    116A 55 718 1150 60 50 810 water cooling 412 722 293 8.4 580
    117A 60 697 1050 50 40 800 water cooling 405 740 365 9.8 560
    118A 40 752 1100 39 45 780 water cooling 506 430 341 9.8 520
  • [Measurement and Evaluation]
  • The microstructures and mechanical properties of the obtained steel products were measured by the above-described methods. The results are shown in Table 3. The meanings of the symbols of the microstructures are as follows. Note that the remainders of the microstructures were pearlite, MA phase, and ferrite.
    • Bu: upper bainite
    • BL: lower bainite
    • M: martensite
    • residual y: residual austenite
  • For the toughness, the average value of the Charpy impact absorption energy at -110°C, and the average value of the Charpy impact absorption energy at -110°C after PWHT in which the holding temperature was 600°C, the holding time was 2 hours, and the rate of temperature increase and the rate of temperature decrease in the temperature region of 425°C or more were 55°C/h, respectively were measured. [Table 3]
    No. microstructure (area ratio) aspect ratio average value of prior γ grains average crystal grain diameter [µm] YS [MPa] TS [MPa] YR [%] base metal toughness KV2[J] toughness after PWHT KV2[J] thermal cycling toughness KV2[J] toughness after thermal cycling and PWHT KV2 [J] notes
    BL+M [%] Bu+BL+M [%] residual γ [%]
    2A 27.4 92.3 0.1 2.9 22.6 564 643 88 189 151 examples of present invention
    3A 22.4 92.6 0.0 2.8 17.1 534 623 86 239 196
    4A 22.8 94.1 0.1 2.6 16.7 510 624 82 239 221
    6A 35.1 92.4 0.2 3.1 17.4 568 653 87 243 225
    7A 35.7 92.8 0.3 3.3 15.6 563 661 85 312 319
    8A 33.1 92.1 0.2 3.0 23.9 582 672 87 189 188
    9A 38.4 94.3 0.2 3.2 21.6 576 678 85 179 180
    10A 50.8 94.3 0.5 2.8 13.3 615 729 84 288 285
    11A 55.1 95.2 0.4 2.7 14.8 631 765 82 282 280
    12A 65.9 93.4 0.7 3.2 12.4 659 774 85 285 268
    13A 68.3 96.1 0.4 3.4 11.3 661 759 87 312 297
    14A 65.4 93.9 0.5 3.2 16.5 668 752 89 228 222
    15A 64.2 95.8 0.4 3.1 15.3 665 765 87 242 221
    16A 61.9 95.1 0.3 3.0 17.1 658 748 88 229 211
    17A 91.7 96.0 0.6 3.1 17.4 723 834 87 242 239
    19A 98.1 98.1 0.7 3.0 17.9 715 834 86 252 234
    20A 93.2 96.3 0.8 2.9 18.3 780 910 86 210 208
    21A 94.4 98.1 0.5 2.8 15.6 723 845 86 242 221
    22A 92.5 96.8 0.7 2.7 14.3 754 866 87 253 234
    24A 81.9 91.2 0.4 1.5 27.4 534 645 83 143 101
    25A 46.3 93.0 0.3 3.2 28.7 534 673 79 140 138
    26A 82.1 91.2 0.4 1.5 27.5 664 787 84 146 107
    28A 96.4 98.1 1.5 2.6 16.3 881 991 89 156 121 comparative example
    30A 95.4 97.1 1.9 2.9 17.8 912 1049 87 112 98
    31A 89.1 93.4 0.3 2.8 18.3 743 865 86 156 34
    32A 9.3 91.3 0.1 2.7 17.6 520 654 80 31 25
    101A 33.2 92.9 0.3 3.3 16.2 571 662 86 248 210 138 126 examples of present invention
    102A 23.9 93.8 0.2 3.4 16.1 583 657 89 238 231 135 133
    103A 40.3 92.2 0.3 3.2 16.6 569 671 85 228 196 142 122
    104A 62.1 96.1 0.5 3.6 13.8 663 753 88 286 279 173 171
    105A 65.4 95.4 0.4 3.2 13.4 671 759 88 276 245 188 171
    106A 63.7 97.2 0.6 3.4 12.2 669 770 87 271 268 179 176
    107A 92.2 96.9 1.1 3.0 15.8 753 852 88 249 243 164 167
    108A 98.3 98.3 0.9 3.4 14.8 746 864 86 253 228 157 138
    109A 95.4 98.2 0.8 3.3 15.1 751 870 86 244 216 161 145
    110A 39.1 93.1 0.4 2.7 27.1 585 673 87 133 105 145 128
    111A 53.4 94.0 0.5 2.8 13.2 618 734 84 288 285 177 175
    112A 56.8 95.2 0.4 2.7 12.2 632 764 83 282 280 183 182
    113A 63.2 95.1 0.5 2.8 12.0 639 770 83 288 285 189 188
    114A 17.1 76.2 0.2 2.9 38.5 515 588 88 80 75 45 42 comparative example
    115A 18.4 77.4 0.2 3.0 37.9 516 590 87 77 74 42 43
    116A 97.2 97.9 1.2 2.8 16.1 878 982 89 142 138 39 33
    117A 96.3 98.2 1.1 2.7 15.8 880 988 89 138 135 36 32
    118A 22.4 68.1 0.3 2.8 15.8 412 523 79 148 133 116 103
  • Nos. 2A - 26A, 101A - 113A are Examples of the present invention, and Nos. 28A - 32A, 114A - 118A are Comparative Examples.
  • In No. 28A, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • In No. 30A, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive. Because there was also too much residual γ, sufficient low-temperature toughness was not obtained.
  • In No. 31A, because Mn fell outside of the upper limit, the low-temperature toughness after PWHT was low.
  • In No. 32A, because the cooling rate of the direct quenching was low, the total area ratio of the lower bainite and martensite was insufficient, and sufficient low-temperature toughness was not obtained.
  • In Nos. 114A and 115A, value α was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • In Nos. 116A and 117A, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • In No. 118A, the start temperature of the direct quenching was too low, and the total area ratio of the upper bainite, lower bainite and martensite was insufficient, and the strength was insufficient.
  • In contrast to the Comparative Examples, in the Examples of the present invention, the chemical compositions and microstructures of the steel products were controlled appropriately, and the tensile strengths were in the appropriate range of 615 MPa or more and 930 MPa or less. In addition, low-temperature toughness at -110°C of 100 J or more was obtained regardless of whether before or after PWHT.
  • <Manufacturing by Reheat Quenching and Tempering> [Manufacturing of Steel Product]
  • First, slabs having the chemical compositions shown in Table 4 were cast by continuous casting. The balance, which is other than the components listed in Table 4, is Fe and impurities. Further, blank cells mean that the alloy elements were not intentionally added in the steelmaking process. The underlines mean that the value is outside of the scope of the present disclosure. [Table 4]
    No. chemical composition (mass%)
    C Si Mn P S Ni Al N O Ti Nb Mg Ca REM Cu Cr Mo V B α
    2B 0.13 0.13 1.86 0.010 0.0057 5.99 0.034 0.0022 0.0024 6.9
    4B 0.12 0.21 1.50 0.006 0.0046 5.84 0.004 0.0015 0.0078 0.003 0.0071 0.03 5.7
    6B 0.05 0.11 0.72 0.005 0.0035 5.76 0.035 0.0071 0.0017 0.002 0.004 0.49 0.44 0.12 6.0
    7B 0.07 0.20 1.21 0.007 0.0019 5.69 0.028 0.0026 0.0014 0.21 0.21 0.0015 8.7
    8B 0.14 0.22 1.18 0.007 0.0028 5.73 0.022 0.0031 0.0018 0.0013 0.23 0.15 7.7
    9B 0.18 0.24 1.37 0.005 0.0031 5.98 0.026 0.0027 0.0025 0.17 0.08 8.7
    10B 0.07 0.11 0.55 0.006 0.0022 5.31 0.022 0.0018 0.0031 0.51 0.26 0.46 0.0004 7.7
    11B 0.14 0.14 0.76 0.008 0.0029 5.44 0.038 0.0074 0.0044 0.0012 0.0021 0.64 0.70 9.9
    14B 0.07 0.15 0.92 0.010 0.0122 5.38 0.052 0.0024 0.0017 1.23 0.38 0.27 12.2
    15B 0.05 0.14 0.79 0.008 0.0040 5.23 0.039 0.0047 0.0025 0.003 0.29 0.45 0.55 0.03 11.6
    16B 0.06 0.16 1.03 0.009 0.0081 5.48 0.031 0.0021 0.0022 0.001 0.0013 0.48 0.36 0.31 11.1
    17B 0.11 0.11 1.33 0.006 0.0062 5.89 0.008 0.0066 0.0016 0.39 0.41 0.13 14.2
    19B 0.09 0.08 1.07 0.008 0.0039 5.14 0.033 0.0033 0.0022 0.002 0.0022 1.10 13.9
    20B 0.08 0.13 0.91 0.011 0.0072 5.19 0.027 0.0037 0.0018 0.47 0.76 0.25 14.9
    21B 0.13 0.05 1.15 0.009 0.0042 5.39 0.038 0.0031 0.0027 0.002 0.48 0.22 14.5
    22B 0.07 0.10 0.85 0.007 0.0060 5.01 0.022 0.0024 0.0019 0.004 0.0022 0.45 0.66 0.31 12.8
    24B 0.13 0.11 1.72 0.014 0.0079 5.91 0.025 0.0026 0.0018 0.002 6.3
    25B 0.07 0.12 1.01 0.010 0.0051 5.47 0.034 0.0021 0.0015 0.08 3.5
    26B 0.17 0.05 1.78 0.013 0.0016 5.06 0.071 0.0038 0.0021 0.16 0.27 0.21 18.1
    29B 0.06 0.14 2.55 0.014 0.0013 5.11 0.026 0.0031 0.0018 0.14 0.07 0.22 11.4
    101B 0.12 0.15 1.44 0.009 0.0034 5.54 0.028 0.0026 0.0029 5.1
    102B 0.07 0.11 1.32 0.012 0.0042 4.89 0.032 0.0031 0.0032 0.019 0.25 0.44 8.2
    103B 0.05 0.09 1.29 0.007 0.0028 5.98 0.033 0.0036 0.0037 0.040 0.30 0.17 0.07 8.0
    104B 0.08 0.16 1.25 0.008 0.0045 4.82 0.003 0.0037 0.0026 0.012 0.42 0.50 9.6
    105B 0.11 0.14 0.96 0.005 0.0058 5.43 0.027 0.0042 0.0042 0.030 0.35 0.22 10.5
    106B 0.15 0.13 1.14 0.007 0.0036 5.88 0.029 0.0028 0.0035 0.35 0.54 0.08 11.9
    107B 0.07 0.09 1.64 0.008 0.0056 5.22 0.028 0.0046 0.0031 0.42 0.42 0.18 13.8
    108B 0.09 0.14 1.36 0.006 0.0042 5.46 0.026 0.0029 0.0027 0.015 0.0031 0.0022 0.30 0.34 14.5
    109B 0.06 0.11 1.28 0.009 0.0028 5.71 0.031 0.0038 0.0041 0.21 0.34 0.35 12.9
    110B 0.15 0.14 1.56 0.005 0.0067 5.05 0.033 0.0019 0.0035 5.7
    111B 0.07 0.14 1.25 0.008 0.0028 4.91 0.032 0.0031 0.0025 0.0005 0.44 0.53 9.4
    112B 0.12 0.11 0.92 0.006 0.0052 5.48 0.031 0.0038 0.0037 0.0005 0.30 0.24 10.1
    113B 0.14 0.14 1.19 0.005 0.0030 5.82 0.025 0.0032 0.0038 0.0005 0.25 0.45 0.08 10.6
    114B 0.09 0.14 0.90 0.013 0.0032 5.23 0.032 0.0025 0.0023 0.07 3.3
    115B 0.08 0.15 1.21 0.011 0.0029 5.38 0.031 0.0029 0.0034 0.14 3.6
    116B 0.14 0.09 1.86 0.015 0.0023 5.15 0.035 0.0045 0.0025 0.12 0.29 0.19 17.3
    117B 0.12 0.13 1.74 0.011 0.0014 5.23 0.037 0.0032 0.0033 0.16 0.31 0.28 19.2
    118B 0.11 0.13 0.78 0.012 0.0082 5.21 0.037 0.0027 0.0029 0.002 0.002 0.45 5.7
    119B 0.17 0.09 1.36 0.009 0.0056 6.08 0.029 0.0026 0.0041 0.002 0.0018 0.32 0.38 0.34 25.3
  • Next, steel products were manufactured from these slabs under the manufacturing conditions listed in Table 5. "Temper heat treatment" is the heating temperature in the tempering treatment after the quenching. [Table 5]
    No. plate thickness (mm) rolling conditions Ac3 [°C] reheat quenching conditions Temper heat treatment [°C]
    heating temperature [°C] hot rolling cumulative rolling reduction ratio [%] cooling after rolling reheat quenching temperature [°C] cooling after reheating
    2B 40 1210 55 water cooling 699 1030 water cooling 520
    4B 19 1130 63 water cooling 717 880 water cooling 630
    6B 40 1150 50 water cooling 756 910 water cooling 620
    7B 50 1190 39 air cooling 760 930 water cooling 590
    8B 35 1180 60 water cooling 719 1020 water cooling 620
    9B 25 1125 45 air cooling 691 760 water cooling 580
    10B 40 1220 58 air cooling 774 880 water cooling -
    11B 25 1130 55 air cooling 718 900 water cooling 530
    14B 55 1050 38 air cooling 753 890 water cooling 640
    15B 45 1170 42 air cooling 794 930 water cooling 590
    16B 60 1130 48 water cooling 762 830 water cooling 550
    17B 55 1150 38 air cooling 711 840 water cooling 520
    19B 50 1050 59 air cooling 793 880 water cooling 570
    20B 45 1130 50 water cooling 757 840 water cooling 470
    21B 40 1150 68 air cooling 731 800 water cooling 480
    22B 35 1130 45 water cooling 768 860 water cooling 600
    24B 55 1220 19 air cooling 700 850 water cooling 490
    25B 43 1150 43 air cooling 758 900 water cooling 570
    26B 50 1100 39 water cooling 714 930 water cooling 520
    29B 57 1180 45 air cooling 744 890 water cooling 590
    101B 70 1200 70 air cooling 723 850 water cooling -
    102B 60 1120 80 water cooling 778 930 water cooling 590
    103B 80 1150 68 air cooling 755 900 water cooling 630
    104B 60 1200 75 air cooling 773 880 water cooling 520
    105B 50 1100 80 water cooling 745 900 water cooling 580
    106B 45 1150 85 air cooling 708 930 water cooling 610
    107B 60 1100 75 air cooling 744 870 water cooling 540
    108B 50 1250 80 water cooling 752 890 water cooling 580
    109B 45 1150 85 air cooling 754 920 water cooling 620
    110B 60 1100 65 water cooling 721 810 water cooling 520
    111B 55 1150 78 air cooling 779 860 water cooling 560
    112B 50 1200 83 water cooling 741 910 water cooling 530
    113B 45 1100 82 air cooling 714 950 water cooling 600
    114B 50 1100 75 water cooling 755 880 water cooling 540
    115B 40 1150 70 air cooling 748 900 water cooling 600
    116B 60 1200 70 water cooling 718 950 water cooling 530
    117B 50 1150 67 air cooling 733 920 water cooling 550
    118B 50 1200 75 air cooling 748 590 water cooling 480
    119B 50 1050 80 water cooling 691 830 water cooling 560
  • [Measurement and Evaluation]
  • The microstructures and mechanical properties of the obtained steel products were measured by the above-described methods. The results are shown in Table 6. The meanings of the symbols of the microstructures are as follows. Note that the remainders of the microstructures were MA phase and ferrite.
    • Bu: upper bainite
    • BL: lower bainite
    • M: martensite
    • residual γ: residual austenite
  • For the toughness, the average value of the Charpy impact absorption energy at -110°C, and the average value of the Charpy impact absorption energy at -110°C after PWHT in which the holding temperature was 600°C, the holding time was 2 hours, and the rate of temperature increase and the rate of temperature decrease in the temperature region of 425°C or more were 55°C/h, respectively were measured. [Table 6]
    No. microstructure (area ratio) aspect ratio average value of prior γ grains average crystal grain diameter [µm] YS [MPa] TS [MPa] YR [%] base metal toughness KV2[J] toughness after PWHT KV2[J] thermal cycling toughness KV2[J] toughness after thermal cycling and PWHT KV2 [J] notes
    BL+M [%] Bu+BL+M [%] residual γ [%]
    2B 25.2 92.1 0.0 1.1 23.2 569 654 87 146 122 examples of present invention
    4B 24.7 92.7 0.0 1.3 16.4 513 628 82 221 190
    6B 36.2 92.5 0.1 1.2 17.3 572 661 87 248 222
    7B 37.7 93.6 0.2 1.1 15.6 561 657 85 312 319
    8B 34.4 93.2 0.1 1.0 22.4 578 669 86 148 145
    9B 37.1 93.1 0.2 1.1 17.4 581 684 85 233 230
    10B 52.7 95.4 0.4 1.2 14.1 621 734 85 281 278
    11B 55.9 93.7 0.5 1.1 13.8 642 773 83 285 282
    14B 67.3 95.2 0.4 1.4 14.2 658 745 88 232 228
    15B 62.1 94.8 0.3 1.2 16.4 672 778 86 251 232
    16B 64.3 95.9 0.4 1.2 16.7 651 739 88 233 218
    17B 92.8 95.2 0.7 1.1 14.5 731 844 87 245 240
    19B 91.3 97.1 0.8 1.3 15.4 722 846 85 256 238
    20B 92.9 97.3 0.7 1.2 18.3 779 912 85 214 210
    21B 98.2 98.2 0.6 1.1 15.6 736 857 86 252 232
    22B 90.0 96.8 0.6 1.2 14.1 749 858 87 262 241
    24B 38.1 92.3 0.2 1.4 27.5 542 653 83 137 102
    25B 10.2 80.2 0.0 1.2 41.2 510 568 90 68 67 comparative example
    26B 95.3 98.1 1.3 1.1 17.0 891 992 90 159 119
    29B 87.9 95.1 0.8 1.3 17.2 736 859 86 155 30
    101B 26.2 92.3 0.2 1.1 19.4 605 683 89 231 220 135 118 examples of present invention
    102B 36.4 93.1 0.3 1.2 17.2 573 663 86 220 197 143 131
    103B 34.8 93.0 0.2 1.1 17.5 570 659 86 227 204 142 129
    104B 57.2 94.8 0.6 1.2 16.1 645 765 84 240 218 186 161
    105B 60.2 95.7 0.7 1.1 15.6 674 770 88 252 228 192 175
    106B 63.8 96.9 0.7 1.3 15.3 680 778 87 239 235 181 178
    107B 93.4 97.1 1.1 1.2 14.2 731 856 85 245 224 162 141
    108B 93.1 98.2 1.2 1.1 15.1 752 862 87 251 236 158 142
    109B 92.0 98.1 0.9 1.3 14.8 744 858 87 254 250 172 169
    110B 25.3 90.2 0.2 1.3 26.6 528 624 85 140 123 135 114
    111B 55.8 94.3 0.4 1.2 13.8 646 759 83 279 276 182 181
    112B 64.3 94.8 0.4 1.3 14.2 661 757 88 241 240 185 182
    113B 66.1 95.2 0.5 1.2 14.3 674 775 86 255 251 195 192
    114B 9.2 78.3 0.1 1.3 40.4 501 566 89 66 63 43 32 comparative example
    115B 10.1 79.1 0.0 1.2 39.8 512 573 89 68 69 41 37
    116B 96.2 98.2 0.9 1.2 16.1 873 986 89 142 138 39 33
    117B 97.3 98.1 1.2 1.1 15.8 884 995 89 138 135 36 32
    118B 11.4 53.0 0.1 1.8 16.6 437 526 83 161 142 127 112
    119B 96.2 96.8 1.9 1.2 18.2 936 1070 87 63 42 25 18
  • Nos. 2B - 24B and 101B - 113B are Examples of the present invention, and Nos. 25B - 29B and 114B - 119B are Comparative Examples.
  • In No. 25B, value α was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • In No. 26B, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • In No. 29B, because Mn fell outside of the upper limit, the low-temperature toughness after PWHT was low.
  • In Nos. 114B and 115B, value α was less than the lower limit value of the present disclosure, and the hardenability was insufficient, and the strength was insufficient. Sufficient low-temperature toughness also was not obtained.
  • In Nos. 116B and 117B, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive.
  • In No. 118B, the reheating quenching temperature was too low, and the total area ratio of the upper bainite, lower bainite and martensite was insufficient, and the strength was insufficient.
  • In No. 119B, value α exceeded the upper limit value of the present disclosure, and the hardenability was too high, and the strength was excessive. Further, because there was also too much residual γ, sufficient low-temperature toughness was not obtained.
  • In contrast to the Comparative Examples, in the Examples of the present invention, the chemical compositions and microstructures of the steel products were controlled appropriately, and the tensile strengths were in the appropriate range of 615 MPa or more and 930 MPa or less. In addition, low-temperature toughness at -110°C of 100 J or more was obtained regardless of whether before or after PWHT. In particularly suitable structures of the present disclosure, low-temperature toughness at -110°C of 150 J or more was obtained regardless of whether before or after PWHT.
  • Industrial Applicability
  • The steel products relating to the present disclosure can be used mainly for transport tanks of liquefied carbon dioxide. Further, the steel products relating to the present disclosure can also be used in other welded structures such as buildings, bridges, ships, pipelines, offshore structures, pressure vessels and tanks.
  • The disclosures of Japanese Patent Application No. 2023-042399 and Japanese Patent Application No. 2023-042402 filed on March 16, 2023 are, in their entireties, incorporated by reference into the present specification. All publications, patent applications, and technical standards mentioned in the present specification are incorporated by reference into the present specification to the same extent as if such individual publication, patent application, or technical standard was specifically and individually put forth herein.

Claims (6)

  1. A steel product having a chemical composition comprising, in mass%,
    C: 0.03% or more and 0.20% or less,
    Si: 0.01% or more and 0.50% or less,
    Mn: 0.10% or more and 2.00% or less,
    P: 0.025% or less,
    S: 0.0250% or less,
    Ni: 4.51% or more and 6.10% or less,
    Al: 0.001% or more and 0.100% or less,
    O: 0.0100% or less,
    N: 0.0100% or less,
    Cu: 0 - 1.50%,
    Cr: 0 - 3.00%,
    Mo: 0 - 2.00%,
    B: 0 - 0.0050%,
    Nb: 0 - 0.050%,
    Ti: 0 - 0.050%,
    V: 0 - 0.10%,
    Mg: 0 - 0.0200%,
    Ca: 0 - 0.0200%,
    REM: 0 - 0.0200%,
    balance: Fe and impurities,
    and in which α expressed by following formula (1) is 5.0 or more and 16.0 or less,
    wherein:
    a tensile strength is 615 MPa or more and 930 MPa or less, and
    a microstructure of a region that is 1/4 of a thickness in a thickness direction from a surface of the steel product contains lower bainite and martensite, and a total of area ratios of the lower bainite and the martensite is 15.0% or more, and a total of area ratios of upper bainite and the lower bainite and the martensite is 90.0% or more, and an area ratio of residual austenite is less than 1.7%. α = 0.50 × √[C] × (1+0.64[Si]) × (1+4.10[Mn]) × (1+0.27[Cu]) × (1+0.52[Ni]) × (1+2.33[Cr]) × (1+3.14[Mo])
    wherein [element symbol] in formula (1) represents content (mass%) of a respectively corresponding element contained in the steel product, and, in a case in which an element is not contained, zero is substituted in therefor.
  2. The steel product of Claim 1, wherein, in the microstructure of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product, an average crystal grain diameter is 20.0 µm or less.
  3. The steel product of Claim 1 or Claim 2, wherein a Charpy impact absorption energy at -110°C is 150 J or more.
  4. The steel product of any one of Claim 1 through Claim 3, wherein, in a case in which a heat treatment, in which a rate of temperature increase and a rate of temperature decrease in a temperature region of 425°C or more are 55°C/h and temperature is held for 2 hours at 600°C, is carried out on the steel product, a Charpy impact absorption energy at -110°C of portions where the heat treatment has been carried out is 150 J or more.
  5. The steel product of any one of Claim 1 through Claim 4, wherein an aspect ratio of prior austenite crystal grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is 1.5 or more.
  6. The steel product of any one of Claim 1 through Claim 4, wherein an aspect ratio of prior austenite crystal grains of the region that is 1/4 of the thickness in the thickness direction from the surface of the steel product is less than 1.5.
EP24771022.1A 2023-03-16 2024-03-15 Steel Pending EP4682285A1 (en)

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JPH06192729A (en) 1992-12-25 1994-07-12 Kawasaki Steel Corp Production of low temperature use steel excellent in weldability
JPH07331328A (en) 1994-06-03 1995-12-19 Kawasaki Steel Corp Method for manufacturing high strength steel with excellent low temperature toughness
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JP2019081930A (en) 2017-10-31 2019-05-30 新日鐵住金株式会社 Nickel-containing steel plate for low temperature excellent in toughness and method for manufacturing the same
WO2020184162A1 (en) 2019-03-13 2020-09-17 Jfeスチール株式会社 Thick steel sheet and production method therefor
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See also references of WO2024190920A1

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