EP4656758A1 - High-strength steel sheet and method for manufacturing same - Google Patents

High-strength steel sheet and method for manufacturing same

Info

Publication number
EP4656758A1
EP4656758A1 EP24767131.6A EP24767131A EP4656758A1 EP 4656758 A1 EP4656758 A1 EP 4656758A1 EP 24767131 A EP24767131 A EP 24767131A EP 4656758 A1 EP4656758 A1 EP 4656758A1
Authority
EP
European Patent Office
Prior art keywords
amount
steel sheet
less
heat treatment
rolled steel
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
EP24767131.6A
Other languages
German (de)
French (fr)
Inventor
Ryusuke ISHITO
Junya TOBATA
Hidekazu Minami
Yuki Toji
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.)
JFE Steel Corp
Original Assignee
JFE 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 JFE Steel Corp filed Critical JFE Steel Corp
Publication of EP4656758A1 publication Critical patent/EP4656758A1/en
Pending legal-status Critical Current

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    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C23C2/022Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
    • C23C2/0224Two or more thermal pretreatments
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/18Hardening; Quenching with or without subsequent tempering
    • C21D1/25Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • 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
    • C21D8/0236Cold rolling
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    • 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
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • 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
    • C21D8/0273Final recrystallisation annealing
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    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • 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
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/008Ferrous alloys, e.g. steel alloys containing tin
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/08Ferrous alloys, e.g. steel alloys containing nickel
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/10Ferrous alloys, e.g. steel alloys containing cobalt
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/12Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/14Ferrous alloys, e.g. steel alloys containing titanium or zirconium
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/16Ferrous alloys, e.g. steel alloys containing copper
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/26Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/38Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
    • C23C2/06Zinc or cadmium or alloys based thereon
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    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/26After-treatment
    • C23C2/28Thermal after-treatment, e.g. treatment in oil bath
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    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/26After-treatment
    • C23C2/28Thermal after-treatment, e.g. treatment in oil bath
    • C23C2/29Cooling or quenching
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    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C2/00Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/34Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
    • C23C2/36Elongated material
    • C23C2/40Plates; Strips
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    • C23GCLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
    • C23G1/00Cleaning or pickling metallic material with solutions or molten salts
    • C23G1/02Cleaning or pickling metallic material with solutions or molten salts with acid solutions
    • C23G1/08Iron or steel
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    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D3/00Electroplating: Baths therefor
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    • C25D3/22Electroplating: Baths therefor from solutions of zinc
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    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
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    • 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
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    • C21METALLURGY OF IRON
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    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/005Ferrite
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    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite

Definitions

  • the present invention relates to a high strength steel sheet and a method for manufacturing the same.
  • delayed fracture may occur due to an increase in residual stress in the component or a deterioration of delayed fracture resistance of the steel sheet itself.
  • the delayed fracture is a phenomenon in which when a formed component is placed in a hydrogen entering environment, hydrogen enters a steel sheet constituting the component, whereby interatomic bonding strength decreases or local deformation occurs, thus causing fine cracks, and development of the fine cracks leads to fracturing.
  • high strength steel sheets used in automobiles are required to be resistant to cracking at a bent ridge portion (i.e., required to have excellent bendability) during bending from a formability viewpoint.
  • skeletal parts of automobiles have many end surfaces formed through shearing, and such shear end surfaces are required to be free from cracking caused by bending forming (bending).
  • shear end surface depends on the shear clearance, and occurrence of cracking at a shear end surface also depends on the shear clearance.
  • high strength steel sheets used in automobiles need to have a wide optimal clearance range with respect to bending forming of shear end surfaces.
  • an object of the present invention is to provide a high strength steel sheet having a tensile strength (TS) of not less than 1,180 MPa, having excellent bendability and excellent delayed fracture resistance, and having a wide optimal clearance range with respect to bending forming of a shear end surface, as well as a method for manufacturing the same.
  • TS tensile strength
  • the present invention provides the following [1] to [5].
  • the present invention can provide a high strength steel sheet having a tensile strength (TS) of not less than 1,180 MPa, having excellent bendability and excellent delayed fracture resistance, and having a wide optimal clearance range with respect to bending forming of a shear end surface, as well as a method for manufacturing the same.
  • TS tensile strength
  • a high strength steel sheet of the present embodiment (hereinafter also referred to as the "present high strength steel sheet”) includes a steel sheet, and may further include a plating layer on a surface of the steel sheet as described later.
  • the steel sheet included in the present high strength steel sheet has the chemical composition and microstructure (steel structure) which are to be described later, and satisfies an instability index k and an instability index d which are to be described later.
  • high strength means having a tensile strength (TS) of not less than 1,180 MPa.
  • the high strength steel sheet has a tensile strength (TS) of not less than 1,180 MPa, has excellent bendability and excellent delayed fracture resistance, and has a wide optimal clearance range with respect to bending forming of a shear end surface.
  • TS tensile strength
  • optimal clearance range with respect to bending forming of a shear end surface is also simply called “optimal clearance range.”
  • the thickness of the steel sheet is not particularly limited and is, for example, not less than 0.5 mm and not more than 3.0 mm.
  • present chemical composition The chemical composition of the steel sheet included in the present high strength steel sheet (hereinafter, also referred to as “present chemical composition”) is described.
  • the unit "%" used for the chemical composition means “mass%” unless otherwise noted.
  • C is an element that is one of important basic components of steel and that influences the amount of martensite and the total amount of ferrite and bainitic ferrite.
  • the C content is not less than 0.030%, preferably not less than 0.050%, and more preferably not less than 0.100%.
  • the C content is not more than 0.500%, preferably not more than 0.400%, and more preferably not more than 0.350%.
  • Si is an element that is one of important basic components of steel and that influences the TS and the amount of retained austenite.
  • the Si content is not less than 0.50%, preferably not less than 0.55%, and more preferably not less than 0.60%.
  • the Si content is not more than 2.50%, preferably not more than 2.00%, and more preferably not more than 1.80%.
  • Mn is an element that is one of important basic components of steel and that influences the amount of martensite and the total amount of ferrite and bainitic ferrite.
  • the Mn content is not less than 1.50%, preferably not less than 2.00%, and more preferably not less than 2.20%.
  • the Mn content is not more than 5.00%, preferably not more than 4.50%, and more preferably not more than 4.00%.
  • the P content is not more than 0.100%, preferably not more than 0.070%, and more preferably not more than 0.030%.
  • the lower limit thereof is not particularly limited.
  • P is a solid solution strengthening element and is capable of increasing the strength of the steel sheet.
  • the P content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • the S content is not more than 0.0200%, preferably not more than 0.0050%, and more preferably not more than 0.0025%.
  • the S content is preferably not less than 0.0001%, more preferably not less than 0.0003%, and even more preferably not less than 0.0005% due to production engineering constraints.
  • Al is present as an oxide and embrittles the steel sheet, resulting in lower delayed fracture resistance.
  • the Al content is not more than 1.000%, preferably not more than 0.500%, more preferably not more than 0.150%, and even more preferably not more than 0.070%.
  • the lower limit thereof is not particularly limited.
  • Al is capable of suppressing the generation of a carbide during heat treatments, which will be described later, and promoting the generation of retained austenite.
  • the Al content is preferably not less than 0.001%, more preferably not less than 0.005%, and even more preferably not less than 0.010%.
  • N is present as a nitride and embrittles the steel sheet, resulting in lower delayed fracture resistance.
  • the N content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • the N content is preferably not less than 0.0001%, more preferably not less than 0.0005%, and even more preferably not less than 0.0010% due to production engineering constraints.
  • the O content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • the O content is preferably not less than 0.0001%, more preferably not less than 0.0007%, and even more preferably not less than 0.0015% due to production engineering constraints.
  • the present inventors found, through an earnest study, that Nb influences the instability index k of retained austenite.
  • the Nb content is not less than 0.005%, preferably not less than 0.008%, and more preferably not less than 0.010%.
  • the Nb content is not more than 0.100%, preferably not more than 0.080%, and more preferably not more than 0.050%.
  • the present chemical composition may further include at least one element (another element) selected from the group consisting of the elements described below, in percentage by mass.
  • the contents of Ti and V are each not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • Ti and V form fine carbides, nitrides, or carbonitrides during hot rolling or heat treatments, which will be described later, thereby increasing the strength of the steel sheet.
  • the contents of Ti and V are each preferably not less than 0.001%, more preferably not less than 0.005%, and even more preferably not less than 0.015%.
  • the contents of Ta and W are each not more than 0.10%, preferably not more than 0.09%, and more preferably not more than 0.08%.
  • Ta and W form fine carbides, nitrides, or carbonitrides during hot rolling or heat treatments, which will be described later, thereby increasing the strength of the steel sheet.
  • the contents of Ta and W are each preferably not less than 0.01%, more preferably not less than 0.03%, and even more preferably not less than 0.05%.
  • the B content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0060%.
  • the lower limit thereof is not particularly limited.
  • B segregates in a prior austenite grain boundary during heat treatments to be described later, thus improving the hardenability.
  • the B content is preferably not less than 0.0003%, more preferably not less than 0.0005%, and even more preferably not less than 0.0010%.
  • the contents of Cr, Mo, and Ni are each not more than 1.00%, preferably not more than 0.80%, and more preferably not more than 0.50%.
  • the lower limits thereof are not particularly limited.
  • Cr, Mo, and Ni are elements that improve the hardenability
  • the contents of Cr, Mo, and Ni are each preferably not less than 0.01%, more preferably not less than 0.04%, and even more preferably not less than 0.08%.
  • the Co content is not more than 0.010%, preferably not more than 0.008%, and more preferably not more than 0.006%.
  • the lower limit thereof is not particularly limited.
  • Co is an element that improves the hardenability
  • the Co content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • the Cu content is not more than 1.00%, preferably not more than 0.80%, and more preferably not more than 0.60%.
  • the lower limit thereof is not particularly limited.
  • the Cu content is preferably not less than 0.01%, more preferably not less than 0.03%, and even more preferably not less than 0.05%.
  • the Sn content is not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • the lower limit thereof is not particularly limited.
  • Sn is an element that improves the hardenability
  • the Sn content is preferably not less than 0.001%, more preferably not less than 0.010%, and even more preferably not less than 0.020%.
  • the Sb content is not more than 0.200%, preferably not more than 0.100%, and more preferably not more than 0.050%.
  • the lower limit thereof is not particularly limited.
  • Sb is an element that controls the surface layer softening thickness and allows for adjustment of the strength
  • the Sb content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • the contents of Ca, Mg, and REM are each not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • Ca, Mg, and REM are elements that spheroidize the shapes of nitrides and sulfides and improve the ultimate deformability of the steel sheet.
  • the contents of Ca, Mg, and REM are each preferably not less than 0.0005%, more preferably not less than 0.0010%, and even more preferably not less than 0.0015%.
  • the contents of Zr and Te are each not more than 0.100%, preferably not more than 0.080%, and more preferably not more than 0.060%.
  • Zr and Te are elements that spheroidize the shapes of nitrides and sulfides and improve the ultimate deformability of the steel sheet.
  • the contents of Zr and Te are each preferably not less than 0.001%, more preferably not less than 0.008%, and even more preferably not less than 0.015%.
  • the Hf content is not more than 0.10%, preferably not more than 0.09%, and more preferably not more than 0.08%.
  • the lower limit thereof is not particularly limited.
  • Hf is an element that spheroidizes the shapes of nitrides and sulfides and improves the ultimate deformability of the steel sheet.
  • the Hf content is preferably not less than 0.01%, more preferably not less than 0.02%, and even more preferably not less than 0.03%.
  • the Bi content is not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • the lower limit thereof is not particularly limited.
  • the Bi content is preferably not less than 0.001%, more preferably not less than 0.020%, even more preferably not less than 0.050%, and particularly preferably not less than 0.090%.
  • the balance in the present chemical composition consists of Fe and inevitable impurities.
  • present microstructure the microstructure of the steel sheet included in the present high strength steel sheet.
  • Total amount of ferrite and bainitic ferrite not more than 10%
  • the total amount of ferrite and bainitic ferrite is not more than 10%, preferably not more than 9%, and more preferably not more than 8%.
  • the lower limit thereof is not particularly limited.
  • the amounts of ferrite and bainitic ferrite are obtained in the following manner.
  • the steel sheet is polished to expose, as an observation surface, an L cross section at the 1/4 sheet thickness position (the position corresponding to 1/4 of the sheet thickness from the surface of the steel sheet in the depth direction).
  • the observation surface is etched using 3 vol% Nital and then observed in 10 fields with a scanning electron microscope (SEM) at a magnification of 2,000X, whereby an SEM image of each field is obtained.
  • SEM scanning electron microscope
  • ferrite and bainitic ferrite are observed as recessed structures with their inside portions being flat.
  • the area fraction (unit: %) of ferrite and bainitic ferrite in each SEM image is obtained, and the average of the obtained area fractions of the 10 fields is defined as the total amount of ferrite and bainitic ferrite.
  • the amount of retained austenite is not less than 3%, preferably not less than 5%, more preferably not less than 7%, and even more preferably not less than 8% because excellent bendability can be achieved.
  • the amount of retained austenite is not more than 20%, preferably not more than 15%, and more preferably not more than 13% because excellent delayed fracture resistance can be achieved.
  • the amount of retained austenite is determined in the following manner.
  • the steel sheet is polished to expose an L cross section at a position 0.1 mm deeper than the 1/4 sheet thickness position.
  • This L cross section is further polished by 0.1 mm in the depth direction by chemical polishing to obtain an observation surface.
  • integral intensity ratios of diffraction peaks are determined using CoK ⁇ radiation in an X-ray diffraction (XRD) instrument. More specifically, integral intensity ratios between diffraction peaks of respective planes ⁇ 200 ⁇ , ⁇ 220 ⁇ , and ⁇ 311 ⁇ of fcc iron and those of respective planes ⁇ 200 ⁇ , ⁇ 211 ⁇ , and ⁇ 220 ⁇ of bcc iron are determined.
  • the average of nine integral intensity ratios is defined as the volume fraction (unit: %) of the amount of retained austenite, and the obtained value is specified as the amount of retained austenite.
  • the amount of martensite is not less than 70%, preferably not less than 75%, and more preferably not less than 80% because a TS of not less than 1,180 MPa can be achieved.
  • tempered martensite is important in terms of the contribution to achievement of a high TS, and the amount of tempered martensite is preferably not less than 80%.
  • the amount of martensite is determined in the following manner.
  • the amount of retained austenite and the total amount of ferrite and bainitic ferrite are obtained by the foregoing methods. Next, the sum of those amounts is subtracted from 100%, and the obtained value (unit: %) is defined as the amount of martensite.
  • the amount of martensite herein includes both amounts of hardened martensite and tempered martensite.
  • the amount of retained austenite is the volume fraction as described above, and this is substantially equivalent to the area fraction. Accordingly, the amount of retained austenite is, together with the total amount of ferrite and bainitic ferrite which is the area fraction, subtracted from 100%.
  • the present inventors found, through an earnest study, that the instability index k of retained austenite (also simply referred to as "instability index k”) influences the optimal clearance range.
  • the instability index k is less than 6.1, preferably not more than 5.0, more preferably not more than 4.0, and even more preferably not more than 3.5.
  • the instability index k is for example not less than 1.0, preferably not less than 1.5, and more preferably not less than 2.0.
  • the present inventors found, through an earnest study, that the instability index d of retained austenite in an initial stage of working (also simply referred to as "instability index d”) influences the delayed fracture resistance and the optimal clearance range.
  • the instability index d When the instability index d is too high, the stability of retained austenite in an initial stage of working is low, and the retained austenite excessively transforms to hard martensite in the initial stage of working and would act as starting points of generation of delayed fractures in a hydrogen entering environment, thus lowering the delayed fracture resistance.
  • the instability index d is less than 5.7, preferably not more than 5.0, more preferably not more than 4.0, and even more preferably not more than 3.5.
  • the instability index d is for example not less than -15.0, preferably not less than -10.0, and more preferably not less than -5.0.
  • the instability index k and the instability index d are determined in the following manner.
  • FIG. 1 is a schematic view showing a specimen used in the tensile test.
  • FIG. 2 is a graph schematically showing the relation between tensile stress applied to a specimen 1 and tensile strain during the tensile test.
  • tensile stress is applied to a specimen to impart tensile strain (tensile plasticity strain).
  • tensile strain tensile plasticity strain
  • a plurality of specimens to each of which given tensile strain ⁇ has been imparted in the range of 0% to 10% (0 to 0.10) are obtained in this manner.
  • the tensile strain ⁇ before working (before impartment of tensile strain) is 0%.
  • the obtained approximation formula is applied to Formula (1) below, and the slope a of the approximation formula is obtained as the instability index k of retained austenite.
  • log f ⁇ ⁇ k ⁇ ⁇ + log f ⁇ 0
  • fy represents the amount of retained austenite when the tensile strain ⁇ is imparted
  • f ⁇ 0 represents the amount of retained austenite before working.
  • f ⁇ 0 represents the actual measurement value of the amount of retained austenite before working
  • f ⁇ 0 represents the estimate value of retained austenite before working
  • FIG. 3 is an exemplary graph showing the relation between the tensile strain ⁇ and the amount of retained austenite.
  • FIG. 4 is another example of the graph.
  • FIG. 5 is still another example of the graph.
  • the slope a (instability index k) of the approximation formula in FIG. 3 is 2.3 and is smaller than the slope a (instability index k) of the approximation formula in FIG. 4 , that is, 11.9.
  • the slope a (instability index k) of the approximation formula being small indicates that the change in the amount of retained austenite is small during working, and the stability of retained austenite is good.
  • the slope a (instability index k) of the approximation formula is as small as 4.0.
  • the slope of the approximation formula is large as far as an initial stage of working (initial stage of the tensile test) is concerned. That is, in this case, the stability of retained austenite is insufficient in the initial stage of working.
  • the present high strength steel sheet may further have a plating layer on a surface of the steel sheet for the purpose of improving corrosion resistance and other properties.
  • Examples of the plating layer include a galvanizing layer, a galvannealing layer, and an electrogalvanizing layer.
  • the plating layer is formed by a plating treatment to be described later.
  • the coating weight of the plating layer is not particularly limited and is preferably 20 to 80 g/m 2 per one side.
  • present manufacturing method a method for manufacturing a high strength steel sheet according to the present embodiment.
  • present manufacturing method is also a method for manufacturing the present high strength steel sheet described above.
  • the temperature at which a steel slab, the steel sheet, or the like is heated or cooled which is described below, means a surface temperature of the steel slab, the steel sheet, or the like, unless otherwise specified.
  • a method of manufacturing molten steel which becomes a steel slab is not particularly limited, and known methods using a converter, an electric furnace, or the like are applicable. It is preferable to obtain a steel slab from molten steel by a continuous casting method for the sake of preventing macro-segregation.
  • a steel slab having the present chemical composition described above is retained at a slab heating temperature described below and then hot-rolled to obtain a hot rolled steel sheet.
  • the slab heating temperature is preferably not lower than 1,220°C, more preferably not lower than 1,230°C, and even more preferably higher than 1,230°C.
  • the slab heating temperature is preferably not higher than 1,300°C, more preferably not higher than 1,290°C, and even more preferably not higher than 1,280°C.
  • the hot rolled steel sheet obtained through the hot rolling is cooled.
  • an average cooling rate v 1 from 800°C to 600°C satisfies the range described below.
  • the present inventors found, through an earnest study, that the average cooling rate v 1 from 800°C to 600°C (also simply referred to as "average cooling rate v 1 ”) influences the instability index k of retained austenite.
  • the average cooling rate v 1 is not lower than 30°C/s, preferably not lower than 35°C/s, and more preferably not lower than 40°C/s.
  • the hot rolled steel sheet thus cooled is subjected to pickling and cold rolling to obtain a cold rolled steel sheet.
  • pickling is capable of removing oxides on a surface of the hot rolled steel sheet, pickling is important to ensure good chemical convertibility and good plating quality of the final product, i.e., a high strength steel sheet. Pickling may be performed only once, or may be divided into plural steps.
  • the hot rolled steel sheet is subjected to pickling, thereby obtaining a pickled sheet. Subsequently, the pickled sheet is dried as appropriate.
  • Cold rolling may be performed on the pickled sheet before being dried or after being dried.
  • the rolling reduction in the cold rolling and the sheet thickness after the rolling are not particularly limited.
  • the number of rolling passes and the rolling reduction for each pass are also not particularly limited.
  • the cold rolled steel sheet obtained by the cold rolling is subjected to a heat treatment A, a heat treatment B, and a heat treatment C, as described below, in this order.
  • the heat treatment C is preceded by working described below.
  • the cold rolled steel sheet obtained by the cold rolling is subjected to the heat treatment A.
  • the cold rolled steel sheet is retained (heated) at a temperature T1 described below and then cooled to a cooling stop temperature Ta described below.
  • the cold rolled steel sheet is retained (heated) at the temperature T1.
  • the temperature T1 is too low, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa.
  • the temperature T1 is not lower than 800°C, preferably not lower than 820°C, and more preferably not lower than 840°C.
  • the temperature T1 is for instance not higher than 940°C, preferably not higher than 920°C, and more preferably not higher than 900°C.
  • the retaining time t 1 is 10 seconds or more, preferably 30 seconds or more, and more preferably 50 seconds or more.
  • the retaining time t 1 is for instance 300 seconds or less, preferably 250 seconds or less, and more preferably 200 seconds or less.
  • the cold rolled steel sheet having been retained at the temperature T1 is cooled to the cooling stop temperature Ta.
  • the cooling stop temperature Ta is not lower than 100°C, preferably not lower than 120°C, and more preferably not lower than 140°C.
  • the cooling stop temperature Ta is not higher than (Ms point - 80°C), preferably not higher than (Ms point - 90°C), and more preferably not higher than (Ms point - 100°C).
  • the average cooling rate v 2 is not lower than 20°C/s, preferably not lower than 22°C/s, and more preferably not lower than 24°C/s.
  • the average cooling rate v 2 is for instance not higher than 65°C/s, preferably not higher than 55°C/s, and more preferably not higher than 45°C/s.
  • an average cooling rate v 3 from the Ms point to the cooling stop temperature Ta influences the instability index d of retained austenite in an initial stage of working.
  • the average cooling rate v 3 is not higher than 150°C/s, preferably not higher than 120°C/s, and more preferably not higher than 90°C/s.
  • the average cooling rate v 3 is for instance not lower than 5°C/s, preferably not lower than 8°C/s, and more preferably not lower than 10°C/s.
  • tension F imparted to the cold rolled steel sheet from the Ms point to the cooling stop temperature Ta (also simply referred to as "tension F") influences the instability index d of retained austenite in an initial stage of working.
  • the tension F is not less than 5 MPa, preferably not less than 6 MPa, and more preferably not less than 8 MPa.
  • the tension F is not more than 100 MPa, preferably not more than 50 MPa, and more preferably not more than 25 MPa.
  • Ms 519 - 474 ⁇ [%C] - 30.4 ⁇ [%Mn] - 12.1 ⁇ [%Cr] - 7.5 ⁇ [%Mo] - 17.7 ⁇ [%Ni]
  • [%M] represents the content of an element M in the chemical composition, and when the element M is not contained, [%M] is 0.
  • the cold rolled steel sheet having been cooled to the cooling stop temperature Ta is subjected to the heat treatment B.
  • the cold rolled steel sheet is retained (heated) at a temperature T2 described below and then cooled to a temperature (e.g., room temperature) lower than the temperature T2.
  • the room temperature is 25 ⁇ 5°C, for instance.
  • the cold rolled steel sheet is retained (heated) at the temperature T2. This stabilizes retained austenite.
  • the temperature T2 is not lower than the cooling stop temperature Ta, preferably not lower than (Ta + 10°C), and more preferably not lower than (Ta + 20°C) .
  • the temperature T2 is not higher than 450°C, preferably not higher than 420°C, and more preferably not higher than 400°C.
  • the retaining time t 2 is 5 seconds or more, preferably 50 seconds or more, and more preferably 80 seconds or more.
  • the retaining time t 2 is 1,000 seconds or less, preferably 800 seconds or less, and more preferably 400 seconds or less.
  • the cold rolled steel sheet is wrought to impart equivalent plastic strain to the cold rolled steel sheet after the heat treatment A described above and before the heat treatment C described below.
  • the temperature during the working is not particularly limited.
  • the working may be carried out while the cold rolled steel sheet is retained at the temperature T2 or after the cold rolled steel sheet is cooled to, for example, the room temperature subsequent to the retention at the temperature T2.
  • equivalent plastic strain imparted to the cold rolled steel sheet through the working also simply referred to as "equivalent plastic strain" influences the instability index d of retained austenite in an initial stage of working.
  • the equivalent plastic strain is not less than 0.10%, preferably not less than 0.15%, and more preferably not less than 0.30%.
  • the equivalent plastic strain is not more than 5.00%, preferably not more than 4.00%, and more preferably not more than 3.00%.
  • the number of times the cold rolled steel sheet is wrought is not particularly limited.
  • the working may be divided into plural steps as long as the total equivalent plastic strain imparted to the cold rolled steel sheet through the whole working is within the foregoing range.
  • Examples of the method of working the cold rolled steel sheet include: a method in which the cold rolled steel sheet is subjected to temper rolling; and a method in which the cold rolled steel sheet is wrought using a tension leveler.
  • Examples of the leveler include a tension leveler, a continuous stretcher leveler, and a roller leveler, and a tension leveler is favorable.
  • the equivalent plastic strain is an elongation rate of the steel sheet (cold rolled steel sheet) and is determined from the change in length of the steel sheet before and after working.
  • the cold rolled steel sheet having been cooled to, for example, the room temperature is subjected to the heat treatment C.
  • the cold rolled steel sheet is heated to a temperature T3 described below and then cooled to a temperature (e.g., room temperature) lower than the temperature T3 without being retained at the temperature T3.
  • a temperature e.g., room temperature
  • the temperature T3 is not lower than 150°C, preferably not lower than 160°C, and more preferably not lower than 170°C.
  • the temperature T3 is not higher than 400°C, preferably not higher than 350°C, and more preferably not higher than 300°C.
  • the cold rolled steel sheet having been heated to the temperature T3 is immediately cooled without being retained at the temperature T3 as described above.
  • the average cooling rate in the temperature range described below is controlled to the range described below.
  • the average cooling rate v 4 is not higher than 50.0°C/h, preferably not higher than 48.0°C/h, and more preferably not higher than 45.0°C/h.
  • the average cooling rate v 4 is not lower than 1.0°C/h, preferably not lower than 1.2°C/h, and more preferably not lower than 1.4°C/h due to production engineering constraints.
  • the cold rolled steel sheet having undergone the heat treatment C corresponds to the steel sheet included in the present high strength steel sheet described above.
  • the cold rolled steel sheet may be wrought to again impart an equivalent plastic strain of not less than 0.10% and not more than 5.00%. After the working, the cold rolled steel sheet may be heated at a temperature of not lower than 100°C and not higher than 400°C.
  • the cold rolled steel sheet may be subjected to a plating treatment. A plating layer is thereby formed.
  • the plating treatment is performed, for instance, during or after the heat treatment A described above.
  • a galvanizing treatment or a galvannealing treatment treatment in which alloying is performed after galvanizing treatment
  • the cold rolled steel sheet is cooled from 750°C to 600°C at the average cooling rate v 2 , for example.
  • an electrogalvanizing treatment is performed after the heat treatment B, for example.
  • the electrogalvanizing treatment include a Zn-Ni electric alloy plating treatment, and a pure Zn electroplating treatment.
  • the plating treatment is not limited to the aforementioned galvanizing treatment, galvannealing treatment, or electrogalvanizing treatment.
  • the metal species used in the plating treatment is not limited to Zn and may be other metals (e.g., Al).
  • the coating weight of the plating layer to be formed can be adjusted by performing wiping during the plating treatment.
  • plating treatment can be carried out according to an ordinary method.
  • a series of treatments including the heat treatments A to C and the plating treatment as described above is preferably carried out in a continuous galvanizing line (CGL) for the sake of productivity.
  • CGL continuous galvanizing line
  • the obtained steel slab was retained at a slab heating temperature as shown in Table 2 below and then hot rolled to obtain a hot rolled steel sheet.
  • the hot rolled steel sheet obtained was cooled. In this process, the hot rolled steel sheet was cooled from 800°C to 600°C at the average cooling rate v 1 as shown in Table 2 below.
  • the hot rolled steel sheet thus cooled was pickled and then cold rolled to obtain a cold rolled steel sheet.
  • the cold rolled steel sheet obtained was subjected to the heat treatments A to C under the conditions shown in Table 2 below. Before the heat treatment C, the cold rolled steel sheet was wrought under the conditions shown in Table 2 below.
  • the cold rolled steel sheet (CR) was subjected to a plating treatment (galvanizing treatment, galvannealing treatment, or electrogalvanizing treatment) to obtain a galvanized steel sheet (GI), a galvannealed steel sheet (GA), or an electrogalvanized steel sheet (EG).
  • a plating treatment galvanizing treatment, galvannealing treatment, or electrogalvanizing treatment
  • the galvanizing treatment and the galvannealing treatment were each performed during cooling in the heat treatment A.
  • the electrogalvanizing treatment was performed after the heat treatment B (before the heat treatment C).
  • the bath temperature was set to 470°C for both cases of manufacturing GI and GA.
  • the coating weight of the plating layer was 45 to 72 g/m 2 per one side when GI was manufactured and 45 g/m 2 per one side when GA was manufactured.
  • the alloying temperature was set to 500°C.
  • the composition of the plating layer of GI was the composition including 0.1 to 1.0 mass% of Fe and 0.2 to 1.0 mass% of Al with the balance being Zn and inevitable impurities.
  • the composition of the plating layer of GA was the composition including 7 to 15 mass% of Fe and 0.1 to 1.0 mass% of Al with the balance being Zn and inevitable impurities.
  • the electrogalvanizing treatment was performed such that the plating layer had a coating weight of 30 g/m 2 per one side.
  • each of the cold rolled steel sheet (CR), the galvanized steel sheet (GI), the galvannealed steel sheet (GA), and the electrogalvanized steel sheet (EG) is also simply referred to as "steel sheet.”
  • a JIS No. 5 specimen (gauge length: 50 mm; parallel width: 25 mm) with its longitudinal direction (tensile direction) being perpendicular to the rolling direction was sampled.
  • a tensile test was performed in accordance with JIS Z 2241 under the condition of a crosshead speed of 1.67 x 10 -1 mm/s; thus, the tensile strength (TS) was determined.
  • the strength was determined to be high when the TS was not less than 1,180 MPa.
  • a specimen (width: 30 mm; length: 100 mm) with its longitudinal direction being perpendicular to the rolling direction was sampled.
  • a bending test was performed in accordance with a V-block method stated in JIS Z 2248 to measure a minimum bending radius R with which cracking did not occur at a bent ridge portion.
  • the bendability was determined to be excellent when a value obtained by dividing the minimum bending radius R by the sheet thickness t (R/t) was not more than 6.0.
  • the specimen was immersed in an aqueous solution containing 3 mass% of NaCl and 3 g/L of NH 4 SCN and retained for 24 hours with an applied current density of 0 or 0.05 mA/cm 2 . Thereafter, a tensile test (SSRT test) was performed at a tensile rate of 5 ⁇ m/min to break the specimen, thus determining the tensile strength (TS).
  • SSRT test tensile test
  • the ratio of the TS when the applied current density was 0.05 mA/cm 2 to the TS when the applied current density was 0 mA/cm 2 was obtained as a stress ratio.
  • the optimal clearance range with respect to bending forming of a shear end surface was determined as follows.
  • each of the obtained steel sheets was sheared to sample a specimen (width: 30 mm; length: 100 mm) with its longitudinal direction being perpendicular to the rolling direction.
  • the rake angle in shearing was set to 0° in all examples, and the shear clearance was varied to 5%, 10%, 15%, 20%, 25%, 30%, and 35%.
  • Occurrence or non-occurrence of cracking was checked by observing the shear end surface of the specimen with a digital microscope (RH-2000, manufactured by HIROX Co., Ltd.) at a magnification of 40X.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm]
  • Type Remarks Slab heating temp. [°C] Average cooling rate v 1 [°C/s] Temp. T1 [°C] Retaining time t 1 [s] Average cooling rate v 2 [°C/s] Average cooling rate v 3 [°C/s]
  • Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t 2 [s] Equivalent plastic strain [%] Number of times of working Temp.
  • the steel sheets of Nos. 1 to 8, 10 to 12, 14 to 16, 18 to 20, 22, 24, 26, 28 to 32, 34 to 36, 38, 40, 42 to 44, 46 to 48, 50 to 58, 60, 62, 64, 66, 68, 70, 72, 74, 76, 78, 80, 82, 84, 85, 87, 88, 90, 91, and 93 to 113 had a TS of not less than 1,180 MPa, excellent bendability and excellent delayed fracture resistance, and a wide optimal clearance range.

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Abstract

There is provided a high strength steel sheet having a tensile strength of not less than 1,180 MPa, having excellent bendability and excellent delayed fracture resistance, and having a wide optimal clearance range with respect to bending forming of a shear end surface. A steel sheet included in the high strength steel sheet contains, by mass, C: 0.030%-0.500%, Si: 0.50%-2.50%, Mn: 1.50%-5.00%, P: not more than 0.100%, S: not more than 0.0200%, Al: not more than 1.000%, N: not more than 0.0100%, O: not more than 0.0100%, and Nb: 0.005%-0.100%, with a balance consisting of Fe and inevitable impurities, an amount of martensite is not less than 70%, an amount of retained austenite is 3%-20%, a total amount of ferrite and bainitic ferrite is not more than 10%, an instability index k of retained austenite is less than 6.1, and an instability index d of retained austenite in an initial stage of working is less than 5.7.

Description

    TECHNICAL FIELD
  • The present invention relates to a high strength steel sheet and a method for manufacturing the same.
  • BACKGROUND ART
  • For the purpose of achieving both an improvement in fuel efficiency (reduction in CO2 emission) owing to reduced weight of vehicle bodies and an improvement in collision resistance performance, strengthening of thin steel sheets for automobiles are in progress, and new laws and regulations are also successively introduced.
  • In recent years, cases of applying high strength steel sheets having a tensile strength (TS) of not less than 1,180 MPa (for instance, see Patent Literatures 1 to 3) to main structural parts of automobiles are increasing for the purpose of increasing the strength of vehicle bodies.
  • CITATION LIST PATENT LITERATURE
  • SUMMARY OF INVENTION TECHNICAL PROBLEMS
  • While, conventionally, hot press forming of high strength steel sheets have been vigorously discussed, recently, cold press forming is again being considered from cost and productivity viewpoints.
  • However, when a component is obtained by cold press forming of a high strength steel sheet having a TS of not less than 1,180 MPa, delayed fracture may occur due to an increase in residual stress in the component or a deterioration of delayed fracture resistance of the steel sheet itself.
  • The delayed fracture is a phenomenon in which when a formed component is placed in a hydrogen entering environment, hydrogen enters a steel sheet constituting the component, whereby interatomic bonding strength decreases or local deformation occurs, thus causing fine cracks, and development of the fine cracks leads to fracturing.
  • Aside from that, high strength steel sheets used in automobiles are required to be resistant to cracking at a bent ridge portion (i.e., required to have excellent bendability) during bending from a formability viewpoint.
  • Further, skeletal parts of automobiles have many end surfaces formed through shearing, and such shear end surfaces are required to be free from cracking caused by bending forming (bending).
  • The form of a shear end surface depends on the shear clearance, and occurrence of cracking at a shear end surface also depends on the shear clearance.
  • Hence, high strength steel sheets used in automobiles need to have a wide optimal clearance range with respect to bending forming of shear end surfaces.
  • Therefore, an object of the present invention is to provide a high strength steel sheet having a tensile strength (TS) of not less than 1,180 MPa, having excellent bendability and excellent delayed fracture resistance, and having a wide optimal clearance range with respect to bending forming of a shear end surface, as well as a method for manufacturing the same.
  • SOLUTION TO PROBLEMS
  • The present inventors have made an intensive study and as a result found that when the configuration described below is employed, the foregoing object is achieved. The invention has been thus completed.
  • Specifically, the present invention provides the following [1] to [5].
    1. [1] A high strength steel sheet comprising a steel sheet,
      • wherein the steel sheet has a chemical composition including, by mass,
      • C in an amount of not less than 0.030% and not more than 0.500%,
      • Si in an amount of not less than 0.50% and not more than 2.50%,
      • Mn in an amount of not less than 1.50% and not more than 5.00%,
      • P in an amount of not more than 0.100%,
      • S in an amount of not more than 0.0200%,
      • Al in an amount of not more than 1.000%,
      • N in an amount of not more than 0.0100%,
      • O in an amount of not more than 0.0100%, and
      • Nb in an amount of not less than 0.005% and not more than 0.100%,
      • with a balance consisting of Fe and inevitable impurities,
      • the steel sheet has a microstructure in which an amount of martensite is not less than 70%, an amount of retained austenite is not less than 3% and not more than 20%, and a total amount of ferrite and bainitic ferrite is not more than 10%,
      • an instability index k of retained austenite is less than 6.1, and
      • an instability index d of retained austenite in an initial stage of working is less than 5.7.
    2. [2] The high strength steel sheet according to [1] above,
      • wherein the chemical composition further includes at least one element selected from the group consisting of, by mass,
      • Ti in an amount of not more than 0.200%,
      • V in an amount of not more than 0.200%,
      • Ta in an amount of not more than 0.10%,
      • W in an amount of not more than 0.10%,
      • B in an amount of not more than 0.0100%,
      • Cr in an amount of not more than 1.00%,
      • Mo in an amount of not more than 1.00%,
      • Ni in an amount of not more than 1.00%,
      • Co in an amount of not more than 0.010%,
      • Cu in an amount of not more than 1.00%,
      • Sn in an amount of not more than 0.200%,
      • Sb in an amount of not more than 0.200%,
      • Ca in an amount of not more than 0.0100%,
      • Mg in an amount of not more than 0.0100%,
      • REM in an amount of not more than 0.0100%,
      • Zr in an amount of not more than 0.100%,
      • Te in an amount of not more than 0.100%,
      • Hf in an amount of not more than 0.10%, and
      • Bi in an amount of not more than 0.200%.
    3. [3] The high strength steel sheet according to [1] or [2] above, further comprising a plating layer on a surface of the steel sheet.
    4. [4] A method for manufacturing the high strength steel sheet according to [1] or [2] above, the method comprising:
      • retaining a steel slab having the chemical composition according to [1] or [2] above at a slab heating temperature of not lower than 1,220°C and then performing hot rolling to obtain a hot rolled steel sheet;
      • cooling the hot rolled steel sheet under a condition of an average cooling rate v1 from 800°C to 600°C of not lower than 30°C/s and then performing pickling and cold rolling to obtain a cold rolled steel sheet;
      • performing a heat treatment A in which the cold rolled steel sheet is retained at a temperature T1 of not lower than 800°C for 10 seconds or more and then cooled to a cooling stop temperature Ta of not lower than 100°C and not higher than (Ms point - 80°C),
        where, in the heat treatment A, an average cooling rate v2 from 750°C to 600°C is not lower than 20°C/s, an average cooling rate v3 from the Ms point to the cooling stop temperature Ta is not higher than 150°C/s, and a tension F imparted to the cold rolled steel sheet from the Ms point to the cooling stop temperature Ta is not less than 5 MPa and not more than 100 MPa;
      • after the heat treatment A, performing a heat treatment B in which the cold rolled steel sheet is retained at a temperature T2 of not lower than the cooling stop temperature Ta and not higher than 450°C for 5 seconds or more and 1,000 seconds or less and then cooled;
      • after the heat treatment B, performing a heat treatment C in which the cold rolled steel sheet is heated to a temperature T3 of not lower than 150°C and not higher than 400°C and then cooled without being retained at the temperature T3,
        where, in the heat treatment C, an average cooling rate v4 from 150°C to 50°C is not lower than 1.0°C/s and not higher than 50.0°C/s; and
      • after the heat treatment A and before the heat treatment C, working the cold rolled steel sheet to impart an equivalent plastic strain of not less than 0.10% and not more than 5.00% to the cold rolled steel sheet,
      • wherein the Ms point is represented in a unit of °C and determined by Formula (a): Ms = 519 - 474 × [%C] - 30.4 × [%Mn] - 12.1 × [%Cr] - 7.5 × [%Mo] - 17.7 × [%Ni]
      • in Formula (a), [%M] represents a content of an element M in the chemical composition, and when the element M is not contained, [%M] is 0.
    5. [5] The method for manufacturing the high strength steel sheet according to [4] above,
      wherein the cold rolled steel sheet is subjected to a plating treatment.
    ADVANTAGEOUS EFFECTS OF INVENTION
  • The present invention can provide a high strength steel sheet having a tensile strength (TS) of not less than 1,180 MPa, having excellent bendability and excellent delayed fracture resistance, and having a wide optimal clearance range with respect to bending forming of a shear end surface, as well as a method for manufacturing the same.
  • BRIEF DESCRIPTION OF DRAWINGS
    • [FIG. 1] FIG. 1 is a schematic view showing a specimen used in a tensile test.
    • [FIG. 2] FIG. 2 is a graph schematically showing the relation between tensile stress applied to a specimen and tensile strain during the tensile test.
    • [FIG. 3] FIG. 3 is an exemplary graph showing the relation between tensile strain ε and the amount of retained austenite.
    • [FIG. 4] FIG. 4 is another exemplary graph showing the relation between tensile strain ε and the amount of retained austenite.
    • [FIG. 5] FIG. 5 is still another exemplary graph showing the relation between tensile strain ε and the amount of retained austenite.
    DESCRIPTION OF EMBODIMENTS [High strength steel sheet]
  • A high strength steel sheet of the present embodiment (hereinafter also referred to as the "present high strength steel sheet") includes a steel sheet, and may further include a plating layer on a surface of the steel sheet as described later.
  • The steel sheet included in the present high strength steel sheet has the chemical composition and microstructure (steel structure) which are to be described later, and satisfies an instability index k and an instability index d which are to be described later.
  • The term "high strength" means having a tensile strength (TS) of not less than 1,180 MPa.
  • The high strength steel sheet has a tensile strength (TS) of not less than 1,180 MPa, has excellent bendability and excellent delayed fracture resistance, and has a wide optimal clearance range with respect to bending forming of a shear end surface.
  • Hereinafter, the optimal clearance range with respect to bending forming of a shear end surface is also simply called "optimal clearance range."
  • In summary, the present inventors found the following facts through an earnest study.
    1. (1) By having the amount of martensite being not less than 70% and the total amount of ferrite and bainitic ferrite being not more than 10%, a TS of not less than 1,180 MPa can be achieved.
    2. (2) By having the amount of retained austenite being not less than 3%, excellent bendability can be achieved.
    3. (3) By having the instability index d of retained austenite in an initial stage of working being less than 5.7 and the amount of retained austenite being not more than 20%, excellent delayed fracture resistance can be achieved.
    4. (4) By having the instability index k of retained austenite being less than 6.1 and the instability index d of retained austenite in an initial stage of working being less than 5.7, a wide optimal clearance range can be achieved.
  • The use of the present high strength steel sheet for, for instance, structural parts of automobiles allows vehicle bodies to be lighter, resulting in improved fuel consumption. Thus, the industrial utility value is quite high.
  • <Steel sheet>
  • First, the steel sheet included in the present high strength steel sheet is described.
  • The thickness of the steel sheet is not particularly limited and is, for example, not less than 0.5 mm and not more than 3.0 mm.
  • <<Chemical composition>>
  • The chemical composition of the steel sheet included in the present high strength steel sheet (hereinafter, also referred to as "present chemical composition") is described.
  • The unit "%" used for the chemical composition means "mass%" unless otherwise noted.
  • (C: not less than 0.030% and not more than 0.500%)
  • C is an element that is one of important basic components of steel and that influences the amount of martensite and the total amount of ferrite and bainitic ferrite.
  • When the amount of C is too small, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the C content is not less than 0.030%, preferably not less than 0.050%, and more preferably not less than 0.100%.
  • Meanwhile, when the amount of C is too large, martensite embrittles, resulting in lower delayed fracture resistance. Hence, the C content is not more than 0.500%, preferably not more than 0.400%, and more preferably not more than 0.350%.
  • (Si: not less than 0.50% and not more than 2.50%)
  • Si is an element that is one of important basic components of steel and that influences the TS and the amount of retained austenite.
  • When the amount of Si is too small, the strength of martensite decreases, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the Si content is not less than 0.50%, preferably not less than 0.55%, and more preferably not less than 0.60%.
  • Meanwhile, when the amount of Si is too large, retained austenite excessively increases, and this leads to lower delayed fracture resistance. Hence, the Si content is not more than 2.50%, preferably not more than 2.00%, and more preferably not more than 1.80%.
  • (Mn: not less than 1.50% and not more than 5.00%)
  • Mn is an element that is one of important basic components of steel and that influences the amount of martensite and the total amount of ferrite and bainitic ferrite.
  • When the amount of Mn is too small, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the Mn content is not less than 1.50%, preferably not less than 2.00%, and more preferably not less than 2.20%.
  • Meanwhile, when the amount of Mn is too large, martensite embrittles, resulting in lower delayed fracture resistance. Hence, the Mn content is not more than 5.00%, preferably not more than 4.50%, and more preferably not more than 4.00%.
  • (P: not more than 0.100%)
  • P segregates in a prior austenite grain boundary to embrittle the grain boundary and thus embrittle the steel sheet, resulting in lower delayed fracture resistance. Hence, the P content is not more than 0.100%, preferably not more than 0.070%, and more preferably not more than 0.030%.
  • The lower limit thereof is not particularly limited. However, P is a solid solution strengthening element and is capable of increasing the strength of the steel sheet. Hence, the P content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • (S: not more than 0.0200%)
  • S is present as a sulfide and embrittles the steel sheet, resulting in lower delayed fracture resistance. Hence, the S content is not more than 0.0200%, preferably not more than 0.0050%, and more preferably not more than 0.0025%.
  • While the lower limit is not particularly limited, the S content is preferably not less than 0.0001%, more preferably not less than 0.0003%, and even more preferably not less than 0.0005% due to production engineering constraints.
  • (Al: not more than 1.000%)
  • Al is present as an oxide and embrittles the steel sheet, resulting in lower delayed fracture resistance. Hence, the Al content is not more than 1.000%, preferably not more than 0.500%, more preferably not more than 0.150%, and even more preferably not more than 0.070%.
  • The lower limit thereof is not particularly limited. However, Al is capable of suppressing the generation of a carbide during heat treatments, which will be described later, and promoting the generation of retained austenite. Hence, the Al content is preferably not less than 0.001%, more preferably not less than 0.005%, and even more preferably not less than 0.010%.
  • (N: not more than 0.0100%)
  • N is present as a nitride and embrittles the steel sheet, resulting in lower delayed fracture resistance. Hence, the N content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • While the lower limit is not particularly limited, the N content is preferably not less than 0.0001%, more preferably not less than 0.0005%, and even more preferably not less than 0.0010% due to production engineering constraints.
  • (O: not more than 0.0100%)
  • O is present as an oxide and embrittles the steel sheet, resulting in lower delayed fracture resistance. Hence, the O content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • While the lower limit is not particularly limited, the O content is preferably not less than 0.0001%, more preferably not less than 0.0007%, and even more preferably not less than 0.0015% due to production engineering constraints.
  • (Nb: not less than 0.005% and not more than 0.100%)
  • The present inventors found, through an earnest study, that Nb influences the instability index k of retained austenite.
  • When the amount of Nb is too small, the structure after heat treatments to be described later coarsens, and the instability index k of retained austenite increases. This results in a narrower optimal clearance range. Hence, the Nb content is not less than 0.005%, preferably not less than 0.008%, and more preferably not less than 0.010%.
  • Meanwhile, when the amount of Nb is too large, martensite embrittles, resulting in lower delayed fracture resistance. Hence, the Nb content is not more than 0.100%, preferably not more than 0.080%, and more preferably not more than 0.050%.
  • (Other elements)
  • The present chemical composition may further include at least one element (another element) selected from the group consisting of the elements described below, in percentage by mass.
  • ((Ti and V))
  • When the amounts of Ti and V are too large, a large number of coarse precipitates and inclusions are generated, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the contents of Ti and V are each not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • The lower limits thereof are not particularly limited. However, Ti and V form fine carbides, nitrides, or carbonitrides during hot rolling or heat treatments, which will be described later, thereby increasing the strength of the steel sheet. Hence, the contents of Ti and V are each preferably not less than 0.001%, more preferably not less than 0.005%, and even more preferably not less than 0.015%.
  • ((Ta and W))
  • When the amounts of Ta and W are too large, a large number of coarse precipitates and inclusions are generated, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the contents of Ta and W are each not more than 0.10%, preferably not more than 0.09%, and more preferably not more than 0.08%.
  • The lower limits thereof are not particularly limited. However, Ta and W form fine carbides, nitrides, or carbonitrides during hot rolling or heat treatments, which will be described later, thereby increasing the strength of the steel sheet. Hence, the contents of Ta and W are each preferably not less than 0.01%, more preferably not less than 0.03%, and even more preferably not less than 0.05%.
  • ((B))
  • When the amount of B is too large, cracks are generated inside the steel sheet during casting or hot rolling, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the B content is not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0060%.
  • The lower limit thereof is not particularly limited. However, B segregates in a prior austenite grain boundary during heat treatments to be described later, thus improving the hardenability. Hence, the B content is preferably not less than 0.0003%, more preferably not less than 0.0005%, and even more preferably not less than 0.0010%.
  • ((Cr, Mo, and Ni))
  • When the amounts of Cr, Mo, and Ni are too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the contents of Cr, Mo, and Ni are each not more than 1.00%, preferably not more than 0.80%, and more preferably not more than 0.50%.
  • The lower limits thereof are not particularly limited. However, since Cr, Mo, and Ni are elements that improve the hardenability, the contents of Cr, Mo, and Ni are each preferably not less than 0.01%, more preferably not less than 0.04%, and even more preferably not less than 0.08%.
  • ((Co))
  • When the amount of Co is too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Co content is not more than 0.010%, preferably not more than 0.008%, and more preferably not more than 0.006%.
  • The lower limit thereof is not particularly limited. However, since Co is an element that improves the hardenability, the Co content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • ((Cu))
  • When the amount of Cu is too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Cu content is not more than 1.00%, preferably not more than 0.80%, and more preferably not more than 0.60%.
  • The lower limit thereof is not particularly limited. However, since Cu is an element that improves the hardenability, the Cu content is preferably not less than 0.01%, more preferably not less than 0.03%, and even more preferably not less than 0.05%.
  • ((Sn))
  • When the amount of Sn is too large, cracks are generated inside the steel sheet during casting or hot rolling, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Sn content is not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • The lower limit thereof is not particularly limited. However, since Sn is an element that improves the hardenability, the Sn content is preferably not less than 0.001%, more preferably not less than 0.010%, and even more preferably not less than 0.020%.
  • ((Sb))
  • When the amount of Sb is too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Sb content is not more than 0.200%, preferably not more than 0.100%, and more preferably not more than 0.050%.
  • The lower limit thereof is not particularly limited. However, since Sb is an element that controls the surface layer softening thickness and allows for adjustment of the strength, the Sb content is preferably not less than 0.001%, more preferably not less than 0.003%, and even more preferably not less than 0.005%.
  • ((Ca, Mg, and REM))
  • When the amounts of Ca, Mg, and REM (rare earth metal) are too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the contents of Ca, Mg, and REM are each not more than 0.0100%, preferably not more than 0.0080%, and more preferably not more than 0.0050%.
  • The lower limits thereof are not particularly limited. However, Ca, Mg, and REM are elements that spheroidize the shapes of nitrides and sulfides and improve the ultimate deformability of the steel sheet. Hence, the contents of Ca, Mg, and REM are each preferably not less than 0.0005%, more preferably not less than 0.0010%, and even more preferably not less than 0.0015%.
  • ((Zr and Te))
  • When the amounts of Zr and Te are too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the contents of Zr and Te are each not more than 0.100%, preferably not more than 0.080%, and more preferably not more than 0.060%.
  • The lower limits thereof are not particularly limited. However, Zr and Te are elements that spheroidize the shapes of nitrides and sulfides and improve the ultimate deformability of the steel sheet. Hence, the contents of Zr and Te are each preferably not less than 0.001%, more preferably not less than 0.008%, and even more preferably not less than 0.015%.
  • ((Hf))
  • When the amount of Hf is too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Hf content is not more than 0.10%, preferably not more than 0.09%, and more preferably not more than 0.08%.
  • The lower limit thereof is not particularly limited. However, Hf is an element that spheroidizes the shapes of nitrides and sulfides and improves the ultimate deformability of the steel sheet. Hence, the Hf content is preferably not less than 0.01%, more preferably not less than 0.02%, and even more preferably not less than 0.03%.
  • ((Bi))
  • When the amount of Bi is too large, coarse precipitates and inclusions increase, and the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the Bi content is not more than 0.200%, preferably not more than 0.150%, and more preferably not more than 0.100%.
  • The lower limit thereof is not particularly limited. However, since Bi is an element that reduces the segregation, the Bi content is preferably not less than 0.001%, more preferably not less than 0.020%, even more preferably not less than 0.050%, and particularly preferably not less than 0.090%.
  • With respect to the above-described other elements, when the content of an element is less than its preferable lower limit, the element does not impair the effect of the present invention and is therefore considered an inevitable impurity.
  • (Balance)
  • The balance in the present chemical composition consists of Fe and inevitable impurities.
  • <<Microstructure>>
  • Next, the microstructure of the steel sheet included in the present high strength steel sheet (hereinafter also referred to as "present microstructure") is described.
  • (Total amount of ferrite and bainitic ferrite: not more than 10%)
  • When the amounts of ferrite and bainitic ferrite are too large, it is difficult to achieve a TS of not less than 1,180 MPa. Hence, the total amount of ferrite and bainitic ferrite is not more than 10%, preferably not more than 9%, and more preferably not more than 8%.
  • The lower limit thereof is not particularly limited.
  • The amounts of ferrite and bainitic ferrite are obtained in the following manner.
  • The steel sheet is polished to expose, as an observation surface, an L cross section at the 1/4 sheet thickness position (the position corresponding to 1/4 of the sheet thickness from the surface of the steel sheet in the depth direction). The observation surface is etched using 3 vol% Nital and then observed in 10 fields with a scanning electron microscope (SEM) at a magnification of 2,000X, whereby an SEM image of each field is obtained. In the SEM images, ferrite and bainitic ferrite are observed as recessed structures with their inside portions being flat. The area fraction (unit: %) of ferrite and bainitic ferrite in each SEM image is obtained, and the average of the obtained area fractions of the 10 fields is defined as the total amount of ferrite and bainitic ferrite.
  • (Amount of retained austenite: not less than 3% and not more than 20%)
  • The amount of retained austenite is not less than 3%, preferably not less than 5%, more preferably not less than 7%, and even more preferably not less than 8% because excellent bendability can be achieved.
  • Meanwhile, the amount of retained austenite is not more than 20%, preferably not more than 15%, and more preferably not more than 13% because excellent delayed fracture resistance can be achieved.
  • The amount of retained austenite is determined in the following manner.
  • The steel sheet is polished to expose an L cross section at a position 0.1 mm deeper than the 1/4 sheet thickness position. This L cross section is further polished by 0.1 mm in the depth direction by chemical polishing to obtain an observation surface. For the observation surface, integral intensity ratios of diffraction peaks are determined using CoKα radiation in an X-ray diffraction (XRD) instrument. More specifically, integral intensity ratios between diffraction peaks of respective planes {200}, {220}, and {311} of fcc iron and those of respective planes {200}, {211}, and {220} of bcc iron are determined. The average of nine integral intensity ratios is defined as the volume fraction (unit: %) of the amount of retained austenite, and the obtained value is specified as the amount of retained austenite.
  • (Amount of martensite: not less than 70%)
  • The amount of martensite is not less than 70%, preferably not less than 75%, and more preferably not less than 80% because a TS of not less than 1,180 MPa can be achieved.
  • Of plural types of martensite, tempered martensite is important in terms of the contribution to achievement of a high TS, and the amount of tempered martensite is preferably not less than 80%.
  • The amount of martensite is determined in the following manner.
  • First, the amount of retained austenite and the total amount of ferrite and bainitic ferrite are obtained by the foregoing methods. Next, the sum of those amounts is subtracted from 100%, and the obtained value (unit: %) is defined as the amount of martensite.
  • Accordingly, the amount of martensite herein includes both amounts of hardened martensite and tempered martensite.
  • It should be noted that the amount of retained austenite is the volume fraction as described above, and this is substantially equivalent to the area fraction. Accordingly, the amount of retained austenite is, together with the total amount of ferrite and bainitic ferrite which is the area fraction, subtracted from 100%.
  • <<Instability index k: less than 6.1>>
  • The present inventors found, through an earnest study, that the instability index k of retained austenite (also simply referred to as "instability index k") influences the optimal clearance range.
  • When the instability index k is too high, the stability of retained austenite is low, and the retained austenite excessively transforms to hard martensite in shearing. This decreases the ultimate deformability of the steel sheet, resulting in a narrower optimal clearance range.
  • Hence, the instability index k is less than 6.1, preferably not more than 5.0, more preferably not more than 4.0, and even more preferably not more than 3.5.
  • While the lower limit is not particularly limited, the instability index k is for example not less than 1.0, preferably not less than 1.5, and more preferably not less than 2.0.
  • <<Instability index d: less than 5.7>>
  • The present inventors found, through an earnest study, that the instability index d of retained austenite in an initial stage of working (also simply referred to as "instability index d") influences the delayed fracture resistance and the optimal clearance range.
  • When the instability index d is too high, the stability of retained austenite in an initial stage of working is low, and the retained austenite excessively transforms to hard martensite in the initial stage of working and would act as starting points of generation of delayed fractures in a hydrogen entering environment, thus lowering the delayed fracture resistance.
  • In addition, when the instability index d is too high, retained austenite excessively transforms to hard martensite in an initial stage of working, whereby the ultimate deformability of the steel sheet decreases, resulting in a narrower optimal clearance range.
  • Thus, the instability index d is less than 5.7, preferably not more than 5.0, more preferably not more than 4.0, and even more preferably not more than 3.5.
  • While the lower limit is not particularly limited, the instability index d is for example not less than -15.0, preferably not less than -10.0, and more preferably not less than -5.0.
  • The instability index k and the instability index d are determined in the following manner.
  • First, a tensile test to be described later (the details of which are described in EXAMPLES) is carried out to work a specimen (JIS No. 5 specimen) of a steel sheet.
  • FIG. 1 is a schematic view showing a specimen used in the tensile test. FIG. 2 is a graph schematically showing the relation between tensile stress applied to a specimen 1 and tensile strain during the tensile test.
  • As shown in FIG. 2, tensile stress is applied to a specimen to impart tensile strain (tensile plasticity strain). A plurality of specimens to each of which given tensile strain ε has been imparted in the range of 0% to 10% (0 to 0.10) are obtained in this manner. The tensile strain ε before working (before impartment of tensile strain) is 0%.
  • Thereafter, for a central portion (hatched portion in FIG. 1) of each specimen, the amount of retained austenite when the tensile strain ε is imparted is obtained in the above-described manner. The obtained results are plotted on a graph (horizontal axis: tensile strain ε, vertical axis: logarithm of amount of retained austenite).
  • For the respective plots in the graphs (see FIGs. 3 to 5 to be described later), a first order approximation formula (y = -ax + b) is obtained using the least square method. The obtained approximation formula is applied to Formula (1) below, and the slope a of the approximation formula is obtained as the instability index k of retained austenite. log = k · ε + log 0
  • In Formula (1) above, fy represents the amount of retained austenite when the tensile strain ε is imparted, and fγ0 represents the amount of retained austenite before working.
  • Further, an estimate value of the amount of retained austenite before working (i.e., at the time when the tensile strain ε is 0%) is obtained from the intercept of Formula (1) above. Then, the instability index d of retained austenite before working is obtained based on Formula (2) below. d = 0 fγε 0
  • In Formula (2) above, fγ0 represents the actual measurement value of the amount of retained austenite before working, and fγε0 represents the estimate value of retained austenite before working.
  • FIG. 3 is an exemplary graph showing the relation between the tensile strain ε and the amount of retained austenite. FIG. 4 is another example of the graph. FIG. 5 is still another example of the graph.
  • Comparing FIGs. 3 and 4, the slope a (instability index k) of the approximation formula in FIG. 3 is 2.3 and is smaller than the slope a (instability index k) of the approximation formula in FIG. 4, that is, 11.9.
  • The slope a (instability index k) of the approximation formula being small indicates that the change in the amount of retained austenite is small during working, and the stability of retained austenite is good.
  • Referring to FIG. 5 next, the slope a (instability index k) of the approximation formula is as small as 4.0.
  • In FIG. 5, however, while the estimate value fγε0 of retained austenite before working is 12.3 (log(fγε0) = 1.09), the actual measurement value fγ0 of the amount of retained austenite before working is 18 (log(fγ0) = 1.26), and the instability index d (= fγ0 - fγε0) is as large as 5.7.
  • When the instability index d is large, the slope of the approximation formula is large as far as an initial stage of working (initial stage of the tensile test) is concerned. That is, in this case, the stability of retained austenite is insufficient in the initial stage of working.
  • Hence, when both the instability index k and the instability index d satisfy the foregoing ranges, then retained austenite has excellent stability during working and also in the initial stage of working.
  • <Plating layer>
  • The present high strength steel sheet may further have a plating layer on a surface of the steel sheet for the purpose of improving corrosion resistance and other properties.
  • Examples of the plating layer include a galvanizing layer, a galvannealing layer, and an electrogalvanizing layer. The plating layer is formed by a plating treatment to be described later.
  • The coating weight of the plating layer is not particularly limited and is preferably 20 to 80 g/m2 per one side.
  • [Method for manufacturing high strength steel sheet]
  • Next, a method for manufacturing a high strength steel sheet according to the present embodiment (hereinafter also referred to as "present manufacturing method") is described. The present manufacturing method is also a method for manufacturing the present high strength steel sheet described above.
  • The temperature at which a steel slab, the steel sheet, or the like is heated or cooled, which is described below, means a surface temperature of the steel slab, the steel sheet, or the like, unless otherwise specified.
  • A method of manufacturing molten steel which becomes a steel slab is not particularly limited, and known methods using a converter, an electric furnace, or the like are applicable. It is preferable to obtain a steel slab from molten steel by a continuous casting method for the sake of preventing macro-segregation.
  • <Hot rolling>
  • In the present manufacturing method, first, a steel slab having the present chemical composition described above is retained at a slab heating temperature described below and then hot-rolled to obtain a hot rolled steel sheet.
  • <<Slab heating temperature: not lower than 1,220°C>>
  • An excessively low slab heating temperature leads to insufficient dissolution of inclusions, and accordingly, the steel sheet embrittles, resulting in lower delayed fracture resistance. Hence, the slab heating temperature is preferably not lower than 1,220°C, more preferably not lower than 1,230°C, and even more preferably higher than 1,230°C.
  • While the upper limit is not particularly limited, the slab heating temperature is preferably not higher than 1,300°C, more preferably not higher than 1,290°C, and even more preferably not higher than 1,280°C.
  • <Cooling>
  • The hot rolled steel sheet obtained through the hot rolling is cooled. In this process, an average cooling rate v1 from 800°C to 600°C satisfies the range described below.
  • <<Average cooling rate v1: not lower than 30°C/s>>
  • The present inventors found, through an earnest study, that the average cooling rate v1 from 800°C to 600°C (also simply referred to as "average cooling rate v1") influences the instability index k of retained austenite.
  • When the average cooling rate v1 is too low, coarse Nb-based carbides are excessively precipitated during cooling, and the effect of lowering the instability index k of retained austenite decreases due to Nb. This results in an increased instability index k and a narrower optimal clearance range.
  • Hence, the average cooling rate v1 is not lower than 30°C/s, preferably not lower than 35°C/s, and more preferably not lower than 40°C/s.
  • <Pickling and cold rolling>
  • Next, the hot rolled steel sheet thus cooled is subjected to pickling and cold rolling to obtain a cold rolled steel sheet.
  • Because pickling is capable of removing oxides on a surface of the hot rolled steel sheet, pickling is important to ensure good chemical convertibility and good plating quality of the final product, i.e., a high strength steel sheet. Pickling may be performed only once, or may be divided into plural steps.
  • The hot rolled steel sheet is subjected to pickling, thereby obtaining a pickled sheet. Subsequently, the pickled sheet is dried as appropriate.
  • Cold rolling may be performed on the pickled sheet before being dried or after being dried.
  • The rolling reduction in the cold rolling and the sheet thickness after the rolling are not particularly limited. The number of rolling passes and the rolling reduction for each pass are also not particularly limited.
  • Next, the cold rolled steel sheet obtained by the cold rolling is subjected to a heat treatment A, a heat treatment B, and a heat treatment C, as described below, in this order. The heat treatment C is preceded by working described below.
  • The details thereof are described below.
  • <Heat treatment A>
  • First, the cold rolled steel sheet obtained by the cold rolling is subjected to the heat treatment A.
  • In short, in the heat treatment A, the cold rolled steel sheet is retained (heated) at a temperature T1 described below and then cooled to a cooling stop temperature Ta described below.
  • The conditions for the heat treatment A are described below.
  • <<Temperature T1: not lower than 800°C>>
  • First, the cold rolled steel sheet is retained (heated) at the temperature T1. When the temperature T1 is too low, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa.
  • Hence, the temperature T1 is not lower than 800°C, preferably not lower than 820°C, and more preferably not lower than 840°C.
  • While the upper limit is not particularly limited, the temperature T1 is for instance not higher than 940°C, preferably not higher than 920°C, and more preferably not higher than 900°C.
  • <<Retaining time t1: 10 seconds or more>>
  • When the time for retaining (heating) the cold rolled steel sheet at the temperature T1 (retaining time t1) is too short, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa.
  • Hence, the retaining time t1 is 10 seconds or more, preferably 30 seconds or more, and more preferably 50 seconds or more.
  • While the upper limit is not particularly limited, the retaining time t1 is for instance 300 seconds or less, preferably 250 seconds or less, and more preferably 200 seconds or less.
  • <<Cooling stop temperature Ta: not lower than 100°C and not higher than (Ms point - 80°C)>>
  • Next, the cold rolled steel sheet having been retained at the temperature T1 is cooled to the cooling stop temperature Ta.
  • When the cooling stop temperature Ta is too low, the amount of retained austenite decreases, resulting in lower bendability. Hence, the cooling stop temperature Ta is not lower than 100°C, preferably not lower than 120°C, and more preferably not lower than 140°C.
  • Meanwhile, when the cooling stop temperature Ta is too high, the amount of retained austenite excessively increases, and this leads to lower delayed fracture resistance. Hence, the cooling stop temperature Ta is not higher than (Ms point - 80°C), preferably not higher than (Ms point - 90°C), and more preferably not higher than (Ms point - 100°C).
  • When the cold rolled steel sheet is cooled from the temperature T1 to the cooling stop temperature Ta, the average cooling rates in temperature ranges described below are controlled to the ranges described below.
  • <<Average cooling rate v2: not lower than 20°C/s>>
  • When an average cooling rate v2 from 750°C to 600°C (also simply referred to as "average cooling rate v2") is too low, the amount of martensite decreases, while the total amount of ferrite and bainitic ferrite increases, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the average cooling rate v2 is not lower than 20°C/s, preferably not lower than 22°C/s, and more preferably not lower than 24°C/s.
  • While the upper limit is not particularly limited, the average cooling rate v2 is for instance not higher than 65°C/s, preferably not higher than 55°C/s, and more preferably not higher than 45°C/s.
  • <<Average cooling rate v3: not higher than 150°C/s>>
  • The present inventors found, through an earnest study, that an average cooling rate v3 from the Ms point to the cooling stop temperature Ta (also simply referred to as "average cooling rate v3") influences the instability index d of retained austenite in an initial stage of working.
  • When the average cooling rate v3 is too high, retained austenite coarsens due to a high martensitic transformation rate, and the instability index d of retained austenite in an initial stage of working increases. This results in lower delayed fracture resistance and a narrower optimal clearance range. Hence, the average cooling rate v3 is not higher than 150°C/s, preferably not higher than 120°C/s, and more preferably not higher than 90°C/s.
  • While the lower limit is not particularly limited, the average cooling rate v3 is for instance not lower than 5°C/s, preferably not lower than 8°C/s, and more preferably not lower than 10°C/s.
  • <<Tension F: not less than 5 MPa and not more than 100 MPa>>
  • The present inventors found, through an earnest study, that a tension F imparted to the cold rolled steel sheet from the Ms point to the cooling stop temperature Ta (also simply referred to as "tension F") influences the instability index d of retained austenite in an initial stage of working.
  • When the tension F is too small, martensite nucleation sites decrease, so that retained austenite coarsens, and the instability index d of retained austenite in an initial stage of working increases. This results in lower delayed fracture resistance and a narrower optimal clearance range. Hence, the tension F is not less than 5 MPa, preferably not less than 6 MPa, and more preferably not less than 8 MPa.
  • Meanwhile, when the tension F is too large, martensitic transformation excessively proceeds, so that the amount of retained austenite to be obtained decreases, resulting in lower bendability. Hence, the tension F is not more than 100 MPa, preferably not more than 50 MPa, and more preferably not more than 25 MPa.
  • <<Ms point>>
  • The Ms point (unit: °C) is determined by Formula (a) below. Ms = 519 - 474 × [%C] - 30.4 × [%Mn] - 12.1 × [%Cr] - 7.5 × [%Mo] - 17.7 × [%Ni]
  • In Formula (a) above, [%M] represents the content of an element M in the chemical composition, and when the element M is not contained, [%M] is 0.
  • <Heat treatment B>
  • Next, the cold rolled steel sheet having been cooled to the cooling stop temperature Ta is subjected to the heat treatment B.
  • In short, in the heat treatment B, the cold rolled steel sheet is retained (heated) at a temperature T2 described below and then cooled to a temperature (e.g., room temperature) lower than the temperature T2. The room temperature is 25±5°C, for instance.
  • The conditions for the heat treatment B are described below.
  • <<Temperature T2: not lower than cooling stop temperature Ta and not higher than 450°C>>
  • First, the cold rolled steel sheet is retained (heated) at the temperature T2. This stabilizes retained austenite. When the temperature T2 is too low, a desired amount of retained austenite is not obtained, resulting in lower bendability. Hence, the temperature T2 is not lower than the cooling stop temperature Ta, preferably not lower than (Ta + 10°C), and more preferably not lower than (Ta + 20°C) .
  • Meanwhile, when the temperature T2 is too high, tempering of martensite excessively proceeds, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the temperature T2 is not higher than 450°C, preferably not higher than 420°C, and more preferably not higher than 400°C.
  • <<Retaining time t2: 5 seconds or more and 1,000 seconds or less>>
  • When the time for retaining the cold rolled steel sheet at the temperature T2 (retaining time t2) is too short, stabilization of austenite is insufficient, and the instability index k of retained austenite increases, resulting in a narrower optimal clearance range. Hence, the retaining time t2 is 5 seconds or more, preferably 50 seconds or more, and more preferably 80 seconds or more.
  • Meanwhile, when the retaining time t2 is too long, tempering of martensite excessively proceeds, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the retaining time t2 is 1,000 seconds or less, preferably 800 seconds or less, and more preferably 400 seconds or less.
  • <Working (impartment of equivalent plastic strain)>
  • The cold rolled steel sheet is wrought to impart equivalent plastic strain to the cold rolled steel sheet after the heat treatment A described above and before the heat treatment C described below.
  • The temperature during the working is not particularly limited. For instance, the working may be carried out while the cold rolled steel sheet is retained at the temperature T2 or after the cold rolled steel sheet is cooled to, for example, the room temperature subsequent to the retention at the temperature T2.
  • <<Equivalent plastic strain: not less than 0.10% and not more than 5.00%>>
  • The present inventors found, through an earnest study, that equivalent plastic strain imparted to the cold rolled steel sheet through the working (also simply referred to as "equivalent plastic strain") influences the instability index d of retained austenite in an initial stage of working.
  • When the equivalent plastic strain is too small, unstable retained austenite that transforms in an initial stage of working increases, and accordingly, the instability index d increases, resulting in lower delayed fracture resistance and a narrower optimal clearance range. Hence, the equivalent plastic strain is not less than 0.10%, preferably not less than 0.15%, and more preferably not less than 0.30%.
  • Meanwhile, when the equivalent plastic strain is too large, work-induced transformation of retained austenite excessively proceeds, and the amount of retained austenite to be obtained decreases, resulting in lower bendability. Hence, the equivalent plastic strain is not more than 5.00%, preferably not more than 4.00%, and more preferably not more than 3.00%.
  • <<Number of times of working>>
  • The number of times the cold rolled steel sheet is wrought is not particularly limited.
  • Specifically, the working may be divided into plural steps as long as the total equivalent plastic strain imparted to the cold rolled steel sheet through the whole working is within the foregoing range.
  • For instance, even when the equivalent plastic strain imparted to the cold rolled steel sheet in the first working is less than the foregoing lower limit value, it suffices if the total equivalent plastic strain obtained after the second and subsequent working is not less than the foregoing lower limit value (not more than the foregoing lower limit value).
  • <<Working method>>
  • Examples of the method of working the cold rolled steel sheet include: a method in which the cold rolled steel sheet is subjected to temper rolling; and a method in which the cold rolled steel sheet is wrought using a tension leveler. Examples of the leveler include a tension leveler, a continuous stretcher leveler, and a roller leveler, and a tension leveler is favorable.
  • When temper rolling is performed, the equivalent plastic strain is an elongation rate of the steel sheet (cold rolled steel sheet) and is determined from the change in length of the steel sheet before and after working.
  • When the cold rolled steel sheet is wrought using a tension leveler, the equivalent plastic strain is calculated according to the method described in Reference Literature 1 below. For the calculation, the following data input values are used, a material is assumed to be an elasto-plastic body whose work hardening behavior is linear curing, Bauschinger curing is ignored, and a decrease in tension due to bend loss is ignored. For the working curvature formula, Misaka's formula is used.
  • Number of dividing sheet thickness: 31
    • Young's modulus: 21,000 kgf/mm2
    • Poisson's ratio: 0.3
    • Yield stress: 111 kgf/mm2
    • Plasticity coefficient: 1,757 kgf/mm2
    • Reference Literature 1: Yoshisuke MISAKA, Takeshi MASUI, Sosei to kakou [plasticity and working], 1976, vol. 17, pp. 988-994
    <Heat treatment C>
  • Next, the cold rolled steel sheet having been cooled to, for example, the room temperature is subjected to the heat treatment C.
  • In short, in the heat treatment C, the cold rolled steel sheet is heated to a temperature T3 described below and then cooled to a temperature (e.g., room temperature) lower than the temperature T3 without being retained at the temperature T3.
  • <<Temperature T3: not lower than 150°C and not higher than 400°C>>
  • When the temperature T3 is too low, stabilization of austenite is insufficient, and the instability index k of retained austenite increases, resulting in a narrower optimal clearance range. Hence, the temperature T3 is not lower than 150°C, preferably not lower than 160°C, and more preferably not lower than 170°C.
  • Meanwhile, when the temperature T3 is too high, tempering of martensite excessively proceeds, and this makes it difficult to achieve a TS of not less than 1,180 MPa. Hence, the temperature T3 is not higher than 400°C, preferably not higher than 350°C, and more preferably not higher than 300°C.
  • <<No retention at temperature T3>>
  • If the cold rolled steel sheet is retained at the temperature T3, precipitation of carbides is promoted, so that carbon contributing to stabilization of austenite is consumed. This makes stabilization of austenite insufficient, and the instability index k of retained austenite increases, resulting in a narrower optimal clearance range.
  • Hence, the cold rolled steel sheet having been heated to the temperature T3 is immediately cooled without being retained at the temperature T3 as described above.
  • When the cold rolled steel sheet is cooled from the temperature T3 to, for example, the room temperature, the average cooling rate in the temperature range described below is controlled to the range described below.
  • <<Average cooling rate v4: not lower than 1.0°C/h and not higher than 50.0°C/h>>
  • When an average cooling rate v4 from 150°C to 50°C (also simply referred to as "average cooling rate v4") is too high, concentrating of carbon into austenite during cooling is insufficient. This makes stabilization of austenite insufficient, and the instability index k of retained austenite increases, resulting in a narrower optimal clearance range. Hence, the average cooling rate v4 is not higher than 50.0°C/h, preferably not higher than 48.0°C/h, and more preferably not higher than 45.0°C/h.
  • Meanwhile, the average cooling rate v4 is not lower than 1.0°C/h, preferably not lower than 1.2°C/h, and more preferably not lower than 1.4°C/h due to production engineering constraints.
  • The cold rolled steel sheet having undergone the heat treatment C corresponds to the steel sheet included in the present high strength steel sheet described above.
  • After the heat treatment C, the cold rolled steel sheet may be wrought to again impart an equivalent plastic strain of not less than 0.10% and not more than 5.00%. After the working, the cold rolled steel sheet may be heated at a temperature of not lower than 100°C and not higher than 400°C.
  • <Plating treatment>
  • The cold rolled steel sheet may be subjected to a plating treatment. A plating layer is thereby formed.
  • The plating treatment is performed, for instance, during or after the heat treatment A described above.
  • In the case of performing the plating treatment during the heat treatment A, a galvanizing treatment or a galvannealing treatment (treatment in which alloying is performed after galvanizing treatment) is performed while (or after) the cold rolled steel sheet is cooled from 750°C to 600°C at the average cooling rate v2, for example.
  • In the case of performing the plating treatment after the heat treatment A, an electrogalvanizing treatment is performed after the heat treatment B, for example. Examples of the electrogalvanizing treatment include a Zn-Ni electric alloy plating treatment, and a pure Zn electroplating treatment.
  • It should be noted that the plating treatment is not limited to the aforementioned galvanizing treatment, galvannealing treatment, or electrogalvanizing treatment. The metal species used in the plating treatment is not limited to Zn and may be other metals (e.g., Al).
  • The coating weight of the plating layer to be formed can be adjusted by performing wiping during the plating treatment.
  • Other conditions for the plating treatment are not particularly limited, and the plating treatment can be carried out according to an ordinary method.
  • A series of treatments including the heat treatments A to C and the plating treatment as described above is preferably carried out in a continuous galvanizing line (CGL) for the sake of productivity.
  • [EXAMPLES]
  • The invention is specifically described below by way of examples. However, the invention is not limited to the examples described below.
  • <Manufacture of steel sheet>
  • Molten steel having a chemical composition as shown in Table 1 below with the balance being Fe and inevitable impurities was made in a converter, and a steel slab was obtained by a continuous casting method. In Table 1 below, the underlined figures mean those out of the ranges of the invention (the same applies to Tables 2 and 3 to be described later).
  • The obtained steel slab was retained at a slab heating temperature as shown in Table 2 below and then hot rolled to obtain a hot rolled steel sheet. The hot rolled steel sheet obtained was cooled. In this process, the hot rolled steel sheet was cooled from 800°C to 600°C at the average cooling rate v1 as shown in Table 2 below.
  • The hot rolled steel sheet thus cooled was pickled and then cold rolled to obtain a cold rolled steel sheet.
  • The cold rolled steel sheet obtained was subjected to the heat treatments A to C under the conditions shown in Table 2 below. Before the heat treatment C, the cold rolled steel sheet was wrought under the conditions shown in Table 2 below.
  • In this manner, the cold rolled steel sheet with the final sheet thickness shown in Table 2 below was obtained.
  • In some examples, the cold rolled steel sheet (CR) was subjected to a plating treatment (galvanizing treatment, galvannealing treatment, or electrogalvanizing treatment) to obtain a galvanized steel sheet (GI), a galvannealed steel sheet (GA), or an electrogalvanized steel sheet (EG).
  • The galvanizing treatment and the galvannealing treatment were each performed during cooling in the heat treatment A. The electrogalvanizing treatment was performed after the heat treatment B (before the heat treatment C).
  • As a galvanizing bath, when GI was manufactured, a zinc bath containing 0.20 mass% of Al with the balance being Zn and inevitable impurities was used, and when GA was manufactured, a zinc bath containing 0.14 mass% of Al with the balance being Zn and inevitable impurities was used.
  • The bath temperature was set to 470°C for both cases of manufacturing GI and GA.
  • The coating weight of the plating layer was 45 to 72 g/m2 per one side when GI was manufactured and 45 g/m2 per one side when GA was manufactured.
  • When GA was manufactured, the alloying temperature was set to 500°C.
  • The composition of the plating layer of GI was the composition including 0.1 to 1.0 mass% of Fe and 0.2 to 1.0 mass% of Al with the balance being Zn and inevitable impurities. The composition of the plating layer of GA was the composition including 7 to 15 mass% of Fe and 0.1 to 1.0 mass% of Al with the balance being Zn and inevitable impurities.
  • When EG was manufactured, the electrogalvanizing treatment was performed such that the plating layer had a coating weight of 30 g/m2 per one side.
  • Hereinbelow, each of the cold rolled steel sheet (CR), the galvanized steel sheet (GI), the galvannealed steel sheet (GA), and the electrogalvanized steel sheet (EG) is also simply referred to as "steel sheet."
  • <Observation of microstructure>
  • With respect to each of the obtained steel sheets, the amount of martensite, the amount of retained austenite, and the total amount of ferrite and bainitic ferrite were obtained by the foregoing methods. The results are shown in Table 3 below. In Table 3 below, martensite is denoted as "M," austenite "γ," ferrite "F," and bainitic ferrite "BF."
  • <Instability index k and instability index d>
  • With respect to each of the obtained steel sheets, the instability index k of retained austenite and the instability index d of retained austenite in an initial stage of working were obtained by the foregoing methods. The results are shown in Table 3 below.
  • <Evaluation>
  • With respect to each of the obtained steel sheets, various properties were evaluated through the tests described below. The results are shown in Table 3 below.
  • <<Tensile strength (tensile test)>>
  • From each of the obtained steel sheets, a JIS No. 5 specimen (gauge length: 50 mm; parallel width: 25 mm) with its longitudinal direction (tensile direction) being perpendicular to the rolling direction was sampled. Using the specimen thus sampled, a tensile test was performed in accordance with JIS Z 2241 under the condition of a crosshead speed of 1.67 x 10-1 mm/s; thus, the tensile strength (TS) was determined.
  • The strength was determined to be high when the TS was not less than 1,180 MPa.
  • <<Bendability (bending test)>>
  • From each of the obtained steel sheets, a specimen (width: 30 mm; length: 100 mm) with its longitudinal direction being perpendicular to the rolling direction was sampled. Using the specimen thus sampled, a bending test was performed in accordance with a V-block method stated in JIS Z 2248 to measure a minimum bending radius R with which cracking did not occur at a bent ridge portion.
  • Occurrence or non-occurrence of cracking was checked by observing the bent ridge portion with a digital microscope (RH-2000, manufactured by HIROX Co., Ltd.) at a magnification of 40X.
  • The bendability was determined to be excellent when a value obtained by dividing the minimum bending radius R by the sheet thickness t (R/t) was not more than 6.0.
  • <<Delayed fracture resistance>>
  • From each of the obtained steel sheets, a specimen (parallel width: 6 mm; parallel length: 15 mm) with its width direction being parallel to the rolling direction was sampled. The entire surface of the specimen was ground to a sheet thickness of 1.0 mm, and then a test was performed.
  • The specimen was immersed in an aqueous solution containing 3 mass% of NaCl and 3 g/L of NH4SCN and retained for 24 hours with an applied current density of 0 or 0.05 mA/cm2. Thereafter, a tensile test (SSRT test) was performed at a tensile rate of 5 µm/min to break the specimen, thus determining the tensile strength (TS).
  • The ratio of the TS when the applied current density was 0.05 mA/cm2 to the TS when the applied current density was 0 mA/cm2 was obtained as a stress ratio.
  • In Table 3 below, "C" was provided when the stress ratio was less than 0.70, "B" was provided when it was not less than 0.70 and less than 0.80, and "A" was provided when it was not less than 0.80. In the case of "B" or "A," the delayed fracture resistance was determined to be excellent.
  • <<Optimal clearance range>>
  • The optimal clearance range with respect to bending forming of a shear end surface was determined as follows.
  • First, each of the obtained steel sheets was sheared to sample a specimen (width: 30 mm; length: 100 mm) with its longitudinal direction being perpendicular to the rolling direction. The rake angle in shearing was set to 0° in all examples, and the shear clearance was varied to 5%, 10%, 15%, 20%, 25%, 30%, and 35%.
  • With the specimen obtained through the shearing, a bending test was carried out in accordance with the method described above by use of a punch with which a value obtained by dividing the minimum bending radius R by the sheet thickness t (R/t) became 6.0. Thus, a shear end surface of the specimen was subjected to bending forming (bending). Thereafter, the shear end surface of the specimen was checked for occurrence or non-occurrence of cracking.
  • Occurrence or non-occurrence of cracking was checked by observing the shear end surface of the specimen with a digital microscope (RH-2000, manufactured by HIROX Co., Ltd.) at a magnification of 40X.
  • In Table 3 below, "C" was provided when the shear clearance range with which no cracking occurred in the shear end surface of the specimen was less than 10%, "B" was provided when it was not less than 10% and less than 15%, and "A" was provided when it was not less than 15%. In the case of "B" or "A," the optimal clearance range with respect to bending forming of a shear end surface was determined to be wide. [Table 1]
    Table 1 (1/3)
    Type of Steel Chemical composition [mass%] Remarks
    C Si Mn P S N O Al Nb Ti B Cu Others
    A 0.211 1.03 2.96 0.009 0.0010 0.0060 0.0020 0.030 0.022 IE
    B 0.246 1.13 2.88 0.006 0.0007 0.0030 0.0060 0.021 0.021 IE
    C 0.211 1.18 2.96 0.014 0.0012 0.0040 0.0040 0.040 0.017 IE
    D 0.218 1.18 2.98 0.009 0.0010 0.0050 0.0020 0.017 0.016 IE
    E 0.245 1.35 2.70 0.014 0.0006 0.0010 0.0050 0.031 0.018 IE
    F 0.047 1.02 2.86 0.013 0.0013 0.0050 0.0020 0.038 0.017 IE
    G 0.025 1.35 2.93 0.010 0.0014 0.0030 0.0040 0.028 0.016 CE
    H 0.489 1.27 2.68 0.011 0.0006 0.0050 0.0020 0.017 0.017 IE
    I 0.519 1.07 2.67 0.014 0.0010 0.0060 0.0020 0.037 0.019 CE
    J 0.228 0.52 2.94 0.007 0.0014 0.0040 0.0060 0.031 0.016 IE
    K 0.214 0.41 2.76 0.005 0.0007 0.0010 0.0030 0.023 0.019 CE
    L 0.225 2.48 2.64 0.006 0.0009 0.0050 0.0070 0.055 0.015 IE
    M 0.224 2.57 2.86 0.013 0.0012 0.0040 0.0070 0.060 0.021 CE
    N 0.228 1.12 1.62 0.006 0.0012 0.0050 0.0030 0.014 0.021 IE
    O 0.233 1.05 1.23 0.013 0.0011 0.0070 0.0030 0.038 0.019 CE
    P 0.220 1.29 4.71 0.009 0.0010 0.0030 0.0030 0.024 0.018 IE
    Q 0.237 1.34 5.12 0.008 0.0007 0.0030 0.0060 0.020 0.015 CE
    R 0.248 1.22 2.83 0.097 0.0005 0.0060 0.0030 0.021 0.018 IE
    S 0.215 1.31 2.99 0.115 0.0015 0.0060 0.0040 0.042 0.021 CE
    T 0.245 1.21 2.81 0.013 0.0195 0.0060 0.0030 0.025 0.017 IE
    Table 1 (2/3)
    Type of Steel Chemical composition [mass%] Remarks
    C Si Mn P S N O Al Nb Ti B Cu Others
    U 0.214 1.29 2.84 0.011 0.0215 0.0010 0.0060 0.050 0.021 CE
    V 0.241 1.10 2.83 0.008 0.0014 0.0060 0.0060 0.924 0.022 IE
    W 0.217 1.05 2.68 0.010 0.0014 0.0060 0.0040 1.054 0.022 CE
    X 0.226 1.09 2.75 0.005 0.0013 0.0090 0.0060 0.025 0.021 IE
    Y 0.243 1.31 2.72 0.006 0.0007 0.0120 0.0040 0.035 0.021 CE
    Z 0.222 1.26 2.60 0.008 0.0014 0.0040 0.0090 0.027 0.021 IE
    AA 0.223 1.25 2.70 0.011 0.0011 0.0040 0.0110 0.037 0.021 CE
    AB 0.212 1.22 2.91 0.006 0.0010 0.0040 0.0020 0.038 0.008 IE
    AC 0.213 1.07 3.00 0.006 0.0011 0.0020 0.0030 0.025 0.003 CE
    AD 0.227 1.15 2.61 0.010 0.0011 0.0060 0.0050 0.030 0.080 IE
    AE 0.214 1.30 2.71 0.011 0.0015 0.0010 0.0030 0.012 0.114 CE
    AF 0.216 1.11 2.63 0.006 0.0009 0.0030 0.0030 0.049 0.018 0.042 IE
    AG 0.214 1.30 2.90 0.006 0.0008 0.0030 0.0040 0.024 0.020 0.189 IE
    AH 0.235 1.26 2.64 0.006 0.0011 0.0060 0.0030 0.022 0.017 0.215 CE
    AI 0.217 1.31 2.69 0.011 0.0006 0.0040 0.0030 0.038 0.016 0.0021 IE
    AJ 0.238 1.26 2.61 0.014 0.0014 0.0020 0.0070 0.017 0.017 0.0072 IE
    AK 0.245 1.16 2.75 0.012 0.0006 0.0070 0.0050 0.055 0.021 0.0104 CE
    AL 0.237 1.06 2.72 0.013 0.0015 0.0010 0.0060 0.039 0.021 0.15 IE
    AM 0.232 1.01 2.98 0.014 0.0010 0.0060 0.0030 0.043 0.021 0.96 IE
    AN 0.221 1.05 2.60 0.008 0.0013 0.0050 0.0050 0.024 0.017 1.11 CE
    Table 1 (3/3)
    Type of Steel Chemical composition [mass%] Remarks
    C Si Mn P S N O Al Nb Ti B Cu Others
    AO 0.226 1.03 2.66 0.008 0.0015 0.0030 0.0020 0.028 0.019 V: 0.100 IE
    AP 0.220 1.36 2.79 0.014 0.0010 0.0060 0.0050 0.038 0.018 Ta: 0.10 IE
    AQ 0.223 1.21 2.78 0.013 0.0012 0.0020 0.0040 0.037 0.018 W: 0.09 IE
    AR 0.230 1.18 2.86 0.014 0.0008 0.0050 0.0020 0.045 0.021 Cr: 0.93 IE
    AS 0.238 1.35 2.77 0.008 0.0007 0.0050 0.0050 0.018 0.018 Mo: 0.76 IE
    AT 0.219 1.08 2.85 0.011 0.0013 0.0010 0.0040 0.045 0.022 Co: 0.009 IE
    AU 0.236 1.31 2.85 0.013 0.0008 0.0030 0.0030 0.026 0.015 Ni: 0.13 IE
    AV 0.246 1.09 2.71 0.010 0.0009 0.0060 0.0040 0.018 0.015 Sn: 0.069 IE
    AW 0.231 1.21 2.94 0.014 0.0007 0.0060 0.0040 0.025 0.022 Sb: 0.011 IE
    AX 0.235 1.17 2.78 0.012 0.0010 0.0020 0.0060 0.040 0.021 Ca: 0.0028 IE
    AY 0.235 1.34 2.87 0.010 0.0006 0.0020 0.0010 0.030 0.021 Mg: 0.0056 IE
    AZ 0.247 1.27 2.89 0.011 0.0009 0.0020 0.0030 0.020 0.020 Zr: 0.076 IE
    BA 0.216 1.05 2.94 0.009 0.0005 0.0060 0.0030 0.044 0.019 Te: 0.037 IE
    BB 0.229 1.38 2.93 0.012 0.0005 0.0020 0.0050 0.052 0.019 Hf: 0.08 IE
    BC 0.232 1.37 2.64 0.008 0.0006 0.0060 0.0060 0.046 0.019 REM: 0.0063 IE
    BD 0.234 1.10 2.91 0.008 0.0006 0.0040 0.0030 0.030 0.020 Bi: 0.123 IE
    BE 0.229 1.37 2.72 0.009 0.0015 0.0020 0.0040 0.043 0.020 IE
    BF 0.243 1.27 2.63 0.005 0.0011 0.0030 0.0060 0.038 0.018 IE
    BG 0.242 1.20 2.99 0.010 0.0009 0.0050 0.0050 0.016 0.015 IE
    BH 0.218 1.20 2.72 0.006 0.0013 0.0070 0.0030 0.019 0.018 IE
    BI 0.242 1.25 2.76 0.009 0.0010 0.0050 0.0050 0.013 0.016 IE
    IE: Inventive Example
    CE: Comparative Example
    [Table 2]
    Table 2 (1/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    1 A 1256 43 878 60 34 11 13 329 205 302 252 0.56 1 292 2.2 1.4 CR IE
    2 B 1260 57 876 191 27 18 17 315 195 311 269 0.31 1 246 41.2 1.4 CR IE
    3 B 1254 53 866 128 40 15 11 315 202 318 197 0.53 1 219 2.5 1.4 CR IE
    4 B 1228 44 880 145 25 17 15 315 196 313 160 0.47 1 236 2.1 1.4 CR IE
    5 B 1230 57 875 106 39 18 12 315 186 324 131 0.37 1 294 2.6 1.4 CR IE
    6 B 1256 46 875 91 32 19 16 315 189 337 271 0.54 1 162 2.0 1.4 CR IE
    7 B 1247 60 861 126 39 16 14 315 212 346 159 0.33 1 187 2.6 1.4 CR IE
    8 B 1257 36 864 75 33 14 11 315 187 336 226 0.45 1 270 1.5 1.4 CR IE
    9 B 1260 15 874 109 32 18 10 315 204 304 150 0.39 1 226 2.3 1.4 CR CE
    10 B 1245 51 875 99 37 91 8 315 202 324 107 0.36 1 231 1.8 1.4 CR IE
    11 B 1248 46 872 86 32 101 9 315 199 337 233 0.53 1 185 2.0 1.4 CR IE
    12 B 1255 46 836 67 34 11 16 315 203 343 153 0.38 1 167 1.6 1.4 CR IE
    13 B 1259 54 791 60 37 16 16 315 197 334 101 0.53 1 165 2.5 1.4 CR CE
    14 B 1239 43 869 98 39 13 18 315 206 206 103 0.48 1 208 2.9 1.4 CR IE
    15 B 1235 55 875 171 32 12 10 315 210 210 296 0.38 1 226 2.5 1.4 CR IE
    16 B 1255 41 874 25 38 18 12 315 204 336 238 0.39 1 238 2.0 1.4 CR IE
    17 B 1233 58 869 5 39 20 18 315 203 323 291 0.41 1 200 2.8 1.4 CR CE
    18 B 1256 41 875 58 27 17 10 315 202 321 293 0.37 2 171 2.7 1.4 CR IE
    19 B 1248 51 867 149 40 15 9 315 204 335 204 0.57 3 229 2.9 1.4 CR IE
    20 B 1238 57 879 198 23 11 16 315 214 327 185 0.33 1 226 2.0 1.4 CR IE
    Table 2 (2/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    21 B 1234 47 876 179 16 13 13 315 198 315 237 0.38 1 171 1.9 1.4 CR CE
    22 B 1242 51 868 106 26 131 14 315 198 332 209 0.55 1 294 2.2 1.4 CR IE
    23 B 1235 49 871 194 27 165 11 315 192 308 214 0.39 1 192 2.9 1.4 CR CE
    24 B 1245 42 879 92 32 16 17 315 107 349 250 0.58 1 250 2.4 1.4 CR IE
    25 B 1240 48 868 127 29 15 8 315 98 333 240 0.43 1 173 2.0 1.4 CR CE
    26 B 1256 57 871 184 26 16 16 315 232 325 151 0.54 1 184 2.0 1.4 CR IE
    27 B 1247 58 879 56 28 12 13 315 240 326 149 0.47 1 208 2.6 1.4 CR CE
    28 B 1238 55 875 140 28 19 10 315 202 325 224 0.38 1 289 2.0 1.4 CR IE
    29 B 1239 56 867 170 27 12 9 315 189 329 236 0.38 1 158 2.6 1.4 CR IE
    30 B 1241 52 864 198 38 12 11 315 211 416 119 0.43 1 176 3.0 1.4 CR IE
    31 B 1245 45 860 178 25 17 13 315 207 449 256 0.35 1 294 2.3 1.4 CR IE
    32 B 1231 46 865 162 37 11 18 315 187 341 9 0.30 1 194 2.2 1.4 CR IE
    33 B 1232 43 862 167 36 18 9 315 212 308 2 0.42 1 173 2.5 1.4 CR CE
    34 B 1237 41 878 185 33 16 16 315 209 343 951 0.46 1 189 1.6 1.4 CR IE
    35 B 1244 47 879 180 34 20 12 315 211 328 949 0.46 1 220 2.7 1.4 CR IE
    36 B 1254 53 880 54 37 14 10 315 196 321 253 0.12 1 228 1.6 1.4 CR IE
    37 B 1243 56 865 84 32 16 16 315 193 339 149 0.08 1 270 2.2 1.4 CR CE
    38 B 1239 55 861 90 38 15 9 315 211 347 275 4.95 1 205 2.2 1.4 CR IE
    39 B 1249 41 879 161 27 15 15 315 214 325 148 5.12 1 160 2.7 1.4 CR CE
    40 B 1232 57 863 105 38 17 6 315 200 301 171 0.38 1 155 2.3 1.4 CR IE
    Table 2 (3/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    41 B 1251 57 872 103 33 13 2 315 188 324 243 0.35 1 190 1.8 1.4 CR CE
    42 B 1232 42 862 99 32 17 81 315 197 314 250 0.59 1 246 2.6 1.4 CR IE
    43 B 1238 55 875 188 36 12 92 315 211 304 243 0.37 1 194 1.6 1.4 CR IE
    44 B 1239 46 873 112 31 11 9 315 198 340 116 0.41 1 151 2.0 1.4 CR IE
    45 B 1234 60 871 190 28 16 17 315 206 341 132 0.57 1 141 2.8 1.4 CR CE
    46 B 1255 52 873 151 34 12 16 315 194 322 195 0.55 1 397 1.7 1.4 CR IE
    47 B 1241 42 860 51 35 19 9 315 205 305 217 0.43 1 386 2.3 1.4 CR IE
    48 B 1257 47 873 154 26 15 10 315 191 340 124 0.35 1 189 48.3 1.4 CR IE
    49 B 1259 48 876 115 36 19 18 315 185 307 170 0.49 1 182 55.3 1.4 CR CE
    50 B 1245 42 872 119 27 13 10 315 201 348 115 0.32 1 261 38.0 1.4 CR IE
    51 B 1256 42 861 166 26 13 14 315 198 305 166 0.55 1 284 42.0 1.4 CR IE
    52 B 1251 58 876 181 40 15 11 315 211 322 212 0.53 2 274 2.4 1.4 CR IE
    53 B 1232 53 870 178 33 13 15 315 192 325 285 0.44 5 167 2.1 1.4 CR IE
    54 B 1260 53 875 98 35 18 10 315 185 302 156 0.44 1 264 2.9 1.4 CR IE
    55 C 1245 45 863 56 34 17 14 329 211 309 109 0.33 1 248 1.8 1.4 CR IE
    56 D 1249 41 864 188 30 14 9 325 219 219 237 0.39 1 276 2.1 1.4 CR IE
    57 E 1243 54 863 153 32 16 12 321 208 332 288 0.40 1 159 2.2 1.4 CR IE
    58 F 1240 50 864 91 25 10 10 410 291 317 161 0.44 1 230 2.3 1.4 CR IE
    59 G 1257 56 869 59 40 18 14 418 291 344 101 0.36 1 281 3.0 1.4 GA CE
    60 H 1248 49 878 127 36 14 9 206 113 325 221 0.37 1 285 1.8 1.4 GA IE
    Table 2 (4/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    61 I 1254 50 872 123 31 15 17 192 108 330 112 0.38 1 248 2.5 1.4 GA CE
    62 J 1249 59 877 140 33 14 17 322 202 312 106 0.45 1 205 3.0 1.4 GA IE
    63 K 1248 58 866 112 28 18 14 334 225 317 144 0.52 1 210 41.8 1.4 GA CE
    64 L 1250 40 863 151 39 15 10 332 215 313 231 0.56 1 246 40.7 1.4 CR IE
    65 M 1231 57 874 146 34 11 10 326 223 344 194 0.39 1 274 43.0 1.4 CR CE
    66 N 1235 57 865 168 29 18 13 398 281 335 181 0.37 1 239 31.3 1.4 GA IE
    67 O 1245 50 869 105 30 17 10 406 282 310 154 0.44 1 235 40.8 1.4 GA CE
    68 P 1258 50 866 140 26 16 10 272 163 315 186 0.31 1 201 37.4 1.4 GI IE
    69 Q 1255 58 862 124 34 17 13 251 146 304 238 0.33 1 246 31.8 1.4 GA CE
    70 R 1254 50 867 122 39 15 17 315 199 314 238 0.43 1 224 33.4 1.4 GA IE
    71 s 1255 56 865 68 27 13 12 326 211 304 225 0.31 1 158 42.3 1.4 GA CE
    72 T 1246 41 861 126 35 20 12 317 204 328 269 0.31 1 268 32.9 1.4 GA IE
    73 U 1234 51 866 158 33 12 15 331 221 302 216 0.58 1 278 2.1 1.4 GI CE
    74 v 1253 41 875 159 32 16 14 319 202 317 211 0.40 1 255 2.6 1.4 GA IE
    75 W 1248 50 865 140 31 15 8 335 212 326 178 0.42 1 279 2.2 1.4 GA CE
    76 X 1248 48 874 183 29 18 16 328 204 302 222 0.32 1 204 1.9 1.4 GA IE
    77 Y 1245 49 878 56 36 13 17 321 208 307 103 0.32 1 228 2.0 1.4 GA CE
    78 Z 1233 42 872 189 34 11 12 335 208 349 153 0.41 1 229 2.2 1.4 GA IE
    79 AA 1231 42 866 162 30 17 11 331 219 347 139 0.36 1 208 1.9 1.4 GI CE
    80 AB 1240 54 880 94 30 20 15 330 211 318 105 0.33 1 260 2.0 1.4 GA IE
    Table 2 (5/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    81 AC 1252 56 862 146 35 11 14 327 201 322 141 0.57 1 158 2.7 1.4 GA CE
    82 AD 1249 42 870 84 37 17 15 332 206 317 262 0.48 1 275 2.0 1.4 GA IE
    83 AE 1235 54 866 147 39 13 13 335 235 307 120 0.48 1 226 1.7 1.4 GA CE
    84 AF 1253 48 864 102 27 18 12 337 224 347 176 0.42 1 164 32.5 1.4 CR IE
    85 AG 1244 54 864 80 26 11 14 329 206 308 169 0.55 1 201 43.9 1.4 CR IE
    86 AH 1240 48 870 118 36 18 14 327 200 323 120 0.46 1 291 35.6 1.4 GA CE
    87 AI 1236 49 865 165 31 10 13 334 223 336 188 0.45 1 192 43.5 1.4 GA IE
    88 AJ 1248 40 869 179 31 20 11 327 226 308 232 0.48 1 254 31.2 1.4 GA IE
    89 AK 1249 55 868 99 27 18 13 319 196 332 211 0.41 1 231 35.6 1.4 GA CE
    90 AL 1256 58 869 120 35 11 15 324 223 328 107 0.47 1 274 42.8 1.4 GA IE
    91 AM 1250 42 863 114 36 15 15 318 200 302 264 0.40 1 288 35.4 1.4 GA IE
    92 AN 1231 55 862 136 26 12 11 335 220 337 167 0.51 1 151 332 1.4 GA CE
    93 AO 1223 46 868 161 34 17 9 331 212 311 202 0.43 1 182 32.7 1.5 CR IE
    94 AP 1245 36 861 66 35 19 17 330 226 338 150 0.53 1 191 33.2 1.6 CR IE
    95 AQ 1237 50 802 174 39 11 15 329 214 303 287 0.41 1 259 43.5 1.2 CR IE
    96 AR 1238 46 877 29 32 18 17 312 206 338 107 0.44 1 152 2.8 1.1 CR IE
    97 AS 1253 47 880 195 23 14 16 316 187 328 174 0.43 1 191 2.6 1.4 CR IE
    98 AT 1246 47 877 184 38 133 9 329 211 301 185 0.41 1 205 2.4 1.5 CR IE
    99 AU 1236 46 872 58 26 13 16 318 102 334 172 0.49 1 285 1.7 1.6 CR IE
    100 AV 1230 43 865 159 30 18 11 320 238 302 202 0.32 1 178 2.3 1.4 CR IE
    Table 2 (6/6)
    No. Type of steel Hot rolling Cooling Heat treatment A Heat treatment B Working Heat treatment C Final sheet thickness [mm] Type Remarks
    Slab heating temp. [°C] Average cooling rate v1 [°C/s] Temp. T1 [°C] Retaining time t1 [s] Average cooling rate v2 [°C/s] Average cooling rate v3 [°C/s] Tension F [MPa] Ms point [°C] Cooling stop temp. Ta [°C] Temp. T2 [°C] Retaining time t2 [s] Equivalent plastic strain [%] Number of times of working Temp. T3 [°C] Average cooling rate v4 [°C/h]
    101 AW 1235 46 863 199 38 13 14 320 210 334 144 0.58 1 222 2.5 1.4 CR IE
    102 AX 1250 41 878 75 39 15 17 323 219 310 259 0.44 1 180 2.3 1.5 CR IE
    103 AY 1256 49 880 113 39 14 13 320 201 403 209 0.47 1 204 1.9 1.6 CR IE
    104 AZ 1234 44 870 56 25 16 11 314 202 349 6 0.53 1 151 2.7 1.2 CR IE
    105 BA 1250 51 874 89 27 13 15 327 215 314 803 0.37 1 186 2.6 1.4 CR IE
    106 BB 1247 47 877 198 39 16 14 321 215 348 152 0.14 1 235 3.0 1.1 CR IE
    107 BC 1257 57 878 88 37 17 12 329 217 322 241 4.17 1 252 2.5 1.1 CR IE
    108 BD 1244 55 879 148 35 19 5 320 207 305 109 0.40 1 222 2.6 1.6 CR IE
    109 BE 1241 56 870 131 40 95 13 328 210 210 226 0.38 1 162 32.7 1.6 CR IE
    110 BF 1251 49 872 152 29 94 15 324 195 309 288 0.44 1 224 44.6 1.2 EG IE
    111 BG 1241 44 863 130 34 10 17 313 205 307 144 0.43 1 160 37.6 2.2 EG IE
    112 BH 1246 42 865 52 27 14 13 333 231 344 165 0.30 1 291 31.2 0.6 EG IE
    113 BI 1254 56 878 73 39 13 15 320 204 338 184 0.40 1 168 36.9 1.5 EG IE
    IE: Inventive Example
    CE: Comparative Example
  • [Table 3]
  • Table 3 (1/3)
    No. Type of steel Final sheet thickness [mm] Amount of M [%] Amount of retained γ [%] Total amount of F and BF [%] Instability index k Instability index d TS [MPa] Minimum bending radius R [mm] R/t Delayed fracture resistance Optimal clearance range Remarks
    1 A 1.4 89 8 3 2.7 -2.4 1572 5.5 3.9 A A IE
    2 B 1.4 86 11 3 2.3 -1.2 1679 4.5 3.2 A A IE
    3 B 1.4 82 11 7 2.5 -1.0 1359 4.5 3.2 A A IE
    4 B 1.4 83 11 6 2.1 2.0 1439 5.5 3.9 B A IE
    5 B 1.4 85 9 6 2.4 2.2 1439 5.5 3.9 B A IE
    6 B 1.4 86 9 5 3.3 1.9 1519 4.5 3.2 A A IE
    7 B 1.4 83 12 5 2.3 0.0 1519 4.5 3.2 A A IE
    8 B 1.4 83 11 6 4.8 0.5 1439 5.5 3.9 A B IE
    9 B 1.4 80 12 8 11.9 -0.3 1279 4.5 3.2 A C CE
    10 B 1.4 87 8 5 2.4 -0.5 1519 5.0 3.6 A A IE
    11 B 1.4 88 9 3 2.9 -2.3 1679 3.5 2.5 A A IE
    12 B 1.4 76 14 10 2.2 1.4 1211 4.0 2.9 A A IE
    13 B 1.4 68 14 18 3.4 0.5 1012 5.5 3.9 A A CE
    14 B 1.4 89 8 3 3.4 1.4 1679 6.0 4.3 A A IE
    15 B 1.4 86 8 6 3.4 -2.4 1439 4.0 2.9 A A IE
    16 B 1.4 83 8 9 2.4 -2.3 1193 2.0 1.4 A A IE
    17 B 1.4 80 9 11 2.0 2.0 1001 4.0 2.9 A A CE
    18 B 1.4 86 8 6 3.1 -2.7 1439 4.5 3.2 A A IE
    19 B 1.4 86 11 3 2.6 0.2 1679 5.5 3.9 A A IE
    20 B 1.4 77 14 9 2.0 -2.5 1186 1.0 0.7 A A IE
    21 B 1.4 67 14 19 3.2 -1.0 1044 5.0 3.6 A A CE
    22 B 1.4 82 12 6 2.9 4.6 1439 5.0 3.6 B B IE
    23 B 1.4 79 18 3 4.0 5.7 1679 5.0 3.6 C C CE
    24 B 1.4 92 6 2 2.5 -2.0 1759 8.0 5.7 A A IE
    25 B 1.4 96 2 2 3.0 -1.1 1759 9.0 6.4 A A CE
    26 B 1.4 81 17 2 3.3 1.8 1759 6.0 4.3 B A IE
    27 B 1.4 76 22 2 2.4 -0.4 1759 5.0 3.6 C A CE
    28 B 1.4 85 9 6 2.9 0.6 1439 5.5 3.9 A A IE
    29 B 1.4 84 9 7 3.3 -0.2 1359 5.0 3.6 A A IE
    30 B 1.4 86 8 6 2.9 -0.7 1191 3.5 2.5 A A IE
    31 B 1.4 82 11 7 3.1 -1.9 1206 6.0 4.3 A A IE
    32 B 1.4 84 9 7 4.9 0.5 1359 5.0 3.6 A B IE
    33 B 1.4 82 11 7 6.1 0.4 1359 6.0 4.3 A C CE
    34 B 1.4 85 9 6 3.1 -1.7 1199 6.0 4.3 A A IE
    35 B 1.4 85 10 5 2.0 2.6 1189 5.0 3.6 A A IE
    36 B 1.4 86 11 3 2.1 4.7 1679 6.0 4.3 B B IE
    37 B 1.4 86 9 5 3.4 6.6 1519 6.0 4.3 C C CE
    38 B 1.4 89 7 4 2.1 2.1 1599 8.0 5.7 A A IE
    39 B 1.4 92 1 7 3.5 0.7 1359 10.0 7.1 A A CE
    40 B 1.4 82 12 6 2.4 4.7 1439 3.0 2.1 B B IE
    41 B 1.4 85 11 4 3.3 8.8 1599 0.5 0.4 C C CE
    42 B 1.4 90 7 3 3.1 -10.2 1679 7.2 5.1 A A IE
    43 B 1.4 90 6 4 2.2 -9.2 1599 7.4 5.3 A A IE
    44 B 1.4 87 9 4 4.9 -2.4 1599 6.5 4.6 A B IE
    45 B 1.4 85 9 6 9.7 0.1 1439 5.5 3.9 A C CE
    46 B 1.4 88 10 2 3.2 2.6 1213 3.0 2.1 A A IE
    47 B 1.4 81 12 7 2.2 1.7 1202 0.5 0.4 A A IE
    48 B 1.4 88 9 3 5.0 -0.5 1679 4.0 2.9 A B IE
    49 B 1.4 88 9 3 9.8 -0.8 1679 3.0 2.1 A C CE
    50 B 1.4 83 12 5 2.7 -2.5 1599 6.5 4.6 A A IE
    51 B 1.4 85 11 4 2.9 1.0 1343 5.5 3.9 A A IE
    52 B 1.4 89 9 2 2.6 -1.8 1759 6.5 4.6 A A IE
    53 B 1.4 85 10 5 2.2 1.8 1519 5.0 3.6 A A IE
    54 B 1.4 83 10 7 2.4 -0.8 1359 6.0 4.3 A A IE
    55 C 1.4 84 10 6 2.5 -2.3 1343 6.0 4.3 A A IE
    56 D 1.4 81 12 7 2.3 -1.3 1285 4.0 2.9 A A IE
    57 E 1.4 90 8 2 3.0 1.4 1759 6.0 4.3 A A IE
    58 F 1.4 83 8 9 2.3 1.1 1210 5.0 3.6 A A IE
    59 G 1.4 69 15 16 2.6 -0.6 1041 30 2.1 A A CE
    60 H 1.4 84 9 7 2.0 -2.7 1719 6.5 4.6 B A IE
    61 I 1.4 85 9 6 2.9 -0.9 1824 7.0 5.0 C A CE
    62 J 1.4 83 9 8 3.4 2.8 1190 6.0 4.3 A A IE
    63 K 1.4 84 10 6 2.4 1.7 990 5.5 3.9 A A CE
    64 L 1.4 84 14 2 2.2 -0.3 1773 3.0 2.1 B A IE
    65 M 1.4 82 16 2 2.5 -2.5 1792 0.5 0.4 C A CE
    66 N 1.4 83 8 9 2.3 -1.7 1191 4.0 2.9 A A IE
    67 O 1.4 68 16 16 2.5 -1.1 989 30 2.1 A A CE
    68 P 1.4 85 9 6 2.1 1.6 1500 6.5 4.6 B A IE
    69 Q 1.4 83 12 5 2.2 1.6 1663 5.5 3.9 C A CE
    70 R 1.4 90 8 2 3.2 3.0 1768 5.5 3.9 B A IE
    71 S 1.4 82 11 7 3.1 -1.2 1286 4.0 2.9 C A CE
    72 T 1.4 83 10 7 2.6 2.9 1356 4.5 3.2 B A IE
    73 U 1.4 82 10 8 2.2 2.2 1191 5.5 3.9 C A CE
    74 V 1.4 86 10 4 2.6 2.6 1578 5.0 3.6 B A IE
    75 W 1.4 87 11 2 2.8 2.7 1652 5.5 3.9 C A CE
    76 X 1.4 85 8 7 3.3 -1.4 1287 6.0 4.3 B A IE
    77 Y 1.4 86 9 5 3.2 1.0 1511 6.0 4.3 C A CE
    78 Z 1.4 85 11 4 2.2 -2.0 1516 6.0 4.3 B A IE
    79 AA 1.4 86 9 5 2.9 -1.7 1446 6.0 4.3 C A CE
    80 AB 1.4 89 8 3 4.5 -0.5 1585 4.5 3.2 A B IE
    81 AC 1.4 87 10 3 7.1 -1.1 1584 6.0 4.3 A C CE
    82 AD 1.4 84 9 7 2.5 2.0 1284 5.0 3.6 B A IE
    83 AE 1.4 81 12 7 2.1 2.2 1263 5.0 3.6 C A CE
    84 AF 1.4 85 11 4 2.1 2.0 1208 4.5 3.2 A A IE
    85 AG 1.4 83 9 8 2.9 0.3 1196 5.5 3.9 B A IE
    86 AH 1.4 85 11 4 2.9 -3.0 1929 5.5 3.9 C A CE
    87 AI 1.4 88 9 3 2.8 -2.9 1186 4.0 2.9 A A IE
    88 AJ 1.4 86 11 3 3.4 -0.5 1645 5.5 3.9 B A IE
    89 AK 1.4 83 12 5 2.9 -0.3 1893 5.5 3.9 C A CE
    90 AL 1.4 87 9 4 2.6 -0.2 1186 5.0 3.6 A A IE
    91 AM 1.4 82 10 8 2.8 -2.5 1235 6.0 4.3 B A IE
    92 AN 1.4 83 9 8 2.9 0.4 1906 6.5 4.6 C A CE
    93 AO 1.5 83 10 7 3.1 -0.6 1276 6.5 4.3 A A IE
    94 AP 1.6 87 10 3 4.7 2.8 1611 5.5 3.4 A B IE
    95 AQ 1.2 83 8 9 3.4 -0.7 1216 4.0 3.3 A A IE
    96 AR 1.1 82 9 9 2.6 1.5 1198 4.0 3.6 A A IE
    97 AS 1.4 83 8 9 2.5 -2.5 1212 5.0 3.6 A A IE
    98 AT 1.5 86 8 6 3.0 4.7 1352 4.5 3.0 B B IE
    99 AU 1.6 89 6 5 2.7 -0.2 1499 9.0 5.6 A A IE
    100 AV 1.4 84 14 2 2.8 0.4 1744 6.0 4.3 B A IE
    101 AW 1.4 85 8 7 2.5 0.7 1324 6.5 4.6 A A IE
    102 AX 1.5 85 10 5 2.2 -1.6 1482 6.5 4.3 A A IE
    103 AY 1.6 84 8 8 3.3 0.6 1201 5.5 3.4 A A IE
    104 AZ 1.2 85 11 4 4.8 0.9 1612 4.0 3.3 A B IE
    105 BA 1.4 90 8 2 3.5 1.4 1193 5.5 3.9 A A IE
    106 BB 1.1 87 11 2 3.2 4.8 1729 4.0 3.6 B B IE
    107 BC 1.1 86 7 7 2.0 1.8 1317 6.0 5.5 A A IE
    108 BD 1.6 86 11 3 2.3 4.9 1643 7.0 4.4 B B IE
    109 BE 1.6 88 8 4 2.4 2.6 1553 6.5 4.1 A A IE
    110 BF 1.2 84 10 6 2.6 1.5 1422 5.0 4.2 A A IE
    111 BG 2.2 87 10 3 2.2 2.9 1679 3.0 1.4 A A IE
    112 BH 0.6 82 10 8 3.2 1.5 1188 2.0 3.3 A A IE
    113 BI 1.5 87 9 4 2.4 -0.9 1587 6.5 4.3 A A IE
    IE: Inventive Example
    CE: Comparative Example
  • <Summary of Evaluation Results>
  • As shown in Table 3 above, the steel sheets of Nos. 1 to 8, 10 to 12, 14 to 16, 18 to 20, 22, 24, 26, 28 to 32, 34 to 36, 38, 40, 42 to 44, 46 to 48, 50 to 58, 60, 62, 64, 66, 68, 70, 72, 74, 76, 78, 80, 82, 84, 85, 87, 88, 90, 91, and 93 to 113 (Inventive Examples) had a TS of not less than 1,180 MPa, excellent bendability and excellent delayed fracture resistance, and a wide optimal clearance range.
  • In contrast, the steel sheets of Nos. 9, 13, 17, 21, 23, 25, 27, 33, 37, 39, 41, 45, 49, 59, 61, 63, 65, 67, 69, 71, 73, 75, 77, 79, 81, 83, 86, 89, and 92 (Comparative Examples) were insufficient in at least one of TS, bendability, delayed fracture resistance, or optimal clearance range.

Claims (5)

  1. A high strength steel sheet comprising a steel sheet,
    wherein the steel sheet has a chemical composition including, by mass,
    C in an amount of not less than 0.030% and not more than 0.500%,
    Si in an amount of not less than 0.50% and not more than 2.50%,
    Mn in an amount of not less than 1.50% and not more than 5.00%,
    P in an amount of not more than 0.100%,
    S in an amount of not more than 0.0200%,
    Al in an amount of not more than 1.000%,
    N in an amount of not more than 0.0100%,
    O in an amount of not more than 0.0100%, and
    Nb in an amount of not less than 0.005% and not more than 0.100%,
    with a balance consisting of Fe and inevitable impurities,
    the steel sheet has a microstructure in which an amount of martensite is not less than 70%, an amount of retained austenite is not less than 3% and not more than 20%, and a total amount of ferrite and bainitic ferrite is not more than 10%,
    an instability index k of retained austenite is less than 6.1, and
    an instability index d of retained austenite in an initial stage of working is less than 5.7.
  2. The high strength steel sheet according to claim 1,
    wherein the chemical composition further includes at least one element selected from the group consisting of, by mass,
    Ti in an amount of not more than 0.200%,
    V in an amount of not more than 0.200%,
    Ta in an amount of not more than 0.10%,
    W in an amount of not more than 0.10%,
    B in an amount of not more than 0.0100%,
    Cr in an amount of not more than 1.00%,
    Mo in an amount of not more than 1.00%,
    Ni in an amount of not more than 1.00%,
    Co in an amount of not more than 0.010%,
    Cu in an amount of not more than 1.00%,
    Sn in an amount of not more than 0.200%,
    Sb in an amount of not more than 0.200%,
    Ca in an amount of not more than 0.0100%,
    Mg in an amount of not more than 0.0100%,
    REM in an amount of not more than 0.0100%,
    Zr in an amount of not more than 0.100%,
    Te in an amount of not more than 0.100%,
    Hf in an amount of not more than 0.10%, and
    Bi in an amount of not more than 0.200%.
  3. The high strength steel sheet according to claim 1 or 2, further comprising a plating layer on a surface of the steel sheet.
  4. A method for manufacturing the high strength steel sheet according to claim 1 or 2, the method comprising:
    retaining a steel slab having the chemical composition according to claim 1 or 2 at a slab heating temperature of not lower than 1,220°C and then performing hot rolling to obtain a hot rolled steel sheet;
    cooling the hot rolled steel sheet under a condition of an average cooling rate v1 from 800°C to 600°C of not lower than 30°C/s and then performing pickling and cold rolling to obtain a cold rolled steel sheet;
    performing a heat treatment A in which the cold rolled steel sheet is retained at a temperature T1 of not lower than 800°C for 10 seconds or more and then cooled to a cooling stop temperature Ta of not lower than 100°C and not higher than (Ms point - 80°C),
    where, in the heat treatment A, an average cooling rate v2 from 750°C to 600°C is not lower than 20°C/s, an average cooling rate v3 from the Ms point to the cooling stop temperature Ta is not higher than 150°C/s, and a tension F imparted to the cold rolled steel sheet from the Ms point to the cooling stop temperature Ta is not less than 5 MPa and not more than 100 MPa;
    after the heat treatment A, performing a heat treatment B in which the cold rolled steel sheet is retained at a temperature T2 of not lower than the cooling stop temperature Ta and not higher than 450°C for 5 seconds or more and 1,000 seconds or less and then cooled;
    after the heat treatment B, performing a heat treatment C in which the cold rolled steel sheet is heated to a temperature T3 of not lower than 150°C and not higher than 400°C and then cooled without being retained at the temperature T3,
    where, in the heat treatment C, an average cooling rate v4 from 150°C to 50°C is not lower than 1.0°C/s and not higher than 50.0°C/s; and
    after the heat treatment A and before the heat treatment C, working the cold rolled steel sheet to impart an equivalent plastic strain of not less than 0.10% and not more than 5.00% to the cold rolled steel sheet,
    wherein the Ms point is represented in a unit of °C and determined by Formula (a): Ms = 519 - 474 × [%C] - 30.4 × [%Mn] - 12.1 × [%Cr] - 7.5 × [%Mo] - 17.7 × [%Ni]
    in Formula (a), [%M] represents a content of an element M in the chemical composition, and when the element M is not contained, [%M] is 0.
  5. The method for manufacturing the high strength steel sheet according to claim 4,
    wherein the cold rolled steel sheet is subjected to a plating treatment.
EP24767131.6A 2023-03-06 2024-03-05 High-strength steel sheet and method for manufacturing same Pending EP4656758A1 (en)

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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015193897A (en) 2014-03-17 2015-11-05 株式会社神戸製鋼所 High-strength cold-rolled steel sheet and high-strength hot-dip galvanized steel sheet excellent in ductility and bendability, and methods for producing them
WO2019187090A1 (en) 2018-03-30 2019-10-03 日本製鉄株式会社 Steel sheet and manufacturing method therefor
WO2020174805A1 (en) 2019-02-25 2020-09-03 Jfeスチール株式会社 High-strength steel sheet and method for manufacturing same

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Publication number Priority date Publication date Assignee Title
CN112004955B (en) * 2018-04-23 2022-03-04 日本制铁株式会社 Steel member and method for manufacturing same
US12428700B2 (en) * 2021-06-11 2025-09-30 Jfe-Steel Corporation High strength steel sheet and method for manufacturing the same

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015193897A (en) 2014-03-17 2015-11-05 株式会社神戸製鋼所 High-strength cold-rolled steel sheet and high-strength hot-dip galvanized steel sheet excellent in ductility and bendability, and methods for producing them
WO2019187090A1 (en) 2018-03-30 2019-10-03 日本製鉄株式会社 Steel sheet and manufacturing method therefor
WO2020174805A1 (en) 2019-02-25 2020-09-03 Jfeスチール株式会社 High-strength steel sheet and method for manufacturing same

Non-Patent Citations (2)

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Title
See also references of WO2024185764A1
YOSHISUKE MISAKATAKESHI MASUI, SOSEI TO KAKOU, vol. 17, 1976, pages 988 - 994

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JPWO2024185764A1 (en) 2024-09-12
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