US20250154633A1 - Zinc-plated steel sheet and method for producing same - Google Patents

Zinc-plated steel sheet and method for producing same Download PDF

Info

Publication number
US20250154633A1
US20250154633A1 US18/839,195 US202318839195A US2025154633A1 US 20250154633 A1 US20250154633 A1 US 20250154633A1 US 202318839195 A US202318839195 A US 202318839195A US 2025154633 A1 US2025154633 A1 US 2025154633A1
Authority
US
United States
Prior art keywords
steel sheet
less
zinc
layer
alloy layer
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
US18/839,195
Other languages
English (en)
Inventor
Yusuke TSUNEMI
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nippon Steel Corp
Original Assignee
Nippon Steel Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Nippon Steel Corp filed Critical Nippon Steel Corp
Assigned to NIPPON STEEL CORPORATION reassignment NIPPON STEEL CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: TSUNEMI, Yusuke
Publication of US20250154633A1 publication Critical patent/US20250154633A1/en
Pending legal-status Critical Current

Links

Images

Classifications

    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
    • C21D1/74—Methods of treatment in inert gas, controlled atmosphere, vacuum or pulverulent material
    • C21D1/76—Adjusting the composition of the atmosphere
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00—Heat treatment of ferrous alloys
    • C21D6/005—Heat treatment of ferrous alloys containing Mn
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C18/00—Alloys based on zinc
    • C22C18/04—Alloys based on zinc with aluminium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/001—Ferrous alloys, e.g. steel alloys containing N
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/008—Ferrous alloys, e.g. steel alloys containing tin
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
    • C23C2/0222—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating in a reactive atmosphere, e.g. oxidising or reducing atmosphere
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
    • C23C2/0224—Two or more thermal pretreatments
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
    • C23C2/06—Zinc or cadmium or alloys based thereon
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/26—After-treatment
    • C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/26—After-treatment
    • C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
    • C23C2/29—Cooling or quenching
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
    • C23C2/34—Hot-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
    • C23C2/36—Elongated material
    • C23C2/40—Plates; Strips

Definitions

  • the present invention relates to a zinc-plated steel sheet and a method for manufacturing the zinc-plated steel sheet.
  • High strength steel sheets are used as a steel sheet for a vehicle in order to reduce the amount of carbon dioxide emission by reducing the weight of the vehicle to improve the fuel consumption, and ensure the safety of passengers.
  • high strength galvannealed steel sheets are recently used as a steel sheet for a vehicle in order to ensure sufficient corrosion resistance of the vehicle body and its component (see, for example, Patent Document 1).
  • a high strength steel sheet to be provided for a component for a vehicle is required to have not only strength but also properties, such as uniform elongation, necessary for forming a component (for example, formability, elongation, and bending resistance).
  • properties such as uniform elongation, necessary for forming a component (for example, formability, elongation, and bending resistance).
  • TRIP transformation induced plasticity
  • DP steel sheets which have a soft phase and a hard phase.
  • LME liquid metal embrittlement
  • Such an LME crack is easily caused in high alloys such as TRIP steel sheets and DP steel sheets.
  • spot welding of a high strength TRIP steel sheet remarkably causes an LME crack.
  • the high strength TRIP steel sheet is a steel sheet having higher concentrations of C, Si, and Mn than normal high strength steel sheets, and containing residual austenite to have excellent energy absorption capacity and press formability.
  • a zinc-plated steel sheet assumed to be applied to a component for a vehicle is required to have high LME resistance.
  • Patent Document 2 discloses a steel sheet, a hot-dip galvanized steel sheet, and a galvannealed steel sheet excellent in resistance to liquid metal embrittlement cracking, in which the steel sheet has, from a surface of the base metal to a depth of 5.0 ⁇ m or more, an internal oxide layer in which at least one part of a grain boundary is covered with an oxide, and in a region from the surface of the base metal to a depth of 5.0 ⁇ m, the grain boundary coverage by the oxide is 60% or more.
  • Patent Document 2 discloses that generation of LME is suppressed by making a layer in which internal oxidation occurs be present to a predetermined depth and increasing the coverage of the grain boundary by the oxide.
  • Patent Document 2 bending fatigue strength and bending resistance are not considered.
  • an object of the present invention is to provide a zinc-plated steel sheet having high strength and being excellent in LME resistance and bending fatigue strength without deterioration of the bending resistance.
  • the present inventors have studied a method of enhancing LME resistance and bending fatigue strength in a high strength zinc-plated steel sheet.
  • the LME resistance can be improved, without deterioration of the bending resistance, by providing an Fe—Al alloy layer having a predetermined thickness between a base steel sheet and a zinc-plated layer.
  • the bending fatigue strength is improved by forming a predetermined internal oxide layer at the surface of the base steel sheet.
  • control of the annealing step and the plating step is effective for the formation of such a Fe—Al alloy layer and an internal oxide layer.
  • the present invention has been made in view of the above findings.
  • the gist of the present invention is as follows.
  • a zinc-plated steel sheet includes a base steel sheet, a Fe—Al alloy layer formed on at least a part of a surface of the base steel sheet, and a zinc-plated layer formed on the surface of the base steel sheet or a surface of the Fe—Al alloy layer, in which the base steel sheet has a chemical composition including, in mass %, C: 0.10 to 0.40%, Si: 0.10 to 3.00%, Mn: 1.00 to 5.00%, sol.Al: 0.001 to 1.500%, P: 0.0010 to 0.0300%, S: 0.0200% or less, N: 0.0100% or less, O: 0.0100% or less, Ti: 0 to 0.200%, B: 0 to 0.0100%, Cr: 0 to 1.000%, Mo: 0 to 1.000%, Ni: 0 to 1.000%, Cu: 0 to 1.000%, Sn: 0 to 0.500%, Nb: 0 to 0.200%, V: 0 to
  • the chemical composition of the base steel sheet may contain, in mass %, one or more selected from the group consisting of Ti: 0.005 to 0.200%, B: 0.0005 to 0.0100%, Cr: 0.001 to 1.000%, Mo: 0.001 to 1.000%, Ni: 0.001 to 1.000%, Cu: 0.001 to 1.000%, Sn: 0.001 to 0.500%, Nb: 0.001 to 0.200%, V: 0.001 to 0.500%, W: 0.001 to 0.500%, Ca: 0.0001 to 0.0100%, Mg: 0.0001 to 0.0100%, Bi: 0.0001 to 0.0100%, Sb: 0.0001 to 0.1000%, Zr: 0.0001 to 0.0100%, and REM: 0.0001 to 0.1000%.
  • a method for manufacturing a zinc-plated steel sheet according to another aspect of the present invention includes an annealing step of holding a steel sheet at an annealing temperature of 700 to 1000° C. for 1 second or more to anneal the steel sheet, the steel sheet having a chemical composition including, in mass %, C: 0.10 to 0.40%, Si: 0.10 to 3.00%, Mn: 1.00 to 5.00%, sol.Al: 0.001 to 1.500%, P: 0.0010 to 0.0300%, S: 0.0200% or less, N: 0.0100% or less, O: 0.0100% or less, Ti: 0 to 0.200%, B: 0 to 0.0100%, Cr: 0 to 1.000%, Mo: 0 to 1.000%, Ni: 0 to 1,000%, Cu: 0 to 1.000%, Sn: 0 to 0.500%, Nb: 0 to 0.200%, V: 0 to 0.500%, W: 0 to 0.500%, Ca: 0 to 0.0
  • the steel sheet in the plating step, is cooled to a temperature of 440 to 550° C. at an average cooling rate of 0.5° C./sec or more, is immersed in a plating bath containing Zn as a main component and having an effective Al amount of 0.050 to 0.250 mass %, is pulled up from the plating bath, then is cooled so that a temperature of the steel sheet reaches 400° C. within 10 seconds, and subsequently is cooled to 350° C. or less so that at an average cooling rate from 400° C. to 350° C. is 1.0° C./sec or more and 5.0° C./sec or less.
  • a zinc-plated steel sheet can be provided that has high strength and sufficient bending resistance and is excellent in LME resistance and bending fatigue strength.
  • FIG. 1 is a schematic view showing an example of a cross section of a steel sheet according to the present embodiment.
  • a zinc-plated steel sheet according to an embodiment of the present invention (sometimes simply referred to as a steel sheet according to the present embodiment) and a method for manufacturing the zinc-plated steel sheet will be described.
  • FIG. 1 is a schematic view showing an example of a cross section of a steel sheet according to the present embodiment.
  • a steel sheet 1 according to the present embodiment includes a base steel sheet 10 having a predetermined chemical composition, a Fe—Al alloy layer 20 formed on at least a part of a surface of the base steel sheet, and a zinc-plated layer 30 formed on the surface of the base steel sheet 10 or a surface of the Fe—Al alloy layer 20 .
  • the base steel sheet 10 has an internal oxide layer 11 on a surface layer area on the interface side with the Fe—Al alloy layer 20 or the zinc-plated layer 30 .
  • the zinc-plated layer 30 is formed on the Fe—Al alloy layer in a portion where the Fe—Al alloy layer 20 is formed on the surface of the base steel sheet 10 , and the zinc-plated layer 30 is formed on the base steel sheet 10 in a portion where the Fe—Al alloy layer 20 is not formed.
  • the Fe—Al alloy layer and the zinc-plated layer are formed only on one surface, but the layers may be also formed on another surface in the same manner.
  • a range indicated by values interposing “to” includes, in principle, values as a lower limit and an upper limit in the range. However, a numerical value indicated with the term “more than” or “less than” is not included in the range.
  • the base steel sheet 10 included in the steel sheet 1 according to the present embodiment contains the following elements.
  • the unit “%” of the amount of each element means % by mass.
  • C is an essential element for high-strengthening of the steel sheet. Sufficient tensile strength cannot be obtained at a C content of less than 0.10%. Therefore, the C content is 0.10% or more. The C content is preferably 0.12% or more. C is also an element that contributes to formation of residual austenite. The residual austenite contributes to an improvement in elongation by the TRIP effect. In the case of obtaining this effect, the C content is preferably 0.16% or more.
  • the C content is 0.40% or less. From the viewpoint of suppressing deterioration of press formability and weldability, the C content is preferably 0.30% or less.
  • Si is a solid solution strengthening element and is an element effective for high-strengthening of the steel sheet. Si is also an element that contributes to formation of residual austenite. In order to obtain these effects, the Si content is 0.10% or more. The Si content is preferably 0.30% or more.
  • the Si content is 3.00% or less.
  • the Si content is preferably 2.00% or less.
  • Mn manganese
  • Mn content is 1.00% or more.
  • the Mn content is preferably 1.50% or more.
  • the Mn content is 5.00% or less. From the viewpoint of suppressing deterioration of the weldability and the low temperature toughness, the Mn content is preferably 3.20% or less.
  • Al is an element having an action of deoxidizing steel. Al is also an element that contributes to formation of residual austenite. In order to obtain these effects, the sol.Al content is 0.001% or more. The sol. Al content is preferably 0.005% or more.
  • the sol.Al content is 1.500% or less.
  • the sol.Al content is preferably 1.000% or less.
  • P (phosphorus) is a solid solution strengthening element and is an element effective for high-strengthening of the steel sheet.
  • the P content is 0.0010% or more.
  • the P content is preferably 0.0050% or more.
  • the P content is 0.0300% or less.
  • the P content is preferably 0.0200% or less.
  • S sulfur is an element that causes hot embrittlement and inhibits weldability and corrosion resistance. If the S content is more than 0.0200%, the hot workability, the weldability, and the corrosion resistance significantly deteriorate, and therefore the S content is 0.0200% or less.
  • the S content is preferably 0.0100% or less.
  • the S content is preferably low, and may be 0%, but the manufacturing cost is greatly increased by lowering the S content to less than 0.0001%. Therefore, the S content may be 0.0001% or more. The S content may be 0.0010% or more.
  • N nitrogen
  • nitrogen is an element that forms a coarse nitride in steel and causes deterioration of bending resistance and hole expandability. If the N content is more than 0.0100%, the deterioration is significant, and therefore the N content is 0.0100% or less.
  • the N content is preferably 0.0050% or less.
  • the N content is preferably low, and may be 0%, but extreme lowering of the N content increases the denitrogenation cost, and therefore the N content may be 0.0005% or more from the viewpoint of economic efficiency.
  • O oxygen
  • the O content is preferably 0.0070% or less.
  • the O content is preferably low, and may be 0%, but from the viewpoint of manufacturing cost, the O content may be 0.0001% or more.
  • the O content may be 0.0010% or more.
  • the steel sheet according to the present embodiment may contain the above-described elements and a remainder of Fe and an impurity.
  • one or more elements (optional elements) selected from Ti, B, Cr, Mo, Ni, Cu, Sn, Nb, V, W, Ca, Mg, Bi, Sb, Zr, and REM shown below may be further contained for the purpose of improving various properties.
  • Optional elements may be not contained, and therefore the lower limit is 0%.
  • Ti titanium is an element that suppresses formation of BN, which is a factor of hardenability deterioration, by fixing N in a form of TiN in steel. Ti is also an element that refines the austenite grain size at the time of heating and thus improves the toughness. In the case of obtaining this effect, the Ti content is preferably 0.005% or more. The Ti content is more preferably 0.010% or more.
  • the Ti content is 0.200% or less.
  • the Ti content is preferably 0.050% or less
  • B is an element that segregates at an austenite grain boundary during welding, strengthens the grain boundary, and contributes to improvement of resistance to liquid metal embrittlement cracking (LME resistance).
  • LME resistance liquid metal embrittlement cracking
  • the B content is preferably 0.0005% or more.
  • the B content is more preferably 0.0008% or more.
  • the B content is 0.0100% or less.
  • the B content is preferably 0.0050% or less.
  • Cr chromium
  • Mo mobdenum
  • Ni nickel
  • Cu copper
  • Sn tin
  • one or more selected from Cr, Mo, Ni, Cu, and Sn are each preferably contained at a content of 0.001% or more, more preferably 0.010% or more, and still more preferably 0.050% or more.
  • Nb (niobium), V (vanadium), and W (tungsten) are a carbide forming element, and are an element effective for high-strengthening of the steel sheet.
  • one or more selected from Nb, V, and W are each preferably contained at a content of 0.001% or more, more preferably 0.005% or more, and still more preferably 0.010% or more.
  • the Nb content is 0.200% or less, and both of the V content and the W content are 0.500% or less.
  • the Nb content is preferably 0.100% or less, and both of the V content and the W content are preferably 0.300% or less.
  • Ca calcium
  • Mg magnesium
  • Sb antimony
  • Zr zirconium
  • REM rare earth elements
  • Bi bismuth
  • Mn substitutional alloying element
  • one or more selected from Ca, Mg, Bi, Sb, Zr, and REM are each preferably contained at a content of 0.0001% or more, and more preferably 0.0010% or more.
  • all of the Ca content, the Mg content, the Bi content, and the Zr content are 0.0100% or less.
  • the Sb content and the REM content are 0.1000% or less. All of the Ca content, the Mg content, the Bi content, and the Zr content are preferably 0.0080% or less, and more preferably 0.0060% or less.
  • the Sb content and the REM content are preferably 0.0800% or less, more preferably 0.0600% or less, and still more preferably 0.0200% or less.
  • REM refers to 17 elements including Sc, Y, and lanthanoids in total, and the REM content means the total amount of these elements.
  • a lanthanoid is industrially added in the form of a misch metal.
  • the chemical composition of the base steel sheet of the steel sheet according to the present embodiment can be determined with the following method.
  • the chemical composition of the base steel sheet is to be measured as a general method.
  • the measurement is to be performed by, for example, inductively coupled plasma-atomic emission spectrometry (ICP-AES).
  • ICP-AES inductively coupled plasma-atomic emission spectrometry
  • the sol.Al is to be measured by ICP-AES using a filtrate after thermal decomposition of a sample with an acid.
  • C and S are to be measured with a combustion-infrared absorption method
  • N is to be measured with an inert gas fusion-thermal conductivity method
  • O is to be measured with an inert gas fusion-non-dispersive infrared absorption method.
  • the chemical composition is to be analyzed after removing the plated layer by mechanical grinding.
  • the chemical composition of the base steel sheet of the steel sheet according to the present embodiment contains C, Si, Mn, sol.Al, P, S, O, and N, and the remainder of Fe and an impurity.
  • the chemical composition contains C, Si, Mn, sol.Al, P, S, O, and N, and further contains one or more elements selected from Ti, B, Cr, Mo, Ni, Cu, Sn, Nb, V, W, Ca, Mg, Bi, Sb, Zr, and REM, and the remainder of Fe and an impurity.
  • the impurity is an element mixed in a raw material or mixed during the manufacturing process.
  • the amount of the impurity is preferably 0.5% or less in total, and more preferably 0.1% or less in total.
  • the base steel sheet of the steel sheet according to the present embodiment is not limited in terms of the metallographic structure, but in the case of obtaining a tensile strength of 980 MPa or more, the total volume percentage of fresh martensite and tempered martensite is preferably 40% or more in the metallographic structure at the 1/4 thickness position, which is a range of 1/8 to 3/8 of the sheet thickness from the surface and has a center on the position of 1/4 of the sheet thickness in the sheet thickness direction from the surface of the base steel sheet.
  • the total volume percentage is more preferably more than 50%, and still more preferably 55% or more.
  • the total volume percentage of fresh martensite and tempered martensite is preferably 80% or more.
  • the metallographic structure other than fresh martensite and tempered martensite is, for example, one or more of ferrite, bainite, pearlite, cementite, and residual austenite.
  • the volume percentage of ferrite, bainite, martensite (tempered martensite and fresh martensite), pearlite, cementite, and residual austenite contained in the metallographic structure at the 1/4 thickness position can be measured using the following method.
  • a sample is collected to have an observed section that is a cross section parallel to the rolling direction and the sheet thickness direction of the steel sheet, and the observed section is polished and etched with nital.
  • a visual field is set to have an area of 250 ⁇ m 2 or more, and 5 visual fields in total are observed with a field emission scanning electron microscope (FE-SEM) at a magnification of 5000 times in the range of 1/8 to 3/8 of the thickness having a center on the position of 1/4 of the thickness from the surface. Then, the area fraction of each of ferrite, bainite, tempered martensite, fresh martensite, pearlite, cementite, and residual austenite is measured and regarded as the volume percentage.
  • FE-SEM field emission scanning electron microscope
  • a region having a substructure in the grains and including a carbide precipitated with a plurality of variants is determined as tempered martensite.
  • a region including cementite precipitated in a lamellar shape is determined as pearlite or cementite.
  • a region having a low brightness with no substructure recognized is determined as ferrite.
  • a region having a high brightness and a substructure that is not exposed by etching is determined as fresh martensite or residual austenite. The remainder is determined as bainite.
  • Each volume percentage is calculated with a point counting method to determine the volume percentage of each microstructure.
  • the volume percentage of fresh martensite can be determined by subtracting the volume percentage of residual austenite determined with an EBSD method described below from the volume percentage of fresh martensite or residual austenite
  • the volume percentage of residual austenite at the 1/4 thickness position is evaluated by high-resolution crystal structural analysis using an EBSD method (electron backscatter diffraction method). Specifically, a sample is collected to have an observed section that is a cross section parallel to the rolling direction and the sheet thickness direction of the steel sheet, and the observed section is polished and finished into a mirror surface. Furthermore, electrolytic polishing or mechanical polishing using colloidal silica is performed to remove the machined layer on the surface layer.
  • EBSD method electron backscatter diffraction method
  • the data obtained by the EBSD method is analyzed using “OIM Analysis 6.0” manufactured by TSL Solutions K.K. From the observation result at each position, a region determined as FCC iron is determined as residual austenite, and the volume percentage of each residual austenite at the 1/4 thickness position is calculated.
  • the base steel sheet 10 included in the steel sheet 1 according to the present embodiment has an internal oxide layer of 0.2 ⁇ m or more from the surface (interface with the Fe—Al alloy layer 20 , or interface with the zinc-plated layer 30 in a portion where the Fe—Al alloy layer 20 is not formed) in the sheet thickness direction (internal oxide layer having a thickness of 0.2 ⁇ m or more).
  • the internal oxide layer is a layer in which at least a part of the grain boundary of the base metal is covered with an oxide of an easily oxidizable element such as Si or Mn (an oxide is observed on the grain boundary during observation of a cross section).
  • the grain boundary coverage by the oxide in the internal oxide layer 11 is 60% or more.
  • the grain boundary coverage is the percentage (%) of the length of the grain boundary covered with the oxide in the total length of the grain boundary in the internal oxide layer 11 .
  • the thickness of the internal oxide layer 11 is less than 0.2 ⁇ m or the grain boundary coverage is less than 60%, the effect of improving the fatigue strength is not sufficiently obtained.
  • the thickness of the internal oxide layer 11 does not have a particular upper limit, but if the thickness is more than 3.0 ⁇ m, the effect of improving the fatigue strength is saturated, and deterioration of the deformability may cause deterioration of the bendability, and therefore the thickness of the internal oxide layer 11 is preferably 3.0 ⁇ m or less.
  • an easily oxidizable element such as Si or Mn is present as an oxide at the grain boundary, concentration of the oxide on the surface of the base metal is suppressed.
  • concentration of the oxide on the surface of the base metal is suppressed.
  • the oxide formed on the base metal surface deteriorates the wettability of the hot-dip plated metal, and also causes bare spots. Therefore, formation of the internal oxide layer can prevent occurrence of bare spots and improve the plating property.
  • the oxide is mainly formed on the grain boundary in the internal oxide layer 11 , and therefore the oxide is often present in a network shape.
  • the thickness of the internal oxide layer (the depth at which the internal oxide layer is present) and the grain boundary coverage of the internal oxide layer are determined with the following method.
  • a sample for microstructure observation is collected from the steel sheet so that the microstructure of a cross section in the sheet thickness direction can be observed.
  • a surface parallel to the rolling direction and the sheet thickness direction is subjected to wet polishing with emery paper, and further subjected to buffing using diamond abrasive grains having an average size of 1 ⁇ m to finish the observed section into a mirror surface.
  • polishing using colloidal silica is performed using a suspension containing an alcohol as a solvent.
  • an increase in the load during polishing may further introduce strain, and therefore the load is suppressed during polishing. Therefore, for example, in polishing with colloidal silica, automatic polishing may be performed for 1 hour at an output set to 40% using VibroMet 2 manufactured by Buehler.
  • the surface layer area of the observed section of the sample prepared with the above-described procedure is observed using a SEM and SEM-EBSD. From an observation magnification of 1000 to 9000 times, a magnification is selected at which the microstructure includes 10 or more grains of ferrite, and for example, the magnification is set to 3000 times.
  • an oxide present at a grain boundary is confirmed from a reflected electron image in the SEM.
  • the color tone depends on the atomic number (or mass), and therefore the oxide and the steel structure can be easily distinguished.
  • the microstructure observation of the reflected electron image for example, when a state of a small atomic number (or mass) is set to be displayed in a “black color tone”; an oxide having a smaller mass than iron is displayed in a black color tone in the observation image.
  • the microstructure of the steel sheet surface layer area is photographed in five visual fields, and the state of presence of the internal oxide is confirmed.
  • the observed maximum depth of the internal oxide layer is regarded as the thickness of the internal oxide layer.
  • crystal orientation data of BCC-iron is acquired by SEM-EBSD at the same position as the visual field observed in the above-described SEM-reflected electron image.
  • the magnification for the measurement is any magnification selected from 1000 to 9000 times, and may be, for example, the same magnification as in the above-described observation of the SEM-reflected electron image.
  • the interval of the measurement (step) is set to 0.01 to 0.1 ⁇ m, and an interval of 0.05 ⁇ m may be selected.
  • the Fe—Al alloy layer 20 having an average thickness of 1 nm or more is formed on the surface of the base steel sheet 10 at a coverage of 40% or more.
  • the Fe—Al alloy layer 20 is formed between the base steel sheet 10 and the zinc-plated layer 30 .
  • the average thickness of the Fe—Al alloy layer is 1 nm or more, and the coverage is 40% or more.
  • the average thickness of the Fe—Al alloy layer is preferably 5 nm or more, more preferably 10 nm or more, and still more preferably 20 nm or more.
  • the coverage by the Fe—Al alloy layer is preferably 50% or more, and more preferably 60% or more.
  • the upper limit of the coverage is not required to be limited, but the cost to obtain a coverage of 100% is significantly high, and therefore the coverage may be less than 100%, or 98% or less.
  • the coverage is the percentage (%) of the length of the interface between the Fe—Al alloy layer and the base steel sheet in the length of the surface of the base steel sheet when viewed in a cross section in the thickness direction.
  • the average thickness of the Fe—Al alloy layer and the coverage by the Fe—Al alloy layer are determined with the following method.
  • a sample is collected to have an observed section that is a cross section parallel to the rolling direction and the sheet thickness direction of the steel sheet.
  • the vicinity of the surface of the base steel sheet is photographed using a FE-SEM in the range of 1.5 ⁇ m 2 or more/1 visual field at a magnification of 50000 times.
  • the Fe—Al alloy layer is observed in a black color in the reflected electron image at the interface between the base phase and the plated layer, and thus the Fe—Al alloy layer is visually determined, and the thickness of the Fe—Al alloy layer is measured.
  • the photographing is performed at 5 locations/1 visual field for 5 visual fields, and the average value of the thickness of the Fe—Al alloy layer in 5 visual fields (25 locations) is regarded as the average thickness of the Fe—Al alloy layer of the steel sheet according to the present embodiment.
  • the length of the interface between the base steel sheet and the Fe—Al alloy layer is measured in the length of the surface of the base steel sheet in the observed visual field and the coverage is determined.
  • the measurement is performed for five visual fields, and the average of the coverages of the visual fields is regarded as the coverage of the steel sheet according to the present embodiment.
  • the steel sheet 1 includes the zinc-plated layer 30 on the surface of the base steel sheet 10 (a portion without the Fe—Al alloy layer) and/or the Fe—Al alloy layer 20 (a portion having the Fe—Al alloy layer on the base steel sheet).
  • the zinc-plated layer is, for example, a hot-dip galvanized layer.
  • the zinc-plated layer means a plated layer containing 80 mass % or more of Zn. The presence of the hot-dip galvanized layer on the surface improves the corrosion resistance.
  • the adhesion amount of the zinc-plated layer is not particularly limited. However, if the adhesion amount is too large, the amount of molten zinc during welding is increased. Therefore, from the viewpoint of more effectively suppressing occurrence of LME, the adhesion amount is preferably 100 g/m 2 or less, and more preferably 80 g/m 2 or less.
  • the adhesion amount is preferably 10 g/m 2 or more.
  • the chemical composition of the zinc-plated layer is not limited, and, for example, preferably includes Al: 0.1 to 2.0% and Fe: 5.0% or less in mass %, with a remainder of Zn and an impurity.
  • the amount of the impurity is preferably 0.1 mass % or less in total.
  • the adhesion amount and the chemical composition of the zinc-plated layer are determined with the following method.
  • the plated layer is melted using hydrochloric acid containing an inhibitor, and the weights before and after the melt are compared to determine the adhesion amount.
  • the solution obtained by the melt is quantitatively analyzed by ICP to measure the chemical composition of the plated layer.
  • the steel sheet according to the present embodiment is desired to have a high strength.
  • the tensile strength is 980 MPa or more.
  • the tensile strength is preferably 1050 MPa or more, and more preferably 1100 MPa or more.
  • the tensile strength is more than 2000 MPa, the residual stress at the time of welding is increased and causes a crack in the internal oxide layer on the grain boundary, and thus the effect of suppressing an LME crack remarkably deteriorates. Therefore, the tensile strength is 2000 MPa or less.
  • An effect of the steel sheet according to the present embodiment can be obtained as long as the steel sheet has the above-described characteristics regardless of the manufacturing method.
  • the manufacturing conditions described below are preferable because the steel sheet can be stably manufactured.
  • the steel sheet according to the present embodiment can be manufactured by annealing and plating a steel sheet (hot-rolled steel sheet or cold-rolled steel sheet) to be a base steel sheet under predetermined conditions.
  • the conditions for manufacturing the steel sheet to be subjected to the annealing step are not limited.
  • a hot-rolled steel sheet can be manufactured by casting molten steel having the above-described chemical composition under normal conditions to form a steel piece, and then subjecting the steel piece to hot rolling under normal conditions.
  • a cold-rolled steel sheet can be manufactured by subjecting the hot-rolled steel sheet to cold rolling under normal conditions.
  • the annealing step includes a heating process of heating a steel sheet having a predetermined chemical composition (the same chemical composition as that of the steel sheet according to the present embodiment to be obtained) to an annealing temperature (maximum heating temperature) of 700 to 1000° C. and a holding process of holding the heated steel sheet at the annealing temperature for 1 second or more.
  • the annealing is preferably performed by passing the steel sheet through a continuous annealing line.
  • an annealing temperature is less than 700° C., the amount of austenite is insufficient, and a sufficient amount of hard structure cannot be ensured in phase transformation during subsequent cooling, so that a sufficient tensile strength cannot be obtained. Therefore, the annealing temperature is 700° C. or more.
  • the annealing temperature is preferably 720° C. or more.
  • the annealing temperature is 1000° C. or less.
  • the annealing temperature is preferably 900° C. or less.
  • the steel sheet is heated to an annealing temperature (maximum heating temperature: 700 to 1000° C.).
  • the average heating rate in a first temperature range of 400 to 650° C. is 2.0° C./sec or more
  • the average heating rate in a second temperature range of 650° C. to the annealing temperature is 0.5 to 5.0° C./sec
  • (P(H2O)/P(H2)) of the atmosphere is 0.05 to 2.00 in the second temperature range.
  • dislocations are mainly recovered during heating. If the average heating rate in this temperature range is 2.0° C./sec or more, recovery of dislocations is suppressed, and thus many dislocations to be nuclei of recrystallization can remain. In this case, recrystallization that occurs in a temperature range of 650° C. or more can occur in many places.
  • the upper limit of the average heating rate in the first temperature range is not limited, but the average heating rate is preferably 20.0° C./sec or less from the viewpoint of cost.
  • the second temperature range of 650° C. to the annealing temperature is a temperature range in which recrystallization occurs, and is a temperature range in which an internal oxide layer is formed by controlling the atmosphere.
  • the average heating rate in this temperature range is more than 5.0° C./sec, recrystallization of the steel sheet proceeds before an oxide is formed in the surface layer area, and coarse ferrite grains are generated. In this case, an internal oxide layer in which the grain boundary is covered with an oxide is not formed.
  • the average heating rate is less than 0.5° C./sec, a decarburization reaction may excessively proceed, and the tensile strength of the steel sheet may deteriorate.
  • (P(H2O)/P(H2)) which is the ratio of the water vapor partial pressure P(H2O) to the hydrogen partial pressure P(H2) in the atmosphere in the furnace, is less than 0.05, a sufficient internal oxide layer cannot be ensured. Therefore, (P(H2O)/P(H2)) is 0.05 or more. (P(H2O)/P(H2)) is preferably 0.07 or more, and more preferably 0.10 or more.
  • (P(H2O)/P(H2)) is more than 2.00, decarburization excessively proceeds, the thickness of the decarburized layer is increased, and the tensile strength of the steel sheet decreases. Therefore, (P(H2O)/P(H2)) is 2.00 or less. (P(H2O)/P(H2)) is preferably 1.50 or less, and more preferably 1.20 or less.
  • the average heating rate in the first temperature range is preferably higher than the average heating rate in the second temperature range, and the average heating rate in the first temperature range is more preferably higher than the average heating rate in the second temperature range by 2.0° C./sec or more.
  • the steel sheet After heating to the annealing temperature as described above, the steel sheet is held at a predetermined maximum heating temperature for 1 second or more. If the holding time is less than 1 second, the steel sheet is not sufficiently austenitized. In this case, a sufficient amount of hard structure cannot be ensured in phase transformation during subsequent cooling, so that a sufficient tensile strength cannot be obtained.
  • the upper limit of the holding time is not particularly limited. However, if the holding time is too long, the manufacturability of the steel sheet is impaired, and therefore the upper limit value of the holding time is preferably 1000 seconds.
  • the steel sheet after the annealing step is cooled from the annealing temperature to a temperature of 440 to 550° C. at an average cooling rate of 0.5° C./sec or more, and the steel sheet is immersed in a plating bath containing Zn as a main component and having an effective Al amount of 0.050 to 0.250 mass %, pulled up from the plating bath, and then cooled so that the temperature of the steel sheet reaches 400° C. within 10 seconds, and subsequently cooled to 350° C. or less at an average cooling rate of 1.0° C./sec or more and 5.0° C./sec or less in a range of 400 to 350° C.
  • a zinc-plated layer is formed on the surface of the steel sheet, and a Fe—Al alloy layer is formed on at least a part of the interface between the steel sheet and the plated layer.
  • the average cooling rate to a temperature of 440 to 550° C. is less than 0.5° C./sec, a hard structure is not formed in the base steel sheet, and the strength decreases.
  • the cooling stop temperature (the temperature of the steel sheet at the time of immersion in the plating bath) is less than 440° C., application of a large amount of heat to the plating bath is necessary for maintaining the plating temperature, and thus the manufacturing cost is increased.
  • the temperature of the steel sheet at the time of immersing the steel sheet in the plating bath is more than 550° C., equipment for removing a large amount of heat from the plating bath is necessary for maintaining the plating bath temperature, and thus the manufacturing cost is increased.
  • the composition of the plating bath in which the steel sheet is immersed contains Zn as a main component (for example, at a content of 80 mass % or more), and is not limited as long as the effective Al amount (value obtained by subtracting the total Fe amount from the total Al amount in the plating bath) is 0.050 to 0.250 mass %.
  • the composition may include another element, for example, one or more selected from Ag, B, Be, Bi, Ca, Cd, Co, Cr, Cs, Cu, Ge, Hf, I, K, La, Li, Mg, Mn, Mo, Na, Nb, Ni, Pb, Rb, S, Si, Sn, Sr, Ta, Ti, V, W, Zr, and REM, as necessary.
  • the effective Al amount in the plating bath is less than 0.050 mass %, the formation of a Fe—Al alloy layer becomes insufficient. Furthermore, intrusion of Fe into the plating layer may excessively proceed, leading to deterioration of the plating adhesion.
  • the effective Al amount in the plating bath is preferably 0.065 mass % or more.
  • the effective Al amount in the plating bath is more than 0.250 mass %, an Al-based oxide that inhibits movement of Fe atoms and Zn atoms is generated at the boundary between the steel sheet and the plated layer, and the plating adhesion may deteriorate.
  • the effective Al amount in the plating bath is preferably 0.180 mass % or less.
  • the plating bath temperature is not limited, but is preferably 450 to 490° C. If the plating bath temperature is less than 450° C., the viscosity of the plating bath excessively increases, control of the plated layer thickness becomes difficult, and the external appearance of the hot-dip galvanized steel sheet may be impaired.
  • the plating bath temperature is preferably 455° C. or more.
  • the plating bath temperature is preferably 480° C. or less.
  • the steel sheet After the steel sheet is pulled up from the plating bath, the steel sheet is cooled so that the temperature of the steel sheet reaches 400° C. within 10 seconds while the adhesion amount is adjusted by wiping with an N 2 gas or the like, and then cooled to 350° C. or less at an average cooling rate of 1.0° C./sec or more and 5.0° C./sec or less in a range of 400 to 350° C.
  • Alloying of the plated layer with the base phase proceeds mainly at a temperature of 400° C. or more. Therefore, excessive alloying of the plated layer can be prevented by cooling the steel sheet so that the time of pulling up from the plating bath to the time at which the temperature reaches 400° C. is 10 seconds or less (so that the temperature reaches 400° C. within 10 seconds). If the time to 400° C. is more than 10 seconds, not a Fe—Al alloy layer but a Fe—Zn alloy layer is formed, and a predetermined Fe—Al alloy layer cannot be obtained.
  • the average cooling rate in a range of 400 to 350° C. is set to 5.0° C./sec or less so that the time at 400 to 350° C. is 10.0 seconds or more, and thus a Fe—Al alloy layer is formed at the interface between the plated layer and the base phase, and the coverage can be 40% or more.
  • the average cooling rate in a range of 400 to 350° C. is 1.0° C./sec or more.
  • the plating bath temperature is more than 450° C., and that the temperature reaches 400° C. within 10 seconds (that is, the average cooling rate to 400° C. is more than 5.0° C./sec) and then the average cooling rate in a range of 400 to 350° C. is 5.0° C./sec or less so that the average cooling rate to 400° C. is higher than the average cooling rate in a range of 400 to 350° C.
  • the two-stage cooling as described above appropriately forms a Fe—Al alloy layer at the interface between the zinc-plated layer and the base steel sheet.
  • the Fe—Al alloy layer formed at the interface between the zinc-plated layer and the base steel sheet takes in and integrates the internal oxide at the grain boundary of the steel sheet surface layer area.
  • the average cooling rate to 400° C. is more preferably 6.0° C./sec or more.
  • the steel sheet after the plating step may be subjected to skin pass rolling for the purpose of shape adjustment and the like.
  • the rolling rate is preferably 0.5% or less.
  • a slab having a chemical composition described in Tables 1-1 to Tables 1 ⁇ 4 was hot-rolled and coiled to obtain a hot-rolled steel sheet having a sheet thickness of 3.0 mm. This hot-rolled steel sheet was cold-rolled to obtain a cold-rolled steel sheet having a sheet thickness of 1.6 mm.
  • This cold-rolled steel sheet was heated to an annealing temperature and held under conditions shown in Tables 2-1 and 2-2.
  • the steel sheet was cooled to a temperature of 440 to 550° C., and then immersed in a plating bath to form a zinc-plated layer.
  • the steel sheet After immersion in the plating bath, the steel sheet was cooled so that the values of the cooling time and the average cooling rate to 400° C. were as in Tables 2-1 and 2-2. Thereafter, cooling was switched, and the steel sheet was cooled to 350° C. or less so that the value of the average cooling rate in a range of 400 to 350° C. was as in Tables 2-1 and 2-2.
  • the base steel sheet was observed with the above-described method, and the thickness of the internal oxide layer, the grain boundary coverage of the internal oxide layer, and the microstructure at the 1/4 thickness position were observed.
  • Tables 3-1 and 3-2 show the results.
  • the adhesion amount of the zinc-plated layer was 10 to 80 g/m 2 .
  • the obtained zinc-plated steel sheet was evaluated for tensile strength (TS), LME resistance, bending fatigue strength, and bending resistance in the following manner.
  • a JIS No. 5 tensile test piece was collected in the direction (width direction) perpendicular to the rolling direction and the thickness direction of the zinc-plated steel sheet (the rolling direction and the sheet thickness direction of the base steel sheet), and subjected to a tensile test in accordance with JIS Z 2241: 2011 to measure the tensile strength (TS).
  • a tensile strength of 980 MPa or more was determined to be a high strength.
  • An evaluation material having a size of 30 mm ⁇ 30 mm was collected from the zinc-plated steel sheet, and two sheets of this evaluation material were overlapped each other and energized under the following conditions to perform a spot welding test.
  • Electrode ⁇ 8, R40
  • the current was set so that the nugget diameter was 5 mm.
  • Length of crack is 80 ⁇ m or less: OK (excellent in LME resistance)
  • Length of crack is more than 80 ⁇ m: NG
  • a bending test was performed in accordance with VDA 238-100, and the bending angle (°) at this time was evaluated as follows.
  • the test piece was collected in the direction in which the bending ridgeline was parallel to the rolling direction.
  • test piece was a No. 1 test piece having a width of 30 mm and an R of 40 mm.
  • the tensile strength was low, or the internal oxide layer and the Fe—Al alloy layer were not formed in a preferable state, and therefore at least one of the LME resistance, the bending fatigue strength, or the bending resistance was poor.
  • a zinc-plated steel sheet that has high strength and sufficient bending resistance and is excellent in LME resistance and bending fatigue strength can be provided.
  • Such a steel sheet is useful as a high-strength steel sheet for a vehicle.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Oil, Petroleum & Natural Gas (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Coating With Molten Metal (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
US18/839,195 2022-02-25 2023-01-27 Zinc-plated steel sheet and method for producing same Pending US20250154633A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2022-027919 2022-02-25
JP2022027919 2022-02-25
PCT/JP2023/002565 WO2023162573A1 (ja) 2022-02-25 2023-01-27 亜鉛めっき鋼板およびその製造方法

Publications (1)

Publication Number Publication Date
US20250154633A1 true US20250154633A1 (en) 2025-05-15

Family

ID=87765508

Family Applications (1)

Application Number Title Priority Date Filing Date
US18/839,195 Pending US20250154633A1 (en) 2022-02-25 2023-01-27 Zinc-plated steel sheet and method for producing same

Country Status (7)

Country Link
US (1) US20250154633A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP4484590A4 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JPWO2023162573A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
KR (1) KR20240144265A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CN (1) CN118742664A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
MX (1) MX2024010245A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
WO (1) WO2023162573A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0537674Y2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 1986-11-28 1993-09-22
WO2013047821A1 (ja) * 2011-09-30 2013-04-04 新日鐵住金株式会社 焼付硬化性に優れた高強度溶融亜鉛めっき鋼板、高強度合金化溶融亜鉛めっき鋼板、並びにそれらの製造方法
PL3378965T3 (pl) * 2016-02-25 2021-01-25 Nippon Steel Corporation Blacha stalowa cienka o dużej wytrzymałości cynkowana zanurzeniowo na gorąco o doskonałej odporności na łuszczenie przy uderzeniu oraz odporności na korozję obszaru poddawanego obróbce
WO2018043453A1 (ja) 2016-08-30 2018-03-08 Ｊｆｅスチール株式会社 薄鋼板およびその製造方法
JP6281671B1 (ja) * 2017-07-31 2018-02-21 新日鐵住金株式会社 溶融亜鉛めっき鋼板
EP3663425B1 (en) * 2017-07-31 2024-03-06 Nippon Steel Corporation Hot-dip galvanized steel sheet
JP6388099B1 (ja) 2017-12-15 2018-09-12 新日鐵住金株式会社 鋼板、溶融亜鉛めっき鋼板および合金化溶融亜鉛めっき鋼板
KR102516012B1 (ko) * 2019-04-19 2023-03-31 닛폰세이테츠 가부시키가이샤 도금 강판
WO2021224662A1 (en) * 2020-05-07 2021-11-11 Arcelormittal Annealing method of steel
JP7211478B2 (ja) 2020-08-11 2023-01-24 株式会社三洋物産 遊技機

Also Published As

Publication number Publication date
EP4484590A1 (en) 2025-01-01
CN118742664A (zh) 2024-10-01
EP4484590A4 (en) 2025-06-18
JPWO2023162573A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 2023-08-31
KR20240144265A (ko) 2024-10-02
WO2023162573A1 (ja) 2023-08-31
MX2024010245A (es) 2024-09-02

Similar Documents

Publication Publication Date Title
CN111492075B (zh) 钢板、热浸镀锌钢板和合金化热浸镀锌钢板
JP6264507B2 (ja) 高強度亜鉛めっき鋼板及びその製造方法
KR102252841B1 (ko) 고강도 아연 도금 강판 및 그 제조 방법
KR102626001B1 (ko) 강판 및 그 제조 방법
US9109275B2 (en) High-strength galvanized steel sheet and method of manufacturing the same
CN111433380A (zh) 高强度镀锌钢板及其制造方法
JP6897882B2 (ja) 熱延鋼板およびその製造方法
US12270088B2 (en) Steel sheet and method for manufacturing same
KR102513331B1 (ko) 고강도 열연 도금 강판
JPWO2019130713A1 (ja) 高強度鋼板およびその製造方法
JP7276618B2 (ja) 高強度冷延鋼板およびその製造方法
KR20220144405A (ko) 강판, 부재 및 그들의 제조 방법
JP7260073B1 (ja) 高強度鋼板，高強度めっき鋼板及びそれらの製造方法，並びに部材
JP6460238B2 (ja) 鋼板、溶融亜鉛めっき鋼板、及び合金化溶融亜鉛めっき鋼板、並びにそれらの製造方法
CN115362275A (zh) 钢板、部件及其制造方法
WO2017009938A1 (ja) 鋼板、溶融亜鉛めっき鋼板、及び合金化溶融亜鉛めっき鋼板、並びにそれらの製造方法
KR102748708B1 (ko) 강판 및 그 제조 방법
WO2022071305A1 (ja) 鋼板
KR20240027747A (ko) 고강도 강판
US20250154633A1 (en) Zinc-plated steel sheet and method for producing same
WO2023095870A1 (ja) 亜鉛めっき鋼板
WO2024241645A1 (ja) 高強度鋼板およびその製造方法
CN120380182A (zh) 热冲压成形体
KR20250121067A (ko) 냉연 강판 및 그 제조 방법

Legal Events

Date Code Title Description
AS Assignment

Owner name: NIPPON STEEL CORPORATION, JAPAN

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:TSUNEMI, YUSUKE;REEL/FRAME:068313/0396

Effective date: 20240813

STPP Information on status: patent application and granting procedure in general

Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION