US20180230570A1 - High strength hot dip galvanised steel strip - Google Patents

High strength hot dip galvanised steel strip Download PDF

Info

Publication number
US20180230570A1
US20180230570A1 US15/580,776 US201615580776A US2018230570A1 US 20180230570 A1 US20180230570 A1 US 20180230570A1 US 201615580776 A US201615580776 A US 201615580776A US 2018230570 A1 US2018230570 A1 US 2018230570A1
Authority
US
United States
Prior art keywords
steel strip
temperature
strip
hot dip
amount
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.)
Abandoned
Application number
US15/580,776
Other languages
English (en)
Inventor
Joost Willem Hendrik van Krevel
Cornelia IONESCU
Bernard Leo Ennis
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.)
Tata Steel Ijmuiden BV
Original Assignee
Tata Steel Ijmuiden BV
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 Tata Steel Ijmuiden BV filed Critical Tata Steel Ijmuiden BV
Assigned to TATA STEEL IJMUIDEN B.V. reassignment TATA STEEL IJMUIDEN B.V. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: IONESCU, Cornelia, VAN KREVEL, JOOST WILLEM HENDRIK, ENNIS, BERNARD LEO
Publication of US20180230570A1 publication Critical patent/US20180230570A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/52Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/002Heat treatment of ferrous alloys containing Cr
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/005Heat treatment of ferrous alloys containing Mn
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D6/00Heat treatment of ferrous alloys
    • C21D6/008Heat treatment of ferrous alloys containing Si
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0205Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
    • 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 by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0236Cold rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0278Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • C21D8/0463Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment following hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/0447Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the heat treatment
    • C21D8/0473Final recrystallisation annealing
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/06Ferrous alloys, e.g. steel alloys containing aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/28Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/32Ferrous alloys, e.g. steel alloys containing chromium with boron
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/38Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/58Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
    • CCHEMISTRY; METALLURGY
    • 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
    • C23C2/02Pretreatment 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
    • 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
    • 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
    • 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
    • C23C2/26After-treatment
    • 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
    • C23C2/34Hot-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
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/001Austenite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/002Bainite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/005Ferrite
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2211/00Microstructure comprising significant phases
    • C21D2211/008Martensite
    • 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 by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0221Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
    • C21D8/0226Hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties 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 by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0273Final recrystallisation annealing
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21DMODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/46Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals

Definitions

  • the invention relates to a high strength hot dip galvanised steel strip having improved formability, such as used in the automotive industry.
  • the invention also relates to a method for producing such steel strip.
  • Formability is not the only requirement for a TRIP assisted dual phase steel strip.
  • the alloying elements should be low in amount to make the cost of the steel. as low as possible, and it should be as easy as possible to produce the steel strip at a is broader width both in the hot rolling mill and in the cold rolling mill.
  • the steel strip should be easy to coat with a zinc based coating, the steel strip has to have high strength and a good weldability, and should also exhibit a good surface quality.
  • the balance being Fe and inevitable impurities.
  • the inventors have found that by a careful selection of the amounts of the main constituting elements of the steel, being carbon, manganese, silicon, aluminium, chromium and boron, a high strength hot dip galvanised steel strip can be produced that has the required formability, homogeneity, processability, strength and elongation, while at the same time providing a sufficient weldability, coatability and surface quality.
  • the inventors have especially found that it is advantageous to add boron to the composition of the steel.
  • the hot rolled steel can be cooled fast enough on the run-out table to get a coiling temperature that provides a suitable microstructure for further processing.
  • the inventors due to the addition of boron, the inventors have found that the properties of the end product have a high degree of homogeneity.
  • the steel strip can be produced in a width that is commercially interesting.
  • TRIP assisted steel grades can be made by intercritically annealing of the cold rolled strip so that ferrite nucleation is not required.
  • adding boron improves the hardenability of the steel, resulting in the possibility to use less of the other alloying elements. This results in an improved dimensional window for the steel strip, meaning a higher width to thickness ratio while the mechanical properties of the steel over the width of the strip remain suitable.
  • C 0.10-0.21 mass %.
  • Carbon has to be present in an amount that is high enough to ensure hardenability and the formation of martensite at the cooling rates available in a conventional annealing/galvanising line, Martensite is required to deliver adequate strength. Free carbon also enables stabilisation of austenite which delivers improved work hardening potential and good formability for the resulting strength level. A lower limit of 0,10 mass % is needed for these reasons. A maximum level of 0.21 mass % a has been found to be essential to ensure good weldability.
  • Mn 1.75-2.50 mass %.
  • Manganese is added to increase hardenability thus making the formation of hard phases like martensite or bainite easier within the cooling rate capability of a conventional continuous annealing/galvanising line.
  • Manganese also contributes to the solid solution strengthening which increases the tensile strength and strengthens the ferrite phase, and also helps to stabilise retained austenite, Manganese lowers the transformation temperature range of the dual phase steel, thus lowering the required annealing temperature to levels that can be readily attained in a conventional continuous annealing/galvanising line.
  • a lower limit of 1.75 mass % is needed for the above reasons. This lower limit is possible in view of the addition of other elements, such as boron.
  • a maximum level of 2.50 mass % is imposed to ensure acceptable rolling forces in the hot mill and to ensure acceptable rolling forces in the cold mill by ensuring sufficient transformation of the dual phase steel to soft transformation products (fenite and pearlite). This maximum level is also given in view of the stronger segregation during casting and the forming of a band of martensite in the strip at higher values.
  • the amount of manganese is between 1.9 and 2.3 mass %, more preferably between 2.0 and 2.2 mass %.
  • Si 0.04-0.60 mass %.
  • Silicon provides solid solution strengthening thus enabling the attainment of high strength, and the stabilisation of austenite via strengthening of the ferrite matrix. Silicon very effectively retards the formation of carbides during overaging, thus keeping carbon in solution for stabilisation of austenite. For these reasons a lower limit of 0.04 mass % is needed. A maximum level of 0.60 mass % is imposed in view of the coatability of the steel strip, since high levels of silicon lead to unacceptable coating quality due to reduced adherence.
  • Al 0.20-1.40 mass %. Aluminium is added to liquid steel for the purpose of de-oxidation. In the right quantity it also provides an acceleration of the bainite transformation, thus enabling bainite formation within the time constraints imposed by the annealing section of a conventional continuous annealing/galvanising line. Aluminium also retards the formation of carbides thus keeping carbon in solution, thus causing partitioning to austenite during overaging, and promoting the stabilisation of austenite. A lower level of 0.20 mass % is required for the above reasons. A maximum level of 1.40 mass % is imposed for castability, since high aluminium contents lead to poisoning of the casting mould slag and consequently an increase in mould slag viscosity, leading to incorrect heat transfer and lubrication during casting.
  • Cr max 0.50 mass %. Chrome is added to increase hardenability. Chrome promotes formation of ferrite. A maximum level of 0.50 mass % is imposed to ensure that not too much martensite forms at the cost or retained austenite. It is also possible to add no chrome. Preferably, the amount of Cr is between 0.01 and 0.40 mass %, more preferably between 0.02 and 0.25 mass %.
  • Titanium max 0.20%. Titanium is mainly added to strengthen the steel, A maximum level of 0.20 is imposed to limit the cost of the steel. It is also possible to add no Ti,
  • Ca max 0.004 mass %.
  • the addition of calcium modifies the morphology of manganese sulphide inclusions. When calcium is added the inclusions get a globular rather than an elongated shape. Elongated inclusions, also called stringers, may act as planes of weakness along Which lamellar tearing and delamination fracture can occur. The avoidance of stringers is beneficial for forming processes of steel sheets which entail the expansion of holes or the stretching of flanges and promotes isotropic forming behaviour.
  • Calcium treatment also prevents the formation of hard, angular, abrasive alumina inclusions in aluminium deoxidised steel types, forming instead calcium aluminate inclusions which are softer and globular at rolling temperatures, thereby improving the material's processing characteristics.
  • some inclusions occurring in molten steel have a tendency to block the nozzle, resulting in lost output and increased costs.
  • Calcium treatment reduces the propensity for blockage by promoting the formation of low melting point species which will not clog the caster nozzles. It is also possible to add no calcium when the sulphur content is very low.
  • the amount of Ca is between 0.0005 and 0.003 mass %.
  • P 0.001-0.025 mass %.
  • Phosphorus interferes with the formation of carbides, and therefore some phosphorus in the steel is advantageous.
  • phosphorus can make steel brittle upon welding, so the amount of phosphorus should he carefully controlled during steelmaking, especially in combination with other embrittling elements such as sulphur and nitrogen.
  • embrittling elements such as sulphur and nitrogen.
  • boron it is possible to have more phosphorus in the steel then usual.
  • the content of Nitrogen is limited to max 0.015 wt % as is typical for continuous casting plants. Usually, the amount of N is between 0.001 and 0.010 wt %.
  • the ranges for aluminium, boron, silicon, chromium and manganese are chosen such that a correct balance is found to deliver a transformation that is as homogeneous as possible on the run-out table and during coil cooling, to ensure a steel strip that can be cold rolled, and to provide a starting structure enabling rapid dissolution of carbon in the annealing line to promote hardenability and correct ferritic/bainitic transformation behaviour.
  • aluminium accelerates and chromium decelerates the bainitic transformation the right balance between aluminium and chromium has to be present to produce the right quantity of bainite within the timescales permitted by a conventional hot dip galvanising line with a restricted overage section. In practice, this means that the content of aluminium should be higher than the content of chromium.
  • the amounts of Al and Si are chosen such that 0.60% ⁇ Al+Si ⁇ 1.40%
  • the amounts of Mn and Cr are chosen such that Mn+Cr>2.00%.
  • the amounts of Al and Si are chosen such that Si ⁇ Al.
  • Aluminium and silicon together should be maintained between 0.60 and 1.40 mass % to ensure suppression of carbides in the end product and stabilisation of a sufficient amount of austenite, with the correct composition, to provide a desirable extension of formability.
  • Manganese and chromium together should be above 2.00 mass % to ensure sufficient hardenability for formation of martensite and/or bainite and thus achievement of strength in a conventional continuous annealing line and hot dip galvanising line.
  • Mn aids to stabilise retained austenite.
  • Mn+Cr should be above 2.10 mass %, especially when the amount of Si is low.
  • Al should preferably be present in an amount equal to or higher then Si in view of a good zinc coatability.
  • element C is present in an amount of 0.13-0.18%. In this range the hardenability of the steel is optimal while the weldability of the steel is enhanced, also by the presence of boron. More preferably element C is present in an amount of 0.14-0.17%. This amount of C has been found to work well in practice.
  • element Si is present in an amount of 0.05-0.50%, more preferably 0.05-0.40%.
  • a amount of silicon lower then 0.50% improves the coatability of the steel strip, even more so when the amount of silicon is below 0.40%.
  • element Al is present in an amount of 0.30-1.20%, preferably an amount of 0.40-1.00%.
  • a raised lower level of aluminium has the same effect as a higher amount of silicon, but hardly increases the strength of the steel.
  • a lower upper limit of aluminium improves the castability of the steel.
  • the amount of element B is preferably between 0.0011 and 0.0040%, more preferably between 0.0013 and 0.0030%. to provide the desired hardenability and hence bring sufficient strength.
  • the amount of Ti is preferably max 0.10% so as to limit the cost of the steel and keep the dimensional window as large as possible. More preferably, the amount of Ti is between 0.005 and 0.05%.
  • the hot dip galvanised steel strip has an ultimate tensile strength Rill above 750 MPa and/or a 0.2% proof strength Rp of 430-700 MPa, preferably the difference between the middle and the edges of the steel strip being less then 75 MPa for both Rp and/or Rm, more preferably this difference being less then 60 MPa.
  • Rill ultimate tensile strength
  • Rp 0.2% proof strength
  • the hot dip galvanised steel strip has a microstructure, consisting of 20-50 volume % ferrite, 10-25 volume % retained austenite+martensite, of which 5-12% retained austenite, the remainder being tempered martensite, bainite and cementite.
  • a method for producing a high strength hot dip galvanised steel strip as defined above, wherein the cast steel is hot rolled to a thickness of 2.0-4.0 mm and coiled at a Coiling Temperature CT below Bs ⁇ 20° C. temperature and above Ms+60° C. temperature, the strip is cold rolled with a reduction of 40% or more, after which the strip is intercritically annealed at a temperature between Ac1 and Ac3 temperature, and the strip is averaged at a temperature below Bs temperature to form bainite and/or tempered martensite, after which the strip is hot dip galvanised.
  • the hot rolled coil has a microstructure consisting of 50-70 volume % ferrite, 20-50 volume % pearlite and/or bainite, and less then 10% cementite.
  • the coil has the right properties for further processing, especially for the annealing step, and can be cold rolled in a wide dimensional window.
  • the hot dip galvanised strip is tension rolled with a reduction of 0.2-0.8%. This percentage of tension rolling can provide the right mechanical properties to the strip, such as the tight strength level, while the other properties remain inside the desired window.
  • a method for producing a high strength hot dip galvanised complex phase steel strip wherein the cast steel is hot rolled to a thickness of 2.0-4.0 mm and coiled at a Coiling Temperature CT below Bs ⁇ 20° C. temperature and above Ms+60° C. temperature, the strip is cold rolled with a reduction of 40% or more, after which the strip is annealed at a temperature above Ad temperature plus 50° C., and the strip is overaged at a temperature below Bs temperature to form bainite and/or tempered martensite, after which the strip is hot dip galvanised.
  • This complex phase steel strip can be made due to the precise Coiling Temperature and the prescribed annealing and overaging temperatures.
  • this hot dip galvanised complex phase steel strip is tension rolled with a reduction of 0.4-2.0%, preferably with a reduction of 0.4-1.2%.
  • This percentage of tension rolling can provide the right mechanical properties to the strip, such as the right strength level, while the other properties remain inside the desired window.
  • FIG. 1 shows measurement of the ultimate tensile strength Rm and 0.2% proof strength Rp after annealing.
  • compositions of line trialled materials Unless indicated different, the compositions are defined in mill-wt %. Bs and Ms values were calculated from 1 . Al ⁇ Cast C Mn P Si Cr B ppm zo Ti N ppm Al + Si Mn + Cr Bs ⁇ 20° C. Ms +60° C.
  • the material was hot and subsequently cold rolled to a typical gauge in the range 0.8-2.0 mm.
  • microstructure and phase fractions defined is provided in FIG. 2 .
  • the microstructure over different sampling positions over the coil is provided in Table 2.
  • the microstructure is given for the head, middle and tail of a coil.
  • M indicates the middle of the strip, R the right hand side.
  • a Dual Phase steel strip was produced.
  • the hot roll finishing temperature was approximately 875° C. for all casts but for cast 4 , as indicated above.
  • the coiling temperature was between 500-520° C., well between Bs ⁇ 20° C. and Ms+60° C., Subsequently, the material was cold rolled and intercritically annealed at around 800° C., and the overage temperature was 400° C. After hot dip galvanising, the strip was temper rolled with a reduction of around 0.3%,
  • a Complex Phase steel strip was produced.
  • the hot roll finishing temperature was approximately 875° C.
  • the coiling temperature was 550° C.
  • the material was cold rolled and intercritically annealed at around 840° C., and the overage temperature was 400° C. After hot dip galvanising, the strip was temper rolled with a reduction of 1.0%.
  • FIG. 2 shows typical microstructures (Nital etched) obtained at the middle of the hot rolled strip product, after coiling and cooling down. Used is the composition of cast 1 .
  • the coiling temperature CT was 500° C.
  • the right-hand picture shows the same material but after a coiling temperature of 550° C.
  • the dark phase is perlite/bainite and the light phase is ferrite; black dots are cementite.
  • perlite/bainite is present in 25-35%, ferrite 60-70% and cementite less than 10%.
  • perlitelbainite is present in 20-30%, ferrite 65-75% and cementite less than 10%.
  • FIG. 3 shows the variation in Rm and Rp over the width of the strip.
  • FIG. 3 a shows this variation for a strip composition that is not according to the invention, having a composition of 0.15 C, 2.05 Mn, 0.2 Cr, 0.7 Al, 0.07 Si, 0.015 Nb and 0.004 N (in wt %).
  • the difference in Rrn between middle and edge of the strip is approximately 100 MPa, the difference in Rp is approximately 50 MPa.
  • FIG. 3 b shows the variation in Rm and Rp for a strip with the composition of cast 1 .
  • This figure shows that it is possible to get a variation between the middle and the edge of the strip that is less than 20 MPa for both Rm and Rp.
  • FIG. 3 c shows in fact the same for a strip with the composition of cast 3 .
  • the strip shown in FIGS. 3 b and 3 c has been manufactured in accordance with the method of the invention.
  • FIG. 4 shows three different ways of graphically indicating the microstructures of the casts after using the method of the invention. These are the well known Picral, Nital and LePera representations. In the Picral graphs black represents bainite or tempered martensite. In the Nital graph the white spots indicate ferrite. In contrast, in the LePera graph white indicates (tempered) martensite+retained austenite. The differences between DP800 on the left-hand side and CP800 on the right-hand side are clearly visible.
  • the length indications in FIGS. 2 and 4 all indicate a length of 10 ⁇ m.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Heat Treatment Of Sheet Steel (AREA)
  • Coating With Molten Metal (AREA)
US15/580,776 2015-07-01 2016-06-24 High strength hot dip galvanised steel strip Abandoned US20180230570A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP15020109 2015-07-01
EPEP15020109.3 2015-07-01
PCT/EP2016/064704 WO2017001303A1 (fr) 2015-07-01 2016-06-24 Bande d'acier galvanisé à chaud à haute résistance

Publications (1)

Publication Number Publication Date
US20180230570A1 true US20180230570A1 (en) 2018-08-16

Family

ID=53783025

Family Applications (1)

Application Number Title Priority Date Filing Date
US15/580,776 Abandoned US20180230570A1 (en) 2015-07-01 2016-06-24 High strength hot dip galvanised steel strip

Country Status (9)

Country Link
US (1) US20180230570A1 (fr)
JP (1) JP2018524471A (fr)
KR (1) KR20180025852A (fr)
CN (1) CN107787375A (fr)
BR (1) BR112017023814A2 (fr)
CA (1) CA2989710A1 (fr)
MX (1) MX2017016843A (fr)
WO (1) WO2017001303A1 (fr)
ZA (1) ZA201707294B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020245627A1 (fr) * 2019-06-03 2020-12-10 Arcelormittal Tôle d'acier laminée à froid et revêtue et son procédé de fabrication
US10927429B2 (en) 2015-12-15 2021-02-23 Tata Steel Ijmuiden B.V. High strength hot dip galvanised steel strip

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020058330A1 (fr) * 2018-09-19 2020-03-26 Sms Group Gmbh Acier avancé à haute limite d'élasticité, bande en acier composée de cet acier ainsi que procédé pour la fabrication d'une bande en acier
WO2020221628A1 (fr) * 2019-04-30 2020-11-05 Tata Steel Ijmuiden B.V. Procédé de production d'une bande laminée sur mesure à recuit discontinu
WO2020245626A1 (fr) * 2019-06-03 2020-12-10 Arcelormittal Tôle d'acier laminée à froid et revêtue et son procédé de fabrication
DE102020110319A1 (de) 2020-04-15 2021-10-21 Salzgitter Flachstahl Gmbh Verfahren zur Herstellung eines Stahlbandes mit einem Mehrphasengefüge und Stahlband hinzu
CN113355604B (zh) * 2021-06-25 2022-05-24 攀钢集团攀枝花钢铁研究院有限公司 低成本700MPa级热镀锌复相钢板及其制备方法
CN117802400A (zh) * 2022-09-23 2024-04-02 宝山钢铁股份有限公司 一种低点焊裂纹敏感性的带镀层超高强钢及其制造方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1867746A1 (fr) * 2005-03-31 2007-12-19 JFE Steel Corporation Tôle d'acier allié galvanisé à chaud et procédé servant à produire celle-ci
US20080175743A1 (en) * 2005-03-31 2008-07-24 Jfr Steel Corporation, A Corporation Of Japan Alloyed Hot-Dip Galvanized Steel Sheet and Method of Producing the Same
WO2013037485A1 (fr) * 2011-09-13 2013-03-21 Tata Steel Ijmuiden B.V. Acier en bandes galvanisé à chaud à haute résistance
US20180363082A1 (en) * 2015-12-15 2018-12-20 Tata Steel Ijmuiden B.V. High strength hot dip galvanised steel strip

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101151392A (zh) * 2005-03-31 2008-03-26 杰富意钢铁株式会社 合金化热镀锌钢板及其制造方法
EP2009128A1 (fr) * 2007-06-29 2008-12-31 ArcelorMittal France Acier au silicium galvanisé ou recuit après galvanisation
JP2013515167A (ja) * 2009-12-21 2013-05-02 タタ、スティール、アイモイデン、ベスローテン、フェンノートシャップ 高強度溶融亜鉛めっき鋼帯
WO2011126064A1 (fr) * 2010-03-31 2011-10-13 新日本製鐵株式会社 Tôle en acier galvanisé au trempé à haute résistance présentant une excellente aptitude au formage et procédé de fabrication de cette dernière
CN105247089B (zh) * 2013-03-11 2018-07-20 塔塔钢铁艾默伊登有限责任公司 高强度热浸镀锌复相钢带材

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1867746A1 (fr) * 2005-03-31 2007-12-19 JFE Steel Corporation Tôle d'acier allié galvanisé à chaud et procédé servant à produire celle-ci
US20080175743A1 (en) * 2005-03-31 2008-07-24 Jfr Steel Corporation, A Corporation Of Japan Alloyed Hot-Dip Galvanized Steel Sheet and Method of Producing the Same
WO2013037485A1 (fr) * 2011-09-13 2013-03-21 Tata Steel Ijmuiden B.V. Acier en bandes galvanisé à chaud à haute résistance
US20180363082A1 (en) * 2015-12-15 2018-12-20 Tata Steel Ijmuiden B.V. High strength hot dip galvanised steel strip

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10927429B2 (en) 2015-12-15 2021-02-23 Tata Steel Ijmuiden B.V. High strength hot dip galvanised steel strip
WO2020245627A1 (fr) * 2019-06-03 2020-12-10 Arcelormittal Tôle d'acier laminée à froid et revêtue et son procédé de fabrication

Also Published As

Publication number Publication date
CA2989710A1 (fr) 2017-01-05
JP2018524471A (ja) 2018-08-30
ZA201707294B (en) 2019-02-27
MX2017016843A (es) 2018-04-24
KR20180025852A (ko) 2018-03-09
WO2017001303A1 (fr) 2017-01-05
CN107787375A (zh) 2018-03-09
BR112017023814A2 (pt) 2018-07-31

Similar Documents

Publication Publication Date Title
US20180230570A1 (en) High strength hot dip galvanised steel strip
EP2971209B1 (fr) Bande dýacier à phase complexe galvanisé à chaud haute résistance
US20170051378A1 (en) High-strength cold rolled steel sheet having excellent ductility, hot-dip galvanized steel sheet and method for manufacturing same
EP2768989B1 (fr) Acier en bandes galvanisé à chaud à haute résistance
WO2017002883A1 (fr) Tôle d'acier laminée à froid de haute résistance, tôle d'acier galvanisée de haute résistance et tôle d'acier recuite après galvanisation de haute résistance
US20120018058A1 (en) Process for manufacturing a cold rolled trip steel product
KR101850122B1 (ko) 복합조직강, 복합조직강으로 제조된 냉연 평판 제품 및 제조 방법
KR20130099138A (ko) 복합조직강, 복합조직강으로 제조된 냉연 평판 제품 및 제조 방법
WO2020065422A1 (fr) Tôle d'acier laminée à chaud et son procédé de fabrication
CN110050083B (zh) 低温域冲缘加工性优异的高强度钢板及其制造方法
JP7464887B2 (ja) 鋼板およびその製造方法
JP6543732B2 (ja) 曲げ加工性に優れた超高強度熱延鋼板及びその製造方法
JP2007063604A (ja) 伸びと穴拡げ性に優れた溶融亜鉛めっき高強度鋼板およびその製造方法
KR20150075306A (ko) 굽힘 가공성이 우수한 초고강도 열연강판 및 그 제조 방법
EP3390040B2 (fr) Bande d'acier galvanisé à chaud haute résistance
CN113692456B (zh) 剪切加工性优异的超高强度钢板及其制造方法
CN114641587A (zh) 耐久性优异的厚复合组织钢及其制造方法
JP2007119842A (ja) 伸びフランジ成形性に優れた高強度溶融亜鉛めっき鋼板の製造方法
JP6684905B2 (ja) 剪断加工性に優れた高強度冷延鋼板及びその製造方法
EP3317431B1 (fr) Bande d'acier galvanisé à chaud haute résistance
JP6541504B2 (ja) 製造安定性に優れた高強度高延性鋼板、及びその製造方法、並びに高強度高延性鋼板の製造に用いられる冷延原板
KR100978734B1 (ko) 복합조직강판 및 이를 제조하는 방법
JP2016194136A (ja) 製造安定性に優れた高強度高延性鋼板、及びその製造方法、並びに高強度高延性鋼板の製造に用いられる冷延原板
US20230026116A1 (en) Steel sheet for a structure with excellent seawater corrosion resistance and method of manufacturing same
CN114846167A (zh) 加工性优异的高强度钢板及其制造方法

Legal Events

Date Code Title Description
AS Assignment

Owner name: TATA STEEL IJMUIDEN B.V., NETHERLANDS

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:VAN KREVEL, JOOST WILLEM HENDRIK;IONESCU, CORNELIA;ENNIS, BERNARD LEO;SIGNING DATES FROM 20171113 TO 20171123;REEL/FRAME:044337/0246

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

Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION

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

Free format text: NON FINAL ACTION MAILED

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

Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER

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

Free format text: FINAL REJECTION MAILED

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

Free format text: ADVISORY ACTION MAILED

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION