WO2019106895A1 - 高強度亜鉛めっき鋼板およびその製造方法 - Google Patents
高強度亜鉛めっき鋼板およびその製造方法 Download PDFInfo
- Publication number
- WO2019106895A1 WO2019106895A1 PCT/JP2018/030693 JP2018030693W WO2019106895A1 WO 2019106895 A1 WO2019106895 A1 WO 2019106895A1 JP 2018030693 W JP2018030693 W JP 2018030693W WO 2019106895 A1 WO2019106895 A1 WO 2019106895A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- less
- steel sheet
- plating
- temperature
- steel
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- 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
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0242—Flattening; Dressing; Flexing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying 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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
- C21D9/54—Furnaces for treating strips or wire
- C21D9/56—Continuous furnaces for strip or wire
- C21D9/561—Continuous furnaces for strip or wire with a controlled atmosphere or vacuum
-
- 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
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
- C21D9/54—Furnaces for treating strips or wire
- C21D9/56—Continuous furnaces for strip or wire
- C21D9/562—Details
-
- 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
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
- C21D9/54—Furnaces for treating strips or wire
- C21D9/56—Continuous furnaces for strip or wire
- C21D9/573—Continuous furnaces for strip or wire with cooling
-
- 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
- C21D9/52—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for wires; for strips ; for rods of unlimited length
- C21D9/54—Furnaces for treating strips or wire
- C21D9/56—Continuous furnaces for strip or wire
- C21D9/573—Continuous furnaces for strip or wire with cooling
- C21D9/5735—Details
-
- 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
- C22C18/02—Alloys based on zinc with copper 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
- C22C38/008—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
- C22C38/06—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
- C22C38/08—Ferrous alloys, e.g. steel alloys containing nickel
-
- 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
- C22C38/16—Ferrous alloys, e.g. steel alloys containing 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
-
- 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
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—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
- C22C38/38—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
-
- 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
- C22C38/60—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
- C23C2/0224—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
-
- 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
- C23C2/04—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
- C23C2/12—Aluminium 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
-
- 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
- C23C2/261—After-treatment in a gas atmosphere, e.g. inert 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
- C23C2/26—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
-
- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
-
- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
- C23C30/005—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process on hard metal substrates
-
- 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
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12785—Group IIB metal-base component
- Y10T428/12792—Zn-base component
- Y10T428/12799—Next to Fe-base component [e.g., galvanized]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12958—Next to Fe-base component
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12951—Fe-base component
- Y10T428/12972—Containing 0.01-1.7% carbon [i.e., steel]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
- Y10T428/24967—Absolute thicknesses specified
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/26—Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension
- Y10T428/263—Coating layer not in excess of 5 mils thick or equivalent
- Y10T428/264—Up to 3 mils
- Y10T428/265—1 mil or less
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/27—Web or sheet containing structurally defined element or component, the element or component having a specified weight per unit area [e.g., gms/sq cm, lbs/sq ft, etc.]
Definitions
- the present invention relates to a high strength galvanized steel sheet which is excellent in resistance to hydrogen embrittlement which tends to be a problem as the strength increases and which is suitable for a construction material and a collision resistant part of a car, and a method of manufacturing the same.
- Patent Documents 1 to 4 are documents relating to characteristics such as high strength.
- Patent Document 1 discloses a hot-dip galvanized steel sheet excellent in workability and having a high yield ratio and high strength, and a method of manufacturing the same.
- Patent Document 2 discloses a method of providing a steel plate having a tensile strength of 980 MPa or more, exhibiting a high yield ratio, and being excellent in workability (specifically, strength-ductility balance).
- Patent Document 3 discloses high-strength hot-dip galvanized steel excellent in plating appearance, corrosion resistance, resistance to peeling during plating, resistance to peeling during high processing, and workability during high processing using a high strength steel plate containing Si and Mn as a base material. Disclosed is a plated steel plate and a method of manufacturing the same.
- Patent Document 4 discloses a method of manufacturing a high strength plated steel sheet having excellent delayed fracture resistance.
- Patent Documents 5 and 6 are documents relating to this hydrogen embrittlement.
- Patent Document 5 discloses a plated steel sheet for hot press excellent in delayed fracture resistance and a method of manufacturing the same.
- the precipitates in steel are utilized, and the penetration of diffusible hydrogen is suppressed as much as possible depending on the manufacturing process conditions before plating, and hydrogen in steel after plating is trapped as non-diffusible hydrogen.
- Patent Document 6 discloses a high-strength steel plate excellent in welded portion hydrogen embrittlement of a steel plate having a base material strength (TS) of about 870 MPa and a method of manufacturing the same.
- TS base material strength
- Patent Document 6 the hydrogen embrittlement is improved by dispersing the oxide in the steel.
- Patent Document 1 since the steel structure is a composite structure containing ferrite and martensite, the high yield ratio is only about 0.70 although the yield ratio is high. Moreover, in patent document 1, since Si and Mn are contained abundantly, plating quality is inadequate. Furthermore, the resistance to hydrogen embrittlement has not been positively improved.
- Patent Document 3 in the annealing step before plating, the hydrogen concentration in the furnace atmosphere is limited to 20 vol% or more, and the annealing temperature is limited to 600 to 700 ° C. Due to the metallographic structure, it is difficult to apply to materials having an Ac3 point exceeding 800 ° C. Furthermore, when the hydrogen concentration in the atmosphere in the annealing furnace is high, the hydrogen concentration in the steel increases, and it can not be said that the hydrogen embrittlement resistance is sufficient.
- Patent Document 4 although the delayed fracture resistance after processing is improved, the hydrogen concentration during annealing is also high, hydrogen remains in the base material itself, and the hydrogen embrittlement resistance is inferior.
- Patent Document 5 when a large amount of precipitates on the order of several microns is present, the mechanical properties of the material itself are degraded.
- Patent Document 6 since the upper limit of the in-furnace hydrogen concentration of the continuous plating line is 60%, a large amount of hydrogen is taken into the steel when annealing to a high temperature of A c3 or more. Therefore, the method of Patent Document 6 can not produce an ultra-high strength steel plate excellent in hydrogen embrittlement resistance of TS ⁇ 1100 MPa.
- the present invention is an ultra-high-strength plated steel sheet that is concerned about hydrogen embrittlement, and is excellent in the appearance of plating and the resistance to hydrogen embrittlement of the material together with a material that achieves high yield strength with high demand.
- An object of the present invention is to provide a high strength galvanized steel sheet having a suitable high yield strength and a method of manufacturing the same.
- the inventors of the present invention have studied the relationship between tensile strength (TS) and yield strength (YS) for various steel plates, and resistance spot weld nugget as plating property and hydrogen embrittlement resistance. We examined the coexistence of overcoming of the crack of the crack. As a result, in addition to the component composition of the steel sheet, the above problems have been solved by appropriately adjusting the manufacturing conditions to form an optimal steel structure and controlling the amount of hydrogen in the steel. Specifically, the present invention provides the following.
- the steel composition is mass%, C: 0.10% or more and 0.30% or less, Si: less than 1.2%, Mn: 2.0% or more and 3.5% or less, P: 0.010% 70% or less of S: 0.002% or less, Al: 1% or less, N: 0.006% or less, and the balance of the component composition consisting of Fe and unavoidable impurities, and the area ratio % Or more (including 100%), less than 20% of ferrite (including 0%), and steel structure containing less than 5% (including 0%) of retained austenite, and the amount of diffusible hydrogen in the steel 0.20 mass ppm or less of a steel plate, and a galvanized layer having an Fe content of 8 to 15% by mass on a surface of the steel plate and a plating adhesion amount per one surface of 20 to 120 g / m 2 , the provided, Mn oxide content contained in the galvanized layer is 0.050 g / m 2 or more , And the tensile strength of more than 1
- the component composition may further contain, in mass%, one or more of Ti, Nb, V, and Zr in total of 0.005 to 0.1%, and one or more of Mo, Cr, Cu, and Ni.
- the component composition further contains, in mass%, one or two selected from Sb: 0.001 to 0.1% and Sn: 0.001 to 0.1% [1] or The high strength galvanized steel sheet according to [2].
- % And dew point Dp 50 ° C. or less, at a temperature T (° C.) of 200 ° C. or more and 350 ° C. or less, for a time t (hr) or more that satisfies the equation (1) at 0.005 (hr) or more A post heat treatment step, and a method of manufacturing a high strength galvanized steel sheet.
- the width trim is performed before the post heat treatment step, and the residence time t (hr) of staying at a temperature T (° C.) of 200 ° C. or more and 350 ° C. or less in the post heat treatment step is 0.005 (hr)
- T temperature
- t residence time
- the tensile strength is high at 1100 MPa or higher, preferably 1150 MPa or higher, and the yield ratio (yield strength ratio) is 0.85 or higher, and excellent in surface properties (platability and surface appearance)
- yield strength ratio yield strength ratio
- a high strength galvanized steel sheet excellent in hydrogen embrittlement can be obtained.
- the high-strength galvanized steel sheet of the present invention comprises a steel sheet and a galvanized layer formed on the surface of the steel sheet. Below, it demonstrates in order of a steel plate and a zinc plating layer.
- composition of the steel plate is as follows. In the following description, “%” which is a unit of content of a component means “mass%”.
- C 0.10% to 0.30% (C: 0.10 to 0.30%)
- C is an element effective for increasing the strength of the steel plate, and contributes to the increase in strength by forming martensite, which is one of the hard phases of the steel structure.
- the C content needs to be 0.10% or more. Preferably it is 0.11% or more, More preferably, it is 0.12% or more.
- the C content exceeds 0.30%, in the present invention, the spot weldability is significantly deteriorated, and at the same time, the steel sheet becomes hard due to the increase in the strength of martensite, and the formability such as ductility tends to decrease. Therefore, the C content is 0.30% or less. From the viewpoint of property improvement, the content is preferably 0.28% or less, more preferably 0.25% or less.
- Si less than 1.2% Si is an element that contributes to high strength mainly by solid solution strengthening, and the decrease in ductility relative to the increase in strength is relatively small, and it contributes not only to strength but also to the balance improvement between strength and ductility Do.
- Si easily forms a Si-based oxide on the surface of the steel sheet, which may cause non-plating, stabilizes austenite at the time of annealing, and facilitates formation of retained austenite in the final product. Therefore, it is sufficient to add only the amount necessary for securing the strength, and from that viewpoint, the Si content is desirably 0.01% or more. More preferably, it is 0.02% or more. More preferably, it is 0.05% or more.
- the upper limit is made less than 1.2% from the viewpoint of plating property and retained austenite formation. Preferably it is 1.0% or less. More preferably, it is 0.9% or less.
- Mn 2.0% or more and 3.5% or less Mn is effective as an element contributing to high strength by solid solution strengthening and martensite formation. In order to acquire this effect, it is necessary to make Mn content 2.0% or more. Preferably it is 2.1% or more, more preferably 2.2% or more. On the other hand, if the Mn content exceeds 3.5%, spot weld cracking occurs, and the steel structure is likely to be uneven due to segregation of Mn and the workability is reduced. If the Mn content exceeds 3.5%, Mn is likely to be concentrated as an oxide or a composite oxide on the surface of the steel sheet, which may cause non-plating. Therefore, the Mn content is set to 3.5% or less. Preferably it is 3.3% or less, more preferably 3.0% or less.
- P 0.010% or less
- P is an effective element that contributes to the strengthening of the steel sheet by solid solution strengthening.
- the content exceeds 0.010%, workability such as weldability and stretch flangeability is reduced. Therefore, the P content is made 0.010% or less.
- it is 0.008% or less, more preferably 0.007% or less.
- the lower limit is not particularly specified, but if it is less than 0.001%, the production efficiency and the dephosphorization cost increase in the production process, so it is preferably 0.001% or more.
- S 0.002% or less
- S is a harmful element which causes hot embrittlement, causes a decrease in weldability, or is present as a sulfide-based inclusion in a steel to reduce the workability of a steel sheet. is there. For this reason, it is preferable to reduce the S content as much as possible. Therefore, the S content is made 0.002% or less.
- the lower limit is not particularly specified, but if it is less than 0.0001%, production efficiency and cost increase in the current manufacturing process are caused, and therefore, it is preferable to be 0.0001% or more.
- Al 1% or less Al is added as a deoxidizer.
- the content is preferably 0.01% or more from the viewpoint of obtaining the effect. More preferably, it is 0.02% or more.
- the Al content exceeds 1%, the raw material cost will rise, and it will also cause surface defects of the steel sheet, so 1% is made the upper limit.
- it is 0.4% or less, more preferably 0.1% or less.
- the N content is set to 0.006% or less, preferably 0.005% or less, and more preferably 0.004% or less.
- the content is preferably as small as possible from the viewpoint of ductility improvement by cleaning of the ferrite, but in order to lower the production efficiency and increase the cost in the manufacturing process, the preferable lower limit is made 0.0001% or more. More preferably, it is 0.0010% or more, further preferably 0.0015% or more.
- the component composition of the above-described steel sheet may contain, as optional components, one or more of Ti, Nb, V, and Zr in total of 0.005 to 0.1% and / or one or more of Mo, Cr, Cu, and Ni. A total of 0.005 to 0.5% and / or B: 0.0003 to 0.005% may be contained.
- Ti, Nb, V, and Zr form carbides and nitrides (which may be carbonitrides) with C and N, and contribute to high strengthening of the steel sheet, particularly to high YR by forming fine precipitates.
- these elements are also effective for trap sites (detoxification) of hydrogen in steel.
- an excessive content exceeding 0.1% in total increases the deformation resistance at the time of cold rolling to inhibit the productivity, and the presence of excessive or coarse precipitates reduces the ductility of the ferrite, and Decreases the formability such as ductility, bendability and stretch flangeability. Then, it is preferable to make the said total into 0.1% or less. More preferably, it is 0.08% or less, more preferably 0.06% or less.
- Mo, Cr, Cu, Ni, and B are elements that contribute to high strength in order to enhance the hardenability and facilitate the formation of martensite. Then, it is preferable to make one or more types in Mo, Cr, Cu, and Ni into 0.005% or more in total. More preferably, it is 0.01% or more, further preferably 0.05% or more. Moreover, in the case of B, 0.0003% or more is preferable, More preferably, it is 0.0005% or more, More preferably, it is 0.0010% or more. In addition, with Mo, Cr, Cu, and Ni, excessive addition exceeding 0.5% in total leads to saturation of effects and cost increase.
- the upper limit is made into 0.5%. Since Ni has the effect of suppressing the generation of surface defects due to the Cu content, it is desirable to include Ni when it is contained. In particular, it is preferable to contain Ni at a half or more of the Cu content. Also for B, the above lower limit is provided to obtain the effect of suppressing the formation of ferrite that occurs in the annealing and cooling process. In addition, when the B content exceeds 0.005%, the effect is saturated. Excess hardenability also has disadvantages such as weld cracking during welding.
- the component composition of the above steel sheet may contain, as optional components, Sb: 0.001 to 0.1% and / or Sn: 0.001 to 0.1%.
- Sb and Sn are elements effective for suppressing the reduction in strength of the steel sheet by suppressing decarburization, denitrification, deasphalting and the like. Moreover, since it is effective also to spot weld cracking suppression, the Sn content and the Sb content are each preferably 0.001% or more. More preferably, it is 0.003% or more, still more preferably 0.005% or more. However, in both Sn and Sb, the excess content exceeding 0.1% reduces the workability such as the stretch flangeability of the steel sheet. Therefore, the Sn content and the Sb content are both preferably 0.1% or less. More preferably, it is 0.030% or less, still more preferably 0.010% or less.
- the component composition of the above-described steel sheet may contain Ca: 0.0010% or less as an optional component.
- the Ca content is preferably 0.0010% or less. More preferably, it is 0.0005% or less, more preferably 0.0003% or less. Further, the lower limit is not particularly limited, but it may be difficult in some cases not to contain Ca at all in production, so in consideration of it, the Ca content is preferably 0.00001% or more. More preferably, it is 0.00005% or more.
- the balance other than the above is Fe and unavoidable impurities.
- the optional component is an unavoidable impurity because the effect of the present invention is not impaired.
- Steel structure is area ratio, 70% or more (including 100%) of bainite and martensite (including tempered martensite), less than 20% (including 0%) of ferrite, and less than 5% of retained austenite Including 0%).
- the area ratio of less than 20% is acceptable for obtaining the yield strength of the present invention. Preferably it is 15% or less, more preferably 10% or less.
- the lower limit is not particularly limited, but is preferably 1% or more, more preferably 2% or more, and still more preferably 3% or more.
- generated at comparatively high temperature here is regarded as a ferrite, without distinguishing with a ferrite by observation by the scanning electron microscope as described in the below-mentioned Example.
- tempered martensite and bainite are hard phases, and the area ratio of these hard phases is important in the present invention because high tensile strength and yield strength are obtained. Martensite is particularly hard and is effective for enhancing the steel plate strength. Tempered martensite and bainite (as mentioned above, bainite without carbides is regarded as ferrite, so bainite as used herein means bainite containing carbides) is a structure that is particularly important for obtaining high yield strength is there. From the above, the total of these hard phases is made 70% or more in area ratio. Preferably it is 80% or more, More preferably, it is 85% or more, More preferably, it is 90% or more. The upper limit is preferably 100% or less, preferably 99% or less, and more preferably 98% or less.
- the bainite in these hard phases is preferably 20% or more and 50% or less. Moreover, 49% or less is preferable with respect to the whole structure
- Retained austenite less than 5% (including 0%) Austenite (fcc phase) has higher hydrogen storage capacity than ferrite (bcc phase). Therefore, when this retained austenite is transformed to martensite by stress induction such as processing, there is a concern that diffusible hydrogen in the steel may be increased. Therefore, make it less than 5%. More preferably, it is 4% or less, more preferably 3% or less. Although the lower limit is not particularly limited, it is preferably 0% or more, more preferably 1% or more.
- the steel structure may contain precipitates such as pearlite and carbide in the remaining portion as a structure other than the above-described structure.
- the area ratio of these other structures is preferably 10% or less, more preferably 5% or less.
- the area ratio in the above steel structure adopts the result obtained by the method described in the examples.
- a more specific method of measuring the area ratio is described in the examples, but briefly as follows.
- the above area ratio is represented by the structure in the area of 1 ⁇ 4 thickness position (1/8 to 3 ⁇ 8) of the plate thickness from the surface, and after polishing the L cross section (plate thickness cross section parallel to the rolling direction) of the steel plate It corrodes with a liquid, and three or more fields of view are observed by SEM with a magnification of 1500 times, and an image photographed and analyzed is determined.
- the said steel plate is 0.20 mass ppm (mass.ppm) or less of the amount of diffusible hydrogen in steel obtained by measuring by the method as described in an Example. Diffusive hydrogen in steel degrades hydrogen embrittlement resistance. If the amount of diffusible hydrogen in the steel exceeds 0.20 mass ppm and becomes excessive, for example, cracking of the weld nugget tends to occur during welding. In the present invention, it was revealed that the improvement effect is obtained by setting the amount of diffusible hydrogen in the steel which is the base material to 0.20 mass ppm or less before welding. Preferably it is 0.15 mass ppm or less, More preferably, it is 0.10 mass ppm or less, More preferably, it is 0.08 mass ppm or less.
- the lower limit is not particularly limited, but is preferably as small as possible, so the lower limit is 0 mass ppm. It is necessary to reduce the amount of diffusible hydrogen of the base material to 0.20 mass ppm or less before welding, and in the product after welding, if the amount of diffusible hydrogen of the base material portion is 0.20 mass ppm or less It can be considered that it was 0.20 mass ppm or less before welding.
- the zinc plating layer contains 20 to 120 g / m 2 of plating per one side and 8 to 15% by mass of Fe.
- the adhesion amount is less than 20 g / m 2 , it will be difficult to ensure corrosion resistance. Therefore, the adhesion amount is 20 g / m 2 or more, preferably 25 g / m 2 or more, and more preferably 30 g / m 2 or more. On the other hand, if it exceeds 120 g / m 2 , the plating peeling resistance deteriorates. Therefore, the adhesion amount is 120 g / m 2 or less, preferably 100 g / m 2 or less, more preferably 80 g / m 2 or less.
- the Mn oxide formed in the heat treatment step before plating reacts with the plating bath and the steel plate to form an FeAl or FeZn alloy phase, which is taken into the plating, and has a plating property, Plating resistance is improved.
- the amount of Mn oxide contained in the galvanized layer is more than 0.050 g / m 2 , the formation reaction of the FeAl or FeZn alloy phase becomes insufficient, resulting in the occurrence of non-plating and a decrease in the peel resistance to plating.
- the amount of Mn oxide in the plating layer is set to 0.050 g / m 2 or less.
- the amount of Mn oxide in the plating layer is preferably 0.005 g / m 2 or more and 0.050 g / m 2 or less.
- the measurement of the amount of Mn oxides in a zinc plating layer is performed by the method as described in an Example.
- the galvanized layer contains 8 to 15% by mass of Fe.
- the Fe content in the zinc plating layer is 8% or more by mass%, it can be said that the Fe—Zn alloy layer is sufficiently obtained.
- it is 9% or more, more preferably 10% or more.
- the Fe content is 15% or less.
- it is 14% or less, More preferably, it is 13% or less.
- components other than Fe, Zn of remainder, and unavoidable impurities contained in a zinc plating layer are not specifically limited.
- the zinc plating layer contains, for example, 0.001% to 1.0% of Al by mass%, and Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, One or two or more selected from Ti, Be, Bi and REM may be contained in a total of 0 to 30%.
- the zinc plating layer which has Fe content in the said range is an alloying galvanization layer.
- the method for producing a high strength galvanized steel sheet according to the present invention includes an annealing step, a plating step, and a post heat treatment step.
- a cold rolled material having the above-mentioned component composition is contained in an annealing furnace atmosphere having a hydrogen concentration H of 1 vol% or more and 13 vol% or less, and the temperature T in the annealing furnace: (A c 3 point ⁇ 20 ° C.) After heating (soaking) to a temperature of 5 s (seconds) or more, it is cooled and retained in a temperature range of 400 to 550 ° C. for 10 s or more.
- the cold rolled material used in the manufacturing method of the present invention is manufactured from a steel material.
- the steel material is manufactured by a continuous casting method generally called a slab (slab).
- the purpose of adopting the continuous casting method is to prevent macro segregation of alloy components.
- the steel material may be manufactured by an ingot method, a thin slab casting method, or the like.
- the steel slab is manufactured, it is cooled to room temperature and then reheated, and then it is hot-rolled by charging it into a heating furnace as it is, without cooling to around room temperature.
- Either a method of hot rolling immediately after performing a slight supplementary heat, or a method of hot rolling while maintaining a high temperature state after casting may be used.
- the conditions of the hot rolling are not particularly limited, but the steel material having the above-mentioned component composition is heated at a temperature of 1100 ° C. or more and 1350 ° C. or less, subjected to hot rolling with a finish rolling temperature of 800 ° C. or more and 950 ° C. or less.
- the condition of winding at a temperature of not less than ° C and not more than 700 ° C is preferable.
- these preferable conditions are demonstrated.
- the heating temperature of the steel slab is preferably in the range of 1100 ° C. or more and 1350 ° C. or less. If the temperature is out of the upper limit temperature range, the precipitates present in the steel slab are easily coarsened, and for example, it may be disadvantageous when securing strength by precipitation strengthening. In addition, coarse precipitates may act as nuclei in the subsequent heat treatment to adversely affect the structure formation. On the other hand, it is useful to reduce cracks and irregularities on the surface of the steel sheet by scaling off bubbles and defects on the surface of the slab by appropriate heating to achieve a smooth steel surface. In order to acquire such an effect, it is preferable to set it as 1100 degreeC or more.
- the heated steel slab is subjected to hot rolling including rough rolling and finish rolling.
- a steel slab becomes a sheet bar by rough rolling, and becomes a hot-rolled coil by finish rolling.
- hot rolling conditions the following are preferable.
- Finish rolling temperature 800 ° C. or more and 950 ° C. or less is preferable.
- the finish rolling temperature 800 ° C. or more
- the structure obtained by the hot-rolled coil tends to be uniform. Being able to make the tissue uniform at this stage contributes to the uniformity of the final product's tissue. If the structure is non-uniform, workability such as ductility, bendability, stretch flangeability and the like is reduced.
- the temperature exceeds 950 ° C. the amount of oxide (scale) formation increases, the interface between the base iron and the oxide becomes rough, and the surface quality after pickling and cold rolling may deteriorate.
- the formability of the steel plate similar to the steel slab such as strength, bendability and stretch flangeability, may be reduced.
- cooling is started within 3 seconds after finishing rolling to finish the refining and homogenization of the structure, and the temperature range from [finish rolling temperature] to [finish rolling temperature -100] ° C. It is preferable to cool at an average cooling rate of 10 to 250 ° C./s.
- the winding temperature is preferably 450 to 700.degree. If the temperature immediately before coil winding after hot rolling, that is, the coiling temperature is 450 ° C. or higher, it is preferable from the viewpoint of fine precipitation of carbides when Nb or the like is added, if the coiling temperature is 700 ° C. or lower It is preferable because cementite precipitates do not become too coarse. Also, if the temperature range is less than 450 ° C. or more than 700 ° C., the structure is likely to change during holding after being wound into a coil, and rolling due to non-uniformity of the metal structure of the material in cold rolling in the post process It is easy for troubles to occur. A more preferable winding temperature is 500 ° C. or more and 680 ° C. or less from the viewpoint of granulation of the hot-rolled sheet structure.
- a cold rolling process is performed. Usually, after removing the scale by pickling, cold rolling is applied to form a cold rolled coil. This pickling is performed as needed.
- the cold rolling is preferably performed at a rolling reduction of 20% or more. This is to obtain a uniform and fine microstructure in the subsequent heating. If the amount is less than 20%, coarse particles may be easily formed during heating, or an uneven structure may be easily formed, and as described above, there is a concern that the strength and processability of the final product plate after heat treatment may be reduced. Deteriorate the surface properties.
- the upper limit of the rolling reduction is not particularly defined, but because of the high strength steel plate, the high rolling reduction may result in poor shape in addition to the reduction in productivity due to the rolling load.
- the rolling reduction is preferably 90% or less.
- the above is the method for producing a cold rolled material.
- the annealing step the cold rolled material, the hydrogen concentration H: at 1 vol% or more 13 vol% or less of the annealing furnace atmosphere, the annealing furnace temperature T: (A c3 point -20 °C) ⁇ 900 °C 5 seconds or more at a temperature After heating, it is cooled and retained in a temperature range of 400 to 550 ° C. for 10 seconds or more.
- Annealing furnace temperature T (A c3 point ⁇ 20 ° C.) to the temperature range of 900 ° C. or less
- the average heating rate is not particularly limited, but the average heating rate is less than 10 ° C./s because of uniform structure. Is preferred. Further, from the viewpoint of suppressing a decrease in production efficiency, the average heating rate is preferably 1 ° C./s or more.
- the heating temperature (temperature in the annealing furnace) T is set to (Ac 3 point ⁇ 20 ° C.) to 900 ° C. in order to secure both the material and the plating property.
- the heating temperature is less than (A c3 point ⁇ 20 ° C.)
- the ferrite fraction becomes high, so that the strength can not be obtained or the formation of bainite becomes difficult.
- the heating temperature exceeds 900 ° C., the crystal grains are coarsened to deteriorate workability such as bendability and stretch flangeability, which is not preferable.
- Mn and Si are easily concentrated on the surface to inhibit the plating property.
- the heating temperature exceeds the Ac3 point and exceeds 900 ° C., the load on the facility is high, and there is a possibility that the production can not be stably performed.
- heating is performed for 5 seconds or more at a temperature T in an annealing furnace: (A c 3 point ⁇ 20 ° C.) to 900 ° C. 180 seconds or less is preferable in order to prevent excessive austenite grain size coarsening. Further, the heating time is set to 5 seconds or more from the viewpoint of homogenization of the tissue.
- the hydrogen concentration H in the temperature range from (A c3 point ⁇ 20 ° C.) to 900 ° C. is 1 to 13 vol%.
- the plating property is secured, and at the same time, excessive hydrogen penetration into the steel is prevented. If the hydrogen concentration is less than 1 vol%, non-plating occurs frequently.
- the hydrogen concentration exceeds 13 vol%, the effect on the plateability is saturated, and at the same time, the penetration of hydrogen into the steel is remarkably increased, and the hydrogen embrittlement resistance of the final product is deteriorated.
- the hydrogen concentration does not have to be in the range of 1 vol% or more except for the temperature range of (A c3 point ⁇ 20 ° C.) to 900 ° C.
- bainite is an important structure to obtain high YS. In order to produce this and to make the bainite area ratio 20% or more of the hard phase, it is necessary to stay for 10 s or more in this temperature range. Residence below 400 ° C. tends to fall below the temperature of the subsequent plating bath, which is not preferable because it degrades the quality of the plating bath. In that case, the plate temperature may be heated to the plating bath, so the lower limit of the above temperature range is set to 400.degree.
- the cooling stop temperature may be 400 to 550 ° C. as described above, but it is also possible to once cool to a temperature lower than this and to make it stay in a temperature range of 400 to 550 ° C. by reheating. In this case, when the temperature is cooled to the Ms point or lower, tempering may be performed after martensite is generated.
- the steel sheet after the annealing step is subjected to plating treatment, alloying treatment, and cooling to 100 ° C. or less at an average cooling rate of 3 ° C./s or more.
- the plating adhesion amount per one surface is made to be 20 to 120 g / m 2 .
- the Fe content is 8 to 15% by mass.
- the galvanized layer in which the Fe content is in the above range is an alloyed galvanized layer.
- Al 0.001% to 1.0% is contained.
- the zinc plating layer contains a predetermined amount of Mn oxide, it contains Mn. Containing 0 to 30% in total of one or more selected from Pb, Sb, Si, Sn, Mg, Mn, Ni, Cr, Co, Ca, Cu, Li, Ti, Be, Bi and REM It is also good. The remainder is Zn and unavoidable impurities.
- the method of plating treatment is preferably hot-dip galvanizing treatment.
- the conditions may be set as appropriate.
- the alloying process heated after hot dip galvanization is performed. For example, a process of holding in a temperature range of 480 to 600 ° C. for about 1 to 60 seconds can be exemplified. By this treatment, an alloyed zinc plated layer having an Fe content of 8 to 15% is obtained.
- the alloy After the above alloying treatment, the alloy is cooled to 100 ° C. or less at an average cooling rate of 3 ° C./s or more. This is to obtain martensite which is essential for high strength. If it is less than 3 ° C./s, it is difficult to obtain martensite necessary for strength, and if cooling is stopped at a temperature higher than 100 ° C., martensite is excessively tempered (self-tempered) at this point, austenite It is because it does not become martensite and transforms to ferrite, making it difficult to obtain the required strength.
- a post heat treatment step is performed after the plating step.
- the plated steel sheet after the plating step was treated with a hydrogen concentration of H: 10 vol. % And dew point Dp: 50 ° C. or less, at a temperature T (° C.) of 200 ° C. or more and 350 ° C. or less, for a time t (hr) or more that satisfies the equation (1) at 0.005 (hr) or more Process.
- a post heat treatment step is performed to obtain high yield strength and to reduce the amount of diffusible hydrogen in the steel.
- Hydrogen concentration H 10 vol.
- the hydrogen concentration H is preferably as low as 5 vol. % Or less is preferable, more preferably 2 vol. % Or less.
- the lower limit of the hydrogen concentration H is not particularly limited and is preferably as small as described above, but it is difficult to excessively reduce the hydrogen concentration, so the preferable lower limit is 1 vol% or more.
- preferable dew point Dp is 45 degrees C or less, More preferably, it is 40 degrees C or less.
- the lower limit of the dew point Dp is not particularly limited, but is preferably ⁇ 80 ° C. or more from the viewpoint of production cost.
- the upper limit of the temperature is set to 350 ° C.
- it is 340 degrees C or less, More preferably, it is 330 degrees C or less.
- the lower limit of the temperature to be retained is less than 200 ° C.
- YR does not increase.
- the lower limit of the temperature is set to 200.degree.
- it is 210 degreeC or more, More preferably, it is 220 degreeC or more.
- the above is the method for producing a high strength galvanized steel sheet according to the present invention, but after the cold rolling and before annealing, the cold rolled sheet obtained by cold rolling is subjected to a temperature from Ac1 point to Ac3 point + 50 ° C. It is also possible to carry out a pretreatment step of heating the area and pickling.
- a c1 point-heated to a temperature range of A c3 point + 50 °C "heating to a temperature range of c1 point A-A c3 point + 50 °C", in order to guarantee a high yield strength and plating properties due to the formation of steel structure in the final product It is a condition of It is preferable in terms of material to obtain a structure including ferrite and martensite before the subsequent annealing step. Furthermore, it is preferable to concentrate oxides such as Mn in the surface layer portion of the steel sheet by this heating also from the viewpoint of the plating property. From that point of view, heating is performed to a temperature range of A c1 point to A c3 point + 50 ° C.
- the acid pickling after the heating is subsequent heat treatment to ensure the plating property by heating at a temperature range of 3 or more of A c , so oxides such as Si and Mn concentrated in the surface layer of the steel sheet are removed by acid pickling Do.
- temper rolling is performed at an elongation rate of 0.1% or more after cooling of the plating process. Temper rolling may not be performed. In addition to the purpose of shape correction and surface roughness adjustment, temper rolling is performed at an elongation rate of 0.1% or more for the purpose of stably obtaining YS. For shape correction and surface roughness adjustment, leveler processing may be performed instead of temper rolling. Excessive temper rolling introduces excessive strain on the surface of the steel sheet and lowers the evaluation value of ductility and stretch flangeability. In addition, excessive temper rolling reduces ductility, and because of the high strength steel plate, equipment load also increases. Then, it is preferable to make the rolling reduction of temper rolling into 3% or less.
- width trimming before or after the temper rolling.
- coil width adjustment can be performed.
- width trimming prior to the post heat treatment step hydrogen in the steel can be efficiently released by the subsequent post heat treatment.
- a residence time t (hr) of staying at a temperature T (° C.) of 200 ° C. or more and 350 ° C. or less in the post heat treatment step is 0.005 (hr) or more and (2) It suffices to satisfy the condition. 115-18.3 ⁇ ln (t) ⁇ T (2)
- the temperature can be shortened if the temperature conditions are the same, and the temperature can be lowered if the conditions of the residence time are the same.
- Molten steel of the composition shown in Table 1 was melted by a converter and made into a slab by a continuous casting machine.
- the slab was heated to 1200 ° C. to form a hot rolled coil at a finish rolling temperature of 840 ° C. and a coil winding temperature of 610 ° C.
- This hot rolled coil was used as a cold rolled material having a thickness of 1.4 mm and a cold rolling reduction of 50%.
- This cold rolled material is heated to 810 ° C. ((Ac3 point ⁇ 20 ° C.) to 900 ° C.) and retained for 60 seconds by annealing treatment in an annealing furnace atmosphere with a hydrogen concentration of 9 vol% and a dew point of ⁇ 30 ° C.
- Amount of hydrogen in steel was measured by the following method. First, a test piece of about 5 ⁇ 30 mm was cut out from the alloyed galvanized steel sheet subjected to the post heat treatment. Then, using a router, the plating on the surface of the test specimen was removed and placed in a quartz tube. Then, after replacing the inside of the quartz tube with Ar, the temperature was raised at 200 ° C./hr and hydrogen generated up to 400 ° C. was measured by gas chromatography. Thus, the amount of released hydrogen was measured by a temperature rising analysis method. The cumulative value of the amount of hydrogen detected in the temperature range from room temperature (25 ° C.) to less than 210 ° C. was taken as the diffusible hydrogen amount.
- FIG. 1 shows the relationship between the amount of diffusible hydrogen and the minimum nugget diameter.
- the steel structure and the like are within the scope of the present invention.
- the molten steel of the composition shown in Table 2 is melted by a converter and made into a slab by a continuous casting machine, then hot rolling, cold rolling, heating (annealing), pickling under various conditions shown in Table 2 (Table 2 In the case of “ ⁇ ” in the above, the concentration of HCl in the pickling solution was adjusted to 5 mass% and the solution temperature was adjusted to 60 ° C.), annealing and plating treatment, temper rolling, width trim, post heat treatment A high strength galvanized steel sheet (product sheet) of .4 mm thickness was manufactured. In addition, in cooling (cooling after plating treatment), it was cooled to 100 ° C. or less by passing it through a water bath having a water temperature of 40 ° C.
- the evaluation method is as follows.
- Texture observation Specimens for texture observation were taken from the galvanized steel sheet, and after grinding the L cross section (plate thickness cross section parallel to the rolling direction), it was corroded with nital solution and it was near 1/4 t (t is the total thickness) from the surface by SEM.
- the volume fraction of retained austenite was quantified by X-ray diffraction intensity.
- F means ferrite
- M means hardened martensite
- B means bainite
- residual ⁇ means retained austenite.
- JIS No. 5 tensile test specimen (JIS Z 2201) was taken from a galvanized steel sheet in a direction perpendicular to the rolling direction, and a tensile test was conducted at a constant tensile speed (cross head speed) of 10 mm / min.
- the yield strength (YS) is the value obtained by reading 0.2% proof stress from the slope of the stress range of 150 to 350 MPa
- the tensile strength is the value obtained by dividing the maximum load in the tensile test by the initial cross section of the test piece parallel portion
- the plate thickness in calculation of the cross-sectional area of the parallel portion was the plate thickness value including plating thickness.
- the non-plating defect means an area on the order of several ⁇ m to several mm where plating does not exist and the steel plate is exposed.
- the amount of diffusible hydrogen in the steel was measured in the same manner as in Example 1.
- the amount of Mn oxide in the zinc plating layer is carried out by dissolving the plating layer with dilute hydrochloric acid to which an inhibitor is added and using ICP emission spectrometry for the amount of Mn oxide in the zinc plating layer. It measured using.
- Hydrogen Embrittlement As an evaluation of hydrogen embrittlement resistance, hydrogen embrittlement of resistance spot welds of steel plates was evaluated. The evaluation method is the same as in Example 1.
- the welding current value was set as the condition for forming the nugget diameter according to each steel plate strength.
- the nugget diameter was 3.8 mm at 1100 to 1250 MPa, 4.8 mm at 1250 to 1400 MPa, and 6 mm at 1400 MPa or more.
- the spacer spacing at both ends was 40 mm, and the steel plate and the spacer were previously fixed by welding. After leaving it for 24 hours after welding, the spacer portion was cut off, and the cross section of the weld nugget was observed to evaluate the presence or absence of a crack (crack). In the table, no crack is indicated by "o", and crack is indicated by "x”.
- the obtained results are shown in Table 4.
- the invention examples had good TS, YR, surface properties and weldability. Either of the comparative examples was inferior. Further, from the comparison between the inventive example and the comparative example, the relationship between the diffusible hydrogen amount and the weldability is the same as that in FIG. 1 within the range of the component composition and steel structure of the present invention. When the content is 20 mass ppm or less, it can be understood that the resistance spot weld nugget cracking evaluation is good as resistance to hydrogen embrittlement.
- the high strength galvanized steel sheet of the present invention not only has high tensile strength but also has a high yield strength ratio, good surface properties and resistance to hydrogen embrittlement. For this reason, when the present invention is applied mainly to a framework part of a car body, especially the cabin periphery which affects the collision safety, it contributes to the weight reduction of the vehicle body by the high strength and thin wall effect together with the improvement of its safety performance. As a result, the present invention can also contribute to environmental aspects such as CO 2 emission. In addition, since the present invention has good surface properties and plating quality, it is possible to positively apply it to a part where there is a concern about corrosion due to rain and snow, such as a foot. For this reason, according to the present invention, the performance improvement can also be expected with regard to the rust and corrosion resistance of the vehicle body. Such characteristics are effective not only to automobile parts but also to civil engineering, construction and home appliance fields.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- General Chemical & Material Sciences (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Coating With Molten Metal (AREA)
Abstract
Description
[6]さらに、前記焼鈍工程の前に冷延素材を、Ac1点~Ac3点+50℃の温度域まで加熱し、酸洗する前処理工程を備える[5]に記載の高強度亜鉛めっき鋼板の製造方法。
本発明の高強度亜鉛めっき鋼板は、鋼板と、該鋼板の表面に形成された亜鉛めっき層とを備える。以下では、鋼板、亜鉛めっき層の順で説明する。
Cは鋼板の高強度化に有効な元素であり、鋼組織の硬質相の一つであるマルテンサイトを形成することで高強度化に寄与する。これらの効果を得るためには、C含有量は0.10%以上とすることが必要である。好ましくは0.11%以上、より好ましくは0.12%以上である。一方、C含有量が0.30%を超えると、本発明ではスポット溶接性が顕著に劣化すると同時に、マルテンサイトの強度増加により鋼板が硬質化し、延性などの成形性が低下する傾向にある。したがってC含有量は0.30%以下とする。特性改善の観点から、好ましくは0.28%以下、より好ましくは0.25%以下とする。
Siは主に固溶強化により高強度化に寄与する元素であり、強度上昇に対して延性の低下が比較的少なく強度のみならず強度と延性のバランス向上にも寄与する。一方でSiは鋼板表面にSi系酸化物を形成しやすく、不めっきの原因となる場合があると共に、焼鈍時にオーステナイトを安定化させ、最終製品に残留オーステナイトを形成させやすくする。したがって、強度確保に必要な分だけ添加すればよく、その観点からはSi含有量は0.01%以上が望ましい。より好ましくは0.02%以上である。さらに好ましくは0.05%以上である。めっき性や残留オーステナイト生成の観点からその上限を1.2%未満とする。好ましくは1.0%以下である。より好ましくは0.9%以下である。
Mnは固溶強化およびマルテンサイト形成により高強度化に寄与する元素として有効である。この効果を得るためにMn含有量は2.0%以上にする必要がある。好ましくは2.1%以上、より好ましくは2.2%以上である。一方、Mn含有量が3.5%を超えるとスポット溶接部割れを招くと共に、Mnの偏析などに起因して鋼組織にムラを生じやすくなり、加工性の低下を招く。また、Mn含有量が3.5%を超えると、Mnは鋼板表面に酸化物あるいは複合酸化物として濃化しやすく、不めっきの原因となる場合がある。そこで、Mn含有量を3.5%以下とする。好ましくは3.3%以下、より好ましくは3.0%以下である。
Pは、固溶強化により鋼板の高強度化に寄与する有効な元素である。その含有量が0.010%を超えると溶接性や、伸びフランジ性などの加工性が低下する。そこで、P含有量は0.010%以下とする。好ましくは0.008%以下、より好ましくは0.007%以下である。下限は特に規定しないが0.001%未満では製造過程において生産能率低下と脱燐コスト増を招くため、好ましくは0.001%以上とする。
Sは熱間脆性を起こす原因となったり、溶接性の低下をもたらしたり、鋼中に硫化物系介在物として存在して鋼板の加工性を低下させる有害な元素である。このため、S含有量は極力低減することが好ましい。そこで、S含有量は0.002%以下とする。下限は特に規定しないが0.0001%未満では現状の製造過程において生産能率低下とコスト増を招くため、0.0001%以上とすることが好ましい。
Alは脱酸材として添加される。その効果を得る観点から好ましい含有量は0.01%以上である。より好ましくは0.02%以上である。一方Al含有量が1%を超えると原料コストの上昇を招くほか、鋼板の表面欠陥を誘発する原因にもなるため1%を上限とする。好ましくは0.4%以下、より好ましくは0.1%以下である。
N含有量が0.006%を超えると鋼中に過剰な窒化物が生成して延性や靭性を低下させるほか、鋼板の表面性状の悪化を招くことがある。このためN含有量は0.006%以下、好ましくは0.005%以下、より好ましくは0.004%以下とする。フェライトの清浄化による延性向上の観点からは含有量は極力少ない方が好ましいが、製造過程における生産能率低下とコスト増を招くため好ましい下限は0.0001%以上とする。より好ましくは0.0010%以上、さらに好ましくは0.0015%以上である。
フェライトの存在は、高い引張強さおよび降伏強さを得る観点から好ましくないが、本発明の降伏強さを得るためには面積率で20%未満まで許容される。好ましくは15%以下、より好ましくは10%以下である。下限は特に限定されないが、1%以上が好ましく、より好ましくは2%以上、さらに好ましくは3%以上である。なお、ここで比較的高温で生成した炭化物を含まないベイナイトは後述の実施例に記載の走査電子顕微鏡での観察ではフェライトとの区別はせず、フェライトとみなす。
焼入れままのマルテンサイト、焼戻しマルテンサイトおよびベイナイトは硬質相であり、高い引張強さと降伏強さを得るため、これら硬質相の面積率が本発明において重要である。マルテンサイトは特に硬質であり、鋼板強度を高めるために有効である。焼戻しマルテンサイトとベイナイト(上記の通り、炭化物を含まないベイナイトはフェライトとみなされるため、ここで言うベイナイトは炭化物を含むベイナイトを意味する)は、特に高い降伏強さを得るために重要な組織である。以上より、これら硬質相の合計を面積率で70%以上とする。好ましくは80%以上、より好ましくは85%以上、さらに好ましくは90%以上である。上限について好ましくは、100%以下、好ましくは99%以下、さらに好ましくは98%以下である。
オーステナイト(fcc相)はフェライト(bcc相)に比べ、水素吸蔵能が高い。そのため、この残留オーステナイトが、加工など応力誘起によりマルテンサイトに変態した場合、鋼中の拡散性水素を増加させる懸念がある。そのため5%未満にする。より好ましくは4%以下、さらに好ましくは3%以下である。下限は特に限定しないが好ましくは0%以上、より好ましくは1%以上である。
本発明の高強度亜鉛めっき鋼板の製造方法は、焼鈍工程と、めっき工程と、後熱処理工程とを有する。
高い降伏強さを得るため、また、鋼中の拡散性水素量を低減させるため、後熱処理工程を行う。水素濃度H:10vol.%以下かつ露点Dp:50℃以下の炉内雰囲気にすることで、鋼中の拡散性水素量の増加を抑えることができる。水素濃度Hは少ない方が好ましく5vol.%以下が好ましく、より好ましくは2vol.%以下である。水素濃度Hの下限は特に限定されず、上記の通り少ない方が好ましいが、水素濃度を過度に低下させるのは困難であることから、好ましい下限は1vol%以上である。また、上記効果を得るために、好ましい露点Dpは45℃以下、より好ましくは40℃以下である。露点Dpの下限は特に限定されないが、製造コストの観点からは-80℃以上が好ましい。
「Ac1点~Ac3点+50℃の温度域に加熱」は、鋼組織の形成による高い降伏強さとめっき性を最終製品で担保するための条件である。引続く焼鈍工程の前に、フェライトとマルテンサイトを含む組織を得ておくことが材質上好ましい。さらに、めっき性の観点からもこの加熱により鋼板表層部にMnなどの酸化物を濃化させることが望ましい。その観点で、Ac1点~Ac3点+50℃の温度域に加熱する。ここで、上述のAc1やAc3については以下の式で得られる値を用いた。
Ac1=751-27C+18Si-12Mn-23Cu-23Ni+24Cr+23Mo-40V-6Ti+32Zr+233Nb-169Al-895B
Ac3=910-203(C)1/2+44.7Si-30Mn-11P+700S+400Al+400Tiとする。
なお、上記式における元素記号は各元素の含有量を意味し、含有しない成分は0とする。
115-18.3×ln(t)≦T (2)
(2)式から明らかなように、(1)式の場合と比較して、温度条件が同じであれば短時間化でき、滞留時間の条件が同じであれば低温化することができる。
鋼中の水素量を以下の方法で測定した。先ず、後熱処理まで施した合金化亜鉛めっき鋼板から、5×30mm程度の試験片を切り出した。次いで、ルータを使って試験片表面のめっきを除去して石英管中に入れた。次いで、石英管中をArで置換した後、200℃/hrで昇温し、400℃までに発生した水素をガスクロマトグラフにより測定した。このように、昇温分析法にて放出水素量を測定した。室温(25℃)から210℃未満の温度域で検出された水素量の累積値を拡散性水素量とした。
耐水素脆性の評価として、鋼板の抵抗スポット溶接部のナゲット割れを評価した。評価方法は、30×100mmの板の両端に板厚2mmの板をスペーサとして挟み、スペーサ間の中央をスポット溶接にて接合して試験片を作製した。この際、スポット溶接は、インバータ直流抵抗スポット溶接機を用い、電極はクロム銅製の先端径6mmのドーム型を用いた。加圧力は380kgf、通電時間は16サイクル/50Hz、保持時間は5サイクル/50Hzとした。溶接電流値を変化させて種々のナゲット径のサンプルを作製した。
亜鉛めっき鋼板から組織観察用試験片を採取し、L断面(圧延方向に平行な板厚断面)を研磨後、ナイタール液で腐食しSEMで表面から1/4t(tは全厚)近傍の位置を1500倍の倍率で3視野以上を観察して撮影した画像を解析した(観察視野ごとに面積率を測定し、平均値を算出した)。ただし、残留オーステナイトの体積率(体積率を面積率とみなす)についてはX線回折強度により定量した。表4のFはフェライト、Mは焼入れままマルテンサイト、M’は焼戻しマルテンサイト、Bはベイナイト、残留γは残留オーステナイトを意味する。
亜鉛めっき鋼板から圧延方向に対して直角方向にJIS5号引張試験片(JISZ2201)を採取し、引張速度(クロスヘッドスピード)10mm/min一定で引張試験を行った。降伏強さ(YS)は、応力150-350MPa弾性域の傾きから0.2%耐力を読み取った値とし、引張強さは引張試験における最大荷重を初期の試験片平行部断面積で除した値とした。平行部の断面積算出における板厚はめっき厚込みの板厚値を用いた。
めっき後,後熱処理したのちの外観を目視観察し、不めっき欠陥が全くないものを「○」、不めっき欠陥が発生したものを「×」、不めっき欠陥はないがめっき外観ムラなどが生じたものは「△」とした。なお、不めっき欠陥とは数μm~数mm程度のオーダーで、めっきが存在せず鋼板が露出している領域を意味する。
鋼中の拡散性水素量の測定は、実施例1と同様の方法で行った。
亜鉛めっき層中のMn酸化物量の測定は、亜鉛めっき層中のMn酸化物量については、めっき層を、インヒビターを添加した希塩酸で溶解し、ICP発光分光分析法を使用して測定した。
耐水素脆性の評価として、鋼板の抵抗スポット溶接部の水素脆性を評価した。評価方法は、実施例1と同様である。溶接電流値は、それぞれの鋼板強度に応じたナゲット径を形成する条件とした。1100~1250MPaでは、3.8mm、1250~1400MPaでは4.8mm、1400MPa以上では6mmのナゲット径とした。実施例1同様、両端のスペーサ間隔は40mmとし、鋼板とスペーサは、予め溶接により固縛した。溶接後24時間放置したのち、スペーサ部を切り落として、溶接ナゲットの断面観察をおこない、割れ(亀裂)の有無の評価をおこなった。表中、亀裂なしを「○」、亀裂ありを「×」であらわした。
Claims (9)
- 鋼組成が質量%で、
C:0.10%以上0.30%以下、
Si:1.2%未満、
Mn:2.0%以上3.5%以下、
P:0.010%以下、
S:0.002%以下、
Al:1%以下、
N:0.006%以下を含有し、残部がFeおよび不可避的不純物からなる成分組成と、
面積率で、マルテンサイトおよびベイナイトを70%以上(100%を含む)、フェライトを20%未満(0%を含む)、残留オーステナイトを5%未満(0%を含む)含む鋼組織と、を有し、
鋼中の拡散性水素量が0.20質量ppm以下の鋼板と、
該鋼板の表面に、Fe含有量が質量%で8~15%であり、片面あたりのめっき付着量が20~120g/m2である亜鉛めっき層と、を備え、
前記亜鉛めっき層に含まれるMn酸化物量が0.050g/m2以下であり、
引張強さが1100MPa以上、降伏比が0.85以上である高強度亜鉛めっき鋼板。 - 前記成分組成は、さらに、質量%で、
Ti、Nb、V、Zrのうち1種以上を合計で0.005~0.1%、
Mo、Cr、Cu、Niのうち1種以上を合計で0.005~0.5%および
B:0.0003~0.005%から選ばれる少なくとも1つを含有する請求項1に記載の高強度亜鉛めっき鋼板。 - 前記成分組成は、さらに、質量%で、
Sb:0.001~0.1%およびSn:0.001~0.1%から選ばれる1種又は2種を含有する請求項1または2に記載の高強度亜鉛めっき鋼板。 - 前記成分組成は、さらに、質量%で、
Ca:0.0010%以下を含有する請求項1~3のいずれかに記載の高強度亜鉛めっき鋼板。 - 請求項1~4のいずれかに記載の成分組成を有する冷延素材を、水素濃度H:1vol.%以上13vol.%以下の焼鈍炉内雰囲気で、焼鈍炉内温度T:Ac3点-20℃~900℃の温度域に5秒以上滞留させた後、冷却し、400~550℃の温度域に10秒以上滞留させる焼鈍工程と、
前記焼鈍工程後の鋼板を、めっき処理し、合金化処理し、平均冷却速度3℃/s以上で、100℃以下まで冷却するめっき工程と、
前記めっき工程後のめっき鋼板を、水素濃度H:10vol.%以下かつ露点Dp:50℃以下の炉内雰囲気で、200℃以上350℃以下の温度T(℃)に、0.005(hr)以上で(1)式を満たす時間t(hr)以上滞留させる後熱処理工程と、を備える高強度亜鉛めっき鋼板の製造方法。
130-18.3×ln(t)≦T (1) - さらに、前記焼鈍工程の前に冷延素材を、Ac1点~Ac3点+50℃の温度域まで加熱し、酸洗する前処理工程を備える請求項5に記載の高強度亜鉛めっき鋼板の製造方法。
- 前記めっき工程後、0.1%以上の伸長率で調質圧延を施す請求項5または6に記載の高強度亜鉛めっき鋼板の製造方法。
- 前記後熱処理工程後に、幅トリムをする請求項7に記載の高強度亜鉛めっき鋼板の製造方法。
- 前記後熱処理工程前に、幅トリムを行い、
前記後熱処理工程における、200℃以上350℃以下の温度T(℃)で滞留する滞留時間t(hr)が、0.005(hr)以上かつ(2)式を満たす請求項7に記載の高強度亜鉛めっき鋼板の製造方法。
115-18.3×ln(t)≦ T (2)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP18884774.3A EP3719157B1 (en) | 2017-11-29 | 2018-08-20 | High-strength galvanized steel sheet, and method for manufacturing same |
| US16/766,398 US11408059B2 (en) | 2017-11-29 | 2018-08-20 | High-strength galvanized steel sheet and method for manufacturing same |
| MX2020005475A MX2020005475A (es) | 2017-11-29 | 2018-08-20 | Chapa de acero galvanizada de alta resistencia y metodo para fabricar la misma. |
| JP2018560920A JP6525114B1 (ja) | 2017-11-29 | 2018-08-20 | 高強度亜鉛めっき鋼板およびその製造方法 |
| CN201880076648.3A CN111433380B (zh) | 2017-11-29 | 2018-08-20 | 高强度镀锌钢板及其制造方法 |
| KR1020207015197A KR102402864B1 (ko) | 2017-11-29 | 2018-08-20 | 고강도 아연 도금 강판 및 그의 제조 방법 |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2017228555 | 2017-11-29 | ||
| JP2017-228555 | 2017-11-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2019106895A1 true WO2019106895A1 (ja) | 2019-06-06 |
Family
ID=66664765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP2018/030693 Ceased WO2019106895A1 (ja) | 2017-11-29 | 2018-08-20 | 高強度亜鉛めっき鋼板およびその製造方法 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US11408059B2 (ja) |
| EP (1) | EP3719157B1 (ja) |
| JP (1) | JP6525114B1 (ja) |
| KR (1) | KR102402864B1 (ja) |
| CN (1) | CN111433380B (ja) |
| MX (1) | MX2020005475A (ja) |
| WO (1) | WO2019106895A1 (ja) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2022202108A1 (ja) * | 2021-03-24 | 2022-09-29 | Jfeスチール株式会社 | 亜鉛系めっき鋼板およびその製造方法 |
| WO2022202107A1 (ja) * | 2021-03-24 | 2022-09-29 | Jfeスチール株式会社 | 亜鉛系めっき鋼板および冷延鋼板 |
| EP4063525A4 (en) * | 2019-11-22 | 2022-11-23 | Nippon Steel Corporation | COATED STEEL ELEMENT, COATED STEEL SHEET AND METHOD OF MAKING SAME |
| WO2024224638A1 (ja) * | 2023-04-28 | 2024-10-31 | Jfeスチール株式会社 | 合金化溶融亜鉛めっき鋼板の製造方法 |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102402864B1 (ko) | 2017-11-29 | 2022-05-27 | 제이에프이 스틸 가부시키가이샤 | 고강도 아연 도금 강판 및 그의 제조 방법 |
| KR102423555B1 (ko) * | 2017-11-29 | 2022-07-20 | 제이에프이 스틸 가부시키가이샤 | 스팟 용접용 고강도 아연 도금 강판 및 그의 제조 방법 |
| JP6673534B2 (ja) * | 2018-03-30 | 2020-03-25 | Jfeスチール株式会社 | 高強度亜鉛めっき鋼板、高強度部材およびそれらの製造方法 |
| JP6631760B1 (ja) * | 2018-03-30 | 2020-01-15 | Jfeスチール株式会社 | 高強度亜鉛めっき鋼板および高強度部材 |
| JP6711464B2 (ja) * | 2018-03-30 | 2020-06-17 | Jfeスチール株式会社 | 高強度亜鉛めっき鋼板の製造方法および高強度部材の製造方法 |
| KR102469708B1 (ko) | 2018-03-30 | 2022-11-21 | 제이에프이 스틸 가부시키가이샤 | 고강도 아연 도금 강판, 고강도 부재 및 그들의 제조 방법 |
| WO2020241861A1 (ja) * | 2019-05-31 | 2020-12-03 | 日本製鉄株式会社 | ホットスタンプ用めっき鋼板 |
| CN112080685B (zh) * | 2020-07-31 | 2022-06-03 | 河钢股份有限公司 | 一种吉帕级超高强度钢板及其生产方法 |
| MX2023005276A (es) * | 2020-11-06 | 2023-07-26 | Jfe Steel Corp | Lámina de acero con galvanoplastia a base de fe, lámina de acero recubierta por electrodeposición, pieza automotriz, método de producción de lámina de acero recubierta por electrodeposición, y método de producción de lámina de acero con galvanoplastia a base de fe. |
| MX2023007615A (es) * | 2020-12-24 | 2023-07-13 | Jfe Steel Corp | Lamina de acero galvanizada por inmersion en caliente y metodo de fabricacion de la misma. |
| MX2023014591A (es) | 2021-06-11 | 2023-12-15 | Jfe Steel Corp | Chapa de acero de alta resistencia y metodo para fabricar la misma. |
| KR102905605B1 (ko) | 2021-06-11 | 2025-12-30 | 제이에프이 스틸 가부시키가이샤 | 고강도 강판 및 그의 제조 방법 |
| CN117545867A (zh) * | 2021-06-24 | 2024-02-09 | 杰富意钢铁株式会社 | 热浸镀锌钢板及其制造方法和部件 |
| MX2024011506A (es) | 2022-03-25 | 2024-09-24 | Jfe Steel Corp | Lamina de acero de alta resistencia y metodo de fabricacion de la misma. |
| WO2023181642A1 (ja) | 2022-03-25 | 2023-09-28 | Jfeスチール株式会社 | 高強度鋼板およびその製造方法 |
| CN118804993A (zh) | 2022-03-25 | 2024-10-18 | 杰富意钢铁株式会社 | 高强度钢板及其制造方法 |
| WO2023181643A1 (ja) | 2022-03-25 | 2023-09-28 | Jfeスチール株式会社 | 高強度鋼板およびその製造方法 |
| WO2023181640A1 (ja) | 2022-03-25 | 2023-09-28 | Jfeスチール株式会社 | 高強度鋼板およびその製造方法 |
| CN118829740A (zh) | 2022-03-25 | 2024-10-22 | 杰富意钢铁株式会社 | 高强度钢板及其制造方法 |
| CN116590614B (zh) * | 2023-04-26 | 2025-10-28 | 华南理工大学 | 一种含Nb、Ti超高强度冷轧双相钢及其制备方法 |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5438302B2 (ja) | 1972-08-19 | 1979-11-20 | ||
| JP2007231373A (ja) | 2006-03-01 | 2007-09-13 | Nippon Steel Corp | 溶接部の耐水素脆性に優れる高強度鋼板及びその製造方法 |
| JP2011111671A (ja) | 2009-11-30 | 2011-06-09 | Nippon Steel Corp | 延性及び耐遅れ破壊特性の良好な引張最大強度900MPa以上を有する高強度鋼板および高強度冷延鋼板の製造方法、高強度亜鉛めっき鋼板の製造方法 |
| JP2012041597A (ja) | 2010-08-18 | 2012-03-01 | Nippon Steel Corp | 耐遅れ破壊特性に優れたホットプレス用めっき鋼板及びその製造方法 |
| WO2013047836A1 (ja) * | 2011-09-30 | 2013-04-04 | 新日鐵住金株式会社 | 亜鉛めっき鋼板及びその製造方法 |
| JP2013213232A (ja) | 2012-03-30 | 2013-10-17 | Kobe Steel Ltd | 加工性に優れた高降伏比高強度鋼板 |
| JP2015151607A (ja) | 2014-02-18 | 2015-08-24 | Jfeスチール株式会社 | 高強度溶融亜鉛めっき鋼板およびその製造方法 |
| WO2016092733A1 (ja) * | 2014-12-12 | 2016-06-16 | Jfeスチール株式会社 | 高強度冷延鋼板及びその製造方法 |
| JP2016130356A (ja) * | 2015-01-09 | 2016-07-21 | 株式会社神戸製鋼所 | めっき性、加工性、および耐遅れ破壊特性に優れた高強度めっき鋼板、並びにその製造方法 |
| WO2017131055A1 (ja) * | 2016-01-27 | 2017-08-03 | Jfeスチール株式会社 | 高降伏比型高強度亜鉛めっき鋼板及びその製造方法 |
| EP3243923A1 (en) * | 2015-01-07 | 2017-11-15 | Posco | Super high strength plated steel sheet having tensile strength of 1300 mpa or more, and manufacturing method therefor |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5438302B2 (ja) | 2008-10-30 | 2014-03-12 | 株式会社神戸製鋼所 | 加工性に優れた高降伏比高強度の溶融亜鉛めっき鋼板または合金化溶融亜鉛めっき鋼板とその製造方法 |
| JP5252142B1 (ja) | 2011-07-29 | 2013-07-31 | 新日鐵住金株式会社 | 成形性に優れた高強度鋼板、高強度亜鉛めっき鋼板及びそれらの製造方法 |
| WO2013047589A1 (ja) | 2011-09-26 | 2013-04-04 | 株式会社 フジミインコーポレーテッド | 希土類元素を含んだ溶射用粉末及び皮膜、並びに前記皮膜を備えた部材 |
| JP6111522B2 (ja) * | 2012-03-02 | 2017-04-12 | Jfeスチール株式会社 | 高強度溶融亜鉛めっき鋼板及びその製造方法 |
| JP5821912B2 (ja) | 2013-08-09 | 2015-11-24 | Jfeスチール株式会社 | 高強度冷延鋼板およびその製造方法 |
| JP6052473B1 (ja) * | 2015-01-28 | 2016-12-27 | Jfeスチール株式会社 | 高強度冷延鋼板、高強度めっき鋼板及びこれらの製造方法 |
| EP3409808B1 (en) | 2016-01-27 | 2020-03-04 | JFE Steel Corporation | High-yield ratio high-strength galvanized steel sheet, and method for producing same |
| JP2017145441A (ja) * | 2016-02-16 | 2017-08-24 | 日新製鋼株式会社 | 黒色表面被覆高強度鋼板およびその製造方法 |
| KR102423555B1 (ko) * | 2017-11-29 | 2022-07-20 | 제이에프이 스틸 가부시키가이샤 | 스팟 용접용 고강도 아연 도금 강판 및 그의 제조 방법 |
| KR102402864B1 (ko) | 2017-11-29 | 2022-05-27 | 제이에프이 스틸 가부시키가이샤 | 고강도 아연 도금 강판 및 그의 제조 방법 |
| JP6711464B2 (ja) | 2018-03-30 | 2020-06-17 | Jfeスチール株式会社 | 高強度亜鉛めっき鋼板の製造方法および高強度部材の製造方法 |
-
2018
- 2018-08-20 KR KR1020207015197A patent/KR102402864B1/ko active Active
- 2018-08-20 EP EP18884774.3A patent/EP3719157B1/en active Active
- 2018-08-20 JP JP2018560920A patent/JP6525114B1/ja active Active
- 2018-08-20 WO PCT/JP2018/030693 patent/WO2019106895A1/ja not_active Ceased
- 2018-08-20 MX MX2020005475A patent/MX2020005475A/es unknown
- 2018-08-20 CN CN201880076648.3A patent/CN111433380B/zh active Active
- 2018-08-20 US US16/766,398 patent/US11408059B2/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5438302B2 (ja) | 1972-08-19 | 1979-11-20 | ||
| JP2007231373A (ja) | 2006-03-01 | 2007-09-13 | Nippon Steel Corp | 溶接部の耐水素脆性に優れる高強度鋼板及びその製造方法 |
| JP2011111671A (ja) | 2009-11-30 | 2011-06-09 | Nippon Steel Corp | 延性及び耐遅れ破壊特性の良好な引張最大強度900MPa以上を有する高強度鋼板および高強度冷延鋼板の製造方法、高強度亜鉛めっき鋼板の製造方法 |
| JP2012041597A (ja) | 2010-08-18 | 2012-03-01 | Nippon Steel Corp | 耐遅れ破壊特性に優れたホットプレス用めっき鋼板及びその製造方法 |
| WO2013047836A1 (ja) * | 2011-09-30 | 2013-04-04 | 新日鐵住金株式会社 | 亜鉛めっき鋼板及びその製造方法 |
| JP2013213232A (ja) | 2012-03-30 | 2013-10-17 | Kobe Steel Ltd | 加工性に優れた高降伏比高強度鋼板 |
| JP2015151607A (ja) | 2014-02-18 | 2015-08-24 | Jfeスチール株式会社 | 高強度溶融亜鉛めっき鋼板およびその製造方法 |
| WO2016092733A1 (ja) * | 2014-12-12 | 2016-06-16 | Jfeスチール株式会社 | 高強度冷延鋼板及びその製造方法 |
| EP3243923A1 (en) * | 2015-01-07 | 2017-11-15 | Posco | Super high strength plated steel sheet having tensile strength of 1300 mpa or more, and manufacturing method therefor |
| JP2016130356A (ja) * | 2015-01-09 | 2016-07-21 | 株式会社神戸製鋼所 | めっき性、加工性、および耐遅れ破壊特性に優れた高強度めっき鋼板、並びにその製造方法 |
| WO2017131055A1 (ja) * | 2016-01-27 | 2017-08-03 | Jfeスチール株式会社 | 高降伏比型高強度亜鉛めっき鋼板及びその製造方法 |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP4063525A4 (en) * | 2019-11-22 | 2022-11-23 | Nippon Steel Corporation | COATED STEEL ELEMENT, COATED STEEL SHEET AND METHOD OF MAKING SAME |
| WO2022202108A1 (ja) * | 2021-03-24 | 2022-09-29 | Jfeスチール株式会社 | 亜鉛系めっき鋼板およびその製造方法 |
| WO2022202107A1 (ja) * | 2021-03-24 | 2022-09-29 | Jfeスチール株式会社 | 亜鉛系めっき鋼板および冷延鋼板 |
| JP7144711B1 (ja) * | 2021-03-24 | 2022-09-30 | Jfeスチール株式会社 | 亜鉛系めっき鋼板およびその製造方法 |
| JP7144710B1 (ja) * | 2021-03-24 | 2022-09-30 | Jfeスチール株式会社 | 亜鉛系めっき鋼板および冷延鋼板 |
| US12480177B2 (en) | 2021-03-24 | 2025-11-25 | Jfe Steel Corporation | Galvanized steel sheet and method for producing same |
| WO2024224638A1 (ja) * | 2023-04-28 | 2024-10-31 | Jfeスチール株式会社 | 合金化溶融亜鉛めっき鋼板の製造方法 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3719157A1 (en) | 2020-10-07 |
| US11408059B2 (en) | 2022-08-09 |
| JPWO2019106895A1 (ja) | 2019-12-12 |
| MX2020005475A (es) | 2020-08-27 |
| KR20200083519A (ko) | 2020-07-08 |
| EP3719157B1 (en) | 2024-05-01 |
| EP3719157A4 (en) | 2020-12-02 |
| US20200377978A1 (en) | 2020-12-03 |
| KR102402864B1 (ko) | 2022-05-27 |
| JP6525114B1 (ja) | 2019-06-05 |
| CN111433380A (zh) | 2020-07-17 |
| CN111433380B (zh) | 2022-12-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6525114B1 (ja) | 高強度亜鉛めっき鋼板およびその製造方法 | |
| JP6544494B1 (ja) | 高強度亜鉛めっき鋼板およびその製造方法 | |
| JP6631760B1 (ja) | 高強度亜鉛めっき鋼板および高強度部材 | |
| JP5858199B2 (ja) | 高強度溶融亜鉛めっき鋼板及びその製造方法 | |
| EP3309273B1 (en) | Galvannealed steel sheet and method for manufacturing same | |
| JP5983895B2 (ja) | 高強度鋼板およびその製造方法、ならびに高強度亜鉛めっき鋼板の製造方法 | |
| EP2527484B1 (en) | Method for manufacturing a high-strength galvanized steel sheet having excellent formability and spot weldability | |
| JP6249140B1 (ja) | 高降伏比型高強度亜鉛めっき鋼板及びその製造方法 | |
| JP2008280608A (ja) | 加工性および溶接性に優れる高強度溶融亜鉛めっき鋼板およびその製造方法 | |
| JP3812279B2 (ja) | 加工性および歪時効硬化特性に優れた高降伏比型高張力溶融亜鉛めっき鋼板およびその製造方法 | |
| JP6950826B2 (ja) | 高強度鋼板、熱延鋼板の製造方法、冷延フルハード鋼板の製造方法および高強度鋼板の製造方法 | |
| JP2013241636A (ja) | 低降伏比型高強度溶融亜鉛めっき鋼板、低降伏比型高強度合金化溶融亜鉛めっき鋼板、低降伏比型高強度溶融亜鉛めっき鋼板の製造方法、および低降伏比型高強度合金化溶融亜鉛めっき鋼板の製造方法 | |
| JP7311808B2 (ja) | 鋼板及びその製造方法 | |
| CN116806274A (zh) | 高强度钢板及其制造方法 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ENP | Entry into the national phase |
Ref document number: 2018560920 Country of ref document: JP Kind code of ref document: A |
|
| 121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 18884774 Country of ref document: EP Kind code of ref document: A1 |
|
| ENP | Entry into the national phase |
Ref document number: 20207015197 Country of ref document: KR Kind code of ref document: A |
|
| NENP | Non-entry into the national phase |
Ref country code: DE |
|
| ENP | Entry into the national phase |
Ref document number: 2018884774 Country of ref document: EP Effective date: 20200629 |
|
| WWG | Wipo information: grant in national office |
Ref document number: MX/A/2020/005475 Country of ref document: MX |