WO2013047808A1 - 高強度溶融亜鉛めっき鋼板及びその製造方法 - Google Patents
高強度溶融亜鉛めっき鋼板及びその製造方法 Download PDFInfo
- Publication number
- WO2013047808A1 WO2013047808A1 PCT/JP2012/075194 JP2012075194W WO2013047808A1 WO 2013047808 A1 WO2013047808 A1 WO 2013047808A1 JP 2012075194 W JP2012075194 W JP 2012075194W WO 2013047808 A1 WO2013047808 A1 WO 2013047808A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- less
- steel sheet
- hot
- dip galvanized
- average
- Prior art date
Links
- 229910001335 Galvanized steel Inorganic materials 0.000 title claims abstract description 26
- 239000008397 galvanized steel Substances 0.000 title claims abstract description 26
- 238000000034 method Methods 0.000 title description 18
- 230000008569 process Effects 0.000 title description 3
- 229910001566 austenite Inorganic materials 0.000 claims abstract description 72
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 70
- 239000010959 steel Substances 0.000 claims abstract description 70
- 229910000859 α-Fe Inorganic materials 0.000 claims abstract description 27
- 229910001563 bainite Inorganic materials 0.000 claims abstract description 14
- 239000012535 impurity Substances 0.000 claims abstract description 11
- 229910000734 martensite Inorganic materials 0.000 claims abstract description 10
- 239000002245 particle Substances 0.000 claims abstract description 7
- 229910001562 pearlite Inorganic materials 0.000 claims abstract description 6
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 4
- 230000000717 retained effect Effects 0.000 claims description 40
- 238000005452 bending Methods 0.000 claims description 26
- 238000001816 cooling Methods 0.000 claims description 21
- 238000005096 rolling process Methods 0.000 claims description 17
- 238000004519 manufacturing process Methods 0.000 claims description 16
- 238000000137 annealing Methods 0.000 claims description 12
- 238000005098 hot rolling Methods 0.000 claims description 12
- 239000000463 material Substances 0.000 claims description 9
- 238000007747 plating Methods 0.000 claims description 9
- 238000005275 alloying Methods 0.000 claims description 7
- 238000005246 galvanizing Methods 0.000 claims description 6
- 230000009467 reduction Effects 0.000 claims description 3
- 238000005097 cold rolling Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 26
- 238000005728 strengthening Methods 0.000 description 21
- 230000001965 increasing effect Effects 0.000 description 11
- 230000009466 transformation Effects 0.000 description 8
- 230000007423 decrease Effects 0.000 description 6
- 230000002411 adverse Effects 0.000 description 5
- 239000003153 chemical reaction reagent Substances 0.000 description 5
- 238000001953 recrystallisation Methods 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 4
- 230000003287 optical effect Effects 0.000 description 4
- 238000001556 precipitation Methods 0.000 description 4
- 229910052761 rare earth metal Inorganic materials 0.000 description 4
- 229920006395 saturated elastomer Polymers 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- 229910052684 Cerium Inorganic materials 0.000 description 3
- 229910001567 cementite Inorganic materials 0.000 description 3
- 239000013078 crystal Substances 0.000 description 3
- 230000003111 delayed effect Effects 0.000 description 3
- 230000006866 deterioration Effects 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 description 3
- 229910052746 lanthanum Inorganic materials 0.000 description 3
- 238000000691 measurement method Methods 0.000 description 3
- 239000002244 precipitate Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 230000002829 reductive effect Effects 0.000 description 3
- 238000011160 research Methods 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000009749 continuous casting Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 229910052747 lanthanoid Inorganic materials 0.000 description 2
- 150000002602 lanthanoids Chemical class 0.000 description 2
- 239000010410 layer Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 229910001568 polygonal ferrite Inorganic materials 0.000 description 2
- 238000011002 quantification Methods 0.000 description 2
- 239000013585 weight reducing agent Substances 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 208000010392 Bone Fractures Diseases 0.000 description 1
- 206010017076 Fracture Diseases 0.000 description 1
- 229910001122 Mischmetal Inorganic materials 0.000 description 1
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000010960 cold rolled steel Substances 0.000 description 1
- 230000002596 correlated effect Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000004453 electron probe microanalysis Methods 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000000445 field-emission scanning electron microscopy Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000000265 homogenisation Methods 0.000 description 1
- 238000010191 image analysis Methods 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000000670 limiting effect Effects 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 238000005554 pickling Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 238000007711 solidification Methods 0.000 description 1
- 230000008023 solidification Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing 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
- B32B15/01—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
-
- 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
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
-
- 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
- C21D8/0278—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
- C21D8/0284—Application of a separating or insulating coating
-
- 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
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0426—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
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0436—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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/04—Alloys based on zinc with aluminium as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/14—Ferrous alloys, e.g. steel alloys containing titanium or zirconium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
-
- 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
- C23C2/06—Zinc or cadmium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
-
- 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
- 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
- C21D2211/005—Ferrite
-
- 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]
Definitions
- the present invention relates to a hot-dip galvanized steel sheet excellent in bendability used for structural materials for automobiles and the like and having a high strength (for example, a tensile strength of 980 MPa or more) and a method for producing the same.
- High-strength steel sheets are also required to have improved bendability as well as elongation.
- Patent Document 1 measures the homogenization of the structure and adds precipitation strengthening to the ferrite single phase to provide high strength.
- a technique for making the structure uniform is disclosed in Patent Document 2 by a structure mainly composed of bainite.
- Patent Document 3 discloses a high-strength, high-ductile molten zinc containing a ferrite phase of 30 to 90% by volume fraction, 5% or more of bainite, 10% or less of martensite, and 5 to 30% of retained austenite phase.
- a plated steel sheet is disclosed.
- the density of dislocations contained in the steel sheet is 8 ⁇ 10 11 (pieces / mm 2 ) or less, the quasi-static strength (FS1) at a strain rate of 0.0067 (s ⁇ 1 ),
- the present invention has been made in order to solve the conventional problems, and in the retained austenitic steel having a tensile strength of 980 MPa or more, it is a technique found as a result of intensive studies to improve V bendability, It is an object of the present invention to provide a high-strength hot-dip galvanized steel sheet excellent in elongation and V-bendability and a method for producing the same.
- the present inventor has imparted compressive residual stress to the residual austenite phase, thereby improving the stability of the residual austenite more than before. It has been found that it works effectively on local deformation of bending.
- the present inventor has optimized the roll diameter, tension, and number of passes in repeated bending during overaging (OA) treatment in order to impart compressive residual stress to the residual austenite phase. It has been found that controlling the residual stress in the austenite phase by control provides a sufficient effect on elongation and V bendability. As a result of further research based on the above findings, the present inventor can combine the condition control in repeated bending during overaging (OA) treatment with the concentration in the austenite phase and the control of the particle size. Since the stability of the retained austenite phase can be increased, it has been found that it is more effective for elongation and V-bendability.
- OA repeated bending during overaging
- the mechanism by which the above effect can be obtained in the present invention is estimated as follows.
- Residual austenitic steel controls the ferrite transformation and bainite transformation during annealing to increase the C concentration in the austenite, leaving austenite in the steel structure of the product, and the high strength and high elongation due to the TRIP effect of this retained austenite It is a steel plate.
- it is a mixed structure it is presumed that such retained austenitic steel was not a steel excellent in bendability.
- the inventors have made various steels with different amounts of C, Si, and Mn dissolved, hot-rolled, cold-rolled, and annealed in the laboratory in order to make the TRIP effect act on bendability effectively.
- Various methods for obtaining the required tensile strength, ductility, V bendability, and plating properties were examined by hot dip galvanizing.
- the present inventors have found that it also effectively acts on local deformation of the bending portion of the compressive stress portion inside the bending stress portion outside the bending portion.
- the present invention has been completed based on the above findings.
- the present invention can include, for example, the following aspects.
- a high-strength hot-dip galvanized steel sheet Among the austenites, the austenite grains in the range where the average residual stress ⁇ R satisfies the formula (1) is 50% or more, ⁇ 400 MPa ⁇ ⁇ R ⁇ 200 MPa (1)
- a hot-dip galvanized steel sheet comprising a hot-dip galvanized layer containing less than 7% by mass of Fe on the surface of the steel sheet, the balance being Zn, Al and inevitable impurities.
- Annealing is performed at a maximum temperature of 700 to 900 ° C., and is cooled within a temperature range of 350 ° C. to 550 ° C. at an average cooling rate of 0.1 to 200 ° C./sec. Hold for 1000 seconds or less,
- the steel plate after being held in the temperature range is immersed in a hot dip galvanizing bath, and after the plating treatment, alloying is performed in a temperature range of 470 to 580 ° C., and the steel plate is in a temperature range of 350 ° C. to 550 ° C.
- a method for producing a hot-dip galvanized steel sheet wherein an average stress in a longitudinal direction applied to the steel sheet during the repeated bending is 2 to 50 MPa.
- a high-strength hot-dip galvanized steel sheet excellent in ductility and V bendability is provided.
- the hot-dip galvanized steel sheet can be manufactured relatively easily and stably. For this reason, the hot-dip galvanized steel sheet of the present invention can be optimally used particularly as a steel sheet for automobiles aiming at weight reduction in recent years, and its industrial value is extremely large.
- 4 is a graph showing a relationship between residual stress in a retained austenite phase and a minimum bending radius R. It is a graph which shows the range with which average residual stress (sigma) R of an austenite grain satisfy
- the high-strength thin steel sheet of the present invention focuses on improving the stability of the retained austenite phase in the retained austenitic steel.
- the present invention is based on the finding that by controlling the residual stress and aspect ratio of the retained austenite phase, the stability can be enhanced to the utmost and strength, elongation and V-bending can be achieved at a high level. It is.
- the structure of the hot dip galvanized steel sheet of the present invention is mainly composed of a ferrite phase and a bainite phase and needs to contain 3% or more of a retained austenite phase.
- martensite may be contained, but when the ferrite phase and the bainite phase are not mainly used, the elongation tends to be remarkably lowered.
- Residual stress in the retained austenite phase is one of the most important in the present invention. As shown in FIG. 1, the lower the residual stress in the retained austenite phase, the smaller the minimum bending radius R, especially at 15 MPa or less. Each residual austenite grain is imparted with compressive residual stress in the manufacturing process, so that the martensitic transformation during processing is delayed, and as a result, the stability of the entire phase is increased. In order to achieve this, as shown in FIG. 2, ⁇ r is minimized within a range where the average residual stress ⁇ R of the austenite grains satisfies the formula (1). As shown in FIG. 3, when the austenite grains satisfying the formula (1) are 50% or more, the minimum bending radius R is stably minimized. ⁇ 400 MPa ⁇ ⁇ R ⁇ 200 MPa (1)
- the residual austenite ratio measuring method may be any method as long as the accuracy is guaranteed.
- the residual austenite ratio may be measured by chemical polishing up to 1/4 thickness from the surface layer of the specimen plate.
- the residual austenite was quantified from the (200) and (211) area strengths of ferrite and the (200), (220) and (311) area strengths of austenite by the monochromatic MoK ⁇ ray.
- ⁇ R may be any measurement method as long as the accuracy is guaranteed under the condition that the residual stress can be accurately obtained.
- ⁇ R is 1 ⁇ 4 of the surface layer of the specimen plate.
- the residual stress of any 50 residual austenite grains was carefully measured using a highly accurate X-ray diffraction stress measurement method with a 5 ⁇ m ⁇ beam system. A proportion of residual austenite grains falling within the range can be obtained.
- the average particle size of retained austenite is preferably 10 ⁇ m or less. As shown in FIG. 4, when it exceeds 10 ⁇ m, the dispersion of the retained austenite phase is coarse, and the TRIP effect cannot be sufficiently exhibited, so that the elongation is lowered.
- the average particle diameter (average equivalent circle diameter) may be measured by any method as long as accuracy is guaranteed. For example, a section of the steel sheet in the rolling direction or perpendicular to the rolling direction using a night reagent. The cross section was corroded and quantified by observation with a 500 times optical microscope.
- the aspect ratio of the retained austenite grains is 0.5 or more and 0.95 or less with respect to the rolling direction, the minimum bending radius is desirably minimized. If it exceeds 0.95 or less than 0.5, the stability of retained austenite at the time of bending deformation varies.
- the aspect ratio may be measured by any method as long as accuracy is ensured. For example, the section of the steel sheet in the rolling direction or the direction perpendicular to the rolling direction is corroded by a night reagent. After quantification by observation with an optical microscope of 500 times, after measuring the grain size in the rolling direction and the grain size in the direction perpendicular to the rolling with image processing software on 30 residual austenite grains, the average of them was obtained. The value was taken as the representative value of the material.
- the average C concentration of retained austenite also greatly contributes to the stability of retained austenite. As shown in FIG. 6, when the average C concentration is less than 0.7% by mass%, the stability of retained austenite becomes extremely low, so that the TRIP effect cannot be obtained effectively and the elongation deteriorates. On the other hand, even if it exceeds 1.5%, not only the elongation improving effect is saturated but also the cost for producing it increases, so that it is preferably 0.7% or more and 1.5% or less.
- the C concentration may be any measurement method as long as accuracy is guaranteed under the condition that the decomposition concentration can be accurately obtained. For example, the C concentration is 0 using EPMA attached to the FE-SEM. It can be obtained by carefully measuring the C concentration at a pitch of less than 5 ⁇ m.
- C is an element that can increase the strength of the steel sheet. However, if it is less than 0.1%, it becomes difficult to achieve both a tensile strength of 980 MPa or more and workability. On the other hand, if it exceeds 0.40%, it becomes difficult to ensure spot weldability. For this reason, the range of C content is made 0.1 to 0.40% or less.
- the C content is preferably from 0.1 to 0.38, and more preferably from 0.12 to 0.38.
- Si is a strengthening element and is effective in increasing the strength of the steel sheet. Moreover, since addition of cementite is suppressed and it contributes to stabilization of a retained austenite, addition is essential. If it is less than 0.01%, the effect of increasing the strength is small, and if it exceeds 0.5%, the workability decreases. Therefore, the Si content is in the range of 0.01 to 0.5%. The Si content is preferably 0.02 to 0.5%, more preferably 0.1 to 0.45.
- Mn is a strengthening element and is effective in increasing the strength of the steel sheet. However, if it is less than 1.0%, it is difficult to obtain a tensile strength of 980 MPa or more. On the contrary, if the amount is too large, co-segregation with P and S is promoted, and the workability is remarkably deteriorated, so 3.0% is made the upper limit.
- the Mn content is preferably 1.0 to 2.8%, more preferably 1.2 to 2.8%.
- O forms an oxide and degrades elongation, bendability and hole expandability, so it is necessary to suppress the addition amount.
- oxides often exist as inclusions, and when they are present on the punched end surface or cut surface, they form notched scratches and coarse dimples on the end surface, so when expanding holes or during strong processing, It causes stress concentration and becomes the starting point of crack formation, resulting in a significant deterioration of hole expansibility or bendability.
- the upper limit of the O content is set to 0.006% or less. That is, O is limited to 0.006% or less as an impurity.
- the upper limit of the O content is preferably 0.005% or less, and more preferably 0.004% or less.
- the O content is less than 0.0001%, an excessive cost increase is caused and this is not economically preferable, so this is a substantial lower limit.
- P tends to segregate in the central part of the plate thickness of the steel sheet, causing the weld to become brittle. If it exceeds 0.04%, the brittleness of the weld becomes remarkable, so the appropriate range is made 0.04% or less. That is, P is limited to 0.04% or less as an impurity.
- the P content is preferably 0.03% or less, and more preferably 0.02 or less.
- the lower limit of P is not particularly defined, it is preferable to set this value as the lower limit because it is economically disadvantageous to set it to less than 0.0001%.
- S adversely affects weldability and manufacturability during casting and hot rolling. For this reason, the upper limit is made 0.01% or less. That is, S is limited to 0.01% or less as an impurity.
- the S content is preferably 0.004% or less, and more preferably 0.003% or less.
- the lower limit value of S is not particularly defined, but it is economically disadvantageous to set it to less than 0.0001%, so this value is preferably set as the lower limit value. Further, since S is combined with Mn to form coarse MnS, it is necessary to reduce it as much as possible in order to deteriorate the bendability and hole expandability.
- Al may be added because it promotes ferrite formation and improves ductility. It can also be used as a deoxidizer. If it is less than 0.1%, the effect is insufficient. On the other hand, excessive addition increases the number of Al-based coarse inclusions, causing deterioration of hole expansibility and surface damage. For this reason, the upper limit of Al addition is set to 3.0%.
- the Al content is preferably 0.1 to 2.9%, and more preferably 0.15 to 2.9%.
- Al + Si is 0.5% or more. This Al + Si is preferably 0.5 to 4%, and more preferably 0.51 to 3.5%.
- N forms coarse nitrides and degrades bendability and hole expandability, so it is necessary to suppress the addition amount.
- N exceeds 0.01%, this tendency becomes remarkable, so the range of N content is set to 0.01% or less. In addition, it is better to use less because it causes blowholes during welding.
- the N content is preferably 0.005% or less, and more preferably 0.004% or less. Although the lower limit is not particularly defined, the effect of the present invention is exhibited. However, if the N content is less than 0.0005%, the manufacturing cost is significantly increased, and this is a substantial lower limit.
- Mo is a strengthening element and is important for improving hardenability. However, if the content is less than 0.02%, these effects cannot be obtained, so the lower limit is set to 0.02%. On the other hand, if the content exceeds 0.5%, the manufacturability during production and hot rolling is adversely affected, so the upper limit was made 0.5%.
- Nb is a strengthening element. It contributes to increasing the strength of steel sheets by strengthening precipitates, strengthening fine grains by suppressing the growth of ferrite crystal grains, and strengthening dislocations by suppressing recrystallization. If the addition amount is less than 0.01%, these effects cannot be obtained, so the lower limit is made 0.01%. If the content exceeds 0.1%, the precipitation of carbonitrides increases and the formability deteriorates, so the upper limit is made 0.1%.
- Ti is a strengthening element. It contributes to increasing the strength of steel sheets by strengthening precipitates, strengthening fine grains by suppressing the growth of ferrite crystal grains, and strengthening dislocations by suppressing recrystallization. If the addition amount is less than 0.01%, these effects cannot be obtained, so the lower limit is made 0.01%. If the content exceeds 0.2%, precipitation of carbonitride increases and formability deteriorates, so the upper limit is set to 0.2%.
- V is a strengthening element. It contributes to increasing the strength of steel sheets by strengthening precipitates, strengthening fine grains by suppressing the growth of ferrite crystal grains, and strengthening dislocations by suppressing recrystallization. If the addition amount is less than 0.005%, these effects cannot be obtained, so the lower limit is made 0.005%. If the content exceeds 0.1%, the precipitation of carbonitrides increases and the formability deteriorates, so the upper limit is made 0.1%.
- Cr Cr is a strengthening element and is important for improving hardenability. However, if less than 0.1%, these effects cannot be obtained, so the lower limit is made 0.1%. Conversely, if the content exceeds 2.0%, the manufacturability during production and hot rolling is adversely affected, so the upper limit is set to 2.0%.
- a total of 0.0005 to 0.05% of one or more selected from Ca, Mg, and REM can be added.
- Ca, Mg, and REM are elements used for deoxidation, and it is preferable to contain one or two or more in total of 0.0005% or more.
- REM is Rare Earth Metal.
- the total content is 0.0005 to 0.05%.
- REM is often added by misch metal and may contain lanthanoid series elements in combination with La and Ce. Even if these lanthanoid series elements other than La and Ce are included as inevitable impurities, the effect of the present invention is exhibited. However, the effects of the present invention are exhibited even when metal La or Ce is added.
- Cu is a strengthening element and is important for improving hardenability.
- Cu may be added because it improves the wettability of hot-dip plating and promotes the alloying reaction.
- the lower limit is made 0.04%.
- the upper limit was made 2.0%.
- Ni is a strengthening element and is important for improving hardenability.
- Ni may be added because it improves the wettability of hot-dip plating and promotes the alloying reaction. However, if less than 0.02%, these effects cannot be obtained, so the lower limit is made 0.02%. On the other hand, if the content exceeds 1%, the manufacturability during production and hot rolling is adversely affected, so the upper limit is made 1.0%.
- B is effective for strengthening grain boundaries and strengthening steel by addition of 0.0003% or more, but when the addition amount exceeds 0.07%, the effect is not only saturated but also during hot rolling.
- the upper limit is set to 0.07% because production is reduced.
- the main phase is ferrite, and retained austenite with a volume ratio of 8% or more is dispersed to ensure a maximum tensile strength of 980 MPa or more. For this reason, it is necessary to contain retained austenite.
- acicular ferrite may be included in addition to polygonal ferrite.
- the reason why the main phase is ferrite is that ductility is improved by using ferrite having a high ductility as the main phase. If the main phase ferrite phase is less than 40%, sufficient ductility cannot be secured and it is not suitable for practical use. Therefore, the volume fraction of the main phase ferrite is set to 40% or more.
- the inclusion of retained austenite achieves higher strength and further improvement in ductility. If the volume fraction is less than 8%, it is difficult to obtain the effect, so the lower limit is made less than 8%.
- the upper limit is set to 60% or less because if it exceeds 60%, the volume fraction of the main phase ferrite phase is less than 40% and sufficient ductility cannot be ensured.
- the bainite structure is unavoidably contained because it is utilized for stabilizing retained austenite. In order to further increase the strength, martensite may be contained.
- the manufacturing method of the high-strength hot-dip galvanized steel sheet according to the present invention will be described below.
- the slab before hot rolling is subjected to normal hot rolling after continuous casting.
- the temperature is set to 1100 ° C. or higher as it is after continuous casting or by reheating. Below this temperature, the homogenous treatment is insufficient and the strength and V bendability are reduced.
- the slab is hot-rolled at a finishing temperature of 850 ° C. or higher and 970 ° C. or lower. If the finishing temperature is less than 850 ° C., it becomes ( ⁇ + ⁇ ) two-phase rolling, resulting in a decrease in ductility. If it exceeds 970 ° C., the austenite grain size becomes coarse, the ferrite phase fraction becomes small, and the ductility is reduced. This is because of a decrease.
- the prototype material can be cold-rolled by 40% or more. If it is less than this, recrystallization and reverse transformation during annealing are suppressed, and elongation decreases.
- the maximum temperature during annealing is 700 ° C or higher and 900 ° C or lower.
- the temperature is lower than 700 ° C., the recrystallization of the ferrite phase during annealing is delayed, which causes a decrease in elongation.
- the martensite fraction increases and the elongation deteriorates.
- the cooling rate after annealing is preferably 0.1 ° C./second or more and 200 ° C./second or less on average.
- the average cooling rate is more preferably 1.2 ° C./second or more and 14 ° C./second or less, and particularly preferably 1.8 seconds or more and 11 ° C./second or less.
- the cooling end point temperature and subsequent holding or cooling are important techniques for controlling the bainite formation and determining the C concentration of retained austenite.
- the cooling end point temperature is less than 350 ° C., a large amount of martensite is generated, the steel strength is excessively increased, and in addition, it becomes difficult to leave austenite, so that the elongation is greatly deteriorated.
- the temperature exceeds 550 ° C. the bainite transformation is delayed, and in addition, cementite is generated during the holding or cooling, and the concentration of C in the retained austenite is lowered. Therefore, the cooling stop temperature at which 8% or more of retained austenite having a high C concentration can be generated, and the holding or cooling temperature are preferably 350 ° C. or more and 550 ° C. or less.
- the holding or cooling time is preferably 1 second or more and 1000 seconds or less.
- the holding or cooling time is preferably 110 to 800 seconds, and more preferably 150 to 400 seconds.
- Residual stress control in the austenite phase and the aspect ratio control of the retained austenite grains are possible by optimal control of the roll diameter, tension, and number of passes in repeated bending during holding time (during overaging (OA) treatment).
- OA overaging
- the roll diameter is preferably as small as possible to give a certain strain. However, if it is 50 mm or less, the roll rigidity is lowered and stable strain cannot be applied. On the other hand, when it exceeds 2000 mm, the surface contact portion increases and it becomes difficult to apply a large strain locally. Therefore, the roll diameter is preferably 50 mm or more and 2000 mm or less. More preferably, the lower limit is 350 mm or more. The upper limit is preferably 1000 mm or less.
- the tension is an important value for determining the aspect ratio in the longitudinal direction, which is organized by the longitudinal average stress, which is the value obtained by dividing the value by the plate cross-sectional area (plate thickness x plate width).
- the tension is suitably 50 MPa or less.
- This tension is preferably 45 MPa or less, and more preferably 40 MPa or less.
- the lower limit is not particularly defined, it is preferably 2 MPa or more, and more preferably 10 MPa or more in consideration of the plate passing property of the steel sheet, particularly meandering. Furthermore, with regard to the number of passes, the greater the number, the greater the number of bending and unbending, and the easier the residual stress control becomes, but the effect is small with one pass. Therefore, two or more passes are usually preferred.
- the number of times of bending is preferably 6 passes or less, and more preferably 5 passes or less.
- this technique can also perform an alloying process after immersion.
- the alloying treatment of the plating is performed in the range of 470 ° C. or more and 580 ° C. If the temperature is lower than this, alloying becomes insufficient, and if it exceeds this, it becomes an overalloy and the corrosion resistance is remarkably deteriorated.
- Table 2 shows the heat treatment conditions and the plating treatment conditions.
- Tensile properties were evaluated by C direction tension of a JIS No. 5 tensile test piece. Identification of structure, observation of existing position, and measurement of average particle diameter (average equivalent circle diameter) and occupancy ratio are 500 times to 1000 times by corroding a steel sheet rolling section or a section perpendicular to the rolling direction with a night reagent. was quantified by observation with an optical microscope. The V-bending characteristics were tested in accordance with JISZ2248, and punches 0.5 mm, 1 mm, and 2 mm were evaluated. The visual judgment was as follows, and “ ⁇ ” was accepted. ⁇ : No cracking ⁇ : Slight cracking (several cracks occur on the outer surface of the bend) ⁇ : Crack occurrence
- the method for measuring the retained austenite ratio is performed on a surface that is chemically polished to a thickness of 1/4 from the surface layer of the specimen plate, and the strength of the ferrite (200) and (211) areas by the mono-colored MoK ⁇ rays is increased. Residual austenite was quantified from the (200), (220) and (311) area strengths of stenite.
- the method for measuring the residual stress ( ⁇ R) of the retained austenite phase was performed on a surface that had been chemically polished from the surface layer of the specimen plate to 1 ⁇ 4 thickness, and was obtained from an average value of 10 points using a high-resolution X-ray diffractometer.
- the high-resolution X-ray diffractometer used in this experiment is Bruker AXS's D8 DISCOVER Hybrid Super Speed Solution.
- the residual stress ( ⁇ R) can be obtained from the following equation (2) using the strain ( ⁇ R) obtained from the diffraction surface interval distribution from the apparatus and the Young's modulus (E) of the steel material.
- ⁇ R ⁇ R ⁇ E (2)
- Experiment No. “A” to “o” are examples of the present invention, and all the characteristics passed, and a steel sheet having the target characteristics was obtained. On the other hand, in Experiment No. in which the component or production method is outside the scope of the present invention. One of the characteristics of “p” to “ag” is rejected.
- a high-strength hot-dip galvanized steel sheet excellent in elongation and V bendability is provided.
- the hot-dip galvanized steel sheet can be manufactured relatively easily and stably. For this reason, the hot-dip galvanized steel sheet of the present invention can be optimally used particularly as a steel sheet for automobiles aiming at weight reduction in recent years, and its industrial value is extremely large.
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)
- Heat Treatment Of Sheet Steel (AREA)
- Coating With Molten Metal (AREA)
Abstract
Description
高強度鋼板において,残留オーステナイトを鋼組織に持つ残留オーステナイト鋼は、 TRIP効果を利用して、高強度であるにも関わらず、非常に高い伸びをもつことが知られている。この残留オーステナイト鋼において、さらに伸びを高めるべく、例えば、特許文献1では、残留オーステナイトの分率を高く確保しつつ、2種類のフェライト(ベイニティックフェライト、ポリゴナルフェライト)を制御して均一伸びを確保する技術が開示されている。
一方、引張強度が980MPa以上の高強度鋼板の成形においては、引張強度が440MPa以下の低強度鋼板成形時に主体的であった絞り成形ではなく、曲げ成形を中心に加工されることが多い。高強度鋼板においても伸び同様に曲げ性の向上が求められる。
また、特許文献3には、体積分率で30~90%のフェライト相、5%以上のベイナイト、10%以下のマルテンサイト、および5~30%の残留オーステナイト相を含む高強度高延性溶融亜鉛めっき鋼板が開示されている。特許文献4には、鋼板に含まれる転位の密度が8×1011(個/mm2)以下であり、歪速度0.0067(s-1)での準静的強度(FS1)と、歪速度1000(s-1)での動的強度(FS2)との比からなる静動比(=FS2/FS1)が1.05以上である高強度冷延鋼板が開示されている。
しかしながら、現在、高強度鋼板においても更に高い強度、加工性が要求されており、これらの要求にこたえられる、十分に高いレベルでの伸びとV曲げ性を両立する技術は知られていない。
残留オーステナイト鋼は焼鈍中のフェライト変態、ベイナイト変態を制御して、オーステナイト中のC濃度を高めることで、製品の鋼組織にオーステナイトを残し、この残留オーステナイトのTRIP効果によって、高い伸びを持つ高強度鋼板である。しかしながら、混合組織であることから、このような残留オーステナイト鋼は曲げ性に優れた鋼ではなかったものと推定される。
これに対して、本発明者らは、TRIP効果を曲げ性に効果的に作用させるべく、C、Si、Mn量を変えた種々の鋼について、実験室で溶解、熱延、冷延、焼鈍、溶融亜鉛めっきを行い、所用の引張強度、延性、V曲げ性、めっき性を得るための方法を種々検討した。
このような鋭意検討の結果、上記目的に効果的な種々の成分を特定するのみならず、残留オーステナイト相への圧縮の残留応力を付与することが、残留オーステナイトの安定性をこれまで以上に高めるのみならず、曲げ外側の引張応力部曲げ内側の圧縮応力部曲げの局部変形に有効にも作用することを見出した。
本発明は、例えば、以下の態様を包含することができる。
C:0.10%以上、0.4%以下、
Si:0.01%以上、0.5%以下、
Mn:1.0%以上、3.0%以下、
O:0.006%以下、
P:0.04%以下、
S:0.01%以下、
Al:0.1以上、3.0%以下、
N:0.01%以下、
Si+Al≧0.5%を含有し、残部Feおよび不可避不純物からなる鋼板であって、
さらに該鋼板が、体積分率で主相としてフェライトを40%以上とし、残留オーステナイトを8%以上~60%以下含有し、残部組織がベイナイト、マルテンサイト、パーライトのいずれか1種又は2種以上より成る高強度溶融亜鉛めっき鋼板であり、
前記オーステナイトのうち、平均残留応力σRが式(1)を満たす範囲にあるオーステナイト粒が50%以上であり、
-400MPa≦σR ≦200MPa (1)
前記鋼板表面に、Feを7質量%未満を含有し、残部がZn、Alおよび不可避的不純物からなる溶融亜鉛めっき層を有することを特徴とする溶融亜鉛めっき鋼板。
Mo:0.02%以上、0.5%以下、
Nb:0.01%以上、0.10%以下、
Ti:0.01%以上、0.20%以下、
V:0.005%以上、0.10%以下、
Cr:0.1%以上、2.0%以下、
Ca:0.0005%以上、0.05%以下、
Mg:0.0005%以上、0.05%以下、
REM:0.0005%以上、0.05%以下、
Cu:0.04%以上、2.0%以下、
Ni:0.02%以上、1.0%以下、
B:0.0003%以上、0.007%以下
の1種または2種以上を含有することを特徴とする〔1〕~〔3〕のいずれか1項に記載の溶融亜鉛めっき鋼板。
C:0.10%以上、0.4%以下、
Si:0.01%以上、0.5%以下、
Mn:1.0%以上、3.0%以下、
O:0.006%以下、
P:0.04%以下、
S:0.01%以下、
Al:0.1以上、3.0%以下、
N:0.01%以下、
Si+Al≧0.5%を含有し、残部Feおよび不可避不純物からなる鋼材に;
熱延スラブ温度が1100℃以上、仕上げ温度が850~970℃で熱間圧延処理を施し、
前記熱間圧延後の鋼板を、650℃以下の温度域まで平均で10~200℃/秒で冷却し、650℃以下の温度範囲で巻取り、
該鋼板に圧下率40%以上で冷間圧延を施し、
焼鈍時の最高温度が700~900℃で焼鈍し、平均で0.1~200℃/秒の冷却速度で350℃~550℃の温度域内に冷却し、その後、該温度域内で1秒以上、1000秒以下保持し、
該温度域内で保持後の鋼板を、溶融亜鉛めっき浴に浸漬し、該めっき処理後、470~580℃の温度範囲で合金化処理を施し、且つ
前記鋼板を350℃~550℃の温度域内で保持するに際して、ロール径が50~2000mmのロールを用いて鋼板を繰り返し折り曲げることにより、該鋼板に歪みを付与し、さらに、
該繰り返し折り曲げ時に前記鋼板に印加される長手方向の平均応力が2~50MPaであることを特徴とする溶融亜鉛めっき鋼板の製造方法。
〔6〕 前記繰り返し折り曲げ時のパス数が2~6パスであることを特徴とする〔5〕に記載の溶融亜鉛めっき鋼板の製造方法。
これを達成するためには、図2に示すように、このオーステナイト粒の平均残留応力σRが式(1)を満たす範囲でΣrが最小となる。また図3に示すように、この式(1)を満足するオーステナイト粒が50%以上ある場合、安定して最小曲げ半径Rが最小となる。
-400MPa≦σR ≦200MPa (1)
C:Cは、鋼板の強度を上昇できる元素である。しかしながら、0.1%未満であると980MPa以上の引張強度と加工性を両立することが難しくなる。一方、0.40%超となるとスポット溶接性の確保が困難となる。このため、C含有量の範囲を0.1~0.40%以下とする。C含有量は、0.1~0.38であることが好ましく、0.12~0.38であることが更に好ましい。
本発明において、Al+Siは、0.5%以上である。このAl+Siは、0.5~4%であることが好ましく、0.51~3.5%であることが更に好ましい。
本鋼板では、主相をフェライトとし、体積率8%以上の残留オーステナイトを分散させることで、980MPa以上の引張最大強度を確保している。このことから、残留オーステナイトを含む必要がある。フェライト相の形態としてはポリゴナルフェライトの他に、アシキュラーフェライトを含んでも良い。主相をフェライトとしたのは、延性に富むフェライトを主相とすることで延性を向上させるためである。主相フェライト相が40%未満では十分な延性を確保できず実用に適さないことから、主相フェライトの体積分率は40%以上とする。
熱間圧延前のスラブは、連続鋳造後に通常の熱延を施す。
例えば、連続鋳造後そのまま、または、再加熱により1100℃以上とする。この温度未満では、均質処理が不十分で、強度とV曲げ性の低下を起こす。
次いで、仕上げ温度を850℃以上、970℃以下としてスラブを熱間圧延する。仕上げ温度が、850℃未満では(α+γ)2相域圧延となり、延性の低下をもたらすからであり、970℃を超えるとオーステナイト粒径が粗大になって、フェライト相分率が小さくなって、延性が低下するからである。
酸洗後は試作材に40%以上の冷間圧延を施すことができる。これ未満では、焼鈍中の再結晶や逆変態が抑制されて、伸びの低下を起こす。
さらに、パス数については、数が多いほど曲げ・曲げ戻しの回数が増え、残留応力制御が容易になるが、1パスではその効果が小さい。したがって、2パス以上が通常は好ましい。この曲げ回数は、6パス以下であることが好ましく、5パス以下であることが更に好ましい。
表1に示した成分組成を有する鋼を製造し、冷却凝固後1200℃まで再加熱し、880℃にて仕上圧延を行い、冷却後550℃まで,平均冷却速度60℃/秒冷却後、表2の巻取り温度で巻取りを行った。その後、この熱延板を50%の冷間圧延した。その後連続焼鈍にて、表2に示した条件にて、焼鈍処理を行った。
実生産ラインでの過時効(OA)処理時の繰り返し曲げにおけるロール径、張力、パス数の効果を想定し、焼鈍処理のOA時に複数の異なる局率、張力、回数を付与し、残留応力に与える影響を評価した。
引張特性は、JIS5号引張試験片のC方向引張にて評価した。組織の同定、存在位置の観察および平均粒径(平均円相当径)と占有率の測定は、ナイタ-ル試薬により鋼板圧延方向断面または圧延方向と直角な断面を腐食して500倍~1000倍の光学顕微鏡観察により定量化した。
V曲げ特性は、JISZ2248に則した試験を行い、パンチR0.5mm、1mm、2mmについて実施し、目視観察で下記のように判断し、「○」を合格とした。
○:ワレ無し
△:微ワレ発生(複数のクラックが曲げ外表面に発生)
×:ワレ発生
σR=εR×E (2)
Claims (6)
- 質量%で、
C:0.10%以上、0.4%以下、
Si:0.01%以上、0.5%以下、
Mn:1.0%以上、3.0%以下、
O:0.006%以下、
P:0.04%以下、
S:0.01%以下、
Al:0.1以上、3.0%以下、
N:0.01%以下、
Si+Al≧0.5%を含有し、残部Feおよび不可避不純物からなる鋼板であって、
さらに該鋼板が、体積分率で主相としてフェライトを40%以上とし、残留オーステナイトを8%以上~60%以下含有し、残部組織がベイナイト、マルテンサイト、パーライトのいずれか1種又は2種以上より成る高強度溶融亜鉛めっき鋼板であり、
前記オーステナイトのうち、平均残留応力σRが式(1)を満たす範囲にあるオーステナイト粒が50%以上であり、
-400MPa≦σR≦200MPa (1)
前記鋼板表面に、Feを7質量%未満を含有し、残部がZn、Alおよび不可避的不純物からなる溶融亜鉛めっき層を有することを特徴とする溶融亜鉛めっき鋼板。 - 前記オーステナイトの平均粒径が10μm以下、オーステナイト中の平均C濃度が質量%で0.7%以上、1.5%以下であることを特徴とする請求項1に記載の溶融亜鉛めっき鋼板。
- 前記オーステナイト粒の圧延方向に対する平均アスペクト比が0.5以上、0.95以下であることを特徴とする請求項1または2に記載の溶融亜鉛めっき鋼板。
- さらに、質量%で、
Mo:0.02%以上、0.5%以下、
Nb:0.01%以上、0.10%以下、
Ti:0.01%以上、0.20%以下、
V:0.005%以上、0.10%以下、
Cr:0.1%以上、2.0%以下、
Ca:0.0005%以上、0.05%以下、
Mg:0.0005%以上、0.05%以下、
REM:0.0005%以上、0.05%以下、
Cu:0.04%以上、2.0%以下、
Ni:0.02%以上、1.0%以下、
B:0.0003%以上、0.007%以下
の1種または2種以上を含有することを特徴とする請求項1または2に記載の溶融亜鉛めっき鋼板。 - 質量%で、
C:0.10%以上、0.4%以下、
Si:0.01%以上、0.5%以下、
Mn:1.0%以上、3.0%以下、
O:0.006%以下、
P:0.04%以下、
S:0.01%以下、
Al:0.1以上、3.0%以下、
N:0.01%以下、
Si+Al≧0.5%を含有し、残部Feおよび不可避不純物からなる鋼材に;
熱延スラブ温度が1100℃以上、仕上げ温度が850~970℃で熱間圧延処理を施し、
前記熱間圧延後の鋼板を、650℃以下の温度域まで平均で10~200℃/秒で冷却し、650℃以下の温度範囲で巻取り、
該鋼板に圧下率40%以上で冷間圧延を施し、
焼鈍時の最高温度が700~900℃で焼鈍し、平均で0.1~200℃/秒の冷却速度で350℃~550℃の温度域内に冷却し、その後、該温度域内で1秒以上、1000秒以下保持し、
該温度域内で保持後の鋼板を、溶融亜鉛めっき浴に浸漬し、該めっき処理後、470~580℃の温度範囲で合金化処理を施し、且つ
前記鋼板を350℃~550℃の温度域内で保持するに際して、ロール径が50~2000mmのロールを用いて鋼板を繰り返し折り曲げることにより、該鋼板に歪みを付与し、さらに、
該繰り返し折り曲げ時に前記鋼板に印加される長手方向の平均応力が2~50MPaであることを特徴とする溶融亜鉛めっき鋼板の製造方法。 - 前記繰り返し折り曲げ時のパス数が2~6パスであることを特徴とする請求項5に記載の溶融亜鉛めっき鋼板の製造方法。
Priority Applications (13)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014117650/02A RU2573455C2 (ru) | 2011-09-30 | 2012-09-28 | Высокопрочный, гальванизированный горячим способом стальной лист и способ его получения |
ES12834788.7T ES2645994T3 (es) | 2011-09-30 | 2012-09-28 | Chapa de acero de alta resistencia, galvanizada por inmersión en caliente, y proceso para producirla |
JP2013516046A JP5310968B1 (ja) | 2011-09-30 | 2012-09-28 | 高強度溶融亜鉛めっき鋼板及びその製造方法 |
MX2014003797A MX369428B (es) | 2011-09-30 | 2012-09-28 | Láminas de acero de alta resistencia, galvanizadas por inmersión en caliente y proceso para producir las mismas. |
KR1020147006820A KR101608605B1 (ko) | 2011-09-30 | 2012-09-28 | 고강도 용융 아연 도금 강판 및 그 제조 방법 |
CN201280047853.XA CN103857814B (zh) | 2011-09-30 | 2012-09-28 | 高强度热浸镀锌钢板及其制造方法 |
EP12834788.7A EP2762579B2 (en) | 2011-09-30 | 2012-09-28 | High-strength hot-dip galvanized steel sheet and process for producing same |
PL12834788T PL2762579T3 (pl) | 2011-09-30 | 2012-09-28 | Blacha stalowa cienka cynkowana na gorąco o dużej wytrzymałości i sposób jej wytwarzania |
BR112014007530-1A BR112014007530B1 (pt) | 2011-09-30 | 2012-09-28 | chapa de aço galvanizada por imersão a quente de alta resistência e processo para produção da mesma |
US14/348,538 US9551055B2 (en) | 2011-09-30 | 2012-09-28 | Process for producing high-strength hot-dip galvanized steel sheet |
CA2849285A CA2849285C (en) | 2011-09-30 | 2012-09-28 | High-strength hot-dip galvanized steel sheet and process for producing the same |
ZA2014/02309A ZA201402309B (en) | 2011-09-30 | 2014-03-27 | High-strength hot-dip galvanized steel sheet and process for producing the same |
US15/376,305 US10351936B2 (en) | 2011-09-30 | 2016-12-12 | High-strength hot-dip galvanized steel sheet and process for producing the same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2011-217143 | 2011-09-30 | ||
JP2011217143 | 2011-09-30 |
Related Child Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US14/348,538 A-371-Of-International US9551055B2 (en) | 2011-09-30 | 2012-09-28 | Process for producing high-strength hot-dip galvanized steel sheet |
US15/376,305 Division US10351936B2 (en) | 2011-09-30 | 2016-12-12 | High-strength hot-dip galvanized steel sheet and process for producing the same |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2013047808A1 true WO2013047808A1 (ja) | 2013-04-04 |
Family
ID=47995831
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2012/075194 WO2013047808A1 (ja) | 2011-09-30 | 2012-09-28 | 高強度溶融亜鉛めっき鋼板及びその製造方法 |
Country Status (14)
Country | Link |
---|---|
US (2) | US9551055B2 (ja) |
EP (1) | EP2762579B2 (ja) |
JP (1) | JP5310968B1 (ja) |
KR (1) | KR101608605B1 (ja) |
CN (1) | CN103857814B (ja) |
BR (1) | BR112014007530B1 (ja) |
CA (1) | CA2849285C (ja) |
ES (1) | ES2645994T3 (ja) |
MX (1) | MX369428B (ja) |
PL (1) | PL2762579T3 (ja) |
RU (1) | RU2573455C2 (ja) |
TW (1) | TWI504757B (ja) |
WO (1) | WO2013047808A1 (ja) |
ZA (1) | ZA201402309B (ja) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015196843A (ja) * | 2014-03-31 | 2015-11-09 | Jfeスチール株式会社 | 鋼帯内における材質のバラツキが小さい成形性に優れた高強度合金化溶融亜鉛めっき鋼帯およびその製造方法 |
WO2016132680A1 (ja) * | 2015-02-17 | 2016-08-25 | Jfeスチール株式会社 | 高強度冷延薄鋼板およびその製造方法 |
WO2016136625A1 (ja) * | 2015-02-27 | 2016-09-01 | 株式会社神戸製鋼所 | 高強度高延性鋼板 |
JP2019506530A (ja) * | 2016-01-18 | 2019-03-07 | アルセロールミタル | 優れた成形性を有する高強度鋼板及びこれを製造する方法 |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107148488B (zh) * | 2015-01-07 | 2020-02-07 | Posco公司 | 拉伸强度为1300Mpa以上的超高强度镀覆钢板及其制造方法 |
CN105986175B (zh) * | 2015-03-02 | 2018-01-16 | 中国钢铁股份有限公司 | 高强度高延展性钢材的制造方法 |
MX2018007185A (es) | 2015-12-15 | 2018-08-01 | Tata Steel Ijmuiden Bv | Cinta de acero galvanizada por inmersion en caliente de alta resistencia. |
KR102115278B1 (ko) | 2016-02-25 | 2020-05-26 | 닛폰세이테츠 가부시키가이샤 | 내충격 박리성 및 가공부 내식성이 우수한 고강도 용융 아연 도금 강판 |
KR102557715B1 (ko) | 2016-05-10 | 2023-07-20 | 유나이테드 스테이츠 스틸 코포레이션 | 고강도 철강 제품 및 이의 제조를 위한 소둔 공정 |
US11993823B2 (en) | 2016-05-10 | 2024-05-28 | United States Steel Corporation | High strength annealed steel products and annealing processes for making the same |
US11560606B2 (en) | 2016-05-10 | 2023-01-24 | United States Steel Corporation | Methods of producing continuously cast hot rolled high strength steel sheet products |
CN106801198B (zh) * | 2017-02-07 | 2018-02-09 | 和县隆盛精密机械有限公司 | 一种适用于机械臂弯曲件的合金铸件及其热处理工艺 |
CN110337505B (zh) | 2017-02-28 | 2021-06-29 | 杰富意钢铁株式会社 | 高强度钢板及其制造方法 |
CN111247264A (zh) * | 2017-10-20 | 2020-06-05 | 杰富意钢铁株式会社 | 高强度钢板及其制造方法 |
MX2020004029A (es) | 2017-10-20 | 2020-08-13 | Jfe Steel Corp | Lamina de acero de alta resistencia y metodo para la fabricacion de la misma. |
JP6787523B1 (ja) * | 2019-01-30 | 2020-11-18 | Jfeスチール株式会社 | 高強度鋼板およびその製造方法 |
CN113330127B (zh) * | 2019-03-06 | 2022-10-25 | 日本制铁株式会社 | 热轧钢板 |
MX2021008807A (es) * | 2019-03-06 | 2021-08-24 | Nippon Steel Corp | Lamina de acero laminada en caliente. |
CN110202868B (zh) * | 2019-07-15 | 2021-03-23 | 哈尔滨工业大学 | 一种Nb/高Nb-TiAl层状复合材料及其制备方法 |
US12116688B2 (en) * | 2019-12-20 | 2024-10-15 | Nippon Steel Corporation | Ni-plated steel sheet, and method for manufacturing Ni-plated steel sheet |
WO2021182395A1 (ja) | 2020-03-11 | 2021-09-16 | 日本製鉄株式会社 | 熱延鋼板 |
KR102678185B1 (ko) * | 2022-04-20 | 2024-06-26 | 닛폰세이테츠 가부시키가이샤 | 용융 도금 강재 |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59219473A (ja) | 1983-05-26 | 1984-12-10 | Nippon Steel Corp | カラ−エツチング液及びエツチング方法 |
JPH0488125A (ja) | 1990-07-30 | 1992-03-23 | Nippon Steel Corp | 伸びフランジ性と延性の優れた高強度熱延鋼板の製造方法 |
JP2002030403A (ja) | 2000-07-14 | 2002-01-31 | Sumitomo Metal Ind Ltd | 合金化溶融亜鉛めっき鋼板とその製造方法 |
JP2003306746A (ja) | 2002-04-18 | 2003-10-31 | Jfe Steel Kk | 加工性に優れた高張力鋼板ならびにその製造方法および加工方法 |
JP2005133201A (ja) | 2003-08-29 | 2005-05-26 | Kobe Steel Ltd | 加工性に優れた高張力鋼板およびその製法 |
JP2006265671A (ja) * | 2005-03-25 | 2006-10-05 | Nisshin Steel Co Ltd | 加工性及び耐溶融金属脆化割れ性に優れた合金化溶融亜鉛めっき高張力鋼板 |
JP2008189985A (ja) * | 2007-02-02 | 2008-08-21 | Sumitomo Metal Ind Ltd | 局部延性能に優れた熱延鋼板及びその製造方法 |
WO2011065591A1 (ja) * | 2009-11-30 | 2011-06-03 | 新日本製鐵株式会社 | 耐水素脆化特性に優れた引張最大強度900MPa以上の高強度鋼板及びその製造方法 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0613958B1 (en) | 1992-05-25 | 2000-08-23 | Nippon Steel Corporation | Process for continuously annealing steel strip |
KR960016462B1 (ko) | 1994-03-02 | 1996-12-12 | 신니뽄 세이데스 가부시끼가이샤 | 강 스트립의 연속어닐링장치 및 그의 장력제어장치와 장력제어방법 |
EP1431406A1 (en) * | 2002-12-20 | 2004-06-23 | Sidmar N.V. | A steel composition for the production of cold rolled multiphase steel products |
ATE471996T1 (de) * | 2003-03-31 | 2010-07-15 | Nippon Steel Corp | Nach dem heisstauchverfahren mit legiertem zink beschichtetes stahlblech und herstellungsverfahren dafür |
CA2521710C (en) * | 2003-04-10 | 2009-09-29 | Nippon Steel Corporation | High strength molten zinc plated steel sheet and process of production of same |
JP4235030B2 (ja) * | 2003-05-21 | 2009-03-04 | 新日本製鐵株式会社 | 局部成形性に優れ溶接部の硬さ上昇を抑制した引張強さが780MPa以上の高強度冷延鋼板および高強度表面処理鋼板 |
JP5250938B2 (ja) | 2005-03-31 | 2013-07-31 | Jfeスチール株式会社 | 延性に優れる低降伏比型高強度合金化溶融亜鉛めっき鋼板およびその製造方法 |
JP5250939B2 (ja) | 2005-03-31 | 2013-07-31 | 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 |
JP4956998B2 (ja) | 2005-05-30 | 2012-06-20 | Jfeスチール株式会社 | 成形性に優れた高強度溶融亜鉛めっき鋼板およびその製造方法 |
RU2418094C2 (ru) * | 2006-01-30 | 2011-05-10 | Ниппон Стил Корпорейшн | Высокопрочный горячеоцинкованный погружением стальной лист и высокопрочный отожженный после цинкования стальной лист с превосходными формуемостью и способностью к нанесению гальванопокрытия и способы изготовления и устройства для изготовления таких листов |
EP1887746A1 (de) | 2006-08-09 | 2008-02-13 | MintNet GmbH | Sicherungssystem und -verfahren für elektronische Post |
EP2009127A1 (en) * | 2007-06-29 | 2008-12-31 | ArcelorMittal France | Process for manufacturing a galvanized or a galvannealed steel sheet by DFF regulation |
EP2009129A1 (en) * | 2007-06-29 | 2008-12-31 | ArcelorMittal France | Process for manufacturing a galvannealed steel sheet by DFF regulation |
CN101999007B (zh) | 2008-04-10 | 2012-12-12 | 新日本制铁株式会社 | 扩孔性和延展性的平衡极良好、疲劳耐久性也优异的高强度钢板和镀锌钢板以及这些钢板的制造方法 |
JP5479366B2 (ja) | 2009-04-22 | 2014-04-23 | 新日鉄住金エンジニアリング株式会社 | 冷延鋼板の製造方法及びその製造設備 |
JP5651964B2 (ja) | 2010-02-16 | 2015-01-14 | 新日鐵住金株式会社 | 延性及び穴広げ性並びに耐食性に優れた合金化溶融亜鉛めっき鋼板及びその製造方法 |
JP5488129B2 (ja) * | 2010-03-31 | 2014-05-14 | 新日鐵住金株式会社 | 冷延鋼板およびその製造方法 |
-
2012
- 2012-09-28 WO PCT/JP2012/075194 patent/WO2013047808A1/ja active Application Filing
- 2012-09-28 MX MX2014003797A patent/MX369428B/es active IP Right Grant
- 2012-09-28 RU RU2014117650/02A patent/RU2573455C2/ru not_active IP Right Cessation
- 2012-09-28 US US14/348,538 patent/US9551055B2/en active Active
- 2012-09-28 KR KR1020147006820A patent/KR101608605B1/ko active IP Right Grant
- 2012-09-28 CN CN201280047853.XA patent/CN103857814B/zh active Active
- 2012-09-28 BR BR112014007530-1A patent/BR112014007530B1/pt not_active IP Right Cessation
- 2012-09-28 TW TW101135893A patent/TWI504757B/zh not_active IP Right Cessation
- 2012-09-28 CA CA2849285A patent/CA2849285C/en not_active Expired - Fee Related
- 2012-09-28 EP EP12834788.7A patent/EP2762579B2/en active Active
- 2012-09-28 ES ES12834788.7T patent/ES2645994T3/es active Active
- 2012-09-28 PL PL12834788T patent/PL2762579T3/pl unknown
- 2012-09-28 JP JP2013516046A patent/JP5310968B1/ja active Active
-
2014
- 2014-03-27 ZA ZA2014/02309A patent/ZA201402309B/en unknown
-
2016
- 2016-12-12 US US15/376,305 patent/US10351936B2/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59219473A (ja) | 1983-05-26 | 1984-12-10 | Nippon Steel Corp | カラ−エツチング液及びエツチング方法 |
JPH0488125A (ja) | 1990-07-30 | 1992-03-23 | Nippon Steel Corp | 伸びフランジ性と延性の優れた高強度熱延鋼板の製造方法 |
JP2002030403A (ja) | 2000-07-14 | 2002-01-31 | Sumitomo Metal Ind Ltd | 合金化溶融亜鉛めっき鋼板とその製造方法 |
JP2003306746A (ja) | 2002-04-18 | 2003-10-31 | Jfe Steel Kk | 加工性に優れた高張力鋼板ならびにその製造方法および加工方法 |
JP2005133201A (ja) | 2003-08-29 | 2005-05-26 | Kobe Steel Ltd | 加工性に優れた高張力鋼板およびその製法 |
JP2006265671A (ja) * | 2005-03-25 | 2006-10-05 | Nisshin Steel Co Ltd | 加工性及び耐溶融金属脆化割れ性に優れた合金化溶融亜鉛めっき高張力鋼板 |
JP2008189985A (ja) * | 2007-02-02 | 2008-08-21 | Sumitomo Metal Ind Ltd | 局部延性能に優れた熱延鋼板及びその製造方法 |
WO2011065591A1 (ja) * | 2009-11-30 | 2011-06-03 | 新日本製鐵株式会社 | 耐水素脆化特性に優れた引張最大強度900MPa以上の高強度鋼板及びその製造方法 |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2015196843A (ja) * | 2014-03-31 | 2015-11-09 | Jfeスチール株式会社 | 鋼帯内における材質のバラツキが小さい成形性に優れた高強度合金化溶融亜鉛めっき鋼帯およびその製造方法 |
WO2016132680A1 (ja) * | 2015-02-17 | 2016-08-25 | Jfeスチール株式会社 | 高強度冷延薄鋼板およびその製造方法 |
JPWO2016132680A1 (ja) * | 2015-02-17 | 2017-04-27 | Jfeスチール株式会社 | 高強度冷延薄鋼板およびその製造方法 |
US20180057916A1 (en) * | 2015-02-17 | 2018-03-01 | Jfe Steel Corporation | Thin high-strength cold-rolled steel sheet and method of producing the same |
US10626485B2 (en) | 2015-02-17 | 2020-04-21 | Jfe Steel Corporation | Thin high-strength cold-rolled steel sheet and method of producing the same |
WO2016136625A1 (ja) * | 2015-02-27 | 2016-09-01 | 株式会社神戸製鋼所 | 高強度高延性鋼板 |
JP2016160467A (ja) * | 2015-02-27 | 2016-09-05 | 株式会社神戸製鋼所 | 高強度高延性鋼板 |
JP2019506530A (ja) * | 2016-01-18 | 2019-03-07 | アルセロールミタル | 優れた成形性を有する高強度鋼板及びこれを製造する方法 |
US11466335B2 (en) | 2016-01-18 | 2022-10-11 | Arcelormittal | High strength steel sheet having excellent formability and a method of manufacturing the steel sheet |
Also Published As
Publication number | Publication date |
---|---|
PL2762579T3 (pl) | 2018-01-31 |
CA2849285A1 (en) | 2013-04-04 |
CN103857814A (zh) | 2014-06-11 |
KR20140048331A (ko) | 2014-04-23 |
BR112014007530B1 (pt) | 2018-12-11 |
US9551055B2 (en) | 2017-01-24 |
JP5310968B1 (ja) | 2013-10-09 |
US10351936B2 (en) | 2019-07-16 |
US20170088922A1 (en) | 2017-03-30 |
EP2762579B1 (en) | 2017-08-16 |
RU2014117650A (ru) | 2015-11-10 |
CA2849285E (en) | 2013-04-04 |
EP2762579A1 (en) | 2014-08-06 |
MX2014003797A (es) | 2014-11-13 |
ES2645994T3 (es) | 2017-12-11 |
TWI504757B (zh) | 2015-10-21 |
EP2762579B2 (en) | 2021-03-03 |
CA2849285C (en) | 2016-04-19 |
KR101608605B1 (ko) | 2016-04-01 |
CN103857814B (zh) | 2016-01-20 |
JPWO2013047808A1 (ja) | 2015-03-30 |
ZA201402309B (en) | 2015-03-25 |
TW201317366A (zh) | 2013-05-01 |
MX369428B (es) | 2019-11-08 |
BR112014007530A2 (pt) | 2017-04-04 |
US20140227556A1 (en) | 2014-08-14 |
RU2573455C2 (ru) | 2016-01-20 |
EP2762579A4 (en) | 2015-07-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5310968B1 (ja) | 高強度溶融亜鉛めっき鋼板及びその製造方法 | |
KR102407357B1 (ko) | 고강도 냉연 강판 및 그의 제조 방법 | |
US8657969B2 (en) | High-strength galvanized steel sheet with excellent formability and method for manufacturing the same | |
US9580779B2 (en) | High strength steel sheet having excellent formability and method for manufacturing the same | |
US8430975B2 (en) | High strength galvanized steel sheet with excellent formability | |
JP6292353B2 (ja) | 薄鋼板及びめっき鋼板、並びに薄鋼板の製造方法及びめっき鋼板の製造方法 | |
JP6274360B2 (ja) | 高強度亜鉛めっき鋼板、高強度部材及び高強度亜鉛めっき鋼板の製造方法 | |
JP2011195956A (ja) | 伸びと穴拡げに優れた高強度薄鋼板およびその製造方法 | |
US20220220577A1 (en) | High strength member, method for manufacturing high strength member, and method for manufacturing steel sheet for high strength member | |
KR102544887B1 (ko) | 고강도 용융 아연 도금 강판 및 그의 제조 방법 | |
US11186889B2 (en) | High-strength steel sheet and manufacturing method therefor | |
KR102217100B1 (ko) | 고강도 강판 및 그 제조 방법 | |
JP6032173B2 (ja) | 引張最大強度980MPaを有する耐遅れ破壊特性に優れた高強度鋼板、高強度溶融亜鉛めっき鋼板、並びに、高強度合金化溶融亜鉛めっき鋼板 | |
WO2023153096A1 (ja) | 冷延鋼板 | |
WO2023153097A1 (ja) | 冷延鋼板およびその製造方法 | |
WO2022190959A1 (ja) | 冷延鋼板及びその製造方法 | |
WO2022190958A1 (ja) | 冷延鋼板及びその製造方法 | |
WO2024190415A1 (ja) | 鋼板 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ENP | Entry into the national phase |
Ref document number: 2013516046 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: 12834788 Country of ref document: EP Kind code of ref document: A1 |
|
ENP | Entry into the national phase |
Ref document number: 20147006820 Country of ref document: KR Kind code of ref document: A |
|
ENP | Entry into the national phase |
Ref document number: 2849285 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: 14348538 Country of ref document: US Ref document number: MX/A/2014/003797 Country of ref document: MX |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
ENP | Entry into the national phase |
Ref document number: 2014117650 Country of ref document: RU Kind code of ref document: A |
|
REEP | Request for entry into the european phase |
Ref document number: 2012834788 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2012834788 Country of ref document: EP |
|
REG | Reference to national code |
Ref country code: BR Ref legal event code: B01A Ref document number: 112014007530 Country of ref document: BR |
|
ENP | Entry into the national phase |
Ref document number: 112014007530 Country of ref document: BR Kind code of ref document: A2 Effective date: 20140328 |