EP3186406B1 - Bande en acier à faible teneur en alliage, à haute résistance et laminé à froid - Google Patents
Bande en acier à faible teneur en alliage, à haute résistance et laminé à froid Download PDFInfo
- Publication number
- EP3186406B1 EP3186406B1 EP15757135.7A EP15757135A EP3186406B1 EP 3186406 B1 EP3186406 B1 EP 3186406B1 EP 15757135 A EP15757135 A EP 15757135A EP 3186406 B1 EP3186406 B1 EP 3186406B1
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- European Patent Office
- Prior art keywords
- strip
- steel strip
- mpa
- sheet
- blank
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- 229910000922 High-strength low-alloy steel Inorganic materials 0.000 title claims description 26
- 229910000831 Steel Inorganic materials 0.000 claims description 42
- 239000010959 steel Substances 0.000 claims description 42
- 230000009467 reduction Effects 0.000 claims description 33
- 238000000137 annealing Methods 0.000 claims description 30
- 239000000203 mixture Substances 0.000 claims description 23
- 238000000576 coating method Methods 0.000 claims description 18
- 239000011248 coating agent Substances 0.000 claims description 16
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 13
- 229910052725 zinc Inorganic materials 0.000 claims description 13
- 239000011701 zinc Substances 0.000 claims description 13
- 238000005097 cold rolling Methods 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 11
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 238000004519 manufacturing process Methods 0.000 claims description 8
- 238000005266 casting Methods 0.000 claims description 6
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 5
- 239000012535 impurity Substances 0.000 claims description 4
- 238000005098 hot rolling Methods 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 239000010936 titanium Substances 0.000 description 20
- 239000011572 manganese Substances 0.000 description 15
- 239000010955 niobium Substances 0.000 description 15
- 229910052719 titanium Inorganic materials 0.000 description 15
- 239000000523 sample Substances 0.000 description 14
- 238000005096 rolling process Methods 0.000 description 12
- 239000002244 precipitate Substances 0.000 description 11
- 238000005728 strengthening Methods 0.000 description 10
- 229910052748 manganese Inorganic materials 0.000 description 9
- 229910052758 niobium Inorganic materials 0.000 description 9
- 229910052720 vanadium Inorganic materials 0.000 description 9
- 229910052799 carbon Inorganic materials 0.000 description 8
- 238000001953 recrystallisation Methods 0.000 description 8
- 239000011651 chromium Substances 0.000 description 7
- 238000001556 precipitation Methods 0.000 description 7
- 239000010949 copper Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 6
- 229910052750 molybdenum Inorganic materials 0.000 description 6
- 229910052710 silicon Inorganic materials 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 5
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 229910052698 phosphorus Inorganic materials 0.000 description 4
- 239000000243 solution Substances 0.000 description 4
- 238000005482 strain hardening Methods 0.000 description 4
- 229910052718 tin Inorganic materials 0.000 description 4
- 239000011135 tin Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 3
- 239000004411 aluminium Substances 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 229910001563 bainite Inorganic materials 0.000 description 3
- 230000000052 comparative effect Effects 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- 229910052717 sulfur Inorganic materials 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- 238000005275 alloying Methods 0.000 description 2
- 229910052787 antimony Inorganic materials 0.000 description 2
- 229910052797 bismuth Inorganic materials 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 239000006101 laboratory sample Substances 0.000 description 2
- 229910052745 lead Inorganic materials 0.000 description 2
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- INZDTEICWPZYJM-UHFFFAOYSA-N 1-(chloromethyl)-4-[4-(chloromethyl)phenyl]benzene Chemical compound C1=CC(CCl)=CC=C1C1=CC=C(CCl)C=C1 INZDTEICWPZYJM-UHFFFAOYSA-N 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 238000003723 Smelting Methods 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 239000010960 cold rolled steel Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- 238000005246 galvanizing Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
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- 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
- 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
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- 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
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- 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
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- 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
- C21D8/0278—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
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- 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
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- 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
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- 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
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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- 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
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- 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
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- 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
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- 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
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- 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
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- 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
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- 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
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- 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
-
- 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
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- 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
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- 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
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- 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
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- 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
- C23F—NON-MECHANICAL REMOVAL OF METALLIC MATERIAL FROM SURFACE; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL; MULTI-STEP PROCESSES FOR SURFACE TREATMENT OF METALLIC MATERIAL INVOLVING AT LEAST ONE PROCESS PROVIDED FOR IN CLASS C23 AND AT LEAST ONE PROCESS COVERED BY SUBCLASS C21D OR C22F OR CLASS C25
- C23F17/00—Multi-step processes for surface treatment of metallic material involving at least one process provided for in class C23 and at least one process covered by subclass C21D or C22F or class C25
Definitions
- the invention relates to a high strength low alloy steel strip, sheet or blank.
- the invention also relates to a method for producing such a high strength low alloy steel strip.
- High strength low alloy steel is well known in the art.
- HSLA steels are often used in the automotive industry.
- HSLA steels are for instance defined in the specification of the Verband Der Automobilindustrie (VDA). Reference is made to the VDA 239-100 Material specification of August 2011.
- VDA Verband Der Automobilindustrie
- cold rolled HSLA steels are indicated with a steel grade number, for instance CR420LA, wherein CR stands for cold rolled, the number 420 stands for the lower limit of the yield strength Rp0,2 in longitudinal direction, and LA stands for low alloy.
- the VDA specification gives a chemical composition for HSLA steels containing Ti and Nb, apart from the standard alloying elements C, Mn, Si and Al, to provide for the high strength.
- Thin HSLA steel strip, sheet or blank is usually coated with an aluminium coating or a zinc coating. If a zinc coating is used, the coating is often applied as a hot dip galvanised or hot dip galvannealed coating.
- JP2007009317 discloses a high-strength cold-rolled steel sheet having excellent formability for an extension flange comprising 0.03-0.15% C, 1.4-3.5% Mn, 0.05% P or less, 0.01% S or less, 0.15% Al or less, 0.01% N or less, 0.005-0.05% Ti, 0.005-0.04% Nb, 0.0003-0.0020% B, balance Fe, and a method of manufacturing it.
- a high strength low alloy steel strip, sheet or blank, coated with zinc or a zinc alloy having the following composition in weight%:
- the inventors have found that when Ti and V are used as a combination of alloying elements, instead of the combination of Ti and Nb as known from the VDA specification, a steel is produced that provides lower mill loads.
- the Ti and V levels have to be used in combination with a specific level for C, Mn and Si, as specified according to the invention. Within the ranges of the invention, it is possible to achieve a yield strength Rp0,2 of at least 420 MPa.
- the HSLA steel according to the invention contains no added Cr, Cu, Mo and Nb. These elements are not needed to provide a HSLA steel with the required yield strength.
- Vanadium provides precipitation strengthening and some grain refinement. At a concentration lower than 0.04 wt% V the volume of vanadium-carbide precipitates is not sufficient to provide enough additional precipitation strengthening to reach a strength of 420 MPa for Rp0,2. At concentrations higher than 0.15 wt% V recrystallisation is suppressed during annealing. This limits elongation.
- Titanium also provides precipitation strengthening and some grain refinement. At concentrations higher than 0.07 wt% Ti the work hardening during cold rolling will rise significantly, limiting a high cold reduction. On the other hand, the inventors have found that a concentration lower than 0.02 wt% Ti will decrease the total elongation of the steel strip, sheet or blank. The combination of the right amount of Ti and V appears to generate a special microstructure providing both a high strength and elongation.
- Carbon is useful to increase the solution strengthening and thus gain more strength. Therefore, at least 0.03 wt% C should be added. However a too high concentration will limit the cold rolling and will decrease the elongation. For this reason, the amount of carbon is limited to 0.07 wt%.
- Nitrogen has an effect similar to that of C.
- This element will combine preferentially with Al and Ti to form AlN and TiN precipitates.
- TiN precipitates are formed at high temperatures already in the re-heating oven, but also during hot rolling and during coiling. They are large precipitates (several microns) that do not increase the strength.
- AlN can also form at high temperature. Nevertheless with a fast cooling and a coiling temperature lower than 650 °C, their precipitation can be partly stopped, keeping in solid solution a source of Al and N that precipitates during the continuous annealing and that may contribute to the precipitation strengthening. If a large amount of N is added (>0.008wt%) elongation is degraded and cracking of slabs occurs.
- Silicon is used for solution strengthening, but at a high concentration (>0.2 wt% Si) it will deteriorate the surface quality.
- the smelting cost to remove the Si becomes too high if the concentration is below 0.01 wt% Si.
- Phosphorus is used for solution strengthening, but a high concentration will deteriorate the steel ductility. Therefore, the concentration should be below 0.03 wt% P.
- Aluminium is used as deoxidizer in steel and its minimum amount should be 0.005 wt% Al to ensure the deoxidation. At a concentration higher than 0.1 wt% Al, the occurrence of surface defects resulting from alumina clusters increases.
- Niobium is kept as low as possible and even avoided because it will increase significantly the work hardening and thus limit the cold reduction of wide strip. Moreover at a concentration higher than 0.03 wt% Nb, it has a great effect on the recrystallisation temperature which makes the use of a high annealing temperature necessary (higher than 800 °C) to obtain reasonably recrystallised HSLA.
- the steel as of claim 1 may contain C: 0.04 - 0.06 Mn: 0.80 - 1.40, preferably Mn: 0.80 - 1.30 Si: 0.01 - 0.1 and preferably Si 0.01 - 0.05 Al: 0.015 - 0.055 Cr: ⁇ 0.05 Cu: ⁇ 0.05 N: 0.002 - 0.008 O: ⁇ 0.005 Ti: 0.02 - 0.06 V: 0.05 - 0.15 Mo: ⁇ 0.01 and preferably 0 ⁇ Mo ⁇ 0.01 Nb: ⁇ 0.02 and preferably Nb: ⁇ 0.01 Ca: ⁇ 0.01.
- Narrowing the Carbon range gives the best elongation for a given strength level. Increasing the minimum C level increases the proof stress of the material. Reducing the upper C level minimises cold rolling loads and achieves the best combination of maximum width and elongation at this higher strength level.
- Narrowing the Aluminium range improves the deoxidation and limits the risk on surface defects.
- Titanium retards recrystallisation. Minimising the maximum Ti level can assist in optimising the elongation for a given strength level.
- Niobium level further assist in being able to roll wider at a given strength level of the cold rolled and annealed product
- Minimising the remaining elements further assist in improving elongation at a given strength level.
- the steel strip, sheet or blank has a yield strength Rp0,2 in longitudinal direction of at least 460 MPa, more preferably a yield strength Rp0,2 of at most 580 MPa.
- the automotive industry prefers to use HSLA steel having such a yield strength, in accordance with the VDA specification.
- the steel strip, sheet or blank has an elongation A80mm in longitudinal direction of at least 15%. This is the elongation a CR460LA steel grade should possess according to the VDA specification.
- the steel strip, sheet or blank has a tensile strength Rm in longitudinal direction of at least 480 MPa, more preferably a tensile strength Rm of at least 520 MPa, more preferably a tensile strength Rm of at most 680 MPa.
- tensile strengths are preferred for by the automotive industry, in accordance with the VDA specification.
- the zinc or zinc alloy coating is a hot dip galvanized or hot dip galvannealed coating. These are the generally used zinc coatings in the automotive industry.
- the zinc alloy coating comprises 0.5 to 4 wt% Al and 0.5 to 3.2 wt% Mg, the remainder being zinc and traces of other elements.
- the coating preferably has a thickness between 5 and 15 ⁇ m per side, more preferably a thickness between 6 and 13 ⁇ m per side.
- This is a so-called AlMgZn coating providing an improved corrosion protection in comparison to the usual zinc coatings.
- the other elements that can be present are Pb or Sb, Ti, Ca, Mn, Sn, La, Ce, Cr, Ni, Zr or Bi.
- Pb, Sn, Bi and Sb are usually added to form spangles. These elements can be present in small amounts, less than 0.5 wt% each, usually less then 0.2 wt% each, often less then 0.2 wt% in total.
- the HSLA strip Due to the coiling temperature, reduction rate and annealing temperature of the strip in accordance with the method of the second aspect of the invention, it is possible to provide the HSLA strip with the composition according to the first aspect of the invention with a yield strength Rp0,2 of at least 420 MPa.
- the coiling temperature is affecting the precipitation of V and mainly VC.
- a small amount of VC is present that helps the cold rolling (less work hardening).
- the volume of VC precipitates will increase, increasing the work hardening and thus making the cold rolling more difficult, which at the end will limit the width of the strip to be cold rolled at the defined cold reduction.
- the VC precipitates will start to coarsen and then the benefit of the precipitation strengthening in the cold rolled annealed end material will be lowered.
- Bainite will increase cold rolling loads. It is preferential to avoid bainite, hence temperatures below 500°C are not recommended.
- the upper limit of the annealing temperature is governed by the coarsening/dissolution of VC precipitates. This upper limit should be at least 20 °C lower than the solubility temperature of VC precipitates.
- the solubility of VC precipitates is depending on the V (and C) concentration. In counter part, the volume of VC precipitates will affect the recrystallisation of the steel; the greater the VC volume, the higher the recrystallisation temperature is.
- V concentration in the steel composition a balance should be found between the cold rolling reduction and the concentration of C, Mn, N and Ti, in order to define a annealing temperature.
- the annealed strip is hot dip coated with a zinc or zinc alloy coating.
- the continuous annealing is directly followed by the hot dip coating with zinc or a zinc alloy.
- the coated strip is cold rolled in a temper mill with a reduction of 0.1 - 3.0 %, preferably 0.2 - 2.0 %.
- the temper rolling provides the strip with an improved surface quality. At higher levels of temper rolling an increased yield strength is seen as well as the removal of yield point elongation (Luders lines).
- the strip is cold rolled at a width of at least 1400 mm, preferably at a width of at least 1600 mm, more preferably at a width of at least 1800 mm, with a gauge of 0.7 - 2.0 mm.
- the HSLA with Ti and V has an improved ductility compared to HSLA with Ti and Nb or with Nb and V.
- the coiling temperature of the hot rolled strip is between 550° C and 600° C and/or the overall cold rolling reduction is 60 - 70 % and/or the annealing temperature is between 760° C and 800° C.
- the steel used in the method has a composition as provided by the preferred embodiment of the composition according to the first aspect of the invention.
- the produced steel strip has a yield strength Rp0,2 of at least 420 MPa, preferably a yield strength Rp0,2 of at least 460 MPa, more preferably a yield strength Rp0,2 of at most 580 MPa.
- the produced steel strip has an elongation A80mm of at least 15%.
- a number of strips has been produced as full production material. Samples of these strips are indicated with the numbers 1, 2, 3 and 4. For each sample a variant A and B is tested, wherein the variants A and B each time have the same composition, see Table 1, but for which variants A and B different coiling temperatures and different temper rolling reductions are used. The information about the coiling temperature and temper rolling reduction, together with the cold reduction percentage and the annealing temperature, is given in Table 2.
- Table 1 composition in wt% Sample C Mn P S Si Al Ti V Nb Mo N 1A 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 1B 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 2A 0,045 1,296 0,01 0,004 0,025 0,031 0,048 0,082 0,001 0,003 0,0047 2B 0,045 1,296 0,01 0,004 0,025 0,031 0,048 0,082 0,001 0,003 0,0047 3A 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 3B 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 4A 0,045 1,296 0,01 0,004 0,025 0,031 0,048 0,082 0,001 0,003
- Table 2 shows that for a composition in accordance with the invention it is possible to reach a yield strength Rp0,2 of at least 420 MPa for a cold reduction of 60 %, and with the right choice of composition, coiling temperature and annealing temperature it is even possible to reach a yield strength Rp0,2 of at least 460 MPa, see samples 2, 3 and 4.
- the temper rolling reduction for these samples has been at most 1 %.
- Table 2 also shows that the elongation A80mm is usually at least 15 % for the samples tested. Only for sample 4A, which has the highest yield strength Rp0,2, the elongation A80mm is slightly lower than 15 %.
- Table 2 processing values and resulting strength and elongation Sample Coiling Temp Cold reduction Annealing Temp Temper Rolling Rp0.2 Rm A80 (°C) (%) (°C) (%) (MPa) (MPa) (%) 1A 600 60 780 0,2 437 514 23,9 1B 550 60 780 1 422 524 20,1 2A 650 60 800 1 463 579 17,0 2B 550 60 800 0,1 460 568 19,9 3A 550 60 780 1 497 569 16,8 3B 600 60 780 1 495 571 15,4 4A 650 60 800 1 532 618 14,6 4B 550 60 800 1 501 590 17
- Table 3 shows laboratory samples 5 and 6 from the same production material as used for sample 1A and 1B, which samples 5 and 6 have been processed with annealing temperatures near the limits or outside the range provided according to the invention.
- Sample 5 shows that with an annealing temperature that is too high, the Rp0,2 will be too low.
- Sample 6 shows that when the annealing temperature is quite low, the elongation A80mm is lower than desired. Samples 5 and 6 thus show that the annealing temperature is quite critical for reaching the desired properties.
- Table 3 processing values and resulting strength and elongation Sample Coiling Temp Cold reduction Annealing Temp Temper Rolling Rp0.2 Rm A80 (°C) (%) (°C) (%) (MPa) (MPa) (%) 5 550 60 830 0 402 450 24,4 6 550 60 760 0 627 527 12,2
- a further number of strips has been produced as full production material as well. Samples of these strips are indicated with the number 1 when they have the same composition as sample 1 above. Other examples are indicated with sample 7 to 14.
- sample 1 a variant C, D and E is tested, wherein the variants each time have the same composition, see Table 6, but for which variants different coiling temperatures and different temper rolling reductions are used.
- sample 7, 8, 9 and 10 a variant A and B has been tested, wherein the variants A and B each time have the same composition, but in most cases a different coiling temperature, annealing temperature or temper rolling reduction is used.
- samples 11 - 14 each time only one variant has been tested.
- Table 6 composition in wt% Sample C Mn P S Si Al Ti V Nb Mo N 1C 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 1D 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 1E 0,045 0,915 0,012 0,004 0,022 0,027 0,047 0,061 0 0,003 0,0039 7A 0,062 0,892 0,013 0,003 0,028 0,032 0,049 0,105 0,001 0,006 0,0029 7B 0,062 0,892 0,013 0,003 0,028 0,032 0,049 0,105 0,001 0,006 0,0029 8A 0,05 0,88 0,01 0,003 0,02 0,034 0,051 0,103 0,001 0,006 0,0038 8B 0,05 0,88 0,01 0,003 0,02 0,034 0,051 0,103 0,001 0,006 0,0038 8B 0,05 0,88 0,01
- Table 7 shows also that for a composition in accordance with the invention it is possible to reach a yield strength Rp0,2 of at least 420 MPa for a cold reduction of 60 or 65 %, and with the right choice of composition, coiling temperature and annealing temperature it is even possible to reach a yield strength Rp0,2 of at least 460 MPa, see samples 1C, 1D, 1E and samples 7A, 7B, 8A, 8B, 11, 12, 13 and 14.
- the temper rolling reduction for most of these samples has been at most 1 %; only for samples 8A, 8B and 14 the temper rolling reduction has been 1,4 %.
- Table 7 also shows that the elongation A80mm is usually at least 15 % for the samples tested. Only for samples 13 and 14, which have a very high yield strength Rp0,2, the elongation A80mm is somewhat lower than 15 %.
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Claims (15)
- Bande, feuille ou flan d'acier, faiblement allié à haute résistance revêtue de zinc ou d'un alliage de zinc, possédant la composition suivante en % en poids :C : 0,03 à 0,07,Mn : 0,70 à 1,60,Si : 0,01 à 0,2,Al : 0,005 à 0,1,Cr : ≤0,1,Cu : ≤0,2,N : ≤0,008,P : ≤0,03,S : ≤0,025,O : ≤0,01,Ti: 0,02 à 0,07,V: 0,04 à 0,15Mo : ≤0,03,Nb : ≤0,03,Ca : ≤0,05,le reste étant du fer et des impuretés inévitables,
ladite bande, feuille ou flan d'acier possédant une limite d'élasticité Rp 0,2 supérieure ou égale à 420 MPa. - Bande, feuille ou flan d'acier selon la revendication 1, dans laquelle Mn : 0,80 à 1,40, de préférence Mn : 0,80 à 1,30.
- Bande, feuille ou flan d'acier selon la revendication 1 ou 2, ladite bande, feuille ou flan d'acier possédant une limite d'élasticité Rp 0,2 selon la direction longitudinale supérieure ou égale à 460 MPa, de préférence une limite d'élasticité Rp 0,2 inférieure ou égale à 580 MPa.
- Bande, feuille ou flan d'acier selon l'une quelconque des revendications précédentes, ladite bande, feuille ou flan d'acier possédant un allongement A 80 mm selon la direction longitudinale d'au moins 15 %.
- Bande, feuille ou flan d'acier selon l'une quelconque des revendications précédentes, ladite bande, feuille ou flan d'acier possédant une résistance à la traction Rm selon la direction longitudinale supérieure ou égale à 480 MPa, de préférence une résistance à la traction Rm supérieure ou égale à 520 MPa, idéalement une résistance à la traction Rm inférieure ou égale à 680 MPa.
- Bande, feuille ou flan d'acier selon l'une quelconque des revendications précédentes 1 à 4, ledit revêtement de zinc ou d'alliage de zinc étant un revêtement galvanisé par immersion à chaud ou recuit après galvanisation par immersion à chaud.
- Bande, feuille ou flan d'acier selon l'une quelconque des revendications précédentes, ledit revêtement en alliage de zinc comprenant de 0,5 à 4 % en poids de Al et de 0,5 à 3,2 % en poids de Mg, le reste étant du zinc et des traces d'autres éléments, ledit revêtement possédant de préférence une épaisseur comprise entre 5 et 15 µm par côté, idéalement une épaisseur comprise entre 6 et 13 µm par côté.
- Procédé permettant la fabrication d'une bande d'acier faiblement allié à haute résistance comprenant les étapes suivantes :
production d'un acier en fusion possédant la composition de la revendication 1, coulage de l'acier en fusion dans un appareil de coulage, laminage à chaud de la coulée à une température finale supérieure ou égale à 880°C en une bande, bobinage la bande laminée à chaud à une température de bobinage allant de 500°C à 650°C, laminage à froid de la bande avec une réduction globale de 50 à 75%, recuit en continu de la bande à une température de recuit comprise entre 750°C et 820°C. - Procédé selon la revendication 8, ladite bande recuite étant revêtue par immersion à chaud d'un revêtement de zinc ou d'alliage de zinc.
- Procédé selon la revendication 9, ladite bande revêtue étant laminée à froid dans un laminoir de finissage avec une réduction allant de 0,1 à 3,0%, de préférence une réduction allant de 0,2 à 2,0%.
- Procédé selon la revendication 8, 9 ou 10, ladite bande étant laminée à froid à une largeur supérieure ou égale à 1400 mm, de préférence à une largeur supérieure ou égale à 1600 mm, idéalement à une largeur supérieure ou égale à 1800 mm, avec une épaisseur allant de 0,7 à 2,0 mm.
- Procédé selon la revendication 8, 9, 10 ou 11, ladite température de bobinage de la bande laminée à chaud étant comprise entre 550°C et 600°C et/ou la réduction globale par laminage à froid étant comprise entre 60 et 70 % et/ou ladite température de recuit étant comprise entre 760°C et 800°C.
- Procédé selon l'une quelconque des revendications 8 à 12, ladite bande d'acier possédant une composition telle que fournie par la revendication 2.
- Procédé selon l'une quelconque des revendications 8 à 13, ladite bande d'acier produite possédant une limite d'élasticité Rp 0,2 supérieure ou égale à 420 MPa, de préférence une limite d'élasticité Rp 0,2 supérieure ou égale à 460 MPa, idéalement une limite d'élasticité Rp 0,2 inférieure ou égale à 580 MPa.
- Procédé selon l'une quelconque des revendications 8 à 15, ladite bande d'acier produite possédant un allongement A 80 mm supérieure ou égale à 15%.
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PCT/EP2015/001724 WO2016030010A1 (fr) | 2014-08-25 | 2015-08-24 | Acier faiblement allié haute résistance laminé à froid |
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EP (1) | EP3186406B1 (fr) |
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CN106086647B (zh) * | 2016-07-13 | 2018-02-06 | 河北钢铁股份有限公司邯郸分公司 | 一种低合金高强钢q460c及其生产方法 |
WO2021180964A1 (fr) * | 2020-03-13 | 2021-09-16 | Tata Steel Ijmuiden B.V. | Bande d'acier laminée à chaud ayant des propriétés améliorées |
CN111575592B (zh) * | 2020-06-28 | 2021-10-29 | 马鞍山钢铁股份有限公司 | 一种屈服强度460MPa级的低合金高强钢及生产方法 |
WO2023062210A1 (fr) * | 2021-10-15 | 2023-04-20 | Tata Steel Ijmuiden B.V. | Bande d'acier laminée à froid faiblement alliée à haute résistance hybride et recuite et son procédé de production |
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US4398970A (en) * | 1981-10-05 | 1983-08-16 | Bethlehem Steel Corporation | Titanium and vanadium dual-phase steel and method of manufacture |
US6465114B1 (en) * | 1999-05-24 | 2002-10-15 | Nippon Steel Corporation | -Zn coated steel material, ZN coated steel sheet and painted steel sheet excellent in corrosion resistance, and method of producing the same |
JP3840864B2 (ja) * | 1999-11-02 | 2006-11-01 | Jfeスチール株式会社 | 高張力溶融亜鉛めっき鋼板およびその製造方法 |
JP4267367B2 (ja) * | 2002-06-19 | 2009-05-27 | 新日本製鐵株式会社 | 原油油槽用鋼およびその製造方法、原油油槽およびその防食方法 |
JP4730056B2 (ja) * | 2005-05-31 | 2011-07-20 | Jfeスチール株式会社 | 伸びフランジ成形性に優れた高強度冷延鋼板の製造方法 |
WO2007015541A1 (fr) * | 2005-08-03 | 2007-02-08 | Sumitomo Metal Industries, Ltd. | Feuille d’acier laminée à chaud, feuille d’acier laminée à froid et procédé de production correspondant |
JP4518029B2 (ja) * | 2006-02-13 | 2010-08-04 | 住友金属工業株式会社 | 高張力熱延鋼板とその製造方法 |
JP4736853B2 (ja) * | 2006-02-28 | 2011-07-27 | Jfeスチール株式会社 | 析出強化型高強度薄鋼板およびその製造方法 |
JP4940813B2 (ja) * | 2006-03-06 | 2012-05-30 | Jfeスチール株式会社 | TS×Elの値が21000MPa・%以上である溶融亜鉛めっき鋼板の製造方法 |
EP1857566B1 (fr) * | 2006-05-15 | 2017-05-03 | ThyssenKrupp Steel Europe AG | Produit d'acier plat revêtu avec une revêtement de protection contre la corrosion et procédé de son fabrication |
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JP4926814B2 (ja) * | 2007-04-27 | 2012-05-09 | 新日本製鐵株式会社 | 降伏点伸びを制御した高強度鋼板とその製造方法 |
JP5326403B2 (ja) * | 2007-07-31 | 2013-10-30 | Jfeスチール株式会社 | 高強度鋼板 |
ES2578952T3 (es) * | 2008-03-27 | 2016-08-03 | Nippon Steel & Sumitomo Metal Corporation | Chapa de acero laminada en frío, chapa de acero galvanizado de alta resistencia y chapa de acero galvanizado por inmersión en caliente aleada de alta resistencia que tiene excelente conformabilidad y soldabilidad, y métodos para fabricar las mismas |
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 |
CA2772026C (fr) * | 2009-08-31 | 2013-11-19 | Nippon Steel Corporation | Feuille d'acier galvanise a chaud tres resistante et son procede de production |
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2015
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- 2015-08-24 KR KR1020177005778A patent/KR20170047254A/ko unknown
- 2015-08-24 WO PCT/EP2015/001724 patent/WO2016030010A1/fr active Application Filing
- 2015-08-24 CN CN201580045534.9A patent/CN107075652A/zh active Pending
- 2015-08-24 US US15/504,941 patent/US20170275724A1/en not_active Abandoned
- 2015-08-24 MX MX2017002410A patent/MX2017002410A/es unknown
- 2015-08-24 BR BR112017003147A patent/BR112017003147A2/pt not_active IP Right Cessation
- 2015-08-24 JP JP2017511320A patent/JP2018502213A/ja active Pending
- 2015-08-24 CA CA2959096A patent/CA2959096C/fr not_active Expired - Fee Related
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2017
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Publication number | Publication date |
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WO2016030010A1 (fr) | 2016-03-03 |
ZA201700943B (en) | 2018-12-19 |
MX2017002410A (es) | 2017-05-23 |
EP3186406A1 (fr) | 2017-07-05 |
CN107075652A (zh) | 2017-08-18 |
CA2959096C (fr) | 2019-06-25 |
BR112017003147A2 (pt) | 2017-11-28 |
CA2959096A1 (fr) | 2016-03-03 |
JP2018502213A (ja) | 2018-01-25 |
US20170275724A1 (en) | 2017-09-28 |
KR20170047254A (ko) | 2017-05-04 |
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