WO2021034851A1 - High strength steel products and annealing processes for making the same - Google Patents
High strength steel products and annealing processes for making the same Download PDFInfo
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- WO2021034851A1 WO2021034851A1 PCT/US2020/046847 US2020046847W WO2021034851A1 WO 2021034851 A1 WO2021034851 A1 WO 2021034851A1 US 2020046847 W US2020046847 W US 2020046847W WO 2021034851 A1 WO2021034851 A1 WO 2021034851A1
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- Prior art keywords
- steel sheet
- sheet product
- weight percent
- rolled steel
- high strength
- Prior art date
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- 238000000034 method Methods 0.000 title claims abstract description 116
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 109
- 239000010959 steel Substances 0.000 title claims abstract description 109
- 238000000137 annealing Methods 0.000 title claims abstract description 65
- 229910001566 austenite Inorganic materials 0.000 claims description 45
- 229910000859 α-Fe Inorganic materials 0.000 claims description 24
- 230000000717 retained effect Effects 0.000 claims description 22
- 229910000734 martensite Inorganic materials 0.000 claims description 19
- 238000002791 soaking Methods 0.000 claims description 14
- 238000000576 coating method Methods 0.000 claims description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 9
- 239000011248 coating agent Substances 0.000 claims description 9
- 239000011572 manganese Substances 0.000 claims description 9
- 239000011701 zinc Substances 0.000 claims description 9
- 229910052725 zinc Inorganic materials 0.000 claims description 9
- 229910052710 silicon Inorganic materials 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 238000005246 galvanizing Methods 0.000 claims description 6
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 3
- 239000000203 mixture Substances 0.000 abstract description 23
- 230000002349 favourable effect Effects 0.000 abstract description 10
- 239000000047 product Substances 0.000 description 51
- 238000001816 cooling Methods 0.000 description 22
- 238000010438 heat treatment Methods 0.000 description 18
- 238000010791 quenching Methods 0.000 description 16
- 239000010960 cold rolled steel Substances 0.000 description 12
- 230000000171 quenching effect Effects 0.000 description 12
- 238000001887 electron backscatter diffraction Methods 0.000 description 10
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 10
- 239000000463 material Substances 0.000 description 9
- 230000000052 comparative effect Effects 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 8
- 239000007789 gas Substances 0.000 description 7
- 230000001590 oxidative effect Effects 0.000 description 7
- 239000000758 substrate Substances 0.000 description 7
- 238000005496 tempering Methods 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 238000007796 conventional method Methods 0.000 description 3
- 230000006698 induction Effects 0.000 description 3
- 229910052748 manganese Inorganic materials 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 229910052719 titanium Inorganic materials 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 2
- 239000000956 alloy Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910001567 cementite Inorganic materials 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 239000012535 impurity Substances 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000003595 mist Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 238000012360 testing method Methods 0.000 description 2
- UXVMQQNJUSDDNG-UHFFFAOYSA-L Calcium chloride Chemical compound [Cl-].[Cl-].[Ca+2] UXVMQQNJUSDDNG-UHFFFAOYSA-L 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 150000001335 aliphatic alkanes Chemical class 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000005244 galvannealing Methods 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000010191 image analysis Methods 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- KFZAUHNPPZCSCR-UHFFFAOYSA-N iron zinc Chemical compound [Fe].[Zn] KFZAUHNPPZCSCR-UHFFFAOYSA-N 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000006104 solid solution Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
- 238000003466 welding Methods 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
- C21D9/48—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals deep-drawing sheets
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- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
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- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/185—Hardening; Quenching with or without subsequent tempering from an intercritical temperature
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- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/19—Hardening; Quenching with or without subsequent tempering by interrupted quenching
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/25—Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
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- 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
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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
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- C21D1/28—Normalising
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- C—CHEMISTRY; METALLURGY
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- 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
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- C21D6/005—Heat treatment of ferrous alloys containing Mn
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- C—CHEMISTRY; METALLURGY
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- 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
- C21D6/008—Heat treatment of ferrous alloys containing Si
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- 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
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- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
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- 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
- C21D8/0405—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 of ferrous alloys
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- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
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- 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
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- 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
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- 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
- C21D8/0447—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 heat treatment
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- 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
- C21D8/0447—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 heat treatment
- C21D8/0463—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 heat treatment following hot rolling
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- 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
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- 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
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C22C38/00—Ferrous alloys, e.g. steel alloys
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- 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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- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
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- 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
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- 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
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- C23C2/0224—Two or more thermal pretreatments
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- 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
- C23C2/26—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
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
- C25D5/34—Pretreatment of metallic surfaces to be electroplated
- C25D5/36—Pretreatment of metallic surfaces to be electroplated of iron or steel
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D7/00—Electroplating characterised by the article coated
- C25D7/06—Wires; Strips; Foils
- C25D7/0614—Strips or foils
-
- 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
Definitions
- the present invention relates to high strength steel products having favorable properties, and to annealing processes for making such products.
- AHSS advanced high strength steel
- These Generation 3 steels have a favorable balance of tensile strength and elongation, typically in a UTS-TE range of about 20,000 MPa% or greater.
- the steel industry has had a difficult time commercializing Generation 3 AHSS as the majority of approaches require high alloy content, e.g., typically greater than 4 weight percent manganese, which results in difficulties when manufacturing such steels with conventional steel production equipment.
- currently available AHSS has been difficult to weld by techniques such as spot welding, have been difficult to coat with zinc-based galvanic coatings, and have been difficult to manufacture into the thin gauge sheet needed for wide scale application.
- the present invention provides steel sheet products having controlled compositions that are subjected to two-step annealing processes to produce sheet products having desirable microstructures and favorable mechanical properties such as high strength and ultra- high formability.
- the steel sheet products may be cold rolled or hot rolled.
- Steels processed in accordance with the present invention exhibit favorable combined ultimate tensile strength and total elongation (UTS-TE) properties, e.g., of greater than 25,000 MPa-% when tested using standard subsize ASTM or full size JIS tensile testing procedures.
- UTS-TE ultimate tensile strength and total elongation
- steels produced in accordance with the present invention exhibit favorable combinations of TE and hole expansion, i.e., both global formability and local formability are good. Steels with these properties fall into the category of Generation 3 advanced high strength steels, and are highly desired by various industries including automobile manufacturers.
- An aspect of the present invention is to provide a high strength rolled steel sheet product comprising from 0.12 to 0.5 weight percent C, from 1 to 3 weight percent Mn, and from 0.8 to 3 weight percent of a combination of Si and Al, wherein the steel sheet product has been subjected to a two-step annealing process, comprises ferrite and substantially equiaxed retained austenite grains having an average aspect ratio of less than 3:1, and has a combination of ultimate tensile strength and total elongation UTS-TE of greater than 25,000 MPa%.
- Another aspect of the present invention is to provide a method of producing a high strength rolled steel sheet product comprising from 0.12 to 0.5 weight percent C, from 1 to 3 weight percent manganese, and from 0.8 to 3 weight percent of a combination of Si and Al.
- the method comprises subjecting the steel sheet product to a first step annealing process to achieve a predominantly martensitic microstructure, and subjecting the steel sheet product to a second step process comprising soaking the sheet product in an intercritical regime at a temperature of from 720 to 850°C, followed by holding the sheet product at a temperature of from 370 to 445°C.
- Fig. 1 includes plots of temperature versus time illustrating a two-step annealing process in accordance with an embodiment of the present invention.
- Fig. 2 includes plots of temperature versus time illustrating a two-step annealing process in accordance with another embodiment of the present invention.
- Fig. 3 is a plot of temperature versus time illustrating a two-step annealing process that combines the two-step thermal process with an optional zinc-based hot-dipped coating operation in a single production facility.
- Fig. 4 is a plot of temperature versus time for a second step of an annealing process defining soaking and holding zones in the thermal cycle in accordance with an embodiment of the invention.
- Figs. 5 and 6 are electron backscatter diffraction (EBSD) photomicrographs illustrating the microstructure of a high strength steel sheet product in accordance with an embodiment of the invention.
- EBSD electron backscatter diffraction
- Fig. 7 is an optical photomicrograph of a steel sheet product subjected to the thermal process shown in Fig. 1, showing darker ferrite grains and lighter austenite grains.
- Fig. 8 is a bar graph illustrating aspect ratios of the austenite grains shown in Fig. 7.
- Figs. 9 and 10 are graphs for a high strength steel sheet product showing austenite and ferrite grain size distributions in accordance with an embodiment of the invention.
- Figs. 11 is EBSD photomicrograph illustrating the microstructure of a high strength steel sheet product processed as shown in Fig. 1.
- Figs. 12 and 13 are EBSD photomicrographs showing steel sheet products processed as shown in Fig. 2.
- Fig. 14 is an EBSD photomicrograph of a steel sheet product processed as shown in Fig. 3.
- Fig. 15 is a graph of total elongation vs. ultimate tensile strength for high strength steel sheet products of the present invention in comparison with other steel sheet products processed outside the scope of the present invention.
- Fig. 16 is a graph of total elongation vs. ultimate tensile strength for high strength steel products produced in mill trials in accordance with embodiments of the present invention.
- Fig. 17 is a plot of temperature versus time for cold rolled and hot rolled substrates processed with a thermal cycle in accordance with an embodiment of the invention.
- Fig. 18 is an EBSD photomicrograph of a cold rolled steel sheet substrate subjected to the thermal process shown in Fig. 17 showing darker ferrite grains and lighter retained austenite grains.
- Fig. 19 is an EBSD photomicrograph of a hot rolled steel sheet substrate subjected to the thermal process shown in Fig. 17 showing darker ferrite grains and lighter retained austenite grains.
- the high strength steel sheet products of the present invention have controlled compositions that, in combination with controlled annealing processes, produce desirable microstructures and favorable mechanical properties including high strengths and ultra-high formabilities.
- the steel composition may include carbon, manganese and silicon, along with any other suitable alloying additions known to those skilled in the art. Examples of steel compositions including ranges of C, Mn, Si, Al, Ti, and Nb are listed in Table 1 below.
- the steel compositions may include minor or impurity amounts of other elements, such as 0.015 max S, 0.03 max P, 0.2 max Cu, 0.02 max Ni, 0.2 max Cr, 0.2 max Mo, 0.1 max Sn, 0.015 max N, 0.1 max V, and 0.004 max B.
- minor or impurity amounts of other elements such as 0.015 max S, 0.03 max P, 0.2 max Cu, 0.02 max Ni, 0.2 max Cr, 0.2 max Mo, 0.1 max Sn, 0.015 max N, 0.1 max V, and 0.004 max B.
- substantially free when referring to the composition of the steel sheet product, means that a particular element or material is not purposefully added to the composition, and is only present as an impurity or in trace amounts.
- C provides increased strength and promotes the formation of retained austenite.
- Mn provides hardening and acts as a solid solution strengthener.
- Si inhibits iron carbide precipitation during heat treatment, and increases austenite retention.
- A1 inhibits iron carbide precipitation during heat treatment, and increases austenite retention.
- Ti and Nb may act as a strength-enhancing grain refiners.
- A1 may be present in an amount of at least 0.1 weight percent or at least 0.2 weight percent.
- A1 may be present in an amount of from 0.5 to 1.2 weight percent, or from 0.7 to 1.1 weight percent, in certain embodiments.
- the steel sheet product may be substantially free of Al.
- the ultimate tensile strength (UTS) of the steel sheet products range from 700 to 1,100 MPa or more. In certain embodiments, the steel sheet product has an ultimate tensile strength of greater than 700 MPa, for example, from 720 to 1,100 MPa, or from 750 to 1,050 MPa.
- the steel sheet products have a total elongation (TE) typically greater than 22 percent, for example, greater than 27 percent, or greater than 33 percent.
- TE total elongation
- the steel sheet product may have a total elongation of at least 20% or at least 25% or at least 27%, e.g., from 22 to 45%, or from 25 to 40%.
- the steel sheet products may possess lambda (l) values as measured by a standard hole expansion test typically greater than 20 percent, for example, greater than 25 percent, or greater than 30 percent, or greater than 35 percent.
- the whole expansion ratio or lambda may be greater than 20%, for example, from 22 to 80%, or from 25 to 60%.
- the final microstructure of the steel sheet products may primarily comprise ferrite, e.g., at least 50% up to 80% or higher, with lesser amounts of retained austenite, e.g., from 5 to 25%, and minor amounts of fresh martensite, e.g., from 0 to 10% or 15%.
- the amounts of ferrite, austenite and martensite may be determined by standard EBSD techniques.
- retained austenite content may be determined by magnetic saturation methods. Unless otherwise specified herein, the volume percent of retained austenite is determined by the EBSD technique.
- the retained austenite comprises from 1 to 25 volume percent, for example, from 5 to 20 volume percent.
- the amount of fresh martensite may comprise less than 15 volume percent, or less than 10 volume percent, or less than 5 volume percent.
- the steel sheet product is substantially free of fresh martensite. It has been found that when fresh martensite amounts are greater than 15%, hole expansion values decrease significantly, e.g., local formability is significantly decreased.
- At least a portion of the ferrite may be formed during the heating section, as described below, by recrystallization and/or tempering of martensite, or during the cooling and holding section of the second annealing process by austenite decomposition.
- Some of the ferrite may be considered bainitic ferrite.
- the ferrite, austenite and martensite phases are fine grained, e.g., having average grain sizes of less than 10 microns, for example, less than 5 microns, or less than 3 microns.
- ferrite grain size may range from less than 10 microns, for example, less than 8 microns, or less than 6 microns.
- Average austenite grain size may range from less than 2 microns, for example, less than 1 micron, or less than 0.5 micron. Martensite grain size, when present, may range from less than 10 microns, for example, less than 8 microns, or less than 6 microns.
- the austenite grains may be substantially equiaxed, e.g., having average aspect ratios less than 3 : 1 or less than 2:1, for example, about 1:1. It has been found that amounts of retained austenite below about 5% results in significantly decreased total elongations (TE). It has further been found that amounts of retained austenite above 25% can only be obtained at very high carbon levels, which results in poor weldability.
- a two-step annealing process is used to produce advanced high strength steel products with favorable mechanical properties, such as those described above.
- multiple methodologies for undertaking the heat treatment may be used. Examples of two-step annealing processes are shown in Figs. 1-3 and described below.
- Fig. 1 represents a continuous annealing line (CAL) followed by a continuous annealing line (CAL) production route.
- Fig. 2 represents a CAL plus continuous galvanizing line (CGL) production route.
- Fig. 3 represents a specially designed line allowing for both CAL + CAL or CAL + CGL steps to take place in a single facility. While a direct-fired furnace (DFF) followed by a radiant tube (RT) furnace embodiment is shown in Fig. 3, other embodiments such as all radiant tube, electric radiant heating, and the like may be used to achieve the desired thermal cycles.
- DFF direct-fired furnace
- RT radiant tube
- the goal of the first step of the annealing process is to achieve a martensitic microstructure in the cold rolled or hot rolled steel sheet product.
- an annealing temperature above the A3 temperature may typically be used, for example, an annealing temperature of at least 820°C may be used.
- the first stage annealing temperature may typically range from 830 to 980°C, for example, from 830 to 940°C, or from 840 to 930°C, or from 860 to 925°C.
- the peak annealing temperature may be typically held for at least 20 seconds, for example, from 20 to 500 seconds, or from 30 to 200 seconds.
- Heating may be accomplished by conventional techniques such as a non-oxidizing or oxidizing direct-fired furnace (DFF), oxygen-enriched DFI, induction, gas radiant tube heating, electric radiant heating, and the like.
- DFF non-oxidizing or oxidizing direct-fired furnace
- Examples of heating systems that may be adapted for use in the processes of the present invention are disclosed in U.S. Patent Nos. 5,798,007; 7,368,689; 8,425,225; and 8,845,324, U.S. Patent Application No. 2009/0158975, and Published PCT Application No. WO/2015083047, assigned to Fives Stein. Additional examples of heating systems that may be adapted for use in the processes of the present invention include U.S. Patent No. 7,384,489 assigned to Drever International, and U.S. Patent No. 9,096,918 assigned to Nippon Steel and Sumitomo Metal Corporation. Any other suitable known types of heating systems and processes may be adapted for use in Step 1 and Step 2.
- DFF non-oxidizing or
- the cold rolled or hot rolled steel sheet is quenched to room temperature, or to a controlled temperature above room temperature, as more fully described below.
- the quench temperature may not necessarily be room temperature but should be below the martensite start temperature (M s ), and preferably below the martensite finish temperature (MF), to form a microstructure of predominantly martensite.
- M s martensite start temperature
- MF martensite finish temperature
- the steel sheet product may be cooled to a temperature below 300°C, for example, below 200°C.
- Quenching may be accomplished by conventional techniques such as water quenching, submerged knife/nozzle water quenching, gas cooling, rapid cooling using a combination of cold, warm or hot water and gas, water solution cooling, other liquid or gas fluid cooling, chilled roll quench, water mist spray, wet flash cooling, non-oxidizing wet flash cooling, and the like.
- a quench rate of from 30 to 2,000°C/sec may typically be used.
- cooling and quenching systems and processes may be adapted for use in the processes of the present invention.
- Suitable cooling/quenching systems and processes conventionally used on a commercial basis may include water quench, water mist cooling, dry flash and wet flash, oxidizing and non-oxidizing cooling, alkane fluid to gas phase change cooling, hot water quenching, including two-step water quenching, roll quenching, high percentage hydrogen or helium gas jet cooling, and the like.
- dry flash and/or wet flash oxidizing and non-oxidizing cooling/quenching such as disclosed in published PCT Application No. W02015/083047 to Fives Stein may be used.
- the martensite can be optionally tempered to soften the steel somewhat to make further processing more feasible. Tempering takes place by raising the temperature of the steel in the range of room temperature to about 500°C and holding for up to 600 seconds. If tempering is utilized, the tempering temperature may be held constant, or may be varied within this preferred range.
- the temperature is ramped down to room temperature.
- the rate of such ramp-down may typically range from 1 to 40°C/sec, for example, from 2 to 20°C/sec. In the case of a single pass facility furnace, as in Fig. 3, tempering may not be necessary.
- the second step of the annealing process may include a first stage that is conducted at relatively high annealing temperature, and a second stage that is conducted at relatively low temperature. These stages are defined as the “soaking” and “holding” zones of the second anneal, as described in Fig. 4. The temperatures are controlled in order to promote the formation of the desired microstructure in the final product.
- a soaking zone temperature between Ai and A3 may be used, for example, an annealing temperature of at least 720°C may be used.
- the soaking zone temperature may typically range from 720 to 850°C, for example, from 760 to 825°C.
- the peak annealing temperature may be typically held for at least 15 seconds, for example, from 20 to 300 seconds, or from 30 to 150 seconds.
- the soaking zone temperature may be achieved by heating the steel from a relatively low temperature below M s , e.g., room temperature, at an average rate of from 0.5 to 50°C/sec, for example, from about 2 to 20°C/sec.
- the ramp-up may take from 25 to 800 seconds, for example, from 100 to 500 seconds.
- the first stage heating of the second step may be accomplished by any suitable heating system or process, such as using radiant heating, induction heating, direct fired furnace heating and the like.
- the steel may be cooled to a controlled temperature above room temperature to the holding zone.
- the steel sheet product is maintained at a temperature above 300°C between the second step soaking process and the second step holding process. Cooling from the soaking to holding zone may be accomplished by conventional techniques such as water cooling, gas cooling and the like. An average cooling rate of from 5 to 400°C/sec may typically be used. Any suitable types of cooling and quenching systems may be adapted for use in cooling from the soaking temperature to the holding temperature, including those described above.
- the holding zone step is carried out at a typical temperature of from 360 to 445°C, for example, from 370 to 440°C.
- the holding zone may be held for up to 800 seconds, for example, from 30 to 600 seconds.
- the holding zone temperature may be held constant, or may be varied somewhat within the preferred temperature range.
- the steel may be reheated, such as by induction or other heating method, to enter a hot-dip coating pot at the proper temperature for good coating results, if the steel is to be hot-dip coated.
- the temperature may be ramped down to room temperature.
- a ramp-down may typically take from 10 to 1,000 seconds, for example, from about 20 to 500 seconds.
- the rate of such ramp-down may typically range from 1 to l,000°C/sec, for example, from 2 to 20°C/sec.
- one or both of the first-step and second- step annealing processes may be performed on a continuous annealing line (CAL). After going through a CAL+CAL process, the steel may be electrogalvanized to produce a zinc based coated product.
- CAL continuous annealing line
- the annealed steel sheet is hot-dip galvanized at the end of the holding zone.
- Galvanizing temperatures may typically range from 440 to 480°C, for example, from 450 to 470°C.
- the galvanizing step may be performed as part of the second-step annealing process on a continuous galvanizing line (CGL), e.g., as shown in Fig. 2.
- This CAL + CGL process can be used to produce both a zinc-based or zinc alloy-based hot-dip galvanized product or reheated after coating to produce an iron-zinc galvanneal type coated product.
- An optional nickel-based coating step can take place between the CAL and CGL steps in the process to improve zinc coating properties.
- a galvanized product or zinc-based alloy hot-dip coated product can also be made on a specially designed CGL in which the two-step annealing can take place in a single line, as shown in Fig. 3. Galvannealing can also be an option in this case.
- a single production facility can also be specially designed and built to combine the two-step thermal process to produce uncoated Generation 3 steels as defined in the invention.
- the microstructure of the resultant product is shown in Figs. 5 and 6.
- EBSD techniques using commercial ED AX orientation imaging microscopy software show the dark ferrite grains and light austenite grains in Fig. 5.
- the microstructure of the resultant product is shown in Fig. 11.
- Mechanical properties of Sample No. 2 are listed in Table 2.
- Grain size distributions of austenite and ferrite are shown in Figs. 9 and 10, respectively.
- the average austenite grain size is less than 1 micron and the average ferrite grain size is less than 10 microns.
- the microstructure includes about 80 volume percent ferrite with an average grain size of about 5 microns, about 10 volume percent retained austenite having substantially equiaxed grains and an average grain size of about 0.5 micron, and about 10 volume percent fresh martensite with an average grain size of about 5 microns.
- Mechanical properties of Sample No. 1 are listed in Table 2 below.
- the microstructure of the resultant product is shown in Figs. 12 and 13.
- austenite is light in color and ferrite is dark in color.
- Mechanical properties of Sample No. 3 are listed in Table 2.
- the microstructure of the resultant product is shown in Figure 14.
- austenite is light in color and ferrite is dark in color.
- Mechanical properties of Sample No. 4 are listed in Table 2.
- FIG. 7 is an optical image showing the micro structure of the steel shown in Fig. 2, Sample No. 6, which was subjected to the two-step annealing process shown in Fig. 1.
- the dark regions of the photomicrograph are ferrite grains, while the light regions are austenite grains.
- Fig. 8 is a graph illustrating the aspect ratios of the austenite grains shown in Fig. 7.
- the optical image of Fig. 7 was used to determine the aspect ratios of the austenite grains using image analysis with commercially available software. Fig. 7 shows that the average aspect ratio is less than 3:1 for the austenite grains.
- Fig. 15 plots the total elongation (TE) and ultimate tensile strength (UTS) of Samples 1-8 of Examples 1-8, as well as Samples C1-C12 of Comparative Examples C1-C12. A line corresponding to UTS-TE of 25,000 is roughly drawn in Fig. 15.
- the high strength steel sheet samples produced in accordance with the present invention possess superior combinations of strength and elongation versus the comparative samples, i.e., high total elongation properties at high UTS levels are observed for the inventive examples.
- the Sample 1 through Sample 8 steels fall into the category of Generation 3 advanced high strength steels, which are highly desirable for automotive and other industries.
- Mill trials were conducted for samples labeled M1-M5 in Table 3 below using either the CAL+CAL or CAL+CGL process.
- Samples Ml, M2 and M5 the CAL+CAL processing times and temperatures shown in Fig. 1 were used.
- Samples M3 and M4 the CAL+CGL processing times and temperatures shown in Fig. 2 were used.
- Fig. 16 shows the strength-elongation balance of the mill trial materials, all meeting a minimum UTS-TE of 25,000.
- the trial materials exhibited lambda values greater than 20%.
- Figs. 18 and 19 show similar austenite contents, distributions and morphologies.
- Fig. 18 shows the austenite content of cold rolled sample 11 A
- Fig. 19 shows the austenite content of hot rolled sample 12A.
- a fine, predominantly equiaxed distribution of austenite is observed in both microstructures.
- any numerical range recited herein is intended to include all sub-ranges subsumed therein.
- a range of “1 to 10” is intended to include all sub-ranges between (and including) the recited minimum value of 1 and the recited maximum value of 10, that is, having a minimum value equal to or greater than 1 and a maximum value of equal to or less than 10.
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Abstract
Description
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Priority Applications (8)
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BR112022003136A BR112022003136A2 (en) | 2019-08-19 | 2020-08-18 | High strength rolled steel sheet product, and method for producing a high strength rolled steel sheet product |
CA3151124A CA3151124A1 (en) | 2019-08-19 | 2020-08-18 | High strength steel products and annealing processes for making the same |
CN202080066399.7A CN114630914A (en) | 2019-08-19 | 2020-08-18 | High strength steel product and annealing method for producing the same |
EP20764876.7A EP4018005A1 (en) | 2019-08-19 | 2020-08-18 | High strength steel products and annealing processes for making the same |
KR1020227009048A KR20220050935A (en) | 2019-08-19 | 2020-08-18 | High-strength steel products and annealing processes for their manufacture |
JP2022508773A JP2022544765A (en) | 2019-08-19 | 2020-08-18 | High strength steel product and annealing process for making same |
MX2022002080A MX2022002080A (en) | 2019-08-19 | 2020-08-18 | High strength steel products and annealing processes for making the same. |
AU2020335005A AU2020335005A1 (en) | 2019-08-19 | 2020-08-18 | High strength steel products and annealing processes for making the same |
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US16/544,127 US11993823B2 (en) | 2016-05-10 | 2019-08-19 | High strength annealed steel products and annealing processes for making the same |
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CN114630914A (en) | 2022-06-14 |
KR20220050935A (en) | 2022-04-25 |
JP2022544765A (en) | 2022-10-21 |
MX2022002080A (en) | 2022-03-17 |
BR112022003136A2 (en) | 2022-05-17 |
CA3151124A1 (en) | 2021-02-25 |
AU2020335005A1 (en) | 2022-03-03 |
EP4018005A1 (en) | 2022-06-29 |
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