BR112012031466B1 - METHOD OF PRODUCING AN EXCELLENT AUSTENTIC STEEL SHEET IN RESISTANCE TO DELAYED FRACTURE AND STRIP OR SHEET - Google Patents
METHOD OF PRODUCING AN EXCELLENT AUSTENTIC STEEL SHEET IN RESISTANCE TO DELAYED FRACTURE AND STRIP OR SHEET Download PDFInfo
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- BR112012031466B1 BR112012031466B1 BR112012031466-1A BR112012031466A BR112012031466B1 BR 112012031466 B1 BR112012031466 B1 BR 112012031466B1 BR 112012031466 A BR112012031466 A BR 112012031466A BR 112012031466 B1 BR112012031466 B1 BR 112012031466B1
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- 238000000034 method Methods 0.000 title claims abstract description 29
- 230000003111 delayed effect Effects 0.000 title claims abstract description 9
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 21
- 239000010959 steel Substances 0.000 claims abstract description 21
- 239000000463 material Substances 0.000 claims description 40
- 238000000137 annealing Methods 0.000 claims description 34
- 238000000576 coating method Methods 0.000 claims description 20
- 239000011248 coating agent Substances 0.000 claims description 19
- 238000010438 heat treatment Methods 0.000 claims description 15
- 229910052782 aluminium Inorganic materials 0.000 claims description 13
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 11
- 238000001816 cooling Methods 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 9
- 238000005246 galvanizing Methods 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 229910052720 vanadium Inorganic materials 0.000 claims description 7
- 238000005097 cold rolling Methods 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 6
- 238000003475 lamination Methods 0.000 claims description 5
- 238000004519 manufacturing process Methods 0.000 claims description 5
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 4
- 238000005554 pickling Methods 0.000 claims description 4
- 229910052710 silicon Inorganic materials 0.000 claims description 4
- 238000005098 hot rolling Methods 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 229910052748 manganese Inorganic materials 0.000 claims description 2
- 229910052698 phosphorus Inorganic materials 0.000 claims description 2
- 229910052717 sulfur Inorganic materials 0.000 claims description 2
- 238000004804 winding Methods 0.000 claims description 2
- 238000007654 immersion Methods 0.000 claims 1
- 229910052739 hydrogen Inorganic materials 0.000 description 8
- 239000001257 hydrogen Substances 0.000 description 8
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 6
- 229910052725 zinc Inorganic materials 0.000 description 6
- 239000011701 zinc Substances 0.000 description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 5
- 229910052760 oxygen Inorganic materials 0.000 description 5
- 239000001301 oxygen Substances 0.000 description 5
- 238000001556 precipitation Methods 0.000 description 5
- 238000001953 recrystallisation Methods 0.000 description 5
- 238000005275 alloying Methods 0.000 description 4
- 238000009792 diffusion process Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- ZLANVVMKMCTKMT-UHFFFAOYSA-N methanidylidynevanadium(1+) Chemical class [V+]#[C-] ZLANVVMKMCTKMT-UHFFFAOYSA-N 0.000 description 4
- 239000002244 precipitate Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 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 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 2
- 229910000937 TWIP steel Inorganic materials 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- YZCKVEUIGOORGS-UHFFFAOYSA-N Hydrogen atom Chemical compound [H] YZCKVEUIGOORGS-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910000756 V alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000005764 inhibitory process Effects 0.000 description 1
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N iron oxide Inorganic materials [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 1
- 235000013980 iron oxide Nutrition 0.000 description 1
- VBMVTYDPPZVILR-UHFFFAOYSA-N iron(2+);oxygen(2-) Chemical class [O-2].[Fe+2] VBMVTYDPPZVILR-UHFFFAOYSA-N 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 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 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 230000006911 nucleation Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000012925 reference material Substances 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 230000008719 thickening Effects 0.000 description 1
- 210000000689 upper leg Anatomy 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/68—Temporary coatings or embedding materials applied before or during heat treatment
- C21D1/70—Temporary coatings or embedding materials applied before or during heat treatment while heating or quenching
-
- 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
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0436—Cold rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0442—Flattening; Dressing; Flexing
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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
- C21D8/04—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
- C21D8/0473—Final recrystallisation annealing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/34—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for tyres; for rims
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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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- 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
- C22C38/02—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
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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
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
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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
- C23C2/0222—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating in a reactive atmosphere, e.g. oxidising or reducing atmosphere
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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
- 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
Abstract
método de produção de um aço austenítico. a presente invenção refere-se a um método de produção de uma chapa de aço austenítica excelente em resistência à fratura retardada e a um aço produzindo assim.method of producing an austenitic steel. The present invention relates to a method of producing an excellent austenitic steel plate in delayed fracture resistance and to a steel thereby producing.
Description
[001] A presente invenção refere-se a um método de produção de uma chapa de aço austenítica excelente em resistência à fratura retardada.[001] The present invention relates to a method of producing an austenitic steel sheet excellent in delayed fracture resistance.
[002] Visando a economia de combustível e segurança no caso de colisões, aços de alta resistência são mais e mais usados na indústria automobilística. Isto requer o uso de material estrutural que combina uma alta resistência à tração com alta ductilidade. Ligas austeníticas compreendendo como principais elementos ferro, carbono e altos níveis de manganês, as quais podem ser laminadas a quente e laminadas a frio e ter uma resistência que pode exceder 1.000 MPa. O modo de deformação desses aços depende da energia de falha de empilhamento: para uma energia de falha de empilhamento suficientemente alta, o modo observado de deformação mecânica é maclação, o que resulta em uma alta capacidade de encruamento. Agindo como um obstáculo para a propagação de deslocamentos, as maclas aumentam a tensão para deformação plástica. Entretanto, quando a energia de falha de empilhamento excede um certo limite, o deslizamento de deslocamentos perfeitos se torna o principal mecanismo de deformação e o encruamento é reduzido. E conhecido que a sensibilidade à fratura retardada aumenta com a resistência mecânica, em particular após certas operações de conformação a frio, uma vez que um alta tensão residual são passíveis de permanecerem após a deformação. Em combinação com o hidrogênio atômico possivelmente presente no metal, essas tensões são passíveis de resultar em fraturas retardadas, quer dizer, fraturas que ocorrem um certo tempo após a deformação. O hidrogênio pode progressivamente se acumular por difusão[002] Aiming at fuel economy and safety in the event of collisions, high strength steels are more and more used in the automobile industry. This requires the use of structural material that combines high tensile strength with high ductility. Austenitic alloys comprising as main elements iron, carbon and high levels of manganese, which can be hot-rolled and cold-rolled and have a strength that can exceed 1,000 MPa. The deformation mode of these steels depends on the stack failure energy: for a sufficiently high stack failure energy, the observed mode of mechanical deformation is maclation, which results in a high hardening capacity. Acting as an obstacle to the propagation of displacements, the thighs increase the stress for plastic deformation. However, when stacking failure energy exceeds a certain limit, sliding from perfect displacements becomes the main deformation mechanism and hardening is reduced. It is known that the sensitivity to delayed fracture increases with mechanical strength, in particular after certain cold forming operations, since a high residual stress is likely to remain after deformation. In combination with the atomic hydrogen possibly present in the metal, these stresses are likely to result in delayed fractures, that is, fractures that occur a certain time after deformation. Hydrogen can progressively accumulate by diffusion
Petição 870190028860, de 26/03/2019, pág. 4/22Petition 870190028860, of 03/26/2019, p. 4/22
2/11 nos defeitos do retículo cristalino, como interfaces de matriz/inclusões, contorno de macla e contorno de grão. É nessas últimas áreas que o hidrogênio pode se tornar prejudicial quando alcançar uma concentração crítica após um certo tempo. Para um tamanho de grão constante, o tempo necessário para alcançar um nível crítico depende da concentração inicial do hidrogênio móvel, da intensidade do campo da concentração da tensão residual e da cinética da difusão do hidrogênio. [003] Em circunstâncias particulares, pequenas quantidades de hidrogênio podem ser introduzidas em algumas etapas da fabricação do aço tais como decapagem química ou eletroquímica, recozimento sob atmosferas especiais, eletrogalvanização ou galvanização por imersão a quente. Operações de usinagem subsequentes usando óleos lubrificantes e graxas podem também provocar a produção de hidrogênio após a decomposição dessas substâncias a altas temperaturas.2/11 in the defects of the crystalline lattice, such as matrix / inclusions interfaces, skin contour and grain contour. It is in these latter areas that hydrogen can become harmful when it reaches a critical concentration after a period of time. For a constant grain size, the time required to reach a critical level depends on the initial concentration of the moving hydrogen, the intensity of the residual stress concentration field and the hydrogen diffusion kinetics. [003] In particular circumstances, small amounts of hydrogen can be introduced in some stages of steelmaking such as chemical or electrochemical pickling, annealing under special atmospheres, electroplating or hot-dip galvanizing. Subsequent machining operations using lubricating oils and greases can also cause the production of hydrogen after the decomposition of these substances at high temperatures.
[004] É um objetivo dessa invenção fornecer um método de produção de uma chapa de aço austenítica excelente em resistência à fratura retardada.[004] It is an objective of this invention to provide a method of producing an austenitic steel sheet excellent in delayed fracture resistance.
[005] É também um objetivo desta invenção fornecer um método de produção de uma chapa de aço austenítica tendo um limite de escoamento aumentado e uma excelente capacidade de soldagem.[005] It is also an objective of this invention to provide a method of producing an austenitic steel sheet having an increased yield limit and excellent weldability.
[006] É outro objetivo desta invenção fornecer um método de produção de uma chapa de aço austenítica que seja eficiente em energia e simples em comparação com o caminho convencional para esse tipo de aço.[006] It is another objective of this invention to provide a method of producing an austenitic steel sheet that is energy efficient and simple compared to the conventional way for this type of steel.
[007] De acordo com a invenção, um ou mais desses objetivos é alcançado pelo fornecimento de um método de produção de chapa de aço austenítica excelente em resistência à fratura retardada compreendendo[007] According to the invention, one or more of these objectives is achieved by providing an excellent austenitic steel sheet production method in resistance to delayed fracture comprising
- lingotar um lingote, ou uma placa de lingotamento contí- ingot an ingot, or a continuous ingot plate
Petição 870190028860, de 26/03/2019, pág. 5/22Petition 870190028860, of 03/26/2019, p. 5/22
3/11 nuo, ou uma placa fina de lingotamento contínuo, ou uma tira lingotada, a sua composição compreendendo, em % em peso:3/11 bare, or a thin continuous caster plate, or a caster strip, its composition comprising, in% by weight:
- 0,50% - 0,80% de C- 0.50% - 0.80% of C
- 10 - 17% de Mn- 10 - 17% Mn
- pelo menos 1,0% de Al- at least 1.0% Al
- no máximo 0,5% de Si- maximum 0.5% Si
- no máximo 0,020% de S- at most 0.020% S
- no máximo 0,050% de P- maximum 0.050% P
- 50 - 200 ppm de N- 50 - 200 ppm N
- 0,050 - 0,25% de V o saldo sendo ferro e as inevitáveis impurezas inerentes à fabricação;- 0.050 - 0.25% of V, the balance being iron and the inevitable impurities inherent in manufacturing;
- fornecer uma tira laminada a quente pela laminação do lingote, da placa lingotada continuamente, da placa fina lingotada continuamente, ou da tira lingotada até a espessura desejada na laminação a quente.- supply a hot-rolled strip by laminating the ingot, the continuously cast ingot, the thin continuously cast ingot, or the ingot strip to the desired thickness in the hot lamination.
- laminar a frio a tira laminada a quente até a espessura final desejada.- cold-laminate the hot-rolled strip to the desired final thickness.
- executar o recozimento contínuo da tira laminada a frio em um processo compreendendo aquecer a tira a uma taxa de aquecimento Vh até uma temperatura de recozimento Ta por um tempo de recozimento ta seguido de resfriamento a uma taxa de resfriamento Vc e onde Ta está entre 750°C e 850°C.- carrying out the continuous annealing of the cold rolled strip in a process comprising heating the strip at a heating rate Vh to an annealing temperature T a for an annealing time t a followed by cooling at a cooling rate Vc and where T a is between 750 ° C and 850 ° C.
[008] Usando-se um alto teor de alumínio, a energia de falha de empilhamento (SFE) do aço aumenta. Quaisquer efeitos adversos dos elementos que diminuam a SFE, tais como silício, são neutralizados pela adição de alumínio. Adicionalmente, o alumínio diminui a atividade e a capacidade de difusão do carbono na austenita, o que reduz a força motriz para formação de carbonetos. O vanádio, que é adicionado como uma adição de elemento de liga essencial, forma carbonetos.[008] Using a high aluminum content, the stacking failure energy (SFE) of the steel increases. Any adverse effects of the elements that decrease SFE, such as silicon, are neutralized by the addition of aluminum. Additionally, aluminum decreases the activity and the diffusion capacity of carbon in austenite, which reduces the driving force for carbide formation. Vanadium, which is added as an addition of an essential alloying element, forms carbides.
Petição 870190028860, de 26/03/2019, pág. 6/22Petition 870190028860, of 03/26/2019, p. 6/22
4/114/11
Esses carbonetos de vanádio agem como absorvedores de hidrogênio se e quando o tamanho e a distribuição dos carbonetos de vanádio estiverem corretos. O teor de alumínio aumentado é, portanto, essencial para controlar a precipitação de carboneto de vanádio porque evita que o carboneto de vanádio engrosse devido à atividade reduzida do carbono e à capacidade de difusão como resultado da presença do alumínio. Os inventores descobriram que pelo menos 1,0% de Al e de 0,050% a 0,25% de V são necessários para alcançar isso. Teores de alumínio mais baixos levam a carbonetos de vanádio muito gossos, tornando-os assim ineficazes como sorvedouros de hidrogênio, e a quantidade de vanádio precisa ser controlada entre os valores mencionados para alcançar um número suficiente de pequenos precipitados, Valores mais altos de V levam a uma nucleação prévia dos precipitados e assim inevitavelmente em menos precipitados e mais grossos, com o que valores abaixo de 0,050% de V resultam simplesmente em poucos precipitados, mesmo se eles forem suficientemente finos. O tratamento de recozimento é crucial pelo fato de que ele controla a precipitação dos carbonetos de vanádio e provoca a recristalização da microestrutura deformada a frio provocada pela laminação a frio para resultar em uma estrutura de grão fino. Em uma configuração preferida, o teor de silício é muito baixo, isto é, a nível de impureza. Em princípio, o teor de alumínio é limitado apenas pelo fato de que o aço da invenção é um aço austenítico. Em uma configuração, o teor máximo de alumínio é 5%. Preferivelmente o teor de alumínio é pelo menos 1,25% e/ou no máximo 3,5%, mais preferivelmente pelo menos 1,5% e/ou no máximo 2,5%.These vanadium carbides act as hydrogen absorbers if and when the size and distribution of the vanadium carbides is correct. The increased aluminum content is therefore essential to control vanadium carbide precipitation because it prevents the vanadium carbide from thickening due to the reduced activity of the carbon and the diffusion capacity as a result of the presence of aluminum. The inventors found that at least 1.0% Al and 0.050% to 0.25% V are needed to achieve this. Lower aluminum contents lead to very greasy vanadium carbides, thus rendering them ineffective as hydrogen sinks, and the amount of vanadium needs to be controlled within the mentioned values to reach a sufficient number of small precipitates, Higher values of V lead prior nucleation of the precipitates and thus inevitably less precipitates and thicker ones, with which values below 0.050% of V simply result in few precipitates, even if they are sufficiently fine. The annealing treatment is crucial in that it controls the precipitation of vanadium carbides and causes the cold deformed microstructure to be recrystallized by cold rolling to result in a fine grain structure. In a preferred configuration, the silicon content is very low, that is, at the level of impurity. In principle, the aluminum content is limited only by the fact that the steel of the invention is an austenitic steel. In one configuration, the maximum aluminum content is 5%. Preferably the aluminum content is at least 1.25% and / or at most 3.5%, more preferably at least 1.5% and / or at most 2.5%.
[009] Em uma configuração a temperatura máxima de recozimento Ta é 825°C ou até mesmo 800°C. Em uma configuração, a taxa de resfriamento Vc está entre 10 e 100°C/s. A taxa de resfriamento preferível está entre 20 e 80°C/s. A taxa de aquecimento está preferivel[009] In a configuration the maximum annealing temperature Ta is 825 ° C or even 800 ° C. In one configuration, the cooling rate Vc is between 10 and 100 ° C / s. The preferred cooling rate is between 20 and 80 ° C / s. Heating rate is preferable
Petição 870190028860, de 26/03/2019, pág. 7/22Petition 870190028860, of 03/26/2019, p. 7/22
5/11 mente entre 3 e 60°C/s. O tempo de recozimento ta está preferivelmente entre 15 e 300 segundos.5/11 between 3 and 60 ° C / s. The annealing time t a is preferably between 15 and 300 seconds.
[0010] Em uma configuração preferida, a temperatura máxima de recozimento Ta é de 775°C a 795°C (isto é, 785 ± 10°C).[0010] In a preferred configuration, the maximum annealing temperature T a is 775 ° C to 795 ° C (ie 785 ± 10 ° C).
[0011] Preferivelmente o material de tira de aço foi decapado antes da laminação a frio. A decapagem é (frequentemente) necessária antes da laminação a frio para remover óxidos, para evitar a laminação de óxidos. Preferivelmente, o material de tira laminada a frio é produzido a partir de um material de tira laminada a quente ou uma correia de material de tira.[0011] Preferably the steel strip material was stripped before cold rolling. Pickling is (often) necessary before cold rolling to remove oxides, to prevent lamination of oxides. Preferably, the cold-rolled strip material is produced from a hot-rolled strip material or a strip of strip material.
[0012] Em uma configuração preferida da invenção, durante o resfriamento a uma taxa de resfriamento Vc após o recozimento contínuo, a tira é alimentada através de um banho de imersão a quente para fornecer um revestimento metálico por imersão a quente da tira em um banho fundido do metal fazendo o revestimento metálico. Esse processo leva a um processo muito rápido e econômico para produzir uma tira de aço metalicamente revestida. O revestimento metálico pode ser qualquer revestimento comum conhecido tais como zinco ou liga de zinco, onde o zinco pode estar ligado com elementos tais como alumínio e/ou magnésio.[0012] In a preferred embodiment of the invention, during cooling to a cooling rate Vc after continuous annealing, the strip is fed through a hot dip bath to provide a hot dip metal coating of the strip in a bath molten metal making the metallic coating. This process leads to a very fast and economical process to produce a metal-coated steel strip. The metallic coating can be any common known coating such as zinc or zinc alloy, where the zinc can be bonded with elements such as aluminum and / or magnesium.
[0013] Em outra configuração da invenção, a tira é decapada após o recozimento contínuo e onde a tira é provida de um revestimento metálico por decapagem após o recozimento seguida de aquecimento até uma temperatura abaixo da temperatura de recozimento contínuo antes de a tira ser levada através de um banho de imersão a quente para fornecer um revestimento metálico pela imersão da tira metálica em um banho de metal fundido fazendo o revestimento metálico. Esse processo alternativo está disponível se o processo econômico conforme descrito acima não for preferido. Pode haver problemas de adesão com certos revestimentos metálicos específicos para os quais um tra[0013] In another embodiment of the invention, the strip is stripped after continuous annealing and where the strip is provided with a metallic coating by pickling after annealing followed by heating to a temperature below the temperature of continuous annealing before the strip is taken through a hot dip bath to provide a metallic coating by immersing the metallic strip in a molten metal bath making the metallic coating. This alternative process is available if the economic process as described above is not preferred. There may be adhesion problems with certain specific metallic coatings for which a tra
Petição 870190028860, de 26/03/2019, pág. 8/22Petition 870190028860, of 03/26/2019, p. 8/22
6/11 tamento de decapagem pode ser necessário. Após a decapagem, não é necessário nem desejável aquecer a tira acima da temperatura Ta. É preferível que a temperatura de aquecimento permaneça abaixo de Ta.6/11 paint stripping may be required. After blasting, it is neither necessary nor desirable to heat the strip above temperature Ta. It is preferable that the heating temperature remains below Ta.
[0014] Com esse método, o material de tira é aquecido apenas até uma temperatura suficientemente alta para formar uma camada de inibição fechada. Essa temperatura é menor que a temperatura de recozimento contínuo normal necessário por razões metalúrgicas (tais como recristalização para influenciar as propriedades mecânicas). A formação de óxidos na superfície do material de tira de aço é, assim, reduzida.[0014] With this method, the strip material is heated only to a temperature high enough to form a closed inhibition layer. This temperature is less than the normal continuous annealing temperature required for metallurgical reasons (such as recrystallization to influence mechanical properties). The formation of oxides on the surface of the steel strip material is thus reduced.
[0015] Preferivelmente, a temperatura abaixo da temperatura de recozimento contínuo está entre 400°C e 600°C. Nessa faixa de temperaturas a formação de óxidos é consideravelmente reduzida, e o material de tira é suficientemente aquecido para a subsequente galvanização por imersão a quente.[0015] Preferably, the temperature below the continuous annealing temperature is between 400 ° C and 600 ° C. In this temperature range the formation of oxides is considerably reduced, and the strip material is sufficiently heated for subsequent hot dip galvanizing.
[0016] De acordo com uma configuração preferida, o Fe no material de tira é reduzido durante ou após o aquecimento até uma temperatura abaixo da temperatura de recozimento contínuo e antes da galvanização por imersão a quente.[0016] According to a preferred configuration, the Fe in the strip material is reduced during or after heating to a temperature below the temperature of continuous annealing and before hot dip galvanizing.
[0017] Reduzindo-se o material de tira, os óxidos de ferro que são formados são reduzidos, e dessa forma a quantidade de óxidos presentes na superfície do material de tira antes da galvanização por imersão a quente é consideravelmente diminuída.[0017] By reducing the strip material, the iron oxides that are formed are reduced, and in this way the amount of oxides present on the surface of the strip material before hot dip galvanizing is considerably reduced.
[0018] Preferivelmente, a redução é executada usando-se H2N2, mais preferivelmente usando-se 5 - 30% de H2N2 na atmosfera de redução. Foi descoberto que com o uso dessa atmosfera a maioria dos óxidos pode ser removida.[0018] Preferably, the reduction is carried out using H2N2, more preferably using 5 - 30% H2N2 in the reducing atmosphere. It has been found that with the use of this atmosphere, most oxides can be removed.
[0019] De acordo com uma configuração preferida, uma quantidade em excesso de O2 é fornecida na atmosfera durante ou após o[0019] According to a preferred configuration, an excess amount of O2 is supplied in the atmosphere during or after the
Petição 870190028860, de 26/03/2019, pág. 9/22Petition 870190028860, of 03/26/2019, p. 9/22
7/11 aquecimento do material de tira e antes da redução do material de tira. O fornecimento de uma quantidade em excesso de oxigênio melhora a qualidade da superfície do material de tira de aço antes da galvanização por imersão a quente, e assim também a qualidade da camada de zinco revestida no material de tira AHSS. É suposto que o oxigênio se aglutine aos elementos de liga no material de tira AHSS tanto na superfície do material de tira quanto internamente, e que dessa forma os óxidos formados não podem migrar para a superfície do material de tira.7/11 heating the strip material and before reducing the strip material. The supply of an excess amount of oxygen improves the surface quality of the steel strip material before hot dip galvanizing, as well as the quality of the zinc layer coated on the AHSS strip material. It is assumed that oxygen is bound to the alloying elements in the AHSS strip material both on the surface of the strip material and internally, and that thus the oxides formed cannot migrate to the surface of the strip material.
[0020] A atmosfera de redução que segue após a oxidação reduzirá então os óxidos na superfície do material de tira, e dessa forma a quantidade de óxidos na superfície do material de tira é consideravelmente reduzida ou até mesmo ausente, como as experiências mostraram. Preferivelmente, a quantidade excessiva de O2 é fornecida em uma quantidade de 0,05 - 5% de O2. Essa quantidade de oxigênio foi descoberta ser suficiente.[0020] The reducing atmosphere that follows after oxidation will then reduce the oxides on the surface of the strip material, and thus the amount of oxides on the surface of the strip material is considerably reduced or even absent, as experiments have shown. Preferably, the excessive amount of O2 is supplied in an amount of 0.05 - 5% O2. That amount of oxygen was found to be sufficient.
[0021] Em uma configuração preferida da invenção, material de tira de aço TWIP ligadas com V conforme a invenção foi laminado a quente, decapado e laminado a frio, e recozido continuamente até uma temperatura conforme a invenção, e decapada novamente. Então o material de tira é aquecido até uma temperatura de 527°C em uma linha de recozimento, e posteriormente galvanizada por imersão a quente em um banho de galvanização a aproximadamente 450°C.[0021] In a preferred embodiment of the invention, TWIP steel strip material bonded with V according to the invention was hot rolled, pickled and cold rolled, and continuously annealed to a temperature according to the invention, and pickled again. The strip material is then heated to a temperature of 527 ° C in an annealing line, and subsequently hot-dip galvanized in a galvanizing bath at approximately 450 ° C.
[0022] Durante o aquecimento do material de tira até a temperatura de 527°C, uma quantidade excessiva de 1% de O2 é fornecida. O oxigênio é fornecido a tal alta temperatura de modo que não apenas forma óxidos na superfície do material de tira, mas também a alguma profundidade sob a superfície e aglutina os elementos de liga. Após o fornecimento do oxigênio, o material de tira é reduzido usando-se aproximadamente 5% de H2N2. A redução do material de tira remove[0022] During the heating of the strip material to a temperature of 527 ° C, an excessive amount of 1% O2 is supplied. Oxygen is supplied at such a high temperature so that it not only forms oxides on the surface of the strip material, but also at some depth under the surface and binds the alloying elements. After delivery of oxygen, the strip material is reduced using approximately 5% H2N2. Reducing the strip material removes
Petição 870190028860, de 26/03/2019, pág. 10/22Petition 870190028860, of 03/26/2019, p. 10/22
8/11 os óxidos da superfície, mas os óxidos formados sob a superfície permanecem onde estão e não podem migrar para a superfície.8/11 the oxides on the surface, but the oxides formed under the surface remain where they are and cannot migrate to the surface.
[0023] Assim, pela redução os óxidos da superfície são efetivamente removidos e nenhum óxido novo pode ser formado na superfície. Esses óxidos, quando não removidos, provocam uma má adesão da camada de zinco ao substrato, resultando em pontos brilhantes, descamação e a formação de fraturas na camada de zinco quando o material é dobrado. É presumido que, pela redução normal, os elementos de liga migram para a superfície muito rapidamente a temperaturas de ligação e assim formam óxidos na superfície novamente antes que ocorra a galvanização por imersão a quente. Qualquer que possa ser o mecanismo exato, foi descoberto que o uso desse método diminui ou quase elimina a quantidade de óxidos descoberta em uma camada de zinco galvanizada por imersão a quente em um aço TWIP ligada com Vanádio.[0023] Thus, by reducing the surface oxides are effectively removed and no new oxides can be formed on the surface. These oxides, when not removed, cause poor adhesion of the zinc layer to the substrate, resulting in bright spots, flaking and the formation of fractures in the zinc layer when the material is bent. It is assumed that, by normal reduction, the alloying elements migrate to the surface very quickly at bonding temperatures and thus form oxides on the surface again before hot dip galvanizing occurs. Whatever the exact mechanism may be, it has been found that using this method decreases or almost eliminates the amount of oxides discovered in a hot dip galvanized zinc layer in a TWIP steel bonded with Vanadium.
[0024] Em uma configuração da invenção, a redução da laminação a frio está entre 10 e 90%, mais preferivelmente entre 30 e 85, ainda mais preferivelmente entre 45 e 80%.[0024] In a configuration of the invention, the reduction of cold rolling is between 10 and 90%, more preferably between 30 and 85, even more preferably between 45 and 80%.
[0025] Em uma configuração da invenção, a tira recozida sofre laminação de encruamento com uma redução de 0,5 a 10% antes de, ou após, o revestimento metálico ter sido fornecido à tira.[0025] In an embodiment of the invention, the annealed strip undergoes hardening lamination with a reduction of 0.5 to 10% before, or after, the metallic coating has been supplied to the strip.
[0026] Em uma configuração da invenção, o teor de vanádio está entre 0,06 e 0,22%.[0026] In one embodiment of the invention, the vanadium content is between 0.06 and 0.22%.
[0027] Em um segundo aspecto da invenção, é fornecida uma tira ou chapa produzida por um método conforme qualquer uma das reivindicações 1 a 6, onde o aço preferivelmente é provido com um revestimento metálico. Em uma configuração preferida da invenção, a tira ou chapa é usada para a produção de peças automotivas internas ou externas ou rodas ou para aplicações formação hidráulica;[0027] In a second aspect of the invention, a strip or sheet produced by a method according to any one of claims 1 to 6 is provided, where the steel is preferably provided with a metallic coating. In a preferred embodiment of the invention, the strip or sheet is used for the production of internal or external automotive parts or wheels or for hydraulic forming applications;
[0028] A invenção será agora também explicada por meio dos[0028] The invention will now also be explained through the
Petição 870190028860, de 26/03/2019, pág. 11/22Petition 870190028860, of 03/26/2019, p. 11/22
9/11 exemplos não limitativos a seguir.9/11 non-limiting examples to follow.
[0029] As composições químicas dos materiais usados nesse estudo estão mostradas na Tabela 1.[0029] The chemical compositions of the materials used in this study are shown in Table 1.
Tabela 1 - Composição química dos materiais estudados (inclusive material semi-industrial de referência livre se Si) (todos em % em peso, Saldo: Fe e impurezas)Table 1 - Chemical composition of the materials studied (including semi-industrial free reference material if Si) (all in% by weight, Balance: Fe and impurities)
*Baixo = nível de impureza [0030] A temperatura de término de laminação (FRT) foi escolhida para garantir a recristalização da microestrutura deformada e a temperatura de bobinamento foi mantida abaixo de 500°C para evitar a precipitação de carbonetos. A recristalização não depende apenas da FRT, mas também depende do tempo, da tensão de laminação acumulada desde o último evento de recristalização durante a laminação a quente e da taxa de tensão.* Low = level of impurity [0030] The rolling end temperature (FRT) was chosen to guarantee the recrystallization of the deformed microstructure and the winding temperature was kept below 500 ° C to prevent carbide precipitation. Recrystallization not only depends on the FRT, but also depends on the time, the rolling tension accumulated since the last recrystallization event during hot rolling and the stress rate.
[0031] Todos os materiais laminados a quente foram laminados a frio a 50% e subsequentemente recozidos para recristalização. Ciclos de recozimento diferentes foram aplicados para determinar os parâmetros de recozimento opcionais. Note que os alongamentos foram entre 45% e 50% para todas as amostras, exceto para aquelas que não foram recristalizadas (36-45%) e o material recozido a 920°C (65%). Uma vez que a resistência é considerada ser mais importante, a discussão a seguir vai focar nesse aspecto.[0031] All hot rolled materials were cold rolled 50% and subsequently annealed for recrystallization. Different annealing cycles were applied to determine the optional annealing parameters. Note that the stretches were between 45% and 50% for all samples, except for those that were not recrystallized (36-45%) and the material annealed at 920 ° C (65%). Since resistance is considered to be more important, the following discussion will focus on this aspect.
[0032] Para temperaturas de recozimento até 750°C, o material amolece devido a uma fração aumentada de material recristalizado e[0032] For annealing temperatures up to 750 ° C, the material softens due to an increased fraction of recrystallized material and
Petição 870190028860, de 26/03/2019, pág. 12/22Petition 870190028860, of 03/26/2019, p. 12/22
10/11 provavelmente algum crescimento de grão. A essas temperaturas, o efeito da precipitação é limitado. A diferença entre os materiais (totalmente recristalizados) recozidos a 775°C e 800°C é pequena porque a precipitação é considerada ótima nessa região de temperaturas para minimizar o crescimento do grão. Com base nessas observações, a temperatura de recozimento recomendada é 785°C ± 10°C.11/10 probably some grain growth. At these temperatures, the effect of precipitation is limited. The difference between the materials (fully recrystallized) annealed at 775 ° C and 800 ° C is small because precipitation is considered optimal in this temperature region to minimize grain growth. Based on these observations, the recommended annealing temperature is 785 ° C ± 10 ° C.
Tabela 1 - Propriedades mecânicas dos materiais após laminação a frio a 50% e recozimentoTable 1 - Mechanical properties of materials after cold rolling at 50% and annealing
[0033] Os resultados da fratura retardada e da fratura de corrosão de tensão no grau ligado com V mostram uma menor susceptibilidade à formação de fraturas à medida que o material é recozido a uma maior temperatura. Para a sensibilidade à fratura de corrosão de tensão, a adição de V é claramente benéfica a uma temperatura de recozimento[0033] The results of the delayed fracture and the stress corrosion fracture in the V-bonded degree show a lower susceptibility to fracture formation as the material is annealed at a higher temperature. For stress corrosion fracture sensitivity, the addition of V is clearly beneficial at an annealing temperature
Petição 870190028860, de 26/03/2019, pág. 13/22Petition 870190028860, of 03/26/2019, p. 13/22
11/11 de 750°C, mas também a temperaturas de recozimento mais altas. [0034] As ligas de V foram submetidas a testes de soldagem por pontos. A fratura a quente na solda foi grandemente reduzida comparada com o material livre de Si não ligado com V.11/11 at 750 ° C, but also at higher annealing temperatures. [0034] V alloys were subjected to spot welding tests. The hot fracture in the weld was greatly reduced compared to the Si free material not bonded with V.
Petição 870190028860, de 26/03/2019, pág. 14/22Petition 870190028860, of 03/26/2019, p. 14/22
Claims (13)
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Application Number | Priority Date | Filing Date | Title |
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EP10165596.7 | 2010-06-10 | ||
EP10165596 | 2010-06-10 | ||
PCT/EP2011/002868 WO2011154153A1 (en) | 2010-06-10 | 2011-06-10 | Method of producing an austenitic steel |
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BR112012031466A2 BR112012031466A2 (en) | 2016-11-08 |
BR112012031466B1 true BR112012031466B1 (en) | 2019-07-09 |
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BR112012031466-1A BR112012031466B1 (en) | 2010-06-10 | 2011-06-10 | METHOD OF PRODUCING AN EXCELLENT AUSTENTIC STEEL SHEET IN RESISTANCE TO DELAYED FRACTURE AND STRIP OR SHEET |
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US (1) | US20130118647A1 (en) |
EP (1) | EP2580359B1 (en) |
JP (1) | JP6009438B2 (en) |
KR (1) | KR101900963B1 (en) |
CN (1) | CN102939394A (en) |
BR (1) | BR112012031466B1 (en) |
WO (1) | WO2011154153A1 (en) |
ZA (1) | ZA201300240B (en) |
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DE102013003516A1 (en) * | 2013-03-04 | 2014-09-04 | Outokumpu Nirosta Gmbh | Process for the production of an ultra-high-strength material with high elongation |
DE102015111866A1 (en) | 2015-07-22 | 2017-01-26 | Salzgitter Flachstahl Gmbh | Formable lightweight structural steel with improved mechanical properties and process for the production of semi-finished products from this steel |
EP4119683A1 (en) * | 2015-12-28 | 2023-01-18 | United States Steel Corporation | Delayed cracking prevention during drawing of high strength steel |
KR101747034B1 (en) * | 2016-04-28 | 2017-06-14 | 주식회사 포스코 | Ultra high strength and high ductility steel sheet having excellent yield ratio, and method for manufacturing the same |
WO2017203315A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
US11414721B2 (en) | 2016-05-24 | 2022-08-16 | Arcelormittal | Method for the manufacture of TWIP steel sheet having an austenitic matrix |
WO2017203314A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Twip steel sheet having an austenitic matrix |
WO2017203310A1 (en) | 2016-05-24 | 2017-11-30 | Arcelormittal | Method for producing a twip steel sheet having an austenitic microstructure |
WO2017203309A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Twip steel sheet having an austenitic matrix |
WO2017203312A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
WO2017203311A1 (en) * | 2016-05-24 | 2017-11-30 | Arcelormittal | Cold rolled and annealed steel sheet, method of production thereof and use of such steel to produce vehicle parts |
DE102016117508B4 (en) | 2016-09-16 | 2019-10-10 | Salzgitter Flachstahl Gmbh | Process for producing a flat steel product from a medium manganese steel and such a flat steel product |
KR101889185B1 (en) | 2016-12-21 | 2018-08-16 | 주식회사 포스코 | Hot-rolled steel sheet having superior formability and fatigue property, and method for manufacturing the same |
CN108929991B (en) * | 2017-05-26 | 2020-08-25 | 宝山钢铁股份有限公司 | Hot-dip plated high manganese steel and manufacturing method thereof |
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DE69226946T2 (en) * | 1991-12-30 | 1999-05-12 | Po Hang Iron & Steel | AUSTENITIC MANGANIC STEEL SHEET WITH HIGH DEFORMABILITY, STRENGTH AND WELDABILITY AND METHOD |
FR2731713B1 (en) * | 1995-03-14 | 1997-04-11 | Ugine Sa | PROCESS FOR THE MANUFACTURE OF A SHEET OF ELECTRIC STEEL WITH ORIENTED GRAINS FOR THE PRODUCTION OF MAGNETIC TRANSFORMER CIRCUITS IN PARTICULAR |
KR970043162A (en) * | 1995-12-30 | 1997-07-26 | 김종진 | Annealing heat treatment method and pickling method of high manganese cold rolled steel |
FR2881144B1 (en) * | 2005-01-21 | 2007-04-06 | Usinor Sa | PROCESS FOR MANUFACTURING FERRO-CARBON-MANGANIZED AUSTENITIC STEEL TILES HAVING HIGH RESISTANCE TO DELAYED CRACKING, AND SHEETS THUS PRODUCED |
KR20070099684A (en) * | 2005-02-02 | 2007-10-09 | 코루스 스타알 베.뷔. | Austenitic steel having high strength and formability, method of producing said steel and use thereof |
KR100742833B1 (en) * | 2005-12-24 | 2007-07-25 | 주식회사 포스코 | High Mn Steel Sheet for High Corrosion Resistance and Method of Manufacturing Galvanizing the Steel Sheet |
KR100851158B1 (en) * | 2006-12-27 | 2008-08-08 | 주식회사 포스코 | High Manganese High Strength Steel Sheets With Excellent Crashworthiness, And Method For Manufacturing Of It |
WO2008135445A1 (en) * | 2007-05-02 | 2008-11-13 | Corus Staal B.V. | Method for hot dip galvanising of ahss or uhss strip material, and such material |
KR20090070509A (en) * | 2007-12-27 | 2009-07-01 | 주식회사 포스코 | High manganese coated steel sheet having high strength and ductility and manufacturing method thereof |
KR100985286B1 (en) * | 2007-12-28 | 2010-10-04 | 주식회사 포스코 | High Manganese Steel Having High Strength and Excellent Delayed Fracture Resistance and Manufacturing Method Thereof |
EP2090668A1 (en) * | 2008-01-30 | 2009-08-19 | Corus Staal BV | Method of producing a high strength steel and high strength steel produced thereby |
EP2257394B1 (en) * | 2008-01-30 | 2018-11-07 | Tata Steel IJmuiden BV | Method of producing a hot-rolled twip-steel and a twip-steel product produced thereby |
KR101079472B1 (en) * | 2008-12-23 | 2011-11-03 | 주식회사 포스코 | Method for Manufacturing High Manganese Hot Dip Galvanizing Steel Sheet with Superior Surface Property |
EP2208803A1 (en) * | 2009-01-06 | 2010-07-21 | ThyssenKrupp Steel Europe AG | High-tensile, cold formable steel, steel flat product, method for producing a steel flat product and use of a steel flat product |
-
2011
- 2011-06-10 JP JP2013513585A patent/JP6009438B2/en active Active
- 2011-06-10 BR BR112012031466-1A patent/BR112012031466B1/en not_active IP Right Cessation
- 2011-06-10 KR KR1020127032074A patent/KR101900963B1/en active IP Right Grant
- 2011-06-10 CN CN2011800284065A patent/CN102939394A/en active Pending
- 2011-06-10 WO PCT/EP2011/002868 patent/WO2011154153A1/en active Application Filing
- 2011-06-10 EP EP11725880.6A patent/EP2580359B1/en active Active
- 2011-06-10 US US13/699,516 patent/US20130118647A1/en not_active Abandoned
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2013
- 2013-01-10 ZA ZA2013/00240A patent/ZA201300240B/en unknown
Also Published As
Publication number | Publication date |
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CN102939394A (en) | 2013-02-20 |
US20130118647A1 (en) | 2013-05-16 |
WO2011154153A1 (en) | 2011-12-15 |
EP2580359B1 (en) | 2017-08-09 |
JP2013534566A (en) | 2013-09-05 |
ZA201300240B (en) | 2014-03-26 |
BR112012031466A2 (en) | 2016-11-08 |
EP2580359A1 (en) | 2013-04-17 |
KR20130111214A (en) | 2013-10-10 |
KR101900963B1 (en) | 2018-09-20 |
JP6009438B2 (en) | 2016-10-19 |
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