ES3055855T3 - Coated steel sheet and high strength press hardened steel part and method of manufacturing the same - Google Patents
Coated steel sheet and high strength press hardened steel part and method of manufacturing the sameInfo
- Publication number
- ES3055855T3 ES3055855T3 ES21819985T ES21819985T ES3055855T3 ES 3055855 T3 ES3055855 T3 ES 3055855T3 ES 21819985 T ES21819985 T ES 21819985T ES 21819985 T ES21819985 T ES 21819985T ES 3055855 T3 ES3055855 T3 ES 3055855T3
- Authority
- ES
- Spain
- Prior art keywords
- steel sheet
- steel
- layer
- mass
- temperature
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C47/00—Winding-up, coiling or winding-off metal wire, metal band or other flexible metal material characterised by features relevant to metal processing only
- B21C47/02—Winding-up or coiling
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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
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
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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
- C21D6/00—Heat treatment of ferrous alloys
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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
- C21D8/00—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
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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
- C21D8/00—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
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- C—CHEMISTRY; METALLURGY
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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
- C21D8/00—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties of ferrous metals or ferrous alloys 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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- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0278—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular surface treatment
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- C—CHEMISTRY; METALLURGY
- 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 of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for drawing, e.g. for deep-drawing
- C21D8/0421—Modifying the physical properties of ferrous metals or ferrous alloys by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for drawing, e.g. for deep-drawing characterised by the working steps
- C21D8/0436—Cold rolling
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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
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/40—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for rings; for bearing races
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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
- 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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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- 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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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of manganese
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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
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
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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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- 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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- 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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- C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
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- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/12—Aluminium or alloys based thereon
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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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- 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
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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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- C23C2/29—Cooling or quenching
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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
- C23C2/34—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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- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
- C23G1/02—Cleaning or pickling metallic material with solutions or molten salts with acid solutions
- C23G1/08—Iron or steel
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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
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
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- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- General Chemical & Material Sciences (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Heat Treatment Of Steel (AREA)
- Heat Treatment Of Articles (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Electroplating Methods And Accessories (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Physical Vapour Deposition (AREA)
Abstract
La invención trata de una chapa de acero revestida y una pieza de acero endurecido a presión que tiene una composición que comprende, en porcentaje en peso: C 0,26-0,40%, Mn 0,5-1,8%, Si 0,1-1,25%, Al 0,01-0,1%, Cr 0,1-1,0%, Ti 0,01-0,1%, B 0,001-0,004%, P <= 0,020%, S <= 0,010%, N <= 0,010% siendo el resto de la composición hierro e impurezas inevitables resultantes de la fundición. La pieza de acero endurecida a presión comprende un volumen que tiene una microestructura que comprende, en fracción de superficie, más del 95% de martensita y menos del 5% de bainita, una capa de revestimiento en la superficie de la pieza de acero, una capa de interdifusión ferrítica entre la capa de revestimiento y el volumen, y una relación entre el ancho de grano ferrítico en la capa de interdifusión GWint sobre el tamaño de grano de austenita anterior en el volumen PAGSbulk, que satisface la siguiente ecuación (GWint/PAGSbulk) -1 >= 30%. (Traducción automática con Google Translate, sin valor legal)The invention relates to a coated steel sheet and a pressure-hardened steel part having a composition comprising, in weight percentage: C 0.26-0.40%, Mn 0.5-1.8%, Si 0.1-1.25%, Al 0.01-0.1%, Cr 0.1-1.0%, Ti 0.01-0.1%, B 0.001-0.004%, P <= 0.020%, S <= 0.010%, N <= 0.010%, the remainder of the composition being iron and unavoidable impurities resulting from smelting. The pressure-hardened steel part comprises a bulk having a microstructure comprising, as a surface fraction, more than 95% martensite and less than 5% bainite, a coating layer on the surface of the steel part, a ferritic interdiffusion layer between the coating layer and the bulk, and a ratio of the ferritic grain width in the interdiffusion layer GWint to the austenite grain size above in the bulk PAGSbulk, satisfying the following equation (GWint/PAGSbulk) - 1 >= 30%.
Description
[0001] DESCRIPCIÓN[0001] DESCRIPTION
[0002] Lámina de acero recubierta y pieza de acero endurecido por presión a alta resistencia y su procedimiento de fabricación[0002] Coated steel sheet and high-strength pressure-hardened steel part and its manufacturing process
[0003] La presente invención se refiere a láminas de acero recubiertas y a piezas de acero endurecido por presión a alta resistencia que tienen buenas propiedades de capacidad de flexión.[0003] The present invention relates to coated steel sheets and to high-strength pressure-hardened steel parts that have good bending capacity properties.
[0004] Las piezas endurecidas por presión a alta resistencia pueden usarse como elementos estructurales en vehículos automotores para funciones de antiintrusión o absorción de energía.[0004] High-strength pressure-hardened parts can be used as structural elements in motor vehicles for anti-intrusion or energy-absorbing functions.
[0005] En dicho tipo de aplicaciones, es deseable producir piezas de acero que combinen alta resistencia mecánica, alta resistencia al impacto y buena resistencia a la corrosión. Por otra parte, uno de los principales desafíos en la industria automotriz es disminuir el peso de los vehículos para mejorar su eficiencia en consumo de combustible en vista de la conservación global del medio ambiente, sin descuidar los requisitos de seguridad.[0005] In such applications, it is desirable to produce steel parts that combine high mechanical strength, high impact resistance, and good corrosion resistance. Furthermore, one of the main challenges in the automotive industry is to reduce vehicle weight to improve fuel efficiency in light of global environmental conservation, without neglecting safety requirements.
[0006] Esta reducción de peso se puede lograr en particular gracias al uso de piezas de acero con una microestructura martensítica o bainítica/martensítica.[0006] This weight reduction can be achieved in particular through the use of steel parts with a martensitic or bainitic/martensitic microstructure.
[0007] La publicación WO2016104881 se refiere a una pieza de conformación por prensado en caliente usada como parte estructural de un vehículo o similares, que requiere características de resistencia al impacto y, más particularmente, que tiene una resistencia a la tracción de 1300 MPa o superior y un procedimiento de fabricación de la misma calentando un material de acero a una temperatura a la que se puede formar una fase única de austenita, y templando y conformando en caliente el mismo usando un molde. Para obtener tales propiedades, la lámina de acero base comprende una capa de ferrita delgada inferior a 50 μm en la superficie, y el tamaño y la densidad de los carburos deben controlarse. Esta capa de ferrita en el sustrato permite inhibir la propagación de las grietas finas formadas en la capa de enchapado a la base, pero da lugar a una baja capacidad de flexión con un ángulo de flexión inferior a 70°.[0007] Publication WO2016104881 relates to a hot-formed part used as a structural component of a vehicle or similar, requiring impact resistance characteristics and, more particularly, having a tensile strength of 1300 MPa or higher, and a manufacturing process involving heating a steel material to a temperature at which a single austenite phase can be formed, and quenching and hot-forming the same using a die. To obtain such properties, the base steel sheet comprises a thin ferrite layer less than 50 μm thick on the surface, and the size and density of the carbides must be controlled. This ferrite layer on the substrate inhibits the propagation of fine cracks formed in the plating layer to the base, but results in low bending capacity with a bending angle of less than 70°.
[0008] La publicación WO2018179839 se refiere a una pieza prensada en caliente obtenida prensando en caliente una lámina de acero que tiene una microestructura que cambia en la dirección del espesor, con una capa blanda hecha de al menos 90 % de ferrita, una capa de transición hecha de ferrita y martensita y una capa dura principalmente martensítica y con una alta resistencia y una alta capacidad de flexión. Para obtener tales propiedades, la lámina de acero laminada en frío se recuece en una atmósfera con una temperatura de punto de rocío que comprendiendo de 50 °C a 90 °C, lo que podría ser perjudicial para el recubrimiento con aleación de aluminio. En los documentos US2017/260599A1 y WO2018/220540A1 se describe la técnica anterior adicional.[0008] Publication WO2018179839 relates to a hot-pressed part obtained by hot-pressing a steel sheet having a microstructure that changes in the thickness direction, with a soft layer made of at least 90% ferrite, a transition layer made of ferrite and martensite, and a hard, primarily martensitic layer, exhibiting high strength and high bending capacity. To obtain such properties, the cold-rolled steel sheet is annealed in an atmosphere with a dew point temperature ranging from 50°C to 90°C, which could be detrimental to the aluminum alloy coating. Further prior art is described in documents US2017/260599A1 and WO2018/220540A1.
[0009] Por lo tanto, el objeto de la invención es resolver el problema mencionado anteriormente y proporcionar una pieza de acero endurecido por presión que tenga una combinación de altas propiedades mecánicas con la resistencia a la tracción TS superior o igual a 1500 MPa y un ángulo de flexión superior a 70°. La pieza de acero endurecido por presión según la invención tiene un límite elástico YS superior o igual a 1250 MPa.[0009] Therefore, the object of the invention is to solve the aforementioned problem and provide a pressure-hardened steel part having a combination of high mechanical properties with a tensile strength TS greater than or equal to 1500 MPa and a bending angle greater than 70°. The pressure-hardened steel part according to the invention has a yield strength YS greater than or equal to 1250 MPa.
[0010] Otro objeto de la invención es obtener una lámina de acero recubierta que pueda transformarse por conformación en caliente en dicha pieza de acero endurecido por presión.[0010] Another object of the invention is to obtain a coated steel sheet that can be transformed by hot forming into said pressure-hardened steel piece.
[0011] El objeto de la presente invención se logra proporcionando una lámina de acero según la reivindicación 1. Otro objeto se logra proporcionando el procedimiento según la reivindicación 2. Otro objeto de la presente invención se logra proporcionando una pieza de acero endurecido por presión según la reivindicación 3. La pieza de acero también puede comprender las características de la reivindicación 4. Otro objeto se logra proporcionando el procedimiento según la reivindicación 5.[0011] The object of the present invention is achieved by providing a steel sheet according to claim 1. Another object is achieved by providing the process according to claim 2. Another object of the present invention is achieved by providing a pressure-hardened steel piece according to claim 3. The steel piece may also comprise the features of claim 4. Another object is achieved by providing the process according to claim 5.
[0012] La invención se describirá ahora en detalle y se ilustrará por ejemplos sin introducir limitaciones, con referencia a las figuras adjuntas:[0012] The invention will now be described in detail and illustrated by examples without introducing limitations, with reference to the accompanying figures:
[0013] - la Figura 1a ilustra una sección esquemática de la lámina de acero recubierta del ensayo 4, que no es según la invención[0013] - Figure 1a illustrates a schematic section of the coated steel sheet of test 4, which is not according to the invention
[0014] - la Figura 1b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 4, que no es según la invención[0014] - Figure 1b represents a schematic section of the pressure-hardened steel piece of test 4, which is not according to the invention
[0015] - la Figura 2a ilustra una sección esquemática de la lámina de acero recubierta del ensayo 3, que no es según la invención[0015] - Figure 2a illustrates a schematic section of the coated steel sheet of test 3, which is not according to the invention
[0016] - la Figura 2b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 3, que no es según la invención[0016] - Figure 2b represents a schematic section of the pressure-hardened steel piece of test 3, which is not according to the invention
[0017] - la Figura 3a ilustra una sección esquemática de la lámina de acero recubierta del ensayo 2, que es según la invención - la Figura 3b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 2, que es según la invención[0017] - Figure 3a illustrates a schematic section of the coated steel sheet of test 2, which is according to the invention - Figure 3b represents a schematic section of the pressure-hardened steel piece of test 2, which is according to the invention
[0018] - la Figura 4a ilustra una sección esquemática de la lámina de acero recubierta del ensayo 1, que es según la invención - la Figura 4b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 1, que es según la invención[0018] - Figure 4a illustrates a schematic section of the coated steel sheet of test 1, which is according to the invention - Figure 4b represents a schematic section of the pressure-hardened steel piece of test 1, which is according to the invention
[0019] - la Figura 5a ilustra una sección esquemática de la lámina de acero recubierta del ensayo 5, que no es según la invención[0019] - Figure 5a illustrates a schematic section of the coated steel sheet of test 5, which is not according to the invention
[0020] - la Figura 5b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 5, que no es según la invención[0020] - Figure 5b represents a schematic section of the pressure-hardened steel piece of test 5, which is not according to the invention
[0021] A continuación, se describirá la composición del acero según la invención, expresándose el contenido en porcentaje en peso.[0021] The composition of the steel according to the invention will now be described, with the content expressed as a percentage by weight.
[0022] Según la invención, el contenido de carbono está comprendido entre 0,26 % y 0,40 % para garantizar una resistencia satisfactoria. Por encima del 0,40 % de carbono, se puede reducir la soldabilidad y la capacidad de flexión de la lámina de acero. Si el contenido de carbono es inferior a 0,26 %, la resistencia a la tracción no alcanzará el valor objetivo.[0022] According to the invention, the carbon content is between 0.26% and 0.40% to ensure satisfactory strength. Above 0.40% carbon, the weldability and bending capacity of the steel sheet may be reduced. If the carbon content is less than 0.26%, the tensile strength will not reach the target value.
[0023] El contenido de manganeso está comprendido entre 0,5 % y 1,8 %. Por encima del 1,8 % de adición, el riesgo de segregación central aumenta en detrimento de la capacidad de flexión. Por debajo del 0,5 %, la capacidad de endurecimiento de la lámina de acero se reduce. Preferentemente, el contenido de manganeso está comprendido entre 0,5 % y 1,3 %.[0023] The manganese content is between 0.5% and 1.8%. Above 1.8% addition, the risk of central segregation increases, impairing flexural strength. Below 0.5%, the hardenability of the steel sheet is reduced. Preferably, the manganese content is between 0.5% and 1.3%.
[0024] Según la invención, el contenido de silicio está comprendido entre 0,1 % y 1,25 %. El silicio es un elemento que participa en el endurecimiento en solución sólida. Se añade silicio para limitar la formación de carburos. Por encima del 1,25 % se forman óxidos de silicio en la superficie, lo que perjudica la capacidad de recubrimiento del acero. Por otra parte, la soldabilidad de la lámina de acero puede verse reducida. Preferentemente, el contenido de silicio está comprendido entre 0,2 % y 1,25 %. Más preferentemente, el contenido de silicio es del 0,3 % al 1,25 %. Más preferentemente, el contenido de silicio es del 0,3 % al 1 %.[0024] According to the invention, the silicon content is between 0.1% and 1.25%. Silicon is an element involved in solid solution hardening. Silicon is added to limit carbide formation. Above 1.25%, silicon oxides form on the surface, which impairs the steel's coating capacity. Furthermore, the weldability of the steel sheet may be reduced. Preferably, the silicon content is between 0.2% and 1.25%. More preferably, the silicon content is from 0.3% to 1.25%. More preferably, the silicon content is from 0.3% to 1%.
[0025] El contenido de aluminio está comprendido entre 0,01 % y 0,1 %, dado que es un elemento muy efectivo para desoxidar el acero en la fase líquida durante su elaboración. El aluminio puede proteger el boro si el contenido de titanio no es suficiente. El contenido de aluminio es inferior al 0,1 % para evitar problemas de oxidación y formación de ferrita durante el endurecimiento por presión. Preferentemente, el contenido de aluminio está comprendido entre 0,01 % y 0,05 %.[0025] The aluminum content is between 0.01% and 0.1%, as it is a very effective element for deoxidizing steel in the liquid phase during its processing. Aluminum can protect boron if the titanium content is insufficient. The aluminum content is less than 0.1% to avoid oxidation problems and ferrite formation during pressure hardening. Preferably, the aluminum content is between 0.01% and 0.05%.
[0026] Según la invención, el contenido de cromo está comprendido entre 0,1 % y 1,0 %. El cromo es un elemento que participa en el endurecimiento en solución sólida y debe ser superior al 0,1 %. El contenido de cromo es inferior al 1,0 % para limitar los problemas de procesabilidad y el coste.[0026] According to the invention, the chromium content is between 0.1% and 1.0%. Chromium is an element that participates in solid solution hardening and must be greater than 0.1%. The chromium content is less than 1.0% to limit processability problems and cost.
[0027] El contenido de titanio está comprendido entre 0,01 % y 0,1 % con el fin de proteger el boro de la formación de BN. El contenido de titanio se limita a 0,1 % para evitar la formación de TiN.[0027] The titanium content is between 0.01% and 0.1% in order to protect boron from the formation of BN. The titanium content is limited to 0.1% to prevent the formation of TiN.
[0028] Según la invención, el contenido de boro está comprendido entre 0,001 % y 0,004 %. El boro mejora la capacidad de endurecimiento del acero. El contenido de boro no es superior al 0,004 % para evitar el riesgo de rotura del desbaste plano durante la colada continua.[0028] According to the invention, the boron content is between 0.001% and 0.004%. Boron improves the hardenability of the steel. The boron content does not exceed 0.004% to avoid the risk of breakage of the flat roughing during continuous casting.
[0029] Algunos elementos se pueden añadir opcionalmente.[0029] Some elements can be added optionally.
[0030] Se puede añadir níquel hasta un 0,5 % como elemento opcional, ya que puede reducir sustancialmente la sensibilidad a la fractura retardada.[0030] Nickel up to 0.5% can be added as an optional element, as it can substantially reduce sensitivity to delayed fracture.
[0031] Se puede añadir opcionalmente un contenido de molibdeno de hasta un 0,40 %. Como el boro, el molibdeno mejora la capacidad de endurecimiento del acero. El molibdeno no es superior al 0,40 % para limitar el coste.[0031] A molybdenum content of up to 0.40% may be added optionally. Like boron, molybdenum improves the hardenability of the steel. The molybdenum content is not greater than 0.40% to limit cost.
[0032] Según la invención, se puede añadir opcionalmente hasta un 0,08 % de niobio para mejorar la ductilidad del acero. Por encima del 0,08 % de adición, el riesgo de formación de carburos NbC o Nb(C,N) aumenta en detrimento de la capacidad de flexión. Preferentemente, el contenido de niobio es inferior o igual al 0,05 %.[0032] According to the invention, up to 0.08% niobium may be optionally added to improve the ductility of the steel. Above 0.08% addition, the risk of NbC or Nb(C,N) carbide formation increases, impairing the bending capacity. Preferably, the niobium content is less than or equal to 0.05%.
[0033] El calcio también se puede añadir hasta un 0,1 % como un elemento opcional. La adición de Ca en la etapa líquida permite crear óxidos finos que promueven la colabilidad de la colada continua.[0033] Calcium can also be added up to 0.1% as an optional element. The addition of Ca in the liquid stage allows the creation of fine oxides that promote the castability of the continuous casting.
[0034] El resto de la composición del acero es hierro e impurezas resultantes de la fundición. A este respecto, P, S y N al menos se consideran elementos residuales que son impurezas inevitables. Su contenido es inferior al 0,010 % para S, inferior al 0,020 % para P e inferior al 0,010 % para N.[0034] The remainder of the steel composition is iron and impurities resulting from smelting. In this respect, P, S, and N are at least considered residual elements that are unavoidable impurities. Their content is less than 0.010% for S, less than 0.020% for P, and less than 0.010% for N.
[0035] A continuación, se describirá la microestructura de la lámina de acero recubierta según la invención.[0035] The microstructure of the coated steel sheet according to the invention will now be described.
[0036] Una sección de una lámina de acero recubierta de la invención se representa esquemáticamente en la Fig.3a y la Fig.4a. La lámina de acero recubierta comprende una masa (2) cubierta por una capa descarburada (3) comprendiendo en la parte superior una capa de ferrita que tiene un espesor de 1 μm a 100 μm (4), y una capa de recubrimiento (1). Preferentemente, el espesor de la capa de ferrita está comprendido entre 20 μm y 100 μm. Más preferentemente, el espesor de la capa de ferrita es de 25 μm a 100 μm. Más preferentemente, el espesor de la capa de ferrita es de 30 μm a 80 μm.[0036] A section of a coated steel sheet of the invention is schematically represented in Fig. 3a and Fig. 4a. The coated steel sheet comprises a mass (2) covered by a decarburized layer (3) comprising, on top, a ferrite layer having a thickness of 1 μm to 100 μm (4), and a coating layer (1). Preferably, the thickness of the ferrite layer is between 20 μm and 100 μm. More preferably, the thickness of the ferrite layer is from 25 μm to 100 μm. More preferably, the thickness of the ferrite layer is from 30 μm to 80 μm.
[0037] La masa de la lámina de acero recubierta (2) tiene una microestructura comprendiendo, en una fracción superficial, del 60 % al 90 % de ferrita, siendo el resto islas de martensita-austenita, perlita o bainita.[0037] The mass of the coated steel sheet (2) has a microstructure comprising, in a surface fraction, 60% to 90% ferrite, the remainder being islands of martensite-austenite, pearlite or bainite.
[0038] Esta ferrita se forma durante el recocido intercrítico de la lámina de acero laminada en frío. El resto de la microestructura es austenita al final de la homogeneización, que se transforma en islas de martensita-austenita, perlita o bainita durante el enfriamiento de la lámina de acero.[0038] This ferrite forms during the intercritical annealing of the cold-rolled steel sheet. The remainder of the microstructure is austenite at the end of homogenization, which transforms into islands of martensite-austenite, pearlite, or bainite during cooling of the steel sheet.
[0039] La capa descarburada presente en la parte superior de la masa se obtiene durante el recocido de la lámina de acero laminada en frío gracias al control de la atmósfera en el horno para establecer una temperatura de punto de rocío estrictamente superior a -10 °C e inferior o igual a 20 °C.[0039] The decarburized layer present on the top of the mass is obtained during the annealing of the cold-rolled steel sheet by controlling the atmosphere in the furnace to establish a dew point temperature strictly above -10 °C and below or equal to 20 °C.
[0040] La lámina de acero recubierta según la invención se puede producir por cualquier procedimiento de fabricación adecuado y el experto en la materia puede definir uno. Sin embargo, se prefiere usar el procedimiento según la invención, comprendiendo las etapas siguientes:[0040] The coated steel sheet according to the invention can be produced by any suitable manufacturing process, and one can be defined by a person skilled in the art. However, the process according to the invention is preferred, comprising the following steps:
[0041] Un semiproducto que puede ser laminado en caliente adicionalmente se proporciona con la composición de acero descrita anteriormente. El semiproducto se recalienta a una temperatura comprendida entre 1150 °C y 1300 °C.[0041] A semi-finished product that can be further hot-rolled is provided with the steel composition described above. The semi-finished product is reheated to a temperature between 1150 °C and 1300 °C.
[0042] A continuación, la lámina de acero se lamina en caliente a una temperatura de laminación en caliente de acabado comprendida entre 800 °C y 950 °C.[0042] Next, the steel sheet is hot rolled at a finishing hot rolling temperature of between 800 °C and 950 °C.
[0043] A continuación, el acero laminado en caliente se enfría y bobina a una temperatura T<bobina>inferior a 670 °C y, opcionalmente, se decapa para eliminar la oxidación.[0043] Next, the hot-rolled steel is cooled and coiled to a temperature T<coil> below 670 °C and, optionally, pickled to remove rust.
[0044] A continuación, la lámina de acero bobinada se lamina en frío para obtener una lámina de acero laminada en frío. La relación de reducción de laminación en frío está comprendida preferentemente entre 20 % y 80 %. Por debajo del 20 %, no se favorece la recristalización durante el tratamiento térmico posterior, lo que puede perjudicar la ductilidad de la lámina de acero. Por encima del 80 %, existe el riesgo de agrietamiento de los bordes durante la laminación en frío.[0044] The coiled steel sheet is then cold-rolled to obtain a cold-rolled steel sheet. The cold-rolling reduction ratio is preferably between 20% and 80%. Below 20%, recrystallization is not favored during subsequent heat treatment, which may impair the ductility of the steel sheet. Above 80%, there is a risk of edge cracking during cold rolling.
[0045] La lámina de acero se recuece a continuación en una atmósfera de HNx con de 0 % a 15 % de H2, a una temperatura de recocido T<A>comprendida entre 700 °C y 850 °C y se mantiene a dicha temperatura de recocido T<A>durante un tiempo de mantenimiento t<A>comprendido entre 10 s y 1200 s, con el fin de obtener una lámina de acero recocida. Por debajo de 700 °C, la cinética de formación de la capa descarburada es demasiado lenta para obtener una capa de ferrita en su parte superior. El tiempo de mantenimiento t<A>es superior o igual a10 s para permitir que se forme la capa de ferrita, y por debajo o igual a 1200 s para limitar el espesor de esta capa de ferrita.[0045] The steel sheet is then annealed in an HNx atmosphere with 0% to 15% H2, at an annealing temperature T<A> between 700 °C and 850 °C and held at that annealing temperature T<A> for a holding time t<A> between 10 s and 1200 s, in order to obtain an annealed steel sheet. Below 700 °C, the kinetics of decarburized layer formation are too slow to obtain a ferrite layer on top. The holding time t<A> is greater than or equal to 10 s to allow the ferrite layer to form, and less than or equal to 1200 s to limit the thickness of this ferrite layer.
[0046] Durante este recocido, la atmósfera en el horno se controla para que tenga una temperatura de punto de rocío T<DP1>estrictamente superior a -10 °C e inferior o igual a 20 °C con el fin de formar una capa descarburada según la invención. Si T<DP1>es inferior o igual a -10 °C, la formación de la capa descarburada se ralentiza y la capa de ferrita no se forma en su parte superior. La capacidad de flexión de la pieza de acero será demasiado baja. Si T<DP1>es superior a 20 °C, la superficie de la lámina de acero puede estar completamente oxidada, lo que perjudica la capacidad de recubrimiento y las propiedades mecánicas de la lámina.[0046] During this annealing process, the atmosphere in the furnace is controlled to have a dew point temperature T<DP1> strictly above -10 °C and below or equal to 20 °C in order to form a decarburized layer according to the invention. If T<DP1> is below or equal to -10 °C, the formation of the decarburized layer is slowed, and the ferrite layer does not form on top. The bending capacity of the steel part will be too low. If T<DP1> is above 20 °C, the surface of the steel sheet may be completely oxidized, which impairs the coating capacity and mechanical properties of the sheet.
[0047] En una realización de la invención, la lámina de acero recocida se calienta a una temperatura de recocido T2 comprendida entre 700 °C y 850 °C y se mantiene a dicha temperatura T2 durante un tiempo de mantenimiento t2 comprendido entre 10 s y 1200 s, teniendo la atmósfera un punto de rocío T<DP2>estrictamente superior a -10 °C e inferior o igual a 20 °C.[0047] In one embodiment of the invention, the annealed steel sheet is heated to an annealing temperature T2 between 700 °C and 850 °C and held at said temperature T2 for a holding time t2 between 10 s and 1200 s, the atmosphere having a dew point T<DP2> strictly above -10 °C and less than or equal to 20 °C.
[0048] A continuación, la lámina de acero se recubre con un recubrimiento de aleación de aluminio.[0048] Next, the steel sheet is coated with an aluminum alloy coating.
[0049] Ahora se describirá la microestructura de la pieza de acero endurecido por presión según la invención. Una sección de la pieza de acero endurecido por presión se representa esquemáticamente en la Fig.3b y la Fig.4b.[0049] The microstructure of the pressure-hardened steel part according to the invention will now be described. A section of the pressure-hardened steel part is shown schematically in Fig. 3b and Fig. 4b.
[0050] La pieza de acero comprende sucesivamente desde la masa hasta la superficie de la pieza de acero: - una masa (7) que tiene una microestructura comprendiendo, en fracción superficial, más del 95 % de martensita y menos del 5 % de bainita,[0050] The steel part comprises successively from the mass to the surface of the steel part: - a mass (7) having a microstructure comprising, in the surface fraction, more than 95% martensite and less than 5% bainite,
[0051] - una capa de interdifusión ferrítica (6),[0051] - a ferritic interdiffusion layer (6),
[0052] - una capa de recubrimiento (5) a base de aluminio.[0052] - an aluminum-based coating layer (5).
[0053] Durante el calentamiento de la pieza en bruto de acero cortada de la lámina de acero según la invención, todos los elementos microestructurales de la masa se transforman en austenita, y la ferrita de la capa descarburada se transforma en austenita con un tamaño de grano más ancho que la austenita de la masa. Después del conformado en caliente, la pieza de acero se templa en troquel. La capa de interdifusión crece a partir de la capa de austenita de tamaño de grano ancho anterior, por lo que tiene un ancho de grano mayor que el tamaño de grano austenítico anterior en la masa. La relación entre el ancho de grano ferrítico en la capa de interdifusión GW<int>con respecto al tamaño de grano de austenita anterior en la masa PAGS<masa>, satisface la siguiente ecuación:[0053] During the heating of the steel blank cut from the steel sheet according to the invention, all the microstructural elements of the bulk material transform into austenite, and the ferrite of the decarburized layer transforms into austenite with a grain size wider than the austenite of the bulk material. After hot forming, the steel blank is die-quenched. The interdiffusion layer grows from the previous broad-grained austenite layer, and thus has a grain width greater than the previous austenitic grain size in the bulk material. The ratio of the ferritic grain width in the interdiffusion layer GW<int> to the previous austenite grain size PAGS<bulk> satisfies the following equation:
[0056] [0056]
[0058] con el fin de mejorar la capacidad de flexión de la lámina de acero, sin deteriorar las propiedades mecánicas.[0058] in order to improve the bending capacity of the steel sheet, without deteriorating the mechanical properties.
[0059] El ancho de grano ferrítico es la distancia promedio entre dos límites de grano paralelos, estando los límites de grano orientados en la dirección del espesor de la lámina. La combinación de la temperatura de recocido T<A>, el tiempo de recocido t<A>y la temperatura del punto de rocío T<DP1>según la invención promueve la formación de un gran ancho de grano GW<int>en la capa de interdifusión. Por otra parte, el tratamiento térmico de la pieza en bruto de acero antes de la conformación por prensado regula el crecimiento del grano austenítico y de este modo el PAGS en la masa.[0059] The ferritic grain width is the average distance between two parallel grain boundaries, with the grain boundaries oriented in the direction of the sheet thickness. The combination of annealing temperature T<A>, annealing time t<A>, and dew point temperature T<DP1> according to the invention promotes the formation of a large grain width GW<int> in the interdiffusion layer. Furthermore, the heat treatment of the steel blank prior to press forming regulates the growth of the austenitic grain and thus the PAGS in the bulk.
[0060] En una realización, la pieza de acero endurecido por presión puede comprender además una capa de martensita con un gradiente de carbono entre la masa y la capa de interdifusión, como se representa por (8) en la Fig. 4b. Durante el calentamiento de la pieza en bruto de acero, el carbono se difunde desde la masa a la superficie. La parte superior de ferrita de la capa descarburada se transforma a continuación en una capa de austenita con un gradiente de carbono. Durante el temple en troquel, esta capa de austenita con un gradiente de carbono se transforma en una capa de martensita con un gradiente de carbono.[0060] In one embodiment, the pressure-hardened steel part may further comprise a martensite layer with a carbon gradient between the bulk and the interdiffusion layer, as represented by (8) in Fig. 4b. During heating of the steel blank, carbon diffuses from the bulk to the surface. The ferrite upper portion of the decarburized layer then transforms into an austenite layer with a carbon gradient. During die quenching, this austenite layer with a carbon gradient transforms into a martensite layer with a carbon gradient.
[0061] La pieza de acero endurecido por presión según la invención tiene una resistencia a la tracción TS superior o igual a 1500 MPa y un ángulo de flexión superior a 70°. El ángulo de flexión se ha determinado en piezas endurecidas por prensión según la norma de flexión del procedimiento VDA238-100 (con normalización a un espesor de 1,5 mm).[0061] The pressure-hardened steel part according to the invention has a tensile strength TS greater than or equal to 1500 MPa and a bending angle greater than 70°. The bending angle was determined on pressure-hardened parts according to the bending standard of procedure VDA238-100 (normalized to a thickness of 1.5 mm).
[0062] Según la invención, el límite elástico YS es superior o igual a 1250 MPa. TS e YS se miden según la norma ISO, ISO 6892-1.[0062] According to the invention, the elastic limit YS is greater than or equal to 1250 MPa. TS and YS are measured according to ISO standard, ISO 6892-1.
[0063] La pieza de acero endurecido por presión según la invención se puede producir por cualquier procedimiento de fabricación adecuado y el experto en la materia puede definir uno. Sin embargo, se prefiere usar el procedimiento según la invención, comprendiendo las etapas siguientes:[0063] The pressure-hardened steel part according to the invention can be produced by any suitable manufacturing process, and one can be defined by a person skilled in the art. However, the process according to the invention is preferred, comprising the following steps:
[0064] Una lámina de acero recubierta según la invención se corta a una forma predeterminada para obtener una pieza en bruto de acero. La pieza en bruto de acero se calienta a continuación a una temperatura comprendida entre 880 °C y 950 °C durante 10 s a 900 s para obtener una pieza en bruto de acero calentada.[0064] A coated steel sheet according to the invention is cut to a predetermined shape to obtain a steel blank. The steel blank is then heated to a temperature between 880 °C and 950 °C for 10 s to 900 s to obtain a heated steel blank.
[0065] A continuación, la pieza en bruto calentada se transfiere a una prensa de conformación antes de conformarse en caliente y templarse en troquel.[0065] Next, the heated blank is transferred to a forming press before being hot formed and die-hardened.
[0066] La invención se ilustrará ahora mediante los siguientes ejemplos, que de ninguna manera son limitativos. Ejemplo[0066] The invention will now be illustrated by the following examples, which are in no way limiting. Example
[0067] 6 calidades, cuyas composiciones se recogen en la tabla 1, se fundieron en semiproductos y se procesaron hasta obtener láminas de acero, a continuación, piezas de acero, siguiendo los parámetros del proceso recogidos en la tabla 2.[0067] 6 qualities, whose compositions are listed in Table 1, were melted into semi-finished products and processed into steel sheets, then steel parts, following the process parameters listed in Table 2.
[0068] Tabla 1 - Composiciones[0068] Table 1 - Compositions
[0069] Las composiciones analizadas se reúnen en la siguiente tabla, donde el contenido del elemento se expresa en porcentaje en peso.[0069] The analyzed compositions are grouped in the following table, where the content of the element is expressed as a percentage by weight.
[0071] [0071]
[0072] [0072]
[0074] Tabla 2 - Parámetros del proceso[0074] Table 2 - Process parameters
[0075] Los semiproductos de acero, tal como se fundieron, se recalentaron a 1200 °C, se laminaron en caliente con una temperatura de laminado en caliente de acabado comprendida entre 800 y 950 °C, se bobinaron a 550 °C y se laminaron en frío con una tasa de reducción del 60 %. A continuación, las láminas de acero se calientan a una temperatura T<A>y se mantienen a dicha temperatura durante un tiempo de mantenimiento t<A>, en una atmósfera de HNx con un 5 % de H<2>, que tiene un punto de rocío controlado. A continuación, las láminas de acero se enfriaron a una temperatura de 560 a 700 °C y, a continuación, se recubrieron por inmersión en caliente con un recubrimiento de aluminio-silicio comprendiendo un 10 % de silicio.[0075] The steel semi-finished products, as melted, were reheated to 1200 °C, hot-rolled to a final hot-rolling temperature between 800 and 950 °C, coiled at 550 °C, and cold-rolled at a reduction rate of 60%. The steel sheets were then heated to a temperature T<A> and held at that temperature for a holding time t<A>, in an atmosphere of HNx with 5% H<2>, having a controlled dew point. The steel sheets were then cooled to a temperature of 560 to 700 °C and subsequently hot-dip coated with an aluminum-silicon coating comprising 10% silicon.
[0076] Las muestras 1, 2, 5 y 6 se sometieron a un segundo recocido a una temperatura T<2>antes del recubrimiento, siendo la lámina de acero mantenida a dicha temperatura T<2>durante un tiempo de mantenimiento t<2>, en una atmósfera de HNx con un 5 % de H<2>y un punto de rocío controlado. Se aplicaron las siguientes condiciones específicas:[0076] Samples 1, 2, 5, and 6 were subjected to a second annealing at a temperature T<2> prior to coating, with the steel sheet being held at this temperature T<2> for a holding time t<2>, in an HNx atmosphere with 5% H<2> and a controlled dew point. The following specific conditions were applied:
[0079] [0079]
[0081] Valores subrayados: no corresponden a la invención[0081] Underlined values: do not correspond to the invention
[0082] Las láminas de acero recubiertas se analizaron y las propiedades correspondientes de la capa descarburada se recogen en la tabla 3.[0082] The coated steel sheets were analyzed and the corresponding properties of the decarburized layer are collected in Table 3.
[0083] T l - Pr i l r r l l min r r i r[0083] T l - Pr i l r r l l min r r i r
[0086] [0086]
[0088] [0052]A continuación, las láminas de acero recubiertas se cortaron para obtener una pieza en bruto de acero, se calentaron a 900 ° C durante 6 minutos y se conformaron en caliente. Las piezas de acero se analizaron y la microestructura correspondiente, el ancho de grano ferrítico en la capa de interdifusión GW<int>y el tamaño de grano de austenita anterior en la masa PAGS<masa>se recogen en la tabla 4. Las propiedades mecánicas se recogen en la Tabla 5.[0088] [0052]Next, the coated steel sheets were cut to obtain a steel blank, heated to 900 °C for 6 minutes and hot-formed. The steel blanks were analyzed and the corresponding microstructure, ferritic grain width in the interdiffusion layer GW<int> and the previous austenite grain size in the PAGS<mass> are collected in Table 4. The mechanical properties are collected in Table 5.
[0089] T l 4 - Mi r r r l i z r n r i r r i n[0089] T l 4 - Mi r r r l i z r n r i r r i n
[0092] [0092]
[0094] Las fracciones superficiales, el ancho del grano ferrítico en la capa de interdifusión y PAGS se determinan mediante el siguiente procedimiento: se corta una muestra de la pieza de acero endurecido por presión, se pule y se graba con un reactivo conocido per se, para revelar la microestructura. Posteriormente, la sección se examina a través de un microscopio óptico o electrónico de barrido, por ejemplo, con un microscopio electrónico de barrido con una pistola de emisión de campo (“Field Emission Gun”, “FEG-SEM”) con un aumento superior a 5000x, que se acopla a un dispositivo de BSE (Back Scattered Electron, BSE).[0094] The surface fractions, ferritic grain width in the interdiffusion layer, and PAGS are determined by the following procedure: a sample is cut from the pressure-hardened steel part, polished, and etched with a known reagent to reveal the microstructure. Subsequently, the section is examined using an optical or scanning electron microscope, for example, a scanning electron microscope with a field emission gun (“FEG-SEM”) at a magnification greater than 5000x, coupled to a back-scattered electron (BSE) device.
[0095] T l - Pr i m ni l i z r n r i r r i n[0095] T l - Pr i m ni l i z r n r i r r i n
[0098] [0098]
[0100] Los ejemplos muestran que las piezas de acero según la invención, a saber, los ejemplos 1-2, son los únicos que muestran todas las propiedades objetivo gracias a sus composiciones y microestructuras específicas.[0100] The examples show that the steel parts according to the invention, namely examples 1-2, are the only ones that exhibit all the target properties thanks to their specific compositions and microstructures.
[0101] La Figura 3a representa una sección esquemática de la lámina de acero recubierta del ensayo 2. La combinación de parámetros de proceso de la invención, temperatura de recocido T<A>, tiempo de recocido t<A>y temperatura de punto de rocío T<DP1>permiten obtener una capa descarburada (3), donde se forma una capa de ferrita en la parte superior (4).[0101] Figure 3a represents a schematic section of the coated steel sheet from test 2. The combination of process parameters of the invention, annealing temperature T<A>, annealing time t<A> and dew point temperature T<DP1>, allows obtaining a decarburized layer (3), where a ferrite layer is formed on top (4).
[0102] A continuación, la lámina de acero recubierta se conforma en caliente. La Fig.3b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 2.[0102] Next, the coated steel sheet is hot-formed. Fig. 3b shows a schematic section of the pressure-hardened steel part from test 2.
[0103] El ancho de grano de la ferrita formada en la capa de interdifusión (5) es una herencia de la capa de ferrita pura donde tiene lugar la formación de austenita durante el calentamiento, con un tamaño de grano mayor. La capa de interdifusión crece en este grano de austenita de gran tamaño. El ancho de grano de la ferrita en la capa de interdifusión (6) es entonces superior al tamaño de grano de austenita anterior en la masa (7), lo que conduce a una buena capacidad de flexión con un ángulo de flexión superior a 70°.[0103] The grain width of the ferrite formed in the interdiffusion layer (5) is inherited from the pure ferrite layer where austenite formation occurs during heating, with a larger grain size. The interdiffusion layer grows within this larger austenite grain. The ferrite grain width in the interdiffusion layer (6) is therefore greater than the previous austenite grain size in the mass (7), leading to good bending capacity with a bending angle greater than 70°.
[0104] La Figura 4a representa una sección esquemática de la lámina de acero recubierta del ensayo 1. La combinación de los parámetros del proceso de la invención, la temperatura de recocido T<A>, el tiempo de recocido t<A>y la temperatura del punto de rocío T<DP1>permiten obtener una capa descarburada (3), donde se forma una capa de ferrita en la parte superior (4), más gruesa que en el ensayo 1 debido al mayor contenido de C.[0104] Figure 4a represents a schematic section of the coated steel sheet from test 1. The combination of the process parameters of the invention, the annealing temperature T<A>, the annealing time t<A> and the dew point temperature T<DP1> allow obtaining a decarburized layer (3), where a ferrite layer is formed on the top (4), thicker than in test 1 due to the higher C content.
[0105] A continuación, la lámina de acero recubierta se conforma en caliente. La Fig.4b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 1.[0105] Next, the coated steel sheet is hot-formed. Fig. 4b shows a schematic section of the pressure-hardened steel part from test 1.
[0106] El ancho de grano de la ferrita formada en la capa de interdifusión (6) es una herencia de la capa de ferrita pura donde tiene lugar la formación de austenita durante el calentamiento, con un tamaño de grano mayor. La capa de interdifusión crece en este grano de austenita de gran tamaño. El ancho de grano de la ferrita en la capa de interdifusión (6) es entonces superior al tamaño de grano de austenita anterior en la masa (7), lo que conduce a una buena capacidad de flexión con un ángulo de flexión superior a 70°. Por otra parte, debido a la gruesa capa de ferrita (4) en la lámina de acero recubierta, se forma una capa de martensita con un gradiente de carbono entre la masa y la capa de interdifusión en la pieza de acero endurecido por presión, lo que conduce a una resistencia a la tracción superior a 1500 MPa.[0106] The ferrite grain width formed in the interdiffusion layer (6) is inherited from the pure ferrite layer where austenite formation occurs during heating, resulting in a larger grain size. The interdiffusion layer grows within this larger austenite grain. The ferrite grain width in the interdiffusion layer (6) is therefore greater than the austenite grain size in the bulk (7), leading to good bending capacity with a bending angle greater than 70°. Furthermore, due to the thick ferrite layer (4) in the coated steel sheet, a martensite layer with a carbon gradient forms between the bulk and the interdiffusion layer in the pressure-hardened steel part, resulting in a tensile strength exceeding 1500 MPa.
[0107] En el ensayo 3, la lámina de acero recubierta tiene una capa descarburada, sin capa de ferrita en su parte superior, como se representa esquemáticamente en la Fig.2a. La ausencia de capa de ferrita se debe a la baja temperatura del punto de rocío T<DP1>de -10° C, que ralentiza la cinética de la descarburación.[0107] In test 3, the coated steel sheet has a decarburized layer, without a ferrite layer on its top, as shown schematically in Fig. 2a. The absence of a ferrite layer is due to the low dew point temperature T<DP1> of -10° C, which slows down the decarburization kinetics.
[0108] A continuación, la lámina de acero recubierta se conforma en caliente. La Figura 2b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 3. Debido a la ausencia de la capa de ferrita, el ancho del grano ferrítico en la capa de interdifusión (6) es entonces equivalente al tamaño de grano de austenita anterior en la masa (7), lo que lleva a un ángulo de flexión bajo por debajo de 70°.[0108] Next, the coated steel sheet is hot-formed. Figure 2b represents a schematic section of the pressure-hardened steel part from test 3. Due to the absence of the ferrite layer, the ferritic grain width in the interdiffusion layer (6) is then equivalent to the previous austenite grain size in the bulk (7), leading to a low bending angle below 70°.
[0109] En el ensayo 4, la temperatura de bajo punto de rocío T<DP1>de -40 °C implica ausencia de la capa descarburada y la capa de ferrita en la lámina de acero recubierta.[0109] In test 4, the low dew point temperature T<DP1> of -40 °C implies absence of the decarburized layer and ferrite layer on the coated steel sheet.
[0110] La Fig.1a representa una sección esquemática de la lámina de acero recubierta de este ensayo, con la capa de recubrimiento (1) y la masa (2).[0110] Fig.1a represents a schematic section of the coated steel sheet from this test, with the coating layer (1) and the mass (2).
[0111] A continuación, la lámina de acero recubierta se conforma en caliente. La Figura 1b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 4. Debido a la ausencia de la capa de ferrita, el ancho del grano ferrítico en la capa de interdifusión (6) es entonces equivalente al tamaño de grano de austenita anterior en la masa (7), lo que lleva a un ángulo de flexión bajo por debajo de 70°.[0111] Next, the coated steel sheet is hot-formed. Figure 1b represents a schematic section of the pressure-hardened steel part from test 4. Due to the absence of the ferrite layer, the ferritic grain width in the interdiffusion layer (6) is then equivalent to the previous austenite grain size in the bulk (7), leading to a low bending angle below 70°.
[0112] En el ensayo 5, la lámina de acero se mantiene durante 10.800 s a temperatura de homogeneización, lo que forma en la lámina de acero recubierta una capa de ferrita más gruesa en la capa descarburada que los ensayos anteriores. La Fig.5a representa una sección esquemática de la lámina de acero recubierta del ensayo 5, con la capa de recubrimiento (1), la capa descarburada (3), la capa de ferrita más gruesa (4) con un tamaño de grano más grueso y la masa (2).[0112] In test 5, the steel sheet is held for 10,800 s at the homogenization temperature, which forms a thicker ferrite layer in the decarburized layer of the coated steel sheet than in the previous tests. Fig. 5a shows a schematic section of the coated steel sheet from test 5, with the coating layer (1), the decarburized layer (3), the thicker ferrite layer (4) with a coarser grain size, and the mass (2).
[0113] A continuación, la lámina de acero recubierta se conforma en caliente y la Fig.5b representa una sección esquemática de la pieza de acero endurecido por presión del ensayo 5. Durante el calentamiento de la pieza de acero, la microestructura de la masa es austenítica, y la capa gruesa de ferrita se transforma en una capa de austenita con gradiente de carbono. Pero debido al espesor de la capa de ferrita superior a 100 µm, una capa de ferrita permanece presente entre la capa de interdifusión y la capa de austenita con gradiente de carbono.[0113] Next, the coated steel sheet is hot-formed, and Fig. 5b shows a schematic section of the pressure-hardened steel part from test 5. During heating of the steel part, the bulk microstructure is austenitic, and the thick ferrite layer transforms into a carbon-gradient austenite layer. However, due to the ferrite layer thickness exceeding 100 µm, a ferrite layer remains between the interdiffusion layer and the carbon-gradient austenite layer.
[0114] Durante el templado en troquel de la pieza de acero, la capa de ferrita todavía está presente y la capa de austenita con gradiente de carbono se transforma en una capa de martensita con gradiente de carbono, lo que produce una capa multifásica. Esto desencadena una disminución del límite elástico.[0114] During die hardening of the steel part, the ferrite layer is still present and the carbon-gradient austenite layer transforms into a carbon-gradient martensite layer, resulting in a multiphase layer. This triggers a decrease in the yield strength.
[0115] En el ensayo 6, la lámina de acero tiene un bajo contenido de carbono del 0,21 %. Este bajo contenido de carbono combinado con los parámetros del proceso, produce una capa descarburada en la lámina de acero recubierta con la capa de ferrita. Sin embargo, debido al bajo nivel de carbono, no se alcanza el límite elástico ni la resistencia a la tracción de la pieza de acero endurecido por presión.[0115] In test 6, the steel sheet has a low carbon content of 0.21%. This low carbon content, combined with the process parameters, produces a decarburized layer on the steel sheet coated with the ferrite layer. However, due to the low carbon level, the yield strength and tensile strength of the pressure-hardened steel part are not achieved.
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| PCT/IB2021/061291 WO2022130101A1 (en) | 2020-12-16 | 2021-12-03 | Coated steel sheet and high strength press hardened steel part and method of manufacturing the same |
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| BR112018012606A2 (en) * | 2016-02-25 | 2018-12-04 | Nippon Steel & Sumitomo Metal Corporation | A high intensity hot-dip zinc-coated carbon steel sheet excellent in shock-proof fissility and processing section corrosion resistance |
| EP3438311B1 (en) * | 2016-03-31 | 2020-06-24 | JFE Steel Corporation | Steel sheet, coated steel sheet, method for producing hot-rolled steel sheet, method for producing cold-rolled full hard steel sheet, method for producing heat-treated steel sheet, method for producing steel sheet, and method for producing coated steel sheet |
| US20180237877A1 (en) * | 2017-02-17 | 2018-08-23 | GM Global Technology Operations LLC | Mitigating liquid metal embrittlement in zinc-coated press hardened steels |
| CN110475891B (en) | 2017-03-30 | 2021-03-12 | 杰富意钢铁株式会社 | Hot-pressed member and method for manufacturing same |
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| WO2019171157A1 (en) * | 2018-03-09 | 2019-09-12 | Arcelormittal | A manufacturing process of press hardened parts with high productivity |
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- 2021-12-03 CA CA3200721A patent/CA3200721A1/en active Pending
- 2021-12-03 EP EP21819985.9A patent/EP4263882B1/en active Active
- 2021-12-03 UA UAA202303395A patent/UA130032C2/en unknown
- 2021-12-03 KR KR1020237018582A patent/KR20230100737A/en active Pending
- 2021-12-03 HU HUE21819985A patent/HUE073352T2/en unknown
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| UA130032C2 (en) | 2025-10-15 |
| EP4628621A3 (en) | 2025-12-03 |
| MX2023007039A (en) | 2023-06-23 |
| JP7665755B2 (en) | 2025-04-21 |
| US20240102138A1 (en) | 2024-03-28 |
| ZA202305067B (en) | 2024-06-26 |
| HUE073352T2 (en) | 2026-01-28 |
| FI4263882T3 (en) | 2025-11-13 |
| JP2023553672A (en) | 2023-12-25 |
| JP2025108506A (en) | 2025-07-23 |
| BR112023008984A2 (en) | 2024-02-06 |
| CN116568828A (en) | 2023-08-08 |
| PL4263882T3 (en) | 2025-12-22 |
| WO2022130101A1 (en) | 2022-06-23 |
| EP4628621A2 (en) | 2025-10-08 |
| EP4263882A1 (en) | 2023-10-25 |
| MA62604B1 (en) | 2025-10-31 |
| CA3200721A1 (en) | 2022-06-23 |
| KR20230100737A (en) | 2023-07-05 |
| WO2022129995A1 (en) | 2022-06-23 |
| EP4263882B1 (en) | 2025-10-01 |
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