WO2024248366A1 - 도금 강재 및 그 제조방법 - Google Patents
도금 강재 및 그 제조방법 Download PDFInfo
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- WO2024248366A1 WO2024248366A1 PCT/KR2024/006554 KR2024006554W WO2024248366A1 WO 2024248366 A1 WO2024248366 A1 WO 2024248366A1 KR 2024006554 W KR2024006554 W KR 2024006554W WO 2024248366 A1 WO2024248366 A1 WO 2024248366A1
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/04—Alloys based on zinc with aluminium as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/06—Zinc or cadmium or alloys based thereon
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
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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
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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
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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
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
- C23C2/29—Cooling or quenching
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/34—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
- C23C2/36—Elongated material
- C23C2/40—Plates; Strips
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- 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
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
- C23C28/025—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only with at least one zinc-based layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/02—2 layers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/06—Coating on the layer surface on metal layer
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2255/00—Coating on the layer surface
- B32B2255/20—Inorganic coating
- B32B2255/205—Metallic coating
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2307/00—Properties of the layers or laminate
- B32B2307/70—Other properties
- B32B2307/732—Dimensional properties
- B32B2307/737—Dimensions, e.g. volume or area
- B32B2307/7375—Linear, e.g. length, distance or width
- B32B2307/7376—Thickness
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/20—Zinc
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2311/00—Metals, their alloys or their compounds
- B32B2311/30—Iron, e.g. steel
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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
Definitions
- the present invention relates to a plated steel and a method for manufacturing the same, and more specifically, to a plated steel having excellent corrosion resistance at a processed portion and a method for manufacturing the same.
- Hot-dip galvanized steel has excellent self-sacrificial properties and is widely used in construction materials and home appliances.
- zinc (Zn) acts as a sacrificial anode on the exposed iron portion, causing zinc loss from the plating layer.
- This sacrificial anode action of zinc plays an excellent role in suppressing rust of the base iron in a corrosive environment, but has the problem of somewhat low sacrificial anode efficiency.
- the plating bath process in which magnesium (Mg) is added to zinc (Zn) has a problem that the surface quality deteriorates as the magnesium (Mg) content increases due to the reaction with oxygen in the air to generate oxides.
- an inert gas nitrogen
- an oxidation-free chamber is used to minimize contact with oxygen in the wiping process area.
- the magnesium (Mg) content increases due to the characteristics of high-corrosion-resistant plating steel, corrosion resistance improves, but it has the disadvantage of requiring additional processes due to magnesium (Mg) oxidation and making operation difficult due to oxides.
- magnesium (Mg) can be added with a low content, but the primary Zn phase formed during solidification of the plating layer is formed in a relatively coarse shape, and the area where the coarse primary Zn phase is formed in a corrosive environment develops into an area with poor corrosion resistance.
- the magnesium (Mg) content is low, the amount of eutectic phase containing magnesium (Mg) is reduced, making it difficult to exhibit high corrosion resistance.
- the eutectic phase containing magnesium (Mg) has high hardness, which acts as a starting point for cracks in the plating layer during processing, and the base iron exposed by the cracks causes a rapid decrease in corrosion resistance in a corrosive environment.
- the technical problem to be achieved by the present invention is to provide a highly corrosion-resistant plated steel having excellent corrosion resistance and crack resistance in a processed portion, and a method for manufacturing the same.
- a method for manufacturing a plated steel comprises the steps of: (a) providing a base iron; (b) passing the base iron through a plating bath containing aluminum (Al), magnesium (Mg), and zinc (Zn), thereby forming a plating layer on the base iron, the plating layer comprising 1 to 3 wt% of aluminum (Al), 1 to 2 wt% of magnesium (Mg), and the remainder being zinc (Zn) and other unavoidable impurities; and (c) cooling the plating layer at a cooling rate of 10 to 30°C/sec, wherein the weight ratio of aluminum to magnesium in the plating layer is 1.2 or more.
- the thickness of the plated layer may be 15 ⁇ m to 50 ⁇ m.
- the plating layer after performing the cooling step includes a primary Zn phase structure and a eutectic phase structure, and the primary Zn phase structure may have a multilayer structure in the height direction of the plating layer.
- the area fraction of the primary Zn phase structure having the multilayer structure within the plated layer may be 30% or more.
- the primary Zn phase structure may be formed first in the cooling step, and the eutectic structure may be formed after the formation of the primary Zn phase structure.
- a plated steel material comprises: a base steel; and a plating layer formed on the base steel, the plating layer comprising 1 to 3 wt% of aluminum (Al), 1 to 2 wt% of magnesium (Mg), and the remainder being zinc (Zn) and other unavoidable impurities; wherein the weight ratio of aluminum to magnesium in the plating layer is 1.2 or more.
- the plating layer includes a primary Zn phase structure and a eutectic phase structure, and the primary Zn phase structure may have a multilayer structure in the height direction of the plating layer.
- the area fraction of the primary Zn phase structure having the multilayer structure within the plated layer may be 30% or more.
- the thickness of the plated layer may be 15 ⁇ m to 50 ⁇ m.
- a plated steel having excellent corrosion resistance at a processed portion and a method for manufacturing the same can be implemented. Specifically, by forming a structure of a primary Zn phase of a plating layer in a multilayer structure, a highly corrosion-resistant plated steel having excellent crack resistance at a processed portion and excellent corrosion resistance and a method for manufacturing the same can be implemented.
- FIG. 1 is a flow chart illustrating a method for manufacturing a plated steel according to one embodiment of the present invention.
- Figure 2 is a photograph of a cross-section of a plating layer in a plated steel according to Comparative Example 5 as an experimental example of the present invention.
- FIG. 3 is a photograph of a cross-section of a plating layer in a plated steel according to Example 3 as an experimental example of the present invention.
- a plated steel having excellent corrosion resistance at a machined portion according to an embodiment of the present invention and a method for manufacturing the same are described in detail.
- the terms described below are appropriately selected in consideration of their functions in the present invention, and the definitions of these terms should be made based on the contents throughout this specification.
- FIG. 1 is a flow chart illustrating a method for manufacturing a plated steel according to one embodiment of the present invention.
- a method for manufacturing a plated steel includes (a) a step of providing a base steel (S10); (b) a step of annealing the base steel (S20); (c) a step of passing the annealed base steel through a plating bath containing aluminum (Al), magnesium (Mg), and zinc (Zn) to form a plating layer on the base steel composed of 1 to 3 wt% of aluminum (Al), 1 to 2 wt% of magnesium (Mg), and the remainder being zinc (Zn) and other unavoidable impurities (S30); and (d) a step of cooling the plating layer at a cooling rate of 10 to 30°C/sec (S40).
- Al phase, Zn phase, and MgZn 2 phase are formed in the plating layer depending on the amount of Al and Mg added to the Zn plating bath.
- a binary eutectic phase with a lamellar shape, a ternary eutectic phase with a MgZn 2 phase containing Al and a Zn phase having a lamellar shape, and a MgZn 2 phase with a polygonal structure are formed.
- the Al phase with a dendritic structure and the MgZn 2 phase with a polygonal structure are mainly formed in compositions with high addition amounts of Al and Mg.
- the composition range in which the Al phase with a dendritic structure and the MgZn 2 phase with a polygonal structure are formed is excluded in order to improve the workability of the plating layer.
- the addition amount of Al in the present invention can be controlled to 3 wt% or less, and the addition amount of Mg can be controlled to 2 wt% or less.
- the present invention improves the structure of the primary Zn phase of the plating layer in order to improve the phenomenon in which corrosion resistance is reduced due to crack propagation within the plating layer of the machined portion in a high-corrosion-resistant plating steel.
- the fraction of the primary Zn phase must be increased, but this will simultaneously decrease the fraction of the process that improves corrosion resistance, thereby reducing the corrosion resistance again.
- the primary Zn phase is formed as a single layer as shown in Fig. 2.
- the primary Zn phase single layer structure can be defined as a plating layer microstructure structure in which the primary Zn phase is continuously connected from the plating layer surface to the base iron for at least 80% of the plating layer thickness based on the cross-section of the plating layer.
- the primary Zn-phase single-layer structure itself has excellent crack resistance in the plating layer, but cracks easily progress because there is little Zn in the surrounding process that can prevent crack propagation.
- the single-layer Zn phase is not sufficient to form a strong passive film when corrosion progresses in a corrosive environment, so excessive production of the primary Zn-phase single-layer structure is not advantageous from the perspective of corrosion resistance.
- the present invention discloses a technical idea of minimizing crack propagation and improving corrosion resistance by forming a structure of a primary Zn phase existing in a plating layer from a single-layer structure to a multi-layer structure.
- the multilayer structure of the primary Zn phase refers to the microstructure of the plating layer in which the area fraction of two or more primary Zn phases overlapping and existing in a multilayer structure is 30% or more based on the cross-section of the plating layer, as shown in Fig. 3.
- the existence of two or more primary Zn phases overlapping and existing in a multilayer structure may mean that when the plating layer is viewed vertically from the upper side to the lower side, two or more primary Zn phases exist in a multilayer structure in a position where they at least partially overlap.
- the above-described primary Zn phase multilayer structure may include a structure in which the primary Zn phase is divided into two or more separate layers in the thickness height direction of the cross-section of the plating layer.
- a predetermined separation space may be interposed between the primary Zn phases divided into separate layers in the above-described primary Zn phase multilayer structure, and the width of the predetermined separation space may have a range of 0.1 to 5 ⁇ m.
- Each of the primary Zn phases constituting the above primary Zn phase multilayer structure may exist, for example, at least two or more throughout the thickness of the plating layer from the surface of the plating layer to the base iron.
- composition range of the plating bath (plating layer) is proposed as aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the remainder zinc (Zn).
- Al aluminum
- Mg magnesium
- Zn remainder zinc
- the composition of the plating bath and the composition of the plating layer can be considered to be almost the same.
- aluminum (Al) is added in an amount less than 1 wt%, it cannot sufficiently perform its role of reducing the oxidation of magnesium (Mg). If aluminum (Al) is added in an amount exceeding 3 wt%, a large amount of ternary process phase is generated, which may cause a large number of cracks to occur during processing.
- magnesium (Mg) When magnesium (Mg) is added in amounts less than 1 wt%, the process fraction for exhibiting corrosion resistance is insufficient, and when magnesium (Mg) is added in amounts exceeding 2 wt%, cracks are more likely to occur during processing due to the formation of a large amount of process fraction.
- the ratio of aluminum (Al) and magnesium (Mg) added to the plating bath should be at least 1:1 to minimize magnesium (Mg) oxidation, and preferably 1.2:1 or more. That is, the weight ratio of aluminum and magnesium in the plating bath is preferably 1.2 or more.
- Aluminum (Al) present in the molten metal reacts with oxygen in the air to form a dense oxide film, which prevents oxygen from being supplied to the surface of the molten metal, thereby preventing magnesium (Mg) from being oxidized.
- the order of phases generated during solidification is that the primary Zn phase is generated first, and the eutectic phase is solidified after the formation of the primary Zn phase structure.
- the cooling rate In order to implement the composition intended for the invention within the plating layer, the cooling rate must be controlled within the range of 10 to 30°C/s, and can be strictly controlled within the range of 12 to 25°C/s.
- the Zn single phase may solidify and exist as a single layer in the plating layer.
- the cooling rate exceeds 30°C/s, there is a concern that the plating surface shape may be deformed by the high-pressure cooling gas.
- the thickness of the plating layer In order for the primary Zn phase to form a multilayer structure in the plating layer, there is a limitation on the thickness of the plating layer.
- the thickness of the plating layer must be at least 15 ⁇ m thick and 50 ⁇ m thinner. If the plating layer thickness is thinner than 15 ⁇ m, it is not sufficient to form a multilayer structure of the primary Zn single phase, and if the plating layer thickness exceeds 50 ⁇ m, a flow pattern is created on the plating surface during solidification, which deteriorates the plating quality.
- the primary Zn phase of the multilayer structure In order for the primary Zn phase of the multilayer structure to sufficiently prevent crack propagation and improve corrosion resistance, the primary Zn phase of the multilayer structure must be composed of a phase fraction of 30% or more based on the cross-section of the plating layer.
- a method for manufacturing a plated steel comprises the steps of: (a) providing a base steel; (b) passing the base steel through a plating bath containing aluminum (Al), magnesium (Mg), and zinc (Zn) to form a plating layer on the base steel, the plating layer comprising 1 to 3 wt% of aluminum (Al), 1 to 2 wt% of magnesium (Mg), and the remainder being zinc (Zn) and other unavoidable impurities; and (c) cooling the plating layer at a cooling rate of 10 to 30°C/sec, wherein the weight ratio of aluminum to magnesium in the plating layer is 1.2 or more, and the thickness of the plating layer may be 15 ⁇ m to 50 ⁇ m.
- the plating layer after performing the cooling step includes a primary Zn phase structure and a eutectic structure, wherein the primary Zn phase structure may have a multilayer structure in the height direction of the plating layer.
- the area fraction of the primary Zn phase structure having the multilayer structure in the plating layer may be 30% or more.
- the primary Zn phase structure is formed first, and the eutectic phase structure can be formed after the formation of the primary Zn phase structure.
- a plated steel includes: a base steel; and a plating layer formed on the base steel, the plating layer comprising 1 to 3 wt% of aluminum (Al), 1 to 2 wt% of magnesium (Mg), and the remainder being zinc (Zn) and other unavoidable impurities; wherein a weight ratio of aluminum to magnesium in the plating layer is 1.2 or more.
- the plating layer includes a primary Zn phase structure and a eutectic structure, and the primary Zn phase structure may have a multilayer structure in a height direction of the plating layer. An area fraction of the primary Zn phase structure having the multilayer structure in the plating layer may be 30% or more.
- a thickness of the plating layer may be 15 ⁇ m to 50 ⁇ m.
- a specimen by immersing a 0.7 mm thick steel sheet in an alkaline solution at 50°C for 30 minutes, then washing it with water to remove foreign substances and oil on the surface. This specimen is annealed and then plated. Annealing is performed in a reducing atmosphere consisting of 5 to 20% hydrogen and 80 to 95% nitrogen, and the annealing heat treatment temperature is 700 to 850°C.
- Plating is performed by cooling the annealed heat-treated specimen to the plating bath temperature, immersing it in the plating bath for 2 seconds, then pulling it up and adjusting the plating thickness according to conditions through nitrogen wiping. At this time, the plating bath temperature is set to 430°C to 480°C.
- the cold rolled steel sheet constituting the above-mentioned steel has a composition of carbon: 0.15 wt%, manganese: 0.6 wt%, phosphorus: 0.05 wt%, sulfur: 0.05 wt%, and the remainder is iron (Fe).
- Table 1 shows the composition and process conditions of the plated steel according to the experimental examples of the present invention, and the evaluation results for the processability of the plated layer, the corrosion resistance of the processed part, and the appearance quality of the plated surface according to the composition. It can be understood that the composition implementing the example among the experimental examples has a manufacturing tolerance of ⁇ 5% within the proposed composition range.
- the Zn, Al, and Mg items represent the composition (unit: weight%) in the plating process
- the plating thickness item is the thickness of the final plating layer
- the cooling rate is the cooling rate in the cooling step (S40) illustrated in Fig. 1
- the multilayer structure primary Zn phase fraction item represents the area fraction of the primary Zn phase multilayer structure based on the cross-section of the final plating layer.
- ⁇ indicates a case where no cracks are observed with the naked eye
- ⁇ indicates a case where relatively thin and fine cracks are observed with the naked eye
- ⁇ indicates a case where relatively thick and small cracks are observed with the naked eye, but there are concerns about the plating layer peeling off due to the large number of cracks
- X indicates a case where relatively thick and large cracks are observed with the naked eye.
- ⁇ item corresponds to a case where the red rust occurrence time is 1,100 hours or longer
- ⁇ item corresponds to a case where the red rust occurrence time is approximately 900 hours
- ⁇ item corresponds to a case where the red rust occurrence time is approximately 700 hours
- X item corresponds to a case where the red rust occurrence time is approximately 600 hours.
- an item of ⁇ is a case where there is no visual flow pattern, no attachment of oxide dross, and no oxide wrinkles
- an item of X is a case where there is any one of a visual flow pattern, oxide dross, or oxide wrinkle.
- Examples 1 to 8 satisfy a composition range of aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the remainder being zinc (Zn), wherein the weight ratio of aluminum to magnesium is 1.2 or more, and the base iron is immersed in a plating bath having a temperature of 430 to 480°C, and then a plating layer having a thickness of 15 ⁇ m to 50 ⁇ m is formed by nitrogen wiping, and then cooling at a cooling rate of 10 to 30°C/sec, it can be confirmed that the area fraction of the primary Zn phase structure having a multilayer structure in the formed plating layer is 30% or more.
- Comparative Example 1 is a Zn-Al plated steel without magnesium (Mg) added.
- the time for red rust occurrence was evaluated by a salt spray test using a 5% NaCl solution at 35°C on the machined area after 3T bending. As a result, the time for red rust occurrence was measured to be approximately 600 hours, confirming that the corrosion resistance of the machined area is not good.
- Comparative Example 3 is a case where the plating bath composition satisfies the composition range of aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the balance is zinc (Zn), but the weight ratio of aluminum to magnesium in the plating bath does not satisfy 1.2 or more and falls short. It can be confirmed that the degree of crack occurrence in the processed portion after 3T bending is not so great as to cause no visible cracks, but rather that relatively thin and fine cracks are observed with the naked eye, and that the appearance quality of the plating surface is not good.
- the weight ratio of aluminum to magnesium in the plating bath does not satisfy 1.2 or more and falls short, the aluminum added to minimize magnesium (Mg) oxidation in the plating bath is insufficient to sufficiently prevent oxygen from being supplied to the surface layer of the molten metal, which causes magnesium (Mg) to be oxidized, which may result in poor appearance quality of the plating surface.
- Comparative Example 4 is a case where the plating bath composition satisfies the composition range of aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the balance is zinc (Zn), and the weight ratio of aluminum and magnesium in the plating bath satisfies 1.2 or more, but the thickness of the plating layer does not satisfy the range of 15 ⁇ m to 50 ⁇ m and falls short. If the plating layer thickness is thinner than 15 ⁇ m, it is not sufficient to form a primary Zn single phase into a multilayer structure. It was confirmed that the area fraction of the primary Zn phase having a multilayer structure in the plating layer does not satisfy the range of 30% or more and falls short.
- Comparative Example 5 satisfies the composition range of aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the balance zinc (Zn), the weight ratio of aluminum and magnesium in the plating bath is 1.2 or more, and the thickness of the plating layer satisfies the range of 15 ⁇ m to 50 ⁇ m, but in the cooling step of Fig.
- the Zn single phase solidifies as a single layer in the plating layer, and it is confirmed that the area fraction of the primary Zn phase structure having a multilayer structure in the plating layer does not satisfy the range of 30% or more and falls below it, and after 3T bending, relatively thick and small cracks are observed with the naked eye in the processed area, but it is confirmed that the cracks are so numerous that the plating layer may fall off, and thus the plating layer processability is not good, and as a result of evaluating the time for occurrence of red rust in a salt spray test with a 5% NaCl solution at 35°C on the processed area after 3T bending, red rust It can be confirmed that the occurrence time is approximately 700 hours and less than 1100 hours.
- Comparative Example 6 is a case where the plating bath composition satisfies the composition range of aluminum (Al): 1 to 3 wt%, magnesium (Mg): 1 to 2 wt%, and the balance zinc (Zn), and the weight ratio of aluminum to magnesium in the plating bath is 1.2 or more, but the thickness of the plating layer does not satisfy the range of 15 ⁇ m to 50 ⁇ m and exceeds it, and it can be confirmed that a flow pattern is created on the plating surface during solidification, and the appearance quality of the plating surface is not good.
- Al aluminum
- Mg magnesium
- Zn balance zinc
- Comparative Example 7 is a case where the aluminum (Al) content in the plating bath exceeds 3 wt%, and a large amount of ternary eutectic phase is generated within the plating layer, causing a large number of plating layer cracks to occur.
- the corrosion resistance of the processed area decreases due to a decrease in the fraction of the primary Zn phase and an increase in the fraction of the ternary eutectic phase, which causes a large number of plating layer cracks to occur during processing.
- Comparative Example 8 is a case where the cooling speed exceeds 30°C/sec, and due to the high cooling pressure, uneven oxide wrinkles are generated on the plating surface, which deteriorates the appearance quality of the plating surface.
- Comparative Example 9 is a case where the plating bath composition exceeds 2 wt% of magnesium (Mg), and a large amount of two-phase phase is generated within the plating layer, resulting in a large number of plating layer tracks. Even in this case, as in Comparative Example 7, a large number of cracks are generated in the plating layer during processing due to a decrease in the fraction of the primary Zn phase and an increase in the fraction of the two-phase phase, thereby reducing the corrosion resistance of the processed area.
- Mg magnesium
- the structure of the primary Zn phase of the plating layer can be controlled from a single layer to a multilayer structure, thereby realizing a highly corrosion-resistant plating steel having excellent crack resistance at the processed part and corrosion resistance and a manufacturing method thereof.
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Abstract
Description
| 구분 | Zn | Al | Mg | 도금두께 (㎛) |
냉각속도 (℃/s) |
다층구조 초정Zn상 분율 |
도금층 가공성 |
가공부 내식성 |
도금표면 외관 품질 |
| 비교예1 | Bal. | 0.2 | - | - | - | - | ◎ | X | ○ |
| 비교예2 | Bal. | 1 | 0.5 | 15 | 12 | 5 | ◎ | ○ | ○ |
| 비교예3 | Bal. | 1 | 2 | 15 | 12 | 31 | ○ | ◎ | x |
| 비교예4 | Bal. | 2 | 1 | 10 | 12 | 17 | △ | △ | ○ |
| 비교예5 | Bal. | 2 | 1.2 | 15 | 5 | 23 | △ | △ | ○ |
| 비교예6 | Bal. | 2 | 1.2 | 52 | 12 | 62 | ◎ | ◎ | X |
| 비교예7 | Bal. | 3.5 | 1.2 | 20 | 10 | 41 | △ | △ | ○ |
| 비교예8 | Bal. | 2 | 1.2 | 25 | 35 | 38 | ◎ | ◎ | X |
| 비교예9 | Bal. | 2 | 2.2 | 52 | 12 | 25 | △ | △ | ○ |
| 실시예1 | Bal. | 2 | 1 | 15 | 12 | 35 | ○ | ○ | ○ |
| 실시예2 | Bal. | 2 | 1.2 | 20 | 12 | 36 | ○ | ○ | ○ |
| 실시예3 | Bal. | 2 | 1.5 | 25 | 15 | 40 | ◎ | ◎ | ○ |
| 실시예4 | Bal. | 2 | 1.5 | 20 | 25 | 51 | ◎ | ◎ | ○ |
| 실시예5 | Bal. | 2.5 | 1.5 | 30 | 20 | 54 | ◎ | ◎ | ○ |
| 실시예6 | Bal. | 1.7 | 1 | 30 | 15 | 67 | ◎ | ◎ | ○ |
| 실시예7 | Bal. | 1.5 | 1 | 25 | 10 | 62 | ○ | ○ | ○ |
| 실시예8 | Bal. | 1.8 | 1.4 | 20 | 10 | 52 | ◎ | ◎ | ○ |
Claims (9)
- (a) 소지철을 제공하는 단계;(b) 상기 소지철을 알루미늄(Al), 마그네슘(Mg) 및 아연(Zn)을 함유하는 도금욕에 통과시켜, 상기 소지철 상에 알루미늄(Al): 1 ~ 3중량%, 마그네슘(Mg): 1 ~ 2중량% 및 잔부가 아연(Zn)과 기타 불가피한 불순물로 이루어진 도금층을 형성하는 단계; 및(c) 상기 도금층을 10 ~ 30℃/sec의 냉각속도로 냉각하는 단계;를 포함하되,상기 도금층 내 알루미늄과 마그네슘의 중량비는 1.2 이상인,도금 강재의 제조방법.
- 제 1 항에 있어서,상기 도금층의 두께는 15㎛ ~ 50㎛인 것을 특징으로 하는,도금 강재의 제조방법.
- 제 2 항에 있어서,상기 냉각하는 단계를 수행한 후의 상기 도금층은 초정 Zn상 조직 및 공정상 조직을 포함하되, 상기 초정 Zn상 조직은 상기 도금층의 높이 방향으로 다층 구조를 가지는 것을 특징으로 하는,도금 강재의 제조방법.
- 제 3 항에 있어서,상기 도금층 내 상기 다층 구조를 가지는 초정 Zn상 조직의 면적분율은 30% 이상인,도금 강재의 제조방법.
- 제 3 항에 있어서,상기 냉각하는 단계에서 상기 초정 Zn상 조직이 먼저 생성되고 상기 공정상 조직은 상기 초정 Zn상 조직의 생성 이후에 생성되는 것을 특징으로 하는,도금 강재의 제조방법.
- 소지철; 및상기 소지철 상에 형성된, 알루미늄(Al): 1 ~ 3중량%, 마그네슘(Mg): 1 ~ 2중량% 및 잔부가 아연(Zn)과 기타 불가피한 불순물로 이루어진 도금층; 을 포함하며,상기 도금층 내 알루미늄과 마그네슘의 중량비는 1.2 이상인,도금 강재.
- 제 6 항에 있어서,상기 도금층은 초정 Zn상 조직 및 공정상 조직을 포함하되,상기 초정 Zn상 조직은 상기 도금층의 높이 방향으로 다층 구조를 가지는,도금 강재.
- 제 7 항에 있어서,상기 도금층 내 상기 다층 구조를 가지는 초정 Zn상 조직의 면적분율은 30% 이상인,도금 강재.
- 제 7 항에 있어서,상기 도금층의 두께는 15㎛ ~ 50㎛인 것을 특징으로 하는,도금 강재.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP24815744.8A EP4722406A1 (en) | 2023-05-31 | 2024-05-14 | Plated steel and manufacturing method therefor |
| CN202480033367.5A CN121152894A (zh) | 2023-05-31 | 2024-05-14 | 镀覆钢及其制造方法 |
| US19/394,071 US20260078470A1 (en) | 2023-05-31 | 2025-11-19 | Plated steel and manufacturing method therefor |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR1020230070565A KR102800596B1 (ko) | 2023-05-31 | 2023-05-31 | 도금 강재 및 그 제조방법 |
| KR10-2023-0070565 | 2023-05-31 |
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| US19/394,071 Continuation US20260078470A1 (en) | 2023-05-31 | 2025-11-19 | Plated steel and manufacturing method therefor |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005105367A (ja) | 2003-09-30 | 2005-04-21 | Nippon Steel Corp | 溶接性と延性に優れた高降伏比高強度冷延鋼板および高降伏比高強度溶融亜鉛めっき鋼板、並びに、高降伏比高強度合金化溶融亜鉛めっき鋼板とその製造方法 |
| KR20150135605A (ko) * | 2014-05-22 | 2015-12-03 | 동부제철 주식회사 | 도금 강판 및 그 제조방법 |
| KR20200136066A (ko) * | 2019-05-27 | 2020-12-07 | 현대제철 주식회사 | 도금강판 및 그 제조방법 |
| KR20220089028A (ko) * | 2020-12-21 | 2022-06-28 | 주식회사 포스코 | 내식성 및 내열성이 우수한 도금 강판 및 이의 제조방법 |
| US11505858B2 (en) * | 2016-12-22 | 2022-11-22 | Posco | Alloy-plated steel material having excellent crack resistance, and method for manufacturing same |
| KR20230021116A (ko) * | 2020-06-08 | 2023-02-13 | 쇼강 그룹 컴퍼니 리미티드 | 용융 아연-알루미늄-마그네슘 도금 강판 및 그 제조 방법 |
-
2023
- 2023-05-31 KR KR1020230070565A patent/KR102800596B1/ko active Active
-
2024
- 2024-05-14 EP EP24815744.8A patent/EP4722406A1/en active Pending
- 2024-05-14 CN CN202480033367.5A patent/CN121152894A/zh active Pending
- 2024-05-14 WO PCT/KR2024/006554 patent/WO2024248366A1/ko not_active Ceased
-
2025
- 2025-11-19 US US19/394,071 patent/US20260078470A1/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2005105367A (ja) | 2003-09-30 | 2005-04-21 | Nippon Steel Corp | 溶接性と延性に優れた高降伏比高強度冷延鋼板および高降伏比高強度溶融亜鉛めっき鋼板、並びに、高降伏比高強度合金化溶融亜鉛めっき鋼板とその製造方法 |
| KR20150135605A (ko) * | 2014-05-22 | 2015-12-03 | 동부제철 주식회사 | 도금 강판 및 그 제조방법 |
| US11505858B2 (en) * | 2016-12-22 | 2022-11-22 | Posco | Alloy-plated steel material having excellent crack resistance, and method for manufacturing same |
| KR20200136066A (ko) * | 2019-05-27 | 2020-12-07 | 현대제철 주식회사 | 도금강판 및 그 제조방법 |
| KR20230021116A (ko) * | 2020-06-08 | 2023-02-13 | 쇼강 그룹 컴퍼니 리미티드 | 용융 아연-알루미늄-마그네슘 도금 강판 및 그 제조 방법 |
| KR20220089028A (ko) * | 2020-12-21 | 2022-06-28 | 주식회사 포스코 | 내식성 및 내열성이 우수한 도금 강판 및 이의 제조방법 |
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| CN121152894A (zh) | 2025-12-16 |
| EP4722406A1 (en) | 2026-04-08 |
| US20260078470A1 (en) | 2026-03-19 |
| KR20240171927A (ko) | 2024-12-09 |
| KR102800596B1 (ko) | 2025-04-28 |
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