WO2023121194A1 - 강도와 연신율이 우수한 냉연강판 및 그 제조방법 - Google Patents
강도와 연신율이 우수한 냉연강판 및 그 제조방법 Download PDFInfo
- Publication number
- WO2023121194A1 WO2023121194A1 PCT/KR2022/020758 KR2022020758W WO2023121194A1 WO 2023121194 A1 WO2023121194 A1 WO 2023121194A1 KR 2022020758 W KR2022020758 W KR 2022020758W WO 2023121194 A1 WO2023121194 A1 WO 2023121194A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- steel sheet
- cold
- rolled steel
- equation
- less
- Prior art date
Links
- 239000010960 cold rolled steel Substances 0.000 title claims abstract description 66
- 238000004519 manufacturing process Methods 0.000 title claims description 30
- 238000000034 method Methods 0.000 title claims description 17
- 230000002787 reinforcement Effects 0.000 claims abstract description 47
- 239000002131 composite material Substances 0.000 claims abstract description 22
- 239000013078 crystal Substances 0.000 claims abstract description 16
- 239000012535 impurity Substances 0.000 claims abstract description 10
- 229910000831 Steel Inorganic materials 0.000 claims description 174
- 239000010959 steel Substances 0.000 claims description 174
- 238000005096 rolling process Methods 0.000 claims description 48
- 230000009467 reduction Effects 0.000 claims description 31
- 238000007747 plating Methods 0.000 claims description 21
- 238000005097 cold rolling Methods 0.000 claims description 17
- 238000000137 annealing Methods 0.000 claims description 13
- 229910052718 tin Inorganic materials 0.000 claims description 13
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 12
- 229910001128 Sn alloy Inorganic materials 0.000 claims description 10
- 229910052782 aluminium Inorganic materials 0.000 claims description 9
- 229910052799 carbon Inorganic materials 0.000 claims description 9
- 229910052748 manganese Inorganic materials 0.000 claims description 9
- 229910052758 niobium Inorganic materials 0.000 claims description 9
- 238000005098 hot rolling Methods 0.000 claims description 8
- 239000004615 ingredient Substances 0.000 claims description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 6
- 239000011651 chromium Substances 0.000 claims description 6
- 229910052698 phosphorus Inorganic materials 0.000 claims description 6
- 229910052710 silicon Inorganic materials 0.000 claims description 6
- 238000004804 winding Methods 0.000 claims description 6
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 238000010438 heat treatment Methods 0.000 claims description 4
- 238000009713 electroplating Methods 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 3
- 238000007598 dipping method Methods 0.000 claims description 2
- 238000003303 reheating Methods 0.000 claims description 2
- 230000000052 comparative effect Effects 0.000 description 57
- 239000000463 material Substances 0.000 description 38
- 239000011572 manganese Substances 0.000 description 19
- 239000010955 niobium Substances 0.000 description 16
- 230000000694 effects Effects 0.000 description 9
- 238000005728 strengthening Methods 0.000 description 9
- 239000000203 mixture Substances 0.000 description 8
- 238000000465 moulding Methods 0.000 description 8
- 230000007423 decrease Effects 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000006104 solid solution Substances 0.000 description 6
- 238000007792 addition Methods 0.000 description 5
- 235000013305 food Nutrition 0.000 description 5
- 238000001556 precipitation Methods 0.000 description 5
- 230000008569 process Effects 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 238000001953 recrystallisation Methods 0.000 description 4
- 235000013361 beverage Nutrition 0.000 description 3
- 239000004033 plastic Substances 0.000 description 3
- 239000002244 precipitate Substances 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 229910020810 Sn-Co Inorganic materials 0.000 description 2
- 229910020938 Sn-Ni Inorganic materials 0.000 description 2
- 229910020994 Sn-Zn Inorganic materials 0.000 description 2
- 229910018757 Sn—Co Inorganic materials 0.000 description 2
- 229910008937 Sn—Ni Inorganic materials 0.000 description 2
- 229910009069 Sn—Zn Inorganic materials 0.000 description 2
- 230000032683 aging Effects 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 238000004064 recycling Methods 0.000 description 2
- 238000009628 steelmaking Methods 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910001566 austenite Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 235000020971 citrus fruits Nutrition 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000005261 decarburization Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 231100000053 low toxicity Toxicity 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 150000007524 organic acids Chemical class 0.000 description 1
- 235000005985 organic acids Nutrition 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 239000000123 paper Substances 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000007639 printing Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 229910052717 sulfur Inorganic materials 0.000 description 1
- 239000011593 sulfur Substances 0.000 description 1
- 238000009864 tensile test Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0236—Cold rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0273—Final recrystallisation annealing
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
- C21D8/0421—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing characterised by the working steps
- C21D8/0426—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/12—Ferrous alloys, e.g. steel alloys containing tungsten, tantalum, molybdenum, vanadium, or niobium
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
- C23C2/0224—Two or more thermal pretreatments
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/024—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by cleaning or etching
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/26—After-treatment
- C23C2/28—Thermal after-treatment, e.g. treatment in oil bath
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
Definitions
- One embodiment of the present invention relates to a cold-rolled steel sheet having excellent workability and a manufacturing method thereof. More specifically, it relates to a cold-rolled steel sheet suitable for making parts requiring durability and complex molding due to its excellent strength and workability, and a manufacturing method thereof.
- Steel, plastic, glass, paper, or aluminum are used as containers for storing beverages or food.
- steel is the most widely used after plastic and aluminum because its price is very low compared to other materials.
- plastic and aluminum are complicated to recover and the cost of recycling is high, steel is becoming more popular as a material for containers in terms of recycling resources.
- These steel materials are mostly processed and used in the form of tin (Sn)-plated cans to store food or beverages.
- Cans for food or beverages are small and easy to transport and should not be damaged during transportation. Therefore, the steel material for cans requires good workability in order to be processed into a desired shape, and at the same time, high strength enough to maintain the shape even with a thin thickness is required.
- a material with low machinability should take a straight shape.
- structural durability can be additionally secured by adding a bead to the can body when forming.
- materials with low machinability cannot be used in parts that require complex molding, such as the EOE (Easy-Open-End) part of a can, this material can be applied to more diverse parts if the steel material secures machinability.
- the thickness of the material for cans is continuously getting thinner to reduce the amount of material used when manufacturing cans.
- the material becomes thinner there is a problem that it is not easy to maintain the desired shape. Therefore, in order to overcome this advantage, higher and higher strength is required for steel materials used as cans.
- the steel sheet for a can has high strength, elongation naturally tends to decrease according to its physical properties. Therefore, the steel sheet has a problem in that high strength and elongation, which are difficult to be compatible with each other, must be simultaneously increased. Furthermore, when molding a material with excessively high strength, high processing force is required and the mold is easily worn.
- One embodiment of the present invention is to provide a cold-rolled steel sheet with excellent strength and elongation and a manufacturing method thereof. More specifically, it is intended to provide a cold-rolled steel sheet that is excellent in strength and elongation at the same time and can be used as a material for cans, and a manufacturing method thereof.
- Cold-rolled steel sheet having excellent strength and elongation contains C: 0.04 ⁇ 0.08%, Si: 0.05% or less (excluding 0%), Mn: 0.1 ⁇ 0.6%, Al: 0.02 ⁇ 0.06%, P: 0.015% or less (excluding 0%), S: 0.015% or less (excluding 0%), N: 0.006% or less (excluding 0%), Nb: including 0.02 to 0.04% And, the remainder includes Fe and other unavoidable impurities, and the component enhancement index defined by the following [Equation 1] may be 470 or less.
- the cold-rolled steel sheet having excellent strength and elongation according to an embodiment of the present invention may have a grain aspect ratio of 2.15 or less defined by the following [Equation 2].
- the cold-rolled steel sheet having excellent strength and elongation according to an embodiment of the present invention may have a composite reinforcement index of 500 to 600 defined by the following [Equation 3].
- the cold-rolled steel sheet having excellent strength and elongation according to an embodiment of the present invention preferably has a yield strength of 500 to 600 MPa and an elongation of 8% or more.
- the cold-rolled steel sheet having excellent strength and elongation according to an embodiment of the present invention may further include a plating layer on one or both sides of the cold-rolled steel sheet, and the plating layer at this time is plated with tin, tin alloy, or chrome to a thickness of 5 ⁇ m or less. It could be
- C 0.04 ⁇ 0.08%, Si: 0.05% or less (excluding 0%), Mn: 0.1 ⁇ 0.6%, Al : 0.02 to 0.06%, P: 0.015% or less (excluding 0%), S: 0.015% or less (excluding 0%), N: 0.006% or less (excluding 0%), Nb: 0.02 to 0.04 %, the remainder includes Fe and other unavoidable impurities, and a slab preparation step of preparing and reheating a slab having a component enhancement index defined by Equation 1 below of 470; preparing a hot-rolled steel sheet by hot-rolling the slab and hot-rolling the finish at Ar3 or higher; winding the hot-rolled steel sheet at 560 to 700° C.; manufacturing a cold-rolled steel sheet by cold-rolling the rolled hot-rolled steel sheet at a reduction ratio of 80 to 95%; annealing the cold-rolled steel sheet at a
- the slab is preferably heated at 1,150 ° C. or higher.
- the secondary rolling is preferably performed at a rolling reduction of 4 to 10%.
- the cold-rolled steel sheet manufactured after the secondary rolling may have a grain aspect ratio of 2.15 or less defined by the following [Equation 2].
- the cold-rolled steel sheet manufactured after the secondary rolling may have a composite reinforcement index of 500 to 600 defined by [Equation 3] below.
- a plating layer may be further formed by hot-dipping or electroplating on one or both sides of the cold-rolled steel sheet.
- the plating layer may be plated with tin, tin alloy, or chrome to a thickness of 5 ⁇ m or less.
- a cold-rolled steel sheet that is excellent in strength and elongation at the same time and can be used as a material for a can.
- tin or tin alloy is plated on a steel sheet for a can to exhibit a high yield strength of 500 to 600 MPa and an elongation of 8% or more to be used in a bead molding body and a part such as EOE of a can.
- An easy cold-rolled steel sheet can be provided.
- first, second and third are used to describe, but are not limited to, various parts, components, regions, layers and/or sections. These terms are only used to distinguish one part, component, region, layer or section from another part, component, region, layer or section. Accordingly, a first part, component, region, layer or section described below may be referred to as a second part, component, region, layer or section without departing from the scope of the present invention.
- % means weight%, and 1ppm is 0.0001 weight%.
- the meaning of further including an additional element means replacing and including iron (Fe) as much as the additional amount of the additional element.
- One embodiment of the present invention relates to a cold-rolled steel sheet for a can, which is manufactured into a can through molding after tin plating, and the material for the corresponding application must have excellent strength and high elongation to secure workability.
- a method for increasing productivity by minimizing the load in the steelmaking process is also considered.
- the present inventors have confirmed that it is possible to provide a cold-rolled steel sheet for cans by simultaneously securing desired levels of strength and elongation by precisely controlling the type and content of alloy elements and optimizing the manufacturing process conditions. led to the invention.
- the cold-rolled steel sheet having excellent strength and elongation at the same time contains C: 0.04 ⁇ 0.08%, Si: 0.05% or less (excluding 0%), Mn: 0.1 ⁇ 0.6%, Al: 0.02% by weight. ⁇ 0.06%, P: 0.015% or less (excluding 0%), S: 0.015% or less (excluding 0%), N: 0.006% or less (excluding 0%), Nb: 0.02 to 0.04% and the balance includes Fe and other unavoidable impurities.
- the content of each component means % by weight.
- C content is low, it is difficult to be used as a structural material due to low strength, and an excessively low content of C may include 0.04% by weight or more because a refining process is additionally required to reduce productivity. C can effectively increase strength even with a small content, but if it is excessive, workability can be greatly reduced, so the upper limit can be limited to 0.08% by weight or less. More specifically, C may be included in an amount of 0.05 to 0.07% by weight.
- Si is an element that can be used as a decarburization agent and is difficult to completely exclude because it can contribute to the improvement of strength by solid solution strengthening. However, if it is excessive, Si-based oxide is generated on the surface during annealing, which may cause defects during plating, thereby degrading plating properties. Therefore, in consideration of this, the upper limit may be limited to 0.05% by weight or less. More specifically, Si may be included in an amount of 0.005 to 0.03% by weight.
- Mn is an element that prevents hot shortness due to solid solution S by combining with solid solution S in steel and precipitating as MnS. In order to achieve this effect, it may be included in an amount of 0.1% by weight or more. In addition, it is employed in the steel and has the effect of increasing the strength of the steel together with C. However, if it is excessive, the workability of the steel is lowered, so it may be limited to 0.6% by weight or less. In addition, there are many standards that regulate the Mn content to 0.6% or less for steel materials for food use, and if it exceeds this, it may cause problems in use for the intended purpose. More specifically, Mn may be included in an amount of 0.30 to 0.60% by weight.
- Al is an element with a very high deoxidation effect, and it reacts with N in steel to precipitate AlN, thereby preventing deterioration in formability due to dissolved N. Therefore, 0.02% by weight or more of Al may be included. However, when a large amount is added, the ductility is rapidly reduced, so the content may be limited to 0.06% by weight or less. More specifically, 0.02 to 0.05% by weight of Al may be included.
- P below a certain amount does not significantly reduce the ductility of the steel and can increase the strength, but if it is added in excess of 0.015% by weight, it is segregated at the grain boundary and hardens the steel excessively and the elongation decreases, so it is limited to 0.015% by weight or less. can do. More specifically, P may include 0.015% by weight or less. More specifically, P may include 0.003 to 0.010% by weight.
- the precipitation of MnS should be induced through the addition of Mn. It is undesirable to add more than the limiting range because the more S is, the corresponding level of Mn must be additionally added. Therefore, the upper limit of S can be limited to 0.015% by weight. More specifically, S may include 0.003 to 0.010% by weight.
- N is contained as an unavoidable element in steel, but N, which exists in a solid solution state, causes aging and greatly deteriorates workability. It is preferable to limit the upper limit to 0.0060% by weight or less in order to minimize the decrease in ductility due to aging. More specifically, 0.0015 to 0.0050% by weight of N may be included.
- Nb is combined with C to precipitate as fine NbC and exerts a precipitation strengthening effect.
- NbC is excessively formed, recrystallization is suppressed during annealing after cold rolling, and annealing at a high temperature is required.
- the content of Nb is 0.02 to 0.04%.
- the present inventors found that the strength of the hot-rolled steel sheet manufactured from the range for each component was proportional to the component enhancement index defined by [Equation 1] below.
- the component enhancement index of [Equation 1] exceeds 470, the strength of the steel sheet is high, so cold rolling is difficult. Therefore, the component enhancement index defined by [Equation 1] contains C, Mn, and Nb within a range not exceeding 470. It is desirable to limit In addition, when the component reinforcement index of [Equation 1] is, for example, less than 350, the strength of the steel is low, and a high secondary rolling reduction is required to compensate for this, but there is a problem that the elongation is greatly reduced accordingly, so the lower limit value of [Equation 1] It is desirable to limit
- the component enhancement index of [Equation 1] is derived recursively through experiments within the component range of the present invention, and may not be applied outside the component range.
- the remainder preferably includes Fe and unavoidable impurities, and the steel material of the present invention does not exclude the addition of other compositions.
- the unavoidable impurities may be unintentionally mixed from raw materials or the surrounding environment in the normal steel manufacturing process, and cannot be excluded.
- the above unavoidable impurities can be understood by those skilled in the ordinary steel manufacturing field.
- the cold-rolled steel sheet having excellent strength and elongation according to an embodiment of the present invention may have a grain aspect ratio of 2.15 or less defined by the following [Equation 2].
- Grain aspect ratio (average value of long axis length of crystal grains) / (average value of minor axis length of crystal grains) --- [Equation 2]
- the average grain length in the major axis direction measures the average grain diameter in the rolling direction (RD direction), and the average value can be obtained by dividing the number of crystal grains present in the corresponding length in the rolling direction of an arbitrary length.
- the average length of the grain minor direction can be obtained as the average value by measuring the diameter of the average grain in the thickness direction of the steel sheet and dividing the number of grains present with respect to the thickness of the steel sheet.
- the crystal grain aspect ratio may be 1.80 to 2.15.
- the yield strength of the steel sheet increases as the reduction ratio increases during secondary rolling. It is preferable to combine them appropriately.
- the composite reinforcement index according to [Equation 3] is related to the component reinforcement index according to [Equation 1] and the crystal grain aspect ratio according to [Equation 2], and this composite reinforcement index value obtains a yield strength of 500 to 600 MPa after plating.
- the composite reinforcement index value of [Equation 3] has 500 to 600.
- the value of the composite reinforcement index is preferably 520 to 580.
- the cold-rolled steel sheet according to one embodiment of the present invention is excellent in strength and elongation at the same time.
- the yield strength may be 500 to 600 MPa
- the elongation may be 8.0% or more.
- a plated steel sheet according to an embodiment of the present invention includes a cold-rolled steel sheet and a plating layer positioned on one side or both sides of the cold-rolled steel sheet.
- the metal included in the plating layer may be one or more of tin (Sn), tin alloys (Sn-Ni, Sn-Co, Sn-Zn), or chromium (Cr).
- the Sn or Sn alloy plating layer formed on the cold-rolled steel sheet is difficult to discolor in the air, has low toxicity to the human body, and is stable to organic acids of food or citrus fruits, so it can be applied intimately to household products.
- the tin or tin alloy plating layer may be plated to a thickness of 5 ⁇ m or less by an electroplating method.
- the thickness of the plating layer is preferably 0.1 to 3.5 ⁇ m.
- a method of manufacturing a cold-rolled steel sheet having excellent strength and elongation includes the steps of hot-rolling a slab to prepare a hot-rolled steel sheet; Winding the hot-rolled steel sheet; Cold-rolling the hot-rolled steel sheet to produce a cold-rolled steel sheet and annealing the cold-rolled steel sheet.
- a hot-rolled steel sheet is manufactured by hot-rolling a slab.
- the alloy composition of the slab is the same as that of the aforementioned cold-rolled steel sheet, overlapping descriptions will be omitted. Since the alloy composition is not substantially changed during the manufacturing process of the cold-rolled steel sheet, the alloy composition of the slab and the cold-rolled steel sheet are substantially the same.
- the slabs Before hot rolling the slabs may be reheated to a temperature of 1,150°C or higher. Since most of the precipitates present in the steel must be re-dissolved, a temperature of 1,150 ° C or higher may be required. More specifically, it may be heated to 1,200 °C or more in order to dissolve the precipitate well.
- a hot-rolled steel sheet is manufactured by hot finishing rolling the slowly cooled slab at a temperature of Ar 3 or higher.
- the reason for limiting the hot rolling finishing temperature to Ar 3 or higher is to perform rolling in the austenite single phase region.
- the Ar 3 temperature is slightly different depending on the content of the component elements, but since it is a temperature that can be understood by a person skilled in the steel manufacturing field, a detailed description thereof will be omitted. More specifically, the finish rolling temperature may be 900° C. or higher.
- the hot-rolled steel sheet is wound at 560 to 700°C.
- Precipitation of NbC may be affected by the winding temperature. That is, if the coiling temperature is too low, NbC may not be smoothly deposited inside the steel sheet, and even if the coiling temperature is too high, NbC may not be smoothly deposited. Therefore, the coiling temperature of the hot-rolled steel sheet according to an embodiment of the present invention may be 560 to 700 °C. In this way, by limiting the winding temperature, NbC is optimally precipitated to secure the required level of strength.
- a preferred winding temperature may be 580 to 680 °C.
- the hot-rolled steel sheet according to an embodiment of the present invention preferably has a yield strength of 470 MPa or less. If the yield strength of the hot-rolled steel sheet exceeds 470 MPa, the productivity of cold rolling is poor, so it is preferable to limit it as such.
- the hot-rolled steel sheet is cold-rolled.
- a cold-rolled steel sheet is manufactured by cold-rolling a hot-rolled steel sheet wound in a coil state at a reduction ratio of 80 to 95%.
- the reduction ratio not only determines the final thickness of the cold-rolled steel sheet, but also increases the strength of the steel sheet by work hardening during cold rolling.
- the thickness of the hot-rolled steel sheet is preferably 2.0 to 4.0 mm.
- the reduction ratio In order to cold-roll such a hot-rolled steel sheet as thin as 0.4 mm or less, the reduction ratio must be 80% or more. Therefore, it is preferable to apply a reduction ratio of 80% or more for cold rolling according to an embodiment of the present invention.
- the reduction ratio of cold rolling is preferably 80 to 95%.
- the cold-rolled steel sheet is annealed at a temperature of 720 to 800 ° C.
- the annealing temperature is determined to remove the internal stress accumulated in the steel sheet during cold rolling and to properly secure workability.
- the annealing temperature needs to be annealed at a sufficiently high temperature so that recrystallization occurs sufficiently. Since the NbC precipitate has an effect of inhibiting recrystallization, it is preferable to annealing at a temperature of 720 ° C. or higher that can overcome this.
- annealing is performed at 800° C. or higher, since the strength of the steel sheet is reduced at high temperatures, the steel sheet may be broken when the thickness of the steel sheet is thinned, so annealing may be performed at a temperature of 720 to 800° C.
- a final steel sheet is manufactured by performing secondary rolling on the annealed steel sheet.
- the secondary rolling be performed at a rolling reduction of 4 to 10%. Since the steel sheet annealed under the above conditions does not have sufficient strength, secondary rolling is performed to obtain a desired level of strength in one embodiment of the present invention. For this purpose, it is preferable to perform secondary rolling at a rolling reduction of 4% or more. However, since the elongation decreases when the reduction ratio exceeds 10%, it is not guaranteed to secure the required level of workability.
- a plating layer is formed on one or both surfaces of the steel sheet manufactured in the above process.
- the metal included in the plating layer may be one or more of tin (Sn), tin alloys (Sn-Ni, Sn-Co, Sn-Zn), or chromium (Cr).
- a reflow process of 200 ° C or higher or a dry heat treatment process after printing may be performed, and in the case of such a heating process, the material of the steel sheet may change .
- the yield strength generally increases and the elongation decreases. Similar results can be obtained when the material change effect is maintained at 200° C. for 20 minutes on an uncoated steel sheet. From the consumer's point of view, since the strength and elongation after plating are important, it is preferable to measure the final material of the steel sheet of the present invention after maintaining it at 200 ° C. for 20 minutes.
- the secondary rolling is performed at a rolling reduction of 4 to 10%, which is the range of an embodiment of the present invention.
- the yield strength of the steel sheet increases. Therefore, in order to secure the yield strength of the level suggested in one embodiment of the present invention, it is preferable to control the reinforcing factor of the steel sheet component and the strengthening effect due to the secondary rolling by appropriately combining them together.
- a steel having the composition shown in Table 1 was prepared, and the components indicated actual values.
- the slabs were reheated to 1,240 ° C, hot-rolled at 900 ° C or higher to a thickness of 2 mm, and then wound at a temperature of 620 ° C to manufacture a hot-rolled steel sheet.
- These hot-rolled steel sheets were cold-rolled at a reduction ratio of 90% to prepare a 0.2 mm cold-rolled steel sheet.
- continuous annealing was performed on the cold-rolled steel sheet under the condition of maintaining the temperature at 760° C. for 40 seconds. If the secondary rolling was performed on the annealed steel sheets as described above, the reduction ratio of the secondary rolling at this time is shown in Table 1 together.
- the crystal grain aspect ratio can be obtained by observing and calculating the shape of each crystal grain through optical microscope observation for the cross section in the rolling direction.
- the strength and elongation of the hot-rolled steel sheet and the final material were measured through a tensile test at room temperature after coil manufacture.
- inventive steels 1 to 19 satisfy all of the component content proposed in the present invention, the component reinforcement index of [Equation 1], the grain aspect ratio of [Equation 2], and the composite reinforcement index of [Equation 3].
- the yield strength of the hot-rolled steel sheet is less than 470 MPa, there is no problem in productivity through each detailed manufacturing process including cold rolling.
- inventive steels 1 to 19 have a yield strength of 500 to 600 MPa and an elongation of 8% or more after heat treatment of the final material at 200 ° C for 20 minutes. can know that
- inventive steels 14 and 15 even though the component enhancement index of [Equation 1] is high enough to approach 470, the secondary reduction ratio is low at 4.2 and 5.0, and the grain aspect ratio of [Equation 2] is also low at 1.92 and 1.95, so it is suitable. It can be seen that the complex reinforcement index of [Equation 3] can be obtained. As a result, it can be confirmed that the inventive steels 14 and 15 were also able to secure a suitable level of final material.
- Comparative Steels 1 to 4 had a component strengthening index of [Equation 1] exceeding 470, and the yield strength of the hot-rolled steel sheet also exceeded 470 MPa, resulting in poor cold rolling properties.
- the comparative steels 5 and 6 had a rolling reduction ratio of the second rolling exceeding 10%, and accordingly, the crystal grain aspect ratio in [Equation 2] exceeded 2.15 and the elongation was also less than 8%.
- the component reinforcement index of [Equation 1] was properly controlled to 470 or less in Comparative Steels 5 and 6, the composite reinforcement index of [Equation 3] exceeded 600, indicating that the yield strength also exceeded 600 MPa. This makes it possible to know that if the reduction ratio of the secondary rolling is excessively high, the yield strength is exceeded and the elongation is insufficient.
- Comparative Steels 7 to 20 satisfy the criteria presented in one embodiment of the present invention in both the component reinforcement index of [Equation 1] and the crystal grain aspect ratio of [Equation 2], but the composite reinforcement index of [Equation 3] is 500 It can be seen that it does not meet the criteria presented as less than.
- the strength of the hot-rolled steel sheet is 470 MPa or less, and the cold-rollability is good, but the yield strength of the final material is less than 500, which is less than the yield strength of the target value presented.
- the component reinforcement index of [Equation 1] is low, and the comparative steels 17 to 20 have a low reduction ratio of secondary rolling.
- the component reinforcement index of [Equation 1] is low, there is no problem in cold rolling, and when the rolling reduction of secondary rolling is low, high elongation is secured due to the low crystal grain aspect ratio of [Equation 2], but composite reinforcement of [Equation 3] It can be seen that sufficient strengthening effect to obtain the final yield strength cannot be secured because the index does not meet the standard presented.
- comparative steel 23 In the case of comparative steel 23, the component reinforcement index of [Equation 1] and the crystal grain aspect ratio of [Equation 2] exceed the presented standards. In this case, the composite reinforcement index of [Equation 2] also exceeds the presented standards, for the same reason. unsuitable for use In addition, comparative steel 23 has excessively high strength of hot-rolled steel sheet, so it has poor cold-rollability and a high reduction ratio in secondary rolling, exceeding the grain shape ratio in [Equation 2] and also showing that the final elongation does not meet the proposed standard. You can check.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Heat Treatment Of Sheet Steel (AREA)
Abstract
Description
구분 | 성분 함량 (wt%) |
2차압하율
(%) |
|||||||
C | Si | Mn | Al | P | S | N | Nb | ||
발명강1 | 0.042 | 0.02 | 0.52 | 0.04 | 0.007 | 0.006 | 0.003 | 0.030 | 7.0 |
발명강2 | 0.058 | 0.02 | 0.49 | 0.04 | 0.007 | 0.005 | 0.003 | 0.031 | 7.0 |
발명강3 | 0.070 | 0.02 | 0.52 | 0.04 | 0.007 | 0.006 | 0.003 | 0.029 | 7.0 |
발명강4 | 0.079 | 0.02 | 0.52 | 0.04 | 0.006 | 0.006 | 0.003 | 0.031 | 7.0 |
발명강5 | 0.075 | 0.02 | 0.15 | 0.04 | 0.006 | 0.006 | 0.003 | 0.037 | 7.0 |
발명강6 | 0.067 | 0.02 | 0.30 | 0.04 | 0.007 | 0.006 | 0.003 | 0.035 | 7.0 |
발명강7 | 0.062 | 0.02 | 0.39 | 0.04 | 0.007 | 0.006 | 0.003 | 0.032 | 7.0 |
발명강8 | 0.062 | 0.02 | 0.47 | 0.04 | 0.007 | 0.006 | 0.003 | 0.029 | 7.0 |
발명강9 | 0.056 | 0.02 | 0.59 | 0.04 | 0.007 | 0.006 | 0.003 | 0.028 | 7.0 |
발명강10 | 0.078 | 0.02 | 0.55 | 0.04 | 0.007 | 0.006 | 0.003 | 0.023 | 7.0 |
발명강11 | 0.060 | 0.02 | 0.50 | 0.04 | 0.007 | 0.006 | 0.003 | 0.037 | 7.0 |
발명강12 | 0.053 | 0.02 | 0.20 | 0.04 | 0.008 | 0.006 | 0.003 | 0.039 | 7.0 |
발명강13 | 0.079 | 0.02 | 0.25 | 0.04 | 0.007 | 0.006 | 0.003 | 0.029 | 7.0 |
발명강14 | 0.072 | 0.02 | 0.49 | 0.04 | 0.007 | 0.006 | 0.003 | 0.037 | 4.2 |
발명강15 | 0.065 | 0.02 | 0.58 | 0.04 | 0.008 | 0.006 | 0.003 | 0.035 | 5.0 |
발명강16 | 0.061 | 0.02 | 0.54 | 0.04 | 0.007 | 0.006 | 0.003 | 0.032 | 6.0 |
발명강17 | 0.057 | 0.02 | 0.47 | 0.04 | 0.008 | 0.006 | 0.003 | 0.031 | 7.0 |
발명강18 | 0.064 | 0.02 | 0.50 | 0.04 | 0.006 | 0.006 | 0.003 | 0.029 | 8.0 |
발명강19 | 0.059 | 0.02 | 0.49 | 0.04 | 0.007 | 0.006 | 0.003 | 0.028 | 8.8 |
비교강1 | 0.085 | 0.02 | 0.55 | 0.04 | 0.007 | 0.006 | 0.003 | 0.035 | 7.0 |
비교강2 | 0.062 | 0.02 | 0.51 | 0.04 | 0.007 | 0.006 | 0.003 | 0.045 | 7.0 |
비교강3 | 0.075 | 0.02 | 0.85 | 0.04 | 0.006 | 0.006 | 0.003 | 0.038 | 7.0 |
비교강4 | 0.077 | 0.02 | 0.55 | 0.04 | 0.007 | 0.006 | 0.003 | 0.038 | 7.0 |
비교강5 | 0.060 | 0.02 | 0.54 | 0.04 | 0.007 | 0.006 | 0.003 | 0.031 | 10.7 |
비교강6 | 0.060 | 0.02 | 0.52 | 0.04 | 0.007 | 0.006 | 0.003 | 0.028 | 12.1 |
비교강7 | 0.021 | 0.02 | 0.54 | 0.04 | 0.007 | 0.006 | 0.003 | 0.028 | 7.0 |
비교강8 | 0.042 | 0.02 | 0.15 | 0.04 | 0.007 | 0.006 | 0.003 | 0.025 | 8.5 |
비교강9 | 0.057 | 0.02 | 0.05 | 0.04 | 0.007 | 0.006 | 0.003 | 0.030 | 7.0 |
비교강10 | 0.054 | 0.02 | 0.15 | 0.04 | 0.007 | 0.006 | 0.003 | 0.029 | 7.0 |
비교강11 | 0.054 | 0.02 | 0.49 | 0.04 | 0.007 | 0.006 | 0.003 | 0.012 | 7.0 |
비교강12 | 0.055 | 0.02 | 0.51 | 0.04 | 0.007 | 0.006 | 0.003 | 0.021 | 7.0 |
비교강13 | 0.050 | 0.02 | 0.32 | 0.04 | 0.006 | 0.006 | 0.003 | 0.027 | 7.0 |
비교강14 | 0.060 | 0.02 | 0.25 | 0.04 | 0.007 | 0.006 | 0.003 | 0.026 | 7.0 |
비교강15 | 0.043 | 0.02 | 0.52 | 0.04 | 0.007 | 0.006 | 0.003 | 0.021 | 7.0 |
비교강16 | 0.041 | 0.02 | 0.11 | 0.04 | 0.007 | 0.006 | 0.003 | 0.023 | 7.0 |
비교강17 | 0.060 | 0.02 | 0.50 | 0.04 | 0.006 | 0.006 | 0.003 | 0.038 | 3.0 |
비교강18 | 0.066 | 0.02 | 0.50 | 0.04 | 0.008 | 0.006 | 0.003 | 0.029 | 4.2 |
비교강19 | 0.058 | 0.02 | 0.54 | 0.04 | 0.007 | 0.007 | 0.003 | 0.027 | 5.4 |
비교강20 | 0.042 | 0.02 | 0.53 | 0.04 | 0.008 | 0.006 | 0.003 | 0.025 | 6.2 |
비교강21 | 0.075 | 0.02 | 0.53 | 0.04 | 0.007 | 0.006 | 0.003 | 0.036 | 8.5 |
비교강22 | 0.070 | 0.02 | 0.58 | 0.04 | 0.007 | 0.006 | 0.003 | 0.034 | 8.7 |
비교강23 | 0.090 | 0.02 | 0.11 | 0.04 | 0.007 | 0.006 | 0.003 | 0.045 | 10.1 |
구분 | 성분강화지수 [수식1] |
결정립 형상비 [수식2] |
복합강화지수 [수식3] |
열연강판 항복강도 (MPa) |
소재 재질 (200℃ 20분 유지 후) |
|
항복강도 (MPa) |
연신율 (%) |
|||||
발명강1 | 404.0 | 2.05 | 531.4 | 413.4 | 522.2 | 10.0 |
발명강2 | 422.0 | 2.02 | 531.9 | 421.6 | 522.5 | 9.9 |
발명강3 | 427.0 | 1.99 | 520.5 | 424.9 | 523.0 | 9.7 |
발명강4 | 446.0 | 2.01 | 550.6 | 433.1 | 548.7 | 10.3 |
발명강5 | 435.0 | 2.03 | 551.5 | 445.1 | 551.1 | 10.2 |
발명강6 | 431.5 | 2.01 | 538.1 | 430.9 | 541.1 | 10.4 |
발명강7 | 421.0 | 2.05 | 547.0 | 418.2 | 542.1 | 10.1 |
발명강8 | 414.0 | 2.02 | 525.6 | 411.0 | 523.0 | 10.0 |
발명강9 | 415.0 | 2.06 | 545.0 | 416.6 | 544.4 | 10.1 |
발명강10 | 408.0 | 2.05 | 534.9 | 413.2 | 524.3 | 9.9 |
발명강11 | 455.0 | 2.02 | 564.4 | 450.2 | 556.7 | 9.8 |
발명강12 | 428.0 | 2.03 | 543.0 | 434.2 | 537.9 | 10.0 |
발명강13 | 409.0 | 2.05 | 533.6 | 416.7 | 537.4 | 10.2 |
발명강14 | 466.0 | 1.92 | 524.8 | 468.2 | 517.2 | 12.9 |
발명강15 | 458.0 | 1.95 | 535.3 | 448.1 | 543.0 | 12.6 |
발명강16 | 435.0 | 1.99 | 530.8 | 423.9 | 541.4 | 11.5 |
발명강17 | 419.0 | 2.05 | 544.8 | 416.7 | 536.2 | 10.4 |
발명강18 | 419.0 | 2.02 | 530.3 | 417.0 | 530.6 | 9.0 |
발명강19 | 408.0 | 2.07 | 543.7 | 410.5 | 542.5 | 8.2 |
비교강1 | 475.0 | 2.05 | 598.7 | 475.3 | 599.5 | 9.7 |
비교강2 | 498.0 | 2.03 | 613.4 | 493.5 | 603.4 | 10.3 |
비교강3 | 510.0 | 2.02 | 619.5 | 514.6 | 609.9 | 9.9 |
비교강4 | 482.0 | 2.04 | 601.1 | 483.8 | 605.2 | 10.0 |
비교강5 | 429.0 | 2.19 | 624.0 | 437.9 | 613.1 | 6.5 |
비교강6 | 412.0 | 2.23 | 625.6 | 402.2 | 629.4 | 4.9 |
비교강7 | 375.0 | 2.04 | 496.9 | 373.4 | 492.8 | 10.5 |
비교강8 | 342.0 | 2.10 | 492.4 | 343.4 | 489.0 | 8.2 |
비교강9 | 372.0 | 2.00 | 470.1 | 370.5 | 461.1 | 9.8 |
비교강10 | 374.0 | 1.99 | 468.9 | 372.9 | 468.9 | 10.4 |
비교강11 | 323.0 | 1.99 | 419.4 | 320.7 | 426.2 | 10.4 |
비교강12 | 371.0 | 2.01 | 478.1 | 377.9 | 469.9 | 10.4 |
비교강13 | 377.0 | 2.01 | 479.5 | 388.2 | 478.1 | 10.4 |
비교강14 | 375.0 | 2.01 | 479.6 | 375.3 | 485.9 | 10.3 |
비교강15 | 360.0 | 2.00 | 461.0 | 353.7 | 456.0 | 9.9 |
비교강16 | 327.0 | 2.05 | 453.6 | 317.3 | 445.8 | 10.0 |
비교강17 | 460.0 | 1.83 | 472.8 | 465.1 | 480.0 | 13.7 |
비교강18 | 421.0 | 1.91 | 476.9 | 415.5 | 477.5 | 12.7 |
비교강19 | 407.0 | 1.97 | 494.5 | 414.6 | 488.2 | 11.4 |
비교강20 | 380.0 | 2.01 | 486.5 | 391.2 | 486.5 | 10.3 |
비교강21 | 468.0 | 2.11 | 623.9 | 460.3 | 624.8 | 8.7 |
비교강22 | 458.0 | 2.09 | 604.8 | 450.4 | 603.3 | 8.3 |
비교강23 | 486.0 | 2.16 | 664.2 | 489.7 | 670.8 | 6.9 |
Claims (12)
- 중량%로 C: 0.04 ~ 0.08%, Si: 0.05% 이하(0%를 제외한다), Mn: 0.1 ~ 0.6%, Al: 0.02 ~ 0.06%, P: 0.015% 이하(0%를 제외한다), S: 0.015% 이하(0%를 제외한다), N: 0.006% 이하(0%를 제외한다), Nb: 0.02 ~ 0.04%를 포함하고, 나머지는 Fe 및 기타 불가피한 불순물을 포함하며,하기 [수식 1]로 정의되는 성분 강화지수가 470이하이고,하기 [수식 2]로 정의되는 결정립 형상비가 2.15 이하이며,하기 [수식 3]으로 정의되는 복합 강화지수가 500 ~ 600인 강도와 연신율이 우수한 냉연강판.[수식 1]: 성분 강화지수 = 160 + 1,000C + 100Mn + 5,000Nb(단, 수식 1의 C, Mn, Nb은 각 성분의 중량%를 의미한다.)[수식 2]: 결정립 형상비=[(결정립 장축길이)/(결정립 단축길이)]의 평균값[수식 3]: 복합 강화지수 = [수식 1] + ([수식 2] - 1.8) X 600
- 제1항에 있어서,상기 냉연강판의 항복강도가 500 ~ 600MPa인 강도와 연신율이 우수한 냉연강판.
- 제1항에 있어서,상기 냉연강판의 연신율이 8% 이상인 강도와 연신율이 우수한 냉연강판.
- 제1항에 기재된 냉연강판 및 상기 냉연강판의 일면 또는 양면에 위치하는 도금층을 포함하는 도금 강판.
- 제4항에 있어서,상기 도금강판은 주석, 주석합금 또는 크롬이 두께 5㎛이하로 도금된 도금강판.
- 중량%로 C: 0.04 ~ 0.08%, Si: 0.05% 이하(0%를 제외한다), Mn: 0.1 ~ 0.6%, Al: 0.02 ~ 0.06%, P: 0.015% 이하(0%를 제외한다), S: 0.015% 이하(0%를 제외한다), N: 0.006% 이하(0%를 제외한다), Nb: 0.02 ~ 0.04%를 포함하고, 나머지는 Fe 및 기타 불가피한 불순물을 포함하며, 하기 [수식 1]로 정의되는 성분 강화지수가 470 이하인 슬라브 준비하여 재가열하는 슬라브 준비 단계;상기 슬라브를 열간압연하고 Ar3 이상에서 마무리 열간압연하여 열연강판을 제조하는 단계;상기 열연강판을 560 내지 700℃에서 권취하는 단계;상기 권취된 열연강판을 80 내지 95% 압하율로 냉간압연하여 냉연강판을 제조하는 단계;상기 냉연강판을 720 내지 800℃의 온도에서 소둔하는 단계; 및상기 소둔한 냉연강판을 2차 압연하는 단계를 포함하는 강도 및 연신율이 우수한 냉연강판의 제조방법.[수식 1]: 성분 강화지수 = 160 + 1,000C + 100Mn + 5,000Nb(단, 수식 1의 C, Mn, Nb은 각 성분의 중량%를 의미한다.)
- 제6항에 있어서,상기 슬라브 준비단계에서, 상기 슬라브는 1,150℃ 이상에서 가열하는 강도 및 연신율이 우수한 냉연강판의 제조방법.
- 제6항에 있어서,상기 2차 압연은 4 ~ 10%의 압하율로 압연하는 강도 및 연신율이 우수한 냉연강판의 제조방법.
- 제6항에 있어서,상기 2차 압연 이후의 냉연강판은 하기 [수식 2]로 정의되는 결정립 형상비가 2.15 이하인 강도와 연신율이 우수한 냉연강판의 제조방법.[수식 2]: 결정립 형상비=[(결정립 장축길이)/(결정립 단축길이)]의 평균값
- 제6항에 있어서,상기 2차 압연 이후의 냉연강판은 하기 [수식 3]으로 정의되는 복합 강화지수가 500 ~ 600인 강도와 연신율이 우수한 냉연강판의 제조방법.[수식 3]: 복합 강화지수 = [수식 1] + ([수식 2] - 1.8) X 600
- 제6항에 기재된 방법으로 냉연강판을 제조하는 단계; 및상기 냉연강판의 일면 또는 양면에 용융도금 내지 전기도금하여 도금층을 형성하는 단계를 더 포함하는 도금 강판의 제조 방법.
- 제11항에 있어서,상기 도금청을 형성하는 단계는 주석, 주석합금 또는 크롬 중 어느 하나 이상을 두께 5㎛ 이하로 도금하는 도금강판의 제조방법.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP22911827.8A EP4455340A1 (en) | 2021-12-21 | 2022-12-19 | Cold-rolled steel sheet having excellent strength and elongation and method for manufacturing same |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020210183663A KR20230094461A (ko) | 2021-12-21 | 2021-12-21 | 강도와 연신율이 우수한 냉연강판 및 그 제조방법 |
KR10-2021-0183663 | 2021-12-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2023121194A1 true WO2023121194A1 (ko) | 2023-06-29 |
Family
ID=86903382
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/KR2022/020758 WO2023121194A1 (ko) | 2021-12-21 | 2022-12-19 | 강도와 연신율이 우수한 냉연강판 및 그 제조방법 |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP4455340A1 (ko) |
KR (1) | KR20230094461A (ko) |
WO (1) | WO2023121194A1 (ko) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20000034959A (ko) * | 1998-11-25 | 2000-06-26 | 에모토 간지 | 캔용 강철 스트립 및 그의 제조 방법 |
KR20020072646A (ko) * | 2001-03-12 | 2002-09-18 | 한국기계연구원 | 초내식용 크롬/크롬-엑스 합금도금층의 제조방법 |
KR20030035697A (ko) * | 2001-11-02 | 2003-05-09 | 주식회사 포스코 | 시효성, 내부식성 및 내꺽임성이 우수한 고강도 주석도금강판의 제조방법 |
JP2007291457A (ja) * | 2006-04-26 | 2007-11-08 | Nikko Kinzoku Kk | ウィスカーが抑制されたCu−Zn合金耐熱Snめっき条 |
KR20130002419A (ko) * | 2011-06-29 | 2013-01-08 | 현대제철 주식회사 | 상소둔 강판 및 그 제조방법 |
-
2021
- 2021-12-21 KR KR1020210183663A patent/KR20230094461A/ko unknown
-
2022
- 2022-12-19 EP EP22911827.8A patent/EP4455340A1/en active Pending
- 2022-12-19 WO PCT/KR2022/020758 patent/WO2023121194A1/ko active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR20000034959A (ko) * | 1998-11-25 | 2000-06-26 | 에모토 간지 | 캔용 강철 스트립 및 그의 제조 방법 |
KR20020072646A (ko) * | 2001-03-12 | 2002-09-18 | 한국기계연구원 | 초내식용 크롬/크롬-엑스 합금도금층의 제조방법 |
KR20030035697A (ko) * | 2001-11-02 | 2003-05-09 | 주식회사 포스코 | 시효성, 내부식성 및 내꺽임성이 우수한 고강도 주석도금강판의 제조방법 |
JP2007291457A (ja) * | 2006-04-26 | 2007-11-08 | Nikko Kinzoku Kk | ウィスカーが抑制されたCu−Zn合金耐熱Snめっき条 |
KR20130002419A (ko) * | 2011-06-29 | 2013-01-08 | 현대제철 주식회사 | 상소둔 강판 및 그 제조방법 |
Also Published As
Publication number | Publication date |
---|---|
EP4455340A1 (en) | 2024-10-30 |
KR20230094461A (ko) | 2023-06-28 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2022004969A1 (ko) | 열간 프레스용 강판 및 이의 제조 방법 | |
WO2020222394A1 (ko) | 핫 스탬핑 부품 및 그 제조방법 | |
WO2010074370A1 (ko) | 고강도 고연신 강판 및 열연강판, 냉연강판, 아연도금강판 및 아연도금합금화강판의 제조방법 | |
WO2017111290A1 (ko) | Pwht 저항성이 우수한 저온 압력용기용 강판 및 그 제조 방법 | |
WO2015099222A1 (ko) | 용접성 및 버링성이 우수한 열연강판 및 그 제조방법 | |
WO2017222159A1 (ko) | 가공성이 우수한 고강도 냉연강판 및 그 제조 방법 | |
WO2011105652A1 (ko) | 도금성이 우수한 고강도 강판 및 그 제조 방법 | |
WO2017051998A1 (ko) | 도금 강판 및 이의 제조방법 | |
WO2016182098A1 (ko) | 굽힘 가공성이 우수한 초고강도 열연강판 및 그 제조 방법 | |
WO2021085800A1 (ko) | 항복비가 향상된 오스테나이트계 스테인리스강 및 그 제조 방법 | |
WO2013154254A1 (ko) | 재질 균일성이 우수한 고탄소 열연강판 및 이의 제조방법 | |
WO2010074458A2 (ko) | 딥드로잉성이 우수하고 고항복비를 갖는 고강도 냉연강판, 이를 이용한 용융아연도금강판, 합금화 용융아연도금강판 및 이들의 제조방법 | |
WO2011081236A1 (ko) | 열간 프레스 가공성이 우수한 열처리 강화형 강판 및 그 제조방법 | |
WO2016047840A1 (ko) | 압연강판 및 그의 제조방법 | |
WO2023121194A1 (ko) | 강도와 연신율이 우수한 냉연강판 및 그 제조방법 | |
WO2021125564A1 (ko) | 클램프용 고강도 페라이트계 스테인리스강 및 그 제조방법 | |
WO2021125724A2 (ko) | 내열성과 성형성이 우수한 냉연강판 및 그 제조방법 | |
WO2022097989A1 (ko) | 선영성이 우수한 고강도 아연계 도금강판 및 그 제조방법 | |
WO2021261884A1 (ko) | 생산성 및 원가 절감 효과가 우수한 고강도 오스테나이트계 스테인리스강 및 이의 제조방법 | |
WO2023113558A1 (ko) | 프레스 성형성이 우수한 냉연강판, 아연도금강판, 및 이들의 제조 방법 | |
WO2019031773A1 (ko) | 표면 품질, 강도 및 연성이 우수한 도금강판 | |
WO2023075287A1 (ko) | 페라이트계 스테인리스강 및 그 제조방법 | |
WO2022103058A1 (ko) | 내파우더링성이 우수한 소부경화형 용융아연도금강판 및 이의 제조방법 | |
WO2022131635A1 (ko) | 강도, 성형성 및 표면 품질이 우수한 도금강판 및 이의 제조방법 | |
WO2009157661A9 (ko) | 표면특성 및 내2차 가공취성이 우수한 소부경화강 및 그 제조방법 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 22911827 Country of ref document: EP Kind code of ref document: A1 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 18719157 Country of ref document: US Ref document number: 2401003833 Country of ref document: TH |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
ENP | Entry into the national phase |
Ref document number: 2022911827 Country of ref document: EP Effective date: 20240722 |