WO2017111449A1 - 도금성이 우수한 고강도 용융 아연계 도금 강재 및 그 제조방법 - Google Patents
도금성이 우수한 고강도 용융 아연계 도금 강재 및 그 제조방법 Download PDFInfo
- Publication number
- WO2017111449A1 WO2017111449A1 PCT/KR2016/014983 KR2016014983W WO2017111449A1 WO 2017111449 A1 WO2017111449 A1 WO 2017111449A1 KR 2016014983 W KR2016014983 W KR 2016014983W WO 2017111449 A1 WO2017111449 A1 WO 2017111449A1
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- WIPO (PCT)
- Prior art keywords
- dip galvanized
- galvanized steel
- strength hot
- less
- base iron
- Prior art date
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- 238000007747 plating Methods 0.000 title claims abstract description 116
- 238000000034 method Methods 0.000 title claims abstract description 29
- 239000000463 material Substances 0.000 title claims abstract description 8
- 229910000831 Steel Inorganic materials 0.000 title abstract description 43
- 239000010959 steel Substances 0.000 title abstract description 43
- 239000011701 zinc Substances 0.000 title abstract description 12
- 229910052725 zinc Inorganic materials 0.000 title abstract description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 title abstract description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 153
- 229910052742 iron Inorganic materials 0.000 claims abstract description 71
- 229910018134 Al-Mg Inorganic materials 0.000 claims abstract description 23
- 229910018467 Al—Mg Inorganic materials 0.000 claims abstract description 23
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 9
- 239000000956 alloy Substances 0.000 claims abstract description 9
- 229910001335 Galvanized steel Inorganic materials 0.000 claims description 38
- 239000008397 galvanized steel Substances 0.000 claims description 38
- 238000000137 annealing Methods 0.000 claims description 20
- 238000004519 manufacturing process Methods 0.000 claims description 14
- 229910052710 silicon Inorganic materials 0.000 claims description 14
- 229910052782 aluminium Inorganic materials 0.000 claims description 13
- 229910052748 manganese Inorganic materials 0.000 claims description 13
- 239000012535 impurity Substances 0.000 claims description 11
- 230000008719 thickening Effects 0.000 claims description 10
- 238000010438 heat treatment Methods 0.000 claims description 9
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims description 5
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 5
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 5
- 229910052804 chromium Inorganic materials 0.000 claims description 5
- 239000010960 cold rolled steel Substances 0.000 claims description 5
- 239000001301 oxygen Substances 0.000 claims description 5
- 230000003746 surface roughness Effects 0.000 claims description 5
- 229910052698 phosphorus Inorganic materials 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 3
- 229910001873 dinitrogen Inorganic materials 0.000 claims description 3
- 239000011261 inert gas Substances 0.000 claims description 3
- 229910052719 titanium Inorganic materials 0.000 claims description 3
- 229910006639 Si—Mn Inorganic materials 0.000 claims description 2
- 229910052757 nitrogen Inorganic materials 0.000 claims description 2
- 239000011572 manganese Substances 0.000 description 25
- 230000000694 effects Effects 0.000 description 14
- 239000011651 chromium Substances 0.000 description 10
- 230000007547 defect Effects 0.000 description 10
- 230000015572 biosynthetic process Effects 0.000 description 8
- 239000000203 mixture Substances 0.000 description 8
- 238000007789 sealing Methods 0.000 description 8
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 229910000859 α-Fe Inorganic materials 0.000 description 5
- 239000000853 adhesive Substances 0.000 description 4
- 230000001070 adhesive effect Effects 0.000 description 4
- 238000000354 decomposition reaction Methods 0.000 description 4
- 238000001336 glow discharge atomic emission spectroscopy Methods 0.000 description 4
- 239000010936 titanium Substances 0.000 description 4
- 229910004298 SiO 2 Inorganic materials 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- 229910001566 austenite Inorganic materials 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000007667 floating Methods 0.000 description 3
- 229910000765 intermetallic Inorganic materials 0.000 description 3
- 229910000734 martensite Inorganic materials 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000010955 niobium Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910017706 MgZn Inorganic materials 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 229910052796 boron Inorganic materials 0.000 description 2
- KRVSOGSZCMJSLX-UHFFFAOYSA-L chromic acid Substances O[Cr](O)(=O)=O KRVSOGSZCMJSLX-UHFFFAOYSA-L 0.000 description 2
- 230000000052 comparative effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- AWJWCTOOIBYHON-UHFFFAOYSA-N furo[3,4-b]pyrazine-5,7-dione Chemical compound C1=CN=C2C(=O)OC(=O)C2=N1 AWJWCTOOIBYHON-UHFFFAOYSA-N 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 230000001590 oxidative effect Effects 0.000 description 2
- 239000011574 phosphorus Substances 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000001953 recrystallisation Methods 0.000 description 2
- 238000007670 refining Methods 0.000 description 2
- 229920006395 saturated elastomer Polymers 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- 229910019142 PO4 Inorganic materials 0.000 description 1
- 230000003078 antioxidant effect Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 239000012153 distilled water Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000010419 fine particle Substances 0.000 description 1
- 238000005246 galvanizing Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000010309 melting process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 229910052758 niobium Inorganic materials 0.000 description 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 1
- 229910001562 pearlite Inorganic materials 0.000 description 1
- NBIIXXVUZAFLBC-UHFFFAOYSA-K phosphate Chemical compound [O-]P([O-])([O-])=O NBIIXXVUZAFLBC-UHFFFAOYSA-K 0.000 description 1
- 239000010452 phosphate Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 238000011946 reduction process Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000007790 solid phase Substances 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 238000006557 surface reaction Methods 0.000 description 1
- -1 titanium Chemical compound 0.000 description 1
- 239000011573 trace mineral Substances 0.000 description 1
- 235000013619 trace mineral Nutrition 0.000 description 1
- 230000009466 transformation Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Chemical compound O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- UGZADUVQMDAIAO-UHFFFAOYSA-L zinc hydroxide Chemical compound [OH-].[OH-].[Zn+2] UGZADUVQMDAIAO-UHFFFAOYSA-L 0.000 description 1
- 229940007718 zinc hydroxide Drugs 0.000 description 1
- 229910021511 zinc hydroxide Inorganic materials 0.000 description 1
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- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
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- 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
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
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- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
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- 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/30—Ferrous alloys, e.g. steel alloys containing chromium with cobalt
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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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/32—Ferrous alloys, e.g. steel alloys containing chromium with boron
Definitions
- the present invention relates to a high strength hot dip galvanized steel having excellent plating properties and a method of manufacturing the same.
- High-strength steel contains a large amount of oxidizing elements such as Si and Mn, compared to general steel, and it is easy to form an oxide that prevents plating on the surface during annealing.
- Patent Document 1 Korean Patent Publication No. 10-2014-0061669
- One of several objects of the present invention is to provide a high strength hot dip galvanized steel having excellent plating properties and a method of manufacturing the same.
- An Al enriched layer formed at the interface of the plated layer, and the occupied area ratio of the Al enriched layer is 70% or more (including 100%) to provide a high strength hot dip galvanized steel.
- the step of preparing a small iron containing Si: 0.01 to 1.6% by weight and Mn: 1.2 to 3.1% by weight the iron is 760 under the condition of dew point temperature of -60 ⁇ -10 Annealing heat treatment at a temperature of ⁇ 850, and immersing the annealing heat-treated iron in a Zn-Al-Mg-based plating bath and plating to obtain a high strength hot dip galvanized steel. It provides a method for manufacturing steel.
- the high strength hot dip galvanized steel according to the present invention has an excellent plating property.
- FIG. 1 is a scanning electron microscope (SEM) image of an interface layer of a hot dip galvanized steel according to Inventive Example 7.
- SEM scanning electron microscope
- FIG. 2 is a scanning electron microscope (SEM) image of an interface layer of a hot dip galvanized steel according to Comparative Example 5.
- SEM scanning electron microscope
- FIG. 3 is a schematic diagram schematically showing a hot dip plating apparatus in which a sealing box is installed.
- Hot-dip galvanized steel of the present invention comprises a base iron and Zn-Al-Mg-based plating layer.
- the base iron may be a steel sheet or steel wire.
- the composition of the base iron is not particularly limited except for Si and Cr, but as an example, in weight%, C: 0.05 to 0.25%, Si: 0.01 to 1.6%, Mn: 0.5 to 3.1%, P: 0.001-0.10%, Al: 0.01-0.8%, balance Fe and unavoidable impurities may be included. It is noted that the content of each component described below is based on weight unless otherwise specified.
- Carbon is a very useful element to improve the strength of steel and to secure the composite structure of ferrite and martensite.
- the present invention preferably contains 0.05% or more, and more preferably 0.07% or more.
- the content is excessive, the toughness and weldability of the steel may deteriorate. It is preferable to be included in 0.25% or less, and more preferably included in 0.23% or less in terms of preventing this.
- Silicon is a useful element for securing strength without lowering the ductility of steel materials. Moreover, it is an element which accelerates ferrite formation and promotes martensite formation by encouraging carbon concentration to unmorphed austenite. In order to obtain such an effect in the present invention, it is preferable to include 0.01% or more, and more preferably 0.05% or more. However, when the content is excessive, surface properties and weldability may be degraded. In terms of preventing this, it is preferably included in less than 1.6%, more preferably contained in less than 1.4%.
- Manganese not only contributes greatly to strength increase as a solid solution strengthening element, but also serves to promote the formation of a complex structure composed of ferrite and martensite. In order to obtain such an effect in the present invention, it is preferable to include 0.5% or more, and more preferably 1.2% or more. However, when the content is excessive, weldability and hot rolling property may be deteriorated. It is preferable to include 3.1% or less, and more preferably 2.9% or less in view of preventing this.
- Phosphorus is a typical solid solution strengthening element added to the steel to improve its strength.
- the content is excessive, not only the weldability is deteriorated, but also the material variation of each part of the steel may be caused due to the central segregation generated during playing. It is preferable to be included in 0.10% or less, and more preferably contained in 0.07% or less in view of preventing this.
- Aluminum is usually added for deoxidation of steel, but in the present invention it is added for ductility improvement. Moreover, aluminum serves to suppress the production of carbides formed in the osmosis process and to raise the strength. In order to obtain such an effect in the present invention, it is preferably included 0.01% or more, more preferably 0.02% or more. However, if the content is excessive, the internal oxidation during the cold-rolled annealing develops, it may interfere with the alloying during the alloying heat treatment and increase the alloying temperature excessively. It is preferable to include 0.8% or less, and more preferably 0.6% or less in view of preventing this.
- coarse AlN may be determined by reaction with Al in the steel, thereby degrading the mechanical properties of the steel. It is preferable to be included in 0.03% or less, and more preferably contained in 0.02% or less in view of preventing this.
- the rest is Fe.
- impurities which are not intended from the raw material or the surrounding environment may be inevitably mixed, and thus cannot be excluded. Since these impurities are known to those skilled in the art, not all of them are specifically mentioned in the present specification.
- a representative example of such impurities may be S. Since the ductility may deteriorate when the content of S in the base iron increases, it is preferable to manage the content to 0.03% or less.
- the base iron is Cr: 0.9% or less (excluding 0%), B: 0.004% or less (excluding 0%), Mo: 0.1% or less ( 0%), Co: 1.0% or less (excluding 0%), Ti: 0.2% or less (excluding 0%) and Nb: 0.2% or less (excluding 0%) may further include one or more selected. have.
- Chromium serves to improve the strength of the steel and improve the hardenability. However, when the content is excessive, not only the effect is saturated, but also the ductility of the steel may deteriorate. It is preferable to include 0.9% or less, and more preferably 0.8% or less in view of preventing this.
- Boron is a grain boundary strengthening element, which improves fatigue characteristics of spot welds, prevents grain boundary brittleness due to phosphorus, and delays transformation of austenite into pearlite during cooling during annealing.
- the content is excessive, not only the workability of the steel is deteriorated, but also the boron is excessively concentrated on the surface thereof, which may cause plating adhesion deterioration. It is preferable to be included in 0.004% or less, and more preferably contained in 0.003% or less in terms of preventing this.
- Molybdenum serves to improve the secondary workability and plating resistance.
- the content is more than 0.1% the effect is saturated bar is preferably included in the present invention 0.1% or less.
- Cobalt improves the strength of the steel, and serves to improve the wettability of the molten zinc by suppressing oxide formation during high temperature annealing. However, if the content is excessive, the ductility of the steel may be rapidly deteriorated. In order to prevent this, it is preferable to include 1.0% or less, more preferably 0.5% or less.
- Titanium is a useful element for increasing strength of steels and refining grains.
- the content is excessive, not only the manufacturing cost increases but also the ductility of the ferrite may be deteriorated due to the formation of excessive precipitates.
- it is preferable to include 0.2% or less, more preferably 0.1% or less.
- Nb 0.2% or less (excluding 0%)
- Niobium like titanium, is a useful element for increasing the strength of steels and refining grains.
- the content is excessive, not only the manufacturing cost increases but also the ductility of the ferrite may be deteriorated due to the formation of excessive precipitates. In terms of preventing this, it is preferable to include 0.2% or less, more preferably 0.1% or less.
- the Zn-Al-Mg-based plating layer is formed on the surface of the base iron, and serves to prevent corrosion of the base iron in a corrosive environment.
- the composition of the Zn-Al-Mg-based plating layer is not particularly limited.
- Mg 0.5-3.5%
- Al 0.2-15%
- Mg plays a very important role in improving the corrosion resistance of the hot-dip galvanized steel and effectively prevents corrosion of the hot-dip galvanized steel by forming a dense zinc hydroxide-based corrosion product on the surface of the plated layer under a corrosive environment.
- the desired corrosion resistance in the present invention should be included at least 0.5% by weight, more preferably at least 0.9% by weight.
- Mg oxidizing dross rapidly increases on the bath surface of the plating bath, and the antioxidant effect by the addition of trace elements is offset.
- Mg should be included in an amount of 3.5% by weight or less, and more preferably, 3.2% by weight or less.
- Al suppresses the formation of Mg oxide dross in the plating bath and improves the corrosion resistance of the plated steel by forming a Zn-Al-Mg based intermetallic compound by reacting with Zn and Mg in the plating bath.
- it should be included 0.2 wt% or more, more preferably 0.9 wt% or more.
- Al should be included in an amount of 15% by weight or less, and more preferably, 12% by weight or less.
- the hot-dip galvanized steel of the present invention includes an Al thickening layer formed at the interface between the base iron and the Zn-Al-Mg-based alloy plating layer, the area ratio of the Al thickening layer is 70% or more (including 100%), more preferably , 73% or more (including 100%).
- the occupied area ratio is the ratio of the area of the Al enriched layer to the area of the base iron when the plane is assumed without considering three-dimensional bending or the like when viewed from the surface of the plated steel in the thickness direction of the base iron. Means.
- hot-dip galvanized steel sheets made of high-strength steel to which a large amount of Si and Mn are added as in the present invention are known to be inferior in plating property and plating adhesion. Therefore, the present inventors have studied in depth to solve this problem, and as a result, the plating property and plating adhesion deterioration of the hot-dip galvanized steel sheet made of high-strength steel containing a large amount of Si and Mn are formed on the surface of the base iron. It is found that the oxide is not dense at the interface between the base iron and the plated layer, and a coarse Al thickened layer is formed. Furthermore, when the occupied area ratio of the Al thickened layer is 70% or more, the Al thickened layer has fine particles. It has been found to have a form that is formed continuously, significantly improving the plating property and plating adhesion.
- Al in the Al thickening layer is preferably present in combination with a ratio close to the stoichiometric ratio of Fe and the intermetallic compound.
- most of Al is present in the form of Al 4 Fe 13 , and part of Al 5 Fe 2 . May exist.
- the sum of the content of Al and Fe contained in the Al thickening layer may be 50% by weight or more (excluding 100% by weight), 65% by weight or less (excluding 100% by weight). If the sum of the contents of Al and Fe is less than 50% by weight, the Al thickening layer may not be uniformly formed due to the impurities, or the physical bonding force between the base iron and the plating layer is weakened, so that the plating layer is not locally formed. , The plating adhesion may be reduced.
- the Al enriched layer further includes impurity elements such as O, Si, Mn, and Cr, and these impurity elements are those remaining in the annealing oxide or diffused from the ferrous iron and remain in the Al enriched layer.
- impurity elements such as O, Si, Mn, and Cr
- these impurity elements are those remaining in the annealing oxide or diffused from the ferrous iron and remain in the Al enriched layer.
- the oxide on the surface of the iron is completely reduced and extinguished, but some of them are left in the middle of or below the Al enrichment layer as small pieces of unreduced state.
- the base iron reacts with Al
- the base iron components Mn, Si, and Cr are mixed into the Al thickening layer.
- Zn, which is a main component of the plating bath, and Si, which is a trace impurity of the plating bath are also incorporated into some Al enriched layers.
- the Al enriched layer may be I or less, 0.40 or less, more preferably 0.38 or less, even more preferably 0.35 or less, as defined by Equation 1 or 2 below. Equation 1 is applied when the base iron does not contain Cr, and Equation 2 is applied when the base iron contains Cr.
- Equations 1 and 2 are conditional expressions for securing 70% or more of the occupied area ratio of the Al enriched layer, and the higher the I value, the higher the residual ratio of the annealed oxide in the Al enriched layer. On the other hand, the lower the I value is, the more advantageous it is to secure the occupancy area ratio of the Al enriched layer. Therefore, the lower limit thereof is not particularly limited in the present invention.
- a specific apparatus and method for measuring the content of oxygen and metal elements included in the Al enriched layer is not particularly limited, but may be measured using, for example, GDOES (Glow Discharge Optical Emission Spectrometry). .
- GDOES Glow Discharge Optical Emission Spectrometry
- the Al thickening layer exists at the interface between the base iron and the Zn-Al-Mg-based plating layer as described above, it is difficult to confirm the structure and the like unless the Zn-Al-Mg-based plating layer is removed.
- a zinc-based plated steel is immersed in a chromic acid solution capable of chemically dissolving only the Zn-Al-Mg-based plating layer on the upper portion thereof for 30 seconds without damaging the Al thickening layer, thereby dissolving all of the Zn-Al-Mg-based plating layer.
- the content of oxygen and metal elements included in the Al enriched layer may be measured by using GDOES (Glow Discharge Optical Emission Spectrometry).
- GDOES Gas Discharge Optical Emission Spectrometry
- standard of an Al thickened layer needs to be based on the point where Fe is observed to 0 to 84 weight% when analyzing from the surface of an analysis sample to the inside. This is because the point where the Fe content is 84% by weight or more can be seen as the Al enriched layer area because it is affected by the small iron.
- the base iron may include an internal oxide layer formed directly below the surface thereof
- the average thickness (nm) of the internal oxide layer is preferably 100 ⁇ [Si] / [Mn] or more.
- the thicker the average thickness (nm) of the internal oxide layer is advantageous in reducing the content of Si in the annealed oxide on the steel surface, but the upper limit thereof is not particularly limited in the present invention, but if the thickness is too thick, Al, An element such as Mg penetrates deep into the steel surface along the internal oxide while reducing the internal oxide, whereby cracking defects may occur.
- the upper limit may be limited to 1,500 nm, preferably 1,450 nm.
- the type of the oxide constituting the internal oxide layer is not particularly limited, but for example, the internal oxide layer may include Si-only oxide and Si-Mn composite oxide.
- the ratio of the Si content to the Mn content contained in the internal oxide layer of Si and Mn is a, the ratio of the Si content to the Mn content contained in the iron, except for the internal oxide layer of Si and Mn
- b / a> 1 may be satisfied.
- the b / a value is controlled to exceed 1, it may be advantageous to secure the desired I value.
- the high strength hot dip galvanized steel of the present invention described above can be produced by various methods, the production method is not particularly limited. However, it can be manufactured by the following method as an embodiment.
- the base iron may be a cold rolled steel sheet, in this case, the surface roughness (Ra) of the cold rolled steel sheet is preferably 2.0 ⁇ m or less.
- the surface roughness of the base iron before plating not only the surface area increases, but also the dislocation density increases to form an oxide that is unfavorable to the surface reaction during hot dip plating, thereby forming the desired Al enriched layer. Can be disadvantageous.
- the lower limit thereof is not particularly limited in the present invention, but when the surface roughness of the base iron is too low, it is difficult to operate due to the sliding phenomenon of the steel during rolling. Since it may be disturbed, the lower limit can be limited to 0.3 ⁇ m in terms of preventing this.
- an annealing heat treatment of the base iron is performed by the ferrous iron structure to recover recrystallization.
- Such annealing heat treatment may be performed at a temperature of 760 ° C. to 850 ° C., which is sufficient to recover the recrystallization.
- control of the dew point temperature is important for forming the desired Al thickened layer.
- the dew point temperature is controlled at -60 to -10 deg. If, because the dew point temperature to form a more stable oxides SiO 2 dense oxide film on the steel surface carrying the case less than -60 °C, and the growth speed is fast generation of MnO in oxides does not occur well. In this case, the subsequent melting process Reduction and decomposition of the oxide film during the plating is less likely to occur, it is difficult to form the target Al thickened layer.
- the dew point temperature during the annealing heat treatment is more preferably controlled at -40 to -10 ° C. It is more preferable to manage at -30 ⁇ -15 ⁇ ⁇ . This is to reduce the Si content in the annealed oxide by forming an internal oxide layer of a suitable thickness.
- the annealing heat treatment may be performed in an atmosphere of hydrogen gas and residual nitrogen gas of 3 to 30% by volume. If the hydrogen gas is less than 3% by volume, it may be difficult to effectively suppress the surface oxide. On the other hand, when the hydrogen gas exceeds 30% by volume, the cost of increasing the hydrogen content increases and the risk of explosion is excessive. Will increase.
- the annealing heat-treated base iron is immersed in a Zn-Al-Mg system plating bath, and plating is performed to obtain a high strength hot dip galvanized steel.
- a specific method for obtaining a high strength hot dip galvanized steel is not particularly limited, but the following method may be used to further maximize the effect of the present invention.
- the oxides such as Si and Mn formed on the surface of the base iron in the annealing process are smoothly decomposed during the plating process, and the Al enriched layer is uniformly formed on the surface of the base iron, the plating bath temperature And management of surface temperature of the base iron introduced into the plating bath, dross defects formed on the surface of the plating bath, or the like.
- the temperature of the plating bath is preferably maintained at 430 ° C or higher, and more preferably at 440 ° C or higher.
- the higher the temperature of the plating bath has an advantageous side to the plating characteristics, but if the temperature is too high may cause the oxidation of Mg from the surface of the plating bath and the problem that the outer wall of the plating port is eroded from the plating bath. .
- the temperature of the plating bath is preferably maintained at 470 ° C. or lower, and preferably maintained at 460 ° C. or lower.
- the surface temperature of the base iron introduced into the plating bath should be equal to or higher than the plating bath temperature in terms of decomposition of surface oxides and Al concentration. Particularly, in order to maximize the effect of the present invention, it is preferable to control the surface temperature of the ferrous iron introduced into the plating bath to 5 ° C or more relative to the plating bath temperature, and more preferably to control it to 15 ° C or more relative to the plating bath temperature. .
- the upper limit of the temperature may be compared with the plating bath temperature. It is preferable to control so that it may not be 30 degreeC or more, and it is more preferable to control so that it may not be 20 degreeC or more with respect to plating bath temperature.
- the plating bath has dross defects mixed in the solid phase.
- the surface of the plating bath has a dross containing a MgZn 2 component as a floating dross floating on the surface of the plating bath due to Al and Mg oxides and a cooling effect. Not only the defect but also the Al concentration layer formed at the interface between the plated layer and the base iron interferes.
- a sealing box is installed at a position where the ferrous iron introduced into the plating bath is drawn out of the plating bath. Can be.
- FIG. 3 is a schematic diagram schematically showing a hot dip plating apparatus in which a sealing box is installed.
- the sealing box (sealing box) may be formed on the surface of the plating bath of the base iron is drawn out of the plating bath, the supply box for supplying the inert gas on one side of the sealing box (sealing box) It may be connected.
- the distance d between the base steel and the sealing box needs to be limited to 5 to 100 cm. If the separation distance is less than 5 cm, there is a risk that the plating liquid may spring up due to the atmosphere instability caused by the vibration of the small steel and the movement of the small steel in a narrow space, causing plating defects. This is because it may increase excessively.
- the steel After preparing a steel having a composition (% by weight) of Table 1, the steel was processed into a 1.5 mm thick cold rolled steel sheet. Thereafter, annealing was performed for 40 seconds at a temperature of up to 780 ° C. under a nitrogen gas atmosphere containing 5% by volume of hydrogen, and immersed in a zinc-based plating bath having the composition shown in Table 2 to obtain a plated steel material. At this time, the temperature of the zinc plating bath was made constant at 450 degreeC.
- plating appearance grade and plating adhesion for each of the plated steels were evaluated and shown in Table 2 below. Specific evaluation criteria of plating appearance grade and plating adhesion are as follows.
- the grade is divided based on the area where plating non-uniformity occurs or unplated. If there are no recognized defects, there are non-uniform defects of 1st grade and less than 3 area%. Grade 4, if non-uniform defects of less than 30 area% occurred, grade 4, non-uniformity or unplated defects of more than 30 area% were divided into 5 grades.
- the occupied area ratio of the Al enriched layer was controlled to 70% or more, and accordingly, the plating property and the plating adhesion were excellent. can confirm.
- FIG. 1 is a SEM (Scanning Electron Microscope) image of observing an interfacial layer of a hot dip galvanized steel according to Inventive Example 7, and FIG. 2 is an SEM of an interfacial layer of a hot dip galvanized steel according to Comparative Example 5 (Scanning Electron Microscope) image.
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Abstract
Description
Claims (18)
- Si: 0.01~1.6중량% 및 Mn: 1.2~3.1중량%를 포함하는 소지철;Zn-Al-Mg계 합금 도금층; 및상기 소지철 및 상기 Zn-Al-Mg계 합금 도금층 계면에 형성된 Al 농화층을 포함하고,상기 Al 농화층의 점유 면적율은 70% 이상(100% 포함)인 고강도 용융 아연계 도금 강재.
- 제1항에 있어서,상기 Al 농화층은 하기 식 1로 정의되는 I가 0.40 이하인 고강도 용융 아연계 도금 강재.[식 1] I = [O]/{[Si]+[Mn]+[Fe]}(여기서, [O]. [Si], [Mn] 및 [Fe] 각각은 Al 농화층에 포함된 해당 원소의 함량(중량%)을 의미함)
- 제1항에 있어서,상기 소지철은 Cr: 0.9중량% 이하(0중량% 제외)을 더 포함하고,상기 Al 농화층은 하기 식 2로 정의되는 I가 0.40 이하인 고강도 용융 아연계 도금 강재.[식 2] I = [O]/{[Si]+[Mn]+[Cr]+[Fe]}(여기서, [O]. [Si], [Mn], [Cr] 및 [Fe] 각각은 Al 농화층에 포함된 해당 원소의 함량(중량%)을 의미함)
- 제1항에 있어서,상기 Al 농화층에 포함된 Al 및 Fe의 함량의 합은 50중량% 이상(100중량% 제외)인 고강도 용융 아연계 도금 강재.
- 제1항에 있어서,상기 소지철은, 중량%로, C: 0.05~0.25%, Si: 0.01~1.6%, Mn: 0.5~3.1%, P: 0.001~0.10%, Al: 0.01~0.8%, N: 0.001~0.03%, 잔부 Fe 및 불가피한 불순물을 포함하는 고강도 용융 아연계 도금 강재.
- 제5항에 있어서,상기 소지철은, 중량%로, Cr: 0.9% 이하(0% 제외), B: 0.004% 이하(0% 제외), Mo: 0.1% 이하(0% 제외), Co: 1.0% 이하(0% 제외), Ti: 0.2% 이하(0% 제외) 및 Nb: 0.2% 이하(0% 제외)로 이루어진 군으로부터 선택된 1종 이상을 더 포함하는 고강도 용융 아연계 도금 강재.
- 제1항에 있어서,상기 Zn-Al-Mg계 합금 도금층은, 중량%로, Al: 0.2~15%, Mg: 0.5~3.5%, 잔부 Zn 및 불가피한 불순물을 포함하는 고강도 용융 아연계 도금 강재.
- 제1항에 있어서,상기 소지철에 포함된 Mn의 함량에 대한 Si의 함량의 비([Si]/[Mn])가 0.3 이상이고, 상기 소지철은 그 표면 직하에 형성된 내부 산화물층을 포함하며, 상기 내부 산화물층의 평균 두께(nm)는 100×[Si]/[Mn] 이상인 고강도 용융 아연계 도금 강재.
- 제8항에 있어서,상기 내부 산화물층의 평균 두께는 1,500nm 이하인 고강도 용융 아연계 도금 강재.
- 제8항에 있어서,상기 내부 산화물층은 Si 단독 산화물 및 Si-Mn 복합 산화물을 포함하는 고강도 용융 아연계 도금 강재.
- 제8항에 있어서,상기 Si 및 Mn의 내부 산화물층에 함유된 Mn 함량에 대한 Si 함량의 비를 a, 상기 Si 및 Mn의 내부 산화물층을 제외한 소지철에 함유된 Mn 함량에 대한 Si 함량의 비를 b라 할 때, b/a>1을 만족하는 고강도 용융 아연계 도금 강재.
- Si: 0.01~1.6중량% 및 Mn: 1.2~3.1중량%를 포함하는 소지철을 준비하는 단계;상기 소지철을 이슬점 온도 -60~-10℃의 조건 하 760~850℃의 온도에서 소둔 열처리하는 단계; 및상기 소둔 열처리된 소지철을 Zn-Al-Mg계 도금욕에 침지하고, 도금을 행하여 고강도 용융 아연계 도금 강재를 얻는 단계;를 포함하는 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 소지철은 냉연강판이고, 상기 냉연강판의 표면 조도(Ra)는 2.0μm 이하인 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 소지철에 포함된 Mn의 함량에 대한 Si의 함량의 비([Si]/[Mn])가 0.3 이상이고,상기 소둔 열처리시 이슬점 온도는 -40~-10℃인 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 소둔 열처리는 3~30부피%의 수소 가스 및 잔부 질소 가스 분위기에서 행하는 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 Zn-Al-Mg계 도금욕의 온도는 430~470℃인 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 Zn-Al-Mg계 도금욕에 침지되는 소지철의 표면 온도는 상기 Zn-Al-Mg계 도금욕의 온도 대비 5℃ 이상 내지 30℃ 이하인 고강도 용융 아연계 도금 강재의 제조방법.
- 제12항에 있어서,상기 Zn-Al-Mg계 도금욕의 표면 분위기는 3부피% 이하(0부피% 포함)의 산소 및 잔부 불활성 가스 분위기인 고강도 용융 아연계 도금 강재의 제조방법.
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2021508777A (ja) * | 2017-12-26 | 2021-03-11 | ポスコPosco | 表面品質及び耐食性に優れた亜鉛合金めっき鋼材及びその製造方法 |
JP2022509656A (ja) * | 2018-11-29 | 2022-01-21 | ポスコ | 表面外観及び低温接合脆性に優れた溶融亜鉛メッキ鋼板 |
EP3733918B1 (en) | 2017-12-26 | 2022-08-31 | Posco | Zinc alloy plated steel material having excellent corrosion resistance after being processed and method for manufacturing same |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101758529B1 (ko) * | 2014-12-24 | 2017-07-17 | 주식회사 포스코 | 인산염 처리성과 스폿 용접성이 우수한 아연합금도금강판 및 그 제조방법 |
KR102119970B1 (ko) * | 2018-11-14 | 2020-06-05 | 주식회사 포스코 | 표면품질과 연속생산성이 우수한 고강도 냉연강판과 이의 제조방법 |
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KR102453006B1 (ko) * | 2020-12-18 | 2022-10-12 | 주식회사 포스코 | 도금성이 우수한 고강도 용융아연도금강판 및 그 제조방법 |
CN113025937B (zh) * | 2021-02-07 | 2023-03-17 | 首钢集团有限公司 | 一种热浸镀锌钢板及其制备方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101115816B1 (ko) * | 2010-12-29 | 2012-03-09 | 주식회사 포스코 | 표면특성이 우수한 열간 프레스용 고망간 아연도금강판 및 이를 이용한 열간 프레스 성형부품 |
KR20120041619A (ko) * | 2010-10-21 | 2012-05-02 | 주식회사 포스코 | 도금성 및 밀착성이 우수한 용융아연 도금강판 및 그 제조방법 |
KR101324836B1 (ko) * | 2008-10-01 | 2013-11-01 | 신닛테츠스미킨 카부시키카이샤 | 용융 도금 강판의 제조 방법 및 용융 도금 장치 |
KR20150075323A (ko) * | 2013-12-25 | 2015-07-03 | 주식회사 포스코 | 도금 밀착성이 우수한 용융아연도금강판 및 그 제조방법 |
KR101569505B1 (ko) * | 2014-12-24 | 2015-11-30 | 주식회사 포스코 | 내박리성이 우수한 hpf 성형부재 및 그 제조방법 |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH04318157A (ja) * | 1991-04-16 | 1992-11-09 | Nippon Steel Corp | 難めっき性鋼板の溶融金属めっき法 |
US6398884B1 (en) * | 1999-02-25 | 2002-06-04 | Kawasaki Steel Corporation | Methods of producing steel plate, hot-dip steel plate and alloyed hot-dip steel plate |
JP3675419B2 (ja) * | 2002-03-25 | 2005-07-27 | 住友金属工業株式会社 | 溶融Zn−Al−Mg合金めっき鋼板と成形加工品 |
JP5098190B2 (ja) * | 2006-03-08 | 2012-12-12 | Jfeスチール株式会社 | 高強度溶融亜鉛系めっき鋼板の製造方法 |
EP3421634A1 (en) | 2007-02-23 | 2019-01-02 | Tata Steel IJmuiden B.V. | Cold rolled and continuously annealed high strength steel strip and method for producing said steel |
JP2010126757A (ja) * | 2008-11-27 | 2010-06-10 | Jfe Steel Corp | 高強度溶融亜鉛めっき鋼板およびその製造方法 |
JP5593771B2 (ja) * | 2009-03-31 | 2014-09-24 | Jfeスチール株式会社 | 高強度溶融亜鉛めっき鋼板の製造方法 |
JP5206705B2 (ja) * | 2009-03-31 | 2013-06-12 | Jfeスチール株式会社 | 高強度溶融亜鉛めっき鋼板およびその製造方法 |
CN102482753B (zh) | 2009-08-31 | 2014-08-06 | 新日铁住金株式会社 | 高强度热浸镀锌钢板及其制造方法 |
CN104388870B (zh) * | 2009-12-29 | 2017-04-12 | Posco公司 | 一种热压模塑部件 |
DE102010017354A1 (de) * | 2010-06-14 | 2011-12-15 | Thyssenkrupp Steel Europe Ag | Verfahren zum Herstellen eines warmgeformten und gehärteten, mit einer metallischen Korrosionsschutzbeschichtung überzogenen Stahlbauteils aus einem Stahlflachprodukt |
US9234267B2 (en) | 2010-11-26 | 2016-01-12 | Jfe Steel Corporation | Hot-dip Al—Zn coated steel sheet |
WO2013002575A2 (ko) * | 2011-06-28 | 2013-01-03 | 주식회사 포스코 | 도금층의 안정성이 우수한 열간 프레스 성형용 도금강판 |
PT2834383T (pt) | 2012-04-05 | 2021-09-29 | Tata Steel Ijmuiden Bv | Tira de aço com um baixo teor de si |
KR101417304B1 (ko) | 2012-07-23 | 2014-07-08 | 주식회사 포스코 | 내식성 및 표면외관이 우수한 용융아연합금 도금강판 및 그 제조방법 |
KR101528008B1 (ko) | 2012-10-23 | 2015-06-10 | 주식회사 포스코 | 표면품질 및 도금밀착성이 우수한 용융아연도금강판 및 이의 제조방법 |
JP5907055B2 (ja) * | 2012-12-14 | 2016-04-20 | Jfeスチール株式会社 | 溶融亜鉛めっき鋼板 |
JP5826321B2 (ja) * | 2013-03-27 | 2015-12-02 | 日新製鋼株式会社 | めっき密着性に優れた溶融亜鉛系めっき鋼板の製造方法 |
JP5850005B2 (ja) * | 2013-08-12 | 2016-02-03 | Jfeスチール株式会社 | 溶融亜鉛系めっき用鋼板の製造方法 |
CN104419867B (zh) | 2013-09-05 | 2016-09-07 | 鞍钢股份有限公司 | 1250MPa级超高强锌铝镁镀层钢板及其生产方法 |
KR101639843B1 (ko) | 2013-12-24 | 2016-07-14 | 주식회사 포스코 | 열간 프레스 성형용 도금강판 및 그 제조방법 |
-
2015
- 2015-12-24 KR KR1020150186561A patent/KR102075182B1/ko active IP Right Grant
-
2016
- 2016-12-21 US US16/064,757 patent/US11306381B2/en active Active
- 2016-12-21 CN CN201680076292.4A patent/CN108474095B/zh active Active
- 2016-12-21 JP JP2018532627A patent/JP6727305B2/ja active Active
- 2016-12-21 EP EP16879316.4A patent/EP3396007A1/en active Pending
- 2016-12-21 WO PCT/KR2016/014983 patent/WO2017111449A1/ko active Application Filing
-
2022
- 2022-03-15 US US17/694,942 patent/US11692259B2/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101324836B1 (ko) * | 2008-10-01 | 2013-11-01 | 신닛테츠스미킨 카부시키카이샤 | 용융 도금 강판의 제조 방법 및 용융 도금 장치 |
KR20120041619A (ko) * | 2010-10-21 | 2012-05-02 | 주식회사 포스코 | 도금성 및 밀착성이 우수한 용융아연 도금강판 및 그 제조방법 |
KR101115816B1 (ko) * | 2010-12-29 | 2012-03-09 | 주식회사 포스코 | 표면특성이 우수한 열간 프레스용 고망간 아연도금강판 및 이를 이용한 열간 프레스 성형부품 |
KR20150075323A (ko) * | 2013-12-25 | 2015-07-03 | 주식회사 포스코 | 도금 밀착성이 우수한 용융아연도금강판 및 그 제조방법 |
KR101569505B1 (ko) * | 2014-12-24 | 2015-11-30 | 주식회사 포스코 | 내박리성이 우수한 hpf 성형부재 및 그 제조방법 |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2021508777A (ja) * | 2017-12-26 | 2021-03-11 | ポスコPosco | 表面品質及び耐食性に優れた亜鉛合金めっき鋼材及びその製造方法 |
US11332816B2 (en) | 2017-12-26 | 2022-05-17 | Posco | Zinc alloy plated steel material having excellent surface quality and corrosion resistance |
EP3733918B1 (en) | 2017-12-26 | 2022-08-31 | Posco | Zinc alloy plated steel material having excellent corrosion resistance after being processed and method for manufacturing same |
US11643714B2 (en) | 2017-12-26 | 2023-05-09 | Posco Co., Ltd | Method for manufacturing zinc alloy plated steel material having excellent surface quality and corrosion resistance |
JP2022509656A (ja) * | 2018-11-29 | 2022-01-21 | ポスコ | 表面外観及び低温接合脆性に優れた溶融亜鉛メッキ鋼板 |
JP7244727B2 (ja) | 2018-11-29 | 2023-03-23 | ポスコ カンパニー リミテッド | 表面外観及び低温接合脆性に優れた溶融亜鉛メッキ鋼板 |
US11801665B2 (en) | 2018-11-29 | 2023-10-31 | Posco Co., Ltd | Hot-dip galvanized steel sheet having excellent surface appearance and low-temperature bonding brittleness |
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