WO2022139278A1 - Qt열처리된 고탄소 열연강판, 고탄소 냉연강판, qt열처리된 고탄소 냉연강판 및 이들의 제조방법 - Google Patents
Qt열처리된 고탄소 열연강판, 고탄소 냉연강판, qt열처리된 고탄소 냉연강판 및 이들의 제조방법 Download PDFInfo
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 105
- 239000010959 steel Substances 0.000 title claims abstract description 105
- 229910052799 carbon Inorganic materials 0.000 title claims abstract description 74
- 239000010960 cold rolled steel Substances 0.000 title claims abstract description 66
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 title abstract description 18
- 239000012535 impurity Substances 0.000 claims abstract description 17
- 229910052721 tungsten Inorganic materials 0.000 claims abstract description 15
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 13
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 13
- 238000000034 method Methods 0.000 claims description 45
- 238000010438 heat treatment Methods 0.000 claims description 33
- 229910001562 pearlite Inorganic materials 0.000 claims description 26
- 238000001816 cooling Methods 0.000 claims description 24
- 229910000734 martensite Inorganic materials 0.000 claims description 23
- 238000003303 reheating Methods 0.000 claims description 23
- 229910001567 cementite Inorganic materials 0.000 claims description 21
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims description 20
- 229910000859 α-Fe Inorganic materials 0.000 claims description 19
- 238000005097 cold rolling Methods 0.000 claims description 18
- 238000000137 annealing Methods 0.000 claims description 16
- 238000005496 tempering Methods 0.000 claims description 14
- 229910001563 bainite Inorganic materials 0.000 claims description 12
- 238000005098 hot rolling Methods 0.000 claims description 12
- 229910052720 vanadium Inorganic materials 0.000 claims description 6
- 150000001247 metal acetylides Chemical class 0.000 abstract description 7
- 230000000052 comparative effect Effects 0.000 description 18
- 238000005299 abrasion Methods 0.000 description 16
- 230000000694 effects Effects 0.000 description 16
- 229910001566 austenite Inorganic materials 0.000 description 12
- 239000000203 mixture Substances 0.000 description 12
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- 239000000463 material Substances 0.000 description 8
- 230000003647 oxidation Effects 0.000 description 6
- 238000007254 oxidation reaction Methods 0.000 description 6
- 230000000717 retained effect Effects 0.000 description 6
- 230000009466 transformation Effects 0.000 description 5
- 230000003749 cleanliness Effects 0.000 description 4
- 239000006104 solid solution Substances 0.000 description 4
- 229910000677 High-carbon steel Inorganic materials 0.000 description 3
- 230000032683 aging Effects 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- 239000011159 matrix material Substances 0.000 description 3
- 229910052758 niobium Inorganic materials 0.000 description 3
- 239000002436 steel type Substances 0.000 description 3
- 238000009628 steelmaking Methods 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 229910052750 molybdenum Inorganic materials 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000003009 desulfurizing effect Effects 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000445 field-emission scanning electron microscopy Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
-
- 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
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/18—Hardening; Quenching with or without subsequent tempering
- C21D1/25—Hardening, combined with annealing between 300 degrees Celsius and 600 degrees Celsius, i.e. heat refining ("Vergüten")
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
- C21D1/32—Soft annealing, e.g. spheroidising
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- 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
- C21D8/0205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips of ferrous alloys
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—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
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
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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
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
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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
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/24—Ferrous alloys, e.g. steel alloys containing chromium with vanadium
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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
- C22C38/26—Ferrous alloys, e.g. steel alloys containing chromium with niobium or tantalum
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/003—Cementite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/009—Pearlite
Definitions
- the present invention relates to a QT heat-treated high-carbon hot-rolled steel sheet, a high-carbon cold-rolled steel sheet, a QT heat-treated high-carbon cold-rolled steel sheet, and a manufacturing method thereof.
- High carbon steel refers to steel containing 0.3% or more of carbon or about 0.15% of carbon and other alloying elements. In general, as the carbon content increases, the hardness and strength of steel increase, so carbon is used as the most economical and effective element to control the physical properties of steel.
- steel types are classified according to the carbon content, and the steel type having the highest carbon content among steel types currently produced in converters is SK120, and the carbon content of SK120 is 1.15 to 1.25%.
- the SK120 can obtain higher hardness by phase transformation of the microstructure into martensite through rapid cooling heat treatment at a high temperature in the austenite single phase region.
- reheating is performed in the austenite region to secure toughness, and then tempering is performed.
- this series of heat treatment process is called QT (Quenching-Tempering).
- SK120 contains 1.15 to 1.25% of C, it has excellent hardness and toughness after QT heat treatment, but has a disadvantage in that it has low wear resistance because it is composed of a single tempered martensite phase.
- cementite has a hardness of 1300 Hv, and there is no significant difference in hardness from tempered martensite, which is a base material, so it is difficult to expect excellent wear resistance.
- cementite is all dissolved in the reheating temperature section during the QT heat treatment process, there is a disadvantage that a high degree of heat treatment technology is required.
- One aspect of the present invention is to provide a QT heat-treated high-carbon hot-rolled steel sheet, a high-carbon cold-rolled steel sheet, a QT heat-treated high carbon cold-rolled steel sheet, and a manufacturing method thereof.
- One embodiment of the present invention by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03% or less, S: 0.03% or less, Al: 0.02% or less, the balance contains Fe and other unavoidable impurities, the microstructure is area%, carbide: 0.1-20%, the balance includes tempered martensite, the carbide is To provide a high carbon hot-rolled steel sheet subjected to QT heat treatment with an average size of 0.1 to 20 ⁇ m.
- Another embodiment of the present invention is by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03% or less, S: 0.03% or less, Al: 0.02% or less, the balance Fe and other unavoidable impurities are included, and the microstructure is by area%, ferrite: 20 to 99.9%, cementite: 10% or less, pearlite: 50% or less, and Carbide: Contains 0.1 to 20%, and the carbide provides a high-carbon cold-rolled steel sheet having an average size of 0.1 to 20 ⁇ m.
- Another embodiment of the present invention is by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03 % or less, S: 0.03% or less, Al: 0.02% or less, the balance contains Fe and other unavoidable impurities, and the microstructure is area%, carbide: 0.1-20%, the balance includes tempered martensite, the carbide provides a high-carbon cold-rolled steel sheet subjected to QT heat treatment with an average size of 0.1 to 20 ⁇ m.
- Another embodiment of the present invention is by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03 % or less, S: 0.03% or less, Al: 0.02% or less, the remainder of preparing a hot-rolled steel sheet containing Fe and other unavoidable impurities; reheating the prepared hot-rolled steel sheet at 740 to 1100°C; cooling the reheated hot-rolled steel sheet at a cooling rate of 10° C./s or more; and tempering the cooled hot-rolled steel sheet at 150 to 600°C.
- Another embodiment of the present invention is by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03 % or less, S: 0.03% or less, Al: 0.02% or less, the remainder of preparing a hot-rolled steel sheet containing Fe and other unavoidable impurities; and cold-rolling the prepared hot-rolled steel sheet to obtain a cold-rolled steel sheet.
- Another embodiment of the present invention is by weight%, C: 1.0 to 1.4%, Si: 0.1 to 0.4%, Mn: 0.1 to 0.8%, Cr: 0.3 to 11%, W: 0.05 to 2.5%, P: 0.03 % or less, S: 0.03% or less, Al: 0.02% or less, the remainder of preparing a hot-rolled steel sheet containing Fe and other unavoidable impurities; cold-rolling the prepared hot-rolled steel sheet to obtain a cold-rolled steel sheet; reheating the cold-rolled steel sheet at 740 to 1100°C; cooling the reheated cold-rolled steel sheet at a cooling rate of 10° C./s or more; and tempering the cooled cold-rolled steel sheet at 150 to 600°C.
- the high carbon steel of the present invention will be described.
- an alloy composition of the high carbon steel of the present invention will be described. Unless otherwise specified, the content of the alloy composition described below means wt%.
- C is an alloying element that has the greatest effect on improving the strength and hardness of steel.
- C is an element that stably forms austenite, and has a solid solution strengthening effect when present in a solid solution state because of its small size.
- C since C has a low solid solution limit in the ferrite structure, it meets with alloying elements that form carbides to form precipitates, or combines with Fe to form cementite (Fe3C), thereby exerting a strengthening effect. Because C has a fast diffusion rate, redistribution occurs quickly even if it is maintained at a high temperature for a short time. Therefore, it has the greatest influence on increasing the hardness of martensite, and at the same time increases the wear resistance of the steel.
- the content of C is preferably in the range of 1.0 to 1.4%.
- the lower limit of the C content is more preferably 1.05%.
- the upper limit of the C content is more preferably 1.35%, and even more preferably 1.3%.
- Si is an element that stably forms ferrite, and is dissolved in ferrite to improve strength.
- the content of Si preferably has a range of 0.1 to 0.4%.
- the upper limit of the Si content is more preferably 0.35%.
- Mn is effective in improving the cleanliness of steel as a deoxidizing and desulfurizing agent. In addition, it is added to secure hardenability in consideration of the cooling level.
- the Mn content is preferably in the range of 0.1 to 0.8%.
- the upper limit of the Mn content is more preferably 0.7%, and even more preferably 0.6%.
- Cr is a ferrite stabilizing element and is an element that is dissolved in a matrix structure to secure hardenability.
- the Cr combines with C to form a hard Cr 7 C 3 carbide, there is an effect of improving hardness and abrasion resistance.
- the content of Cr is preferably in the range of 0.3 to 11%.
- the upper limit of the Cr content is more preferably 10.5%.
- W improves wear resistance by combining with C to form a hard carbide of 2300 to 2800 Hv.
- W is added in an amount of 0.05% or more.
- the content of W is preferably in the range of 0.05 to 2.5%.
- the upper limit of the W content is more preferably 2.45% or less, and even more preferably 2.35% or less.
- P is an impurity that has not been filtered out during the steelmaking process, and when it is contained as little as possible, cleanliness and processability are improved.
- the upper limit is managed as 0.03% in consideration of economic feasibility.
- S is an impurity that has not been filtered out during the steelmaking process, and as it is contained as little as possible, cleanliness and processability are improved.
- the upper limit is managed as 0.03% in consideration of economic feasibility.
- Al is an element commonly used as a deoxidizer in the steelmaking process, and is added to ensure cleanliness. However, in the present invention, it is managed at 0.02% or less in consideration of the effect and economic feasibility.
- the remainder may include Fe and unavoidable impurities. Inevitable impurities may be unintentionally mixed in a typical steel manufacturing process, and this cannot be entirely excluded, and those skilled in the ordinary steel manufacturing field can easily understand the meaning.
- the present invention does not entirely exclude the addition of compositions other than the above-mentioned steel composition.
- the present invention in addition to the above alloy composition, V: 0.8% or less (excluding 0%), Mo: 2.5% or less (excluding 0%) and Nb: 1.5% or less (excluding 0%) selected from the group consisting of It may further include one or more types.
- V 0.8% or less (excluding 0%)
- V combines with C to form a hard carbide of about 2300 Hv to improve wear resistance.
- the content of V is preferably in the range of 0.8% or less.
- the lower limit of the V content is more preferably 0.01%, and even more preferably 0.05%.
- the upper limit of the V content is more preferably 0.7%.
- Mo is combined with C alone or in combination with elements such as V and Nb to form a hard carbide to improve wear resistance. Also, like Cr, there is an effect of improving hardenability. However, when the Mo exceeds 2.5%, there is a risk of causing brittleness due to excessive hardenability. Accordingly, the Mo content is preferably 2.5% or less. The lower limit of the Mo content is more preferably 0.1%, even more preferably 0.2%. The upper limit of the Mo content is more preferably 2.4%.
- Nb 1.5% or less (excluding 0%)
- Nb combines with C to form hard carbides, improving wear resistance.
- the precipitation temperature of Nb is high at about 1300° C., when it is added in a large amount, there is a risk of forming coarse carbides and lowering the toughness, so it is preferable to add it in an amount of 1.5% or less.
- the Nb content is preferably 1.5% or less.
- the lower limit of the Nb content is more preferably 0.05%, even more preferably 0.1%.
- the upper limit of the Nb content is more preferably 1.2%.
- the microstructure of the QT heat-treated high-carbon hot-rolled steel sheet of the present invention is preferably carbide: 0.1 to 20%, and the balance includes tempered martensite in area%.
- the present invention can secure excellent abrasion resistance as well as resistance to impact by including tempered martensite as a matrix structure.
- the present invention increases abrasion resistance by securing an appropriate fraction of carbides. If the fraction of the carbide is less than 0.1%, there is a disadvantage that it is difficult to expect abrasion resistance due to the hard carbide, and if it exceeds 20%, there is a disadvantage that the material is easily destroyed by brittleness.
- the lower limit of the carbide fraction is more preferably 0.2%, and still more preferably 0.5%.
- the upper limit of the carbide fraction is more preferably 18%, even more preferably 16%.
- the type of the carbide is not particularly limited, and for example, it may be a single or complex carbide containing at least one of W, V, Mo and Nb.
- the microstructure of the QT heat-treated high-carbon hot-rolled steel sheet of the present invention may inevitably contain at least one of ferrite, pearlite, bainite and retained austenite in a total amount of less than 10% in the manufacturing process. When the total amount of at least one of ferrite, pearlite, bainite, and retained austenite is 10% or more, hardness may decrease.
- the total amount of at least one of ferrite, pearlite, bainite and retained austenite is more preferably 7% or less, and still more preferably 5%.
- the carbide may have an average size of 0.1 to 20 ⁇ m. If the size of the carbide is less than 0.1 ⁇ m, the effect of improving the hardness is insignificant, if it exceeds 20 ⁇ m may cause brittleness of the steel.
- the lower limit of the average size of the carbide is more preferably 0.3 ⁇ m, and even more preferably 0.5 ⁇ m.
- the upper limit of the average size of the carbide is more preferably 17 ⁇ m, and even more preferably 15 ⁇ m.
- the QT heat-treated high-carbon hot-rolled steel sheet according to an embodiment of the present invention provided as described above may have a hardness of 350 Hv or more.
- the wear resistance test was performed by the ASTM G99 method, the QT heat-treated high-carbon hot-rolled steel sheet had a wear loss of 35 mg or less when the reheating temperature before QT was 800°C, and the wear loss was 27mg when the reheating temperature before QT was 850°C or less, and when the reheating temperature before QT is 900°C, the wear loss may be 25 mg or less. Through this, excellent hardness and abrasion resistance can be secured at the same time.
- the microstructure of the high carbon cold-rolled steel sheet of the present invention may include, in area%, ferrite: 20 to 99.9%, cementite: 10% or less, pearlite: 50% or less, and carbide: 0.1 to 20%.
- the lower limit of the ferrite fraction is more preferably 30%, still more preferably 40%.
- the upper limit of the ferrite fraction is more preferably 99.8%, even more preferably 99.5%. If the cementite exceeds 20%, there is a disadvantage in that it is difficult to process due to the brittleness of the material.
- the lower limit of the cementite fraction is more preferably 0.1%, even more preferably 0.3%.
- the upper limit of the cementite fraction is more preferably 8%, even more preferably 7%.
- the lower limit of the pearlite fraction is more preferably 1%, even more preferably 5%.
- the upper limit of the pearlite fraction is more preferably 40%, and even more preferably 30%. If the fraction of the carbide is less than 0.1%, there is a disadvantage that it is difficult to expect abrasion resistance due to the hard carbide, and if it exceeds 20%, there is a disadvantage that the material is easily destroyed by brittleness.
- the lower limit of the carbide fraction is more preferably 0.2%, and still more preferably 0.5%.
- the upper limit of the carbide fraction is more preferably 18%, even more preferably 16%.
- the carbide may have an average size of 0.1 to 20 ⁇ m. If the size of the carbide is less than 0.1 ⁇ m, the effect of improving the hardness is insignificant, if it exceeds 20 ⁇ m may cause brittleness of the steel.
- the lower limit of the average size of the carbide is more preferably 0.3 ⁇ m, and even more preferably 0.5 ⁇ m.
- the upper limit of the average size of the carbide is more preferably 17 ⁇ m, and even more preferably 15 ⁇ m.
- the high-carbon cold-rolled steel sheet according to an embodiment of the present invention provided as described above may have a hardness of 350 Hv or less. By securing such low hardness, high formability can be ensured, and through this, part molding, which is a post-process, can be smoothly formed.
- the microstructure of the QT heat-treated high-carbon cold-rolled steel sheet of the present invention is preferably carbide: 0.1-20%, and the balance includes tempered martensite in area%.
- the present invention can secure excellent abrasion resistance as well as resistance to impact by including tempered martensite as a matrix structure.
- the present invention increases abrasion resistance by securing an appropriate fraction of carbides. If the fraction of the carbide is less than 0.1%, there is a disadvantage that it is difficult to expect abrasion resistance due to the hard carbide, and if it exceeds 20%, there is a disadvantage that the material is easily destroyed by brittleness.
- the lower limit of the carbide fraction is more preferably 0.2%, and still more preferably 0.5%.
- the upper limit of the carbide fraction is more preferably 18%, even more preferably 16%.
- the type of the carbide is not particularly limited, and for example, it may be a single or complex carbide containing at least one of W, V, Mo and Nb.
- the microstructure of the QT heat-treated high-carbon hot-rolled steel sheet of the present invention may inevitably contain at least one of ferrite, pearlite, bainite and retained austenite in a total amount of less than 10% in the manufacturing process. When the total amount of at least one of ferrite, pearlite, bainite, and retained austenite is 10% or more, hardness may decrease.
- the total amount of at least one of ferrite, pearlite, bainite and retained austenite is more preferably 7% or less, and still more preferably 5%.
- the carbide may have an average size of 0.1 to 20 ⁇ m. If the size of the carbide is less than 0.1 ⁇ m, the effect of improving the hardness is insignificant, if it exceeds 20 ⁇ m may cause brittleness of the steel.
- the lower limit of the average size of the carbide is more preferably 0.3 ⁇ m, and even more preferably 0.5 ⁇ m.
- the upper limit of the average size of the carbide is more preferably 17 ⁇ m, and even more preferably 15 ⁇ m.
- the QT heat-treated high-carbon cold-rolled steel sheet according to an embodiment of the present invention provided as described above may have a hardness of 350 Hv or more.
- the QT heat-treated high-carbon cold-rolled steel sheet may have a wear loss of 25 mg or less when the reheating temperature before QT is 900°C. Through this, excellent hardness and abrasion resistance can be secured at the same time.
- a hot-rolled steel sheet having the above-described alloy composition is prepared.
- the step of preparing the hot-rolled steel sheet includes heating the slab at 1100 to 1300 °C; and hot rolling the heated slab at 700 to 1100°C. If the heating temperature of the slab is less than 1100 °C, it may be difficult to roll due to a low degree of aging, and if it exceeds 1300 °C, high-temperature oxidation may occur or the slab may be melted locally depending on whether there is a temperature deviation in the furnace There is this. If the hot rolling temperature is less than 700 °C, the strength of the material is high, there is a disadvantage that the hot rolling load may be large, if it exceeds 1100 °C, the surface quality may be inferior due to high temperature oxidation.
- the hot-rolled steel sheet prepared in this way may have a microstructure of at least one of pearlite, pearlite in which cementite is partially precipitated at grain boundaries, bainite, and martensite.
- the prepared hot-rolled steel sheet may have a hardness of 200Hv or more.
- the hot-rolled steel sheet is reheated at 740 to 1100°C.
- the reheating temperature of the hot-rolled steel sheet is less than 740 °C, there is a disadvantage that martensite transformation does not occur after rapid cooling because austenite cannot be secured.
- the lower limit of the reheating temperature of the hot-rolled steel sheet is more preferably 800 °C.
- the upper limit of the reheating temperature of the hot-rolled steel sheet is more preferably 1050 °C.
- the reheated hot-rolled steel sheet is cooled at a cooling rate of 10° C./s or more.
- the cooling rate is more preferably 40°C or more, more preferably 90°C/s or more, and most preferably 100°C/s or more.
- the upper limit thereof is not particularly limited. However, it may be difficult to exceed 200°C/s due to design limitations.
- the cooled hot-rolled steel sheet is tempered at 150 ⁇ 600 °C. If the tempering temperature is less than 150 °C, there is a disadvantage that the dislocation recovery is insufficient, there is no tempering effect, if it exceeds 600 °C, there is a disadvantage that phase transformation may occur.
- the lower limit of the said tempering temperature it is more preferable that it is 170 degreeC, and it is still more preferable that it is 190 degreeC.
- the upper limit of the lower limit of the tempering temperature is more preferably 500°C, even more preferably 450°C, and most preferably 380°C.
- a hot-rolled steel sheet having the above-described alloy composition is prepared.
- the step of preparing the hot-rolled steel sheet includes heating the slab at 1100 to 1300 °C; and hot rolling the heated slab at 700 to 1100°C. If the heating temperature of the slab is less than 1100 °C, it may be difficult to roll due to a low degree of aging, and if it exceeds 1300 °C, high-temperature oxidation may occur or the slab may be melted locally depending on whether there is a temperature deviation in the furnace There is this. If the hot rolling temperature is less than 700 °C, the strength of the material is high, there is a disadvantage that the hot rolling load may be large, if it exceeds 1100 °C, the surface quality may be inferior due to high temperature oxidation.
- the hot-rolled steel sheet prepared in this way may have a microstructure of at least one of pearlite, pearlite in which cementite is partially precipitated at grain boundaries, bainite, and martensite.
- the prepared hot-rolled steel sheet may have a hardness of 200Hv or more.
- the spheroidizing annealing heat treatment is intended to suppress the occurrence of defects in equipment or impossible to perform the cold rolling process due to the high strength of the hot-rolled steel sheet. That is, the spheroidizing annealing heat treatment is to reduce the strength through spheroidization of cementite having high strength, so that the cold rolling process is smoothly performed. If the spheroidizing annealing heat treatment temperature is less than 630 °C, the time required for spheroidization may be excessively long and there may be a disadvantage in that economical efficiency is lowered.
- the lower limit of the spheroidizing annealing heat treatment temperature is more preferably 650°C, and even more preferably 670°C.
- the upper limit of the spheroidizing annealing heat treatment temperature is more preferably 830 °C, even more preferably 810 °C.
- the hot-rolled steel sheet is cold-rolled to obtain a cold-rolled steel sheet.
- the cold rolling process may be performed by a method conventionally performed in the art. Therefore, in the present invention, as long as a cold-rolled steel sheet having a desired thickness can be obtained, the cold-rolling process is not particularly limited.
- the manufacturing method of the high-carbon cold-rolled steel sheet may include performing the above-mentioned spheroidizing annealing heat treatment and cold rolling process once or twice or more.
- a hot-rolled steel sheet having the above-described alloy composition is prepared.
- the step of preparing the hot-rolled steel sheet includes heating the slab at 1100 to 1300 °C; and hot rolling the heated slab at 700 to 1100°C. If the heating temperature of the slab is less than 1100 °C, it may be difficult to roll due to a low degree of aging, and if it exceeds 1300 °C, high-temperature oxidation may occur or the slab may be melted locally depending on whether there is a temperature deviation in the furnace There is this. If the hot rolling temperature is less than 700 °C, the strength of the material is high, there is a disadvantage that the hot rolling load may be large, if it exceeds 1100 °C, the surface quality may be inferior due to high temperature oxidation.
- the hot-rolled steel sheet prepared in this way may have a microstructure of at least one of pearlite, pearlite in which cementite is partially precipitated at grain boundaries, bainite, and martensite.
- the prepared hot-rolled steel sheet may have a hardness of 200Hv or more.
- the spheroidizing annealing heat treatment is intended to suppress the occurrence of defects in equipment or impossible to perform the cold rolling process due to the high strength of the hot-rolled steel sheet. That is, the spheroidizing annealing heat treatment is to reduce the strength through spheroidization of cementite having high strength, so that the cold rolling process is smoothly performed. If the spheroidizing annealing heat treatment temperature is less than 630 °C, the time required for spheroidization may be excessively long and there may be a disadvantage in that economical efficiency is lowered.
- the lower limit of the spheroidizing annealing heat treatment temperature is more preferably 650°C, and even more preferably 670°C.
- the upper limit of the spheroidizing annealing heat treatment temperature is more preferably 830 °C, even more preferably 810 °C.
- the hot-rolled steel sheet is cold-rolled to obtain a cold-rolled steel sheet.
- the cold rolling process may be performed by a method conventionally performed in the art. Therefore, in the present invention, as long as a cold-rolled steel sheet having a desired thickness can be obtained, the cold-rolling process is not particularly limited.
- the cold-rolled steel sheet is reheated at 740 to 1100°C.
- austenite cannot be secured and martensite transformation does not occur after rapid cooling.
- the lower limit of the reheating temperature of the cold-rolled steel sheet is more preferably 800 °C.
- the upper limit of the reheating temperature of the cold rolled steel sheet is more preferably 1050 °C.
- the reheated cold-rolled steel sheet is cooled at a cooling rate of 10° C./s or more.
- the cooling rate is more preferably 40°C or more, more preferably 90°C/s or more, and most preferably 100°C/s or more.
- the upper limit thereof is not particularly limited. However, it may be difficult to exceed 200°C/s due to design limitations.
- the cooled cold-rolled steel sheet is tempered at 150 ⁇ 600 °C. If the tempering temperature is less than 150 °C, there is a disadvantage that the dislocation recovery is insufficient, there is no tempering effect, if it exceeds 600 °C, there is a disadvantage that phase transformation may occur.
- the lower limit of the said tempering temperature it is more preferable that it is 170 degreeC, and it is still more preferable that it is 190 degreeC.
- the upper limit of the lower limit of the tempering temperature is more preferably 500°C, even more preferably 450°C, and most preferably 380°C.
- the slab having the alloy composition shown in Table 1 below was heated at 1200°C, and then hot-rolled at 900°C to obtain a hot-rolled steel sheet.
- the hardness of the hot-rolled steel sheet was measured and shown together in Table 1 below.
- the hot-rolled steel sheet thus obtained was reheated at 800° C., 850° C. and 900° C., respectively, cooled at a cooling rate of 80° C./s, and tempered at 200° C. to prepare a QT heat-treated hot-rolled steel sheet.
- the fraction of microstructure was calculated using ThermoCalc software based on thermodynamic properties.
- the size of the carbide was observed using an FE-SEM scanning electron microscope. Specifically, the specimen was polished to #400 ⁇ #2000 using sandpaper, then final polishing was performed with a 1 ⁇ m diamond abrasive, treated with 2% nital etchant, and then observed using an image analysis program. .
- Hardness was measured using a Vickers hardness tester. At this time, the average value was calculated by repeating the test 5 times with a measurement load of 10 kg.
- Ball-on-disk test was performed according to ASTM G99 method to evaluate abrasion resistance. At this time, the test was conducted by rubbing a test piece processed in the form of a disk with a diameter of 31mm and a thickness of 5mm and a SiC ball with a diameter of 12.7mm at room temperature for 3600 seconds at a force of 50N and a speed of 1000rpm. proceeded Abrasion resistance was expressed as a value obtained by subtracting the weight after abrasion from the weight before abrasion of the test piece, that is, the amount of wear loss.
- the present invention has excellent hardness and wear resistance by securing the microstructure and carbide size to be obtained. Able to know.
- the slab having the alloy composition of Table 1 described in Example 1 was heated at 1200°C, and then hot rolled at 900°C to obtain a hot-rolled steel sheet, and the hot-rolled steel sheet was subjected to spheroidal annealing heat treatment at 770°C, followed by cold rolling. A cold rolled steel sheet was manufactured. In addition, the cold-rolled steel sheet was reheated at 900°C, cooled at a cooling rate of 40°C/s, and then tempered at 210°C to prepare a QT heat-treated cold-rolled steel sheet.
- Microstructure, hardness and abrasion resistance were measured using the same method as in Example 1.
- the present invention has excellent hardness and wear resistance as it secures the desired microstructure and carbide size. Able to know.
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Abstract
Description
구분 | 합금조성(중량%) | 경도 (Hv) |
|||||||||
C | Si | Mn | P | S | Cr | W | V | Mo | Nb | ||
종래강 (SK120) |
1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.45 | - | - | - | - | 324 |
비교강1 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.45 | 0.02 | - | - | - | 345 |
발명강1 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.45 | 0.5 | - | - | - | 352 |
발명강2 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.45 | 1.4 | - | - | - | 455 |
발명강3 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.45 | 2.3 | - | - | - | 423 |
발명강4 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 10 | 0.5 | - | - | - | 546 |
발명강5 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.15 | - | - | 462 |
발명강6 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.3 | - | - | 443 |
발명강7 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.6 | - | - | 484 |
비교강2 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | - | 0.6 | - | - | 487 |
발명강8 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | - | 0.5 | - | 432 |
발명강9 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | - | 1 | - | 465 |
발명강10 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | - | 2 | - | 520 |
비교강3 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | - | - | 2 | - | 518 |
발명강11 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | - | - | 0.5 | 346 |
발명강12 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | - | - | 1 | 354 |
발명강13 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.15 | 1.5 | - | 501 |
발명강14 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.3 | 1 | - | 495 |
비교강4 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | - | 0.5 | 1.2 | - | 508 |
발명강15 | 1.2 | 0.25 | 0.3 | 0.008 | 0.001 | 0.55 | 0.5 | 0.3 | - | 0.5 | 365 |
구분 | QT열처리된 열연강판 미세조직 |
경도(Hv) | 마모감량(mg) | ||||||
템퍼드 마르텐사이트 (면적%) |
탄화물 (면적%) |
탄화물 크기 (㎛) |
800℃ | 850℃ | 900℃ | 800℃ | 850℃ | 900℃ | |
종래강 (SK120) |
100.0 | 0 | - | 387 | 449 | 733 | 38.5 | 31.2 | 26.8 |
비교강1 | 100.0 | 0 | - | 390 | 453 | 760 | 36.2 | 34.1 | 26.5 |
발명강1 | 99.86 | 0.14 | 5 | 478 | 703 | 878 | 33.3 | 26.4 | 21.8 |
발명강2 | 99.4 | 0.6 | 6 | 819 | 902 | 879 | 26.7 | 21.3 | 21.7 |
발명강3 | 98.9 | 1.1 | 8 | 832 | 916 | 968 | 27 | 21.5 | 20.4 |
발명강4 | 85.9 | 14.1 | 5 | 556 | 819 | 823 | 34.8 | 22.9 | 23.1 |
발명강5 | 99.6 | 0.4 | 3 | 503 | 845 | 942 | 32.5 | 24.8 | 23.7 |
발명강6 | 99.3 | 0.7 | 7 | 558 | 859 | 922 | 29.3 | 21.5 | 23.9 |
발명강7 | 98.6 | 1.4 | 10 | 521 | 882 | 949 | 30.1 | 21.9 | 20.5 |
비교강2 | 98.7 | 1.3 | 0.05 | 466 | 720 | 934 | 40 | 30 | 25.7 |
발명강8 | 99.54 | 0.46 | 0.5 | 958 | 1004 | 949 | 22.6 | 21 | 23.8 |
발명강9 | 98.5 | 1.5 | 6 | 909 | 939 | 892 | 22.8 | 23.2 | 22.6 |
발명강10 | 95.1 | 4.9 | 10 | 983 | 957 | 886 | 25.3 | 26.6 | 22.2 |
비교강3 | 95.3 | 4.7 | 0.03 | 965 | 944 | 857 | 35 | 27.5 | 25.3 |
발명강11 | 99.3 | 0.7 | 8 | 633 | 935 | 948 | 27.3 | 21 | 20.9 |
발명강12 | 98.6 | 1.4 | 10 | 745 | 912 | 916 | 25.4 | 21 | 21.4 |
발명강13 | 97.0 | 3 | 0.5 | 1027 | 1008 | 938 | 19.2 | 21.8 | 24.3 |
발명강14 | 98.4 | 1.6 | 1 | 993 | 995 | 961 | 22.8 | 22.4 | 20.3 |
비교강4 | 97.9 | 2.1 | 0.05 | 1009 | 986 | 906 | 36.5 | 28 | 25 |
발명강15 | 98.7 | 1.3 | 5 | 777 | 935 | 943 | 25 | 22.2 | 20.1 |
구분 | 냉연강판 미세조직 | 경도 (Hv) |
|||
페라이트(면적%) | 시멘타이트(면적%) | 탄화물(면적%) | 탄화물크기(㎛) | ||
종래강 (SK120) |
94.11 | 5.9 | 0 | - | 230 |
비교강1 | 94.09 | 5.9 | 0 | - | 238 |
발명강1 | 94.33 | 5.7 | 0.14 | 5 | 243 |
발명강2 | 95.1 | 4.9 | 0.6 | 6 | 251 |
발명강3 | 95.9 | 4.1 | 1.1 | 8 | 254 |
발명강4 | 100 | 0.0 | 14.1 | 5 | 281 |
발명강5 | 94.32 | 5.7 | 0.4 | 3 | 247 |
발명강6 | 95 | 5.0 | 0.7 | 7 | 252 |
발명강7 | 96.27 | 3.7 | 1.4 | 10 | 253 |
비교강2 | 96.1 | 3.9 | 1.3 | 0.05 | 243 |
발명강8 | 94.5 | 5.5 | 0.46 | 0.5 | 253 |
발명강9 | 95.5 | 4.5 | 1.5 | 6 | 258 |
발명강10 | 97.9 | 2.1 | 4.9 | 10 | 261 |
비교강3 | 97.6 | 2.4 | 4.7 | 0.03 | 260 |
발명강11 | 95.2 | 4.8 | 0.7 | 8 | 246 |
발명강12 | 96.4 | 3.6 | 1.4 | 10 | 249 |
발명강13 | 96.9 | 3.1 | 3 | 0.5 | 257 |
발명강14 | 96.3 | 3.7 | 1.6 | 1 | 251 |
비교강4 | 97 | 3.0 | 2.1 | 0.05 | 290 |
발명강15 | 96.2 | 3.8 | 1.3 | 5 | 248 |
구분 | QT열처리된 냉연강판 미세조직 |
경도(Hv) | 마모감량(mg) | ||
템퍼드 마르텐사이트 (면적%) |
탄화물 (면적%) |
탄화물 크기 (㎛) |
|||
종래강 (SK120) |
100.0 | 0 | - | 733 | 26.8 |
비교강1 | 100.0 | 0 | - | 760 | 26.5 |
발명강1 | 99.86 | 0.14 | 5 | 878 | 21.8 |
발명강2 | 99.4 | 0.6 | 6 | 879 | 21.7 |
발명강3 | 98.9 | 1.1 | 8 | 968 | 20.4 |
발명강4 | 85.9 | 14.1 | 5 | 823 | 23.1 |
발명강5 | 99.6 | 0.4 | 3 | 942 | 23.7 |
발명강6 | 99.3 | 0.7 | 7 | 922 | 23.9 |
발명강7 | 98.6 | 1.4 | 10 | 949 | 20.5 |
비교강2 | 98.7 | 1.3 | 0.05 | 934 | 25.7 |
발명강8 | 99.54 | 0.46 | 0.5 | 949 | 23.8 |
발명강9 | 98.5 | 1.5 | 6 | 892 | 22.6 |
발명강10 | 95.1 | 4.9 | 10 | 886 | 22.2 |
비교강3 | 95.3 | 4.7 | 0.03 | 857 | 25.3 |
발명강11 | 99.3 | 0.7 | 8 | 948 | 20.9 |
발명강12 | 98.6 | 1.4 | 10 | 916 | 21.4 |
발명강13 | 97.0 | 3 | 0.5 | 938 | 24.3 |
발명강14 | 98.4 | 1.6 | 1 | 961 | 20.3 |
비교강4 | 97.9 | 2.1 | 0.05 | 906 | 25 |
발명강15 | 98.7 | 1.3 | 5 | 943 | 20.1 |
Claims (25)
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하고,미세조직은 면적%로, 탄화물: 0.1~20%, 잔부 템퍼드 마르텐사이트를 포함하며,상기 탄화물은 평균 크기가 0.1~20㎛인 QT열처리된 고탄소 열연강판.
- 청구항 1에 있어서,상기 열연강판은 추가로 V: 0.8% 이하(0%는 제외), Mo: 2.5% 이하(0%는 제외) 및 Nb: 1.5% 이하(0%는 제외)로 이루어지는 그룹으로부터 선택된 1종 이상을 더 포함하는 QT열처리된 고탄소 열연강판.
- 청구항 1에 있어서,상기 열연강판은 350Hv 이상의 경도를 갖는 QT열처리된 고탄소 열연강판.
- 청구항 1에 있어서,상기 열연강판은 QT전 재가열 온도가 800℃일 때 마모감량이 35mg 이하이고, QT전 재가열 온도가 850℃일 때 마모감량이 27mg 이하이며, QT전 재가열 온도가 900℃일 때 마모감량이 25mg 이하인 QT열처리된 고탄소 열연강판.
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하고,미세조직은 면적%로, 페라이트: 20~99.9%, 시멘타이트: 10% 이하, 펄라이트: 50% 이하 및 탄화물: 0.1~20%를 포함하며,상기 탄화물은 평균 크기가 0.1~20㎛인 고탄소 냉연강판.
- 청구항 5에 있어서,상기 냉연강판은 추가로 V: 0.8% 이하(0%는 제외), Mo: 2.5% 이하(0%는 제외) 및 Nb: 1.5% 이하(0%는 제외)로 이루어지는 그룹으로부터 선택된 1종 이상을 더 포함하는 고탄소 냉연강판.
- 청구항 5에 있어서,상기 냉연강판은 350Hv 이하의 경도의 갖는 고탄소 냉연강판.
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하고,미세조직은 면적%로, 탄화물: 0.1~20%, 잔부 템퍼드 마르텐사이트를 포함하며,상기 탄화물은 평균 크기가 0.1~20㎛인 QT열처리된 고탄소 냉연강판.
- 청구항 8에 있어서,상기 냉연강판은 추가로 V: 0.8% 이하(0%는 제외), Mo: 2.5% 이하(0%는 제외) 및 Nb: 1.5% 이하(0%는 제외)로 이루어지는 그룹으로부터 선택된 1종 이상을 더 포함하는 QT열처리된 고탄소 냉연강판.
- 청구항 8에 있어서,상기 냉연강판은 350Hv 이상의 경도를 갖는 QT열처리된 고탄소 냉연강판.
- 청구항 8에 있어서,상기 냉연강판은 QT전 재가열 온도가 900℃일 때 마모감량이 25mg 이하인 QT열처리된 고탄소 냉연강판.
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하는 열연강판을 준비하는 단계;상기 준비된 열연강판을 740~1100℃에서 재가열하는 단계;상기 재가열된 열연강판을 10℃/s 이상의 냉각속도로 냉각하는 단계; 및상기 냉각된 열연강판을 150~600℃에서 템퍼링하는 단계;를 포함하는 QT열처리된 고탄소 열연강판의 제조방법.
- 청구항 12에 있어서,상기 열연강판을 준비하는 단계는 슬라브를 1100~1300℃에서 가열하는 단계; 및 상기 가열된 슬라브를 700~1100℃에서 열간압연하는 단계;를 포함하는 QT열처리된 고탄소 열연강판의 제조방법.
- 청구항 12에 있어서,상기 준비된 열연강판은 펄라이트, 입계에 시멘타이트가 일부 석출된 펄라이트, 베이나이트 및 마르텐사이트 중 1종 이상의 미세조직을 갖는 QT열처리된 고탄소 열연강판의 제조방법.
- 청구항 12에 있어서,상기 준비된 열연강판은 200Hv 이상의 경도를 갖는 QT열처리된 고탄소 열연강판의 제조방법.
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하는 열연강판을 준비하는 단계; 및상기 준비된 열연강판을 냉간압연하여 냉연강판을 얻는 단계;를 포함하는 고탄소 냉연강판의 제조방법.
- 청구항 16에 있어서,상기 열연강판을 준비하는 단계는 슬라브를 1100~1300℃에서 가열하는 단계; 및 상기 가열된 슬라브를 700~1100℃에서 열간압연하는 단계;를 포함하는 고탄소 냉연강판의 제조방법.
- 청구항 16에 있어서,상기 준비된 열연강판은 펄라이트, 입계에 시멘타이트가 일부 석출된 펄라이트, 베이나이트 및 마르텐사이트 중 1종 이상의 미세조직을 갖는 고탄소 냉연강판의 제조방법.
- 청구항 16에 있어서,상기 준비된 열연강판은 200Hv 이상의 경도를 갖는 고탄소 냉연강판의 제조방법.
- 청구항 16에 있어서,상기 냉간압연 전, 상기 열연강판을 630~850℃에서 구상화소둔 열처리하는 단계;를 추가로 포함하는 고탄소 냉연강판의 제조방법.
- 중량%로, C: 1.0~1.4%, Si: 0.1~0.4%, Mn: 0.1~0.8%, Cr: 0.3~11%, W: 0.05~2.5%, P: 0.03% 이하, S: 0.03% 이하, Al: 0.02% 이하, 잔부 Fe 및 기타 불가피한 불순물을 포함하는 열연강판을 준비하는 단계;상기 준비된 열연강판을 냉간압연하여 냉연강판을 얻는 단계;상기 냉연강판을 740~1100℃에서 재가열하는 단계;상기 재가열된 냉연강판을 10℃/s 이상의 냉각속도로 냉각하는 단계; 및상기 냉각된 냉연강판을 150~600℃에서 템퍼링하는 단계;를 포함하는 QT열처리된 고탄소 냉연강판의 제조방법.
- 청구항 21에 있어서,상기 열연강판을 준비하는 단계는 슬라브를 1100~1300℃에서 가열하는 단계; 및 상기 가열된 슬라브를 700~1100℃에서 열간압연하는 단계;를 포함하는 QT열처리된 고탄소 냉연강판의 제조방법.
- 청구항 21에 있어서,상기 준비된 열연강판은 펄라이트, 입계에 시멘타이트가 일부 석출된 펄라이트, 베이나이트 및 마르텐사이트 중 1종 이상의 미세조직을 갖는 QT열처리된 고탄소 냉연강판의 제조방법.
- 청구항 21에 있어서,상기 준비된 열연강판은 200Hv 이상의 경도를 갖는 QT열처리된 고탄소 냉연강판의 제조방법.
- 청구항 21에 있어서,상기 냉간압연 전, 상기 열연강판을 630~850℃에서 구상화소둔 열처리하는 단계;를 추가로 포함하는 QT열처리된 고탄소 냉연강판의 제조방법.
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KR20170075783A (ko) * | 2015-08-14 | 2017-07-03 | 가부시키가이샤 도쿠슈 긴조쿠 엑셀 | 고탄소 냉연 강판 및 그의 제조 방법 |
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JP2009001910A (ja) * | 2008-08-04 | 2009-01-08 | Komatsu Ltd | 高硬度高靭性鋼 |
KR20120073407A (ko) * | 2010-12-27 | 2012-07-05 | 주식회사 포스코 | 연성이 우수한 성형 부재용 강판, 성형 부재 및 그 제조방법 |
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