WO2022139190A1 - 열적 안정성이 우수한 고항복비 초고강도 강판 및 그 제조방법 - Google Patents
열적 안정성이 우수한 고항복비 초고강도 강판 및 그 제조방법 Download PDFInfo
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- WO2022139190A1 WO2022139190A1 PCT/KR2021/017014 KR2021017014W WO2022139190A1 WO 2022139190 A1 WO2022139190 A1 WO 2022139190A1 KR 2021017014 W KR2021017014 W KR 2021017014W WO 2022139190 A1 WO2022139190 A1 WO 2022139190A1
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- steel sheet
- steel
- strength
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 24
- 229910000797 Ultra-high-strength steel Inorganic materials 0.000 title abstract description 6
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 99
- 239000010959 steel Substances 0.000 claims abstract description 99
- 238000010438 heat treatment Methods 0.000 claims abstract description 55
- 238000001816 cooling Methods 0.000 claims description 40
- 229910000734 martensite Inorganic materials 0.000 claims description 24
- 229910052758 niobium Inorganic materials 0.000 claims description 17
- 229910052719 titanium Inorganic materials 0.000 claims description 17
- 229910052750 molybdenum Inorganic materials 0.000 claims description 16
- 230000014509 gene expression Effects 0.000 claims description 15
- 238000005275 alloying Methods 0.000 claims description 14
- 229910052804 chromium Inorganic materials 0.000 claims description 14
- 238000000034 method Methods 0.000 claims description 14
- 229910001563 bainite Inorganic materials 0.000 claims description 13
- 229910052799 carbon Inorganic materials 0.000 claims description 13
- 238000003303 reheating Methods 0.000 claims description 11
- 229910052720 vanadium Inorganic materials 0.000 claims description 11
- 229910052782 aluminium Inorganic materials 0.000 claims description 10
- 238000005098 hot rolling Methods 0.000 claims description 10
- 229910052748 manganese Inorganic materials 0.000 claims description 10
- 229910052757 nitrogen Inorganic materials 0.000 claims description 10
- 229910052710 silicon Inorganic materials 0.000 claims description 10
- 229910052796 boron Inorganic materials 0.000 claims description 9
- 239000012535 impurity Substances 0.000 claims description 9
- 229910052698 phosphorus Inorganic materials 0.000 claims description 9
- 229910052717 sulfur Inorganic materials 0.000 claims description 9
- 229910000859 α-Fe Inorganic materials 0.000 claims description 9
- 238000005096 rolling process Methods 0.000 claims description 7
- 238000004804 winding Methods 0.000 claims description 4
- 239000010955 niobium Substances 0.000 description 36
- 239000010936 titanium Substances 0.000 description 35
- 239000011572 manganese Substances 0.000 description 25
- 239000011651 chromium Substances 0.000 description 24
- 230000000694 effects Effects 0.000 description 23
- 230000015572 biosynthetic process Effects 0.000 description 17
- 230000000052 comparative effect Effects 0.000 description 13
- 239000002244 precipitate Substances 0.000 description 13
- 239000006104 solid solution Substances 0.000 description 13
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 10
- 230000008859 change Effects 0.000 description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 9
- 238000005728 strengthening Methods 0.000 description 9
- 239000000463 material Substances 0.000 description 7
- 150000001247 metal acetylides Chemical class 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 238000001556 precipitation Methods 0.000 description 6
- 238000005496 tempering Methods 0.000 description 6
- 238000003466 welding Methods 0.000 description 6
- 229910045601 alloy Inorganic materials 0.000 description 5
- 239000000956 alloy Substances 0.000 description 5
- 238000005204 segregation Methods 0.000 description 5
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 4
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 4
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 4
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 4
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 4
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 4
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 239000011733 molybdenum Substances 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 4
- 239000011574 phosphorus Substances 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 239000002436 steel type Substances 0.000 description 4
- 239000011593 sulfur Substances 0.000 description 4
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 4
- 229910001566 austenite Inorganic materials 0.000 description 3
- 230000000116 mitigating effect Effects 0.000 description 3
- 238000001953 recrystallisation Methods 0.000 description 3
- 230000009466 transformation Effects 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- 238000012669 compression test Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000009628 steelmaking Methods 0.000 description 2
- 238000009864 tensile test Methods 0.000 description 2
- 229910000967 As alloy Inorganic materials 0.000 description 1
- 241000219307 Atriplex rosea Species 0.000 description 1
- 229910001294 Reinforcing steel Inorganic materials 0.000 description 1
- 229910011214 Ti—Mo Inorganic materials 0.000 description 1
- 230000002159 abnormal effect Effects 0.000 description 1
- 238000000137 annealing Methods 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000001934 delay Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000002401 inhibitory effect Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000001376 precipitating effect Effects 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 210000002784 stomach Anatomy 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
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- 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
- C21D1/02—Hardening articles or materials formed by forging or rolling, with no further heating beyond that required for the formation
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0221—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the working steps
- C21D8/0226—Hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
- C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
- C21D8/0263—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment following hot rolling
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
-
- 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
- C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—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
- 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
- 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
- C22C38/28—Ferrous alloys, e.g. steel alloys containing chromium with titanium or zirconium
-
- 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
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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
- C21D2211/005—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
Definitions
- the present invention relates to an ultra-high strength steel sheet and a method for manufacturing the same, and more particularly, to an ultra-high strength steel sheet with a high yield ratio excellent in thermal stability and a method for manufacturing the same.
- Steel plates used for boom arms of heavy machinery, frames and reinforcements of commercial vehicles, and structural members of construction and mechanical parts may apply heat to some or all of the steel plates and parts for various purposes during the manufacturing process and use.
- a commercial vehicle frame and reinforcement material often needs to be locally shaped for bonding with parts, and for this purpose, local heating and deformation are applied to the steel material.
- the strength of the steel is changed due to this heating process and the durability is inferior. This is because, during the heating process, carbon in a solid solution is rearranged or clustering is formed at dislocations, grain boundaries, etc. to form carbides, thereby causing brittleness of steel.
- the microstructure of martensite, bainite, retained austenite, etc. in the steel also changes, so that the strength of the steel changes rapidly, which also affects the formability and durability.
- Patent Documents 1 and 2 Cr, Mo, Nb, V, etc. are added as alloy components, and a technique for securing high-temperature strength by tempering after hot rolling has been proposed, but this is a technique suitable for manufacturing a steel plate for construction only to
- the strength can be increased to a certain level even when exposed to a high temperature of 600°C or higher for a long time. It can be secured, but there is a problem in that the manufacturing cost becomes excessive, such as having to be tempered.
- thermal stability is excessive for use when exposed to an environment of 600° C. or less for a short time.
- Patent Document 3 is a technique for securing strength in the heat-affected zone of welding by adding Ti, Nb, Cr, Mo, etc., and is suitable for suppressing softening in the welding adjacent part when welding structural members for automobiles.
- the area adjacent to the molten welding material is heated to a high temperature of 600° C. or higher by the heat of welding, and in particular, there is a limitation in that it is heated to a temperature higher than the austenite region.
- Patent Document 4 is a technology to secure high-temperature strength by adding Cr, Mo, Ti, Nb, V, etc., and similarly, it secured strength when exposed to high temperatures of 600° C. or more for a long time, but tensile strength when manufactured under a given component system and manufacturing conditions (TS) It is possible to secure only the strength of 530MPa class, so it is different from giga class ultra-high strength steel in usage and strength.
- TS component system and manufacturing conditions
- Patent Document 1 Korean Patent Publication No. 10-0358939 (Announcement on Oct. 16, 2002)
- Patent Document 2 Korean Patent Publication No. 10-1290382 (published on July 22, 2013)
- Patent Document 3 Korean Patent Publication No. 10-0962745 (published on June 3, 2010)
- Patent Document 4 Korean Patent Publication No. 10-1246390 (published on March 21, 2013)
- C 0.05 to 0.13%, Si: 0.01 to 0.5%, Mn: 0.8 to 2.0%, Cr: 0.005 to 1.2%, Mo: 0.001 to 0.5%, P: 0.001 to 0.02%, S: 0.001 to 0.01%, Al: 0.01 to 0.1%, N: 0.001 to 0.01%, Ti: 0.01 to 0.05%, Nb: 0.001 to 0.03%, V: 0.001 to 0.2%, B: 0.0003 to 0.003 %, the balance Fe and unavoidable impurities;
- the K value defined in the following Relation 1 is -1.05 or more
- the G value defined in the following Relation 2 is 2 to 20,
- Microstructure in terms of area%, contains 60 to 90% of martensite (including tempered martensite), 10 to 40% of bainite and 5% or less of ferrite,
- a steel sheet having a yield ratio of 0.8 or more can be provided.
- K -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb] 2
- the steel sheet may have a tensile strength of 950 MPa or more.
- the tensile strength after heat treatment at 400 to 600° C. may be 80% or more of the tensile strength before heat treatment.
- C 0.05 to 0.13%, Si: 0.01 to 0.5%, Mn: 0.8 to 2.0%, Cr: 0.005 to 1.2%, Mo: 0.001 to 0.5%, P: 0.001 ⁇ 0.02%, S: 0.001 ⁇ 0.01%, Al: 0.01 ⁇ 0.1%, N: 0.001 ⁇ 0.01%, Ti: 0.01 ⁇ 0.05%, Nb: 0.001 ⁇ 0.03%, V: 0.001 ⁇ 0.2%, B: 0.0003 ⁇ Reheating the steel slab containing 0.003%, the remainder Fe and unavoidable impurities, the K value defined in the following Relation 1 is -1.05 or more, and the G value defined in the following Relation 2 is 2 to 20;
- K -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb] 2
- the reheating temperature in the reheating step is 1150 ⁇ 1350 °C
- the rolling end temperature in the hot rolling step may be 850 ⁇ 1150 °C.
- the secondary cooling rate may be less than or equal to 60 °C.
- the present inventors measured changes in the tensile strength at room temperature after heat treatment in a temperature range of 400 to 600° C. for steels having various components and microstructures. As a result, the change in tensile strength It was confirmed that the dependence on the slope of the dynamic strength value measured during the temperature increase of the steel.
- the steel sheet according to an aspect of the present invention is, by weight%, C: 0.05 to 0.13%, Si: 0.01 to 0.5%, Mn: 0.8 to 2.0%, Cr: 0.005 to 1.2%, Mo: 0.001 to 0.5%, P: 0.001 to 0.02%, S: 0.001 to 0.01%, Al: 0.01 to 0.1%, N: 0.001 to 0.01%, Ti: 0.01 to 0.05%, Nb: 0.001 to 0.03%, V: 0.001 to 0.2%, B: 0.0003 0.003%, the balance Fe and unavoidable impurities.
- Carbon (C) is the most economical and effective element for reinforcing steel.
- the amount of carbon (C) is increased, the tensile strength is increased due to an increase in the martensite or bainite fraction. If the content of carbon (C) is less than 0.05%, it is difficult to sufficiently obtain the above-described effects, and if the content exceeds 0.13%, the strength of martensite due to excess carbon (C) increases, but heat treatment in the 400-600 °C section In this case, the solid solution strengthening effect of carbon (C) may be greatly reduced.
- the content of carbon (C) may be 0.05 to 0.13%, a more preferable lower limit may be 0.07%, and a more preferable upper limit may be 0.11%.
- Silicon (Si) is an element advantageous to deoxidize molten steel and has a solid solution strengthening effect, and to improve formability by delaying the formation of coarse carbides.
- the content of silicon (Si) is less than 0.01%, it is difficult to obtain the above-described effect, whereas when the content exceeds 0.5%, red scale is formed on the surface of the steel plate during hot rolling, resulting in poor surface quality of the steel plate. Not only is it very bad, but there is a problem in that weldability is also deteriorated.
- the content of silicon (Si) may be 0.01 to 0.5%, and a more preferable upper limit may be 0.3%.
- Manganese (Mn), like Si, is an effective element for solid-solution strengthening of steel, and may facilitate the formation of martensite and bainite during cooling after heat treatment by increasing the hardenability of steel. If the content of manganese (Mn) is less than 0.8%, the above effect cannot be obtained due to the addition, and if the content exceeds 2.0%, it is advantageous to secure initial strength. After that, the difference in strength may be large. In addition, during the casting of the slab in the casting process, the segregation portion is largely developed at the center of the thickness to cause deviation, and the formation of MnS may be facilitated, resulting in poor ductility.
- the content of manganese (Mn) may be 0.8 to 2.0%, a more preferable lower limit may be 1.0%, and a more preferable upper limit may be 1.8%.
- Chromium (Cr) strengthens the steel as a solid solution, and when cooling, delays the ferrite transformation to help the formation of martensite and bainite. In addition, it contributes to the strength after heat treatment by precipitation of fine complex carbides such as Mo, Ti, Ni, etc. If the content of chromium (Cr) is less than 0.005%, the above effect cannot be obtained due to the addition, and if the content exceeds 1.2%, segregation at the center of the thickness is largely developed similarly to Mn, and the microstructure in the thickness direction is non-uniform. It can also be disadvantageous in terms of alloy cost.
- the content of chromium (Cr) may be 0.005-1.2%, and a more preferable lower limit may be 0.4%.
- Molybdenum (Mo) increases the hardenability of steel to facilitate the formation of martensite and bainite.
- Nb-Ti-Mo-based fine carbide is formed to alleviate the decrease in strength. If the content of molybdenum (Mo) is less than 0.001%, the above effect cannot be obtained according to the addition, and if the content exceeds 0.5%, it may be economically disadvantageous.
- the content of molybdenum (Mo) may be 0.001 to 0.5%, a more preferable lower limit may be 0.05%, and a more preferable upper limit may be 0.3%.
- Phosphorus (P) has a solid solution strengthening effect, but may cause brittleness due to grain boundary segregation.
- manufacturing cost is high, which is economically disadvantageous, and may be insufficient to obtain strength.
- the content exceeds 0.02%, brittleness occurs due to grain boundary segregation, and it is easy to generate fine cracks during molding, and ductility and impact resistance properties can be greatly deteriorated.
- the content of phosphorus (P) may be 0.001 to 0.02%.
- Sulfur (S) is an impurity present in steel, and when its content exceeds 0.01%, it combines with Mn and the like to form non-metallic inclusions. Accordingly, during cutting and processing of steel, microcracks are easy to occur and the impact resistance is greatly reduced. There is this. On the other hand, in order to manufacture the content of sulfur (S) to less than 0.001%, it takes a lot of time during the steel making operation, and thus productivity may be reduced.
- the content of sulfur (S) may be 0.001 to 0.01%.
- Aluminum (Al) is mainly added for deoxidation, and when the content of aluminum (Al) is less than 0.01%, the effect of the addition is insufficient, and when the content exceeds 0.1%, AlN is formed by combining with N. Corner cracks are likely to occur in the slab, and defects may occur due to the formation of inclusions.
- the content of aluminum (Al) may be 0.01 to 0.1%, a more preferable lower limit may be 0.02%, and a more preferable upper limit may be 0.05%.
- Nitrogen (N) is a representative solid solution strengthening element together with C, and forms coarse precipitates with Ti and Al.
- the solid solution strengthening effect of nitrogen (N) is superior to that of C, but there is a problem in that toughness is greatly reduced as the amount of nitrogen (N) in steel increases, and the upper limit thereof is limited to 0.01%.
- the upper limit thereof is limited to 0.01%.
- excessive time is required during the steelmaking operation, resulting in lower productivity.
- the content of nitrogen (N) may be 0.001 to 0.01%.
- Titanium (Ti) is a representative precipitation strengthening element along with Nb, Mo, and V, and contributes to a role of mitigating a decrease in strength due to carbide formation after heat treatment. However, since the temperature for forming precipitates is higher than that of other precipitating elements, the effect is inferior. In addition, coarse TiN is formed with a strong affinity for N. Such TiN has an effect of inhibiting grain growth in the heating process for hot rolling, and it is advantageous to utilize B added to improve hardenability because solid solution N is stabilized.
- titanium (Ti) is less than 0.01%, it is difficult to obtain the above effect, and if the content exceeds 0.05%, there may be a problem in that the low-temperature region impact resistance is inferior due to the generation of coarse TiN and coarsening of precipitates during heat treatment. .
- the content of titanium (Ti) may be 0.01 to 0.05%, and a more preferable upper limit may be 0.03%.
- the C content in the steel is reduced by the formation of carbides, and the effect of reducing strength due to C is alleviated during heat treatment in the range of 400 ⁇ 600°C. If the content of niobium (Nb) is less than 0.001%, the above effect cannot be obtained, and if the content exceeds 0.03%, recrystallization is excessively delayed due to precipitates formed during rolling, and the anisotropy of the steel may be poor.
- the content of niobium (Nb) may be 0.001 to 0.03%, and a more preferable upper limit may be 0.02%.
- V Vanadium (V): 0.001 to 0.2%
- Vanadium (V) is a strong precipitation hardening element, and is an element in which active precipitation occurs in the reheating temperature range. When reheating, it is preferable to add 0.001% or more of vanadium (V) as an element that can compensate for the strength decrease due to martensite annealing by forming precipitates by forming precipitates. However, if the content exceeds 0.2%, economical aspects may be at a disadvantage in
- the content of vanadium (V) may be 0.001 to 0.2%.
- Boron (B) is advantageous in securing initial strength through bainite and martensite by delaying the ferrite transformation. When it exists in a solid solution state in steel, it has the effect of improving the brittleness of steel in a low temperature region by stabilizing grain boundaries, and since BN is formed together with solid solution N, the formation of coarse nitrides can be suppressed. If the content of boron (B) is less than 0.0003%, it is difficult to obtain the above effect, and if the content exceeds 0.003%, it contributes to the initial strength improvement, but does not significantly contribute to the strength improvement after heat treatment, so the strength drop after heat treatment may increase.
- the content of boron (B) may be 0.0003 to 0.003%.
- the steel sheet of the present invention may include the remaining iron (Fe) and unavoidable impurities in addition to the above-described composition. Since unavoidable impurities may be unintentionally incorporated in a normal manufacturing process, they cannot be excluded. Since these impurities are known to anyone skilled in the art of steel manufacturing, all of them are not specifically mentioned in the present specification.
- the steel sheet of the present invention may have a K value of -1.05 or more defined in Relation 1 below.
- the thermal stability of the steel related to the K value in Equation 1 is based on the deformation resistance of the steel to an external force applied to the steel at a given temperature. For example, in a steel material, a high-temperature compression test or a high-temperature tensile test is performed. During the test, the temperature of the material is raised at a constant heating rate and an external force is applied at a constant deformation rate to measure the force per unit area on the material. As such, the slope value of the measured stress-temperature curve is called thermal stability, which can be said to be an intrinsic characteristic of steel.
- the K value of Relation 1 is less than -1.05, thermal stability may be insufficient, and the change in strength before and after heat treatment at 100 to 600° C. may increase.
- the change in yield strength before and after such heat treatment may exhibit a more stable tendency when Relation 2 is simultaneously satisfied. More preferably, it may be -1.03 or more.
- K -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb] 2
- the steel sheet of the present invention may have a G value of 2 to 20 defined in Relation 2 below.
- Relational Expression 2 shows the structural formula for strength after heat treatment by the precipitates, and relates to the formation of fine intragranular precipitates generated during heat treatment.
- Precipitates have the effect of compensating for the reduction in strengthening due to dislocation and solid solution carbon.
- the G value is less than 2
- the formation of precipitates in the steel sheet after heat treatment is insufficient, or the formation of coarse precipitates in the initial steel sheet increases. Reduced precipitate formation may result in insufficient thermal stability.
- the value exceeds 20 the effect of further improving the thermal stability is reduced, and since a large amount of expensive alloying elements must be added, it may be economically disadvantageous. More preferably, it may be 3 or more, and more preferably, it may be 17 or less.
- % indicating the fraction of microstructure is based on the area.
- the microstructure of the steel sheet according to an aspect of the present invention may include 60 to 90% of martensite (including tempered martensite), 10 to 40% of bainite, and 5% or less of ferrite in terms of area%.
- Martensite is a tissue that is unfavorable for securing thermal stability, but is a necessary tissue for securing initial strength. Strength can be secured by solid solution with C and lattice distortion, but during heat treatment, the effect disappears, so a very large change in strength may appear.
- tempered martensite is included as a fraction of martensite.
- the microstructure may contain ferrite in an amount of 5% or less, but if the content exceeds 5%, it is disadvantageous in securing initial strength.
- the steel according to an aspect of the present invention may be manufactured by reheating, hot rolling, cooling and winding a steel slab satisfying the above alloy composition.
- the steel slab satisfying the above alloy composition may be reheated in a temperature range of 1150 to 1350 °C.
- the reheating temperature is less than 1150°C, the precipitate-forming elements such as Nb and Ti are not sufficiently re-dissolved, so during the heat treatment of the manufactured steel sheet, the formation of precipitates is reduced, coarse TiN remains, and the segregation generated during playing It can be difficult to resolve by diffusion.
- the temperature exceeds 1350° C., strength decrease and tissue non-uniformity may occur due to abnormal grain growth of austenite grains.
- the reheated steel slab may be hot rolled to a rolling end temperature of 850 to 1150 °C.
- Nb carbide is formed by strain-induced precipitation, which may be disadvantageous in the formation of fine carbide during heat treatment.
- the microstructure is optimized in order to secure the desired physical properties, and in order to obtain this, the cooling process can be performed by dividing it into two steps.
- the strength of the manufactured steel sheet may be inferior due to the formation of ferrite.
- the primary cooling end temperature exceeds 500°C, ferrite is formed and the initial strength of the steel sheet is lowered, whereas when the temperature is less than 300°C, it is difficult to form bainite in the steel sheet, which is advantageous for securing initial strength, but strength after heat treatment The drop could be large.
- secondary cooling when cooling to a temperature range of 50 to 200°C, auto-tempering occurs and fine carbides are precipitated. This lowers the initial tensile strength, but increases the yield strength to have a high yield ratio, and has the effect of mitigating the strength drop during heat treatment.
- the cooling end temperature is less than 50°C, auto-tempering does not occur and the strength decrease after heat treatment is large. and may affect the fine precipitation of Nb and Ti at high temperatures. More preferably, the secondary cooling rate may be 10 to 60° C./s.
- the secondary cooling rate exceeds 70°C/s, auto-tempering does not occur, and the yield ratio is low and the initial tensile strength is high, so the strength drop after heat treatment may be large.
- the cooling rate is less than 10 °C / s, there is a problem that the auto-tempering effect becomes excessive.
- the steel of the present invention prepared as described above has a tensile strength of 950 MPa or more, a yield ratio of 0.8 or more, and the tensile strength after heat treatment at 400 to 600 ° C. is 80% or more of the tensile strength before heat treatment. It may have a stomach ratio and ultra-high strength characteristics.
- Table 1 below shows the alloy components according to the steel type and the results of calculating Relations 1 and 2 through this.
- steel sheets were manufactured under the conditions shown in Table 2.
- Table 2 shows the rolling end temperature, the primary and secondary cooling termination temperatures, and the primary and secondary cooling rates.
- the reheating temperature not shown in Table 2 was 1250° C., and the thickness of the steel after hot rolling was 3 mm for all steel types.
- K -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb] 2
- Table 3 below shows the microstructure and mechanical properties of the prepared steel sheet.
- the fractions of ferrite, bainite, and martensite were measured and indicated, respectively, and the tensile strength and yield ratio (yield strength/tensile strength) of the manufactured steel were indicated.
- the fraction of martensite was shown including the fraction of tempered martensite.
- the tensile strength was measured after heat treatment of the manufactured steel sheet, and the ratio with the tensile strength before heat treatment was shown. Heat treatment was carried out so as to hold for 15 minutes after heating to 500 °C.
- the tensile test was conducted by taking a JIS 5 standard test piece in a direction parallel to the rolling direction, and the microstructure was measured at 1/4 of the thickness of each steel type. did
- Comparative Steels 1 and 2 had a C content outside the scope of the present invention, and Comparative Steel 1 did not meet the C content of the present invention, and thus the desired microstructure in the present invention was not secured, and thus the tensile strength was was lacking. Comparative Steel 2 was out of the range of Equation 1 due to the excessive C content, and thus did not satisfy the tensile strength ratio before and after heat treatment.
- Comparative Steels 3 and 4 had Mn content outside the range of the present invention, Comparative Steel 3 exceeded the Mn content of the present invention, and Relation 1 was also not satisfied. Due to this, the microstructure could not be secured, and the yield ratio was also inferior. Comparative Steel 4 lacked the Mn content, so it was difficult to secure the microstructure proposed in the present invention, and as a result, the tensile strength was also insufficient.
- Comparative steels 5 and 6 did not satisfy the cooling conditions during the primary cooling, Comparative Steel 5 exceeded the cooling termination temperature range, and Comparative Steel 6 lacked a cooling rate, so that the microstructure desired in the present invention was obtained. It was not satisfactory, and the strength was insufficient.
- Comparative Steel 7 was a case where the secondary cooling rate was exceeded, and martensite was excessively formed, which caused the yield ratio to be insufficient, and the change in tensile strength before and after heat treatment was large, and the tensile strength ratio did not satisfy the scope of the present invention. .
- Comparative Steel 8 did not satisfy Relational Equation 2, and the change in tensile strength before and after heat treatment was large, and thus did not satisfy the tensile strength ratio before and after heat treatment suggested in the present invention.
- Comparative Steel 9 had an excessively low primary cooling termination temperature, resulting in excessive martensite formation, resulting in insufficient yield ratio, and excessive change in tensile strength before and after heat treatment.
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Abstract
Description
Claims (6)
- 중량%로, C: 0.05∼0.13%, Si: 0.01∼0.5%, Mn: 0.8∼2.0%, Cr: 0.005~1.2%, Mo: 0.001∼0.5%, P: 0.001∼0.02%, S: 0.001∼0.01%, Al: 0.01∼0.1%, N: 0.001∼0.01%, Ti: 0.01~0.05%, Nb: 0.001~0.03%, V: 0.001~0.2%, B: 0.0003~0.003%, 잔부 Fe 및 불가피한 불순물을 포함하고,하기 관계식 1에서 정의되는 K 값이 -1.05 이상이고,하기 관계식 2에서 정의되는 G 값이 2~20이며,미세조직은 면적%로, 60~90%의 마르텐사이트(템퍼드 마르텐사이트 포함), 10~40%의 베이나이트 및 5% 이하의 페라이트를 포함하고,항복비가 0.8 이상인 강판.[관계식 1]K = -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb]2(여기서, [C], [Si], [Mn], [Cr], [Mo], [Ti] 및 [Nb]은 해당 합금원소의 중량%이다.)[관계식 2]G = ([Nb]/93+[Mo]/96+[V]/51)/([Ti]/48)(여기서, [Nb], [Mo], [V] 및 [Ti]은 해당 합금원소의 중량%이다.)
- 제1항에 있어서,상기 강판은 인장강도가 950MPa 이상인 강판.
- 제1항에 있어서,상기 강판은 400~600℃에서 열처리 후의 인장강도가 열처리 전 인장강도의 80% 이상인 강판.
- 중량%로, C: 0.05∼0.13%, Si: 0.01∼0.5%, Mn: 0.8∼2.0%, Cr: 0.005~1.2%, Mo: 0.001∼0.5%, P: 0.001∼0.02%, S: 0.001∼0.01%, Al: 0.01∼0.1%, N: 0.001∼0.01%, Ti: 0.01~0.05%, Nb: 0.001~0.03%, V: 0.001~0.2%, B: 0.0003~0.003%, 잔부 Fe 및 불가피한 불순물을 포함하고, 하기 관계식 1에서 정의되는 K 값이 -1.05 이상이고, 하기 관계식 2에서 정의되는 G 값이 2~20인 강 슬라브를 재가열하는 단계;상기 재가열된 강 슬라브를 열간압연하는 단계; 및상기 열간압연된 강판을 300~500℃의 온도범위까지 60℃/s 이상의 냉각속도로 1차 냉각하고, 50~200℃의 온도범위까지 10~70℃/s의 냉각속도로 2차 냉각한 후 권취하는 단계를 포함하는 강판의 제조방법.[관계식 1]K = -0.6-1.42[C]+0.05[Si]-0.16[Mn]-0.08[Cr]-0.03[Mo]+0.09[Ti]+0.08[Nb]2(여기서, [C], [Si], [Mn], [Cr], [Mo], [Ti] 및 [Nb]은 해당 합금원소의 중량%이다.)[관계식 2]G = ([Nb]/93+[Mo]/96+[V]/51)/([Ti]/48)(여기서, [Nb], [Mo], [V] 및 [Ti]은 해당 합금원소의 중량%이다.)
- 제4항에 있어서,상기 재가열 단계에서 재가열 온도는 1150~1350℃이고,상기 열간압연 단계에서 압연종료온도는 850~1150℃인 강판의 제조방법.
- 제4항에 있어서,상기 냉각 시, 2차 냉각속도는 60℃ 이하인 강판의 제조방법.
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EP21911257.0A EP4265782A4 (en) | 2020-12-21 | 2021-11-18 | ULTRA-HIGH-STRENGTH STEEL SHEET WITH HIGH ELASTICITY STRENGTH/TENSILE STRENGTH RATIO, HAVING EXCELLENT THERMAL STABILITY, AND METHOD FOR MANUFACTURING SAME |
JP2023537431A JP2024500150A (ja) | 2020-12-21 | 2021-11-18 | 熱的安定性に優れた高降伏比の超高強度鋼板及びその製造方法 |
CN202180086362.5A CN116710586A (zh) | 2020-12-21 | 2021-11-18 | 热稳定性优异的高屈强比超高强度钢板及其制造方法 |
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- 2021-11-18 CN CN202180086362.5A patent/CN116710586A/zh active Pending
- 2021-11-18 EP EP21911257.0A patent/EP4265782A4/en active Pending
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