US20220298595A1 - Steel sheet for hot forming, hot-formed member, and method for manufacturing same - Google Patents
Steel sheet for hot forming, hot-formed member, and method for manufacturing same Download PDFInfo
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- US20220298595A1 US20220298595A1 US17/639,414 US202017639414A US2022298595A1 US 20220298595 A1 US20220298595 A1 US 20220298595A1 US 202017639414 A US202017639414 A US 202017639414A US 2022298595 A1 US2022298595 A1 US 2022298595A1
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- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 116
- 239000010959 steel Substances 0.000 title claims abstract description 116
- 238000000034 method Methods 0.000 title claims abstract description 44
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 13
- 239000011651 chromium Substances 0.000 claims abstract description 46
- 239000011572 manganese Substances 0.000 claims abstract description 32
- 239000010955 niobium Substances 0.000 claims abstract description 32
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 claims abstract description 20
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 19
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 18
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 18
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 17
- 229910052757 nitrogen Inorganic materials 0.000 claims abstract description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000012535 impurity Substances 0.000 claims abstract description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 9
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 9
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims abstract description 9
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 9
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 9
- 239000010703 silicon Substances 0.000 claims abstract description 9
- 238000010438 heat treatment Methods 0.000 claims description 30
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 23
- 229910000859 α-Fe Inorganic materials 0.000 claims description 23
- 238000000137 annealing Methods 0.000 claims description 12
- 238000005096 rolling process Methods 0.000 claims description 9
- 238000001816 cooling Methods 0.000 claims description 8
- 239000002253 acid Substances 0.000 claims description 7
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 7
- 239000010960 cold rolled steel Substances 0.000 claims description 7
- 229910052759 nickel Inorganic materials 0.000 claims description 7
- 229910052760 oxygen Inorganic materials 0.000 claims description 7
- 239000001301 oxygen Substances 0.000 claims description 7
- 238000005554 pickling Methods 0.000 claims description 7
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 claims description 6
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 claims description 6
- 229910052698 phosphorus Inorganic materials 0.000 claims description 6
- 239000011574 phosphorus Substances 0.000 claims description 6
- 229910052717 sulfur Inorganic materials 0.000 claims description 6
- 239000011593 sulfur Substances 0.000 claims description 6
- 238000003303 reheating Methods 0.000 claims description 2
- 230000000052 comparative effect Effects 0.000 description 67
- 230000003647 oxidation Effects 0.000 description 34
- 238000007254 oxidation reaction Methods 0.000 description 34
- 239000000463 material Substances 0.000 description 18
- 229910001566 austenite Inorganic materials 0.000 description 13
- 230000015572 biosynthetic process Effects 0.000 description 13
- 239000010410 layer Substances 0.000 description 13
- 238000007747 plating Methods 0.000 description 12
- 238000005275 alloying Methods 0.000 description 10
- 238000009864 tensile test Methods 0.000 description 9
- 229910000734 martensite Inorganic materials 0.000 description 8
- 230000001747 exhibiting effect Effects 0.000 description 7
- 239000000203 mixture Substances 0.000 description 7
- 238000005097 cold rolling Methods 0.000 description 6
- 230000007797 corrosion Effects 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 6
- 230000002542 deteriorative effect Effects 0.000 description 6
- 239000000126 substance Substances 0.000 description 5
- 238000010301 surface-oxidation reaction Methods 0.000 description 5
- 238000003466 welding Methods 0.000 description 5
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 229910052782 aluminium Inorganic materials 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000001965 increasing effect Effects 0.000 description 4
- 238000001000 micrograph Methods 0.000 description 4
- 239000002436 steel type Substances 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 238000004458 analytical method Methods 0.000 description 3
- 230000003111 delayed effect Effects 0.000 description 3
- 229910052739 hydrogen Inorganic materials 0.000 description 3
- 239000001257 hydrogen Substances 0.000 description 3
- 239000006104 solid solution Substances 0.000 description 3
- 238000005728 strengthening Methods 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 230000006866 deterioration Effects 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 230000002401 inhibitory effect Effects 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000002244 precipitate Substances 0.000 description 2
- 238000002360 preparation method Methods 0.000 description 2
- 239000000047 product Substances 0.000 description 2
- 238000010791 quenching Methods 0.000 description 2
- 230000000171 quenching effect Effects 0.000 description 2
- 239000002994 raw material Substances 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 229910018125 Al-Si Inorganic materials 0.000 description 1
- 229910018520 Al—Si Inorganic materials 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 239000011247 coating layer Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000004299 exfoliation Methods 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 150000004767 nitrides Chemical class 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000036961 partial effect Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000002829 reductive effect Effects 0.000 description 1
- 238000007670 refining Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000009628 steelmaking Methods 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
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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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/62—Quenching devices
- C21D1/673—Quenching devices for die quenching
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/004—Heat treatment of ferrous alloys containing Cr and Ni
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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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
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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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
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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
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/02—Hardening by precipitation
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D7/00—Modifying the physical properties of iron or steel by deformation
- C21D7/13—Modifying the physical properties of iron or steel by deformation by hot working
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- 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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- 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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- 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
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- 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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- 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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- 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
- C22C38/001—Ferrous alloys, e.g. steel alloys containing N
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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
- C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
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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
- C22C38/26—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
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
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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
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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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel 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
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- C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
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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
- C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
- C22C38/58—Ferrous alloys, e.g. steel alloys containing chromium with nickel with more than 1.5% by weight of 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
- C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/02—Stamping using rigid devices or tools
- B21D22/022—Stamping using rigid devices or tools by heating the blank or stamping associated with heat treatment
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- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/004—Dispersions; Precipitations
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- C—CHEMISTRY; METALLURGY
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- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
Definitions
- the present disclosure relates to a steel sheet for hot forming, a hot-formed member using the same, and a method for manufacturing the same, and more particularly, to a high-strength and non-plated steel sheet which is for hot forming and may be suitable for use in automotive structural members that require collision resistance characteristics, a hot-formed member, and a method for manufacturing the same.
- thickness of materials used for the vehicles may be reduced to increase fuel efficiency, but a decrease in thickness may cause a stability problem in the vehicles and thus enhancement of strength of the material should be accompanied therewith.
- AHSS advanced high strength steels
- DP dual phase steels
- TRIP steels have been developed based on studies on various materials and have been actually applied to automobile parts, and such steel sheets exhibit excellent formability compared to conventional high-strength steels for vehicles.
- a martensitic steel having an ultra-high strength of 1,000 MPa or more may be effective on reducing a weight of the body of a vehicle when used in the vehicle, commercialization of the martensitic structure is difficult due to poor formability.
- a method of preparing a high-strength martensitic structure by cold forming an initial ferritic structure having excellent formability, forming an austenite by heat treatment at a high temperature, and quenching the resultant has been used.
- a problem of poor shape fixability may occur according to the above-described forming method due to phase transformation in a non-constrained sate.
- a volume change is accompanied by a change in the crystal structure from FCC to BCT in phase transformation from austenite to martensite occurring during a cooling process, and accordingly dimensional precision deteriorates.
- an additional process of performing dimensional correction is required.
- Hot press forming is a forming method to increase a strength of a final product by preparing an austenite single phase by heating a steel sheet at a high temperature higher than Ac1 at which processing is easily performed, hot forming the steel sheet by press forming, and forming a low-temperature structure such as martensite by quenching.
- the hot forming is advantageous in that a problem in formability caused during preparation of a high-strength material may be minimized.
- the steel sheet is heated to a high temperature in the case of using the hot press forming method, the surface of the steel sheet is oxidized, and thus a process of removing oxides from the surface of the steel sheet needs to be added after the press forming.
- Patent Document 1 a method disclosed in Patent Document 1 has been proposed.
- a steel sheet coated with Al—Si is heated at a temperature of 850° C. or higher and then hot-pressed to form a martensite structure, the steel sheet is not oxidized during heating due to an Al—coating layer formed on the surface of the steel sheet.
- hot press forming is performed using the Al-coated steel sheet, not only a product having an ultra-high strength of 1,000 MPa may be easily obtained but also a product having high dimensional precision may be obtained, and thus the hot press forming has drawn attention and interest as a very effective method for forming automobile parts on a decrease in weight and an increase in rigidity of vehicles.
- a plating layer includes aluminum as a main phase
- aluminum may be liquified at a temperature higher than a melting point of the plating layer to be fused to a roll in a heating furnace when a blank is heated in a heating furnace or partial exfoliation may occur due to stress.
- a hot-pressed, formed member may be prepared by bonding two or more members using an adhesive.
- a sufficient adhesive strength needs to be maintained to verify adhesive strength.
- a method of testing whether the bonded portion is easily maintained at a high strength by applying a tensile stress in a direction perpendicular to the bonded surface is often used.
- a plating layer is often detached from the inside of the plating layer or an interface between the plating layer and a steel sheet. In this case, a problem of separation of the two members may occur even under a low stress.
- a tailored welded blank which is made by pre-bonding different steel sheets having different thicknesses for decreasing a weight of a vehicle, has been used as a major material in hot press forming.
- the TWB is mainly prepared by laser bonding and it is known that combination of the surface condition of a material and strength of the raw material considerably affects properties.
- breakage of a welded part was observed when deformed by press forming after heat treatment. This is because Al on the plating layer of the surface penetrates into the welded part during laser welding of a TWB material and thus a ferrite phase remains in the welded part after heat treatment to embrittle the welded part.
- an additional process of removing a surface film is suggested before laser welding of the hot dip Al plated steel sheet.
- Patent Document 1 US Patent Publication No. 6,296,805 (Oct. 2, 2001)
- Patent Document 2 Korean Patent Publication No. 10-1696121 (Jan. 6, 2017)
- Patent Document 3 Korean Patent Application Publication No. 10-2018-0131943 (Dec. 11, 2018)
- Patent Document 4 Korean Patent Application Publication No. 10-2015-0075277 (Jul. 3, 2015)
- Embodiments of the present disclosure have been proposed to solve problems described above and provided are a steel sheet for hot forming having ultra-high strength while preventing surface oxidation during hot press forming without using a plating layer, a hot-formed member, and a method for manufacturing the same.
- a steel sheet for hot forming includes, in percent by weight (wt %), 0.05 to 0.3% of carbon (C), 0.5 to 3.0% of silicon (Si), 0.1 to 2.0% of manganese (Mn), 3.0 to 9.0% of chromium (Cr), more than 0% and less than 0.2% of nitrogen (N), 0.03 to 1.0% of niobium (Nb), and the remainder of iron (Fe) and inevitable impurities, wherein a microstructure comprises a ferrite phase and 20 vol % or less of a carbonitride.
- tThe ferrite phase may have an average grain size of 100 ⁇ m or less.
- the steel sheet may satisfy Expression (1) below:
- a content of Cr may be from 3.5 to 5.5%.
- the steel sheet may further include less than 3.0% of nickel (Ni).
- the steel sheet may further include less than 0.1% of phosphorus (P) and less than 0.01% of sulfur (S).
- a hot-formed member includes, in percent by weight (wt %), 0.05 to 0.3% of carbon (C), 0.5 to 3.0% of silicon (Si), 0.1 to 2.0% of manganese (Mn), 3.0 to 9.0% of chromium (Cr), more than 0% and less than 0.2% of nitrogen (N), 0.03 to 1.0% of niobium (Nb), and the remainder of iron (Fe) and inevitable impurities.
- the hot-formed member may satisfy Expression (1) below:
- an average oxygen content may be 20 wt % or less at a point of 0.1 ⁇ m depth from the surface.
- the hot-formed member may have a yield strength of 1,100 MPa or more and a tensile strength of 1,500 MPa or more.
- a content of Cr may be from 3.5 to 5.5%.
- the hot-formed member may further include less than 3.0% of nickel (Ni).
- the hot-formed member may further include less than 0.1% of phosphorus (P) and less than 0.01% of sulfur (S).
- a method for manufacturing a hot-formed member includes: preparing a steel sheet for hot forming comprising, in percent by weight (wt %), 0.05 to 0.3% of carbon (C), 0.5 to 3.0% of silicon (Si), 0.1 to 2.0% of manganese (Mn), 3.0 to 9.0% of chromium (Cr), more than 0% and less than 0.2% of nitrogen (N), 0.03 to 1.0% of niobium (Nb), and the remainder of iron (Fe) and inevitable impurities; heating the steel sheet at a rate of 1 to 1,000 ° C./sec to a temperature range of Ac3+50° C. to Ac3+200° C. and maintaining for 1 to 1,000 seconds; and hot-forming the heated and maintained steel sheet and cooling the steel sheet at a rate of 1 to 1000° C./sec to a temperature below Mf
- the steel sheet for hot forming may satisfy Expression (1) below.
- the steel sheet for hot forming may include a microstructure comprising a ferrite phase and 20 vol % or less of a carbonitride, wherein an average grain size of the ferrite phase is 100 ⁇ m or less.
- a content of Cr in the steel sheet for hot forming may be from 3.5 to 5.5%.
- the steel sheet for hot forming may further include less than 3.0% of nickel (Ni).
- the steel sheet for hot forming may further include less than 0.1% of phosphorus (P) and less than 0.01% of sulfur (S).
- the preparing of the steel sheet for hot forming may include: reheating a slab in a temperature range of 1,000 to 1,300° C.; preparing a hot-rolled steel sheet by finish-rolling the reheated slab in a temperature range higher than Ar3 and equal to or lower than 1,000° C.; coiling the hot-rolled steel sheet in a temperature range higher than Ms and equal to or lower than 850° C.; and acid-pickling the coiled, hot-rolled steel sheet.
- the method may further include: preparing a cold-rolled steel sheet by rolling the acid pickled, hot-rolled steel sheet with a reduction ratio of 30 to 80%; and continuously annealing the cold-rolled steel sheet in a temperature range of 700 to 900° C.
- the method may further include batch-annealing the coiled, hot-rolled or acid-pickled steel sheet in a temperature range of 500 to 850° C. for 1 to 100 hours.
- FIG. 1 is an electron microscope image showing a microstructure of a steel sheet for hot forming according to an embodiment of the present disclosure.
- FIG. 2 is a photograph exemplarily illustrating good formability (a) and poor formability (b) obtained when hot forming is performed using a mini-bumper mold.
- FIG. 3 is a graph illustrating tensile test results of samples of examples and comparative examples which are hot-formed using a plate-shaped mold.
- FIGS. 4 and 5 are electron microscope images of microstructures of steel sheets for hot forming according to an example and a comparative example prior to formation, respectively.
- FIGS. 6 and 7 are graphs illustrating GDS analysis results of hot-formed members obtained using a mini-bumper mold according to an example exhibiting good oxidation resistance and a comparative example exhibiting inferior oxidation resistance with respect to depth from the surface.
- a steel sheet for hot forming according to an embodiment of the present disclosure may include, in percent by weight (wt %), 0.05 to 0.3% of carbon (C), 0.5 to 3.0% of silicon (Si), 0.1 to 2.0% of manganese (Mn), 3.0 to 9.0% of chromium (Cr), more than 0% and less than 0.2% of nitrogen (N), 0.03 to 1.0% of niobium (Nb), and the remainder of iron (Fe) and inevitable impurities, wherein a microstructure includes a ferrite phase and 20 vol % or less of a carbonitride.
- the present inventors have designed optimum alloying elements such as Cr, Si, and Mn to obtain high strength at an equivalent level to that of conventional plated-steel sheet, to inhibit surface oxidation without using a plated layer, and to have excellent formability suitable for preparation of a formed member.
- a steel sheet for hot forming and a hot-formed member may include, in percent by weight (wt %), 0.05 to 0.3% of carbon (C), 0.5 to 3.0% of silicon (Si), 0.1 to 2.0% of manganese (Mn), 3.0 to 9.0% of chromium (Cr), more than 0% and less than 0.2% of nitrogen (N), 0.03 to 1.0% of niobium (Nb), and the remainder of iron (Fe) and inevitable impurities.
- the content of C is from 0.05 to 0.3%.
- C is an element not only effective on stabilization of an austenite phase but also effective on obtaining high strength by solid solution strengthening effects.
- an excess of C may not only deteriorate processibilty due to an increase in a carbide in a microstructure but also deteriorate physical and mechanical properties (e.g., ductility, toughness, and corrosion resistance) of a welded part and a heat-affected portion. Therefore, an upper limit thereof is set to 0.3%.
- C needs to be added in an amount of 0.05% or more to obtain stability of the austenite stability and target mechanical properties.
- C may be added in an amount of 0.15% or more to obtain high strength.
- the C content is not necessarily 0.15% or more.
- the content of Si is from 0.5 to 3.0%.
- Si serving as a deoxidizer during a steelmaking process, is effective on enhancing corrosion resistance and oxidation resistance, and these properties are effective when the Si content is 0.5% or more.
- Si is an element effective on stabilizing a ferrite phase, an excess of Si may promote formation of delta ( ⁇ ) ferrite in a cast slab, thereby not only deteriorating hot processibility but also deteriorating ductility and toughness of a steel material due to solid solution strengthening effects. Therefore, an upper limit thereof is set to 0.7%.
- Si may be added in an amount of 1.0 to 2.0%.
- the content of Mn is from 0.1 to 2.0%.
- Mn as an element effective on stabilizing an austenite phase, is essential to obtain the austenite phase at a high temperature during heat treatment and is added in an amount of 0.1% or more.
- an excess of Mn not only causes an increases in S-based inclusions (MnS) leading to deterioration of ductility, toughness, and corrosion resistance of a steel material but also deteriorates oxidation resistance due to an increase in MnO on the surface of the steel material during heat treatment at a high temperature in an oxidizing atmosphere for forming an austenite structure. Therefore, an upper limit thereof is set to 2.0%.
- the content of Cr is from 3.0 to 9.0%.
- Cr as a ferrite-stabilizing element, is effective on improving corrosion resistance and oxidation resistance, and these properties are effective when the Cr content is 3.0% or more.
- an excess of Cr may cause an increase in Ac1 due to enhancement of stability of ferrite making it difficult to obtain an austenite phase during heat treatment of a steel material. Therefore, an upper limit thereof is set to 9.0%.
- the Cr content may be from 3.5 to 7.0%, preferably, from 3.5 to 5.5%.
- the content of N is more than 0% and less than 0.2%.
- N as not only an austenite phase-stabilizing element but also an element effective on obtaining high strength by solid solution strengthening effects, may decrease the amounts of Ni and Mn, thereby preventing an increase in costs of materials.
- an excess of N may cause formation of a large amount of a nitride in a microstructure, thereby deteriorating processibility.
- delta ( ⁇ ) ferrite formed during a cooling process after casting may cause local formation of nitrogen pin holes, thereby deteriorating quality. Therefore, an upper limit thereof is set to 0.2%.
- the content of Nb is from 0.03 to 1.0%.
- Nb forming a carbonitride of Nb(C,N) at a high temperature
- Nb is effective on preventing coarsening of grains during heat treatment and this property is effective when the Nb content is 0.03% or more.
- Such grain refinement is effective not only on improving processibilty of a steel material at a high temperature but also on enhancing impact resistance.
- an excess of Nb may cause formation of a large amount of the Nb(C,N) carbonitride, thereby decreasing amounts of solute C and N, making it difficult to obtain target mechanical properties. Therefore, an upper limit thereof is set to 1.0%, preferably 0.3%.
- the content of Ni is less than 3.0%.
- Ni is not an essential element in the present disclosure because manufacturing costs are increased thereby.
- an austenite phase may be easily formed at a high temperature.
- an upper limit thereof is set to 3.0%.
- the content of P is less than 0.1%.
- an upper limit thereof is set to 0.1%.
- the content of S is less than 0.01%.
- an upper limit thereof is set to 0.01%.
- the remaining component of the composition of the present disclosure is iron (Fe).
- the composition may include unintended impurities inevitably incorporated from raw materials or surrounding environments, and thus addition of other alloy components is not excluded.
- the impurities are not specifically mentioned in the present disclosure, as they are known to any person skilled in the art of manufacturing.
- the steel sheet for hot forming of the present disclosure has a microstructure including a ferrite phase and 20 vol % or less of a carbonitride. Because good hot formability is required to prevent cracks or bursts on the surface during hot forming, e.g., hot press forming (HPF), grain refinement is required in a ferrite phase.
- hot press forming HPF
- the steel sheet for hot forming may include a ferrite phase having an average grain size of 100 ⁇ m or less.
- the average grain size of the ferrite phase is controlled by the chemical composition of alloying elements.
- Nb is added to reduce in size of grains and coarsening of grains may be prevented at a high temperature, and thus addition of Nb is essential.
- the ranges of contents of C and N which form the carbonitride with Nb are also important to control the average grain size.
- the content of Cr is too low, e.g., less than 3.0%, grains are coarsened, thereby deteriorating formability.
- the steel sheet for hot forming may be a hot-rolled steel sheet obtained by batch annealing, a cold-rolled steel sheet obtained by continuous annealing, or a hot-rolled steel sheet obtained by acid pickling without performing annealing.
- the grain size of steel sheets provided to hot forming may generally be controlled by annealing, excellent formability may be obtained during hot forming regardless of performing annealing when the range of the chemical composition of alloying elements of the present disclosure is satisfied.
- the steel sheet for hot forming may satisfy Expression (1) below.
- oxidation resistance may be obtained by adjusting the contents of Si, Cr, C, and Mn to satisfy Expression (1) although a plating layer is not formed.
- the contents of oxidation-inhibiting elements such as Cr and Si have the greatest influence on oxidation resistance of a hot-formed member, the oxidation resistance is also sensitive to the contents of C and Mn that promote formation of precipitates and oxides as well thereby deriving Expression (1) above.
- the contents of Cr and Si are low, dense formation of Cr and Si oxides is inhibited and a thick Fe oxide is formed on the surface layer.
- formation of a Cr carbide increases to reduce the Cr content in a matrix, thereby causing formation of an Fe oxide.
- a Mn oxide is formed thereby deteriorating oxidation resistance on the surface.
- Oxidation behavior of the surface layer sensitively changes during hot forming due to influence of various alloying elements as described above, It is important to define the quality of oxidation resistance of the surface layer, and the hot-formed member according to an embodiment of the present disclosure may have an average oxygen content of 20 wt % or less at a point of 0.1 ⁇ m depth from the surface.
- a steel sheet for hot forming may be manufactured according to a well-known manufacturing process as a cold-rolled steel sheet or an acid-pickled, hot-rolled steel sheet, but manufacturing conditions are not particularly limited.
- An example of the method for manufacturing the steel sheet for hot forming is as follows.
- An ingot or slab having the above-described chemical composition of alloying elements is heated in a temperature range of 1,000 to 1,300° C. and hot-rolled. At a heating temperature below 1,000° C., it is difficult to homogenize the slab structure, and at a heating temperature exceeding 1,300° C., an oxide layer may be excessively formed and manufacturing costs may increase.
- hot finish rolling is performed in a temperature range higher than Ar3 and equal to or lower than 1,000° C.
- a finish rolling temperature of Ar3 or less recrystallization rolling may be easily induced making it difficult to control formation of a surface mixed structure and a steel sheet.
- the finish rolling temperature exceeds 1,000° C., hot-rolled grains may be easily coarsened.
- the hot-rolled steel sheet may be coiled in a temperature range higher than Ms and equal to or lower than 850° C.
- a coiling temperature is Ms or below, it is difficult to perform a subsequent cold rolling due to too high strength of the hot-rolled steel.
- the coiling temperature is higher than 850° C., a thickness of an oxide layer excessively increases making it difficult to perform acid pickling on the surface.
- the hot-rolled steel sheet may be hot-formed immediately after acid pickling. Meanwhile, the acid pickling and cold rolling may be performed to control the thickness of the steel sheet more precisely. Although a cold rolling reduction ratio after acid pickling is not particularly limited, the cold rolling may be performed with a reduction ratio of 30 to 80% to obtain a target thickness. In this regard, to reduce a rolling load of the cold rolling, if required, the hot-rolled steel sheet or the previously acid-pickled, hot-rolled steel sheet may be batch-annealed. In this regard, although batch annealing conditions are not particularly limited, the batch annealing may be performed at a temperature of 500 to 850° C. for 1 to 100 hours to reduce strength of the hot-rolled steel sheet.
- the cold-annealed, cold-rolled steel sheet may be continuously annealed.
- a continuous annealing heat treatment process is not particularly limited, the heat treatment may be performed in a temperature range of 700 to 900° C.
- the hot-rolled steel sheet or cold-rolled, annealed steel sheet prepared as described above may be hot-formed to prepare a hot-formed member.
- the prepared steel sheet for hot forming is heated to a temperature range of Ac3+50° C. to Ac3+200° C. at a heating rate of 1 to 1,000° C./sec. At a heating rate below 1° C./sec, it is difficult to obtain sufficient productivity. Also, a too long heating time not only excessively increases a grain size to deteriorate impact toughness but also excessively forms oxides on the surface of the formed member to deteriorate spot weldability. To increase the heating rate to exceed 1,000° C./sec, expensive equipment is required.
- the heat treatment may be maintained in the temperature range of Ac3+50° C. to Ac3+200° C. for 1 to 1,000 seconds.
- a heating temperature below Ac3+50° C. there is a high possibility that ferrite is formed while a blank is transferred from a heating furnace to a mold, thereby failing to obtain a target strength.
- the heating temperature exceeds Ac3+200° C. an excess of oxides on the surface of the formed member makes it difficult to obtain spot weldability and coating property during a subsequent process.
- the hot-formed member is cooled to a temperature below Mf simultaneously with the hot forming and a cooling rate may be controlled in a range of 1 to 1000° C./sec.
- a cooling rate below 1° C./sec, undesirable ferrite is formed making it difficult to obtain a tensile strength 1,500 MPa or more.
- a cooling rate exceeding 1,000° C./sec expensive, specified equipment is required.
- Ingot materials having chemical compositions of alloying elements shown in Table 1 were below melted, heated in a furnace at a temperature of 1,180° C. for 2 hours, and hot-rolled to obtain hot-rolled steel sheets having a final thickness of 3 mm. Subsequently, the hot-rolled steel sheets were acid-pickled for cold rolling, cold-rolled with a reduction ratio of 60%, and annealed at 760° C. to obtain steel sheets for hot forming.
- FIG. 1 is an electron microscope image illustrating a microstructure of a steel sheet for hot forming according to an embodiment of the present disclosure. Referring to FIG. 1 , it may be confirmed that a microstructure of a cold-rolled, annealed steel sheet for hot forming includes 20 vol % of a carbonitride in a ferrite matrix structure.
- the steel sheets for hot forming prepared as described above were hot-formed and heat treatment conditions therefor are shown in Table 2 below.
- the steel sheets were put into a furnace pre-heated to 950° C., maintained for 5.5 minutes, air-cooled for 12 seconds, hot-formed in a mold, and quenched to room temperature at a cooling rate of 30° C./sec or more.
- a first mold was a plate-shaped mold for forming the hot-formed member and performing a tensile test to evaluate physical properties after hot forming
- a second mold was prepared as a mini-bumper mold to evaluate formability and oxidation resistance.
- FIG. 2 is a photograph exemplarily illustrating good formability (a) and poor formability (b) obtained when hot forming is performed using a mini-bumper mold after hot forming.
- (b) of FIG. 2 cracks or bursts occurred on the surfaces during hot forming in some of the comparative examples and they were indicated as “poor” in Table 2.
- good formability as shown in (a) of FIG. 2 was indicated as “good”.
- Oxidation resistance of the hot-formed members obtained using the mini-bumper mold was evaluated based on whether excessive oxide scales were locally formed on the surface. A case in which surface oxidation was inhibited was indicated as “good” and a case in which excessive oxide scales were locally formed was indicated as “inferior”.
- FIG. 3 is a graph illustrating tensile test results of the hot-formed samples of examples and comparative examples using a plate-shaped mold, and the tensile test was performed according to JIS 13 B standards. Upon comparison among all of the tensile test curves of the examples and comparative examples, it was confirmed that fracture did not occur before exhibiting a maximum strength but occurred after the maximum tensile strength was obtained as shown in FIG. 3 .
- Patent Document 2 Korean Patent Publication No. 10-1696121
- occurrence of a fracture was observed before a maximum strength was obtained in a tensile curve, and a normal fracture was not observed in the tensile test due to the high H content in the steel sheet. That is, this indicates that hydrogen delayed fracture resistance may be judged based on the results of the tensile curve obtained from the tensile test.
- the hot-formed member prepared using the chemical composition of the alloying elements according to the present disclosure a tensile behavior, in which fracture occurred after a tensile strength reached a maximum level, was observed and thus excellent hydrogen delayed fracture resistance was confirmed.
- FIGS. 4 and 5 are electron microscope images of microstructures of steel sheets for hot forming according to an example and a comparative example prior to formation, respectively.
- FIG. 4 is a photograph of the microstructure of Example 2 before hot forming
- FIG. 5 is a photograph of the microstructure of Comparative Example 1 before hot forming.
- FIGS. 6 and 7 are graphs illustrating GDS analysis results of hot-formed members using a mini-bumper mold according to an example exhibiting good oxidation resistance and a comparative example exhibiting inferior oxidation resistance with respect to depth from the surface.
- GDS glow discharge spectrometer
- the average oxygen content exceeds 20 wt % at a point of 0.1 ⁇ m depth from the surface in the comparative example exhibiting inferior oxidation resistance of FIG. 7 , it was confirmed that the average oxygen content was about 2 to 3 wt % at a point of 0.1 ⁇ m depth from the surface in the example exhibiting good oxidation resistance of FIG. 6 . Based on these results, it was confirmed that the average oxygen content needs to be controlled to 20 wt % or less at a point of 0.1 ⁇ m depth from the surface to obtain good oxidation resistance of a final hot-formed member.
- Comparative Examples 1 to 9 to which Nb was not added grain refinement did not occur before hot forming, and thus poor formability was obtained. Among them, inferior oxidation resistance was observed in Comparative Examples 3 to 5 due to negative values of Expression (1). However, in the cases of Comparative Examples 6 and 7, good oxidation resistance was obtained despite negative values of Expression (1) because Al, effective on oxidation resistance, was added in an amount of 0.5% or more.
- Sb was further added to the steel types of Comparative Examples 18 to 23.
- Sb was oxidized at a hot forming temperature of 950° C. to be present as scales in the form of ash resulting in inferior oxidation resistance although Expression (1) was satisfied in Comparative Examples 18 to 20.
- the steel sheet for hot forming according to the present disclosure may be applied to automotive structural members because ultra-high strength may be obtained simultaneously inhibiting surface oxidation during hot press forming without using a plating layer.
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- 2020-09-01 EP EP20860644.2A patent/EP4008800A4/en active Pending
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- 2020-09-01 JP JP2022513945A patent/JP7461464B2/ja active Active
- 2020-09-01 WO PCT/KR2020/011684 patent/WO2021045476A1/ko unknown
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US20190390295A1 (en) * | 2017-03-30 | 2019-12-26 | Jfe Steel Corporation | Hot pressed part and method of manufacturing same |
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CN114391049A (zh) | 2022-04-22 |
WO2021045476A1 (ko) | 2021-03-11 |
JP7461464B2 (ja) | 2024-04-03 |
KR20210027841A (ko) | 2021-03-11 |
EP4008800A1 (en) | 2022-06-08 |
KR102279900B1 (ko) | 2021-07-22 |
JP2022546124A (ja) | 2022-11-02 |
EP4008800A4 (en) | 2022-11-30 |
CN114391049B (zh) | 2023-03-03 |
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